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4–8 JANUARY 2016 SAN DIEGO, CA

The Largest Event for Aerospace Research, Development, and Technology

FINAL PROGRAM www.aiaa-SciTech.org #aiaaSciTech

16-928 WHAT’S IMPOSSIBLE TODAY WON’T BE TOMORROW.

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Learn more at lockheedmartin.com

© 2014 LOCKHEED MARTIN CORPORATION VC377_164 Executive Steering Committee AIAA SciTech 2016 2O16 Welcome Welcome to the AIAA Science and Technology Forum and Exposition 2016 (AIAA SciTech 2016) – the world’s largest event for aerospace research, development, and technology. We are confident that you will come away from San Diego inspired and with the tools necessary to continue shaping the future of aerospace in new and exciting ways.

From hearing preeminent industry thought leaders, to attending sessions where cutting- edge research will be unveiled, to interacting with peers – this will be a most fulfilling week! Our organizing committee has worked hard over the past year to ensure that our plenary sessions examine the most critical issues facing aerospace today, such as aerospace science and Richard George Lesieutre technology policy, lessons learned from a half century of aerospace innovation, resilient design, Christiansen The Pennsylvania and unmanned aerial systems. We will also focus on how AIAA and other stakeholders in State University Sierra Lobo, Inc. academia, government, and industry can work together to best serve the aerospace community.

The Forum 360 program offers you the chance to dive deeper into the topics discussed in the plenary sessions and consider them from multiple angles. Topics to be covered include: how scientists and engineers can communicate better with the public about their work and achievements; how the International Space Station can be used to further research and development; how lessons from other industries can improve cybersecurity in ; how additive manufacturing can be used for aerospace applications; what educators can do to put the “E” in STEM; and what design and imagination lessons can be captured from Hollywood Mason Peck Robie for use in aerospace. Samanta Roy Cornell University The forum’s technical program provides opportunities to hear the presentation of Lockheed Martin groundbreaking research across the aerospace science and technology fields. These Corporation presentations will not only show you how your peers are overcoming the challenges that are posed by the advancement of aerospace science and technology, but will stimulate your own creativity, inspiring you to tackle new challenges and further progress the state of the art in our community.

While you are with us this week, be sure to spend some time in the Exposition Hall. More than 50 companies and organizations are showcasing their innovative products and services and with the wide variety of technology on display, you are sure to see something new.

John Tracy Ann Zulkosky AIAA SciTech 2016 offers something for every aerospace professional, regardless of the role you play in our community. We are excited to offer you this program, and we can’t wait to see The Company Systems Company how you will take the information presented and lessons learned and use it to shape the future of aerospace and your career!

AIAA SciTech 2016 is proud to feature the following conferences: AIAA/AHS Adaptive Structures Conference AIAA Non-Deterministic Approaches Conference AIAA Aerospace Sciences Meeting AIAA Spacecraft Structures Conference AIAA Atmospheric Flight Mechanics Conference AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference AIAA Information Systems — Infotech@ Aerospace Conference Dynamics Specialists Conference AIAA Guidance, Navigation, and Symposium on Space Resource Utilization Control Conference Wind Energy Symposium AIAA Modeling and Simulation Technologies Conference www.aiaa-SciTech.org 3 #aiaaSciTech IOrganizing Committee

SciTech 2016 Forum General Chair Digital Sensor Systems Mason Peck, Cornell University Maarten Uijt de Haag, Ohio University Domenico Accardo, Università degli Studi di Napoli “Federico II Forum 360 Chair Dynamics Specialists Ann Zulkosky, Lockheed Martin Space Joseph Slater, Wright State University Small Systems Company Jeremy Straub, University of North Dakota Education Young Professional Chairs K. Ravindra, St. Louis University Society and Aerospace Technology Benjamin Marchionna, Lockheed Martin Bradley Steinfeldt, Sandia National Corporation Fluid Dynamics Laboratories Melissa Green, Syracuse University Sam Alberts, Purdue University Software Gas Turbine Engines Chris Thames, NASA Langley Research Center Forum Technical Chairs Guillermo Paniagua, Purdue University Brad Burchett, Rose-Hulman Institute of Space Resources Utilization Symposium Technology Green Engineering Julie Kleinhenz, NASA Glenn Research Center Larry Leavitt, NASA Langley Research Misty Davies, NASA Ames Research Center Center Space Exploration and Operations Shirley Tseng, Tseng, LLC Jeanette Domber, Ball Aerospace & Ground Test Technologies Corp. Stephanie Simerly, NASA Glenn Research Spacecraft Structures Center Samuel “Case” Bradford, Jet Propulsion Forum Deputy Technical Chairs Laboratory Terry Morris, NASA Langley Research Center Guidance, Navigation, and Control Leena Singh, C.S. Draper Laboratory Structural Dynamics Richard Ruff, MathWorks Jack McNamara, The Ohio State University High Speed Air Breathing Propulsion Ben Thacker, Southwest Research Institute Dan Paxson, NASA Glenn Research Center Structures Peter Gustafson, Western Michigan Michael White, Ohio Aerospace Institute History University Kevin Burns, Northrop Grumman Technical Discipline Chairs Corporation Student Paper Competition- AD&S Adaptive Structures Phillips, NASA Marshall Space Farhan Gandhi, Rensselaer Polytechnic Information and Command & Control Systems Flight Center Institute Mike Sotak, Kratos Defense Survivability Aeroacoustics Intelligent Systems Julian Rimoli, Georgia Institute Jeffrey Peters, Rolls-Royce Corporation Nisar Ahmed, University of Colorado, of Technology Boulder Aerodynamic Measurement Technology Systems Engineering Philippe (Phil) Lavoie, University of Toronto Materials John Hsu, California State University, Mohammad Naraghi, A&M University Long Beach Air Breathing Propulsion Systems Integration Larry Leavitt, NASA Langley Research Center Meshing Visualization and Computational Terrestrial Energy Environments Sivaram Arepalli, National Institute Design John Dannenhoffer, Syracuse University of Aerospace Gil Crouse, Sierra Nevada Corporation Modeling and Simulation Technologies Conference Thermophysics Applied Aerodynamics Alaa Elmiligui, NASA Langley Research Michael Martin, Department of Energy Khaled S. Abdol-Hamid, NASA Langley Center Research Center Unmanned Systems Multi-Disciplinary Design Optimization Richard Stansbury, Embry-Riddle Atmospheric Flight Mechanics Edward Alyanak, Air Force Research Aeronautical University Chris Cotting, U.S. Air Force Test Pilot School Laboratory Wind Energy Symposium Communications Systems Non-Deterministic Approaches Matthew Churchfield, National Renewable Eric Butte, Lockheed Martin Masoud Rais-Rohani, Mississippi State Energy Laboratory University Computer Systems Chiping Li, Air Force Office of Plasmadynamics and Lasers Scientific Research Subrata Roy, University of Florida

Design Engineering Propellants and Combustion Lisa Saam, ATA Engineering, Inc. James Gord, Air Force Research Laboratory www.aiaa-SciTech.org 4 #aiaaSciTech IContents

Welcome 3

Organizing Committee 4

Forum Overview 8

Sponsors and Supporters 10

Keynote Speakers and Plenary Sessions 11 www.twitter.com/aiaa Forum 360 12 www.facebook.com/AIAAfan Special Sessions and Events 15 www.youtube.com/AIAATV Educational Events 17 www.linkedin.com/companies/aiaa Networking Events 19 www.flickr.com/aiaaevents Recognition Events 21 instagram.com/AIAAerospace Exposition Hall 25 livestream.com/AIAAVideo/SciTech2016 Exhibitors 28

Join the conversation! General Information 38 #aiaaSciTech

Author and Session Chair Information 40 On-Site Wi Fi Information Committee Meetings and Events 41 Network Name: SCITECH2016 Password: aiaa2016

Sessions at a Glance 47

AIAA is the world’s largest aerospace professional Session Detail Matrix 60 society, serving a diverse range of more than 30,000 individual members from 88 countries, and 95 corporate members. AIAA members help make the world safer, Author and Session Chair Index 186 more connected, more accessible, and more prosperous. For more information, visit www.aiaa.org, or follow us on Twitter @AIAA. Venue Map/Technical Zones 207 www.aiaa-SciTech.org 5 #aiaaSciTech Get Your Conference Info on the Go!

Download the FREE AIAA 2016 Conference Mobile App

MY ITINERARY FROM SCHOLARONE Compatible with iPhone/iPad, Android, and BlackBerry!

FEATURES HOW TO DOWNLOAD Browse Program Any version can be run without an active Internet connection! You can also sync an itinerary you created online with the app by entering your unique itinerary name. View the program at your fingertips MyItinerary Mobile App MyItinerary Web App My Itinerary For optimal use, we recommend • For optimal use, we recommend: iPhone 3GS, iPod Touch (3rd generation), s iPhone 3GS, iPod touch (3rd Create your own conference iPad iOS 4.0, or later schedule generation+), iPad iOS 4.0 or later Download the MyItinerary app by s Most mobile devices using Android searching for “ScholarOne” in the App Conference Info 2.2 or later with the default browser Store directly from your mobile device. Or, Including special events access the link below or scan the QR code s BlackBerry Torch or later device to access the iTunes page for the app. using BlackBerry OS 7.0 with the Take Notes default browser http://itunes.apple.com/us/ Take notes during sessions app/scholarone-my-itinerary/ • Download the MyItinerary app by id497884329?mt=8 accessing the link below or scanning the QR code City Map Select the meeting “AIAA SciTech 2016” http://download.abstractcentral. See the surrounding area and com/aiaa-mst16/index.htm the Manchester Grand Hyatt San Diego • Once downloaded, you can bookmark the site to access it later or add a link Connect to Twitter to your home screen. Tweet about what you’re doing and who you’re meeting with #aiaaSciTech Real-Time Q&A and Polling during AIAA SciTech 2O16 with conferences i/o!

During Plenary and Forum 360 Sessions, go to aiaa.cnf.io

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Participate in Session Polls 1. If Polls are available they will appear at the top of the page. Simply click/tap on a Poll to respond. 2. Choose your response(s) and hit “submit”. 3. After responding you will be able to see the results on your own device!* * Some Poll results may be hidden

NO DOWNLOADING REQUIRED! IForum Overview

SATURDAY/SUNDAY MONDAY TUESDAY 2–3 January 4 January 5 January 0730 hrs Speakers’ Briefing Speakers’ Briefing

0800 hrs Opening Plenary Panel Plenary Panel 0830 hrs

0900 hrs Networking Coffee Break Networking Coffee Break NDA Lecture ASC Lecture 0930 hrs

1000 hrs Technical Forum 360 Technical Forum 360 1030 hrs Continuing Education Sessions Sessions 1100 hrs Courses and 1130 hrs Workshop 1200 hrs 0815–1700 hrs

1230 hrs Saturday and Sunday Networking Lunch On Own Durand Lectureship for Public Recognition Luncheon: Celebrating 1300 hrs Service and Luncheon Achievements in Aerospace Sciences Networking Lunch On Own Concessions open in Sponsored by Lockheed Martin and Information Systems 1330 hrs Seaport Foyer

1400 hrs SCS Lecture DSC Lecture 1430 hrs

1500 hrs Forum 360 Forum 360 Networking Coffee Break Networking 1530 hrs Sponsored by Bastion Student/Young Professionals Coffee Break Technical Technologies Technical Networking Sessions Sessions 1600 hrs Sunday Rising Leaders in Aerospace 1630 hrs Leadership Exchange – Speed Mentoring (1545–1715 hrs) 1700 hrs Sponsored by Northrop Grumman

1730 hrs AIAA Dryden Lectureship in Research Governance Update 1800 hrs 1830 hrs Student Welcome Reception Rising Leaders Associate in Aerospace Sunday Reception Fellows Opening Reception in Exposition Hall 1900 hrs Sponsored by The Boeing Company Reception Sponsored by Honda Hall opens at 1815 hrs Aircraft Company 1930 hrs

2000 hrs

2030 hrs AIAA Associate Fellows Dinner 2100 hrs (Tickets 2130 hrs Required)

2200 hrs

2230 hrs

www.aiaa-SciTech.org 8 #aiaaSciTech IForum Overview

WEDNESDAY THURSDAY FRIDAY 6 January 7 January 8 January 0730 hrs Speakers’ Briefing Speakers’ Briefing Speakers’ Briefing

0800 hrs Keynote Plenary Panel Keynote 0830 hrs Networking Coffee Break Networking Coffee Break Networking Coffee 0900 hrs in Exposition Hall in Exposition Hall Break 0930 hrs

1000 hrs AV Week Annual Workforce Survey Forum Results Technical Sessions Forum 360 360 1030 hrs Supported by Rising Technical Sessions Technical Sessions Leaders in Aerospace

1100 hrs Exposition 1130 hrs Hall Open Hall opens 1200 hrs Exposition Rising at 0845 hrs Leaders in Hall Open Recognition Luncheon: Aerospace– 1230 hrs Hall opens Celebrating Achievements Lunch and at 0845 hrs in Aerospace Design/ Networking Lunch Learn with Structures, Outstanding On Own Test Pilot 1300 hrs Luncheon in Exposition Hall Educators, and Literary Tucker Excellence Concessions open in Hamilton Exposition Hall 1330 hrs

1400 hrs

1430 hrs Forum Forum 360 1500 hrs 360 Technical Sessions Networking Coffee Break 1530 hrs Technical Sessions Networking Coffee Break in Exposition Hall 1600 hrs Corporate Member 1630 hrs Reception

1700 hrs

1730 hrs Women at Scitech 1800 hrs Happy SDM Lecture Hour and 1830 hrs Keynote (open to all 1900 hrs attendees) 1930 hrs

2000 hrs

2030 hrs

2100 hrs

2130 hrs

www.aiaa-SciTech.org 9 #aiaaSciTech ISponsors and Supporters

AIAA would like to thank the following organizations for their support of AIAA SciTech 2016:

Premier Sponsor Durand Lectureship Sponsor

Executive Sponsor Rising Leaders in Aerospace Leadership Exchange – Speed Mentoring Sponsor

Young Professional Program: Rising Livestream Sponsor Leaders in Aerospace Reception Sponsor Student Reception Sponsor

Sustaining Small Business and Tuesday Twitter Board Sponsor Lanyard Sponsor Afternoon Coffee Break Sponsor

Supporting Sponsors



Quantify Every Uncertainty.

www.aiaa-SciTech.org 10 #aiaaSciTech IKeynote Speakers and Plenary Sessions

Get the big picture on science and technology from the leading authorities in the field during these high-level discussions and presentations. Monday, 4 January Wednesday, 6 January 0800–0900 hrs Seaport A-E 0800–0900 hrs Seaport A-E Opening Plenary Opening Plenary Aerospace Science and Technology Policy in the 2016 Designing for Resilience Political Arena Jeff Holland, Director, U.S. Army Engineer Research and Moderator: Courtney Stadd, Management Advisor, Development Center Catalyst Partners, LLC Panelists: Thursday, 7 January Mark Albrecht, Chairman of the Board, USSpace, LLC 0800–0900 hrs Seaport A-E Carissa Christensen, Managing Partner, The Tauri Group Jacques Gansler, Founder, Chair, and CEO, The Gansler Group Opening Plenary Daniel Goldin, Chairman, President & CEO, Intellisis Corporation Timothy Persons, Chief Scientist, U.S. Government Aerospace Frontiers – Strengthening Collaboration Accountability Office For Continued Progress Moderator: John Tracy, Chief Technology Officer and Senior A “MUST ATTEND” EVENT FOR ALL MEMBERS Vice President, Engineering, Operations and Technology, The Boeing Company 1730–1830 hrs Seaport A-E Panelists: AIAA Governance Update Morteza Gharib, Hans W. Liepmann Professor of Aeronautics and Bioinspired Engineering, Vice Provost, California e Future of AIAA: Why Governance Institute of Technology Matters to You Keoki Jackson, Chief Technology Officer, Lockheed Martin James F. Albaugh, President, AIAA Corporation This session will detail the proposed changes to the Institute’s Sandy Magnus, Executive Director, AIAA constitution recommended by the Governance Working Group Darryll Pines, Professor, University of Maryland and endorsed by the Board of Directors. Jim Albaugh will Jaiwon Shin, Associate Administrator, Aeronautics Research introduce a forward-thinking governance structure that is Mission Directorate, NASA essential to positioning AIAA to be a proactive organization— Steve Walker, Deputy Director, DARPA shaping the future of aerospace for decades to come. He will discuss the voting process that will begin in March and why your involvement is so important. Please join us! Friday, 8 January Tuesday, 5 January 0800–0900 hrs Seaport A-E 0800–0900 hrs Seaport A-E Opening Plenary Opening Plenary Commercial Use of Unmanned Systems Aerospace Generations – Lessons Learned from a Treggon Owens, Founding Partner & CEO, Aerial MOB, LLC Half Century of Innovation in Aerospace Technology Moderator: Mason Peck, Associate Professor, Sibley School of Mechanical and Aerospace Engineering, Cornell University Panelists: William A. Anders, U.S. Air Force (ret.) Zac Manchester, Postdoctoral Fellow, Agile Robotics Laboratory, Harvard University Hans Mark, Professor Emeritus, The University of Texas, Austin Mary Popp, Propulsion Engineer, Lockheed Martin Corporation www.aiaa-SciTech.org 11 #aiaaSciTech IForum 360

1400–1600 hrs Seaport F-G Cybersecurity Below 30,000 Feet—Applying Lessons from Other Industries Moderator: Chan D. Lieu, Senior Legislative Advisor, Venable, LLP Panelists: Jeffrey Carr, CEO, Taia Global These conversations will cover a spectrum of Scott Erven, Associate Director, Protiviti timely topics including programs, systems, policy, Jake Olcott, Vice President, Business Development, BitSight operations, applications, platforms and more! Wednesday, 6 January Monday, 4 January 0930–1130 hrs Seaport F-G 0930–1130 hrs Seaport F-G Additive Manufacturing – Applications and Distilling Your Message: Putting Yourself Back Opportunities for the Aerospace Industry into Your Science and Engineering Moderator: Robert Yancey, Vice President, Aerospace & Composites, Altair Engineering Moderator: Christine O’Connell, Associate Director, Alan Alda Center for Communicating Science, Stony Brook Panelists: University Greg Arend, Additive Manufacturing Development Leader, 1400–1600 hrs Seaport F-G Jason Dunn, Co-Founder and CTO, Made In Space Research Enabling and Enabled by a Cis-Lunar Franck Mouriaux, General Manager, Structures, RUAG Schweiz One-year Mission AG, RUAG Space Chauncey Wu, Structural Mechanics and Concepts Branch, Moderator: Michael Moloney, Director for Space and NASA Langley Research Center Aeronautics, Space Studies Board and the Aeronautics and Space Engineering Board, National Academies of Sciences, Engineering, and Medicine 1400–1600 hrs Seaport F-G Space Exploration Through Advancing Tuesday, 5 January Technologies 0930–1130 hrs Seaport F-G Moderator: Steve Gaddis, Director, Game Changing Innovation in Space—How Researchers Can Development Program, NASA Leverage the ISS National Laboratory for Panelists: Pioneering Research & Development Molly Anderson, Principal Technologist, Next Gen Life Support, NASA Moderator: Gregory Johnson, President and Executive Michelle Munk, Principal Technologist, Entry, Descent, and Director, Center for the Advancement of Science in Space Landing, NASA (CASIS) Matthew Simon, Habitat Design Lead, Human Panelists: Architecture Team, NASA Dan Blaettler, Senior Program Manager, Center for the Advancement of Science in Space (CASIS) George Nelson, Manager, ISS Technology and Science Research Office, NASA Andrew Rush, President, Made In Space, Inc.

www.aiaa-SciTech.org 12 #aiaaSciTech IForum 360

Thursday, 7 January 0930–1130 hrs Seaport F-G Putting the E in STEM Moderator: Meredith Drosback, Assistant Director for Education and Physical Sciences, Office of Science and Technology Policy, Executive Office of the President Panelists Edward J. Coyle, John B. Peatman Distinguished Professor of Electrical and Computer Engineering, Georgia Institute of Technology Thea Sahr, Director of Programs, DiscoverE

1400–1600 hrs Seaport F-G Learning from Hollywood Moderator: Rick Loverd, Program Director, The Science & Entertainment Exchange, National Academies of Science, Engineering, and Medicine

www.aiaa-SciTech.org 13 #aiaaSciTech ForumI 360

This multidimensional program features a leadership exchange/speed mentoring, panel session, Q&A with top industry leaders, and multiple RISING opportunities for networking. These exciting and energetic activities will provide access to top aerospace leaders and their perspectives, with subject inLEADERS AEROSPACE matter relevant to your career stage.

Monday, 4 January Wednesday, 6 January 1830–1930 hrs Seaport H 1000–1100 hrs Seaport H Reception Aviation Week Annual Workforce Survey Results The reception will kick off the Rising Leaders in Aerospace Every year Aviation Week conducts a survey on the aerospace events and is a perfect opportunity for young leaders to mingle workforce. The most recent survey had information that is with others who will be participating at AIAA SciTech as extremely relevant to younger professionals, including work- attendee, presenter, or veteran professional. Come meet other life balance. This panel will include an Aviation Week executive participants in a casual environment. You’re bound to see them who helped conduct the survey as well as several others who again at the Speaker, Networking, or Panel event. were heavily involved. Sponsored by: Come and get a “Reality Check as Competition for Talent Increases.” Moderator: Carole Rickard Hedden, Executive Editorial Director, Aviation Week Executive Intelligence Panelists: Tuesday, 5 January Jim Adams, Partner, PwC/Strategy& 1545–1715 hrs Seaport H Clarke Havener, Global Sector Leader A&D, Korn Ferry Lauren Smith, Concept Development Engineer, Northrop Leadership Exchange – Speed Mentoring Grumman Aerospace Systems A networking event for young aerospace leaders, age 35 and under. Thursday, 7 January Mentors include: 1200–1330 hrs Seaport H Mike Griffin, Schafer Corporation James Kenyon, Pratt & Whitney Lunch and Learn with Test Pilot Tucker Hamilton Sandy Magnus, AIAA Keynote Speaker: MAJ Tucker Hamilton, Experimental Dimitri Mavris, Georgia Institute of Technology Fighter Test Pilot, Timothy Persons, U.S. Government Accountability Office Tucker Hamilton is an experimental test pilot for the U.S. Mary Popp, Lockheed Martin Corporation Air Force. He will be sharing his presentation: “Making a Difference at Mach 2.” He’ll share what it is like to be an Masoud Rais-Rohani, Mississippi State University experimental fighter test pilot, and share his personal stories Al Romig, National Academy of Engineering including major life-threatening aircraft accidents, close Ash Sater, eddi app saves, combat flying revelations, serendipitous opportunities Sarah Shull, NASA Johnson Space Center testing first-of-its-kind technology, flying over 30 aircraft Courtney Stadd, Catalyst Partners, LLC from a zeppelin to a MiG-15 to an A-10, and managing the Joint Strike Fighter Developmental Test program for all three Julie Van Kleeck, Aerojet services. Through these experiences you will learn not just Sponsored by : what a Test Pilot does, but also gain encouragement through lessons learned on how to make a difference in your local communities. And did we mention cool flight test videos! Box lunches will be available for the first 125 young professionals who attend.

www.aiaa-SciTech.org 14 #aiaaSciTech ISpecial Sessions and Events

Monday, 4 January Tuesday, 5 January 1230–1400 hrs SeaportA-E 1730–1830 hrs Seaport F-G Durand Lectureship for Public Service Dryden Lectureship in Research and Luncheon Blended Body Technology Readiness oughts on Complex Systems Solutions in the 21st Robert H. Liebeck, Senior Technical Fellow, The Boeing Century Company Ronald M. Sega, Colorado State University Thursday, 7 January

Sponsored by: 1730–1930 hrs Seaport F-G Women at SciTech Happy Hour and Keynote Reception: 1830–1915 hrs Seaport Foyer Ann Zulkosky, Lockheed Martin Space Systems Company Dinner: 1930–2230 hrs Seaport F-G To celebrate women’s accomplishments in aerospace and aeronautics and to provide an opportunity for women to 2016 Associate Fellows Recognition Ceremony network and share their experiences, AIAA and the AIAA and Dinner (Ticketed Event) Diversity Working Group are cosponsoring the “Women Each year, the Institute recognizes exemplary professionals at SciTech Happy Hour and Keynote.” The event is open to for their accomplishments in engineering or scientific work, everyone. outstanding merit and contributions to the art, science, or technology of aeronautics or astronautics.

The Class of 2016 Associate Fellows will be officially recognized during the Associate Fellows Recognition Ceremony and Dinner on Monday evening, 4 January 2016.

Please support your colleagues, and join us for the induction of the 2016 Associate Fellows. Tickets to this celebrated event are available on a first-come, first-served basis and can be purchased for $100 via the AIAA SciTech 2016 registration form, the 2016 Associate Fellow Dinner event registration form, or on site (based on availability).

www.aiaa-SciTech.org 15 #aiaaSciTech INNOVATION THIS IS WHAT WE DO.

It’s anything but a drone. The Northrop Grumman X-47B is the first and only unmanned aircraft to autonomously launch from and land on an aircraft carrier. By evolving the revolutionary B-2 Stealth ’s tailless, blended-wing shape, it won a Collier Trophy for greatest achievement in American aviation.

©2015 Northrop Grumman Corporation www.northropgrumman.com/stealth IEducational Events

AIAA is committed to keeping aerospace professionals at their technical best, and provides an ongoing source of learning, community, professional connections, and career development. Gain the knowledge you need to excel in your field or to move confidently into a new one. Learn how to interact with students and teachers, and help inspire the next generation of aerospace leaders.

Tuesday, 5 January

Career Workshop: Communications and 1100-1200 hrs Vista AB Connections for Your Career Striking Out on Your Own or Within an Need to find a competitive edge to advance in your career? Organization Wondering what skills you should develop and leverage to take the next steps? The Communications and Connections Are you ready to strike out on your own? This session for Your Career workshop at AIAA SciTech 2016 will provide will feature a panel of entrepreneurs and intrepreneurs— some building blocks to help you—whether you are starting innovating within a large corporation. Panelists will share out in your career, looking to move up the ladder in your their experiences and thoughts about how they took the leap organization, or wanting a refresher on some core skills. and how they have effected change within our industry. Moderator: Bob Wessels, Subcontracts Program Senior 0915–1000 hrs Vista AB Manager, Lockheed Martin Space Systems Company Technical Writing Panelists include: Alan Cain, President, Innovative Technology Applications Presenter: Paul Park, Retired Chief Engineer, Lockheed Company, LLC Martin Aeronautics Jane Hansen, President, HRP Systems, Inc. Technical writing is rarely taught in college engineering Brett Hoffstadt, PMP, Project Manager, 3Sixty Integrated programs, therefore students enter the workforce without effective writing skills. This session will present basic Dave Mitchell, President, Mitchell Aerospace Research techniques for creating clear, succinct, and effective technical prose. 1500–1545 hrs Vista AB

1000–1115 hrs Vista AB Making the Most of Networking Networking is an important skillset to help advance your Presentation Skills career. This session will highlight how effective networking Presenter: May-chen Martin-Kuo, Senior Scientist, can impact your career positively. Panelists will share their Spreadtrum Communications, Inc., and District Director, experiences and provide tips about how best to develop and Toastmasters International District 5 utilize your networks. Making your point clearly, succinctly, and with impact is Panel Discussion: Networking Experiences at important to your career development. This session will cover Beneted My Career key elements in making effective presentations, including: Moderator: Bob Wessels, Subcontracts Program Senior • Developing & Delivering Presentation – Avoiding Death Manager, Lockheed Martin Space Systems Company by PowerPoint Panelists include: • Speech – Making a Point in 3 Minutes or Less Larry Brase, Technical Fellow/Senior Manager, The Boeing Company • Engaging the Audience – They Snooze, You Lose Basil Hassan, Senior Manager, Sandia National Laboratories Laura McGill, Vice President, Engineering, Raytheon Company Bob Wessels, Subcontracts Program Senior Manager, Lockheed Martin Space Systems Company

www.aiaa-SciTech.org 17 #aiaaSciTech IEducational Events

Tuesday, 5 January (continued)

1630–1730 hrs Regatta B Membership Matters: How Far Will You Go? Did you know there are six grades of AIAA membership spanning from Student Member to Honorary Fellow? Membership elevation is a step toward recognition of one’s professional status and accomplishments. In this panel session, hosted by the AIAA Diversity Working Group, learn how to apply for and encourage nomination of members who qualify for membership advancements. Moderators: Susan Frost, Research Scientist, NASA Ames Research Center, and Hsiao-hua Burke, Principal Staff, MIT-Lincoln Lab Panelists include: Luisella Giulicchi, Spacecraft Engineering and AIV Manager, European Space Agency Basil Hassan, Senior Manager, Sandia National Laboratories Achille Messac, Professor, Mississippi State University Helen L. Reed, Professor, Texas A&M University Mary L. Snitch, Senior Manager, Lockheed Martin

Wednesday, 6 January

1830–2000 hrs Harbor A Crawford Slip Method Workshop on Networking This will be an interactive exchange on networking, unlike anything you’ve ever experienced. Participants will not be pushed into parlor games, or set up with touchy-feely interviews. Oddly, you will be tasked to write furiously during an intensive 90-minute session in complete SILENCE! Then a presentation and discussion will commence for the final half hour. Your efforts will result in an AIAA pamphlet: “How to Network at a Conference.”

Please come prepared to closely follow very precise directions. This will ensure your ideas are faithfully captured, so that your problems and issues with networking get solved.

An ability to write simple, direct sentences in the English language is required.

www.aiaa-SciTech.org 18 #aiaaSciTech INetworking Events

Understanding the importance of networking with colleagues new and old, a series of activities have been planned that will help you connect with current colleagues and new acquaintances. Student/Young Professionals Networking Networking Coffee Breaks Sunday, 3 January 1530–1700 hrs Promenade AB Coffee breaks allow even more time for making new contacts, This will be an opportunity for students to speak directly continuing discussions from sessions, visiting the Exposition with young professionals in the aerospace industry. This Hall, or checking emails and voicemails to keep in touch with unique opportunity will provide students with the ability to the office while you are at the forum. Coffee breaks will be ask questions about transitioning from the university to the located in the following locations and times: workplace. Find out from those who have made the transition Monday, 4 January 0700, 0900, and 1530 hrs; within the past 3–10 years about the process. Find out what Session Room Foyers they wish they had known then. Connect with people in the industry who have a firm grasp of exactly what you might be Tuesday, 5 January 0700, 0900, and 1530 hrs; feeling and wondering. Session Room Foyers

Student Welcome Reception Sponsored by: Sunday, 3 January, 1800–1930 hrs Seaport H Wednesday, 6 January 0700 hrs; Session Room Foyers AIAA SciTech has the largest gatherings of students of all of 0900, 1530 hrs; Exposition Hall the AIAA forums. Come meet fellow students who you are sure to see again throughout the week. Many student award Thursday, 7 January 0700 and 1530 hrs; winners and presenters will be in attendance. Also, Executive Session Room Foyers Director Sandy Magnus will address the attendees, as will a 0900 hrs; Exposition Hall representative from the corporate sponsors. All attendees are Friday, 8 January 0700 and 0900 hrs; welcome. Session Room Foyers Members of the AIAA Board of Directors and the Technical Activities Committee will also be in attendance. Take advantage of this chance to meet AIAA key members and learn about opportunities that are available. Opening Reception Sponsored by: Tuesday, 5 January Exposition Hall 1815–2000 hrs Take this opportunity to engage new contacts and refresh old Concessions ones. A ticket for the reception is required and included in the registration fee where indicated. Additional tickets for guests Cash-only concessions will be offered on the following days may be purchased upon registration or on site, as space is and locations: available. Monday, 4 January, 1230–1400 hrs, in the Seaport Foyer on the 2nd level of the Hyatt. Come join us for the SciTech specialty cocktail: the CosmicRita! Thursday, 7 January, 1200–1400 hrs, in the Exposition Hall on the lobby level of the Hyatt.

www.aiaa-SciTech.org 19 #aiaaSciTech INetworking Events

Luncheon in the Exposition Hall USS Midway Museum Tour Wednesday, 6 January Exposition Hall Friday, 8 January 1245 hrs 1230–1400 hrs The AIAA San Diego Section has organized a self-guided A ticket is required and is included in the registration fee tour of the USS Midway Museum. Fellow AIAA members and where indicated. AIAA SciTech attendees should meet near the Registration desk and then walk to the USS Midway (5–7 minutes) for a “group” tour of the USS Midway. Women at SciTech Happy Hour and Keynote If you did not get a chance to purchase tickets ahead of time online, just stop by the San Diego Section booth in the Thursday, 7 January Seaport F-G Exposition Hall as they will have some available for purchase. 1730–1930 hrs AIAA SciTech 2016 Attendees: $14 Ann Zulkosky, Lockheed Martin Space Systems Company AIAA San Diego Members: $14 To celebrate women’s accomplishments in aerospace and aeronautics and to provide an opportunity for women to Students: $13 network and share their experiences, AIAA and the AIAA Nonmembers: $17 Diversity Working Group are cosponsoring the “Women at SciTech Happy Hour and Keynote.” The event is open to everyone.

www.aiaa-SciTech.org 20 #aiaaSciTech Recognition Events

Join with AIAA throughout the forum as we celebrate our industry’s discoveries and achievements from the small but brilliantly simple innovations that affect everyday lives to the major discoveries and missions that fuel our collective human drive to explore and accomplish amazing things. Monday, 4 January 0900–1000 hrs Harbor A Reception: 1830–1915 hrs Seaport Foyer Dinner: 1930–2230 hrs Seaport F-G Non-Deterministic Approaches Lecture 2016 Associate Fellows Recognition Ceremony A Bayesian Framework for Assessment of Model and Dinner Uncertainty Each year, the Institute recognizes exemplary professionals Armen Der Kiureghian, President, American University for their accomplishments in engineering or scientific work, of Armenia; Taisei Professor of Civil Engineering Emeritus, outstanding merit and contributions to the art, science, or University of California, Berkeley technology of aeronautics or astronautics. Members of the Class of 2016 Associate Fellows will be 1400–1500 hrs Harbor A officially recognized during the Associate Fellows Recognition Ceremony and Dinner. Spacecraft Structures Lecture A ticket for the dinner is required and not included in the registration fee. Additional tickets for guests may be purchased Technology Development and Infusion for the James upon registration or on site, as space is available. Webb Telescope Sun Shield James Moore, Division Vice President, ManTech (NeXolve) Tuesday, 5 January 0900–1000 hrs Harbor A 1530–1730 hrs Harbor A Spacecraft Structures Panel Adaptive Structures Lecture Adaptive Aerospace Structures – An Air Force Infusing New Structures Technology Into Perspective Space Systems Gregory W. Reich, Air Force Research Laboratory, Moderators: W. Keith Belvin, NASA Langley Research AFRL/RQVC Center and Greg Agnes, Jet Propulsion Laboratory, California Institute of Technology 1030–1230 hrs Harbor A Adaptive Structures Panel Where’s My Morphing Aircra? Reections Based on Twenty Years of Adaptive Aerostructures Moderator: Farhan Gandhi, Rosalind and John J. Redfern Jr. ‘33 Endowed Chair in Aerospace Engineering, and Aerospace Program Director, Rensselaer Polytechnic Institute Panelists: Jayanth Kudva, NextGen Aeronautics Daniel Newman, The Boeing Company Friedrich Straub, The Boeing Company Edward White, The Boeing Company

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Certificate of Merit for Best Papers: Tuesday, 5 January (continued) CFD Flow Visualization Showcase 1230–1400 hrs Seaport A-E Most Artistic Flow Visualization Animation — “The Effect of Initial Conditions on Streamwise Vortices in the Plane Recognition Luncheon: Celebrating Achievements Turbulent Mixing Layer,” AIAA 2015-2617, William A. in Aerospace Sciences and Information Systems McMullan and Stephen J. Garrett, University of Leicester. A ticket for the luncheon is required and included in the registration fee where indicated. Additional tickets for guests may Most Quantitatively Descriptive Flow Visualization be purchased upon registration or on site, as space is available. Animation — “EPIC – An Extract Plug-In Components Toolkit for in-Situ Extracts Architecture,” AIAA 2015-3410, The following awards will be presented: Earl Duque and Daniel Hiepler, Intelligent Light; Robert Haimes, Massachusetts Institute of Technology; Christopher Aerospace Guidance, Navigation and Control Award Stone, Computational Science and Engineering, LLC; Steven Kyle. T. Alfriend E. Gorrell, Matthew Jones, and Ronald A. Spencer, Brigham Young University TEES Distinguished Research Chair Professor Department of Aerospace Engineering Texas A&M University College Station, Texas Most Comprehensive Flow Visualization Animation — “A Multi-Phase CFD Technique with Cavitation and Fluid- “For significant lifetime contributions to spacecraft formation-flying Structure Interaction,” AIAA 2015-3419, Hong Q. Yang, CFD technologies, fostering international scientific cooperation, and Research Corporation. leadership to the aerospace guidance and control communities.” deFlorez Award For Flight Simulation Computational Fluid Dynamics Student Best Paper John M. Hanson “Improving High-Order Finite Element Approximation Alternate Lead Systems Engineer, Through Geometrical Warping,” AIAA 2015-2605, Devina NASA Marshall Space Flight Center Sanjaya and Krzysztof Fidkowski, University of Michigan. Huntsville Alabama Guidance, Navigation and Control Best Paper “For outstanding innovations and contributions in flight “Swarm Assignment and Trajectory Optimization Using Variable-Swarm, Distributed Auction Assignment and Model simulation applications for launch vehicle design, development, Predictive Control,” AIAA 2015-0599, Daniel Morgan and and requirements verification.” Soon-Jo Chung, University of Illinois at Urbana-Champaign; Intelligent Systems Award and Fred Hadaegh, Jet Propulsion Laboratory. Frank L. Lewis Intelligent Systems Best Paper Moncrief-O’Donnell Chair and Head, Advanced Controls and “Trajectory Prediction and Alerting for Aircraft Mode and Sensors Group Energy State Awareness,” AIAA 2015-1113, Kimberlee Shish, University of Texas at Arlington Research Institute Millennium Engineering and Integration Company; John Ft. Worth, Texas Kaneshige, Diana Acosta, Stefan Schuet, Avinash Madavan, NASA Ames Research Center; Thomas Lombaerts, German “For contributions to intelligent neural-adaptive control and Aerospace Center (DLR); and Lynne Martin, San Jose State highly influential textbooks that have advanced the capability of University. autonomous .” Modeling & Simulation Best Paper Lawrence Sperry Award “A Coupled Lateral/Directional Flight Dynamics and Joshua Rovey Structural Model for Flight Control Design,” AIAA 2015-0906, Ondrej Juhasz and Mark Tischler, NASA Ames Research Associate Professor Center; and Steven Hagerott, David Staples, and Javier Missouri University of Science & Technology Fuentealba, Textron Aviation. Rolla, Missouri “For exceptional contributions to research in the areas of plasmadynamics and space propulsion, and to the Missouri S&T AIAA Student Branch.” Mechanics and Control of Flight Award Srinivas R. Vadali Professor, Department of Aerospace Engineering Texas A&M University College Station, Texas “For lasting contribution to the understanding of the relative motion of formations and the control of this relative m o t i o n .” www.aiaa-SciTech.org 22 #aiaaSciTech IRecognition Events

Tuesday, 5 January (continued) Faculty Advisor Award Amrutur V. Anilkumar Announcement of Student Competition Winners Professor, Department of Mechanical Engineering Vanderbilt University Atmospheric Flight Mechanics Nashville, Tennessee Guidance Navigation And Control “For passionate promotion of novel aerospace design activities, community outreach and mentoring of students to success at national competitions and pursuit of aerospace engineering 1400–1500 hrs Harbor A careers.” Dynamic Specialists Lecture History Manuscript Award Alexander C. MacDonald e / Sky-Crane Program Executive for Emerging Space, Office of the Chief Landing System Technologist, NASA Headquarters Civil and Commercial Space Division, NASA Jet Propulsion Jeffrey Umland, Engineering Fellow, Jet Propulsion Laboratory Laboratory “The Long Space Age: An Economic Perspective on the History of 1530–1730 hrs Harbor A the American Space Exploration.” Dynamic Specialists Panel Pendray Aerospace Literature Award David K. Schmidt Panel Discussion and Open Forum on the 2nd Professor Emeritus, Department of Mechanical and Aerospace Aeroelastic Prediction Workshop Engineering University of Colorado-Colorado Springs Colorado Springs, Colorado Wednesday, 6 January “For sustaining and influential contributions to aerospace literature in the area of aerospace vehicle dynamics and control, 1800–1900 hrs Seaport F-G including the comprehensive textbook, Modern Flight Dynamics.” Structures, Structural Dynamics, and Materials Lecture SDM Award Anthony M. Waas Real-Life Problems are Multidisciplinary Boeing-Egtvedt Endowed Chair, Ivatury Raju, Technical Fellow for Structures, NASA Chairperson, William E. Boeing Department of Aeronautics and Astronautics, University of Washington Thursday, 7 January Washington “For pioneering contributions to the development of innovative, 1200–1400 hrs Seaport A-E experimentally validated, computational methods for progressive damage analysis of polymer and hot ceramic composite materials Recognition Luncheon: Celebrating Achievements and structures.” in Aerospace Design/Structures, Outstanding Abe M. Zarem Award for Distinguished Achievement–Aeronautics Educators, and Literary Excellence Ayodeji T. Bode-Oke Speaker: Michael Gazarik, Technology Director, Ball University of Virginia Aerospace & Technologies Corp. Charlottesville, Virginia A ticket for the luncheon is required and included in the AIAA Foundation Abe M. Zarem Educator Award registration fee where indicated. Additional tickets for guests may Haibo Dong be purchased upon registration or on site, as space is available. Associate Professor, Mechanical and Aerospace Engineering The following awards will be presented: University of Virginia Charlottesville, Virginia Aerospace Design Engineering Award The Boeing Hypersonic Design/MDAO Team The Boeing Company Huntington Beach, California Award Accepted by Kevin Bowcutt, Team Lead “For the design of novel hypersonic vehicle concepts and development of the multidisciplinary analysis and optimization tools critical for success.” www.aiaa-SciTech.org 23 #aiaaSciTech IRecognition Events

Thursday, 7 January (continued) Spacecraft Structures Best Paper “Recent Advances in Heliogyro Solar Sail Structural Dynamics, 1230–1400 hrs Seaport A-E Stability, and Control Research,” AIAA 2015-0431, William Wilkie, Jay Warren, Lucas Horta, Karen Lyle, and Jer-Nan Recognition Luncheon: Celebrating Achievements Juang, NASA Langley Research Center; Samuel Gibbs and Earl Dowell, Duke University; and Daniel Guerrant and Dale in Aerospace Design/Structures, Outstanding Lawrence, University of Colorado, Boulder. Educators, and Literary Excellence Announcement of Student Competition Winners Certificate of Merit for Best Papers Jefferson Goblet Student Paper Award ASME/Boeing Best Paper The Harry H. and Lois G. Hilton Student Paper “Computational Techniques for the Thermostructural Analysis Award in Structures of Composites” AIAA 2015-0462, Vinay Goyal, Jacob Rome, Lockheed Martin Student Paper Award in Structures Matthew Conway, James Tuck-Lee and Steven Frolik, The Aerospace Corporation. American Society for Composites Student Paper in Composites Award Collier Research Hypersizer/AIAA Structures Best Paper Southwest Research Institute Student Paper Award in Non- “Mass Optimization of Variable Angle Tow, Variable Thickness Deterministic Approaches Panels with Static Failure and Buckling Constraints” AIAA 2015-0452, Rainer MJ Groh and Paul Weaver, University of Bristol.

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The Exposition Hall is the hub of activity during this event—from seeing exhibitor displays to enjoying networking breaks and other functions. Some major networking events are held in the Exposition Hall to give attendees and exhibitors an opportunity to connect with partners, industry thought leaders, and collaborators who can help move your business forward. Exposition Hall Hours New This Year! Enter To Win A Full Conference Registration For AIAA SciTech 2017! Tuesday, 5 January Opening Reception* 1815–2000 hrs Complete the raffle ticket (behind your registration badge) Wednesday, 6 January 0845–1600 hrs and drop it off at any of the raffle boxes in the Exposition Luncheon* 1230–1400 hrs Hall. Winner will be notified by email and does not need to be present to win. Thursday, 7 January 0845–1400 hrs Raffle is open to all AIAA SciTech 2016 attendees. Employees/ *A ticket is required to attend. contractors of the American Institute of Aeronautics and Astronautics or credentialed members of the media are not Concessions eligible to win. Cash-only concessions will be offered on Thursday, 7 January, 1200–1400 hrs, in the Exposition Hall on the lobby level of the Hyatt.

AIAA Pavilion Stop by the AIAA Pavilion, located in the Exposition Hall, 30% Off All Books at AIAA SciTech 2016 to browse publications and merchandise, learn about your membership benefits, and meet AIAA staff. AIAA Publications is offering a special discount on all titles featured at AIAA SciTech 2016. Attendees can take AIAA Foundation advantage of a 30% discount off the list price of all books for sale at the AIAA Bookstore located in the AIAA Pavilion. Come visit us in the AIAA Pavilion. Did you know that the This show special will only be available during the forum! AIAA Foundation is celebrating its 20th anniversary? To Take advantage of these super savings and visit the AIAA celebrate this milestone, we are asking our members to help Bookstore! us accomplish an amazing feat: if 10,000 members donate at least $20 each, we will raise $200,000. If you make your Meet the Author Sessions donation on site you will be entered into a drawing for a 2-night stay at the Gaylord Texan during AIAA SciTech Thomas R. Yechout 2017.* Winners will be announced at the plenary session Introduction to Aircraft Flight Mechanics, 2E on Friday. In addition, we are hosting a Silent Auction with Tuesday, 5 January some cool aerospace items up for bid. Come visit us at the AIAA Pavilion and check it out! AIAA Pavilion Welcome Reception

Leland M. Nicolai Fundamentals of Aircraft and Design, Vols. 1 & 2 AIAA Pavilion Wednesday, 6 January 0900-0930; 1530-1600 hrs Thursday, 7 January 0900-0930

Daniel P. Raymer Aircraft Design, 5E and RDSWin Student Wednesday, 6 January AIAA Pavilion * Please note: a donation is not necessary to be entered in the raffle. Luncheon www.aiaa-SciTech.org 25 #aiaaSciTech ExpositionI Hall

Charging Stations

Software Cradle ANSYS MathWorks AIAA PAVILION eddi Vehicle XFlow Airborne j2 Aircraft COMSOL CFD Systems Dynamics 720 AIAA eddi Ennova San Diego NIA Chapter NASA Aeronautics Research TEN TECH Pointwise Directorate Cambridge Flow Tetra MicroCraft Triumph Presidio LLC Solutions CEI Inc. 215 516 Smart Nat'l Academies Granta Material Orbital of Sciences, SmartUQ LaVision Engineering & Corporation ATK Medicine Design 213 216 315 316 415 Energy University Research Tri Models Photron Exhibitor Consultants MetaComp of Kansas Lounge ADS CFD Allied BETA Inc. Powers LLC NRO Cray G.R.A.S. Astos CAE 210 ONR Solutions Boeing Aurora GmbH Neft Gaz NUMECA SG Flight Collier Sciences Tadqiqot USA 208 309 308 409 Cambridge University TSI, Inc. DARcorp Press SEDS Higher UCRI Aerion AMRDEC NASA Orbits Technologies Intelligent Lockheed CD- Light Martin adapco Kamatics Tecplot UTRC dSpace RWG Dantec 201 202 301 302 502

ENTRAN E

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Exhibitors by Booth Number (êindicates AIAA Corporate Members)

209 ADS CFD Inc. 715 Micro Craft, Inc 303 Aerion Technologies (formerly Desktop Aeronautics) 716 NASA Aeronautics Research Directorate 617 AIAA San Diego Section 704 NASA Space Technology Mission Directorate 520 Airborne Systems 415 National Academies of Science, Engineering, 210 Allied Powers LLC and Medicine ê 522 ANSYS, Inc. 516 National Institute of Aerospace (NIA) 308 Astos Solutions GmbH 510 National Reconnaissance Office (NRO) 208 607 JV Neft Gaz Tadqiqot 609 BETA CAE Systems USA, Inc. 720 j2 Aircraft Dynamics 409 Boeing Technology Services ê 708 NUMECA USA, Inc. 218 Cambridge Flow Solutions 309 Office of Naval Research ê 606 Cambridge University Press 315 Orbital ATK 602 CD-adapco 611 Photron 317 Computational Engineering International (CEI) 318 Pointwise, Inc. ê 619 COMSOL 715 Presidio Components Inc. 709 Cray 706 SEDS @ UCSD 702 Dantec Dynamics, Inc. 207 SG — Space and Ground Engineering Solutionsê 205 DARCorporation ê 213 Smart Material Corporation 202 dSPACE ê 216 SmartUQ 211 Energy Research Consultants 221 Software Cradle 217 Ennova-CFD 301 Tecplot, Inc. ê 714 Granta Design 215 TEN TECH LLC 710 G.R.A.S. Sound & Vibration 417 Tetra Research Corporation 203 Higher Orbits ê 512 Tri Models, Inc. 508 Hypersizer - Collier Research ê 616 Triumph Aerospace Systems — Newport News 302 Intelligent Light ê 705 TSI, Inc. 720 j2 Aircraft Dynamics 201 Research Center (UTRC) 701 Kamatics/RWG 204 University of Cincinnati Research Institute (UCRI) 316 LaVision, Inc. 711 University of Kansas - Aerospace Short ® ê 502 Lockheed Martin Skunk Works Course Program 621 MathWorks 219 XFlow CFD 610 Metacomp Technologies

www.aiaa-SciTech.org 27 #aiaaSciTech Exhibitors ADS CFD Inc 209 ANSYS, Inc. 522 60 Saint Timothy Court 2600 ANSYS Drive Danville, CA 94526 Cannonsburg, PA 15317 www.adscfd.com www.ansys.com [email protected] [email protected] ADS CFD is a provider of design and analysis software for the ANSYS provides simulation driven product development turbomachinery industry. Our software suite is built around solutions to help companies meet their key business initiatives. the aerospace-class CFD solver, Code LEO. Organizations trust We have solutions for optimizing aerodynamics, designing an ADS CFD in the design of their radial and axial compressors environmental control system, working with multifunctional and turbines when high fidelity and fast turnaround time are composites, creating next generation propulsion systems or required. developing millions of lines of embedded software.

Aerion Technologies (formerly Desktop Aeronautics) 303 Astos Solutions GmbH 308 1900 Embarcadero Road Meitnerstr. 8 Suite 101 Stuttgart, Germany 78089 Astos Palo Alto, CA 94303 www.astos.de Solutions www.desktopaero.com [email protected] [email protected] Astos Solutions provides software and hardware solutions for Aerion Technologies (formerly Desktop Aeronautics) creates mission and system concept analysis, spacecraft design and tools for aerodynamic design and analysis of aerospace trajectory optimization, GNC/AOCS sizing and simulation, vehicles. Our flagship product, GoCart, is an intuitive aerial GNC/AOCS SCOE, pointing error engineering, real-time vehicle design tool built around NASA’s renowned Cartesian sensor simulation, gravity field identification, magnetic Euler CFD solver, Cart3D. Our customer list includes the cleanliness, highly realistic space scenario visualization. major players from the aerospace and defense industry. BETA CAE Systems USA, Inc. 609 AIAA San Diego Section 617 29800 Middlebelt Road PO Box 3898 Suite #100 San Diego, CA 92163-1898 Farmington Hills, MI 48334 www.aiaa-sd.org www.ansa-usa.com [email protected] [email protected] The San Diego Section was one of the earliest of groups in both BETA CAE Systems is an engineering services company that the IAS and the ARS. Since these two groups merged in 1963, distributes & supports the industry leading ANSA & META the San Diego section has been a vibrant organization hosting software. ANSA is a CAE pre-processing and morphing tool many national AIAA conferences and activities. We are now for FE & CFD Analysis, for full-model build, from CAD to honored to be the host city for SciTech, and look forward to its solver input file, in one integrated environment. return in future years. Boeing Technology Services 409 Airborne Systems 520 7755 E. Marginal Way S Mail Code 1W-02 5800 Magnolia Avenue Seattle, WA 98108 Pennsauken, NJ 08109 www.boeing.com/bts www.airborne-sys.com [email protected] Boeing is the world’s leading aerospace company, and Airborne Systems is the world leader in the design, employs more than 169,000 people around the world. development, fabrication, test and integration of Entry Descent Boeing Technology Services (BTS) is the point of access to and Landing Systems (EDLS), including parachutes systems, more than 500 testing facilities across the US. BTS contracts Air Bag Landing Attenuation systems, Inflatable Aerodynamic with companies, educational institutions, and government Decelerators. We provide EDLS systems for various aircraft organizations for use of Boeing laboratories. and spacecraft and is leading the development of new technologies including Inflatable Aerodynamic Decelerators.

www.aiaa-SciTech.org 28 #aiaaSciTech Exhibitors Cambridge Flow Solutions 218 COMSOL 619 House 1 New England Executive Park Vision Park Burlinton, Ma 01803 Histon www.comsol.com Cambridge, Cambridgshire, [email protected] UK CB24 9AD www.cambridgeflowsolutions.com/ COMSOL is a global provider of simulation software for [email protected] product design and research to technical enterprises, research labs, and universities. Its COMSOL Multiphysics® product is Cambridge Flow Solutions develops Boxer, a fully-scalable an integrated software environment for creating physics-based simulation environment encompassing advanced geometry, models and simulation apps. A particular strength is its ability mesh generation and CFD software, tailored to complex to account for coupled physics phenomena. applications and HPC. It is the power behind efficient higher- order LES solver technology, and behind BOXERMesh, the reliable and easy-to-use parallel mesh generation system. Cray 709 901 Fifth Avenue Suite 1000 Seattle, WA 981642 Cambridge University Press 606 www.cray.com 32 Avenue of the Americas [email protected] New York, NY 10013 www.cambridge.org/us/academic Global supercomputing leader Cray builds innovative systems [email protected] and solutions enabling researchers in academia, government, and industry to meet existing and future simulation and Cambridge’s publishing in books and journals combines state- analytics challenges. of-the-art content with the highest standards of scholarship, writing and production. Visit our stand to browse new titles, available at a 20% discount, and to pick up sample issues of Dantec Dynamics, Inc. 702 our journals. Visit our website to see everything we do: www. 750 Blue Point Road cambridge.org/us/academic. Holtville, NY 11742 www.dantecdynamics.com CD-adapco 602 [email protected] Dantec Dynamics is a leading developer and supplier of 60 Broadhollow Road advanced measurement systems for fluid mechanics, solid Melville, NY 11747 www.cd-adapco.com mechanics, microfluidics, spray analysis and combustion [email protected] technology. Our products include: PIV, CTA, LDA, PDA, PLIF, DIC, and more. Measurement data include velocity, CD-adapco is the world’s largest independent CFD focused turbulence, particle size, concentration, temperature, provider of engineering simulation software, support and combustion species, strain/stress and vibration. services. We have over 30 years of experience in engineering simulation. The scope of our activities extends well beyond software development to encompass a wide range of CAE DARCorp 205 engineering services in both CFD and FEA. 1440 Wakarusa Drive Suite 500 Lawrence, KS 66049 Computational Engineering International 317 www.darcorp.com 2166 N. Salem Street [email protected] Apex, NC 27523 DARcorporation has been offering aeronautical engineering www.ceisoftware.com [email protected] software and consulting services since 1991. Our projects include single/multi-engine propeller and jet , EnSight is a data visualization software used in CFD & FEA. Business Jets, Very Light Jets (VLJ), Kit, LSA and Experimental EnSight is easy to learn, has a powerful calculator, Python aircraft, VTOL aircraft, UAVs for civil and military scripting, batch and interactive usage & high quality graphics. applications and hybrid air/ground vehicles. New in EnSight 10.1 is case comparison, native polyhedral support, improved HPC model support, much faster particle rendering and many more enhancements.

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dSPACE 202 G.R.A.S. Sound & Vibration 710 50131 Pontiac Trail 2234 E Enterprise Parkway Wixom, MI 48393-2020 Twinsburg, OH 44087 www.dspaceinc.com www.gras.us [email protected] [email protected] dSPACE is the world’s leading provider of hardware and From the beginning of GRAS, we have been involved in software tools for developing and testing sophisticated aerospace testing. Our dedication to aerospace partners to electronic control systems. dSPACE tools are used in high- find new ways of testing – GRAS has become an integral part performance engine development, navigation systems, of the industry. From standard microphones, to customized propulsion, real-time flight maneuver simulation and other flyover arrays, or for extreme sound pressures, we have applications. Learn more at www.dspaceinc.com. the microphones which will help you develop tomorrow’s . Energy Research Consultants 211 23342 South Pointe Drive, Suite E Higher Orbits 203 Laguna Hills, CA 92653-1422 ENERGY DC Metro Area www.ERC-Ltd.com RESEARCH www.higherorbits.org [email protected] CONSULTANTS [email protected] ERC provides specialized measurement Higher Orbits strives to launch students to and engineering services to commercial and government higher levels of performance, leadership clients. Non-intrusive diagnostic methods are used to measure and teamwork by using the wonder of spaceflight to ignite a reacting and non-reacting flow phenomena such as velocity, passion for Science, Technology, Engineering & Math (STEM). species, temperature, and droplet size, velocity and mass Mankind’s journey into space serves as an ideal launchpad to excite students of all ages about STEM, Leadership and flux. Expertise ranges from the basic science to practical working to fulfill their dreams and ambitions. configurations.

® Ennova-CFD 217 HyperSizer - Collier Research Corporation 508 760 Pilot House Dr. Ste. A 2150 Allston Way Newport News, VA 23606 Suite 250 www.hypersizer.com Berkeley, CA 94704 [email protected] www.ennova-cfd.com [email protected] As Collier Research Corporation’s flagship product, HyperSizer Software performs design, stress analysis, and detail sizing grid generation software for computational optimization for aerospace vehicles fabricated with composite fluid dynamics (CFD). Automated mesh generation for or metallic materials. On average, the software reduces the unstructured, structured and hybrid grids for internal and weight of structures by 20-40%, an exceptional achievement for external flows. aerostructures.

Granta Design 714 Intelligent Light 302 300 Rustat House 301 Route 17 N. 7th Floor 62 Clifton Road Rutherford, NJ 07070 Cambridge, Cambridgeshire UK www.ilight.com CB1 7EG [email protected] www.grantadesign.com [email protected] Intelligent Light provides post-processing, data management Granta Design is the materials information technology leader. and big data visualization capability for CFD. Thousands of Our materials data and information management solutions users rely on the industry leading FieldView software and our help aerospace enterprises to: manage data on composites, custom engineering services to maximize their productivity metals, and plastics; enable better materials decisions; reduce and effectiveness. Let us help you eliminate bottlenecks and regulatory and environmental risk; and provide materials achieve breakthrough results. support for design, analysis, and simulation.

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Kamatics/RWG 701 Metacomp Technologies 610 1330 Blue Hills Ave 28632 Roadside Drive, Suite 255 Bloomfield, CT 06002 Agoura Hills, CA 91301 www.kaman.com/engineered www.metacomptech.com [email protected] [email protected] For decades, Kamatics (USA) and RWG have been designing, Metacomp Technologies develops and disseminates simulation testing, and manufacturing the highest performing bearings software and services in multiple physics areas. ICMP and flight critical parts in the industry, excelling under the (Integral Computational Multi-Physics) is our unified most demanding conditions. vision for Multi-Physics simulations which simplifies the complexities of the individual disciplines. ICMP provides a single environment for Mesh Generation, CFD and Structural LaVision, Inc. 316 Analyses, and Visualization of results. 211 W. Michigan Avenue, Suite 100 Ypsilanti, MI 48197 www.lavisioninc.com Micro Craft, Inc. 615 [email protected] 207 Big Springs Ave. LaVision provides integrated imaging systems to scientific, Tullahoma, TN 37388 industrial and education markets. LaVision has extensive www.microcraft.aero experience in optical techniques such as 2-D, stereo and [email protected] tomographic particle image velocimetry, gaseous and liquid Micro Craft, Inc. is a 100% Employee Owned Small Business laser induced fluorescence, shadography for multi-phase flows, located in Tullahoma, Tennessee. We produce flight hardware digital image correlation for deformation/strain, high-speed for a wide variety of aircraft, wind tunnel models and space and ultra-high-speed imaging, and intensified camera systems. flight hardware. We possess excellent capabilities in design and test engineering services. Lockheed Martin Skunk Works® 502 1011 Lockheed Way NASA Aeronautics Research Directorate 716 Palmdale, CA 935997 NASA Headquarters www.lockheedmartin.com/ 300 E Street, SW us/aeronautics/skunkworks.html Washington, D.C. 20546 [email protected] www.aeronautics.nasa.gov The Skunk Works is focused on the critical aircraft for Research conducted by NASA’s Aeronautics Research Mission tomorrow. Advanced technology solutions draw on our world- Directorate has directly benefited today’s air transportation class capabilities in conceptual design, systems engineering system, aviation industry, and the passengers and businesses and integration, complex project management, software who rely on aviation every day. Our tools and technologies have development and rapid prototyping. already increased the capacity and improved the efficiency, safety, and environmental compatibility of the air transportation system. NASA continues to explore research and develop MathWorks 621 tools and technologies that can be integrated into even more 3 Apple Hill Drive advanced and efficient aircraft and airspace systems, including Natick, MA 01760 enabling game-changing concepts for the future. www.mathworks.com MathWorks is the leading developer of mathematical computing software. Engineers and scientists worldwide rely on its products NASA’s Space Technology 704 to accelerate the pace of discovery, innovation, and development. Mission Directorate For more information visit www.mathworks.com. NASA Headquarters 300 E Street, SW Washington, DC 20546 www..gov/spacetech Technology Drives Exploration. The nation’s investments in space technology enable NASA to make a difference in the world around us. The Space Technology Mission Directorate (STMD) is responsible for developing the crosscutting, pioneering, new technologies and capabilities needed by the agency to achieve its current and future missions.

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National Academies of Sciences, 415 Office of Naval Research 309 Engineering, and Medicine 875 North Randolph Street 500 Fifth Street NW Arlington, VA 22203 Washington, DC 20001 www.onr.navy.mil www.nationalacademies.org/rap [email protected] [email protected] The Office of Naval Research’s Naval The National Academies of Sciences, Engineering, and Air Warfare and Weapons division supports the Navy’s power Medicine conducts the NRC Research Associateship Programs projection needs, fostering the technology development of that offer awards for postdoctoral, senior, and graduate naval aircraft, structures, propulsion, autonomy, energetics, research in US federal laboratories and affiliated institutions. directed energy and electric weapons. Visit us at Booth #309. Awards include competitive stipends, relocation, professional travel and a health insurance plan. Complete information and online applications are on the website. Orbital ATK 315 77 Raynor Avenue Ronkonkoma, NY 11779 National Institute of Aerospace 516 [email protected] www.OrbitalATK.com 100 Exploration Way Hampton, VA 23666 Orbital ATK specializes in the design, build and delivery of www.NIAnet.org space, defense and aviation-related systems for customers [email protected] worldwide, both as a prime contractor and a supplier. We The National Institute of Aerospace is a non-profit research also offer a wide range of T&E services including flight and graduate education institute created in 2002 to conduct and load simulation; structural and environmental testing; leading-edge aerospace and atmospheric research, develop shock, vibration and thermal analysis; blast, ballistic and new technologies for the nation and help inspire the next fragmentation analysis and customized services. www. generation of scientists and engineers. OrbitalATK.com

National Reconnaissance Office (NRO) 510 Photron 611 14675 Lee Road 9520 Padgett Street, Suite 110 Chantilly, VA 21051 San Diego, CA 92126 https://acq.westfields.net www.photron.com [email protected] [email protected] NRO’s Director’s Innovation Initiative invests in advanced Photron has fifty years’ experience in manufacturing high- technologies, fosters innovation, and provides funding to speed video cameras for slow motion analysis of events improve our capabilities. It presents an opportunity for occurring to fast to understand. Systems include incredibly developers not traditionally associated with the NRO to light sensitive cameras; mega pixel to 21,000 frames per second participate in building the NRO of the 21st Century. (fps), high-G imagers for hostile environments, miniature remote head cameras and high definition digital motion analyzers. NUMECA USA, Inc. 708 1044 Larkin Street San Francisco, CA 94109 Pointwise, Inc. 318 www.numeca.com 213 S. Jennings Avenue [email protected] Fort Worth, TX 76104 www.pointwise.com Based on the most advanced technology, NUMECA CFD [email protected] software is known for its application-driven features and interface, optimal solutions, multi-physics models, high Pointwise, Inc. is solving the top problems facing engineering accuracy, speed and general user-friendliness. NUMECA analysts today: mesh generation for computational fluid solutions cover a wide range of aerospace flow analyses and dynamics. Manufacturing firms and research organizations use are recognized by a large number of commercial and military Pointwise’s mesh generation software to seamlessly bridge the groups. gap between CAD and computational fluid dynamics analysis. Find more information at pointwise.com.

www.aiaa-SciTech.org 32 #aiaaSciTech IExhibitors

Presidio Components, Inc. 715 SmartUQ 216 7169 Construction Court 1245 E. Washington Ave San Diego, CA 92121 Suite 210  www.presideiocomponents.com Madison, WI 53703 Quantify Every Uncertainty. [email protected] www.smartuq.com [email protected] US manufacturer of Space Qualified Ceramic Capacitors (QPL, NASA DWG, DSCC Approved Test Lab). Markets: Power SmartUQ software provides breakthrough analytics and Supplies SMD 0201-2225, SMPS Stacks to 180uF, High Voltage uncertainty quantification solutions for simulation and testing. Radial Leads, Crystal Oscillators, RF/MW Wirebondable Using advanced statistics and stochastic methods, SmartUQ allows engineers to quickly analyze Big Data, understand the Single Layers, Bypass and Broadband Bypass, SMD Broadband probabilities of all what-if scenarios, accelerate simulation DC Block, Lowest ESR Ultra-Porcelain for RF Power/Hi Q cycles, easily calibrate models, and create innovative designs applications. with greater confidence. SEDS@UCSD 706 Software Cradle Co., Ltd. 221 9500 Gilman Dr. La Jolla, CA 92093 50 Chestnut Street [email protected] Suite A-214 [email protected] Beavercreek, OH 45440 www.cradle-cfd.com We are the Students for the Exploration and Development [email protected] of Space here at UC San Diego. We are the first student organization to design, print, and test two 3D-Printed Software Cradle is a leading provider of general purpose Engines! Computational Fluid Dynamics (CFD) software including SC/Tetra (unstructured mesh), scSTREAM (Cartesian mesh), and HeatDesigner (Cartesian mesh for electronics). Since 1984, SG – Space & Ground Engineering Solutions 207 Cradle has established itself as a major innovator for advancing 6A Aigiidon Street the role of simulation in engineering design. Athens, Attica, Greece 11853 www.sg-incorp.com [email protected] Tecplot, Inc 301 SG Company provides integrated engineering solutions 3535 Factoria Blvd SE, Suite 550 for air/space-based earth monitoring systems and develops Bellevue, WA 98006 www.tecplot.com special techniques for UAS (Unmanned Aerial Systems) earth [email protected] observation applications in various disciplines. When you work with Tecplot you gain a partner you can trust, with 35 years of experience and more than 47,000 users Smart Material Corporation 213 worldwide, offering the fastest and most versatile desktop 2170 Main Street, Suite 302 visual data analysis tools on the market. Whether performing Sarasota, FL 34237 simulations, analyses or experiments, you can quickly explore www.smart-material.com your data and present high-quality images and animations [email protected] exactly the way you want – and it’s easy. Smart Material Corp. manufactures and develops advanced piezoelectric composites and electronics for actuators, sensors, TEN TECH LLC 215 energy harvesting and ultrasound transducers, including the MFC (Macro Fiber Composite) used for De-Icing, 5777 W Century Boulevard, Suite 830 TENTECH LLC Wing morphing, control, Vibration control, Energy , CA 90045 engineering services www.tentechllc.com Harvesting from Vibration, Structural Health Monitoring. [email protected] TEN TECH LLC is an ITAR-registered company serving the A&D industry with high-end mechanical engineering design, test and analysis services with emphasis on thermal, shock and vibration. TEN TECH LLC also provides sales and support for the SIMULIA, CATIA and ENOVIA lines of 3DS product as well as the 3DEXPERIENCE Platform with A&D focus.

www.aiaa-SciTech.org 33 #aiaaSciTech IExhibitors

Tetra Research Corporation 417 TSI, Inc. 705 420 Park Ave. West 500 Cardigan Road Princeton, IL 61356 Shoreview, MN 55126 www.tetraresearch.com www.tsi.com [email protected] [email protected] Tetra Research specializes in Loci/CHEM development and For over 50 years, TSI has been providing a complete applications. Loci/CHEM is a unique CFD software tool line of fluid diagnostics systems for air/gas flow research used by NASA and industry partners for stage separation, including: Particle Image Velocimetry, TR-Volumetric PIV, solid motor ignition and other multi-disciplinary analyses. Laser Doppler Velocimetry and Hot Wire Anemometry. These We provide support, customized development and training systems can be used for measuring supersonic to low speed services to allow you to make the most productive use of Loci/ flows, giving details of the fluid statistics. CHEM. UCRI 204 Tri Models Inc. 512 One Stetson Place 5191 Drive ML 0647 Huntington Beach, CA 92649 Cincinnati, OH 45221 www.ucri.org UNIVERSITY of CINCINNATI www.trimodels.com RESEARCH INSTITUTE [email protected] [email protected] UCRI is an independent not-for-profit 501(c)(3) organization Tri Models is the Premier supplier of Wind Tunnel Models & which serves for the University of Cincinnati (UC). UCRI Ground Test hardware for the global aerospace community. makes it easy for the industry partners to connect with UC We play a vital role in the development of new systems for the on business ideas, research projects, resource needs and other companies. Whether you have a new program or are industry essentials. refining an existing vehicle, Tri Models can help. University of Kansas 711 Triumph Aerospace Systems 616 12600 Quivira Road 703 Middle Ground Boulevard Overland Park, KS 66062 Newport News, VA 23606 https://aeroshortcourses.ku.edu www.triumphgroup.com/companies [email protected] /triumpn-aeros-ace-systems-newport-news [email protected] The KU Aerospace Short Course Program is one of the most respected non-credit professional development programs in Triumph Aerospace Systems is an industry leader in the the world. Our outstanding instructors—drawn from industry, development, engineering and manufacture of complex academia and government experts—translate theory into aerospace hardware, and prototype systems for force practical application, so you can return to work and solve real- measurement devices, ground test and flight applications. We world problems immediately. provide new balances, turn-key model positions systems, and calibrations to the wind tunnel industry.

www.aiaa-SciTech.org 34 #aiaaSciTech IExhibitors

United Technologies Research Center (UTRC) 201 XFlow CFD 219 4th Floor 40 Chellis Street Penrose Business Centre White River Junction, VT 05001 Penrose Wharf, Cork Ireland www.xflowusa.com www.utrc.utc.com [email protected].

United Technologies Research Center delivers advanced XFlow™ CFD is the next-generation, meshless CFD package for technologies to the businesses of United Technologies Corp. modeling external aerodynamics of fixed-wing and aircraft. (UTC) to improve the performance, energy efficiency and XFlow supports complex motion of complicated moving parts to cost of UTC products and processes. UTRC also engages with model dynamic effects of control surface motion in flight, high-lift UTC business units and external research organizations to (take-off and landing) configurations and/or separation of munitions expand the boundaries of science and technology through or separable stores. research and innovation, delivering technology options that meet and anticipate the needs of the marketplace. Founded in 1929, UTRC is headquartered in East Hartford, Connecticut. and has research and development subsidiaries established in Shanghai, , and Cork, Ireland. UTRC’s affiliate, United Technologies Research Center, Inc., has a research facility in Berkeley, California. Find out what it means to Be Curious at www.utrc.utc.com.

www.aiaa-SciTech.org 35 #aiaaSciTech May 16-20, 2016 Daejeon, Korea

Expanding the Space Community

Hosted in 2016 by the Korea Our attendees are technologists, Aerospace Research Institute (KARI) scientists, managers of space agencies and the American Institute for and academics. They share experiences, Aeronautics and Astronautics (AIAA), challenges and innovative solutions with SpaceOps is a biennial technical forum colleagues from around the globe. of the space operations community focused on state-of-the-art operations principles, methods and tools.

Technical Programs for SpaceOps 2016 include:

• Operations Concepts and Flight Execution • Ground Systems, Communications and Data Processing • Mission Design and Management • Planning and Scheduling • and Commercial Space Operations • Guidance, Navigation and Control • Cross Support, Interoperability and Standards • Human Systems and Operations • Launcher, and Operations • Emerging Space Operations in Asia and Developing Countries

Registration Opens 1 February 2016 Learn more: www.spaceops2016.org IN 2016 the AIAA Foundation is celebrating 20 YEARS of making a direct impact in K–12 classrooms, 20 YEARS of our hands-on STEM-focused activities, 20 YEARS of our college scholarships, 20 YEARS of our design competitions and 20 YEARS of our student conferences & awards. Be part of the celebration and join us as we launch the 20/20 “Celebrate 20 years with a $20 donation” fundraising campaign to engage our membership like never before. Through the 20/20 campaign, AIAA IS ASKING ALL MEMBERS TO DONATE $20 and with the goal of 10,000 members each donating $20, the AIAA Foundation will raise $200,000.

YOUR $20 DONATION will provide leadership and resource opportunities for our future aerospace leaders.

DONATE TODAY! www.aiaafoundation.org

#AdvancingAerospace

15-875 Foundation2020-ad-fullpage.indd 1 11/24/15 8:49 AM IGeneral Information

AIAA Registration Hours Conference Proceedings AIAA Registration will be located on the second floor of the Proceedings for the forum will be available online. The cost hotel in the Palm and Seaport Foyers is included in the registration fee where indicated. Online Sunday, 3 January 1500–1900 hrs proceedings will be available on Monday, 4 January. Monday, 4 January –Thursday, 7 January 0700–1730 hrs Instructions to Access Proceedings: 1. To view proceedings, visit www.aiaa.org >ARC>Meeting Papers. Friday, 8 January 0700–1230 hrs a. Log in with the link at the top right of the page. b. Select the appropriate conference from the list. c. Search for individual papers with the Quick Search Wi-Fi Internet Access On Site toolbar in the upper-right corner of the page: AIAA is providing limited Wi-Fi service for attendees to use i. By paper number: Click the Paper Number link, select while on site. To keep this service available and optimized for the conference year, and enter the paper number. all attendees, please do not download files larger than 2MB, ii. Use the Search textbox to find papers by author, create multiple sessions across multiple devices, or download title, or keyword. The Advanced Search link provides multiple files in one session. If you receive an error message additional search information and options. that an AIAA server is blocking your current IP address, please inform the AIAA registration desk. 2. All manuscript files submitted by four days prior to the conference are currently in the proceedings. Files submitted Network Name: SCITECH2016 after that date, both original and revised manuscripts, will Password: aiaa2016 not be available until the final proceedings update, which may take up to 15 business days after the last day of the 1. View Available Wireless Networks conference. 2. Connect to “SCITECH2016” Network 3. Direct any questions concerning access to proceedings and/ 3. Enter the Password aiaa2016 or ARC to [email protected]. 4. Open your Web Browser, begin surfing Manuscript Revisions For Assistance, please call our Meeting Room Internet 5. Manuscript revision is open for all presenting authors Support at 619.796.5551. from 0900 hrs Eastern Time, Monday, 4 January through 2000 hrs Eastern Time, Wednesday, 20 January. Revisions submitted during this period are limited to minor changes AIAA Livestream Channel only (e.g., typos and the like). Changes to content are not permitted. Visit livestream.com/aiaavideo/scitech2016 to view selected keynotes, plenaries, and Forum 360 sessions. Share the link 6. Revisions submitted for manuscripts already online will with colleagues who couldn’t attend the conference, so they not refresh until after the proceedings have been updated, can watch live or view later. which may take up to 15 business days after the last day of the conference.

Sponsored by: Certificate of Attendance Certificates of Attendance are available for attendees who request documentation at the forum itself. Beginning Wednesday, 6 January, you will be able to create and print Social Media at #aiaaSciTech your certificate at AIAA Registration. AIAA offers this service to better serve the needs of the professional community. Interested in participating in social media at #aiaaSciTech? Claims of hours or applicability toward professional education Use the hashtag #aiaaSciTech and watch for your Tweets and requirements are the responsibility of the participant. Instagrams to be displayed at the conference. There will again be a Twitter contest running throughout AIAA SciTech 2016. Meet your rivals and have fun networking with other science and engineering professionals at the official Tweet Up, which will be held at Redfield’s Sports Bar inside the conference hotel at 5:00 p.m. on 6 January 2016. Official Contest Rules: www.aiaa-scitech.org/TwitterContest/

www.aiaa-SciTech.org 38 #aiaaSciTech IGeneral Information

Employment Opportunities Young Professional Guide for Gaining AIAA members can post and browse resumes, browse job Management Support listings, and access other online employment resources by Young professionals have the unique opportunity to meet and visiting the AIAA Career Center at careercenter.aiaa.org. learn from some of the most important people in the business by attending conferences and participating in AIAA activities. A detailed online guide, published by the AIAA Young Membership Professional Committee, is available to help you gain support AIAA is your vital lifelong link to the collective creativity and and financial backing from your company. The guide explains brainpower of the aerospace profession and a champion for the benefits of participation, offers recommendations, and its achievements. Included in the nonmember full conference provides an example letter for seeking management support registration fee is a one-year AIAA membership. Students who and funding, and shows you how to get the most out of your are not yet members may apply their registration fee toward participation. The online guide can be found on the AIAA their first year’s student member dues. (Membership is not website at www.aiaa.org/YPGuide. included in discounted group-rate registration.) Badge Policy AIAA forum badges are provided to those attendees who have paid for a registration to the event (and must be worn at all times to participate in all forum activities). Badges are not provided at the registration desk for committee meetings. To AIAA Foundation Celebrates 20 Years obtain a SciTech badge, you must register for the forum. The AIAA Foundation exists to inspire students by developing programs that will shape the next generation of aerospace professionals. As we celebrate our 20th anniversary, help us Nondiscriminatory Practices accomplish an amazing feat. Please consider donating $20 for the 20 years of leadership and resources that the AIAA AIAA accepts registrations irrespective of race, creed, sex, Foundation has provided. With a goal of having 10,000 members color, physical handicap, and national or ethnic origin. each donate $20, the AIAA Foundation will raise $200,000. Your generous gift will contribute to the wealth of resources that AIAA develops to support STEM education at every level. Restrictions Our mission to promote education and recognize excellence in Photos, video, or audio recording of sessions or exhibits, as the aerospace community is funded by visionaries just like you. well as the unauthorized sale of AIAA-copyrighted material, is You can make a difference. prohibited. The AIAA Foundation has already accelerated the future of aerospace by: • Funding more than 1,200 K–12 Classroom Grants, impacting over 120,000 precollege students • Awarding aerospace scholarships to more than 1,300 undergraduate and graduate students • Supporting more than 400 student conferences, engaging more than 13,000 students with practical, hands-on STEM-based projects • Sponsoring design competitions that have generated more than 1,200 teams, engaging more than 14,000 students • Inspiring more than 200 student branches, 8,000 student members, and 4,000 Educator Associates with resources to further their career path To make a donation on site, please visit the AIAA Pavilion in the Exposition Hall, and be entered to win a 2-night complimentary stay at the Gaylord Texan during AIAA SciTech 2017.* For more information about the AIAA Foundation and to make a donation online, please visit www.aiaafoundation.org. *Please note: a donation is not necessary to be entered in the raffle. www.aiaa-SciTech.org 39 #aiaaSciTech GeneralI Information

Author and Session Chair Information

Speakers’ Briefings in Session Rooms Audiovisual Authors who are presenting papers will meet with session chairs Each session room will be preset with the following: one LCD and co-chairs in their session rooms for a short 30-minute projector, one screen, one microphone and sound system briefing on the day of their sessions to exchange bios and review (if necessitated by room size), and one laser pointer. Laptop final details prior to the session. Please attend on the day of computers will also be provided. You may also use your own your session(s). Laptops preloaded with the Speaker Briefing computer. Any additional audiovisual equipment requested on preparation slides will be provided in each session room. site will be at cost to the presenter. Please note that AIAA does Speaker’s Briefing schedule is as follows: not provide security in the session rooms and recommends Monday, 4 January–Friday, 8 January: 0730 hrs that items of value not be left unattended. Speakers’ Practice Room “No Paper, No Podium” and “No Podium, No Paper” Policy Speakers who wish to practice their presentations may do so in the Solana Beach B room located on the third level of the If a written paper is not submitted by the final manuscript Seaport Tower. A sign-up sheet will be posted on the door. In deadline, authors will not be permitted to present the paper at consideration of others, please limit practice time to 30-minute the forum. Also, if the paper is not presented at the forum, it increments. will be withdrawn from the proceedings. It is the responsibility of those authors whose papers or presentations are accepted to Session Chair Reports ensure that a representative attends the conference to present the paper. These policies are intended to improve the quality of All session chairs are asked to complete a session chair report to the program for attendees. evaluate their session for future planning. AIAA has partnered with Canvas Solutions to provide an electronic Session Chair Journal Publication Report form. You can download the FREE mobile app in your App Store, AppWorld, or Marketplace by searching for AIAA has prior publication rights to any paper presented “Canvas Solutions, Inc.” The mobile app is free, so please be at its conferences. Authors who are seeking the opportunity sure to download it. Detailed instructions will be provided in for peer-reviewed publication are encouraged to submit the session rooms. If you do not have a tablet or a smartphone, their papers for consideration by one of the Institute’s simply use the report form as a guide and enter your session archival journals: AIAA Journal; Journal of Aircraft; Journal chair report information at the session chair reporting computer of Air Transportation; Journal of Guidance, Control, and station located on site near the AIAA registration area. Report Dynamics; Journal of Propulsion and Power; Journal of data will be collected and used for future planning purposes, Spacecraft and Rockets; Journal of Thermophysics and Heat including session topics and room allocations. Please submit Transfer; or Journal of Aerospace Information Systems your session chair report electronically by Friday, 8 January. (formerly Journal of Aerospace Computing, Information, and Communication). You may now submit your paper online at http://mc.manuscriptcentral.com/aiaa

AIAA is the world’s largest aerospace professional society, serving a diverse range of more than 30,000 individual members from 88 countries, and 95 corporate members. AIAA members help make the world safer, more connected, more accessible, and more prosperous. For more information, visit www.aiaa.org, or follow us on Twitter @AIAA. American Institute of Aeronautics and Astronautics 12700 Sunrise Valley Drive, Suite 200 Reston, VA 20191-5807 703.264.7500 or 800.639.AIAA (2422) Fax: 703.264.7657 [email protected] www.aiaa.org

www.aiaa-SciTech.org 40 #aiaaSciTech ICommittee Meetings and Events

Time Title Location Sunday, 3 January 2016 1200-1700 TAC TC/PC Chair Training Torrey Hills AB 1300-1700 TAC Director/Deputy Director Training Hillcrest A 1430-1500 APATC Liaisons Subcommittee Golden Hill A 1430-1600 General Standards and Architecture Tutorial Hillcrest BC 1500-1600 APATC Education Subcommittee Golden Hill A 1500-1600 APATC Honors & Awards Subcommittee Gaslamp A 1500-1600 APATC Membership & Nominations Subcommittee Gaslamp B 1500-1600 APATC Planning Subcommittee Cortez Hill A 1500-1600 APATC Publicity & Publications Subcommittee Cortez Hill B 1530-1700 Student / Young Professional Networking Mission Beach A 1600-1700 APATC Steering Subcommittee Gaslamp A 1600-1700 FDTC Algorithm Development (High Order Methods) Golden Hill A 1600-1730 Structural Dynamics of Rocket Engines Tutorial Old Town AB 1700-1800 GTTC Steering Subcommittee Gaslamp CD 1700-2000 Applied Aerodynamics TC Torrey Hills AB 1715-1815 FDTC Large Eddy Simulation DG Golden Hill A 1800-1900 GTTC Introduction/Overview Gaslamp CD 1800-2030 Structures TC Regatta AB 1800-2200 GNCTC Graduate Student Paper Competition Balboa A 1800-2200 Atmospheric Flight Mechanics TC Hillcrest B-D 1830-2000 FDTC Steering Committee Golden Hill A 1900-2000 GTTC Publications Subcommittee Gaslamp CD 1900-2100 FDTC Transition DG Old Town AB 1900-2100 FDTC Low Re Number DG - Preparation Meeting La Jolla AB 1900-2100 TAC Propulsion and Energy Group Meeting Hillcrest A 1900-2100 TAC Aircraft and Atmospheric Systems Group Meeting Solana Beach A 1900-2100 TAC Information Systems Group Meeting Gaslamp A 1900-2100 TAC Aerospace Design and Structures Group Meeting Gaslamp B 1900-2100 TAC Engineering and Technology Management Group Meeting Cortez Hill A 1900-2100 TAC Space and Missiles Group Meeting Cortez Hill B 1900-2200 TAC Program Committees Group Meeting Balboa C 2000-2100 GTTC Conferences Subcommittee Gaslamp CD 2000-2100 AMTTC Conferences Subcommittee Torrey Hills AB Monday, 4 January 2016 0800-0900 HSABPTC Steering Committee Conference Parlor 705 0800-1600 GTTC Internal Balance WG Cityview A 0900-1000 ABPTCs Steering Committee Conference Parlor 705 0900-1100 Journals Subcommittee Conference Parlor 724 1000-1100 HSABPTC Meeting Mission Beach A 1000-1100 ABPSITC Meeting Cityview B 1000-1100 GTETC Meeting Conference Parlor 705 1100-1200 Books Subcommittee Conference Parlor 724 1100-1200 PAW Workshop Mission Beach A www.aiaa-SciTech.org 41 #aiaaSciTech ICommittee Meetings and Events

Time Title Location Monday, 4 January 2016 (continued) 1100-1300 Solid Rockets TC Cityview B 1200-1300 ABPTCs Conference Subcommittee Conference Parlor 705 1200-1400 Aircraft Electric Propulsion Path Forward Solana Beach A 1230-1400 GNCTC Undergraduate Conference Experience in GNC Conference Parlor 717 1300-1500 Education Series Editorial Advisory Board Conference Parlor 724 1300-1500 SEC Reorganization TG Mission Beach A 1400-1500 ABPTCs Honors & Awards Subcommittee Conference Parlor 705 1500-1600 ABPTCs Education Subcommittee Conference Parlor 705 1500-1600 FDTC Free Shear and Mixing Layer Control Mission Beach A 1500-1700 Progress Series Editorial Advisory Board Conference Parlor 706 1500-1700 Relevancy Working Group Conference Parlor 733 1730-1830 The Future of AIAA: Why Governance Matters to You Seaport ABCDE 1600-1700 ABPTCs Communications Subcommittee Conference Parlor 705 1630-1730 FDTC Modal Decomposition DG Hillcrest D 1700-1800 ABPTCs Membership Subcommittee Conference Parlor 705 1700-1800 APATC Missile & Projectile Aeroprediction DG Cityview A 1700-1800 AMTTC New Member Orientation Conference Parlor 706 1700-1830 CASE 2016 Planning Meeting La Jolla B 1700-1830 FDTC Flow Control and Fluid App SC Conference Parlor 734 1700-1900 ABPTCs WGs (TC Meeting Prep) Conference Parlor 733 1730-1830 FDTC Turbulence Model Benchmarking DG Harbor D 1730-1930 Aerospace @ Illinois Alumni Reception Regatta A 1730-2000 SCSTC Handbook on Testing Large Structures Conference Parlor 724 1730-2030 Flight Testing TC Conference Parlor 717 1800-1900 GTTC Awards Subcommittee Coronado B 1800-2000 AMTTC Awards Subcommittee Conference Parlor 706 1800-2100 Society and Aerospace Technology TC Cityview B 1830-1915 2016 Associate Fellows Reception Seaport Foyer Terrace 1830-1930 MATTC ICME Prize Planning Torrey Hills AB 1830-2100 CASE 2016 Applied Complexity Workshop Planning La Jolla B 1830-2130 Energy Optimized Aircraft and Equipment Systems PC Harbor D 1900-2000 GTTC Education and Student Activities Subcommittee Regatta BC 1900-2030 APATC Validation of Numerical Models DG Cityview A 1900-2100 ABPTCs Meeting Cortez Hill AB 1900-2100 FDTC CFD Subcommittee America’s Cup A 1900-2100 FDTC Fundamentals Subcommittee America’s Cup B 1900-2100 Adaptive Structures TC Coronado D 1900-2130 Propellants and Combustion TC Coronado E 1900-2200 Aircraft Design TC Coronado A 1900-2200 Career and Professional Development Committee Conference Parlor 733 1900-2200 TAC Aerospace Sciences Group Meeting Hillcrest AB 1900-2200 MVCETC Meshing Subcommittee Cortez Hill C 1900-2200 Terrestrial Energy Systems TC Coronado B www.aiaa-SciTech.org 42 #aiaaSciTech ICommittee Meetings and Events

Time Title Location Monday, 4 January 2016 (continued) 1900-2200 Small Satellite TC Mission Beach A 1930-2130 MATTC ICME Subcommittee Torrey Hills AB 1930-2230 2016 Associate Fellows Ceremony and Dinner - Ticket Required Seaport FG Tuesday, 5 January 2016 0800-0900 Audit Committee Conference Parlor 705 0800-1000 2017 Associate Fellows Committee Cityview AB 0800-1000 Journal of Guidance, Control and Dynamics Editorial Advisory Board Mission Beach A 0800-1000 International Activities Committee Torrey Hills AB 0900-1000 Publications Ethical Standards Subcommittee Conference Parlor 724 0900-1000 RAC III Meeting - By Invite Only Conference Parlor 705 0900-1100 ISC Awards Brunch - By Invite Only Seaport H 0900-1100 RAC I Conference Parlor 706 0915-1545 Career Workshop: Communications and Connections for Your Career Vista AB 0900-1700 GTTC Dual Flow Reference Nozzle WG Conference Parlor 717 1000-1100 Publications Awards Subcommittee Conference Parlor 724 1000-1200 Journal of Propulsion and Power Editorial Advisory Board Mission Beach A 1000-1200 TAC New Initiatives Subcommittee Cityview AB 1030-1130 RAC IV Meeting - By Invite Only Conference Parlor 705 1030-1200 Finance Committee Torrey Hills AB 1100-1200 Publications Review Subcommittee Conference Parlor 724 1200-1730 Region and Section Activities Committee Mission Beach A 1230-1630 GTTC Model Attitude & Deformation WG Conference Parlor 734 1300-1500 Student Activities Committee Cityview AB 1300-1500 SEC/CoSs Joint Meeting Torrey Hills AB 1400-1500 HyTASP PC Steering Committee Conference Parlor 705 1500-1600 TPTC Best Paper Subcommittee Conference Parlor 705 1500-1700 LM Aeronautics Meeting Torrey Hills AB 1500-1800 Public Policy Committee Meeting Cityview AB 1600-1700 TPTC Awards Subcommittee Conference Parlor 705 1600-1700 TPTC Education Subcommittee Conference Parlor 706 1600-1800 Journal of Spacecraft and Rockets Editorial Advisory Board Conference Parlor 733 1630-1730 Membership Matters: How Far Will You Go? Regatta B 1630-1730 GEPC Conference Subcommittee Conference Parlor 724 1630-1830 Journal of Thermophysics and Heat Transfer Editorial Advisory Board Conference Parlor 734 1700-1800 TPTC Publicity Subcommittee Conference Parlor 705 1700-1800 TPTC Conferences Subcommittee Conference Parlor 706 1700-1900 Computational Fluid Dynamics Committee on Standards (CFD CoS) Torrey Hills AB 1730-1830 GEPC Leadership Team Conference Parlor 724 1800-1900 FDTC Future of Fluids Subcommittee Conference Parlor 706 1800-1900 APATC DG Hillcrest A 1800-1900 Liquid Propulsion TC Mission Beach A 1800-1900 TPTC Nominations Subcommittee Conference Parlor 705 www.aiaa-SciTech.org 43 #aiaaSciTech ICommittee Meetings and Events

Time Title Location Tuesday, 5 January 2016 (continued) 1800-1900 TPTC Publications Subcommittee Conference Parlor 717 1800-2100 Unmanned Systems PC America’s Cup D 1830-2100 Publications Committee America’s Cup AB 1830-2130 Intelligent Systems TC Coronado E 1830-2130 Transformational Flight PC Balboa AB 1830-2130 ASME Wind Energy TC Cityview AB 1830-2230 Membership Committee Conference Parlor 734 1900-2100 Plasmadynamics and Lasers TC Torrey Hills AB 1900-2200 Aerospace Department Chair Association Meeting Harbor B 1900-2200 Fluid Dynamics TC Cortez Hill AB 1900-2200 Aeroacoustics TC Mission Beach A 1900-2200 Materials TC Coronado A 1900-2200 Pressure Gain Combustion PC Hillcrest A 1900-2200 Sensor Systems and Information Fusion TC Conference Parlor 706 1900-2200 Thermophysics TC Coronado D 1900-2300 Aerodynamics Measurement Technology TC Coronado B 1930-2130 HyTASP PC Harbor F 1930-2230 Structures TC Harbor H Wednesday, 6 January 2016 0800-1200 GTTC Dual Flow Reference Nozzle WG Conference Parlor 706 0800-1200 GTTC Future of Ground Test WG Conference Parlor 724 0800-1700 Systems Engineering TC Mission Beach A 0900-1100 Standards Executive Council (SEC) Meeting Conference Parlor 705 0900-1200 Cross Check Workshop and Journal Editors in Chief Conference Parlor 733 0900-1200 DETC Subcommittee Meeting Conference Parlor 717 0930-1200 Foundation Board of Trustees Cityview A 0930-1200 Region and Section Activities Committee Torrey Hills AB 0930-1200 TAC Executive Board Cityview B 1200-1700 Technical Activities Committee Seaport H 1300-1600 DETC Subcommittee Meeting Conference Parlor 717 1300-1600 Corporate Member Committee Meeting Torrey Hills AB 1300-1700 GTTC Uncertainty Analysis WG Conference Parlor 705 1330-1500 RAC II Meeting Conference Parlor 706 1330-1630 Honors and Awards Committee Cityview B 1330-1630 Institute Development Committee Cityview A 1400-1700 Aerospace Cyber Security WG Conference Parlor 724 1500-1700 Education Activities Committee (EAC) Conference Parlor 706 1700-1800 Short Course Brainstorming Session Torrey Hills AB 1700-1800 AMTTC Nominations Subcommittee Conference Parlor 706 1700-1900 Emerging Technologies Committee Conference Parlor 724 1700-2000 Digital Avionics TC Conference Parlor 705 1730-1830 FDTC Low Re DG Cityview B 1730-1830 FDTC Free Shear and Mixing Layer Control Cityview A www.aiaa-SciTech.org 44 #aiaaSciTech ICommittee Meetings and Events

Time Title Location Wednesday, 6 January 2016 (continued) 1730-2000 Green Engineering PC Old Town A 1800-1900 GTTC New Member and Mentors Meeting Conference Parlor 706 1800-1930 FDTC Non-Equilibrium DG Coronado E 1800-2000 APATC Rotorcraft Simulations & Performance Predictions DG Coronado D 1800-2100 History TC Mission Beach A 1800-2100 V/STOL Aircraft Systems TC Ocean Beach 1800-2100 Design Engineering TC Conference Parlor 717 1800-2200 Guidance, Navigation and Control TC Torrey Hills AB 1800-2200 Spacecraft Structures TC Harbor H 1830-1930 ASME Structures and Materials TC Cityview A 1830-2000 Crawford Slip Method Workshop on Networking Harbor A 1830-2030 AMTTC Update Presentation/Student Event Seaport H 1830-2030 Journal of Aircraft Editorial Advisory Board America’s Cup CD 1830-2030 Publications Book Authors Appreciation Reception Bankers Hill 1830-2030 Aurora Flight Sciences Harbor C 1830-2130 Multidisciplinary Design Optimization TC Harbor F 1830-2130 Survivability TC Cityview B 1830-2200 Software TC Solana Beach A 1900-2000 FDTC Flow Control on Unmanned Aircraft Balboa C 1900-2000 FDTC Solver Technology for Turbulent Flows La Jolla AB 1900-2100 Plasma Aerodynamics DG Harbor D 1900-2200 Meshing, Visualization and Computational Environments TC Coronado A 1900-2200 Non-Deterministic Approaches TC Coronado B 1900-2200 Structural Dynamics TC Harbor E 1930-2100 Academic Affairs Committee Meeting Cityview A 2000-2100 FDTC High Speed Flow Control La Jolla AB Thursday, 7 January 2016 0800-1000 AIAA Journal Editorial Advisory Board Cityview AB 0800-1200 GTTC Flow Quality WG Mission Beach A 0900-1200 Board of Directors Torrey Hills AB 1000-1100 SciTech 2017 Technical Program Committee Cityview AB 1230-1400 AIAA Ethics Committee Torrey Hills AB 1330-1730 Governance Retreat I - By Invite Only Cityview AB 1400-1600 GTTC Statiscally Defensible Test Methods Focus Group Mission Beach A 1730-1830 APATC Low Boom DG Mission Beach A 1730-2000 SCSTC High Strain Composites Subcommittee Harbor G 1730-2030 Ground Testing TC Torrey Hills AB 1830-2130 Modeling and Simulation TC Mission Beach A Friday, 8 January 2016 0800-1200 Governance Retreat II - By Invite Only Cityview AB 0800-1700 GTTC Industry WG Torrey Hills A

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Abbreviation Title Date Start Time End Time Location Aeroacoustics 5-AA-1 Aeroacoustics - Jet Noise I 4-Jan 0900 hrs 1230 hrs Nautical 58-AA-2 Computational Aeroacoustics I 4-Jan 1400 hrs 1730 hrs Nautical 115-AA-3 Aeroacoustics - Jet Noise II 5-Jan 0900 hrs 1230 hrs Nautical 167-AA-4 Computational Aeroacoustics II 5-Jan 1400 hrs 1730 hrs Nautical 221-AA-5 Aeroacoustics - Advanced Measurement and Experiment 6-Jan 0900 hrs 1230 hrs Nautical 272-AA-6 Aeroacoustics - Fan, Rotor, and Airframe Noise 6-Jan 1400 hrs 1730 hrs Nautical Air Breathing Propulsion Systems Integration 6-ABPSI-1/GEPC-1 NASA ERA Systems Integration I 4-Jan 0900 hrs 1230 hrs Golden Hill B 59-ABPSI-2/GEPC-2 NASA ERA Systems Integration II 4-Jan 1400 hrs 1730 hrs Golden Hill B 116-ABPSI-3 Inlets 5-Jan 0900 hrs 1230 hrs Golden Hill B 168-ABPSI-4 Propulsion Integration 5-Jan 1400 hrs 1730 hrs Golden Hill B 222-ABPSI-5 High Speed Propulsion Integration 6-Jan 0900 hrs 1230 hrs Hillcrest D Aircraft Design 117-ACD-1 Aircraft Design Issues I 5-Jan 0900 hrs 1230 hrs Cortez Hill A 169-ACD-2 Aircraft Design Issues II 5-Jan 1400 hrs 1730 hrs Cortez Hill A 170-ACD-3 Aircraft Wing Design 5-Jan 1400 hrs 1730 hrs Bankers Hill 223-ACD-4 Electric Aircraft Design 6-Jan 0900 hrs 1230 hrs Bankers Hill 224-ACD-5 Transport Aircraft Design I 6-Jan 0900 hrs 1230 hrs Cortez Hill A 273-ACD-6 Aircraft Design Tools 6-Jan 1400 hrs 1730 hrs Bankers Hill 274-ACD-7 Transport Aircraft Design II 6-Jan 1400 hrs 1730 hrs Cortez Hill A 325-ACD-8 Unmanned Aerial Vehicle Design 7-Jan 0900 hrs 1230 hrs Cortez Hill A 326-ACD-9 Conceptual Aircraft Design Working Group 21, CADWG 7-Jan 0900 hrs 1200 hrs Hillcrest D 374-ACD-11 Micro Air Vehicle Design 7-Jan 1400 hrs 1730 hrs Cortez Hill A 428-ACD-13 Aircraft Design Optimization 8-Jan 0900 hrs 1230 hrs Bankers Hill Atmospheric Flight Mechanics 7-AFM-1 Biometric Flight Mechanics 4-Jan 0900 hrs 1230 hrs Cortez Hill A 8-AFM-2 Atmospheric Entry, Hypersonic Flight and Aeroassist Technology I 4-Jan 0900 hrs 1230 hrs Cortez Hill B 60-AFM-3 Special Session: Flight Testing in Education 4-Jan 1400 hrs 1730 hrs Bankers Hill 61-AFM-4 Atmospheric Entry, Hypersonic Flight and Aeroassist Technology II 4-Jan 1400 hrs 1730 hrs Cortez Hill B 118-AFM-5 Launch Vehicle, Missile, and Projectile Flight Mechanics I 5-Jan 0900 hrs 1230 hrs Cortez Hill B 171-AFM-6 Launch Vehicle, Missile, and Projectile Flight Mechanics II 5-Jan 1400 hrs 1730 hrs Cortez Hill B 225-AFM-7 Aircraft Flight Dynamics, Handling Qualities, and Performance I 6-Jan 0900 hrs 1230 hrs Harbor A 226-AFM-8 Special Session: LOC-5: Aircraft Loss of Control (LOC) Modeling Methods 6-Jan 0900 hrs 1230 hrs Coronado B 275-AFM-9 Aircraft Flight Dynamics, Handling Qualities, and Performance II 6-Jan 1400 hrs 1730 hrs Harbor A 327-AFM-10 Small/Mini/Micro Aerial Vehicles 7-Jan 0900 hrs 1230 hrs Hillcrest B 328-AFM-11 Aerodynamic Prediction Methods, Aircraft Flight Dynamics, Handling 7-Jan 0900 hrs 1230 hrs Harbor A Qualities, and Performance 375-AFM-12 Special Session: Realizing Performance Adaptive Aeroelastic Wing: 7-Jan 1400 hrs 1730 hrs Coronado D Progress and Challenges 376-AFM-13 Flight Test and System Identification I 7-Jan 1400 hrs 1730 hrs Harbor A 429-AFM-14 Aeroserovelastic (ASE) Control, Modeling, Simulation, and Optimization 8-Jan 0900 hrs 1230 hrs Cortez Hill A 430-AFM-15 Flight Test and System Identification II 8-Jan 0900 hrs 1230 hrs Harbor A www.aiaa-SciTech.org 46 #aiaaSciTech ISessions at a Glance

Abbreviation Title Date Start Time End Time Location Aerodynamic Measurement Technology 9-AMT-1 Velocimetry I 4-Jan 0900 hrs 1230 hrs Balboa B 62-AMT-2 Spectroscopy and Combustion Applications 4-Jan 1400 hrs 1730 hrs Balboa B 172-AMT-4 Velocimetry II 5-Jan 1400 hrs 1730 hrs Harbor D 227-AMT-5 Tomographic, Holographic and Other Volumetric Measurements 6-Jan 0900 hrs 1230 hrs Harbor D 276-AMT-6/PC-11/ Special Walter Lempert Memorial Session II (Invited) 6-Jan 1400 hrs 1730 hrs Harbor D PDL-8 329-AMT-7 Error Sources and Calibration of Instruments 7-Jan 0900 hrs 1230 hrs Harbor D 377-AMT-8 High Speed Facility Measurements 7-Jan 1400 hrs 1730 hrs Harbor D 431-AMT-9 Surface Pressure and Skin Friction Measurements 8-Jan 0900 hrs 1230 hrs Harbor D 10-AMT-10/SD-15 Advances in Fluid-Structural Interaction Experimentation 4-Jan 0900 hrs 1230 hrs Coronado D Applied Aerodynamics 11-APA-2 Special Session: Simulation of Rotor in Hover I 4-Jan 0900 hrs 1230 hrs Coronado E 12-APA-3 Aerodynamic Testing: Flight and Large Scale 4-Jan 0900 hrs 1230 hrs America’s Cup C 13-APA-4 & Supersonic Aerodynamics 4-Jan 0900 hrs 1230 hrs America’s Cup D 63-APA-6/FD-7 Special Session: Advances in Fundamental Unsteady Low Reynolds 4-Jan 1400 hrs 1730 hrs Coronado D Number Flows AVT-202 64-APA-7 Aerodynamic Design: Analysis, Methodologies, and Optimization 4-Jan 1400 hrs 1730 hrs America’s Cup B Techniques I 65-APA-8 Special Session: Simulation of Rotor in Hover II 4-Jan 1400 hrs 1730 hrs Coronado E 66-APA-9 High Angle of Attack and High Lift Aerodynamics 4-Jan 1400 hrs 1730 hrs America’s Cup C 67-APA-10 Test and Prediction Techniques for High-Speed Flows 4-Jan 1400 hrs 1730 hrs America’s Cup D 119-APA-11 Special Session: Space Launch System (SLS) Induced Environments I 5-Jan 0900 hrs 1230 hrs Coronado D 120-APA-12 Applied CFD & Numerical Correlations with Experimental Data I 5-Jan 0900 hrs 1230 hrs America’s Cup B 121-APA-13 Aerodynamic Design: Analysis, Methodologies, and Optimization 5-Jan 0900 hrs 1230 hrs America’s Cup C Techniques II 122-APA-14 Special Session: CREATE-AV HPC Multiphysics Applications of Full- 5-Jan 0900 hrs 1230 hrs Coronado E Up Air Vehicles I 123-APA-15 Flow Control Applications & Demonstrations I 5-Jan 0900 hrs 1230 hrs America’s Cup D 173-APA-16 Special Session: Space Launch System (SLS) Induced Environments II 5-Jan 1400 hrs 1730 hrs Coronado D 174-APA-17 Applied CFD & Numerical Correlations with Experimental Data II 5-Jan 1400 hrs 1730 hrs America’s Cup B 175-APA-18 Aerodynamic Design: Analysis, Methodologies, and Optimization 5-Jan 1400 hrs 1730 hrs America’s Cup C Techniques III 176-APA-20 Propeller/Rotorcraft/Wind Turbine Aerodynamics I 5-Jan 1400 hrs 1730 hrs Americas’ Cup D 228-APA-22 Special Session: CREATE-AV HPC Multiphysics Applications of Full- 6-Jan 0900 hrs 1230 hrs Coronado E Up Air Vehicles II

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Abbreviation Title Date Start Time End Time Location Applied Aerodynamics (continued) 229-APA-23/FD-27 Special Session: NASA’s Revolutionary Computational Aerosciences I 6-Jan 0900 hrs 1230 hrs Coronado D 230-APA-24 Low Speed, Low Reynolds Number Aerodynamics 6-Jan 0900 hrs 1230 hrs America’s Cup B 231-APA-25 Aerodynamic Testing: Wind-Tunnel I 6-Jan 0900 hrs 1230 hrs America’s Cup C 232-APA-26 Unsteady Aerodynamics I 6-Jan 0900 hrs 1230 hrs America’s Cup D 277-APA-27 Special Session: Aerodynamic Design Optimization Benchmark 6-Jan 1400 hrs 1730 hrs Coronado D Problems I 278-APA-28 Special Session: CREATE-AV HPC Multiphysics Applications of Full- 6-Jan 1400 hrs 1730 hrs Coronado E Up Air Vehicles III 279-APA-29 Flow Control Applications & Demonstrations II 6-Jan 1400 hrs 1730 hrs America’s Cup C 280-APA-30 Unsteady Aerodynamics II 6-Jan 1400 hrs 1730 hrs America’s Cup D 330-APA-32 Special Session: Aerodynamic Design Optimization Benchmark 7-Jan 0900 hrs 1230 hrs Coronado D Problems II 331-APA-33 Applied CFD & Numerical Correlations with Experimental Data III 7-Jan 0900 hrs 1230 hrs America’s Cup D 332-APA-34 Aerodynamic-Structural Dynamics Interactions I 7-Jan 0900 hrs 1230 hrs America’s Cup B 333-APA-35/FD-41 Special Session: NASA’s Revolutionary Computational Aerosciences II 7-Jan 0900 hrs 1230 hrs Coronado E 334-APA-36 Airfoil/Wing/Configuration Aerodynamics I 7-Jan 0900 hrs 1230 hrs America’s Cup C 378-APA-37 Special Session: Sea-Based Aviation Aeromechanics Computational 7-Jan 1400 hrs 1730 hrs Coronado E Analysis 379-APA-38 Aerodynamic Testing: Wind-Tunnel II 7-Jan 1400 hrs 1730 hrs America’s Cup B 380-APA-39 Airfoil/Wing/Configuration Aerodynamics II 7-Jan 1400 hrs 1730 hrs America’s Cup C 381-APA-40 Propeller/Rotorcraft/Wind Turbine Aerodynamics II 7-Jan 1400 hrs 1730 hrs America’s Cup D 432-APA-41 Applied CFD & Numerical Correlations with Experimental Data IV 8-Jan 0900 hrs 1230 hrs America’s Cup D 433-APA-42 Aerodynamic-Structural Dynamics Interactions II 8-Jan 0900 hrs 1230 hrs Coronado D 434-APA-43 Lowspeed Flow Environment and UAV Integration 8-Jan 0900 hrs 1230 hrs America’s Cup C 435-APA-44 Special Session: Low Boom Activities 8-Jan 0900 hrs 1230 hrs Coronado E 436-APA-45 Airfoil/Wing/Configuration Aerodynamics III 8-Jan 0900 hrs 1230 hrs America’s Cup B Adaptive Structures 68-ASC-1 EU FP7 CHANGE (Special Session) 4-Jan 1400 hrs 1730 hrs Gaslamp D 177-ASC-2 Modeling and Analysis 5-Jan 1400 hrs 1730 hrs Gaslamp D 233-ASC-3 Design and Testing 6-Jan 0900 hrs 1230 hrs Gaslamp D 281-ASC-4 Wing Leading and Morphing 6-Jan 1400 hrs 1730 hrs Gaslamp D 335-ASC-5 Shape Memory Alloys 7-Jan 0900 hrs 1230 hrs Gaslamp D 382-ASC-6 Health Monitoring 7-Jan 1400 hrs 1730 hrs Gaslamp D Computer Systems 124-CMS-1/CPS-1 Communication, Computing and Information Processing 5-Jan 0900 hrs 1230 hrs Regatta B Digital Avionics 437-DA-2 Avionics Technologies for Safe and Efficient Vehicle Operation in 8-Jan 0900 hrs 1230 hrs Regatta A National Airspace Design Engineering 125-DE-1 Design Processes and Tools 5-Jan 0900 hrs 1230 hrs Old Town A 178-DE-2 Innovative Designs in Aerospace / Design Education 5-Jan 1400 hrs 1730 hrs Old Town A

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Abbreviation Title Date Start Time End Time Location Dynamics Specialists 337-EDU-1 Advancing Aerospace Education I 7-Jan 0900 hrs 1230 hrs Bankers Hill 235-DSC-2 Adaptive Aeroelastic Wing Shaping Control 6-Jan 0900 hrs 1230 hrs Gaslamp C 282-DSC-3 High Speed Systems 6-Jan 1400 hrs 1730 hrs Gaslamp C 336-DSC-4 Aircraft Loads Prediction - Special Session 7-Jan 0900 hrs 1230 hrs Gaslamp C 383-DSC-5 Nonlinear Aeroelasticity 7-Jan 1400 hrs 1730 hrs Gaslamp C 438-DSC-6 Aeroelasticity 8-Jan 0900 hrs 1230 hrs Balboa C Education 337-EDU-1 Advancing Aerospace Education I 7-Jan 0900 hrs 1230 hrs Bankers Hill 384-EDU-2 Advancing Aerospace Education II 7-Jan 1400 hrs 1730 hrs Bankers Hill Fluid Dynamics 14-FD-1/APA-5 Special Session: Low Re & Bio-Inspired Flows Discussion Group (Invited) 4-Jan 0900 hrs 1230 hrs Harbor E 15-FD-2 Acoustics and Compressible Flow Transition 4-Jan 0900 hrs 1230 hrs Promenade B 16-FD-3 Aerodynamic Flow Control 4-Jan 0900 hrs 1230 hrs Cove 17-FD-4 CFD Applications and Design 4-Jan 0900 hrs 1230 hrs Pier 18-FD-5 CFD: Time Integration and Preconditioning 4-Jan 0900 hrs 1230 hrs Promenade A 19-FD-6 Shock Boundary Layer Interaction I 4-Jan 0900 hrs 1230 hrs Harbor F 69-FD-8 Airfoil Flow Control 4-Jan 1400 hrs 1730 hrs Cove 70-FD-9 CFD Simulation of Vortex Flows 4-Jan 1400 hrs 1730 hrs Pier 126-FD-10 CFD: Turbulence Modeling 5-Jan 0900 hrs 1230 hrs Promenade A 71-FD-11 Compressible Boundary Layers 4-Jan 1400 hrs 1730 hrs Harbor D 72-FD-12 DNS/LES Techniques 4-Jan 1400 hrs 1730 hrs Harbor E 73-FD-13 Jet Flows I 4-Jan 1400 hrs 1730 hrs Promenade B 74-FD-14 Shock Boundary Layer Interaction II 4-Jan 1400 hrs 1730 hrs Harbor F 127-FD-15 Aqueous Flow Control and Flow Control Experiments 5-Jan 0900 hrs 1230 hrs Cove 128-FD-16 Boundary-Layer Transition 5-Jan 0900 hrs 1230 hrs Promenade B 129-FD-17 CFD: Cartesian and Mapped Grids 5-Jan 0900 hrs 1230 hrs Pier 130-FD-18 RANS/LES and Its Applications 5-Jan 0900 hrs 1230 hrs Harbor E 131-FD-19 Shock Boundary Layer Interaction III 5-Jan 0900 hrs 1230 hrs Harbor F 75-FD-20 Stability and Transition of Hypersonic Flows I 4-Jan 1400 hrs 1730 hrs Promenade A 179-FD-21 Bio-Inspired Flows 5-Jan 1400 hrs 1730 hrs Promenade B 180-FD-22 CFD: Error Estimation and Mesh Adaptation 5-Jan 1400 hrs 1730 hrs Pier 181-FD-23/PDL-6 DBD Plasma Actuators II 5-Jan 1400 hrs 1730 hrs Harbor F 182-FD-24 Stability and Transition of Hypersonic Flows II 5-Jan 1400 hrs 1730 hrs Promenade A 183-FD-25 Wing Aerodynamics 5-Jan 1400 hrs 1730 hrs Cove 184-FD-26/APA-21 Special Session: Evaluation of RANS Solvers on Benchmark 5-Jan 1400 hrs 1730 hrs Harbor E Aerodynamic Flows I 236-FD-28 CFD: Higher-Order Methods I 6-Jan 0900 hrs 1230 hrs Pier 237-FD-29 Flow Control Methods and Simulations 6-Jan 0900 hrs 1230 hrs Cove 238-FD-30 Jet Flows II 6-Jan 0900 hrs 1230 hrs Promenade B 239-FD-31 RANS/LES Methods and Techniques I 6-Jan 0900 hrs 1230 hrs Harbor E 240-FD-32 Subsonic Boundary Layers 6-Jan 0900 hrs 1230 hrs Harbor F

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Abbreviation Title Date Start Time End Time Location Fluid Dynamics (continued) 241-FD-33 Surface Roughness & Disturbances in Supersonic Flow 6-Jan 0900 hrs 1230 hrs Promenade A 283-FD-34 CFD: Higher-Order Methods II 6-Jan 1400 hrs 1730 hrs Pier 284-FD-35 Discontinuous Galerkin Methods 6-Jan 1400 hrs 1730 hrs Harbor F 285-FD-36 Multiphase Flow I: Simulations and Models 6-Jan 1400 hrs 1730 hrs Promenade B 286-FD-37 Unsteady Vortex Flows 6-Jan 1400 hrs 1730 hrs Promenade A 287-FD-38 Unsteady Wing Aerodynamics 6-Jan 1400 hrs 1730 hrs Cove 288-FD-39/APA-31 Special Session: Evaluation of RANS Solvers on Benchmark 6-Jan 1400 hrs 1730 hrs Harbor E Aerodynamic Flows II 338-FD-42 CFD: Meshfree Methods and Non-Equilibrium Gas Dynamics 7-Jan 0900 hrs 1230 hrs Pier 339-FD-43 Experimental Investigations of High-Speed Flow 7-Jan 0900 hrs 1230 hrs Harbor F 340-FD-44 Multiphase Flow II: Liquid-Gas and Engines 7-Jan 0900 hrs 1230 hrs Promenade B 341-FD-45 RANS/LES Methods and Techniques II 7-Jan 0900 hrs 1230 hrs Harbor E 342-FD-46 Vortex Flows I 7-Jan 0900 hrs 1230 hrs Promenade A 385-FD-47 CFD: Multiphase and Multi-Species Flows 7-Jan 1400 hrs 1730 hrs Pier 386-FD-48 Exploiting Hardware and Software Advances in CFD 7-Jan 1400 hrs 1730 hrs Cove 387-FD-49 Flow-Control Actuators 7-Jan 1400 hrs 1730 hrs Cortez Hill C 388-FD-50 Flux Reconstruction/Correction Procedure via Reconstruction (FR/CPR) 7-Jan 1400 hrs 1730 hrs Harbor F 389-FD-51 RANS/LES of Separated Flows 7-Jan 1400 hrs 1730 hrs Harbor E 390-FD-52 Reacting Flows 7-Jan 1400 hrs 1730 hrs Promenade B 391-FD-53 Vortex Flows II: Experimental Investigations 7-Jan 1400 hrs 1730 hrs Promenade A 439-FD-54 CFD: Overset Methods 8-Jan 0900 hrs 1230 hrs Pier 440-FD-55 High-Speed Flow Methods & Simulations 8-Jan 0900 hrs 1230 hrs Harbor E 441-FD-56 Incompressible Flow Transition 8-Jan 0900 hrs 1230 hrs Harbor F 442-FD-57 Pitching/Heaving/Flapping Surfaces 8-Jan 0900 hrs 1230 hrs Cove 443-FD-58 Separated Fluid Flows 8-Jan 0900 hrs 1230 hrs Promenade B 444-FD-59 Vortex Flows III: Dynamical Systems Methods 8-Jan 0900 hrs 1230 hrs Promenade A 321-FD-60 Transition Open Forum 6-Jan 1830 hrs 2200 hrs Old Town B Green Engineering 185-GEPC-3 Noise Reduction and Flight Demonstrations 5-Jan 1400 hrs 1730 hrs America’s Cup A 289-GEPC-4 Alternative Fuels and Green Engineering Computations 6-Jan 1400 hrs 1730 hrs America’s Cup B Guidance, Navigation, and Control 20-GNC-1 Vehicle & Flight Control Validation 4-Jan 0900 hrs 1230 hrs Hillcrest A 21-GNC-2 Spacecraft Attitude Control I 4-Jan 0900 hrs 1230 hrs Hillcrest B 22-GNC-3 Invited Session: LOC-1, Onboard Systems for LOC Prevention and 4-Jan 0900 hrs 1230 hrs Coronado B Recovery – Problem Analysis and Upset Prevention Methods 23-GNC-4 Invited Session: EDL-1, Entry, Descent and Landing GN&C Technology I 4-Jan 0900 hrs 1230 hrs Coronado A 24-GNC-5 Aerospace Robotics and Unmanned/Autonomous Systems I 4-Jan 0900 hrs 1230 hrs Hillcrest C 76-GNC-6 Control Theory and Applications 4-Jan 1400 hrs 1730 hrs Hillcrest A 77-GNC-7 Spacecraft Attitude Control II 4-Jan 1400 hrs 1730 hrs Hillcrest B 78-GNC-8 Invited Session: LOC-2, Onboard Systems for LOC Prevention and Recovery 4-Jan 1400 hrs 1730 hrs Coronado B – Real-Time Failure Detection, Isolation, and Redundancy Management

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Abbreviation Title Date Start Time End Time Location Guidance, Navigation, and Control (continued) 79-GNC-9 Invited Session: EDL-2, Entry, Descent and Landing GN&C Technology II 4-Jan 1400 hrs 1730 hrs Coronado A 80-GNC-10 Aerospace Robotics and Unmanned/Autonomous Systems II 4-Jan 1400 hrs 1730 hrs Hillcrest C 132-GNC-11 Adaptive Control 5-Jan 0900 hrs 1230 hrs Hillcrest A 133-GNC-12 Spacecraft Parameter Estimation and Modeling 5-Jan 0900 hrs 1230 hrs Hillcrest B 134-GNC-13 Invited Session: LOC-3, Onboard Systems for LOC Prevention and 5-Jan 0900 hrs 1230 hrs Coronado B Recovery – Resilient Flight Control and Guidance Systems 135-GNC-14 Aerospace Robotics and Unmanned/Autonomous Systems III 5-Jan 0900 hrs 1230 hrs Hillcrest C 136-GNC-15 Planning and Control for Mini/Micro UAVs 5-Jan 0900 hrs 1230 hrs Hillcrest D 186-GNC-16 Optimal Control: Methods and Applications 5-Jan 1400 hrs 1730 hrs Hillcrest A 187-GNC-17 Spacecraft Formations and Rendezvous 5-Jan 1400 hrs 1730 hrs Hillcrest B 188-GNC-18 Invited Session: LOC-4, Onboard Systems for LOC Prevention and 5-Jan 1400 hrs 1730 hrs Coronado B Recovery – Upset Recovery and System Validation 189-GNC-19 Aerospace Robotics and Unmanned/Autonomous Systems IV 5-Jan 1400 hrs 1730 hrs Hillcrest C 190-GNC-20 Control of Bio-Inspired Mini/Micro UAVs 5-Jan 1400 hrs 1730 hrs Hillcrest D 242-GNC-21 Spacecraft De-Orbiting, Reentry and Landing 6-Jan 0900 hrs 1230 hrs Hillcrest B 243-GNC-22 GN&C Sensor Systems 6-Jan 0900 hrs 1230 hrs Hillcrest A 244-GNC-23 Aerospace Robotics and Unmanned/Autonomous Systems V 6-Jan 0900 hrs 1230 hrs Hillcrest C 290-GNC-24 Spacecraft Trajectory Optimization and Orbit Control 6-Jan 1400 hrs 1730 hrs Hillcrest B 291-GNC-25 Invited Session: Advances in Guidance and Control of Unmanned Air 6-Jan 1400 hrs 1730 hrs Hillcrest A Vehicles 292-GNC-26 H Infinity, Nonlinear, and Adaptive Flight Control 6-Jan 1400 hrs 1730 hrs Hillcrest C 293-GNC-27 Control of Multirotor Aircraft 6-Jan 1400 hrs 1730 hrs Cortez Hill B 343-GNC-28 Invited Session: Interval Management: Operational Concept, Integration, 7-Jan 0900 hrs 1230 hrs Coronado B and Benefits 344-GNC-29 Novel Navigation, Estimation and Tracking I 7-Jan 0900 hrs 1230 hrs Hillcrest A 345-GNC-30/ACD-10 Aircraft GNC I 7-Jan 0900 hrs 1230 hrs Hillcrest C 346-GNC-31 GNC Concepts in Air Traffic Control 7-Jan 0900 hrs 1230 hrs Cortez Hill B 392-GNC-32 Invited Session: Interval Management: Avionics Algorithms and 7-Jan 1400 hrs 1730 hrs Coronado B Performance Analysis 393-GNC-33 Novel Navigation, Estimation and Tracking II 7-Jan 1400 hrs 1730 hrs Hillcrest A 394-GNC-34/ACD-12 Aircraft GNC II 7-Jan 1400 hrs 1730 hrs Hillcrest C 395-GNC-35 Trajectory Design 7-Jan 1400 hrs 1730 hrs Cortez Hill B 396-GNC-36 Missile and Integrated Guidance & Control 7-Jan 1400 hrs 1730 hrs Hillcrest B 445-GNC-37 Invited Session: Flight Experience of Cassini Spacecraft Attitude Control 8-Jan 0900 hrs 1230 hrs Coronado B at Saturn 446-GNC-38 Vision-Based Sensing and Optical Navigation 8-Jan 0900 hrs 1230 hrs Hillcrest A 447-GNC-39 Flight Control of Unmanned Vehicles 8-Jan 0900 hrs 1230 hrs Hillcrest C 448-GNC-40 Intelligent and Cooperative Control in Aerospace Applications 8-Jan 0900 hrs 1230 hrs Cortez Hill B 449-GNC-41 Missile and Entry Vehicle Guidance 8-Jan 0900 hrs 1230 hrs Hillcrest B

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Abbreviation Title Date Start Time End Time Location Ground Testing 25-GT-1 SAMURAI - Testing and Simulation of Real Engine Flows I (Invited) 4-Jan 0900 hrs 1230 hrs Harbor I 81-GT-2 SAMURAI - Testing and Simulation of Real Engine Flows II (Invited) 4-Jan 1400 hrs 1730 hrs Hillcrest D 137-GT-3 High Reynolds Number Aerodynamics and Testing (Invited) 5-Jan 0900 hrs 1230 hrs Harbor B 191-GT-4 Integration of Experimental and Computational Methods (Invited) 5-Jan 1400 hrs 1730 hrs Harbor H 245-GT-5 Ground Test Studies and Techniques 6-Jan 0900 hrs 1230 hrs Cortez Hill B 347-GT-7 Aerodynamic Force Measurement and NFMTC Update (Invited) 7-Jan 0900 hrs 1230 hrs Cove 397-GT-8 Model Attitude, Deformation, and Data Acquisition Techniques (Invited) 7-Jan 1400 hrs 1730 hrs Hillcrest D 450-GT-9 Ground Test Methodologies and CFD Integration 8-Jan 0900 hrs 1230 hrs Hillcrest D Gas Turbine Engines 26-GTE-1 Turbine Technologies 4-Jan 0900 hrs 1230 hrs Gaslamp D 27-GTE-2 Cycles and Auxiliary Systems 4-Jan 0900 hrs 1230 hrs Harbor H 82-GTE-3 Compression Systems I 4-Jan 1400 hrs 1730 hrs Gaslamp C 138-GTE-4 Compression Systems II 5-Jan 0900 hrs 1230 hrs Cortez Hill C 139-GTE-5 Turbine Cooling I 5-Jan 0900 hrs 1230 hrs Gaslamp D 192-GTE-6 Gas Turbine Engine with Pressure Gain Combustion 5-Jan 1400 hrs 1730 hrs Harbor C 193-GTE-7 Turbine Cooling II 5-Jan 1400 hrs 1730 hrs Harbor B 246-GTE-8 Combustion I 6-Jan 0900 hrs 1230 hrs Cortez Hill C 294-GTE-10 Combustion II 6-Jan 1400 hrs 1730 hrs Cortez Hill C 348-GTE-11 Jet Noise 7-Jan 0900 hrs 1230 hrs Cortez Hill C 349-GTE-12 Methodologies for Advanced Components 7-Jan 0900 hrs 1230 hrs Golden Hill A 398-GTE-13 Noise 7-Jan 1400 hrs 1730 hrs Old Town A 399-GTE-14 Experimental Tools 7-Jan 1400 hrs 1730 hrs Old Town B 451-GTE-15 Combustion III 8-Jan 0900 hrs 1230 hrs Gaslamp B 452-GTE-16 Numerical Tools 8-Jan 0900 hrs 1230 hrs Old Town A History 140-HIS-1 Aerospace Archives: All is not Lost - Keepers of the Right Stuff 5-Jan 0900 hrs 1230 hrs America’s Cup A 247-HIS-2 Aerospace History 6-Jan 0900 hrs 1230 hrs America’s Cup A 295-HIS-3 Boeing Centennial 1916-2016 I 6-Jan 1400 hrs 1730 hrs America’s Cup A 350-HIS-4 Boeing Centennial 1916-2016 II 7-Jan 0900 hrs 1230 hrs America’s Cup A 400-HIS-5 History of AIAA 7-Jan 1400 hrs 1730 hrs America’s Cup A High Speed Air Breathing Propulsion 28-HSABP-1 Advances in Pressure Gain Combustion I - RDE & PDE 4-Jan 0900 hrs 1230 hrs Harbor B 141-HSABP-2 Scramjet Combustors 5-Jan 0900 hrs 1230 hrs Regatta A 194-HSABP-3 Scramjet Performance and Optimization 5-Jan 1400 hrs 1730 hrs Regatta A 248-HSABP-4 Scramjet Inlets 6-Jan 0900 hrs 1230 hrs Regatta A 296-HSABP-5 Advances in Pressure Gain Combustion II - RDE & PDE 6-Jan 1400 hrs 1730 hrs Regatta A 351-HSABP-6 Advances in Pressure Gain Combustion III - RDE, PDE, & Pulse Combustion 7-Jan 0900 hrs 1230 hrs Regatta A 402-HSABP-7 Computational Analysis of Scramjets 7-Jan 1400 hrs 1730 hrs Regatta A Information and Command & Control Systems 195-ICC-2 Information and Command and Control Systems 5-Jan 1400 hrs 1730 hrs Regatta B

www.aiaa-SciTech.org 52 #aiaaSciTech ISessions at a Glance

Abbreviation Title Date Start Time End Time Location Intelligent Systems 29-IS-1/ICC-1/ Student Paper Competition -- Information Systems Group 4-Jan 0900 hrs 1230 hrs Regatta B DA-1 83-IS-2 Intelligent and Adaptive Aerospace Control 4-Jan 1400 hrs 1730 hrs Regatta B 142-IS-3 Big Data Analytics 5-Jan 0900 hrs 1100 hrs Coronado A 165-IS-4 Intelligent Systems Autonomy Roadmap Panel 5-Jan 1100 hrs 1230 hrs Coronado A 196-IS-5 Novel Aerospace Applications of Intelligent Systems 5-Jan 1400 hrs 1730 hrs Regatta C 297-IS-7 Machine Learning and Probabilistic Reasoning for Intelligent UAS 6-Jan 1400 hrs 1730 hrs Regatta B 352-IS-9 Intelligent Human-Automation Interaction 7-Jan 0900 hrs 1230 hrs Regatta B 403-IS-11 Intelligent Mission Design and Vehicle Control 7-Jan 1400 hrs 1730 hrs Regatta B 453-IS-13 Intelligent Integrated Systems Health Management 8-Jan 0900 hrs 1230 hrs Regatta B International Student Conference 30-ISC-1 International Student Conference - Undergraduate Category 4-Jan 0900 hrs 1230 hrs Torrey Hills A 31-ISC-2 International Student Conference - Masters Category 4-Jan 0900 hrs 1230 hrs Torrey Hills B 84-ISC-3 International Student Conference -Team Category 4-Jan 1400 hrs 1730 hrs Torrey Hills B 85-ISC-4 ISC-Community Outreach Category 4-Jan 1400 hrs 1530 hrs Torrey Hills A Materials 33-MAT-1 Nanostructured Materials I 4-Jan 0900 hrs 1230 hrs Gaslamp B 34-MAT-2 Fatigue & Fracture I 4-Jan 0900 hrs 1230 hrs Gaslamp C 87-MAT-3 Materials Testing & Characterization I 4-Jan 1400 hrs 1730 hrs Gaslamp B 144-MAT-4 Materials Testing & Characterization II 5-Jan 0900 hrs 1230 hrs Gaslamp B 198-MAT-5 Fatigue & Fracture II 5-Jan 1400 hrs 1730 hrs Gaslamp B 199-MAT-6 Nanostructured Materials II 5-Jan 1400 hrs 1730 hrs Gaslamp C 249-MAT-7 Integrated Computational Materials Engineering (ICME) 6-Jan 0900 hrs 1230 hrs Gaslamp B 298-MAT-8 Advanced Materials and Processing 6-Jan 1400 hrs 1730 hrs Gaslamp B 353-MAT-9 Materials & Design for Additive Manufacturing 7-Jan 0900 hrs 1230 hrs Gaslamp B 409-MAT-10 Work Force Development for Integrated Computational Materials 7-Jan 1400 hrs 1700 hrs Gaslamp B Engineering Multidisciplinary Design Optimization 35-MDO-1 Aero & Structural Technology Investigations 4-Jan 0900 hrs 1230 hrs Balboa A 88-MDO-2 Design Space Exploration 4-Jan 1400 hrs 1730 hrs Balboa A 145-MDO-3 Propulsion & Thermal Design Considerations 5-Jan 0900 hrs 1230 hrs Balboa A 200-MDO-4 Topology Methods and Applications 5-Jan 1400 hrs 1730 hrs Balboa A 250-MDO-5 Aeroelastic Sensitivity Analysis & Applications 6-Jan 0900 hrs 1230 hrs Balboa A 299-MDO-6 Design Including Uncertainty & Frameworks 6-Jan 1400 hrs 1730 hrs Balboa A 354-MDO-7 Mission Driven Design 7-Jan 0900 hrs 1230 hrs Balboa A 404-MDO-8 Sensitivity Derivations & Optimization Applications 7-Jan 1400 hrs 1730 hrs Balboa A

www.aiaa-SciTech.org 53 #aiaaSciTech ISessions at a Glance

Abbreviation Title Date Start Time End Time Location Modeling and Simulation Technologies 36-MST-1 Modeling and Simulation of Air Traffic Management I 4-Jan 0900 hrs 1230 hrs Golden Hill A 37-MST-2 Special Topics in Modeling and Simulation 4-Jan 0900 hrs 1230 hrs Hillcrest D 89-MST-3 Modeling and Simulation of Air Traffic Management II 4-Jan 1400 hrs 1730 hrs Golden Hill A 146-MST-4 Modeling of Space Systems and Dynamics 5-Jan 0900 hrs 1230 hrs Golden Hill A 201-MST-5 Uninhabited Aerial Systems and Vehicle Dynamics 5-Jan 1400 hrs 1730 hrs Golden Hill A 251-MST-6 Human Factors, Perception, and Cueing 6-Jan 0900 hrs 1230 hrs Golden Hill A 252-MST-7 Modeling of Vehicle Dynamics, Systems, and Environments 6-Jan 0900 hrs 1230 hrs Golden Hill B 300-MST-8 Hardware-in-the-Loop Simulation 6-Jan 1400 hrs 1730 hrs Golden Hill A 301-MST-9 Invited Session: LOC-6, Simulation-Based Evaluations for Improved 6-Jan 1400 hrs 1730 hrs Coronado B Pilot Insights and Training for LOC Prevention and Recovery 302-MST-10 Motion Systems, Visual Systems, and Image Generation 6-Jan 1400 hrs 1730 hrs Golden Hill B 355-MST-11 Model Design and Development 7-Jan 0900 hrs 1230 hrs Golden Hill B 405-MST-12 Computational Methods I 7-Jan 1400 hrs 1730 hrs Golden Hill B 406-MST-13 Model and Simulation Verification and Validation 7-Jan 1400 hrs 1730 hrs Golden Hill A 454-MST-14 Rotorcraft Modeling and Simulation Technologies 8-Jan 0900 hrs 1230 hrs Golden Hill A 455-MST-15 Computational Methods II 8-Jan 0900 hrs 1230 hrs Golden Hill B Meshing, Visualization, and Computational Environments 356-MVC-1 Grid Generation 7-Jan 0900 hrs 1230 hrs Nautical 407-MVC-2 Geometry & Computational Environments 7-Jan 1400 hrs 1730 hrs Nautical Non-Deterministic Approaches 90-NDA-1 Surrogate Modeling Approaches for Uncertainty Quantification and 4-Jan 1400 hrs 1730 hrs Old Town B Reliability Estimation 147-NDA-2 Analysis and Optimization Under Uncertainty 5-Jan 0900 hrs 1230 hrs Old Town B 202-NDA-3 Testing in Support of Model Calibration or Uncertainty Quantification 5-Jan 1400 hrs 1730 hrs Old Town B 253-NDA-4 Model Calibration, Verification, Validation, Uncertainty 6-Jan 0900 hrs 1230 hrs Old Town B Quantification 303-NDA-5 Non-Deterministic Methods 6-Jan 1400 hrs 1730 hrs Old Town B 357-NDA-6 Reliability and Life Prediction 7-Jan 0900 hrs 1230 hrs Old Town B Propellants and Combustion 39-PC-1 Combustion Chemistry 4-Jan 0900 hrs 1230 hrs Harbor C 40-PC-2 Advanced Concepts, Combustion Diagnostics, Environmental Impact 4-Jan 0900 hrs 1230 hrs Cortez Hill C 92-PC-3 Combustion Diagnostics 4-Jan 1400 hrs 1730 hrs Harbor B 93-PC-4 Detonations, Explosions, and Supersonic Combustion 4-Jan 1400 hrs 1730 hrs Harbor C 94-PC-5 High-Pressure Combustion, Fuel Technology 4-Jan 1400 hrs 1730 hrs Cortez Hill C 149-PC-6 Heterogeneous Propellants and Combustion, Fuel Technology 5-Jan 0900 hrs 1230 hrs Harbor C 204-PC-8 Micro-Propulsion, Plasma Discharges, Autoignition 5-Jan 1400 hrs 1730 hrs Cortez Hill C 255-PC-9/GTE-9 Rotating-Detonation Engines 6-Jan 0900 hrs 1230 hrs Harbor B 256-PC-10 Laminar Flames 6-Jan 0900 hrs 1230 hrs Harbor C 305-PC-12 Spray and Droplet Combustion I 6-Jan 1400 hrs 1730 hrs Harbor B 306-PC-13 Turbulent Combustion I - Experiments 6-Jan 1400 hrs 1730 hrs Harbor C 359-PC-14 Spray and Droplet Combustion II 7-Jan 0900 hrs 1230 hrs Harbor B 360-PC-15 Turbulent Combustion II - Fuel Chemistry 7-Jan 0900 hrs 1230 hrs Harbor C

www.aiaa-SciTech.org 54 #aiaaSciTech ISessions at a Glance

Abbreviation Title Date Start Time End Time Location Propellants and Combustion (continued) 410-PC-16 Rocket & Air-Breathing Combustion I - Combustion Instabilities, 7-Jan 1400 hrs 1730 hrs Harbor B Supercritical Conditions 411-PC-17 Turbulent Combustion III - Large-Eddy Simulations 7-Jan 1400 hrs 1730 hrs Harbor C 457-PC-18 Rocket & Air-Breathing Combustion II 8-Jan 0900 hrs 1230 hrs Harbor B 458-PC-19 Turbulent Combustion IV 8-Jan 0900 hrs 1230 hrs Harbor C Plasmadynamics and Lasers 41-PDL-1 Plasma Assisted Combustion 4-Jan 0900 hrs 1230 hrs Harbor D 42-PDL-2 DBD Plasma Actuators I 4-Jan 0900 hrs 1230 hrs Ocean Beach 95-PDL-3 Plasma Based Flow Control 4-Jan 1400 hrs 1730 hrs Ocean Beach 96-PDL-4 Laser Discharge and Applications 4-Jan 1400 hrs 1730 hrs Cortez Hill A 150-PDL-5/PC-7/ Special Walter Lempert Memorial Session I (Invited) 5-Jan 0900 hrs 1230 hrs Harbor D AMT-3 257-PDL-7 ns-DBD Plasma Actuator 6-Jan 0900 hrs 1230 hrs Ocean Beach 307-PDL-9/FD-40 Experimental and Numerical Studies of Large Eddy Structures 6-Jan 1400 hrs 1730 hrs Ocean Beach 361-PDL-10 Novel Plasma Actuators, Concepts and Systems 7-Jan 0900 hrs 1230 hrs Old Town A 362-PDL-11 Plasma Diagnostics 7-Jan 0900 hrs 1230 hrs Ocean Beach 412-PDL-12 Plasma Propulsion 7-Jan 1400 hrs 1730 hrs Ocean Beach 459-PDL-13 Numerical Modeling of Plasmas 8-Jan 0900 hrs 1230 hrs Ocean Beach Society and Aerospace Technology 401-SAT-1 Society and Aerospace Technology 7-Jan 1400 hrs 1730 hrs America’s Cup A Small Satellites 151-SATS-1 Small Satellites - Technologies I 5-Jan 0900 hrs 1230 hrs Ocean Beach 205-SATS-2 Small Satellites - Technologies II 5-Jan 1400 hrs 1730 hrs Ocean Beach 308-SATS-3 Small Satellites - Missions 6-Jan 1400 hrs 1730 hrs Hillcrest D Spacecraft Structures 152-SCS-1 Spacecraft Antennas and Apertures 5-Jan 0900 hrs 1230 hrs Balboa B 206-SCS-2 High-Strain Composite Materials and Structures 5-Jan 1400 hrs 1730 hrs Balboa B 258-SCS-3 Spacecraft Membranes, Booms, and Trusses I 6-Jan 0900 hrs 1230 hrs Balboa B 309-SCS-4 Spacecraft Membranes, Booms, and Trusses II 6-Jan 1400 hrs 1730 hrs Balboa B 363-SCS-5 Spacecraft Solar Array Structures I 7-Jan 0900 hrs 1230 hrs Balboa B 413-SCS-6 Spacecraft Solar Array Structures II 7-Jan 1400 hrs 1730 hrs Balboa B 460-SCS-7 Packaging and Deployment of Spacecraft Structures 8-Jan 0900 hrs 1230 hrs Balboa B Structural Dynamics 43-SD-1 Structural Dynamic Modeling and Analysis 4-Jan 0900 hrs 1230 hrs Balboa C 44-SD-2 Energy Harvesting 4-Jan 0900 hrs 1230 hrs Gaslamp A 97-SD-3 Reduced Order Modeling I 4-Jan 1400 hrs 1730 hrs Balboa C 98-SD-4 Dynamic Loads, Response, and Vibration I 4-Jan 1400 hrs 1730 hrs Gaslamp A 153-SD-5 Turbomachinery / Structural Health Monitoring 5-Jan 0900 hrs 1230 hrs Balboa C 154-SD-6 Dynamics, Feedback Control, and Aeroservoelasticity I 5-Jan 0900 hrs 1230 hrs Gaslamp A 259-SD-7 Dynamics, Feedback Control, and Aeroservoelasticity II 6-Jan 0900 hrs 1230 hrs Balboa C 310-SD-8 Passive Control and Damping 6-Jan 1400 hrs 1730 hrs Balboa C 311-SD-9 Gust Loads, Response, and Control 6-Jan 1400 hrs 1730 hrs Gaslamp A www.aiaa-SciTech.org 55 #aiaaSciTech ISessions at a Glance

Abbreviation Title Date Start Time End Time Location Structural Dynamics (continued) 364-SD-10 Reduced Order Modeling II 7-Jan 0900 hrs 1230 hrs Balboa C 414-SD-12 System ID 7-Jan 1400 hrs 1730 hrs Balboa C 415-SD-13 Flutter 7-Jan 1400 hrs 1730 hrs Gaslamp A 461-SD-14 Dynamic Loads, Response, and Vibration II 8-Jan 0900 hrs 1230 hrs Gaslamp A Systems Engineering 45-SE-1 Systems Engineering I 4-Jan 0900 hrs 1230 hrs America’s Cup B 99-SE-2 Systems Engineering II 4-Jan 1400 hrs 1730 hrs La Jolla B 207-SE-3 Systems Engineering III 5-Jan 1400 hrs 1730 hrs Balboa C Sensor Systems 260-SEN-1 Novel Sensor Systems and Sensing Techniques I 6-Jan 0900 hrs 1230 hrs Regatta C 312-SEN-2 Novel Sensor Systems and Sensing Techniques II 6-Jan 1400 hrs 1730 hrs Regatta C 365-SEN-3 Advanced Data Fusion Techniques 7-Jan 0900 hrs 1230 hrs Regatta C Space Exploration and Operations 46-SEO-1 Intelligent and Autonomous Systems for Improving Space Exploration 4-Jan 0900 hrs 1230 hrs America’s Cup A and Operations 100-SEO-2 Innovative Ideas for Exploring and Operating Space Missions 4-Jan 1400 hrs 1730 hrs America’s Cup A Software Systems 47-SOF-1 Software Architecture and Robust Software Engineering 4-Jan 0900 hrs 1030 hrs Regatta A 56-SOF-2 Lightweight Perfection: Why and How You Should Review Code for 4-Jan 1030 hrs 1230 hrs Regatta A Small Teams 101-SOF-3 Software Challenges in Aerospace Symposium 4-Jan 1400 hrs 1600 hrs Regatta A 261-SOF-5/UMS-5/ Assurance of Autonomy Symposium I 6-Jan 0900 hrs 1230 hrs Coronado A IS-6 313-SOF-6/UMS-7/ Assurance of Autonomy Symposium II 6-Jan 1400 hrs 1730 hrs Coronado A IS-8 366-SOF-7/UMS- Assurance of Autonomy Symposium III 7-Jan 0900 hrs 1200 hrs Coronado A 8/IS-10 416-SOF-8/UMS- Assurance of Autonomy Symposium IV 7-Jan 1400 hrs 1730 hrs Coronado A 9/IS-12 Space Resources Utilization 48-SRE-1 Extraterrestrial Water: Prospecting and Acquisition 4-Jan 0900 hrs 1230 hrs Bankers Hill 155-SRE-2 ISRU Technologies and Trades 5-Jan 0900 hrs 1230 hrs Bankers Hill Structures 49-STR-1 Aircraft Structural Design I 4-Jan 0900 hrs 1230 hrs La Jolla A 50-STR-2 Challenges in the Design of Joined 4-Jan 0900 hrs 1230 hrs La Jolla B 102-STR-3 Aircraft Structural Design II 4-Jan 1400 hrs 1730 hrs La Jolla A 156-STR-4 Special Session: USAF Benchmarking of Composite Fatigue Prediction 5-Jan 0900 hrs 1230 hrs La Jolla A Methods 157-STR-5 Failure Analysis and Prediction I 5-Jan 0900 hrs 1230 hrs La Jolla B 208-STR-6 Composite Fatigue Damage Prediction Methods 5-Jan 1400 hrs 1730 hrs La Jolla A 209-STR-7 Failure Analysis and Prediction II 5-Jan 1400 hrs 1730 hrs La Jolla B 262-STR-8 Design, Test and Analysis of Composite Structures I 6-Jan 0900 hrs 1230 hrs La Jolla A 263-STR-9 Other Topics in Structures 6-Jan 0900 hrs 1230 hrs La Jolla B www.aiaa-SciTech.org 56 #aiaaSciTech ISessions at a Glance

Abbreviation Title Date Start Time End Time Location Structures (continued) 314-STR-10 Design, Test and Analysis of Composite Structures II 6-Jan 1400 hrs 1730 hrs La Jolla A 315-STR-11 Structural Joints and Repairs 6-Jan 1400 hrs 1730 hrs La Jolla B 367-STR-12 Spacecraft Structural Design 7-Jan 0900 hrs 1230 hrs La Jolla A 368-STR-13 Buckling, Fatigue, and Fracture of Structures I 7-Jan 0900 hrs 1230 hrs La Jolla B 417-STR-14 Composite Laminate Optimization 7-Jan 1400 hrs 1730 hrs La Jolla A 418-STR-15 Buckling, Fatigue, and Fracture of Structures II 7-Jan 1400 hrs 1730 hrs La Jolla B 462-STR-16 Special Session: Stiffened, Stitched Composite Structures 8-Jan 0900 hrs 1230 hrs La Jolla A 463-STR-17 Impact Damage in Composites 8-Jan 0900 hrs 1230 hrs La Jolla B Survivability 264-SUR-1 Air and Space Survivability I 6-Jan 0900 hrs 1230 hrs Old Town A 316-SUR-2 Air and Space Survivability II 6-Jan 1400 hrs 1730 hrs Old Town A Terrestial Energy 51-TES-1 The State and Future of Energy Systems 4-Jan 0900 hrs 1230 hrs Old Town A 52-TES-2/TP-1 Joint Session: Heat Transfer in Terrestrial Energy Systems 4-Jan 0900 hrs 1230 hrs Old Town B 103-TES-3 Fluids and Combustion in Power Systems 4-Jan 1400 hrs 1730 hrs Old Town A 158-TES-4 Electrochemical Power for Aerospace Missions 5-Jan 0900 hrs 1230 hrs Gaslamp C 210-TES-5 Design of Energy Systems 5-Jan 1400 hrs 1730 hrs Gaslamp A Thermophysics 53-TP-2 Thermal Protection System, Ablation and Surface Catalysis I 4-Jan 0900 hrs 1230 hrs Harbor G 104-TP-3 Non-Equilibrium Flows, Non-Equilibrium Radiation and Rarefied 4-Jan 1400 hrs 1730 hrs Harbor G Flows I 105-TP-4 Heat Transfer: Conduction, Convection, Phase Change, Radiation, and 4-Jan 1400 hrs 1730 hrs Harbor H Conjugate Heat Transfer 159-TP-5 Aerothermodynamics I 5-Jan 0900 hrs 1230 hrs Harbor G 211-TP-6 Special Session: Aerothermodynamics of Meteor Entries 5-Jan 1400 hrs 1730 hrs Harbor G 265-TP-7 Aerothermodynamics II 6-Jan 0900 hrs 1230 hrs Harbor G 317-TP-8 Thermal Protection System, Ablation and Surface Catalysis II 6-Jan 1400 hrs 1730 hrs Harbor G 369-TP-9 Non-Equilibrium Flows, Non-Equilibrium Radiation and Rarefied 7-Jan 0900 hrs 1230 hrs Harbor G Flows II 419-TP-10 Experimental Measurements and Techniques in Heat Transfer and 7-Jan 1400 hrs 1730 hrs Harbor G Related Physical Phenomena 464-TP-11 Thermal Systems and Devices: Cryogenics, Thermal Management, and 8-Jan 0900 hrs 1230 hrs Harbor G Microdevices 465-TP-12 Special Session: University Space Systems Programs and Microgravity 8-Jan 0900 hrs 1230 hrs Harbor H Flight Activities

www.aiaa-SciTech.org 57 #aiaaSciTech SessionsI at a Glance

Abbreviation Title Date Start Time End Time Location Unmanned Systems 54-UMS-1 Unmanned Systems: Mission Management and Planning Technologies 4-Jan 0900 hrs 1230 hrs Regatta C 106-UMS-2 Unmanned Systems - Flight Dynamics and Control 4-Jan 1400 hrs 1730 hrs Regatta C 160-UMS-3 Unmanned Systems: Missions and Applications 5-Jan 0900 hrs 1230 hrs Regatta C 212-UMS-4 Unmanned Systems: UAS Integration into National Airspace System 5-Jan 1400 hrs 1730 hrs Coronado A and Civil Applications 266-UMS-6 Unmanned Systems: Novel Platforms and Controls 6-Jan 0900 hrs 1230 hrs Regatta B 420-UMS-10 Unmanned Systems: Detect-and-Avoid I 7-Jan 1400 hrs 1730 hrs Regatta C 466-UMS-11 Unmanned Systems: Detect-and-Avoid II 8-Jan 0900 hrs 1230 hrs Regatta C Wind Energy 107-WE-1 Wind Energy: Wind Turbine Aerodynamics Improvements and 4-Jan 1400 hrs 1730 hrs Harbor I Analysis 161-WE-2 Wind Energy: Wind Turbine Aerodynamics Modeling I 5-Jan 0900 hrs 1230 hrs Harbor H 162-WE-3 Wind Energy: Structural Dynamics and Materials 5-Jan 0900 hrs 1230 hrs Harbor I 213-WE-4 Wind Energy: Aero-Elastic Modeling and Validation 5-Jan 1400 hrs 1730 hrs Harbor I 267-WE-5 Wind Energy: Wind Turbine Aerodynamics Modeling II 6-Jan 0900 hrs 1230 hrs Harbor H 268-WE-6 Wind Energy: Rotor Design 6-Jan 0900 hrs 1230 hrs Harbor I 318-WE-7 Wind Energy: Wind Turbine Wakes 6-Jan 1400 hrs 1730 hrs Harbor I 370-WE-8 Wind Energy: VAWT Aerodynamics 7-Jan 0900 hrs 1230 hrs Harbor H 371-WE-9 Wind Energy: Wind Turbine and Wind Plant Control 7-Jan 0900 hrs 1230 hrs Harbor I 421-WE-10 Wind Energy: Wind Plant Aerodynamics and Atmospheric Inflow 7-Jan 1400 hrs 1730 hrs Harbor H 422-WE-11 Wind Energy: Offshore Wind Systems 7-Jan 1400 hrs 1730 hrs Harbor I 467-WE-12 Wind Energy: Wind Plant Optimization 8-Jan 0900 hrs 1230 hrs Harbor I

www.aiaa-SciTech.org 58 #aiaaSciTech Sunday Sunday, 3 January 2016 1-NW-1 Student Welcome Reception Seaport H 1800 - 1930 hrs All students and attendees welcome Monday Monday, 4 January 2016 2-NW-2 Monday Early Morning Networking Coffee Break Session Room Foyers 0700 - 0730 hrs Monday, 4 January 2016 3-SB-1 Monday Morning Speakers’ Briefing Session Rooms 0730 - 0800 hrs Monday, 4 January 2016 4-PLNRY-1 Monday Morning Plenary Panel Seaport A-E 0800 - 0900 hrs Aerospace S&T Policy in the 2016 Political Arena Moderator: Courtney Stadd, Management Advisor, Catalyst Partners, LLC

Panelists: Timothy Persons Daniel Goldin Jacques Gansler Carissa Christensen Mark Albrecht

Chief Scientist Chairman, President & CEO Founder, Chair and CEO Managing Partner Chairman of the Board U.S. Government Accountability Office Intellisis Corporation The Gansler Group The Tauri Group USSpace, LLC

Monday, 4 January 2016 5-AA-1 Aeroacoustics - Jet Noise I Nautical Chaired by: K. AHUJA, Georgia Institute of Technology and D. NARK, NASA Langley Research Center 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2016-0001 AIAA-2016-0002 AIAA-2016-0003 AIAA-2016-0004 AIAA-2016-0005 AIAA-2016-0006 Mean Velocity and Turbulence Numerical Investigation of Fluctuating Pressure Gradients in Extracting Near-Field Structures Scale-specific Intermittency and Including Finite Surface Span Measurements of Supersonic Jets Supersonic Jet Noise Suppression Heated Supersonic Jets Related to Noise Production in High Spatio-temporal Correlations in a Effects in Empirical Jet-Surface with Fluidic Inserts via Downstream Microjet Fluidic K. Lowe, Virginia Polytechnic Institute Speed Jets Supersonic Jet Interaction Noise Models R. Powers, S. Hromisin, D. McLaughlin, Injection and State University, Blacksburg, VA; C. P. Kan, J. Lewalle, M. Glauser, Syracuse U. Sasidharan Nair, L. Agostini, D. C. Brown, NASA Glenn Research Center, P. Morris, Pennsylvania State University, H. Pourhashem, NYU Polytechnic School Nelson, Innovative Technology Applications University, Syracuse, NY; S. Gogeneni, Gaitonde, Ohio State University, Columbus, Cleveland, OH University Park, PA of Engineering, Brooklyn, NY; I. Kalkhoran, Company, LLC, Chesterfield, MO Spectral Energies, LLC, Dayton, OH; B. OH NYU Tandon School of Engineering, Kiel, Air Force Research Laboratory, Wright- Brooklyn, NY Patterson AFB, OH Monday, 4 January 2016 6-ABPSI-1/GEPC-1 NASA ERA Systems Integration I Golden Hill B Chaired by: L. LEAVITT, N A S A and K. JAMES 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2016-0007 Oral Presentation AIAA-2016-0008 AIAA-2016-0009 AIAA-2016-0010 AIAA-2016-0011 AIAA-2016-0012 Overview Of ERA Integrated Summary of the Configuration Wind Tunnel Model Design and Overview of Low-speed Experimental Evaluation of Inlet Turbine Powered Simulator Phased Acoustic Array Technology Demonstration (ITD) 51A Development of the BWB-009H1 Fabrication of a 5.75% Scale Aerodynamic Tests on a 5.75% Distortion on an Ejector Powered Calibration and Testing for Hybrid Measurements of a 5.75% Hybrid Ultra-High Bypass (UHB) Integration Concept Vehicle for ERA Integrated Blended-Wing-Body Twin Jet Scale Blended-Wing-Body Twin Jet Hybrid Wing Body at Take-off and Wing Body Powered Airframe Wing body Aircraft (Invited) for Hybrid Wing Body (HWB) (Invited) Technology Demonstration (ITD) 51A Configuration (Invited) Configuration (Invited) Landing Conditions (Invited) Integration (Invited) N. Burnside, W. Horne, NASA Ames J. Flamm, NASA Langley Research Center, Ultra-High Bypass (UHB) Integration E. Dickey, N. Princen, J. Bonet, G. Ige, The D. Vicroy, NASA Langley Research Center, M. Carter, P. Shea, J. Flamm, NASA Langley K. Long, NASA Ames Research Center, Research Center, Moffett Field, CA; K. Hampton, VA; K. James, NASA Ames Research for Hybrid Wing Body (HWB) (Invited) Boeing Company, Huntington Beach, CA Hampton, VA; E. Dickey, N. Princen, M. Research Center, Hampton, VA; M. Schuh, K. Moffett Field, CA; P. Shea, J. Flamm, Elmer, R. Cheng, L. Brusniak, The Boeing Center, Moffett Field, CA; J. Bonet, The Boeing J. Bonet, N. Princen, The Boeing Company, Beyar, The Boeing Company, Huntington James, NASA Ames Research Center, Moffett NASA Langley Research Center, Hampton, Company, Huntington Beach, CA Company, Huntington Beach, CA Huntington Beach, CA; D. Roman, The Boeing Beach, CA Field, CA; M. Sexton, The Boeing Company, VA; D. Tompkins, M. Beyar, The Boeing Company, Long Beach, CA Huntington Beach, CA; et al. Company, Huntington Beach, CA Monday, 4 January 2016 7-AFM-1 Biometric Flight Mechanics Cortez Hill A Chaired by: R. LIND, University of Florida and M. XIN, University of Missouri 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2016-0013 AIAA-2016-0014 AIAA-2016-0015 AIAA-2016-0016 AIAA-2016-0017 AIAA-2016-0018 Oral Presentation The Dynamics of Passive Wing- Aerodynamic Model Identification Effect of Unsteady Aerodynamics Dynamic Stability of a Hawkmoth- Minimum-Time Transition of Effects of Advance Ratio on the Systems level analysis of resonant Pitching in Hovering Flight of of a Clap-and-Fling Flapping-Wing on the Trim of Hovering Insects and scale Flapping-wing Micro Air FWMAVs from Hovering to Forward Aerodynamic Characteristics of an mechnisms for flapping-wing flyers Flapping Micro Air Vehicles Using MAV: a Comparison between Quasi- FWMAVs Vehicle during Forward Flight Flight Insect Wing in Forward Flight J. Kok, University of South Australia, Three-Dimensional Aerodynamic steady and Black-box Approaches A. Mouy, French Air Force Academy, Salon J. Kim, J. Han, S. Choi, J. Han, Korea A. Hussein, Virginia Polytechnic Institute J. Han, J. Han, Korea Advanced Institute Mawson Lakes, Australia; J. Chahl, Simulations S. Armanini, J. Caetano, C. de Visser, G. de Provence, France; A. Rossi, ENSMA, Advanced Institute of Science and and State University, Blacksburg, VA; of Science and Technology, Daejeon, Defence Science and Technology

L. Chang, N. Perez-Arancibia, University of de Croon, M. Mulder, Delft University of Chasseneuil-du-Poitou, France; H. Taha, Technology, Daejeon, South Korea H. Taha, University of California, Irvine, South Korea ; J. Chang, Korea Aerospace Organisation, Edinburgh, Australia Southern California, Los Angeles, CA Technology, Delft, The Netherlands University of California, Irvine, Irvine, CA Irvine, CA University, Goyang, South Korea Monday, 4 January 2016 8-AFM-2 Atmospheric Entry, Hypersonic Flight and Aeroassist Technology I Cortez Hill B Chaired by: M. BOLENDER, Air Force Research Lab and T. BERGER, US Army Aviation Development Directorate-AFDD 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2016-0019 AIAA-2016-0020 AIAA-2016-0021 AIAA-2016-0022 AIAA-2016-0023 AIAA-2016-0024 High Mass Mars Exploration using Incorporation of Ablative Shape Strategies for Landing Large Stability Analysis of Multibody Robust Aerial Deployment of Mars Application of Taylor Series Slender Entry Vehicles Change into Conceptual Hypersonic Ballistic Coefficient Vehicles on Systems for Mars Descent and with Tilted Folding-Axis Integration to Reentry Problems K. Mall, M. Grant, Purdue University, West Mission Design Mars Landing K. Fujita, Japan Aerospace Exploration M. Bergsma, E. Mooij, Delft University of Lafayette, IN H. Saranathan, M. Grant, Purdue T. Anderson, Z. Putnam, R. Braun, Georgia E. Mooij, Delft University of Technology, Agency (JAXA), Sagamihara, Japan; H. Technology, Delft, The Netherlands University, West Lafayette, IN Institute of Technology, Atlanta, GA Delft, The Netherlands Nagai, Tohoku University, Sendai, Japan; A. Oyama, Japan Aerospace Exploration Agency (JAXA), Sagamihara, Japan Monday, 4 January 2016 9-AMT-1 Velocimetry I Balboa B Chaired by: D. PLEMMONS, Aerospace Testing Alliance (ATA) and T. ECKER, Virginia Tech 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2016-0025 AIAA-2016-0026 AIAA-2016-0027 AIAA-2016-0028 AIAA-2016-0029 AIAA-2016-0030 100-kHz burst-mode particle image Velocity Measurements in an Arcjet Particle Image Velocimetry for Towards shear flow measurements Scale-up of the Time-Resolved Velocity Spectrum Estimation in velocimetry: space-time correlations Erosion Test Facility Transonic Unsteady Flow Field using FLEET Doppler Global Velocimetry Shock–Boundary Layer Interaction and considerations for spatial and D. Plemmons, N. Galyen, E. Smith, R. around a Rocket Fairing Model Y. Zhang, N. Calvert, A. Dogariu, R. Miles, Technique T. Jiang, A. Schreyer, French Space Agency temporal resolution Porter, Arnold Engineering Development S. Koike, K. Nakakita, Japan Aerospace Princeton University, Princeton, NJ T. Ecker, K. Lowe, W. Ng, Virginia (CNES), Paris, France; L. Larchevêque, J. Miller, Air Force Research Laboratory, Center, Arnold AFB, TN Exploration Agency (JAXA), Chofu, Japan; Polytechnic Institute and State University, S. Piponniau, Aix-Marseille University, Wright-Patterson AFB, OH; N. Jiang, D. Thul, S. Tsutsumi, Japan Aerospace Exploration Blacksburg, VA Marseille, France; D. Pierre, National M. Slipchenko, J. Mance, Spectral Energies, Agency (JAXA), Sagamihara, Japan Center for Scientific Research (CNRS), LLC, Dayton, OH; T. Meyer, Purdue University, Marseille, France West Lafayette, IN; et al. Monday, 4 January 2016 10-AMT-10/SD-15 Advances in Fluid-Structural Interaction Experimentation Coronado D Chaired by: J. WAGNER, Sandia National Laboratories and T. BEBERNISS 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs Oral Presentation Oral Presentation Oral Presentation Oral Presentation Oral Presentation Oral Presentation Oral Presentation Advancements and Experimental Optical Full-field Response Verification High-Speed Fluid-Structure Simultaneous time-resolved Structural Response to Fluid/ Digital image correlation used for FSI measurements of nuclear fuel Measurement Challenges of of Wind Tunnel Tests on Inflatable Interaction Experiments at Sandia PIV, and force measurements of Acoustic Coupling dynamic full-field deformation and bundles during earthquakes Shock-Boundary Layer Interaction Aerodynamic Decelerators National Laboratories membrane wings N. Murray, University of Mississippi, strain measurements: Examples P. Bardet, N. Weichselbaum, S. Influence on the Dynamic Response A. Calomino, K. Johnson, M. Cheatwood, K. Casper, J. Wagner, S. Beresh, J. B. Ganapathisubramani, University of University, University, MS and applications Hussain, George Washington University, of a Flexible Panel NASA Langley Research Center, Hampton, VA; Henfling, R. Spillers, Sandia National Southampton, Southampton, United P. Reu, Sandia National Laboratories, Washington, D.C.

T. Beberniss, Air Force Research A. Cassell, G. Swanson, C. Kazemba, NASA Laboratories, Albuquerque, NM Kingdom Albuquerque, NM Laboratory, Wright-Patterson AFB, OH Ames Research Center, Moffett Field, CA Monday, 4 January 2016 11-APA-2 Special Session: Simulation of Rotor in Hover I Coronado E Chaired by: N. HARIHARAN, CREATE-AV and R. NARDUCCI, Boeing Defense, Space & Security 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2016-0031 AIAA-2016-0032 AIAA-2016-0033 AIAA-2016-0034 AIAA-2016-0035 Aerodynamic Modeling A Comparison of CFD Hover Assessment of S-76 Rotor Hover Numerical simulation of Hovering Direct Comparsion of Hover Prediction of S-76 Rotor with Tip-Shape Predictions for the Sikorsky S-76 Performance in Ground Effect S-76 Helicopter Rotor including Far- Workshop Results Variations: Review of AIAA Rotor Using an Unstructured Mixed Mesh Field Analysis E. Duque, A. Toyoda, M. Burklund, Intelligent Standardized Hover Evaluations R. Jain, Army Research Development and Method P. Gardarein, A. Le Pape, ONERA, Meudon, Light, Rutherford, NJ; N. Hariharan, CREATE AV N. Hariharan, CREATE AV Team, Lorton, Engineering Center, Moffett Field, CA J. Hwang, J. Choi, O. Kwon, Korea France Team, Patuxent River, MD; R. Narducci, The VA; R. Narducci, The Boeing Company, Advanced Institute of Science and Boeing Company, Philadelphia, PA; C. Stone, Philadelphia, PA; T. Egolf, Technology, Daejeon, South Korea Computational Science and Engineering, LLC, Corporation, Stratford, CT , IL Monday, 4 January 2016 12-APA-3 Aerodynamic Testing: Flight and Large Scale Americas Cup C Chaired by: S. MASSEY, NASA-Langley Research Center and M. PARK, NASA-Langley Research Center 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2016-0036 AIAA-2016-0037 AIAA-2016-0038 AIAA-2016-0039 AIAA-2016-0040 AIAA-2016-0041 AIAA-2016-0042 Flight Testing of FlexFloilTM An Autonomous, Traversable Evaluation of the Hinge Moment and Measurements of Dynamic Aerodynamic Tests Conducted on a High lift INflight VAlidation (HINVA) Determination of Power Required Adaptive Compliant Trailing Edge Boundary-Layer Probe for Flight Normal Force Aerodynamic Loads Interface Between Ship and Large Scale Nose and - Overview about the 2nd Flight Test through Accelerated Flight with S. Kota, FlexSys, Inc., Ann Arbor, MI; Testing from a Seamless Adaptive Compliant Helicopter Air Wakes Cavity Model in the ARA Transonic Campaign Application to Unmanned Vehicles P. Flick, Air Force Research Laboratory, H. Koch, P. Scholz, R. Kerbstadt, Trailing Edge in Flight C. Friedman, George Washington Wind Tunnel R. Rudnik, German Aerospace Center L. Soltmann, C. Hall, North Carolina State Wright-Patterson AFB, OH; F. Collier, NASA M. Wermes, Technical University of E. Miller, J. Cruz, S. Lung, NASA Armstrong University, Washington, D.C.; J. Duplessis, D. Greenwell, A. Hill, Aircraft Research (DLR), Braunschweig, Germany; D. University, Raleigh, NC Langley Research Center, Hampton, VA Braunschweig, Braunschweig, Germany Flight Research Center, Edwards, CA; S. Kota, French Air Force Academy, Salon de Association Ltd., Bedford, ; Schwetzler, , Bremen, Germany G. Ervin, K. Lu, FlexSys, Inc., Ann Arbor, Provence, France; M. Snyder, George M. Quinn, University of Manchester, MI; et al. Washington University, Washington, D.C. Manchester, United Kingdom Monday, 4 January 2016 13-APA-4 Transonic & Supersonic Aerodynamics Americas Cup D Chaired by: C. ROSEMA, US Army AMRDEC and M. FOSSATI, McGill University 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2016-0043 AIAA-2016-0044 AIAA-2016-0045 AIAA-2016-0046 AIAA-2016-0047 Computation of High-Subsonic Influence of transition on the flow Large-Eddy Simulation of Shock- Numerical Investigation of Investigation Of Diffusers For Two and Transonic Flows by a Lattice downstream of normal shock wave- Induced Flow Separation Control Using Supersonic Flow Over a Wall- Stream Supersonic Wind Tunnels Boltzmann Method -boundary layer interactions SparkJet Concept Mounted Cylinder M. Prabakar, T. M. Thiruchengode, Indian P. Gopalakrishnan, Y. Li, R. Zhang, H. T. Davidson, H. Babinsky, University of G. Yang, Beihang University, Beijing, China; P. Morgan, Ohio Aerospace Institute, Institute of Technology Madras, Chennai, Chen, Exa Corporation, Burlington, MA Cambridge, Cambridge, United Kingdom Y. Yao, University of the West of England, Dayton, OH; S. Sherer, M. Visbal, Air Force India Bristol, United Kingdom; J. Fang, T. Gan, L. Lu, Research Laboratory, Wright-Patterson

Beihang University, Beijing, China AFB, OH Monday, 4 January 2016 14-FD-1/APA-5 Special Session: Low Re & Bio-inspired Flows Discussion Group (Invited) Harbor E Chaired by: M. GREEN, Syracuse University 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs Oral Presentation Oral Presentation Oral Presentation Oral Presentation Oral Presentation Discussion Vortex dynamics around translating Discrete-Vortex Method for Advances in Low-Dimensional Applications of unsteady Unsteady Separated Flow and pitching wings and fins Separated Flows, Augmented with Data-Driven Systems Modeling for aerodynamic reduced-order models Associated with Cross-Flow Turbines K. Taira, Florida State University, Shedding Criteria from Boundary Unsteady Nonlinear Aerodynamics from experiments B. Strom, B. Polagye, S. Brunton, Tallahassee, FL; M. Green, Syracuse Layer Solutions M. Hemati, University of Minnesota, K. Granlund, North Carolina State University of Washington, Seattle, University, Syracuse, NY K. Ramesh, University of Glasgow, Minneapolis, Minneapolis, MN University, Raleigh, NC Seattle, WA Glasgow, United Kingdom Monday, 4 January 2016 15-FD-2 Acoustics and Compressible Flow Transition Promenade B Chaired by: R. KING, NASA-Langley Research Center and R. GOSSE, WPAFB 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2016-0048 AIAA-2016-0049 AIAA-2016-0050 AIAA-2016-0051 AIAA-2016-0052 Acoustic Radiation from a Mach 14 Numerical Study of Wave Trains Measurements in a Transitioning Transient Growth Analysis of Effect of Freejet Upstream Flow Turbulent Boundary layer in Supersonic Flow over a Cone Boundary Layer at Compressible Boundary Layers with Conditions on Flow-Acoustic Resonant C. Zhang, L. Duan, Missouri University of Compression Corner Freestream Mach 3.5 Parabolized Stability Equations Interactions in Transitional Airfoils Science and Technology, Rolla, MO A. Novikov, A. Fedorov, Moscow Institute R. King, A. Chou, P. Balakumar, L. Owens, P. Paredes, M. Choudhari, F. Li, C. L. Nguyen, V. Golubev, R. Mankbadi, Embry- of Physics and Technology, Zhukovsky, M. Kegerise, NASA Langley Research Chang, NASA Langley Research Center, Riddle Aeronautical University, Daytona Russia ; I. Egorov, TsAGI, Zhukovsky, Center, Hampton, VA Hampton, VA Beach, FL; M. Roger, École Centrale de Lyon, Russia Ecully, France; M. Visbal, Air Force Research Laboratory, Wright-Patterson AFB, OH Monday, 4 January 2016 16-FD-3 Aerodynamic Flow Control Cove Chaired by: J. LIN, NASA-Langley Research Center and D. WILLIAMS, Illinois Institute of Technology 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2016-0053 AIAA-2016-0054 AIAA-2016-0055 AIAA-2016-0056 AIAA-2016-0057 AIAA-2016-0058 Aerodynamic Control of Coupled Separation Control With Investigation of Trapped Vorticity An Overview of Active Flow Control Conical Forebody Flow Control Modeling Dynamic Lift Response to Body-Wake Interactions Cooperative Actuation Concentrations Effected by Hybrid Enhanced Vertical Tail Technology Using Thick Dielectric Barrier Actuation T. Lambert, B. Vukasinovic, A. Glezer, M. Blechschmidt, K. Bauer, Airbus, Munich, Actuation in an Offset Diffuser Development Plasma Actuators X. An, D. Williams, Illinois Institute of Georgia Institute of Technology, Atlanta, Germany; W. Nitsche, Berlin Institute of T. Burrows, Z. Gong, B. Vukasinovic, A. J. Lin, M. Andino, M. Alexander, NASA Y. Long, H. Li, X. Meng, H. Hu, Technology, Chicago, IL; J. Eldredge, GA Technology, Berlin, Germany Glezer, Georgia Institute of Technology, Langley Research Center, Hampton, Northwestern Polytechnical University, University of California, Los Angeles, Atlanta, GA VA; E. Whalen, The Boeing Company, Xi’an, China; F. Liu, S. Luo, University of Los Angeles, CA; T. Colonius, California Hazelwood, MO; M. Spoor, J. Tran, The California, Irvine, Irvine, CA Institute of Technology, Pasadena, CA Boeing Company, Seattle, WA; et al. Monday, 4 January 2016 17-FD-4 CFD Applications and Design Pier Chaired by: P. PERSSON 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2016-0059 AIAA-2016-0060 AIAA-2016-0061 AIAA-2016-0062 AIAA-2016-0063 AIAA-2016-0064 AIAA-2016-0065 CFD Studies of Hybrid Air Vehicles Numerical Study of Water Impact Hybrid Quasi Molecular-Continuum Development of a Parallel A Surface Vorticity Panel Method High-Order, Time-Dependent One-Dimensional Approach M. Carrion, M. Biava, R. Steijl, G. Barakos, of an Elastic Cylindrical Shell Using Modeling of Supercooled Large Lagrangian Particle Tracking Code D. Pate, B. German, Georgia Institute of Aerodynamic Optimization using a to Modeling of Reflected and University of Liverpool, Liverpool, United Coupled FVM-FEM Method Droplet Dynamics for In-flight Icing for 3D Multi-Block Curvilinear Grids Technology, Atlanta, GA Discontinuous Galerkin Discretization Transmitted Pressure Pulses in Kingdom; D. Stewart, Hybrid Air Vehicles, Q. Qu, R. Wang, H. Guo, P. Liu, Beihang Conditions A. Kulkarni, J. Edwards, North Carolina of the Navier-Stokes Equations Ducts Bedford, United Kingdom University, Beijing, China; R. Agarwal, V. Abdollahi, W. Habashi, M. Fossati, State University, Raleigh, NC M. Zahr, Stanford University, Stanford, CA; M. Golbabaei-Asl, A. Povitsky, University of Washington University in St. Louis, St. McGill University, Montréal, Canada P. Persson, University of California, Berkeley, Akron, Akron, OH Louis, MO

Berkeley, CA Monday, 4 January 2016 18-FD-5 CFD: Time Integration and Preconditioning Promenade A Chaired by: T. PULLIAM, NASA Ames Research Center and K. CASSEL, Illinois Institute of Technology 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2016-0066 AIAA-2016-0067 AIAA-2016-0068 AIAA-2016-0069 AIAA-2016-0070 AIAA-2016-0071 AIAA-2016-0072 Towards Efficient Parallel-in-Time Implicit Time Marching Methods Cost Effective Multi-Resolution Toward an Optimal Solver for Time- Finite Volume Implementation of The Role of Dispersion and Highly-Accurate Filter-Based Simulation of Periodic Flows for Large-Scale High-Accuracy Analysis Applied to Implicit spectral Solutions on Unstructured the Harmonic Balance Method for Dissipation on Stabilization Artificial-Dissipation Schemes for J. Leffell, Science and Technology Corporation, Simulations of Compressible Flows Temporal Integration Meshes Periodic Non-Linear Flows Strategies for Time-Accurate Stiff Unsteady Fluid Systems Moffett Field, CA; J. Sitaraman, Parallel Y. Du, J. Ekaterinaris, Embry-Riddle S. Chae, Pusan National University, Busan, N. Mundis, D. Mavriplis, University of G. Cvijetic, University of Zagreb, Zagreb, Simulations N. Mundis, ERC Inc., Edwards AFB, CA; A. Geometric Algorithms, LLC, Sunnyvale, CA; Aeronautical University, Daytona Beach, FL South Korea ; H. Kang, Dongyang Mirae Wyoming, Laramie, Laramie, WY Croatia; H. Jasak, Wikki, Ltd., London, A. Edoh, University of California, Los Edoh, University of California, Los Angeles, V. Lakshminarayan, Science and Technology University, Seoul, South Korea ; S. Oh, United Kingdom; V. Vukcevic, University of Angeles, Los Angeles, CA; N. Mundis, ERC Los Angeles, CA; V. Sankaran, Air Force Corporation, Moffett Field, CA; A. Wissink, Pusan National University, Busan, South Zagreb, Zagreb, Croatia Inc., Edwards AFB, CA; A. Karagozian, Research Laboratory, Edwards AFB, CA Army Aviation and Missile Research Korea ; K. Yee, Seoul National University, University of California, Los Angeles, Development and Engineering Center, Moffett Seoul, South Korea Los Angeles, CA; V. Sankaran, Air Force Field, CA Research Laboratory, Edwards AFB, CA Monday, 4 January 2016 19-FD-6 Shock Boundary Layer Interaction I Harbor F Chaired by: N. BISEK, Air Force Reseach Laboratory and J. LITTLE, The University of Arizona 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2016-0073 AIAA-2016-0074 AIAA-2016-0075 AIAA-2016-0076 AIAA-2016-0077 AIAA-2016-0078 On the length and time scales of Forced Navier-Stokes-based An Experiment Investigation on Effect of Upstream Boundary Layer Shock Wave Boundary Layer Response of a shock train to a laminar shock wave boundary Analysis of Low-Frequency Shock-induced Turbulent Boundary on Unsteadiness of Swept-Ramp Interaction Unsteadiness: The downstream back pressure forcing layer interaction Dynamics in a Shock/Turbulent Layer Separation Flow-field Shock/Boundary Layer Interactions Effects of Configuration and R. Klomparens, J. Driscoll, M. Gamba, M. Diop, S. Piponniau, Aix-Marseille Boundary Layer Interaction X. Zhao, China Academy of Aerospace at Mach 2 Strength University of Michigan, Ann Arbor, Ann University, Marseille, France; D. Pierre, M. Adler, D. Gaitonde, Ohio State Aerodynamics, Beijing, China L. Vanstone, M. Saleem, S. Seckin, N. J. Threadgill, P. Bruce, Imperial College Arbor, MI National Center for Scientific Research University, Columbus, OH Clemens, University of Texas, Austin, London, London, United Kingdom (CNRS), Marseille, France Austin, TX Monday, 4 January 2016 20-GNC-1 Vehicle & Flight Control Validation Hillcrest A Chaired by: K. WISE, Boeing Defense, Space & Security and A. NARANG-SIDDARTH, University of Washington 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2016-0079 AIAA-2016-0080 AIAA-2016-0081 AIAA-2016-0082 AIAA-2016-0083 AIAA-2016-0084 AIAA-2016-0085 Geometric Nonlinear Controllability Local Linear Controllability and Efficient Nonlinear Actuator Fault The Influence of Control Surface Efficient Methods for Flight Flight Testing of a Gain-Scheduled Piloted Simulator Evaluation of a Analysis for Airplane Flight Observability Analysis of Nonlinear Reconstruction System Faults on Flexible Aircraft Envelope Estimation through Stability and Control Augmentation Model-Independent Fault-Tolerant Dynamics Systems with Continuation Methods P. Lu, E. Van Kampen, Q. Chu, Delft W. Fan, H. Liu, R. Kwong, University of Reachability Analysis System for a Quad-Tilt-Wing UAV Flight Control System A. Hassan, H. Taha, University of M. Spetzler, A. Narang-Siddarth, University University of Technology, Delft, The Toronto, Toronto, Canada J. Stapel, C. de Visser, E. Van Kampen, Q. H. Totoki, Y. Ochi, National Defense D. Tang, D. Pool, O. Stroosma, Q. Chu, C. California, Irvine, Irvine, CA of Washington, Seattle, Seattle, WA Netherlands Chu, Delft University of Technology, Delft, Academy, Yokosuka, Japan; M. Sato, K. de Visser, Delft University of Technology, The Netherlands Muraoka, Japan Aerospace Exploration Delft, The Netherlands Agency (JAXA), Mitaka, Japan Monday, 4 January 2016 21-GNC-2 Spacecraft Attitude Control I Hillcrest B Chaired by: J. LIU, Boeing Defense, Space & Security and J. THIENEL, NASA Goddard Space Flight Center 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2016-0086 AIAA-2016-0087 AIAA-2016-0088 AIAA-2016-0089 AIAA-2016-0090 AIAA-2016-0091 Spacecraft Attitude Stabilization Design and Stability of an On-Orbit Formulation of Torque-Optimal Simulation of Malfunctions for the Fault-Tolerant Architecture of Two Simulation of an Electromechanical using Magnetorquers with Attitude Control System Using Guidance Trajectories for a CubeSat ISS Double-Gimbal Control Moment Parallel Double-Gimbal Variable- Spin Motor System of a Control Separation between Measurement Reaction Control Thrusters with Degraded Reaction Wheels Gyroscope Speed Control Moment Gyros Moment Gyroscope and Actuation R. Hall, CRM Solutions, Inc., Huntsville, S. Kedare, S. Ulrich, Carleton University, R. Inampudi, Lockheed Martin Corporation, T. Sasaki, T. Shimomura, Osaka Prefecture R. Inampudi, Lockheed Martin Corporation, F. Celani, University of Rome “La AL; S. Hough, Dynamic Concepts, Inc., Ottawa, Canada Houston, TX; J. Gordeuk, GHG Corporation, University, Sakai, Japan Houston, TX; J. Gordeuk, GHG Corporation, Sapienza”, Rome, Italy Huntsville, AL; C. Orphee, NASA Marshall Webster, TX Webster, TX Space Flight Center, Huntsville, AL; K. Clements, ERC Inc., Huntsville, AL Monday, 4 January 2016 22-GNC-3 Invited Session: LOC-1, Onboard Systems for LOC Prevention and Recovery – Problem Analysis and Upset Prevention Methods Coronado B Chaired by: C. BELCASTRO, NASA-Langley Research Center and D. CRIDER, National Transportation Safety Board 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2016-0092 AIAA-2016-0093 AIAA-2016-0094 AIAA-2016-0095 AIAA-2016-0096 AIAA-2016-0097 Aircraft Loss of Control: Problem Design and Piloted Simulator Flight Safety Assessment and Pilot Perception Model Supports the Mathematical Multi-Sensory Model A Computational Analysis of the Analysis for the Development and Evaluation of Adaptive Safe Flight Management to Prevent Loss of Analysis of Vestibular Illusions in of Spatial Orientation Impact of Pilot Awareness of Validation of Technology Solutions Envelope Protection Algorithm Control Due to In-Flight Icing Flight Accidents B. McGrath, Embry-Riddle Aeronautical Control Surface Deflection on C. Belcastro, J. Foster, NASA Langley T. Lombaerts, G. Looye, German Aerospace S. Balachandran, E. Atkins, University of E. Groen, J. Bos, M. Houben, TNO, University, Daytona Beach, FL; B. Expectation of Aircraft State Research Center, Hampton, VA; R. Newman, Center (DLR), Oberpfaffenhofen, Germany; Michigan, Ann Arbor, Ann Arbor, MI Soesterberg, The Netherlands Mortimer, Engineering Acoustics, Inc., L. Whitcher, A. Pritchett, A. Bozan, Georgia Crew Systems, Inc., Seattle, WA; L. Groff, J. Ellerbroek, M. Rodriguez y Martin, Casselberry, FL; S. Drakunov, J. French, Institute of Technology, Atlanta, GA D. Crider, National Transportation Safety Delft University of Technology, Delft, The Embry-Riddle Aeronautical University, Board, Washington, D.C.; D. Klyde, Systems Netherlands Daytona Beach, FL Technology, Inc., Hawthorne, CA Monday, 4 January 2016 23-GNC-4 Invited Session: EDL-1, Entry, Descent and Landing GN&C Technology I Coronado A Chaired by: J. CARSON, NASA Jet Propulsion Laboratory and R. SOSTARIC, NASA-Johnson Space Center 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2016-0098 AIAA-2016-0099 AIAA-2016-0100 AIAA-2016-0101 AIAA-2016-0102 An Inertial Dual-State State Estimator Approach-Phase Precision Landing GN&C Subsystem Concept for Safe Flyover Modeling of Planetary Pits Maraia Capsule Flight Testing and for Precision Planetary Landing with with Hazard Relative Navigation: Precision Landing of the Proposed A. Balakumar, N. Bhasin, O. Daids, R. Results for Entry, Descent, and Hazard Detection and Avoidance Terrestrial Test Campaign Results of Lunar MARE Robotic Science Mission Shanor, K. Snyder, W. Whittaker, Carnegie Landing (EDL) R. Bishop, University of South Florida, Tampa, the Morpheus/ALHAT Project J. Carson, NASA Johnson Space Center, Mellon University, Pittsburgh, PA A. Strahan, R. Sostaric, NASA Johnson FL; T. Crain, Intuitive Machines, Inc., Houston, T. Crain, Intuitive Machines, Inc., Houston, Houston, TX; A. Johnson, Jet Propulsion Space Center, Houston, TX TX; K. DeMars, Missouri University of Science TX; R. Bishop, University of South Florida, Laboratory, California Institute of Technology, and Technology, Rolla, MO; C. Hanak, Intuitive Tampa, FL; J. Carson, N. Trawny, Jet Pasadena, CA; G. Hines, NASA Langley Machines, Inc., Houston, TX; J. Carson, N. Propulsion Laboratory, California Institute Research Center, Hampton, VA; W. Johnson, Trawny, Jet Propulsion Laboratory, California of Technology, Pasadena, CA; J. Sullivan, NASA Johnson Space Center, Houston, TX; Institute of Technology, Pasadena, CA; et al. NASA Johnson Space Center, Houston, F. Anderson, Southwest Research Institute, TX; J. Christian, University, Boulder, CO; S. Lawrence, Arizona State Morgantown, WV; et al. University, Tempe, AZ; et al. Monday, 4 January 2016 24-GNC-5 Aerospace Robotics and Unmanned/Autonomous Systems I Hillcrest C Chaired by: M. AKELLA, University of Texas at Austin and S. ULRICH, Carleton University 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2016-0103 AIAA-2016-0104 AIAA-2016-0105 AIAA-2016-0106 AIAA-2016-0107 Modeling and Attitude Control of Three Dimensional Optimum Path An Improved Model-Based Characterization of Flow Field Nonlinear Control of a Fixed-Wing Tri-Tilt Ducted Fan Vehicle Calculation for Autonomous Parafoil Observer for Inertial Navigation for Divergence for MAVs Vertical UAV using Support Vector Machine Y. Seo, Y. Kim, Seoul National University, S. Bhandari, Y. Lu, A. Raheja, D. Tang,

Vehicles in High Altitude Ballooning Quadrotors with Low Cost IMUs. Control Landing Seoul, South Korea S. Lee, Alfred University, Alfred, NY; J. D. Hanley, T. Bretl, University of Illinois, H. Ho, G. de Croon, Delft University of California Polytechnic State University, Conner, A. Arena, Oklahoma State University, Urbana-Champaign, Urbana, IL Technology, Delft, The Netherlands Pomona, CA Stillwater, OK Monday, 4 January 2016 25-GT-1 SAMURAI - Testing and Simulation of Real Engine Flows I (Invited) Harbor I Chaired by: J. QUEST, ETW GmbH and B. MILLS, AEDC/ ATA 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2016-0108 AIAA-2016-0109 AIAA-2016-0110 AIAA-2016-0111 AIAA-2016-0112 Flow field investigations in the free Large-scale density gradient SAMURAI - jet noise source analysis Aerodynamic Performance Correlation analysis between the jet bypass jet flow of a V2527 engine visualization of the V2527 engine of a V2500 engine Characteristics of the Installed exhaust velocity and microphone- at Ground Operation using SPIV jet flow at Ground Operation using H. Siller, A. Bassetti, S. Funke, German V2527 Fan at Ground Operation array acoustic measurements for a A. Schroeder, R. Geisler, D. Schanz, B. BOS Aerospace Center (DLR), Berlin, Germany D. Schönweitz, R. Becker, P. Ebel, R. turbo-fan engine Wrede, J. Agocs, German Aerospace R. Geisler, A. Schroeder, D. Schanz, J. Schnell, M. Schroll, German Aerospace A. Bassetti, T. Berkefeld, A. Schroeder, H. Center (DLR), Göttingen, Germany Agocs, German Aerospace Center (DLR), Center (DLR), Cologne, Germany Siller, B. Wrede, German Aerospace Center Göttingen, Germany (DLR), Berlin, Germany Monday, 4 January 2016 26-GTE-1 Turbine Technologies Gaslamp D Chaired by: G. WELCH, NASA Glenn Research Center and J. EBACHER, Rolls-Royce 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2016-0113 AIAA-2016-0114 AIAA-2016-0115 AIAA-2016-0116 AIAA-2016-0117 The Effect of Profile Contouring on Reynolds Number Effects on Three Dimensional Turbine Blade Flow Disturbance Environment in Effects of Modeled Stator Wake Secondary Flow Structures in Low the Secondary Flow of Profile Optimization Using Evolutionary Low Pressure Turbines on a Low Pressure Turbine Blade Pressure Turbines Contoured Low Pressure Turbines Algorithm with Viscous Flow J. Cui, P. Tucker, University of Cambridge, Dynamic Performance P. Bear, M. Wolff, Wright State University, C. Marks, R. Sondergaard, Air Force Analysis Cambridge, United Kingdom J. Masud, U. Safdar, O. Khan, S. Ahmed, Dayton, OH; C. Marks, R. Sondergaard, Research Laboratory, Wright-Patterson C. Thorn, R. Hartfield, Auburn University, Air University, Islamabad, Pakistan Air Force Research Laboratory, Wright- AFB, OH; P. Bear, M. Wolff, Wright State Auburn, AL Patterson AFB, OH University, Dayton, OH Monday, 4 January 2016 27-GTE-2 Cycles and Auxiliary Systems Harbor H Chaired by: J. TAI, Georgia Institute of Technology and G. PANIAGUA, Purdue University 0900 hrs 0930 hrs 1000 hrs 1030 hrs AIAA-2016-0118 AIAA-2016-0119 AIAA-2016-0120 AIAA-2016-0121 Micro-Gas Turbine Thrust Meanline Analysis of Turbines with Development and Testing of a Expected Performance of a Jetcat Enhancement via Flow Angularity Choked Flow in the Object-Oriented Fuzzy Logic Controller for a Small P200 as a Gas Generator Corrections Turbomachinery Analysis Code Turbojet Engine N. Grannan, J. Hoke, Innovative Scientific N. Kidder, A. Motsinger, K. Ruff, B. E. Hendricks, NASA Glenn Research Center, S. Ekinci, S. Usenmez, Aerotim Solutions, Inc., Dayton, OH; S. Bailie, F. Jackson, B. Novitsky, Ohio State Cleveland, OH Engineering, LLC, Ankara, Turkey; I. Schauer, Air Force Research Laboratory, University, Columbus, OH Yavrucuk, O. Uzol, Middle East Technical Wright-Patterson AFB, OH University, Ankara, Turkey

Monday, 4 January 2016 28-HSABP-1 Advances in Pressure Gain Combustion I - RDE & PDE Harbor B Chaired by: D. PAXSON, NASA Glenn Research Center and K. KAILASANATH, Naval Research Laboratory 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2016-0122 AIAA-2016-0123 AIAA-2016-0124 AIAA-2016-0125 AIAA-2016-0126 AIAA-2016-0127 AIAA-2016-0128 Experimental Performance Evaluation Development of High-Frequency Hollow Rotating Detonation High Fidelity Simulations of a Starting Transients and Detonation Design of a Premixed Fuel-Oxidizer Experimental Validation of of 3N-Class Pulse Detonation Thruster Pulse Detonation Combustor Combustor Non-Premixed Rotating Detonation Onset Behavior in a Rotating System to Prevent Flashback in a Expanded Centerbodiless RDE using Liquid Purge Method without Purging Material V. Ganesh Kumar, A. St. George, E. Engine Detonation Combustor Rotating Detonation Engine Design S. Takagi, K. Hosono, K. Matsuoka, J. K. Muto, K. Matsuoka, J. Kasahara, Gutmark, University of Cincinnati, P. Cocks, A. Holley, United Technologies A. St. George, R. Driscoll, V. Ganesh I. Andrus, P. King, M. Polanka, Air Force W. Stoddard, A. St. George, R. Driscoll, V. Kasahara, Nagoya University, Nagoya, Japan; Nagoya University, Nagoya, Japan; H. Cincinnati, OH Corporation, East Hartford, CT; B. Rankin, Kumar, E. Gutmark, University of Institute of Technology, Wright-Patterson AFB, Ganesh Kumar, E. Gutmark, University of A. Matsuo, Keio University, Tokyo, Japan; I. Watanabe, A. Matsuo, Keio University, Air Force Research Laboratory, Wright- Cincinnati, Cincinnati, OH OH; F. Schauer, Air Force Research Laboratory, Cincinnati, Cincinnati, OH Funaki, Japan Aerospace Exploration Agency Yokohama, Japan; T. Endo, Hiroshima Patterson AFB, OH Wright-Patterson AFB, OH; J. Hoke, Innovative (JAXA), Sagamihara, Japan University, Higashi-Hiroshima, Japan Scientific Solutions, Inc., Centerville, OH Monday, 4 January 2016 29-IS-1/ICC-1/DA-1 Student Paper Competition -- Information Systems Group Regatta B Chaired by: M. SOTAK and T. YUCELEN, Missouri University of Science & Technology 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2016-0129 AIAA-2016-0130 AIAA-2016-0131 AIAA-2016-0132 AIAA-2016-0133 Intent-based Abstraction for Formal Belief Space Hierarchical Planning Incremental Scheduling with Upper Simple Adaptive Control with PID Combined Flight Management Verification of Flight Deck Mode in the Now for Unmanned Aerial and Lowerbound Temporospatial for MIMO Fault Tolerant Flight System and Flight Data Recorder Confusion Vehicles Constraints Control Design for General Aviation using Tablet J. Suraj Nandiganahalli, S. Lee, I. Hwang, C. Moses, Northeastern University, Boston, G. Sturla, M. Gombolay, J. Shah, T. Nishiyama, S. Suzuki, University of Computers Purdue University, West Lafayette, IN MA; R. Chipalkatty, Draper Laboratory, Massachusetts Institute of Technology, Tokyo, Bunkyo, Japan; M. Sato, K. Masui, J. Adams, C. Merrett, Carleton University, Cambridge, MA Cambridge, MA Japan Aerospace Exploration Agency Ottawa, Canada (JAXA), Mitaka, Japan Monday, 4 January 2016 30-ISC-1 International Student Conference - Undergraduate Category Torrey Hills A Chaired by: L. HANSEN, HRP Systems, Inc. 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2016-0134 AIAA-2016-0135 AIAA-2016-0136 AIAA-2016-0137 AIAA-2016-0138 AIAA-2016-0139 AIAA-2016-0140 Dynamic Impact Response and Improved Digital Holographic Correlation-based Depth Estimation Investigation of the Effect of Blade Aerodynamic Evaluation of the Preliminary Evaluation of an Dynamic Coupling Effects on Twin Simulation of Intrumented Interferometry for Two- with a Plenoptic Camera Kinematics and Reynolds Number on NASA Microgravity Unmanned Electromyographically Controlled Supersonic Impinging Jets Projectile using Bond-Based Dimensional Plasma Density W. Roberts, B. Thurow, Auburn University, the Aerodynamic Performance of a Aerial Vehicle Quadrotor M. Wong, Monash University, Melbourne, Peridynamics Measurements Auburn, AL Small-Scale Vertical Axis Wind Turbine J. Castagnetta, R. Larson, U.S. Air Force A. Azocar, Texas A&M University, College Australia T. Buckley, Michigan State University, East E. Forbes, University of Washington, with Dynamic Blade Pitching Academy, Colorado Springs, CO Station, TX Lansing, MI Seattle, Seattle, WA A. Mills, University of Maryland, College Park, College Park, MD; M. Benedict, Texas A&M University, College Station, TX; I. Chopra, University of Maryland, College Park, College Park, MD Monday, 4 January 2016 31-ISC-2 International Student Conference - Masters Category Torrey Hills B Chaired by: J. CORBETS 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2016-0141 AIAA-2016-0142 AIAA-2016-0143 AIAA-2016-0144 AIAA-2016-0145 AIAA-2016-0146 AIAA-2016-0147 Design and Fabrication of a Meso- On Steady Trkalian High Speed Development of Rate Gyroscope On the Development of a Robotic Discrete-time Modified State Experimental Investigation of Beyond Nyquist by Pouring Space scale Aircraft using a Cycloidal Flows: Swirling Compressible Characterization Tools with Application Hummingbird Observer Implementation on a Two Dynamic Stall on Pliant Wings for into Time Rotor Propulsion System Motion in Solid Rocket Motors to Helium Exposure Testing D. Coleman, M. Benedict, Texas A&M Wheeled Inverted Pendulum Robot Micro Air Vehicles J. Schneiders, R. Dwight, F. Scarano, G. Andrews, E. Shrestha, I. Chopra, O. Cecil, J. Majdalani, Auburn University, E. Hilgemann, H. Ruch, J. Cutler, University of University, College Station, TX J. Stumfoll, Missouri University of Science N. Osterberg, Oregon State University, Delft University of Technology, Delft, The

University of Maryland, College Park, Auburn, AL Michigan, Ann Arbor, Ann Arbor, MI and Technology, Rolla, MO Corvallis, OR Netherlands College Park, MD Monday, 4 January 2016 32-LEC-1 NDA Lecture Harbor A 0900 - 1000 hrs

A Bayesian Framework for Assessment of Model Uncertainty Armen Der Kiureghian President, American University of Armenia Taisei Professor of Civil Engineering Emeritus, University of California, Berkeley Monday, 4 January 2016 33-MAT-1 Nanostructured Materials I Gaslamp B Chaired by: B. BHAT, NASA Marshall Space Flight Center and S. ROY, The University of Alabama and G. ODEGARD 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2016-0148 AIAA-2016-0149 AIAA-2016-0150 AIAA-2016-0151 AIAA-2016-0152 AIAA-2016-0153 AIAA-2016-0154 Structure-Process-Property Study Woven Hierarchical Aerospace Nanoparticle Alignment using Influence of Waviness on the Thermal conductivity via atomistic Mode I Fracture Toughness of Non-covalent Functionalization of CNT of Aligned Carbon Nanotube Composite Laminates with Oscillating Magnetic Fields Elastic Properties of Aligned modeling for epoxy-SWNT Aligned Carbon Nanotube Epoxy and Graphene and Its Application to Interlaminar Reinforcement in Woven Aligned Carbon Nanotube Bulk for Scalable Nanocomposite Carbon Nanotube Polymer Matrix composites Nanocomposites Hybrid Carbon/Epoxy Composites Carbon Fiber Prepreg Laminate Reinforcement Manufacturing Nanocomposites N. Fasanella, V. Sundararaghavan, D. Lidston, C. Parschau, C. Chappelle, D. A. Avila, V. Munhoz, A. Oliveira, N. Menezes, E. Kalfon-Cohen, D. Lewis, Massachusetts R. Li, E. Antunes, A. Liotta, C. Parschau, M. Spencer, N. Yamamoto, Pennsylvania I. Stein, B. Wardle, Massachusetts University of Michigan, Ann Arbor, MI Lewis, B. Wardle, Massachusetts Institute Federal University of Minas Gerais, Belo Institute of Technology, Cambridge, MA; J. M. Payne, B. Wardle, Massachusetts State University, University Park, PA Institute of Technology, Cambridge, MA of Technology, Cambridge, MA Horizonte, Brazil; S. Leao, University Center Ravine, National Composites Center, Kettering, Institute of Technology, Cambridge, MA Newton Paiva, Belo Horizonte, Brazil; C. OH; B. Wardle, Massachusetts Institute of Silva, Federal University of Minas Gerais, Belo Technology, Cambridge, MA Horizonte, Brazil Monday, 4 January 2016 34-MAT-2 Fatigue & Fracture I Gaslamp C Chaired by: R. FERTIG, University of Wyoming and G. SEIDEL, Virginia Polytechnic Institute and State Universit 0900 hrs 0930 hrs 1000 hrs AIAA-2016-0155 AIAA-2016-0156 AIAA-2016-0157 Multiscale Modeling of Effective Utilization of a Linear Solver for High-energy hydroforming for the Piezoresistivity in Nanocomposite Multiscale Design and Optimization aerospace industry Bounded Explosives of Microstructures in an Airframe S. Van Der Veen, L. Barcenas, Airbus, A. Chaurasia, G. Seidel, Virginia Panel Buckling Problem Toulouse, France; H. Groeneveld, V. Polytechnic Institute and State University, P. Acar, V. Sundararaghavan, University of Bhoelai, 3D Metal Forming, Lelystad, The Blacksburg, VA Michigan, Ann Arbor, MI Netherlands ; J. Sinke, Delft University of Technology, Delft, The Netherlands Monday, 4 January 2016 35-MDO-1 Aero & Structural Technology Investigations Balboa A Chaired by: J. GRAY, NASA Glenn Research Center and S. CHOI, Virginia Polytechnic Institute and State University 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2016-0158 AIAA-2016-0159 AIAA-2016-0160 AIAA-2016-0161 AIAA-2016-0162 AIAA-2016-0163 AIAA-2016-0164 Flight Vehicle Structural Design Performance Evaluation of a Aerostructural Optimization of a Cure Rate Tailoring of Thick Co-Design of Strain-Actuated Solar Adaptive Variable-Fidelity Analysis Aerodynamic Optimisation of Non- Processes for a Common Bulkhead Morphing Trailing Edge Using Low Sweep Transonic Wing with Composites Via Temperature Arrays for Precision Pointing and and Design for A Tailless Aircraft planar Lifting Surfaces and an MPCV Spacecraft Adapter Multipoint Aerostructural Design Shock Control Bump Controlled Vascular Pathways Jitter Reduction with Innovative Control Effectors S. Skinner, H. Zare-Behtash, University of P. Aggarwal, P. Hull, NASA Marshall Space Optimization A. Elham, B. Timmer, Delft University of M. O’Donnell, Y. Mahadik, C. Ward, C. Chilan, D. Herber, Y. Nakka, S. Chung, under Model-Form Uncertainty Glasgow, Glasgow, United Kingdom Flight Center, Huntsville, AL D. Burdette, G. Kenway, J. Martins, Technology, Delft, The Netherlands University of Bristol, Bristol, United J. Allison, University of Illinois, Urbana- Y. Jo, Korea Advanced Institute of Science University of Michigan, Ann Arbor, Ann Kingdom Champaign, Urbana, IL and Technology, Daejeon, South Korea ; J. Arbor, MI Park, S. Choi, Virginia Polytechnic Institute and State University, Blacksburg, VA; D. Lee, Korea Advanced Institute of Science and Technology, Daejeon, South Korea Monday, 4 January 2016 36-MST-1 Modeling and Simulation of Air Traffic Management I Golden Hill A Chaired by: J. SCHROEDER, Federal Aviation Administration and D. CARTMELL, Boeing Engineering Operations & Technology 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2016-0165 AIAA-2016-0166 AIAA-2016-0167 AIAA-2016-0168 AIAA-2016-0169 Probabilistic Airport Aceptance Rate Effects of Aircraft Mass and Creating severe weather model Analyzing Feasibility of Continuous Human-in-the-Loop Simulation Prediction Weather Data Errors on Trajectory for arrival manager by analyzing Descent Operation Following Fixed- Analysis of Conflict Resolution J. Cox, M. Kochenderfer, Stanford Optimization and Benefits the flight data of weather front flight Path Angle from Oceanic Route Maneuvers Using an Air Traffic University, Stanford, CA Estimation passage to Tokyo International Airport Control Simulation N. Wickramasinghe, M. Brown, Electronic A. Tezuka, Waseda University, Tokyo, E. Itoh, N. Wickramasinghe, H. Hirabayashi, K. H. Oh, S. Jeong, K. Choi, H. Lee, Inha Navigation Research Institute, Tokyo, Japan; A. Senoguchi, Electronic Navigation Uejima, S. Fukushima, Electronic Navigation University, Incheon, South Korea Japan; Y. Miyamoto, Y. Miyazawa, Kyushu Research Institute, Tokyo, Japan Research Institute, Tokyo, Japan University, Fukuoka, Japan Monday, 4 January 2016 37-MST-2 Special Topics in Modeling and Simulation Hillcrest D Chaired by: P. ZAAL, NASA Ames Research Center and A. ELMILIGUI, NASA Langley Research Center 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2016-0170 AIAA-2016-0171 AIAA-2016-0172 AIAA-2016-0173 AIAA-2016-0174 AIAA-2016-0175 AIAA-2016-0176 Modeling And Simulation of Compressor Performance Modeling Development of a Cockpit-Pilot Model Aerodynamic Modelling of a 5-MW Optimal Attitude Control of a Extracting measurements from Simulation of Spatial Automatic Spacecraft Pointing Modes Using and Prognostics Using Artificial for Thermal Comfort Optimization Wind Turbine for Development and 6U CubeSat with a Four-Wheel operational flight data using the Assembly System Based on Stewart Quaternion-Based Nonlinear Neural Networks During Long-Mission Flight Application of Real-Time Nonlinear Pyramid Reaction Wheel Array and flare example Platform Control Laws S. Ritz, J. Dahlen, Simulations Plus, J. Schminder, R. Gårdhagen, E. Nilsson, Receding Horizon Control Magnetic Torque Coils C. Wang, L. Drees, F. Holzapfel, Technical J. Qi, C. Wang, Beihang University, H. Bel, A. Aly, A. Youssef, Y. Elhalwagy, Inc., Lancaster, CA; R. Hartfield, Auburn Linköping University, Linköping, Sweden; P. Galvani, Federal University of ABC, São K. Gross, Air Force Research Laboratory, University of Munich, Munich, Germany Beijing, China Military Technical College, Cairo, Egypt University, Auburn, AL; W. Woltosz, K. Storck, Saab, Linköping, Sweden; M. Paulo, Brazil; F. Sun, K. Turkoglu, San Jose Wright-Patterson AFB, OH; R. Patrick, E. Simulations Plus, Inc., Lancaster, CA Karlsson, Linköping University, Linköping, State University, San Jose, CA Swenson, J. Agte, Air Force Institute of Sweden Technology, Wright-Patterson AFB, OH Monday, 4 January 2016 38-NW-3 Monday Late Morning Networking Coffee Break Session Room Foyers 0900 - 0930 hrs Monday, 4 January 2016 39-PC-1 Combustion Chemistry Harbor C Chaired by: H. CHELLIAH, University of Virginia and Y. JU, Princeton University 0900 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2016-0177 AIAA-2016-0178 AIAA-2016-0179 AIAA-2016-0180 AIAA-2016-0181 AIAA-2016-0182

An Overview of the National Jet Fuels Combustion Program Shock Tube Measurements of Jet Shock Tube Ignition and CH4 Time- Reduced-species mechanisms for Consistent Chemical Mechanism Modeling Chemical Mechanism for M. Colket, Self, East Hartford, CT; J. Heyne, University of Dayton, Dayton, OH; M. Rumizen, and Rocket Fuels Histories during Propanal Oxidation the combustion of cyclohexane from Collaborative Data Processing Surrogate Jet Fuel under Scramjet Federal Aviation Administration, Burlington, MA; J. Edwards, Air Force Research Laboratory, D. Davidson, Y. Zhu, S. Wang, T. Parise, B. Koroglu, O. Pryor, J. Lopez, L. Nash, using the Local Self Similarity N. Slavinskaya, U. Riedel, M. Abbasi, J. Operating Conditions Wright-Patterson AFB, OH; M. Gupta, Federal Aviation Administration, Washington, D.C.; W. R. Sur, R. Hanson, Stanford University, S. Vasu, University of Central Florida, Tabulation method Starke, German Aerospace Center (DLR), W. Huang, F. Chen, H. Liu, X. Huang, Roquemore, Air Force Research Laboratory, Wright-Patterson AFB, OH; et al. Stanford, CA Orlando, FL P. Kourdis, California Institute of Stuttgart, Germany; A. Tursynbai, Kazakh Shanghai Jiao Tong University, Shanghai, Technology, Pasadena, CA; J. Bellan, Jet National University, Almaty, Kazakhstan; China Propulsion Laboratory, California Institute M. Frenklach, University of California, of Technology, Pasadena, CA Berkeley, Berkeley, CA; et al. Monday, 4 January 2016 40-PC-2 Advanced Concepts, Combustion Diagnostics, Environmental Impact Cortez Hill C Chaired by: I. BOXX, DLR - German Aerospace Center and Y. IKEDA, Imagineering, Inc. 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2016-0183 AIAA-2016-0184 AIAA-2016-0185 AIAA-2016-0186 AIAA-2016-0187 AIAA-2016-0188 AIAA-2016-0189 Green Propellant Infusion Mission Nano-ignition Torch Applied to Cryogenic Investigation of Confined Turbulent PIV Measurement for Diffusion Effect of Reactant Inlet Temperature High-Speed Imaging of Ignition Direct Numerical Simulation (GPIM), Advancing the State of H2/O2 Coaxial Jet Jet Flames Using kHz-Rate Flame in A Porous Cylindrical on Passive Mitigation of behind Reflected Shock Waves of Turbulent Lean Methane-Air Propulsion System Safety and A. Badakhshan, ERC Inc., Edwards, CA; S. Diagnostics Burner Thermo-acoustic Instabilities by D. Davidson, A. Tulgestke, R. Hanson, Bunsen Flame with Mixture Performance Danczyk, Air Force Research Laboratory, Edwards, Z. Yin, I. Boxx, M. Stöhr, O. Lammel, W. K. Pan, C. Guo, National Taiwan University, Implementation of 3D Additive Stanford University, Stanford, CA Inhomogeneities C. McLean, Ball Aerospace & Technologies CA; D. Forliti, Sierra Lobo, Inc., Edwards, CA; I. Meier, German Aerospace Center (DLR), Taipei, Taiwan Manufactured Metallic Porous Insert S. Luca, A. Attili, F. Bisetti, King Abdullah Corporation, Boulder, CO Leyva, Air Force Office of Scientific Research, Stuttgart, Germany J. Kornegay, D. Depperschmidt, A. Agrawal, University of Science and Technology, Arlington, VA; D. Talley, Air Force Research University of Alabama, Tuscaloosa, Tuscaloosa, Thuwal, Saudi Arabia Laboratory, Edwards, CA AL Monday, 4 January 2016 41-PDL-1 Plasma Assisted Combustion Harbor D Chaired by: I. ADAMOVICH, Ohio University and J. ROVEY, Missouri University of Science & Technology 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2016-0190 AIAA-2016-0191 AIAA-2016-0192 AIAA-2016-0193 AIAA-2016-0194 AIAA-2016-0195 Simulations of plasma-assisted Plasma Assisted Combustion Kinetics of plasma-assisted Effects of Axial Stretch on the Flame Plasma assisted GT combustion Parallel On-the-fly Adaptive combustion flames in coaxial Mechanism for Hydrogen and oxidation of methane Propagation Enhancement of Large A. Starikovskiy, Princeton University, Kinetics for Non-equilibrium K. Togai, N. Tsolas, R. Yetter, Pennsylvania Princeton, NJ; A. Zagorskiy, T. Wind, F. microwave reactors Small Hydrocarbons Hydrocarbons by Addition of Ozone Plasma Discharges of C2H4/O2/ J. Zimmerman, A. Palla, D. King, D. A. Starikovskiy, Princeton University, State University, University Park, PA M. Pinchak, University of Cincinnati, Cincinnati, Guethe, GE Power, Baden, Switzerland Ar Mixture Carroll, CU Aerospace, LLC, Champaign, Princeton, NJ; N. Aleksandrov, Moscow OH; T. Ombrello, C. Carter, Air Force Research S. Yang, V. Yang, W. Sun, Georgia Institute IL; C. Mitsingas, R. Rajasegar, University Institute of Physics and Technology, Laboratory, Wright-Patterson AFB, OH; E. of Technology, Atlanta, GA; S. Nagaraja, of Illinois, Urbana-Champaign, Urbana, Moscow, Russia Gutmark, University of Cincinnati, Cincinnati, , Schenectady, IL; et al. OH; V. Katta, Innovative Scientific Solutions, NY; W. Sun, Y. Ju, Princeton University, Inc., Dayton, OH Princeton, NJ; et al. Monday, 4 January 2016 42-PDL-2 DBD Plasma Actuators I Ocean Beach Chaired by: K. KONTIS, University of Glasgow 0900 hrs 0930 hrs 1000 hrs 1030 hrs AIAA-2016-0196 AIAA-2016-0197 AIAA-2016-0198 AIAA-2016-0199 Electrode Material Degradation Direct Position Control of Dielectric PIV-Estimated DBD Plasma-Actuator Coaxial DBD Actuator Design for Monitoring for Durable Dielectric Barrier Discharge Filaments Thrust Verified by Measurement in Control of a Hydrogen Diffusion Barrier Discharge Plasma Actuators M. Paliwoda, J. Rovey, Missouri University Quiescent Air Flame Manufacturing of Science and Technology, Rolla, MO L. Wu, C. Gao, X. Yan, Northwestern J. Retter, R. Fontaine, J. Freund, N. A. Iwakawa, M. De Giorgi, University Polytechnical University, Xi’an, China; F. Glumac, G. Elliott, University of Illinois,

of Salento, Lecce, Italy; L. Francioso, Liu, S. Luo, University of California, Irvine, Urbana-Champaign, Urbana, IL A. Taurino, National Research Council Irvine, CA (CNR), Lecce, Italy; P. Lavoie, University of Toronto, Toronto, Canada Monday, 4 January 2016 43-SD-1 Structural Dynamic Modeling and Analysis Balboa C Chaired by: C. HEBERT, Sierra Nevada Corporation and M. ROSS, Sandia National Laboratories 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2016-0200 AIAA-2016-0201 AIAA-2016-0202 AIAA-2016-0203 AIAA-2016-0204 AIAA-2016-0205 Joining 3-D Finite Elements to Constrained-Energy Cross-Well The Evaluation of an Icosahedron’ Evaluating the stiffness of conic Force Reconstruction from Ejection Towards a Fluid-Structure Variational Asymptotic Beam Actuation of the Duffing-Holmes Eigenvalue interfacing parts : a practical method Tests of Aircraft Stores Used for Interaction Solver for Problems Models Oscillator A. Palazotto, L. Just, Air Force Institute of for finite element model updating Model Predictions and Missing/ with Large Deformations Within the H. Hoseini, D. Hodges, Georgia Institute of M. Zarepoor, O. Bilgen, Old Dominion Technology, Wright-Patterson AFB, OH based on experimental modal testing Bad Gages Open-Source SU2 Suite Technology, Atlanta, GA University, Norfolk, VA A. Letarte, S. Joncas, École de Technologie M. Ross, M. Starr, A. Urbina, J. Cap, R. Sanchez, R. Palacios, Imperial College Supérieure, Montréal, Canada; A. Ross, École A. Brink, Sandia National Laboratories, London, London, United Kingdom; T. Polytechnique de Montréal, Montréal, Canada; Albuquerque, NM Economon, H. Kline, J. Alonso, Stanford F. Martin, Canadian Space Agency, Saint- University, Stanford, CA; F. Palacios, The Hubert, Canada Boeing Company, Long Beach, CA Monday, 4 January 2016 44-SD-2 Energy Harvesting Gaslamp A Chaired by: D. KUMAR, University of Michigan and K. SINGH, Miami Univeristy 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2016-0206 AIAA-2016-0207 AIAA-2016-0208 AIAA-2016-0209 AIAA-2016-0210 AIAA-2016-0211 Toward broadband resistive- The Role of Sweep Rate in Energy Representation and comparative Piezoaeroelastic investigation on Energy Harvesting From Aeroelastic Enhanced stability identi cation inductive piezoelectric energy Harvesting study of electromagnetic-piezoelectric the control and energy harvesting Instabilities and global response prediction of harvesters T. Hynds, J. Kauffman, University of galloping energy harvesters of galloping systems N. Hosking, Z. Sotoudeh, Rensselaer galloping energy harvesters H. Abdelmoula, A. Abdelkefi, Central Florida, Orlando, FL U. Javed, New Mexico State University, Las H. Abdelmoula, A. Abdelkefi, New Mexico Polytechnic Institute, Troy, NY U. Javed, A. Abdelkefi, New Mexico State State University, Las Cruces, NM Cruces, NM; H. Dai, Huazhong University of State University, Las Cruces, NM University, Las Cruces, NM; I. Akhtar, Science and Technology, Wuhan, China; A. National University of Sciences and Abdelkefi, New Mexico State University, Las Technology, Islamabad, Pakistan Cruces, NM Monday, 4 January 2016 45-SE-1 Systems Engineering I Americas Cup B Chaired by: J. EILER, Stellar Solutions, Inc. and M. FRENCH, Rolls-Royce Corp 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2016-0212 AIAA-2016-0213 AIAA-2016-0214 AIAA-2016-0215 AIAA-2016-0216 Theoretical Foundations for the Can the Capability Maturity Model® A Systems Engineering Approach Integrated Assessment of Aircraft A Methodology for Sizing and Analysis Discipline of Systems Engineering Contribute to a Common Model for to the Conceptual Design of a and Novel Subsystem Architectures of Electric Propulsion Subsystems for S. Johnson, University of Colorado, Systems Engineering? Martian UAV in Early Design Unmanned Aerial Vehicles Colorado Springs, Colorado Springs, CO; J. V. Johnson, Textron Aviation, Wichita, KS S. D’Urso, K. Tsai, P. Chadha, H. Hilton, I. Chakraborty, D. Mavris, Georgia Institute G. Cinar, Georgia Institute of Technology, Day, Jet Propulsion Laboratory, California University of Illinois, Urbana-Champaign, of Technology, Atlanta, GA Atlanta, GA; M. Emeneth, PACE America Inc., Institute of Technology, Pasadena, CA Urbana, IL Seattle, WA; D. Mavris, Georgia Institute of Technology, Atlanta, GA Monday, 4 January 2016 46-SEO-1 Intelligent and Autonomous Systems for Improving Space Exploration and Operations Americas Cup A Chaired by: D. LAVALLEE, The Johns Hopkins University Applied Physics Laboratory and S. VAN Y, Accenture Limited 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2016-0217 AIAA-2016-0218 AIAA-2016-0219 AIAA-2016-0220 AIAA-2016-0221 Optimization of Injection Space Data Integrator: FAA’s A High-Heritage Blunt-Body Entry, Impactor Missions to Europa and Impact and Crashworthiness Parameters for Slightly Inclined Innovative Platform for Launch and Descent, and Landing Concept for Ganymede: Seismic Approach for Characteristics of Venera Type Geosynchronous Orbits Reentry Operations Human Mars Exploration Estimating Icy Crust Thickness Landers for Future Venus Missions J. Shan, N. Bijnens, York University, L. Mutuel, Sierra Nevada Corporation, H. Price, Jet Propulsion Laboratory, California A. Franqui, S. Seufert, M. Cosenza, M. K. Schroeder, J. Bayandor, Virginia Toronto, Canada Sparks, NV; D. Murray, Federal Aviation Institute of Technology, Pasadena, CA; R. Okutsu, Catholic University of America, Polytechnic Institute and State University, Administration, Washington, D.C. Braun, Georgia Institute of Technology, Atlanta, Washington, D.C. Blacksburg, VA; J. Samareh, NASA Langley GA; R. Manning, E. Sklyanski, Jet Propulsion Research Center, Hampton, VA Laboratory, California Institute of Technology, Pasadena, CA Monday, 4 January 2016 47-SOF-1 Software Architecture and Robust Software Engineering Regatta A Chaired by: C. THAMES, NASA Langley Research Center 0900 hrs 0930 hrs AIAA-2016-0222 AIAA-2016-0223 Formally Verified Run Time Assurance New Requirement-Definition and Architecture of a 6U CubeSat Attitude Verification Techniques According to Control System DO-178C, DO-331, and DO-333 K. Gross, M. Clark, J. Hoffman, Air Force U. Eisemann, dSPACE GmbH, Paderborn, Research Laboratory, Wright-Patterson AFB, Germany; J. Allen, dSPACE Inc., Wixom, OH; A. Fifarek, LinQuest, Dayton, OH; K. MI Rattan, Wright State University, Dayton, OH; E. Swenson, Air Force Institute of Technology, Wright-Patterson AFB, OH; et al. Monday, 4 January 2016 48-SRE-1 Extraterrestrial Water: Prospecting and Acquisition Bankers Hill Chaired by: J. KLEINHENZ, NASA Glenn Research Center 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2016-0224 Oral Presentation AIAA-2016-0225 AIAA-2016-0226 AIAA-2016-0227 AIAA-2016-0228 Oral Presentation Accessing, Drill and Operating at Sample Acqusition Systems for a Laboratory Apparatus for Evaluating Extraction and Capture of Mechanical Properties of Icy Mars Near-Infrared monitoring of Regolith Volatile Recovery at the Lunar South Pole: Status of Free-Flying Unmanned Robotic Volatiles Production from Meteorites Water from Martian Regolith Regolith Simulant: Assessment of a volatiles in frozen lunar simulants Simulated Lunar Environment European Plans and Activities System to Support Interplanetary and Simulants: Design and Testing Experimental Proof-of-Concept Potential ISRU Feedstock while drilling J. Kleinhenz, NASA Glenn Research Center, R. Fisackerly, J. Carpenter, B. Houdou, G. Bodies Prospecting and L. Gertsch, Missouri University of Science and D. Linne, J. Kleinhenz, NASA Glenn R. Ash, J. Emery, B. Crane, J. Ricci, Old T. Roush, A. Colaprete, R. Elphic, J. Cleveland, OH; G. Paulsen, K. Zacny, Visentin, ESA, Noordwijk, The Netherlands Characterization Missions Technology, Rolla, MO; A. Abbud-Madrid, C. Research Center, Cleveland, OH Dominion University, Norfolk, VA Forgione, B. White, R. McMurray, NASA Honeybee Robotics, Pasadena, CA; S. ; F. Rizzi, M. Savoia, Selex ES, Nerviano, Dreyer, Colorado School of Mines, Golden, CO; Ames Research Center, Moffett Field, Schmidt, D. Boucher, Deltion Innovations, K. Zacny, B. Yaggi, J. Spring, P. Chu, Italy; et al. Honeybee Robotics, Pasadena, CA; R. J. Heniff, Missouri University of Science and CA; et al. Ltd., Capreol, Canada Mueller, T. Ebert, NASA Kennedy Space Technology, Rolla, MO; D. Linne, NASA Glenn Center, Cape Canaveral, FL; et al. Research Center, Cleveland, OH; J. Mantovani, NASA Kennedy Space Center, Cape Canaveral, FL; et al. Monday, 4 January 2016 49-STR-1 Aircraft Structural Design I La Jolla A Chaired by: M. WOLFF, Gulfstream Aerospace Corporation and P. MARDANPOUR 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2016-0229 AIAA-2016-0230 AIAA-2016-0231 AIAA-2016-0232 AIAA-2016-0233 AIAA-2016-0234 AIAA-2016-0235 Conceptual Design and Structural Moving Aerospace Structural A Historical Assessment of Building Structural Loads Analysis of a Determination of Load Path Using Preliminary Wing Study of General Bi-Level Optimization of a Optimization of NASA Environmentally Design Practice to a Load and Block Development Test Programs for Carrier Onboard Delivery Aircraft Streamline Analogy and Galerkin Aviation Aircraft with PRSEUS Conceptual Metallic Wing Box with Responsible Aviation (ERA) Hybrid Resistance Factor Approach Modern Military Aircraft B. Flansburg, Lockheed Martin Method panels Stiffness Constraints Wing Body Aircraft C. Larsen, NASA Johnson Space Center, D. Norwood, Lockheed Martin Corporation, Corporation, Marietta, GA K. Gharibi, A. Tamijani, Embry-Riddle V. Papapetrou, A. Tamijani, D. Kim, Embry- A. Noevere, A. Wilhite, Georgia Institute of J. Quinlan, F. Gern, NASA Langley Research Houston, TX; I. Raju, NASA Langley Fort Worth, TX; G. Hahn, P. Joyce, R. Wippich- Aeronautical University, Daytona Beach, FL Riddle Aeronautical University, Daytona Technology, Atlanta, GA Center, Hampton, VA Research Center, Hampton, VA Dienhart, The Boeing Company, St. Louis, MO Beach, FL Monday, 4 January 2016 50-STR-2 Challenges in the Design of Joined Wings La Jolla B Chaired by: R. CAVALLARO, Technion, Israel Institute of Technology and L. DEMASI, San Diego State University College of Engineering 0900 hrs 0930 hrs 1000 hrs 1030 hrs AIAA-2016-0236 AIAA-2016-0237 AIAA-2016-0238 AIAA-2016-0239 Minimum Induced Theorems for Transonic Aeroelastic Analysis Aeroelasticity of Joined Wings: Distributed Optical Sensing in Multi-Wing Systems for Multidisciplinary Design Unique Aspects and Challenges Composite Laminate Adhesive Bonds L. Demasi, San Diego State University, San Optimization Applications R. Cavallaro, Technion--Israel Institute of L. Meadows, R. Sullivan, Mississippi State Diego, CA; G. Monegato, Technical University W. Mallik, R. Kapania, J. Schetz, Virginia Technology, Haifa, Israel; L. Demasi, San University, Mississippi State, MS; K. Vehorn, of Turin, Turin, Italy; R. Cavallaro, Technion-- Polytechnic Institute and State University, Diego State University, San Diego, CA; R. University of Dayton Research Institute, Israel Institute of Technology, Haifa, Israel Blacksburg, VA Bombardieri, University of Pisa, Pisa, Italy Dayton, OH Monday, 4 January 2016 51-TES-1 The State and Future of Energy Systems Old Town A 0900 - 1230 hrs Moderators: Tom Shih, Purdue University and Ashwani Gupta, University of Maryland

Nanoscale Thermal Tranport Thermal Energy Storage Materials Control Issues in Thermal Management Challenges and Opportunities in Thermal Management Integration of Dynamic Thermal Systems Tim Fisher Patrick Shamberger Andrew Alleyne Tom Shih Mitch Wolf Purdue University Texas A&M University University of Illinois, Urbana–Champaign Purdue University Wright State University

Monday, 4 January 2016 52-TES-2/TP-1 Joint Session: Heat Transfer in Terrestrial Energy Systems Old Town B Chaired by: D. PYTEL, Lockheed Martin Space Systems and A. HASHEMI, Lockheed Martin Space Systems

0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2016-0240 AIAA-2016-0241 AIAA-2016-0242 AIAA-2016-0243 Oral Presentation Oral Presentation Mist cooling ratios analysis in Jet Impingement Heat Transfer Effect of porous insert on flame Design of a Supersonic Oxy- Eulerian-Lagrangian modeling of Study of Kaplan Hydro Turbine rectangular passage with 45-deg Enhancement on a -roughened dynamics in a lean premixed swirl- Methane Combustor for Direct particle-laden flow Performance angled rib Flat Plate stabilized combustor using planar Power Extraction S. Davis, G. Jacobs, San Diego State Y. Yen, T. ElHammal, R. Amano, University H. Alhajeri, J. Amaral Teixeira, A. Addali A. Alenezi, J. Amaral Teixeira, A. Addali laser-induced flueorescence M. Hernandez, L. Cabrera , O. Vidana, M. University, San Diego, CA of Wisconsin, Milwaukee, Glendale, WI A., A. Gamil A. A., A. Alenezi, Cranfield A., A. Gamil A. A., H. Alhajeri, Cranfield J. Allen, University of Alabama, Chaidez, N. Love, University of Texas, El University, Cranfield, United Kingdom University, Cranfield, United Kingdom Tuscaloosa, Tuscaloosa, AL; B. Fisher, Paso, El Paso, TX Naval Research Laboratory, Washington, D.C.; A. Agrawal, University of Alabama, Tuscaloosa, Tuscaloosa, AL Monday, 4 January 2016 53-TP-2 Thermal Protection System, Ablation and Surface Catalysis I Harbor G Chaired by: D. KUNTZ, Sandia National Laboratories and D. HASH, NASA - ARC 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2016-0244 AIAA-2016-0245 AIAA-2016-0246 AIAA-2016-0247 AIAA-2016-0248

Laser Ablation of Dielectrics for Radiative Transfer In A Rigid Near-Surface CO2 Tunable Diode Numerical Prediction of Tungsten Effect of spalled particles thermal Development of High Temperature Carbon Material Under Arcjet Flow Laser Absorption Spectroscopy Ablation under Arc Heater degradation on a hypersonic flow Sapphire Based Pressure Transducers Condition Concentration Measurements in the Experimental Conditions field environment P. Woerner, W. Oates, Florida State University, T. Sakai, T. Horiuchi, T. Suzuki, H. Fukui, LENS-XX Expansion Tunnel Facility S. Noh, K. Kim, Seoul National University, R. Davuluri, H. Zhang, A. Martin, Tallahassee, FL; M. Sheplak, University Nagoya University, Nagoya, Japan; Y. J. Weisberger, P. DesJardin, State Seoul, South Korea University of Kentucky, Lexington, of Florida, Gainesville, Gainesville, FL; D. Ishida, Japan Aerospace Exploration University of New York, Buffalo, NY; Lexington, KY Blood, Valparaiso University, Valparaiso, IN; Agency (JAXA), Chofu, Japan M. MacLean, R. Parker, Z. Carr, CUBRC, D. Mills, University of Florida, Gainesville, Buffalo, NY Gainesville, FL Monday, 4 January 2016 54-UMS-1 Unmanned Systems: Mission Management and Planning Technologies Regatta C Chaired by: M. LOGAN, NASA Langley Research Center and M. ANDERSON 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2016-0249 AIAA-2016-0250 AIAA-2016-0251 AIAA-2016-0252 AIAA-2016-0253 AIAA-2016-0254 AIAA-2016-0255 Comprehensive Safety System Privacy Aware Mission Planning Hierarchical Path Planning Using Experimental Assessment of Online Navigation and Guidance Strategy BugFlood: A bug inspired algorithm Development of an Area of Interest Design and Development for and Video Masking for UAV Q-Learning and Incremental Dynamic Soaring Optimization for Planning for UAV Urban Operation for efficient path planning in an Extended Coverage Loitering Path Unmanned Aerial Vehicles Systems Approximate Dynamic Small Unmanned Aircraft Y. Watanabe, A. Veillard, ONERA, obstacle rich environment Planner Formation Flight System R. Martin, Brigham Young University, Programming W. Silva, E. Frew, University of Colorado, Toulouse, France; C. Chanel, University of N. Sharma, Indraprastha Institute of J. Wilhelm, J. Rojas, West Virginia D. Wei, Nanyang Technological University, Provo, UT; A. Hall, C. Brinton, Mosaic Y. Zhou, E. Van Kampen, Q. Chu, Delft Boulder, Boulder, CO Toulouse, Toulouse, France Information Technology Delhi, New Delhi, University, Morgantown, WV Singapore, Singapore ATM, Inc., Leesburg, VA; K. Franke, J. University of Technology, Delft, The India; J. Pinto, University of Porto, Porto, Hedengren, Brigham Young University, Netherlands Portugal; P. Sujit, Indraprastha Institute of Provo, UT Information Technology Delhi, New Delhi, India Monday, 4 January 2016 55-PANEL-1 Monday Morning Forum 360 Seaport F-G 0930 - 1130 hrs Distilling Your Message: Putting yourself back into your science and engineering Facilitator: Christine O’Connell, Associate Director, Alan Alda Center for Communicating Science, Stony Brook University - School of Journalism Effective science communication is necessary in fostering ongoing conversations between scientists and engineers, policy makers, and the general public, as well as promoting science literacy. The ability to communicate directly and vividly can help with securing funding, collaborating across disciplines, and strengthening research. The challenge is for scientists to be clear and engaging without oversimplifying the science. This interactive presentation suggests tools and examples to help scientists and engineers communicate in ways that resonate with people outside of their field about what they do and why it matters. We will cover general principles in how to craft clear, conversational statements, and avoid jargon. Participants will be actively engaged in explaining scientific material and engineering principles to lay people to develop and practice clarity in speaking to non-scientists and engineers about their work. Monday, 4 January 2016

56-SOF-2 Lightweight Perfection: Why and How You Should Review Code for Small Teams Regatta A 1030 - 1230 hrs A panel of experts will teach participants why you should run code reviews even for development teams of two, and how to run code reviews in small teams.

Panelists: Misty Davies Jim Murphy Chris Thames NASA Ames Research Center NASA Ames Research Center NASA Langley Research Center

Monday, 4 January 2016 57-LUNCH-1 Durand Lectureship for Public Service and Luncheon Seaport A-E 1230 - 1400 hrs

Thoughts on Complex Systems Solutions in the 21st Century Ronald M. Sega Vice President for Energy, the Environment, and Applied Research Colorado State University Research Foundation Monday, 4 January 2016 58-AA-2 Computational Aeroacoustics I Nautical Chaired by: A. LYRINTZIS and S. ARUNAJATESAN, Sandia National Labs 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2016-0256 AIAA-2016-0257 AIAA-2016-0258 AIAA-2016-0259 AIAA-2016-0260 AIAA-2016-0261 Numerical Simulation of the Noise Implementation of a Wall-Modeled Detached Eddy Simulation of High- Lattice Boltzmann Method for Noise estimation of beveled trailing A study of the influence of grid from Tandem Cylinder Flow with Sharp Immersed Boundary Method in Lift Wing Slat Track and Cut-Out Aeroacoustic Simulations with edges using an integral and resolution and axial extent on the Spectral Difference Method a High-Order Large Eddy Simulation Noise Block-Structured Cartesian Grid boundary element method prediction of jet turbulence and J. Gao, X. Li, Beihang University, Beijing, Tool for Jet Aeroacoustics X. Wang, Z. Hu, University of T. Ishida, Japan Aerospace Exploration W. van der Velden, A. van Zuijlen, A. noise China N. Dhamankar, G. Blaisdell, Purdue University, Southampton, Southampton, United Agency (JAXA), Chofu, Japan de Jong, H. Bijl, Delft University of C. Bogey, O. Marsden, École Centrale de West Lafayette, IN; A. Lyrintzis, Embry-Riddle Kingdom Technology, Delft, The Netherlands Lyon, Ecully, France Aeronautical University, Daytona Beach, FL Monday, 4 January 2016 59-ABPSI-2/GEPC-2 NASA ERA Systems Integration II Golden Hill B Chaired by: J. FLAMM, NASA Langley Research Center and G. DALE, Air Force Research Laboratory 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs AIAA-2016-0262 AIAA-2016-0263 AIAA-2016-0264 AIAA-2016-0265 AIAA-2016-0266 AIAA-2016-0267 Oral Presentation NASA ERA Integrated CFD for Wind NASA Environmentally Responsible Computational Evaluation of Inlet Estimating Flow-Through Balance CFD Predictions for Transonic Impact of Ultra-High Bypass/ Preferred System Concept System Tunnel Testing of Hybrid Wing-Body Aviation Hybrid Wing Body Flow- Distortion on an Ejector Powered Momentum Tares with CFD Performance of the ERA Hybrid Hybrid Wing Body Integration on Assessment (Invited) Configuration (Invited) Through Wind Tunnel CFD Hybrid Wing Body at Takeoff and (Invited) Wing-Body Configuration (Invited) Propulsion System Perrformance J. Bonet, N. Princen, K. Elmer, P. Camacho, J. Garcia, J. Melton, M. Schuh, K. James, (Invited) Landing Conditions (Invited) J. Melton, K. James, NASA Ames Research K. Deere, J. Luckring, S. McMillin, J. and Operability (Invited) D. Tompkins, The Boeing Company, K. Long, NASA Ames Research Center, M. Schuh, J. Garcia, NASA Ames Research M. Sexton, D. Tompkins, The Boeing Center, Moffett Field, CA; J. Flamm, NASA Flamm, NASA Langley Research Center, W. Lord, G. Hendricks, M. Kirby, Pratt & Huntington Beach, CA Moffett Field, CA; D. Vicroy, NASA Langley Center, Moffett Field, CA; M. Carter, K. Deere, Company, Huntington Beach, CA; K. Deere, Langley Research Center, Hampton, VA; Hampton, VA; D. Roman, The Boeing Whitney, East Hartford, CT; S. Ochs, R. Lin, Research Center, Hampton, VA; et al. NASA Langley Research Center, Hampton, S. McMillin, M. Carter, NASA Langley K. Long, NASA Ames Research Center, Company, Long Beach, CA L. Hardin, United Technologies Corporation,

VA; P. Stremel, Science and Technology Research Center, Hampton, VA; M. Schuh, Moffett Field, CA East Hartford, CT Corporation, Moffett Field, CA; D. Tompkins, NASA Ames Research Center, Moffett The Boeing Company, Huntington Beach, CA Field, CA; et al. Monday, 4 January 2016 60-AFM-3 Special Session: Flight Testing in Education Bankers Hill Chaired by: M. COTTING, US Air Force Test Pilot School and N. SARIGUL-KLIJN, University of California, Davis 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs AIAA-2016-0268 AIAA-2016-0269 AIAA-2016-0270 AIAA-2016-0271 AIAA-2016-0272 AIAA-2016-0273 AIAA-2016-0274 Balancing Education and Training at Undergraduate Learn by Doing Flight Test Education at The Ohio Flight Testing of Stability Boundary Systems Test and Evaluation Flight Testing with Senior Design Teaching Flight Testing Through the USAF Test Pilot School - Invited Flight Test Curriculum - Invited State University - Invited and Dynamic Separation in a Education at NPS Students - Invited Soaring - Invited M. Cotting, W. Gray, U.S. Air Force Test K. Colvin, California Polytechnic State J. Gregory, M. McCrink, Ohio State University Environment - Invited O. Yakimenko, Naval Postgraduate School, C. Hall, North Carolina State University, J. Stewart, Virginia Polytechnic Institute Pilot School, Edwards AFB, CA University, San Luis Obispo, CA University, Columbus, OH N. Sarigul-Klijn, University of California, Monterey, CA Raleigh, NC and State University, Blacksburg, VA Davis, Davis, CA Monday, 4 January 2016 61-AFM-4 Atmospheric Entry, Hypersonic Flight and Aeroassist Technology II Cortez Hill B Chaired by: M. GRANT, Purdue University and C. KARLGAARD, Analytical Mechanics Associates Inc 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2016-0275 AIAA-2016-0276 AIAA-2016-0277 AIAA-2016-0278 AIAA-2016-0279 AIAA-2016-0280 Rapid Indirect Trajectory Rapid Indirect Trajectory Tree Based Trajectory Planning for Review and Assessment of the Entry Guidance by Onboard Dynamic Stability Analysis of Optimization on Highly Parallel Optimization of a Hypothetical Mars Aerocapture. Steep Lifting Entry Closed-Form Trajectory Planning and Tracking Hypersonic Transport during Computing Architectures Long Range Weapon System A. Chakrabarty, S. Swei, D. Prabhu, NASA Trajectory Solution K. Webb, P. Lu, Iowa State University, Reentry T. Antony, M. Grant, Purdue University, M. Grant, T. Antony, Purdue University, Ames Research Center, Moffett Field, CA Z. Putnam, R. Braun, Georgia Institute of Ames, IA G. Guruswamy, NASA Ames Research West Lafayette, IN West Lafayette, IN Technology, Atlanta, GA Center, Moffett Field, CA Monday, 4 January 2016 62-AMT-2 Spectroscopy and Combustion Applications Balboa B Chaired by: A. CUTLER, The George Washington University and S. KEARNEY, Sandia National Laboratories 1400 hrs 1430 hrs 1500 hrs 1530 hrs AIAA-2016-0281 AIAA-2016-0282 AIAA-2016-0283 AIAA-2016-0284

Hybrid fs/ps Rotational CARS Hybrid fs/ps CARS for Sooting and Quantitative O2 Measurements Evaluation of Hybrid fs/ps coherent Temperature and Oxygen Particle-laden Flames in Flames at Elevated Pressures anti-Stokes Raman scattering Measurements in a Sooting, K. Gabet Hoffmeister, D. Guildenbecher, by Laser-induced Breakdown temperature and pressure sensitivity S. Kearney, Sandia National Laboratories, Turbulent C2H4-Fueled Jet Flame Spectroscopy at combustor relevant conditions S. Kearney, D. Guildenbecher, K. Gabet Albuquerque, NM Y. Wu, C. Smith, Z. Zhang, University of C. Dedic, J. Michael, Iowa State University, Hoffmeister, C. Winters, T. Grasser, J. Tennessee, Knoxville, Knoxville, TN Ames, IA; J. Miller, Air Force Research Hewson, Sandia National Laboratories, Laboratory, Wright-Patterson AFB, OH; Albuquerque, NM T. Meyer, Purdue University, West Lafayette, IN Monday, 4 January 2016 63-APA-6/FD-7 Special Session: Advances in Fundamental Unsteady Low Reynolds Number Flows AVT-202 Coronado D Chaired by: H. BABINSKY, University of Cambridge and M. OL, US Air Force Reseach Laboratory 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs AIAA-2016-0285 AIAA-2016-0286 AIAA-2016-0287 AIAA-2016-0288 AIAA-2016-0289 AIAA-2016-0290 Next Steps in the Fundamentals of Unsteady Flat Plates: a Cursory Low Reynolds Number Acceleration Unsteady Aerodynamics of Pitching Leading Edge Vortex Evolution and Parametric Variations in Aspect Low Order Modelling of Lift Forces Highly Unsteady Aerodynamics Review (Invited - AVT202 special of Flat Plate Wings at High Low Aspect Ratio Wings: A review Lift Production on Rotating Wings Ratio, Leading Edge and Planform for Unsteady Pitching and Surging session) Incidence (Invited). of AVT-202-panel results (Invited (Invited) Shapes for the Rectilinear Pitch Wings. M. Ol, Air Force Research Laboratory, R. Stevens, H. Babinsky, University of Paper) A. Jones, F. Manar, University of Cases of AVT-202 (Invited) H. Babinsky, R. Stevens, University of Wright-Patterson AFB, OH; H. Babinsky, Cambridge, Cambridge, United Kingdom; L. Bernal, University of Michigan, Ann Maryland, College Park, College Park, O. Son, O. Cetiner-Yildirim, Istanbul Cambridge, Cambridge, United Kingdom; Cambridge University, Cambridge, United F. Manar, P. Mancini, A. Jones, University Arbor, Ann Arbor, MI MD; N. Phillips, T. Nakata, R. Bomphrey, Technical University, Istanbul, Turkey; A. Jones, University of Maryland, College

Kingdom of Maryland, College Park, College Park, University of London, Hatfield, United R. Stevens, H. Babinsky, Cambridge Park, College Park, MD; L. Bernal, MD; K. Granlund, North Carolina State Kingdom; M. Ringuette, State University of University, Cambridge, United Kingdom; F. University of Michigan, Ann Arbor, Ann University, Raleigh, NC; et al. New York, Buffalo, NY; et al. Manar, P. Mancini, University of Maryland, Arbor, MI; M. Ol, Air Force Research College Park, College Park, MD; et al. Laboratory, Wright-Patterson AFB, OH Monday, 4 January 2016 64-APA-7 Aerodynamic Design: Analysis, Methodologies, and Optimization Techniques I Americas Cup B Chaired by: J. AZEVEDO and P. ANSELL, University of Illinois at Urbana-Champaign 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs AIAA-2016-0291 AIAA-2016-0292 AIAA-2016-0293 AIAA-2016-0294 AIAA-2016-0295 AIAA-2016-0296 AIAA-2016-0297 Using A Fast and Explicit Mesh An Evaluation of Aerodynamic Computational Analysis and Variable-Fidelity Surrogate Parametric Study of the Effects of Least Squares Shadowing An Optimization Approach to Split- Movement Method To Efficiently Analysis Software for use in Optimization of Blockerless Engine Modeling of Lambda Wing a Tubercle’s Geometry on Wing Sensitivity Analysis of Chaotic Flow Winglet Design for Sailplanes Compute Mesh Sensitivity Aircraft MDO Thrust Reverser Concept Transonic Aerodynamic Performance Through the Use of around a Two-Dimensional Airfoil T. Krebs, G. Bramesfeld, Ryerson G. Mura, B. Hinchliffe, N. Qin, University C. Meckstroth, University of Dayton P. Rajput, I. Kalkhoran, New York Performance the Lifting-Line Theory P. Blonigan, Q. Wang, Massachusetts University, Toronto, Canada of Sheffield, Sheffield, United Kingdom; J. Research Institute, Dayton, OH University, Brooklyn, NY D. Bryson, M. Rumpfkeil, University of M. Bolzon, R. Kelso, M. Arjomandi, Institute of Technology, Cambridge, MA; Brezillon, Airbus, Toulouse, France Dayton, Dayton, OH University of Adelaide, Adelaide, Australia E. Nielsen, NASA Langley Research Center, Hampton, VA; B. Diskin, National Institute of Aerospace, Hampton, VA Monday, 4 January 2016 65-APA-8 Special Session: Simulation of Rotor in Hover II Coronado E Chaired by: R. NARDUCCI, Boeing Defense, Space & Security and N. HARIHARAN, CREATE-AV 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs AIAA-2016-0298 AIAA-2016-0299 AIAA-2016-0300 AIAA-2016-0301 AIAA-2016-0302 AIAA-2016-0303 Oral Presentation Performance Impact of Tip Shape Hover Predictions of the S-76 Rotor A Comparative Study of Two Hover Parametric Validation Study for a Performance and Physics of a Investigations of XV-15 Rotor NASA Hover Tests: Overview and Variations on the S-76 Rotor Using using HMB2 - Model to full Scale Prediction Methodologies Hovering Rotor using UT-GENCAS S-76 Rotor in Hover With Non- Hover Performance and Flow Field Plans KCFD G. Barakos, A. Jimenez-Garcia, University R. Eshcol, CD-adapco, Orlando, FL; C. B. Min, B. Wake, United Technologies Contiguous Hybrid Methodologies Using U2NCLE and HELIOS Codes T. Norman, NASA Ames Research Center, J. Abras, Naval Air Systems Command, of Liverpool, Liverpool, United Kingdom Zhou, J. Kim, L. Sankar, Georgia Institute Corporation, East Hartford, CT K. Jacobson, A. Grubb, M. Smith, Georgia C. Sheng, Q. Zhao, University of Toledo, Moffett Field, CA; L. Jenkins, S. Gorton, Patuxent River, MD; N. Hariharan, CREATE of Technology, Atlanta, GA Institute of Technology, Atlanta, GA Toledo, OH; M. Hill, Bell Helicopter NASA Langley Research Center, Hampton, AV Team, Lorton, VA Textron, Inc., Fort Worth, TX VA Monday, 4 January 2016 66-APA-9 High Angle of Attack and High Lift Aerodynamics Americas Cup C Chaired by: J. MURRAY, Sandia National Laboratories and A. SCLAFANI, Boeing Commercial Airplanes 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs AIAA-2016-0304 AIAA-2016-0305 AIAA-2016-0306 AIAA-2016-0307 AIAA-2016-0308 Numerical Simulations of Prediction of Buffet Loads of F-15 with Prediction of Post-Stall Frequency Response Measurements Development of the High Lift Streamwise Vortices on a Generic FUN3D Solver Aerodynamic Characteristics of Flapped Airfoil at High Angles of Common Research Model (HL-CRM): A High-Lift Configuration S. Yang, P. Chen, ZONA Technology, Inc., of wing(s) with separated flow Attack Representative High Lift Configuration T. Landa, R. Radespiel, Technical University Scottsdale, AZ; X. Wang, M. Mignolet, Arizona modeled as a Single Nascent Vortex M. Zakaria, M. Hajj, Virginia Polytechnic for Transonic Transports of Braunschweig, Braunschweig, Germany; State University, Tempe, AZ; D. Pitt, J. Loyet, A. Samuel, R. Mukherjee, Indian Institute Institute and State University, Blacksburg, VA D. Lacy, The Boeing Company, Seattle, WA; J. Wild, German Aerospace Center (DLR), The Boeing Company, St. Louis, MO of Technology Madras, Chennai, India A. Sclafani, The Boeing Company, Long Braunschweig, Germany Beach, CA

Monday, 4 January 2016 67-APA-10 Test and Prediction Techniques for High-speed Flows Americas Cup D Chaired by: X. WANG, Air Force Research Laboratory and C. TILMANN, Air Force Research Laboratory 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs AIAA-2016-0309 AIAA-2016-0310 AIAA-2016-0311 AIAA-2016-0312 AIAA-2016-0313 Effect of Deflection for Roll Computational Analysis, Model Evaluation of Dynamic Pressure- The Incoming Flow Investigation Temperature Measurements by Control on Fin Performance of a Reduction, and Experimental Sensitive Paint for Improved around Geometric Elements in Temperature Sensitive Paint on Fin-Stabilized Projectile Comparison of Model Scale Impinging Analysis of Cavity Flows and CFD Hypersonic Shock Tube. Flexible and Deforming Body in S. Silton, Army Research Laboratory, Jets Validation M. Kotov, I. Kryukov, L. Ruleva, S. Hypersonic Flow Aberdeen Proving Ground, MD; C. Coyle, A. Crowell, Naval Air Systems Command, D. Roberts, N. Stokes, Aircraft Research Solodovnikov, S. Surzhikov, Russian M. Taguchi, R. Maruyama, K. Mori, U.S. Military Academy, West Point, NY Patuxent River, MD; L. Myers, Pennsylvania Association Ltd., Bedford, United Kingdom; Academy of Sciences, Moscow, Russia Nagoya University, Nagoya, Japan State University, University Park, PA M. Quinn, University of Manchester, Manchester, United Kingdom; J. Coppin, T. Birch, DSTL, Portsmouth, United Kingdom Monday, 4 January 2016 68-ASC-1 EU FP7 CHANGE (Special Session) Gaslamp D Chaired by: R. DE BREUKER, TU Delft and R. BARRETT-GONZALEZ, The University of Kansas 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs AIAA-2016-0314 AIAA-2016-0315 AIAA-2016-0316 AIAA-2016-0317 AIAA-2016-0318 MDAO for Aerodynamic Assessment Design and Experiments of a A Hybrid Morphing Trailing Edge Telescopic Wing-Box for a Morphing From development of multi- of a Morphed Wing for the Loiter Warp Induced Camber and Twist Designed for Camber Change of the Wing material skins to morphing flight Segment of a UAV Flight Mission Morphing Leading and Trailing Control Surface P. Gamboa, P. Santos, University of Beira hardware production Y. Yang, S. Ozgen, Y. Yaman, Middle Edge Device I. Tunçöz, Y. Yang, E. Gürses, M. Sahin, Y. Interior, Covilha, Portugal A. Falken, S. Steeger, O. Heintze, INVENT East Technical University, Ankara, Turkey; N. Werter, J. Sodja, G. Spirlet, R. De Yaman, S. Ozgen, Middle East Technical GmbH, Braunschweig, Germany; R. De A. Ciarella, M. Hahn, Aircraft Research Breuker, Delft University of Technology, University, Ankara, Turkey Breuker, Delft University of Technology, Association Ltd., Bedford, United Kingdom; Delft, The Netherlands Delft, The Netherlands C. Beaverstock, Swansea University, Swansea, United Kingdom; et al. Monday, 4 January 2016 69-FD-8 Airfoil Flow Control Cove Chaired by: D. RIZZETTA and J. FARNSWORTH, University of Colorado Boulder 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs AIAA-2016-0319 AIAA-2016-0320 AIAA-2016-0321 AIAA-2016-0322 AIAA-2016-0323 AIAA-2016-0324 AIAA-2016-0325 Open-Loop and Closed-Loop Aero-Servo-Elastic Control of a Aerodynamic Control of a Control Strategies for a Laminar- Effet of Oscillating Winglet on the Flow Seperation and Passive Flow An Experimental Study of Mini-Tabs Trailing-Edge Separation Control on Cyber-Physical FlexibleWing Dynamically Pitching VR-12 Airfoil Flow Compatible High-Lift Wing Development of Wing-Tip Vortex Control on E387 Airfoil for Aerodynamic Load Control a Natural Laminar Flow Airfoil C. Fagley, J. Seidel, T. McLaughlin, U.S. using Discrete Pulsed Actuation Configuration T. Guha, R. Kumar, Florida State A. Heffron, J. Williams, E. Avital, Queen D. Heathcote, I. Gursul, D. Cleaver, R. Gupta, P. Ansell, University of Illinois, Air Force Academy, Colorado Springs, CO; Y. Tan, T. Crittenden, A. Glezer, Georgia D. Rizzetta, M. Visbal, Air Force Research University, Tallahassee, FL Mary University of London, London, United University of Bath, Bath, United Kingdom Urbana-Champaign, Urbana, IL J. Farnsworth, University of Colorado, Institute of Technology, Atlanta, GA Laboratory, Wright-Patterson AFB, OH Kingdom Boulder, Boulder, CO Monday, 4 January 2016 70-FD-9 CFD Simulation of Vortex Flows Pier Chaired by: S. KARMAN, Pointwise, Inc. and D. GARMANN, Air Force Research Laboratory 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2016-0326 AIAA-2016-0327 AIAA-2016-0328 AIAA-2016-0329 AIAA-2016-0330 AIAA-2016-0331 Analysis on -vortex development DNS Study on Motion around Unsteady Evolution of the Tip CFD Simulations of the ERICA Transient Laminar Cross-Flow over Numerical Investigation of Low- in a transitional boundary layer a Vortex Ring in Transitional Vortex on a Stationary and using HMB2 a Rigid Cantilever Plate Pressure Turbine Endwall Flows Y. Wang, S. Chern, Y. Dong, C. Liu, Boundary Layers Oscillating NACA0012 Wing A. Jimenez-Garcia, G. Barakos, University N. DiZinno, G. Vradis, NYU Polytechnic A. Gross, S. Romero, New Mexico State University of Texas, Arlington, Arlington, TX Y. Wang, S. Chern, Y. Yang, C. Liu, D. Garmann, M. Visbal, Air Force Research of Liverpool, Liverpool, United Kingdom School of Engineering, Brooklyn, NY University, Las Cruces, NM; C. Marks, University of Texas, Arlington, Arlington, TX Laboratory, Wright-Patterson AFB, OH R. Sondergaard, Air Force Research Laboratory, Wright-Patterson AFB, OH Monday, 4 January 2016

71-FD-11 Compressible Boundary Layers Harbor D Chaired by: S. GORDEYEV, University of Notre Dame and L. AGOSTINI, The Ohio State University 1400 hrs 1430 hrs 1500 hrs 1530 hrs AIAA-2016-0332 AIAA-2016-0333 AIAA-2016-0334 AIAA-2016-0335 Shock Wave Boundary Layer CFD Investigation of Supersonic Entropy Generation and Transport Causal relationship between large Interaction Control using Bleed with Discretely Modeled Mechanism in Compressible Mixing outer structures and small-scale Repetitive-Pulse Laser Energy Holes in Cambridge Wind Tunnel Layer: A Direct Numerical Study near-wall turbulence in a compressible Depositions S. Duncan, P. Orkwis, M. Ugolotti, K. Shi, S. Morris, A. Jemcov, University of boundary layer at Mach=2.3 A. Iwakawa, T. Tamba, S. Pham, T. Shoda, University of Cincinnati, Cincinnati, OH Notre Dame, Notre Dame, IN L. Agostini, Ohio State University, Columbus, A. Sasoh, Nagoya University, Nagoya, OH; M. Leschziner, Imperial College London, Japan London, United Kingdom; J. Poggie, N. Bisek, Air Force Research Laboratory, Wright- Patterson AFB, OH; D. Gaitonde, Ohio State University, Columbus, OH Monday, 4 January 2016 72-FD-12 DNS/LES Techniques Harbor E Chaired by: F. SCHRANNER and M. RAI, NASA-Ames Research Center 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2016-0336 AIAA-2016-0337 AIAA-2016-0338 AIAA-2016-0339 AIAA-2016-0340 AIAA-2016-0341 Significance of Computational Utilizing Direct Numerical Optimization of an Implicit Validation of a Window-Embedded Turbulent Inflow Generation for the Large Eddy Simulation based Spanwise Domain Length on LES Simulations of Transition and LES Method for Underresolved RANS/LES Method Based on Large-eddy Simulation Technique on Residual-based Variational for the Flowfield with Large Vortex Turbulence in Design Optimization Simulations of Incompressible Flows Synthetic Turbulence Through Globally Neutral Buoyancy Multiscale Method and Lagrangian Structure M. Rai, NASA Ames Research Center, F. Schranner, V. Rozov, N. Adams, Z. Li, H. Chen, Y. Zhang, Tsinghua Perturbations Dynamic Smagorinsky Model H. Fukumoto, University of Tokyo, Bunkyo, Moffett Field, CA Technical University of Munich, Munich, University, Beijing, China C. Umphrey, I. Senocak, Boise State S. Tran, O. Sahni, Rensselaer Polytechnic Japan; H. Aono, Tokyo University of Science, Germany University, Boise, ID Institute, Troy, NY Katsushika, Japan; T. Nonomura, A. Oyama, K. Fujii, Institute of Space and Astronautical Science, Sagamihara, Japan Monday, 4 January 2016 73-FD-13 Jet Flows I Promenade B Chaired by: R. WOSZIDLO, The Boeing Company 1400 hrs 1430 hrs 1500 hrs 1530 hrs AIAA-2016-0342 AIAA-2016-0343 AIAA-2016-0344 AIAA-2016-0345 Comparison between LES and Computational Methodology for Numerical Simulation of Jet Mixing The Time-Resolved Flow Field of a experimental round jet for diesel Investigating the Transient Interaction in a Recessed Coaxial Injector at Jet Emitted by a Fluidic Oscillator fuel spray Between a Reaction Control Jet and a Supercritical Pressure into a Crossflow J. Brulatout, F. Garnier, P. Seers, University Hypersonic Crossflow D. Muto, Kyushu Institute of Technology, F. Ostermann, Technical University of of Québec, Montréal, Canada W. Miller, P. Medwell, M. Kim, University Kitakyushu, Japan; H. Terashima, Berlin, Berlin, Germany; R. Woszidlo, of Adelaide, Adelaide, Australia; C. Doolan, University of Tokyo, Tokyo, Japan; N. University of Kansas, Lawrence, Lawrence, University of New South Wales, Sydney, Tsuboi, Kyushu Institute of Technology, KS; C. Nayeri, C. Paschereit, Technical Australia Kitakyushu, Japan University of Berlin, Berlin, Germany Monday, 4 January 2016 74-FD-14 Shock Boundary Layer Interaction II Harbor F Chaired by: J. BENEK, Air Force Research Lab AFRL/RQ and A. GROSS, New Mexico State University 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs AIAA-2016-0346 AIAA-2016-0347 AIAA-2016-0348 AIAA-2016-0349 AIAA-2016-0350 AIAA-2016-0351 AIAA-2016-0352 New LES of a Hypersonic Shock/ Numerical Investigation of Shock Experimental Study of the Three- Simulation of Hypersonic Shock Wave Assessment of CFD Capability for Shock Wave Boundary Layer Simulations of Incident Shock Turbulent Boundary Layer Boundary-Layer Interactions Dimensionality of Shock Wave- Laminar Boundary Layer Interaction Hypersonic Shock Wave Boundary Interaction in a Hypersonic Laminar Boundary Layer Interactions Interaction A. Gross, New Mexico State University, Boundary Layer Interactions in on Hollow Cylinder Flare Layer Interactions, Part II Flow on a Hollow Cylinder Flare J. Benek, C. Suchyta, Air Force Research C. Helm, M. Martin, University of Las Cruces, NM; H. Fasel, University of Rectangular Inlets N. Kianvashrad, D. Knight, Rutgers, The State M. Rouhi Youssefi, D. Knight, Rutgers, M. Mortazavi, D. Knight, Rutgers, The Laboratory, Wright-Patterson AFB, OH; Maryland, College Park, College Park, MD Arizona, Tucson, Tucson, AZ I. Grossman, P. Bruce, Imperial College University of New Jersey, New Brunswick, NJ The State University of New Jersey, State University of New Jersey, New H. Babinsky, University of Cambridge, London, London, United Kingdom Piscataway, NJ Brunswick, NJ Cambridge, United Kingdom Monday, 4 January 2016 75-FD-20 Stability and Transition of Hypersonic Flows I Promenade A Chaired by: M. BORG, Air Force Research Laboratory and M. KEGERISE, NASA-Langley Research Center 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2016-0353 AIAA-2016-0354 AIAA-2016-0355 AIAA-2016-0356 AIAA-2016-0357 AIAA-2016-0358 Direct Numerical Simulation of Simultaneous Infrared and Instability and Transition Traveling Crossflow Wave Unsteady Heat-Flux Measurements Visualization of Hypersonic Boundary Crossflow Instability Excited by Pressure Measurements of Experiments in the Boeing/AFOSR Predictions on the HIFiRE-5 at of Second-Mode Instability Waves Layer Transition on Elliptic Cone in Microscale Roughness on HIFiRE-5 Crossflow Instability Modes for Mach-6 Quiet Tunnel Mach 6: Stability Analysis vs. Quiet in a Hypersonic Boundary Layer High Enthalpy Shock Tunnel with D. Dinzl, G. Candler, University of HIFiRE-5 C. Sweeney, B. Chynoweth, J. Edelman, Tunnel Data M. Kegerise, S. Rufer, NASA Langley Temperature-Sensitive Paint Minnesota, Twin Cities, Minneapolis, MN M. Borg, Air Force Research Laboratory, S. Schneider, Purdue University, West M. Lakebrink, The Boeing Company, St. Research Center, Hampton, VA T. Nagayama, H. Nagai, Tohoku University, Wright-Patterson AFB, OH Lafayette, IN Louis, MO; M. Borg, Air Force Research Sendai, Japan; H. Tanno, T. Komuro, Japan Laboratory, Wright-Patterson AFB, OH Aerospace Exploration Agency (JAXA), Kakuda, Japan Monday, 4 January 2016 76-GNC-6 Control Theory and Applications Hillcrest A Chaired by: M. SORGENFREI, NASA Ames Research Center and J. ROGERS, Georgia Institute of Technology 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs AIAA-2016-0359 AIAA-2016-0360 AIAA-2016-0361 AIAA-2016-0362 AIAA-2016-0363 AIAA-2016-0364 AIAA-2016-0365 Robust Hover Mode Control of a An Incremental Approximate Observer-Based Sequential Control Robust Control of Uncertain Hardening Control Systems with the Modified Extended State Observer Handling Hidden Coupling Terms Tiltrotor Using Nonlinear Control Dynamic Programming Flight of a Two Time Scale Spring-Mass- Linear Input-Delayed Sampled ICAR Loop Control of Linear Systems in Gain-Sheduling Control Design: Technique Controller Based on Output Damper System Data System Through Use of H. Sells, DESE Research, Inc., Huntsville, C. Heise, S. Schatz, F. Holzapfel, Technical Application to a Pitch-Axis Missile M. Alam, Czech Technical University in Prague, Feedback D. Saha, J. Valasek, Texas A&M Optimization Scheme and Robust AL University of Munich, Munich, Germany Prague, Czech Republic; S. Celikovsky, Czech Y. Zhou, E. Van Kampen, Q. Chu, Delft University, College Station, TX Stability Bound H. Lhachemi, D. Saussié, G. Zhu, Defense Academy of Sciences, Prague, Czech Republic; University of Technology, Delft, The J. Kratz, R. Yedavalli, Ohio State Research and Development Canada, D. Walker, University of Liverpool, Liverpool, Netherlands University, Columbus, OH Montréal, Canada United Kingdom Monday, 4 January 2016 77-GNC-7 Spacecraft Attitude Control II Hillcrest B Chaired by: E. MOOIJ, Delft Technical University of Technology and R. HALL 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2016-0366 AIAA-2016-0367 AIAA-2016-0368 AIAA-2016-0369 AIAA-2016-0370 AIAA-2016-0371 Flexible GN&C architecture enables Recovery of an Uncontrolled, A Bang-Bang Attitude for Deterministic Drift Counteraction Almost Global Stochastic Stabilization Solving Polynomial Optimal Control an innovative control solution Asymmetric Spacecraft with Limited Rotating Rigid Bodies Optimal Control for Attitude Control of Attitude Motion with Unknown Problems via Iterative Convex to repurpose the Kepler Space Controls E. Serpelloni, M. Maggiore, C. Damaren, of Spacecraft with Time-Varying Multiplicative Diffusion Coefficient Optimization Telescope M. Coen, J. Valasek, Texas A&M University of Toronto, Toronto, Canada Mass E. Samiei, New Mexico State University, Las C. Sun, R. Dai, P. Lu, Iowa State D. Putnam, D. Wiemer, I. Gravseth, Ball University, College Station, TX R. Zidek, I. Kolmanovsky, University of Cruces, NM; A. Sanyal, Syracuse University, University, Ames, IA Aerospace & Technologies Corporation, Michigan, Ann Arbor, Ann Arbor, MI Syracuse, NY; E. Butcher, University of Boulder, CO Arizona, Tucson, AZ Monday, 4 January 2016 78-GNC-8 Invited Session: LOC-2, Onboard Systems for LOC Prevention and Recovery – Real-Time Failure Detection, Isolation, and Redundancy Management Coronado B Chaired by: C. BELCASTRO, NASA-Langley Research Center and D. CRIDER, National Transportation Safety Board 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs AIAA-2016-0372 AIAA-2016-0373 AIAA-2016-0374 AIAA-2016-0375 AIAA-2016-0376 Aircraft Fault Detection Using Aircraft Actuator Fault Detection Aerodynamic Modeling from Flight An Innovative Approach to Air Virtual Redundancy for Safety Real-Time Frequency Response and Isolation using Piecewise Data with Unknown Time Skews Data Sensor FDIR for Commercial Assurance in the Presence of Sensor Estimation Constant Fault Estimation Scheme E. Morelli, NASA Langley Research Center, Aircraft Failures J. Grauer, NASA Langley Research Center, H. Lee, S. Snyder, A. Patterson, N. Hampton, VA J. Boskovic, J. Jackson, Scientific Systems M. Devore, N. Gandhi, A. Bateman, Barron Hampton, VA Hovakimyan, University of Illinois, Urbana- Company, Inc., Woburn, MA Associates, Inc., Charlottesville, VA Champaign, Urbana, IL

Monday, 4 January 2016 79-GNC-9 Invited Session: EDL-2, Entry, Descent and Landing GN&C Technology II Coronado A Chaired by: J. CARSON, NASA Jet Propulsion Laboratory and B. ACIKMESE, University of Texas at Austin 1400 hrs 1430 hrs 1500 hrs AIAA-2016-0377 AIAA-2016-0378 AIAA-2016-0379 Verification of a Fully Numerical A Convex Formulation for the Design and Analysis of Map Entry Guidance Algorithm Minimum Fuel Powered-Descent Relative Localization for Access to P. Lu, Iowa State University, Ames, IA; C. Guidance Problem with Drag, Hazardous Landing Sites on Mars Brunner, Odyssey Space Research, LLC, Nonlinear State Constraints, and A. Johnson, Y. Cheng, J. Montgomery, N. Houston, TX; S. Stachowiak, G. Mendeck, Free Final Time Trawny, B. Tweddle, J. Zheng, California M. Tigges, C. Cerimele, NASA Johnson M. Szmuk, B. Acikmese, University of Institute of Technology, Pasadena, CA Space Center, Houston, TX Texas, Austin, Austin, TX Monday, 4 January 2016 80-GNC-10 Aerospace Robotics and Unmanned/Autonomous Systems II Hillcrest C Chaired by: S. ULRICH, Carleton University and T. BOGE, DLR GSOC 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2016-0380 AIAA-2016-0381 AIAA-2016-0382 AIAA-2016-0383 AIAA-2016-0384 AIAA-2016-0385 Trajectory Transcriptions for Unifying Artificial Intelligence and Landmark-Aided Navigation for Optimal Flight Paths in Wireless Bio-inspired Time-to-contact Control A Comparison between Trajectory Potential Autonomy Features in Trajectory Optimization for UAV Air Vehicles Using Learned Object Sensor Networks: Modeling, for Autonomous Quadrotor Vehicles Optimization Methods: Differential UAV Maneuvers Guidance Detectors Simulation, and Flight Test B. Thomsen, M. Zhang, I. Sharf, McGill Dynamic Programming and C. Ashokkumar, G. York , U.S. Air Force R. Cowlagi, J. Sperry, Worcester M. DeAngelo, J. Horn, Pennsylvania State N. Jodeh, R. Cobb, Air Force Institute of University, Montréal, Canada Pseudospectral Optimal Control Academy, Colorado Springs, CO Polytechnic Institute, Worcester, MA University, University Park, PA Technology, Wright-Patterson AFB, OH M. Gandhi, E. Theodorou, Georgia Institute of Technology, Atlanta, GA Monday, 4 January 2016 81-GT-2 SAMURAI - Testing and Simulation of Real Engine Flows II (Invited) Hillcrest D Chaired by: J. QUEST, ETW GmbH and T. WADHAMS, CUBRC 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs AIAA-2016-0386 AIAA-2016-0387 AIAA-2016-0388 AIAA-2016-0389 AIAA-2016-0390 Image Base Fan Blade Deformation Structural Modelling and Validation of Engine performance simulation of Numerical Simulation of a Fully Hybrid RANS/CAA Computation Measurements on an Airbus A320 a V2500 Honeycomb Core Fan Blade the integrated V2527 - Engine Fan Integrated Engine Ground Test of A320 V2527 Engine at Ground V2500 Engine in Ground Operation P. Ebel, R. Schnell, D. Schönweitz, T. Kirmse, F. Wolters, R. Becker, R. Schnell, P. Ebel, D. Keller, German Aerospace Center (DLR), Operation T. Kirmse, P. Ebel, A. Schroeder, German German Aerospace Center (DLR), Stuttgart, German Aerospace Center (DLR), Cologne, Braunschweig, Germany A. Neifeld, R. Ewert, German Aerospace Aerospace Center (DLR), Göttingen, Germany Germany Germany Center (DLR), Braunschweig, Germany Monday, 4 January 2016 82-GTE-3 Compression Systems I Gaslamp C Chaired by: R. ANTHONY and K. SUDER, NASA Glenn Research Center 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs AIAA-2016-0391 AIAA-2016-0392 AIAA-2016-0393 AIAA-2016-0394 AIAA-2016-0395 AIAA-2016-0396 AIAA-2016-0397 A CFD Study and Performance Improved Predictions of Transonic, Computational Investigation of Pulsed-DC Plasma Actuator Computational Simulations of a Effect of Vortex Ingestion on Compressor integration study for a Evaluation of Service-Run Low Aspect Ratio, Axial Compressor Upstream-Propagating Potential Characteristics and Application in Multi-stage Subsonic Research Transonic Fan Stability pulse detonation engine Variable Vanes in a High Pressure Stage Performance and Tip Clearance Disturbances in a Fan Stage Compressor Stall Control Compressor J. Page, Cambridge University, Cambridge, B. Saracoglu, von Kármán Institute for Compressor of a Turbofan Engine Effects K. Gordon, E. Jumper, A. Jemcov, K. Shi, R. McGowen, T. Corke, E. Matlis, K. Sreenivas, R. Webster, E. Hereth, United Kingdom; P. Hield, Rolls-Royce Fluid Dynamics, Rhode-Saint-Genèse, S. Li, R. Ramakrishnan, Air Lines, R. Howard, Air Force Research Laboratory, University of Notre Dame, Notre Dame, IN University of Notre Dame, Notre Dame, University of Tennessee, Chattanooga, Group plc, Bristol, United Kingdom; P. Belgium; G. Paniagua, Purdue University, Inc., Atlanta, GA Wright-Patterson AFB, OH; S. Puterbaugh, IN; R. Kaszeta, C. Gold, Creare, Inc., Chattanooga, TN; N. Key, R. Berdanier, Tucker, Cambridge University, Cambridge, West Lafayette, IN Universal Technology Corporation, Dayton, OH Hanover, NH Purdue University, West Lafayette, IN United Kingdom Monday, 4 January 2016

83-IS-2 Intelligent and Adaptive Aerospace Control Regatta B Chaired by: C. SABO, University of Cincinnati and A. YUCEL, Lockheed Martin Aeronautics 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs AIAA-2016-0398 AIAA-2016-0399 AIAA-2016-0400 AIAA-2016-0401 AIAA-2016-0402 AIAA-2016-0403 AIAA-2016-0404 Demonstration Platform for Trajectory Adaptive Estimation of Disturbance Adaptive Modal Identification and A Zero Filter Augmentation for Robust Post Loss-Of-Control Autonomous Quadcopter Obstacle Avoidance Bio-Inspired Visual Navigation for a Planning of an Autonomous Torque for Orbiting Spacecraft Flutter Suppression Control Adaptive Control of Weakly Minimum Recovery Flight Regimes Using using Biomimetic Algorithms Quadcopter using Optic Flow Nonholonomic Skid-Steer System for Using Recursive Least Squares N. Nguyen, S. Swei, NASA Ames Research Phase Finite-Dimensional Systems Nonlinear Smooth Feedback A. Simpson, C. Sabo, University of C. Sabo, A. Cope, K. Gurney, E. Vasilaki, J. Investigating Spatial Phenomena Method. Center, Moffett Field, CA M. Balas, Embry-Riddle Aeronautical University, Regulators and Neural Network Sheffield, Sheffield, United Kingdom Marshall, University of Sheffield, Sheffield, G. Keller, S. Hening, S. Song, M. Teodorescu, S. Swei, N. Nguyen, NASA Ames Research Daytona Beach, FL; S. Frost, NASA Ames with Nonlinear Observers United Kingdom University of California, Santa Cruz, Santa Center, Moffett Field, CA Research Center, Moffett Field, CA J. Dongmo, JetMech.Inc., Parkville, MD Cruz, CA; B. Guillaume, N. Nguyen, NASA Ames Research Center, Moffett Field, CA; et al. Monday, 4 January 2016 84-ISC-3 International Student Conference -Team Category Torrey Hills B Chaired by: S. CORBETS, Lockheed Martin Corporation 1400 hrs 1430 hrs 1500 hrs 1530 hrs AIAA-2016-0405 AIAA-2016-0406 AIAA-2016-0407 AIAA-2016-0408 L1A Turbine Flow Characterization Design of an Engine Air Particle A Feasibility Experimanet of a Implementation of Flexible Matrix in a Cascade Facility with a T-Bar Separator for Unmanned Aerial Small Scale RTV-655 Cryogenic Composite Actuators into the eSPAARO Turbulence Generator Vehicle Applications Liquid Container for Space Unmanned Air Vehicle G. Gutkin, G. Whitener, Y. Wu, K. Rouser, J. Wolf, E. Shelley, D. Stralka, Cleveland Applications N. Beaty, M. Burns, C. MacNeal, G. Mohan, U.S. Air Force Academy, Colorado Springs, State University, Cleveland, OH D. Pumroy, D. Williams, W. Parker, K. Pyne, C. Weit, Virginia Polytechnic Institute CO University of Memphis, Memphis, TN and State University, Blacksburg, VA; et al. Monday, 4 January 2016 85-ISC-4 ISC-Community Outreach Category Torrey Hills A 1400 - 1530 hrs Atmospheric Teaching Experiment (ATex) - Year Four A Highly Effective Rocket-Based Outreach Program for Youth STEM Engagement Texas A&M Sigma Gamma Tau Community Outreach Daedalus Astronautics @ ASU: Outreach Program Paul S. Kennedy, Elaine C. Khuu, Matt Turk AJ Pollard Steven De Hoog, Michael Pierce, and Austin B. Probe Lauren Brunacini Virginia Polytechnic Institute and State University Auburn University Texas A&M University Arizona State University

Monday, 4 January 2016 86-LEC-2 SCS Lecture Harbor A 1400 - 1500 hrs

Technology Development and Infusion for the James Webb Telescope Sun Shield James Moore Division Vice President ManTech (NeXolve) Monday, 4 January 2016 87-MAT-3 Materials Testing & Characterization I Gaslamp B Chaired by: S. WANTHAL, The Boeing Company and J. RANSOM, NASA-Langley Research Center 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs AIAA-2016-0409 AIAA-2016-0410 AIAA-2016-0411 AIAA-2016-0412 AIAA-2016-0413 Investigating Sub-surface Interpreting High Temperature Computationally Intelligent Image Real Time In-Situ Sensing of Spin-Up Wear Analysis Microstructure in Fiber Reinforced Deformation Behavior of a Ceramic Processing Techniques for Crack Damage Evolution in Carbon through Experimental Testing and Polymer Composites via X-Ray Matrix Composite via High Energy Detection in Structural Components Nanotube-Polymer Nanocomposites Computational Modeling

Tomography Characterization X-rays and Numerical Simulation from Imaged Data under Impact Loading A. Zakrajsek, J. Childress, M. Bohun, U.S. Air R. Agyei, B. Sharma, M. Sangid, Purdue A. Manero, S. Sofronsky, University of D. Gillaugh, Air Force Research Laboratory, E. Sengezer, G. Seidel, Virginia Polytechnic Force, Wright-Patterson AFB, OH; S. Naboulsi, University, West Lafayette, IN Central Florida, Orlando, FL; K. Artzt, Wright-Patterson AFB, OH; J. Beck, Institute and State University, Blacksburg, Air Force Research Laboratory, Wright- S. Hackemann, J. Wischek, German Perceptive Engineering Analytics, Lino VA Patterson AFB, OH; R. Vogel, U.S. Air Force, Aerospace Center (DLR), Cologne, Lakes, MN; J. Brown, T. George, O. Scott- Wright-Patterson AFB OH; N. Lindsey, Air Force Germany; J. Okasinski, Argonne National Emuakpor, C. Holycross, Air Force Research Research Laboratory, Wright-Patterson AFB, Laboratory, Argonne, IL; et al. Laboratory, Wright-Patterson AFB, OH OH; et al. Monday, 4 January 2016 88-MDO-2 Design Space Exploration Balboa A Chaired by: T. TAKAHASHI, Arizona State University and B. STANFORD, NASA Langley Research Center 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs AIAA-2016-0414 AIAA-2016-0415 AIAA-2016-0416 AIAA-2016-0417 AIAA-2016-0418 AIAA-2016-0419 AIAA-2016-0420 An Evolutionary Multi-Architecture A Heuristic Approach to Finding Comparison of Adaptive Design Adaptive Model Refinement in Rapid Multi-Objective Aerodynamic Multi-Fidelity Aerodynamic Shape Aircraft Wing Optimization based Multi-Objective Optimization the Preferred Design Variable Space Exploration Methods Applied Surrogate-based Multiobjective Design Using Co-Kriging and Space Optimization Using Manifold on Computationally Efficient Algorithm for Design Space Parameterization for Optimization to S-Duct CFD Simulation Optimization Mapping Mapping Gradient-Enhanced Ordinary Kriging Exploration J. Sinsay, Army Aviation and Missile A. Garbo, B. German, Georgia Institute of S. Chowdhury, Mississippi State University, S. Koziel, Y. Tesfahunegn, Reykjavik J. Ren, L. Leifsson, Iowa State University, Metamodel Building C. Frank, R. Marlier, O. Pinon-Fischer, D. Research Development and Engineering Technology, Atlanta, GA Mississippi State, MS; A. Mehmani, University, Reykjavik, Iceland; A. Amrit, L. Ames, IA; S. Koziel, Y. Tesfahunegn, C. Mortished, J. Ollar, Altair Engineering, Inc., Mavris, Georgia Institute of Technology, Center, Moffett Field, CA; J. Alonso, Cornell University, Ithaca, NY; W. Tong, Leifsson, Iowa State University, Ames, IA Reykjavik University, Reykjavik, Iceland Leamington Spa, United Kingdom; V. Toropov, Atlanta, GA Stanford University, Stanford, CA Syracuse University, Syracuse, NY; A. Queen Mary University of London, London, Messac, Mississippi State University, United Kingdom; J. Sienz, Swansea University, Mississippi State, MS Swansea, United Kingdom Monday, 4 January 2016 89-MST-3 Modeling and Simulation of Air Traffic Management II Golden Hill A Chaired by: B. APONSO, NASA-Ames Research Center and S. BEARD, NASA-Ames Research Center 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2016-0421 AIAA-2016-0422 AIAA-2016-0423 AIAA-2016-0424 AIAA-2016-0425 AIAA-2016-0426 Using Airport Fast-Time Simulation Global Simulation of Aviation Validation Study on Descent Simulation Approach to the Next Generation Flight A Self-Separation Algorithm for Models to Increase the Quality of Operations Trajectory Optimization and Resilience Engineering Assessment Management System Simulator High-Density Air Corridor Allocated Airport Capacity Utilization Studies B. Sridhar, K. Sheth, NASA Ames Research Scheduling Improvement using of the ATM System in Crisis S. Park, V. Vaddi, J. Kwan, Optimal to Optimal Flight Trahectories C. Schinwald, Technical University of Center, Moffett Field, CA; H. Ng, A. Actual Operation Data Scenarios Synthesis, Inc., Los Altos, CA Y. Nakamura, Electronic Navigation Munich, Garching, Germany; K. Plötner, Morando, University of California, Santa N. Takeichi, Tokyo Metropolitan University, A. Errico, E. Filippone, R. Palumbo, D. Research Institute, Chofu, Japan; N. Bauhaus Luftfahrt e.V., Ottobrunn, Cruz, Moffett Field, CA; J. Li, SGT, Inc., Hino, Japan; J. Ishihara, Y. Abumi, Nagoya Pascarella, F. Gargiulo, Italian Aerospace Takeichi, Tokyo Metropolitan University, Germany; M. Hornung, Technical University Moffett Field, CA University, Nagoya, Japan Research Center (CIRA), Capua, Italy Hino, Japan of Munich, Garching, Germany Monday, 4 January 2016 90-NDA-1 Surrogate Modeling Approaches for Uncertainty Quantification and Reliability Estimation Old Town B Chaired by: J. BROWN and R. GRANDHI, Wright State University 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs AIAA-2016-0427 AIAA-2016-0428 AIAA-2016-0429 AIAA-2016-0430 AIAA-2016-0431 AIAA-2016-0432 AIAA-2016-0433 Sensitivity Analysis-Based Engineering Design Exploration A Set of Test Problems and Results Surrogate Modeling of Full-Field Application of Interval Predictor A Comparison of Metamodeling Sparse polynomial surrogates for Surrogate Modeling of Limit States Utilizing Locally-Optimized in Assessing Method Performance Pressure Measurements from Models to Space Radiation Techniques via Numerical aerodynamic computations with Z. Hu, S. Mahadevan, Vanderbilt Covariance Kriging for Calculating Low Probabilities Supersonic Wind Tunnel Experiments Shielding Experiments random inputs University, Nashville, TN D. Clark, H. Bae, Wright State University, of Failure G. Bartram, R. Perez, Universal Technology L. Crespo, S. Kenny, D. Giesy, R. Norman, L. Crespo, S. Kenny, D. Giesy, NASA E. Savin, A. Resmini, J. Peter, ONERA, Dayton, OH V. Romero, L. Swiler, M. Ebeida, S. Corporation, Dayton, OH; B. Smarslok, Air S. Blattnig, NASA Langley Research Center, Langley Research Center, Hampton, VA Châtillon, France Mitchell, Sandia National Laboratories, Force Research Laboratory, Wright-Patterson Hampton, VA AFB, OH

Albuquerque, NM Monday, 4 January 2016 91-PANEL-2 Monday Afternoon Forum 360 Seaport F-G 1400 - 1600 hrs Research Enabling and Enabled by a Cis-Lunar One-year Mission Moderator: Michael Moloney, Director for Space and Aeronautics Space Studies Board Aeronautics and Space Engineering Board, National Academies of Sciences, Engineering, and Medicine Monday, 4 January 2016 92-PC-3 Combustion Diagnostics Harbor B Chaired by: A. CASWELL and A. STEINBERG, University of Toronto 1400 hrs 1430 hrs 1500 hrs 1530 hrs AIAA-2016-0434 AIAA-2016-0435 AIAA-2016-0436 AIAA-2016-0437 Measurements of Hydrocarbon Measurements of Turbulent Swirl Evaluation of Gappy Proper DSMC Simulations of a Absorbance at High Temperatures Flame Dynamics in an Ethylene- Orthogonal Decomposition for Gas Photoionization Mass Spectrometer and Pressures fuelled Gas Turbine Model Combustor Turbine Combustor Flows Q. Guan, G. Ellison, J. Daily, University D. Maqbool, C. Cadou, University of at Elevated Pressure P. Saini, Q. An, A. Steinberg, University of of Colorado, Boulder, Boulder, CO; J. Maryland, College Park, College Park, MD I. Boxx, German Aerospace Center (DLR), Toronto, Toronto, Canada Stanton, University of Texas, Austin, Stuttgart, Germany; C. Carter, Air Force Austin, TX; M. Ahmed, Lawrence Berkeley Research Laboratory, Wright-Patterson AFB, National Laboratory, Berkeley, CA OH; K. Geigle, W. Meier, German Aerospace Center (DLR), Stuttgart, Germany Monday, 4 January 2016 93-PC-4 Detonations, Explosions, and Supersonic Combustion Harbor C Chaired by: R. PITZ, Vanderbilt University and T. OMBRELLO, Air Force Research Laboratory 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2016-0438 AIAA-2016-0439 AIAA-2016-0440 AIAA-2016-0441 AIAA-2016-0442 AIAA-2016-0443 Diffusion-Flame Ignition by Large-Eddy Simulation of Cheng’s Growth Rate and Flame Structure Investigation of Flame Structure Effect of Elevated Mixture Fluidic Jet Augmentation of a Shock-Wave Impingement on a Supersonic Burner of Turbulent Premixed Flame and Combustion Dynamics using Pressure and Equivalence Ratio on Deflagrated Turbulent Flame for G. Ribert, L. Bouheraoua, P. Domingo, Hydrogen-Air Supersonic Mixing Kernels in Supersonic Flows CH2O PLIF and High-Speed CH* Hydrogen-Air Detonation Cell Size Deflagration-to-Detonation Layer National Center for Scientific Research B. Ochs, D. Fries, D. Scarborough, S. Chemiluminescence in a Premixed C. Babbie, P. King, Air Force Institute of J. Chambers, J. McGarry, K. Ahmed, A. Sanchez, C. Huete, F. Williams, (CNRS), Rouen, France Menon, Georgia Institute of Technology, Dual-Mode Scramjet Combustor Technology, Wright-Patterson AFB, OH; J. University of Central Florida, Orlando, FL University of California, San Diego, La Atlanta, GA P. Allison, K. Frederickson, Ohio State Hoke, Innovative Scientific Solutions, Inc., Jolla, CA University, Columbus, OH; J. Kirik, R. Dayton, OH; F. Schauer, Air Force Research Rockwell, University of Virginia, Charlottesville, Laboratory, Wright-Patterson AFB, OH Charlottesville, VA; W. Lempert, J. Sutton, Ohio State University, Columbus, OH Monday, 4 January 2016 94-PC-5 High-Pressure Combustion, Fuel Technology Cortez Hill C Chaired by: L. SMITH, United Technologies Research Center and K. MCMANUS, GE Global Research Center 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs AIAA-2016-0444 AIAA-2016-0445 AIAA-2016-0446 AIAA-2016-0447 AIAA-2016-0448 AIAA-2016-0449 AIAA-2016-0450 Numerical Simulations of Cool Counterflow Analysis for Experimental Studies of a Low Temperature Autoignition Fuel effects on the performance Quasi-State-Specific QCT Method Comparison of Alternative Jet Flame Propagation Limits and Combustion at High Pressure High-g Ultra-Compact Combustor Behavior of Surrogate Jet Fuels of a recirculation-zone supported for Calculating the Dissociation Fuel Lean Blowouts for Bluff-Body Speeds at Elevated Pressures A. Jorda Juanos, P. Popov, W. Sirignano, at Elevated Pressures and with Targeted Properties in a Rapid burner Rate of Nitrogen in Thermal Non- Stabilized Flames Y. Ju, C. Reuter, Princeton University, University of California, Irvine, Irvine, CA Temperatures Compression Machine V. Katta, Innovative Scientific Solutions, Equilibrium B. Huelskamp, Innovative Scientific

Princeton, NJ T. Erdmann, D. Burrus, Innovative D. Valco, K. Min, A. Oldani, University of Inc., Dayton , OH; W. Roquemore, Air S. Voelkel, University of Texas, Austin, Solutions, Inc., Dayton, OH; J. Monfort, Scientific Solutions, Inc., Dayton, OH; D. Illinois, Urbana-Champaign, Urbana, IL; J. Force Research Laboratory, Wright- Austin, TX; V. Raman, University of University of Dayton, Dayton, OH; B. Kiel, Shouse, J. Gross, C. Neuroth, A. Caswell, Edwards, Air Force Research Laboratory, Patterson AFB, OH Michigan, Ann Arbor, Ann Arbor, MI; P. C. Neuroth, A. Caswell, Air Force Research Air Force Research Laboratory, Wright- Wright-Patterson AFB, OH; T. Lee, University of Varghese, University of Texas, Austin, Laboratory, Wright-Patterson AFB, OH Patterson AFB, OH Illinois, Urbana-Champaign, Urbana, IL Austin, TX Monday, 4 January 2016 95-PDL-3 Plasma Based Flow Control Ocean Beach Chaired by: T. MCLAUGHLIN, US Air Force Academy and J. POGGIE, Purdue University- Sch of Aero and Astro 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2016-0451 AIAA-2016-0452 AIAA-2016-0453 AIAA-2016-0454 AIAA-2016-0455 AIAA-2016-0456 Properties of Multi-Spark Plasma Experimental Investigation of Ignition, Sustained Flame, and Plasma Assisted Turbulent Flow Active Control of a Turbulent Exposed-Electrode Geometry Discharge Developed for Flow Dynamic Stall in a Wide Range Extinction of a Dielectric-Barrier- Separation control over a Backward Mixing Layer using Pulsed Laser Effects on DBD Plasma Actuation Control of Mach Numbers by Plasma Discharge Altered Hydrogen Jet in Facing Step and Pulsed Plasma over Conical Forebody V. Boretskij, A. Veklich, S. Fesenko, Actuators with Combined Energy/ a Cross-Flow A. das Gupta, P. Zhao, S. Roy, University A. Singh, J. Little, University of Arizona, D. Zhang, X. Meng, H. Hu, J. Wang, A. Lebid, Taras Shevchenko National Momentum Action R. Fontaine, J. Retter, J. Freund, N. of Florida, Gainesville, Gainesville, FL Tucson, Tucson, AZ Northwestern Polytechnical University, University of Kyiv, Kyiv, Ukraine A. Starikovskiy, R. Miles, Princeton Glumac, G. Elliott, University of Illinois, Xi’an, China; F. Liu, S. Luo, University of University, Princeton, NJ Urbana-Champaign, Urbana, IL California, Irvine, Irvine, CA Monday, 4 January 2016 96-PDL-4 Laser Discharge and Applications Cortez Hill A Chaired by: S. MACHERET, Purdue University 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs AIAA-2016-0457 AIAA-2016-0458 AIAA-2016-0459 AIAA-2016-0460 AIAA-2016-0461 Launch capability of a conceptual Schlieren imaging investigation of Trajectory Control of Small Rotating Laser Thermal Ignition Using a Femtosecond laser discharge and laser-launch system of a spherical successive laser-induced breakdowns Projectiles by Laser Sparks Dual-Pulse Approach small scale turbulence vehicle and a dunut-mode beam in quiescence atmospheric air A. Starikovskiy, C. Limbach, R. Miles, C. Dumitrache, A. Yalin, Colorado State A. Tropina, National University, Kharkov, K. Mori, R. Maruyama, Nagoya University, L. Wermer, S. Im, Worcester Polytechnic Princeton University, Princeton, NJ University, Fort Collins, CO Ukraine; M. Shneider, R. Miles, Princeton Nagoya, Japan Institute, Worcester, MA; M. Bak, University, Princeton, NJ Sungkyunkwan University, Suwon, South Korea Monday, 4 January 2016 97-SD-3 Reduced Order Modeling I Balboa C Chaired by: N. FALKIEWICZ, MIT Lincoln Laboratory and B. GLAZ, U. S. Army Research Laboratory (APG) 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs AIAA-2016-0462 AIAA-2016-0463 AIAA-2016-0464 AIAA-2016-0465 AIAA-2016-0466 Reduced Order Modeling of Highly Model Reduction of Unsteady Flows Reduced Order Models for Efficiency Enhancement of Reduced Reduced-Order Modeling of Flow- Unsteady Flows Using Adaptive using Sparse Coding: Efficient Basis Generation of Large, High Speed Order Model using Variable Fidelity Induced Vibrations in Bellows Joints of Sparse Bases Extraction from Large Datasets Aerodynamic Databases with Jet Modeling Rocket Propulsion Systems R. Deshmukh, Z. Liang, J. McNamara, Z. Liang, R. Deshmukh, J. McNamara, Interactions S. Lee, T. Kim, National University of S. Higgins, R. Davis, University of Georgia, Ohio State University, Columbus, OH Ohio State University, Columbus, OH A. Vanderwyst, A. Shelton, C. Martin, L. Singapore, Singapore, Singapore; S. Jun, Athens, Athens, GA; A. Brown, NASA Marshall Neergaard, Z. Witeof, Leidos Corporation, K. Yee, Seoul National University, Seoul, Space Flight Center, Huntsville, AL Fort Walton Beach, FL South Korea Monday, 4 January 2016 98-SD-4 Dynamic Loads, Response, and Vibration I Gaslamp A Chaired by: T. KINNEY, NASA-Kenndey Space Center and Z. SOTOUDEH, Rensselaer Polytechnic Institute 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs AIAA-2016-0467 AIAA-2016-0468 AIAA-2016-0469 AIAA-2016-0470 AIAA-2016-0471 AIAA-2016-0472 AIAA-2016-0473 Aeroelastic Response of the ACTE Dynamic Behavior of Initially- Dynamic Response of The Influence of Wing Flexibility Damped Free Vibration Response of Impact of the Wing Sweep Angle and Energy Based Representations Transition Section Stressed and Post-Buckled Aeroelastically Tailored Composite on the Stability of a Biomimetic An Adhesively Bonded Stiffened Plate Rib Orientation on Wing Structural of Mechanical Shock for Failure C. Herrera, N. Spivey, S. Lung, NASA Laminated Composite Beams Wing: Analysis and Experiment Flapping Wing Micro Air Vehicle with Plate-Strip Stiffeners Response for Un-Tapered Wings Characterization Armstrong Flight Research Center, J. Kosmatka, University of California, San J. Sodja, N. Werter, M. Natella, Delft in Hover N. Ahmad, R. Kapania, Virginia Polytechnic G. Francois, J. Cooper, P. Weaver, University of V. Babuska, C. Sisemore, J. Booher, Edwards, CA; G. Ervin, FlexSys, Inc., Ann Diego, La Jolla, CA University of Technology, Delft, The J. Bluman, M. Sridhar, C. Kang, University Institute and State University, Blacksburg, VA Bristol, Bristol, United Kingdom Sandia National Laboratories, Arbor, MI; P. Flick, Air Force Research Netherlands ; J. Dillinger, German of Alabama, Huntsville, Huntsville, AL Albuquerque, NM Laboratory, Wright-Patterson AFB, OH Aerospace Center (DLR), Göttingen, Germany; R. De Breuker, Delft University of Technology, Delft, The Netherlands Monday, 4 January 2016 99-SE-2 Systems Engineering II La Jolla B Chaired by: D. DRESS, NASA Langley Research Center 1400 hrs 1430 hrs 1500 hrs AIAA-2016-0474 AIAA-2016-0475 AIAA-2016-0476 Resilience Analysis for Complex Resilient Multi-UAV Operation: Key Agent-Based Flexible Design Contracts Supply Chain Systems Using Concepts and Challenges for Resilient Spacecraft Swarms Bayesian Networks E. Ordoukhanian, A. Madni, University of M. Sievers, Jet Propulsion Laboratory, N. Yodo, P. Wang, Wichita State Southern California, Los Angeles, CA California Institute of Technology, Pasadena, University, Wichita, KS CA; A. Madni, University of Southern California, Los Angeles, CA Monday, 4 January 2016 100-SEO-2 Innovative Ideas for Exploring and Operating Space Missions Americas Cup A Chaired by: L. BRYANT, Jet Propulsion Laboratory and S. BURLEIGH, Jet Propulsion Laboratory 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2016-0477 Oral Presentation AIAA-2016-0478 AIAA-2016-0479 AIAA-2016-0480 AIAA-2016-0481

ASTROSAT - Overview and Technical Adaptive Control Strategy of Transfer trajectory design about A GNC Perspective of the Launch Study of Optimal Transfers from L2 Electromagnetic Propulsion system Architecture of India’s First Space Exploration Rover with Potential doubly synchronous binary and Commissioning of NASA’s New Halo-orbits to Lunar Surface for spacecrafts using geomagnetic Observatory Function Method system SMAP (Soil Moisture Active Passive) Y. Ulybyshev, RSC Energia, Korolev, Russia fields and superconductors. V. Sundararajan, Aerospace India, R. Hatori, Japan Society for Aeronautical and X. Wu, H. Shang , X. Qin, Beijing Institute Spacecraft A. Dadhich, University of Cincinnati, Research Triangle Park, NC Space Sciences, Tokyo, Japan; K. Shibuya, K. of Technology, Beijing, China T. Brown, Jet Propulsion Laboratory, California Cincinnati, OH Uchiyama, Nihon University, Funabashi, Japan Institute of Technology, Pasadena, CA Monday, 4 January 2016 101-SOF-3 Software Challenges in Aerospace Symposium Regatta A Chaired by: J. MURPHY, NASA -Ames Research Center 1400 hrs 1430 hrs 1500 hrs AIAA-2016-0482 AIAA-2016-0483 AIAA-2016-0484 Applying Machine Learning for Soft Computing in Aerospace Towards Generic Requirements Run-time Bug Detection in Aviation F. Briggs, Self, Solomons, MD and Models for Automated Mission Software Tasks with RPAS H. Huang, S. Guyer, J. Rife, Tufts C. Torens, F. Adolf, German Aerospace University, Medford, MA Center (DLR), Braunschweig, Germany; G. Patil, G. Vernekar, Technical University of Chemnitz, Chemnitz, Germany

Monday, 4 January 2016 102-STR-3 Aircraft Structural Design II La Jolla A Chaired by: H. HILTON, University of Illinois at Urbana-Champaign and M. SENSMEIER, Embry-Riddle Aeronautical University 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2016-0485 AIAA-2016-0486 AIAA-2016-0487 AIAA-2016-0488 AIAA-2016-0489 AIAA-2016-0490 Parameterization Framework for Analysis of Designer / Tailored Design and structural analysis of Effects of Shallow-Angle, Thin- Optimization, Manufacturing and Thermal Response of a Spatially Aeroelastic Design Optimization of Linear Aero-Piezo-Viscoelastic unique structures under an internal Ply Laminates on the Structural Testing of a Composite Wing with Graded Metal-Ceramic Structural Bio-Inspired Wing Structural Layout Energy Harvesting vacuum Performace of Composite Wing Maximized Tip Deflection Panel to Non-Uniform Heating in A. Dubois, C. Farhat, Stanford University, H. Hilton, Y. Saito, University of Illinois, B. Cranston, A. Palazotto, Air Force N. Kimber, J. Tian, S. Thielk, P. Chang, Y. Meddaikar, J. Dillinger, German Aerospace Hypersonic Flow Stanford, CA; A. Abukhwejah, King Urbana-Champaign, Urbana, IL Institute of Technology, Wright-Patterson S. Ko, W. Lay, University of Washington, Center (DLR), Göttingen, Germany; J. Sodja, P. Deierling, O. Zhupanska, University Abdulaziz City for Science and Technology, AFB, OH Seattle, Seattle, WA; et al. Delft University of Technology, Delft, The of Iowa, Iowa City, Iowa City, IA; C. Riyadh, Saudi Arabia Netherlands ; H. Mai, German Aerospace Pasiliao, Air Force Research Laboratory, Center (DLR), Göttingen, Germany; R. De Eglin AFB, FL Breuker, Delft University of Technology, Delft, The Netherlands Monday, 4 January 2016 103-TES-3 Fluids and Combustion in Power Systems Old Town A Chaired by: G. JACOBS, San Diego State Univ and F. MASHAYEK, University of Illinois at Chicago 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs AIAA-2016-0492 AIAA-2016-0493 AIAA-2016-0494 AIAA-2016-0495 AIAA-2016-0496 AIAA-2016-0497 AIAA-2016-0498 Comparative Study of Using Multi-Location Fuel Injection Effects Investigation of Heat Transfer and Numerical Investigation of PEM Thermal Field Investigation under Large Eddy Simulation of a Investigation of Alumina Flow Streamlined Bodies as a Passive on NO*/OH* Chemiluminescence in Fluid Mechanics across a Heated Fuel Cell Performance in an Aircraft Distributed Combustion Conditions Supersonic Underexpanded Jet Breakup Process in Solid Rocket Enhancer in Combustor Dilution a High Intensity Combustor Rotating Circular Cylinder in Oxygen–Gas Oxidizer System A. Khalil Hasan, A. Gupta, University of with a High-order Hybrid Central/ Propulsion Chamber System A. Said, A. Gupta, University of Maryland, Crossflow K. Okai, T. Himeno, T. Watanabe, University of Maryland, College Park, College Park, MD WENO-Z Scheme Y. Yen, R. Amano, University of Wisconsin, R. Amano, T. ElHammal, University of College Park, College Park, MD O. Fatta, G. Smaisim, N. Syred, A. Valera- Tokyo, Tokyo, Japan; Y. Yachi, IHI Corporation, D. Quimby, G. Jacobs, San Diego State Milwaukee, Glendale, WI Wisconsin, Milwaukee, Glendale, WI Medina, A. Rageb, Cardiff University, Tokyo, Japan; N. Shinozaki, IHI Aerospace University, San Diego, CA Cardiff, United Kingdom CO., Ltd., Gunma, Japan Monday, 4 January 2016 104-TP-3 Non-Equilibrium Flows, Non-Equilibrium Radiation and Rarefied Flows I Harbor G Chaired by: J. BURT, Universal Technology Corporation and R. GOSSE, WPAFB 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs AIAA-2016-0499 AIAA-2016-0500 AIAA-2016-0501 AIAA-2016-0502 AIAA-2016-0503 AIAA-2016-0504 AIAA-2016-0505 Entropy Production Analysis of Ab initio based model for high Study of Shock-Shock Interactions Molecular Dynamics Studies of Comparison of quantum Effect of reagent energy on State-to-State and reduced-order Burnett Equations Using Classical temperature nitrogen rovibrational Using an Unstructured AMR Octree Nitrogen collision on Graphene and mechanical and empirical potential nonequilibrium O2+O dissociation models for dissociation and Thermodynamics with Gibbs excitation and dissociation DSMC Code Quartz Surfaces energy surfaces and computed rate M. Kulakhmetov, M. Gallis, Purdue energy transfer in aerothermal P. Valentini, T. Schwartzentruber, I. S. Sawant, O. Tumuklu, University of N. Mehta, D. Levin, University of Illinois, University, West Lafayette, IN; A. Equations coefficients for N2 dissociation environments H. Liu, W. Chen, W. Zhao, Zhejiang Nompelis, G. Candler, University of Illinois, Urbana-Champaign, Urbana, IL; Urbana-Champaign, Urbana, IL R. Jaffe, D. Schwenke, NASA Ames Alexeenko, Sandia National Laboratories, A. Munafò, R. Macdonald, M. Panesi, University, Hangzhou, China; R. Agarwal, Minnesota, Minneapolis, Minneapolis, MN B. Korkut, Pennsylvania State University, Research Center, Moffett Field, CA; S. Albuquerque, NM University of Illinois, Urbana-Champaign, Washington University in St. Louis, St. University Park, PA; D. Levin, University of Venturi, M. Panesi, University of Illinois, Urbana, IL Louis, MO Illinois, Urbana-Champaign, Urbana, IL Urbana-Champaign, Urbana, IL; M. Grover, T. Schwartzentruber, University of Minnesota, Minneapolis, Minneapolis, MN Monday, 4 January 2016 105-TP-4 Heat Transfer: Conduction, Convection, Phase Change, Radiation, and Conjugate Heat Transfer Harbor H Chaired by: K. POPE, Memorial University of Newfoundland and E. SHORT, Raytheon Company 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2016-0506 AIAA-2016-0507 AIAA-2016-0508 AIAA-2016-0509 AIAA-2016-0510 AIAA-2016-0511 Inviscid-flow approximation of Limits for Thermionic Emission Analysis of Internal Thermocouple Heat Transport in Aqueous An Experimental Investigation Simulation of Steady Two- radiative ablation of asteroidal from Leading Edges of Hypersonic Data in Carbon/Carbon Using Suspensions of Alumina on Unsteady Heat Transfer and Dimensional Heat Transfer in meteoroids by line-by-line method. Vehicles Inverse Heat Conduction Methods Nanoparticles Transient Icing Process upon Rectangular Micro-Cavities at C. Park, Korea Advanced Institute of Science K. Hanquist, I. Boyd, University of M. Pizzo, Old Dominion University, M. Muraleedharan, D. Sundaram, V. Impingement of Water Droplets Elevated Pressures

and Technology, Daejeon, South Korea Michigan, Ann Arbor, Ann Arbor, MI Norfolk, VA; D. Glass, K. Bey, NASA Yang, Georgia Institute of Technology, H. Li, R. Waldman, H. Hu, Iowa State M. Martin, P. Kumar, Louisiana State Langley Research Center, Hampton, VA Atlanta, GA University, Ames, IA University, Baton Rouge, LA Monday, 4 January 2016 106-UMS-2 Unmanned Systems - Flight Dynamics and Control Regatta C Chaired by: J. JACOB, Oklahoma State University and R. PRAZENICA, Embry-Riddle Aeronautical University, Daytona Beach 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs AIAA-2016-0512 AIAA-2016-0513 AIAA-2016-0514 AIAA-2016-0515 AIAA-2016-0516 Non-linear Model Predictive Control Lateral-Directional Stability of the Dynamic Model of 25% Yak-54 Autonomous Formation Flight Longitudinal Control Considering for Longitudinal and Lateral Near-space Solar-powered Aircraft Unmanned Aerial System of Indoor UAVs Based on Model Trim of Outdoor Blimp Robots for Guidance of a Small Fixed-Wing Y. Chuan, L. Feng, L. Guangjia, Y. R. LaRue, S. Thomas, I. Costa, W. Liu, Predictive Control Disaster Surveillance UAV in Precision Deep Stall Landing Wang, China Academy of Aerospace C. Yeo, University of Kansas, Lawrence, S. Mao, W. Tan, K. Low, Nanyang H. Saiki, National Research Institute of S. Mathisen, K. Gryte, T. Johansen, T. Aerodynamics, Beijing, China Lawrence, KS Technological University, Singapore, Fire and Disaster, Tokyo, Japan Fossen, Norwegian University of Science Singapore and Technology, Trondheim, Norway Monday, 4 January 2016 107-WE-1 Wind Energy: Wind Turbine Aerodynamics Improvements and Analysis Harbor I Chaired by: J. NAUGHTON, University of Wyoming and M. CHURCHFIELD, National Renewable Energy Laboratory 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2016-0517 AIAA-2016-0518 AIAA-2016-0519 AIAA-2016-0520 AIAA-2016-0521 AIAA-2016-0522 Study of Drag Reduction Devices on Application of Vortex Generators to Effects of Mie Vanes and Tip Prediction and Analysis of the Interaction of Atmospheric Turbulence Experimental study of near and far a Flatback Airfoil Wind Turbine Blades Injection on the Performance and Nonsteady Transitional Boundary with Blade Boundary Layer Dynamics wake generated by a Gurney mini M. Manolesos, G. Papadakis, S. Voutsinas, Q. Tian, Frontier Wind, Rocklin, CA; D. Wake Characteristics of a HAWT Layer Dynamics for flow over an on a 5MW Wind Turbine using Blade- flap in turbulent flow National Technical University of Athens, Corson, Altair Engineering, Inc., Malta, NY; A. Abdulrahim, E. Anik, O. Uzol, Middle Oscillating Wind Turbine Airfoil boundary-layer-resolved CFD with J. Delnero, J. Marañón Di Leo, M. Garcia Athens, Greece J. Baker, Frontier Wind, Rocklin, CA East Technical University, Ankara, Turkey using the -Re Transition Model hybrid URANS-LES Sainz, National University of La Plata, La T. Nandi, J. Brasseur, G. Vijayakumar, G. Vijayakumar, J. Brasseur, A. Lavely, B. Plata, Argentina Pennsylvania State University, University Jayaraman, B. Craven, Pennsylvania State Park, PA University, University Park, PA Monday, 4 January 2016 108-NW-4 Monday Afternoon Networking Coffee Break Session Room Foyers 1530 - 1600 hrs Monday, 4 January 2016 109-PANEL-3 SCS: Infusing New Structures Technology Into Space Systems Harbor A 1530 - 1730 hrs Moderators: W. Keith Belvin, NASA Langley Research Center, Greg Agnes, Jet Propulsion Laboratory, California Institute of Technology Monday, 4 January 2016 110-LEC-3 The Future of AIAA: Why Governance Matters to You Seaport A-E 1730 - 1830 hrs James F. Albaugh President AIAA Monday, 4 January 2016 111-NW-5 Rising Leaders Reception Seaport H 1830 - 1930 hrs Tuesday Tuesday, 5 January 2016 112-NW-6 Tuesday Early Morning Networking Coffee Break Session Room Foyers 0700 - 0730 hrs Tuesday, 5 January 2016 113-SB-2 Tuesday Morning Speakers’ Briefing Session Rooms 0730 - 0800 hrs Tuesday, 5 January 2016 114-PLNRY-2 Tuesday Morning Plenary Panel Seaport A-E 0800 - 0900 hrs Aerospace Generations – Lessons Learned from a Half Century of Innovation in Aerospace Technology Moderator: Mason Peck, Associate Professor, Sibley School of Mechanical and Aerospace Engineering, Cornell University

Panelists: Hans Mark Zac Manchester Mary Popp Professor Emeritus Postdoctoral Fellow, Agile Robotics Laboratory Propulsion Engineer U.S. Air Force (ret.) The University of Texas, Austin Harvard University Lockheed Martinn Corporation Tuesday, 5 January 2016 115-AA-3 Aeroacoustics - Jet Noise II Nautical Chaired by: C. BROWN, NASA Glenn and D. NARK, NASA Langley Research Center 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2016-0523 AIAA-2016-0524 AIAA-2016-0525 AIAA-2016-0526 AIAA-2016-0527 AIAA-2016-0528 Quiet Nozzle Concepts for Three- Correlation of events between Acoustic Signature of a Supersonic A Comparison of the Aeroacoustic Flow and Acoustic Features of a Hybrid Approach to Nonlinear Stream Jets near- and far-field of a 3-stream Jet Emanating from a Rectangular Characteristics of Free and Mach 0.9 Jet Using High Frequency Propagation of Jet Noise in D. Papamoschou, V. Phong, J. Xiong, supersonic nozzle C-D Nozzle Impinging Jets with Noise Excitation Complex Environments F. Liu, University of California, Irvine, J. Lewalle, M. Glauser, Syracuse H. Hafsteinsson, N. Andersson, Chalmers Reduction Techniques P. Upadhyay, G. Valentich, F. Alvi, Florida V. Sassanis, A. Sescu, E. Collins, Irvine, CA University, Syracuse, NY; S. Gogineni, C. University of Technology, Göteborg, S. Hromisin, L. Myers, D. McLaughlin, State University, Tallahassee, FL Mississippi State University, Starkville, Ruscher, Spectral Energies, LLC, Dayton, Sweden; B. Malla, E. Gutmark, University P. Morris, Pennsylvania State University, MS; R. Harris, CFD Research Corporation, OH; B. Kiel, Air Force Research Laboratory, of Cincinnati, Cincinnati, OH University Park, PA Huntsville, AL; E. Luke, Mississippi State Wright-Patterson AFB, OH University, Starkville, MS Tuesday, 5 January 2016 116-ABPSI-3 Inlets Golden Hill B Chaired by: E. LOTH, University of Virginia 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2016-0529 AIAA-2016-0530 AIAA-2016-0531 AIAA-2016-0532 AIAA-2016-0533 AIAA-2016-0534 Numerical Investigation on Two SUPIN: A Computational Tool for Interpolation Methods for Inlet Mass Flow Ratio Influence on Shock Measurements of Fan Response An overview of recent results Streamline-Traced Busemann Inlet- Supersonic Inlet Design Distortion Determination and Pressure Spectra for a Low- to Inlet Total Pressure and Swirl using the StreamVane method for Isolators J. Slater, NASA Glenn Research Center, S. Walter, R. Starkey, University of Boom Supersonic Inlet Distortions Produced by Boundary generating tailored swirl distortion F. Xing, Y. Huang, X. Fang, Xiamen Cleveland, OH Colorado, Boulder, Boulder, CO E. Loth, S. Candon, University of Virginia, Layer Ingesting Aircraft Configurations in jet engine research University, Xiamen, China; Y. Yao, Charlottesville, Charlottesville, VA; M. D. Frohnapfel, A. Ferrar, J. Bailey, W. O’Brien, T. Guimaraes Bucalo, K. Lowe, W. O’Brien, University of the West of England, Bristol, Rybalko, University of Illinois, Urbana- K. Lowe, Virginia Polytechnic Institute and Virginia Polytechnic Institute and State United Kingdom Champaign, Urbana, IL

State University, Blacksburg, VA University, Blacksburg, VA Tuesday, 5 January 2016 117-ACD-1 Aircraft Design Issues I Cortez Hill A Chaired by: D. CARTER, Air Force Research Laboratory and D. BENCHERGUI, Bombardier Inc 0900 hrs 0930 hrs 1000 hrs AIAA-2016-0535 AIAA-2016-0536 AIAA-2016-0537 Legacy Aircraft Drag Reduction Planning Technology Development Aircraft Design as a Tool in Achieving D. Carter, Air Force Research Laboratory, Experimentation through Educational Objectives for Engineering Wright-Patterson AFB, OH Quantitative Uncertainty Analysis Concepts in a Core Curriculum K. Gatian, D. Mavris, Georgia Institute of R. Cummings, S. Reed, A. Rolling, S. Brandt, Technology, Atlanta, GA U.S. Air Force Academy, Colorado Springs, CO Tuesday, 5 January 2016 118-AFM-5 Launch Vehicle, Missile, and Projectile Flight Mechanics I Cortez Hill B Chaired by: B. BURCHETT, Rose-Hulman Institute of Technology and B. JOLLY, US Air Force 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2016-0538 AIAA-2016-0539 AIAA-2016-0540 AIAA-2016-0541 AIAA-2016-0542 Projectile Parameter Estimation Euler-Lagrange Optimal Control of Performance Optimization of Coning Motion Instability of Empirical Mode Decomposition Using Meta-Optimization Indirect Fire Symmetric Projectiles Guided Projectiles Using Design of a Spinning Missile Induced by Filtering of Wind Profiles M. Gross, M. Costello, Georgia Institute of A. Nash, B. Burchett, Rose-Hulman Experiments Aeroelasticity B. Sako, The Aerospace Corporation, El Technology, Atlanta, GA Institute of Technology, Terre Haute, IN L. Fowler, J. Rogers, Georgia Institute of S. Zhongjiao, L. Zhao, J. Peng, Beijing Segundo, CA Technology, Atlanta, GA Institute of Technology, Beijing, China Tuesday, 5 January 2016 119-APA-11 Special Session: Space Launch System (SLS) Induced Environments I Coronado D Chaired by: J. BLEVINS, NASA Marshall Space Flight Center and J. PINIER, NASA Langley Research Center 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2016-0543 AIAA-2016-0544 AIAA-2016-0545 AIAA-2016-0546 AIAA-2016-0547 AIAA-2016-0548 Overview of the Space Launch Sensitivity of Space Launch System Effect of Surface Pressure Space Launch System Base Heating Space Launch System Base Heating Space Launch System Base System Ascent Aeroacoustic Buffet Forcing Functions to Buffet Integration Methodology on Launch Test: Experimental Operations and Test: Environments and Base Flow Heating Test: Tunable Diode Laser Environment Test Program Mitigation Options Vehicle Buffet Forcing Functions Results Physics Absorption Spectroscopy A. Herron, W. Crosby, D. Reed, NASA D. Piatak, M. Sekula, R. Rausch, NASA M. Sekula, D. Piatak, R. Rausch, NASA A. Dufrene, CUBRC, Buffalo, NY; M. M. Mehta, NASA Marshall Space Flight Center, R. Parker, Z. Carr, A. Dufrene, CUBRC, Marshall Space Flight Center, Huntsville, Langley Research Center, Hampton, VA Langley Research Center, Hampton, VA Mehta, NASA Marshall Space Flight Huntsville, AL; A. Dufrene, CUBRC, Buffalo, Buffalo, NY; M. Mehta, NASA Marshall AL Center, Huntsville, AL; M. MacLean, NY; M. Seaford, K. Knox, NASA Marshall Space Flight Center, Huntsville, AL CUBRC, Buffalo, NY; M. Seaford, NASA Space Flight Center, Huntsville, AL Marshall Space Flight Center, Huntsville, AL; M. Holden, CUBRC, Buffalo, NY Tuesday, 5 January 2016 120-APA-12 Applied CFD & Numerical Correlations with Experimental Data I Americas Cup B Chaired by: J. SLOTNICK, Boeing Engineering Operations & Technology and C. KIRIS, NASA Ames Research Center 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2016-0549 AIAA-2016-0550 AIAA-2016-0551 AIAA-2016-0552 AIAA-2016-0553 AIAA-2016-0554 AIAA-2016-0555 Simulation of ONERA M6 Wing Inflow Turbulence Effects on A Comparison of Transition Dynamic Stability Analysis of Comparison of Drag Prediction Application of Hybrid Turbulence High Fidelity, High Order, Large Eddy Flows for Assessment of Turbulence Transition Prediction Using a Prediction Methodologies Applied a Reentry Lifting Capsule with Using RANS models and DDES for Method to Transonic Flowfield of a Simulations of a Real Geometry Modeling Capabilities Correlation-Based Transition Model to High Reynolds Number External Detached Eddy Simulation the DLR-F6 Configuration Using Payload Fairing Aircraft Nose Landing Gear on Hybrid R. Silva, J. Azevedo, E. Basso, Aeronautics G. Halila, E. Bigarella, A. Antunes, Flows A. Hashimoto, K. Murakami, T. Aoyama, High Order Schemes S. Tsutsumi, R. Takaki, S. Koike, Japan Unstructured Meshes & Small-scale and Space Institute (IAE), São José dos , São José dos Campos, Brazil; J. C. Langel, R. Chow, C. Van Dam, R. Tagai, S. Koga, S. Nagai, Japan J. Gan, University of Miami, Miami, FL; Aerospace Exploration Agency (JAXA), Many-core Computing System Campos, Brazil Azevedo, Aeronautics and Space Institute Aerospace Exploration Agency (JAXA), Sagamihara, Japan; S. Teramoto, University of California, Davis, Davis, CA Y. Shen, Chinese Academy of Sciences, Y. Lu, A. Demargne, Cambridge Flow Solutions (IAE), São José dos Campos, Brazil Chofu, Japan; et al. Beijing, China; G. Zha, University of University of Tokyo, Hongo, Japan Ltd, Cambridge, United Kingdom; K. Liu, Miami, Miami, FL BoXeR Solutions KK, Kobe, Japan; W. Dawes, Cambridge University, Cambridge, United Kingdom Tuesday, 5 January 2016 121-APA-13 Aerodynamic Design: Analysis, Methodologies, and Optimization Techniques II Americas Cup C Chaired by: K. DENISSEN, Sandia National Labs and A. SCLAFANI, Boeing Commercial Airplanes 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2016-0556 AIAA-2016-0557 AIAA-2016-0558 AIAA-2016-0559 AIAA-2016-0560 AIAA-2016-0561 Part I: Uncertainty Analysis of Multifidelity Optimization for High- A Geometric Comparison of Aerofoil Progressive Subdivision Curves for Using surface sensitivity from mesh Prediction and Experimental Various Design Parameters on Lift Airfoils Shape Parameterisation Methods Aerodynamic Shape Optimisation adjoint solution for transonic wing Evaluation of Planar Wing Winglet Performance J. Demange, A. Savill, T. Kipouros, D. Masters, University of Bristol, Bristol, D. Masters, University of Bristol, Bristol, United drag reduction Spanloads for Minimum Drag J. Masud, Z. Toor, Air University, Cranfield University, Cranfield, United United Kingdom; N. Taylor, MBDA, Bristol, Kingdom; N. Taylor, MBDA, Bristol, United B. Hinchliffe, N. Qin, University of G. Wroblewski, P. Ansell, University of Islamabad, Pakistan; Z. Abbas, U. Ahsun, Kingdom United Kingdom; T. Rendall, C. Allen, D. Poole, Kingdom; T. Rendall, C. Allen, University of Sheffield, Sheffield, United Kingdom Illinois, Urbana-Champaign, Urbana, IL King Saud University, Riyadh, Saudi Arabia University of Bristol, Bristol, United Kingdom Bristol, Bristol, United Kingdom Tuesday, 5 January 2016 122-APA-14 Special Session: CREATE-AV HPC Multiphysics Applications of Full-up Air Vehicles I Coronado E Chaired by: N. HARIHARAN, CREATE-AV and R. MEAKIN 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2016-0562 AIAA-2016-0563 AIAA-2016-0564 AIAA-2016-0565 AIAA-2016-0566 AIAA-2016-0567 AIAA-2016-0568 The CREATE Program: Design and Recent Advancements in the Helios An Assessment of CREATETM-AV HPCMP CREATETM-AV Kestrel Mixing Plane Multi-Stage Introduction to COFFE: The Next- Application of CREATETM-AV Helios Analysis Tools for DoD Weapon Rotorcraft Simulation Code Helios for Apache Hover and Architecture, Capabilities, and Long Turbomachinery Simulation Generation HPCMP CREATETM-AV to Predict CH-47 Dynamic Blade Systems A. Wissink, Army Aviation and Missile Forward Flight Simulations Term Plan for Fixed-Wing Aircraft Capability for Kestrel/Firebolt CFD Solver Loads D. Post, C. Atwood, K. Newmeyer, R. Research Development and Engineering R. Narducci, The Boeing Company, Simulations R. Nichols, D. McDaniel, University of R. Glasby, J. Erwin, University of D. O’Brien, Army Research, Development Meakin, J. D’Angelo, S. Dey, U.S. Army Center, Moffett Field, CA; J. Sitaraman, Parallel Philadelphia, PA; H. Tadghighi, The Boeing S. Morton, R. Meakin, CREATE AV Team, Alabama, Birmingham, Birmingham, AL; K. Tennessee, Oak Ridge, Oak Ridge, TN and Engineering Command, Redstone Corps of Engineers, Lorton, VA Geometric Algorithms, LLC, Sunnyvale, CA; Company, Mesa, AZ Eglin AFB, FL Jason, Aerospace Testing Alliance, Arnold Arsenal, AL B. Jayaraman, B. Roget, V. Lakshminarayan, AFB, TN Science and Technology Corporation, Moffett Field, CA; M. Potsdam, Army Aviation and Missile Research Development and Engineering Center, Moffett Field, CA; et al. Tuesday, 5 January 2016 123-APA-15 Flow Control Applications & Demonstrations I Americas Cup D Chaired by: B. CYBYK, The Johns Hopkins University Applied Physics Laboratory and K. VANDEN, USAF 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2016-0569 AIAA-2016-0570 AIAA-2016-0571 AIAA-2016-0572 AIAA-2016-0573 Simulation of Sweep-Jet Flow Control, Trade Study of 3D Co-Flow Jet Wing LES Analysis on Shock-Vortex Ring LES-based characterization of a Flow around a Finite Circular Single Jet and Full Vertical Tail for Cruise and Takeoff/Landing Interaction suction and oscillatory blowing Cylinder Coated with Porous Media R. Childs, P. Stremel, Science and Technology Performance Y. Yang, J. Tang, C. Liu, University of fluidic actuator H. Yuan, C. Xia, Y. Chen, Z. Yang, Tongji Corporation, Hampton, VA; L. Kushner, A. Lefebvre, G. Zha, University of Miami, Texas, Arlington, Arlington, TX J. Kim, P. Moin, Stanford University, University, Shanghai, China University of California, Santa Cruz, Moffett Coral Gables, FL Stanford, CA; A. Seifert, Tel Aviv University, Field, CA; J. Heineck, B. Storms, NASA Ames Tel Aviv, Israel Research Center, Moffett Field, CA Tuesday, 5 January 2016 124-CMS-1/CPS-1 Communication, Computing and Information Processing Regatta B Chaired by: E. BUTTE, Lockheed Martin Space Systems and C. LI, Air Force Office of Scientific Research 0900 hrs 0930 hrs 1000 hrs 1030 hrs AIAA-2016-0574 AIAA-2016-0575 AIAA-2016-0576 AIAA-2016-0577 Battlefield Airborne Smart Node Pod (SNP) - Big A low cost, secure radio : Big Data Storage and Communications Node (BACN) Capabilities in a Small Package communications system for UAVs Analytics Tool for ATM Researchers K. Burns, K. Smith, Northrop Grumman S. Vaught, M. Rafter, K. Burns, C. Hill, A. Santangelo, sci_Zone, Inc., Holland, A. Tyagi, J. Nanda, Intelligent Automation, Corporation, San Diego, CA Northrop Grumman Corporation, San MI; P. Skentzos, Dornerworks, Grand Inc., Rockville, MD Diego, CA; W. Roeting, George Mason Rapids, MI Universtiy, Fairfax, VA Tuesday, 5 January 2016 125-DE-1 Design Processes and Tools Old Town A Chaired by: G. CREARY, NASA-Langley Research Center and C. DAVIES, Lockheed Martin Aeronautics 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2016-0578 AIAA-2016-0579 AIAA-2016-0580 AIAA-2016-0581 AIAA-2016-0582 AIAA-2016-0583 A High-Fidelity Approach to Global/Local analysis of thermal Sizing Study for First-Order Electric Multirotor UAV Propulsion The Full-Scale Helicopter Flight Ascendancy of Extinction-Reignition on Conceptual Design effects on a threaded fastener Feasibility Assessment of a Space System Sizing for Performance Simulator Design and Fabrication Single-Stage Hybrid Sounding Rocket J. Watson, R. Wlezien, Iowa State B. Devarajan, D. Locatelli, R. Kapania, Vehicle Applied to the Space Prediction and Design Optimization at CCSU in View of Fuels University, Ames, IA Virginia Polytechnic Institute and State Transportation System D. Bershadsky, S. Haviland, E. Johnson, F. Wei, L. Amaya-Bower, A. Gates, D. K. Chiba, University of Electro-Communications, University, Blacksburg, VA; R. Meritt, S. Hussein, B. Chudoba, University of Georgia Institute of Technology, Atlanta, Rose, T. Vasko, Central Connecticut State Tokyo, Japan; H. Yoda, S. Ito, M. Kanazaki, Ahmic Aerospace, LLC, Dayton, OH Texas, Arlington, Arlington, TX GA University, New Britain, CT Tokyo Metropolitan University, Tokyo, Japan; S. Watanabe, Muroran Institute of Technology, Hokkaido, Japan; K. Kitagawa, Japan Aerospace Exploration Agency (JAXA), Sagamihara, Japan; et al. Tuesday, 5 January 2016 126-FD-10 CFD: Turbulence Modeling Promenade A Chaired by: H. NAGIB, IHI AEROSPACE Co., Ltd. 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2016-0584 AIAA-2016-0585 AIAA-2016-0586 AIAA-2016-0587 AIAA-2016-0588 An Adaptive Variational Multiscale Validation of a turbulence Development and Validation of Turbulence Simulation Using Direct A new wall-law for adverse Discontinuous Galerkin Method For methodology using the SST k- a LES Turbulence Wall Model for Gradient Adaptive k- Model pressure gradient flows and Large Eddy Simulation model for adjoint calculation Compressible Flows with Heat Z. Li, H. Zhang, J. Hoagg, S. Bailey, A. modification of k-omega type G. Kuru, M. de la Llave Plata, V. Couaillier, S. Evans, S. Lardeau, CD-adapco, London, Transfer Martin, University of Kentucky, Lexington, RANS turbulence models ONERA, Châtillon, France; R. Abgrall, United Kingdom Lexington, KY

J. Komives, P. Subbareddy, G. Candler, T. Knopp, German Aerospace Center University of Zurich, Zürich, Switzerland; University of Minnesota, Minneapolis, (DLR), Göttingen, Germany F. Coquel, National Center for Scientific Minneapolis, MN Research (CNRS), Palaiseau, Switzerland Tuesday, 5 January 2016 127-FD-15 Aqueous Flow Control and Flow Control Experiments Cove Chaired by: L. CATTAFESTA, FAMU-FSU College of Engineering and R. LEBEAU, Saint Louis University 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2016-0589 AIAA-2016-0590 AIAA-2016-0591 AIAA-2016-0592 AIAA-2016-0593 AIAA-2016-0594 Thrust of a Zero-Net-Mass-Flux Numerical Investigation of Fluidic Oscillators for Drag Pressure Characteristics over 20 An Investigation of Three- Bistable State of High Angle-of- Actuator in Aqueous Crossflow Entrainment Mechanism of Jet Boat Reduction on a Bluff Body in Water deg Cone Forebody at Alpha 35 Dimensional Flow over a Attack Flow over Conical Forebody. B. Ayers, H. Johari, California State Tail Passive Flow Control for Base H. Schmidt, Technical University of Berlin, deg and Re (0.1-0.9)×106 Undulating Inflatable Wing F. Liu, S. Luo, University of California, University, Northridge, CA Drag Reduction Berlin, Germany; R. Woszidlo, University J. Zhao, X. Meng, J. Wang, Northwestern J. Beltz, G. Spencer, J. Krofta, R. LeBeau, Irvine, Irvine, CA; X. Meng, J. Zhao, Y. Yang, G. Zha, University of Miami, Coral of Kansas, Lawrence, Lawrence, KS; C. Polytechnical University, Xi’an, China; F. Saint Louis University, St. Louis, MO Northwestern Polytechnical University, Gables, FL Nayeri, C. Paschereit, Technical University Liu, S. Luo, University of California, Irvine, Xi’an, China of Berlin, Berlin, Germany Irvine, CA Tuesday, 5 January 2016 128-FD-16 Boundary-Layer Transition Promenade B Chaired by: H. REED, Texas A&M University and H. JOHNSON, University of Minnesota 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2016-0595 AIAA-2016-0596 AIAA-2016-0597 AIAA-2016-0598 AIAA-2016-0599 Measurement of HIFiRE-5 Boundary- Global stability analysis on cone Prediction Methodology for 2nd Boundary Layer Stability Analysis Measurements of Instability in Layer Transition in a Mach-6 Quiet models under the conditions of the Mode Dominated Boundary Layer for Stetson’s Mach 6 Blunt Cone Supersonic Flow with Injection by Tunnel with Infrared Thermography HIEST experiments Transition in Hypersonic Wind Experiments Time-Resolved Flow Visualization T. Juliano, L. Paquin, University of Notre Y. Matsuse, M. Saijo, T. Ishihara, Y. Tunnels J. Jewell, R. Kimmel, Air Force Research B. Schmidt, J. Shepherd, California Dame, Notre Dame, IN; M. Borg, Air Force Ogino, N. Ohnishi, Tohoku University, E. Marineau, Arnold Engineering Laboratory, Wright-Patterson AFB, OH Institute of Technology, Pasadena, CA Research Laboratory, Wright-Patterson Sendai, Japan; H. Tanno, Japan Aerospace Development Center, Silver Spring, MD AFB, OH Exploration Agency (JAXA), Kakuda, Japan Tuesday, 5 January 2016 129-FD-17 CFD: Cartesian and Mapped Grids Pier Chaired by: S. KARMAN, Pointwise, Inc. and H. DONG, University of Virginia 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2016-0600 AIAA-2016-0601 AIAA-2016-0602 AIAA-2016-0603 AIAA-2016-0604 AIAA-2016-0605 AIAA-2016-0606 A Cartesian Cut-Cell Approach for A Novel Simple Cut-Cell Method Cartesian Cut-Cell and GFM A Cartesian Immersed Boundary A Fourth-Order Viscous Operator on Anisotropic Patch-Based Adaptive A hierarchical Cartesian method for Modelling Air and Water Droplet for Robust Flow Simulation on Approaches to Free-Surface and Method to Simulate Stably Mapped Grids Mesh Refinement for Finite-Volume conjugate heat transfer involving Flow Cartesian Grids Moving Boundary Interaction Stratified Turbulent Flows L. Owen, S. Guzik, X. Gao, Colorado State Methods moving bodies L. Wutschitz, N. Nikiforakis, University of M. Harada, Y. Tamaki, Y. Takahashi, T. W. Bennett, L. Michael, N. Nikiforakis, C. Umphrey, Boise State University, University, Fort Collins, CO J. Christopher , X. Gao, S. Guzik, Colorado G. Brito Gadeschi, M. Meinke, W. Cambridge, Cambridge, United Kingdom Imamura, University of Tokyo, Tokyo, University of Cambridge, Cambridge, Boise, ID; R. DeLeon, University of Idaho, State University, Fort Collins, CO Schroeder, RWTH Aachen University, Japan United Kingdom Boise, Boise, ID; I. Senocak, Boise State Aachen, Germany University, Boise, ID

Tuesday, 5 January 2016 130-FD-18 RANS/LES and Its Applications Harbor E Chaired by: X. GAO, Colorado State Univ and B. SMITH, Lockheed Martin Aeronautics 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2016-0607 AIAA-2016-0608 AIAA-2016-0609 AIAA-2016-0610 AIAA-2016-0611 AIAA-2016-0612 Simulation Using Flamelet A Comparison Study of Turbulence LES/RANS Modeling of Turbulent Impact of Periodic Boundary Turbulence Modeling for Realistic A New DES Model Based on Wray- Radiation Modeling Models in RANS Simulations of Mixing in a Jet in Crossflow at Low Conditions on the Flow Field in an Computation of Internal Flow in Agarwal Turbulence Model for J. Doom, South Dakota State University, Rotor 67 Momentum Ratios Axial Fan Liquid Ejector Pumps Simulation of Wall-Bounded Flows Brookings, SD N. Spotts, X. Gao, Colorado State J. Prause, Y. Emmi, B. Noll, M. Aigner, German A. Pogorelov, M. Meinke, W. Schroeder, RWTH J. Masud, M. Imran, Air University, H. Xu, T. Wray, R. Agarwal, Washington University, Fort Collins, CO Aerospace Center (DLR), Stuttgart, Germany Aachen University, Aachen, Germany Islamabad, Pakistan University in St. Louis, St. Louis, MO Tuesday, 5 January 2016 131-FD-19 Shock Boundary Layer Interaction III Harbor F Chaired by: J. SIVASUBRAMANIAN, The University of Arizona and D. GAITONDE, The Ohio State University 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2016-0613 AIAA-2016-0614 AIAA-2016-0615 AIAA-2016-0616 AIAA-2016-0617 AIAA-2016-0618 Numerical Investigation of Numerical Investigation of a Conditional analysis of Ramp Separation Response to Simulation of Supersonic Turbulent Direct Numerical Simulation of Shock Shockwave Boundary Layer Normal Shock Wave Boundary unsteadiness in shock boundary Laser-Induced Breakdown Disturbed Non-Reactive Flow in Ramp-Cavity Waves Passed by Multiple Particles by Interactions in Supersonic Flows Layer Interaction in a 4.3 Aspect layer interactions Boundary Layer at Mach 4.5 Combustor Using a Discontinuous Using Immersed Boundary Method J. Sivasubramanian, H. Fasel, University of Ratio Test Section M. Waindim, L. Agostini, Ohio State S. Im, L. Wermer, Worcester Polytechnic Spectral Element Method Y. Mizuno, S. Takahashi, Tokai University, Arizona, Tucson, Tucson, AZ M. Pizzella, S. Warning, M. Jennerjohn, University, Columbus, OH; L. Larchevêque, Institute, Worcester, MA; D. Baccarella, Q. Liu, Z. Ghiasi, J. Komperda, D. Li, F. Hiratsuka, Japan; T. Nonomura, Japan M. McQuilling, Saint Louis University, St. National Center for Scientific Research B. McGann, University of Notre Dame, Notre Mashayek, University of Illinois, Chicago, Aerospace Exploration Agency (JAXA), Louis, MO; A. Purkey, R. Scharnhorst, The (CNRS), Marseille, France; D. Gaitonde, Dame, IN; H. Do, Seoul National University, Chicago, IL Sagamihara, Japan; T. Nagata, K. Fukuda, Boeing Company, St. Louis, MO; et al. Ohio State University, Columbus, OH Seoul, South Korea Tokai University, Hiratsuka, Japan Tuesday, 5 January 2016 132-GNC-11 Adaptive Control Hillcrest A Chaired by: M. BALAS, Embry-Riddle Aeronautical University and F. HOLZAPFEL 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2016-0619 AIAA-2016-0620 AIAA-2016-0621 AIAA-2016-0622 AIAA-2016-0623 AIAA-2016-0624 An L1 Adaptive Output Feedback Direct Uncertainty Minimization Adaptive Model Tracking Control Nonlinear Adaptive Robust Control An LMI-Based Hedging Approach Adaptive flow control of rotating Controller using Modified Piecewise Framework in the Presence of for Weakly Minimum Phase Linear with Linear Matrix Inequalities to Adaptive Control with Actuator wind turbine blades based on the Constant Adaptation Law Unknown Control Effectiveness for Infinite-Dimensional Systems in Applied to a Quadrotor Dynamics in the Presence of Unknown Beddoes-Leishman model using M. Bichlmeier, Technical University of Model Reference Adaptive Control Hilbert Space Using a Zero Filter D. Kun, I. Hwang, Purdue University, West Control Effectiveness trailing-edge flaps Munich, Munich, Germany B. Gruenwald, T. Yucelen, Missouri M. Balas, Embry-Riddle Aeronautical Lafayette, IN B. Gruenwald, D. Wagner, T. Yucelen, Missouri M. Balas, Embry-Riddle Aeronautical University of Science and Technology, University, Daytona Beach, FL; S. Frost, University of Science and Technology, Rolla, University, Daytona Beach, FL; N. Li, Yang Rolla, MO; J. Muse, Air Force Research NASA Ames Research Center, Moffett MO; J. Muse, Air Force Research Laboratory, Zhou University, Yang Zhou, China Laboratory, Wright-Patterson AFB, OH Field, CA Wright-Patterson AFB, OH Tuesday, 5 January 2016 133-GNC-12 Spacecraft Parameter Estimation and Modeling Hillcrest B Chaired by: U. SHANKAR, The Johns Hopkins University Applied Physics Laboratory and J. REED, United Launch Alliance, LLC 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2016-0625 AIAA-2016-0626 AIAA-2016-0627 AIAA-2016-0628 AIAA-2016-0629 AIAA-2016-0630 Attitude Estimation Employing Spin-Axis Tilt Estimation for Angular Velocity Bounds via Light Realization of a Two-Synodic-Period Development of an Air-Bearing Flying Beacon Aided Entry Common Frame Error Spinning Spacecraft Curve Glint Duration Earth-Mars Cycler Inclinable Turntable for Testing Navigation for Mars Orbiter-Lander Representations H. Soken, S. Sakai, K. Asamura, Y. J. Hinks, J. Crassidis, State University of M. Naeije, E. Mooij, Delft University of Tether Deployment Integrated Mission M. Andrle, Lincoln Laboratory, Nakamura, T. Ken, Japan Aerospace New York, Amherst, NY Technology, Delft, The Netherlands U. Bindra, Z. Zhu, York University, North T. Qin, S. Zhu, P. Cui, Beijing Institute of Massachusetts Institute of Technology, Exploration Agency (JAXA), Sagamihara, York, Canada Technology, Beijing, China Lexington, MA; J. Crassidis, State Japan

University of New York, Amherst, NY Tuesday, 5 January 2016 134-GNC-13 Invited Session: LOC-3, Onboard Systems for LOC Prevention and Recovery – Resilient Flight Control and Guidance Systems Coronado B Chaired by: D. CRIDER, National Transportation Safety Board and C. BELCASTRO, NASA-Langley Research Center 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2016-0631 AIAA-2016-0632 AIAA-2016-0633 AIAA-2016-0634 AIAA-2016-0635 AIAA-2016-0636 L1 Stability Augmentation System for ‘Can I Get L1 On?!’ Providing An L1 Adaptive Backup Flight Safe Flight Using One Aerodynamic Robust Adaptive Control Allocation Online Pilot Model Parameter Calspan’s Variable-Stability Learjet Consistent Handling Qualities on Control Law for Transport Aircraft Control Surface for an Octocopter under Actuator Estimation Using Sub-Scale Aircraft K. Ackerman, E. Xargay, R. Choe, N. Calspan’s Variable-Stability Learjet with Vertical-Tail Damage R. Venkataraman, P. Seiler, University of Faults Flight Data Hovakimyan, University of Illinois, Urbana- M. Cotting, R. Jeffrey, M. Blackstun, T. D. Sun, R. Choe, E. Xargay, N. Minnesota, Minneapolis, Minneapolis, MN H. Yoon, V. Cichella, N. Hovakimyan, T. Mandal, Y. Gu, West Virginia University, Champaign, Urbana, IL; M. Cotting, R. Jeffrey, Fulkerson, T. Lau, S. Stephens, Air Force Hovakimyan, University of Illinois, Urbana- University of Illinois, Urbana-Champaign, Morgantown, WV U.S. Air Force Test Pilot School, Edwards AFB, Test Pilot School, Edwards AFB, CA; et al. Champaign, Urbana, IL Urbana, IL CA; et al. Tuesday, 5 January 2016 135-GNC-14 Aerospace Robotics and Unmanned/Autonomous Systems III Hillcrest C Chaired by: B. TWEDDLE, Jet Propulsion Laboratory and K. SEWERYN, Space Research Centre Polish Academy of Sciences 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2016-0637 AIAA-2016-0638 AIAA-2016-0639 AIAA-2016-0640 AIAA-2016-0641 AIAA-2016-0642 A novel approach with safety Adaptive Step-length RRT Algorithm A New Centrality Measure Based on Cohesive Autonomous Navigation Attitude Stabilization of an Control analysis for a contactless metrics for real-time exploration of for Improved Coverage Formation Response System Uncooperative Spacecraft in an de-tumbling method based on eddy uncertain environments M. McCourt, C. Ton, S. Mehta, University C. Robertson, A. Sinclair, Auburn D. Kuether, Texas A&M University, College Orbital Environment using Visco- currents: problem definition and T. Mannucci, E. Van Kampen, C. de Visser, of Florida, Shalimar, Shalimar, FL; J. University, Auburn, AL; E. Doucette, Air Station, TX; B. Morrell, University of Elastic Tethers approximate proposed solutions. Q. Chu, Delft University of Technology, Curtis, Air Force Research Laboratory, Force Research Laboratory, Eglin AFB, FL Sydney, New South Wales, Australia; G. K. Hovell, S. Ulrich, Carleton University, N. Ortiz Gómez, S. Walker, Southampton Delft, The Netherlands Eglin AFB, FL Chamitoff, M. Bishop, D. Mortari, Texas Ottawa, Canada University, Southampton, United Kingdom; M. A&M University, College Station, TX; P. Jankovic, DFKI, Bremen, Germany; J. Romero Gibbens, University of Sydney, New South Martín, Strathclyde University, Glasgow, United Wales, Australia; et al. Kingdom; F. Kirchner, DFKI, Bremen, Germany; M. Vasile, Strathclyde University, Glasgow, United Kingdom Tuesday, 5 January 2016 136-GNC-15 Planning and Control for Mini/Micro UAVs Hillcrest D Chaired by: A. LAMPTON, Systems Technology, Inc. and M. LIU, MIT - Massachusetts Institute of Technology 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2016-0643 AIAA-2016-0644 AIAA-2016-0645 AIAA-2016-0646 AIAA-2016-0647 Observer Based Controllers for UAV Smooth Trajectory Planning for UAV Flight Test Evaluation of Fusion Rudder Augmented Trajectory Absolute Localization using Image Maneuver Options MAVs with Airspace Restrictions Algorithms for Estimation of Angle Correction for Small Unmanned Alignment and Particle Filtering C. Ashokkumar, G. York , U.S. Air Force S. Upadhyay, A. Ratnoo, Indian Institute of of Attack and Sideslip Angle Aerial Vehicles and the Effects on G. Van Dalen, Delft University of Academy, Colorado Springs, CO Science, Bangalore, India Technology, Delft, The Netherlands ; D. P. Tian, H. Chao, University of Kansas, Fixed Camera Imagery Lawrence, KS; Y. Gu, West Virginia T. Fisher, R. Sharma, Utah State Magree, E. Johnson, Georgia Institute of University, Morgantown, WV; S. Hagerott, University, Logan, UT Technology, Atlanta, GA Textron Aviation, Wichita, KS Tuesday, 5 January 2016 137-GT-3 High Reynolds Number Aerodynamics and Testing (Invited) Harbor B Chaired by: R. PARYZ and J. QUEST, ETW GmbH 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs Oral Presentation AIAA-2016-0648 Oral Presentation Oral Presentation Oral Presentation AIAA-2016-0649 AIAA-2016-0650 Testing a Laminar Wing Bizjet Force Measurement Improvements Overview of Data Quality from Pretest and Setup Bay for High Upgrades and Enhancements of the Application of Lifetime-based Development of a Highly Sensitive Model at High Reynolds Number to the National Transonic Facility a Semi-Span Wind Tunnel Model Reynolds Propulsion Airframe European Windtunnel (ETW) Pressure-Sensitive Paint Technique Temperature-Sensitive Paint for O. Colin, Dassault Group, Rueil-Malmaison, Sidewall Mounted Support System Tested in NASA’s National Transonic Integration Testing at the National H. Quix, German Aerospace Center (DLR), to Cryogenic Wind Tunnel Test Measurements under Cryogenic France D. Butler, S. Balakrishna, ViGYAN, Inc., Facility at Transonic Conditions Transonic Facility Cologne, Germany D. Yorita, German Aerospace Center Temperatures (100 – 160 K) Hampton, VA; C. Cagle, D. Chan, NASA J. Hooker, A. Wick, Lockheed Martin M. Acheson, R. Hudgins, G. Jones, NASA (DLR), Göttingen, Germany Conditions Langley Research Center, Hampton, VA; S. Corporation, Acworth, GA; D. Chan, NASA Langley Research Center, Hampton, VA C. Klein, German Aerospace Center (DLR), Goodliff, Jacobs, Hampton, VA; G. Jones, Langley Research Center, Hampton, VA; Göttingen, Germany NASA Langley Research Center, Hampton, R. Plumley, Air Force Research Laboratory, VA; et al. Wright-Patterson AFB, OH Tuesday, 5 January 2016 138-GTE-4 Compression Systems II Cortez Hill C Chaired by: R. BERDANIER, Purdue University and K. SUDER, NASA Glenn Research Center 0900 hrs 0930 hrs 1000 hrs AIAA-2016-0651 AIAA-2016-0652 AIAA-2016-0653 Quantifying Blockage in a Evaluation of New Blade Concept 3-D Separation Control in a Linear Multistage Compressor for Different for Turbofan Engines Cascade with Diffusion Tip Clearances using Steady and A. Soueidan, R. LeBeau, Saint Louis C. Kleven, T. Corke, University of Unsteady Pressure Measurements University, St. Louis, MO Notre Dame, Notre Dame, IN; D. Frias, R. Berdanier, N. Key, Purdue University, D. Hanson, N. Nolcheff, West Lafayette, IN International, Inc., Phoenix, AZ Tuesday, 5 January 2016 139-GTE-5 Turbine Cooling I Gaslamp D Chaired by: G. WOO, General Electric Global Research 0900 hrs 0930 hrs AIAA-2016-0654 AIAA-2016-0655 Design of a High Pressure Turbine Heat Transfer in a Rotating Two-pass Nozzle Guide Vane with Effective Film Square Channel Representing Internal Cooling System on Leading Edge Cooling of Gas Turbine Blades F. Kiyici, T. Aksu, S. Uslu, TOBB University of R. Amano, S. Beyhaghi, University of Economics and Technology, Ankara, Turkey Wisconsin, Milwaukee, Glendale, WI Tuesday, 5 January 2016 140-HIS-1 Aerospace Archives: All is not Lost - Keepers of the Right Stuff Americas Cup A 0900 - 1230 hrs The AIAA History Technical Committee works to highlight the record of aerospace advances and recognize their impacts on modern society.To help dispel the myth that all the aerospace legacy materials of people and institutions have been lost, this session will provide a basic overview of what exists, where it is, and how it may be accessed. During this series of presentations, experts will talk about the collections of their respective organizations, “best practices” and the individual and institutional opportunities for preserving records.

Moderator: Cam Martin, NASA Armstrong Flight Research Center

Panelists: Joseph C. Anselmo William P. Barry Tom D. Crouch Brook Engebretson Editor in Chief Chief Historian Senior Curator, National Air & Space Museum Aerospace History Project Aviation Week & Space Technology NASA Smithsonian Institution Huntington-USC Institute on California and the West Tracy B. Grimm Katrina B. Pescador Stephanie M. Smith Barron Hilton Archivist for Flight and Space Exploration Director of Library & Archives 412th Test Wing History Office Purdue University Libraries San Diego Air & Space Museum Edwards AFB, California

Tuesday, 5 January 2016 141-HSABP-2 Scramjet Combustors Regatta A Chaired by: R. HARTFIELD, Auburn University and O. POWELL 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2016-0656 AIAA-2016-0657 AIAA-2016-0658 AIAA-2016-0659 AIAA-2016-0660 AIAA-2016-0661 AIAA-2016-0662 WIDECARS Measurements of a Dynamic Response of Supersonic Establishing the Controlling Common-Path Measurement of Fast Data Processing for Optical Ignition of Light Hydrocarbon Turbulent Diffusion Flux of Premixed Ethylene-Air Flame in a Flow to Short Duration Normal Parameters of Ignition in High-Speed H2O, CO, and CO2 via TDLAS Absorption Measurements Mixtures Relevant to Thermal Transverse Jet into Pseudo-Shock Small-Scale Dual-Mode Scramjet Flow Injection Flow for Combustion Progress in a K. Busa, M. Brown, Air Force Research Cracking of Jet Fuels Wave Combustor C. Guarnaccio, Air Force Institute of T. Ombrello, C. Carter, Air Force Research Hydrocarbon-Fueled Scramjet Laboratory, Wright-Patterson AFB, OH P. Gokulakrishnan, C. Fuller, M. Klassen, T. Lee, Tohoku University, Sendai, Japan; E. Gallo, L. Cantu, A. Cutler, George Technology, Wright-Patterson AFB, OH; T. Laboratory, Wright-Patterson AFB, OH; B. K. Busa, M. Brown, M. Gruber, Air Force Combustion Science & Engineering, Inc., T. Kouchi, Okayama University, Okayama, Washington University, Washington, Ombrello, Air Force Research Laboratory, McGann, University of Notre Dame, Notre Research Laboratory, Wright-Patterson Columbia, MD; Y. Zhu, D. Davidson, R. Japan; Y. Oka, G. Masuya, Tohoku D.C.; R. Rockwell, C. Goyne, J. McDaniel, Wright-Patterson AFB, OH; B. Bentley, Dame, IN; H. Do, Seoul National University, AFB, OH; J. France, University of Hanson, Stanford University, Stanford, University, Sendai, Japan University of Virginia, Charlottesville, Air Force Institute of Technology, Wright- Seoul, Korea (the Democratic People’s Michigan, Ann Arbor, MI CA; et al. Charlottesville, VA Patterson AFB, OH Republic of); D. Peterson, Innovative Scientific Solutions, Inc., Dayton, OH Tuesday, 5 January 2016 142-IS-3 Big Data Analytics Coronado A 0900 - 1100 hrs

Sam Adhikari Dave Kasik Manjula Ambur Anne Kao Bryan Matthews Dragos Margineantu Sysoft and Rutgers University The Boeing Company NASA Langley Research Center The Boeing Company NASA Ames Research Center The Boeing Company

Tuesday, 5 January 2016 143-LEC-4 ASC Lecture Harbor A 0900 - 1000 hrs

Adaptive Aerospace Structures – An Air Force Perspective Gregory W. Reich Air Force Research Laboratory, AFRL/RQVC Tuesday, 5 January 2016 144-MAT-4 Materials Testing & Characterization II Gaslamp B Chaired by: J. RANSOM, NASA-Langley Research Center and R. NAIK, Pratt & Whitney 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2016-0663 AIAA-2016-0664 AIAA-2016-0665 AIAA-2016-0666 AIAA-2016-0667 AIAA-2016-0668 Effect of Silane Treated Electrospun Acoustic Emission Beamforming for Experimental Investigation of Laser Comparisons between Forced- Numerical Determination of Development of creep-dominant

SiO2 Nanofibers Interleaving on Detecting and Localizing Damage Machining of Sapphire for High Response and Hysteretic Energy Mechanical Properties for Flexible creep-fatigue testing for Alloy 617 Mode I Fracture Toughness of Glass in Composite Materials Temperature Pressure Transducers Damping Assessment Methods Material Systems F. Tahir, Y. Liu, Arizona State University, Epoxy Composites J. Rivey, G. Lee, J. Yang, University of H. Bal, W. Oates, R. Kumar, Florida State O. Scott-Emuakpor, B. Langley, C. J. Hill, R. Braun, Georgia Institute of Tempe, AZ

V. Suryawanshi, L. Zhang, A. Kelkar, Washington, Seattle, Seattle, WA; Y. Kim, University, Tallahassee, FL; D. Mills, M. Holycross, T. George, B. Runyon, J. Technology, Atlanta, GA University of North Carolina, Greensboro, SM Instruments, Daejeon, South Korea ; Sheplak, University of Florida, Gainesville, Justice, Air Force Research Laboratory, Greensboro, NC S. Kim, Korea Aerospace Research Institute Gainesville, FL Wright-Patterson AFB, OH (KARI), Daejeon, South Korea Tuesday, 5 January 2016 145-MDO-3 Propulsion & Thermal Design Considerations Balboa A Chaired by: D. ALLISON, Optimal Flight Sciences LLC and G. RUSSELL 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2016-0669 AIAA-2016-0670 AIAA-2016-0671 AIAA-2016-0672 AIAA-2016-0673 AIAA-2016-0674 Thermodynamics For Gas Turbine Fuel Thermal Management System Aircraft System Affects Including Impact of High Energy Pulsed An Aerospace Vehicle Model An Overview of the Optimized Cycles With Analytic Derivatives in Consideration in Conceptual Design Propulsion and Air Cycle Machine Systems on an Aircraft’s Power and Including a Cryogenic Thermal Integrated Multidisciplinary OpenMDAO Sizing Coupled Interactions Thermal Management System Subsystem Systems Program J. Gray, J. Chin, T. Hearn, E. Hendricks, E. Alyanak, Air Force Research Laboratory, D. Allison, Optimal Flight Sciences, R. Roberts, A. Donovan, S. Nuzum, M. S. Nuzum, R. Roberts, M. Wolff, Wright R. Reuter, S. Iden, R. Snyder, D. Allison, T. Lavelle, NASA Glenn Research Center, Wright-Patterson AFB, OH; D. Allison, LLC, Dayton, OH; E. Alyanak, Air Force Wolff, Wright State University, Dayton, OH State University, Dayton, OH Air Force Research Laboratory, Wright- Cleveland, OH; J. Martins, University of Optimal Flight Sciences, LLC, Dayton, OH Research Laboratory, Wright-Patterson Patterson AFB, OH Michigan, Ann Arbor, Ann Arbor, MI AFB, OH; K. Shimmin, PC Krause and Associates, West Lafayette, IN Tuesday, 5 January 2016 146-MST-4 Modeling of Space Systems and Dynamics Golden Hill A Chaired by: A. HIMMLER, dSPACE, Inc. and D. KEATING 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2016-0675 AIAA-2016-0676 AIAA-2016-0677 AIAA-2016-0678 AIAA-2016-0679 Optimal Attitude Control of Agile High-Fidelity General-Purpose A Method for Launch Vehicle Modeling SMAP Spacecraft Attitude Empirical Data Driven Model for Spacecraft Using Combined Robotic Simulation Framework Performance Analysis via Surrogate Control Estimation Error Using Shape and Dynamics Estimation of Reaction Wheel and Control for Artificially Intelligent Space Modeling Signal Generation Model Large Deployable Membrane Space Moment Gyroscope Arrays Exploration Vehicles M. Steffens, S. Edwards, D. Mavris, Georgia F. Rizvi, Jet Propulsion Laboratory, Structure C. Doupe, E. Swenson, Air Force Institute S. Walker, J. Shan, York University, Institute of Technology, Atlanta, GA; P. Dees, California Institute of Technology, M. Yamazaki, Nihon University, Chiba, of Technology, Wright-Patterson AFB, OH Toronto, Canada Jacobs, Huntsville, AL; M. Diaz, Georgia Pasadena, CA Japan Institute of Technology, Atlanta, GA Tuesday, 5 January 2016 147-NDA-2 Analysis and Optimization Under Uncertainty Old Town B Chaired by: S. DORMOHAMMADI and P. WANG, Wichita State University 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2016-0680 AIAA-2016-0681 AIAA-2016-0682 AIAA-2016-0683 AIAA-2016-0684 Multi-fidelity Methods in Incorporation of Risk Preferences in Probabilistic Design Analysis of Using Normalized Parameter Application of Bayesian Theory Aerodynamic Robust Optimization a Value-Based Systems Engineering Bellows Type Pogo Accumulator Perturbations to Investigate to Interval Based Representation A. Padron, J. Alonso, Stanford University, Framework for a Satellite System D. Ransom, Southwest Research Institute, Design, Sensitivity Analysis, and of Epistemic Uncertainty for Stanford, CA; M. Eldred, Sandia National H. Kannan, Iowa State University, Ames, San Antonio, TX Uncertainty Quantification a Decomposed Multilevel Laboratories, Albuquerque, NM IA; B. Mesmer, University of Alabama, E. Forster, P. Beran, R. Kolonay, Air Force Optimization Framework Huntsville, Huntsville, AL; C. Bloebaum, Research Laboratory, Wright-Patterson I. Dettwiller, M. Rais-Rohani, Mississippi Iowa State University, Ames, IA AFB, OH; H. Bae, Wright State University, State University, Mississippi State, MS

Dayton, OH Tuesday, 5 January 2016 148-NW-7 Tuesday Late Morning Networking Coffee Break Session Room Foyers 0900 - 0930 hrs Tuesday, 5 January 2016 149-PC-6 Heterogeneous Propellants and Combustion, Fuel Technology Harbor C Chaired by: A. GNANASKANDAN, Jet Propulsion Laboratory and T. JACKSON, University of Florida Gainesville 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2016-0685 AIAA-2016-0686 AIAA-2016-0687 AIAA-2016-0688 AIAA-2016-0689 AIAA-2016-0690 AIAA-2016-0691 Microwave-Supported Plasma Combustion of Sonochemically- Size-Resolved Burn Rate Direct-Deposition to Create High Functional Group Analysis of The effect of fuel composition Three-dimensional Structures in Combustion Enhancement of Generated Amorphous Reactive Measurements of Metal Particle Loading Propellants with Evaporation and Liquid Combustion on the non-premixed flame Hypergolic Ignition Process and Composite Solid Propellants Using Mixed-Metal Nanopowders in an NanoParticles Controlled Architecture: Combustion of Jet-A and Its Surrogate Fuel structure of LNG/LOx mixtures at Flame Holding Mechanisms for Alkali Metal Dopants n-Decane Spray Flame R. Jacob, Y. Zong, Y. Yang, University of and Mechanical Properties Based On Quantitative FT-IR supercritical pressure Hydrazine/Nitrogen Dioxide Un- J. Lynch, M. Ballestero, R. Cazin, J. M. Weismiller, B. Fisher, Z. Huba, A. Maryland, College Park, College Park, MD; X. Li, M. Zachariah, University of Measurements P. Lapenna, P. Ciottoli, F. Creta, University like Doublet Impinging Gas Jets Michael, T. Sippel, Iowa State University, Epshteyn, S. Tuttle, B. Williams, Naval S. Li, Tsinghua University, Beijing, China; Maryland, College Park, College Park, MD Y. Liu, B. Walker, University of Michigan, of Rome “La Sapienza”, Rome, Italy Y. Daimon, H. Tani, Japan Aerospace Ames, IA Research Laboratory, Washington, D.C. M. Zachariah, University of Maryland, Flint, Flint, MI Exploration Agency (JAXA), Tsukuba, College Park, College Park, MD Japan; H. Terashima, University of Tokyo, Tokyo, Japan; M. Koshi, Yokohama National University, Yokohama, Japan Tuesday, 5 January 2016 150-PDL-5/PC-7/AMT-3 Special Walter Lempert Memorial Session I (Invited) Harbor D Chaired by: R. MILES, Princeton University and I. ADAMOVICH, Ohio University 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs Oral Presentation Oral Presentation Oral Presentation Oral Presentation Oral Presentation Oral Presentation “It’s Amazing What You May See If What we learned from Walter Nice Guys Can Finish First: Walter Remembering Prof. Walter Lempert Plasma Assisted Low Temperature Short Pulses, Big Impact: Walter You Only Look”: Walter Lempert’s Lempert Lempert’s Legacy of Scholarship and J. Tishkoff, Air Force Office of Scientific Combustion Lempert and ns Discharge Kinetics Legacy in Science. S. Macheret, Purdue University, West Comradeship Research, Arlington, VA; M. Gundersen, Y. Ju, J. Lefkowitz, Princeton University, M. Kushner, University of Michigan, Ann I. Adamovich, Ohio State University, Lafayette, IN; R. Yetter, Pennsylvania C. Carter, Air Force Research Laboratory, University of Southern California, Los Princeton, NJ Arbor, Ann Arbor, MI Columbus, OH State University, University Park, PA Wright-Patterson AFB, OH; G. Elliott, University Angeles, CA of Illinois, Urbana-Champaign, Urbana, IL Tuesday, 5 January 2016 151-SATS-1 Small Satellites - Technologies I Ocean Beach Chaired by: J. STRAUB, University of North Dakota 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2016-0692 AIAA-2016-0693 AIAA-2016-0694 AIAA-2016-0695 AIAA-2016-0696 AIAA-2016-0697 Micro Pulsed Plasma Thrusters for Spherical Reaction Wheel System Designing, Building, and Testing a Electrical Power System of SRMSAT Fabrication of Asymmetric Implementation of three DoFs Attitude Control of a Low Earth For Satellite Attitude Control Mesh Ka-band Parabolic Deployable - 2 Nanostructures for Plasmonic Force small satellite ground simulation Orbiting CubeSat H. Paku, R. Takehana, K. Uchiyama, Nihon Antenna (KaPDA) for CubeSats S. Pavuluri, SRM University, Propulsion system N. Gatsonis, Y. Lu, J. Blandino, M. University, Funabashi, Japan J. Sauder, N. Chahat, R. Hodges, E. Peral, Jet Kattankulathur, India J. Maser, J. Rovey, X. Yang, Missouri H. Yao, Y. Wang, J. Cui, J. Bao, H. Yang, Demetriou, Worcester Polytechnic Institute, Propulsion Laboratory, California Institute of University of Science and Technology, Z. Zhu, Tsinghua University, Beijing, Worcester, MA; N. Paschalidis, NASA Technology, Pasadena, CA; Y. Rahmat-Samii, Rolla, MO China; et al. Goddard Space Flight Center, Greenbelt, University of California, Los Angeles, Los MD Angeles, CA; M. Thomson, Jet Propulsion Laboratory, California Institute of Technology, Pasadena, CA Tuesday, 5 January 2016 152-SCS-1 Spacecraft Antennas and Apertures Balboa B Chaired by: M. SILVER, MIT Lincoln Laboratory and H. FANG 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2016-0698 AIAA-2016-0699 AIAA-2016-0700 AIAA-2016-0701 AIAA-2016-0702 AIAA-2016-0703 AIAA-2016-0704 System Design Study of a Measuring Critical Alignments of Design and Deployment Testing of Concept Design of 15m class Energy-Efficient Active Reflectors with Shape-Control Experiment of Space Shape Control of a Reflector Based Deployable Reflector Antenna with the James Webb Space Telescope the Multi-Arm Radial Composite Light Weight Deployable Antenna Improved Mechanical Stability and Reconfigurable Reflector Using on Generalized Zernike Functions Flexible Shell Segments Aft Optics Subsystem (MARCO) Reflector Antenna Reflector for L-band SAR Improved Thermal Performance Antenna Reception Power L. Lan, S. Jiang, Y. Zhou, H. Fang, J. Footdale, LoadPath, LLC, Albuquerque, A. Barto, B. Gallagher, J. Knight, K. J. Footdale, LoadPath, LLC, Albuquerque, Application S. Bradford, D. Hofmann, S. Roberts, J. H. Sakamoto, Tokyo Institute of Technology, Shanghai YS Information Technology Co., NM; J. Banik, Air Force Research Smith, Ball Aerospace & Technologies NM; J. Banik, Air Force Research K. Nakamura, N. Nakamura, Technosolver Steeves, Jet Propulsion Laboratory, California Tokyo, Japan; H. Tanaka, National Defense Ltd., Shanghai, China; Z. Wu, J. Du, Dalian Laboratory, Kirtland AFB, NM Corporation, Boulder, CO Laboratory, Kirtland AFB, NM Corporation, Fujisawa, Japan; S. Ozawa, Institute of Technology, Pasadena, CA; Acadamy of Japan, Kanagawa, Japan; K. University of Technology, Dalian, China A. Uematsu, H. Hoshino, T. Kimura, Japan C. Wojnar, Missouri University of Science Ishimura, A. Doi, Japan Aerospace Exploration Aerospace Exploration Agency (JAXA), and Technology, Rolla, MO; D. Kochmann, Agency (JAXA), Kanagawa, Japan; Y. Kono, Tsukuba, Japan California Institute of Technology, Pasadena, N. Matsumoto, National Astronomical CA Observatory of Japan, Tokyo, Japan; et al. Tuesday, 5 January 2016 153-SD-5 Turbomachinery / Structural Health Monitoring Balboa C Chaired by: D. JOHNSON, NASA Glenn Research Center and J. BLACK, Virginia Tech 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2016-0705 AIAA-2016-0706 AIAA-2016-0707 AIAA-2016-0708 AIAA-2016-0709 AIAA-2016-0710 Analysis of Damage Assessment Reduced Order Geometric Mistuning The Development of an Active Evaluation of Fiber Optic Strain Frequency Domain Statistical Frequency Domain Statistical of Large Hailstone Ingestion into Models using Principal Component Damping and Stiffness Technique Sensors for Applications in Damage Identification Damage Identification Applied to Advanced High Bypass Propulsion Analysis Approximations for Turbomachinery using Shape Structural Health Monitoring Development and Analytical Study an Experimental Composite Plate system E. Henry, J. Brown, Air Force Research Memory Alloys B. Martins, J. Kosmatka, University of J. Oliver, J. Kosmatka, C. Farrar, J. Conte, J. Oliver, J. Kosmatka, C. Farrar, J. Conte, Y. Song, J. Bayandor, Virginia Polytechnic Laboratory, Wright-Patterson AFB, OH; J. R. Wischt, N. Garafolo, University of California, San Diego, La Jolla, CA University of California, San Diego, La University of California, San Diego, La Institute and State University, Blacksburg, VA Beck, Perceptive Engineering Analytics, Lino Akron, Akron, OH Jolla, CA Jolla, CA Lakes, MN Tuesday, 5 January 2016 154-SD-6 Dynamics, Feedback Control, and Aeroservoelasticity I Gaslamp A Chaired by: S. SMITH, University of Kentucky and J. MCNAMARA, The Ohio State University 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2016-0711 AIAA-2016-0712 AIAA-2016-0713 AIAA-2016-0714 AIAA-2016-0715 AIAA-2016-0716 Model-Predictive Control of Flexible Optimal Selection of Control Inverse Dynamics for Deceleration Feedback control of integrally Active Piezoelectric Actuation Spacecraft Docking with Type II Aircraft Dynamics using Nonlinear Surfaces for Active Aeroelastic Control of Deployment of Linked actuated membrane wings: a and Control of Highly Flexible Superconductor Flux Pinning and Reduced-Order Models Control of Prescribed Modes Panel Structure in Space computational study Multifunctional Wings Potential Energy Capture Y. Wang, A. Wynn, R. Palacios, Imperial R. Brown, K. Singh, Miami University, M. Takatsuka, Nagoya University, Nagoya, S. Buoso, R. Palacios, Imperial College N. Tsushima, W. Su, University of R. Caracciolo, F. Zhu, M. Peck, Cornell College London, London, United Kingdom Oxford, OH Japan London, London, United Kingdom Alabama, Tuscaloosa, Tuscaloosa, AL University, Ithaca, NY Tuesday, 5 January 2016

155-SRE-2 ISRU technologies and trades Bankers Hill Chaired by: L. GERTSCH, Missouri University of Science and Technology and D. LINNE, NASA Glenn Research Center 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2016-0717 AIAA-2016-0718 AIAA-2016-0719 AIAA-2016-0720 AIAA-2016-0721 Exploration Sampling of Regolith from Dynamic Elasto-Plastic Impact Force Aquaponics: An Option for In-situ Liquefaction and Storage of In-Situ

Augmented by In-Situ Resource Utilizing Magnetic Force in a Special Planetary Drilling Production of Mission Consumables O2 on the surface of Mars Utilization: Mercury and Saturn M. Adachi, R. Obata, A. Shigeta, H. Mechanism K. Kalbacher de Marquez, E. Marquez D. Hauser, W. Johnson, NASA Glenn Propulsion Investigations Kawamoto, Waseda University, Tokyo, R. Malla, L. Vila, University of Connecticut, Gonzalez, Autonomous University of Research Center, Cleveland, OH B. Palaszewski, NASA Glenn Research Japan Storrs, Storrs, CT Chihuahua, Chihuahua, Mexico Center, Cleveland, OH Tuesday, 5 January 2016 156-STR-4 Special Session: USAF Benchmarking of Composite Fatigue Prediction Methods La Jolla A Chaired by: S. CLAY and S. ENGELSTAD, Lockheed Martin Aeronautics 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2016-0722 AIAA-2016-0723 AIAA-2016-0724 AIAA-2016-0725 AIAA-2016-0726 AIAA-2016-0727 AIAA-2016-0728 Assessment of Multiscale Design Fatigue Damage Prediction in 3D delamination profile Assessment of Composite Damage Progressive Failure Simulation A Continuum Damage and Discrete A Micromechanical Approach to System for Fatigue Life Prediction Quasi-Isotropic Open-Hole Tension reconstruction for composite Growth Tools for Aircraft Structure in Laminated Composites under Crack Approach for Fatigue Low Cycle Fatigue Analysis and of Advanced Composite Aircraft Coupon using the Kinetic Theory laminates using inverse heat Part II Fatigue Loading by Using Discrete Damage Prediction of Laminated Life Prediction of Heterogeneous Structures of Fracture conduction S. Engelstad, Lockheed Martin Damage Modeling Composites Materials J. Fish, Columbia University, New York, R. Dalgarno, D. Robbins, AutoDesk, Inc., T. Peng, Y. Liu, Arizona State University, Corporation, Marietta, GA; S. Clay, Air K. Hoos, University of Dayton Research E. Fang, X. Cui, J. Lua, Global Engineering H. Sertse, W. Yu, Purdue University, West NY; Z. Yuan, J. Wollschlager, Altair Laramie, WY; J. Action, S. Engelstad, Tempe, AZ Force Research Laboratory, Wright- Institute, Dayton, OH; E. Iarve, University and Materials, Inc., Princeton, NJ Lafayette, IN Engineering, Inc., Troy, MI Lockheed Martin Corporation, Marietta, GA Patterson AFB, OH of Texas, Arlington, Arlington, TX; M. Braginsky, E. Zhou, University of Dayton Research Institute, Dayton, OH; D. Mollenhauer, Air Force Research Laboratory, Wright-Patterson AFB, OH Tuesday, 5 January 2016 157-STR-5 Failure Analysis and Prediction I La Jolla B Chaired by: A. PALAZOTTO and L. HARDAWAY, Ball Aerospace & Technologies Corporation 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2016-0729 AIAA-2016-0730 AIAA-2016-0731 AIAA-2016-0732 AIAA-2016-0733 AIAA-2016-0734 AIAA-2016-0735 Micro-Scale Crack Propagation The EST Model for Predicting Effect of Strength Variation Along A Comparative Study of Local Effect of Notch on the Failure In situ study of static and dynamic A Selectively Activated Continuum- Using the eXtended Finite Element Progressive Damage and Failure of a Single Fiber on Micro-Scale and Nonlocal Domain Integration Response of Oxide/Oxide Ceramic strain energy density at notch roots Coupled Extrinsic Cohesive Model Method Open Hole Bending Specimens Damage Development in UD-FRPs for XFEM Based Stress Intensity Composites and fatigue cracks using digital W. Peterson, D. Cairns, Montana State V. Goyal, R. Jorge, University of Puerto A. Joseph, University of Michigan, Ann N. Parambil, K. Fathima, S. Gururaja, Factor Extraction for Fatigue Life D. Zhang, University of Connecticut, image correlation University, Bozeman, MT Rico, Mayaguez, Arbor, Ann Arbor, MI; A. Waas, University Indian Institute of Science, Bangalore, Prediction Storrs, Storrs, CT; P. Meyer, University C. Holycross, H. Shen, Ohio State of Washington, Seattle, Seattle, WA; E. India X. Ren, A. Sadeghirad, N. Simon, J. Lua, of Michigan, Ann Arbor, MI; A. Waas, University, Columbus, OH; O. Scott- Pineda, NASA Glenn Research Center, Global Engineering and Materials, Inc., University of Washington, Seattle, Emuakpor, T. George, Air Force Research Cleveland, OH Princeton, NJ Seattle, WA Laboratory, Wright-Patterson AFB, OH Tuesday, 5 January 2016 158-TES-4 Electrochemical Power for Aerospace Missions Gaslamp C 0900 - 1230 hrs Moderator: Farzad Mashayek, University of Illinois, Chicago

Space lithium ion battery problems and future mission needs Materials Challenges and Opportunities for Energy Storage at Extremely Low Temperatures ESA/ITT Project, Electrochemical Phenomena in Microgravity Rao Surampudi Shirley Meng Vadim Lvovich NASA Jet Propulsion Laboratory University of California, San Diego NASA Glenn Research Center Development and testing of advanced energy storage systems at UC San Diego for power system Lithium Deposition Issues in Zero G and/or Electrolysis Challenges in Zero G Developments and opportunities for fuel cells William Torre Yasuhiro Fukunaka Thomas Fuller

University of California, San Diego Waseda University Georgia Institute of Technology

Tuesday, 5 January 2016 159-TP-5 Aerothermodynamics I Harbor G Chaired by: M. BARNHARDT, NASA-Ames and X. WANG, Air Force Research Laboratory 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2016-0736 AIAA-2016-0737 AIAA-2016-0738 AIAA-2016-0739 AIAA-2016-0740 AIAA-2016-0741 AIAA-2016-0742 High Fidelity Modeling of Thermal Assessment of Vibrational Uncertainty and Sensitivity Analysis Analysis of CO2 Plasma Infrared Analysis of VUV radiation Radiative Gas Dynamics of Large Radiative Gas Dynamics of MSL at Relaxation and Dissociation of Nonequilibrium for State Resolved of Afterbody Radiative Heating Radiation Measurements measurements from high Superorbital Space Vehicle at Angle Angle of Attack Oxygen Simulation of a Hypersonic Flow Predictions for Earth Entry S. Nishimura, University of Shizuoka, temperature air mixtures of Attack S. Surzhikov, Russian Academy of D. Andrienko, I. Boyd, University of J. Burt, E. Josyula, Air Force Research T. West, NASA Langley Research Center, Shizuoka, Japan; A. Lemal, H. Takayanagi, A. Lemal, Japan Aerospace Exploration S. Surzhikov, Russian Academy of Sciences, Moscow, Russia Michigan, Ann Arbor, Ann Arbor, MI Laboratory, Wright-Patterson AFB, OH Hampton, VA; S. Hosder, Missouri S. Nomura, S. Matsuyama, K. Fujita, Agency (JAXA), Chofu, Japan; S. Sciences, Moscow, Russia University of Science and Technology, Japan Aerospace Exploration Agency Nishimura, Shizuoka University, Shizuoka, Rolla, MO; C. Johnston, NASA Langley (JAXA), Chofu, Japan Japan; S. Nomura, H. Takayanagi, S. Research Center, Hampton, VA Matsuyama, K. Fujita, Japan Aerospace Exploration Agency (JAXA), Chofu, Japan Tuesday, 5 January 2016 160-UMS-3 Unmanned Systems: Missions and Applications Regatta C Chaired by: R. STANSBURY, Embry-Riddle Aeronautical University and J. VALASEK, Texas A&M University 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2016-0743 AIAA-2016-0744 AIAA-2016-0745 AIAA-2016-0746 AIAA-2016-0747 A Dual-Use Unmanned Aerial Flight Analysis of an Autonomous Unmanned Aircraft Operations at Dynamic Re-plan of the Loyal UAV-carried Long-distance Wi-Fi System for Precision Agriculture Parafoil Recovery System for High Texas A&M University – Corpus Wingman Optimal Control Problem Communication Infrastructure and Search and Rescue Applications Altitude Descent Systems Christi in a Changing Mission Environment J. Xie, University of North Texas, Denton, A. Weber, University of Michigan, Ann J. Chin, NASA Glenn Research Center, D. Bridges, Texas A&M University, Corpus C. Humphreys, R. Cobb, D. Jacques, J. TX; F. AI-Emrani, Amazon.com, Denton, Arbor, Ann Arbor, MI; N. Lauer, University Cleveland, OH; S. Dunker, D. Montague, Christi, TX; D. Yoel, American Aerospace Reeger, Air Force Institute of Technology, TX; Y. Gu, Y. Wan, S. Fu, University of of Maryland, College Park, College Airborne Systems, Santa Ana, CA; J. Advisors, Inc., Radnor, PA Wright-Patterson AFB, OH North Texas, Denton, TX Park, MD; J. Brady, University of Alaska, Niehaus, D. Goodenow, NASA Glenn Anchorage, Anchorage, AK; C. Branyan, Research Center, Cleveland, OH University of Arizona, Tucson, Tucson, AZ; M. Goodstein, State University of New York, Buffalo, NY; A. Gupta, Purdue University, West Lafayette, IN; et al. Tuesday, 5 January 2016 161-WE-2 Wind Energy: Wind Turbine Aerodynamics Modeling I Harbor H Chaired by: S. SCHRECK, NREL 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2016-0748 AIAA-2016-0749 AIAA-2016-0750 AIAA-2016-0751 AIAA-2016-0752 Improving Airfoil Drag Prediction Higher-Order Accurate Simulations Aeroacoustic Calculations of Wind Analytical actuator disc solution for Analytical Method to Determine a G. Ramanujam, University of Twente, of Wind Turbine Flow Fields: A Poor Turbine Noise with the Actuator unsteady load Tip Loss Factor for Highly-Loaded Enschede, The Netherlands ; H. Man’s Approach Line/ Navier-Stokes Technique W. Yu, C. Simao Ferreira, G. van Kuik, Wind Turbine Rotors Ozdemir, ECN, Petten, The Netherlands K. Sreenivas, A. Mittal, L. Taylor, H. Debertshaeuser, W. Shen, W. Zhu, Delft University of Technology, Delft, The S. Schmitz, Pennsylvania State University, ; H. Hoeijmakers, University of Twente, L. Hereth, University of Tennessee, Technical University of Denmark, Lyngby, Netherlands University Park, PA; D. Maniaci, Sandia Enschede, The Netherlands Chattanooga, Chattanooga, TN Denmark National Laboratories, Albuquerque, NM Tuesday, 5 January 2016 162-WE-3 Wind Energy: Structural Dynamics and Materials Harbor I Chaired by: D. CAIRNS, Montana State University 0900 hrs 0930 hrs 1000 hrs 1030 hrs AIAA-2016-0753 AIAA-2016-0754 AIAA-2016-0755 AIAA-2016-0756 Partitioned nonlinear structural The Usage of Parameterized Fracture and Fatigue of Thick Influence of Fabric Architecture on analysis of wind turbines using Fatigue Spectra and Physics-Based Adhesive Joints in Wind Turbine Damage Progression Evidenced by BeamDyn Systems Engineering Models for Blade Structures Acoustic Emission Measurements Q. Wang, M. Sprague, J. Jonkman, Determination of Wind Turbine D. Cairns, Montana State University, D. Miller, D. Samborsky, D. Cairns, M. National Renewable Energy Laboratory, Component Sizing Bozeman, MT Schuster, A. Lolatte, Montana State Golden, CO T. Parsons, P. Veers, Y. Guo, National University, Bozeman, MT Renewable Energy Laboratory, Golden, CO Tuesday, 5 January 2016 163-PANEL-4 Tuesday Morning Forum 360 Seaport F-G 0930 - 1130 hrs Innovation in Space: How Researchers Can Leverage the ISS National Laboratory for Pioneering Research & Development Moderator: Greg Johnson, President & Executive Director, Center for the Advancement of Science in Space (CASIS)

Panelists: Andrew Rush Dan Blaettler George Nelson President Senior Program Manager Manager, ISS Technology and Science Research Office Made In Space, Inc. Center for the Advancement of Science in Space (CASIS) NASA Johnson Space Center Tuesday, 5 January 2016 164-PANEL-5 ASC: Where’s My Morphing Aircraft? Reflections Based on Twenty Years of Adaptive Aerostructures Harbor A 1030 - 1230 hrs Moderator: Farhan Gandhi, Rosalind and John J. Redfern Jr. ‘33 Endowed Chair in Aerospace Engineering, and Aerospace Program Director, Rensselaer Polytechnic Institute

Panelists: Jayanth Kudva Edward White Friedrich Straub Daniel Newman NextGen Aeronautics The Boeing Company The Boeing Company The Boeing Company

Tuesday, 5 January 2016 165-IS-4 Intelligent Systems Autonomy Roadmap Panel Coronado A 1100 - 1230 hrs Panel Chairs: Nhan Nguyen, NASA Ames Research Center, Christopher Tschan, The Aerospace Corporation

Panelists: Ella Atkins Danette Allen John Valasek University of Michigan NASA Langley Research Center Texas A&M University

Tuesday, 5 January 2016 166-LUNCH-2 Recognition Luncheon: Celebrating Achievements in Aerospace Sciences and Information Systems Seaport A-E 1230 - 1400 hrs Tuesday, 5 January 2016 167-AA-4 Computational Aeroacoustics II Nautical Chaired by: X. LI, Beihang University and S. ARUNAJATESAN, Sandia National Labs 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2016-0757 AIAA-2016-0758 AIAA-2016-0759 AIAA-2016-0760 AIAA-2016-0761 AIAA-2016-0762 Linking Lagrangian & Acoustic Numerical Simulations for Effect of Flow-Acoustic Resonant Numerical Investigations of Bio- Investigation of the mechanisms of Coupled Overset Unstructured Wave Dynamics via Finite-Time Supersonic Jet Noise Reduction Interactions on Aerodynamic Response Inspired Blade Designs to Reduce jet-engine core noise using large- Discontinuous Galerkin Method for Lyapunov Exponent Fields Using Fluidic Inserts of Transitional Airfoils Broadband Noise in Aircraft eddy simulation Jet Noise Prediction D. Gonzalez, Naval Surface Warfare M. Kapusta, R. Powers, P. Morris, D. V. Golubev, J. Hayden, L. Nguyen, S. Salehian, Engines and Wind Turbines J. O’Brien, J. Kim, M. Ihme, Stanford R. Harris, CFD Research Corporation, Center, Indian Head, MD; R. Speth, D. McLaughlin, Pennsylvania State University, R. Mankbadi, Embry-Riddle Aeronautical B. Agrawal, A. Sharma, Iowa State University, Stanford, CA Huntsville, AL; E. Collins, E. Luke, A. Gaitonde, Ohio State University, Columbus, University Park, PA University, Daytona Beach, FL; C. Pasiliao, Air University, Ames, IA Sescu, Mississippi State University, OH; M. Lewis, Institute for Defense Force Research Laboratory, Eglin AFB, FL; et al. Mississippi State, MS Analyses, Washington, D.C. Tuesday, 5 January 2016 168-ABPSI-4 Propulsion Integration Golden Hill B Chaired by: D. BENCHERGUI, Bombardier Inc 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs AIAA-2016-0763 AIAA-2016-0764 AIAA-2016-0765 AIAA-2016-0766 AIAA-2016-0767 AIAA-2016-0768 AIAA-2016-0769 Investigation of the impact of a Aerodynamics of Aero-Engine Gas Temperature Measurement using Aerodynamic Interference for Aero- Progress in Optimizing the Experimental Performance of a Small A Transient Aircraft/Jet-Engine Variable Area Fan Nozzle on the Installation FTIR Spectroscopy in Small Internal Engine Installations Propulsive Aircraft Scale Pressure Wave Supercharger Simulator for Education overall performance of an UHBR- T. Stankowski, D. MacManus, Cranfield Combustion Engines T. Stankowski, D. MacManus, Cranfield Concept M. Mataczynski, Air Force Research J. Dionisopoulos, M. Danilevsky, E. Highlift-Configuration University, Cranfield, United Kingdom; C. M. Deutsch, J. Ausserer, M. Polanka, Air Force University, Cranfield, United Kingdom; C. J. Bijewitz, A. Seitz, A. Isikveren, Laboratory, Wright-Patterson AFB, OH; Kellogg, G. Christensen, D. Nguyen, R. S. Ritter, German Aerospace Center (DLR), Sheaf, N. Grech, Rolls-Royce Group plc, Institute of Technology, Wright-Patterson AFB, Sheaf, N. Grech, Rolls-Royce Group plc, M. Hornung, Bauhaus Luftfahrt e.V., D. Paxson, NASA Glenn Research Center, Davis, University of California, Davis, Braunschweig, Germany Derby, United Kingdom OH; P. Litke, A. Caswell, Air Force Research Derby, United Kingdom Ottobrunn, Germany Cleveland, OH; M. Polanka, Air Force Institute Davis, CA Laboratory, Wright-Patterson AFB, OH; K. of Technology, Wright-Patterson AFB, OH; J. Grinstead, Innovative Scientific Solutions, Inc., Hoke, Innovative Scientific Solutions, Inc., Dayton, OH Dayton, OH Tuesday, 5 January 2016 169-ACD-2 Aircraft Design Issues II Cortez Hill A Chaired by: R. BARRETT-GONZALEZ, The University of Kansas and J. MERRET, Gulfstream Aerospace Corporation 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2016-0770 AIAA-2016-0771 AIAA-2016-0772 AIAA-2016-0773 AIAA-2016-0774 AIAA-2016-0775 A Simple Method for High-Lift Engine/Inlet Matching for Influence of Engine Intake/Exhaust Variable Camber Application to Tracking PRSEUS Technical Progress Aircraft Concepts Modeling with Propeller Conceptual Design Supersonic Aircraft Design on Wing Design of Civil Aircraft Aircraft in Formation Flight with Reduction of Performance Subdivision Surfaces M. Patterson, N. Borer, NASA Langley C. Dickman, T. Takahashi, Arizona State by Means of Knowledge Discovery Y. Liu, E. Stumpf, RWTH Aachen University, Uncertainty Through Technology K. Amadori, C. Jouannet, Saab, Linköping, Research Center, Hampton, VA; B. University, Tempe, AZ Techniques Aachen, Germany Development and Demonstration Sweden German, Georgia Institute of Technology, N. Endo, M. Kanazaki, Tokyo Metropolitan Phases Atlanta, GA University, Hino, Japan; M. Murayama, K. J. Corman, D. Mavris, Georgia Institute of Yamamoto, Japan Aerospace Exploration Technology, Atlanta, GA Agency (JAXA), Mitaka, Japan Tuesday, 5 January 2016 170-ACD-3 Aircraft Wing Design Bankers Hill Chaired by: D. HALL, DHC Engineering and C. BIL, RMIT University 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2016-0776 AIAA-2016-0777 AIAA-2016-0778 AIAA-2016-0779 AIAA-2016-0780 AIAA-2016-0781 Aerodynamic Design of a Winglet A Novel Three Dimensional Aircraft Aeroelastic Analysis of High Apect Aircraft High-Lift Aerodynamic A Physics-Based Methodology for Wing Design Challenges Explained: for the Dassault Falcon 10 Wing Design Method Using High Ratio Wings Analysis Using a Surface-Vorticity Cantilever and -Braced Wing A Study of the Finite Wing Effects N. El Haddad, L. Gonzalez-Linero, Embry- Order Bezier Curves A. Suleman, University of Victoria, Victoria, Solver Weight Estimation of Camber, Thickness, and Twist Riddle Aeronautical University, Daytona C. Im, Palos Verdes Peninsula High School, Canada; F. Afonso, Technical University E. Olson, C. Albertson, NASA Langley D. Locatelli, B. Riggins, R. Kapania, J. J. Jensen, T. Takahashi, Arizona State Beach, FL Rolling Hills Estates, CA of Lisbon, Lisbon, Portugal; C. Spada, Research Center, Hampton, VA Schetz, Virginia Polytechnic Institute University, Tempe, AZ Technical University of Turin, Turin, Italy and State University, Blacksburg, VA; T.

Poquet, Snecma, Moissy-Cramayel, France Tuesday, 5 January 2016 171-AFM-6 Launch Vehicle, Missile, and Projectile Flight Mechanics II Cortez Hill B Chaired by: F. FRESCONI, US Army Research Lab and T. RICHARDSON, University of Bristol 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2016-0782 AIAA-2016-0783 AIAA-2016-0784 AIAA-2016-0785 AIAA-2016-0786 AIAA-2016-0787 Flight Behavior of an Asymmetric A Proposed Ascent Abort Flight Test Part-I : Aerodynamic Data Part-II : Effect of Design SHEFEX II - A First Aerodynamic Rapid Characterization of Munitions Body through Spark Range for the Max Launch Abort System Generation and 6 DOF Trajectory Modifications on Computed and Atmospheric Post-Flight Using Neural Networks Experiments using Roll-Yaw P. Tartabini, M. Gilbert, B. Starr, NASA Calculation of a Baseline Large- Trajectory of a Large-Caliber Analysis M. Carpenter, N. Speakman, R. Hartfield, Resonance for Yaw Enhancement Langley Research Center, Hampton, VA Caliber Spinning Projectile Spinning Projectile M. Franze, German Aerospace Center Auburn University, Auburn, AL F. Fresconi, B. Guidos, I. Celmins, Army J. Masud, F. Chughtai, Air University, J. Masud, F. Chughtai, Air University, (DLR), Brunswick, Germany Research Laboratory, Aberdeen Proving Islamabad, Pakistan; S. Akhtar, National Islamabad, Pakistan; S. Akhtar, National Ground, MD; W. Hathaway, Arrow Tech University of Sciences and Technology, University of Sciences and Technology, Associates, Burlington, VT Risalpur, Pakistan Risalpur, Pakistan Tuesday, 5 January 2016 172-AMT-4 Velocimetry II Harbor D Chaired by: K. LOWE and T. JENKINS, MetroLaser Inc 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2016-0788 AIAA-2016-0789 AIAA-2016-0790 AIAA-2016-0791 AIAA-2016-0792 AIAA-2016-0793 A Hybrid Technique for Laser Flare Comparison of Pulse-Burst PIV Three component LDV probe for AFRL- Pulse-Burst PIV Measurements of Three-Component Unseeded Measurements of Gas-Phase Reduction Data to Simultaneous Conventional TGF for SWBLI Studies Transient Phenomena in a Shock Velocity Diagnostic for Jet Engine Velocity during Shock-Particle D. Cadel, D. Shin, K. Lowe, Virginia PIV Data C. DeSio, University of Alabama, Tuscaloosa, Tube Exhaust Flows Interactions using Pulse-Burst PIV Polytechnic Institute and State University, S. Beresh, J. Wagner, J. Henfling, R. Tuscaloosa, AL; K. Miller, Lockheed Martin J. Wagner, S. Beresh, E. Demauro, K. T. Jenkins, C. Hess, MetroLaser, Inc., E. Demauro, J. Wagner, S. Beresh, Blacksburg, VA Spillers, B. Pruett, Sandia National Corporation, Manassas, VA; P. Schinetsky, N. Casper, D. Guildenbecher, B. Pruett, Laguna Hills, CA P. Farias, B. Pruett, Sandia National Laboratories, Albuquerque, NM Chaganti, B. Brooker, University of Alabama, Sandia National Laboratories, Albuquerque, Laboratories, Albuquerque, NM Tuscaloosa, Tuscaloosa, AL; J. Tinapple, Air NM; et al. Force Research Laboratory, Wright-Patterson AFB, OH; et al. Tuesday, 5 January 2016 173-APA-16 Special Session: Space Launch System (SLS) Induced Environments II Coronado D Chaired by: R. GOMEZ and J. PINIER, NASA Langley Research Center 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2016-0794 AIAA-2016-0795 AIAA-2016-0796 AIAA-2016-0797 AIAA-2016-0798 SLS Discussion Global Comparison of CFD Space Launch System Aerodynamic Space Launch System Booster Inviscid and Viscous CFD Analysis Space Launch System Booster and Wind Tunnel Derived F&M Database Uncertainty Separation Aerodynamic Testing of Booster Separation for the Space Separation Aerodynamic Database Databases for the Space Launch Quantification Methodologies at the NASA Langley Unitary Plan Launch System Vehicle Development and Uncertainty System A. Favaregh, H. Houlden, ViGYAN, Inc., Wind Tunnel D. Dalle, S. Rogers, H. Lee, W. Chan, Quantification M. Hemsch, ViGYAN, Inc., Hampton, VA Hampton, VA; J. Pinier, NASA Langley F. Wilcox, J. Pinier, D. Chan, NASA Langley NASA Ames Research Center, Moffett D. Chan, NASA Langley Research Center,

Research Center, Hampton, VA; M. Research Center, Hampton, VA; W. Crosby, Field, CA Hampton, VA; D. Dalle, S. Rogers, NASA Hemsch, ViGYAN, Inc., Hampton, VA NASA Marshall Space Flight Center, Ames Research Center, Moffett Field, CA; Huntsville, AL J. Pinier, F. Wilcox, NASA Langley Research Center, Hampton, VA; R. Gomez, NASA Johnson Space Center, Houston, TX Tuesday, 5 January 2016 174-APA-17 Applied CFD & Numerical Correlations with Experimental Data II Americas Cup B Chaired by: M. PARK, NASA-Langley Research Center and M. FOSSATI, McGill University 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs AIAA-2016-0799 AIAA-2016-0800 AIAA-2016-0801 AIAA-2016-0802 AIAA-2016-0803 Transonic Numerical and Experimental Numerical and laboratory An Experimental and Numerical Computational and Experimental CFD Predictions of Unsteady Aero- Investigation into Unconventional experiments on a new wing-body-tail Study on a Small-Scale Joined- Investigation into Flapping Wing Loads from Vortex Shedding on Lambda Wing Control Surfaces configuration Wing Aircraft Propulsion A-320 Landing Gear Door M. Paul, Air Force Research Laboratory, L. Smith, University of Pretoria, Pretoria, South Z. Teo, T. New, Nanyang Technological H. Hoeijmakers, J. Mulder, University of M. Tomac, A. Rizzi, Royal Institute of Kirtland AFB, NM; M. Rein, German Aerospace Africa; T. Davis, G. Spedding, University of University, Singapore, Singapore; B. Twente, Enschede, The Netherlands Technology (KTH), Stockholm, Sweden Center (DLR), Göttingen, Germany Southern California, Los Angeles, CA; J. Meyer, Nagel, V. Gollnick, German Aerospace University of Pretoria, Pretoria, South Africa Center (DLR), Hamburg, Germany Tuesday, 5 January 2016 175-APA-18 Aerodynamic Design: Analysis, Methodologies, and Optimization Techniques III Americas Cup C Chaired by: P. ANSELL, University of Illinois at Urbana-Champaign and K. DENISSEN, Sandia National Labs 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs AIAA-2016-0804 AIAA-2016-0805 AIAA-2016-0806 AIAA-2016-0807 AIAA-2016-0808 AIAA-2016-0809 AIAA-2016-0810 Evaluation of Load Analysis Low Order Supersonic Nozzle Flight Dynamics Modeling of a Gradient based aerodynamic Sensitivity and Stability Derivative A Continuous Adjoint Method for Surrogate-based Robust Airfoil Methods for NASA’s GIII Adaptive Design using Superimposed Propeller-Driven Cargo Airplane shape optimization using the FIVER Analysis using an Efficient Adjoint Viscous Flows at All Speeds Optimization under Aleatory Flight Compliant Trailing Edge Project Characteristics K. Biber, Bartin University, Bartin, Turkey embedded boundary method Harmonic Balance Technique H. Lee, S. Lee, Inha University, Incheon, Condition and Geometric Uncertainties J. Cruz, E. Miller, NASA Armstrong Flight O. Jegede, W. Crowther, University of D. De Santis, M. Zahr, C. Farhat, Stanford A. Kaminsky, K. Ekici, University of South Korea L. Shi, Z. Han, M. Shahbaz, W. Song, Research Center, Edwards, CA Manchester, Manchester, United Kingdom University, Stanford, CA Tennessee, Knoxville, Knoxville, TN Northwestern Polytechnical University, Xi’an, China Tuesday, 5 January 2016 176-APA-20 Propeller/Rotorcraft/Wind Turbine Aerodynamics I Americas Cup D Chaired by: J. RAULEDER, Technical University of Munich and M. CALVERT, U.S. Army AMRDEC 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs AIAA-2016-0811 AIAA-2016-0812 AIAA-2016-0813 AIAA-2016-0814 AIAA-2016-0815 Implicit Hybrid mesh Method for Computational Analysis of Multi- Time Marching Simulations of Wind Structured Overlapping Grid Open Rotor Computational the Computation of Rotorcraft Rotor Flows Turbine Blades Subject to Particle Simulations of Contra-Rotating Aeroacoustic Analysis with an Flows S. Yoon, H. Lee, T. Pulliam, NASA Ames Erosion Open Rotor Noise Immersed Boundary Method M. Woodgate, G. Barakos, University of Research Center, Moffett Field, CA G. Fiore, M. Selig, University of Illinois, J. Housman, C. Kiris, NASA Ames Research C. Brehm, Science and Technology Liverpool, Liverpool, United Kingdom Urbana-Champaign, Urbana, IL Center, Moffett Field, CA Corporation, Moffett Field, CA; M. Barad, C. Kiris, NASA Ames Research Center, Moffett Field, CA

Tuesday, 5 January 2016 177-ASC-2 Modeling and Analysis Gaslamp D Chaired by: O. BILGEN, Old Dominion University and J. KAUFFMAN, University of Central Florida 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs AIAA-2016-0816 AIAA-2016-0817 AIAA-2016-0818 AIAA-2016-0819 AIAA-2016-0820 AIAA-2016-0821 AIAA-2016-0822 Design optimization of a morphing A Multistep Morphing Structures Induced Strain Actuation for Solid- Design and Analysis of the Link Aero-electro-mechanical Coupling Hybrid Position Feedback Control Multiscale modeling of electrical flap device using variable stiffness Design Approach Applied to State : A Geometric Mechanism in the Flapping Wing of Electro-Active Membrane Wings of Bistable Structures transport in carbon nanotube-metal- materials Different Types of Applications in Configuration Study MAV Using Flexible Multi-Body I. Barbu, R. de Kat, B. M. Simsek, O. Bilgen, Old Dominion polymer composite materials. Q. Ai, P. Weaver, M. Azarpeyvand, Aerospace F. Hauris, O. Bilgen, Old Dominion Dynamic Analysis Ganapathisubramani, University of University, Norfolk, VA S. Shenogin, University of Dayton Research University of Bristol, Bristol, United L. da Rocha-Schmidt, L. Datashvili, H. University, Norfolk, VA J. Jeon, H. Cho, Y. Kim, J. Lee, S. Shin, Southampton, Southampton, United Institute, Dayton, OH; J. Lee, Universal Kingdom Baier, Technical University of Munich, C. Kim, Seoul National University, Seoul, Kingdom Technology Corporation, Dayton, OH; Garching, Germany South Korea ; et al. A. Voevodin, A. Roy, Air Force Research Laboratory, Wright-Patterson AFB, OH Tuesday, 5 January 2016 178-DE-2 Innovative Designs in Aerospace / Design Education Old Town A Chaired by: J. CUTSHALL, Southwest Research Institute and J. WANG, Kingston University 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs AIAA-2016-0823 AIAA-2016-0824 AIAA-2016-0825 AIAA-2016-0826 AIAA-2016-0827 Framework for Probabilistic Design of an Automated On- Extending Low-Cost Linux Computers A Beagle Bone Black Baed AHRS AREND: A Sensor Aircraft to support Analysis of Future Energy Demand Meal Delivery System for Education and Applications in for Control of Small UAS and Small Wildlife Rangers Technologies: Hybrid-Electric Under Emerging and Evolving Embedded Control and Robotics Sounding Rockets J. Koster, A. Buysse, University of Colorado, Propulsion Passenger Requirements H. Briggs, ATA Engineering, Inc., San Diego, C. Hall, North Carolina State University, Boulder, Boulder, CO; L. Smith, J. Huyssen, C. Justin, A. Ramamurthy, S. Briceno, D. C. Frank, M. Deveraux, R. Ausseil, D. CA; J. Strawson, T. Bewley, University of Raleigh, NC University of Pretoria, Pretoria, South Africa; J. Mavris, Georgia Institute of Technology, Mavris, Georgia Institute of Technology, California, San Diego, La Jolla, CA Hotchkiss, J. Malangoni, Metropolia University Atlanta, GA Atlanta, GA of Applied Sciences, Helsinki, Finland; et al. Tuesday, 5 January 2016 179-FD-21 Bio-inspired Flows Promenade B Chaired by: K. GRANLUND, North Carolina State University and H. DONG, University of Virginia 1400 hrs 1430 hrs 1500 hrs 1530 hrs AIAA-2016-0828 AIAA-2016-0829 AIAA-2016-0830 AIAA-2016-0831 Effect of rotational phase on the Experimental Study of the Three- Wake Dynamics and Structure of a Theoretical Investigation of the flow topology and force production Dimensional Wake of a Trapezoidal Heaving Flexible Foil Based on PIV Aerodynamics of Membrane MAV of a flapping flat-plate wing Pitching Panel Measurements Wings with Cambered Frames S. Krishna, Syracuse University, Syracuse, J. King, R. Kumar, M. Green, Syracuse F. Siala, A. Totpal, J. Liburdy, Oregon State A. Wrist, J. Hubner, University of Alabama, NY; K. Mulleners, Swiss Federal Institute University, Syracuse, NY University, Corvallis, OR Tuscaloosa, Tuscaloosa, AL of Technology, Lausanne, Switzerland; M. Green, Syracuse University, Syracuse, NY Tuesday, 5 January 2016 180-FD-22 CFD: Error Estimation and Mesh Adaptation Pier Chaired by: K. FIDKOWSKI, University of Michigan and C. ROY, Virginia Tech 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs AIAA-2016-0832 AIAA-2016-0833 AIAA-2016-0834 AIAA-2016-0835 AIAA-2016-0836 AIAA-2016-0837 AIAA-2016-0838 Continuous adjoint based error Development of a High-Order A Truncation Error Based Mesh A Local Sampling Approach to Discretization Error Estimation by Entropy residual as an adaptation Robust moving-mesh algorithms for estimation and r-refinement for the Space-Time Matrix-Free Adjoint Adaption Metric for CFD Anisotropic Metric-Based Mesh the Error Transport Equation on indicator for simulations of hybrid stretched meshes: Application active-flux method Solver T. Phillips, C. Ollivier Gooch, University of Optimization Unstructured Meshes - Applications unsteady ows to moving boundaries problems K. Ding, K. Fidkowski, P. Roe, University of M. Ceze, L. Diosady, S. Murman, NASA British Columbia, Vancouver, Canada K. Fidkowski, University of Michigan, Ann to Viscous Flows Y. Lv, M. Ihme, Stanford University, J. Landry, A. Soulaïmani, University of Québec, Michigan, Ann Arbor, Ann Arbor, MI Ames Research Center, Moffett Field, CA Arbor, Ann Arbor, MI G. Yan, C. Ollivier Gooch, University of Stanford, CA Montréal, Canada; E. Luke , Mississippi State British Columbia, Vancouver, Canada University, Starkville, MS; A. Ben Haj Ali, Bombardier Aerospace, Montréal, Canada Tuesday, 5 January 2016 181-FD-23/PDL-6 DBD Plasma Actuators II Harbor F Chaired by: M. SAMIMY, The Ohio State University and J. ROVEY, Missouri University of Science & Technology 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs AIAA-2016-0839 AIAA-2016-0840 AIAA-2016-0841 AIAA-2016-0842 AIAA-2016-0843 AIAA-2016-0844 AIAA-2016-0845 Control of Boundary Layer Improving the Performance of Control of a Non-Resonating Laminar-Separation-Bubbles Flow Flow Separation Control over a Boeing Experimental Study of Effects of The Phenomenology and Physics Separation and the Wake of a DBD Plasma Actuator Model Supersonic Cavity Using Plasma Control over Airfoil Using SDBD Vertol VR-7 using NS-DBD Plasma Frequency for Burst Wave on a DBD of Peristaltic Flow Acceleration an Airfoil using ns-DBD Plasma through Modification of Boundary Actuators Plasma Actuator Actuators Plasma Actuator for Separation Induced by Multiple DBD Plasma Actuators Condition Parameters N. Webb, M. Samimy, Ohio State M. Li, X. Meng, H. Li, F. Liu, S. Luo, A. Esfahani, A. Singhal, C. Clifford, M. S. Sekimoto, University of Tokyo, Sagamihara, Actuators Based on PIV T. Ashcraft, K. Decker, J. Little, University J. Laten, R. LeBeau, Saint Louis University, University, Columbus, OH Northwestern Polytechnical University, Samimy, Ohio State University, Columbus, OH Japan; T. Nonomura, K. Fujii, Japan Aerospace L. Feng, C. Gao, Z. Lv, B. Wu, L. Wu, of Arizona, Tucson, Tucson, AZ St. Louis, MO Xi’an, China Exploration Agency (JAXA), Sagamihara, Northwestern Polytechnical University, Japan Xi’an, China Tuesday, 5 January 2016 182-FD-24 Stability and Transition of Hypersonic Flows II Promenade A Chaired by: H. REED, Texas A&M University and M. CHOUDHARI, NASA-Langley Research Center 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs AIAA-2016-0846 AIAA-2016-0847 AIAA-2016-0848 AIAA-2016-0849 AIAA-2016-0850 Numerical Investigation of Transition Prediction in Hypersonic Secondary Instability Analysis of Gortler Modified Mack-modes on a Stabilization of the Hypersonic Laminar-Turbulent Transition for a Boundary Layers Using Receptivity Crossflow on a Hypersonic Yawed Hypersonic Flared Cone Boundary Layer by Finite- Flared Cone at Mach 6 and Freestream Spectra Straight Circular Cone J. Kuehl, Baylor University, Waco, TX; P. Amplitude Streaks J. Sivasubramanian, H. Fasel, University of P. Balakumar, A. Chou, NASA Langley A. Moyes, Texas A&M University, College Paredes, Technical University of Madrid, J. Ren, S. Fu, Beijing Institute of Arizona, Tucson, Tucson, AZ Research Center, Hampton, VA Station, TX; P. Paredes, NASA Langley Madrid, Spain Technology, Beijing, China; A. Hanifi, Royal Research Center, Hampton, VA; T. Kocian, Institute of Technology (KTH), Stockholm, H. Reed, Texas A&M University, College Sweden Station, TX Tuesday, 5 January 2016 183-FD-25 Wing Aerodynamics Cove Chaired by: R. AGARWAL, Washington University in St Louis and R. CUMMINGS, US Air Force Academy 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs AIAA-2016-0851 AIAA-2016-0852 AIAA-2016-0853 AIAA-2016-0854 AIAA-2016-0855 AIAA-2016-0856 AIAA-2016-0857 Drag, Lift and Effective Angle of Experimental investigation of the Effect of the leading and trailing Experimental Study of Thin and Steady Aerodynamics of Thick and Flow Physics of a Multi-Element The effect of aspect ratio on the Attack from the Wake of an Airfoil in wake of a lifting wing with cut-in edge geometry on the fluid- Thick Airfoils at Low Reynolds Cambered Airfoils with Porosity Airfoil in Ground Effect near-wake flow of rectangular the Open-Jet Wind Tunnel sinusoidal trailing edges structural coupling of membrane Numbers Gradients Q. Qu, B. Ju, L. Huang, P. Liu, Beihang wings D. Faleiros, University of Twente, Enschede, S. Prigent, O. Buxton, P. Bruce, Imperial aerofoils E. Garcia, P. Yu, V. Durgesh, H. Johari, R. Hajian, J. Jaworski, Lehigh University, University, Beijing, China; R. Agarwal, A. DeVoria, K. Mohseni, University of The Netherlands ; M. Tuinstra, National College London, London, United Kingdom S. Serrano Galiano, R. Sandberg, California State University, Northridge, CA Bethlehem, PA Washington University in St. Louis, St. Florida, Gainesville, Gainesville, FL Aerospace Laboratory (NLR), Marknesse, The University of Southampton, Southampton, Louis, MO Netherlands ; H. Hoeijmakers, University of United Kingdom Twente, Enschede, The Netherlands Tuesday, 5 January 2016 184-FD-26/APA-21 Special Session: Evaluation of RANS Solvers on Benchmark Aerodynamic Flows I Harbor E Chaired by: B. DISKIN, National Institute of Aerospace and H. LUO, North Carolina State University 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs AIAA-2016-0858 AIAA-2016-0859 AIAA-2016-0860 AIAA-2016-0861 AIAA-2016-0862 Grid-Converged Reynolds Averaged Spatial Convergence of Three Assessment of Preconditioner for High-Order Discontinuous Galerkin High-Order Output-Based Adaptive Navier Stokes Solutions for Dimensional Turbulent Flows a USM3D Hierarchical Adaptive Mesh Resolved Turbulent Flow Simulations of Turbulent Flow in Benchmark Three-Dimensional M. Park, W. Anderson, NASA Langley Nonlinear Iteration Method (HANIM) Simulations of NASA Turbulence Three Dimensions (Invited) Cases (Invited) Research Center, Hampton, VA (Invited) Model Validation Cases K. Fidkowski, University of Michigan, Ann B. Diskin, National Institute of Aerospace, M. Pandya, NASA Langley Research Center, M. Brazell, D. Mavriplis, University of Arbor, Ann Arbor, MI; M. Ceze, NASA Ames Hampton, VA; J. Thomas, C. Rumsey, M. Hampton, VA; B. Diskin, National Institute of Wyoming, Laramie, Laramie, WY Research Center, Moffett Field, CA

Pandya, NASA Langley Research Center, Aerospace, Hampton, VA; J. Thomas, N. Frink, Hampton, VA NASA Langley Research Center, Hampton, VA Tuesday, 5 January 2016 185-GEPC-3 Noise Reduction and Flight Demonstrations Americas Cup A Chaired by: N. MADAVAN, NASA-Ames Research Center and G. BEZOS O’CONNOR, NASA-Langley Research Center 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs AIAA-2016-0863 AIAA-2016-0864 Oral Presentation AIAA-2016-0865 AIAA-2016-0866 Assessment of the Noise Reduction Innovative Flow Control Concepts Challenges with Developmenting Green Aerospace Engineering: Entropy Generation Minimisation Potential of Advanced Subsonic for Drag Reduction a Distributed Electric Propulsion A Focus on the Technical and and Exergy analysis approaches for Transport Concepts for NASA’s J. Lin, NASA Langley Research Center, Researach Aircraft Economical Hurdles of Next aerospace applications - A review Environmentally Responsible Hampton, VA; E. Whalen, The Boeing S. Ginn, D. Hines, S. Clarke, M. Redifer, Generation Lithium-Ion Batteries D. Hayes, M. Lone, J. Whidborne, Aviation Project Company, Hazelwood, MO; J. Eppink, E. NASA Armstrong Flight Research Center, A. Gohardani, R. Dunn, N. Millecam, Cranfield University, Cranfield, United R. Thomas, C. Burley, C. Nickol, NASA Siochi, M. Alexander, M. Andino, NASA Edwards, CA Infineon Technologies AG, Irvine, CA Kingdom; E. Coetzee, Airbus, Bristol, Langley Research Center, Hampton, VA Langley Research Center, Hampton, VA United Kingdom Tuesday, 5 January 2016 186-GNC-16 Optimal Control: Methods and Applications Hillcrest A Chaired by: H. LIU, University of Toronto and A. AWAD 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs AIAA-2016-0867 AIAA-2016-0868 AIAA-2016-0869 AIAA-2016-0870 AIAA-2016-0871 Exact Hybrid Jacobian Computation Analytical Solution for Optimal Approximate Model Predictive Longitudinal trajectory optimization Monte Rey Methods for Unscented for Optimal Trajectories via Dual Drogue-to-Main Parachute Transition Control for Polynomial of an underwater in finite Optimization Number Theory Altitude for Ballistic Airdrops Systems Using Sum-of-Squares depth water I. Ross, R. Proulx, M. Karpenko, Naval V. D’Onofrio, University of Naples A. Gerlach, Universal Technology Corporation, Programming S. Yoon, J. Kim, Korea Advanced Institute Postgraduate School, Monterey, CA “Federico II”, Naples, Italy; M. Sagliano, Dayton, OH; D. Doman, Air Force Research N. Yokoyama, National Defense Academy, of Science and Technology, Daejeon, Y. Arslantas, German Aerospace Center Laboratory, Wright-Patterson AFB, OH Yokosuka, Japan South Korea (DLR), Bremen, Germany Tuesday, 5 January 2016 187-GNC-17 Spacecraft Formations and Rendezvous Hillcrest B Chaired by: J. THIENEL, NASA Goddard Space Flight Center and I. GRAVSETH 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2016-0872 AIAA-2016-0873 AIAA-2016-0874 AIAA-2016-0875 AIAA-2016-0876 AIAA-2016-0877 An Information-Theoretic Active Game Theoretic Strategies for Spacecraft Formation Keeping via Pose Tracking of a Noncooperative An Inverse Dynamics-Based Analytical Formulation for Light Localization Approach during Relative Spacecraft Rendezvous and Motion Discrete-Time Hamilton-Jacobi Spacecraft During Docking Trajectory Planner for Autonomous and Fast Low-Thrust Guidance Circumnavigation in Orbit Synchronization Theory Maneuvers Using a Time-of-Flight Docking to a Tumbling Target Design to Perform Multi-Target M. Kontitsis, P. Tsiotras, E. Theodorou, Georgia M. Innocenti, V. Tartaglia, University of K. Lee, C. Park, Yonsei University, Seoul, Sensor J. Ventura, Technical University of Munich, On-Orbit Servicing Institute of Technology, Atlanta, GA Pisa, Pisa, Italy South Korea ; T. Lee, George Washington J. Ventura, A. Fleischner, U. Walter, Munich, Germany; M. Ciarcia, M. Romano, L. Bucci, M. Lavagna, Technical University University, Washington, D.C.; S. Park, Technical University of Munich, Munich, Naval Postgraduate School, Monterey, CA; of Milan, Milan, Italy Yonsei University, Seoul, South Korea Germany U. Walter, Technical University of Munich, Munich, Germany Tuesday, 5 January 2016 188-GNC-18 Invited Session: LOC-4, Onboard Systems for LOC Prevention and Recovery – Upset Recovery and System Validation Coronado B Chaired by: D. CRIDER, National Transportation Safety Board and C. BELCASTRO, NASA-Langley Research Center 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs AIAA-2016-0878 AIAA-2016-0879 AIAA-2016-0880 AIAA-2016-0881 AIAA-2016-0882 Stall Recovery Guidance Algorithms Development and Pilot-In-The-Loop Aircraft Trim Recovery from Highly Real-Time Extended Kalman Filter AirSTAR Beyond Visual Range Based on Constrained Control Evaluation of Robust Upset- Nonlinear Upset Conditions Stability Indicator System Description and Preliminary Approaches Recovery Guidance B. Chang, H. Kwatny, E. Ballouz, D. K. Lassak, Y. Gu, West Virginia University, Test Results V. Stepanyan, University of California, Santa N. Richards, N. Gandhi, A. Bateman, Hartman, Drexel University, Philadelphia, Morgantown, WV K. Cunningham, D. Cox, J. Foster, S. Cruz, Santa Cruz, CA; K. Krishnakumar, J. Barron Associates, Inc., Charlottesville, PA Riddick, S. Laughter, NASA Langley Kaneshige, D. Acosta, NASA Ames Research VA; D. Klyde, A. Lampton, Systems Research Center, Hampton, VA

Center, Moffett Field, CA Technology, Inc., Hawthorne, CA Tuesday, 5 January 2016 189-GNC-19 Aerospace Robotics and Unmanned/Autonomous Systems IV Hillcrest C Chaired by: T. BOGE, DLR GSOC and M. AKELLA, University of Texas at Austin 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs AIAA-2016-0883 AIAA-2016-0884 AIAA-2016-0885 AIAA-2016-0886 AIAA-2016-0887 AIAA-2016-0888 AIAA-2016-0889 Integral Vector Field Path Following Control Laws Development for a Trajectory Optimization of Space Autonomous Determination of Spin Autonomous Navigation of a Vision-Aided Navigation for a Free- Trajectory Optimization for for a Stratospheric Satellite Free-Flying Unmanned Robotic Manipulator with Non-zero Angular Rate and Rotation Axis of Rocket Balloon over Saturn’s Moon Titan Flying Unmanned Robotic System Proximity Operations Around T. Chen, Z. Zewei, M. Zhu, Z. Wu, Beihang System to Support Interplanetary Momentum During Orbital Capture Bodies based on Point Clouds K. Garg, E. Mooij, Delft University of to Support Interplanetary Bodies Tumbling Geometrical Constraints University, Beijing, China Bodies Prospecting and Maneuver H. Gomez Martinez, B. Eissfeller, Technology, Delft, The Netherlands Prospecting and Characterization via Legendre Polynomials Characterization Missions. T. Rybus, K. Seweryn, Space Research University of the German Federal Armed Missions J. Shi, S. Ulrich, Carleton University, A. Perez Rocha, H. Moncayo, R. Prazenica, Centre of the Polish Academy of Sciences Forces, Neubiberg, Germany R. Prazenica, Z. Kern, T. John, H. Moncayo, Ottawa, Canada; A. Allen, MacDonald, Embry-Riddle Aeronautical University, (CBK PAN), Warsaw, Poland; J. Sasiadek, Embry-Riddle Aeronautical University, Daytona Dettwiler and Associates, Ltd., Brampton, Daytona Beach, FL; K. Zacny, Honeybee Carleton University, Ottawa, Canada Beach, FL; K. Zacny, Honeybee Robotics, Canada Robotics, Pasadena, CA; R. Mueller, M. Pasadena, CA; R. Mueller, NASA Kennedy Dupuis, NASA Kennedy Space Center, Cape Space Center, Cape Canaveral, FL; et al. Canaveral, FL; et al. Tuesday, 5 January 2016 190-GNC-20 Control of Bio-inspired Mini/Micro UAVs Hillcrest D Chaired by: H. TAHA, University of California, Irvine and L. SINGH, The Charles Stark Draper Laboratory, Inc. 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2016-0890 AIAA-2016-0891 AIAA-2016-0892 AIAA-2016-0893 AIAA-2016-0894 AIAA-2016-0895

A Combined Geometric-Control- A Fuzzy Control Strategy for UAV Kinematic Selection for a Tailless Transient Dynamic Analysis and L1 Adaptive Control for a Single Optimal UAV Rendezvous on a UGV Averaging to Optimum Trim of Perching using Varying Tau-dot Flapping Wing Micro-Air Vehicle Control of a Morphing UAV Coaxial Rotor MAV A. Rucco, P. Sujit, A. Aguiar, J. Sousa, Hovering FWMAVs and Insects W. Chi, K. Low, K. Hoon, Nanyang I. Weintraub, Air Force Research Laboratory, N. Prabhakar, R. Prazenica, S. M. Harada, R. Ichikawa, S. Watanabe, University of Porto, Porto, Portugal H. Taha, University of California, Irvine, Irvine, Technological University, Singapore, Wright-Patterson AFB, OH; D. Sigthorsson, Gudmundsson, M. Balas, Embry-Riddle National Defense Academy, Yokosuka, CA; D. Allen, S. Tahmasian, C. Woolsey, M. Singapore InfoSciTech, Wright-Patterson AFB, OH; M. Aeronautical University, Daytona Beach, FL Japan; K. Bollino, Naval Postgraduate Hajj, Virginia Polytechnic Institute and State Oppenheimer, D. Doman, Air Force Research School, Monterey, CA University, Blacksburg, VA Laboratory, Wright-Patterson AFB, OH Tuesday, 5 January 2016 191-GT-4 Integration of Experimental and Computational Methods (Invited) Harbor H Chaired by: S. DUNN, Jacobs Technology and V. CANACCI, Jacobs Technology 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs AIAA-2016-0896 Oral Presentation Oral Presentation AIAA-2016-0897 Oral Presentation Direction and Integration of EFD Education and Training of the Next Modeling and Simulation for The Air Force Digital Thread/ Developing a Briefing Targeted and CFD, a Summary of Two Panel Generation of Aerospace Engineers Research Digital Twin - Life Cycle Integration for Non-Engineers: The Role and Sessions R. Kumar, Florida State University, A. Washburn, NASA Langley Research and Use of Computational and Importance of Experimental and S. Dunn, NASA Langley Research Center, Tallahassee, FL Center, Hampton, VA Experimental Knowledge. Computational Capabilities in the Hampton, VA E. Kraft, Arnold Engineering Development Development of New Aerospace Center, Arnold AFB, TN Products. S. Dunn, Jacobs, Hampton, VA; V. Canacci, Jacobs, Cleveland, OH Tuesday, 5 January 2016 192-GTE-6 Gas Turbine Engine with Pressure Gain Combustion Harbor C Chaired by: G. MEHOLIC, The Aerospace Corporation and S. HEISTER, Purdue University 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2016-0898 AIAA-2016-0899 AIAA-2016-0900 AIAA-2016-0901 AIAA-2016-0902 AIAA-2016-0903 Mono-dimensional analysis of the Design of an Actively Valved Computationally Quantifying The Design of a Small-Scale Wave Development of a Three- Testing and Characterization of MagnetoHydrodynamic effect in and Acoustically Resonant Pulse Loss Mechanisms in a Rotating Rotor for Use As a Modified dimensional Transient Wall Heat a Liquid Hydrocarbon Fueled Rotating Detonation Combustors Combustor for Pressure-gain Detonation Engine Brayton-Cycle Engine Transfer Model of a Rotating Rotating Detonation Engine J. Braun, B. Saracoglu, T. Magin, von Combustion Applications P. Strakey, D. Ferguson, A. Sisler, M. McClearn, M. Polanka, Air Force Detonation Combustor J. Shepard, M. Polanka, Air Force Institute Kármán Institute for Fluid Dynamics, J. Lisanti, W. Roberts, King Abdullah National Energy Technology Laboratory, Institute of Technology, Wright-Patterson A. Roy, P. Strakey, T. Sidwell, D. Ferguson, of Technology, Wright-Patterson AFB, OH; Rhode-Saint-Genèse, Belgium; G. University of Science and Technology, Morgantown, WV; A. Nix, West Virginia AFB, OH; M. Mataczynski, F. Schauer, National Energy Technology Laboratory, A. Naples, Innovative Scientific Solutions, Paniagua, Purdue University, West Thuwal, Saudi Arabia University, Morgantown, WV Air Force Research Laboratory, Wright- Morgantown, WV; A. Sisler, A. Nix, West Inc., Dayton, OH; F. Schauer, Air Force Lafayette, IN Patterson AFB, OH; D. Paxson, NASA Virginia University, Morgantown, WV Research Laboratory, Wright-Patterson Glenn Research Center, Cleveland, OH AFB, OH Tuesday, 5 January 2016 193-GTE-7 Turbine Cooling II Harbor B Chaired by: A. NIX and R. ANTHONY 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs AIAA-2016-0904 AIAA-2016-0905 AIAA-2016-0906 AIAA-2016-0907 AIAA-2016-0908 AIAA-2016-0909 AIAA-2016-0910 Film Coolant Property Variation Jet Diameter Effect on Spatial Concentration Fields and An Experimental Investigation of Effect of Inlet Flow Condition on Study of the attainable flow topologies Wind Tunnel Testing of Turbine in Scaling Gas Turbine Cooling Impingement Jet Cooling on the Trajectory Investigation of Single Row Shroud Cooling Using an Upstream Heat Transfer in Pin-Fin Cooling in a supersonic blunt trailing edge at Blade Tip Flows Effectiveness Leading Edge of a Turbine Blade Film Cooling at Various Inclination Slot and Angled Discrete Holes Configurations various blowing ratios S. Lavagnoli, C. De Maesschalck, V. C. Wiese, J. Rutledge, M. Polanka, R. S. Haider, X. Yan, Southern Illinois Angles and Blowing Ratios Using Laser S. Acharya, University of Memphis, S. Singh, Louisiana State University, Y. Gorbachova, E. Valero, Technical University Andreoli, von Kármán Institute for Fluid Ashby, Air Force Institute of Technology, University, Edwardsville, IL Induced Fluorescence Memphis, TN; O. Tamunobere, Louisiana Baton Rouge, LA; S. Acharya, University of Madrid, Madrid, Spain; G. Paniagua, Dynamics, Rhode-Saint-Genèse, Belgium; Wright-Patterson AFB, OH M. Geikie, J. Sosa, C. Fernandes, K. Ahmed, State University, Baton Rouge, LA of Memphis, Memphis, TN; F. Ames, Purdue University, West Lafayette, IN; A. G. Paniagua, D. Cuadrado, Purdue J. Kapat, University of Central Florida, University of North Dakota, Fargo, Martinez-Cava, Airbus, Filton, United Kingdom; University, West Lafayette, IN Orlando, FL Fargo, ND B. Saracoglu, von Kármán Institute for Fluid Dynamics, Rhode-Saint-Genèse, Belgium Tuesday, 5 January 2016 194-HSABP-3 Scramjet Performance and Optimization Regatta A Chaired by: F. MALO-MOLINA, Raytheon Missile Systems and R. SPRINGER, The Johns Hopkins University Applied Physics Laboratory 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs AIAA-2016-0911 AIAA-2016-0912 AIAA-2016-0913 AIAA-2016-0914 AIAA-2016-0915 Reduced Edney Type-IV Cowl Shock- Mulit-Objective Optimization of a The Design of Scramjet Engine A Method to Compute Flameout Parametric Geometry Models for On-Lip Heating By Leading Edge Hypersonic Inlet Using Generalized Configurations for Optimal Limits of Scramjet-Powered Hypersonic Aircraft: Integrated Geometry Optimization Outflow Boundary Conditions in the Operational Temperature and Hypersonic Vehicles External Inlet Compression P. Rodi, Lockheed Martin Corporation, Continuous Adjoint Method Overall Engine Efficiency C. Mbagwu, J. Driscoll, University of K. Kontogiannis, University of Southampton, Houston, TX H. Kline, T. Economon, J. Alonso, Stanford F. Ferguson, N. Dasque, M. Dhanasar, Michigan, Ann Arbor, Ann Arbor, MI Southampton, United Kingdom; N. Taylor,

University, Stanford, CA North Carolina A&T State University, MBDA, Filton, United Kingdom; A. Sobester, Greensboro, NC; I. Blankson, NASA Glenn University of Southampton, Southampton, Research Center, Cleveland, OH United Kingdom Tuesday, 5 January 2016 195-ICC-2 Information and Command and Control Systems Regatta B Chaired by: M. SOTAK and J. MCEVER, The Johns Hopkins University Applied Physics Laboratory 1400 hrs 1430 hrs 1500 hrs 1530 hrs AIAA-2016-0916 AIAA-2016-0917 AIAA-2016-0918 AIAA-2016-0919 An Unknown-Input-Observer LTL Templates for Play-Calling Consensus Based Operating Wildlife Tracking on the Wing Using Based Approach for Cyber Attack Supervisory Control Picture for Distributed Battlefield Unmanned Air Systems Detection in Formation Flying UAVs T. Apker, Naval Research Laboratory, Management S. Tavakoli, A. Heaton, University of L. Lemma, S. Kim, H. Choi, Korea Washington, D.C.; B. Johnson, National K. Neema, Purdue University, West Central Lancashire, Preston, United Advanced Institute of Science and Research Council, Washington, D.C.; L. Lafayette, IN; S. Tamaskar, Cummins, Kingdom Technology, Daejeon, South Korea Humphrey, Air Force Research Laboratory, Inc., Columbus, IN; D. DeLaurentis, Purdue Wright-Patterson AFB, OH University, West Lafayette, IN Tuesday, 5 January 2016 196-IS-5 Novel Aerospace Applications of Intelligent Systems Regatta C Chaired by: C. BOWMAN and C. IPPOLITO, NASA Ames Research Center 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs AIAA-2016-0920 AIAA-2016-0921 AIAA-2016-0922 AIAA-2016-0923 AIAA-2016-0924 Helicopter Cockpit Video Data Intelligent Decentralized Unmanned Generic Clustering Approach Challenges and Opportunities in The Search for Signatures of Space Analysis for Attitude Estimation Aerial Survey of Volcanic Plumes to Track-to-Track Correlation Flight Data Mining: A Review of the Weather Effects using DBSCAN Clustering C. Ippolito, NASA Ames Research Center, for Multisensor-Multitarget State of the Art C. Bowman, Data Fusion & Neural S. Shin, I. Hwang, Purdue University, West Moffett Field, CA; D. Pieri, Jet Propulsion Environments A. Gavrilovski, H. Jimenez, D. Mavris, Networks, LLC, Broomfield, CO Lafayette, IN Laboratory, California Institute of Technology, N. Hanlon, E. Kivelevitch, M. Kumar, K. Georgia Institute of Technology, Atlanta, Pasadena, CA; M. Fladeland, NASA Ames Cohen, University of Cincinnati, Cincinnati, GA; A. Rao, S. Shin, I. Hwang, Purdue Research Center, Moffett Field, CA; J. OH University, West Lafayette, IN; et al. Lohn, J. Dolan, Carnegie Mellon University, Pittsburgh, PA Tuesday, 5 January 2016 197-LEC-5 DSC Lecture Harbor A 1400 - 1500 hrs

The Curiosity/Mars Science Laboratory Sky-Crane Landing System Jeffrey Umland Engineering Fellow Jet Propulsion Laboratory Tuesday, 5 January 2016 198-MAT-5 Fatigue & Fracture II Gaslamp B Chaired by: R. FERTIG, University of Wyoming and J. DUSTIN, GE-Aviation 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2016-0925 AIAA-2016-0926 AIAA-2016-0927 AIAA-2016-0928 AIAA-2016-0929 AIAA-2016-0930 Improved Pre-Strain Method for Experimental, numerical, and A Micromechanical Approach to A novel crack growth equation Anisotropic Fatigue Crack Growth in An equivalent crack growth model Generating Goodman Data with analytical free vibration analyses High Cycle Fatigue Analysis and based on crack tip opening High-Strength Aluminium Alloys for creep fatigue life prediction Vibration-Based Fatigue Testing of open-hole composite plates Life Prediction of Heterogeneous displacement variation S. Van Der Veen, Airbus, Toulouse, France; of metals K. Knapp, Air Force Institute of Technology, B. Aidi, Virginia Polytechnic Institute Materials S. Jiang, W. Zhang, Z. Wang, Beihang H. Dijkers, R. Alderliesten, Delft University D. Pan, F. Tahir, Y. Liu, Arizona State Wright-Patterson AFB, OH; O. Scott-Emuakpor, and State University, Blacksburg, VA; M. H. Sertse, W. Yu, Purdue University, West University, Beijing, China of Technology, Delft, The Netherlands University, Tempe, AZ T. George, C. Holycross, Air Force Research Shaat, A. Abdelkefi, New Mexico State Lafayette, IN Laboratory, Wright-Patterson AFB, OH; A. University, Las Cruces, NM; S. Case, Palazotto, Air Force Institute of Technology, Virginia Polytechnic Institute and State Wright-Patterson AFB, OH University, Blacksburg, VA Tuesday, 5 January 2016 199-MAT-6 Nanostructured Materials II Gaslamp C Chaired by: G. ODEGARD and B. WARDLE, Massachusettes Institute of Technology 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs AIAA-2016-0931 AIAA-2016-0932 AIAA-2016-0933 AIAA-2016-0934 AIAA-2016-0935 AIAA-2016-0936 AIAA-2016-0937 Effect of Combining Suspended Effect of Amount of Nylon-66 Grains size and rigid rotations Effects of POSS Addition on Modeling of strain gradient-based A Coupled Electromechanical Experimental Characterization and Particle Shapes on Shear Nanofiber Interleaf on Impact effects on the dynamics and pull-in Bisphenol-E Cyanate Ester Network nanoparticle composite plates with Peridynamics Framework for Computational Analysis of Mode Thickening Fluid Behavior Performance of AS4/3501-6 instability of electrostatically- J. Piness, J. Wiggins, University of surface elasticity Modeling Carbon Nanotube I Fracture Toughness of a Nano- C. Kabanda Mihigo, T. Lacy, S. Kundu, Carbon Epoxy Composite Laminate actuated beams Southern Mississippi, Hattiesburg, MS M. Shaat, A. Abdelkefi, New Mexico State Reinforced Polymer Composites Cellulose Z-Pin Reinforced Carbon C. Pittman , H. Toghiani, J. Warren, H. Ahmed, K. Shivakumar, North Carolina M. Shaat, A. Abdelkefi, New Mexico State University, Las Cruces, NM N. Prakash, G. Seidel, Virginia Polytechnic Fiber Laminate Mississippi State University, Starkville, MS A&T State University, Greensboro, NC University, Las Cruces, NM Institute and State University, Blacksburg, VA K. Talamadupula, S. Berry, J. O’Donnell, G. Seidel, B. Goodell, Virginia Polytechnic Institute and State University, Blacksburg, VA Tuesday, 5 January 2016 200-MDO-4 Topology Methods and Applications Balboa A Chaired by: J. DEATON, Adjoint Technologies and M. KOBAYASHI, Hawaii Evolutionary Development, LLC 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2016-0938 AIAA-2016-0939 AIAA-2016-0940 AIAA-2016-0941 AIAA-2016-0942 AIAA-2016-0943 Multi-scale Topology Optimization Large-Scale Compliance- A New Topology Optimization Experimental Validation of On a Bio-Inspired Design Methodology Combined mesh and penalization P. Dunning, H. Kim, University of Bath, Minimization and Buckling Method for Simultaneous Design Structures Optimised for Frequency for the Simultaneous Topology, Shape, adaptivity based topology Bath, United Kingdom Topology Optimization of the of Component Layout and Frame Constraints and Dynamic Loading Sizing and Subsystem Placement optimization Undeformed Common Research Structure of Aircraft Wing D. Munk, N. Giannelis, G. Vio, University Optimization of Aircrafts D. Gupta, M. Langelaar, F. van Keulen, Model Wing M. Bakhtiarinejad, S. Lee, University of of Sydney, Sydney, Australia M. Kobayashi, Hawaii Evolutionary Delft University of Technology, Delft, The T. Chin, G. Kennedy, Georgia Institute of Maryland, Baltimore County, Baltimore, Development, LLC, Honolulu, HI; R. Kolonay, Netherlands Technology, Atlanta, GA MD; J. Joo, Air Force Research Laboratory, J. Deaton, R. Reuter, Air Force Research Wright-Patterson AFB, OH Laboratory, Wright-Patterson AFB, OH Tuesday, 5 January 2016 201-MST-5 Uninhabited Aerial Systems and Vehicle Dynamics Golden Hill A Chaired by: D. KEATING and P. KENNEY, NASA Langley Research Center 1400 hrs 1430 hrs 1500 hrs 1530 hrs AIAA-2016-0944 AIAA-2016-0945 AIAA-2016-0946 AIAA-2016-0947 UAV Control and Simulation Using Recursive Bayesian Estimation of Arduino Based Low-Cost Experimental Simulation Enviroment for Testing Trajectory Transcriptions Bat Flapping Flight Using Kinematic Unmanned Aerial Flight System For UAS Collision Avoidance System C. Ashokkumar, G. York , U.S. Air Force Trees Attitude Determination in Autonomous S. Bhandari, E. Gomez, D. Garcia, M. Academy, Colorado Springs, CO M. Bender, H. McClelland, A. Kurdila, R. Flights Piana, M. Ritterbush, California Polytechnic Mueller, Virginia Polytechnic Institute and J. Rico, K. Turkoglu, San Jose State University, State University, Pomona, CA State University, Blacksburg, VA San Jose, CA Tuesday, 5 January 2016 202-NDA-3 Testing in Support of Model Calibration or Uncertainty Quantification Old Town B Chaired by: E. WALKER, NASA Langley Research Center and B. SMARSLOK, Air Force Reseach Laboratory 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2016-0948 AIAA-2016-0949 AIAA-2016-0950 AIAA-2016-0951 AIAA-2016-0952 AIAA-2016-0953 Robust Statistical Modeling of Improved Test Planning and Analysis Simulating Future Test and A-B Basis Allowable Test Reduction Robust Test Resource Allocation Experimental Validation of Piezoelectric Axial Fatigue Tests Through the Use of Advanced Redesign Considering Epistemic Approach and Composite Generic using Global Sensitivity Analysis Polynomial Chaos Theory on an using Bayesian Model Averaging Statistical Methods Model Uncertainty Basis Strength Values C. Li, S. Mahadevan, Vanderbilt University, Aircraft T-Tail J. Beck, Perceptive Engineering Analytics, L. Green, NASA Langley Research Center, N. Price, University of Florida, Gainesville, F. Abdi, AlphaSTAR Corporation, Long Nashville, TN P. Cheema, D. Munk, N. Giannelis, G. Vio, Lino Lakes, MN; O. Scott-Emuakpor, J. Hampton, VA; K. Maxwell, University of Gainesville, FL; M. Balesdent, . Defoort, Beach, CA; E. Clarkson, Wichita State University of Sydney, Sydney, Australia Brown, T. George, C. Holycross, Air Force Minnesota, Minneapolis, Minneapolis, MN; ONERA, Palaiseau, France; R. Le Riche, University, Wichita, KS; C. Godines, S. Research Laboratory, Wright-Patterson D. Glass, W. Vaughn, NASA Langley Research École Nationale Supérieure des Mines DorMohammadi , AlphaSTAR Corporation, AFB, OH Center, Hampton, VA; W. Barger, University of de Saint-Étienne, Saint-Etienne, France; Long Beach, CA Washington, Seattle, Seattle, WA; M. Cook, N. Kim, R. Haftka, University of Florida, Brigham Young University, Provo, UT Gainesville, Gainesville, FL Tuesday, 5 January 2016 203-PANEL-6 Tuesday Afternoon Forum 360 Seaport F-G 1400 - 1600 hrs Cybersecurity Below 30,000 Feet—Applying Lessons From Other Industries Moderator: Chan Lieu, Senior Legislative Advisor, Venable,

Panelists: Jeffrey Carr Scott Erven Jake Olcott CEO Associate Director VP Business Development Taia Global Protiviti BitSight Tuesday, 5 January 2016 204-PC-8 Micro-Propulsion, Plasma Discharges, Autoignition Cortez Hill C Chaired by: C. CADOU, University of Maryland and M. COIL, Orbital Technologies Corporation 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs AIAA-2016-0954 AIAA-2016-0955 AIAA-2016-0956 AIAA-2016-0957 AIAA-2016-0958 AIAA-2016-0959 AIAA-2016-0960 Performance Testing of Various Coarse graining of Ethylammonium Near-blowoff dynamics of lean Monte Carlo Simulation of the Measurements of Low Temperature Comparative Shock-Tube Study of The Effect of Ozone Addition

Nozzle Designs for Water Nitrate using Effective Field Coarse premixed flames stabilized on a Effect of “Hot” Atoms on Active Oxidation of n-Heptane/O2/Ar Autoignition and Plasma-Assisted on Autoignition and Flame Electrolysis Thruster Graining Method meso-scale bluff body Species Production in High-Voltage Mixtures in Nanosecond-pulsed Ignition of C2-Hydrocarbons Stabilization Y. Liu, Air Force Institute of Technology, N. Mehta, D. Levin, University of Illinois, Y. Kim, B. Lee, H. Im, King Abdullah Pulsed Discharges Plasma Discharges I. Kosarev, S. Kindysheva, E. Plastinin, X. Gao, J. Zhai, W. Sun, Georgia Institute Wright-Patterson AFB, OH Urbana-Champaign, Urbana, IL University of Science and Technology, N. Aleksandrov, A. Ponomarev, Moscow A. Rousso, J. Lefkowitz, Y. Ju, Princeton N. Aleksandrov, Moscow Institute of of Technology, Atlanta, GA; T. Ombrello, Thuwal, Saudi Arabia Institute of Physics and Technology, University, Princeton, NJ Physics and Technology, Moscow, Russia C. Carter, Air Force Research Laboratory, Moscow, Russia ; A. Starikovskiy, ; A. Starikovskiy, Princeton University, Wright-Patterson AFB, OH Princeton University, Princeton, NJ Princeton, NJ Tuesday, 5 January 2016 205-SATS-2 Small Satellites - Technologies II Ocean Beach Chaired by: J. STRAUB, University of North Dakota 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2016-0961 AIAA-2016-0962 AIAA-2016-0963 AIAA-2016-0964 AIAA-2016-0965 AIAA-2016-0966 Selection of an Inertial Dual Propulsion System Design for Development of an Additively System Design and Dynamic Feasibility for Orbital Life Extension Utilizing the Globalstar Network for Measurement Unit for High Small Spacecraft Manufactured Microthruster for Analysis for Sail Deployment for of a CubeSat Flying in the Lower Satellite Communications in Low Accuracy CubeSat Attitude A. Ratheesh, K. Naik, P. Putambekar, P. Nanosatellite Applications Cube Satellite CNUSAIL-1 Thermosphere Earth Orbit Determination Shrivastava, J. Dhanasekaran, P. Malani, K. Gagne, D. Hitt, University of Vermont, S. Song, Y. Yoo, S. Koo, S. Kim, J. Suk, J. Blandino, N. Martinez, M. Demetriou, N. A. Santangelo, sci_Zone, Inc., Holland, M. Sorgenfrei, M. Nehrenz, D. Kemp, SRM University, Chennai, India; et al. Burlington, Burlington, VT; M. McDevitt, Chungnam National University, Daejeon, Gatsonis, Worcester Polytechnic Institute, MI; P. Skentzos, Dornerworks, Grand NASA Ames Research Center, Moffett GreenScale Technologies, South South Korea Worcester, MA; N. Paschalidis, NASA Goddard Rapids, MI

Field, CA Burlington, VT Space Flight Center, Greenbelt, MD Tuesday, 5 January 2016 206-SCS-2 High-Strain Composite Materials and Structures Balboa B Chaired by: D. MURPHY, Orbital ATK-Space Components and J. STEEVES, NASA JPL 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs AIAA-2016-0967 AIAA-2016-0968 AIAA-2016-0969 AIAA-2016-0970 AIAA-2016-0971 Deployment Testing of Flexible Reconfigurable Deployable CubeSat Precision High Strain Composite Folding and Deployment of Free Deployment of a Sparse- Composite Hinges in Bi-Material Solar Arrays Usin Thin Composite Hinges for the Deployable In-Space Closed Cross-Section Dual-Matrix Isogrid Column with High Strain Beams Flexures Coherent Imaging Telescope Composite Booms Composite Ribs J. Sauder, Jet Propulsion Laboratory, R. Yasin, M. Santer, Imperial College M. Silver, M. Echter, B. Reid, Lincoln M. Sakovsky, S. Pellegrino, California S. Jeon, LoadPath, LLC, Albuquerque, NM; California Institute of Technology, London, London, United Kingdom Laboratory, Massachusetts Institute of Institute of Technology, Pasadena, CA; H. J. Banik, M. Peterson, Air Force Research Pasadena, CA; B. Trease, University of Technology, Lexington, MA; J. Banik, Air Force Mallikarachchi, University of Moratuwa, Laboratory, Kirtland AFB, NM Toledo, Toledo, OH Research Laboratory, Kirtland AFB, NM Katubedda, Sri Lanka Tuesday, 5 January 2016 207-SE-3 Systems Engineering III Balboa C Chaired by: M. BAILEY, Defense Acquisition University and V. JOHNSON, Textron Aviation 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs AIAA-2016-0972 AIAA-2016-0973 AIAA-2016-0974 AIAA-2016-0975 AIAA-2016-0976 A Game Theory approach to Understanding the Impact of Quantifying the Effect of Orbit The Devil is in the Detail – Fundamentals of Weapon System Bargaining over Attributes of Uncertainty on the Fidelity of the Altitude on Mission Cost for Earth Continuous Airworthiness of Sustainment Complex Systems in the context of Value Model Observation Satellites Aircraft Servo Control Units C. Vono, Self, Ogden, UT Value-Driven Design T. Subramanian, A. Khol, H. Kannan, A. Shao, A. Madni, J. Wertz, University of T. Lammering, P. Forschner, L. Faleiro, T. G. Bhatia , H. Kannan, C. Bloebaum, Iowa E. Winer, C. Bloebaum, Iowa State Southern California, Los Angeles, CA Schneider, Liebherr-Aerospace Lindenberg State University, Ames, IA University, Ames, IA GmbH, Lindenberg , Germany Tuesday, 5 January 2016 208-STR-6 Composite Fatigue Damage Prediction Methods La Jolla A Chaired by: G. MABSON, Boeing Engineering Operations & Technology and K. LIN, University of Washington 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2016-0977 AIAA-2016-0978 AIAA-2016-0979 AIAA-2016-0980 AIAA-2016-0981 AIAA-2016-0982 Fatigue Analysis of Notched Fatigue Validation of Composite Fatigue Life Prediction of Three-Dimensional Delamination Interlaminar Fatigue Growth for Fatigue Life of Postbuckled Laminates: A Time-Efficient Macro- Open Hole Analysis Technique IM7/977-3 Composite Laminates Analysis in Composite Open Hole Fail-Safe Life Limit Analysis Structures with Indentation Mechanical Approach for Standard and Nonstandard with Multispatial/Multitemporal Tensile Specimens with Cohesive B. Flansburg, Lockheed Martin Damage P. Naghipour, Ohio Aerospace Institute, Laminate - Part 2 Homogenization Zone Method Corporation, Marietta, GA; C. Rousseau, C. Davila, NASA Langley Research Center, Cleveland, OH; E. Pineda, B. Bednarcyk, F. Abdi, C. Godines, S. DorMohammadi M. Bogdanor, C. Oskay, Vanderbilt B. Bartan, B. Acar, ROKETSAN Missile Lockheed Martin Corporation, Fort Hampton, VA; C. Bisagni, Delft University S. Arnold, NASA Glenn Research Center, , AlphaSTAR Corporation, Long Beach, University, Nashville, TN Industries, Inc., Ankara, Turkey; A. Kayran, Worth, TX; J. Action, Lockheed Martin of Technology, Delft, The Netherlands Cleveland, OH; A. Waas, University of CA; L. Minnetyan, Clarkson University, Middle East Technical University, Ankara, Corporation, Marietta, GA Michigan, Ann Arbor, Ann Arbor, MI Potsdam, NY Turkey Tuesday, 5 January 2016 209-STR-7 Failure Analysis and Prediction II La Jolla B Chaired by: C. MERRETT, Carleton University and P. AGGARWAL, NASA Marshall Space Flight Center 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs AIAA-2016-0983 AIAA-2016-0984 AIAA-2016-0985 AIAA-2016-0986 AIAA-2016-0987 AIAA-2016-0988 AIAA-2016-0989 Progressive Failure Based On Strain A Residual Strength Prediction Probabilistic First Ply Failure Thermal Ablation in Fiber- Residual Stress Failure Prediction of Predicting Composite Fatigue Life A Beam Theory for Progressively Invariant Failure Theory Methodology for Composite Analysis of Wind Turbine Blade Reinforced Composite Laminates Adhesive Bonded Joints Through a of Wind Turbine Blades Using Elastic Damage in Fiber-Reinforced V. Goyal, C. Garcia, University of Puerto Laminates Wth Surface Damage Laminates Subjected to Continuing Lightning Combined CZ and XFEM Model Constituent-Level Physics and Realistic Composite Structures Rico, Mayaguez, Under Tensile Loading G. Mustafa, A. Suleman, C. Crawford, Current V. Goyal, University of Puerto Rico, Aerodynamic Load F. Jiang, W. Yu, Purdue University, West S. Russell, Triumph Aerostructures, University of Victoria, Victoria, Canada Y. Wang, O. Zhupanska, University of Mayaguez, F. Bhuiyan, D. Mavriplis, R. Fertig, University Lafayette, IN Arlington, TX Iowa, Iowa City, Iowa City, IA of Wyoming, Laramie, Laramie, WY Tuesday, 5 January 2016 210-TES-5 Design of Energy Systems Gaslamp A Chaired by: S. AREPALLI 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs AIAA-2016-0990 AIAA-2016-0991 AIAA-2016-0992 AIAA-2016-0993 AIAA-2016-0994 AIAA-2016-0995 AIAA-2016-0996 Component and System Modeling Analysis of a Directly Heated Development of Self-Healing A modified Cellular automaton model On the Computations of Aircraft Smoke Behaviour and Numerical Investigations of Flow of a Direct Power Extraction System Oxyfuel Supercritical Power Materials for use in Wind Turbine evaluation of the dendritic nucleation Postcrash Fires Management in Domed Mosques Patterns and Thermal Comfort in O. Vidana, M. Chaidez, B. Lovich, J. Generation System Blades and growth during alloys solidification E. Khalil, M. Othman, Cairo University, E. Khalil, E. Bialy, W. Abdelmaksoud, O. Air-Conditioned Gymnastic Sport Aboud, M. Hernandez, L. Cabrera , A. Chowdhury, L. Bugarin, A. Badhan, A. Matt, S. Strong, R. Amano, University A. Reikher, Shilloh Industry, Milwaukee, WI; R. Giza, Egypt Selim, Cairo University, Giza, Egypt Facility University of Texas, El Paso, El Paso, N. Love, University of Texas, El Paso, El of Wisconsin, Milwaukee, Glendale, WI Amano, University of Wisconsin, Milwaukee, E. Khalil, T. AlHababi, Cairo University, TX; et al. Paso, TX Glendale, WI Cairo, Egypt Tuesday, 5 January 2016 211-TP-6 Special Session: Aerothermodynamics of Meteor Entries Harbor G Chaired by: A. BRANDIS, ERC Incorporated and D. PRABHU, ERC Incorporated 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs Oral Presentation AIAA-2016-0997 Oral Presentation Oral Presentation Oral Presentation AIAA-2016-0998 AIAA-2016-0999 NASA’s New Program to The internal structure of Earth- Computational Modeling of Thermophysics issues relevant to Shock Layer Characteristics of Numerical Simulation of Bolide Entry Airborne observations of an Characterize Risk of Potential impacting meteoroids: The view from Asteroid Airbursts high-speed Earth entry of large Meteors at Entry Velocities below with Ground Footprint Prediction asteroid entry for high fidelity Asteroid Strikes the microscope, the laboratory bench, M. Boslough, Sandia National asteroids 25 km/s M. Aftosmis, M. Nemec, D. Mathias, NASA modeling J. Arnold, C. Burkhard, E. Venkatapathy, and the telescope. Laboratories, Albuquerque, NM D. Prabhu, D. Saunders, R. Jaffe, E. Stern, C. Johnston, NASA Langley Research Ames Research Center, Moffett Field, CA; M. P. Jenniskens, SETI Institute, Mountain D. Morrison, NASA Ames Research Center, D. Sears, K. Bryson, D. Ostrowski, NASA Ames Y. Chen, S. White, NASA Ames Research Center, Hampton, VA; A. Brandis, NASA Berger, New York University, New York, NY View, CA; J. Grinstead, NASA Ames Moffett Field, CA Research Center, Moffett Field, CA Center, Moffett Field, CA; et al. Ames Research Center, Moffett Field, CA Research Center, Moffett Field, CA Tuesday, 5 January 2016 212-UMS-4 Unmanned Systems: UAS Integration into National Airspace System and Civil Applications Coronado A Chaired by: A. LACHER, The MITRE Corporation and V. SCHULTZ, NASA Langley Research Center 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2016-1000 AIAA-2016-1001 AIAA-2016-1002 AIAA-2016-1003 AIAA-2016-1004 AIAA-2016-1005 Safety Assessment of Unmanned A Game Theoretical Modeling and The Impact of Suggestive Maneuver Linear-Optimization-Based Use of a Small Unmanned Wildfire Plume Tracking and Aerial Vehicle Operations in an Simulation Framework For The Guidance on UAS Pilot Performing Path Planning Algorithm for an Aircraft System for autonomous Dynamics Using UAS Integrated Airspace Integration Of Unmanned Aircraft the Detect and Avoid Function Agricultural UAV fire spotting at the Great Dismal F. Keating, T. Mitchell, J. Kidd, J. Jacob, Y. Jenie, E. Van Kampen, J. Ellerbroek, J. Systems In To The National Airspace R. Rorie, L. Fern, San Jose State A. Noriega, R. Anderson, Embry-Riddle Swamp Oklahoma State University, Stillwater, OK Hoekstra, Delft University of Technology, N. Musavi, Bilkent University, Ankara, University, San Jose, CA; J. Shively, NASA Aeronautical University, Daytona Beach, FL M. Logan, L. Glaab, NASA Langley Delft, The Netherlands Turkey; K. Tekelioğlu, Bogazici University, Ames Research Center, Moffett Field, CA Research Center, Hampton, VA; T. Craig, Ankara, Turkey; Y. Yildiz, K. Gunes, D. U.S. Fish and Wildlife Service, Suffolk, VA Onural, Bilkent University, Ankara, Turkey Tuesday, 5 January 2016 213-WE-4 Wind Energy: Aero-Elastic Modeling and Validation Harbor I Chaired by: L. MANUEL, University of Texas at Austin 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs AIAA-2016-1006 AIAA-2016-1007 AIAA-2016-1008 AIAA-2016-1009 AIAA-2016-1010 The Unsteady Aerodynamic Development and Validation of a Verification and Validation of FAST Aeroelastic stability evaluation of Using Pretwist to Reduce Power Response of an Airfoil with New Unsteady Airfoil Aerodynamics for Aero-Elastically Tailored Blades bend-twist coupled composite wind Loss of Bend-Twist Coupled Blades Microtabs and it’s Implications for Model Within AeroDyn S. Guntur, S. Schreck, J. Jonkman, turbine blades designed for load A. Stäblein, C. Tibaldi, M. Hansen, Aerodynamic Damping R. Damiani, G. Hayman, Q. Wang, J. National Renewable Energy Laboratory, alleviation in wind turbine systems Technical University of Denmark, Roskilde, M. Lennie, A. Bach, G. Pechlivanoglou, C. Jonkman, National Renewable Energy Golden, CO; M. Singh, M. Hind, Siemens, T. Farsadi, A. Kayran, Middle East Technical Denmark Nayeri, C. Paschereit, Technical University Laboratory, Golden, CO; A. Gonzalez, Boulder, CO University, Ankara, Turkey

of Berlin, Berlin, Germany CENER, Navarra, Spain Tuesday, 5 January 2016 214-NW-8 Tuesday Afternoon Networking Coffee Break Session Room Foyers 1530 - 1600 hrs Tuesday, 5 January 2016 215-PANEL-7 DSC: Panel Discussion and Open Forum on the 2nd Aeroelastic Prediction Workshop Harbor A 1530 - 1730 hrs Tuesday, 5 January 2016 216-LEC-6 Dryden Lectureship in Research Seaport F-G 1730 - 1830 hrs

Blended Wing Body Technology Readiness Robert H. Liebeck Senior Technical Fellow The Boeing Company Tuesday, 5 January 2016 217-NW-9 Reception in the Exposition Hall Exposition Hall 1830 - 2000 hrs Doors Open at 1815 hrs. Wednesday Wednesday, 6 January 2016 218-NW-10 Wednesday Early Morning Networking Coffee Break Session Room Foyers 0700 - 0730 hrs Wednesday, 6 January 2016 219-SB-3 Wednesday Morning Speakers’ Briefing Session Rooms 0730 - 0800 hrs Wednesday, 6 January 2016 220-PLNRY-3 Wednesday Morning Keynote Seaport A-E 0800 - 0900 hrs

Designing for Resilience Jeff Holland Director U.S. Army Engineer Research and Development Center Wednesday, 6 January 2016 221-AA-5 Aeroacoustics - Advanced Measurement and Experiment Nautical Chaired by: E. NESBITT, The Boeing Company and C. ROYALTY, Honeywell 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2016-1011 AIAA-2016-1012 AIAA-2016-1013 AIAA-2016-1014 AIAA-2016-1015 AIAA-2016-1016 On the factors affecting the Tomographic-PIV investigation of Vibro-acoustic analysis of flight PIV Investigation of the Flow Past Supersonic Jet Impingement on a Vibroacoustic loads during the end performance of the generalized the flow over serrated trailing- test data comprising fuselage Solid and Slitted Sawtooth Serrated Model-scale Jet Blast Deflector effects regime of clustered rockets cross validation method in the edges vibrations, external pressure and Trailing Edges T. Worden, C. Shih, F. Alvi, Florida State R. Rojo, C. Tinney, University of Texas, context of nearfield acoustic F. Avallone, C. Arce Leon, S. Pröbsting, interior cabin noise measurements C. Arce Leon, F. Avallone, S. Pröbsting, University, Tallahassee, FL Austin, Austin, TX; J. Ruf, NASA Marshall holography K. Lynch, D. Ragni, Delft University of M. Norambuena, M. Böswald, Y. Govers, D. Ragni, Delft University of Technology, Space Flight Center, Huntsville, AL K. Chelliah, G. Raman, R. Muehleisen, Technology, Delft, The Netherlands German Aerospace Center (DLR), Delft, The Netherlands Illinois Institute of Technology, Chicago, IL Göttingen, Germany Wednesday, 6 January 2016 222-ABPSI-5 High Speed Propulsion Integration Hillcrest D Chaired by: S. BAUER, NASA LaRC and P. SHEA, NASA Langley Research Center 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2016-1017 AIAA-2016-1018 AIAA-2016-1019 AIAA-2016-1020 AIAA-2016-1021 Numerical analysis for higher Numerical simulation of shock Multistage Optimization Applied Bi-Objective Switching Control Design Shock Wave Structure of Supersonic ejector-jet performance in the RBCC trains in a 3D channel to the Hypersonic Inward Turning for a Tradeoff between Acceleration Droplets in Under-expanded Jet engine combustor model R. Fiévet, H. Koo, V. Raman, University Inlet Design and Unstart in Hypersonic Airframe/ Y. Kim, Korea Aerospace Research Institute S. Hasegawa, K. Tani, S. Ueda, Japan of Michigan, Ann Arbor, Ann Arbor, MI; A. J. Wang, J. Cai, Northwestern Propulsion Models (KARI), Daejeon, South Korea Aerospace Exploration Agency (JAXA), Auslender, NASA Langley Research Center, Polytechnical University, Xi’an, China X. Hao, J. Chang, B. Wen, Z. Zhang, Harbin Kakua, Japan Hampton, VA Institute of Technology, Harbin, China Wednesday, 6 January 2016 223-ACD-4 Electric Aircraft Design Bankers Hill Chaired by: R. VOS and R. BARRETT-GONZALEZ, The University of Kansas 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2016-1022 AIAA-2016-1023 AIAA-2016-1024 AIAA-2016-1025 AIAA-2016-1026 Overcoming the Adoption Barrier to Comparison of Heat Exchanger and A Highly Efficient Solid Oxide Fuel Modeling of Electric Motor Driven Design and Optimization of Short- Electric Flight Thermal Energy Storage Designs Cell Power System for an All- Variable Pitch Propellers for Range Aluminum-Air Powered N. Borer, C. Nickol, F. Jones, R. Yasky, K. for Aircraft Thermal Management Electric Commuter Airplane Flight Conceptual Aircraft Design Aircraft Woodham, J. Fell, NASA Langley Research Systems Demonstrator R. McDonald, California Polytechnic State J. Vegh, J. Alonso, Stanford University, Center, Hampton, VA; et al. W. Reed, M. von Spakovsky, P. Raj, T. Stoia, S. Atreya, P. O’Neil, The Boeing University, San Luis Obispo, CA Stanford, CA Virginia Polytechnic Institute and State Company, Huntington Beach, CA University, Blacksburg, VA Wednesday, 6 January 2016 224-ACD-5 Transport Aircraft Design I Cortez Hill A Chaired by: M. ORR, Boeing Commercial Airplanes and J. MERRET, Gulfstream Aerospace Corporation 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2016-1027 AIAA-2016-1028 AIAA-2016-1029 AIAA-2016-1030 AIAA-2016-1031 AIAA-2016-1032 Conceptual Design of a Single-Aisle Mission Analysis and Aircraft Design Study for a Highly Fuel Assessment of the Performance Design, Economic Competitiveness, Conceptual Design of Biplane with Turboelectric Commercial Transport Sizing of a Hybrid-Electric Regional Efficient Regional Transport Potential of Advanced Subsonic and Profitability of a 2025 LNG High Aspect Ratio Wings as Next with Fuselage Boundary Layer Aircraft J. Kirkman, D. Wood, T. Knight, M. Transport Concepts for NASA’s Fueled Turboprop for the LNG Air Generation Civil Jet Transport Ingestion K. Antcliff, M. Guynn, T. Marien, D. Wells, Gurczak, C. Rothlsiberger, K. Pan, Arizona Environmentally Responsible Transportation System T. Masuko, T. Imamura, K. Rinoie, J. Welstead, NASA Langley Research NASA Langley Research Center, Hampton, State University, Tempe, AZ; et al. Aviation Project J. Gibbs, B. Nagel, German Aerospace University of Tokyo, Tokyo, Japan; T. Center, Hampton, VA; J. Felder, NASA VA; S. Schneider, M. Tong, NASA Glenn C. Nickol, NASA Langley Research Center, Center (DLR), Hamburg, Germany Nomura, Japan Aerospace Exploration Glenn Research Center, Cleveland, OH Research Center, Cleveland, OH Hampton, VA; W. Haller, NASA Glenn Agency (JAXA), Chofu, Japan Research Center, Cleveland, OH Wednesday, 6 January 2016 225-AFM-7 Aircraft Flight Dynamics, Handling Qualities, and Performance I Harbor A Chaired by: M. LONE, Cranfield University and B. LEONHARDT, Northrop Grumman Corporation 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2016-1033 AIAA-2016-1034 AIAA-2016-1035 AIAA-2016-1036 AIAA-2016-1037 AIAA-2016-1038 An Approach to Flight Control with Switch-Induced Simulated PIO: Dynamics and Aerodynamics of a Low-Speed Stability and Control Modeling and Bifurcation Analysis Analysis of Spin Characteristics of a Large Time Delays Derived from a Relay Feedback as a Flight Test Landing Airplane during a High- of a Reduced Scale Long-Range of Combat Aircraft Dynamics under High Performance Aircraft with High Pulsive Human Control Strategy Technique for Pilot-in-the-Loop Speed Lateral Runway Departure Supersonic Configuration with Lateral C.M. Shift Alpha Yawing Moment Asymmetry T. Fricke, F. Holzapfel, Technical University Stability D. Horak, K. Renze, National Reduced-Size or No Vertical Tail B. Mukherjee, M. Sinha, Indian Institute of J. Masud, B. Malik, Air University, Islamabad, of Munich, Garching, Germany W. Gray, U.S. Air Force Test Pilot School, Transportation Safety Board, Washington, S. Langston, C. Nelson, E. Livne, University Technology Kharagpur, Kharagpur, India Pakistan; S. Akhtar, National University of Edwards AFB, CA D.C. of Washington, Seattle, Seattle, WA Sciences and Technology, Risalpur, Pakistan Wednesday, 6 January 2016 226-AFM-8 Special Session: LOC-5: Aircraft Loss of Control (LOC) Modeling Methods Coronado B Chaired by: C. BELCASTRO, NASA-Langley Research Center and D. CRIDER, National Transportation Safety Board 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2016-1039 AIAA-2016-1040 AIAA-2016-1041 AIAA-2016-1042 AIAA-2016-1043 Parameter Estimation for Extending Semi-Analytical and Empirical Status of Computational Aerodynamic Nonlinear Unsteady Aerodynamic Extending the operational envelope Flight Models into Post-Stall Regime Approaches to Aircraft Modeling Tools for Aircraft Loss-of- Modeling Using Wind Tunnel and of a turbofan engine simulation - Invited Configuration Effects on Post-Stall Control - Invited Computational Data - Invited into the sub-idle region - Invited S. Liu, Z. Luo, G. Moszczynski, P. Grant, Aerodynamics - Invited N. Frink, P. Murphy, H. Atkins, S. Viken, P. Murphy, V. Klein, N. Frink, NASA Langley J. Chapman, T. Guo, NASA Glenn Research University of Toronto, Toronto, Canada T. Teng, T. Zhang, P. Grant, University of J. Petrilli, NASA Langley Research Center, Research Center, Hampton, VA Center, Cleveland, OH Toronto, Toronto, Canada Hampton, VA; A. Gopalarathnam, North Carolina State University, Raleigh, NC; et al. Wednesday, 6 January 2016 227-AMT-5 Tomographic, Holographic and Other Volumetric Measurements Harbor D Chaired by: B. THUROW, Auburn University and C. GOYNE, University of Virginia 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2016-1044 AIAA-2016-1045 AIAA-2016-1046 AIAA-2016-1047 AIAA-2016-1048 AIAA-2016-1049 AIAA-2016-1050 kHz Rate Digital In-line Holography A Preliminary Comparison of Three Optical phase conjugate digital 3-D Visualization of Compressible Instantaneous Pressure Instantaneous Pressure Tomographic schlieren system for Applied to Quantify Secondary Dimensional Particle Tracking and inline holography for correcting Flow Using a Plenoptic Camera and Measurements from Large-Scale Reconstruction from Measured visualisation of supersonic jet Droplets from the Aerodynamic Sizing using Plenoptic Imaging and aberrations in particle-laden flames Background Oriented Schlieren Tomo-PTV with HFSB Tracers past a Pressure Gradient using Rotating N. Raju, Technical University of Munich (TUM Breakup of a Liquid Column in a Digital In-line Holography K. Gabet Hoffmeister, S. Kearney, J. Klemkowsky, B. Thurow, Auburn Surface-Mounted Finite Cylinder Parallel Ray Method Asia), Singapore, Singapore; M. Prabakar, Shock-Tube E. Munz, Auburn University, Auburn, AL; D. D. Guildenbecher, Sandia National University, Auburn, AL; R. Mejia-Alvarez, J. Schneiders, G. Caridi, A. Sciacchitano, X. Liu, J. Moreto, S. Siddle-Mitchell, San Indian Institute of Technology Madras, D. Guildenbecher, J. Wagner, J. Olles, E. Guildenbecher, P. Farias, Sandia National Laboratories, Albuquerque, NM Los Alamos National Laboratory, Los F. Scarano, Delft University of Technology, Diego State University, San Diego, CA Chennai, India; B. Medhi, Indian Institute of Demauro, P. Farias, T. Grasser, Sandia National Laboratories, Albuquerque, NM; B. Thurow, Alamos, NM Delft, The Netherlands Science, Bangalore, India; O. Oliver M, T. M. Laboratories, Albuquerque, NM; et al. Auburn University, Auburn, AL Thiruchengode, Indian Institute of Technology Madras, Chennai, India Wednesday, 6 January 2016 228-APA-22 Special Session: CREATE-AV HPC Multiphysics Applications of Full-up Air Vehicles II Coronado E Chaired by: N. HARIHARAN, CREATE-AV and A. WISSINK, US Army Aeroflightdynamics Directorate 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2016-1051 AIAA-2016-1052 AIAA-2016-1053 AIAA-2016-1054 AIAA-2016-1055 AIAA-2016-1056 AIAA-2016-1057 Accuracy and Performance CREATE-MG Capstone version 5 X-56A Aeroelastic Flight Test Comparison Between HPCMP Time dependent Forcing for Flow Unstructured/Structured Overset Maneuvering Rotorcraft Simulations Improvements to Kestrel’s Near- Applications Predictions CREATETM-AV COFFE and Kestrel Control on a FlutteringWing using Methods for Flow Solver Using Using CREATE A/VTM Helios Body Flow Solver D. Hine, J. Forsythe, B. Green, B. Hallissy, D. Reasor, Air Force Research Laboratory, for Two and Three-Dimensional HPCMP CREATE™-AV Kestrel Hamiltonian Paths and Strand Grids B. Roget, Science and Technology Corporation, D. McDaniel, R. Nichols, CREATE Kestrel E. Lynch, T. Shafer, Naval Air Systems Eglin AFB, FL; K. Bhamidipati, Air Force Turbulent Flow Cases S. Jurgen, U.S. Air Force Academy, Y. Jung, B. Govindarajan, J. Baeder, Moffett Field, CA; J. Sitaraman, Parallel Team, Arnold AFB, TN; T. Eymann, R. Command, Patuxent River, MD Test Center, Edwards AFB, CA; A. Chin, R. Glasby, J. Erwin, University of Colorado Springs, CO University of Maryland, College Park, Geometric Algorithms, LLC, Sunnyvale, CA; A. NASA Armstrong Flight Research Center, Wissink, Army Aviation and Missile Research Starr, S. Morton, CREATE Kestrel Team, Tennessee, Oak Ridge, Oak Ridge, TN College Park, MD Eglin AFB, FL Edwards, CA Development and Engineering Center, Moffett Field, CA Wednesday, 6 January 2016 229-APA-23/FD-27 Special Session: NASA’s Revolutionary Computational Aerosciences I Coronado D Chaired by: M. MALIK, NASA-Langley Research Center and M. ROGERS, NASA-Ames Research Center 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs Oral Presentation AIAA-2016-1058 AIAA-2016-1059 AIAA-2016-1060 AIAA-2016-1061 AIAA-2016-1062 Revolutionary Computational Towards an Entropy Stable A Space-Time Discontinuous- The Space-Time Conservative Schemes Overview of the NASA Glenn Flux An Overview of Combined Aerosciences (Invited) Spectral Element Framework for Galerkin Approach for Separated for Large-Scale, Time-Accurate Flow Reconstruction Based High-Order Uncertainty and A-Posteriori M. Malik, NASA Langley Research Center, Computational Fluid Dynamics Flows Simulations with Tetrahedral Meshes Unstructured Grid Code Error Bound Estimates for CFD Hampton, VA M. Carpenter, M. Parsani, E. Nielsen, S. Murman, L. Diosady, A. Garai, M. Ceze, B. Venkatachari, National Institute of S. Spiegel, J. DeBonis, H. Huynh, NASA Calculations NASA Langley Research Center, Hampton, NASA Ames Research Center, Moffett Aerospace, Hampton, VA; C. Streett, C. Chang, Glenn Research Center, Cleveland, OH T. Barth, NASA Ames Research Center, VA; T. Fisher, Sandia National Laboratories, Field, CA NASA Langley Research Center, Hampton, Moffett Field, CA Albuquerque, NM VA; D. Friedlander, X. Wang, S. Chang, NASA Glenn Research Center, Cleveland, OH Wednesday, 6 January 2016 230-APA-24 Low Speed, Low Reynolds Number Aerodynamics Americas Cup B Chaired by: K. VANDEN, USAF 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2016-1063 AIAA-2016-1064 AIAA-2016-1065 AIAA-2016-1066 AIAA-2016-1067 AIAA-2016-1068 Performance Conscience Lateral Analytical Aerodynamic Model of Time Spectral Method for Unsteady Experimental Investigation Three-dimensional Effects in the Further Insight into Stratified Stability Tuning of Low Aspect Ratio Chordwise Flexible Flapping Wings Confined Viscous Flows with of Three-Dimensional Flow Wake Vortex Formation of Flapping Turbulent Wakes Behind Wings Flyers in Forward Flight Variable Inflow Velocity at Low Development by Pitching Low- Flat Plate in Hover S. Gunasekaran, A. Altman, University of T. Linehan, K. Mohseni, University of D. Kodali, C. Kang, University of Alabama, Reynolds Numbers Aspect-Ratio Wing S. Chintamani, A. Rege, B. Dennis, K. Dayton, Dayton, OH Florida, Gainesville, Gainesville, FL Huntsville, Huntsville, AL D. Mateescu, A. Khaled, McGill University, H. Yu, National Defense University, Subbarao, University of Texas, Arlington, Montréal, Canada Taoyuan, Taiwan; L. Bernal, University of Arlington, TX Michigan, Ann Arbor, Ann Arbor, MI Wednesday, 6 January 2016 231-APA-25 Aerodynamic Testing: Wind-Tunnel I Americas Cup C Chaired by: J. MURRAY, Sandia National Laboratories and G. GATLIN, NASA Langley Research Center 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2016-1069 AIAA-2016-1070 AIAA-2016-1071 AIAA-2016-1072 AIAA-2016-1073 Dynamic Wind Tunnel Simulation of Schlieren Visualization Technique for Experimental Investigation of the Detection of Unsteady Boundary Wind Tunnel Testing of Wings in Aircraft Wake Vortex Trajectory in High-Enthalpy and Low-Density Flow Turbulent Aerodynamic Environment Layer Transition Using Three Spin Ground Proximity. with LED Light Source Produced by a Generic Ship Experimental Methods A. Ragheb, M. Selig, University of Illinois, J. Holt, K. Garry, Cranfield University, N. Morimoto, J. Yamashita, A. Tabata, S. Aso, A. Sydney, J. Ramsey, K. Kimmel, Naval K. Richter, C. Wolf, A. Gardner, C. Urbana-Champaign, Urbana, IL Bedford, United Kingdom Y. Tani, Kyushu University, Fukuoka, Japan Surface Warfare Center, West Bethesda, MD Merz, German Aerospace Center (DLR), Göttingen, Germany

Wednesday, 6 January 2016 232-APA-26 Unsteady Aerodynamics I Americas Cup D Chaired by: J. FARNSWORTH, University of Colorado Boulder and M. JURKOVICH, US Air Force 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2016-1074 AIAA-2016-1075 AIAA-2016-1076 AIAA-2016-1077 AIAA-2016-1078 AIAA-2016-1079 Direct Eddy Simulation of Flap Least Squares Spectral Element Time Resolved Flow Field Collaborative Evaluation of CFD-to- Unsteady Aerodynamics and Detached-Eddy Simulation of Side-Edge Flow Method For Laminar Compressible Investigations of Low Reynolds ROM Dynamic Modeling Trailing-edge Vortex Sheet of An Ground Effect on the Wake of a S. Balakrishnan, K. Shariff, NASA Ames Flows number Transient Maneuvers M. Ghoreyshi, U.S. Air Force Academy, Airfoil High-Speed Train Research Center, Moffett Field, CA J. Hasbestan, J. Newman, A. Arabshahi, H. Ehlers, R. Konrath, German Aerospace Colorado Springs, CO; N. Frink, NASA Langley X. Xia, K. Mohseni, University of Florida, C. Xia, X. Shan, Z. Yang, Tongji University, University of Tennessee, Chattanooga, Center (DLR), Göttingen, Germany; M. Research Center, Hampton, VA; M. van Gainesville, Gainesville, FL Shanghai, China Chattanooga, TN Börner, University of the German Federal Rooij, National Aerospace Laboratory (NLR), Armed Forces, Munich, Germany; R. Amsterdam, The Netherlands ; A. Lofthouse, R. Wokoeck, R. Radespiel, Technical University of Cummings, U.S. Air Force Academy, Colorado Braunschweig, Braunschweig, Germany Springs, CO; S. Nayani, Analytical Services & Materials, Inc., Hampton, VA Wednesday, 6 January 2016 233-ASC-3 Design and Testing Gaslamp D Chaired by: D. MCGOWAN, NASA Langley Research Center and R. BOTEZ, Ecole de Technologie Superieure 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2016-1080 AIAA-2016-1081 AIAA-2016-1082 AIAA-2016-1083 AIAA-2016-1084 AIAA-2016-1085 AIAA-2016-1086 Solid-State Rotor: A Feasibility Transient Flow Analysis and Static Self-adaptive morphing wing Numerical Optimization and Adaptive Control and Actuation Design and Testing of a Lattice- Primary Structural Components Study Bench Measurements for an Active model, smart actuated and Experimental Testing of a Morphing System Development for Biomimetic based Cellular Component Active Characterization of an Adaptive O. Bilgen, T. Alberts, Old Dominion Trailing-Edge Flap controlled by using a multiloop Wing with System Morphing Twist Wing Trailing Edge Device (ATED) University, Norfolk, VA U. Visconti, W. Eun, J. Kang, J. Lim, J. controller based on a laminar flow A. Koreanschi, S. Oliviu, T. Ayrault, R. N. Nigam, Y. Zhang, P. Chen, Intelligent N. Cramer, University of California, Santa I. Dimino, A. Concilio, Italian Aerospace Sim, S. Shin, Seoul National University, real time optimizer Botez, University of Québec, Montréal, Automation, Inc., Rockville, MD; G. Wolfe, T. Cruz, Santa Cruz, CA; K. Cheung, S. Swei, Research Center (CIRA), Capua, Italy; R. Seoul, South Korea L. Grigorie, R. Botez, A. Popov, University Canada; M. Mamou, Y. Mebarki, National Pillsbury, N. Wereley, University of Maryland, NASA Ames Research Center, Moffett Pecora, University of Naples “Federico II”, of Québec, Montréal, Canada Research Council Canada, Ottawa, Canada College Park, College Park, MD; et al. Field, CA Naples, Italy Wednesday, 6 January 2016 234-DSC-1 Fluid-Structure Interaction in High Speed Flows Gaslamp A Chaired by: P. TAYLOR, Gulfstream Aerospace Corporation and M. BHATIA, Mississippi State University 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2016-1087 AIAA-2016-1088 AIAA-2016-1089 AIAA-2016-1090 AIAA-2016-1091 AIAA-2016-1092 Mutual Interaction of Measurement and simulation of Efficient Treatment of Viscous An Integrated Aerothermoelastic Aeroelastic Instability Boundaries Elastic-Viscoplastic Effects on Fluid- Aerothermally Compliant Structures hypersonic fluid-structural interaction Interactions for Aerothermoelastic Analysis Framework for Predicting for Reflecting Oblique Shockwaves Thermal-Structural Interactions and Boundary Layer Transition in on a cantilevered plate in a Mach Loads Prediction in High-Speed the Response of Composite Panels on Compliant Panels J. LaFontaine, A. Gogulapati, J. Hypersonic Flows 6 flow Flows D. Huang, P. Friedmann, University of N. Boyer, J. McNamara, D. Gaitonde, Ohio McNamara, Ohio State University, Z. Riley, J. McNamara, Ohio State G. Currao, A. Neely, University of New K. Brouwer, A. Gogulapati, J. McNamara, Michigan, Ann Arbor, Ann Arbor, MI State University, Columbus, OH Columbus, OH University, Columbus, OH South Wales at the Australian Defence Force Ohio State University, Columbus, OH Academy, Canberra, Australia; D. Buttsworth, R. Choudhury, University of Southern Queensland, Toowoomba, Australia Wednesday, 6 January 2016 235-DSC-2 Adaptive Aeroelastic Wing Shaping Control Gaslamp C Chaired by: N. NGUYEN, NASA-Ames Research Center and F. NITZSCHE, Carleton University 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2016-1093 AIAA-2016-1094 AIAA-2016-1095 AIAA-2016-1096 AIAA-2016-1097 Fuzzy Model-Based Optimal Inertial Force Coupling to Nonlinear Mission Adaptive Wing Shape Drag Identification and Reduction Static and Dynamic Aeroelastic Variance Control of Flexible Aircraft Aeroelasticity of Flexible Wing Determination for Highly Flexible Technology (DIRECT) for Tailoring with Variable Camber with Actuator Amplitude and Rate Aircraft Aeroelastic Aircraft Commercial Aircraft Control Constraints. N. Nguyen, NASA Ames Research Center, W. Su, University of Alabama, Tuscaloosa, J. Boskovic, R. Wise, J. Jackson, Scientific B. Stanford, NASA Langley Research S. Swei, NASA Ames Research Center, Moffett Moffett Field, CA; E. Ting, S. Lebofsky, Tuscaloosa, AL; S. Swei, NASA Ames Systems Company, Inc., Woburn, MA Center, Hampton, VA

Field, CA; M. Ayoubi, Santa Clara University, Stinger Ghaffarian Technologies, Inc., Research Center, Moffett Field, CA; G. Santa Clara, CA; N. Nguyen, NASA Ames Moffett Field, CA Zhu, Michigan State University, East Research Center, Moffett Field, CA Lansing, MI Wednesday, 6 January 2016 236-FD-28 CFD: Higher-Order Methods I Pier Chaired by: Z. WANG, University of Kansas and T. EYMANN, CREATE-AV/Kestrel 0900 hrs 0930 hrs 1000 hrs 1030 hrs AIAA-2016-1098 AIAA-2016-1099 AIAA-2016-1100 AIAA-2016-1101 Vertex–Centered, High-Order Finite Element Analysis of Boundary A Novel Efficient Reconstruction Hyperbolic Navier-Stokes Solver for Schemes for Turbulent Flows Layer Flows using a Mixed B-spline Scheme for Unstructured Grids based Three-Dimensional Flows H. Yang, R. Harris, CFD Research Setting on Hybrid Meshes on Iterative Least-Squares methods Y. Nakashima, N. Watanabe, Software Cradle Corporation, Huntsville, AL A. Zhang, O. Sahni, Rensselaer Polytechnic Y. Tamaki, T. Imamura, University of Tokyo, Company, Ltd., Osaka, Japan; H. Nishikawa, Institute, Troy, NY Tokyo, Japan National Institute of Aerospace, Hampton, VA Wednesday, 6 January 2016 237-FD-29 Flow Control Methods and Simulations Cove Chaired by: M. WEI, New Mexico State Universtiy 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2016-1102 AIAA-2016-1103 AIAA-2016-1104 AIAA-2016-1105 AIAA-2016-1106 AIAA-2016-1107 Domain Decomposition in POD- Improving Separation Control with Improved Delayed Detached Eddy Parametric Investigation of On the Symmetrization in POD- Reduction of Aerodynamic Drag Galerkin Projection for Flows with Noise-Robust Variants of Dynamic Simulation of Flow Structures Under-Expanded Jet Receptivity to Galerkin Model for Linearized on a Commercial Pickup Truck via Moving Boundary Mode Decomposition behind A Backward-Facing Step Asymmetric Active Control Compressible Flows External Flow Devices H. Gao, M. Wei, New Mexico State M. Hemati, University of Minnesota, R. Hu, L. Wang, S. Fu, Tsinghua University, D. Gonzalez, Naval Surface Warfare M. Tabandeh, M. Wei, New Mexico State C. Spike, T. Finn, E. Dubreuil, A. Wessner, University, Las Cruces, NM Minneapolis, Minneapolis, MN; E. Deem, Beijing, China Center, Indian Head, MD; D. Gaitonde, University, Las Cruces, NM; J. Collins, S. Lee, Alfred University, Alfred, NY Florida State University, Tallahassee, Ohio State University, Columbus, OH; Army Research Laboratory, Aberdeen FL; M. Williams, C. Rowley, Princeton M. Lewis, Institute for Defense Analyses, Proving Ground, MD University, Princeton, NJ; L. Cattafesta, Washington, D.C. Florida State University, Tallahassee, FL Wednesday, 6 January 2016 238-FD-30 Jet Flows II Promenade B Chaired by: J. NAUGHTON, University of Wyoming and M. GLAUSER, Syracuse University 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2016-1108 AIAA-2016-1109 AIAA-2016-1110 AIAA-2016-1111 AIAA-2016-1112 AIAA-2016-1113 Identifying Coherent Structures in a Physics of Twinjet Plume Investigation of Rectangular Jet Experimental Investigation of the An Axisymmetric Underexpanded An Investigation of Twin Supersonic 3-Stream Supersonic Jet Flow Using Interactions Issuing From a Varying Cross- Structure of Turbulent Swirling Jets Jet Flowing Parallel to an Adjacent Jet Coupling Time-Resolved Schlieren Imaging K. Goparaju, D. Gaitonde, S. Bhaumik, Section Nozzle E. DeMillard, J. Naughton, University of Planar Surface C. Kuo, J. Cluts, M. Samimy, Ohio State A. Tenney, T. Coleman, J. Lewalle, M. Ohio State University, Columbus, OH; D. S. Sengupta, L. Agostini, U. Sasidharan Wyoming, Laramie, Laramie, WY R. Hortensius, G. Elliott, J. Dutton, University, Columbus, OH Glauser, Syracuse University, Syracuse, Garmann, Air Force Research Laboratory, Nair, D. Gaitonde, Ohio State University, University of Illinois, Urbana-Champaign, NY; B. Kiel, Air Force Research Laboratory, Dayton, OH Columbus, OH Urbana, IL Washington, D.C.; S. Gogineni, Spectral Energies, LLC, Dayton, OH Wednesday, 6 January 2016 239-FD-31 RANS/LES Methods and Techniques I Harbor E Chaired by: P. MORGAN, Ohio Aerospace Institute and R. BOND 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2016-1114 AIAA-2016-1115 AIAA-2016-1116 AIAA-2016-1117 AIAA-2016-1118 AIAA-2016-1119 Computation of Turbulent Flow in a High-Fidelity Simulations of the Analysis of spatio-temporal wake Numerical Prediction of the Minimum Dynamic Hybrid RANS/LES Modeling low-Reynolds-number Lid-Driven 2D Cavity and a 3D Box HIFiRE-6 Flow Path modes of space launchers at Height of Roughness Strip for Artificial Computations of a Supersonic Cavity flow over rough airfoils Using a Number of Turbulence Models N. Bisek, Air Force Research Laboratory, transonic flow Transition on Swept Wings E. Hassan, Air Force Research Laboratory, D. Kessler, R. Johnson, A. Corrigan, J. H. Nagapetyan, T. Wray, R. Agarwal, Wright-Patterson AFB, OH V. Statnikov, B. Roidl, M. Meinke, W. Y. Tian, Z. Zhang, . Zhai, Northwestern Wright-Patterson AFB, OH; D. Peterson, Thomas, S. Qidwai, Naval Research Washington University in St. Louis, St. Schroeder, RWTH Aachen University, Polytechnical University, Xi’an, China; K. Qu, Innovative Scientific Solutions, Inc., Dayton, Laboratory, Washington, D.C. Louis, MO Aachen, Germany City University of New York, New York, NY OH; K. Walters, E. Luke, Mississippi State

University, Starkville, MS Wednesday, 6 January 2016 240-FD-32 Subsonic Boundary Layers Harbor F Chaired by: Z. BERGER and A. SESCU, Mississippi State University 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2016-1120 AIAA-2016-1121 AIAA-2016-1122 AIAA-2016-1123 AIAA-2016-1124 Turbulence Amplitude Modulation Simultaneous Wall Shear Stress and Can Surface Streaks Counteract An Experimental Study on The Interaction of Rectangular Synthetic in an Externally Forced, Subsonic Velocity Measurements in a Flat Boundary Layer Streaks? Transient Behavior of Wind-Driven Jet with a Turbulent Boundary Layer Turbulent Boundary Layer Plate Turbulent Boundary Layer A. Sescu, Mississippi State University, Water Runback over a Flat Surface G. Gomit, University of Southampton, P. Ranade, University of Notre Dame, R. Pabon, C. Barnard, L. Ukeiley, M. Starkville, MS; M. Afsar, Imperial College K. Zhang, H. Hu, Iowa State University, Southampton, United Kingdom; Z. Berger, Notre Dame, IN; S. Duvvuri, B. McKeon, Sheplak, University of Florida, Gainesville, London, London, United Kingdom Ames, IA University of Toronto, Toronto, Canada; California Institute of Technology, Gainesville, FL B. Ganapathisubramani, University of Pasadena, CA; S. Gordeyev, K. Southampton, Southampton, United Kingdom; Christensen, E. Jumper, University of Notre P. Lavoie, University of Toronto, Toronto, Dame, Notre Dame, IN Canada Wednesday, 6 January 2016 241-FD-33 Surface Roughness & Disturbances in Supersonic Flow Promenade A Chaired by: J. POGGIE, Purdue University- Sch of Aero and Astro and R. BOWERSOX, Texas A&M University 0900 hrs 0930 hrs 1000 hrs 1030 hrs AIAA-2016-1125 AIAA-2016-1126 AIAA-2016-1127 AIAA-2016-1128 A Parametric Study into the Effects Fluid-Structure Interactions using Computation of Turbulent Heat Flux Direct Numerical Simulation of of Surface Roughness Spacing Controlled Disturbances on a with Roughness Induced Transition in Shock/Boundary Layer Interaction on the Transition of Hypersonic Slender Cone at Mach 8 High Enthalpy Shock Tunnel HIEST over Surface Roughness Using the Boundary Layers K. Casper, S. Beresh, J. Henfling, R. T. Ishihara, Y. Ogino, N. Ohnishi, Tohoku High-Oder FR/CPR-LLAV Method O. Taylor, P. Bruce, Imperial College Spillers, Sandia National Laboratories, University, Sendai, Japan; H. Tanno, Japan M. Yu, University of Maryland, Baltimore London, London, United Kingdom Albuquerque, NM Aerospace Exploration Agency (JAXA), County, Baltimore, MD Kakuda, Japan; K. Sawada, Tohoku University, Sendai, Japan Wednesday, 6 January 2016 242-GNC-21 Spacecraft De-Orbiting, Reentry and Landing Hillcrest B Chaired by: J. REED, United Launch Alliance, LLC and U. SHANKAR, The Johns Hopkins University Applied Physics Laboratory 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2016-1129 AIAA-2016-1130 AIAA-2016-1131 AIAA-2016-1132 AIAA-2016-1133 AIAA-2016-1134 Tether Dynamics Analysis for Active Station Relocation and Deorbit Aerodynamic Oscillation and Attitude Two-Dimensional Experimental Passive Hazard Detection for Online Landing Site Selection Space Debris Removal Using Electric Propulsion Control Analysis for Reentry Capsule Investigation of Base-Extension Planetary Landing Considering Maneuverability H. Linskens, E. Mooij, Delft University of J. Gill, D. Stratemeier, Space Systems/ using OREX Flight Data and Wind Separation Mechanism with Telescopic S. Woicke, E. Mooij, Delft University of Constraint during Mars Powered Technology, Delft, The Netherlands Loral, Palo Alto, CA Tunnel Data Gear Technology, Delft, The Netherlands Descent Phase S. Matsumoto, Y. Kondoh, S. Nagai, R. N. Saeki, S. Hara, Nagoya University, Nagoya, D. Ge, A. Gao, P. Cui, Beijing Institute of Tagai, T. Imada, E. Nakano, Japan Aerospace Japan; M. Otsuki, Japan Aerospace Exploration Technology, Beijing, China

Exploration Agency (JAXA), Tsukuba, Japan Agency (JAXA), Sagamihara, Japan Wednesday, 6 January 2016 243-GNC-22 GN&C Sensor Systems Hillcrest A Chaired by: S. STARIN, NASA-Goddard Space Flight Center and M. MAJJI, State University of New York at Buffalo 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2016-1135 AIAA-2016-1136 AIAA-2016-1137 AIAA-2016-1138 AIAA-2016-1139 AIAA-2016-1140 AIAA-2016-1141 Enhanced detection and isolation of Compound eye sensor for real- Landing Zone Determination Precision Onboard Small Sensor Modelling an Angular Accelerometer Bias Calibration Vacuum temperature field angle of attack sensor faults time aircraft wing deflection for Autonomous Rotorcraft in System for Unmanned Air Vehicle Accelerometer using Frequency- Using Attitude and Angular Velocity simulation and experiments D. Ossmann, German Aerospace Center measurement Surveillance Applications Testing and Control Response Measurements Information of four-mode differential laser (DLR), Oberpfaffenhofen, Germany S. Frost, NASA Ames Research Center, J. Mackay, Lincoln Laboratory, F. Arthurs, J. Valasek, Texas A&M D. Jatiningrum, C. de Visser, M. van Z. Yu, Beijing Institute of Technology, gyroscope Moffett Field, CA; G. Gorospe, C. Teubert, Massachusetts Institute of Technology, University, College Station, TX Paassen, M. Mulder, Delft University of Beijing, China; J. Crassidis, State X. Yu, G. Lu, H. Luo, National University of Stinger Ghaffarian Technologies, Inc., Lexington, MA; G. Ellingson, T. McLain, Technology, Delft, The Netherlands University of New York, Amherst, NY Defence Technology, Changsha, China Moffett Field, CA Brigham Young University, Provo, UT Wednesday, 6 January 2016 244-GNC-23 Aerospace Robotics and Unmanned/Autonomous Systems V Hillcrest C Chaired by: I. SHARF, McGill University and M. LAVAGNA, Politecnico Di Milano 0900 hrs 0930 hrs 1000 hrs 1030 hrs AIAA-2016-1142 AIAA-2016-1143 AIAA-2016-1144 AIAA-2016-1145 Path generation for rendezvous of Autonomous Control of GPS Denied Graph based dynamic policy for Automatic Prevention of Loss of dissimilar UAVs using Particle Swarm Guided Airdrop Systems Using UAV navigation Control Due to Winds by Bandwidth Optimization of Dubin’s curve sets Radio Beacon Feedback T. Mannucci, E. Van Kampen, C. de Visser, Adaptation V. Jouffroy, X. Bovier-Lapierre, Institut M. Cacan, E. Scheuermann, M. Ward, M. Q. Chu, Delft University of Technology, Y. Zhao, J. Zhu, Ohio University, Athens, Polytechnique des Sciences Avancées, Ivry-sur- Costello, Georgia Institute of Technology, Delft, The Netherlands OH Seine, France; O. Ariff, University of Salford, Atlanta, GA Salford, United Kingdom; T. Richer, University of Western Brittany, Brest, France Wednesday, 6 January 2016 245-GT-5 Ground Test Studies and Techniques Cortez Hill B Chaired by: D. LEWIS, Aerospace Testing Alliance (ATA) and G. AYERS, U.S. Air Force 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2016-1146 AIAA-2016-1147 AIAA-2016-1148 AIAA-2016-1149 AIAA-2016-1150 AIAA-2016-1151 AIAA-2016-1152 Dynamic Pressure-Sensitive Paint PIV Measurements of Mach 2.7 Uncertainty Analysis of NASA A New High Channel-Count, High Neural Network Model Predictive Evaluating Environmental Control Free Flight Testing in Hypersonic Demonstration in AEDC Propulsion Turbulent Boundary Layer with Glenn’s 8- by 6- Foot Superonic Scan-Rate, Data Acquisition System Control of Wind Tunnel Test System Thermal Response to Flows: HEXAFLY-INT EFTV Wind Tunnel 16T Varying Reynolds Numbers Wind Tunnel for the NASA Langley Transonic Conditions Degraded Operating Conditions C. Kennell, A. Neely, University of New M. Sellers, M. Nelson, Aerospace Testing J. Brooks, A. Gupta, University of J. Stephens, Sierra Lobo, Inc., Cleveland, Dynamics Tunnel P. Sutcliffe, M. Rennie, University of Notre T. Childs, A. Jones, R. Chen, Loughborough South Wales, Canberra, Australia; D. Alliance, Arnold AFB, TN; J. Crafton, Maryland, College Park, College Park, MD; OH; E. Hubbard, Jacobs, Cleveland, OH; T. Ivanco, D. Piatak, M. Sekula, NASA Dame, Notre Dame, IN University, Loughborough, United Buttsworth, R. Choudhury, University Innovative Scientific Solutions, Inc., M. Smith, E. Marineau, Arnold Engineering J. Walter, Jacobs, Bingham Farms, MI; T. Langley Research Center, Hampton, VA; Kingdom; A. Murray, BAE Systems, of Southern Queensland, Toowoomba, Dayton, OH Development Center, Silver Spring, MD McElroy, Jacobs, Tullahoma, TN S. Simmons, W. Babel, J. Collins, Jacobs, Warton, United Kingdom Australia; M. Tahtali, University of New Hampton, VA; et al. South Wales, Canberra, Australia Wednesday, 6 January 2016 246-GTE-8 Combustion I Cortez Hill C Chaired by: C. SLABAUGH, Purdue University and J. CONVERY, GE Aviation 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2016-1153 AIAA-2016-1154 AIAA-2016-1155 AIAA-2016-1156 AIAA-2016-1157 Combustion Blowoff Effects on the Effect of Aviation Fuel Type and Impact of Internal Entrainment and Analysis of Combustion Oscillations Measurement and Analysis of Central Recirculation Zone using Fuel Injection Conditions on Non- Dilution on Enhancing Distributed in a Staged MLDI Burner using Flame Transfer Functions in a various Syngas mixtures in a reacting Spray Characteristics of Combustion Decomposition Methods and Lean-Premixed, Swirl-Stabilized Tangential Swirl Burner Hybrid Air Blast Fuel Injector A. Khalil Hasan, A. Gupta, University of Recurrence Analysis Combustor with Water Injection H. Baej, A. Valera-Medina, N. Syred, T. Buschhagen, R. Zhang, S. Naik, C. Maryland, College Park, College Park, MD J. Wilhite, B. Dolan, University of Cincinnati, N. Stadlmair, T. Sattelmayer, Technical R. Marsh, P. Bowen, Cardiff University, Slabaugh, S. Meyer, J. Gore, Purdue Cincinnati, OH; L. Kabiraj, Technical University University of Munich, Garching, Germany

Cardiff, United Kingdom University, West Lafayette, IN; et al. of Berlin, Berlin, Germany; R. Villalva Gomez, E. Gutmark, C. Paschereit, University of Cincinnati, Cincinnati, OH Wednesday, 6 January 2016 247-HIS-2 Aerospace History Americas Cup A Chaired by: S. RUSSI, Bigelow Aerospace 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2016-1158 AIAA-2016-1159 AIAA-2016-1160 AIAA-2016-1161 AIAA-2016-1162 AIAA-2016-1163 Portuguese Contribution to John J. Montgomery’s Circulation The First American Aeroplane The American Legion Airplane-- The American Legion Airplane - Southern Nevada Aerospace Early Airplane Design: The Theory of Lift Export Octave Chanute’s 1904 Those Willing to Dare-- Transition to Santa Maria History Industriousness of João Gouveia G. Fogel, San Diego State University, San Glider at the Threshold of Powered L. Forrest, Naval Weapons Station, K. Burns, AIAA San Diego Section, San S. Russi, Bigelow Aerospace, North J. Sousa, Technical University of Lisbon, Diego, CA; C. Harwood, Harwood and Flight. Yorktown, VA Diego, CA , NV; D. Henry, University of Lisbon, Portugal; R. Reis, Embraer, Évora, Associates, Ben Lomond, CA S. Short, National Soaring Museum, Nevada, Las Vegas, Las Vegas, NV Portugal Elmira, NY Wednesday, 6 January 2016 248-HSABP-4 Scramjet Inlets Regatta A Chaired by: B. SARACOGLU, von Karman Institute for Fluid Dynamics and T. SMITH, Boeing Engineering Operations & Technology 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2016-1164 AIAA-2016-1165 AIAA-2016-1166 AIAA-2016-1167 AIAA-2016-1168 Three-Dimensional Nature of Shock Swept shock corner flow interacions Reduced-Order Analysis of Scramjet Reduced-Order Analysis of Dual Comparison of Unstart Induced by Trains in Rectangular Scramjet R. Morajkar, M. Gamba, University of Inlet Operation Mode Scramjet Isolator Operation Mass Addition and Heat Release Isolators Michigan, Ann Arbor, Ann Arbor, MI V. Gopal, D. Wilson, University of Texas, V. Gopal, D. Wilson, University of Texas, S. Im, L. Wermer, Worcester Polytechnic J. Geerts, K. Yu, University of Maryland, Arlington, Arlington, TX Arlington, Arlington, TX Institute, Worcester, MA; D. Baccarella, Q. College Park, College Park, MD Liu, B. McGann, University of Notre Dame, Notre Dame, IN; H. Do, Seoul National University, Seoul, South Korea Wednesday, 6 January 2016 249-MAT-7 Integrated Computational Materials Engineering (ICME) Gaslamp B Chaired by: J. MATLIK, Rolls-Royce Corp and M. SANGID, Purdue University and V. VENKATESH, 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2016-1170 AIAA-2016-1171 AIAA-2016-1172 AIAA-2016-1173 AIAA-2016-1174 Material Design Using a NURBS- Development of a Structural Modeling of Shock Wave Multi-Functional Topology Information Management Workflow based Shape Optimization Finite Element Progressive Failure Propagation through Energetic Optimization of Nanocomposite and Tools Enabling Multiscale A. Najafi, M. Safdari, P. Geubelle, Simulation and Integration into the Solid State Composites using a Beams Modeling Within ICME Paradigm University of Illinois, Urbana-Champaign, ICM2 Framework Taylor-Galerkin Scheme D. Seifert, M. Patil, G. Seidel, Virginia S. Arnold, B. Bednarcyk, NASA Glenn Research Urbana, IL J. Dustin, General Electric Company, A. Duran, V. Sundararaghavan, University Polytechnic Institute and State University, Center, Cleveland, OH; N. Austin, I. Terentjev, Evendale, OH; R. Dalgarno, Autodesk, Inc., of Michigan, Ann Arbor, Ann Arbor, MI Blacksburg, VA; G. Reich, Air Force Research D. Cebon, W. Marsden, Granta Design, Laramie, WY; M. Hockemeyer, General Laboratory, Wright-Patterson AFB, OH Cambridge, United Kingdom Electric Company, Niskayuna, NY Wednesday, 6 January 2016 250-MDO-5 Aeroelastic Sensitivity Analysis & Applications Balboa A Chaired by: T. TAKAHASHI, Arizona State University and D. ALLISON, Optimal Flight Sciences LLC 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2016-1175 AIAA-2016-1176 AIAA-2016-1177 AIAA-2016-1178 AIAA-2016-1179 Development of a High-Fidelity Adjoint Based Structure and Continuum Sensitivity Analysis for Gradient Based Optimization using High-fidelity Aerostructural Time-Dependent Aero-Structural Shape Optimization with Flutter Aeroelastic Shape Optimization Spectral Formulation-Based FSI and Optimization of a High Aspect Ratio Capability for Analysis and Design Constraints M. Kulkarni, R. Canfield, M. Patil, Virginia Coupled Sensitivity Analysis Tow-steered Wing D. Mavriplis, E. Anderson, R. Fertig, M. Z. Zhang, P. Chen, ZONA Technology, Inc., Polytechnic Institute and State University, R. Prasad, Virginia Polytechnic Institute T. Brooks, University of Michigan, Ann Garnich, University of Wyoming, Laramie, Scottsdale, AZ; Q. Wang, Massachusetts Blacksburg, VA and State University, Blacksburg, VA; S. Arbor, Ann Arbor, MI; G. Kennedy, Georgia Laramie, WY Institute of Technology, Cambridge, Yi, Korea Advanced Institute of Science Institute of Technology, Atlanta, GA; J.

MA; Z. Zhou, S. Yang, Z. Wang, ZONA and Technology, Daejeon, South Korea ; S. Martins, University of Michigan, Ann Arbor, Technology, Inc., Scottsdale, AZ Choi, D. Im, Virginia Polytechnic Institute Ann Arbor, MI and State University, Blacksburg, VA Wednesday, 6 January 2016 251-MST-6 Human Factors, Perception, and Cueing Golden Hill A Chaired by: F. CARDULLO, State University of NY and A. ELMILIGUI, NASA Langley Research Center 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2016-1180 AIAA-2016-1181 AIAA-2016-1182 AIAA-2016-1183 AIAA-2016-1184 Development of Spatial On Effects of Failures in Haptic and Identifying Time-Varying Pilot Simulation-based concept Simulating Flight-Deck Mode- Disorientation Demonstration Automated Pilot Support Systems Responses: a Recursive Least- development and evaluation: Confusion Incidents using Human Scenarios for Commercial Pilot M. Maimeri, University of Pisa, Pisa, Squares Based Approach Augmented reality to improve Error Templates Training Italy; M. Olivari, H. Buelthoff, Max M. Olivari, J. Venrooij, F. Nieuwenhuizen, communication between helicopter S. Park, B. Yang, Optimal Synthesis, Inc., D. Klyde, A. Lampton, P. Schulze, Systems Planck Institute for Biological Cybernetics, Max Planck Institute for Biological crew during firefighting operations Los Altos, CA Technology, Inc., Hawthorne, CA Tübingen, Germany; L. Pollini, University Cybernetics, Tübingen, Germany; L. Pollini, R. Arents, M. Klijn, M. Roza, A. de Reus, of Pisa, Pisa, Italy University of Pisa, Pisa, Italy; H. Buelthoff, National Aerospace Laboratory (NLR), Max Planck Institute for Biological Amsterdam, The Netherlands Cybernetics, Tübingen, Germany Wednesday, 6 January 2016 252-MST-7 Modeling of Vehicle Dynamics, Systems, and Environments Golden Hill B Chaired by: S. BEARD, NASA-Ames Research Center and C. ATKINSON, Lockheed Martin Corporation 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2016-1185 AIAA-2016-1186 AIAA-2016-1187 AIAA-2016-1188 AIAA-2016-1189 AIAA-2016-1190 AIAA-2016-1191 Modeling of Inertial Control Surface Simulation Framework for UAS The Trick Simulation Toolkit: A Extending the SPeAD-M86 Model: Online Safe Flight Envelope An Analysis of Stochastic Fast Modeling for Lunar Landing

Hinge Moments Using Quaternion Conceptual Design NASA/Opensource Framework for Incorporating the Effects of F10.7 Prediction for Damaged Aircraft: A Disturbances on Nonlinear Missile- Dynamics Analysis Calculations K. Jerath, Washington State University, Running Time Based Physics Models Variations on Atmospheric Density Database-driven Approach Target Engagements Based on the J. Ding, C. Wang, Beihang University, C. Atkinson, Lockheed Martin Corporation, Pullman, WA; J. Langelaan, Pennsylvania J. Penn, L-3 Communications, Houston, S. Kedare, S. Ulrich, Carleton University, Y. Zhang, C. de Visser, Q. Chu, Delft Adjoint Method Beijing, China Palmdale, CA State University, University Park, PA TX; A. Lin, NASA Johnson Space Center, Ottawa, Canada University of Technology, Delft, The E. Sezer, M. Nalci, ROKETSAN Missile Houston, TX Netherlands Industries, Inc., Ankara, Turkey; A. Kutay, Middle East Technical University, Ankara, Turkey Wednesday, 6 January 2016 253-NDA-4 Model Calibration, Verification, Validation, Uncertainty Quantification Old Town B Chaired by: B. THACKER, Southwest Research Institute and M. RUMPFKEIL, University of Dayton 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2016-1192 AIAA-2016-1193 AIAA-2016-1194 AIAA-2016-1195 AIAA-2016-1196 AIAA-2016-1197 Validation, Uncertainty Sequential Experimental Design and Uncertainty Reduction using Anomaly Detection Using Groups of Development of a Prototype Model- Bridging the Gap between Point Cloud Quantification and Uncertainty Model Calibration for Targeted Events Bayesian Inference and Sensitivity Simulations Form Uncertainty Knowledge Base and CAD: a Method to Assess Form Reduction for a Shock Tube D. Villanueva, Universal Technology Analysis: A Sequential Approach M. Fernandez-Godino, A. Diggs, C. Park, L. Green, NASA Langley Research Center, Error in Aero Structures Simulation Corporation, Dayton, OH; B. Smarslok, Air to the NASA Langley Uncertainty N. Kim, R. Haftka, University of Florida, Hampton, VA A. Forslund, J. Madrid, R. Söderberg, Chalmers C. Park, R. Haftka, N. Kim, University of Force Research Laboratory, Wright-Patterson Quantification Challenge Gainesville, Gainesville, FL University of Technology, Göteborg, Sweden; Florida, Gainesville, Gainesville, FL AFB, OH; R. Perez, Universal Technology S. Sankararaman, NASA Ames Research J. Lööf, S. Knuts, O. Isaksson, GKN Aerospace Corporation, Dayton, OH Center, Moffett Field, CA Engine Systems, Trollhättan, Sweden; et al. Wednesday, 6 January 2016 254-NW-11 Wednesday Late Morning Networking Coffee Break Exposition Hall 0900 - 0930 hrs Wednesday, 6 January 2016 255-PC-9/GTE-9 Rotating-Detonation Engines Harbor B Chaired by: J. HOKE, Innovative Scientific Solutions Incorporated and E. LYNCH, Aerojet Rocketdyne 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2016-1198 AIAA-2016-1199 AIAA-2016-1200 AIAA-2016-1201 AIAA-2016-1202 Evaluation of Mixing Processes in a Time-Resolved In-Situ Absorption Comparison of Simulated and Development and Testing of a Detonation Reignition within a Non-Premixed Rotating Detonation Spectroscopy of a Hydrocarbon-Air Measured Instantaneous Heat Flux High-Pressure Rotating Detonation Rotating Detonation Engine Engine Using Acetone PLIF Rotating Detonation Engine using a in a Rotating Detonation Engine Engine for Rocket Applications J. Burr, K. Yu, University of Maryland, B. Rankin, Air Force Research Laboratory, Fiber-Coupled Tunable Laser System S. Theuerkauf, F. Schauer, R. Anthony, D. Stechmann, S. Heister, Purdue College Park, College Park, MD Wright-Patterson AFB, OH; C. Fugger, K. Rein, S. Roy, Spectral Energies, LLC, Air Force Research Laboratory, Wright- University, West Lafayette, IN D. Richardson, Spectral Energies, LLC, Dayton, OH; B. Sell, Innovative Scientific Patterson AFB, OH; D. Paxson, NASA Beavercreek, OH; K. Cho, J. Hoke, Innovative Solutions, Inc., Dayton, OH; A. Caswell, Air Glenn Research Center, Cleveland, OH; Scientific Solutions, Inc., Dayton, OH; A. Force Research Laboratory, Wright-Patterson C. Stevens, J. Hoke, Innovative Scientific Caswell, Air Force Research Laboratory, Wright- AFB, OH; J. Hoke, Innovative Scientific Solutions, Inc., Dayton, OH Patterson AFB, OH; et al. Solutions, Inc., Dayton, OH; F. Schauer, Air Force Research Laboratory, Wright-Patterson AFB, OH; et al. Wednesday, 6 January 2016 256-PC-10 Laminar Flames Harbor C Chaired by: D. GLAZE, Sandia National Laboratories and P. KOURDIS 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2016-1203 AIAA-2016-1204 AIAA-2016-1205 AIAA-2016-1206 AIAA-2016-1207 AIAA-2016-1208 AIAA-2016-1209 Major Species Investigation of Non- Partially premixed hydrogen-air The Dynamics of Premixed Flames The Effect of Stretch and Heat Loss Flame Dynamics and Structures of A Smart CSP Method and Correlated Analysis of the Ignition of a Premixed Cellular Tubular Flame cellular flames in a tubular burner in Long Narrow Channels on the Anchoring and Response to Partially Premixed Cool Flames Dynamic Adaptive Chemistry Combustible Fuel Spray-Oxidant C. Hall, R. Pitz, Vanderbilt University, D. Tinker, C. Hall, R. Pitz, Vanderbilt M. Matalon, University of Illinois, Urbana- Acoustic Forcing of a Bluff Body C. Reuter, S. Won, Y. Ju, Princeton and Transport Algorithm for Mixture Nashville, TN University, Nashville, TN Champaign, Urbana, IL; V. Kurdyumov, Stabilized Lean Premixed Flame University, Princeton, NJ Computationally Efficient Modeling J. Greenberg, G. Kats, Technion--Israel Department of Energy, Madrid, Spain D. Michaels, K. Kedia, A. Ghoniem, with A Detailed Mechanism Institute of Technology, Haifa, Israel Massachusetts Institute of Technology, W. Sun, Y. Ju, Princeton University, Princeton, Cambridge, MA NJ Wednesday, 6 January 2016 257-PDL-7 ns-DBD Plasma Actuator Ocean Beach Chaired by: S. ROY, University of Florida 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2016-1210 AIAA-2016-1211 AIAA-2016-1212 AIAA-2016-1213 AIAA-2016-1214 AIAA-2016-1215 Pulse-to-Pulse Coupling for Ignition Measurements and kinetic Characterization of efficiency of Kinetics of excited species at high Fluid Motion Induced by Spark CARS / 4-Wave Mixing in Cross-Flow Using Nanosecond- modeling of OH and H number energy deposition of a ns-DBD specific energy deposition: quenching Plasma: Development of Particle Measurements of Electric Field in Pulsed High-Frequency Discharge densities in nanosecond pulse plasma actuator by electrons in the afterglow of a Image Velocimetry Measurements AC Dielectric Barrier Discharges T. Ombrello, Air Force Research Laboratory, J. Van den Broecke, G. Correale, F. B. Singh, L. Rajendran, Purdue University, discharges in CxHy-O2-Ar and CxHy- nanosecond capillary discharge Overlapped with Nanosecond Wright-Patterson AFB, OH; J. Lefkowitz, air mixtures Avallone, Delft University of Technology, N. Lepikhin, A. Klochko, National Center for West Lafayette, IN; M. Giarra, Virginia Duration Voltage Pulses Princeton University, Princeton, NJ C. Winters, A. Chernukho, Z. Eckert, Delft, The Netherlands Scientific Research (CNRS), Palaiseau, France; Polytechnic Institute and State University, B. Goldberg, I. Adamovich, W. Lempert, I. Adamovich, Ohio State University, N. Popov, Moscow State University, Moscow, Blacksburg, VA; S. Bane, P. Vlachos, Ohio State University, Columbus, OH Columbus, OH Russia ; S. Starikovskaia, National Center for Purdue University, West Lafayette, IN Scientific Research (CNRS), Palaiseau, France Wednesday, 6 January 2016 258-SCS-3 Spacecraft Membranes, Booms, and Trusses I Balboa B Chaired by: B. DAVIS, Roccor LLC and G. GRESCHIK, TentGuild Engineering Co 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2016-1216 AIAA-2016-1217 AIAA-2016-1218 AIAA-2016-1219 AIAA-2016-1220 AIAA-2016-1221 Membrane Spin-Up in a Normal Membrane Space Structure with Windmill Torque Estimation of Shape Estimation and Design Mechanical Development of a Viscoelastic Effects in Metal- Gravity Field: Experiments and Sterical Support of Booms and Cables Spin-type Solar Power Sail with Methods for Membrane Structures Novel Inflatable and Rigidizable Polymer Laminate Inflatable Simulations A. Torisaka, Tokyo Metropolitan University, Shape Control to Achieve Appropriate Flatness Structure Structures M. Delapierre, S. Pellegrino, California Hino, Japan; Y. Satoh, Self, Shinjyuku, J. Kikuchi, T. Chujo, University of Tokyo, T. Nishizawa, H. Sakamoto, Tokyo G. Secheli, A. Viquerat, G. Aglietti, A. Viquerat, University of Surrey, Guildford, Institute of Technology, Pasadena, CA Japan; T. Akita, Chiba Institute of Technology, Bunkyo, Japan; Y. Shirasawa, Japan Institute of Technology, Tokyo, Japan University of Surrey, Guildford, United United Kingdom; M. Schenk, University of Narashino, Japan; M. Natori, Japan Aerospace Aerospace Exploration Agency (JAXA), Kingdom Bristol, Bristol, United Kingdom Exploration Agency (JAXA), Sagamihara, Tsukuba, Japan; O. Mori, Japan Aerospace Japan; H. Yamakawa, T. Miyashita, Waseda Exploration Agency (JAXA), Sagamihara, University, Shinjyuku, Japan Japan Wednesday, 6 January 2016 259-SD-7 Dynamics, Feedback Control, and Aeroservoelasticity II Balboa C Chaired by: M. PATIL, Virginia Tech and A. GREWAL, National Research Council Canada 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2016-1222 AIAA-2016-1223 AIAA-2016-1224 AIAA-2016-1225 AIAA-2016-1226 AIAA-2016-1227 AIAA-2016-1228 Model Order Reduction of Optimal manoeuvres with very Alternative Unsteady Aerodynamic Nonlinear Passive Control Aeroelastic responses identification Active Flutter Suppression Active Vibration Control Applications Aeroservoelastic Model of Flexible flexible wings Uncertainty Modeling Approaches Strategies for Suppression of of a high-aspect-ratio flexible Combining the Receptance Method for Adaptive Aircraft Wings Modelled Aircraft S. Maraniello, R. Simpson, R. Palacios, for Aeroservoelastic Reliability Transonic Flutter wing model and its active flutter and Flutter Margin as Thin-Walled Composite Beams Y. Wang, H. Song, K. Pant, CFD Research Imperial College London, London, United Analysis Z. Yan, S. Ragab, M. Hajj, Virginia suppression strategy Z. Wu, Beihang University, Beijing, China; K. Yildiz, Pennsylvania State University, Corporation, Huntsville, AL; M. Brenner, Kingdom E. Livne, S. Wu, University of Washington, Polytechnic Institute and State University, Z. Lu, Y. Cui, D. Schneider, Z. Zhao, J. Cooper, University of Bristol, Bristol, State College, PA; S. Eken, M. Kaya, Istanbul P. Suh, NASA Armstrong Flight Research Seattle, Seattle, WA Blacksburg, VA X. Chen, K. Lai, National University of United Kingdom Technical University, Istanbul, Turkey Center, Edwards, CA Singapore, Singapore, Singapore; et al. Wednesday, 6 January 2016 260-SEN-1 Novel Sensor Systems and Sensing Techniques I Regatta C Chaired by: D. ACCARDO, University of Naples 0900 hrs 0930 hrs 1000 hrs AIAA-2016-1229 AIAA-2016-1230 AIAA-2016-1231 Acceleration and Velocity Sensing Laser Anemometer for Autonomous Characterization of multiple damage from Measured Strain Systems Operations sites in composites using reduced C. Pak, R. Truax, NASA Armstrong Flight C. Font, T. Apker, F. Santiago, Naval order piezoelectric sensor array Research Center, Edwards, CA Research Laboratory, Washington, D.C. V. Nethala, University of South Carolina, Columbia, Columbia, SC Wednesday, 6 January 2016

261-SOF-5/UMS-5/IS-6 Assurance of Autonomy Symposium I Coronado A 0900 - 1230 hrs Describing Autonomy for System Assurance

In this session, we survey the current state of assurance in autonomous systems, as well as provide a commentary on the state of the art in terms of practices used to achieve assured autonomy. Topics that will be addressed include a discussion of this year’s Workshop on Certification of Non-Deterministic Systems, the recent NRC report on Autonomy Research for Civil Aviation, along with discourse on current practices in the UAS industry as well as at NASA’s Autonomy Incubator.

We begin with a panel discussion to explore these areas, via an interactive Q&A session with the audience. The audience questions will be used to drive and derive directions for investigation that will be captured by the moderators in the report-out. This will be followed by several example lightning-fast (5-minute) talks on new ideas for describing and generating requirements for autonomous systems. Panelists: Danette Allen Andy Thurling Andy Lacher Ella Atkins Lael Rudd NASA Langley Research Center AeroVironment MITRE Corporation University of Michigan Northrop Grumman Corporation

Lightning-fast Talks: Jack Ryan Corey Ippolito Devesh Bhatt NASA Armstrong Flight Research Center NASA Ames Research Center Honeywell International, Inc. Wednesday, 6 January 2016 262-STR-8 Design, Test and Analysis of Composite Structures I La Jolla A Chaired by: A. SELVARATHINAM, Lockheed Martin Corporation and A. NAJAFI, ANSYS, Inc. 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2016-1232 AIAA-2016-1233 AIAA-2016-1234 AIAA-2016-1235 AIAA-2016-1236 AIAA-2016-1237 Role of FEA, Closed-Form, and Extension of Automated 3D Digital Determining Effective Interface Approach of Interlaminar Impact Response of Woven Hybrid Textile Composites as Empirical Models in Certifying Reconstruction to Multi-Directional Fracture Properties of 3D Fiber Characterization for Thick Aircraft Composites with Interlaminar Potential Cryogenic Tank Materials Aircraft Composite Structures Fiber Reinforced Composite Reinforced Foam Core Sandwich Composite Structures Reinforcement M. Islam, R. Avila, A. Castellanos, P. A. Selvarathinam, C. Rousseau, S. Microstructures Structures M. Gurvich, P. Clavette, United A. Castellanos, S. Islam, S. Quevedo, M. Prabhakar, University of Texas, El Paso, Engelstad, L. Flansburg, Lockheed Martin W. Whitacre, Draper Laboratory, Z. Kier, The Aerospace Corporation, El Technologies Corporation, East Hartford, Shuvo, Y. Lin, P. Prabhakar, University of El Paso, TX Corporation, Fort Worth, TX Cambridge, MA; M. Czabaj, University of Segundo, CA; A. Waas, University of CT; M. Robeson, Army Aviation and Missile Texas, El Paso, El Paso, TX Utah, Salt Lake City, Salt Lake City, UT Washington, Seattle, Seattle, WA Research Development and Engineering Center, Fort Eustis, VA Wednesday, 6 January 2016 263-STR-9 Other Topics in Structures La Jolla B Chaired by: I. RAJU, NASA-Langley Research Center and S. RUSSELL, Triumph Aerostructures 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2016-1238 AIAA-2016-1239 AIAA-2016-1240 AIAA-2016-1241 AIAA-2016-1242 An Open Source Reverse Engineering The Effects of Reducing the Structural Simple Test Functions in Meshless Thermally-Driven Morphing with High Nonlinear Modelling of Axially Workflow: Geometry to Optimization Mass of the Transit Habitat on the Local Petrov-Galerkin Methods Temperature Composites Deformable Elastica based on P. Gustafson, A. Geeslin, J. Jastifer, Western Cryogenic Propellant Required for a I. Raju, NASA Langley Research Center, E. Eckstein, University of Bristol, Bristol, United Hyperelasticity Michigan University, Kalamazoo, MI Human Phobos Mission Hampton, VA Kingdom; M. Halbig, NASA Glenn Research F. Jiang, S. Tian, W. Yu, Purdue University, J. Zipay, NASA Johnson Space Center, Center, Cleveland, OH; P. Weaver, University of West Lafayette, IN Houston, TX Bristol, Bristol, United Kingdom Wednesday, 6 January 2016 264-SUR-1 Air and Space Survivability I Old Town A Chaired by: J. RIMOLI, Georgia Institute of Technology and E. FAHRENTHOLD, University of Texas 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2016-1243 AIAA-2016-1244 AIAA-2016-1245 AIAA-2016-1246 AIAA-2016-1247 Crew Compartment Fire Characterization of Hydrodynamic Composition Characterization of Wing Design Utilizing Topology Topology Optimization and CFD Survivability Ram Cavity Dynamics to Transient Cavity Consisting of Multiple Fluids Optimization and Additive Analysis of a Hypersonic Vehicle A. Goss, 96th Test Group, Wright-Patterson Spray A. Lingenfelter, D. Liu, Air Force Institute of Manufacturing AFB, OH A. Lingenfelter, D. Liu, Air Force Institute of Technology, Wright-Patterson AFB, OH D. Walker, D. Liu, A. Jennings, Air Force K. Liu, D. Stelzer, Ohio State University, Technology, Wright-Patterson AFB, OH Institute of Technology, Wright-Patterson Columbus, OH; A. Williamson, D. Liu, AFB, OH Air Force Institute of Technology, Wright- Patterson AFB, OH; A. Jennings, Raytheon Company, Tucson, AZ Wednesday, 6 January 2016 265-TP-7 Aerothermodynamics II Harbor G Chaired by: K. EDQUIST, NASA Langley Research Center 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2016-1248 AIAA-2016-1249 AIAA-2016-1250 AIAA-2016-1251 AIAA-2016-1252 Computational Study of Non- Simulation of O2-N Collisions on Thermochemical Nonequilibrium Analysis of the Temperature Ratio The Effects of Chemical Equilibrium Effects on Hypersonic ab-initio Potential Energy Surfaces CFD Modeling for Hypersonic Flows Effects on the Flow Properties of Nonequilibrium and Surface Boundary-Layer Transition D. Andrienko, I. Boyd, University of Containing Oxygen the Low Reynolds and High Mach Catalyticity on Aerothermodynamic X. Wang, E. Josyula, Air Force Research Michigan, Ann Arbor, Ann Arbor, MI K. Neitzel, D. Andrienko, I. Boyd, number Flow around a Sphere Characteristics of Hypersonic Laboratory, Wright-Patterson AFB, OH University of Michigan, Ann Arbor, Ann T. Nagata, Tokai University, Hiratsuka, Vehicles Arbor, MI Japan; T. Nonomura, Japan Aerospace X. Chen, F. Chen, S. Zhang, H. Liu, Exploration Agency (JAXA), Sagamihara, Shanghai Jiao Tong University, Shanghai, Japan; S. Takahashi, Y. Mizuno, K. China Fukuda, Tokai University, Hiratsuka, Japan Wednesday, 6 January 2016 266-UMS-6 Unmanned Systems: Novel Platforms and Controls Regatta B Chaired by: B. ARGROW, University of Colorado Boulder and R. CHRISTIANSEN, Sierra Lobo, Inc. 0900 hrs 0930 hrs 1000 hrs 1030 hrs AIAA-2016-1253 AIAA-2016-1254 AIAA-2016-1255 AIAA-2016-1256 Real Time Detection And Tracking Design and Control of a Novel Development of a 20 gram Collaboration between Multiple Of Visual Features For Aircraft Tiltrotor Platform Cycloidal-Rotor-Based Micro Air Unmanned Vehicles for Increased Guidance J. Kim, D. Choi, University of Kansas, Vehicle Mission Efficiency H. Chaudhry, E. Smith, K. Kochersberger, Lawrence, Lawrence, KS C. Runco, M. Benedict, Texas A&M S. Bhandari, R. Demonteverde, T. Cecil, E. Virginia Polytechnic Institute and State University, College Station, TX Ito, A. Phan, O. Dadian, California Polytechnic University, Blacksburg, VA State University, Pomona, CA; et al. Wednesday, 6 January 2016 267-WE-5 Wind Energy: Wind Turbine Aerodynamics Modeling II Harbor H Chaired by: J. BRASSEUR, Penn State University and K. WETZEL, Wetzel Engineering 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2016-1257 AIAA-2016-1258 AIAA-2016-1259 AIAA-2016-1260 AIAA-2016-1261 Development of Free Vortex A Novel Approach for Staggered Experimental investigation of Improved Free Vortex Wake Models Wind Farm Large-Eddy Simulations Wake Model for Wind Turbine Fluid-Structure Interaction asymmetric steamwise vortices in a Of Floating Offshore Wind Turbines on Very Coarse Grid Resolutions Aerodynamics under Yaw Condition Simulation of Shape-Adaptive turbulent boundary layer E. Gaertner, S. Liu, M. Lackner, University using an Actuator Line Model H. Abedi, L. Davidson, Chalmers University Airfoils for Wind Turbine Rotor D. Baldacchino, D. Ragni, C. Simao of Massachusetts, Amherst, Amherst, MA L. Martinez, C. Meneveau, R. Stevens, of Technology, Göteborg, Sweden; S. Blades Ferreira, G. van Bussel, Delft University of Johns Hopkins University, Baltimore, MD Voutsinas, National Technical University of I. Ahmed, M. Lawerenz, University of Technology, Delft, The Netherlands Athens, Athens, Greece Kassel, Kassel, Germany

Wednesday, 6 January 2016 268-WE-6 Wind Energy: Rotor Design Harbor I Chaired by: D. GRIFFITH 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2016-1262 AIAA-2016-1263 AIAA-2016-1264 AIAA-2016-1265 AIAA-2016-1266 Aeroelastic Optimization of a 10 Blade Element Momentum Based Blade Load Reduction for a 13 MW Direct and Surrogate-Based Optimal Aerodynamic Design of a MW Wind Turbine Blade with Active Study for Active and Passive Microjets Downwind Pre-Aligned Rotor Optimization of Dual-Rotor Wind Biplane Wind Turbine Blade Trailing Edge Flaps Systems on the NREL 5-MW Turbine C. Qin, E. Loth, University of Virginia, Turbines P. Chiu, R. Wirz, University of California, A. Barlas, C. Tibaldi, F. Zahle, H. Madsen, O. Hurley, R. Chow, M. Blaylock, C. Van Dam, Charlottesville, Charlottesville, VA; S. Lee, A. Thelen, L. Leifsson, A. Sharma, Iowa Los Angeles, Los Angeles, CA Technical University of Denmark, Roskilde, University of California, Davis, Davis, CA P. Moriarty, National Renewable Energy State University, Ames, IA; S. Koziel, Denmark Laboratory, Golden, CO Reykjavik University, Reykjavik, Iceland Wednesday, 6 January 2016 269-PANEL-8 Wednesday Morning Forum 360 Seaport F-G 0930 - 1130 hrs Additive Manufacturing – Applications and Opportunities for the Aerospace Industry Moderator: Robert Yancey, VP Aerospace & Composites, Altair Engineering, Inc.

Panelists: Franck Mouriaux Chauncey Wu Jason Dunn Greg Arend General Manager Structures, RUAG Schweiz AG Structural Mechanics and Concepts Branch Co-Founder and CTO Additive Manufacturing Development Leader RUAG Space NASA Langley Research Center Made In Space United Launch Alliance Wednesday, 6 January 2016 270-LEC-7 Aviation Week Annual Workforce Survey Results Seaport H 1000 - 1100 hrs Moderator: Carole Rickard Hedden, Executive Editorial Director, Aviation Week Exceutive Intelligence Panelists: Jim Adams Clarke Havener Lauren Smith Partner Global Sector Leader A&D Concept Development Engineer PwC/Strategy& Korn Ferry Northrop Grumman Aerospace Systems

Wednesday, 6 January 2016 271-LUNCH-3 Luncheon in the Exposition Hall Exposition Hall 1230 - 1400 hrs Wednesday, 6 January 2016 272-AA-6 Aeroacoustics - Fan, Rotor, and Airframe Noise Nautical Chaired by: J. MENDOZA, United Technologies Research Center and C. ROYALTY, Honeywell 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs AIAA-2016-1267 AIAA-2016-1268 AIAA-2016-1269 AIAA-2016-1270 AIAA-2016-1271 AIAA-2016-1272 AIAA-2016-1273 Evaluation of Skin Friction Drag for Hybrid Feedforward Feedback Noise Broadband Noise from a Rotor at Rotor Broadband Noise Due to Isolated Open Rotor Noise Prediction Efficient Multidisciplinary Optimization Landing Gear Noise Prediction and Liner Applications in Aircraft Control at Remote Locations an Angle to the Mean Flow Surface Roughness during Ice Assessment Using the F31A31 of CROR with Time-Spectral Analysis for Tube-And-Wing and C. Gerhold, National Institute of J. Bean, C. Fuller, Virginia Polytechnic Institute S. Glegg, J. Grant, Florida Atlantic Accretion Historical Blade Set Aeroelastics/Aeroacoustics Analysis Hybrid-Wing-Body Aircraft Aerospace, Hampton, VA; M. Brown, NASA and State University, Blacksburg, VA University, Boca Raton, FL; D. Wisda, B. Cheng, Y. Han, K. Brentner, J. Palacios, D. Nark, W. Jones, D. Boyd, N. Zawodny, S. Yi, D. Lee, Korea Advanced Institute of Y. Guo, NEAT Consulting, Seal Beach, Langley Research Center, Hampton, VA; C. H. Murray, W. Alexander, W. Devenport, P. Morris, Pennsylvania State University, NASA Langley Research Center, Hampton, VA Science and Technology, Daejeon, South Korea CA; C. Burley, R. Thomas, NASA Langley Jasinski, University of Notre Dame, Notre Virginia Polytechnic Institute and State University Park, PA ; S. Choi, D. Im, Virginia Polytechnic Institute Research Center, Hampton, VA Dame, IN University, Blacksburg, VA and State University, Blacksburg, VA Wednesday, 6 January 2016 273-ACD-6 Aircraft Design Tools Bankers Hill Chaired by: P. RAJ, Virginia Polytechnic Institute and State University and W. ANEMAAT, DARcorporation 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2016-1274 AIAA-2016-1275 AIAA-2016-1276 AIAA-2016-1277 AIAA-2016-1278 AIAA-2016-1279 Three-Dimensional Modeling of SUAVE: An Open-Source A Conceptual Design Framework RDSwin : Seamlessly-Integrated Object-Oriented Aircraft Mission Development of a Aircraft High-Lift Components with Environment for Conceptual Vehicle for Performance, Life-Cycle Cost, Aircraft Conceptual Design for Analysis Using NPSS Prediction Method for the Vehicle Sketch Pad Design and Optimization and Safety Evaluation of Suborbital Students & Professionals S. Coogan, Southwest Research Institute, Conceptual Design Phase E. Olson, NASA Langley Research Center, E. Botero, A. Wendorff, T. MacDonald, A. Vehicles D. Raymer, Conceptual Research San Antonio, TX J. Vargas-Jimenez, R. Vos, Delft University Hampton, VA Variyar, J. Vegh, T. Lukaczyk, Stanford C. Frank, M. Atanian, O. Pinon-Fischer, D. Corporation, Playa del Rey, CA of Technology, Delft, The Netherlands University, Stanford, CA; et al. Mavris, Georgia Institute of Technology, Atlanta, GA Wednesday, 6 January 2016 274-ACD-7 Transport Aircraft Design II Cortez Hill A Chaired by: E. DIGIROLAMO, Lockheed Martin Aeronautics and D. CARTER, Air Force Research Laboratory 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs AIAA-2016-1280 AIAA-2016-1281 AIAA-2016-1282 AIAA-2016-1283 AIAA-2016-1284 Improved Field Performance Assessing the Effect of Decreased Application of a low fineness Seat Capacity Selection for an PAXelerate - An Open Source through Regulatory Changes to Longitudinal Stability on Aircraft ratio fuselage to an Advanced Short-Haul Aircraft Passenger Flow Simulation Framework Enable Speed Scheduled Reverse Size and Performance configuration Design for Advanced Aircraft Cabin Layouts Thrust Q. Jansen, R. Vos, Delft University of M. Kruger, R. Huyssen, L. Smith, J. T. Marien, NASA Langley Research Center, M. Schmidt, Munich Aerospace e.V., D. Smith, T. Takahashi, Arizona State Technology, Delft, The Netherlands Meyer, University of Pretoria, Pretoria, Hampton, VA Ottobrunn, Germany; M. Engelmann, T. University, Tempe, AZ South Africa Brügge-Zobel, M. Hornung, Bauhaus Luftfahrt e.V., Ottobrunn, Germany; M. Glas, IABG, Ottobrunn, Germany Wednesday, 6 January 2016 275-AFM-9 Aircraft Flight Dynamics, Handling Qualities, and Performance II Harbor A Chaired by: D. MURRI, NASA Engineering and Safety Center and K. SHWEYK, Boeing Engineering Operations & Technology 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs AIAA-2016-1285 AIAA-2016-1286 AIAA-2016-1287 AIAA-2016-1288 AIAA-2016-1289 AIAA-2016-1290 AIAA-2016-1291 The Utilization of Wingtip Vortices in Trajectory Scripts for Aircraft and Linear Approximation of Flapping Comparisons between Avian and Dynamic Modeling and Analysis of Effects of Basing UAS DAA Aircraft Navigation with Uncertain Formation Flight Aerodynamics for Spacecraft Flight path Analysis Wing Flight Dynamics of a Ross’s Unmanned Aerial Vehicle Approach a VTOL Freewing Concept Requirements on Intruder Speeds Aerodynamics Unmanned Arial Vehicles D. Raymer, Conceptual Research Goose to Thermal Updraft Detection S. Haviland, D. Bershadsky, E. Johnson, Lower Than the Statute Speed Limit C. Ashokkumar, G. York , U.S. Air Force N. Saneholtz, S. Kasper, T. Burke, J. Rapski, Corporation, Playa del Rey, CA E. Bodlak, M. Dessouki, M. Fiser, M. C. Pinkerman, T. O’Connell, A. Arena, Georgia Institute of Technology, Atlanta, D. Jack, K. Hoffler, S. Johnson, Adaptive Academy, Colorado Springs, CO Ohio State University, Columbus, OH Mitchener, University of Kansas, Lawrence, KS Oklahoma State University, Stillwater, OK GA Aerospace Group, Inc., Hampton, VA Wednesday, 6 January 2016 276-AMT-6/PC-11/PDL-8 Special Walter Lempert Memorial Session II (Invited) Harbor D Chaired by: S. BERESH, Sandia National Laboratories and T. MEYER, Purdue University 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs Oral Presentation Oral Presentation Oral Presentation Oral Presentation Oral Presentation Oral Presentation Oral Presentation Walter’s Legacy from his Decade at Walter’s contributions to NASA: the Burst-Mode Diagnostics for Flow Diagnostics for Exploring Recent Developments in Rayleigh CARS Measurements of Electric- Walter Lempert’s contributions to Princeton early years through 1 MHz PLIF Combustion Species: Evolution to 4D Physics of Complex Flows Scattering and Filtered Rayleigh Field: Walter’s Contributions at graduate research and education R. Miles, Princeton University, Princeton, Imaging Imaging and Nonlinear Spectroscopy M. Samimy, Ohio State University, Scattering Imaging in Gas-Phase, Sandia B. Thurow, Auburn University, Auburn, AL NJ N. Jiang, Air Force Research Laboratory, T. Meyer, Iowa State University, Ames, IA; J. Columbus, OH Multi-Phase, and Reacting Flows S. Kearney, Sandia National Laboratories, Wright-Patterson AFB, OH; P. Danehy, NASA Gord, Air Force Research Laboratory, Wright- J. Sutton, Ohio State University, Albuquerque, NM Langley Research Center, Hampton, VA Patterson AFB, OH Columbus, OH Wednesday, 6 January 2016 277-APA-27 Special Session: Aerodynamic Design Optimization Benchmark Problems I Coronado D Chaired by: L. LEIFSSON, Iowa State University and S. LEDOUX, Boeing Engineering Operations & Technology 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs AIAA-2016-1292 AIAA-2016-1293 AIAA-2016-1294 AIAA-2016-1295 AIAA-2016-1296 Progress in Aerodynamic Shape Gradient-Based Optimization of Aerodynamic Shape Optimization Two-Dimensional Adjoint-Based Comparitive Study of Two Optimization Based on the CRM Wing-alone and Wing-body- of the CRM Configuration Including Transonic Aerodynamic Design on Optimization Frameworks Applied to Reynolds-Averaged Navier-Stokes tail Configurations by RANS Adjoint Buffet-Onset Conditions Unstructured Meshes Case III: Induced-Drag Minimization Equations Technique G. Kenway, J. Martins, University of E. Fabiano, D. Mavriplis, University of A. Rizzi, M. Zhang, Royal Institute of D. Koo, D. Zingg, University of Toronto, M. Meheut, A. Dumont, G. Carrier, J. Michigan, Ann Arbor, Ann Arbor, MI Wyoming, Laramie, Laramie, WY Technology (KTH), Stockholm, Sweden; Toronto, Canada Peter, ONERA, Meudon, France S. Nadarajah, McGill University, Montréal, Canada; J. Vos, CFS Engineering, Lausanne, Switzerland Wednesday, 6 January 2016 278-APA-28 Special Session: CREATE-AV HPC Multiphysics Applications of Full-up Air Vehicles III Coronado E Chaired by: N. HARIHARAN, CREATE-AV and J. FORSYTHE 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs AIAA-2016-1297 AIAA-2016-1298 AIAA-2016-1299 AIAA-2016-1300 AIAA-2016-1301 Collaborating with Kestrel Modularization of FUN3D as a Unstructured Sliding Interface Entropy solution at concave corners A Novel Double Link Structure (DLS) T. Tuckey, R. McNally, CREATE AV Team, CREATE-AV Helios Near-body Solver Boundaries in Kestrel and ridges with Applications to Computational Eglin AFB, FL; S. Adamec, University of R. Jain, Army Research Development and D. McDaniel, R. Nichols, J. Klepper, R. Aubry, B. Karamete, E. Mestreau, Engineering and Design Alabama, Birmingham, Birmingham, AL Engineering Center, Moffett Field, CA; R. CREATE Kestrel Team, Arnold AFB, TN S. Dey, Naval Research Laboratory, B. Karamete, R. Aubry, E. Mestreau, S. Dey, Biedron, W. Jones, E. Lee-Rausch, NASA Washington, D.C. Naval Research Laboratory, Washington, D.C. Langley Research Center, Hampton, VA Wednesday, 6 January 2016 279-APA-29 Flow Control Applications & Demonstrations II Americas Cup C Chaired by: D. HUNSAKER, Blucraft, LLC 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs AIAA-2016-1302 AIAA-2016-1303 AIAA-2016-1304 AIAA-2016-1305 AIAA-2016-1306 The Development and Active Flow Control at Low Optimization of Vane-Type Vortex Enhancement of Engine Onflow The Airfoil Thickness Effect on Wavy Demonstration of a Plasma Flow Reynolds Numbers by Periodic Generators for Tiltrotor Wings using Conditions Using Vortex Generators Leading Edge Performance Control System on a 20 kW Wind Airfoil Morphing Computational Fluid Dynamics within Curved Intake Channels B. Mattos, Technological Institute of Turbine G. Jones, M. Santer, G. Papadakis, R. Bevan, D. Poole, C. Allen, T. Rendall, M. Ruetten, German Aerospace Center Aeronautics (ITA), São José dos Campos, J. Cooney, C. Szlatenyi, Navatek, Ltd., Imperial College London, London, United University of Bristol, Bristol, United (DLR), Göttingen, Germany Brazil; J. Meneghini, University of São Paulo, South Kingstown, RI; N. Fine, Self, North Kingdom; M. Debiasi, National University Kingdom São Paulo, Brazil; B. Padilha, A. de Paula, Kingstown, RI of Singapore, Singapore, Singapore Technological Institute of Aeronautics (ITA), São José dos Campos, Brazil Wednesday, 6 January 2016 280-APA-30 Unsteady Aerodynamics II Americas Cup D Chaired by: D. O’BRIEN, US Army RDECOM and J. FARNSWORTH, University of Colorado Boulder 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2016-1307 AIAA-2016-1308 AIAA-2016-1309 AIAA-2016-1310 AIAA-2016-1311 AIAA-2016-1312 A Variational Principle for Unsteady Effects of Upstream Disturbances Characterisation of Buffet on a Civil Transonic Buffet Simulation over Modified Spectral Operators for Experimental analysis of the Compressible Flow on a Pitching NACA0012 Airfoil Aircraft Wing Supercritical Airfoil by Unsteady- Time-Collocation and Time-Spectral flow development on an airfoil Y. Hwang, Z. Sotoudeh, Rensselaer B. Merrill, Y. Peet, Arizona State S. Lawson, D. Greenwell, Aircraft Research FaSTAR Code Solvers harmonically surging into reverse flow Polytechnic Institute, Troy, NY University, Tempe, AZ Association Ltd., Bedford, United Kingdom; T. Ishida, K. Ishiko, A. Hashimoto, T. R. Djeddi, K. Ekici, University of K. Mulleners, University of Maryland, College M. Quinn, University of Manchester, Aoyama, Japan Aerospace Exploration Tennessee, Knoxville, Knoxville, TN Park, College Park, MD; M. Ol, Air Force Manchester, United Kingdom Agency (JAXA), Chofu, Japan; K. Research Laboratory, Wright-Patterson AFB,

Takekawa, Ryoyu Systems Company, Ltd., OH; A. Jones, University of Maryland, College Nagoya, Japan Park, College Park, MD Wednesday, 6 January 2016 281-ASC-4 Wing Leading and Trailing Edge Morphing Gaslamp D Chaired by: G. REICH and F. STRAUB, Boeing Defense, Space & Security 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2016-1313 AIAA-2016-1314 AIAA-2016-1315 AIAA-2016-1316 AIAA-2016-1317 AIAA-2016-1318 Investigation into the Effect of Shape Optimization, Design and Structural Directionally Variable Stiffness to Design, Manufacturing and Wind Structural Design of an Adaptive Wing Safety and Reliability Aspects of Deviation on Variable Camber Testing of a High Deformable Reduce Actuation Requirement in Tunnel Test of a Morphing Wing Trailing Edge for Enhanced Cruise an Adaptive Trailing Edge Device Compliant Wing Performance Adaptive Wing Leading Edge Airfoil Camber Morphing Based on Compliant Structures Performance (ATED) C. Marks, Air Force Research Laboratory, A. Rudenko, M. Radestock, H. Monner, M. DiPalma, F. Gandhi, Rensselaer S. Ricci, A. De Gaspari, L. Riccobene, A. Concilio, I. Dimino, Italian Aerospace I. Dimino, A. Concilio, Italian Aerospace Wright-Patterson AFB, OH; L. Zientarski, German Aerospace Center (DLR), Polytechnic Institute, Troy, NY Technical University of Milan, Milan, Italy Research Center (CIRA), Capua, Italy; R. Research Center (CIRA), Capua, Italy; R. University of Dayton Research Institute, Braunschweig, Germany Pecora, University of Naples “Federico II”, Pecora, University of Naples “Federico II”, Dayton, OH; J. Joo, Air Force Research Naples, Italy; M. Ciminello, Italian Aerospace Naples, Italy Laboratory, Wright-Patterson AFB, OH Research Center (CIRA), Capua, Italy Wednesday, 6 January 2016 282-DSC-3 High Speed Systems Gaslamp C Chaired by: N. FALKIEWICZ, MIT Lincoln Laboratory and E. BLADES, ATA Engineering, Inc. 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs AIAA-2016-1319 AIAA-2016-1320 AIAA-2016-1321 AIAA-2016-1322 AIAA-2016-1323 AIAA-2016-1324 AIAA-2016-1325 Using FUN3D for Aeroelatic, Sonic Towards an Aero-Propulso-Servo- Dynamic Fluid-Thermal-Structural Nonlinear Thermal and Rapid Loads Prediction for Aeroelastic Modeling and Aeroelastic Control-oriented Modeling Boom, and AeroPropulsoServoElastic Elasticity Analysis of a Commercial Interaction Effects in Preliminary Thermoelastic Reduced Order Supersonic and Hypersonic Vehicles Simulation of Very Flexible of an Air-breathing Hypersonic Vehicle (APSE) Analyses of a Supersonic Design of High Speed Vehicles Models of a Hypersonic Vehicle Using CFD Surrogates Munitions P. Sudalagunta, C. Sultan, R. Kapania, L. Configuration J. Connolly, NASA Glenn Research Center, Z. Witeof, L. Neergaard, A. Vanderwyst, R. Klock, C. Cesnik, University of Michigan, D. Zettl, E. Dreyer, B. Grier, J. McNamara, R. Kitson, C. Cesnik, University of Watson, P. Raj, Virginia Polytechnic Institute W. Silva, M. Sanetrik, P. Chwalowski, NASA Cleveland, OH; P. Chwalowski, M. Sanetrik, A. Shelton, C. Martin, Leidos Corporation, Ann Arbor, Ann Arbor, MI Ohio State University, Columbus, OH; C. Michigan, Ann Arbor, Ann Arbor, MI and State University, Blacksburg, VA Langley Research Center, Hampton, VA J. Carlson, W. Silva, NASA Langley Research Eglin AFB, FL; C. Pasiliao, Air Force Pasiliao, Air Force Research Laboratory, Center, Hampton, VA; J. McNamara, Ohio Research Laboratory, Eglin AFB, FL Eglin AFB, FL State University, Columbus, OH; et al. Wednesday, 6 January 2016 283-FD-34 CFD: Higher-Order Methods II Pier Chaired by: H. LUO, North Carolina State University and A. MAZAHERI, NASA-Langley Research Center 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs AIAA-2016-1326 AIAA-2016-1327 AIAA-2016-1328 AIAA-2016-1329 AIAA-2016-1330 AIAA-2016-1331 AIAA-2016-1332 A fast, implicit discontinuous Galerkin Improved Spectral Volume Investigation of Stabilization Summation-by-Parts Operators with A Hybrid Reconstructed High-Order Residual-Distribution Implicit large-eddy simulation of method based on analytical Jacobians Method (SV+ Method) for Hybrid Methods for Multi-Dimensional Minimal Dispersion Error for Accurate Discontinuous Galerkin Method Schemes for Discontinuous Problems compressible flows using the Interior for the compressible Navier-Stokes Unstructured Mesh Summation-by-parts Discretizations and Efficient Flow Calculations for Compressible Flows on on Irregular Triangular Grids Embedded Discontinuous Galerkin equations Y. Sawaki, Tohoku University, Sendai, of the Euler Equations V. Linders, Linköping University, Linköping, Unstructured Grids A. Mazaheri, NASA Langley Research Center, method X. Yang, J. Cheng, C. Wang, H. Luo, North Japan; T. Haga, Japan Aerospace J. Crean, K. Panda, A. Ashley, J. Hicken, Sweden; M. Kupiainen, Swedish J. Cheng, T. Liu, Beihang University, Hampton, VA; H. Nishikawa, National Institute P. Fernandez, C. Nguyen, Massachusetts Carolina State University, Raleigh, NC; J. Si, Exploration Agency (JAXA), Sagamihara, Rensselaer Polytechnic Institute, Troy, NY Meteorological and Hydrological Institute, Beijing, China; H. Luo, North Carolina of Aerospace, Hampton, VA Institute of Technology, Cambridge, MA; X.

Commercial Aircraft Corporation of China, Japan; Y. Ogino, S. Kawai, K. Sawada, Norrköping, Sweden; S. Frankel, Y. Delorme, State University, Raleigh, NC Roca, Barcelona Supercomputing Center, Shanghai, China; A. Pandare, North Carolina Tohoku University, Sendai, Japan Technion--Israel Institute of Technology, Haifa, Barcelona, Spain; J. Peraire, Massachusetts State University, Raleigh, NC Israel; J. Nordstrom, Linköping University, Institute of Technology, Cambridge, MA Linköping, Sweden Wednesday, 6 January 2016 284-FD-35 Discontinuous Galerkin Methods Harbor F Chaired by: J. EKATERINARIS, Embry-Riddle Aeronautical University and J. BENEK, Air Force Research Lab AFRL/RQ 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2016-1333 AIAA-2016-1334 AIAA-2016-1335 AIAA-2016-1336 AIAA-2016-1337 AIAA-2016-1338 A High-order Discontinuous A Direct Discontinuous Galerkin High-Order Cellwise Relaxation A dissipative lter for DG Discontinuous Galerkin for Development of a Perfectly Galerkin Method for Unsteady Flow method for the compressible Navier- Implicit Discontinuous Galerkin discretizations with subcell Advection with Interface-Centered Matched Layer Technique for a Problems Stokes equations on arbitrary grids Scheme for Unsteady Flow discontinuity resolution Reconstruction Discontinuous-Galerkin Spectral- R. Borker, C. Farhat, R. Tezaur, Stanford J. Cheng, Beihang University, Beijing, China; Computations K. Panourgias, University of Patras, Rio, L. Khieu, Institute for Computational Element Method University, Stanford, CA X. Yang, Commercial Aircraft Corporation H. Asada, S. Kawai, K. Sawada, Tohoku Greece; J. Ekaterinaris, Embry-Riddle Science and Technology, Ho Chi Minh, Viet A. Garai, L. Diosady, S. Murman, N. of China, Shanghai, China; T. Liu, Beihang University, Sendai, Japan Aeronautical University, Daytona Beach, FL Nam; K. Fidkowski, E. Johnsen, University Madavan, NASA Ames Research Center, University, Beijing, China; H. Luo, North of Michigan, Ann Arbor, Ann Arbor, MI Moffett Field, CA Carolina State University, Raleigh, NC Wednesday, 6 January 2016 285-FD-36 Multiphase Flow I: Simulations and Models Promenade B Chaired by: D. PELLETIER, École polytechnique de Montréal 1400 hrs 1430 hrs 1500 hrs 1530 hrs AIAA-2016-1339 AIAA-2016-1340 AIAA-2016-1341 AIAA-2016-1342 Modeling of Large Droplets An Adaptive Coupled Level Set Computations of Evolving Oil Droplet Adaptive time integration for Impingement Using a Hybrid and Moment-of-Fluid Method for on Surface of a Wall-Bounded Air Flow separated two-phase viscous flows Taylor-Galerkin Variational Multi- Simulating Droplet Impact and G. Bonnavion, Illinois Institute of Technology, A. Hay, D. Pelletier, Defense Research and Scale Stabilized Level Set Method Solidification on Solid Surfaces with Chicago, IL; W. Dziedzic, Dassault Systemes Development Canada, Montréal, Canada A. Bakkar, W. Habashi, M. Fossati, McGill Application to Aircraft Icing SolidWorks Corporation, Chicago, IL; A. University, Montréal, Canada M. Vahab, C. Pei, M. Hussaini, M. Obabko, Argonne National Laboratory, Sussman, Florida State University, Chicago, IL; H. Nagib, Illinois Institute of Tallahassee, FL; Y. Lian, University of Technology, Chicago, IL Louisville, Louisville, KY Wednesday, 6 January 2016 286-FD-37 Unsteady Vortex Flows Promenade A Chaired by: Z. RUSAK, Rensselaer Polytechnic Institute and J. MORRIDA 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs AIAA-2016-1343 AIAA-2016-1344 AIAA-2016-1345 AIAA-2016-1346 AIAA-2016-1347 AIAA-2016-1348 AIAA-2016-1349 Spanwise Effects on High Speed Resonance Characteristics of Relationship between Transonic Cavity Improvement in prediction Prediction of Dynamic Stability Investigation of Shock Dynamics on Transonic Flow Dynamics Over a Cavity Flows Transonic Flow over a Rectangular Tones and Flowfield Dynamics using capability of Transonic Buffet on using Mapped Chebyshev a Hemisphere Using Pressure and Hemisphere in Flight Y. Sun, Y. Zhang, K. Taira, L. Cattafesta, Cavity using Pulse-Burst PIV Pulse-Burst PIV NASA-CRM Using URANS Pseudospectral Method Optical Measurements J. Morrida, S. Gordeyev, E. Jumper, Florida State University, Tallahassee, FL; B. S. Beresh, J. Wagner, E. Demauro, J. J. Wagner, S. Beresh, K. Casper, E. Demauro, K. Kumada, K. Sawada, Tohoku University, J. Choi, S. Choi, J. Park, D. Im, Virginia J. Morrida, S. Gordeyev, E. Jumper, University University of Notre Dame, Notre Dame, IN George, L. Ukeiley, University of Florida, Henfling, R. Spillers, Sandia National S. Arunajatesan, J. Henfling, Sandia National Sendai, Japan Polytechnic Institute and State University, of Notre Dame, Notre Dame, IN; S. Gogineni,

Gainesville, Gainesville, FL Laboratories, Albuquerque, NM Laboratories, Albuquerque, NM; et al. Blacksburg, VA Spectral Energies, LLC, Dayton, OH; A. Marruffo, D. Wittich, Air Force Research Laboratory, Kirtland AFB, NM Wednesday, 6 January 2016 287-FD-38 Unsteady Wing Aerodynamics Cove Chaired by: C. BARNES, AFRL/RQVA and B. JOLLY, US Air Force 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs AIAA-2016-1350 AIAA-2016-1351 AIAA-2016-1352 AIAA-2016-1353 AIAA-2016-1354 AIAA-2016-1355 AIAA-2016-1356 Two dimensional and three Fluid-Structure Interaction Spectral Decomposition and Scale High-Fidelity LES Simulations of Variation of Leading-Edge Suction Effects of 3D Time-Harmonic High Advance-Ratio Airfoil Streamwise dimensional numerical simulation simulations of a membrane wing Separation of the Dynamic Stall Self-Sustained Pitching Oscillations at Stall for Steady and Unsteady Gust and Turbulence on Unsteady Oscillations: Wind Tunnel vs. Water of cycloidal propellers in hovering with variable compliance Vortices in a Plunging Airfoil on a NACA0012 Airfoil at Airfoil Motions Aerodynamic Responses of Loaded Tunnel status G. Cetraro, R. Sandberg, University of A. Mohan, L. Agostini, Ohio State Transitional Reynolds Numbers S. Narsipur, P. Hosangadi, A. Low-Speed Airfoils H. Mueller-Vahl, D. Greenblatt, Technion--Israel Y. Hu, H. Zhang, G. Wang, Northwestern Southampton, Southampton, United University, Columbus, OH; M. Visbal, C. Barnes, M. Visbal, Air Force Research Gopalarathnam, J. Edwards, North Carolina M. Kazarina, L. Nguyen, V. Golubev, Institute of Technology, Haifa, Israel; M. Ol, Air Polytechnical University, Xi’an, China Kingdom Air Force Research Laboratory, Wright- Laboratory, Wright-Patterson AFB, OH State University, Raleigh, NC Embry-Riddle Aeronautical University, Force Research Laboratory, Wright-Patterson Patterson AFB, OH; D. Gaitonde, Ohio Daytona Beach, FL; S. Borener, D. AFB, OH; K. Granlund, North Carolina State State University, Columbus, OH Hufty, Federal Aviation Administration, University, Raleigh, NC Washington, D.C.; C. Pasiliao, Air Force Research Laboratory, Eglin AFB, FL; et al. Wednesday, 6 January 2016 288-FD-39/APA-31 Special Session: Evaluation of RANS Solvers on Benchmark Aerodynamic Flows II Harbor E Chaired by: A. KATZ and K. FIDKOWSKI, University of Michigan 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs AIAA-2016-1357 AIAA-2016-1358 AIAA-2016-1359 AIAA-2016-1360 AIAA-2016-1361 RANS simulations on TMR 3D test Results of Three-dimensional Turbulent Development and Assessment of a Critical Evaluation of Turbulence Application of HPCMP CREATETM- cases with the Onera elsA flow Flow with FaSTAR Reconstructed Discontinuous Galerkin Modeling with the Flux Correction AV COFFE for Three-Dimensional solver A. Hashimoto, T. Ishida, T. Aoyama, Japan Method for the Compressible Turbulent Method on Strand Grids Turbulent Flow Cases M. Julien, A. Dumont, V. Gleize, D. Aerospace Exploration Agency (JAXA), Chofu, Flows on Hybrid Grids Y. Yanagita, O. Tong, A. Katz, Utah State J. Erwin, R. Glasby, University of Destarac, ONERA, Châtillon, France Japan; K. Takekawa, K. Hayashi, Ryoyu X. Liu, H. Luo, North Carolina State University, University, Logan, UT Tennessee, Oak Ridge, Oak Ridge, TN Systems Company, Ltd., Nagoya, Japan Raleigh, NC Wednesday, 6 January 2016 289-GEPC-4 Alternative Fuels and Green Engineering Computations Americas Cup B Chaired by: N. HICKS and T. ABDEL-SALAM, East Carolina University 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs AIAA-2016-1362 AIAA-2016-1363 AIAA-2016-1364 AIAA-2016-1365 AIAA-2016-1366 AIAA-2016-1367 AIAA-2016-1368 Potential Market Sizes and Adoption Biodiesel for Aviation use in New Comparative Assessment of Air Flow Regimes in Turbulent Swirling On the Computations of Double Computational Analyses of Computations of Aerodynamic Schedules of Liquid Natural Gas Zealand Distribution Systems : Improving Flames in Cylindrical Furnaces Squealer and Flat Gas Turbine Aerodynamic Characteristics of Behaviour of Rectangular Wing with Commercial Aircraft and the LNG Air R. Davies, G. Gunabalan, C. Davies, Indoor Thermal Comfort in Office E. Khalil, K. Samir, Cairo University, Giza, Blades Tips NACA653218airfoil Naca653218airfoil Transportation System Massey University, Palmerston North, Spaces Egypt E. Khalil, Cairo University, Giza, Egypt; H. E. Khalil, Cairo University, Giza, Egypt; E. Khalil, E. AbdelGhany, Cairo University, Giza, J. Gibbs, K. Wicke, T. Schilling, R. Ghosh, B. New Zealand E. Khalil, A. Abou Zeid, Cairo University, El-Zomor, M. Morsy, High Technological O. Abdelattif, Benha University, Cairo, Egypt; O. Abdelattif, Benha University, Cairo, Nagel, O. Pape, German Aerospace Center Giza, Egypt Institute, Cairo, Egypt Egypt; E. AbdelGhany, G. ElHariri, Cairo Egypt; G. ElHariri, Cairo University, Giza, Egypt (DLR), Hamburg, Germany University, Giza, Egypt

Wednesday, 6 January 2016 290-GNC-24 Spacecraft Trajectory Optimization and Orbit Control Hillcrest B Chaired by: J. REED, United Launch Alliance, LLC and U. SHANKAR, The Johns Hopkins University Applied Physics Laboratory 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs AIAA-2016-1369 AIAA-2016-1370 AIAA-2016-1371 AIAA-2016-1372 AIAA-2016-1373 Spinning CubeSats with Liquid The Method of Multiple Scales for Flight-Path Angle Guidance for Three-Dimensional Trajectory An Observability-Based Trajectory Propellant Orbit Propagation with Atmospheric Aero- Maneuvers on Optimization for Lunar Ascent Optimization Considering K. Doyle, M. Peck, Cornell University, Drag Hyperbolic Trajectories Using Gauss Pseudospectral Method Disturbance for Atmospheric Entry Ithaca, NY; L. Jones, Jet Propulsion A. Awad, A. Narang-Siddarth, University A. Mazzaracchio, University of Rome “La L. Ma, Z. Shao, W. Chen, Zhejiang Z. Yu, Z. Zhao, P. Cui, Beijing Institute of Laboratory, California Institute of of Washington, Seattle, Seattle, WA; R. Sapienza”, Rome, Italy University, Hangzhou, China; X. Lv, Z. Technology, Beijing, China Technology, Pasadena, CA Weisman, Air Force Research Laboratory, Song, Beijing Aerospace Automatic Control Kirtland AFB, NM Institute, Beijing, China Wednesday, 6 January 2016 291-GNC-25 Invited Session: Advances in Guidance and Control of Unmanned Air Vehicles Hillcrest A Chaired by: S. CHUNG, University of Illinois at Urbana-Champaign and N. HOVAKIMYAN, University of Illinois at Urbana-Champaign 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs AIAA-2016-1374 AIAA-2016-1375 AIAA-2016-1376 AIAA-2016-1377 AIAA-2016-1378 A Real-Time Framework for Convex Multi-Objective Filter Nonlinear Flight Controller Bio-Inspired Algorithm for Task Robotic Herding Flight using Herding Kinodynamic Planning with Optimization for Output Feedback Synthesis of a Bat-Inspired Micro Allocation in Multi-UAV Search and Primitives and Wavefront Algorithms Application to Quadrotor Obstacle L1-Adaptive Controller Aerial Vehicle Rescue Missions S. Gade, University of Illinois, Urbana- Avoidance H. Jafarnejadsani, H. Lee, N. Hovakimyan, A. Ramezani, X. Shi, S. Chung, S. H. Kurdi, J. How, Massachusetts Institute Champaign, Urbana, IL; A. Paranjape, Indian R. Allen, M. Pavone, Stanford University, University of Illinois, Urbana-Champaign, Hutchinson, University of Illinois, Urbana- of Technology, Cambridge, MA Institute of Technology Bombay, Mumbai, Stanford, CA Urbana, IL Champaign, Urbana, IL India; S. Chung, University of Illinois, Urbana- Champaign, Urbana, IL Wednesday, 6 January 2016 292-GNC-26 H Infinity, Nonlinear, and Adaptive Flight Control Hillcrest C Chaired by: H. TAHA, University of California, Irvine and E. VAN KAMPEN, TU Delft 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs AIAA-2016-1379 AIAA-2016-1380 AIAA-2016-1381 AIAA-2016-1382 AIAA-2016-1383 Sequential Loop Closure Based Adaptive Incremental Backstepping Comparison of Robust and L1 Adaptive Control with Nonlinear Aircraft Flight Control Adaptive Autopilot Design for a Flight Control for a High- Probabilistic LMI-Based Design of Eigenstructure Assignment for Pole Using the Forward Propagating Hypersonic Vehicle Performance Aircraft with Adaptive Flight Controllers with Placement considering Actuator Riccati Equation D. Wiese, A. Annaswamy, Massachusetts Uncertainties Uncertain Input Dynamics Dynamics and Delays A. Prach, O. Tekinalp, Middle East Institute of Technology, Cambridge, MA; P. van Gils, E. Van Kampen, C. de Visser, M. Fravolini, University of Perugia, F. Hellmundt, Airbus Group, Munich, Technical University, Ankara, Turkey; D. J. Muse, M. Bolender, Air Force Research Q. Chu, Delft University of Technology, Perugia, Italy; T. Yucelen, B. Gruenwald, Germany; J. Dodenhöft, F. Holzapfel, Bernstein, University of Michigan, Ann Laboratory, Wright-Patterson AFB, OH; Delft, The Netherlands D. Wagner, Missouri University of Science Technical University of Munich, Garching, Arbor, MI E. Lavretsky, The Boeing Company, and Technology, Rolla, MO; M. Napolitano, Germany Huntington Beach, CA West Virginia University, Morgantown, WV Wednesday, 6 January 2016 293-GNC-27 Control of Multirotor Aircraft Cortez Hill B Chaired by: V. STEPANYAN, University of California, Santa Cruz and J. JUNELL, Jaime Junell 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs AIAA-2016-1384 AIAA-2016-1385 AIAA-2016-1386 AIAA-2016-1387 AIAA-2016-1388 AIAA-2016-1389 AIAA-2016-1390 Identification and reconfigurable Autonomous Position Control Onboard Flow Sensing for Rotary- Self-tuning Gains of a Quadrotor Position Tracking of an Robust Tracking Control of a Adaptive Incremental Nonlinear Control of Impaired Multi-Rotor Analysis of Quadrotor Flight in Wing UAV Pitch Control in Wind using a Simple Model for Policy Underactuated Quadrotor using Quadrotor with Time-Varying Gain Dynamic Inversion for Attitude Drones Urban Wind Gust Conditions D. Yeo, N. Sydney, D. Paley, University of Gradient Reinforcement Learning Model Reference Adaptive Control in the Presence of Uncertainty and Control of Micro Aerial Vehicles V. Stepanyan, University of California, Santa S. Raza, J. Etele, Carleton University, Maryland, College Park, College Park, MD J. Junell, T. Mannucci, Y. Zhou, E. Van A. Abdul Ghaffar , T. Richardson, University Disturbances E. Smeur, Q. Chu, G. de Croon, Delft Cruz, Santa Cruz, CA; K. Krishnakumar, NASA Ottawa, Canada Kampen, Delft University of Technology, of Bristol, Bristol, United Kingdom C. Ton, Air Force Research Laboratory, Eglin University of Technology, Delft, The

Ames Research Center, Moffett Field, CA; A. Delft, The Netherlands AFB, FL; M. McCourt, S. Mehta, University of Netherlands Bencomo, Stinger Ghaffarian Technologies, Florida, Shalimar, Shalimar, FL Inc., Moffett Field, CA Wednesday, 6 January 2016 294-GTE-10 Combustion II Cortez Hill C Chaired by: S. NAIK, Purdue University and C. LI, Air Force Office of Scientific Research 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2016-1391 AIAA-2016-1392 AIAA-2016-1393 AIAA-2016-1394 AIAA-2016-1395 AIAA-2016-1396 Modeling of Methane Ingestion into Mechanisms for Enhanced Flow High-Fidelity Simulations of Fuel Parametric Modeling Investigation Numerical Study on Flame Experimental and Computational Gas Turbine Engines Migration from an Annular, High-g Injection and Atomization of a of a Radially-Staged Low-Emission Stabilization Mechanism of a multi-jet Imaging of Mid-Infrared Radiation J. Delimont, Southwest Research Institute, Ultra Compact Combustor Hybrid Air-Blast Atomizer Aviation Combustor burner with LES Flamelet Approach from a Turbulent Ethylene Flame San Antonio, TX A. Cottle, M. Polanka, Air Force Institute of P. Ma, L. Esclape, S. Carbajal, M. Ihme, C. Heath, NASA Glenn Research Center, Y. Tang, H. Koo, University of Michigan, Ann H. Lalit, R. Kapaku, Purdue University, West Technology, Wright-Patterson AFB, OH Stanford University, Stanford, CA; T. Cleveland, OH Arbor, Ann Arbor, MI; C. Lietz, University of Lafayette, IN; B. Rankin, Air Force Research Buschhagen, S. Naik, Purdue University, Texas, Austin, Austin, TX; V. Raman, University Laboratory, Wright-Patterson AFB, OH; M. West Lafayette, IN; et al. of Michigan, Ann Arbor, Ann Arbor, MI Mueller, Princeton University, Princeton, NJ; J. Gore, Purdue University, West Lafayette, IN Wednesday, 6 January 2016 295-HIS-3 Boeing Centennial 1916-2016 I Americas Cup A Chaired by: S. MUSI 1400 hrs 1530 hrs 1600 hrs 1630 hrs Oral Presentation AIAA-2016-1397 AIAA-2016-1398 AIAA-2016-1399 Boeing Centennial Session Opening Presentation The Boeing Aerodynamical The History of Boeing Heritage Vanguard: A Pre-History of The M. Lombardi, The Boeing Company, Seattle, WA Chamber and its Impact on Companies Impact on Naval Tactical Boeing Company Aeronautics Education at the Aircraft S. Musi, The Boeing Company, Seattle, WA University of Washington R. Dowgwillo, The Boeing Company, St. A. Bruckner, University of Washington, Louis, MO Seattle, Seattle, WA; S. Eberhardt, Self, Leavenworth, WA; J. Lee, S. Musi, The Boeing Company, Seattle, WA Wednesday, 6 January 2016 296-HSABP-5 Advances in Pressure Gain Combustion II - RDE & PDE Regatta A Chaired by: K. KAILASANATH, Naval Research Laboratory and J. KASAHARA, Nagoya University 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs AIAA-2016-1400 AIAA-2016-1401 AIAA-2016-1402 AIAA-2016-1403 AIAA-2016-1404 AIAA-2016-1405 AIAA-2016-1406 Propane-Air Cell Size Correlation to One-Dimensional Numerical A Correlation-Based Method to Parametric Study of an Ethylene- Experimentation of a Premixed Thermodynamic Modeling of Study of Combustion Chamber Temperature and Pressure Investigation on Purging the Quantify the Operating State in a Air Rotating Detonation Engine Rotating Detonation Engine a Rotating Detonation Engine Characteristic Length in C. Stevens, J. Hoke, Innovative Scientific Burned Gas by the Evaporation of Rotating Detonation Combustor Using an Ideal Model Utilizing a Variable Slot Feed Through a Reduced Order Approach Rotating Detonation Engine with Solutions, Inc., Dayton, OH; F. Schauer, Water Droplets in Pulse Detonation A. St. George, V. Ganesh Kumar, R. R. Fievisohn, K. Yu, University of Plenum T. Kaemming, M. Fotia, J. Hoke, Convergent-Divergent Nozzle Air Force Research Laboratory, Wright- Combustor Driscoll, E. Gutmark, University of Maryland, College Park, College Park, MD I. Andrus, P. King, M. Polanka, Air Force Innovative Scientific Solutions, Inc., Y. Kato, K. Ishihara, K. Matsuoka, J. Patterson AFB, OH H. Watanabe, A. Matsuo, Keio University, Cincinnati, Cincinnati, OH Institute of Technology, Wright-Patterson Dayton, OH; F. Schauer, Air Force Research Kasahara, Nagoya University, Nagoya, Yokohama, Japan; K. Muto, K. Matsuoka, AFB, OH; F. Schauer, Air Force Research Laboratory, Wright-Patterson AFB, OH Japan; A. Matsuo, Keio University, J. Kasahara, Nagoya University, Nagoya, Laboratory, Wright-Patterson AFB, OH; J. Yokohama, Japan; I. Funaki, Japan Japan; T. Endo, Hiroshima University, Hoke, Innovative Scientific Solutions, Inc., Aerospace Exploration Agency (JAXA), Higashi-Hiroshima, Japan Centerville, OH Sagamihara, Japan Wednesday, 6 January 2016 297-IS-7 Machine Learning and Probabilistic Reasoning for Intelligent UAS Regatta B Chaired by: D. CASBEER, Air Force Reseach Laboratory and A. AGHA-MOHAMMADI 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2016-1407 AIAA-2016-1408 AIAA-2016-1409 AIAA-2016-1410 AIAA-2016-1411 AIAA-2016-1412 Health-Aware Multi-UAV Planning Analytic Chance Constraints for the Scalable Decentralized Partial Co-operation in an Autonomous, Trajectory Clustering, Modeling and Deep Convolutional Neural using Decentralized Partially Robust Guidance of Autonomous State Estimation with Sensor Decentralised, Unmanned Air Selection with the focus on Airspace Network For Human Detection And Observable Semi-Markov Decision Parafoils Uncertainties Using Factorized Data System for Atmospheric Research Protection Tracking In FLIR Videos Processes A. Ellertson, J. How, Massachusetts Fusion C. Crispin, A. Sobester, University of W. Eerland, S. Box, University of A. Sathyan, University of Cincinnati, S. Omidshafiei, A. Agha-mohammadi, Institute of Technology, Cambridge, MA; L. N. Ahmed, University of Colorado, Southampton, Southampton, United Southampton, Southampton, United Cincinnati, OH; J. Cohen, University of Massachusetts Institute of Technology, Breger, Draper Laboratory, Cambridge, MA Boulder, Boulder, CO; W. Whitacre, Draper Kingdom Kingdom Michigan, Ann Arbor, MI; M. Kumar, Cambridge, MA; C. Amato, University of Laboratory, Cambridge, MA; S. Moon, University of Cincinnati, Cincinnati, OH New Hampshire, Durham, Durham, NH; E. Frew, University of Colorado, Boulder, S. Liu, J. How, Massachusetts Institute of Boulder, CO Technology, Cambridge, MA; J. Vian, The Boeing Company, Seattle, WA Wednesday, 6 January 2016 298-MAT-8 Advanced Materials and Processing Gaslamp B Chaired by: M. NARAGHI, Texas A & M university and D. POWELL, SpaceX 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2016-1413 AIAA-2016-1414 AIAA-2016-1415 AIAA-2016-1416 AIAA-2016-1417 AIAA-2016-1418 Characterizing Mechanical Development of Advanced Flexible Lightweight Adjustable Fabrication of High Thermal Development of a Novel Self- An Experimental Study into Active Properties of Hybrid Alumina Conformal Ablative TPS Fabricated Stiffness Hinge (FLASH) for Conductivity NARloy-Z-Diamond Healing Polymer with High Damping Mechanisms in CNT Carbon Fiber Composites with from Rayon- and Pan-Based Advanced Cable Technology Composite Combustion Chamber Temperature Stability Nanocomposite Piezospectroscopy Carbon Felts J. Mejia-Ariza, L.Garde, Inc., Tustin, Liner for Advanced Rocket Engines Y. Heo, University of Florida, Gainesville, F. Gardea, D. Lagoudas, M. Naraghi, Texas I. Hanhan, A. Selimov, University of M. Gasch, M. Stackpoole, S. White, NASA CA; T. Murphey, Opterus Research and B. Bhat, S. Greene, NASA Marshall Space Gainesville, FL; H. Sodano, University of A&M University, College Station, TX Central Florida, Orlando, FL; D. Carolan, A. Ames Research Center, Moffett Field, CA; Development, Inc., Syracuse, NY Flight Center, Huntsville, AL; J. Singh, Michigan, Ann Arbor, Ann Arbor, MI Taylor, Imperial College London, London, T. Boghozian, ERC Inc., Moffett Field, CA Pennsylvania State University, University United Kingdom; S. Raghavan, University Park, PA of Central Florida, Orlando, FL Wednesday, 6 January 2016 299-MDO-6 Design Including Uncertainty & Frameworks Balboa A Chaired by: M. RAIS-ROHANI, Mississippi State University and J. DEATON, Adjoint Technologies 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2016-1419 AIAA-2016-1420 AIAA-2016-1421 AIAA-2016-1422 AIAA-2016-1423 AIAA-2016-1424 Uncertainty Quantification for Using Multiple Information Sources Optimization Under Uncertainty of Kona: A Parallel Optimization Library Sensitivity analysis methods for A Multi-Disciplinary Study of Future Cargo Hold Fires to Construct Stochastic Databases Parallel Nonlinear Energy Sinks for Engineering-Design Problems uncertainty budgeting in system Fuel Efficient Regional Aircraft A. DeGennaro, M. Lohry, L. Martinelli, C. to Quantify Uncertainty in E. Boroson, S. Missoum, University of A. Dener, P. Meng, J. Hicken, Rensselaer design R. Palma, M. Thomas, A. Balasiu, L. Rowley, Princeton University, Princeton, NJ Certification Maneuvers Arizona, Tucson, Tucson, AZ Polytechnic Institute, Troy, NY; G. Kennedy, M. Opgenoord, K. Willcox, Massachusetts Takamatsu, W. Noonan, T. Takahashi, A. Wendorff, J. Alonso, Stanford Georgia Institute of Technology, Atlanta, GA; Institute of Technology, Cambridge, MA Arizona State University, Tempe, AZ

University, Stanford, CA; S. Bieniawski, J. Hwang, University of Michigan, Ann Arbor, The Boeing Company, Chicago, IL Ann Arbor, MI; J. Gray, NASA Glenn Research Center, Cleveland, OH Wednesday, 6 January 2016 300-MST-8 Hardware-in-the-Loop Simulation Golden Hill A Chaired by: R. RUFF and U. DURAK, DLR-German Aerospace Center 1400 hrs 1430 hrs 1500 hrs 1530 hrs AIAA-2016-1425 AIAA-2016-1426 AIAA-2016-1427 AIAA-2016-1428 Benchmarking Variants of a Integrated Energy and Power How to Realize Coupling of HIL Modeling and Simulation Hardware-in-the-Loop Simulation Management: Validation Testing for Simulations over Large Distances Hardware-in-the-Loop for System Aerosapce Vehicles A. Himmler, dSPACE GmbH, Paderborn, Unmanned Aerial Vehicle E. Aretskin-Hariton, NASA Glenn Research K. Yerkes, Air Force Research Laboratory, Germany A. Shawky Mohamedy, A. Aly, A. Elnashar, Center, Cleveland, OH; A. Zinnecker, N&R Wright-Patterson AFB, OH; B. Eussen, National Military Technical College, Cairo, Egypt Engineering, Inc., Parma Heights, OH; J. Aerospace Laboratory (NLR), Amsterdam, Kratz, D. Culley, NASA Glenn Research The Netherlands ; D. Pratt, Air Force Research Center, Cleveland, OH; G. Thomas, N&R Laboratory, Wright-Patterson AFB, OH; J. Engineering, Inc., Parma Heights, OH van Muijden, National Aerospace Laboratory (NLR), Amsterdam, The Netherlands ; J. Doty, University of Dayton, Dayton, OH Wednesday, 6 January 2016 301-MST-9 Invited Session: LOC-6, Simulation-Based Evaluations for Improved Pilot Insights and Training for LOC Prevention and Recovery. Coronado B Chaired by: C. BELCASTRO, NASA-Langley Research Center and D. CRIDER, National Transportation Safety Board 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2016-1429 AIAA-2016-1430 Oral Presentation Oral Presentation AIAA-2016-1431 AIAA-2016-1432 Upset Prevention and Recovery Global Implementation of Upset Integrated Multidisciplinary Piloted Modeling and Simulation A Computational Model for Are Pilots in Control? How do pilots Training - A Regulator Update Prevention & Recovery Training Simulation Capability for Aircraft Loss Development of a T-Tail Regional Prediction of Pilot Manual Control react to unexpected situations? J. Schroeder, Federal Aviation S. Advani, International Development of of Control (LOC) Research Aircraft for LOC Research Behavior in Air Transport Concepts J. Field, A. Lemmers, E. Boland, National Administration, Moffett Field, CA Technology, Breda, The Netherlands ; J. G. Shah, K. Cunningham, J. Foster, NASA G. Shah, J. Foster, K. Cunningham, D. of Operation Aerospace Laboratory (NLR), Amsterdam, Schroeder, Federal Aviation Administration, Langley Research Center, Hampton, VA; M. Cox, J. Petrilli, N. Frink, NASA Langley D. Dickson, A. Pritchett, A. Bozan, Georgia The Netherlands Washington, D.C.; B. Burks, Alaska Hill, Unisys Corporation, Hampton, VA; T. Research Center, Hampton, VA Institute of Technology, Atlanta, GA Airlines, Seattle, WA Guo, J. Litt, NASA Glenn Research Center, Cleveland, OH Wednesday, 6 January 2016 302-MST-10 Motion Systems, Visual Systems, and Image Generation Golden Hill B Chaired by: P. ZAAL, NASA Ames Research Center and D. CARTMELL, Boeing Engineering Operations & Technology 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs AIAA-2016-1433 AIAA-2016-1434 AIAA-2016-1435 AIAA-2016-1436 AIAA-2016-1437 AIAA-2016-1438 AIAA-2016-1439 ISS Double-Gimbaled CMG Motion Simulator 2-Axis Input Non-intrusive Flight Test A Review of Control Schemes for Modeling and Simulation of Modeling and Simulation Activities Adaptive Control of a Camera- Subsystem Design using the Agile Design for Angular Accelerometer Instrumentation using Video Hydraulic Stewart Platform Flight Hydraulic Hexapod Flight Simulator for Digital Sun Sensor Development Projection System using Vision- Development Method Calibration Recognition Simulator Motion Systems Motion Systems M. Celebi, F. Gulmammadov, TUBITAK, Based Feedback R. Inampudi, Lockheed Martin Corporation, D. Jatiningrum, C. de Visser, M. van J. Ricciardi, C. Minwalla, National Research Y. Huang, D. Pool, O. Stroosma, Q. Chu, Y. Huang, D. Pool, O. Stroosma, Q. Chu, Ankara, Turkey C. Liao, M. Bender, A. Kurdila, S. Houston, TX Paassen, M. Mulder, Delft University of Council Canada, Ottawa, Canada M. Mulder, Delft University of Technology, M. Mulder, Delft University of Technology, Southward, Virginia Polytechnic Institute Technology, Delft, The Netherlands Delft, The Netherlands Delft, The Netherlands and State University, Blacksburg, VA Wednesday, 6 January 2016 303-NDA-5 Non-Deterministic Methods Old Town B Chaired by: S. SANKARARAMAN, SGT Inc., NASA Ames Research Center and P. BERAN, US Air Force Research Laboratory 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs AIAA-2016-1440 AIAA-2016-1441 AIAA-2016-1442 AIAA-2016-1443 AIAA-2016-1444 AIAA-2016-1445 AIAA-2016-1446 Importance Sampling-based A New Approach for Probability of Multifidelity Uncertainty Compositional Uncertainty A Dynamic Data-Driven Approach A Corrector for Probability Dilution Stochastic Models for Fast Analysis Post-Processing Method for Global Failure Analysis with Distributed Propagation in Coupled Analysis via Importance Weighted to Optimal Offline Learning for in Satellite Conjunction Analysis of Unsteady Wing Aerodynamics Sensitivity Analysis Failure Region Multidisciplinary Systems Gibbs Sampling for Coupled Online Flight Capability Estimation M. Balch, Alexandria Validation Consulting, M. Fluck, C. Crawford, University of D. Sparkman, Universal Technology P. Wang, X. Cui, Wichita State University, A. Chaudhuri, K. Willcox, Massachusetts Multidisciplinary Systems B. Isaac, D. Allaire, Texas A&M University, LLC, Alexandria, VA Victoria, Victoria, Canada Corporation, Dayton, OH; H. Millwater, J. Wichita, KS Institute of Technology, Cambridge, MA S. Ghoreishi, D. Allaire, Texas A&M College Station, TX Garza, University of Texas, San Antonio, San University, College Station, TX Antonio, TX; B. Smarslok, Air Force Research Laboratory, Wright-Patterson AFB, OH Wednesday, 6 January 2016 304-PANEL-9 Wednesday Afternoon Forum 360 Seaport F-G 1400 - 1600 hrs Space Exploration Through Advancing Technologies Moderator: Steve Gaddis, Director, Game Changing Development Program, NASA

Panelists: Michelle Munk Molly Anderson Matthew Simon Principal Technologist for Entry, Descent, and Landing Principal Technologist for Next Gen Life Support Habitat Design Lead for the Human Spaceflight Architecture Team NASA NASA NASA Wednesday, 6 January 2016 305-PC-12 Spray and Droplet Combustion I Harbor B Chaired by: M. SOTERIOU, United Technologies Research Center and J. GORE, Purdue University 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs AIAA-2016-1447 AIAA-2016-1448 AIAA-2016-1449 AIAA-2016-1450 AIAA-2016-1451 AIAA-2016-1452 AIAA-2016-1453 Investigation of Reduced Toxicity Impingement and splashing of LES based evaluation of multi- High Fidelity Simulation of Liquid High Heat Flux Surface Coke Hollow-Cone Spray Modeling for Design Procedure of a Movable Hypergolic Fuels – Renewed Efforts droplets on spherical targets component fuel evaporation effects Jet in Crossflow Under Dynamic Deposition and Removal Outwardly Opening Piezoelectric Pintle Injector for Liquid Rocket in the Department of the Navy G. Charalampous, Y. Hardalupas, Imperial at aero-engine conditions Excitation Assessment Injector Engines J. Dennis, J. Clubb, Naval Air Warfare College London, London, United Kingdom V. Sankaran, J. Lee, H. Gao, M. Soteriou, X. Li, M. Soteriou, United Technologies D. Wickham, J. Engel, B. Hitch, A. J. Sim, King Abdullah University of Science M. Son, K. Yu, K. Radhakrishnan, J. Koo, Center, China Lake, CA United Technologies Corporation, East Corporation, East Hartford, CT Wickham, Reaction Systems, Inc., and Technology, Thuwal, Saudi Arabia; J. Korea Aerospace University, Goyang, Hartford, CT Golden, CO Badra, Saudi Aramco, Dhahran, Saudi Arabia; South Korea H. Im, King Abdullah University of Science and Technology, Thuwal, Saudi Arabia Wednesday, 6 January 2016 306-PC-13 Turbulent Combustion I - Experiments Harbor C Chaired by: T. LIEUWEN, Georgia Institute of Technology and B. RANKIN, Air Force Research Laboratory 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs AIAA-2016-1454 AIAA-2016-1455 AIAA-2016-1456 AIAA-2016-1457 AIAA-2016-1686 Experimental Assessment of the Characterization of Aerodynamically Comparison of Three Interacting Experimental studies of freely The Mixture Fraction for High- Turbulent Premixed Combustion Stabilized Flames Using Simultaneous V-Flames to a Single Bluff-Body propagating turbulent premixed Pressure Turbulent Reactive Flows Regime Diagram Boundaries Analysis of Planar and Line-of-Sight Flame at Two Reynolds Numbers kernels in low speed channel flow J. Bellan, Jet Propulsion Laboratory, A. Skiba, T. Wabel, J. Temme, J. Driscoll, Images W. Culler, A. Tyagi, Pennsylvania State D. Fries, B. Ochs, S. Menon, Georgia California Institute of Technology, University of Michigan, Ann Arbor, Ann I. Chterev, B. Emerson, T. Lieuwen, Georgia University, University Park, PA; P. Institute of Technology, Atlanta, GA Pasadena, CA Arbor, MI Institute of Technology, Atlanta, GA Venkateswaran, Trinity College, Hartford,

CT; J. O`Connor, Pennsylvania State University, University Park, PA Wednesday, 6 January 2016 307-PDL-9/FD-40 Experimental and Numerical Studies of Large Eddy Structures Ocean Beach Chaired by: N. BISEK, Air Force Reseach Laboratory 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs AIAA-2016-1458 AIAA-2016-1459 AIAA-2016-1460 AIAA-2016-1461 AIAA-2016-1462 Investigations of Transonic Flow Studies of Flow Topology around Optical investigation of large-scale LES of an Aero-Optical Turret Flow Predictions of Aero-Optical over a Hemisphere using DES Hemisphere at Transonic Speeds Using boundary-layer structures at High Reynolds Number Distortions Using LES with Wall and hybrid RANS/LES Turbulence Time-Resolved Oil Flow Visualization M. Kemnetz, S. Gordeyev, University of E. Mathews, K. Wang, M. Wang, E. Modeling Models S. Gordeyev, A. Vorobiev, E. Jumper, University Notre Dame, Notre Dame, IN Jumper, University of Notre Dame, Notre M. Kamel, K. Wang, M. Wang, University C. Tam, T. Madden, Air Force Research of Notre Dame, Notre Dame, IN; S. Gogineni, Dame, IN of Notre Dame, Notre Dame, IN Laboratory, Kirtland AFB, NM; B. Thurow, Spectral Energies, LLC, Dayton, OH; D. Auburn University, Auburn, AL Wittich, Air Force Research Laboratory, Kirtland AFB, NM Wednesday, 6 January 2016 308-SATS-3 Small Satellites - Missions Hillcrest D Chaired by: J. STRAUB, University of North Dakota 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2016-1463 AIAA-2016-1464 AIAA-2016-1465 AIAA-2016-1466 AIAA-2016-1467 AIAA-2016-1468 The CUSPED Mission: CUbeSat for Simulation-to-Flight 1 (STF-1): A Autonomous Rendezvous and MarsCAT: Mars Array of ionospheric SRMSAT: A Feasibility Study on Dynamics of Chip-scale Spacecraft GNSS Sounding of the Ionosphere- Mission to Enable CubeSat Software- Docking of Two 3U Cubesats Research Satellites using the Small Satellite Mission to Moon Swarms near Irregular Bodies Plasmasphere Electron Density based Verification and Validation Using a Novel Permanent-Magnet CubeSat Ambipolar Thruster A. Ratheesh, K. Barad, K. Naik, S. L. Weis, M. Peck, Cornell University, J. Gross, A. Keesee, J. Christian, Y. J. Morris, S. Zemerick, M. Grubb, J. Lucas, Docking Mechanism E. Bering, L. Pinsky, L. Li, D. Jackson, J. Pavuluri, A. Singha, H. Bhate, SRM Ithaca, NY Gu, E. Scime, West Virginia University, NASA Goddard Space Flight Center, Greenbelt, J. Pei, L. Murchison, V. Stewart, J. Chen, , Houston, TX; University, Chennai, India; et al. Morgantown, WV; A. Komjathy, Jet MD; M. Jaridi, J. Gross, West Virginia Rosenthal, D. Sellers, M. Banchy, NASA H. Reed, Texas A&M University, College Propulsion Laboratory, California Institute University, Morgantown, WV; et al. Langley Research Center, Hampton, VA; Station, TX; et al. of Technology, Pasadena, CA; et al. et al. Wednesday, 6 January 2016 309-SCS-4 Spacecraft Membranes, Booms, and Trusses II Balboa B Chaired by: O. SOYKASAP, Afyon Kocatepe University and H. SAKAMOTO, Tokyo Institute of Technology 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs AIAA-2016-1469 AIAA-2016-1470 AIAA-2016-1471 AIAA-2016-1472 AIAA-2016-1473 AIAA-2016-1474 AIAA-2016-1475 Thermal deformation of very slender An Analysis of a Coiled Tape Spring Stepwise Deployments of Membrane Natural Frequency Optimization Development of Stereo Camera Effects of Damage on Long Term Non-Axisymmetric Inflatable Pressure TRAC booms during Extension and Compression Structure with Rolled-up Braided CFRP and Stability Analysis of Bistable System for Accurate Observation Displacement Data of Woven Fabric Structure (NAIPS) Concept that O. Stohlman, NASA Langley Research Center, A. Hoskin, A. Viquerat, University of Bi-Convex Booms Carbon Fiber Reinforced Plastic of Large Deployable Membranes Webbings under Constant Load for Enables Mass Efficient Packageable Hampton, VA; E. Loper, NASA Marshall Space Surrey, Guildford, United Kingdom N. Okuizumi, Japan Aerospace Exploration Booms for Space Applications in Orbit Inflatable Structures Pressure Vessels with Openings Flight Center, Huntsville, AL Agency (JAXA), Sagamihara, Japan; H. Ikuta, C. Wu, A. Viquerat, G. Aglietti, University Y. Shimoda, K. Watanabe, N. Sakamoto, W. Kenner, NASA Langley Research Center, W. Doggett, T. Jones, J. Watson, J. Warren, S. Hakata, Waseda University, Shinjuku, of Surrey, Surrey, United Kingdom T. Kuratomi, Y. Naito, WEL Research Hampton, VA NASA Langley Research Center, Hampton,

Japan; M. Natori, Japan Aerospace Exploration Company, Ltd., Ichihara, Japan; H. VA; A. Makino, NASA Ames Research Center, Agency (JAXA), Sagamihara, Japan; A. Sakamoto, Tokyo Institute of Technology, Moffett Field, CA; M. Selig, NASA Johnson Watanabe, Sakase Adtech Company, Ltd., Ookayama, Japan; et al. Space Center, Houston, TX; et al. Sakai, Japan; H. Yamakawa, Waseda University, Shinjuku, Japan Wednesday, 6 January 2016 310-SD-8 Passive Control and Damping Balboa C Chaired by: R. MALLA, University of Connecticut and H. KIM, Boeing Defense, Space & Security 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs AIAA-2016-1476 AIAA-2016-1477 AIAA-2016-1478 AIAA-2016-1479 AIAA-2016-1480 AIAA-2016-1481 AIAA-2016-1482 Damping of Sandwich Panels via Finite Element Modeling of Design of Three Parameter Isolator Finite Element Modeling of Fluidic Cellular Lattices with an Internal Structural dynamics analysis and Interfacial Micromechanics and Acoustic Metamaterials Longitudinal Metastructures for for the RWA Disturbance Considering Flexible Matrix Composite (F2MC) Topology for High Stiffness and passive control of wind turbine Load Transfer of Off-Aligned T. Yu, G. Lesieutre, Pennsylvania State Passive Vibration Suppression Flexible Structural Effects Treatments for Bending and Damping vibrations with Tuned Mass Damper Nanocomposites University, University Park, PA K. Reichl, D. Inman, University of G. Park, Korea Advanced Institute of Science Torsional Vibration Control M. DiPalma, F. Gandhi, Rensselaer (TMD) technique R. Kopp, Pennsylvania State University, Michigan, Ann Arbor, Ann Arbor, MI and Technology, Daejeon, South Korea ; M. Krott, K. Miura, C. Rahn, E. Smith, Polytechnic Institute, Troy, NY T. Farsadi, A. Kayran, Middle East University Park, PA; B. Glaz, J. Riddick, Army D. Lee, Agency for Defense Development, Pennsylvania State University, University Technical University, Ankara, Turkey Research Laboratory, Aberdeen Proving Daejeon, South Korea ; J. Han, Korea Park, PA Ground, MD; E. Smith, Pennsylvania State Advanced Institute of Science and Technology, University, University Park, PA Daejeon, South Korea Wednesday, 6 January 2016 311-SD-9 Gust Loads, Response, and Control Gaslamp A Chaired by: D. RAVEH and I. YUNIS, NASA-Langley Research Center 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs AIAA-2016-1483 AIAA-2016-1484 AIAA-2016-1485 AIAA-2016-1486 AIAA-2016-1487 AIAA-2016-1488 AIAA-2016-1489 Probabilistic Gust Loads Analysis Gust Reconstruction from Flight Reduced Order Gust Response Aeroservoelastic Response of Adaptive Finite Element in Time Derived Gust Velocities Extracted Examination of Methods to Accounting for Aeroservoelastic Data Recording via Numerical Simulation using Computational Nonlinear Wind Tunnel Model to Method for Rotorcraft Analysis from Flight Data for Various Separate Gust and Maneuver Load System Uncertainty Optimisation Fluid Dynamics Non-Uniform Gust Field Using Element Size Control Aircraft Factors S. Wu, E. Livne, University of Washington, S. Simeone, C. Agostinelli, T. Rendall, P. Bekemeyer, S. Timme, University of R. Veiberman, M. Weiss, M. Karpel, Technion- S. Kwon, I. Chopra, S. Lee, University of K. Rokhsaz, L. Kliment, Wichita State L. Kliment, K. Rokhsaz, Wichita State Seattle, Seattle, WA University of Bristol, Bristol, United Liverpool, Liverpool, United Kingdom -Israel Institute of Technology, Haifa, Israel; Maryland, College Park, College Park, MD University, Wichita, KS University, Wichita, KS Kingdom; A. Rampurawala, Airbus, F. Fonte, L. Travaglini, S. Ricci, Technical Toulouse, France University of Milan, Milan, Italy Wednesday, 6 January 2016 312-SEN-2 Novel Sensor Systems and Sensing Techniques II Regatta C Chaired by: G. FASANO, University of Naples and D. FAULK, Lockheed Martin Aeronautics 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2016-1490 AIAA-2016-1491 AIAA-2016-1492 AIAA-2016-1493 AIAA-2016-1494 AIAA-2016-1495 Psychophysiological Sensing and Vision-aided Cooperative Multi-band Sensor for Exoplanet Multiple-Target Tracking Networked Cooperative Swarm RF Network Localization Method State Classification for Attention Navigation for UAV Swarms Detection to be Installed Onboard Framework for Aircraft in Airport System for Area Denial Operations for Unmanned Robotics Systems Management in Commercial A. Vetrella, G. Fasano, D. Accardo, Cubesat Ramp Area M. Anderson, J. Rios, D. Stone, J. Cuany, S. Kahnemouyi, A. Pourshafiee, N. Aviation University of Naples “Federico II”, Naples, I. Marcella, G. Rufino, D. Accardo, University V. Vaddi, P. Dutta, H. Lu, J. Tsai, Optimal C. Rasmussen, L. Hale, U.S. Air Force Cramer, H. Kassamnath, K. Obraczka, M. A. Harrivel, C. Liles, C. Stephens, K. Italy of Naples “Federico II”, Naples, Italy; E. Oliva, Synthesis, Inc., Los Altos, CA Academy, Colorado Springs, CO Teodorescu, University of California, Santa Ellis, L. Prinzel, A. Pope, NASA Langley A. Tozzi, National Institute for Astrophysics, Cruz, Santa Cruz, CA Research Center, Hampton, VA Florence, Italy Wednesday, 6 January 2016 313-SOF-6/UMS-7/IS-8 Assurance of Autonomy Symposium II Coronado A 1400 - 1730 hrs Methods for Enabling Autonomy

In this session, we discuss current and upcoming techniques that are driving autonomous system development in aviation and the need for new assurance techniques in order to enable greater assured functionality for autonomous systems. Topics that will be addressed include the design, manufacture, fielding, maintenance and retirement of autonomous systems, including relevant elements such as COA/Certification and regulatory approval. Architectures for autonomy will also be discussed.

We begin the session with subject matter expert talks, addressing the issues inherent in designing and fielding multiple types of autonomous platforms with differing mission capabilities and assurance levels. We will then form moderated breakout groups organized by tools, techniques, capabilities and barriers.

1400 - 1500 hrs Speakers John Valasek Eric Johnson Director of the Center for Autonomous Vehicles and Sensor Systems Lockheed Martin Associate Professor of Avionics Integration Texas A&M University Georgia Institute of Technology 1515 - 1730 hrs Breakout Session We request that the audience help us in exhaustively exploring the capabilities uniquely enabled by autonomy in aviation systems, the current new hardware and mathematical and computational techniques that are enabling this autonomy, and the barriers to assurance. The results of the breakout will be used to generate a report regarding critical needs as well as competencies required to enable assured autonomy. We will also schedule Thursday lightning-fast talks for audience members who are inspired by the day’s proceedings. Wednesday, 6 January 2016 314-STR-10 Design, Test and Analysis of Composite Structures II La Jolla A Chaired by: J. MIN, NASA Glenn Research Center and O. ZHUPANSKA, The University of Iowa 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2016-1496 AIAA-2016-1497 AIAA-2016-1498 AIAA-2016-1499 AIAA-2016-1500 AIAA-2016-1501 Ultra-Flexible Advanced Stiffness Optimization of a Composite Lattice Imperfection Insensitivity Analyses Modeling the Bistability of Vibrational Analysis of Unitized Adhesive-Bonded Shape Memory Truss (U-FAST) for Large Solar Satellite Central Cylinder Structure of Advanced Composite Tow- Laminated Composite Toroidal Slit Curvilinearly Stiffened Composite Alloy Strip Joint for Composite Fan Arrays Using an Efficient Semi-automated Steered Shells Tubes Panels Subjected to In-plane Loads Blade Shape Changing Concept J. Mejia-Ariza, L.Garde, Inc., Tustin, Approach K. Wu, NASA Langley Research Center, G. Knott, A. Viquerat, University of Surrey, W. Zhao, R. Kapania, Virginia Polytechnic J. Min, T. Williams, NASA Glenn Research CA; T. Murphey, Opterus Research and L. Pavlov, B. Smeets, S. Simonian, I. Hampton, VA; B. Farrokh, NASA Goddard Guildford, United Kingdom Institute and State University, Blacksburg, VA Center, Cleveland, OH Development, Inc., Syracuse, NY te Kloeze, ATG Europe, Noordwijk, The Space Flight Center, Greenbelt, MD; B. Netherlands Stanford, NASA Langley Research Center, Hampton, VA; P. Weaver, University of Bristol, Bristol, United Kingdom Wednesday, 6 January 2016 315-STR-11 Structural Joints and Repairs La Jolla B Chaired by: S. TERMAATH, University of Tennessee and D. NORWOOD, Lockheed Martin Aeronautics 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2016-1502 AIAA-2016-1503 AIAA-2016-1504 AIAA-2016-1505 AIAA-2016-1506 AIAA-2016-1507 Analytical and Experimental Delamination Growth of Sensitivity Analysis of Composite Non-linear finite element analysis A Method for Predicting Fastener High Fidelity Bearing and Bypass Studies on Delamination Arrest Redundantly Joined Sandwich Patch Design Parameters under for progressive failure prediction of Hole Elongation in Composite Joints Response and Failure Prediction of in Bolted-Bonded Composite Composites Under Compression Low Velocity Impact Loading composite bolted joints due to Cyclic Loading Composite Bolted Joints Structures C. Phan, E. Lundgren, D. Patel, V. Goyal, Conditions M. Palwankar, A. Popescu, S. J. Bartley-Cho, D. Wang, B. Sheppard, T. N. Simon, E. Fang, J. Lua, Global L. Richard, K. Lin, University of The Aerospace Corporation, El Segundo, S. TerMaath, R. Timilsina, University of Venkataraman, San Diego State Palm, Northrop Grumman Corporation, Engineering and Materials, Inc., Princeton,

Washington, Seattle, Seattle, WA CA Tennessee, Knoxville, Knoxville, TN University, San Diego, CA Redondo Beach, CA; R. Holzwarth, M. NJ Wilkinson, Air Force Research Laboratory, Wright-Patterson AFB, OH Wednesday, 6 January 2016 316-SUR-2 Air and Space Survivability II Old Town A Chaired by: E. FAHRENTHOLD, University of Texas and J. RIMOLI, Georgia Institute of Technology 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs AIAA-2016-1508 AIAA-2016-1509 AIAA-2016-1510 AIAA-2016-1511 AIAA-2016-1512 Multiscale Simulation of Reacting Topology Optimization of a Dynamic Properties of Additively On tensegrity structural dynamics, Surface Roughness of Electron Shock Physics Penetrating Warhead Manufactured 15-5 Stainless reliability, and survivability Beam Melting Ti-6Al-4v Effect on E. Fahrenthold, S. Lee, J. Bass, University W. Graves, D. Liu, A. Palazotto, Air Force Steel and Three-Dimensional J. Rimoli, Georgia Institute of Technology, Ultrasonic Testing of Texas, Austin, Austin, TX Institute of Technology, Wright-Patterson Microstructure Characterization Atlanta, GA E. Hanks, D. Liu, A. Palazotto, Air Force AFB, OH A. Dempsey, D. Liu, A. Palazotto, Air Force Institute of Technology, Wright-Patterson Institute of Technology, Wright-Patterson AFB, OH AFB, OH; R. Abrahams, Air Force Research Laboratory, Wright-Patterson AFB, OH Wednesday, 6 January 2016 317-TP-8 Thermal Protection System, Ablation and Surface Catalysis II Harbor G Chaired by: E. STERN, University of Minnesota and M. HOWARD, Sandia National Laboratories 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2016-1513 AIAA-2016-1514 AIAA-2016-1515 AIAA-2016-1516 AIAA-2016-1517 AIAA-2016-1518 Thermogravimetric Analysis Thermal Ablation Modeling for Investigation of Performance Characterization of Candidate Predicting the Combined Optical and Thermal Testing of Ablators in of Flexible Thermal Protection Silicate Materials Envelope for Phenolic Impregnated Materials for Remote Recession Thermal Response of Polymer Matrix the NASA Johnson Space Center Systems for Thermal Response Y. Chen, NASA Ames Research Center, Carbon Ablator (PICA) Measurements of Ablative Heat Composites with Varying Composite Radiant Heat Test Facility Modeling Moffett Field, CA P. Agrawal, D. Prabhu, ERC Inc., Moffett Shield Materials Properties S. Del Papa, NASA Johnson Space G. Rossman, R. Braun, Georgia Institute of Field, CA; T. Squire, F. Milos, M. B. Butler, M. Winter, F. Panerai, A. T. Godar, University of Dayton Research Center, Houston, TX; J. Milhoan, Barrios Technology, Atlanta, GA Stackpoole, NASA Ames Research Center, Martin, S. Bailey, University of Kentucky, Institute, Dayton, OH; B. Volk , G. Ehlert, Air Technology, Houston, TX; B. Remark, Moffett Field, CA Lexington, Lexington, KY; M. Stackpoole, Force Research Laboratory, Wright-Patterson NASA Johnson Space Center, Houston, TX; NASA Ames Research Center, Moffett AFB, OH; W. Kennedy , Universal Technology L. Suess, Jacobs, Houston, TX Field, CA; et al. Corporation, Dayton, OH; G. Frank, University of Dayton Research Institute, Dayton, OH Wednesday, 6 January 2016 318-WE-7 Wind Energy: Wind Turbine Wakes Harbor I Chaired by: P. MORIARTY, National Renewable Energy Laboratory 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2016-1519 AIAA-2016-1520 AIAA-2016-1521 AIAA-2016-1522 AIAA-2016-1523 AIAA-2016-1524 Megawatt Wind Turbine Far Wake Wake Interaction Effects Using Scaled Aerodynamic Wind Turbine Wake flow characteristics at high Wind tunnel tests on controllable Field Demonstration of the Sandia and Performance Predictions Using a Parallelized Free Vortex Wake Design for Wake Similarity wind speed model wind turbines in yaw Wake Imaging System Capabilities the Unsteady Actuator Line Model Model C. Kelley, D. Maniaci, B. Resor, Sandia H. Madsen, T. Larsen, G. Larsen, K. J. Schottler, A. Hölling, J. Peinke, M. at the Scaled Wind Farm Technology M. Darbandi, A. Behrouzifar, R. Jalali, K. Shaler, K. Kecskemety, J. McNamara, National Laboratories, Albuquerque, NM Hansen, Technical University of Denmark, Hölling, ForWind Center for Wind Energy Facility

Sharif University of Technology, Tehran, Ohio State University, Columbus, OH Roskilde, Denmark Research, Oldenburg, Germany T. Herges, D. Bossert, R. Schmitt, M. Iran ; G. Schneider, University of Waterloo, Johnson, D. Maniaci, C. Glen, Sandia National Waterloo, Canada Laboratories, Albuquerque, NM; et al. Wednesday, 6 January 2016 319-NW-12 Wednesday Afternoon Networking Coffee Break Exposition Hall 1530 - 1600 hrs Wednesday, 6 January 2016 320-LEC-8 SDM Lecture Seaport F-G 1800 - 1900 hrs

Real Life Problems are Multi-Disciplinary Ivatury Raju Technical Fellow for Structures NASA Wednesday, 6 January 2016 321-FD-60 Transition Open Forum Old Town B 1830 - 2200 hrs Thursday Thursday, 7 January 2016 322-NW-13 Thursday Early Morning Networking Coffee Break Session Room Foyers 0700 - 0730 hrs Thursday, 7 January 2016 323-SB-4 Thursday Morning Speakers’ Briefing Session Rooms 0730 - 0800 hrs Thursday, 7 January 2016 324-PLNRY-4 Thursday Morning Plenary Panel Seaport A-E 0800 - 0900 hrs Aerospace Frontiers – Strengthening Collaboration, For Continued Progress Moderator: John Tracy, Chief Technology Officer and Senior Vice President, Engineering, Operations and Technology, The Boeing Company

Panelists: Sandy Magnus Jaiwon Shin Morteza Gharib Executive Director Associate Administrator, Aeronautics Research Mission Directorate Hans W. Liepman Professor of Aeronautics and Bioinspired EngineeringVice Provost AIAA NASA California Institute of Technology Steve Walker Darryll Pines Keoki Jackson Deputy Director Professor Chief Technology Officer DARPA University of Maryland Lockheed Martin Corporation

Thursday, 7 January 2016 325-ACD-8 Unmanned Aerial Vehicle Design Cortez Hill A Chaired by: G. CROUSE, Sierra Nevada Corporation and M. LOGAN, NASA Langley Research Center 0900 hrs 0930 hrs 1000 hrs 1030 hrs AIAA-2016-1525 AIAA-2016-1526 AIAA-2016-1527 AIAA-2016-1528 Design of a Recharge Station for Design and Performance of a A Novel Sea Launch and Recovery Propulsion System Selection and UAVs using Non-Contact Wireless Flexible Aircraft Manufacturing Concept for fixed wing UAVs Modeling for a Quadrotor with Power Transfer Platform N. Sarigul-Klijn, M. Sarigulklijn, University Search and Rescue Mission C. Bil, M. Simic, V. Vojisavljevic, RMIT T. Tao, R. Hansman, Massachusetts of California, Davis, Davis, CA O. Tekinalp, A. Kutay, D. Kaya, D. University, Melbourne, Australia Institute of Technology, Cambridge, MA Kurtulus, Middle East Technical University, Ankara, Turkey; I. Simsek, S. Soysal, GATE Electronics, Ankara, Turkey; et al. Thursday, 7 January 2016 326-ACD-9 Conceptual Aircraft Design Working Group 21, CADWG Hillcrest D 0900 - 1200 hrs Thursday, 7 January 2016 327-AFM-10 Small/Mini/Micro Aerial Vehicles Hillcrest B Chaired by: K. CUNNINGHAM, NASA Langley Research Center and B. JOLLY, US Air Force 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2016-1529 AIAA-2016-1530 AIAA-2016-1531 AIAA-2016-1532 AIAA-2016-1533 A Time-Scale Separation Experimental characterization of a Gust Detection and Mitigation on a Automatic Path Generation for Flow interaction between dissimilar Approach for Time-Varying Model small and micro unmanned aerial Quad Rotor Biplane Multirotor Descents Through Varying UAVs in rendezvous conditions Identification of a Flapping-Wing vehicle propulsion systems D. Yeo, V. Hrishikeshavan, I. Chopra, Air Masses above Ascension Island X. Bovier-Lapierre, V. Jouffroy, Institut Micro Aerial Vehicle R. Fabela, C. Santana, A. Naranjo, L. University of Maryland, College Park, C. Greatwood, T. Richardson, J. Freer, Polytechnique des Sciences Avancées, S. Armanini, C. de Visser, G. de Croon, Amezquita-Brooks, E. Liceaga-Castro, M. College Park, MD University of Bristol, Bristol, United Kingdom; Ivry-sur-Seine, France; T. Richer, Institut M. Mulder, Delft University of Technology, Torres-Reyna, Autonomous University of R. Thomas, University of Birmingham, Polytechnique des Sciences Avancées, Delft, The Netherlands Nuevo León, Monterrey, Mexico Birmingham, United Kingdom; E. Nisbet, Royal Brest, France; O. Ariff, University of Holloway, London, United Kingdom Salford, Salford, United Kingdom Thursday, 7 January 2016 328-AFM-11 Aerodynamic Prediction Methods, Aircraft Flight Dynamics, Handling Qualities, and Performance Harbor A Chaired by: A. DA RONCH, University of Southampton and T. LAVIN, Sandia National Laboratories 0900 hrs 0930 hrs 1000 hrs 1030 hrs AIAA-2016-1534 AIAA-2016-1535 AIAA-2016-1536 AIAA-2016-1537 Aircraft Parameter Estimation Determination of Water Droplet CFD Calculation of Stability and Release Point Determination and Using Optimal Control Methods Collection Efficiency: An Empirical Control Derivatives For Ram-Air Dispersion Reduction for Ballistic C. Göttlicher, M. Gnoth, M. Bittner, F. Approach Parachutes Airdrops Holzapfel, Technical University of Munich, M. Ali, Georgia Institute of Technology, M. Ghoreyshi, U.S. Air Force Academy, J. Vandermey, D. Doman, A. Gerlach, Munich, Germany Atlanta, GA; Q. Ejaz Ur Rehman, S. Colorado Springs, CO; K. Bergeron, Army Air Force Research Laboratory, Wright- Chaudhry, Institute of Space Technology, Research, Development and Engineering Patterson AFB, OH

Islamabad, Pakistan Command, Natick, MA; A. Lofthouse, R. Cummings, U.S. Air Force Academy, Colorado Springs, CO Thursday, 7 January 2016 329-AMT-7 Error Sources and Calibration of Instruments Harbor D Chaired by: G. JONES, NASA-Langley Research Center and P. BARDET, George Washington University 0900 hrs 0930 hrs 1000 hrs 1030 hrs AIAA-2016-1538 AIAA-2016-1539 AIAA-2016-1540 AIAA-2016-1541 A New Load Residual Threshold Optimal Filtering of Hotwire Aerodynamic Parameter Prediction A Development of Dynamic Wind Definition for the Evaluation of Anemometry Data Using Multi- on a Airfoil with Flap via Artificial Tunnel Testing Technique by Using Wind Tunnel Strain-Gage Balance Level Wavelet Decomposition Hair Sensors and Feedforward a Magnetic Suspension and Balance Data I. Choutapalli , University of Texas, Rio Neural Network System N. Ulbrich, T. Volden, Jacobs, Moffett Grande Valley, Edinburg, TX; T. Reynolds, K. Thapa Magar, Wright State Research R. Oshima, H. Sawada, S. Obayashi, Field, CA R. Guyton, C. Tilmann, Air Force Research Institute, Beavercreek, OH; G. Reich, M. Tohoku University, Sendai, Japan Laboratory, Wright-Patterson AFB, OH Rickey, B. Smyers, Air Force Research Laboratory, Wright-Patterson AFB, OH; R. Beblo, University of Dayton Research Institute, Dayton, OH Thursday, 7 January 2016 330-APA-32 Special Session: Aerodynamic Design Optimization Benchmark Problems II Coronado D Chaired by: J. HICKEN, Rensselaer Polytechnic Institute and T. RENDALL, University of Bristol 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2016-1542 AIAA-2016-1543 Oral Presentation AIAA-2016-1544 AIAA-2016-1545 Oral Presentation Aerodynamic Design Optimization Application of Multifidelity Application of OPTIMENGA A Global and Gradient Based Impact of Shape Parameterisation Multi-round Surrogate-based NASA Common Research Model Benchmark Problems (Discussion) Optimization Techniques to Software to Multi-point Multi- Optimization Study of the AIAA on Aerodynamic Optimisation of Optimization for Benchmark redesign using adjoint-based methods 1Hour Discussion Benchmark Aerodynamic Design constrained Aerodynamic Design Aerodynamic Design Optimization Benchmark Problem Aerodynamic Design Problems on unstructured meshes Problems B. Epstein, Academic College of Tel Discussion Group Test Cases 4 and 5 D. Masters, D. Poole, University of Bristol, Y. Zhang, Z. Han, L. Shi, W. Song, F. Palacios, J. Vassberg, The Boeing Company, J. Ren, A. Thelen, A. Amrit, X. Du, L. Aviv-Yaffo, Tel Aviv, Israel; S. Peigin, S. LeDoux, D. Young, R. Melvin, W. Huffman, Bristol, United Kingdom; N. Taylor, MBDA, Northwestern Polytechnical University, Long Beach, CA; T. Economon, J. Alonso, Leifsson, Iowa State University, Ames, OPTIMENGA-777, Moscow, Russia J. Elliott, B. Basom, The Boeing Company, Bristol, United Kingdom; T. Rendall, C. Xi’an, China Stanford University, Stanford, CA; T. Albring, N. IA; Y. Tesfahunegn, Reykjavik University, Seattle, WA; et al. Allen, University of Bristol, Bristol, United Gauger, Technical University of Kaiserslautern, Reykjavik, Iceland; et al. Kingdom Kaiserslautern, Germany Thursday, 7 January 2016 331-APA-33 Applied CFD & Numerical Correlations with Experimental Data III Americas Cup D Chaired by: C. KIRIS, NASA Ames Research Center and S. MASSEY, NASA-Langley Research Center 0900 hrs 0930 hrs 1000 hrs 1030 hrs AIAA-2016-1546 AIAA-2016-1547 AIAA-2016-1548 AIAA-2016-1549 CFD Validation of Interaction of Fin prediction of iced airfoil Simulation of a Hammerhead Effects of Different Geometries of Trailing Vortex with Downstream aerodynamic characteristics Payload Fairing in the Transonic leading edge on Boundary Layer Control Surface in High Subsonic M. Costes, F. Moens, ONERA, Meudon, Regime Transition Flow France; V. Brunet, Group, Magny S. Murman, L. Diosady, NASA Ames D. Bhatia, Kingston University, London, United J. DeSpirito, Army Research Laboratory, les Hameaux, France Research Center, Moffett Field, CA Kingdom; G. Yang, J. Sun, Northwestern Aberdeen Proving Ground, MD Polytechnical University, Xi’an, China; J.

Wang, P. Barrington, Kingston University, London, United Kingdom; H. Li, Northwestern Polytechnical University, Xi’an, China Thursday, 7 January 2016 332-APA-34 Aerodynamic-Structural Dynamics Interactions I Americas Cup B Chaired by: C. PASILIAO, AFRL/RWWV and A. VANDERWYST, Leidos 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2016-1550 AIAA-2016-1551 AIAA-2016-1552 AIAA-2016-1553 AIAA-2016-1554 AIAA-2016-1555 Methodology Development for Numerical Study of Benchmark Initial Investigations of Supercritical Wind Tunnel Experiments with Spanwise Variation of Stall Flutter Multi-Objective Aerodynamic- Coupled Aeroelastic Analysis of Super-Critical Wing, BSCW, at Airfoil Dynamic Response due to Flexible Plates in Transonic Flows on a Flexible NACA 0018 Finite Structural Optimization of Wing Flutter Flutter Condition Transonic Buffet E. Jinks, P. Bruce, M. Santer, Imperial SpanWing Supercritical Wing of Wide Body W. Yuan, National Research Council A. Jirasek, M. Dalenbring, Swedish R. Carrese, P. Marzocca, RMIT University, College London, London, United Kingdom E. Culler, J. Farnsworth, University of Aircraft Canada, Ottawa, Canada; D. Poirel, Royal Defense Research Agency (FOI), Bundoora, Australia; O. Levinski, Australian Colorado, Boulder, Boulder, CO; C. Fagley, Z. Tong, Y. Zhang, H. Chen, Tsinghua Military College of Canada, Kingston, Stockholm, Sweden; J. Navratil, Brno National University, Melbourne, Australia; T. McLaughlin, U.S. Air Force Academy, University, Beijing, China Canada University of Technology, Brno, Czech N. Joseph, Leading Engineering Application Colorado Springs, CO Republic Providers, Clayton, Australia Thursday, 7 January 2016 333-APA-35/FD-41 Special Session: NASA’s Revolutionary Computational Aerosciences II Coronado E Chaired by: M. MALIK, NASA-Langley Research Center and J. DEBONIS, NASA Glenn Research Center 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2016-1556 AIAA-2016-1557 AIAA-2016-1558 AIAA-2016-1559 AIAA-2016-1560 AIAA-2016-1561 Informing Turbulence Closures With The NASA Juncture Flow Comparison of Experimental Surface Model-Invariant Hybrid Wall-modeled LES in Unstructured Comparison of Turbulent Thermal Computational and Experimental Experiment: Goals, Progress, and and Flow Field Measurements to Computations of Separated Flows Grids: Application to the NASA Diffusivity and Scalar Variance Data. Preliminary Testing (Invited) Computational Results of the Juncture for RCA Standard Test Cases Wall-mounted Hump Models K. Duraisamy, University of Michigan, Ann C. Rumsey, D. Neuhart, M. Kegerise, NASA Flow Model (JFM) (Invited) G. Park, Stanford University, Stanford, CA D. Yoder, NASA Glenn Research Center, Arbor, Ann Arbor, MI Langley Research Center, Hampton, VA N. Roozeboom, NASA Ames Research Center, S. Woodruff, NASA Langley Research Cleveland, OH Moffett Field, CA; H. Lee, Science and Center, Hampton, VA Technology Corporation, Moffett Field, CA; G. Zilliac, T. Pulliam, NASA Ames Research Center, Moffett Field, CA; J. Burces, San Jose State University, San Jose, CA Thursday, 7 January 2016 334-APA-36 Airfoil/Wing/Configuration Aerodynamics I Americas Cup C Chaired by: C. ROSEMA, US Army AMRDEC and K. WAITHE, Gulfstream Aerospace Corporation 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2016-1562 AIAA-2016-1563 AIAA-2016-1564 AIAA-2016-1565 AIAA-2016-1566 Rigid Ram-Air Parachute Experimental investigation of Rediscovering the “Peakey Leading Measurements of a Symmetric Evaluating an Experimental Experiments with Vents aerodynamic performance of Edge”: A Study of the Transonic Wing Morphed by Macro Fiber Streamlined Fairing for a J. Seidel, C. Latscha, G. Venkataraman, airfoils fitted with morphing Properties of Classic Airfoils Composite Actuators Diverterless Supersonic Inlet (DSI) U.S. Air Force Academy, Colorado trailing edges M. Merrell, T. Takahashi, Arizona State M. Debiasi, W. Chan, National University Equipped Aircraft

Springs, CO; K. Bergeron, Army Research, Q. Ai, H. Kamliya Jawahar, M. University, Tempe, AZ of Singapore, Singapore, Singapore; S. J. Masud, O. Khan, Air University, Development and Engineering Command, Azarpeyvand, University of Bristol, Bristol, Jadhav, Birla Institute of Technology & Islamabad, Pakistan Natick, MA; T. McLaughlin, U.S. Air Force United Kingdom Science, Pilani, Goa, India Academy, Colorado Springs, CO Thursday, 7 January 2016 335-ASC-5 Shape Memory Alloys Gaslamp D Chaired by: T. TURNER, NASA-Langley Research Center and E. WHITE, Boeing Engineering Operations & Technology 0900 hrs 0930 hrs 1000 hrs 1030 hrs AIAA-2016-1567 AIAA-2016-1568 AIAA-2016-1569 AIAA-2016-1570 Increased Volume Change in a Shape Experimental Characterization Additive Topological Optimization Synergistic Smart Morphing Memory Alloy Buoyancy Heat Engine of a Shape Memory Alloy-Based of Muscular-Skeletal Structures via AIleron: Capabilites Identification using Auxetic Lattice Cylinders Morphing Radiator Genetic L-System Programming A. Pankonien, L. Gamble, C. Faria, D. A. Angilella, F. Gandhi, Rensselaer Polytechnic C. Bertagne, J. Chong, D. Hartl, J. D. Hartl, G. Reich, P. Beran, Air Force Inman, University of Michigan, Ann Arbor, Institute, Troy, NY; T. Miller, Pennsylvania State Whitcomb, Texas A&M University, College Research Laboratory, Wright-Patterson Ann Arbor, MI University, University Park, PA Station, TX; L. Erickson, R. Sheth, NASA AFB, OH Johnson Space Center, Houston, TX Thursday, 7 January 2016 336-DSC-4 Aircraft Loads Prediction - Special Session Gaslamp C Chaired by: J. COOPER, University of Bristol and K. GRIFFIN, Southwest Research Institute 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2016-1571 AIAA-2016-1572 AIAA-2016-1573 AIAA-2016-1574 AIAA-2016-1575 AIAA-2016-1576 Aircraft Loads Prediction using Bifurcation Analysis of a Nose Nonlinear Static Aeroelasticity of Nonlinear Negative Stiffness Wing- Doublet-Lattice Method Correction Frequency Domain Approach for Enhanced Simulation (ALPES) Landing Gear System High Aspect Ratio Wing Aircraft by Tip Spring Device for Gust Loads by Means of Linearised Frequency Transonic Aerodynamic Modelling J. Cooper, A. Gaitonde, D. Jones, M. I. Tartaruga, M. Lowenberg, J. Cooper, P. FEM and Multibody methods Alleviation Domain Solver Analysis A. Poncet-Montanges, J. Cooper, D. Jones, Lowenberg, P. Sartor, University of Bristol, Sartor, University of Bristol, Bristol, United M. Castellani, J. Cooper, University A. Castrichini, J. Cooper, University of Bristol, C. Valente, D. Jones, A. Gaitonde, J. A. Gaitonde, University of Bristol, Bristol, Bristol, United Kingdom; Y. Lemmens, Kingdom; Y. Lemmens, Siemens, Leuven, of Bristol, Bristol, United Kingdom; Y. Bristol, United Kingdom; T. Wilson, Airbus, Cooper, University of Bristol, Bristol, United Kingdom; Y. Lemmens, Siemens, Siemens, Leuven, Belgium Belgium Lemmens, Siemens, Leuven, Belgium Bristol, United Kingdom; A. Carrella, Y. United Kingdom; Y. Lemmens, Siemens, Leuven, Belgium Lemmens, Siemens, Leuven, Belgium Leuven, Belgium Thursday, 7 January 2016 337-EDU-1 Advancing Aerospace Education I Bankers Hill Chaired by: K. RAVINDRA, Parks College of Engineering, Aviation & Technology 0900 hrs 0930 hrs 1000 hrs 1030 hrs AIAA-2016-1577 AIAA-2016-1578 AIAA-2016-1579 AIAA-2016-1580 Model Rocket Projects for Model Rocket Projects for Case Study of Two Capstone Student Brazilian Space-Tech Vocational Aerospace Engineering Course: Aerospace Engineering Course: Projects from Canada and the United Center Simulation of Flight Trajectories Propellant Analyses Kingdom E. Gonçalves, C. Veras, Brazilian Space T. Campbell, S. Seufert, R. Reis, J. J. Brewer, R. Reis, R. Limberger Tomiozzo, C. Ferlisi, C. Mazzini, E. Laurendeau, Defense Agency (AEB), Brasilia, Brazil Brewer, R. Limberger Tomiozzo, C. M. Okutsu, Catholic University of America, Research and Development Canada, Montréal, Whelan, Catholic University of America, Washington, D.C. Canada; D. Ramasawmy, A. Da Ronch, Washington, D.C.; et al. O. Stalnov, University of Southampton,

Southampton, United Kingdom Thursday, 7 January 2016 338-FD-42 CFD: Meshfree Methods and Non-Equilibrium Gas Dynamics Pier Chaired by: A. KATZ 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2016-1581 AIAA-2016-1582 AIAA-2016-1583 AIAA-2016-1584 AIAA-2016-1585 Development and Validation of a Assessment of a Two-Equation Simulation of Moving Bodies Using Asymptotic Geometry Finite Element Modeling of Non- Multi-Strand Solver for Complex Turbulence Model in the High-Order a Meshfree Method Representation for Complex equilibrium Gasdynamics Beyond Aerodynamic Flows Flux Correction Scheme Z. Duan, Z. Wang, University of Kansas, Configurations the Continuum Regime V. Lakshminarayan, Science and Technology O. Tong, C. Blakely, A. Katz, Utah State Lawrence, Lawrence, KS; L. Duncil, B. O. Tong, Y. Yanagita, A. Katz, Utah State M. Dumas, S. Gao, W. Habashi, M. Corporation, Moffett Field, CA; J. Sitaraman, University, Logan, UT Vu, NASA Kennedy Space Center, Cape University, Logan, UT Fossati, McGill University, Montréal, Parallel Geometric Algorithms, LLC, Sunnyvale, Canaveral, FL Canada; G. Baruzzi, D. Isola, ANSYS, Inc., CA; B. Roget, Science and Technology Montréal, Canada; et al. Corporation, Moffett Field, CA; A. Wissink, Army Aviation and Missile Research Development and Engineering Center, Moffett Field, CA Thursday, 7 January 2016 339-FD-43 Experimental Investigations of High-Speed Flow Harbor F Chaired by: M. BORG, Air Force Research Laboratory and K. CASPER, Sandia National Laboratories 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2016-1586 AIAA-2016-1587 AIAA-2016-1588 AIAA-2016-1589 AIAA-2016-1590 Optical Characterization of Nozzle- Krypton Tagging Velocimetry (KTV) Interactions of Shock Tube Exhaust Flow structure and unsteadiness in Turbulence characteristics of Wall Mach-6 Boundary Layers in Supersonic Turbulent Boundary Flows with Laminar and Turbulent the supersonic wake of a generic supersonic corner flows in a low S. Gordeyev, T. Juliano, University of Notre Layers Flames space launcher aspect ratio rectangular channel Dame, Notre Dame, IN D. Zahradka, N. Parziale, Stevens J. Chan, University of New South Wales, A. Schreyer, S. Stephan, R. Radespiel, R. Morajkar, M. Gamba, University of Institute of Technology, Hoboken, NJ; M. Sydney, Australia; P. Giannuzzi, New Mexico Technical University of Braunschweig, Michigan, Ann Arbor, Ann Arbor, MI Smith, E. Marineau, Arnold Engineering Institute of Mining and Technology, Socorro, Braunschweig, Germany Development Center, Silver Spring, MD NM; K. Kabir, Macquarie University, Sydney, Australia; M. Hargather, New Mexico Institute of Mining and Technology, Socorro, NM; G. Doig, California Polytechnic State University, San Luis Obispo, CA Thursday, 7 January 2016 340-FD-44 Multiphase Flow II: Liquid-gas and Engines Promenade B Chaired by: C. BOURASSA, GE Aviation and D. TROOLIN, TSI Incorporated 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2016-1591 AIAA-2016-1592 AIAA-2016-1593 AIAA-2016-1594 AIAA-2016-1595 AIAA-2016-1596 AIAA-2016-1597 Penetration Height of a Circular Exploration of Liquid Mass Three-dimensional liquid sheet Adaptive simulation of gas-liquid Active Damping of Fuel Slosh Using Influence of Scavenge Geometry Large Length-Scale Thermocapillary Liquid Jet in a Subsonic Gaseous Distribution for Liquid Jets in breakup: vorticity dynamics interfacial flows with surface a Hybrid Magneto-Active Propellant on Separation Efficiency for an Flow Experiment Design and Crossflow: An Eulerian-Lagrangian Subsonic Crossflows Using X-Ray A. Zandian, W. Sirignano, University of tension Management Device Inertial Particle Separator Feasibility Analysis for the ISS FIR

Approach Radiography California, Irvine, Irvine, CA; F. Hussain, A. Hay, S. Etienne, D. Pelletier, Defense L. Paul, B. Sivasubramanian, S. B. Connolly, E. Loth, University of Virginia, S. Alberts, S. Collicott, Purdue University, M. Broumand, M. Farokhi, M. Birouk, K. Lin, Taitech, Inc., Beavercreek, OH; Texas Tech University, Lubbock, TX Research and Development Canada, Putheenveed, S. Gangadharan, Embry- Charlottesville, Charlottesville, VA; P. West Lafayette, IN University of Manitoba, Winnipeg, Canada S. Peltier, C. Carter, J. Donbar, Air Force Montréal, Canada Riddle Aeronautical University, Daytona Snyder, C. Smith, Rolls-Royce Group plc, Research Laboratory, Wright-Patterson Beach, FL Indianapolis, IN AFB, OH; A. Kastengren, Argonne National Laboratory, Argonne, IL Thursday, 7 January 2016 341-FD-45 RANS/LES Methods and Techniques II Harbor E Chaired by: K. CASSEL, Illinois Institute of Technology 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2016-1598 AIAA-2016-1599 AIAA-2016-1600 AIAA-2016-1601 AIAA-2016-1602 A Modified One–Equation A Hybrid RANS-Implicit LES development of an elliptic- Improvements to SST turbulence Unified RANS-LES Simulations of Turbulence Model Based on Approach for the High-Order FR/ blending lag model for industrial model for free shear layers, Separated Flow at High Reynolds Turbulent Kinetic Energy Equation CPR Method applications turbulent separation and Number M. Rahman, Aalto School of Engineering, H. Zhu, S. Fu, Tsinghua University, Beijing, S. Lardeau, CD-adapco, London, United stagnation point anomaly R. Mokhtarpoor, S. Heinz, M. Stoellinger, Helsinki, Finland; R. Agarwal, Washington China; L. Shi, Z. Wang, University of Kingdom; F. Billard, Dassault Group, G. Kalitzin, G. Medic, G. Xia, United University of Wyoming, Laramie, Laramie, University in St. Louis, St. Louis, MO; T. Kansas, Lawrence, KS Saint-Cloud, France Technologies Corporation, East Hartford, CT WY Siikonen, Aalto School of Engineering, Helsinki, Finland Thursday, 7 January 2016 342-FD-46 Vortex Flows I Promenade A Chaired by: K. TAIRA, Florida State University and J. BUCHHOLZ, University of Iowa 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2016-1603 AIAA-2016-1604 AIAA-2016-1605 AIAA-2016-1606 AIAA-2016-1607 Characterization of Aircraft A Simple Model of Asymmetric Response of a Streamwise Vortex/ The Role of Vorticity Transport Vorticity Generation at Sharp Wake Vortex Circulation Decay in Wakes for Periodically Oscillating Wall Interaction to Unsteady in the Detachment of Unsteady Corners Reasonable Worst Case Conditions Airfoils Forcing Leading-Edge Vortices P. Zhang, K. Mohseni, University of Florida, I. De Visscher, Wake Prediction Technologies H. Xuzhao, I. Gursul, University of Bath, S. Benton, J. Bons, Ohio State University, J. Akkala, J. Buchholz, University of Iowa, Gainesville, Gainesville, FL (WaPT), Louvain-la-Neuve, Belgium; V. Bath, United Kingdom Columbus, OH Iowa City, IA Treve, EUROCONTROL, Brussels, Belgium; G. Winckelmans, Wake Prediction Technologies (WaPT), Louvain-la-Neuve, Belgium Thursday, 7 January 2016 343-GNC-28 Invited Session: Interval Management: Operational Concept, Integration, and Benefits Coronado B Chaired by: W. PENHALLEGON, The MITRE Corporation and B. BARMORE 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2016-1608 AIAA-2016-1609 AIAA-2016-1610 AIAA-2016-1611 AIAA-2016-1612 AIAA-2016-1613 AIAA-2016-1614 Interval Management: Concept of Operations for Interval Modeling Schedule and Mixed Leveraging Interval Management Results from a Field Evaluation of Interval Management Operations ASTAR Flight Test: Overview and Development and Implementation Management Arrivals and Terminal Operations on a Graph to Improve Air Traffic Operations Interval Management during an in the Terminal Airspace of Spacing Results of an Airborne Spacing Concept Approach Network during Departure Optimized Profile Descent Arrival Amsterdam Airport Schiphol. R. Roper, M. Koch, NASA Langley Research B. Barmore, NASA Langley Research D. Hicok, Regulus Group, Washington, I. Levitt, T. Steiner, Federal Aviation B. Lascara, C. Guensch, L. Weitz, MITRE and Approach N. De Gelder, National Aerospace Center, Hampton, VA Center, Hampton, VA; W. Penhallegon, D.C.; B. Barmore, NASA Langley Research Administration, Atlantic City, NJ Corporation, McLean, VA; P. Moertl, W. Penhallegon, R. Bone, H. Stassen, Laboratory (NLR), Amsterdam, The L. Weitz, R. Bone, MITRE Corporation, Center, Hampton, VA ASERS, Graz, Austria MITRE Corporation, McLean, VA Netherlands

McLean, VA; I. Levitt, Federal Aviation Administration, Atlantic City, NJ; J. Flores Kriegsfeld, Federal Aviation Administration, Washington, D.C.; et al. Thursday, 7 January 2016 344-GNC-29 Novel Navigation, Estimation and Tracking I Hillcrest A Chaired by: Y. CHENG, Mississippi State University and S. STARIN, NASA-Goddard Space Flight Center 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2016-1615 AIAA-2016-1616 AIAA-2016-1617 AIAA-2016-1618 AIAA-2016-1619 AIAA-2016-1620 Estimation of Gas Concentration from Wind Field Estimation From Airdrop Practical Observer Design for Real- Positive Weighted Compact A General Solution for Update with Suboptimal Gain Functions of a Moving Source with an Unmanned Trajectory Measurements Time Helicopter Weight Estimation Quadrature Rule for Uncertainty Out-of-Sequence Measurements: The Feedback Particle Filter Derived Aerial Vehicle A. Gerlach, Universal Technology J. Warner, J. Rogers, Georgia Institute Propagation and Nonlinear Estimation Augmented Fixed-Lag Smoother from Continuation Method T. Egorova, N. Gatsonis, M. Demetriou, Corporation, Dayton, OH; D. Doman, of Technology, Atlanta, GA; N. Phan, B. Jia, Intelligent Fusion Technology, Inc., H. Yoon, D. Sternberg, K. Cahoy, Y. Matsuura, R. Ohata, K. Nakakuki, R. Worcester Polytechnic Institute, Worcester, MA Air Force Research Laboratory, Wright- Naval Air Systems Command, Patuxent Germantown, MD; M. Xin, University of Massachusetts Institute of Technology, Hirokawa, Mitsubishi Group, Kamakura, Patterson AFB, OH River, MD Missouri, Columbia, Columbia, MO Cambridge, MA Japan Thursday, 7 January 2016 345-GNC-30/ACD-10 Aircraft GNC I Hillcrest C Chaired by: H. TAHA, University of California, Irvine and W. WHITACRE, Draper Laboratory 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2016-1621 AIAA-2016-1622 AIAA-2016-1623 AIAA-2016-1624 AIAA-2016-1625 AIAA-2016-1626

Fuel Flow Control for Extending Fuel Flow Control for Extending Model-Based Engine Control H∞ Loop-Shaping Robust Application of a Kalman Filter for Optimization of the vertical Aircraft Thermal Endurance Part I: Aircraft Thermal Endurance Part II: Architecture with an Extended Differential Thrust Control Reduction of Sensor/Turbulence- trajectory through Time and Energy Underlying Principles Closed Loop Control Kalman Filter Methodology for Lateral/ Induced Noise Within a Model management: A Human-in-the- D. Doman, Air Force Research Laboratory, D. Doman, Air Force Research Laboratory, J. Csank, J. Connolly, NASA Glenn Directional Stability of an Aircraft Reference Adaptive Controller Loop Study Wright-Patterson AFB, OH Wright-Patterson AFB, OH Research Center, Cleveland, OH with a Damaged M. Rafi, J. Steck, J. Watkins, Wichita F. Bussink, R. Verhoeven, A. Marsman, L. Lu, K. Turkoglu, San Jose State State University, Wichita, KS National Aerospace Laboratory (NLR), University, San Jose, CA Amsterdam, The Netherlands ; X. Prats, B. Bendris, Technical University of Catalonia, Barcelona, Spain; J. Montolio, Pildo Labs, Barcelona, Spain; et al. Thursday, 7 January 2016 346-GNC-31 GNC Concepts in Air Traffic Control Cortez Hill B Chaired by: A. CHAKRAVARTHY, Wichita State University 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2016-1627 AIAA-2016-1628 AIAA-2016-1629 AIAA-2016-1630 AIAA-2016-1631 A Dynamic Heads-Up Air Traffic Improving Sense and Avoid using Three-Dimensional Velocity Encounter Rate Estimation of Separation Assurance and Locator & Collision Advisory Display Multi-modal Sensor Fusion for Obstacle Method for UAV’s Continuous Descent Arrival Procedures Scheduling Coordination in the Using Google Glass Non-communicating Threats Uncoordinated Avoidance in Terminal Area Arrival Environment. M. Rafi, B. Chandrasekaran, M. Kusmez, J. Jackson, J. Boskovic, D. Diel, Scientific Maneuver S. Park, Optimal Synthesis, Inc., Los Altos, A. Aweiss, A. Cone, J. Holladay, E. Munoz,

J. Steck, J. He, Wichita State University, Systems Company, Inc., Woburn, MA Y. Jenie, E. Van Kampen, C. de Visser, J. CA; J. Clarke, E. Feron, H. Jimenez, Georgia NASA Ames Research Center, Moffett Wichita, KS Ellerbroek, J. Hoekstra, Delft University of Institute of Technology, Atlanta, GA Field, CA; T. Lewis, NASA Langley Research Technology, Delft, The Netherlands Center, Hampton, VA Thursday, 7 January 2016 347-GT-7 Aerodynamic Force Measurement and NFMTC Update (Invited) Cove Chaired by: R. RHEW, NASA-Langley Research Center and S. COMMO, NASA Langley Research Center 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs Oral Presentation Oral Presentation Oral Presentation Oral Presentation AIAA-2016-1632 National Force Measurement Balance In-Situ Load System (ILS) Balance Calibration Study Update On-board Signal Digitization Pre-Test Assessment of the Use Technology Capability (NFMTC) Demonstration Results D. Landman, Old Dominion University, J. Ponder, NASA Glenn Research Center, Envelope of the Normal Force of a Project Update K. Toro, NASA Langley Research Center, Norfolk, VA Cleveland, OH Wind Tunnel Strain-Gage Balance S. Commo, NASA Langley Research Hampton, VA N. Ulbrich, Jacobs, Moffett Field, CA Center, Hampton, VA Thursday, 7 January 2016 348-GTE-11 Jet Noise Cortez Hill C Chaired by: S. GOGINENI, Spectral Energies, LLC and B. KIEL, Air Force Reseach Laboratory 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2016-1633 AIAA-2016-1634 AIAA-2016-1635 AIAA-2016-1636 AIAA-2016-1637 AIAA-2016-1638 AIAA-2016-1639 Velocity Statistics and Spectra in Noisy Flow Structures in a Heated Perceived Noise Analysis for Characterization of Three-Stream Simple Scaling Of Multi-Stream Jet Noise Characteristics of a Rectangular A near-field investigation of a Three-Stream Jets and Unheated Jet Produced by a Offset Jets Applied to Commercial Jet Flow Fields Plumes For Aeroacoustic Modeling vs Circular Nozzle for Ideally supersonic, multi-stream jet: locating T. Ecker, W. Ng, K. Lowe, Virginia Three-Stream Rectangular Nozzle Supersonic Aircraft B. Henderson, M. Wernet, NASA Glenn J. Bridges, NASA Glenn Research Center, Expanded Jet Flow turbulence mechanisms through Polytechnic Institute and State University, with an Aft Deck D. Huff, B. Henderson, J. Berton, J. Research Center, Cleveland, OH Cleveland, OH K. Viswanath, R. Johnson, A. Corrigan, K. velocity and density measurements Blacksburg, VA; B. Henderson, NASA Glenn C. Ruscher, S. Gogineni, Spectral Energies, Seidel, NASA Glenn Research Center, Kailasanath, Naval Research Laboratory, A. Magstadt, M. Berry, T. Coleman, P. Shea, Research Center, Cleveland, OH; S. Leib, LLC, Dayton, OH; B. Kiel, A. Giese, Air Cleveland, OH Washington, D.C.; P. Mora , F. Baier, University M. Glauser, Syracuse University, Syracuse, NY; Ohio Aerospace Institute, Cleveland, OH Force Research Laboratory, Wright- of Cincinnati, Cincinnati, OH; et al. C. Ruscher, Spectral Energies, LLC, Dayton, Patterson AFB, OH; K. Viswanath, Naval OH; et al. Research Laboratory, Washington, D.C. Thursday, 7 January 2016 349-GTE-12 Methodologies for Advanced Components Golden Hill A Chaired by: B. SARACOGLU, von Karman Institute for Fluid Dynamics and S. DRENNAN, Convergent Science, Inc. 0900 hrs 0930 hrs 1000 hrs AIAA-2016-1640 AIAA-2016-1641 AIAA-2016-1642 Simple and Robust Framework for Simulation of Particle flow in Mode-Tracking in Surrogate-Based Coupled Aerothermal Gas Turbine Inertial Particle Separator with Inverse Identification of Rotor Simulation using Low-Mach and Eulerian Method of Velocity Re- Blade Geometry Using Campbell Compressible Industrial CFD Solvers associated Two-node Quadrature- Diagram P. Legrenzi, K. Kannan, G. Page, based Method of Moment V. Yadav, S. Venkataraman, San Diego Loughborough University, Loughborough, D. Sun, A. Garmory, G. Page, State University, San Diego, CA; S. Bland, United Kingdom; I. Tristanto, Rolls-Royce Loughborough University, Loughborough, NextGen Aeronautics, Danville, VA Group plc, Derby, United Kingdom United Kingdom; I. Tristanto, Rolls-Royce Group plc, Derby, United Kingdom Thursday, 7 January 2016 350-HIS-4 Boeing Centennial 1916-2016 II Americas Cup A Chaired by: S. MUSI 0900 hrs 0930 hrs 1000 hrs AIAA-2016-1643 AIAA-2016-1644 Discussions on Boeing’s 100-year History Dyna-Soar: What Might Have Been The Road to the Modern : Moderator: James Kidrick, President, San Diego Air & Space Museum J. Tishkoff, Air Force Office of Scientific The first Boeing–Douglas Research, Arlington, VA commercial aircraft market battle Michael Lombardi Tom Crouch Mike Lavelle Guy Norris M. Lavelle, Great Planes Heritage, Chief Historian Senior Curator Aviation Historian Senior Editor Issaquah, WA The Boeing Company Smithsonian Institution Aviation Week Closing Remarks John Tracy Chief Technology Officer The Boeing Company

Thursday, 7 January 2016 351-HSABP-6 Advances in Pressure Gain Combustion III - RDE, PDE, & Pulse Combustion Regatta A Chaired by: S. CLAFLIN, Aerojet Rocketdyne and D. PAXSON, NASA Glenn Research Center 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2016-1645 AIAA-2016-1646 AIAA-2016-1647 AIAA-2016-1648 AIAA-2016-1649 AIAA-2016-1650 Enhanced Combustion in Supersonic The Rayleigh Efficiency of Pressure Impact of an Exhaust Throat on High-Repetition-Rate Efficacy of Acoustics in Determining Investigation of a Rotating Flows Using a Pulsed Detonation Gain Combustors Semi-Idealized Rotating Detonation Chemiluminescence Imaging of a the Operating Mode of a Rotating Detonation Engine using Ethylene- Y. Abul-Huda, M. Gamba, University of R. Blackburn, R. Miller, University of Engine Performance Rotating Deotonation Engine Detonation Engine Air Mixture Michigan, Ann Arbor, Ann Arbor, MI Cambridge, Cambridge, United Kingdom D. Paxson, NASA Glenn Research Center, K. Cho, J. Codoni, B. Rankin, J. Hoke, F. N. Pandiya, A. St. George, R. Driscoll, J. Wilhite, R. Driscoll, A. St. George, V. Cleveland, OH Schauer, Air Force Research Laboratory, V. Ganesh Kumar, B. Malla, E. Gutmark, Ganesh Kumar, E. Gutmark, University of Wright-Patterson AFB, OH University of Cincinnati, Cincinnati, OH Cincinnati, Cincinnati, OH Thursday, 7 January 2016 352-IS-9 Intelligent Human-Automation Interaction Regatta B Chaired by: M. GOMBOLAY, MIT and J. SHAH, MIT - Massachusetts Institute of Technology and A. STIMPSON 0900 hrs 0930 hrs 1000 hrs AIAA-2016-1651 AIAA-2016-1652 AIAA-2016-1653 Towards Self-Confidence in Functional Requirements for Cooperative Search Using Human- Autonomous Systems Onboard Intelligent Automation in UAV Teams N. Sweet, N. Ahmed, University of Single Pilot Operations C. Liu, J. Hedrick, University of California, Colorado, Boulder, Boulder, CO; U. M. Cummings, A. Stimpson, M. Clamann, Berkeley, Berkeley, CA Kuter, C. Miller, Smart Information Flow Duke University, Durham, NC Technologies, Minneapolis, MN Thursday, 7 January 2016 353-MAT-9 Materials & Design for Additive Manufacturing Gaslamp B Chaired by: S. WANTHAL, The Boeing Company and T. CLEMENT, Raytheon 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2016-1654 AIAA-2016-1655 AIAA-2016-1656 AIAA-2016-1657 AIAA-2016-1658 Cathodic Protection Tests for the Fire-Retardant Polyamide 11 On the Fatigue Performance of Powder Bed Models – Numerical Data-Driven Certification of Galvanic Corrosion of Airframe Nanocomposites/Elastomer Blends Additively Manufactured Ti-6Al-4V Assessment of As-Built Quality Additively Manufactured Parts Grade CFRP/Al Systems for Selective Laser Sintering: to Enable Rapid Qualification for M. Megahed, H. Mindt, B. Shula, ESI D. Mies, W. Marsden, S. Dyer, S. Warde, T. Morimoto, Japan Aerospace Exploration Further Studies Aerospace Applications Group, Farmington Hills, MI; A. Peralta, J. Granta Design, Cambridge, United Agency (JAXA), Chofu, Japan; J. Koyanagi, R. Ortiz, H. Wu, J. Koo, University of P. Li, D. Warner, Cornell University, Ithaca, Neumann, Honeywell International, Inc., Kingdom Tokyo University of Science, Katsushika, Texas, Austin, Austin, TX NY; A. Fatemi , University of Toledo, Phoenix, AZ Japan Toledo, OH; N. Phan, Naval Air Systems Command, Lexington Park, MD Thursday, 7 January 2016 354-MDO-7 Mission Driven Design Balboa A Chaired by: F. ENGELSEN, The Boeing Company and D. ALLISON, Optimal Flight Sciences LLC 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2016-1659 AIAA-2016-1660 AIAA-2016-1661 AIAA-2016-1662 AIAA-2016-1663 An EGO-like Optimization Wing Aerostructural Optimization An Aircraft Development Allocation-mission-design Waverider Design, Analysis and Framework for Simultaneous under Uncertain Payload Weight and Methodology Aligning Design and optimization of next-generation Performance Evaluation Aircraft Design and Airline Aircraft Range Strategy to Support Key Decision aircraft using a parallel F. Ferguson, N. Dasque, M. Dhanasar, Allocation A. Elham, Delft University of Technology, Delft, Making computational framework North Carolina A&T State University, S. Roy, W. Crossley, Purdue University, The Netherlands ; L. Bahamonde Jacome, F. Burgaud, C. Frank, D. Mavris, Georgia J. Hwang, J. Martins, University of Greensboro, NC; I. Blankson, NASA Glenn West Lafayette, IN Technical University of Madrid, Madrid, Spain Institute of Technology, Atlanta, GA Michigan, Ann Arbor, Ann Arbor, MI Research Center, Cleveland, OH Thursday, 7 January 2016 355-MST-11 Model Design and Development Golden Hill B Chaired by: K. KLOSINSKI, Engineering Systems, Inc. and P. KENNEY, NASA Langley Research Center 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2016-1664 AIAA-2016-1665 AIAA-2016-1666 AIAA-2016-1667 AIAA-2016-1668 AIAA-2016-1669 AIAA-2016-1670 Simulator Design for Flying and A New Method of Flight Path Aerodynamic Model Update Hard Real-Time General-Purpose Design and Development of Design and Validation of a Gust Usage of a Model Following Small Handling Qualities Instruction Reconstruction Using the j2 Using Parameter Identification Robotic Simulations of Autonomous Ground-Based 5-DOF Spacecraft Response Alleviation System Based Scale UAV for Evaluation of ACMI J. Kemper, Calspan Corporation, Edwards, Universal Tool-Kit Supporting a Cessna Grand Air Vehicles Formation Flying Testbed on Generalized Predictive Control Ground System CA; M. Cotting, U.S. Air Force Test Pilot J. Slane, K. Klosinski, R. Osteroos, Caravan Engineering Simulation S. Walker, J. Shan, R. Allison, York Y. Eun, C. Park, S. Park, Yonsei University, W. Zhuang, Z. Wu, C. Yang, C. Huang, S. Jo, J. Kim, K. Choi, Inha University, School, Edwards AFB, CA Engineering Systems Inc., Colorado A. Paris, O. Alaverdi, AMERICAN SYSTEMS University, Toronto, Canada Seoul, South Korea Beihang University, Beijing, China Incheon, South Korea Springs, CO; D. Saracino, AvSafe, St. Corporation, Lexington Park, MD Louis, MO; J. Jeffery, j2 Aircraft Dynamics Ltd., Daresbury, United Kingdom Thursday, 7 January 2016 356-MVC-1 Grid Generation Nautical Chaired by: E. BLADES, ATA Engineering, Inc. and J. MASTERS, AEDC 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2016-1671 AIAA-2016-1672 AIAA-2016-1673 AIAA-2016-1674 AIAA-2016-1675 Optimization-Based Smoothing for The impact of unstructured mesh Automatic 2D high-order viscous Radial basis function mesh Ventus: An Overset Adaptive Extruded Meshes generation approach on truncation mesh generation by Spring-Field deformation including surface Cartesian Simulation Framework S. Karman, M. Remotigue, Pointwise, Inc., error and vector-adding orthogonality for Moving Boundary Problems, Fort Worth, TX H. Fan, C. Ollivier Gooch, University of T. Liu, L. Wang, University of Tennessee, T. Gillebaart, A. van Zuijlen, H. Bijl, Delft Part II - Parallelism and Dynamic British Columbia, Vancouver, Canada Chattanooga, Chattanooga, TN; S. University of Technology, Delft, The Load Balancing Karman, Pointwise, Inc., Fort Worth, Netherlands R. Harris, Self, Huntsville, AL TX; B. Hilbert, University of Tennessee, Chattanooga, Chattanooga, TN Thursday, 7 January 2016 357-NDA-6 Reliability and Life Prediction Old Town B Chaired by: T. KRISHNAMURTHY, NASA-Langley Research Center and E. TUEGEL, USAF 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2016-1676 AIAA-2016-1677 AIAA-2016-1678 AIAA-2016-1679 AIAA-2016-1680 Sequential Subspace Reliability Modeling epistemic uncertainty in Bearing Prognostics Method Based Aerospace electronics-and- Probabilistic PoF based Framework for Method the representation of spatial and on Entropy Decrease at Specific photonics (AEP) reliability has to be Fatigue Life Prediction of Aircraft Gas H. Bae, Wright State University, Dayton, temporal variability in reliability Frequency quantified to be assured Turbine Discs OH; E. Alyanak, Air Force Research analysis D. An, N. Kim, University of Florida, E. Suhir, ERS Company, Los Altos, CA S. Zhu, H. Huang, W. Peng, H. Wang, Laboratory, Wright-Patterson AFB, OH H. Devathi, Z. Hu, S. Mahadevan, Gainesville, Gainesville, FL; J. Choi, Korea University of Electronic Science and Technology Vanderbilt University, Nashville, TN Aerospace University, Goyang, South Korea of China, Chengdu, China; S. Mahadevan,

Vanderbilt University, Nashville, TN Thursday, 7 January 2016 358-NW-14 Thursday Late Morning Networking Coffee Break Exposition Hall 0900 - 0930 hrs Thursday, 7 January 2016 359-PC-14 Spray and Droplet Combustion II Harbor B Chaired by: J. O`CONNOR, Pennsylvania State University and J. HAYNES, GE Global Research Center 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2016-1681 AIAA-2016-1682 AIAA-2016-1683 AIAA-2016-1684 AIAA-2016-1685 Simulations of kerosene droplet Droplet Combustion Characteristics Puffing and Micro-explosion Simulations of Injection of LOX/ Interface-Tracking Simulations of

combustion in vitiated air of Butyl Butyrate, Limonene, and behavior of Ethanol/Jet A-1 Fuel GCH4 under Flashing Conditions Droplet Vaporization and Burning A. Giusti, J. Sidey, Cambridge University, their Blends with Jet A-1 Droplets T. Ramcke, M. Pfitzner, University of the of Hypergolic Propellants Cambridge, United Kingdom; G. Borghesi, D. Chaitanya Kumar Rao, S. Syam, S. S. Syam, D. Chaitanya Kumar Rao, S. German Federal Armed Forces, Neubiberg, H. Tani, Y. Umemura, Y. Daimon, Japan Sandia National Laboratories, Livermore, Karmakar, Indian Institute of Technology Karmakar, R. Joarder, Indian Institute of Germany Aerospace Exploration Agency (JAXA), CA; E. Mastorakos, Cambridge University, Kharagpur, Kharagpur, India Technology Kharagpur, Kharagpur, India Tsukuba, Japan; H. Terashima, Hokkaido Cambridge, United Kingdom University, Sapporo, Japan; M. Koshi, Yokohama National University, Yokohama, Japan Thursday, 7 January 2016 360-PC-15 Turbulent Combustion II - Fuel Chemistry Harbor C Chaired by: C. LI, Air Force Office of Scientific Research and V. SANKARAN, US Air Force/AFRL 0900 hrs 0930 hrs 1000 hrs AIAA-2016-1687 AIAA-2016-1688 AIAA-2016-1689 Impact of Chemical Kinetics Investigation of chemical pathways Predicting and Accelerating Mechanisms on the Predictions of for turbulent Hydrogen-Air Chemistry in High Speed Reacting Bluff Body Stabilized Flames premixed flames Flows S. Sardeshmukh, W. Anderson, Purdue D. Dasgupta, W. Sun, Georgia Institute of T. Wignall, C. Patton, T. Echekki, J. University, West Lafayette, IN Technology, Atlanta, GA; M. Day, Lawrence Edwards, North Carolina State University, Berkeley National Laboratory, Berkeley, Raleigh, NC CA; T. Lieuwen, Georgia Institute of Technology, Atlanta, GA Thursday, 7 January 2016 361-PDL-10 Novel Plasma Actuators, Concepts and Systems Old Town A Chaired by: T. CORKE, University of Notre Dame 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2016-1690 AIAA-2016-1691 AIAA-2016-1692 AIAA-2016-1693 AIAA-2016-1694 Development of plasma actuator Development of Serrated Multi- Multi-point ignition of Hydrogen/ Carbon Nanoparticles in the Modeling of Microplasmas with based on surface sparks for a Electrode Plasma Actuators for Air mixtures with single pulsed Radiation and Acoustic fields the Nano-Engineered Electrodes buffet control Enhanced Force Production nanosecond surface dielectric Vicinity of the Arc Discharge S. Tholeti, A. Alexeenko, S. Macheret, A. Firsov, Y. Isaenkov, M. Shurupov, T. Matsuno, M. Sugahara, H. Kawazoe, barrier discharge. Morphology of M. Shneider, Princeton University, Purdue University, West Lafayette, IN Russian Academy of Sciences, Moscow, Tottori University, Tottori, Japan; H. the discharge in different gases at Princeton, NJ Russia ; S. Leonov, University of Notre Nishida, Tokyo University of Agriculture elevated pressures Dame, Notre Dame, IN and Technology, Koganei, Japan S. Shcherbanev, École Polytechnique, Palaiseau, France; N. Popov, Moscow State University, Moscow, Russia ; S. Starikovskaia, École Polytechnique, Palaiseau, France Thursday, 7 January 2016 362-PDL-11 Plasma Diagnostics Ocean Beach Chaired by: R. MILES, Princeton University 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2016-1695 AIAA-2016-1696 AIAA-2016-1697 AIAA-2016-1698 AIAA-2016-1699 AIAA-2016-1700 In-situ quantitative measurement Phase-Locked Averaged Schlieren Optical Emission Spectroscopy of Development of a Cavity Enhanced Plasma Density Measurements A Comparison of Radar REMPI and of ethylene from n-butane of Periodic Nanosecond-Pulsed DBD the A.C. Plasma Anemometer Thomson and Raman Scattering for Aero-Optic Applications Using Laser Induced Fluorescence for pyrolysis in a flow reactor Actuation in Quiescent Air E. Matlis, C. Marshall, T. Corke, Diagnostic Two-Wavelength Heterodyne Concentration Measurements L. Su, Z. Zhang, University of Tennessee, H. Hu, H. Li, X. Meng, J. Wang, University of Notre Dame, Notre Dame, A. Friss, A. Yalin, Colorado State Interferometry T. Chng, R. Miles, Princeton University, Knoxville, Knoxville, TN Northwestern Polytechnical University, IN; S. Gogineni, Spectral Energies, LLC, University, Fort Collins, CO B. Neiswander, E. Matlis, T. Corke, Princeton, NJ Xi’an, China; F. Liu, S. Luo, University of Beavercreek, OH University of Notre Dame, Notre Dame, IN California, Irvine, Irvine, CA Thursday, 7 January 2016 363-SCS-5 Spacecraft Solar Array Structures I Balboa B Chaired by: R. PAPPA, NASA Langley Research Center and M. CHAMBERLAIN, NASA 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2016-1701 AIAA-2016-1702 AIAA-2016-1703 AIAA-2016-1704 AIAA-2016-1705 AIAA-2016-1706 Structural Design Considerations Rapid Parametric Analysis and Simulation of the Deployment of a Composite Beam Roll-Out Array Development of a Continuous Active Control of Solar Array for a 50 kW-Class Solar Array for Design of Space-Based Solar Arrays Flexible Roll-Up Solar Array Using - A Multifunctional Deployable Advanced Composite Truss Printing Dynamics During Spacecraft NASA’s Asteroid Redirect Mission C. Rupp, L. Schweizer, ATA Engineering, Multi-Body Dynamics Software Structure for Space Power System Maneuvers T. Kerslake, T. Kraft, J. Yim, D. Le, NASA Inc., San Diego, CA; D. Murphy, ATK, B. Ross, N. Woo, MotionPort, LLC, St. Generation Q. McAllister, J. Senne, A. Romanyszyn, B. Ross, N. Woo, MotionPort, LLC, St. Glenn Research Center, Cleveland, OH Goleta, CA George, UT; J. Blandino, Virginia Military T. Stern, K. Steele, Alliance Spacesystems, San Diego Composites, San Diego, CA George, UT; T. Kraft, NASA Glenn Research Institute, Lexington, VA LLC, Los Alamitos, CA Center, Cleveland, OH; J. Blandino, Virginia Military Institute, Lexington, VA Thursday, 7 January 2016 364-SD-10 Reduced Order Modeling II Balboa C Chaired by: S. LIGUORE, Boeing Engineering Operations & Technology and S. RAGHAVAN, University of Central Florida 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2016-1707 AIAA-2016-1708 AIAA-2016-1709 AIAA-2016-1710 AIAA-2016-1711 Using Complex Variables to Large Deformation Modeling of An Optimum Thermal Basis for Modeling Fatigue Crack Geometrically Non-linear Structural Estimate the Derivatives of a Beam Type Structure and a 3D Coupled Structural-Thermal Propagation in a Ti-Alloy at Dynamics using Increased-Order Nonlinear Reduced-Order Models using an Enhanced Modal Reduced Order Models Elevated Temperature within a Modelling J. Hollkamp, Air Force Research Approach R. Murthy, A. Matney, M. Mignolet, Reduced-OrderModel Framework L. Bernhammer, Delft University of Laboratory, Wright-Patterson AFB, OH; P. M. Ritter, German Aerospace Center (DLR), Arizona State University, Tempe, AZ P. O’Hara, United Technologies Technology, Delft, The Netherlands ; O’Hara, Universal Technology Corporation, Göttingen, Germany; C. Cesnik, University Corporation, Dayton, OH; J. Hollkamp, M. Karpel, Technion--Israel Institute of Wright-Patterson AFB, OH of Michigan, Ann Arbor, Ann Arbor, MI Air Force Research Laboratory, Wright- Technology, Haifa, Israel; M. Reyes, H.

Patterson AFB, OH Climent Manez, Airbus, Getafe, Spain Thursday, 7 January 2016 365-SEN-3 Advanced Data Fusion Techniques Regatta C Chaired by: T. FREY, Lockheed Martin Aeronautics 0900 hrs 0930 hrs 1000 hrs AIAA-2016-1712 AIAA-2016-1713 AIAA-2016-1714 Cooperative-timing Attack with Novel Blind Load Balancing Database Completeness Impact on Smart Munitions using Cooperative Scheduling Algorithms for Target Identification Performance Localization in Contested Distributed Tracking Networks K. Engebretson, Lockheed Martin Environments T. Frey, D. Faulk, Lockheed Martin Corporation, Fort Worth, TX R. Sharma, Utah State University, Logan, Corporation, Fort Worth, TX UT; S. Rathinam, Texas A&M University, College Station, TX Thursday, 7 January 2016 366-SOF-7/UMS-8/IS-10 Assurance of Autonomy Symposium III Coronado A 0900 - 1200 hrs Managing Key Issues for Assured Autonomy

In this session, we examine several key challenges that directly impact our ability to generate assurance arguments for increasingly autonomous systems. Topics that will be addressed include human-machine interaction under increasingly autonomous systems, the management of uncertainty, and the management and mitigation of communications criticality.

We will begin with subject matter expert talks highlighting the effects of human-machine teaming on autonomous systems. We then proceed to a panel exploring the issues of uncertainty management and mitigating the effects of communications criticality. We then culminate with as set of lightning-fast (5-minute) talks for all assurance of autonomy themes. We strongly encourage these lightning-fast talks from our participants — please sign up in the Wednesday sessions.

Speaker: Steven Young NASA Langley Research Center Panelists: Kerianne Gross Johann Schumann Jim Murphy Natalia Alexandrov Mats Heimdahl Air Force Research Laboratory NASA Ames Research Center/SGT NASA Ames Research Center NASA Langley Research Center University of Minnesota

Lightning-fast talks: Mike Lowry Kalmanje Krishnakumar Audience Members NASA Ames Research Center NASA Ames Research Center

Thursday, 7 January 2016 367-STR-12 Spacecraft Structural Design La Jolla A Chaired by: J. ZIPAY, NASA-Johnson Space Center 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2016-1715 AIAA-2016-1716 AIAA-2016-1717 AIAA-2016-1718 AIAA-2016-1719 AIAA-2016-1720 The Ultimate Factor of Safety Thermo-structural design of Post-buckling Analysis of Curved Integrated Composite Stiffener Forward Skirt Structural Testing Flutter Analysis of Laminated for Aircraft and Spacecraft – the Hexafly-INT Experimental Honeycomb Sandwhich Panels Structure (ICoSS) Concept for on the Space Launch System (SLS) Curvilinear-Stiffened Plates Its History, Applications and Flight Test Vehicle (EFTV) and Containing Interfacial Disbonds Planetary Entry Vehicles Program R. Fernandes, A. Tamijani, Embry-Riddle Misconceptions Experimental Service Module (ESM) E. Pineda, B. Bednarcyk, T. Krivanek, S. Kellas, NASA Langley Research Center, J. Lohrer, R. Wright, Orbital ATK, Aeronautical University, Daytona Beach, FL J. Zipay, C. Modlin, NASA Johnson Space V. Carandente, R. Scigliano, Italian NASA Glenn Research Center, Cleveland, Hampton, VA Promontory, UT Center, Houston, TX; C. Larsen, NASA Aerospace Research Center (CIRA), OH Engineering Safety Center, Hampton, VA Capua, Italy Thursday, 7 January 2016 368-STR-13 Buckling, Fatigue, and Fracture of Structures I La Jolla B Chaired by: M. SCHULTZ, NASA Langley Research Center and C. BISAGNI 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2016-1721 AIAA-2016-1722 AIAA-2016-1723 AIAA-2016-1724 AIAA-2016-1725 AIAA-2016-1726 Peridynamic Truss Element for Bond-Based Peridynamics with an Peridynamics for Predicting Tensile Mean Stress Effects in Strain Fiber Path Optimization of a Influence of microstructure Viscoelastic Deformation Arbitrary Poisson’s Ratio and Compressive Strength of Energy-based Criterion for Fatigue Symmetric Laminate with a Cutout for arrangement on the responses M. Dorduncu, A. Barut, E. Madenci, Y. Hu, E. Madenci, University of Arizona, Notched Composites Life Prediction Thermal Buckling, Using a Novel Finite of composites beyond one University of Arizona, Tucson, AZ Tucson, Tucson, AZ Y. Hu, E. Madenci, University of Arizona, S. Zhu, Q. Lei, H. Huang, Y. Yang, Element Algorithm representative unit cel. Tucson, Tucson, AZ; N. Phan, Naval Air University of Electronic Science and A. Vijayachandran, P. Acar, V. H. Huang, State University of New York, Systems Command, Patuxent River, MD Technology, Chengdu, China Sundararaghavan, University of Michigan, Ann Stony Brook, NY Arbor, Ann Arbor, MI; A. Waas, University of Washington, Seattle, Seattle, WA Thursday, 7 January 2016 369-TP-9 Non-Equilibrium Flows, Non-Equilibrium Radiation and Rarefied Flows II Harbor G Chaired by: T. SCHWARTZENTRUBER, University of Minnesota and M. KIO, National Space Research & Development Agency 0900 hrs 0930 hrs 1000 hrs AIAA-2016-1727 AIAA-2016-1728 AIAA-2016-1729 Title: Numeircal Simulations of Modeling of Non-equilibrium Investigation of Condensation

Flows over a Small Sphere within Radiation for CO2-N2 Gas Mixtures Effect in CO2 Hypersonic Rarefied Velocity Slip Regime R. Macdonald, A. Munafò, University of Flows C. Cai, New Mexico State University, Las Illinois, Urbana-Champaign, Urbana, IL; C. T. Ozawa, T. Suzuki, K. Fujita, Japan Cruces, NM Johnston, NASA Langley Research Center, Aerospace Exploration Agency (JAXA), Hampton, VA; M. Panesi, University of Chofu, Japan Illinois, Urbana-Champaign, Urbana, IL Thursday, 7 January 2016 370-WE-8 Wind Energy: VAWT Aerodynamics Harbor H Chaired by: D. MANIACI, Sandia National Laboratories 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2016-1730 AIAA-2016-1731 AIAA-2016-1732 AIAA-2016-1733 AIAA-2016-1734 AIAA-2016-1735 Parameterized Vertical-Axis Wind Implicit Large-Eddy Simulation of An Experimental Investigation on Numerical / Experimental Flow Curvature Effects for Aerodynamic Optimization of Turbine Wake Model Using CFD 2D Counter-Rotating Vertical-Axis the Near Wake Characteristics of a Investigation of Airfoil Shape for VAWT: a Review of Virtual Airfoil Vertical Axis Wind Turbine with Vorticity Data Wind Turbines Darrious Vertical-Axis Wind Turbine Small VAWT Transformations and Implementation Trailing Edge Flap E. Tingey, A. Ning, Brigham Young S. Kanner, L. Wang, P. Persson, University M. Khosravi, P. Sarkar, H. Hu, Iowa State W. Yamazaki, Y. Arakawa, Nagaoka in XFOIL S. Ertem, C. Simao Ferreira, Delft University, Provo, UT of California, Berkeley, Berkeley, CA University, Ames, IA University of Technology, Nagaoka, Japan S. van der Horst, J. van de Wiel, C. Simao University of Technology, Delft, The Ferreira, Delft University of Technology, Delft, Netherlands ; M. Gaunaa, H. Madsen, The Netherlands ; N. Ramos García, Technical Technical University of Denmark, Lyngby,

University of Denmark, Lyngby, Denmark Denmark Thursday, 7 January 2016 371-WE-9 Wind Energy: Wind Turbine and Wind Plant Control Harbor I Chaired by: S. FROST, NASA-Ames Research Center 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2016-1736 AIAA-2016-1737 AIAA-2016-1738 AIAA-2016-1739 AIAA-2016-1740 AIAA-2016-1741 Disturbance Accommodating Experimental Evaluation of impact of airfoil performance CFD Analysis on Load Mitigation of Aeroservoelastic analysis of storm- Wake detection for wind farm Control based Independent Blade Extremum Seeking Based Region-2 degradation on annual energy Wind Turbine Utilizing Individual ride-through control strategies for control – Formulation and Pitch Control Design on CART2 Controller for CART3 Wind Turbine production and its mitigation via Pitch Control in Stable ABL wind turbines validation N. Wang, A. Wright, National Renewable Y. Xiao, Y. Li, M. Rotea, University of extremum seeking controls H. Oe, Tokyo University of Science, C. Tibaldi, M. Hansen, Technical University C. Bottasso, S. Cacciola, F. Campagnolo, J. Energy Laboratory, Golden, CO Texas, , Richardson, TX T. Ashuri, M. Rotea, C. Ponnurangam, Katsushika, Japan; Y. Tanabe, Japan of Denmark, Roskilde, Denmark Schreiber, Technical University of Munich, Y. Xiao, University of Texas, Dallas, Aerospace Exploration Agency (JAXA), Munich, Germany Richardson, TX Chofu, Japan; H. Sugawara, Ryoyu Systems Company, Ltd., Shinagawa, Japan; M. Yamamoto, Tokyo University of Science, Katsushika, Japan Thursday, 7 January 2016 372-PANEL-10 Thursday Morning Forum 360 Seaport F-G 0930 - 1130 hrs Putting the E in STEM Moderator: Meredith Drosback, Assistant Director for Education and Physical Sciences, Office of Science and Technology Policy, Executive Office of the President

Panelists: Thea Sahr Edward J. Coyle Director of Programs John B Peatman Distinguished Professor of Electrical and Computer Engineering DiscoverE Georgia Institute of Technology Thursday, 7 January 2016 373-LUNCH-4 Recognition Luncheon: Celebrating Achievements in Aerospace Design/Structures and Literature Seaport A-E 1230 - 1400 hrs Michael Gazarik Technology Director Ball Aerospace & Technologies Corporation Thursday, 7 January 2016 374-ACD-11 Micro Air Vehicle Design Cortez Hill A Chaired by: C. BIL, RMIT University and R. VOS 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs AIAA-2016-1742 AIAA-2016-1743 AIAA-2016-1744 AIAA-2016-1745 AIAA-2016-1746 Development of an In-Flight- Design and manufacture of a Design and manufacture of a self- Effective design of flapping wing Theoretical analysis and Deployable Micro-UAV fixed wing MAV with zimmerman learning flapping wing-actuation actuation mechanisms: theory and experimental verification for sizing T. Tao, R. Hansman, Massachusetts planform system for a Dragonfly-inspired MAV experiments of flapping wing micro air vehicles Institute of Technology, Cambridge, MA M. Hassanalian, A. Abdelkefi, New Mexico J. Kok, University of South Australia, Mawson M. Hassanalian, A. Abdelkefi, New Mexico M. Hassanalian, A. Abdelkefi, M. Wei, State University, Las Cruces, NM Lakes, Australia; J. Chahl, Australian National State University, Las Cruces, NM New Mexico State University, Las Cruces, University, Edinburgh, Australia NM; S. Ziaei-Rad, Isfahan University of Technology, Isfahan, Iran Thursday, 7 January 2016 375-AFM-12 Special Session: Realizing Performance Adaptive Aeroelastic Wing: Progress and Challenges Coronado D Chaired by: B. DANOWSKY, Systems Technology, Inc. and H. PFIFER, University of Minnesota 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs AIAA-2016-1747 AIAA-2016-1748 AIAA-2016-1749 AIAA-2016-1750 AIAA-2016-1751 AIAA-2016-1752 AIAA-2016-1753 mAEWing1: Design, Build, Test - Flight-Dynamics and Flutter Modeling Control Oriented Aeroservoelastic System Identification of a Small Robust Control Design for Active Sensitivity of Robust Flutter Ground Vibration Tests on a Invited and Analyses of a Flexible Flying-Wing Modeling of a Small Flexible Flexible Aircraft - Invited Flutter Suppression Boundary to Model Uncertainties in Flexible Aircraft - C. Regan, B. Taylor, University of Drone - Invited Aircraft using Computational Fluid H. Pfifer, University of Minnesota, J. Theis, H. Pfifer, P. Seiler, University of Aeroservoelastic Systems - Invited Invited Minnesota, Minneapolis, MN D. Schmidt, University of Colorado, Colorado Dynamics and Computational Minneapolis, Minneapolis, MN; B. Minnesota, Minneapolis, Minneapolis, MN A. Kotikalpudi, H. Pfifer, P. Seiler, A. Gupta, P. Seiler, University of Springs, Colorado Springs, CO; W. Zhao, R. Structural Dynamics - Invited Danowsky, Systems Technology, Inc., University of Minnesota, Minneapolis, Minnesota, Minneapolis, Minneapolis, MN; Kapania, Virginia Polytechnic Institute and B. Danowsky, Systems Technology, Inc., Hawthorne, CA Minneapolis, MN B. Danowsky, Systems Technology, Inc., State University, Blacksburg, VA Hawthorne, CA; T. Lieu, A. Coderre-Chabot, Hawthorne, CA CMSoft, Inc., Palo Alto, CA Thursday, 7 January 2016 376-AFM-13 Flight Test and System Identification I Harbor A Chaired by: T. FIELDS, University of Missouri and C. SUCHOMEL, USAF 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs AIAA-2016-1754 AIAA-2016-1755 AIAA-2016-1756 AIAA-2016-1757 AIAA-2016-1758 AIAA-2016-1759 AIAA-2016-1760 Low Cost Alternative to Motion Capture Nonlinear Aircraft Attitude and Flight Test Overview for UAS A Study on the Exhaust Heat Design of Experiments with an Stability Augmentation for Rotor Feasibility of In-Flight Quadrotor Systems for Indoor Flight Testing Using Heading Reference System Failure Integration in the NAS Project Characteristics from a Wing Surface Application to Laminar Flow Control MAV Takeoff and Landing using a Individual Motor Thrust On-board Computer Vision Detection and Identification J. Murphy, NASA Ames Research Center, Depending on the Airfoil Shape at Flight Research Meshed Platform Measurements A. Smith, E. Wang, J. LaCombe, University of P. Lu, E. Van Kampen, C. de Visser, Q. Moffett Field, CA; P. Williams-Hayes, S. Low Reynolds Number A. Tucker, Air Force Research Laboratory, M. Harada, S. Watanabe, R. Ichikawa, J. Bazin, T. Fields, University of Missouri, Nevada, Reno, Reno, NV; T. Fields, University Chu, Delft University of Technology, Delft, Kim, NASA Armstrong Flight Research K. Kamisori, K. Shimoyama, S. Obayashi, Wright-Patterson AFB, OH; H. Reed, W. National Defense Academy, Yokosuka, Kansas City, Kansas City, MO; A. Smith, of Missouri, Kansas City, Kansas City, MO The Netherlands Center, Edwards, CA; W. Bridges, Flight Tohoku University, Sendai, Japan Saric, D. Ward, Texas A&M University, Japan; K. Bollino, Naval Postgraduate Oregon State University, Corvallis, OR Research Associates, Moffett Field, CA; M. College Station, TX School, Monterey, CA Marston, Jacobs, Edwards, CA Thursday, 7 January 2016 377-AMT-8 High Speed Facility Measurements Harbor D Chaired by: J. WAGNER, Sandia National Laboratories and C. JOHANSEN, University of Calgary 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs AIAA-2016-1761 AIAA-2016-1762 AIAA-2016-1763 AIAA-2016-1764 AIAA-2016-1765 AIAA-2016-1766 AIAA-2016-1767 Simultaneous Measurements of Dual-Pump CARS Measurements OH PLIF Visualization of a Premixed Optical Measurements of Shock Development of a Compact Wavelet Analysis of Unsteady Shock- Experimental Investigation of Scalar and Velocity in a Mach 5 in a Vibrationally Nonequilibrium Ethylene-fueled Dual-Mode Scramjet Wave Oscillations in Transonic Focusing Color Schlieren Technique wave Motion on Two-dimensional Unsteady Shock Oscillation by a Turbulent Boundary Layer using Supersonic Mixing Layer Combustor Diffusers by High-Speed Mach- I. Schoegl, A. Pisano, G. Sedky, Louisiana Airfoil with Vortex Generators Forward-Facing Hemisphere at Naphthalene PLIF and PIV M. Nishihara, K. Frederickson, W. Lempert, L. Cantu, E. Gallo, A. Cutler, George Zehnder Interferometers State University, Baton Rouge, LA T. Kouchi, S. Yamaguchi, Okayama University, Mach 3 C. Combs, N. Clemens, University of Ohio State University, Columbus, OH Washington University, Washington, D.C.; T. Ota, S. Nakao, D. Ono, Y. Miyazato, Okayama, Japan; S. Koike, Japan Aerospace T. Mizukaki, Tokai University, Hiratsuka, Texas, Austin, Austin, TX P. Danehy, NASA Langley Research Center, University of Kitakyushu, Kitakyushu, Exploration Agency (JAXA), Tokyo, Japan; Japan; K. Hatanaka, Tohoku University, Hampton, VA; R. Rockwell, University of Japan S. Yanase, Okayama University, Okayama, Sendai, Japan; T. Saito, Muroran Institute Virginia, Charlottesville, VA; C. Johansen, Japan; T. Nakajima, M. Sato, Japan Aerospace of Technology, Muroran, Japan; K. University of Calgary, Calgary, Canada; et al. Exploration Agency (JAXA), Tokyo, Japan; Yamada, Japan Aerospace Exploration et al. Agency (JAXA), Sagamihara, Japan Thursday, 7 January 2016 378-APA-37 Special Session: Sea-Based Aviation Aeromechanics Computational Analysis Coronado E Chaired by: N. HARIHARAN, CREATE-AV and D. FINDLAY 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2016-1768 AIAA-2016-1769 AIAA-2016-1770 AIAA-2016-1771 AIAA-2016-1772 AIAA-2016-1773 CFD Analysis of the F/A-18E Super Shipboard Aircraft Simulation with Project MAGIC CARPET: “Advanced Development and Application of Methods for Characterizing Numerical Simulation of Water- Hornet during Aircraft-Carrier Ship-Relative Navigation Sensor Controls and Displays for Precision the SAFEDI Tool for Virtual Dynamic Rotorcraft Pilot Strategy and Landing Performance of a Regional Landing High-Lift Aerodynamic Modeling Carrier Landings” Interface Ship Airwake Analysis Handling Qualities in the Shipboard Aircraft Conditions C. Wilkinson, D. Findlay, J. Nichols, Naval J. Denham, Naval Air Systems Command, S. Polsky, C. Wilkinson, J. Nichols, Environment Q. Qu, C. Liu, P. Liu, B. Guo, Beihang

B. Green, D. Findlay, Naval Air Systems Air Systems Command, Patuxent River, Patuxent River, MD D. Ayers, J. Mercado-Perez, Naval Air J. Pritchard, R. Wallace, D. Eksuzian, J. University, Beijing, China; R. Agarwal, Command, Patuxent River, MD MD; T. Keck, J.F. Taylor, Inc., Lexington Systems Command, Patuxent River, MD; T. Tritschler, J. O’Connor, Naval Air Systems Washington University in St. Louis, St. Park, MD; D. Bayard, C. Liebe, Jet Davis, AMERICAN SYSTEMS Corporation, Command, Patuxent River, MD Louis, MO Propulsion Laboratory, California Institute Lexington Park, MD of Technology, Pasadena, CA; et al. Thursday, 7 January 2016 379-APA-38 Aerodynamic Testing: Wind-Tunnel II Americas Cup B Chaired by: G. GATLIN, NASA Langley Research Center and D. CHAN, NASA-Langley Research Center 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs AIAA-2016-1774 AIAA-2016-1775 AIAA-2016-1776 AIAA-2016-1777 AIAA-2016-1778 A New Type of Wind Tunnel for the Computational Analysis of the Investigation on the Flow-Field of Quantification of Drag from Flat Qualitative Tuft Flow Visualization Evaluation of Curved Motion Transonic Dynamics Tunnel Using Two Parallel Round Jets Impinging Suspension Line for Parachutes on the Volvo S60 under realistic J. Keogh, T. Barber, University of New FUN3D Normal to a Flat Surface and the Influence of Flow Induced driving Conditions South Wales, Sydney, Australia; S. P. Chwalowski, NASA Langley Research L. Myers, N. Rudenko, D. McLaughlin, Vibrations D. Wieser, Technical University of Berlin, Diasinos, Macquarie University, Sydney, Center, Hampton, VA; E. Quon, Georgia Pennsylvania State University, University T. Siefers, J. Campbell, D. Clark, T. Berlin, Germany; S. Bonitz, Chalmers Australia; G. Doig, California Polytechnic Institute of Technology, Atlanta, GA Park, PA McLaughlin, U.S. Air Force Academy, University of Technology, Göteborg, State University, San Luis Obispo, CA Colorado Springs, CO; K. Bergeron, Army Sweden; C. Nayeri, C. Paschereit, Research, Development and Engineering Technical University of Berlin, Berlin, Command, Natick, MA Germany; A. Broniewicz, L. Larsson, Volvo Car Corporation, Göteborg, Sweden; et al. Thursday, 7 January 2016 380-APA-39 Airfoil/Wing/Configuration Aerodynamics II Americas Cup C Chaired by: E. WALKER, NASA Langley Research Center and M. POST, USAF Academy 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs AIAA-2016-1779 AIAA-2016-1780 AIAA-2016-1781 AIAA-2016-1782 AIAA-2016-1783 Reduction of Induced Drag in Con Summary of First Aerodynamics Near-field Wingtip Vortex A Validation Study of OVERFLOW Aerodynamic shape optimization guration Flight using Wing Twist at Prediction Challenge (APC-I) Characteristics of a Rectangular Wing for Wing-Tip Vortices and static aeroelastic analysis of a Post-Stall Angles of Attack A. Hashimoto, T. Aoyama, Y. Matsuo, M. in Ground Effect D. Schauerhamer, S. Robinson, University morphing trailing edge wing M. Gunasekaran, R. Mukherjee, Indian Ueno, K. Nakakita, S. Hamamoto, Japan Q. Qu, L. Huang, P. Liu, Beihang University, of California, Davis, Davis, CA M. Zhang, C. Yang, Z. Wan, Beihang Institute of Technology Madras, Chennai, Aerospace Exploration Agency (JAXA), Beijing, China; R. Agarwal, Washington University, Beijing, China India Chofu, Japan; et al. University in St. Louis, St. Louis, MO Thursday, 7 January 2016 381-APA-40 Propeller/Rotorcraft/Wind Turbine Aerodynamics II Americas Cup D Chaired by: J. RAULEDER, Technical University of Munich and A. VANDERWYST, Leidos 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs AIAA-2016-1784 AIAA-2016-1785 AIAA-2016-1786 AIAA-2016-1787 AIAA-2016-1788 Adjoint-Based Optimisation of Ducted An Experimental Study on the Aerodynamic Performance Computational and Experimental Multi-disciplinary Design of Small Propellers for Hybrid Air Vehicles Aerodynamics and Aeroacoustic Characterization of Leading Edge Investigations of Coaxial Rotor Rotor Blades in Multiple Rotor M. Biava, M. Carrion, G. Barakos, University Characteristics of Small Propellers Protrusions on Small Propellers Unsteady Loads Configurations of Liverpool, Liverpool, United Kingdom; D. Z. Ning, H. Hu, Iowa State University, K. Moore, A. Ning, Brigham Young R. Singh, H. Kang, Army Research Laboratory, T. Carroll, I. George, G. Bramesfeld, Stewart, Hybrid Air Vehicles, Bedford, United Ames, IA University, Provo, UT Aberdeen Proving Ground, MD; C. Cameron, J. Ryerson University, Toronto, Canada Kingdom Sirohi, University of Texas, Austin, Austin, TX Thursday, 7 January 2016

382-ASC-6 Health Monitoring Gaslamp D Chaired by: R. JHA, Mississippi State University and S. JOSHI, NextGen Aeronautics Inc 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs AIAA-2016-1789 AIAA-2016-1790 AIAA-2016-1791 AIAA-2016-1792 AIAA-2016-1793 The Spacecraft SHM Experiment, Characterization of Aircraft Structural Wavelet Spectral Finite Element In-situ Structural Health Monitoring Harvesting Energy from Internal Flows Part 2: Integration, Challenges and Damage using Guided Wave Based Modeling for Health Monitoring of of Carbon Fiber Reinforced with Piezocomposite Transducers: Early Ground Science Finite Element Analysis for in-Flight Adhesively Bonded Joints Composites with CNT Smart Paint Towards a Self-Powered Low-Cost D. Doyle, S. Lee, J. Stein, B. Cooper, M. Structural Health Management N. Jayakody, R. Jha, Mississippi Y. Atescan, H. Cebeci, Istanbul Technical Blood Pressure Measurement Device Campisi, Air Force Research Laboratory, T. Krishnamurthy, NASA Langley Research State University, Starkville, MS; D. University, Istanbul, Turkey O. Bilgen, Old Dominion University, Norfolk, Kirtland AFB, NM; S. Kessler, Metis Design Center, Hampton, VA; B. Seshadri, National Samaratunga, The Aerospace Corporation, VA; J. Kenerson, Cardiovascular Associates, Corporation, Boston, MA Institute of Aerospace, Hampton, VA; R. Ross, El Segundo, CA Virginia Beach, VA; M. Akpinar-Elci, R. Hattery, NASA Langley Research Center, Hampton, VA Old Dominion University, Norfolk, VA Thursday, 7 January 2016 383-DSC-5 Nonlinear Aeroelasticity Gaslamp C Chaired by: R. PALACIOS, Imperial College London and I. CHOPRA, University of Maryland 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs AIAA-2016-1794 AIAA-2016-1795 AIAA-2016-1796 AIAA-2016-1797 AIAA-2016-1798 AIAA-2016-1799 AIAA-2016-1800 Enhanced Modal Approach for A Reduced Order Model-Based Nonlinear Aerodynamics and Geometrically Non-linear Structural Aeroelastic Modelling of Highly Nonlinear Aeroelastic Analysis of Numerical and Experimental Free-flight Nonlinear Aeroelastic Nonlinear Damping Model: Nonlinear Structures Interaction Modal Model for Aeroelastic Flexible Wings the X-56 Multi-Utility Aeroelastic Investigations on Very Flexible Aero- Simulation of Very Flexible Aircraft Formulation and Application to Post for F-16 Limit Cycle Oscillation Applications C. Howcroft, D. Calderon, L. Lambert, Demonstrator structures M. Ritter, German Aerospace Center Flutter Aeroelastic Behavior Prediction E. Kantor, R. Cavallaro, D. Raveh, M. Castellani, J. Cooper, M. Lowenberg, J. Jones, C. Cesnik, University of Michigan, O. Stalnov, Technical University of Berlin, (DLR), Göttingen, Germany; J. Jones, C. P. Song, X. Wang, M. Mignolet, Arizona Z. Zhang, P. Chen, ZONA Technology, Inc., Technion--Israel Institute of Technology, University of Bristol, Bristol, United Ann Arbor, Ann Arbor, MI Berlin, Germany; A. Da Ronch, University of Cesnik, University of Michigan, Ann Arbor, State University, Tempe, AZ; P. Chen, Scottsdale, AZ; X. Wang, M. Mignolet, Haifa, Israel Kingdom; et al. Southampton, Southampton, United Kingdom Ann Arbor, MI ZONA Technology, Inc., Scottsdale, AZ Arizona State University, Phoenix, AZ Thursday, 7 January 2016 384-EDU-2 Advancing Aerospace Education II Bankers Hill Chaired by: R. LEBEAU, Saint Louis University 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs AIAA-2016-1801 AIAA-2016-1802 AIAA-2016-1803 AIAA-2016-1804 AIAA-2016-1805 Senior Capstone Design Project for From Teamwork to United Courses: Incorporation of Museum-Based Top Down Design Applied to the Aeronautical and Astronautical Preparing Undergraduate Students Summary of a Decade’s Reforms Service Learning into an Aerospace Aerospace Engineering Senior Engineering Major Selection in for Work in a Research and on Undergraduate Aircraft Design Engineering Course Capstone Program First-Year Engineering Students Engineering Environment Education M. Martin, P. Davis, D. Bowles, M. T. Gielda, A. Lee, B. Kirkpatrick, Iowa K. Kecskemety, R. Kajfez, Ohio State V. Naoumov, N. Al Masoud, H. Nguyen, E. H. Liu, C. Wen, K. Sun, M. Luo, Y. Zhou, Lima, Louisiana State University, Baton State University, Ames, IA University, Columbus, OH Patallo, A. Mocarski, Central Connecticut Beihang University, Beijing, China Rouge, LA State University, New Britain, CT Thursday, 7 January 2016 385-FD-47 CFD: Multiphase and Multi-Species Flows Pier Chaired by: M. LIOU, NASA Glenn Research Center 1400 hrs 1430 hrs 1500 hrs 1530 hrs AIAA-2016-1806 AIAA-2016-1807 AIAA-2016-1808 AIAA-2016-1809 Development of a VOF-Based Improved Weighted Compact A High-Order Finite-Volume Method Numerical simulation of laser Interface Capturing Method Using Nonlinear Scheme for Flows with for Combustion energy deposition near a wall a Family of Bounded Compressive Shocks and Material Interfaces: X. Gao, L. Owen, S. Guzik, Colorado State S. Ghosh, Indian Institute of Technology Flux Blending Schemes in an Algorithm and Assessment University, Fort Collins, CO Madras, Chennai, India Existing Finite Volume Flow Solver M. Wong, S. Lele, Stanford University, R. Smith, Naval Surface Warfare Center, Stanford, CA Panama City, FL Thursday, 7 January 2016 386-FD-48 Exploiting Hardware and Software Advances in CFD Cove Chaired by: Q. WANG, MIT 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs AIAA-2016-1810 AIAA-2016-1811 AIAA-2016-1812 AIAA-2016-1813 AIAA-2016-1814 AIAA-2016-1815 AIAA-2016-1816 Data Assimilated Computational Extending a Three-Dimensional Enabling Performance Optimization Towards Portability For A On the Use of Discrete Nonlinear OpenACC directive-based GPU Further Development of the Navier- Fluid Dynamics Algorithm for GPU RANS Solver for Unsteady Grid of CFD Applications with Source-to- Compressible Finite-Volume CFD Reduced-Order Models for the acceleration of an implicit Stokes Equations-Based Mean Flow Combustion Motion and Free-Wake Coupling Source Compiler Technology Code Prediction of Steady-State Flows reconstructed discontinuous Perturbation Technique X. Gao, Y. Wang, N. Overton, I. May, D. Jude, J. Baeder, University of Maryland, J. Riley, X. Gao, S. Guzik, Colorado State D. Curran, C. Allen, S. McIntosh-Smith, Past Parametrically Deformed Galerkin method for compressible M. Waindim, S. Bhaumik, D. Gaitonde, Colorado State University, Fort Collins, College Park, College Park, MD University, Fort Collins, CO University of Bristol, Bristol, United Complex Geometries flows on 3D unstructured grids Ohio State University, Columbus, OH CO; X. Tu, University of Kansas, Lawrence, Kingdom; D. Beckingsale, University of K. Washabaugh, C. Farhat, C. Othmer, J. Lou, North Carolina State University, Lawrence, KS Warwick, Coventry, United Kingdom Stanford University, Stanford, CA Raleigh, NC; Y. Xia, Idaho National Laboratory, Idaho Falls, ID; L. Luo, H. Luo, J. Edwards, F. Mueller, North Carolina State University, Raleigh, NC Thursday, 7 January 2016 387-FD-49 Flow-Control Actuators Cortez Hill C Chaired by: L. PACK MELTON, NASA-Langley Research Center and J. BONS, Ohio State University 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs AIAA-2016-1817 AIAA-2016-1818 AIAA-2016-1819 AIAA-2016-1820 AIAA-2016-1821 AIAA-2016-1822 AIAA-2016-1823 Active Flow Control Using Sweeping Unsteady Flow Simulation of a Flow response to multi-spark and Aerodynamic Load Control through Control of fluid flows using Control of Leading-Edge Airfoil Stall Physics and Control of the Flow Jet Actuators on a Semi-Span Wing Sweeping Jet Actuator Using a Lattice- multi-jet flow actuation Blowing multivariate spline reduced order Using Pulsed Jets over Generic Diamond Shaped Model Boltzmann Method N. Yurchenko, P. Vynogradskyy, K. N. Al-Battal, D. Cleaver, I. Gursul, models K. Hipp, M. Walker, S. Benton, J. Bons, Wing L. Pack Melton, M. Koklu, NASA Langley B. Duda, E. Fares, M. Wessels, Exa Kuzmenko, National Academy of Sciences, University of Bath, Bath, United Kingdom H. Tol, C. de Visser, M. Kotsonis, Delft Ohio State University, Columbus, OH S. Endrikat, B. Roentsch, J. Little, L. Research Center, Hampton, VA Corporation, Stuttgart, Germany; V. Vatsa, Kiev, Ukraine University of Technology, Delft, The Taubert, I. Wygnanski, University of NASA Langley Research Center, Hampton, VA Netherlands Arizona, Tucson, Tucson, AZ Thursday, 7 January 2016 388-FD-50 Flux Reconstruction/Correction Procedure via Reconstruction (FR/CPR) Harbor F Chaired by: H. HUYNH, NASA Glenn Research Center and D. BODONY, University of Illinois at Urbana-Champaign 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2016-1824 AIAA-2016-1825 AIAA-2016-1826 AIAA-2016-1827 AIAA-2016-1828 AIAA-2016-1829 Equivalence between the Energy Extension of the Flux Adaptive RANS Solution with the A high-order flux reconstruction solver A High-Order Dual-Time Stepping Adjoint-based Mesh Adaptation for Stable Flux Reconstruction and Reconstruction Method to High-order Correction Procedure for unsteady incompressible Navier- FR/CPR Method for Unsteady the 3D Navier-Stokes Equations Filtered Discontinuous Galerkin Triangular Elements using via Reconstruction Method Stokes equations on unstructured grids Incompressible Navier-Stokes with the High-order CPR Method Schemes: Numerical Validation Collapsed-Edge Quadrilaterals L. Shi, C. Zhou, Z. Wang, University of with implicit time stepping Equations on Unstructured Moving L. Shi, Z. Wang, University of Kansas, P. Zwanenburg, S. Nadarajah, McGill J. Romero, A. Jameson, Stanford Kansas, Lawrence, Lawrence, KS C. Cox, C. Liang, M. Plesniak, George Grids Lawrence, Lawrence, KS University, Montréal, Canada University, Stanford, CA Washington University, Washington, D.C. L. Wang, M. Yu, University of Maryland, Baltimore County, Baltimore, MD Thursday, 7 January 2016 389-FD-51 RANS/LES of Separated Flows Harbor E Chaired by: D. RIZZETTA 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs AIAA-2016-1830 AIAA-2016-1831 AIAA-2016-1832 AIAA-2016-1833 AIAA-2016-1834 AIAA-2016-1835 AIAA-2016-1836 Simulation of Wing and Nacelle Stall Numerical investigation of flow Detached-Eddy Simulation of flow Low- and Medium-Frequency A Novel Zonal RANS-DES Method Realizable Dynamic Large Eddy Application of a Lattice-Boltzmann R. Radespiel, D. Francois, D. Hoppmann, separation from aircraft tail past a pitching NACA 0015 airfoil Unsteadinesses in a Transitional for Prediction of Accelerated and Simulation of Separated Flows Method to the Separated Flow over S. Klein, P. Scholz, Technical University of surfaces. with pulsed actuation Shock--Boundary Reflection with Separated Flow R. Mokhtarpoor, S. Heinz, M. Stoellinger, the NASA Hump Braunschweig, Braunschweig, Germany; K. A. Masi, J. Cui, P. Tucker, University of L. Wang, L. Li, S. Fu, Tsinghua University, Separation H. Kalsi, P. Tucker, University of University of Wyoming, Laramie, Laramie, B. Duda, E. Fares, Exa GmbH, Stuttgart, Wawrzinek, University of Stuttgart, Stuttgart, Cambridge, Cambridge, United Kingdom Beijing, China L. Larchevêque, Aix-Marseille University, Cambridge, Cambridge, United Kingdom WY; P. Balakumar, NASA Langley Research Germany Germany; et al. Marseille, France Center, Hampton, VA

Thursday, 7 January 2016 390-FD-52 Reacting Flows Promenade B Chaired by: E. HASSAN, Air Force Research Laboratory and M. IHME, Stanford University 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2016-1838 AIAA-2016-1839 AIAA-2016-1840 AIAA-2016-1841 AIAA-2016-1842 AIAA-2016-1843 Compressible Flamelet Model in a Global Analysis of Premixed Identification of unstable coherent High-Speed Flow Field The Effect of Soot nano-Particles The Effects of Baffle Plate on Rule-Based Turbulent Combustion Combustion with Swirl and Vortex modes in reacting swirling flows Measurements of Turbulent Jet Injection on Two-Phase Smoke Aerosol Soot Nano-Aerosol and Pollutant Solver Breakdown and their control Flames Undergoing Shear Layer Formation in a Kerosene-Fired Burner Productions in a JP-Fueled Combustor S. Thakur, J. Wright, Streamline Numerics, Z. Rusak, J. Choi, N. Bourquard, C. Paschereit, Technical University of Manipulation M. Darbandi, M. Ghafourizadeh, Sharif M. Darbandi, M. Ghafourizadeh, Sharif Inc., Gainesville, FL; M. Ihme, Stanford Rensselaer Polytechnic Institute, Troy, Berlin, Berlin, Germany H. Nawroth, C. Paschereit, Technical University of Technology, Tehran, Iran ; G. University of Technology, Tehran, Iran ; G. University, Stanford, CA NY; S. Wang, University of Auckland, University of Berlin, Berlin, Germany Schneider, University of Waterloo, Waterloo, Schneider, University of Waterloo, Waterloo, Auckland, New Zealand Canada Canada Thursday, 7 January 2016 391-FD-53 Vortex Flows II: Experimental Investigations Promenade A Chaired by: I. GURSUL, University of Bath 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs AIAA-2016-1844 AIAA-2016-1845 AIAA-2016-1846 AIAA-2016-1847 AIAA-2016-1848 Transient, Three-Dimensional A Statistical Approach to the Experimental study of tip vortex Wingtip Vortex Behavior in the Interaction of Trailing Vortices with Disturbances Interacting with a High- Identification of Vortical Structures flow from a periodically pitched Vicinity of the Maximum Lift to Downstream Wings Lift Airfoil - Wind Tunnel Experiments During Dynamic Stall with Flow airfoil section Drag Ratio Lift Condition C. Chen, Z. Wang, D. Cleaver, I. Gursul, S. Klein, P. Scholz, R. Radespiel, Technical Control K. Zaman, A. Fagan, M. Mankbadi, NASA M. Memon, A. Altman, University of University of Bath, Bath, United Kingdom University of Braunschweig, Braunschweig, K. Taylor, M. Amitay, Rensselaer Glenn Research Center, Cleveland, OH Dayton, Dayton, OH Germany Polytechnic Institute, Troy, NY Thursday, 7 January 2016 392-GNC-32 Invited Session: Interval Management: Avionics Algorithms and Performance Analysis Coronado B Chaired by: I. LEVITT, Federal Aviation Administration and L. WEITZ, The MITRE Corporation 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2016-1849 AIAA-2016-1850 AIAA-2016-1851 AIAA-2016-1852 AIAA-2016-1853 AIAA-2016-1854 Modeling Uncertainty in Inter- Defining an Error Budget for Development of an Interval Evaluating the Impact of Estimated Designing Stochastic Optimal Closing The Loop: Testing for IM aircraft Spacing Between the Final Required Interval Management Management Algorithm for Time of Arrival Accuracy on Control Laws for Interval Avionics Certification Approach Fix and the Runway Performance Delayed Traffic Interval Management Performance Management S. Bowman, D. Elliott, MITRE Corporation, Threshold L. Weitz, MITRE Corporation, McLean, VA; B. Barmore, K. Swieringa, M. X. Bai, Rutgers University, Piscataway, NJ; T. Gaydos, L. Weitz, MITRE Corporation, McLean, VA; B. Perez, Regulus Group, H. Stassen, L. Weitz, S. Priess, MITRE I. Levitt, Federal Aviation Administration, Underwood, NASA Langley Research L. Weitz, S. Priess, MITRE Corporation, McLean, VA Galloway, NJ; D. Walker, Federal Aviation Corporation, McLean, VA Atlantic City, NJ; J. Martensson, Center, Hampton, VA; T. Abbott, Stinger McLean, VA Administration, Washington, D.C. EUROCONTROL, Brussels, Belgium Ghaffarian Technologies, Inc., Hampton, VA; R. Leonard, Virginia Commonwealth University, Richmond, VA Thursday, 7 January 2016 393-GNC-33 Novel Navigation, Estimation and Tracking II Hillcrest A Chaired by: M. INNOCENTI, University of Pisa and W. FICHTER, University of Stuttgart 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs AIAA-2016-1855 AIAA-2016-1856 AIAA-2016-1857 AIAA-2016-1858 AIAA-2016-1859 AIAA-2016-1860 AIAA-2016-1861 Adaptive Estimation of Nonlinear Norm-constrained Unscented Application of Active-Passive Smooth Singularity Free Solution A Dynamic Sensor Tasking State-Dependent Adaptive Predictive Modeling of Pedestrian Spacecraft Attitude Dynamics with Kalman Filter with Application to Dynamic Consensus Filter Approach to the Three-Dimensional Bearings- Strategy for Tracking Maneuvering Estimation for Impulsively Motion Patterns with Bayesian Time-Varying Moments of Inertia High Area-to-Mass Ratio Space- to Multitarget Tracking Problem for Only Tracking Problem Spacecraft using Multiple Models Maneuvering Spacecraft Tracking Nonparametrics Using On-Board Sensors Debris Tracking Situational Awareness in Unknown L. Schmitt, W. Fichter, University of G. Goff, Air Force Institute of Technology, S. Lee, I. Hwang, Purdue University, West Y. Chen, M. Liu, S. Liu, J. Miller, J. How, J. Hess, E. Swenson, Air Force Institute S. Chee, McGill University, Montréal, Environments Stuttgart, Stuttgart, Germany Wright-Patterson AFB, OH; J. Black, Lafayette, IN Massachusetts Institute of Technology,

of Technology, Wright-Patterson AFB, OH; Canada; J. Forbes, University of Michigan, J. Peterson, T. Yucelen, Missouri University Virginia Polytechnic Institute and State Cambridge, MA F. Leve, Air Force Research Laboratory, Ann Arbor, Ann Arbor, MI of Science and Technology, Rolla, MO University, Blacksburg, VA; J. Beck, Kirtland AFB, NM; J. Black, Virginia Air Force Research Laboratory, Wright- Polytechnic Institute and State University, Patterson AFB, OH; J. Hess, Air Force Blacksburg, VA; G. Goff, Air Force Institute Institute of Technology, Wright-Patterson of Technology, Wright-Patterson AFB, OH AFB, OH Thursday, 7 January 2016 394-GNC-34/ACD-12 Aircraft GNC II Hillcrest C Chaired by: J. HENRICKSON, Texas A&M University and M. OPPENHEIMER, AFRL/RBCA 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2016-1862 AIAA-2016-1863 AIAA-2016-1864 AIAA-2016-1865 AIAA-2016-1866 AIAA-2016-1867 Cooperative Control for Missile Virtual Model Control of Rotorcraft Shape Control of Tensegrity Airfoils Enforcing State Constraints on a Differential Game-Based Control Integrated Control and Display Evasion with Articulated Landing Gear for J. Henrickson, Texas A&M University, Model of a Hypersonic Vehicle Law for Stabilization of Aeroelastic Augmentation for Manual Remote R. Carr, J. Torf, R. Cobb, Air Force Institute Shipboard Landing College Station, TX; R. Skelton, University D. Famularo, J. Valasek, Texas A&M System with Gust Load Flight Control in the Presence of of Technology, Wright-Patterson AFB, OH D. Kim, M. Costello, Georgia Institute of of California, San Diego, La Jolla, CA; J. University, College Station, TX; J. P. Ghorawat, University of Nevada, Las Large Latency Technology, Atlanta, GA Valasek, Texas A&M University, College Muse, M. Bolender, Air Force Research Vegas, Las Vegas, NV; K. Lee, Catholic F. Zhang, T. Fricke, F. Holzapfel, Technical Station, TX Laboratory, Wright-Patterson AFB, OH Kwandong University, Gangwon, South University of Munich, Munich, Germany Korea ; S. Singh, University of Nevada, Las Vegas, Las Vegas, NV Thursday, 7 January 2016 395-GNC-35 Trajectory Design Cortez Hill B Chaired by: D. DOMAN, Air Force Research Laboratory and W. WHITACRE, Draper Laboratory 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs AIAA-2016-1868 AIAA-2016-1869 AIAA-2016-1870 AIAA-2016-1871 AIAA-2016-1872 AIAA-2016-1873 AIAA-2016-1874 Trajectory Specification for Performance Characterization of Efficient Approximation of Optimal Augmenting Wireless Time-of- An Optimization Paradigm for G3-Continuous Trajectory Design Fast Generation of Landing Paths Automation of Terminal Air Traffic Tightly-Coupled GNSS Precise Point High-Order Kinematic Trajectories Arrival Positioning with Terrain Arrival Trajectories usingTrajectory For Fixed-Wing Aircraft Based On for Fixed-Wing Aircraft with Thrust Control Positioning Inertial Navigation J. Mooney, E. Johnson, Georgia Institute of Elevation Measurements for Segmentation and State 6-DoF Kinematics Failure R. Paielli, NASA Ames Research Center, within a Simulation Environment Technology, Atlanta, GA Navigation in absence of GPS Parameterization M. Gros, W. Fichter, University of J. Stephan, W. Fichter, University of Moffett Field, CA R. Watson, V. Sivaneri, J. Gross, West B. Copp, K. Subbarao, University of Texas, H. Yu, E. Van Kampen, J. Mulder, Delft Stuttgart, Stuttgart, Germany Stuttgart, Stuttgart, Germany Virginia University, Morgantown, WV Arlington, Arlington, TX University of Technology, Delft, The Netherlands Thursday, 7 January 2016 396-GNC-36 Missile Autopilots and Integrated Guidance & Control Hillcrest B Chaired by: S. FLEISCHMAN, French-German Institute of Saint-Louis (ISL) and G. STRUB, University of Haute-Alsace 1400 hrs 1430 hrs 1500 hrs 1530 hrs AIAA-2016-1875 AIAA-2016-1876 AIAA-2016-1877 AIAA-2016-1878 Skid-To-Turn Autopilot Design and Extended Kalman Filter Based Integrated guidance and control of Acceleration-free Nonlinear Validation for an Experimental Robust Altitude Controller for Sea agile missiles using the Finite-SDRE Guidance and Tracking Control of Guided Projectile Prototype Skimming Missiles approach Hypersonic Missiles for Maximum G. Strub, French-German Research Institute O. Dulgar, R. Gezer, ROKETSAN Missile J. Yang, Z. Wang, Nanjing University of Target Penetration of Saint-Louis (ISL), Saint-Louis, France; Industries, Inc., Ankara, Turkey; A. Kutay, Science and Technology, Nanjing, China S. Mehta, C. Ton, University of Florida, M. Basset, University of Upper Alsace, Middle East Technical University, Ankara, Shalimar, Shalimar, FL; W. Mackunis, Mulhouse, France Turkey Embry-Riddle Aeronautical University,

Daytona Beach, FL Thursday, 7 January 2016 397-GT-8 Model Attitude, Deformation, and Data Acquisition Techniques (Invited) Hillcrest D Chaired by: R. GUYTON, USAF Wright Lab and B. WILLIAMS, The Aerospace Corporation 1400 hrs 1430 hrs 1500 hrs 1530 hrs AIAA-2016-1879 Oral Presentation Oral Presentation Oral Presentation Development of an Active Damping On-board Remote Model Attitude Projection Moiré Interferometry Model Deformation Methods at System for use with a Single Strut Sensor for the ARFL Vertical Wind Measurement System for Rotorcraft ETW - Recent Applications and Mount Tunnel Applications Ongoing Developments J. Pereira, National Research Council P. Smith, Air Force Research Laboratory, M. Sekula, NASA Langley Research Center, H. Quix, European Transonic Windtunnel, Canada, Ottawa, Canada Wright-Patterson AFB, OH Hampton, VA Cologne, Germany Thursday, 7 January 2016 398-GTE-13 Noise Old Town A Chaired by: B. KIEL, Air Force Reseach Laboratory and S. GOGINENI, Spectral Energies, LLC 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2016-1880 AIAA-2016-1881 AIAA-2016-1882 AIAA-2016-1883 AIAA-2016-1884 AIAA-2016-1885 Level-educed Wavepacket Direct Combustion Noise Simulation Reynolds-Averaged Navier-Stokes An acoustic investigation of a Acoustics from a Rectangular C-D Impact of Scale on the Acoustics Representation of Noise Radiation of a Lean Premixed Swirl Flame Solutions and Noise Predictions for supersonic, multi-stream jet with Nozzle Exhausting Over a Flat from a Conical C-D Nozzle from a High-Performance Military using Stochastic Sound Sources Three-Stream Jets aft deck: Characterization and Surface Interacting with a Flat Surface Aircraft F. Grimm, D. Ohno, S. Werner, M. S. Leib, Ohio Aerospace Institute, acoustically-optimal operating P. Mora , F. Baier, E. Gutmark, University F. Baier, P. Mora , E. Gutmark, University T. Neilsen, K. Gee, B. Harker, Brigham Stöhr, German Aerospace Center (DLR), Cleveland, OH; N. Georgiadis, D. Yoder, conditions of Cincinnati, Cincinnati, OH; K. of Cincinnati, Cincinnati, OH; K. Young University, Provo, UT; M. James, Stuttgart, Germany; R. Ewert, J. Dierke, NASA Glenn Research Center, Cleveland, M. Berry, A. Magstadt, M. Glauser, Syracuse Kailasanath, Naval Research Laboratory, Kailasanath, Naval Research Laboratory, Blue Ridge Research and Consulting, LLC, German Aerospace Center (DLR), OH University, Syracuse, NY; C. Ruscher, S. Washington, D.C. Washington, D.C. Asheville, NC Braunschweig, Germany; et al. Gogineni, Spectral Energies, LLC, Dayton, OH; B. Kiel, Air Force Research Laboratory, Wright- Patterson AFB, OH Thursday, 7 January 2016 399-GTE-14 Experimental tools Old Town B Chaired by: R. ANTHONY and S. LAVAGNOLI, von Karman Institute for Fluid Dynamics 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs AIAA-2016-1886 AIAA-2016-1887 AIAA-2016-1888 AIAA-2016-1889 AIAA-2016-1890 AIAA-2016-1891 AIAA-2016-1892 Experimental investigation of high Uncertainty Analysis of Blade Tip Modeling Far-field Acoustical The Application of Stereoscopic A new thrust stand for testing Measurements and Predictions of Separation Control in a 140 temperature erosion resistance of Timing Methods and Reduced Order Nonlinearity from F-35 Aircraft PIV in a Liquid-Fueled Gas Turbine multi-stream and heat simulated the Three-Dimensional Boundary degree Bend Channel Using AC thermal barrier coating via design Modeling of Integrally Bladed during Ground Run-up Combustor supersonic nozzles Layer in a Turbine Blade Passage and Plasma-sliding-discharge DBD of experiment Rotors B. Reichman, Brigham Young University, A. Pratt, R. Zhang, R. Lucht, C. Slabaugh, J. Valdez, C. Tinney, University of Texas, S. Lynch, Pennsylvania State University, Actuators D. Shin, A. Hamed, University of A. Kamaraj, V. Yadav, S. Venkataraman, Provo, UT; A. Wall, Air Force Research Purdue University, West Lafayette, IN Austin, Austin, TX University Park, PA M. Arthur, T. Samper, T. Corke, University Cincinnati, Cincinnati, OH San Diego State University, San Diego, CA Laboratory, Wright-Patterson AFB, OH; K. of Notre Dame, Notre Dame, IN; D. Gee, T. Neilsen, Brigham Young University, Frias, D. Hanson, N. Nolcheff, Honeywell Provo, UT; J. Downing, M. James, Blue International, Inc., Phoenix, AZ Ridge Research and Consulting, LLC, Asheville, NC; et al. Thursday, 7 January 2016 400-HIS-5 History of AIAA Americas Cup A Chaired by: K. BURNS, Northrop Grumman Corporation 1400 hrs 1430 hrs AIAA-2016-1893 AIAA-2016-1894 The History of the San Diego IAS Howard Marx - The extraordinary Building - Currently the San Diego life of an aerospace engineer Harbor Police Building L. Sweeney, Northrop Grumman K. Burns, AIAA San Diego Section, San Corporation, San Diego, CA

Diego, CA Thursday, 7 January 2016 401-SAT-1 Society and Aerospace Technology Americas Cup A Chaired by: B. STEINFELDT, Georgia Institute of Technology and J. CHRISTIAN, West Virginia University 1400 hrs 1600 hrs 1630 hrs 1700 hrs No Presentations AIAA-2016-1895 AIAA-2016-1896 AIAA-2016-1897 Applications of UAV in Daily Life Advancing Socially Disruptive Medical Astrosociology and Space Z. Shahid, A. Rashid, Ghulam Ishaq Khan Aerospace Technologies Through Medicine: Bringing Together the Institute, Topi, Pakistan Venture Capital Investment Two Branches of Science J. Taylor, J. Matthews, Self, Washington, D.C J. Pass, Astrosociology Research Institute, Huntington Beach, CA Thursday, 7 January 2016 402-HSABP-7 Computational Analysis of Scramjets Regatta A Chaired by: H. HASSAN, North Carolina State University and V. TANGIRALA, General Electric 1400 hrs 1430 hrs 1500 hrs 1530 hrs AIAA-2016-1898 AIAA-2016-1899 AIAA-2016-1900 AIAA-2016-1901 Hybrid Reynolds-Averaged / Large Numerical Predictions of Mixing in Analysis of Combustion Closure A Computational Investigation of Eddy Simulation of Flow in a Model a Supersonic Cavity Flameholder Assumptions in a Dual-Mode Unstart in a Dual-Mode Scramjet SCRamjet Cavity Flameholder D. Peterson, Innovative Scientific Scramjet Combustor L. Riley, Ohio State University, Columbus, R. Baurle, NASA Langley Research Center, Solutions, Inc., Dayton, OH; E. Hassan, W. Chan, University of Michigan, Ann OH; M. Hagenmaier, J. Donbar, Air Force Hampton, VA Air Force Research Laboratory, Wright- Arbor, Ann Arbor, MI; M. Ihme, Stanford Research Laboratory, Wright-Patterson Patterson AFB, OH University, Stanford, CA AFB, OH; D. Gaitonde, Ohio State University, Columbus, OH Thursday, 7 January 2016 403-IS-11 Intelligent Mission Design and Vehicle Control Regatta B Chaired by: C. TSCHAN, The Aerospace Corporation and E. KIVELEVITCH, University of Cincinnati 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs AIAA-2016-1902 AIAA-2016-1903 AIAA-2016-1904 AIAA-2016-1905 AIAA-2016-1906 Design Exploration of a Low-Thurst Detection and Localization using Exploring Non-Aviation Information A Fuzzy Logic Approach for Low Empirical Dynamics Learning and Space Trajectory Problem for Unmanned Aerial Systems for Sources for Aircraft Emergency Altitude UAS Traffic Management Reduction of Motion-Primitive- DESTINY Mission Firefighting Applications Landing Planning (UTM) Based Pattern Generators with T. Watanabe, Japan Aerospace Exploration S. Kukreti, M. Kumar, K. Cohen, University P. Di Donato, National Civil Aviation B. Cook, K. Cohen, E. Kivelevitch, Applications to Flapping Wings Agency (JAXA), Sagamihara, Japan; T. of Cincinnati, Cincinnati, OH Agency, São José dos Campos, Brazil; E. University of Cincinnati, Cincinnati, OH I. Sledge, K. Mohseni, University of Tatsukawa, Tokyo University of Science, Atkins, University of Michigan, Ann Arbor, Florida, Gainesville, Gainesville, FL Shinjuku, Japan; T. Yamamoto, A. Oyama, Ann Arbor, MI Y. Kawakatsu, Japan Aerospace Exploration Agency (JAXA), Sagamihara, Japan Thursday, 7 January 2016 404-MDO-8 Sensitivity Derivations & Optimization Applications Balboa A Chaired by: G. KENNEDY, Georgia Institute of Technology and V. BALABANOV, Boeing Commercial Airplanes 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2016-1907 AIAA-2016-1908 AIAA-2016-1909 AIAA-2016-1910 AIAA-2016-1911 AIAA-2016-1912 A Scalable Adjoint Method for Shape Optimization for Two- Implementation of discrete adjoint Time-dependent Aero-acoustic Trajectory Optimization Procedure Multi-parametric high-order flow Coupled Flexible Multibody Dimensional Acoustic Metamaterials method for parameter sensitivity Adjoint-based Shape Optimization of for Interplanetary Transfers based sensitivity analysis Dynamics and Phononic Crystals with a Time- analysis in chemically reacting Helicopter Rotors in Forward Flight on Direct Collocation Method A. Hay, C. Belley, D. Pelletier, Defense G. Kennedy, Georgia Institute of Dependent Adjoint Formulation flows E. Fabiano, A. Mishra, D. Mavriplis, University D. Somavarapu, E. Wahl, A. Westfall, K. Research and Development Canada, Technology, Atlanta, GA W. Lin, W. Anderson, J. Newman, M. Esfahani, G. Houzeaux, Barcelona of Wyoming, Laramie, Laramie, WY; K. Mani, Turkoglu, San Jose State University, San Montréal, Canada

X. Zhang, University of Tennessee, Supercomputing Center, Barcelona, Spain Rolls-Royce Group plc, Indianapolis, IN Jose, CA Chattanooga, Chattanooga, TN Thursday, 7 January 2016 405-MST-12 Computational Methods I Golden Hill B Chaired by: M. CARTER, NASA-Langley Research Center and P. GRANT, University of Toronto 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2016-1913 AIAA-2016-1914 AIAA-2016-1915 AIAA-2016-1916 AIAA-2016-1917 AIAA-2016-1918 Numerical Investigation of Scale Ice release phenomena modelled A VPM/CFD Coupling Methodology Modeling and simulation of Exploration of POD-Galerkin Multistep Simulation for Three- Factor in Composites Applying by Finite Element models to Study Rotor/Ship Aerodynamic the thermal performance of Techniques for Developing dimensinal Ice Accretion on an Extended Finite Element Method R. Milanese, R. Scigliano, V. De Simone, Interaction a stratospheric airship with Reduced Order Models of the Euler Aircraft Wing P. Behroozinia, J. Bayandor, R. Mirzaeifar, V. Carandente, Italian Aerospace Research N. Rajmohan, C. He, Advanced Rotorcraft photovoltaic array Equations J. Huang, S. Nie, Y. Cao, Beihang Virginia Polytechnic Institute and State Center (CIRA), Capua, Italy Technology, Inc., Sunnyvale, CA Q. Liu, Y. Yang, Z. Li, J. Cai, Chinese C. Huang, W. Anderson, C. Merkle, Purdue University, Beijing, China; Y. Yao, University, Blacksburg, VA Academy of Sciences, Beijing, China University, West Lafayette, IN University of the West of England, Bristol, United Kingdom; J. Yao, University of Lincoln, Lincoln, United Kingdom Thursday, 7 January 2016 406-MST-13 Model and Simulation Verification and Validation Golden Hill A Chaired by: S. KOWALCHUK, Sandia National Laboratories and T. BURRESS, Lockheed Martin Corporation 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs AIAA-2016-1919 AIAA-2016-1920 AIAA-2016-1921 AIAA-2016-1922 AIAA-2016-1923 Validation Process of the Physics- Upgrades to the Horizon Simulation A Systematic LPV/LFR Modelling An overview of Model-Based Consistent Behavioral Abstractions based Modeling of Navigation Framework: Dynamic Model Approach Optimized for Linearised Development Verification/ of Experimental Frame Sensors for Sea-based Aviation Creation, Scripting, and Multi- Gain Scheduling Control Synthesis Validation Processes and S. Ponnusamy, Airbus, Toulouse, France; Automated Landing thread Support S. Fleischmann, S. Theodoulis, French- Technologies in the Aerospace V. Albert, National Center for Scientific N. Good, O. Aboutalib, B. Thai, N. B. Butler, L-3 Communications, Poway, German Research Institute of Saint-Louis Industry Research (CNRS), Toulouse, France; P. Yamaoka, Northrop Grumman Corporation, CA; E. Mehiel, California Polytechnic State (ISL), Saint-Louis, France; E. Laroche, J. Allen, dSPACE Inc., Wixom, MI Thebault, Airbus, Toulouse, France Redondo Beach, CA; C. Kim, Northrop University, San Luis Obispo, CA University of Strasbourg, Illkirch, France; Grumman Corporation, Rolling Meadows, E. Wallner, MBDA, Schrobenhausen, IL; C. Wilkinson, Naval Air Systems Germany; J. Harcaut, MBDA, Paris, France Command, Patuxent River, MD; et al. Thursday, 7 January 2016 407-MVC-2 Geometry & Computational Environments Nautical Chaired by: G. POWER, Aerospace Testing Alliance and J. DANNENHOFFER, Syracuse University 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs AIAA-2016-1924 AIAA-2016-1925 AIAA-2016-1926 AIAA-2016-1927 AIAA-2016-1928 AIAA-2016-1929 AIAA-2016-1930 CGNS test suites for CFD software Generation of Multi-fidelity, Multi- Generation of Parametric Aircraft NASA CFD Vision 2030 Visualization In Situ Infrastructure Enhancements Snapshot Lagrangian Proper Unstructured mesh adaptation for components discipline Air Vehicle Models with Models from a Cloud of Points and Knowledge Extraction: Panel for Data Extract Generation Orthogonal Decomposition of functional outputs. With application M. Poinot, ONERA, Châtillon, France the Engineering Sketch Pad P. Jia, J. Dannenhoffer, Syracuse Summary from AIAA AVIATION 2015 B. Whitlock, S. Legensky, Intelligent Light, Cylinder Wake Flow to two dimensionnal invscid flows. J. Dannenhoffer, Syracuse University, University, Syracuse, NY Conference Rutherford, NJ; J. Forsythe, Naval Air J. Rossetti, J. Dannenhoffer, M. Green, J. Peter, ONERA, Châtillon, France; J.

Syracuse, NY; R. Haimes, Massachusetts E. Duque, Intelligent Light, Rutherford, NJ; S. Systems Command, Patuxent River, MD Syracuse University, Syracuse, NY Desideri, French National Institute for Institute of Technology, Cambridge, MA Imlay, TecPlot, Inc., Bellevue, WA; S. Ahern, Research in Computer Science and Control Computational Engineering International, (INRIA), Sophia-Antipolis, France Apex, NJ; C. Guoning, University of Houston, Houston, TX; D. Kao, NASA Ames Research Center, Moffett Field, CA Thursday, 7 January 2016 408-PANEL-11 Thursday Afternoon Forum 360 Seaport F-G 1400 - 1600 hrs Learning from Hollywood Moderator: Rick Loverd, Program Director, The Science & Entertainment Exchange, National Academy of Sciences Thursday, 7 January 2016 409-MAT-10 Work Force Development for Integrated Computational Materials Engineering Gaslamp B 1400 - 1700 hrs

C. Robert Kenley Sankaran Mahadevan John F. Matlik Ben H. Thackerr Purdue University Vanderbilt University Rolls-Royce Corporation Southwest Research Institute Thursday, 7 January 2016 410-PC-16 Rocket & Air-Breathing Combustion I - Combustion Instabilities, Supercritical Conditions Harbor B Chaired by: D. TALLEY, and B. HITCH, Reaction Systems 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs AIAA-2016-1931 AIAA-2016-1932 AIAA-2016-1933 AIAA-2016-1934 AIAA-2016-1935 Application of Detailed Chemical Low-Probability Events Leading Effects of Kerosene Annulus Length on Direct numerical simulation of Simulation of high-pressure Kinetics to Combustion Instability to Rocket Engine Combustion Mixing Characteristics of Swirl Coaxial transcritical turbulent boundary layers methane flames Modeling Instability Injectors at Supercritical Conditions at supercritical pressures with strong G. Ribert, P. Domingo, X. Petit, National M. Harvazinski, D. Talley, V. Sankaran, Air P. Popov, A. Sideris, W. Sirignano, X. Wang, V. Yang, Georgia Institute of real fluid effects Center for Scientific Research (CNRS), Force Research Laboratory, Edwards AFB, CA University of California, Irvine, Irvine, CA Technology, Atlanta, GA S. Kawai, Tohoku University, Sendai, Japan Rouen, France Thursday, 7 January 2016 411-PC-17 Turbulent Combustion III - Large-Eddy Simulations Harbor C Chaired by: J. OEFELEIN, Sandia National Laboratories and A. COMER, Air Force Institute of Technology 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs AIAA-2016-1936 AIAA-2016-1937 AIAA-2016-1938 AIAA-2016-1939 AIAA-2016-1940 AIAA-2016-1941 AIAA-2016-1942 Modeling and Simulation of Bluff LES Model Assessment for High Simulation of the Cold Flow in a Large Eddy Simulation of a Large eddy simulation of a Flamelet Modeling Studies of a Experimental and numerical Body Stabilized Turbulent Premixed Speed Combustion Ramp-Cavity Combustor Using a Supercritical Fuel Jet in Cross Flow turbulent premixed jet flame using Continuously Variable Resonance investigation into the propagation Flames C. Patton, T. Wignall, J. Edwards, T. DSEM-LES/FMDF Hybrid Scheme using GPU-Acceleration flamelet-generated manifolds Combustor of entropy waves in a small-scale A. Comer, Air Force Institute of Technology, Echekki, North Carolina State University, J. Komperda, Z. Ghiasi, D. Li, F. Mashayek, K. Gottiparthi, R. Sankaran, Oak Ridge W. Song, B. Lee, H. Im, King Abdullah T. Pant, C. Huang, C. Han, S. rig Wright-Patterson AFB, OH; C. Huang, Raleigh, NC University of Illinois, Chicago, Chicago, National Laboratory, Oak Ridge, TN; J. University of Science and Technology, Sardeshmukh, W. Anderson, H. Wang, A. Giusti, N. Worth, E. Mastorakos, Purdue University, Purdue University , IN; IL; A. Irannejad, F. Jaberi, Michigan State Oefelein, Sandia National Laboratories, Thuwal, Saudi Arabia; A. Donini, A. Purdue University, West Lafayette, IN A. Dowling, University of Cambridge, B. Rankin, M. Harvazinski, V. Sankaran, University, East Lansing, MI Livermore, CA Fancello, J. van Oijen, Eindhoven Cambridge, United Kingdom Air Force Research Laboratory, Wright- University of Technology, Eindhoven, The Patterson AFB, OH Netherlands ; et al. Thursday, 7 January 2016 412-PDL-12 Plasma Propulsion Ocean Beach Chaired by: S. ROY, University of Florida and K. XU 1400 hrs 1430 hrs 1500 hrs 1530 hrs AIAA-2016-1943 AIAA-2016-1944 AIAA-2016-1945 AIAA-2016-1946 Synchronized Measurement of Plasma Empirical Determination of Confined versus Unconfined Design of Magnetoplasmadynamic Characteristics In a Hall Effect Thruster Performance Characteristics for Analysis of Split Ring Resonator Thruster Incorporating Friction Stir D. Cunningham, D. Liu, C. Hartsfield, Air Busek 1cm Micro Radio-Frequency Microplasma Source in a Microwave Welding Technique Force Institute of Technology, Wright-Patterson Ion Propulsion System Electrothermal Thruster P. Johnson, Hindustan College of AFB, OH; C. Mullins, C. Farnell, J. Williams, C. Muilenburg, D. Liu, Air Force Institute of R. Dextre, K. Xu, University of Alabama, Engineering and Technology, Coimbatore, Colorado State University, Fort Collins, CO; Technology, Wright-Patterson AFB, OH Huntsville, Huntsville, AL India et al. Thursday, 7 January 2016 413-SCS-6 Spacecraft Solar Array Structures II Balboa B Chaired by: R. PAPPA, NASA Langley Research Center and J. FERNANDEZ 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2016-1947 AIAA-2016-1948 AIAA-2016-1949 AIAA-2016-1950 AIAA-2016-1951 AIAA-2016-1952 UltraFlex and MegaFlex – Shear Between Straight Ribs in The Wrapped Architecture for Large Ultralight Structures for Space Solar Robust, Highly Scalable Solar Array MakerSat: In-Space Additive Advancements in Highly Scalable Spirally Stowed Sheets Photo-Voltaic Arrays Power Satellites System Manufacturing of Large Truss Solar Power G. Greschik, TentGuild Engineering G. Greschik, TentGuild Engineering M. Arya, N. Lee, S. Pellegrino, California W. Francis, B. Davis, M. Lake, Roccor, LLC, Structures Using the Trusselator™ D. Murphy, M. Eskenazi, M. McEachen, J. Company, Boulder, CO Company, Boulder, CO Institute of Technology, Pasadena, CA Louisville, CO Technology Spink, ATK, Goleta, CA R. Hoyt, J. Slostad, J. Cushing, T. Moser, Tethers Unlimited, Inc., Bothell, WA Thursday, 7 January 2016 414-SD-12 System ID Balboa C Chaired by: V. HRISHIKESHAVAN, University of Maryland and W. WELSH, Sikorsky Aircraft Corporation 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2016-1953 AIAA-2016-1954 AIAA-2016-1955 AIAA-2016-1956 AIAA-2016-1957 AIAA-2016-1958 Identification of Nonlinear Dynamic Beam Solutions for Flight Shape Estimation of Very Efficient Clustering Algorithm Using Operational Modal Analysis of Modeling of Artificial Hair Sensors Aeroelastic Behavior of a Wing with Real-Time Simulation and Control Flexible Unmanned Aerial Vehicle Modal Assurance Criterion for a Rotating Cantilever Beam for Vibration Control of Flexible Pitching and Plunging Freeplay via Development of Flexible Rockets Z. Pang, C. Cesnik, University of Michigan, System Identification Using High-Speed Digital Image Wings Higher-Order Spectra Analysis W. Su, C. King, University of Alabama, Ann Arbor, Ann Arbor, MI Z. Wang, D. Sarhaddi, P. Chen, ZONA Correlation W. Su, University of Alabama, Tuscaloosa, M. Candon, H. Ogawa, R. Carrese, P. Tuscaloosa, Tuscaloosa, AL; S. Clark, E. Technology, Inc., Scottsdale, AZ S. Rizo-Patron, J. Sirohi, University of Tuscaloosa, AL; G. Reich, Air Force Marzocca, RMIT University, Melbourne, Griffin, a.i. solutions, Inc., Cape Canaveral, Texas, Austin, Austin, TX Research Laboratory, Wright-Patterson Australia FL; J. Suhey, M. Wolf, NASA Kennedy AFB, OH Space Center, Cape Canaveral, FL Thursday, 7 January 2016 415-SD-13 Flutter Gaslamp A Chaired by: A. SINHA, The Pennsylvania State University and T. BARTKOWICZ, Boeing Defense, Space & Security 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs AIAA-2016-1959 AIAA-2016-1960 AIAA-2016-1961 AIAA-2016-1962 AIAA-2016-1963 AIAA-2016-1964 AIAA-2016-1965 Classical aeroelastic stability Wind Tunnel Flutter Testing of a Development and Wind Tunnel Test Time to Flutter of a Maneuvering Uncertainties in vibratory mode Optimization of High Altitude Long Experimental investigation of an analysis of large composite wind Highly Swept All-Movable Wing of W-WING Whirl Flutter Aeroelastic Viscoelastic Goland Wing shapes and their effect on flutter Endurance (HALE) Vehicle Subject airfoil response under stall-induced turbine blades with a Control Surface Demonstrator C. Merrett, Carleton University, Ottawa, speeds to Flutter Speed Constraint pitching oscillations T. Farsadi, A. Kayran, Middle East Technical D. Pitt, B. Sexton, The Boeing Company, J. Cecrdle, J. Malecek, O. Vich, P. Malinek, Canada D. Pitt, The Boeing Company, St. Louis, K. Roughen, M. Baker, J. Robinson, M4 F. Marques, University of São Paulo, São University, Ankara, Turkey St. Louis, MO; K. Byun, Agency for Aeronautical Research and Test Institute MO; P. Bansal, The Boeing Company, New Engineering, Inc., Long Beach, CA; Z. Liu, Carlos, Brazil; R. Vasconcellos, São Paulo Defense Development, Daejeon, South (VZLÚ), Prague, Czech Republic Delhi, India Facebook, Woodland Hills, CA State University, São Joao da Boa Vista,

Korea Brazil; D. Pereira, University of São Paulo, São Carlos, Brazil Thursday, 7 January 2016 416-SOF-8/UMS-9/IS-12 Assurance of Autonomy Symposium IV Coronado A 1400 - 1730 hrs Assurance Tools and Techniques for Trusted Autonomy

In this session, we explore new concepts and methods to facilitate the Verification and Validation (V&V) and Certification of increasingly autonomous systems. Topics that will be addressed include tools and techniques that can be used to assess and assure Safety and Security, as well as engender trust in increasingly autonomous systems, on the behalf of designers, evaluators, users and the general public will be investigated.

We begin with a panel discussion to address these issues, via an interactive Q&A session with the audience. The audience questions will be used to drive and derive directions for investigation that will be captured by the moderators in the report-out. We will then form moderated breakout groups based on the previously identified barriers to assurance, and then identify promising research and development areas.

1400 - 1500 hrs Panelists: Lee Pike Natarajan Shankar Cristoph Torens Darren Cofer Irene Gregory Galois SRI German Aerospace Center (DLR) Rockwell Collins NASA Langley Research Center

1515 - 1730 hrs Breakout Session We ask that the audience revisit the barriers generated during the previous day and identify promising technologies for autonomy assurance. Thursday, 7 January 2016 417-STR-14 Composite Laminate Optimization La Jolla A Chaired by: R. TAYLOR, Optimal Structures, LLC. and M. RASSAIAN, Boeing Engineering Operations & Technology 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs AIAA-2016-1966 AIAA-2016-1967 AIAA-2016-1968 AIAA-2016-1969 AIAA-2016-1970 Aeroelastic Tailoring of Blended Gradient-Based Optimization of Damping Optimization of Stacking sequence constraints Optimization of variable stiffness Composite Structures using Postbuckled, Steered-Fiber Aircraft Symmetrically Laminated Plates in non-conventional composite composite plates with cut-outs Lamination Parameters Shell Using Equivalent Static Loads with Shear Deformation using laminate optimisation subjected to compression, tension and T. Macquart, N. Werter, R. De Breuker, T. Ungwattanapanit, S. Kamath, H. Baier, Lamination Parameters D. Peeters, M. Abdalla, Delft University of shear using an adjoint formulation Delft University of Technology, Delft, The Technical University of Munich, Garching, M. Kameyama, A. Takahashi, Shinshu Technology, Delft, The Netherlands M. Van Tooren, University of South Carolina, Netherlands Germany University, Nagano, Japan Columbia, Columbia, SC; A. Elham, Delft University of Technology, Delft, The Netherlands Thursday, 7 January 2016 418-STR-15 Buckling, Fatigue, and Fracture of Structures II La Jolla B Chaired by: B. BEDNARCYK, NASA Glenn Research Center and M. MOHAGHEGH, Boeing Commercial Airplanes 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2016-1971 AIAA-2016-1972 AIAA-2016-1973 AIAA-2016-1974 AIAA-2016-1975 AIAA-2016-1976 A Discontinuous Shell Element Buckling Considerations in the Efficient and robust shell design of Post-Buckling Load Redistribution Vibration and Buckling of Parametric Study of Stiffener for the Delamination Analysis of Design of Monolithic Machined space launcher vehicle structures of Stiffened Panels in Aircraft Quadrilateral Variable Stiffness Variables on Post-Buckling Composite Laminates Aluminum Structures L. Friedrich, RWTH Aachen University, Wingbox Structures Laminated Composite Plates Response of Frame-Stiffened S. Yazdani, Leibniz University of Hannover, J. Tucker, S. Russell, B. Mueller, Triumph Aachen, Germany; M. Ruess, University M. Mert, A. Kayran, Middle East Technical M. Henson, B. Wang, University of Texas, Composite Panels Hannover, Germany; W. Rust, University Aerostructures, Arlington, TX of Glasgow, Glasgow, United Kingdom; University, Ankara, Turkey Arlington, Arlington, TX G. Sanz-Douglass, S. Venkataraman, San of Applied Sciences and Arts, Hannover, K. Schröder, RWTH Aachen University, Diego State University, San Diego, CA

Germany; P. Wriggers, Leibniz University of Aachen, Germany Hannover, Hannover, Germany Thursday, 7 January 2016 419-TP-10 Experimental Measurements and Techniques in Heat Transfer and Related Physical Phenomena Harbor G Chaired by: I. SCHOEGL, Louisiana State University and W. TSAI, Cal Maritime 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs AIAA-2016-1977 AIAA-2016-1978 AIAA-2016-1979 AIAA-2016-1980 AIAA-2016-1981 Investigation of Ablative Properties An Experimental Investigation Geometry and Test-Time Effects Thermal Sensitivity Analysis of Spectral, Directional Emittance at through Advanced Video Analysis: on the Convective Heat Transfer on Hypervelocity Shock-Boundary Avionic and Environmental Control Elevated Temperatures for Various Improving Infrared Measurement Process over an Ice Roughened Layer Interaction Subsystems to Variations in Flight Materials through Image-to-Object Airfoil A. Knisely, J. Austin, California Institute of Condition M. Winter, R. Bickel, D. Sekulic, H. Koch, Calibration Y. Liu, H. Hu, Iowa State University, Technology, Pasadena, CA A. Jones, T. Childs, R. Chen, Loughborough B. Butler, H. Fu, University of Kentucky, J. Hunt, J. Koo, University of Texas, Austin, Ames, IA University, Loughborough, United Lexington, Lexington, KY Austin, TX Kingdom; A. Murray, BAE Systems, Warton, United Kingdom Thursday, 7 January 2016 420-UMS-10 Unmanned Systems: Detect-and-Avoid I Regatta C Chaired by: V. SCHULTZ, NASA Langley Research Center and R. STANSBURY, Embry-Riddle Aeronautical University 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2016-1982 AIAA-2016-1983 AIAA-2016-1984 AIAA-2016-1985 AIAA-2016-1986 AIAA-2016-1987 Minimum Required Sensing Range Ranging of Aircraft Using Wide- Inexpensive, Efficient, Light-weight Collision Avoidance System using Vision-Based Proportional Collision Avoidance System for UAS Sense and Avoid Systems baseline Stereopsys Vision-based Collision Avoidance Stereoscopic Vision for Unmanned Navigation for UAS Collision Effectiveness on Low Performance L. Sahawneh, J. Spencer, R. Beard, K. K. Rigby, C. Reinholtz, T. Wilson, Embry- System for Small Unmanned Aerial Aerial Systems Avoidance Unmanned Aircraft Warnick, Brigham Young University, Riddle Aeronautical University, Daytona Vehicles S. Bhandari, T. Srinivasan, J. Gray, M. M. Clark, R. Prazenica, Embry-Riddle E. Londner, Lincoln Laboratory, Provo, UT Beach, FL A. Harmsen, M. Liu, University of British Torstenbo, J. Corral, N. Brown, California Aeronautical University, Daytona Beach, FL Massachusetts Institute of Technology, Columbia, Vancouver, Canada Polytechnic State University, Pomona, Lexington, MA CA; et al. Thursday, 7 January 2016 421-WE-10 Wind Energy: Wind Plant Aerodynamics and Atmospheric Inflow Harbor H Chaired by: J. SITARAMAN 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs AIAA-2016-1988 AIAA-2016-1989 AIAA-2016-1990 AIAA-2016-1991 AIAA-2016-1992 Large Eddy Simulation of 3 X 3 Effect of Inversion-Layer Height Multiscale Kinematic Simulations Coupled Aero-Elastic Multi-Body Measuring power output intermittency wind turbine array using Actuator and Coriolis Forces on Developing of the Stratified Surface Layer Simulation of Two-bladed Wind and unsteady loading in a micro wind Line model with spectral elements Wind-Farm Boundary Layers and interactions with wind turbine Turbines in Wake Arrays farm model T. Chatterjee, Y. Peet, Arizona State D. Allaerts, J. Meyers, Catholic University arrays B. Luhmann, F. Beyer, P. Cheng, University J. Bossuyt, Catholic University of Leuven, University, Tempe, AZ of Leuven, Leuven, Belgium A. Ghate, S. Lele, Stanford University, of Stuttgart, Stuttgart, Germany Leuven, Belgium; C. Meneveau, Johns Stanford, CA Hopkins University, Baltimore, MD; J. Meyers, Catholic University of Leuven, Leuven, Belgium Thursday, 7 January 2016 422-WE-11 Wind Energy: Offshore Wind Systems Harbor I Chaired by: J. JONKMAN, National Renewable Energy Laboratory 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2016-1993 AIAA-2016-1994 AIAA-2016-1995 AIAA-2016-1996 AIAA-2016-1997 AIAA-2016-1998 A Comprehensive Aero-Hydro- On the Development of a Semi- Long-Term Loads on a Large An Aeroelastic Perspective of An Experimental Investigation on uncertainty quantification of the Structural Analysis of a 5-MW Submersible Offshore Floating Offshore Wind Turbine Supported Floating Offshore Wind Turbine the Aeromechanic Performance levelized cost of energy for a 20 Offshore Wind Turbine System: Platform and Mooring System for a by a Semi-Submersible Platform Wake Formation and Instabilities and Wake Characteristics of a Wind mw research wind turbine model Towards Cost-Effective Deployment of 13.2 MW Wind Turbine E. Thomas, J. Liu, A. Goyal, L. Manuel, S. Rodriguez, J. Jaworski, Lehigh Turbine Model Subjected to Pitch T. Ashuri, University of Texas, Dallas, Offshore Wind Turbines in Maryland J. Liu, E. Thomas, L. Manuel, University University of Texas, Austin, Austin, TX University, Bethlehem, PA Motions Richardson, TX; T. Zhang, Dalian Jiaotong S. Smith, A. Syed, D. Chen, M. Yu, W. Zhu, of Texas, Austin, Austin, TX; D. Griffith, H. Hu, M. Khosravi, P. Sarkar, Iowa State University, Dalian, China; D. Qian, M. University of Maryland, Baltimore County, K. Ruehl, M. Barone, Sandia National University, Ames, IA Rotea, University of Texas, Dallas,

Baltimore, MD; R. Liu, Hangzhou Dianzi Laboratories, Albuquerque, NM Richardson, TX University, Hangzhou, China; et al. Thursday, 7 January 2016 423-NW-15 Thursday Afternoon Networking Coffee Break Session Room Foyers 1530 - 1600 hrs Thursday, 7 January 2016 424-NW-16 Women at SciTech Happy Hour and Keynote Seaport F-G 1730 - 1930 hrs Ann Zulkosky Director, NASA Programs, Washington Operations Lockheed Martin Corporation Friday Friday, 8 January 2016 425-NW-17 Friday Early Morning Coffee Break Session Room Foyers 0700 - 0730 hrs Friday, 8 January 2016 426-SB-5 Friday Morning Speakers’ Briefing Session Rooms 0730 - 0800 hrs Friday, 8 January 2016 427-PLNRY-5 Friday Morning Plenary Seaport A-E 0800 - 0900 hrs Commercial Use of Unmanned Systems Treggon Owens Founding Partner & CEO Aerial MOB, LLC Friday, 8 January 2016 428-ACD-13 Aircraft Design Optimization Bankers Hill Chaired by: H. JIMENEZ, Georgia Institute of Technology and S. KOMADINA, Northrop Grumman Aerospace Systems 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2016-1999 AIAA-2016-2000 AIAA-2016-2001 AIAA-2016-2002 AIAA-2016-2003 Aircraft Design for Best Value Multifidelity Conceptual Design Aircraft Design Optimization with Low-Boom / Low-Drag Design Signomial Programming Models for P. Bevilaqua, North American Research and Optimization of Strut-Braced Artificial Intelligence Optimization of Innovative Aircraft Design Associates, Carlsbad, CA Wing Aircraft using Physics Based N. Cavus, German Aerospace Center Supersonic Transport Configuration P. Kirschen, E. Burnell, W. Hoburg, Methods (DLR), Hamburg, Germany B. Naohiko, W. Yamazaki, Nagaoka Massachusetts Institute of Technology, A. Variyar, T. Economon, J. Alonso, University of Technology, Nagaoka, Japan; Cambridge, MA Stanford University, Stanford, CA K. Kusunose, Japan Aerospace Exploration Agency (JAXA), Tokyo, Japan Friday, 8 January 2016 429-AFM-14 Aeroserovelastic (ASE) Control, Modeling, Simulation, and Optimization Cortez Hill A Chaired by: F. PRIOLO, Millennium Engineering and Integration Company and C. HANSON, NASA-Dryden Flight Research Center 0900 hrs 0930 hrs 1000 hrs 1030 hrs AIAA-2016-2004 AIAA-2016-2005 AIAA-2016-2006 AIAA-2016-2007 Control of Limit Cycle Oscillation Control Surface Buffet Load Adaptive Feedback Control for Gust High Fidelity Aeroservoelastic Amplitudes in Nonlinear Aerelastic Measurement using Aircraft Loads Alleviation: from Simulation Model Reduction Methods Systems using Nonlinear Normal Actuators to Wind Tunnel Test P. Schulze, B. Danowsky, Systems Modes B. Danowsky, P. Schulze, Systems Y. Wang, F. Li, China Academy of Technology, Inc., Hawthorne, CA; T. Lieu, H. Shukla, M. Patil, Virginia Polytechnic Technology, Inc., Hawthorne, CA Aerospace Aerodynamics, Beijing, China; CMSoft, Inc., Palo Alto, CA Institute and State University, Blacksburg, VA A. Da Ronch, University of Southampton, Southampton, United Kingdom Friday, 8 January 2016 430-AFM-15 Flight Test and System Identification II Harbor A Chaired by: J. GRAUER, NASA Langley Research Center and Z. PUTNAM, University of Illinois at Urbana-Champaign 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2016-2008 AIAA-2016-2009 AIAA-2016-2010 AIAA-2016-2011 AIAA-2016-2012 AIAA-2016-2013 AIAA-2016-2014 A Methodology for the Robust Parameter Covariance for Aircraft Real-Time Global Nonlinear Online Physical Model Identification Two-point Aerodynamic Model Comparison of Time and Frequency External Stores Grouping for Aero Design Optimization of Flight Aerodynamic Modeling using Aerodynamic Modeling for Learn- for Database-driven Safe Fight Identification from Dynamic Wind Domain Identification of a Fixed- Database Update Dynamic System Identification Recursive Least Squares To-Fly Envelope Prediction of Damaged Tunnel Tests Wing UAV T. Khadeeja Nusrath, J. Singh, National Experiments J. Grauer, NASA Langley Research Center, E. Morelli, NASA Langley Research Center, Aircraft J. Dias, Brazilian Air Force, São José dos O. Simsek, S. Haser, E. Orhan, Turkish Aerospace Laboratory, Banglore, India; A. J. Dykes, D. Mavris, Georgia Institute of Hampton, VA Hampton, VA Y. Zhang, C. de Visser, Q. Chu, Delft Campos, Brazil; R. Girardi, Technological Aerospace Industries, Ankara, Turkey; O. Saraf, Aeronautical Development Agency, Technology, Atlanta, GA University of Technology, Delft, The Institute of Aeronautics (ITA), São José Tekinalp, Middle East Technical University, Bangalore, India Netherlands dos Campos, Brazil Ankara, Turkey Friday, 8 January 2016 431-AMT-9 Surface Pressure and Skin Friction Measurements Harbor D Chaired by: J. NAUGHTON, University of Wyoming and C. KLEIN, DLR - German Aerospace Center 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2016-2015 AIAA-2016-2016 AIAA-2016-2017 AIAA-2016-2018 AIAA-2016-2019 AIAA-2016-2020 Skin-Friction Measurements Using a Characterization of a sapphire Unsteady PSP Measurements on a Polymer/Ceramic PSP with Comparison of Blur Elimination Pressure/Temperature Distribution Luminescent Oil-Film and Molecular optical wall shear stress sensor for Rectangular Cube Reduced Surface Roughness for Techniques for PSP Images of on the Surface of a Free-Flight Object Tagging Velocimetry high-temperature applications N. Roozeboom, S. Murman, NASA Unsteady Pressure Measurement in Rotating Surfaces Measured by PSP/TSP N. Husen, L. Rajendran, Purdue University, D. Mills, University of Florida, Gainesville, Ames Research Center, Moffett Field, Transonic Flow A. Pandey, J. Gregory, Ohio State M. Ishii, National Research Institute of West Lafayette, IN; T. Liu, Western Gainesville, FL; D. Blood, Valparaiso CA; L. Diosady, Science and Technology Y. Sugioka, D. Numata, K. Asai, Tohoku University, Columbus, OH; S. Stanfield, J. Police Science, Japan, Kashiwa, Japan; H. Michigan University, Kalamazoo, MI; University, Valparaiso, IN; M. Sheplak, Corporation, Moffett Field, CA; N. University, Sendai, Japan; S. Koike, K. Crafton, Innovative Scientific Solutions, Goya, T. Miyazaki, University of Electro- J. Sullivan, Purdue University, West University of Florida, Gainesville, Burnside, J. Ross, NASA Ames Research Nakakita, T. Nakajima, Japan Aerospace Inc., Dayton, OH Communications, Chofu, Japan; H. Sakaue, Lafayette, IN Gainesville, FL Center, Moffett Field, CA Exploration Agency (JAXA), Chofu, Japan University of Notre Dame, Notre Dame, IN Friday, 8 January 2016 432-APA-41 Applied CFD & Numerical Correlations with Experimental Data IV Americas Cup D Chaired by: K. CHITALE, Rensselaer Polytechnic Institute 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2016-2021 AIAA-2016-2022 AIAA-2016-2023 AIAA-2016-2024 AIAA-2016-2025 A global time integration approach Validation of Steady RANS Validation of a Transonic Lattice- Stability Derivative Computation of Flight Behaviors of a Complex for realistic unsteady flow Simulations Conducted on the High Boltzmann Method on the NASA Tailless Aircraft using Variable-Fidelity Projectile using a Coupled CFD- computations Maneuverability Airframe Using Common Research Model Aerodynamic Analysis for Control based Simulation Technique: Open- P. Eliasson, Swedish Defense Research Magnetic Resonance Velocimetry B. Konig, E. Fares, Exa GmbH, Stuttgart, Performance Analysis loop Control Agency (FOI), Stockholm, Sweden; Water Channel Testing Germany J. Park, J. Choi, Virginia Polytechnic Institute J. Sahu, F. Fresconi, Army Research T. Lundquist, J. Nordstrom, Linköping M. Wells, C. Snow, C. Coyle, A. Coulter, J. and State University, Blacksburg, VA; Y. Laboratory, Aberdeen Proving Ground, MD University, Linköping, Sweden Spirnak, E. Youn, U.S. Military Academy, Jo, Korea Advanced Institute of Science West Point, NY; et al. and Technology, Daejeon, South Korea ; S. Choi, Virginia Polytechnic Institute and State University, Blacksburg, VA Friday, 8 January 2016 433-APA-42 Aerodynamic-Structural Dynamics Interactions II Coronado D Chaired by: V. VENKATESH, and C. PASILIAO, AFRL/RWWV 0900 hrs 0930 hrs 1000 hrs AIAA-2016-2026 AIAA-2016-2027 AIAA-2016-2028 Aero-Structural Design Analysis and Computational Study A Parametric Study of Factors Optimization of Adaptive Shock of The Aerodynamics, Aeroelasticity Affecting Transonic Shock Control Bumps And Flight Dynamics of Flapping Oscillation E. Jinks, P. Bruce, M. Santer, Imperial Wing Using Linear N. Giannelis, G. Vio, University of Sydney, College London, London, United Kingdom Approximation Sydney, Australia H. Djojodihardjo, Putra University, Serdang, Malaysia Friday, 8 January 2016 434-APA-43 Lowspeed Flow Environment and UAV Integration Americas Cup C Chaired by: D. HUNSAKER, Blucraft, LLC 0900 hrs 0930 hrs 1000 hrs AIAA-2016-2029 AIAA-2016-2030 AIAA-2016-2031 Design and Development of a 3D Numerical Simulations of Parachute Stabilization of Helicopter Sling Printed Unmanned Aerial Vehicle Aerodynamic Characteristics under Loads with Passive and Active C. Banfield, J. Kidd, J. Jacob, Oklahoma Severe Weather Control Surfaces State University, Stillwater, OK T. Wan, C. Cheng, R. Huo, Tamkang D. Cyr, P. Guarino, J. Hitchen, R. Morar, J. University, Taipei, Taiwan Sperry, R. Cowlagi, Worcester Polytechnic Institute, Worcester, MA; et al. Friday, 8 January 2016 435-APA-44 Special Session: Low Boom Activities Coronado E Chaired by: K. WAITHE, Gulfstream Aerospace Corporation and S. CLIFF, NASA-Ames 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2016-2032 AIAA-2016-2033 AIAA-2016-2034 AIAA-2016-2035 AIAA-2016-2036 AIAA-2016-2037 A New F-Function for the Low- Multi-fidelity Low-boom Design Computational and Experimental Wind Tunnel Model Design for Sonic Numerical Examination of Shock A Space Marching Method for Sonic Boom Aircraft Design with Trim Based on Near-field Pressure Study of Supersonic Nozzle Flow Boom Studies of Nozzle Jet Flow with Generator Geometries and Boom Near Field Predictions Requirement Signature and Aft-Deck Interactions Shock Interactions Nozzle Plume Effects on Pressure H. Shen, The Boeing Company, Y. Kasuga, University of Tokyo, Kashiwa, A. Ueno, M. Kanamori, Y. Makino, Japan W. Bruce, University of Virginia, S. Cliff, NASA Ames Research Center, Moffett Signature Hazelwood, MO; D. Lazzara, The Boeing Japan; K. Yoshida, Japan Aerospace Aerospace Exploration Agency (JAXA), Charlottesville, Charlottesville, VA; M. Field, CA; M. Denison, S. Moini-Yekta, Science J. Pearl, University of Vermont, Burlington, Company, Huntington Beach, CA Exploration Agency (JAXA), Mitaka, Japan; Tokyo, Japan Carter, A. Elmiligui, C. Winski, NASA and Technology Corporation, Moffett Field, Burlington, VT; M. Carter, A. Elmiligui, C. H. Ishikawa, ASIRI Corporation, Chiyoda, Langley Research Center, Hampton, VA; S. CA; D. Morr, Millennium Engineering and Winski, NASA Langley Research Center, Japan Nayani, Analytical Services & Materials, Integration Company, Moffett Field, CA; D. Hampton, VA; S. Nayani, Analytical Inc., Hampton, VA; R. Castner, NASA Glenn Durston, NASA Ames Research Center, Moffett Services & Materials, Inc., Hampton, VA Research Center, Cleveland, OH Field, CA Friday, 8 January 2016 436-APA-45 Airfoil/Wing/Configuration Aerodynamics III Americas Cup B Chaired by: C. TILMANN, Air Force Research Laboratory and M. CONWAY, The Aerospace Corporation 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2016-2038 AIAA-2016-2039 AIAA-2016-2040 AIAA-2016-2041 AIAA-2016-2042 Beyond the Elliptical Span Load: Aerodynamic Performance of a Effects of Wake Shapes on High-Lift Aerodynamic Design of Transonic Post-Stall Performance Optimizing Minimum Induced Drag Small-Scale Wingsail Vessel System Aerodynamic Predictions Natural-Laminar-Flow (NLF) Wing Improvement through Bio-inspired Using Enhanced Leading Edge M. Anderson, University of California, San W. Bissonnette, G. Bramesfeld, Ryerson via Surrogate-based Optimization Passive Covert Feathers Suction Diego, La Jolla, CA University, Toronto, Canada Z. Han, J. Chen, Z. Zhu, W. Song, A. Altman, G. Allemand, University of

T. Takahashi, C. Barchfeld, Arizona State Northwestern Polytechnical University, Dayton, Dayton, OH University, Tempe, AZ Xi’an, China Friday, 8 January 2016 437-DA-2 Avionics Technologies for Safe and Efficient Vehicle Operation in National Airspace Regatta A Chaired by: M. UIJT DE HAAG, Ohio University and B. KORN, DLR - German Aerospace Center 0900 hrs 0930 hrs 1000 hrs AIAA-2016-2043 AIAA-2016-2044 AIAA-2016-2045 Evaluating Technologies for Assessing Dual Sensor Enhanced The Use of Enhanced Vision Improved Airplane State Awareness Flight Vision Systems to Enable Systems for See-and-Avoid During and Prediction Equivalent Visual Operations Surface Operations S. Young, NASA Langley Research Center, L. Kramer, NASA Langley Research Center, R. Bailey, NASA Langley Research Center, Hampton, VA; M. Uijt De Haag, Ohio Hampton, VA; T. Etherington, Rockwell Hampton, VA University, Athens, OH; T. Daniels, E. Collins, Cedar Rapids, IA; K. Severance, Evans, NASA Langley Research Center, R. Bailey, S. Williams, S. Harrison, NASA Hampton, VA; K. Shish, Millennium Langley Research Center, Hampton, VA Engineering and Integration Company, Moffett Field, CA; S. Schuet, NASA Ames Research Center, Moffett Field, CA; et al. Friday, 8 January 2016 438-DSC-6 Aeroelasticity Balboa C Chaired by: R. SCOTT, NASA Langley Research Center and D. PITT, Boeing Engineering Operations & Technology 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2016-2046 AIAA-2016-2047 AIAA-2016-2048 AIAA-2016-2049 AIAA-2016-2050 Modeling and Simulation of Aeroelastic Ground Wind Loads Aeroelasticity of Flexible Nonlinear transient Fluid/ Status of the KTH-NASA Wind- Flexible Jet Transport Aircraft Analysis Tool for Launch Vehicles Airfoils with Arbitrary Camber Structure interaction approach Tunnel Test for Acquisition of with Aeroelastically Tailored High- T. Ivanco, NASA Langley Research Center, Deformations using surrogate models: Industrial Transonic Nonlinear Aeroelastic Aspect-Ratio Wings Hampton, VA W. Su, C. King, University of Alabama, application to Data R. Kitson, C. Lupp, C. Cesnik, University of Tuscaloosa, Tuscaloosa, AL vibration excited by engine efflux. W. Silva, NASA Langley Research Center, Michigan, Ann Arbor, Ann Arbor, MI E. Bosco, A. Lucchetti, S. Trapier, Airbus, Hampton, VA; U. Ringertz, D. Eller, Royal Toulouse, France; F. Di Vincenzo, MSC Institute of Technology (KTH), Stockholm, Software Corporation, Toulouse, France; Sweden; D. Keller, NASA Langley Research J. Morlier, N. Gourdain, University of Center, Hampton, VA Toulouse, Toulouse, France Friday, 8 January 2016 439-FD-54 CFD: Overset Methods Pier Chaired by: M. GALBRAITH and S. SHERER, US Air Force 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2016-2051 AIAA-2016-2052 AIAA-2016-2053 AIAA-2016-2054 AIAA-2016-2055 AIAA-2016-2056 High-Order Overset Interpolation Deformable Overset Grid for A Multi-Solver Overset Mesh A implicit, discontinuous Galerkin A mixed overset grid/immersed Recent Developments of the Navier via Weighted Least-Square Unsteady Aerodynamic Simulation Approach for 3D Mixed Element Chimera solver using automatic boundary approach for CFD Stokes Multi Block (NSMB) CFD solver. Polynomials Reconstruction for T. Xiao, N. Qin, University of Sheffield, Variable Order Discretizations differentiation simulations of complex geometries Y. Hoarau, D. Pena, University of Strasbourg, Finite Volume CFD Sheffield, United Kingdom; D. Luo, Nanjing M. Brazell, A. Kirby, J. Sitaraman, D. N. Wukie, P. Orkwis, University of S. Péron, C. Benoit, V. Gleize, I. Mary, M. Strasbourg, France; J. Vos, D. Charbonier, CFS J. Le Gouez, ONERA, Châtillon, France University of Aeronautics and Astronautics, Mavriplis, University of Wyoming, Laramie, Cincinnati, Cincinnati, OH Terracol, ONERA, Châtillon, France Engineering, Lausanne, Switzerland; A. Gehri, Nanjing, China; S. Deng, Delft University Laramie, WY RUAG Aviation, Emmen, Switzerland; M. of Technology, Delft, The Netherlands Braza, Fluid Mechanics Institute of Toulouse (IMFT), Toulouse, France; et al. Friday, 8 January 2016 440-FD-55 High-Speed Flow Methods & Simulations Harbor E Chaired by: K. DURAISAMY, University of Michigan, Ann Arbor and R. GOSSE, WPAFB 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2016-2057 AIAA-2016-2058 AIAA-2016-2059 AIAA-2016-2060 AIAA-2016-2061 AIAA-2016-2062 Shape Optimization of a Blunt Numerical Investigation of Recovery of Freestream Acoustic Simulation of Hypersonic Flows Construction Methodology of A Decoupled Method for the Roe Body in Hypersonic Rarefied and the Near-Field of a Supersonic Disturbances from Stagnation using a Particle-based Ellipsoidal Weighted Upwind Compact Scheme FDS Scheme in the Reacting Gas Reacting Flow for Reducing Both Multistream Jet Pressure Spectrum in Hypersonic Statistical Bhatnagar-Gross-Krook Z. Wang, H. Al-Dujaly, C. Liu, University of Path of FUN3D Drag and Heat Transfer C. Stack, D. Gaitonde, Ohio State Flow Method Texas, Arlington, Arlington, TX K. Thompson, P. Gnoffo, NASA Langley G. Huang, S. Gardner, E. Zishka, C. University, Columbus, OH R. Chaudhry, G. Candler, University of O. Tumuklu, D. Levin, University of Illinois, Research Center, Hampton, VA Seager, R. Agarwal, Washington University Minnesota, Minneapolis, Minneapolis, MN Urbana-Champaign, Urbana, IL in St. Louis, St. Louis, MO Friday, 8 January 2016 441-FD-56 Incompressible Flow Transition Harbor F Chaired by: E. WHITE, Texas A&M University 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2016-2063 AIAA-2016-2064 AIAA-2016-2065 AIAA-2016-2066 AIAA-2016-2067 AIAA-2016-2068 The Effect of Acoustic Forcing on Self-Contradictions in Classical The Interaction of a Swept-Wing A Quantitative Investigation of Evaluation of Miniature Vortex New Vortex Identification Method Instabilities and Breakdown in and Current Turbulence Theory Boundary Layer with Surface Surface Roughness Effects on Generators for Flow Control in and Vortex Ring Development Swept-Wing Flow Over a Backward- and New Turbulence Genearation Excrescences Airfoil Boundary Layer Transition Falkner–Skan Boundary Layers Analysis in Boundary Layer Facing Step Theory T. Saeed, M. Mughal, J. Morrison, Imperial Using Infrared Thermography R. Downs, B. Fallenius, J. Fransson, Royal Transition J. Eppink, NASA Langley Research Center, C. Liu, University of Texas, Arlington, College London, London, United Kingdom T. Beeby, J. Ackermann, C. Langel, Institute of Technology (KTH), Stockholm, C. Liu, Y. Wang, J. Tang, University of Hampton, VA; O. Shishkov, Georgia Arlington, TX R. Chow, C. Van Dam, University of Sweden; H. Mårtensson, GKN Aerospace Texas, Arlington, Arlington, TX Institute of Technology, Atlanta, GA; R. California, Davis, Davis, CA; T. Raffius, Engine Systems, Trollhättan, Sweden Wlezien, Iowa State University, Ames, RWTH Aachen University, Aachen, IA; R. King, M. Choudhari, NASA Langley Germany Research Center, Hampton, VA Friday, 8 January 2016 442-FD-57 Pitching/Heaving/Flapping Surfaces Cove Chaired by: K. MOORED, Lehigh University and B. GANAPATHISUBRAMANI, University of Southampton 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2016-2069 AIAA-2016-2070 AIAA-2016-2071 AIAA-2016-2072 AIAA-2016-2073 AIAA-2016-2074 Lift Enhancement of High Angle On Optimal Oscillating-Foil Power Proper Orthogonal Decomposition A Vortex Sheet/Point Vortex Effects of Structural Motion on the Transient aerodynamics of large of Attack Airfoils Using Periodic Generation in Free and Constrained Analysis of 3-D Wake Structures in Dynamical Model For Unsteady Aerodynamics of the X-56A Airfoil transverse gusts and geometrically Pitching Flow a Pitching-Rolling Plate Separated Flows C. Mertens, S. Pineda, M. Agate, J. Little, similar maneuvers S. Dawson, Princeton University, Princeton, F. Karakas, B. Zaloglu, I. Fenercioglu, C. Li, H. Dong, University of Virginia, D. Darakananda, J. Eldredge, University of University of Arizona, Tucson, Tucson, AZ; G. Perrotta, A. Jones, University of

NJ; M. Hemati, University of Minnesota, Istanbul Technical University, Istanbul, Charlottesville, Charlottesville, VA; Z. California, Los Angeles, Los Angeles, CA; T. A. Gross, New Mexico State University, Maryland, College Park, College Park, MD Minneapolis, Minneapolis, MN; D. Turkey; C. Hoke, J. Young, J. Lai, Liang, Ohio State University, Columbus, Colonius, California Institute of Technology, Las Cruces, NM; H. Fasel, University of Floryan, C. Rowley, Princeton University, University of New South Wales, Canberra, OH Pasadena, CA; D. Williams, Illinois Institute Arizona, Tucson, Tucson, AZ Princeton, NJ Australia; et al. of Technology, Chicago, IL Friday, 8 January 2016 443-FD-58 Separated Fluid Flows Promenade B Chaired by: R. SCHMIT, USAF AFRL 0900 hrs 0930 hrs 1000 hrs 1030 hrs AIAA-2016-2075 AIAA-2016-2076 AIAA-2016-2077 AIAA-2016-2078 Hydrodynamic Wave Generation Stereoscopic Particle Image The Effect of Inflow PIV Investigation in the Centreline inside a Rectangular Cavity Velocimetry measurement of transonic on the Reattachment in Subsonic Plane of a Pressure-Induced R. Schmit, Air Force Research Laboratory, flow over three-dimensional open Flow over a Backward-Facing Step Turbulent Separation Bubble. Wright-Patterson AFB, OH cavities of complex geometry D. Li, Z. Ghiasi, J. Komperda, F. M. Abdelouahab, J. Weiss, University of E. Demauro, S. Beresh, J. Wagner, J. Henfling, Mashayek, University of Illinois, Chicago, Québec, Montréal, Canada R. Spillers, Sandia National Laboratories, Chicago, IL Albuquerque, NM Friday, 8 January 2016 444-FD-59 Vortex Flows III: Dynamical Systems Methods Promenade A Chaired by: D. SMITH, Air Force Office of Scientific Research AFOSR and M. GREEN, Syracuse University 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2016-2079 AIAA-2016-2080 AIAA-2016-2081 AIAA-2016-2082 AIAA-2016-2083 AIAA-2016-2084 Spatiotemporal analysis of Correlation of the Surface Pressure Detection of Near Wall Flow Comparing leading and trailing Numerical Investigation of Flow Numerical Analysis of a fluctuating base pressure and Distribution on a Circular Cylinder Features Using Surface Pressure edge vortex circulation history with Asymmetry Around Slender Body Trailing Edge with Triangular velocity in a blunt trailing edge with Objective Identification of Data vortex identification and tracking at High Angles of Attack Serrations Using Dynamic Mode wake Vortex Formation and Shedding C. Marks, R. Sondergaard, Air Force methods I. AlQadi, E. Eljack, King Abdulaziz Decomposition H. Clark, P. Lavoie, University of Toronto, M. Rockwood, M. Green, Syracuse Research Laboratory, Wright-Patterson Y. Huang, M. Green, Syracuse University, University, Jeddah, Saudi Arabia N. Thomareis, G. Papadakis, Imperial Toronto, Canada University, Syracuse, NY AFB, OH Syracuse, NY College London, London, United Kingdom Friday, 8 January 2016 445-GNC-37 Invited Session: Flight Experience of Cassini Spacecraft Attitude Control at Saturn Coronado B Chaired by: T. BURK, Jet Propulsion Laboratory and J. WEBSTER, Jet Propulsion Laboratory 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs Video Presentation AIAA-2016-2085 AIAA-2016-2086 AIAA-2016-2087 AIAA-2016-2088 AIAA-2016-2089 AIAA-2016-2090 Ring World 4 - New Results from the The Cassini Reaction Wheels: Drag Risk Assessment of Cassini Sun Sensor Thruster-Specific Force Estimation Cassini Operational Sun Sensor Trending Main Engine Assembly (MEA) Extended Bright Bodies – Flight Cassini Mission at Saturn and Spin-Rate Trends from an Aging Performance Degradation due to and Trending of Cassini Hydrazine Risk Management During Proximal Cover Actuator Performance using and Ground Software Challenges Interplanetary Spacecraft at Saturn Hypervelocity Impact Of Ring Dust Thrusters at Saturn Orbit Saturn Ring Plane Crossings Cassini Attitude Control Flight Data on the Cassini Mission at Saturn T. Brown, Jet Propulsion Laboratory, California Particles J. Stupik, T. Burk, Jet Propulsion D. Bates, Jet Propulsion Laboratory, L. Andrade, Jet Propulsion Laboratory, T. Sung, T. Burk, Jet Propulsion Laboratory, Institute of Technology, Pasadena, CA A. Lee, Jet Propulsion Laboratory, California Laboratory, California Institute of California Institute of Technology, California Institute of Technology, Pasadena, California Institute of Technology, Institute of Technology, Pasadena, CA Technology, Pasadena, CA Pasadena, CA CA Pasadena, CA Friday, 8 January 2016 446-GNC-38 Vision-Based Sensing and Optical Navigation Hillcrest A Chaired by: L. POLLINI, University of Pisa and S. WOICKE 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2016-2091 AIAA-2016-2092 AIAA-2016-2093 AIAA-2016-2094 AIAA-2016-2095 AIAA-2016-2096 AIAA-2016-2097 A Vision-aided Nonlinear Observer Position-Based Visual Servoing for Interplanetary Optical Navigation Robust Measurement Planning for Detection and Identification of Vision Navigation Sensor (VNS) Enhancing Inertial Navigation with for Fixed-wing UAV Navigation Target Tracking by a Quadrotor V. Adams, M. Peck, Cornell University, Intersatellite Laser Ranging Objects Using Point Cloud Data for with Adaptive Electronically Structure from Motion Trajectory J. Hosen, Kongsberg Defence Systems, UAV Ithaca, NY M. Salvoldi, D. Choukroun, Ben Gurion Pose Estimation Steerable Flash LIDAR (ESFL) Estimates Kjeller, Norway; H. Helgesen, L. Fusini, M. Popova, H. Liu, University of Toronto, University of the Negev, Beer Sheva, Israel A. Suqi, T. Lim, U.S. Naval Academy, R. Rohrschneider, C. Weimer, J. J. Tharp, B. Woolley, Air Force Institute of T. Fossen, T. Johansen, Centre for Toronto, Canada Annapolis, MD Masciarelli, M. Lieber, C. Adkins, J. Technology, Wright-Patterson AFB, OH Autonomous Operations and Systems, Domber, Ball Aerospace & Technologies Trondheim, Norway Corporation, Boulder, CO

Friday, 8 January 2016 447-GNC-39 Flight Control of Unmanned Vehicles Hillcrest C Chaired by: D. SCHMIDT, Retired f/University of Colorado and M. GROS, Institute of Flight Mechanics and Flight Control 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2016-2098 AIAA-2016-2099 AIAA-2016-2100 AIAA-2016-2101 AIAA-2016-2102 Autonomous Waypoint Stability Augmentation and Active UAV Collision Avoidance based Unified Approach for Velocity Robust Design of Close Formation Transitioning and Loitering for Flutter Suppression of a Flexible on the Solution of the Suicidal Control and Flight State Transition Flight Control via Uncertainty and UnmannedAerial Vehicles via Flying-Wing Drone Pedestrian Differential Game of Unmanned Tiltwing Aircraft Disturbance Estimator Hybrid Control D. Schmidt, University of Colorado, I. Exarchos, P. Tsiotras, Georgia Institute P. Hartmann, C. Meyer, D. Moormann, Q. Zhang, H. Liu, University of Toronto, D. Smith, Raytheon Company, Tucson, AZ; Colorado Springs, Colorado Springs, CO of Technology, Atlanta, GA; M. Pachter, RWTH Aachen University, Aachen, Toronto, Canada R. Sanfelice, University of California, Santa Air Force Institute of Technology, Wright- Germany Cruz, Santa Cruz, CA Patterson AFB, OH Friday, 8 January 2016 448-GNC-40 Intelligent and Cooperative Control in Aerospace Applications Cortez Hill B Chaired by: J. CONNOLLY, NASA Glenn Research Center 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2016-2103 AIAA-2016-2104 AIAA-2016-2105 AIAA-2016-2106 AIAA-2016-2107 AIAA-2016-2108 AIAA-2016-2109 A Cooperative Pursuit Strategy for Collective Circular Motion and Analysis of UAV Kinematic Scalable Cooperative Control Optimal Continuous-Time Job A Beam Rider Concept For Three MAV Waypoint Guidance with a High Speed Evader Cooperative Circumnavigation for Constraints for Rigid Formation Algorithms For the Weapon Target Scheduling for Multiple Low Earth Point Aerial Rendezvous Guidance Arrival Angle and Time Scheduling V. Makkapati, M. Kothari, Indian Institute Nonholonomic Mobile Robots Using Flying Assignment Problem Orbit Satellites P. Anjaly, A. Ratnoo, Indian Institute of Constraints of Technology Kanpur, Kanpur, India Range-based Measurements V. Challa, A. Ratnoo, Indian Institute of K. Volle, J. Rogers, Georgia Institute of D. Cho, H. Kim, H. Choi, Korea Advanced Science, Bangalore, India A. Saleem, A. Ratnoo, Indian Institute of Y. Cao, University of Texas, San Antonio, Science, Bangalore, India Technology, Atlanta, GA; K. Brink, Air Force Institute of Science and Technology, Science, Bangalore, India San Antonio, TX; D. Casbeer, Air Force Research Laboratory, Eglin AFB, FL Daejeon, South Korea Research Laboratory, Wright-Patterson AFB, OH; D. Milutinovic, University of California, Santa Cruz, Santa Cruz, CA; D. Kingston, Air Force Research Laboratory, Wright-Patterson AFB, OH Friday, 8 January 2016 449-GNC-41 Missile and Entry Vehicle Guidance Hillcrest B Chaired by: S. WELLS, Raytheon Missile Systems and P. VERNIS, AIRBUS Defence and Space 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2016-2110 AIAA-2016-2111 AIAA-2016-2112 AIAA-2016-2113 AIAA-2016-2114 AIAA-2016-2115 A Composite Guidance for Dual Inverse Optimal Sliding Mode Nonlinear Impact Angle Control Precision Munition Guidance and A Pitch Controlled Impact-Angle- Onboard Trajectory Generation Range AAM with Side Jet Control Guidance Law against Maneuvering Guidance Law for Stationary Estimation of Target Position in 2-D Constrained Guidance Law for for Entry Vehicles via Adaptive D. Taur, National Chung-Shan Institute of Targets Targets S. Sreeja, Indian Institute of Technology Surface-to-Surface Missiles Multivariate Pseudospectral Science and Technology, Taipei, Taiwan S. He, D. Lin, J. Wang, Beijing Institute of U. Ates, ROKETSAN Missile Industries, Inc., Bombay, Mumbai, India; H. Hablani, S. Varma, H. Parwana, M. Kothari, Indian Interpolation Technology, Beijing, China Ankara, Turkey Indian Institute of Technology Institute of Technology Kanpur, Kanpur, M. Sagliano, German Aerospace Center Gandhinagar, Ahmedabad, India India (DLR), Bremen, Germany; E. Mooij, Delft University of Technology, Delft, The Netherlands ; S. Theil, German Aerospace Center (DLR), Bremen, Germany Friday, 8 January 2016 450-GT-9 Ground Test Methodologies and CFD Integration Hillcrest D Chaired by: S. RYLE, San Diego Wind Tunnel and C. JORGENS, The Boeing Company 0900 hrs 0930 hrs 1000 hrs 1030 hrs AIAA-2016-2116 AIAA-2016-2117 AIAA-2016-2118 AIAA-2016-2119 Migration and deposition Numerical Simulation of a Hypersonic Boundary Layer Wind Tunnel Manoeuvre Rig: A Multi- characteristics of lunar dust on Complete Low-Speed Wind Tunnel Transition Experiments in DOF Test Platform for Model Aircraft the optical element surface in the Circuit Hypervelocity Ballistic Range G S. Araujo-Estrada, University of Bristol, Bristol, simulated electrostatic environment S. Nayani, W. Sellers, A. Tinetti, Analytical T. Swanson, D. Daniel, Arnold Engineering United Kingdom; Z. Gong, Nanjing University Q. Chen, Beijing Jiaotong University , Services & Materials, Inc., Hampton, VA; Development Complex, Arnold AFB, TN of Aeronautics and Astronautics, Nanjing,

Beijing, China; X. Chen, Dongfengrichan S. Brynildsen, ViGYAN, Inc., Hampton, VA; China; M. Lowenberg, S. Neild, University of Vehicle, Guangzhou, China E. Walker, NASA Langley Research Center, Bristol, Bristol, United Kingdom; M. Goman, Hampton, VA De Montfort University, Leicester, United Kingdom Friday, 8 January 2016 451-GTE-15 Combustion III Gaslamp B Chaired by: J. GORE, Purdue University and S. JAMES, Honeywell Inc. 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2016-2120 AIAA-2016-2121 AIAA-2016-2122 AIAA-2016-2123 AIAA-2016-2124 Flamelet Generated Manifolds Emission Characteristics of A P&W Enhancing Flow Migration and LES of a sooting flame in a Estimation and Comparison of for Partially Premixed, Highly Axially Staged Sector Combustor Reducing Emissions in Full Annular pressurized swirl combustor Particle Number Emission Factors Stretched and Non-Adiabatic Z. He, NASA Glenn Research Center, Ultra Compact Combustor H. Koo, V. Raman, University of Michigan, for Petroleum-based and Camelina Combustion in Gas Turbines Cleveland, OH; K. Kopp-Vaughan, Pratt & N. Gilbert, A. Cottle, M. Polanka, Air Force Ann Arbor, Ann Arbor, MI; M. Mueller, Biofuel Blends used in a Honeywell N. Klarmann, T. Sattelmayer, Technical Whitney, Hartford, CT; C. Wey, C. Chang, Institute of Technology, Wright-Patterson Princeton University, Princeton, NJ; K. TFE-109 Turbofan Engine University of Munich, Garching, Germany; NASA Glenn Research Center, Cleveland, AFB, OH; L. Goss, Innovative Scientific Geigle, German Aerospace Center (DLR), J. Shila, M. Johnson, Purdue University, W. Geng, F. Magni, GE Power, Baden, OH; A. Cheung, Pratt & Whitney, Hartford, Solutions, Inc., Dayton, OH Stuttgart, Germany West Lafayette, IN Switzerland CT; C. Lee, NASA Glenn Research Center, Cleveland, OH; et al. Friday, 8 January 2016 452-GTE-16 Numerical Tools Old Town A Chaired by: T. SHIH, Purdue University and P. TUCKER, The Whittle Laboratory 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2016-2125 AIAA-2016-2126 AIAA-2016-2127 AIAA-2016-2128 AIAA-2016-2129 AIAA-2016-2130 Impact of the Specific Heat Ratio Unsteady Simulations of the Effect of Labyrinth Seal Novel Design and Fabrication Wavepacket modeling from full-scale Hierarchical Immersed Boundary On the Noise Generation in a High- Wellborn Diffusing S-Duct Configurations on Leakage of JetCat P90 Diffuser using military jet noise beamforming Method with Smeared Geometry Temperature Supersonic Jet R. Watson, P. Tucker, University of Performance using LES Parametric Design and analyses T. Cao, University of Cambridge, J. Liu, A. Corrigan, K. Kailasanath, B. Cambridge, Cambridge, United Kingdom; Y. Dai, J. Tyacke, P. Tucker, Cambridge Optimization Tools B. Harker, T. Neilsen, K. Gee, Brigham Young Cambridge, United Kingdom; P. Hield, Taylor, Naval Research Laboratory, K. Menzies, Rolls-Royce Group plc, Bristol, University, Cambridge, United Kingdom J. Holden, T. Caley, B. Heberling, C. University, Provo, UT; A. Wall, Air Force Rolls-Royce Group plc, Filton, United Washington, D.C. United Kingdom Cantor, E. Wesseling, A. Hamed, University Research Laboratory, Wright-Patterson AFB, Kingdom; P. Tucker, University of of Cincinnati, Cincinnati, OH; et al. OH; M. James, Blue Ridge Research and Cambridge, Cambridge, United Kingdom Consulting, LLC, Asheville, NC Friday, 8 January 2016 453-IS-13 Intelligent Integrated Systems Health Management Regatta B Chaired by: J. FIGUEROA, NASA Stennis Space Center and C. KULKARNI, NASA Ames Research Center 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2016-2131 AIAA-2016-2132 AIAA-2016-2133 AIAA-2016-2134 AIAA-2016-2135 Predicting Real-Time Safety End-of-discharge and End-of-life Review of Proactive Safety Metrics A Generic Modeling Process to Analysis of Helicopter Maintenance Margins in the National Airspace Prediction in Lithium-ion Batteries for Rotorcraft Operations and Support Functional Fault Model Risk from Accident Data System with Electrochemistry-based Aging Improvements Using Model-Based Development A. Rao, N. Fala, K. Marais, Purdue I. Roychoudhury, L. Spirkovska, M. Daigle, Models Parameter Synthesis and Data Fusion W. Maul, J. Hemminger, Vantage Partners, University, West Lafayette, IN S. Sankararaman, E. Balaban, C. Kulkarni, M. Daigle, C. Kulkarni, NASA Ames A. Payan, A. Gavrilovski, H. Jimenez, D. LLC, Brook Park, OH; R. Oostdyk, SGT, NASA Ames Research Center, Moffett Research Center, Moffett Field, CA Mavris, Georgia Institute of Technology, Inc., Cape Canaveral, FL; R. Bis, NnR

Field, CA; et al. Atlanta, GA Engineering, Cleveland, OH Friday, 8 January 2016 454-MST-14 Rotorcraft Modeling and Simulation Technologies Golden Hill A Chaired by: M. WHITE, The University of Liverpool and M. SEKULA, NASA-Langley Research Center 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2016-2136 AIAA-2016-2137 AIAA-2016-2138 AIAA-2016-2139 AIAA-2016-2140 Coupled Flight Dynamics and CFD Control Augmentation Strategies for An Investigation of Task Specific Implementation and Validation of CFD Validation of a Designed Simulations of Rotorcraft/Terrain used as Personal Aerial Motion Cues for Rotorcraft a 6 Degrees-of-Freedom Nonlinear Quad-Rotor Interactions Vehicles Simulators Helicopter Model C. Zhou, D. Schrage, Georgia Institute of I. Oruc, J. Horn, Pennsylvania State C. Gerboni, Max Planck Institute for Biological M. White, University of Liverpool, C. Gerboni, F. Nieuwenhuizen, H. Technology, Atlanta, GA University, University Park, PA; J. Shipman, Cybernetics, Tübingen, Germany; A. Joos, Liverpool, United Kingdom; S. Manso, Buelthoff, Max Planck Institute for CRAFT Tech, Pipersville, PA University of Stuttgart, Stuttgart, Germany; Australian National University, Melbourne, Biological Cybernetics, Tübingen, Germany F. Nieuwenhuizen, Max Planck Institute for Australia; S. Hodge, BAE Systems, Biological Cybernetics, Tübingen, Germany; Preston, United Kingdom W. Fichter, University of Stuttgart, Stuttgart, Germany; H. Buelthoff, Max Planck Institute for Biological Cybernetics, Tübingen, Germany Friday, 8 January 2016 455-MST-15 Computational Methods II Golden Hill B Chaired by: D. GINGRAS, Bihrle Applied Research Inc. and M. SMITH, Georgia Institute of Technology 0900 hrs 0930 hrs 1000 hrs 1030 hrs AIAA-2016-2141 AIAA-2016-2142 AIAA-2016-2143 AIAA-2016-2144 Aerodynamic Influences on the Mesh Adaptation and Optimization Numerical Analysis of an External Function Extrapolation of Noisy Modeling and Simulation of for Discontinuous Galerkin Methods Store Separation From an Airplane Data using Converging Lines Instabilities on Dynamic Tethered Using a Continuous Mesh Model A. Osman, A. Aly, E. Khalil, O. Abdelattif, Y. Zhang, N. Kim, C. Park, R. Haftka, Loads A. Rangarajan, A. Balan, G. May, RWTH Cairo University, Cairo, Egypt University of Florida, Gainesville, O. Nabipour, J. Clinton, T. Ma, D. Prosser, Aachen University, Aachen, Germany Gainesville, FL M. Smith, Georgia Institute of Technology, Atlanta, GA Friday, 8 January 2016 456-NW-18 Friday Late Morning Networking Coffee Break Session Room Foyers 0900 - 0930 hrs Friday, 8 January 2016 457-PC-18 Rocket & Air-Breathing Combustion II Harbor B Chaired by: B. CHEHROUDI, European Research Council (ERC) and V. RAMAN, University of Michigan 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2016-2145 AIAA-2016-2146 AIAA-2016-2147 AIAA-2016-2148 AIAA-2016-2149 AIAA-2016-2150 Study of the Combustion of Formulation of Equations to Describe Numerical Investigation of Rocket Numerical Simulations of a Single Modeling Fuel Film Cooling on Effect of Nozzle Spacing on NOx Beeswax and Beeswax With the Thermomechanical Response of Engine Combusting Flowfields Injector Gaseous Methane Rocket Rocket Engine Walls Emissions and Lean Operability Aluminum Powder in Hybrid a Gas to Transient, Spatially Resolved G. Ranuzzi, L. Cutrone, D. Cardillo, M. Combustion Chamber J. Bills, D. Crowe, J. Rutledge, Air Force B. Dolan, R. Villalva Gomez, University Propellant Rocket Engine Thermal Energy Addition: Applications Invigorito, Italian Aerospace Research R. Keller, P. Gerlinger, University of Institute of Technology, Wright-Patterson of Cincinnati, Cincinnati, OH; S. Pack, V. Naoumov, H. Nguyen, B. Alcalde, to LPRE Stability Physics Center (CIRA), Capua, Italy Stuttgart, Stuttgart, Germany AFB, OH; E. Coy, Air Force Research United Technologies Corporation, West Central Connecticut State University, New D. Kassoy, University of Colorado, Boulder, Laboratory, Edwards AFB, CA Des Moines, IA; E. Gutmark, University of Britain, CT Boulder, CO Cincinnati, Cincinnati, OH Friday, 8 January 2016 458-PC-19 Turbulent Combustion IV Harbor C Chaired by: J. MILLER, Air Force Research Laboratory 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2016-2151 AIAA-2016-2152 AIAA-2016-2153 AIAA-2016-2154 AIAA-2016-2155 AIAA-2016-2156 On Radiative Heat Transfer Modeling Radiation-Based Validation of Adjoint-based sensitivity analysis An Integrated Predictive Simulation Numerical Investigation of Experimental Investigation of in Numerical Simulation of a Heavy Combustion Simulations and of localized ignition in a non- Model for the Plasma-Assisted Transverse Forcing in a Multi- the Response of Premixed and Duty Steam Generator Comparison to Heat Release in premixed hydrogen-air mixing Ignition of a Fuel Jet in a Turbulent Element, Shear-Coaxial, High Non-premixed Turbulent Flames to M. Darbandi, B. Abrar, M. Barezban, Sharif Rocket Engines layer Crossflow Pressure Combustor Acoustic Forcing. University of Technology, Tehran, Iran ; G. M. Schulze, T. Fiala, T. Sattelmayer, J. Capecelatro, R. Vishnampet, D. Bodony, L. Massa, J. Freund, University of Illinois, P. Tudisco, R. Ranjan, S. Menon, Georgia A. Kypraiou, N. Worth, E. Mastorakos, Schneider, University of Waterloo, Waterloo, Technical University of Munich, Munich, J. Freund, University of Illinois, Urbana- Urbana-Champaign, Urbana, IL Institute of Technology, Atlanta, GA University of Cambridge, Cambridge, Canada; Y. Shamsaei, M. Nematollahi, Germany Champaign, Urbana, IL United Kingdom Abadan Oil Refining Company, Abadan, Iran Friday, 8 January 2016 459-PDL-13 Numerical Modeling of Plasmas Ocean Beach Chaired by: M. WHITE, Ohio Aerospace Institute and L. RAJA, University of Texas at Austin 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2016-2157 AIAA-2016-2158 AIAA-2016-2159 AIAA-2016-2160 AIAA-2016-2161 AIAA-2016-2162 Numerical simulation of DC Premixed combustion simulations Magnetized Electron Flow Hypersonic BL Transition and Experimental and Kinetic Modeling Investigating the Influence of glow discharges for shock wave with a self-consistent plasma model Calculation Using a Hyperbolic Separation Control by Transient Studies of Novel Carbon Monoxide DBD Plasma Actuators on the Skin modification for initiation. System Electrical Discharge Gas Lasers Friction in Integral Boundary Layer K. Kourtzanidis, L. Raja, University of H. Sitaraman, R. Grout, National R. Kawashima, K. Komurasaki, T. A. Houpt, University of Notre Dame, Notre K. Frederickson, M. Yurkovich, E. Jans, A. Formulation Texas, Austin, Austin, TX; S. Coumar, V. Renewable Energy Laboratory, Golden, CO Schönherr, H. Koizumi, University of Dame, IN; F. Falempin, MBDA, Paris, Chernukho, Z. Eckert, J. Rich, Ohio State S. Bal, R. Balbino Dos Santos Pereira , G. L. Lago, Laboratoire ICARE, CNRS, Orléans, Tokyo, Tokyo, Japan France; S. Leonov, University of Notre University, Columbus, OH; et al. de Oliveira Andrade , D. Ragni, Delft University France Dame, Notre Dame, IN of Technology, Delft, The Netherlands Friday, 8 January 2016 460-SCS-7 Packaging and Deployment of Spacecraft Structures Balboa B Chaired by: G. DAVIS, Jet Propulsion Laboratory and M. THOMSON 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2016-2163 AIAA-2016-2164 AIAA-2016-2165 AIAA-2016-2166 AIAA-2016-2167 AIAA-2016-2168 AIAA-2016-2169 In-Space Structural Assembly: Methods for Characterizing the Starshade Mechanical Architecture Starshade Deployable Inner Disk Deployment Properties with Gravity Novel Folding Methods for Structural Dynamic Response of Applications and Technology Reliability of Deployable Modules & Technology Effort Structure Design and Development Compensation Devices for Boom- Deterministic Deployment of Deployable Thin Shell Reflector in W. Belvin, W. Doggett, J. Watson, J. for Large Optical Reflectors D. Webb, B. Hirsch, V. Bach, J. Sauder, S. B. Hirsch, D. Webb, M. Thomson, Jet Membrane Integrated Wrapped Common Space Structures Folded Configuration Dorsey, J. Warren, T. Jones, NASA Langley K. Hogstrom, S. Pellegrino, California Bradford, M. Thomson, California Institute Propulsion Laboratory, California Institute Structures D. Kling, Folded Structures Company, O. Soykasap, S. Karakaya, A. Gayretli, Research Center, Hampton, VA; et al. Institute of Technology, Pasadena, CA of Technology, Pasadena, CA of Technology, Pasadena, CA H. Furuya, T. Yokomatsu, H. Sakamoto, Ringoes, NJ; S. Jeon, LoadPath, LLC, Y. Akcin, Afyon Kocatepe University, Y. Satou, Tokyo Institute of Technology, Albuquerque, NM; J. Banik, Air Force Afyonkarahisar, Turkey Ookayana, Japan Research Laboratory, Kirtland AFB, NM Friday, 8 January 2016 461-SD-14 Dynamic Loads, Response, and Vibration II Gaslamp A Chaired by: W. SCHNEIDER, Lockheed Martin Aeronautics and B. WILLIS, Jacobs Technology 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2016-2170 AIAA-2016-2171 AIAA-2016-2172 AIAA-2016-2173 AIAA-2016-2174 Substructure Versus Property-Level Acoustic Analysis of A Partially Assessing Sine and Random Non-Stationary Random Vibration Exploring Entropy for Continuous Dispersed Modes Calculation Open Spacecraft Cavity using Multi- Stresses and Fatigue Life Analysis Using Multi-Correlated Systems E. Stewart, J. Peck, NASA Marshall Space Domain Boundary Element Method M. Baker, ATA Engineering, Inc., San Random Processes Excitations D. Tufano, Z. Sotoudeh, Rensselaer Flight Center, Huntsville, AL; C. Fulcher, D. Inoyama, R. Agarwal, T. Stoumbos, Diego, CA Y. Li, Southeast University, Nanjing, Polytechnic Institute, Troy, NY Jacobs, Huntsville, AL; T. Bush, TriVector ATK, Dulles, VA China; S. Mulani, University of Alabama, Services, Inc., Huntsville, AL Tuscaloosa, Tuscaloosa, AL; R. Kapania, Virginia Polytechnic Institute and State University, Blacksburg, VA; S. Wu, Q. Fei, Southeast University, Nanjing, China Friday, 8 January 2016 462-STR-16 Special Session: Stiffened, Stitched Composite Structures La Jolla A Chaired by: A. LOVEJOY, NASA-Langley Research Center and A. PRZEKOP, NASA Langley Research Center 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2016-2175 AIAA-2016-2176 AIAA-2016-2177 AIAA-2016-2178 AIAA-2016-2179 AIAA-2016-2180 Testing of a Stitched Composite Testing and Analysis of a Composite Testing and Analysis of a Composite Imparting Barely Visible Impact Compressive Loading and Modeling Tension and Bending Testing of Large-Scale Pressure Box Non-Cylindrical Aircraft Fuselage Non-Cylindrical Aircraft Fuselage Damage to a Stitched Composite of Stitched Composite Stiffeners an Integral T-cap for Stitched D. Jegley, M. Rouse, A. Przekop, A. Structure, Part I: Ultimate Design Structure, Part II: Severe Damage Large-Scale Pressure Box F. Leone, D. Jegley, NASA Langley Composite Airframe Joints Lovejoy, NASA Langley Research Center, Loads A. Przekop, D. Jegley, A. Lovejoy, M. A. Lovejoy, A. Przekop, NASA Langley Research Center, Hampton, VA; K. A. Lovejoy, F. Leone, NASA Langley Hampton, VA A. Przekop, D. Jegley, A. Lovejoy, M. Rouse, NASA Langley Research Center, Research Center, Hampton, VA Linton, The Boeing Company, Huntington Research Center, Hampton, VA Rouse, NASA Langley Research Center, Hampton, VA; H. Wu, The Boeing Beach, CA Hampton, VA; H. Wu, The Boeing Company, Huntington Beach, CA Company, Huntington Beach, CA Friday, 8 January 2016 463-STR-17 Impact Damage in Composites La Jolla B Chaired by: V. RANATUNGA, Air Force Research Laboratory and T. MANN, NASA-Langley Research Center 0900 hrs 0930 hrs 1000 hrs 1030 hrs AIAA-2016-2181 AIAA-2016-2182 AIAA-2016-2183 AIAA-2016-2184 Low Velocity Impact Test and Modeling Axial Impact Response of Correlating Impact, Micro CT Prediction of Low-Velocity Face-on Analysis of Laminated Structures Sandwich Panels using Probability- Inspection, and Residual Strength Impact Response of Composite M. Falugi, Air Force Research Laboratory, Based Finite Element Analysis of Carbon/Epoxy Rods Laminates using High-Fidelity Finite Wright-Patterson AFB, OH W. Ji, Ulsan National Institute of Science D. Jensen, L. Stanford, Brigham Young Element Modeling Techniques and Technology, Ulsan, South Korea ; A. University, Provo, UT S. Thorsson, University of Michigan, Ann Waas, University of Washington, Seattle, Arbor, Ann Arbor, MI; A. Yoshimura, A. Seattle, WA Waas, University of Washington, Seattle, Seattle, WA; M. Rassaian, The Boeing Company, Seattle, WA Friday, 8 January 2016 464-TP-11 Thermal Systems and Devices: Cryogenics, Thermal Management, and Microdevices Harbor G Chaired by: A. WILLIAMS, Air Force Reseach Laboratory and M. MARTIN, Louisiana State University 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2016-2185 AIAA-2016-2186 AIAA-2016-2187 AIAA-2016-2188 AIAA-2016-2189 AIAA-2016-2190 Cavitation Instabilities in an Pulse Chilldown Tests of a Tank-to- Numerical Simulation for Ice Thermo-Mechanical Simulation of Hydraulic-Powered Forced A Study into Refrigeration Cycle Inducer Using Heated Water as a Tank Liquid Hydrogen Propellant Accretion on Rotating Cowling Crooke’s Cantilevers in the Free- Convection Heat Transfer Working Fluids using an Air Cycle Cryogenic Simulant Transfer Line Considering Water Film Shedding Molecular Flow Regime E. Van Wijk, J. Valdes , K. Pope, Y. Machine Environmental Control D. Jackson, J. Schwille, J. Davitian, The J. Hartwig, NASA Glenn Research Center, Z. Mu, X. Shen, G. Lin, X. Bu, Beihang M. Martin, W. Schmieder, Louisiana State Muzychka, Memorial University of System Aerospace Corporation, El Segundo, CA; Cleveland, OH; E. Rame, Universities University, Beijing, China University, Baton Rouge, LA Newfoundland, St. John’s, Canada T. Childs, A. Jones, R. Chen, Loughborough

C. Lettieri, V. Wang, Z. Spakovszky, Space Research Association, Cleveland, University, Loughborough, United Massachusetts Institute of Technology, OH; J. McQuillen, NASA Glenn Research Kingdom; A. Murray, BAE Systems, Cambridge, MA Center, Cleveland, OH Warton, United Kingdom Friday, 8 January 2016 465-TP-12 Special Session: University Space Systems Programs and Microgravity Flight Activities Harbor H Chaired by: E. SILK, NASA-Goddard Space Flight Center and P. YEE, The Aerospace Corporation 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2016-2191 AIAA-2016-2192 Oral Presentation Oral Presentation Oral Presentation AIAA-2016-2193 From ISS to Mars: Twenty Years Kentucky Re-entry Universal Virginia Tech Spaceflight Programs The University of Tennessee Space Astronautical Engineering at USC: Small Probe Flight Testing of of University of Kentucky Student Payload System J. Black, G. Earle, R. McGwier, Virginia Institute: Historic Accomplishments Ten Years After Thermal Protection Systems in Microgravity and Space Systems J. Cooper, J. Stieha, A. Fowler, A. Martin, Polytechnic Institute and State University, and for Space M. Gruntman, University of Southern Simulated Earth Entries Experiments University of Kentucky, Lexington, Blacksburg, VA Related Research California, Los Angeles, CA A. Sidor, T. Anderson, R. Braun, Georgia S. Smith, University of Kentucky, Lexington, Lexington, KY T. Moeller, J. Schmisseur, University of Institute of Technology, Atlanta, GA Lexington, KY; J. Rexroat, Bluegrass Tennessee Space Institute, Tullahoma, TN Embedded Systems, Lexington, KY Friday, 8 January 2016 466-UMS-11 Unmanned Systems: Detect-and-Avoid II Regatta C Chaired by: R. STANSBURY, Embry-Riddle Aeronautical University and R. CHRISTIANSEN, Sierra Lobo, Inc. 0900 hrs 0930 hrs 1000 hrs 1030 hrs AIAA-2016-2194 AIAA-2016-2195 AIAA-2016-2196 AIAA-2016-2197 Optimization-Based Path Planning Unmanned Aircraft System Sense Path-Planning around Obstacles UAV Collision Avoidance using for Separation Assurance on Small and Avoid Integrity and Continuity: for a Quadrotor UAV Using the RRT a Predictive Rapidly-Exploring Unmanned Aircraft Uncertainty in Aircraft Dynamics Algorithm for Indoor Environments Random Tree (RRT) M. Duffield, A. Ning, T. McLain, Brigham M. Jamoom, M. Joerger, B. Pervan, Illinois S. Bhandari, T. Srinivasan, California S. Bhandari, J. Farinella, C. Lay, California Young University, Provo, UT Institute of Technology, Chicago, IL Polytechnic State University, Pomona, CA Polytechnic State University, Pomona, CA Friday, 8 January 2016 467-WE-12 Wind Energy: Wind Plant Optimization Harbor I Chaired by: M. LACKNER, University of Massachusetts 0900 hrs 0930 hrs 1000 hrs 1030 hrs AIAA-2016-2198 AIAA-2016-2199 AIAA-2016-2200 AIAA-2016-2201 Towards Wind Farm Layout Design Adjoint Optimization of wind Farm Reduced order model for optimization Wind Farm Modeling and Using Sensitivity Derivatives Layouts for Systems Engineering of power production from a wind farm Control Using Dynamic Mode Obtained from a Parabolic Method Analysis G. Iungo, University of Texas, Dallas, Decomposition A. Mittal, K. Sreenivas, W. Briley, L. Taylor, R. King, P. Hamlington, University of Richardson, TX; F. Viola, Swiss Federal Institute J. Annoni, J. Nichols, P. Seiler, University University of Tennessee, Chattanooga, Colorado, Boulder, Boulder, CO; K. Dykes, of Technology, Lausanne, Switzerland; U. Ciri, of Minnesota, Minneapolis, Minneapolis, Chattanooga, TN P. Graf, National Renewable Energy S. Leonardi, M. Rotea, University of Texas, MN Laboratory, Golden, CO Dallas, Richardson, TX

Author/Session Chair Index Abbas, Z., 121-APA-13 Acosta, D., 188-GNC-18 Ahmad, N., 98-SD-4 Alexeenko, A., 104-TP-3, 361-PDL-10 An, D., 357-NDA-6 Abbasi, M., 39-PC-1 Action, J., 156-STR-4, 208-STR-6 Ahmed, H., 199-MAT-6 AlHababi, T., 210-TES-5 An, Q., 92-PC-3 Abbott, T., 392-GNC-32 Adachi, M., 155-SRE-2 Ahmed, I., 267-WE-5 Alhajeri, H., 52-TES-2/TP-1 An, X., 16-FD-3 Abbud-Madrid, A., 48-SRE-1 Adamec, S., 278-APA-28 Ahmed, K., 93-PC-4, 193-GTE-7 Ali, M., 328-AFM-11 Anderson, E., 250-MDO-5 Abdalla, M., 417-STR-14 Adamovich, I., 41-PDL-1, 150-PDL-5/PC-7/AMT-3, Ahmed, M., 92-PC-3 Allaerts, D., 421-WE-10 Anderson, F., 23-GNC-4 Abdelattif, O., 289-GEPC-4, 455-MST-15 257-PDL-7 Ahmed, N., 297-IS-7, 352-IS-9 Allaire, D., 303-NDA-5 Anderson, M., 54-UMS-1, 312-SEN-2, 436-APA-45 AbdelGhany, E., 289-GEPC-4 Adams, J., 29-IS-1/ICC-1/DA-1 Ahmed, S., 26-GTE-1 Allemand, G., 436-APA-45 Anderson, R., 212-UMS-4 Abdelkefi, A., 44-SD-2, 198-MAT-5, 199-MAT-6, 3 Adams, N., 72-FD-12 Ahsun, U., 121-APA-13 Allen, A., 189-GNC-19 Anderson, T., 8-AFM-2, 465-TP-12 74-ACD-11 Adams, V., 446-GNC-38 Ahuja, K., 5-AA-1 Allen, C., 121-APA-13, 279-APA-29, 330-APA-32, Anderson, W., 184-FD-26/APA-21, 360-PC-15, Abdelmaksoud, W., 210-TES-5 Addali A., A., 52-TES-2/TP-1 Ai, Q., 177-ASC-2, 334-APA-36 386-FD-48 404-MDO-8, 405-MST-12, 411-PC-17 Abdelmoula, H., 44-SD-2 Adkins, C., 446-GNC-38 Aidi, B., 198-MAT-5 Allen, D., 190-GNC-20 Andersson, N., 115-AA-3 Abdelouahab, M., 443-FD-58 Adler, M., 19-FD-6 AI-Emrani, F., 160-UMS-3 Allen, J., 47-SOF-1, 52-TES-2/TP-1, 406-MST-13 Andino, M., 16-FD-3, 185-GEPC-3 Abdel-Salam, T., 289-GEPC-4 Adolf, F., 101-SOF-3 Aigner, M., 130-FD-18 Allen, R., 291-GNC-25 Andrade, L., 445-GNC-37 Abdi, F., 202-NDA-3, 208-STR-6 Advani, S., 301-MST-9 Akcin, Y., 460-SCS-7 Allison, D., 145-MDO-3, 250-MDO-5, 354-MDO-7 Andreoli, V., 193-GTE-7 Abdollahi, V., 17-FD-4 Afonso, F., 170-ACD-3 Akella, M., 24-GNC-5, 189-GNC-19 Allison, J., 35-MDO-1 Andrews, G., 31-ISC-2 Abdul Ghaffar, A., 293-GNC-27 Afsar, M., 240-FD-32 Akhtar, I., 44-SD-2 Allison, P., 93-PC-4 Andrienko, D., 159-TP-5, 265-TP-7 Abdulrahim, A., 107-WE-1 Aftosmis, M., 211-TP-6 Akhtar, S., 171-AFM-6, 225-AFM-7 Allison, R., 355-MST-11 Andrle, M., 133-GNC-12 Abedi, H., 267-WE-5 Agarwal, R., 17-FD-4, 104-TP-3, 130-FD-18, 183-FD-25, Akita, T., 258-SCS-3 Al Masoud, N., 384-EDU-2 Andrus, I., 28-HSABP-1, 296-HSABP-5 Abgrall, R., 126-FD-10 239-FD-31, 341-FD-45, 378-APA-37, 380-APA-39, Akkala, J., 342-FD-46 Alonso, J., 43-SD-1, 88-MDO-2, 147-NDA-2, Anemaat, W., 273-ACD-6, 326-ACD-9 Aboud, J., 210-TES-5 440-FD-55, 461-SD-14 Akpinar-Elci, M., 382-ASC-6 194-HSABP-3, 223-ACD-4, 299-MDO-6, 330-APA-32, Angilella, A., 335-ASC-5 Aboutalib, O., 406-MST-13 Agate, M., 442-FD-57 Aksu, T., 139-GTE-5 428-ACD-13 Anik, E., 107-WE-1 Abou Zeid, A., 289-GEPC-4 Aggarwal, P., 35-MDO-1, 209-STR-7 Alam, M., 76-GNC-6 AlQadi, I., 444-FD-59 Anjaly, P., 448-GNC-40 Abrahams, R., 316-SUR-2 Agha-mohammadi, A., 297-IS-7 Alaverdi, O., 355-MST-11 Altman, A., 230-APA-24, 391-FD-53, 436-APA-45 Annaswamy, A., 292-GNC-26 Abrar, B., 458-PC-19 Aglietti, G., 258-SCS-3, 309-SCS-4 Al-Battal, N., 387-FD-49 Alvi, F., 115-AA-3, 221-AA-5 Annoni, J., 467-WE-12 Abras, J., 65-APA-8 Agnes, G., 86-LEC-2 Albert, V., 406-MST-13 Aly, A., 37-MST-2, 300-MST-8, 455-MST-15 Ansell, P., 64-APA-7, 69-FD-8, 121-APA-13, 175-APA-18 Abukhwejah, A., 102-STR-3 Agocs, J., 25-GT-1 Alberts, S., 340-FD-44 Alyanak, E., 145-MDO-3, 357-NDA-6 Antcliff, K., 224-ACD-5 Abul-Huda, Y., 351-HSABP-6 Agostinelli, C., 311-SD-9 Alberts, T., 233-ASC-3 Amadori, K., 169-ACD-2 Anthony, R., 82-GTE-3, 193-GTE-7, 255-PC-9/GTE-9, Abumi, Y., 89-MST-3 Agostini, L., 5-AA-1, 71-FD-11, 131-FD-19, 238-FD-30, Albertson, C., 170-ACD-3 Amano, R., 52-TES-2/TP-1, 103-TES-3, 139-GTE-5, 399-GTE-14 Acar, B., 208-STR-6 287-FD-38 Albring, T., 330-APA-32 210-TES-5 Antony, T., 61-AFM-4 Acar, P., 34-MAT-2, 368-STR-13 Agrawal, A., 40-PC-2, 52-TES-2/TP-1 Alcalde, B., 457-PC-18 Amaral Teixeira, J., 52-TES-2/TP-1 Antunes, A., 120-APA-12 Accardo, D., 260-SEN-1, 312-SEN-2 Agrawal, B., 167-AA-4 Alderliesten, R., 198-MAT-5 Amato, C., 297-IS-7 Antunes, E., 33-MAT-1 Acharya, S., 193-GTE-7 Agrawal, P., 317-TP-8 Al-Dujaly, H., 440-FD-55 Amaya-Bower, L., 125-DE-1 Aono, H., 72-FD-12 Acheson, M., 137-GT-3 Agte, J., 37-MST-2 Aleksandrov, N., 41-PDL-1, 204-PC-8 Ames, F., 193-GTE-7 Aoyama, T., 120-APA-12, 280-APA-30, Acikmese, B., 79-GNC-9 Aguiar, A., 190-GNC-20 Alenezi, A., 52-TES-2/TP-1 Amezquita-Brooks, L., 327-AFM-10 288-FD-39/APA-31, 380-APA-39 Ackerman, K., 134-GNC-13 Agyei, R., 87-MAT-3 Alexander, M., 16-FD-3, 185-GEPC-3 Amitay, M., 391-FD-53 Apker, T., 195-ICC-2, 260-SEN-1 Ackermann, J., 441-FD-56 Ahern, S., 407-MVC-2 Alexander, W., 272-AA-6 Amrit, A., 88-MDO-2, 330-APA-32 Aponso, B., 89-MST-3 Author/Session Chair Index Arabshahi, A., 232-APA-26 Ayers, B., 127-FD-15 Ballouz, E., 188-GNC-18 Beaverstock, C., 68-ASC-1 Bey, K., 105-TP-4 Arakawa, Y., 370-WE-8 Ayers, D., 378-APA-37 Banchy, M., 308-SATS-3 Beberniss, T., 10-AMT-10/SD-15 Beyar, M., 6-ABPSI-1/GEPC-1 Araujo-Estrada, S., 450-GT-9 Ayers, G., 245-GT-5 Bane, S., 257-PDL-7 Beblo, R., 329-AMT-7 Beyer, F., 421-WE-10 Arce Leon, C., 221-AA-5 Ayoubi, M., 235-DSC-2 Banfield, C., 434-APA-43 Beck, J., 87-MAT-3, 153-SD-5, 202-NDA-3, 393-GNC-33 Beyhaghi, S., 139-GTE-5 Arena, A., 24-GNC-5, 275-AFM-9 Ayrault, T., 233-ASC-3 Banik, J., 152-SCS-1, 206-SCS-2, 460-SCS-7 Becker, R., 25-GT-1, 81-GT-2 Bezos O’Connor, G., 185-GEPC-3 Arents, R., 251-MST-6 Azarpeyvand, M., 177-ASC-2, 334-APA-36 Bansal, P., 415-SD-13 Beckingsale, D., 386-FD-48 Bhamidipati, K., 228-APA-22 Arepalli, S., 210-TES-5 Azevedo, J., 64-APA-7, 120-APA-12 Bao, J., 151-SATS-1 Bednarcyk, B., 208-STR-6, 249-MAT-7, 367-STR-12, Bhandari, S., 24-GNC-5, 201-MST-5, 266-UMS-6, Aretskin-Hariton, E., 300-MST-8 Azocar, A., 30-ISC-1 Barad, K., 308-SATS-3 418-STR-15 420-UMS-10, 466-UMS-11 Argrow, B., 266-UMS-6 Babbie, C., 93-PC-4 Barad, M., 176-APA-20 Beeby, T., 441-FD-56 Bhasin, N., 23-GNC-4 Ariff, O., 244-GNC-23, 327-AFM-10 Babel, W., 245-GT-5 Barakos, G., 17-FD-4, 65-APA-8, 70-FD-9, 176-APA-20, Behroozinia, P., 405-MST-12 Bhat, B., 33-MAT-1, 298-MAT-8 Arjomandi, M., 64-APA-7 Babinsky, H., 13-APA-4, 63-APA-6/FD-7, 74-FD-14 381-APA-40 Behrouzifar, A., 318-WE-7 Bhate, H., 308-SATS-3 Armanini, S., 7-AFM-1, 327-AFM-10 Babuska, V., 98-SD-4 Barber, T., 379-APA-38 Bekemeyer, P., 311-SD-9 Bhatia, D., 331-APA-33 Arnold, J., 211-TP-6 Baccarella, D., 131-FD-19, 248-HSABP-4 Barbu, I., 177-ASC-2 Bel, H., 37-MST-2 Bhatia, G., 207-SE-3 Arnold, S., 208-STR-6, 249-MAT-7 Bach, A., 213-WE-4 Barcenas, L., 34-MAT-2 Belcastro, C., 22-GNC-3, 78-GNC-8, 134-GNC-13, Bhatia, M., 234-DSC-1 Arslantas, Y., 186-GNC-16 Bach, V., 460-SCS-7 Barchfeld, C., 436-APA-45 188-GNC-18, 226-AFM-8, 301-MST-9 Bhaumik, S., 238-FD-30, 386-FD-48 Arthur, M., 399-GTE-14 Badakhshan, A., 40-PC-2 Bardet, P., 10-AMT-10/SD-15, 329-AMT-7 Bellan, J., 39-PC-1, 306-PC-13 Bhoelai, V., 34-MAT-2 Arthurs, F., 243-GNC-22 Badhan, A., 210-TES-5 Barezban, M., 458-PC-19 Belley, C., 404-MDO-8 Bhuiyan, F., 209-STR-7 Artzt, K., 87-MAT-3 Badra, J., 305-PC-12 Barger, W., 202-NDA-3 Beltz, J., 127-FD-15 Bialy, E., 210-TES-5 Arunajatesan, S., 58-AA-2, 167-AA-4, 286-FD-37 Bae, H., 90-NDA-1, 147-NDA-2, 357-NDA-6 Barlas, A., 268-WE-6 Belvin, W., 86-LEC-2, 460-SCS-7 Biava, M., 17-FD-4, 381-APA-40 Arya, M., 413-SCS-6 Baeder, J., 228-APA-22, 386-FD-48 Barmore, B., 343-GNC-28, 392-GNC-32 Benchergui, D., 117-ACD-1, 168-ABPSI-4 Biber, K., 175-APA-18 Asada, H., 284-FD-35 Baej, H., 246-GTE-8 Barnard, C., 240-FD-32 Bencomo, A., 293-GNC-27 Bichlmeier, M., 132-GNC-11 Asai, K., 431-AMT-9 Bahamonde Jacome, L., 354-MDO-7 Barnes, C., 287-FD-38 Bender, M., 201-MST-5, 302-MST-10 Bickel, R., 419-TP-10 Asamura, K., 133-GNC-12 Bai, X., 392-GNC-32 Barnhardt, M., 159-TP-5 Bendris, B., 345-GNC-30/ACD-10 Biedron, R., 278-APA-28 Ash, R., 48-SRE-1 Baier, F., 348-GTE-11, 398-GTE-13 Barone, M., 422-WE-11 Benedict, M., 30-ISC-1, 31-ISC-2, 266-UMS-6 Bieniawski, S., 299-MDO-6

Ashby, R., 193-GTE-7 Baier, H., 177-ASC-2, 417-STR-14 Barrett-Gonzalez, R., 68-ASC-1, 169-ACD-2, 223-ACD-4 Benek, J., 74-FD-14, 284-FD-35 Bigarella, E., 120-APA-12 Ashcraft, T., 181-FD-23/PDL-6 Bailey, J., 116-ABPSI-3 Barrington, P., 331-APA-33 Ben Haj Ali, A., 180-FD-22 Bijewitz, J., 168-ABPSI-4 Ashley, A., 283-FD-34 Bailey, M., 207-SE-3 Bartan, B., 208-STR-6 Bennett, W., 129-FD-17 Bijl, H., 58-AA-2, 356-MVC-1 Ashokkumar, C., 80-GNC-10, 136-GNC-15, 201-MST-5, Bailey, R., 437-DA-2 Barth, T., 229-APA-23/FD-27 Benoit, C., 439-FD-54 Bijnens, N., 46-SEO-1 275-AFM-9 Bailey, S., 126-FD-10, 317-TP-8 Bartkowicz, T., 415-SD-13 Bentley, B., 141-HSABP-2 Bil, C., 170-ACD-3, 325-ACD-8, 374-ACD-11 Ashuri, T., 371-WE-9, 422-WE-11 Bailie, S., 27-GTE-2 Bartley-Cho, J., 315-STR-11 Benton, S., 342-FD-46, 387-FD-49 Bilgen, O., 43-SD-1, 177-ASC-2, 233-ASC-3, 382-ASC-6 Aso, S., 231-APA-25 Bak, M., 96-PDL-4 Barto, A., 152-SCS-1 Beran, P., 147-NDA-2, 303-NDA-5, 335-ASC-5 Billard, F., 341-FD-45 Atanian, M., 273-ACD-6 Baker, J., 107-WE-1 Bartram, G., 90-NDA-1 Berdanier, R., 82-GTE-3, 138-GTE-4 Bills, J., 457-PC-18 Ates, U., 449-GNC-41 Baker, M., 415-SD-13, 461-SD-14 Barut, A., 368-STR-13 Beresh, S., 10-AMT-10/SD-15, 172-AMT-4, 241-FD-33, Bindra, U., 133-GNC-12 Atescan, Y., 382-ASC-6 Bakhtiarinejad, M., 200-MDO-4 Baruzzi, G., 338-FD-42 276-AMT-6/PC-11/PDL-8, 286-FD-37, 443-FD-58 Birch, T., 67-APA-10 Atkins, E., 22-GNC-3, 403-IS-11 Bakkar, A., 285-FD-36 Basom, B., 330-APA-32 Berger, M., 211-TP-6 Birouk, M., 340-FD-44 Atkins, H., 226-AFM-8 Bal, H., 144-MAT-4 Bass, J., 316-SUR-2 Berger, T., 8-AFM-2 Bis, R., 453-IS-13 Atkinson, C., 252-MST-7 Bal, S., 459-PDL-13 Basset, M., 396-GNC-36 Berger, Z., 240-FD-32 Bisagni, C., 208-STR-6, 368-STR-13 Atreya, S., 223-ACD-4 Balaban, E., 453-IS-13 Bassetti, A., 25-GT-1 Bergeron, K., 328-AFM-11, 334-APA-36, 379-APA-38 Bisek, N., 19-FD-6, 71-FD-11, 239-FD-31, Attili, A., 40-PC-2 Balabanov, V., 404-MDO-8 Basso, E., 120-APA-12 Bergsma, M., 8-AFM-2 307-PDL-9/FD-40 Atwood, C., 122-APA-14 Balachandran, S., 22-GNC-3 Bateman, A., 78-GNC-8, 188-GNC-18 Bering, E., 308-SATS-3 Bisetti, F., 40-PC-2 Aubry, R., 278-APA-28 Balakrishna, S., 137-GT-3 Bates, D., 445-GNC-37 Berkefeld, T., 25-GT-1 Bishop, M., 135-GNC-14 Auslender, A., 222-ABPSI-5 Balakrishnan, S., 232-APA-26 Bauer, K., 16-FD-3 Bernal, L., 63-APA-6/FD-7, 230-APA-24 Bishop, R., 23-GNC-4 Ausseil, R., 178-DE-2 Balakumar, A., 23-GNC-4 Bauer, S., 222-ABPSI-5 Bernhammer, L., 364-SD-10 Bissonnette, W., 436-APA-45 Ausserer, J., 168-ABPSI-4 Balakumar, P., 15-FD-2, 182-FD-24, 389-FD-51 Baurle, R., 402-HSABP-7 Bernstein, D., 292-GNC-26 Bittner, M., 328-AFM-11 Austin, J., 419-TP-10 Balan, A., 455-MST-15 Bayandor, J., 46-SEO-1, 153-SD-5, 405-MST-12 Berry, M., 348-GTE-11, 398-GTE-13 Black, J., 153-SD-5, 393-GNC-33, 465-TP-12 Austin, N., 249-MAT-7 Balas, M., 83-IS-2, 132-GNC-11, 190-GNC-20 Bayard, D., 378-APA-37 Berry, S., 199-MAT-6 Blackburn, R., 351-HSABP-6 Avallone, F., 221-AA-5, 257-PDL-7 Balasiu, A., 299-MDO-6 Bazin, J., 376-AFM-13 Bershadsky, D., 125-DE-1, 275-AFM-9 Blackstun, M., 134-GNC-13 Avila, A., 33-MAT-1 Balbino Dos Santos Pereira, R., 459-PDL-13 Bean, J., 272-AA-6 Bertagne, C., 335-ASC-5 Blades, E., 282-DSC-3, 356-MVC-1 Avila, R., 262-STR-8 Balch, M., 303-NDA-5 Bear, P., 26-GTE-1 Berton, J., 348-GTE-11 Blaisdell, G., 58-AA-2 Avital, E., 69-FD-8 Baldacchino, D., 267-WE-5 Beard, R., 420-UMS-10 Bevan, R., 279-APA-29 Blakely, C., 338-FD-42 Awad, A., 186-GNC-16, 290-GNC-24 Balesdent, M., 202-NDA-3 Beard, S., 89-MST-3, 252-MST-7 Bevilaqua, P., 428-ACD-13 Blanchette, S., 56-SOF-2 Aweiss, A., 346-GNC-31 Ballestero, M., 149-PC-6 Beaty, N., 84-ISC-3 Bewley, T., 178-DE-2 Bland, S., 349-GTE-12 Author/Session Chair Index Blandino, J., 151-SATS-1, 205-SATS-2, 363-SCS-5 Bourquard, N., 390-FD-52 Brown, J., 87-MAT-3, 90-NDA-1, 153-SD-5, 202-NDA-3 Butler, D., 137-GT-3 Carrese, R., 332-APA-34, 414-SD-12 Blankson, I., 194-HSABP-3, 354-MDO-7 Bovier-Lapierre, X., 244-GNC-23, 327-AFM-10 Brown, M., 36-MST-1, 141-HSABP-2, 272-AA-6 Butte, E., 124-CMS-1/CPS-1 Carrier, G., 277-APA-27 Blattnig, S., 90-NDA-1 Bowen, P., 246-GTE-8 Brown, N., 420-UMS-10 Buttsworth, D., 234-DSC-1, 245-GT-5 Carrion, M., 17-FD-4, 381-APA-40 Blaylock, M., 268-WE-6 Bowersox, R., 241-FD-33 Brown, R., 154-SD-6 Buxton, O., 183-FD-25 Carroll, D., 41-PDL-1 Blechschmidt, M., 16-FD-3 Bowles, D., 384-EDU-2 Brown, T., 100-SEO-2, 445-GNC-37 Buysse, A., 178-DE-2 Carroll, T., 381-APA-40 Blevins, J., 119-APA-11 Bowman, C., 196-IS-5 Bruce, P., 19-FD-6, 74-FD-14, 183-FD-25, 241-FD-33, Byun, K., 415-SD-13 Carson, J., 23-GNC-4, 79-GNC-9 Bloebaum, C., 147-NDA-2, 207-SE-3 Bowman, S., 392-GNC-32 332-APA-34, 433-APA-42 Cabrera, L., 52-TES-2/TP-1, 210-TES-5 Carter, C., 41-PDL-1, 92-PC-3, 141-HSABP-2, Blonigan, P., 64-APA-7 Box, S., 297-IS-7 Bruce, W., 435-APA-44 Cacan, M., 244-GNC-23 150-PDL-5/PC-7/AMT-3, 204-PC-8, 340-FD-44 Blood, D., 53-TP-2, 431-AMT-9 Boxx, I., 40-PC-2, 92-PC-3 Bruckner, A., 295-HIS-3 Cacciola, S., 371-WE-9 Carter, D., 117-ACD-1, 274-ACD-7 Bluman, J., 98-SD-4 Boyd, D., 272-AA-6 Brügge-Zobel, T., 274-ACD-7 Cadel, D., 172-AMT-4 Carter, M., 6-ABPSI-1/GEPC-1, 59-ABPSI-2/GEPC-2, Bodlak, E., 275-AFM-9 Boyd, I., 105-TP-4, 159-TP-5, 265-TP-7 Brulatout, J., 73-FD-13 Cadou, C., 92-PC-3, 204-PC-8 405-MST-12, 435-APA-44 Bodony, D., 388-FD-50, 458-PC-19 Boyer, N., 234-DSC-1 Brunet, V., 331-APA-33 Caetano, J., 7-AFM-1 Cartmell, D., 36-MST-1, 302-MST-10 Bogdanor, M., 208-STR-6 Bozan, A., 22-GNC-3, 301-MST-9 Brunner, C., 79-GNC-9 Cagle, C., 137-GT-3 Casbeer, D., 297-IS-7, 448-GNC-40 Boge, T., 80-GNC-10, 189-GNC-19 Bradford, S., 152-SCS-1, 460-SCS-7 Brunton, S., 14-FD-1/APA-5 Cahoy, K., 344-GNC-29 Case, S., 198-MAT-5 Bogey, C., 58-AA-2 Brady, J., 160-UMS-3 Brusniak, L., 6-ABPSI-1/GEPC-1 Cai, C., 369-TP-9 Casper, K., 10-AMT-10/SD-15, 172-AMT-4, 241-FD-33, Boghozian, T., 298-MAT-8 Braginsky, M., 156-STR-4 Bryant, L., 100-SEO-2 Cai, J., 222-ABPSI-5, 405-MST-12 286-FD-37, 339-FD-43 Bohun, M., 87-MAT-3 Bramesfeld, G., 64-APA-7, 381-APA-40, 436-APA-45 Brynildsen, S., 450-GT-9 Cairns, D., 157-STR-5, 162-WE-3 Cassel, K., 18-FD-5, 341-FD-45 Boland, E., 301-MST-9 Brandis, A., 211-TP-6 Bryson, D., 64-APA-7 Calderon, D., 383-DSC-5 Cassell, A., 10-AMT-10/SD-15 Bolender, M., 8-AFM-2, 292-GNC-26, Brandt, S., 117-ACD-1 Bryson, K., 211-TP-6 Caley, T., 452-GTE-16 Castagnetta, J., 30-ISC-1 394-GNC-34/ACD-12 Branyan, C., 160-UMS-3 Bu, X., 464-TP-11 Calomino, A., 10-AMT-10/SD-15 Castellani, M., 336-DSC-4, 383-DSC-5 Bollino, K., 190-GNC-20, 376-AFM-13 Brasseur, J., 107-WE-1, 267-WE-5 Bucci, L., 187-GNC-17 Calvert, M., 176-APA-20 Castellanos, A., 262-STR-8 Bolzon, M., 64-APA-7 Braun, J., 192-GTE-6 Buchholz, J., 342-FD-46 Calvert, N., 9-AMT-1 Castner, R., 435-APA-44 Bombardieri, R., 50-STR-2 Braun, R., 8-AFM-2, 46-SEO-1, 61-AFM-4, 144-MAT-4, Buckley, T., 30-ISC-1 Camacho, P., 59-ABPSI-2/GEPC-2 Castrichini, A., 336-DSC-4 Bomphrey, R., 63-APA-6/FD-7 317-TP-8, 465-TP-12 Buelthoff, H., 251-MST-6, 454-MST-14 Cameron, C., 381-APA-40 Caswell, A., 92-PC-3, 94-PC-5, 168-ABPSI-4,

Bond, R., 239-FD-31 Braza, M., 439-FD-54 Bugarin, L., 210-TES-5 Campagnolo, F., 371-WE-9 255-PC-9/GTE-9 Bone, R., 343-GNC-28 Brazell, M., 184-FD-26/APA-21, 439-FD-54 Buoso, S., 154-SD-6 Campbell, J., 379-APA-38 Cattafesta, L., 127-FD-15, 237-FD-29, 286-FD-37 Bonet, J., 6-ABPSI-1/GEPC-1, 59-ABPSI-2/GEPC-2 Breger, L., 297-IS-7 Burces, J., 333-APA-35/FD-41 Campbell, T., 337-EDU-1 Cavallaro, R., 50-STR-2, 383-DSC-5 Bonitz, S., 379-APA-38 Brehm, C., 176-APA-20 Burchett, B., 118-AFM-5 Campisi, M., 382-ASC-6 Cavus, N., 428-ACD-13 Bonnavion, G., 285-FD-36 Brenner, M., 259-SD-7 Burdette, D., 35-MDO-1 Canacci, V., 191-GT-4 Cazin, R., 149-PC-6 Bons, J., 342-FD-46, 387-FD-49 Brentner, K., 272-AA-6 Burgaud, F., 354-MDO-7 Candler, G., 75-FD-20, 104-TP-3, 126-FD-10, 440-FD-55 Cebeci, H., 382-ASC-6 Booher, J., 98-SD-4 Bretl, T., 24-GNC-5 Burk, T., 445-GNC-37 Candon, M., 414-SD-12 Cebon, D., 249-MAT-7 Borener, S., 287-FD-38 Brewer, J., 337-EDU-1 Burke, T., 275-AFM-9 Candon, S., 116-ABPSI-3 Cecil, O., 31-ISC-2 Borer, N., 169-ACD-2, 223-ACD-4 Brezillon, J., 64-APA-7 Burkhard, C., 211-TP-6 Canfield, R., 250-MDO-5 Cecil, T., 266-UMS-6 Boretskij, V., 95-PDL-3 Briceno, S., 178-DE-2 Burklund, M., 11-APA-2 Cantor, C., 452-GTE-16 Cecrdle, J., 415-SD-13 Borg, M., 75-FD-20, 128-FD-16, 339-FD-43 Bridges, D., 160-UMS-3 Burks, B., 301-MST-9 Cantu, L., 141-HSABP-2, 377-AMT-8 Celani, F., 21-GNC-2 Borghesi, G., 359-PC-14 Bridges, J., 348-GTE-11 Burleigh, S., 100-SEO-2 Cao, T., 452-GTE-16 Celebi, M., 302-MST-10 Borker, R., 284-FD-35 Bridges, W., 376-AFM-13 Burley, C., 185-GEPC-3, 272-AA-6 Cao, Y., 405-MST-12, 448-GNC-40 Celikovsky, S., 76-GNC-6 Börner, M., 232-APA-26 Briggs, F., 101-SOF-3 Burnell, E., 428-ACD-13 Cap, J., 43-SD-1 Celmins, I., 171-AFM-6 Boroson, E., 299-MDO-6 Briggs, H., 178-DE-2 Burns, K., 124-CMS-1/CPS-1, 247-HIS-2, 400-HIS-5 Capecelatro, J., 458-PC-19 Cerimele, C., 79-GNC-9 Bos, J., 22-GNC-3 Briley, W., 467-WE-12 Burns, M., 84-ISC-3 Caracciolo, R., 154-SD-6 Cesnik, C., 282-DSC-3, 364-SD-10, 383-DSC-5, Bosco, E., 438-DSC-6 Brink, A., 43-SD-1 Burnside, N., 6-ABPSI-1/GEPC-1, 431-AMT-9 Carandente, V., 367-STR-12, 405-MST-12 414-SD-12, 438-DSC-6 Boskovic, J., 78-GNC-8, 235-DSC-2, 346-GNC-31 Brink, K., 448-GNC-40 Burr, J., 255-PC-9/GTE-9 Carbajal, S., 294-GTE-10 Cetiner-Yildirim, O., 63-APA-6/FD-7 Boslough, M., 211-TP-6 Brinton, C., 54-UMS-1 Burress, T., 406-MST-13 Cardillo, D., 457-PC-18 Cetraro, G., 287-FD-38 Bossert, D., 318-WE-7 Brito Gadeschi, G., 129-FD-17 Burrows, T., 16-FD-3 Cardullo, F., 251-MST-6 Ceze, M., 180-FD-22, 184-FD-26/APA-21, Bossuyt, J., 421-WE-10 Broniewicz, A., 379-APA-38 Burrus, D., 94-PC-5 Caridi, G., 227-AMT-5 229-APA-23/FD-27 Böswald, M., 221-AA-5 Brooker, B., 172-AMT-4 Burt, J., 104-TP-3, 159-TP-5 Carlson, J., 282-DSC-3 Chadha, P., 45-SE-1 Botero, E., 273-ACD-6 Brooks, J., 245-GT-5 Busa, K., 141-HSABP-2 Carolan, D., 298-MAT-8 Chae, S., 18-FD-5 Botez, R., 233-ASC-3 Brooks, T., 250-MDO-5 Buschhagen, T., 246-GTE-8, 294-GTE-10 Carpenter, J., 48-SRE-1 Chaganti, N., 172-AMT-4 Bottasso, C., 371-WE-9 Broumand, M., 340-FD-44 Bush, T., 461-SD-14 Carpenter, M., 171-AFM-6, 229-APA-23/FD-27 Chahat, N., 151-SATS-1 Boucher, D., 48-SRE-1 Brouwer, K., 234-DSC-1 Bussink, F., 345-GNC-30/ACD-10 Carr, R., 394-GNC-34/ACD-12 Chahl, J., 7-AFM-1, 374-ACD-11 Bouheraoua, L., 93-PC-4 Brown, A., 97-SD-3 Butcher, E., 77-GNC-7 Carr, Z., 53-TP-2, 119-APA-11 Chaidez, M., 52-TES-2/TP-1, 210-TES-5 Bourassa, C., 340-FD-44 Brown, C., 5-AA-1, 115-AA-3 Butler, B., 317-TP-8, 406-MST-13, 419-TP-10 Carrella, A., 336-DSC-4 Chaitanya Kumar Rao, D., 359-PC-14 Author/Session Chair Index Chakrabarty, A., 61-AFM-4 Cheng, R., 6-ABPSI-1/GEPC-1 Chuan, Y., 106-UMS-2 Collins, E., 115-AA-3, 167-AA-4 Crafton, J., 245-GT-5, 431-AMT-9 Chakraborty, I., 45-SE-1 Cheng, Y., 79-GNC-9, 344-GNC-29 Chudoba, B., 125-DE-1 Collins, J., 237-FD-29, 245-GT-5 Craig, T., 212-UMS-4 Chakravarthy, A., 346-GNC-31 Chern, S., 70-FD-9 Chughtai, F., 171-AFM-6 Colonius, T., 16-FD-3, 442-FD-57 Crain, T., 23-GNC-4 Challa, V., 448-GNC-40 Chernukho, A., 257-PDL-7, 459-PDL-13 Chujo, T., 258-SCS-3 Colvin, K., 60-AFM-3 Cramer, N., 233-ASC-3, 312-SEN-2 Chamberlain, M., 363-SCS-5 Cheung, A., 451-GTE-15 Chung, S., 35-MDO-1, 291-GNC-25 Combs, C., 377-AMT-8 Crane, B., 48-SRE-1 Chambers, J., 93-PC-4 Cheung, K., 233-ASC-3 Churchfield, M., 107-WE-1 Comer, A., 411-PC-17 Cranston, B., 102-STR-3 Chamitoff, G., 135-GNC-14 Chi, W., 190-GNC-20 Chwalowski, P., 282-DSC-3, 379-APA-38 Commo, S., 347-GT-7 Crassidis, J., 133-GNC-12, 243-GNC-22 Chan, D., 137-GT-3, 173-APA-16, 379-APA-38 Chiba, K., 125-DE-1 Chynoweth, B., 75-FD-20 Concilio, A., 233-ASC-3, 281-ASC-4 Craven, B., 107-WE-1 Chan, J., 339-FD-43 Chilan, C., 35-MDO-1 Ciarcia, M., 187-GNC-17 Cone, A., 346-GNC-31 Crawford, C., 209-STR-7, 303-NDA-5 Chan, W., 173-APA-16, 334-APA-36, 402-HSABP-7 Childress, J., 87-MAT-3 Ciarella, A., 68-ASC-1 Conner, J., 24-GNC-5 Crean, J., 283-FD-34 Chandrasekaran, B., 346-GNC-31 Childs, R., 123-APA-15 Cichella, V., 134-GNC-13 Connolly, B., 340-FD-44 Creary, G., 125-DE-1 Chanel, C., 54-UMS-1 Childs, T., 245-GT-5, 419-TP-10, 464-TP-11 Ciminello, M., 281-ASC-4 Connolly, J., 282-DSC-3, 345-GNC-30/ACD-10, Crespo, L., 90-NDA-1 Chang, B., 188-GNC-18 Chin, A., 228-APA-22 Cinar, G., 45-SE-1 448-GNC-40 Creta, F., 149-PC-6 Chang, C., 15-FD-2, 229-APA-23/FD-27, 451-GTE-15 Chin, J., 145-MDO-3, 160-UMS-3 Ciottoli, P., 149-PC-6 Conte, J., 153-SD-5 Crider, D., 22-GNC-3, 78-GNC-8, 134-GNC-13, Chang, J., 7-AFM-1, 222-ABPSI-5 Chin, T., 200-MDO-4 Ciri, U., 467-WE-12 Convery, J., 246-GTE-8 188-GNC-18, 226-AFM-8, 301-MST-9 Chang, L., 7-AFM-1 Chintamani, S., 230-APA-24 Claflin, S., 351-HSABP-6 Conway, M., 436-APA-45 Crispin, C., 297-IS-7 Chang, P., 102-STR-3 Chipalkatty, R., 29-IS-1/ICC-1/DA-1 Clamann, M., 352-IS-9 Coogan, S., 273-ACD-6 Crittenden, T., 69-FD-8 Chang, S., 229-APA-23/FD-27 Chitale, K., 432-APA-41 Clark, D., 90-NDA-1, 379-APA-38 Cook, B., 403-IS-11 Crosby, W., 119-APA-11, 173-APA-16 Chao, H., 136-GNC-15 Chiu, P., 268-WE-6 Clark, H., 444-FD-59 Cook, M., 202-NDA-3 Crossley, W., 354-MDO-7 Chapman, J., 226-AFM-8 Chng, T., 362-PDL-11 Clark, M., 47-SOF-1, 420-UMS-10 Cooney, J., 279-APA-29 Crouse, G., 325-ACD-8 Chappelle, C., 33-MAT-1 Cho, D., 448-GNC-40 Clark, S., 414-SD-12 Cooper, B., 382-ASC-6 Crowe, D., 457-PC-18 Charalampous, G., 305-PC-12 Cho, H., 177-ASC-2 Clarke, J., 346-GNC-31 Cooper, J., 98-SD-4, 259-SD-7, 336-DSC-4, 383-DSC-5, Crowell, A., 67-APA-10 Charbonier, D., 439-FD-54 Cho, K., 255-PC-9/GTE-9, 351-HSABP-6 Clarke, S., 185-GEPC-3 465-TP-12 Crowther, W., 175-APA-18 Chatterjee, T., 421-WE-10 Choe, R., 134-GNC-13 Clarkson, E., 202-NDA-3 Cope, A., 83-IS-2 Cruz, J., 12-APA-3, 175-APA-18

Chaudhry, H., 266-UMS-6 Choi, D., 266-UMS-6 Clavette, P., 262-STR-8 Copp, B., 395-GNC-35 Csank, J., 345-GNC-30/ACD-10 Chaudhry, R., 440-FD-55 Choi, H., 195-ICC-2, 448-GNC-40 Clay, S., 156-STR-4 Coppin, J., 67-APA-10 Cuadrado, D., 193-GTE-7 Chaudhry, S., 328-AFM-11 Choi, J., 11-APA-2, 286-FD-37, 357-NDA-6, 390-FD-52, Cleaver, D., 69-FD-8, 387-FD-49, 391-FD-53 Coquel, F., 126-FD-10 Cuany, J., 312-SEN-2 Chaudhuri, A., 303-NDA-5 432-APA-41 Clemens, N., 19-FD-6, 377-AMT-8 Corbets, J., 31-ISC-2 Cui, J., 26-GTE-1, 151-SATS-1, 389-FD-51 Chaurasia, A., 34-MAT-2 Choi, K., 36-MST-1, 355-MST-11 Clement, T., 353-MAT-9 Corbets, S., 84-ISC-3 Cui, P., 133-GNC-12, 242-GNC-21, 290-GNC-24 Cheatwood, M., 10-AMT-10/SD-15 Choi, S., 7-AFM-1, 35-MDO-1, 250-MDO-5, 272-AA-6, Clements, K., 21-GNC-2 Corke, T., 82-GTE-3, 138-GTE-4, 361-PDL-10, Cui, X., 156-STR-4, 303-NDA-5 Chee, S., 393-GNC-33 286-FD-37, 432-APA-41 Cliff, S., 435-APA-44 362-PDL-11, 399-GTE-14 Cui, Y., 259-SD-7 Cheema, P., 202-NDA-3 Chong, J., 335-ASC-5 Clifford, C., 181-FD-23/PDL-6 Corman, J., 169-ACD-2 Culler, E., 332-APA-34 Chehroudi, B., 457-PC-18 Chopra, I., 30-ISC-1, 31-ISC-2, 311-SD-9, 327-AFM-10, Climent Manez, H., 364-SD-10 Corral, J., 420-UMS-10 Culler, W., 306-PC-13 Chelliah, H., 39-PC-1 383-DSC-5 Clinton, J., 455-MST-15 Correale, G., 257-PDL-7 Culley, D., 300-MST-8 Chelliah, K., 221-AA-5 Chou, A., 15-FD-2, 182-FD-24 Clubb, J., 305-PC-12 Corrigan, A., 239-FD-31, 348-GTE-11, 452-GTE-16 Cummings, M., 352-IS-9 Chen, C., 391-FD-53 Choudhari, M., 15-FD-2, 182-FD-24, 441-FD-56 Cluts, J., 238-FD-30 Corson, D., 107-WE-1 Cummings, R., 117-ACD-1, 183-FD-25, 232-APA-26, Chen, D., 422-WE-11 Choudhury, R., 234-DSC-1, 245-GT-5 Cobb, R., 80-GNC-10, 160-UMS-3, 394-GNC-34/ACD-12 Cosenza, M., 46-SEO-1 328-AFM-11 Chen, F., 39-PC-1, 265-TP-7 Choukroun, D., 446-GNC-38 Cocks, P., 28-HSABP-1 Costa, I., 106-UMS-2 Cunningham, D., 412-PDL-12 Chen, H., 13-APA-4, 72-FD-12, 332-APA-34 Choutapalli, I., 329-AMT-7 Coderre-Chabot, A., 375-AFM-12 Costello, M., 118-AFM-5, 244-GNC-23, Cunningham, K., 188-GNC-18, 301-MST-9, 327-AFM-10 Chen, J., 308-SATS-3, 436-APA-45 Chow, R., 120-APA-12, 268-WE-6, 441-FD-56 Codoni, J., 351-HSABP-6 394-GNC-34/ACD-12 Curran, D., 386-FD-48 Chen, P., 66-APA-9, 233-ASC-3, 250-MDO-5, 383-DSC-5, Chowdhury, A., 210-TES-5 Coen, M., 77-GNC-7 Costes, M., 331-APA-33 Currao, G., 234-DSC-1 414-SD-12 Chowdhury, S., 88-MDO-2 Coetzee, E., 185-GEPC-3 Cotting, M., 60-AFM-3, 134-GNC-13, 355-MST-11 Curtis, J., 135-GNC-14 Chen, Q., 450-GT-9 Christensen, G., 168-ABPSI-4 Cohen, J., 297-IS-7 Cottle, A., 294-GTE-10, 451-GTE-15 Cushing, J., 413-SCS-6 Chen, R., 245-GT-5, 419-TP-10, 464-TP-11 Christensen, K., 240-FD-32 Cohen, K., 196-IS-5, 403-IS-11 Couaillier, V., 126-FD-10 Cutler, A., 62-AMT-2, 141-HSABP-2, 377-AMT-8 Chen, T., 189-GNC-19 Christian, J., 23-GNC-4, 308-SATS-3, 401-SAT-1 Coil, M., 204-PC-8 Coulter, A., 432-APA-41 Cutler, J., 31-ISC-2 Chen, W., 104-TP-3, 290-GNC-24 Christiansen, R., 266-UMS-6, 466-UMS-11 Colaprete, A., 48-SRE-1 Coumar, S., 459-PDL-13 Cutrone, L., 457-PC-18 Chen, X., 259-SD-7, 265-TP-7, 450-GT-9 Christopher, J., 129-FD-17 Coleman, D., 31-ISC-2 Cowlagi, R., 80-GNC-10, 434-APA-43 Cutshall, J., 178-DE-2 Chen, Y., 123-APA-15, 211-TP-6, 317-TP-8, 393-GNC-33 Chterev, I., 306-PC-13 Coleman, T., 238-FD-30, 348-GTE-11 Cox, C., 388-FD-50 Cvijetic, G., 18-FD-5 Cheng, B., 272-AA-6 Chu, P., 48-SRE-1 Colin, O., 137-GT-3 Cox, D., 188-GNC-18, 301-MST-9 Cybyk, B., 123-APA-15 Cheng, C., 434-APA-43 Chu, Q., 20-GNC-1, 54-UMS-1, 76-GNC-6, 135-GNC-14, Colket, M., 39-PC-1 Cox, J., 36-MST-1 Cyr, D., 434-APA-43 Cheng, J., 283-FD-34, 284-FD-35 244-GNC-23, 252-MST-7, 292-GNC-26, 293-GNC-27, Collicott, S., 340-FD-44 Coy, E., 457-PC-18 Czabaj, M., 262-STR-8 Cheng, P., 421-WE-10 302-MST-10, 376-AFM-13, 430-AFM-15 Collier, F., 12-APA-3 Coyle, C., 67-APA-10, 432-APA-41 D’Angelo, J., 122-APA-14 Author/Session Chair Index D’Onofrio, V., 186-GNC-16 de Almeida, S., 102-STR-3 De Santis, D., 175-APA-18 Djeddi, R., 280-APA-30 Dulgar, O., 396-GNC-36 D’Urso, S., 45-SE-1 DeAngelo, M., 80-GNC-10 Deshmukh, R., 97-SD-3 Djojodihardjo, H., 433-APA-42 Dumas, M., 338-FD-42 Dadhich, A., 100-SEO-2 Deaton, J., 200-MDO-4, 299-MDO-6 Desideri, J., 407-MVC-2 Do, H., 131-FD-19, 141-HSABP-2, 248-HSABP-4 Dumitrache, C., 96-PDL-4 Dadian, O., 266-UMS-6 Debertshaeuser, H., 161-WE-2 De Simone, V., 405-MST-12 Dodenhöft, J., 292-GNC-26 Dumont, A., 277-APA-27, 288-FD-39/APA-31 Dahlen, J., 37-MST-2 Debiasi, M., 279-APA-29, 334-APA-36 DeSio, C., 172-AMT-4 Dogariu, A., 9-AMT-1 Duncan, S., 71-FD-11 Dai, H., 44-SD-2 DeBonis, J., 229-APA-23/FD-27, 333-APA-35/FD-41 DesJardin, P., 53-TP-2 Doggett, W., 309-SCS-4, 460-SCS-7 Duncil, L., 338-FD-42 Dai, R., 77-GNC-7 De Breuker, R., 68-ASC-1, 98-SD-4, 102-STR-3, DeSpirito, J., 331-APA-33 Doi, A., 152-SCS-1 Dunker, S., 160-UMS-3 Dai, Y., 452-GTE-16 417-STR-14 Dessouki, M., 275-AFM-9 Doig, G., 339-FD-43, 379-APA-38 Dunn, R., 185-GEPC-3 Daids, O., 23-GNC-4 Decker, K., 181-FD-23/PDL-6 Destarac, D., 288-FD-39/APA-31 Dolan, B., 246-GTE-8, 457-PC-18 Dunn, S., 191-GT-4 Daigle, M., 453-IS-13 de Croon, G., 7-AFM-1, 24-GNC-5, 293-GNC-27, Dettwiller, I., 147-NDA-2 Dolan, J., 196-IS-5 Dunning, P., 200-MDO-4 Daily, J., 92-PC-3 327-AFM-10 Deutsch, M., 168-ABPSI-4 Doman, D., 186-GNC-16, 190-GNC-20, 328-AFM-11, Duplessis, J., 12-APA-3 Daimon, Y., 149-PC-6, 359-PC-14 Dedic, C., 62-AMT-2 Devarajan, B., 125-DE-1 344-GNC-29, 345-GNC-30/ACD-10, 395-GNC-35 Dupuis, M., 189-GNC-19 Dale, G., 59-ABPSI-2/GEPC-2 Deem, E., 237-FD-29 Devathi, H., 357-NDA-6 Domber, J., 446-GNC-38 Duque, E., 11-APA-2, 407-MVC-2 Dalenbring, M., 332-APA-34 Deere, K., 59-ABPSI-2/GEPC-2 Devenport, W., 272-AA-6 Domingo, P., 93-PC-4, 410-PC-16 Duraisamy, K., 333-APA-35/FD-41, 440-FD-55 Dalgarno, R., 156-STR-4, 249-MAT-7 Dees, P., 146-MST-4 Deveraux, M., 178-DE-2 Donbar, J., 340-FD-44, 402-HSABP-7 Durak, U., 300-MST-8 Dalle, D., 173-APA-16 Defoort, S., 202-NDA-3 De Visscher, I., 342-FD-46 Dong, H., 129-FD-17, 179-FD-21, 442-FD-57 Duran, A., 249-MAT-7 Damaren, C., 77-GNC-7 De Gaspari, A., 281-ASC-4 de Visser, C., 7-AFM-1, 20-GNC-1, 135-GNC-14, Dong, Y., 70-FD-9 Durgesh, V., 183-FD-25 Damiani, R., 213-WE-4 De Gelder, N., 343-GNC-28 243-GNC-22, 244-GNC-23, 252-MST-7, 292-GNC-26, Dongmo, J., 83-IS-2 Durston, D., 435-APA-44 Danczyk, S., 40-PC-2 DeGennaro, A., 299-MDO-6 302-MST-10, 327-AFM-10, 346-GNC-31, 376-AFM-13, Donini, A., 411-PC-17 Dustin, J., 198-MAT-5, 249-MAT-7 Danehy, P., 276-AMT-6/PC-11/PDL-8, 377-AMT-8 De Giorgi, M., 42-PDL-2 387-FD-49, 430-AFM-15 Donovan, A., 145-MDO-3 Dutta, P., 312-SEN-2 Daniel, D., 450-GT-9 Deierling, P., 102-STR-3 Devore, M., 78-GNC-8 Doolan, C., 73-FD-13 Dutton, J., 238-FD-30 Daniels, T., 437-DA-2 de Jong, A., 58-AA-2 DeVoria, A., 183-FD-25 Doom, J., 130-FD-18 Duvvuri, S., 240-FD-32 Danilevsky, M., 168-ABPSI-4 de Kat, R., 177-ASC-2 Dextre, R., 412-PDL-12 Dorduncu, M., 368-STR-13 Dwight, R., 31-ISC-2 Dannenhoffer, J., 407-MVC-2 de la Llave Plata, M., 126-FD-10 Dey, S., 122-APA-14, 278-APA-28 DorMohammadi, S., 147-NDA-2, 202-NDA-3, 208-STR-6 Dyer, S., 353-MAT-9

Danowsky, B., 375-AFM-12, 429-AFM-14 Delapierre, M., 258-SCS-3 Dhamankar, N., 58-AA-2 Dorsey, J., 460-SCS-7 Dykes, J., 430-AFM-15 Darakananda, D., 442-FD-57 DeLaurentis, D., 195-ICC-2 Dhanasar, M., 194-HSABP-3, 354-MDO-7 Doty, J., 300-MST-8 Dykes, K., 467-WE-12 Darbandi, M., 318-WE-7, 390-FD-52, 458-PC-19 DeLeon, R., 129-FD-17 Dhanasekaran, J., 205-SATS-2 Doucette, E., 135-GNC-14 Dziedzic, W., 285-FD-36 da Rocha-Schmidt, L., 177-ASC-2 Delimont, J., 294-GTE-10 Dias, J., 430-AFM-15 Doupe, C., 146-MST-4 Earle, G., 465-TP-12 Da Ronch, A., 328-AFM-11, 337-EDU-1, 383-DSC-5, Delnero, J., 107-WE-1 Diasinos, S., 379-APA-38 Dowgwillo, R., 295-HIS-3 Ebacher, J., 26-GTE-1 429-AFM-14 Delorme, Y., 283-FD-34 Diaz, M., 146-MST-4 Dowling, A., 411-PC-17 Ebeida, M., 90-NDA-1 das Gupta, A., 95-PDL-3 Del Papa, S., 317-TP-8 Dickey, E., 6-ABPSI-1/GEPC-1 Downing, J., 399-GTE-14 Ebel, P., 25-GT-1, 81-GT-2 Dasgupta, D., 360-PC-15 De Maesschalck, C., 193-GTE-7 Dickman, C., 169-ACD-2 Downs, R., 441-FD-56 Eberhardt, S., 295-HIS-3 Dasque, N., 194-HSABP-3, 354-MDO-7 Demange, J., 121-APA-13 Dickson, D., 301-MST-9 Doyle, D., 382-ASC-6 Ebert, T., 48-SRE-1 Datashvili, L., 177-ASC-2 Demargne, A., 120-APA-12 Di Donato, P., 403-IS-11 Doyle, K., 290-GNC-24 Echekki, T., 360-PC-15, 411-PC-17 Davidson, D., 39-PC-1, 40-PC-2, 141-HSABP-2 DeMars, K., 23-GNC-4 Diel, D., 346-GNC-31 Drakunov, S., 22-GNC-3 Echter, M., 206-SCS-2 Davidson, L., 267-WE-5 Demasi, L., 50-STR-2 Dierke, J., 398-GTE-13 Drees, L., 37-MST-2 Ecker, T., 9-AMT-1, 348-GTE-11 Davidson, T., 13-APA-4 Demauro, E., 172-AMT-4, 227-AMT-5, 286-FD-37, Diggs, A., 253-NDA-4 Drennan, S., 349-GTE-12 Eckert, Z., 257-PDL-7, 459-PDL-13 Davies, C., 125-DE-1, 289-GEPC-4 443-FD-58 DiGirolamo, E., 274-ACD-7 Dress, D., 99-SE-2 Eckstein, E., 263-STR-9 Davies, R., 289-GEPC-4 Demetriou, M., 151-SATS-1, 205-SATS-2, 344-GNC-29 Dijkers, H., 198-MAT-5 Dreyer, C., 48-SRE-1 Economon, T., 43-SD-1, 194-HSABP-3, 330-APA-32, Davila, C., 208-STR-6 DeMillard, E., 238-FD-30 Dillinger, J., 98-SD-4, 102-STR-3 Dreyer, E., 282-DSC-3 428-ACD-13 Davis, B., 258-SCS-3, 413-SCS-6 Demonteverde, R., 266-UMS-6 Dimino, I., 233-ASC-3, 281-ASC-4 Driscoll, J., 19-FD-6, 194-HSABP-3, 306-PC-13 Edelman, J., 75-FD-20 Davis, G., 460-SCS-7 Dempsey, A., 316-SUR-2 Ding, J., 252-MST-7 Driscoll, R., 28-HSABP-1, 296-HSABP-5, 351-HSABP-6 Edoh, A., 18-FD-5 Davis, P., 384-EDU-2 Dener, A., 299-MDO-6 Ding, K., 180-FD-22 Du, J., 152-SCS-1 Edquist, K., 265-TP-7 Davis, R., 97-SD-3, 168-ABPSI-4 Deng, S., 439-FD-54 Dinzl, D., 75-FD-20 Du, X., 330-APA-32 Edwards, J., 17-FD-4, 39-PC-1, 94-PC-5, 287-FD-38, Davis, S., 52-TES-2/TP-1 Denham, J., 378-APA-37 Dionisopoulos, J., 168-ABPSI-4 Du, Y., 18-FD-5 360-PC-15, 386-FD-48, 411-PC-17 Davis, T., 174-APA-17, 378-APA-37 Denison, M., 435-APA-44 Diop, M., 19-FD-6 Duan, L., 15-FD-2 Edwards, S., 146-MST-4 Davitian, J., 464-TP-11 Denissen, K., 121-APA-13, 175-APA-18 Diosady, L., 180-FD-22, 229-APA-23/FD-27, 284-FD-35, Duan, Z., 338-FD-42 Eerland, W., 297-IS-7 Davuluri, R., 53-TP-2 Dennis, B., 230-APA-24 331-APA-33, 431-AMT-9 Dubois, A., 102-STR-3 Egolf, T., 11-APA-2 Dawes, W., 120-APA-12 Dennis, J., 305-PC-12 DiPalma, M., 281-ASC-4, 310-SD-8 Dubreuil, E., 237-FD-29 Egorov, I., 15-FD-2 Dawson, S., 442-FD-57 de Paula, A., 279-APA-29 Diskin, B., 64-APA-7, 184-FD-26/APA-21 Duda, B., 387-FD-49, 389-FD-51 Egorova, T., 344-GNC-29 Day, J., 45-SE-1 Depperschmidt, D., 40-PC-2 Di Vincenzo, F., 438-DSC-6 Duffield, M., 466-UMS-11 Ehlers, H., 232-APA-26 Day, M., 360-PC-15 de Reus, A., 251-MST-6 DiZinno, N., 70-FD-9 Dufrene, A., 119-APA-11 Ehlert, G., 317-TP-8 Author/Session Chair Index Eiler, J., 45-SE-1 Ervin, G., 12-APA-3, 98-SD-4 Fasanella, N., 33-MAT-1 Fleischman, S., 396-GNC-36 Friedlander, D., 229-APA-23/FD-27 Eisemann, U., 47-SOF-1 Erwin, J., 122-APA-14, 228-APA-22, 288-FD-39/APA-31 Fasano, G., 312-SEN-2 Fleischmann, S., 406-MST-13 Friedman, C., 12-APA-3 Eissfeller, B., 189-GNC-19 Esclape, L., 294-GTE-10 Fasel, H., 74-FD-14, 131-FD-19, 182-FD-24, 442-FD-57 Fleischner, A., 187-GNC-17 Friedmann, P., 234-DSC-1 Ejaz Ur Rehman, Q., 328-AFM-11 Esfahani, A., 181-FD-23/PDL-6 Fatemi, A., 353-MAT-9 Flick, P., 12-APA-3, 98-SD-4 Friedrich, L., 418-STR-15 Ekaterinaris, J., 18-FD-5, 284-FD-35 Esfahani, M., 404-MDO-8 Fathima, K., 157-STR-5 Flores Kriegsfeld, J., 343-GNC-28 Fries, D., 93-PC-4, 306-PC-13 Eken, S., 259-SD-7 Eshcol, R., 65-APA-8 Fatta, O., 103-TES-3 Floryan, D., 442-FD-57 Frink, N., 184-FD-26/APA-21, 226-AFM-8, 2 Ekici, K., 175-APA-18, 280-APA-30 Eskenazi, M., 413-SCS-6 Faulk, D., 312-SEN-2, 365-SEN-3 Fluck, M., 303-NDA-5 32-APA-26, 301-MST-9 Ekinci, S., 27-GTE-2 Etele, J., 293-GNC-27 Favaregh, A., 173-APA-16 Fogel, G., 247-HIS-2 Friss, A., 362-PDL-11 Eksuzian, D., 378-APA-37 Etherington, T., 437-DA-2 Fedorov, A., 15-FD-2 Font, C., 260-SEN-1 Frohnapfel, D., 116-ABPSI-3 Eldred, M., 147-NDA-2 Etienne, S., 340-FD-44 Fei, Q., 461-SD-14 Fontaine, R., 42-PDL-2, 95-PDL-3 Frost, S., 83-IS-2, 132-GNC-11, 243-GNC-22, 371-WE-9 Eldredge, J., 16-FD-3, 442-FD-57 Eun, W., 233-ASC-3 Felder, J., 224-ACD-5 Fonte, F., 311-SD-9 Fu, H., 419-TP-10 El Haddad, N., 170-ACD-3 Eun, Y., 355-MST-11 Fell, J., 223-ACD-4 Footdale, J., 152-SCS-1 Fu, S., 160-UMS-3, 182-FD-24, 237-FD-29, Elhalwagy, Y., 37-MST-2 Eussen, B., 300-MST-8 Fenercioglu, I., 442-FD-57 Forbes, E., 30-ISC-1 341-FD-45, 389-FD-51 Elham, A., 35-MDO-1, 354-MDO-7, 417-STR-14 Evans, E., 437-DA-2 Feng, L., 106-UMS-2, 181-FD-23/PDL-6 Forbes, J., 393-GNC-33 Fugger, C., 255-PC-9/GTE-9 ElHammal, T., 52-TES-2/TP-1, 103-TES-3 Evans, S., 126-FD-10 Ferguson, D., 192-GTE-6 Forgione, J., 48-SRE-1 Fujii, K., 72-FD-12, 181-FD-23/PDL-6 ElHariri, G., 289-GEPC-4 Ewert, R., 81-GT-2, 398-GTE-13 Ferguson, F., 194-HSABP-3, 354-MDO-7 Forliti, D., 40-PC-2 Fujita, K., 8-AFM-2, 159-TP-5, 369-TP-9 Eliasson, P., 432-APA-41 Exarchos, I., 447-GNC-39 Ferlisi, C., 337-EDU-1 Forrest, L., 247-HIS-2 Fukuda, K., 131-FD-19, 265-TP-7 Eljack, E., 444-FD-59 Eymann, T., 228-APA-22, 236-FD-28 Fern, L., 212-UMS-4 Forschner, P., 207-SE-3 Fukui, H., 53-TP-2 Eller, D., 438-DSC-6 Fabela, R., 327-AFM-10 Fernandes, C., 193-GTE-7 Forslund, A., 253-NDA-4 Fukumoto, H., 72-FD-12 Ellerbroek, J., 22-GNC-3, 212-UMS-4, 346-GNC-31 Fabiano, E., 277-APA-27, 404-MDO-8 Fernandes, R., 367-STR-12 Forster, E., 147-NDA-2 Fukushima, S., 36-MST-1 Ellertson, A., 297-IS-7 Fagan, A., 391-FD-53 Fernandez, J., 413-SCS-6 Forsythe, J., 228-APA-22, 278-APA-28, 407-MVC-2 Fulcher, C., 461-SD-14 Ellingson, G., 243-GNC-22 Fagley, C., 69-FD-8, 332-APA-34 Fernandez, P., 283-FD-34 Fossati, M., 13-APA-4, 17-FD-4, 174-APA-17, Fulkerson, T., 134-GNC-13 Elliott, D., 392-GNC-32 Fahrenthold, E., 264-SUR-1, 316-SUR-2 Fernandez-Godino, M., 253-NDA-4 285-FD-36, 338-FD-42 Fuller, C., 141-HSABP-2, 272-AA-6 Elliott, G., 42-PDL-2, 95-PDL-3, 150-PDL-5/PC-7/AMT-3, Fala, N., 453-IS-13 Feron, E., 346-GNC-31 Fossen, T., 106-UMS-2, 446-GNC-38 Funaki, I., 28-HSABP-1, 296-HSABP-5

238-FD-30 Faleiro, L., 207-SE-3 Ferrar, A., 116-ABPSI-3 Foster, J., 22-GNC-3, 188-GNC-18, 301-MST-9 Funke, S., 25-GT-1 Elliott, J., 330-APA-32 Faleiros, D., 183-FD-25 Fertig, R., 34-MAT-2, 198-MAT-5, 209-STR-7, 250-MDO-5 Fotia, M., 296-HSABP-5 Furuya, H., 460-SCS-7 Ellis, K., 312-SEN-2 Falempin, F., 459-PDL-13 Fesenko, S., 95-PDL-3 Fowler, A., 465-TP-12 Fusini, L., 446-GNC-38 Ellison, G., 92-PC-3 Falken, A., 68-ASC-1 Fiala, T., 458-PC-19 Fowler, L., 118-AFM-5 Gabet Hoffmeister, K., 62-AMT-2, 227-AMT-5 Elmer, K., 6-ABPSI-1/GEPC-1, 59-ABPSI-2/GEPC-2 Falkiewicz, N., 97-SD-3, 282-DSC-3 Fichter, W., 393-GNC-33, 395-GNC-35, 454-MST-14 France, J., 141-HSABP-2 Gade, S., 291-GNC-25 Elmiligui, A., 37-MST-2, 251-MST-6, 435-APA-44 Fallenius, B., 441-FD-56 Fidkowski, K., 180-FD-22, 184-FD-26/APA-21, Francioso, L., 42-PDL-2 Gaertner, E., 267-WE-5 Elnashar, A., 300-MST-8 Falugi, M., 463-STR-17 284-FD-35, 288-FD-39/APA-31 Francis, W., 413-SCS-6 Gagne, K., 205-SATS-2 Elphic, R., 48-SRE-1 Famularo, D., 394-GNC-34/ACD-12 Field, J., 301-MST-9 Francois, D., 389-FD-51 Gaitonde, A., 336-DSC-4 El-Zomor, H., 289-GEPC-4 Fan, H., 356-MVC-1 Fields, T., 376-AFM-13 Francois, G., 98-SD-4 Gaitonde, D., 5-AA-1, 19-FD-6, 71-FD-11, 131-FD-19, Emeneth, M., 45-SE-1 Fan, W., 20-GNC-1 Fiévet, R., 222-ABPSI-5 Frank, C., 88-MDO-2, 178-DE-2, 273-ACD-6, 354-MDO-7 167-AA-4, 234-DSC-1, 237-FD-29, 238-FD-30, Emerson, B., 306-PC-13 Fancello, A., 411-PC-17 Fievisohn, R., 296-HSABP-5 Frank, G., 317-TP-8 287-FD-38, 386-FD-48, 402-HSABP-7, 440-FD-55 Emery, J., 48-SRE-1 Fang, E., 156-STR-4, 315-STR-11 Fifarek, A., 47-SOF-1 Franke, K., 54-UMS-1 Galbraith, M., 439-FD-54 Emmi, Y., 130-FD-18 Fang, H., 152-SCS-1 Figueroa, J., 453-IS-13 Frankel, S., 283-FD-34 Gallagher, B., 152-SCS-1 Endo, N., 169-ACD-2 Fang, J., 13-APA-4 Filippone, E., 89-MST-3 Franqui, A., 46-SEO-1 Gallis, M., 104-TP-3 Endo, T., 28-HSABP-1, 296-HSABP-5 Fang, X., 116-ABPSI-3 Findlay, D., 378-APA-37 Fransson, J., 441-FD-56 Gallo, E., 141-HSABP-2, 377-AMT-8 Endrikat, S., 387-FD-49 Fares, E., 387-FD-49, 389-FD-51, 432-APA-41 Fine, N., 279-APA-29 Franze, M., 171-AFM-6 Galvani, P., 37-MST-2 Engebretson, K., 365-SEN-3 Farhat, C., 102-STR-3, 175-APA-18, 284-FD-35, Finn, T., 237-FD-29 Fravolini, M., 292-GNC-26 Galyen, N., 9-AMT-1 Engel, J., 305-PC-12 386-FD-48 Fiore, G., 176-APA-20 Frederickson, K., 93-PC-4, 377-AMT-8, 459-PDL-13 Gamba, M., 19-FD-6, 248-HSABP-4, 339-FD-43, Engelmann, M., 274-ACD-7 Faria, C., 335-ASC-5 Firsov, A., 361-PDL-10 Freer, J., 327-AFM-10 351-HSABP-6 Engelsen, F., 354-MDO-7 Farias, P., 172-AMT-4, 227-AMT-5 Fisackerly, R., 48-SRE-1 French, J., 22-GNC-3 Gamble, L., 335-ASC-5 Engelstad, S., 156-STR-4, 262-STR-8 Farinella, J., 466-UMS-11 Fiser, M., 275-AFM-9 French, M., 45-SE-1 Gamboa, P., 68-ASC-1 Eppink, J., 185-GEPC-3, 441-FD-56 Farnell, C., 412-PDL-12 Fish, J., 156-STR-4 Frenklach, M., 39-PC-1 Gamil A. A., A., 52-TES-2/TP-1 Epshteyn, A., 149-PC-6 Farnsworth, J., 69-FD-8, 232-APA-26, 280-APA-30, Fisher, B., 52-TES-2/TP-1, 149-PC-6 Fresconi, F., 171-AFM-6, 432-APA-41 Gan, J., 120-APA-12 Epstein, B., 330-APA-32 332-APA-34 Fisher, T., 136-GNC-15, 229-APA-23/FD-27 Freund, J., 42-PDL-2, 95-PDL-3, 458-PC-19 Gan, T., 13-APA-4 Erdmann, T., 94-PC-5 Farokhi, M., 340-FD-44 Fladeland, M., 196-IS-5 Frew, E., 54-UMS-1, 297-IS-7 Erickson, L., 335-ASC-5 Farrar, C., 153-SD-5 Flamm, J., 6-ABPSI-1/GEPC-1, 59-ABPSI-2/GEPC-2 Frey, T., 365-SEN-3 Ganapathisubramani, B., 10-AMT-10/SD-15, Errico, A., 89-MST-3 Farrokh, B., 314-STR-10 Flansburg, B., 49-STR-1, 208-STR-6 Frias, D., 138-GTE-4, 399-GTE-14 177-ASC-2, 240-FD-32, 442-FD-57 Ertem, S., 370-WE-8 Farsadi, T., 213-WE-4, 310-SD-8, 415-SD-13 Flansburg, L., 262-STR-8 Fricke, T., 225-AFM-7, 394-GNC-34/ACD-12 Gandhi, F., 281-ASC-4, 310-SD-8, 335-ASC-5 Author/Session Chair Index Gandhi, M., 80-GNC-10 George, B., 286-FD-37 Glezer, A., 16-FD-3, 69-FD-8 Gosse, R., 15-FD-2, 104-TP-3, 440-FD-55 Gross, K., 37-MST-2, 47-SOF-1 Gandhi, N., 78-GNC-8, 188-GNC-18 George, I., 381-APA-40 Glumac, N., 42-PDL-2, 95-PDL-3 Gottiparthi, K., 411-PC-17 Gross, M., 118-AFM-5 Ganesh Kumar, V., 28-HSABP-1, 296-HSABP-5, George, T., 87-MAT-3, 144-MAT-4, 157-STR-5, Gnanaskandan, A., 149-PC-6 Göttlicher, C., 328-AFM-11 Grossman, I., 74-FD-14 351-HSABP-6 198-MAT-5, 202-NDA-3 Gnoffo, P., 440-FD-55 Gourdain, N., 438-DSC-6 Grout, R., 459-PDL-13 Gangadharan, S., 340-FD-44 Georgiadis, N., 398-GTE-13 Gnoth, M., 328-AFM-11 Govers, Y., 221-AA-5 Grover, M., 104-TP-3 Gao, A., 242-GNC-21 Gerboni, C., 454-MST-14 Godar, T., 317-TP-8 Govindarajan, B., 228-APA-22 Grubb, A., 65-APA-8 Gao, C., 42-PDL-2, 181-FD-23/PDL-6 Gerhold, C., 272-AA-6 Godines, C., 202-NDA-3, 208-STR-6 Goya, H., 431-AMT-9 Grubb, M., 308-SATS-3 Gao, H., 237-FD-29, 305-PC-12 Gerlach, A., 186-GNC-16, 328-AFM-11, 344-GNC-29 Goff, G., 393-GNC-33 Goyal, A., 422-WE-11 Gruber, M., 141-HSABP-2 Gao, J., 58-AA-2 Gerlinger, P., 457-PC-18 Gogeneni, S., 5-AA-1 Goyal, V., 157-STR-5, 209-STR-7, 315-STR-11 Gruenwald, B., 132-GNC-11, 292-GNC-26 Gao, S., 338-FD-42 German, B., 17-FD-4, 88-MDO-2, 169-ACD-2 Gogineni, S., 115-AA-3, 238-FD-30, 286-FD-37, Goyne, C., 141-HSABP-2, 227-AMT-5 Gruntman, M., 465-TP-12 Gao, X., 129-FD-17, 130-FD-18, 204-PC-8, Gern, F., 49-STR-1 307-PDL-9/FD-40, 348-GTE-11, 362-PDL-11, Graf, P., 467-WE-12 Gryte, K., 106-UMS-2 385-FD-47, 386-FD-48 Gertsch, L., 48-SRE-1, 155-SRE-2 398-GTE-13 Grandhi, R., 90-NDA-1 Gu, Y., 134-GNC-13, 136-GNC-15, 160-UMS-3, Garafolo, N., 153-SD-5 Geubelle, P., 249-MAT-7 Gogulapati, A., 234-DSC-1 Granlund, K., 14-FD-1/APA-5, 63-APA-6/FD-7, 188-GNC-18, 308-SATS-3 Garai, A., 229-APA-23/FD-27, 284-FD-35 Gezer, R., 396-GNC-36 Gohardani, A., 185-GEPC-3 179-FD-21, 287-FD-38 Guan, Q., 92-PC-3 Garbo, A., 88-MDO-2 Ghafourizadeh, M., 390-FD-52 Gokulakrishnan, P., 141-HSABP-2 Grannan, N., 27-GTE-2 Guangjia, L., 106-UMS-2 Garcia, C., 209-STR-7 Gharibi, K., 49-STR-1 Golbabaei-Asl, M., 17-FD-4 Grant, J., 272-AA-6 Guarino, P., 434-APA-43 Garcia, D., 201-MST-5 Ghate, A., 421-WE-10 Gold, C., 82-GTE-3 Grant, M., 8-AFM-2, 61-AFM-4 Guarnaccio, C., 141-HSABP-2 Garcia, E., 183-FD-25 Ghiasi, Z., 131-FD-19, 411-PC-17, 443-FD-58 Goldberg, B., 257-PDL-7 Grant, P., 226-AFM-8, 405-MST-12 Gudmundsson, S., 190-GNC-20 Garcia, J., 59-ABPSI-2/GEPC-2 Ghoniem, A., 256-PC-10 Gollnick, V., 174-APA-17 Grasser, T., 62-AMT-2, 227-AMT-5 Guensch, C., 343-GNC-28 Garcia Sainz, M., 107-WE-1 Ghorawat, P., 394-GNC-34/ACD-12 Golubev, V., 15-FD-2, 167-AA-4, 287-FD-38 Grauer, J., 78-GNC-8, 430-AFM-15 Guethe, F., 41-PDL-1 Gardarein, P., 11-APA-2 Ghoreishi, S., 303-NDA-5 Goman, M., 450-GT-9 Graves, W., 316-SUR-2 Guha, T., 69-FD-8 Gardea, F., 298-MAT-8 Ghoreyshi, M., 232-APA-26, 328-AFM-11 Gombolay, M., 29-IS-1/ICC-1/DA-1, 352-IS-9 Gravseth, I., 77-GNC-7, 187-GNC-17 Guidos, B., 171-AFM-6 Gårdhagen, R., 37-MST-2 Ghosh, R., 289-GEPC-4 Gomez, E., 201-MST-5 Gray, J., 35-MDO-1, 145-MDO-3, 299-MDO-6, Guildenbecher, D., 62-AMT-2, 172-AMT-4, 227-AMT-5 Gardner, A., 231-APA-25 Ghosh, S., 385-FD-47 Gomez, R., 173-APA-16 420-UMS-10 Guillaume, B., 83-IS-2, 261-SOF-5/UMS-5/IS-6,

Gardner, S., 440-FD-55 Giannelis, N., 200-MDO-4, 202-NDA-3, 433-APA-42 Gomez Martinez, H., 189-GNC-19 Gray, W., 60-AFM-3, 225-AFM-7 313-SOF-6/UMS-7/IS-8, 366-SOF-7/UMS-8/IS-10 Garg, K., 189-GNC-19 Giannuzzi, P., 339-FD-43 Gomit, G., 240-FD-32 Greatwood, C., 327-AFM-10 Guimaraes Bucalo, T., 116-ABPSI-3 Gargiulo, F., 89-MST-3 Giarra, M., 257-PDL-7 Gonçalves, E., 337-EDU-1 Grech, N., 168-ABPSI-4 Gulmammadov, F., 302-MST-10 Garmann, D., 70-FD-9, 238-FD-30 Gibbens, P., 135-GNC-14 Gong, Z., 16-FD-3, 450-GT-9 Green, B., 228-APA-22, 378-APA-37 Gunabalan, G., 289-GEPC-4 Garmory, A., 349-GTE-12 Gibbs, J., 224-ACD-5, 289-GEPC-4 Gonzalez, A., 213-WE-4 Green, L., 202-NDA-3, 253-NDA-4 Gunasekaran, M., 380-APA-39 Garnich, M., 250-MDO-5 Gielda, T., 384-EDU-2 Gonzalez, D., 167-AA-4, 237-FD-29 Green, M., 14-FD-1/APA-5, 179-FD-21, 407-MVC-2, Gunasekaran, S., 230-APA-24 Garnier, F., 73-FD-13 Giese, A., 348-GTE-11 Gonzalez-Linero, L., 170-ACD-3 444-FD-59 Gundersen, M., 150-PDL-5/PC-7/AMT-3 Garry, K., 231-APA-25 Giesy, D., 90-NDA-1 Good, N., 406-MST-13 Greenberg, J., 256-PC-10 Gunes, K., 212-UMS-4 Garza, J., 303-NDA-5 Gilbert, M., 171-AFM-6 Goodell, B., 199-MAT-6 Greenblatt, D., 287-FD-38 Guntur, S., 213-WE-4 Gasch, M., 298-MAT-8 Gilbert, N., 451-GTE-15 Goodenow, D., 160-UMS-3 Greene, S., 298-MAT-8 Guo, B., 378-APA-37 Gates, A., 125-DE-1 Gill, J., 242-GNC-21 Goodliff, S., 137-GT-3 Greenwell, D., 12-APA-3, 280-APA-30 Guo, C., 40-PC-2 Gatian, K., 117-ACD-1 Gillaugh, D., 87-MAT-3 Goodstein, M., 160-UMS-3 Gregory, J., 60-AFM-3, 431-AMT-9 Guo, H., 17-FD-4 Gatlin, G., 231-APA-25, 379-APA-38 Gillebaart, T., 356-MVC-1 Gopal, V., 248-HSABP-4 Greschik, G., 258-SCS-3, 413-SCS-6 Guo, T., 226-AFM-8, 301-MST-9 Gatsonis, N., 151-SATS-1, 205-SATS-2, 344-GNC-29 Gingras, D., 455-MST-15 Gopalakrishnan, P., 13-APA-4 Grewal, A., 259-SD-7 Guo, Y., 162-WE-3, 272-AA-6 Gauger, N., 330-APA-32 Ginn, S., 185-GEPC-3 Gopalarathnam, A., 226-AFM-8, 287-FD-38 Grier, B., 282-DSC-3 Guoning, C., 407-MVC-2 Gaunaa, M., 370-WE-8 Girardi, R., 430-AFM-15 Goparaju, K., 238-FD-30 Griffin, E., 414-SD-12 Gupta, A., 103-TES-3, 158-TES-4, 160-UMS-3, Gavrilovski, A., 196-IS-5, 453-IS-13 Giusti, A., 359-PC-14, 411-PC-17 Gorbachova, Y., 193-GTE-7 Griffin, K., 336-DSC-4 245-GT-5, 246-GTE-8, 375-AFM-12 Gaydos, T., 392-GNC-32 Glaab, L., 212-UMS-4 Gord, J., 276-AMT-6/PC-11/PDL-8 Griffith, D., 268-WE-6, 422-WE-11 Gupta, D., 200-MDO-4 Gayretli, A., 460-SCS-7 Glas, M., 274-ACD-7 Gordeuk, J., 21-GNC-2 Grigorie, L., 233-ASC-3 Gupta, M., 39-PC-1 Ge, D., 242-GNC-21 Glasby, R., 122-APA-14, 228-APA-22, 288-FD-39/APA-31 Gordeyev, S., 71-FD-11, 240-FD-32, 286-FD-37, Grimm, F., 398-GTE-13 Gupta, R., 69-FD-8 Gee, K., 398-GTE-13, 399-GTE-14, 452-GTE-16 Glass, D., 105-TP-4, 202-NDA-3 307-PDL-9/FD-40, 339-FD-43 Grinstead, J., 211-TP-6 Gurczak, M., 224-ACD-5 Geerts, J., 248-HSABP-4 Glauser, M., 5-AA-1, 115-AA-3, 238-FD-30, Gordon, K., 82-GTE-3 Grinstead, K., 168-ABPSI-4 Gurney, K., 83-IS-2 Geeslin, A., 263-STR-9 348-GTE-11, 398-GTE-13 Gore, J., 246-GTE-8, 294-GTE-10, 305-PC-12, Groen, E., 22-GNC-3 Gürses, E., 68-ASC-1 Gehri, A., 439-FD-54 Glaz, B., 97-SD-3, 310-SD-8 451-GTE-15 Groeneveld, H., 34-MAT-2 Gursul, I., 69-FD-8, 342-FD-46, 387-FD-49, 391-FD-53 Geigle, K., 92-PC-3, 451-GTE-15 Glaze, D., 256-PC-10 Gorospe, G., 243-GNC-22 Groff, L., 22-GNC-3 Gururaja, S., 157-STR-5 Geikie, M., 193-GTE-7 Glegg, S., 272-AA-6 Gorton, S., 65-APA-8 Gros, M., 395-GNC-35, 447-GNC-39 Guruswamy, G., 61-AFM-4 Geisler, R., 25-GT-1 Gleize, V., 288-FD-39/APA-31, 439-FD-54 Goss, A., 264-SUR-1 Gross, A., 70-FD-9, 74-FD-14, 442-FD-57 Gurvich, M., 262-STR-8 Geng, W., 451-GTE-15 Glen, C., 318-WE-7 Goss, L., 451-GTE-15 Gross, J., 94-PC-5, 308-SATS-3, 395-GNC-35 Gustafson, P., 263-STR-9 Author/Session Chair Index Gutkin, G., 84-ISC-3 Hanson, R., 39-PC-1, 40-PC-2, 141-HSABP-2 He, Z., 451-GTE-15 Hill, C., 124-CMS-1/CPS-1 Hoos, K., 156-STR-4 Gutmark, E., 28-HSABP-1, 41-PDL-1, 115-AA-3, Hao, X., 222-ABPSI-5 Hearn, T., 145-MDO-3 Hill, J., 144-MAT-4 Hoppmann, D., 389-FD-51 246-GTE-8, 296-HSABP-5, 351-HSABP-6, Hara, S., 242-GNC-21 Heath, C., 294-GTE-10 Hill, M., 65-APA-8, 301-MST-9 Horak, D., 225-AFM-7 398-GTE-13, 457-PC-18 Harada, M., 129-FD-17, 190-GNC-20, 376-AFM-13 Heathcote, D., 69-FD-8 Hilton, H., 45-SE-1, 102-STR-3 Horiuchi, T., 53-TP-2 Guyer, S., 101-SOF-3 Harcaut, J., 406-MST-13 Heaton, A., 195-ICC-2 Himeno, T., 103-TES-3 Horn, J., 80-GNC-10, 454-MST-14 Guynn, M., 224-ACD-5 Hardalupas, Y., 305-PC-12 Heberling, B., 452-GTE-16 Himmler, A., 146-MST-4, 300-MST-8 Horne, W., 6-ABPSI-1/GEPC-1 Guyton, R., 329-AMT-7, 397-GT-8 Hardaway, L., 157-STR-5 Hebert, C., 43-SD-1 Hinchliffe, B., 64-APA-7, 121-APA-13 Hornung, M., 89-MST-3, 168-ABPSI-4, 274-ACD-7 Guzik, S., 129-FD-17, 385-FD-47, 386-FD-48 Hardin, L., 59-ABPSI-2/GEPC-2 Hedengren, J., 54-UMS-1 Hind, M., 213-WE-4 Hortensius, R., 238-FD-30 Habashi, W., 17-FD-4, 285-FD-36, 338-FD-42 Hargather, M., 339-FD-43 Hedrick, J., 352-IS-9 Hine, D., 228-APA-22 Hosangadi, P., 287-FD-38 Hablani, H., 449-GNC-41 Hariharan, N., 11-APA-2, 65-APA-8, 122-APA-14, Heffron, A., 69-FD-8 Hines, D., 185-GEPC-3 Hosder, S., 159-TP-5 Hackemann, S., 87-MAT-3 228-APA-22, 278-APA-28, 378-APA-37 Heineck, J., 123-APA-15 Hines, G., 23-GNC-4 Hoseini, H., 43-SD-1 Hafsteinsson, H., 115-AA-3 Harker, B., 398-GTE-13, 452-GTE-16 Heintze, O., 68-ASC-1 Hinks, J., 133-GNC-12 Hosen, J., 446-GNC-38 Haftka, R., 202-NDA-3, 253-NDA-4, 455-MST-15 Harmsen, A., 420-UMS-10 Heinz, S., 341-FD-45, 389-FD-51 Hipp, K., 387-FD-49 Hoshino, H., 152-SCS-1 Haga, T., 283-FD-34 Harris, R., 115-AA-3, 167-AA-4, 236-FD-28, 356-MVC-1 Heise, C., 76-GNC-6 Hirabayashi, H., 36-MST-1 Hoskin, A., 309-SCS-4 Hagenmaier, M., 402-HSABP-7 Harrison, S., 437-DA-2 Heister, S., 192-GTE-6, 255-PC-9/GTE-9 Hirokawa, R., 344-GNC-29 Hosking, N., 44-SD-2 Hagerott, S., 136-GNC-15 Harrivel, A., 312-SEN-2 Helgesen, H., 446-GNC-38 Hirsch, B., 460-SCS-7 Hosono, K., 28-HSABP-1 Hahn, G., 49-STR-1 Hartfield, R., 26-GTE-1, 37-MST-2, 141-HSABP-2, Hellmundt, F., 292-GNC-26 Hitch, B., 305-PC-12, 410-PC-16 Hotchkiss, J., 178-DE-2 Hahn, M., 68-ASC-1 171-AFM-6 Helm, C., 74-FD-14 Hitchen, J., 434-APA-43 Houben, M., 22-GNC-3 Haider, S., 193-GTE-7 Hartl, D., 335-ASC-5 Hemati, M., 14-FD-1/APA-5, 237-FD-29, 442-FD-57 Hitt, D., 205-SATS-2 Houdou, B., 48-SRE-1 Haimes, R., 407-MVC-2 Hartman, D., 188-GNC-18 Hemminger, J., 453-IS-13 Ho, H., 24-GNC-5 Hough, S., 21-GNC-2 Hajian, R., 183-FD-25 Hartmann, P., 447-GNC-39 Hemsch, M., 173-APA-16 Hoagg, J., 126-FD-10 Houlden, H., 173-APA-16 Hajj, M., 66-APA-9, 190-GNC-20, 259-SD-7 Hartsfield, C., 412-PDL-12 Henderson, B., 348-GTE-11 Hoarau, Y., 439-FD-54 Houpt, A., 459-PDL-13 Hakata, S., 309-SCS-4 Hartwig, J., 464-TP-11 Hendricks, E., 27-GTE-2, 145-MDO-3 Hoburg, W., 428-ACD-13 Housman, J., 176-APA-20 Halbig, M., 263-STR-9 Harvazinski, M., 410-PC-16, 411-PC-17 Hendricks, G., 59-ABPSI-2/GEPC-2 Hockemeyer, M., 249-MAT-7 Houzeaux, G., 404-MDO-8

Hale, L., 312-SEN-2 Harwood, C., 247-HIS-2 Henfling, J., 10-AMT-10/SD-15, 172-AMT-4, 241-FD-33, Hodge, S., 454-MST-14 Hovakimyan, N., 78-GNC-8, 134-GNC-13, 291-GNC-25 Halila, G., 120-APA-12 Hasbestan, J., 232-APA-26 286-FD-37, 443-FD-58 Hodges, D., 43-SD-1 Hovell, K., 135-GNC-14 Hall, A., 54-UMS-1 Hasegawa, S., 222-ABPSI-5 Heniff, J., 48-SRE-1 Hodges, R., 151-SATS-1 How, J., 291-GNC-25, 297-IS-7, 393-GNC-33 Hall, C., 12-APA-3, 60-AFM-3, 178-DE-2, 256-PC-10 Haser, S., 430-AFM-15 Hening, S., 83-IS-2 Hoeijmakers, H., 161-WE-2, 174-APA-17, 183-FD-25 Howard, M., 317-TP-8 Hall, D., 170-ACD-3 Hash, D., 53-TP-2 Henrickson, J., 394-GNC-34/ACD-12 Hoekstra, J., 212-UMS-4, 346-GNC-31 Howard, R., 82-GTE-3 Hall, R., 21-GNC-2, 77-GNC-7 Hashemi, A., 52-TES-2/TP-1 Henry, D., 247-HIS-2 Hoffler, K., 275-AFM-9 Howcroft, C., 383-DSC-5 Haller, W., 224-ACD-5 Hashimoto, A., 120-APA-12, 280-APA-30, Henry, E., 153-SD-5 Hoffman, J., 47-SOF-1 Hoyt, R., 413-SCS-6 Hallissy, B., 228-APA-22 288-FD-39/APA-31, 380-APA-39 Henson, M., 418-STR-15 Hofmann, D., 152-SCS-1 Hrishikeshavan, V., 327-AFM-10, 414-SD-12 Hamamoto, S., 380-APA-39 Hassan, A., 20-GNC-1 Heo, Y., 298-MAT-8 Hogstrom, K., 460-SCS-7 Hromisin, S., 5-AA-1, 115-AA-3 Hamed, A., 399-GTE-14, 452-GTE-16 Hassan, E., 239-FD-31, 390-FD-52, 402-HSABP-7 Herber, D., 35-MDO-1 Hoke, C., 442-FD-57 Hu, H., 16-FD-3, 95-PDL-3, 105-TP-4, 240-FD-32, Hamlington, P., 467-WE-12 Hassan, H., 402-HSABP-7 Hereth, E., 82-GTE-3 Hoke, J., 27-GTE-2, 28-HSABP-1, 93-PC-4, 168-ABPSI-4, 362-PDL-11, 370-WE-8, 381-APA-40, 419-TP-10, Han, C., 411-PC-17 Hassanalian, M., 374-ACD-11 Hereth, L., 161-WE-2 255-PC-9/GTE-9, 296-HSABP-5, 351-HSABP-6 422-WE-11 Han, J., 7-AFM-1, 310-SD-8 Hatanaka, K., 377-AMT-8 Herges, T., 318-WE-7 Holden, J., 452-GTE-16 Hu, R., 237-FD-29 Han, Y., 272-AA-6 Hathaway, W., 171-AFM-6 Hernandez, M., 52-TES-2/TP-1, 210-TES-5 Holden, M., 119-APA-11 Hu, Y., 287-FD-38, 368-STR-13 Han, Z., 175-APA-18, 330-APA-32, 436-APA-45 Hatori, R., 100-SEO-2 Herrera, C., 98-SD-4 Holladay, J., 346-GNC-31 Hu, Z., 58-AA-2, 90-NDA-1, 357-NDA-6 Hanak, C., 23-GNC-4 Hattery, R., 382-ASC-6 Herron, A., 119-APA-11 Holley, A., 28-HSABP-1 Huang, C., 355-MST-11, 405-MST-12, 411-PC-17 Hanhan, I., 298-MAT-8 Hauris, F., 177-ASC-2 Hess, C., 172-AMT-4 Hölling, A., 318-WE-7 Huang, D., 234-DSC-1 Hanifi, A., 182-FD-24 Hauser, D., 155-SRE-2 Hess, J., 393-GNC-33 Hölling, M., 318-WE-7 Huang, G., 440-FD-55 Hanks, E., 316-SUR-2 Haviland, S., 125-DE-1, 275-AFM-9 Hewson, J., 62-AMT-2 Hollkamp, J., 364-SD-10 Huang, H., 101-SOF-3, 357-NDA-6, 368-STR-13 Hanley, D., 24-GNC-5 Hay, A., 285-FD-36, 340-FD-44, 404-MDO-8 Heyne, J., 39-PC-1 Holt, J., 231-APA-25 Huang, J., 405-MST-12 Hanlon, N., 196-IS-5 Hayashi, K., 288-FD-39/APA-31 Hicken, J., 283-FD-34, 299-MDO-6, 330-APA-32 Holycross, C., 87-MAT-3, 144-MAT-4, 157-STR-5, Huang, L., 183-FD-25, 380-APA-39 Hanquist, K., 105-TP-4 Hayden, J., 167-AA-4 Hicks, N., 289-GEPC-4 198-MAT-5, 202-NDA-3 Huang, W., 39-PC-1 Hansen, K., 318-WE-7 Hayes, D., 185-GEPC-3 Hicok, D., 343-GNC-28 Holzapfel, F., 37-MST-2, 76-GNC-6, 132-GNC-11, Huang, X., 39-PC-1 Hansen, L., 30-ISC-1, 85-ISC-4 Hayman, G., 213-WE-4 Hield, P., 82-GTE-3, 452-GTE-16 225-AFM-7, 292-GNC-26, 328-AFM-11, Huang, Y., 116-ABPSI-3, 302-MST-10, 444-FD-59 Hansen, M., 213-WE-4, 371-WE-9 Haynes, J., 359-PC-14 Higgins, S., 97-SD-3 394-GNC-34/ACD-12 Huba, Z., 149-PC-6 Hansman, R., 325-ACD-8, 374-ACD-11 He, C., 405-MST-12 Hilbert, B., 356-MVC-1 Holzwarth, R., 315-STR-11 Hubbard, E., 245-GT-5 Hanson, C., 429-AFM-14 He, J., 346-GNC-31 Hilgemann, E., 31-ISC-2 Hooker, J., 137-GT-3 Hubner, J., 179-FD-21 Hanson, D., 138-GTE-4, 399-GTE-14 He, S., 449-GNC-41 Hill, A., 12-APA-3 Hoon, K., 190-GNC-20 Hudgins, R., 137-GT-3 Author/Session Chair Index Huelskamp, B., 94-PC-5 Isaksson, O., 253-NDA-4 Jayakody, N., 382-ASC-6 Johnson, R., 239-FD-31, 348-GTE-11 Kajfez, R., 384-EDU-2 Huete, C., 93-PC-4 Ishida, T., 58-AA-2, 280-APA-30, 288-FD-39/APA-31 Jayaraman, B., 107-WE-1, 122-APA-14 Johnson, S., 45-SE-1, 275-AFM-9 Kalbacher de Marquez, K., 155-SRE-2 Huff, D., 348-GTE-11 Ishida, Y., 53-TP-2 Jeffery, J., 355-MST-11 Johnson, V., 45-SE-1, 207-SE-3 Kalfon-Cohen, E., 33-MAT-1 Huffman, W., 330-APA-32 Ishihara, J., 89-MST-3 Jeffrey, R., 134-GNC-13 Johnson, W., 23-GNC-4, 155-SRE-2 Kalitzin, G., 341-FD-45 Hufty, D., 287-FD-38 Ishihara, K., 296-HSABP-5 Jegede, O., 175-APA-18 Johnston, C., 159-TP-5, 211-TP-6, 369-TP-9 Kalkhoran, I., 5-AA-1, 64-APA-7 Hull, P., 35-MDO-1 Ishihara, T., 128-FD-16, 241-FD-33 Jegley, D., 462-STR-16 Jolly, B., 118-AFM-5, 287-FD-38, 327-AFM-10 Kalsi, H., 389-FD-51 Humphrey, L., 195-ICC-2 Ishii, M., 431-AMT-9 Jemcov, A., 71-FD-11, 82-GTE-3 Joncas, S., 43-SD-1 Kamaraj, A., 399-GTE-14 Humphreys, C., 160-UMS-3 Ishikawa, H., 435-APA-44 Jenie, Y., 212-UMS-4, 346-GNC-31 Jones, A., 63-APA-6/FD-7, 245-GT-5, 280-APA-30, Kamath, S., 417-STR-14 Hunsaker, D., 279-APA-29, 434-APA-43 Ishiko, K., 280-APA-30 Jenkins, L., 65-APA-8 419-TP-10, 442-FD-57, 464-TP-11 Kamel, M., 307-PDL-9/FD-40 Hunt, J., 419-TP-10 Ishimura, K., 152-SCS-1 Jenkins, T., 172-AMT-4 Jones, D., 336-DSC-4 Kameyama, M., 417-STR-14 Huo, R., 434-APA-43 Isikveren, A., 168-ABPSI-4 Jennerjohn, M., 131-FD-19 Jones, F., 223-ACD-4 Kaminsky, A., 175-APA-18 Hurley, O., 268-WE-6 Islam, M., 262-STR-8 Jennings, A., 264-SUR-1 Jones, G., 137-GT-3, 279-APA-29, 329-AMT-7 Kamisori, K., 376-AFM-13 Husen, N., 431-AMT-9 Islam, S., 262-STR-8 Jenniskens, P., 211-TP-6 Jones, J., 383-DSC-5 Kamliya Jawahar, H., 334-APA-36 Hussain, F., 340-FD-44 Isola, D., 338-FD-42 Jensen, D., 463-STR-17 Jones, L., 290-GNC-24 Kan, P., 5-AA-1 Hussain, S., 10-AMT-10/SD-15 Ito, E., 266-UMS-6 Jensen, J., 170-ACD-3 Jones, T., 309-SCS-4, 460-SCS-7 Kanamori, M., 435-APA-44 Hussaini, M., 285-FD-36 Ito, S., 125-DE-1 Jeon, J., 177-ASC-2 Jones, W., 272-AA-6, 278-APA-28 Kanazaki, M., 125-DE-1, 169-ACD-2 Hussein, A., 7-AFM-1 Itoh, E., 36-MST-1 Jeon, S., 206-SCS-2, 460-SCS-7 Jonkman, J., 162-WE-3, 213-WE-4, 422-WE-11 Kaneshige, J., 188-GNC-18 Hussein, S., 125-DE-1 Iungo, G., 467-WE-12 Jeong, S., 36-MST-1 Joo, J., 200-MDO-4, 281-ASC-4 Kang, C., 98-SD-4, 230-APA-24 Hutchinson, S., 291-GNC-25 Ivanco, T., 245-GT-5, 438-DSC-6 Jerath, K., 252-MST-7 Joos, A., 454-MST-14 Kang, H., 18-FD-5, 381-APA-40 Huynh, H., 229-APA-23/FD-27, 388-FD-50 Iwakawa, A., 42-PDL-2, 71-FD-11 Jewell, J., 128-FD-16 Jorda Juanos, A., 94-PC-5 Kang, J., 233-ASC-3 Huyssen, J., 178-DE-2 Jaberi, F., 411-PC-17 Jha, R., 382-ASC-6 Jorge, R., 157-STR-5 Kannan, H., 147-NDA-2, 207-SE-3 Huyssen, R., 274-ACD-7 Jack, D., 275-AFM-9 Ji, W., 463-STR-17 Jorgens, C., 450-GT-9 Kannan, K., 349-GTE-12 Hwang, I., 29-IS-1/ICC-1/DA-1, 132-GNC-11, 196-IS-5, Jackson, B., 27-GTE-2 Jia, B., 344-GNC-29 Joseph, A., 157-STR-5 Kanner, S., 370-WE-8 393-GNC-33 Jackson, D., 308-SATS-3, 464-TP-11 Jia, P., 407-MVC-2 Joseph, N., 332-APA-34 Kantor, E., 383-DSC-5

Hwang, J., 11-APA-2, 299-MDO-6, 354-MDO-7 Jackson, J., 78-GNC-8, 235-DSC-2, 346-GNC-31 Jiang, F., 209-STR-7, 263-STR-9 Joshi, S., 382-ASC-6 Kao, D., 407-MVC-2 Hwang, Y., 280-APA-30 Jackson, T., 149-PC-6 Jiang, N., 9-AMT-1, 276-AMT-6/PC-11/PDL-8 Josyula, E., 159-TP-5, 265-TP-7 Kapaku, R., 294-GTE-10 Hynds, T., 44-SD-2 Jacob, J., 106-UMS-2, 212-UMS-4, 434-APA-43 Jiang, S., 152-SCS-1, 198-MAT-5 Jouannet, C., 169-ACD-2 Kapania, R., 50-STR-2, 98-SD-4, 125-DE-1, 170-ACD-3, Iarve, E., 156-STR-4 Jacob, R., 149-PC-6 Jiang, T., 9-AMT-1 Jouffroy, V., 244-GNC-23, 327-AFM-10 282-DSC-3, 314-STR-10, 375-AFM-12, 461-SD-14 Ichikawa, R., 190-GNC-20, 376-AFM-13 Jacobs, G., 52-TES-2/TP-1, 103-TES-3 Jimenez, H., 196-IS-5, 346-GNC-31, 428-ACD-13, Joyce, P., 49-STR-1 Kapat, J., 193-GTE-7 Iden, S., 145-MDO-3 Jacobson, K., 65-APA-8 453-IS-13 Ju, B., 183-FD-25 Kapusta, M., 167-AA-4 Ige, G., 6-ABPSI-1/GEPC-1 Jacques, D., 160-UMS-3 Jimenez-Garcia, A., 65-APA-8, 70-FD-9 Ju, Y., 39-PC-1, 41-PDL-1, 94-PC-5, Karagozian, A., 18-FD-5 Ihme, M., 167-AA-4, 180-FD-22, 294-GTE-10, Jadhav, S., 334-APA-36 Jinks, E., 332-APA-34, 433-APA-42 150-PDL-5/PC-7/AMT-3, 204-PC-8, 256-PC-10 Karakas, F., 442-FD-57 390-FD-52, 402-HSABP-7 Jafarnejadsani, H., 291-GNC-25 Jirasek, A., 332-APA-34 Jude, D., 386-FD-48 Karakaya, S., 460-SCS-7 Ikeda, Y., 40-PC-2 Jaffe, R., 104-TP-3, 211-TP-6 Jo, S., 355-MST-11 Juliano, T., 128-FD-16, 339-FD-43 Karamete, B., 278-APA-28 Ikuta, H., 309-SCS-4 Jain, R., 11-APA-2, 278-APA-28 Jo, Y., 35-MDO-1, 432-APA-41 Julien, M., 288-FD-39/APA-31 Karlgaard, C., 61-AFM-4 Im, C., 170-ACD-3 Jalali, R., 318-WE-7 Joarder, R., 359-PC-14 Jumper, E., 82-GTE-3, 240-FD-32, 286-FD-37, Karlsson, M., 37-MST-2 Im, D., 250-MDO-5, 272-AA-6, 286-FD-37 James, K., 6-ABPSI-1/GEPC-1, 59-ABPSI-2/GEPC-2 Jodeh, N., 80-GNC-10 307-PDL-9/FD-40 Karmakar, S., 359-PC-14 Im, H., 204-PC-8, 305-PC-12, 411-PC-17 James, M., 398-GTE-13, 399-GTE-14, 452-GTE-16 Joerger, M., 466-UMS-11 Jun, S., 97-SD-3 Karman, S., 70-FD-9, 129-FD-17, 356-MVC-1 Im, S., 96-PDL-4, 131-FD-19, 248-HSABP-4 James, S., 451-GTE-15 Johansen, C., 377-AMT-8 Junell, J., 293-GNC-27 Karpel, M., 311-SD-9, 364-SD-10 Imada, T., 242-GNC-21 Jameson, A., 388-FD-50 Johansen, T., 106-UMS-2, 446-GNC-38 Jung, Y., 228-APA-22 Karpenko, M., 186-GNC-16 Imamura, T., 129-FD-17, 224-ACD-5, 236-FD-28 Jamoom, M., 466-UMS-11 Johari, H., 127-FD-15, 183-FD-25 Jurgen, S., 228-APA-22 Kasahara, J., 28-HSABP-1, 296-HSABP-5 Imlay, S., 407-MVC-2 Jankovic, M., 135-GNC-14 John, T., 189-GNC-19 Jurkovich, M., 232-APA-26 Kasper, S., 275-AFM-9 Imran, M., 130-FD-18 Jans, E., 459-PDL-13 Johnsen, E., 284-FD-35 Just, L., 43-SD-1 Kassamnath, H., 312-SEN-2 Inampudi, R., 21-GNC-2, 302-MST-10 Jansen, Q., 274-ACD-7 Johnson, A., 23-GNC-4, 79-GNC-9 Justice, J., 144-MAT-4 Kassoy, D., 457-PC-18 Inman, D., 310-SD-8, 335-ASC-5 Jaridi, M., 308-SATS-3 Johnson, B., 195-ICC-2 Justin, C., 178-DE-2 Kastengren, A., 340-FD-44 Innocenti, M., 187-GNC-17, 393-GNC-33 Jasak, H., 18-FD-5 Johnson, D., 153-SD-5 Kabanda Mihigo, C., 199-MAT-6 Kasuga, Y., 435-APA-44 Inoyama, D., 461-SD-14 Jasinski, C., 272-AA-6 Johnson, E., 125-DE-1, 136-GNC-15, 275-AFM-9, Kabir, K., 339-FD-43 Kaszeta, R., 82-GTE-3 Invigorito, M., 457-PC-18 Jason, K., 122-APA-14 395-GNC-35 Kabiraj, L., 246-GTE-8 Kato, Y., 296-HSABP-5 Ippolito, C., 196-IS-5 Jastifer, J., 263-STR-9 Johnson, H., 128-FD-16 Kaemming, T., 296-HSABP-5 Kats, G., 256-PC-10 Irannejad, A., 411-PC-17 Jatiningrum, D., 243-GNC-22, 302-MST-10 Johnson, K., 10-AMT-10/SD-15 Kahnemouyi, S., 312-SEN-2 Katta, V., 41-PDL-1, 94-PC-5 Isaac, B., 303-NDA-5 Javed, U., 44-SD-2 Johnson, M., 318-WE-7, 451-GTE-15 Kailasanath, K., 28-HSABP-1, 296-HSABP-5, Katz, A., 288-FD-39/APA-31, 338-FD-42 Isaenkov, Y., 361-PDL-10 Jaworski, J., 183-FD-25, 422-WE-11 Johnson, P., 412-PDL-12 348-GTE-11, 398-GTE-13, 452-GTE-16 Kauffman, J., 44-SD-2, 177-ASC-2 Author/Session Chair Index Kawai, S., 283-FD-34, 284-FD-35, 410-PC-16 Khalil Hasan, A., 103-TES-3, 246-GTE-8 Kiyici, F., 139-GTE-5 Kono, Y., 152-SCS-1 Kumar, D., 44-SD-2 Kawakatsu, Y., 403-IS-11 Khan, O., 26-GTE-1, 334-APA-36 Klarmann, N., 451-GTE-15 Konrath, R., 232-APA-26 Kumar, M., 196-IS-5, 297-IS-7, 403-IS-11 Kawamoto, H., 155-SRE-2 Khieu, L., 284-FD-35 Klassen, M., 141-HSABP-2 Kontis, K., 42-PDL-2 Kumar, P., 105-TP-4 Kawashima, R., 459-PDL-13 Khol, A., 207-SE-3 Klein, C., 137-GT-3, 431-AMT-9 Kontitsis, M., 187-GNC-17 Kumar, R., 69-FD-8, 144-MAT-4, 179-FD-21, 191-GT-4 Kawazoe, H., 361-PDL-10 Khosravi, M., 370-WE-8, 422-WE-11 Klein, S., 389-FD-51, 391-FD-53 Kontogiannis, K., 194-HSABP-3 Kun, D., 132-GNC-11 Kaya, D., 325-ACD-8 Kianvashrad, N., 74-FD-14 Klein, V., 226-AFM-8 Koo, D., 277-APA-27 Kundu, S., 199-MAT-6 Kaya, M., 259-SD-7 Kidd, J., 212-UMS-4, 434-APA-43 Kleinhenz, J., 48-SRE-1 Koo, H., 222-ABPSI-5, 294-GTE-10, 451-GTE-15 Kuntz, D., 53-TP-2 Kayran, A., 208-STR-6, 213-WE-4, 310-SD-8, Kidder, N., 27-GTE-2 Klemkowsky, J., 227-AMT-5 Koo, J., 305-PC-12, 353-MAT-9, 419-TP-10 Kuo, C., 238-FD-30 415-SD-13, 418-STR-15 Kiel, B., 5-AA-1, 94-PC-5, 115-AA-3, 238-FD-30, Klepper, J., 278-APA-28 Koo, S., 205-SATS-2 Kupiainen, M., 283-FD-34 Kazarina, M., 287-FD-38 348-GTE-11, 398-GTE-13 Kleven, C., 138-GTE-4 Kopp, R., 310-SD-8 Kuratomi, T., 309-SCS-4 Kazemba, C., 10-AMT-10/SD-15 Kier, Z., 262-STR-8 Klijn, M., 251-MST-6 Kopp-Vaughan, K., 451-GTE-15 Kurdi, H., 291-GNC-25 Kearney, S., 62-AMT-2, 227-AMT-5, Kikuchi, J., 258-SCS-3 Kliment, L., 311-SD-9 Koreanschi, A., 233-ASC-3 Kurdila, A., 201-MST-5, 302-MST-10 276-AMT-6/PC-11/PDL-8 Kim, C., 177-ASC-2, 406-MST-13 Kline, H., 43-SD-1, 194-HSABP-3 Korkut, B., 104-TP-3 Kurdyumov, V., 256-PC-10 Keating, D., 146-MST-4, 201-MST-5 Kim, D., 49-STR-1, 394-GNC-34/ACD-12 Kling, D., 460-SCS-7 Korn, B., 437-DA-2 Kurtulus, D., 325-ACD-8 Keating, F., 212-UMS-4 Kim, H., 200-MDO-4, 310-SD-8, 448-GNC-40 Klochko, A., 257-PDL-7 Kornegay, J., 40-PC-2 Kuru, G., 126-FD-10 Keck, T., 378-APA-37 Kim, J., 7-AFM-1, 65-APA-8, 123-APA-15, 167-AA-4, Klock, R., 282-DSC-3 Koroglu, B., 39-PC-1 Kushner, L., 123-APA-15 Kecskemety, K., 318-WE-7, 384-EDU-2 186-GNC-16, 266-UMS-6, 355-MST-11 Klomparens, R., 19-FD-6 Kosarev, I., 204-PC-8 Kushner, M., 150-PDL-5/PC-7/AMT-3 Kedare, S., 21-GNC-2, 252-MST-7 Kim, K., 53-TP-2 Klosinski, K., 355-MST-11 Koshi, M., 149-PC-6, 359-PC-14 Kusmez, M., 346-GNC-31 Kedia, K., 256-PC-10 Kim, M., 73-FD-13 Klyde, D., 22-GNC-3, 188-GNC-18, 251-MST-6 Kosmatka, J., 98-SD-4, 153-SD-5 Kusunose, K., 428-ACD-13 Keesee, A., 308-SATS-3 Kim, N., 202-NDA-3, 253-NDA-4, 357-NDA-6, Knapp, K., 198-MAT-5 Koster, J., 178-DE-2 Kutay, A., 252-MST-7, 325-ACD-8, 396-GNC-36 Kegerise, M., 15-FD-2, 75-FD-20, 333-APA-35/FD-41 455-MST-15 Knight, D., 74-FD-14 Kota, S., 12-APA-3 Kuter, U., 352-IS-9 Kelkar, A., 144-MAT-4 Kim, S., 144-MAT-4, 195-ICC-2, 205-SATS-2, Knight, J., 152-SCS-1 Kothari, M., 448-GNC-40, 449-GNC-41 Kuzmenko, K., 387-FD-49 Kellas, S., 367-STR-12 376-AFM-13 Knight, T., 224-ACD-5 Kotikalpudi, A., 375-AFM-12 Kwan, J., 89-MST-3 Keller, D., 81-GT-2, 438-DSC-6 Kim, T., 97-SD-3 Knisely, A., 419-TP-10 Kotov, M., 67-APA-10 Kwatny, H., 188-GNC-18

Keller, G., 83-IS-2 Kim, Y., 24-GNC-5, 144-MAT-4, 177-ASC-2, 204-PC-8, Knopp, T., 126-FD-10 Kotsonis, M., 387-FD-49 Kwon, O., 11-APA-2 Keller, R., 457-PC-18 222-ABPSI-5 Knott, G., 314-STR-10 Kouchi, T., 141-HSABP-2, 377-AMT-8 Kwon, S., 311-SD-9 Kelley, C., 318-WE-7 Kimber, N., 102-STR-3 Knox, K., 119-APA-11 Kourdis, P., 39-PC-1, 256-PC-10 Kwong, R., 20-GNC-1 Kellogg, E., 168-ABPSI-4 Kimmel, K., 231-APA-25 Knuts, S., 253-NDA-4 Kourtzanidis, K., 459-PDL-13 Kypraiou, A., 458-PC-19 Kelso, R., 64-APA-7 Kimmel, R., 128-FD-16 Ko, S., 102-STR-3 Kowalchuk, S., 406-MST-13 L. de Oliveira Andrade, G., 459-PDL-13 Kemnetz, M., 307-PDL-9/FD-40 Kimura, T., 152-SCS-1 Kobayashi, M., 200-MDO-4 Koyanagi, J., 353-MAT-9 Lacher, A., 212-UMS-4 Kemp, D., 205-SATS-2 Kindysheva, S., 204-PC-8 Koch, H., 12-APA-3, 419-TP-10 Koziel, S., 88-MDO-2, 268-WE-6 Lackner, M., 267-WE-5, 467-WE-12 Kemper, J., 355-MST-11 King, C., 414-SD-12, 438-DSC-6 Koch, M., 343-GNC-28 Kraft, E., 191-GT-4 LaCombe, J., 376-AFM-13 Ken, T., 133-GNC-12 King, D., 41-PDL-1 Kochenderfer, M., 36-MST-1 Kraft, T., 363-SCS-5 Lacy, D., 66-APA-9 Kenerson, J., 382-ASC-6 King, J., 179-FD-21 Kochersberger, K., 266-UMS-6 Kramer, L., 437-DA-2 Lacy, T., 199-MAT-6 Kennedy, G., 200-MDO-4, 250-MDO-5, 299-MDO-6, King, P., 28-HSABP-1, 93-PC-4, 296-HSABP-5 Kochmann, D., 152-SCS-1 Kratz, J., 76-GNC-6, 300-MST-8 LaFontaine, J., 234-DSC-1 404-MDO-8 King, R., 15-FD-2, 441-FD-56, 467-WE-12 Kocian, T., 182-FD-24 Krebs, T., 64-APA-7 Lago, V., 459-PDL-13 Kennedy, W., 317-TP-8 Kingston, D., 448-GNC-40 Kodali, D., 230-APA-24 Krishna, S., 179-FD-21 Lagoudas, D., 298-MAT-8 Kennell, C., 245-GT-5 Kinney, T., 98-SD-4 Koga, S., 120-APA-12 Krishnakumar, K., 188-GNC-18, 293-GNC-27 Lai, J., 442-FD-57 Kenner, W., 309-SCS-4 Kio, M., 369-TP-9 Koike, S., 9-AMT-1, 120-APA-12, 377-AMT-8, 431-AMT-9 Krishnamurthy, T., 357-NDA-6, 382-ASC-6 Lai, K., 259-SD-7 Kenney, P., 201-MST-5, 355-MST-11 Kipouros, T., 121-APA-13 Koizumi, H., 459-PDL-13 Krivanek, T., 367-STR-12 Lake, M., 413-SCS-6 Kenny, S., 90-NDA-1 Kirby, A., 439-FD-54 Kok, J., 7-AFM-1, 374-ACD-11 Krofta, J., 127-FD-15 Lakebrink, M., 75-FD-20 Kenway, G., 35-MDO-1, 277-APA-27 Kirby, M., 59-ABPSI-2/GEPC-2 Koklu, M., 387-FD-49 Krott, M., 310-SD-8 Lakshminarayan, V., 18-FD-5, 122-APA-14, 338-FD-42 Keogh, J., 379-APA-38 Kirchner, F., 135-GNC-14 Kolmanovsky, I., 77-GNC-7 Kruger, M., 274-ACD-7 Lalit, H., 294-GTE-10 Kerbstadt, R., 12-APA-3 Kirik, J., 93-PC-4 Kolonay, R., 147-NDA-2, 200-MDO-4 Kryukov, I., 67-APA-10 Lambert, L., 383-DSC-5 Kern, Z., 189-GNC-19 Kiris, C., 120-APA-12, 176-APA-20, 331-APA-33 Komadina, S., 428-ACD-13 Kuehl, J., 182-FD-24 Lambert, T., 16-FD-3 Kerslake, T., 363-SCS-5 Kirkman, J., 224-ACD-5 Komives, J., 126-FD-10 Kuether, D., 135-GNC-14 Lammel, O., 40-PC-2 Kessler, D., 239-FD-31 Kirkpatrick, B., 384-EDU-2 Komjathy, A., 308-SATS-3 Kukreti, S., 403-IS-11 Lammering, T., 207-SE-3 Kessler, S., 382-ASC-6 Kirmse, T., 81-GT-2 Komperda, J., 131-FD-19, 411-PC-17, 443-FD-58 Kulakhmetov, M., 104-TP-3 Lampton, A., 136-GNC-15, 188-GNC-18, 251-MST-6 Key, N., 82-GTE-3, 138-GTE-4 Kirschen, P., 428-ACD-13 Komurasaki, K., 459-PDL-13 Kulkarni, A., 17-FD-4 Lan, L., 152-SCS-1 Khadeeja Nusrath, T., 430-AFM-15 Kitagawa, K., 125-DE-1 Komuro, T., 75-FD-20 Kulkarni, C., 453-IS-13 Landa, T., 66-APA-9 Khaled, A., 230-APA-24 Kitson, R., 282-DSC-3, 438-DSC-6 Kondoh, Y., 242-GNC-21 Kulkarni, M., 250-MDO-5 Landman, D., 347-GT-7 Khalil, E., 210-TES-5, 289-GEPC-4, 455-MST-15 Kivelevitch, E., 196-IS-5, 403-IS-11 Konig, B., 432-APA-41 Kumada, K., 286-FD-37 Landry, J., 180-FD-22 Author/Session Chair Index Langel, C., 120-APA-12, 441-FD-56 176-APA-20, 291-GNC-25, 333-APA-35/FD-41 Li, F., 15-FD-2, 429-AFM-14 Litt, J., 301-MST-9 Loyet, J., 66-APA-9 Langelaan, J., 252-MST-7 Lee, J., 177-ASC-2, 295-HIS-3, 305-PC-12 Li, H., 16-FD-3, 105-TP-4, 181-FD-23/PDL-6, Little, J., 19-FD-6, 95-PDL-3, 181-FD-23/PDL-6, Lu, G., 243-GNC-22 Langelaar, M., 200-MDO-4 Lee, K., 187-GNC-17, 394-GNC-34/ACD-12 331-APA-33, 362-PDL-11 387-FD-49, 442-FD-57 Lu, H., 312-SEN-2 Langley, B., 144-MAT-4 Lee, N., 413-SCS-6 Li, J., 89-MST-3 Liu, C., 70-FD-9, 123-APA-15, 352-IS-9, 378-APA-37, Lu, K., 12-APA-3 Langston, S., 225-AFM-7 Lee, S., 24-GNC-5, 29-IS-1/ICC-1/DA-1, 97-SD-3, 1 Li, L., 308-SATS-3, 389-FD-51 440-FD-55, 441-FD-56 Lu, L., 13-APA-4, 345-GNC-30/ACD-10 Lapenna, P., 149-PC-6 75-APA-18, 200-MDO-4, 237-FD-29, 268-WE-6, Li, M., 181-FD-23/PDL-6 Liu, D., 264-SUR-1, 316-SUR-2, 412-PDL-12 Lu, P., 20-GNC-1, 61-AFM-4, 77-GNC-7, 79-GNC-9, Larchevêque, L., 9-AMT-1, 131-FD-19, 389-FD-51 311-SD-9, 316-SUR-2, 382-ASC-6, 393-GNC-33 Li, N., 132-GNC-11 Liu, F., 16-FD-3, 42-PDL-2, 95-PDL-3, 115-AA-3, 376-AFM-13 Lardeau, S., 126-FD-10, 341-FD-45 Lee, T., 94-PC-5, 141-HSABP-2, 187-GNC-17 Li, P., 353-MAT-9 127-FD-15, 181-FD-23/PDL-6, 362-PDL-11 Lu, Y., 24-GNC-5, 120-APA-12, 151-SATS-1 Laroche, E., 406-MST-13 Lee-Rausch, E., 278-APA-28 Li, R., 33-MAT-1 Liu, H., 20-GNC-1, 39-PC-1, 104-TP-3, 186-GNC-16, Lu, Z., 259-SD-7 Larsen, C., 49-STR-1, 367-STR-12 Lefebvre, A., 123-APA-15 Li, S., 82-GTE-3, 149-PC-6 265-TP-7, 384-EDU-2, 446-GNC-38, 447-GNC-39 Lua, J., 156-STR-4, 157-STR-5, 315-STR-11 Larsen, G., 318-WE-7 Leffell, J., 18-FD-5 Li, X., 58-AA-2, 149-PC-6, 167-AA-4, 305-PC-12 Liu, J., 21-GNC-2, 422-WE-11, 452-GTE-16 Luca, S., 40-PC-2 Larsen, T., 318-WE-7 Lefkowitz, J., 150-PDL-5/PC-7/AMT-3, 204-PC-8, Li, Y., 13-APA-4, 371-WE-9, 461-SD-14 Liu, K., 120-APA-12, 264-SUR-1 Lucas, J., 308-SATS-3 Larson, R., 30-ISC-1 257-PDL-7 Li, Z., 72-FD-12, 126-FD-10, 405-MST-12 Liu, M., 136-GNC-15, 393-GNC-33, 420-UMS-10 Lucchetti, A., 438-DSC-6 Larsson, L., 379-APA-38 Legensky, S., 407-MVC-2 Lian, Y., 285-FD-36 Liu, P., 17-FD-4, 183-FD-25, 378-APA-37, 380-APA-39 Lucht, R., 399-GTE-14 LaRue, R., 106-UMS-2 Le Gouez, J., 439-FD-54 Liang, C., 388-FD-50 Liu, Q., 131-FD-19, 248-HSABP-4, 405-MST-12 Luckring, J., 59-ABPSI-2/GEPC-2 Lascara, B., 343-GNC-28 Legrenzi, P., 349-GTE-12 Liang, Z., 97-SD-3, 442-FD-57 Liu, R., 422-WE-11 Luhmann, B., 421-WE-10 Lassak, K., 188-GNC-18 Lei, Q., 368-STR-13 Liao, C., 302-MST-10 Liu, S., 226-AFM-8, 267-WE-5, 297-IS-7, 393-GNC-33 Lukaczyk, T., 273-ACD-6 Laten, J., 181-FD-23/PDL-6 Leib, S., 348-GTE-11, 398-GTE-13 Liburdy, J., 179-FD-21 Liu, T., 283-FD-34, 284-FD-35, 356-MVC-1, 431-AMT-9 Luke, E., 115-AA-3, 167-AA-4, 180-FD-22, 239-FD-31 Latscha, C., 334-APA-36 Leifsson, L., 88-MDO-2, 268-WE-6, 277-APA-27, Liceaga-Castro, E., 327-AFM-10 Liu, W., 106-UMS-2 Lundgren, E., 315-STR-11 Lau, T., 134-GNC-13 330-APA-32 Lidston, D., 33-MAT-1 Liu, X., 227-AMT-5, 288-FD-39/APA-31 Lundquist, T., 432-APA-41 Lauer, N., 160-UMS-3 Lele, S., 385-FD-47, 421-WE-10 Liebe, C., 378-APA-37 Liu, Y., 144-MAT-4, 149-PC-6, 156-STR-4, 169-ACD-2, Lung, S., 12-APA-3, 98-SD-4 Laughter, S., 188-GNC-18 Lemal, A., 159-TP-5 Lieber, M., 446-GNC-38 198-MAT-5, 204-PC-8, 419-TP-10 Luo, D., 439-FD-54 Laurendeau, E., 337-EDU-1 Lemma, L., 195-ICC-2 Lietz, C., 294-GTE-10 Liu, Z., 415-SD-13 Luo, H., 184-FD-26/APA-21, 243-GNC-22, 283-FD-34, Lavagna, M., 187-GNC-17, 244-GNC-23 Lemmens, Y., 336-DSC-4 Lieu, T., 375-AFM-12, 429-AFM-14 Livne, E., 225-AFM-7, 259-SD-7, 311-SD-9 284-FD-35, 288-FD-39/APA-31, 386-FD-48

Lavagnoli, S., 193-GTE-7, 399-GTE-14 Lemmers, A., 301-MST-9 Lieuwen, T., 306-PC-13, 360-PC-15 Locatelli, D., 125-DE-1, 170-ACD-3 Luo, L., 386-FD-48 LaVallee, D., 46-SEO-1 Lempert, W., 93-PC-4, 257-PDL-7, 377-AMT-8 Liguore, S., 364-SD-10 Lofthouse, A., 232-APA-26, 328-AFM-11 Luo, M., 384-EDU-2 Lavelle, M., 350-HIS-4 Lennie, M., 213-WE-4 Liles, C., 312-SEN-2 Logan, M., 54-UMS-1, 212-UMS-4, 325-ACD-8 Luo, S., 16-FD-3, 42-PDL-2, 95-PDL-3, 127-FD-15, Lavelle, T., 145-MDO-3 Leonard, R., 392-GNC-32 Lim, J., 233-ASC-3 Lohn, J., 196-IS-5 181-FD-23/PDL-6, 362-PDL-11 Lavely, A., 107-WE-1 Leonardi, S., 467-WE-12 Lim, T., 446-GNC-38 Lohrer, J., 367-STR-12 Luo, Z., 226-AFM-8 Lavin, T., 328-AFM-11 Leone, F., 462-STR-16 Lima, M., 384-EDU-2 Lohry, M., 299-MDO-6 Lupp, C., 438-DSC-6 Lavoie, P., 42-PDL-2, 240-FD-32, 444-FD-59 Leonhardt, B., 225-AFM-7 Limbach, C., 96-PDL-4 Lolatte, A., 162-WE-3 Lv, X., 290-GNC-24 Lavretsky, E., 292-GNC-26 Leonov, S., 361-PDL-10, 459-PDL-13 Limberger Tomiozzo, R., 337-EDU-1 Lombaerts, T., 22-GNC-3 Lv, Y., 180-FD-22 Lawerenz, M., 267-WE-5 Le Pape, A., 11-APA-2 Lin, A., 252-MST-7 Lombardi, M., 295-HIS-3 Lv, Z., 181-FD-23/PDL-6 Lawrence, S., 23-GNC-4 Lepikhin, N., 257-PDL-7 Lin, D., 449-GNC-41 Londner, E., 420-UMS-10 Lynch, E., 228-APA-22, 255-PC-9/GTE-9 Lawson, S., 280-APA-30 Le Riche, R., 202-NDA-3 Lin, G., 464-TP-11 Lone, M., 185-GEPC-3, 225-AFM-7 Lynch, J., 149-PC-6 Lay, C., 466-UMS-11 Leschziner, M., 71-FD-11 Lin, J., 16-FD-3, 185-GEPC-3 Long, K., 6-ABPSI-1/GEPC-1, 59-ABPSI-2/GEPC-2 Lynch, K., 221-AA-5 Lay, W., 102-STR-3 Lesieutre, G., 310-SD-8 Lin, K., 208-STR-6, 315-STR-11, 340-FD-44 Long, Y., 16-FD-3 Lynch, S., 399-GTE-14 Lazzara, D., 435-APA-44 Letarte, A., 43-SD-1 Lin, R., 59-ABPSI-2/GEPC-2 Lööf, J., 253-NDA-4 Lyrintzis, A., 58-AA-2 Le, D., 363-SCS-5 Lettieri, C., 464-TP-11 Lin, W., 404-MDO-8 Looye, G., 22-GNC-3 M. Thiruchengode, T., 13-APA-4, 227-AMT-5 Leao, S., 33-MAT-1 Leve, F., 393-GNC-33 Lin, Y., 262-STR-8 Loper, E., 309-SCS-4 Ma, L., 290-GNC-24 Leavitt, L., 6-ABPSI-1/GEPC-1 Levin, D., 104-TP-3, 204-PC-8, 440-FD-55 Lind, R., 7-AFM-1 Lopez, J., 39-PC-1 Ma, P., 294-GTE-10 LeBeau, R., 127-FD-15, 138-GTE-4, 181-FD-23/PDL-6, Levinski, O., 332-APA-34 Linders, V., 283-FD-34 Lord, W., 59-ABPSI-2/GEPC-2 Ma, T., 455-MST-15 384-EDU-2 Levitt, I., 343-GNC-28, 392-GNC-32 Lindsey, N., 87-MAT-3 Loth, E., 116-ABPSI-3, 268-WE-6, 340-FD-44 Mabson, G., 208-STR-6 Lebid, A., 95-PDL-3 Lewalle, J., 5-AA-1, 115-AA-3, 238-FD-30 Linehan, T., 230-APA-24 Lou, J., 386-FD-48 Macdonald, R., 104-TP-3, 369-TP-9 Lebofsky, S., 235-DSC-2 Lewis, D., 33-MAT-1, 245-GT-5 Lingenfelter, A., 264-SUR-1 Love, N., 52-TES-2/TP-1, 210-TES-5 MacDonald, T., 273-ACD-6 LeDoux, S., 277-APA-27, 330-APA-32 Lewis, M., 167-AA-4, 237-FD-29 Linne, D., 48-SRE-1, 155-SRE-2 Lovejoy, A., 462-STR-16 Macheret, S., 96-PDL-4, 150-PDL-5/PC-7/AMT-3, Lee, A., 384-EDU-2, 445-GNC-37 Lewis, T., 346-GNC-31 Linskens, H., 242-GNC-21 Lovich, B., 210-TES-5 361-PDL-10 Lee, B., 204-PC-8, 411-PC-17 Leyva, I., 40-PC-2 Linton, K., 462-STR-16 Low, K., 106-UMS-2, 190-GNC-20 Mackay, J., 243-GNC-22 Lee, C., 451-GTE-15 Lhachemi, H., 76-GNC-6 Liotta, A., 33-MAT-1 Mackunis, W., 396-GNC-36 Lee, D., 35-MDO-1, 272-AA-6, 310-SD-8 Li, C., 124-CMS-1/CPS-1, 202-NDA-3, 294-GTE-10, Liou, M., 385-FD-47 Lowe, K., 5-AA-1, 9-AMT-1, 116-ABPSI-3, 172-AMT-4, MacLean, M., 53-TP-2, 119-APA-11 Lee, G., 144-MAT-4 360-PC-15, 442-FD-57 Lisanti, J., 192-GTE-6 348-GTE-11 MacManus, D., 168-ABPSI-4 Lee, H., 36-MST-1, 78-GNC-8, 173-APA-16, 175-APA-18, Li, D., 131-FD-19, 411-PC-17, 443-FD-58 Litke, P., 168-ABPSI-4 Lowenberg, M., 336-DSC-4, 383-DSC-5, 450-GT-9 MacNeal, C., 84-ISC-3 Author/Session Chair Index Macquart, T., 417-STR-14 Marais, K., 453-IS-13 Matalon, M., 256-PC-10 McKeon, B., 240-FD-32 Merret, J., 169-ACD-2, 224-ACD-5 Madavan, N., 185-GEPC-3, 284-FD-35 Maraniello, S., 259-SD-7 Mateescu, D., 230-APA-24 McLain, T., 243-GNC-22, 466-UMS-11 Merrett, C., 29-IS-1/ICC-1/DA-1, 209-STR-7, 415-SD-13 Madden, T., 307-PDL-9/FD-40 Marañón Di Leo, J., 107-WE-1 Mathews, E., 307-PDL-9/FD-40 McLaughlin, D., 5-AA-1, 115-AA-3, 167-AA-4, Merrill, B., 280-APA-30 Madenci, E., 368-STR-13 Marcella, I., 312-SEN-2 Mathias, D., 211-TP-6 379-APA-38 Mert, M., 418-STR-15 Madni, A., 99-SE-2, 207-SE-3 Mardanpour, P., 49-STR-1 Mathisen, S., 106-UMS-2 McLaughlin, T., 69-FD-8, 95-PDL-3, 332-APA-34, Mertens, C., 442-FD-57 Madrid, J., 253-NDA-4 Marien, T., 224-ACD-5, 274-ACD-7 Matlik, J., 249-MAT-7 334-APA-36, 379-APA-38 Merz, C., 231-APA-25 Madsen, H., 268-WE-6, 318-WE-7, 370-WE-8 Marineau, E., 128-FD-16, 245-GT-5, 339-FD-43 Matlis, E., 82-GTE-3, 362-PDL-11 McLean, C., 40-PC-2 Mesmer, B., 147-NDA-2 Maggiore, M., 77-GNC-7 Marks, C., 26-GTE-1, 70-FD-9, 281-ASC-4, 444-FD-59 Matney, A., 364-SD-10 McManus, K., 94-PC-5 Messac, A., 88-MDO-2 Magin, T., 192-GTE-6 Marlier, R., 88-MDO-2 Matsumoto, N., 152-SCS-1 McMillin, S., 59-ABPSI-2/GEPC-2 Mestreau, E., 278-APA-28 Magni, F., 451-GTE-15 Marques, F., 415-SD-13 Matsumoto, S., 242-GNC-21 McMurray, R., 48-SRE-1 Meyer, C., 447-GNC-39 Magree, D., 136-GNC-15 Marquez Gonzalez, E., 155-SRE-2 Matsuno, T., 361-PDL-10 McNally, R., 278-APA-28 Meyer, J., 174-APA-17, 274-ACD-7 Magstadt, A., 348-GTE-11, 398-GTE-13 Marruffo, A., 286-FD-37 Matsuo, A., 28-HSABP-1, 296-HSABP-5 McNamara, J., 97-SD-3, 154-SD-6, 234-DSC-1, Meyer, P., 157-STR-5 Mahadevan, S., 90-NDA-1, 202-NDA-3, 357-NDA-6 Marsden, O., 58-AA-2 Matsuo, Y., 380-APA-39 282-DSC-3, 318-WE-7 Meyer, S., 246-GTE-8 Mahadik, Y., 35-MDO-1 Marsden, W., 249-MAT-7, 353-MAT-9 Matsuoka, K., 28-HSABP-1, 296-HSABP-5 McQuillen, J., 464-TP-11 Meyer, T., 9-AMT-1, 62-AMT-2, 276-AMT-6/PC-11/PDL-8 Mai, H., 102-STR-3 Marsh, R., 246-GTE-8 Matsuse, Y., 128-FD-16 McQuilling, M., 131-FD-19 Meyers, J., 421-WE-10 Maimeri, M., 251-MST-6 Marshall, C., 362-PDL-11 Matsuura, Y., 344-GNC-29 Meadows, L., 50-STR-2 Michael, J., 62-AMT-2, 149-PC-6 Majdalani, J., 31-ISC-2 Marshall, J., 83-IS-2 Matsuyama, S., 159-TP-5 Meakin, R., 122-APA-14 Michael, L., 129-FD-17 Majji, M., 243-GNC-22 Marsman, A., 345-GNC-30/ACD-10 Matt, A., 210-TES-5 Mebarki, Y., 233-ASC-3 Michaels, D., 256-PC-10 Makino, A., 309-SCS-4 Marston, M., 376-AFM-13 Matthews, J., 401-SAT-1 Meckstroth, C., 64-APA-7 Mies, D., 353-MAT-9 Makino, Y., 435-APA-44 Mårtensson, H., 441-FD-56 Mattos, B., 279-APA-29 Meddaikar, Y., 102-STR-3 Mignolet, M., 66-APA-9, 364-SD-10, 383-DSC-5 Makkapati, V., 448-GNC-40 Martensson, J., 392-GNC-32 Maul, W., 453-IS-13 Medhi, B., 227-AMT-5 Milanese, R., 405-MST-12 Malangoni, J., 178-DE-2 Martin, A., 53-TP-2, 126-FD-10, 317-TP-8, 465-TP-12 Mavriplis, D., 18-FD-5, 184-FD-26/APA-21, 209-STR-7, Medic, G., 341-FD-45 Miles, R., 9-AMT-1, 95-PDL-3, 96-PDL-4, Malani, P., 205-SATS-2 Martin, C., 97-SD-3, 140-HIS-1, 282-DSC-3 250-MDO-5, 277-APA-27, 404-MDO-8, 439-FD-54 Medwell, P., 73-FD-13 150-PDL-5/PC-7/AMT-3, 276-AMT-6/PC-11/PDL-8, Malecek, J., 415-SD-13 Martin, F., 43-SD-1 Mavris, D., 45-SE-1, 88-MDO-2, 117-ACD-1, 146-MST-4, Megahed, M., 353-MAT-9 362-PDL-11

Malik, B., 225-AFM-7 Martin, M., 74-FD-14, 105-TP-4, 384-EDU-2, 464-TP-11 169-ACD-2, 178-DE-2, 196-IS-5, 273-ACD-6, Meheut, M., 277-APA-27 Milhoan, J., 317-TP-8 Malik, M., 229-APA-23/FD-27, 333-APA-35/FD-41 Martin, R., 54-UMS-1 354-MDO-7, 430-AFM-15, 453-IS-13 Mehiel, E., 406-MST-13 Millecam, N., 185-GEPC-3 Malinek, P., 415-SD-13 Martinelli, L., 299-MDO-6 Maxwell, K., 202-NDA-3 Mehmani, A., 88-MDO-2 Miller, C., 352-IS-9 Mall, K., 8-AFM-2 Martinez, L., 267-WE-5 May, G., 455-MST-15 Meholic, G., 192-GTE-6 Miller, D., 162-WE-3 Malla, B., 115-AA-3, 351-HSABP-6 Martinez, N., 205-SATS-2 May, I., 386-FD-48 Mehta, M., 119-APA-11 Miller, E., 12-APA-3, 175-APA-18 Malla, R., 155-SRE-2, 310-SD-8 Martinez-Cava, A., 193-GTE-7 Mazaheri, A., 283-FD-34 Mehta, N., 104-TP-3, 204-PC-8 Miller, J., 9-AMT-1, 62-AMT-2, 393-GNC-33, 458-PC-19 Mallik, W., 50-STR-2 Martins, B., 153-SD-5 Mazzaracchio, A., 290-GNC-24 Mehta, S., 135-GNC-14, 293-GNC-27, 396-GNC-36 Miller, K., 172-AMT-4 Mallikarachchi, H., 206-SCS-2 Martins, J., 35-MDO-1, 145-MDO-3, 250-MDO-5, Mazzini, C., 337-EDU-1 Meier, W., 40-PC-2, 92-PC-3 Miller, R., 351-HSABP-6 Malo-Molina, F., 194-HSABP-3 277-APA-27, 354-MDO-7 Mbagwu, C., 194-HSABP-3 Meinke, M., 129-FD-17, 130-FD-18, 239-FD-31 Miller, T., 335-ASC-5 Mamou, M., 233-ASC-3 Maruyama, R., 67-APA-10, 96-PDL-4 McAllister, Q., 363-SCS-5 Mejia-Alvarez, R., 227-AMT-5 Miller, W., 73-FD-13 Manar, F., 63-APA-6/FD-7 Mary, I., 439-FD-54 McClearn, M., 192-GTE-6 Mejia-Ariza, J., 298-MAT-8, 314-STR-10 Mills, A., 30-ISC-1 Mance, J., 9-AMT-1 Marzocca, P., 332-APA-34, 414-SD-12 McClelland, H., 201-MST-5 Melton, J., 59-ABPSI-2/GEPC-2 Mills, B., 25-GT-1 Mancini, P., 63-APA-6/FD-7 Masciarelli, J., 446-GNC-38 McCourt, M., 135-GNC-14, 293-GNC-27 Melvin, R., 330-APA-32 Mills, D., 53-TP-2, 144-MAT-4, 431-AMT-9 Mandal, T., 134-GNC-13 Maser, J., 151-SATS-1 McCrink, M., 60-AFM-3 Memon, M., 391-FD-53 Millwater, H., 303-NDA-5 Manero, A., 87-MAT-3 Mashayek, F., 103-TES-3, 131-FD-19, 411-PC-17, McDaniel, D., 122-APA-14, 228-APA-22, 278-APA-28 Mendeck, G., 79-GNC-9 Milos, F., 317-TP-8 Mani, K., 404-MDO-8 443-FD-58 McDaniel, J., 141-HSABP-2 Mendoza, J., 272-AA-6 Milutinovic, D., 448-GNC-40 Maniaci, D., 161-WE-2, 318-WE-7, 370-WE-8 Masi, A., 389-FD-51 McDevitt, M., 205-SATS-2 Meneghini, J., 279-APA-29 Min, B., 65-APA-8 Mankbadi, M., 391-FD-53 Massa, L., 458-PC-19 McDonald, R., 223-ACD-4 Meneveau, C., 267-WE-5, 421-WE-10 Min, J., 314-STR-10 Mankbadi, R., 15-FD-2, 167-AA-4 Massey, S., 12-APA-3, 331-APA-33 McEachen, M., 413-SCS-6 Menezes, N., 33-MAT-1 Min, K., 94-PC-5 Mann, T., 463-STR-17 Masters, D., 121-APA-13, 330-APA-32 McElroy, T., 245-GT-5 Meng, P., 299-MDO-6 Mindt, H., 353-MAT-9 Manning, R., 46-SEO-1 Masters, J., 356-MVC-1 McEver, J., 195-ICC-2 Meng, X., 16-FD-3, 95-PDL-3, 127-FD-15, Minnetyan, L., 208-STR-6 Mannucci, T., 135-GNC-14, 244-GNC-23, 293-GNC-27 Mastorakos, E., 359-PC-14, 411-PC-17, 458-PC-19 McGann, B., 131-FD-19, 141-HSABP-2, 248-HSABP-4 181-FD-23/PDL-6, 362-PDL-11 Minwalla, C., 302-MST-10 Manolesos, M., 107-WE-1 Masud, J., 26-GTE-1, 121-APA-13, 130-FD-18, McGarry, J., 93-PC-4 Menon, S., 93-PC-4, 306-PC-13, 458-PC-19 Mirzaeifar, R., 405-MST-12 Manso, S., 454-MST-14 171-AFM-6, 225-AFM-7, 334-APA-36 McGowan, D., 233-ASC-3 Menzies, K., 452-GTE-16 Mishra, A., 404-MDO-8 Mantovani, J., 48-SRE-1 Masui, K., 29-IS-1/ICC-1/DA-1 McGowen, R., 82-GTE-3 Mercado-Perez, J., 378-APA-37 Missoum, S., 299-MDO-6 Manuel, L., 213-WE-4, 422-WE-11 Masuko, T., 224-ACD-5 McGrath, B., 22-GNC-3 Meritt, R., 125-DE-1 Mitchell, S., 90-NDA-1 Mao, S., 106-UMS-2 Masuya, G., 141-HSABP-2 McGwier, R., 465-TP-12 Merkle, C., 405-MST-12 Mitchell, T., 212-UMS-4 Maqbool, D., 92-PC-3 Mataczynski, M., 168-ABPSI-4, 192-GTE-6 McIntosh-Smith, S., 386-FD-48 Merrell, M., 334-APA-36 Mitchener, M., 275-AFM-9 Author/Session Chair Index Mitsingas, C., 41-PDL-1 Morrell, B., 135-GNC-14 Murphy, J., 101-SOF-3, 376-AFM-13 Naoumov, V., 384-EDU-2, 457-PC-18 Niehaus, J., 160-UMS-3 Mittal, A., 161-WE-2, 467-WE-12 Morrida, J., 286-FD-37 Murphy, P., 226-AFM-8 Naples, A., 192-GTE-6 Nielsen, E., 64-APA-7, 229-APA-23/FD-27 Miura, K., 310-SD-8 Morris, J., 308-SATS-3 Murray, A., 245-GT-5, 419-TP-10, 464-TP-11 Napolitano, M., 292-GNC-26 Nieuwenhuizen, F., 251-MST-6, 454-MST-14 Miyamoto, Y., 36-MST-1 Morris, P., 5-AA-1, 115-AA-3, 167-AA-4, 272-AA-6 Murray, D., 46-SEO-1 Naraghi, M., 298-MAT-8 Nigam, N., 233-ASC-3 Miyashita, T., 258-SCS-3 Morris, S., 71-FD-11 Murray, H., 272-AA-6 Narang-Siddarth, A., 20-GNC-1, 290-GNC-24 Nikiforakis, N., 129-FD-17 Miyazaki, T., 431-AMT-9 Morrison, D., 211-TP-6 Murray, J., 66-APA-9, 231-APA-25 Naranjo, A., 327-AFM-10 Nilsson, E., 37-MST-2 Miyazato, Y., 377-AMT-8 Morrison, J., 441-FD-56 Murray, N., 10-AMT-10/SD-15 Narducci, R., 11-APA-2, 65-APA-8, 122-APA-14 Ning, A., 370-WE-8, 381-APA-40, 466-UMS-11 Miyazawa, Y., 36-MST-1 Morsy, M., 289-GEPC-4 Murri, D., 275-AFM-9 Nark, D., 5-AA-1, 115-AA-3, 272-AA-6 Ning, Z., 381-APA-40 Mizukaki, T., 377-AMT-8 Mortari, D., 135-GNC-14 Murthy, R., 364-SD-10 Narsipur, S., 287-FD-38 Nisbet, E., 327-AFM-10 Mizuno, Y., 131-FD-19, 265-TP-7 Mortazavi, M., 74-FD-14 Musavi, N., 212-UMS-4 Nash, A., 118-AFM-5 Nishida, H., 361-PDL-10 Mocarski, A., 384-EDU-2 Mortimer, B., 22-GNC-3 Muse, J., 132-GNC-11, 292-GNC-26, Nash, L., 39-PC-1 Nishihara, M., 377-AMT-8 Modlin, C., 367-STR-12 Mortished, C., 88-MDO-2 394-GNC-34/ACD-12 Natella, M., 98-SD-4 Nishikawa, H., 236-FD-28, 283-FD-34 Moeller, T., 465-TP-12 Morton, S., 122-APA-14, 228-APA-22 Musi, S., 295-HIS-3, 350-HIS-4 Natori, M., 258-SCS-3, 309-SCS-4 Nishimura, S., 159-TP-5 Moens, F., 331-APA-33 Moser, T., 413-SCS-6 Mustafa, G., 209-STR-7 Naughton, J., 107-WE-1, 238-FD-30, 431-AMT-9 Nishiyama, T., 29-IS-1/ICC-1/DA-1 Moertl, P., 343-GNC-28 Moses, C., 29-IS-1/ICC-1/DA-1 Muto, D., 73-FD-13 Navratil, J., 332-APA-34 Nishizawa, T., 258-SCS-3 Mohaghegh, M., 418-STR-15 Moszczynski, G., 226-AFM-8 Muto, K., 28-HSABP-1, 296-HSABP-5 Nawroth, H., 390-FD-52 Nitsche, W., 16-FD-3 Mohan, A., 287-FD-38 Motsinger, A., 27-GTE-2 Mutuel, L., 46-SEO-1 Nayani, S., 232-APA-26, 435-APA-44, 450-GT-9 Nitzsche, F., 235-DSC-2 Mohan, G., 84-ISC-3 Mouy, A., 7-AFM-1 Muzychka, Y., 464-TP-11 Nayeri, C., 73-FD-13, 127-FD-15, 213-WE-4, Nix, A., 192-GTE-6, 193-GTE-7 Mohseni, K., 183-FD-25, 230-APA-24, 232-APA-26, Moyes, A., 182-FD-24 Myers, L., 67-APA-10, 115-AA-3, 379-APA-38 379-APA-38 Noevere, A., 49-STR-1 342-FD-46, 403-IS-11 Mu, Z., 464-TP-11 Nabipour, O., 455-MST-15 Neely, A., 234-DSC-1, 245-GT-5 Noh, S., 53-TP-2 Moin, P., 123-APA-15 Muehleisen, R., 221-AA-5 Naboulsi, S., 87-MAT-3 Neema, K., 195-ICC-2 Nolcheff, N., 138-GTE-4, 399-GTE-14 Moini-Yekta, S., 435-APA-44 Mueller, B., 418-STR-15 Nadarajah, S., 277-APA-27, 388-FD-50 Neergaard, L., 97-SD-3, 282-DSC-3 Noll, B., 130-FD-18 Mokhtarpoor, R., 341-FD-45, 389-FD-51 Mueller, F., 386-FD-48 Naeije, M., 133-GNC-12 Nehrenz, M., 205-SATS-2 Nompelis, I., 104-TP-3 Mollenhauer, D., 156-STR-4 Mueller, M., 294-GTE-10, 451-GTE-15 Nagai, H., 8-AFM-2, 75-FD-20 Neifeld, A., 81-GT-2 Nomura, S., 159-TP-5

Moncayo, H., 189-GNC-19 Mueller, R., 48-SRE-1, 189-GNC-19, 201-MST-5 Nagai, S., 120-APA-12, 242-GNC-21 Neild, S., 450-GT-9 Nomura, T., 224-ACD-5 Monegato, G., 50-STR-2 Mueller-Vahl, H., 287-FD-38 Nagapetyan, H., 239-FD-31 Neilsen, T., 398-GTE-13, 399-GTE-14, 452-GTE-16 Nonomura, T., 72-FD-12, 131-FD-19, Monfort, J., 94-PC-5 Mughal, M., 441-FD-56 Nagaraja, S., 41-PDL-1 Neiswander, B., 362-PDL-11 181-FD-23/PDL-6, 265-TP-7 Monner, H., 281-ASC-4 Muilenburg, C., 412-PDL-12 Nagata, T., 131-FD-19, 265-TP-7 Neitzel, K., 265-TP-7 Noonan, W., 299-MDO-6 Montague, D., 160-UMS-3 Mukherjee, B., 225-AFM-7 Nagayama, T., 75-FD-20 Nelson, C., 5-AA-1, 225-AFM-7 Norambuena, M., 221-AA-5 Montgomery, J., 79-GNC-9 Mukherjee, R., 66-APA-9, 380-APA-39 Nagel, B., 174-APA-17, 224-ACD-5, 289-GEPC-4 Nelson, M., 245-GT-5 Nordstrom, J., 283-FD-34, 432-APA-41 Montolio, J., 345-GNC-30/ACD-10 Mulani, S., 461-SD-14 Naghipour, P., 208-STR-6 Nematollahi, M., 458-PC-19 Noriega, A., 212-UMS-4 Mooij, E., 8-AFM-2, 77-GNC-7, 133-GNC-12, Mulder, J., 174-APA-17, 395-GNC-35 Nagib, H., 126-FD-10, 285-FD-36 Nemec, M., 211-TP-6 Norman, R., 90-NDA-1 189-GNC-19, 242-GNC-21, 449-GNC-41 Mulder, M., 7-AFM-1, 243-GNC-22, 302-MST-10, Naik, K., 205-SATS-2, 308-SATS-3 Nesbitt, E., 221-AA-5 Norman, T., 65-APA-8 Moon, S., 297-IS-7 327-AFM-10 Naik, R., 144-MAT-4 Nethala, V., 260-SEN-1 Norwood, D., 49-STR-1, 315-STR-11 Mooney, J., 395-GNC-35 Mulleners, K., 179-FD-21, 280-APA-30 Naik, S., 246-GTE-8, 294-GTE-10 Neuhart, D., 333-APA-35/FD-41 Novikov, A., 15-FD-2 Moore, K., 381-APA-40 Mullins, C., 412-PDL-12 Naito, Y., 309-SCS-4 Neumann, J., 353-MAT-9 Novitsky, B., 27-GTE-2 Moored, K., 442-FD-57 Munafò, A., 104-TP-3, 369-TP-9 Najafi, A., 249-MAT-7, 262-STR-8 Neuroth, C., 94-PC-5 Numata, D., 431-AMT-9 Moormann, D., 447-GNC-39 Mundis, N., 18-FD-5 Nakajima, T., 377-AMT-8, 431-AMT-9 New, T., 174-APA-17 Nuzum, S., 145-MDO-3 Mora, P., 348-GTE-11, 398-GTE-13 Munhoz, V., 33-MAT-1 Nakakita, K., 9-AMT-1, 380-APA-39, 431-AMT-9 Newman, J., 232-APA-26, 404-MDO-8 O`Connor, J., 306-PC-13, 359-PC-14 Morajkar, R., 248-HSABP-4, 339-FD-43 Munk, D., 200-MDO-4, 202-NDA-3 Nakakuki, K., 344-GNC-29 Newman, R., 22-GNC-3 O’Brien, D., 122-APA-14, 280-APA-30 Morando, A., 89-MST-3 Munoz, E., 346-GNC-31 Nakamura, K., 152-SCS-1 Newmeyer, K., 122-APA-14 O’Brien, J., 167-AA-4 Morar, R., 434-APA-43 Munz, E., 227-AMT-5 Nakamura, N., 152-SCS-1 Ng, H., 89-MST-3 O’Brien, W., 116-ABPSI-3 Morelli, E., 78-GNC-8, 430-AFM-15 Mura, G., 64-APA-7 Nakamura, Y., 89-MST-3, 133-GNC-12 Ng, W., 9-AMT-1, 348-GTE-11 O’Connell, T., 275-AFM-9 Moreto, J., 227-AMT-5 Murakami, K., 120-APA-12 Nakano, E., 242-GNC-21 Nguyen, C., 283-FD-34 O’Connor, J., 378-APA-37 Morgan, P., 13-APA-4, 239-FD-31 Muraleedharan, M., 105-TP-4 Nakao, S., 377-AMT-8 Nguyen, D., 168-ABPSI-4 O’Donnell, J., 199-MAT-6 Mori, K., 67-APA-10, 96-PDL-4 Muraoka, K., 20-GNC-1 Nakashima, Y., 236-FD-28 Nguyen, H., 384-EDU-2, 457-PC-18 O’Donnell, M., 35-MDO-1 Mori, O., 258-SCS-3 Murayama, M., 169-ACD-2 Nakata, T., 63-APA-6/FD-7 Nguyen, L., 15-FD-2, 167-AA-4, 287-FD-38 O’Hara, P., 364-SD-10 Moriarty, P., 268-WE-6, 318-WE-7 Murchison, L., 308-SATS-3 Nakka, Y., 35-MDO-1 Nguyen, N., 83-IS-2, 235-DSC-2 O’Neil, P., 223-ACD-4 Morimoto, N., 231-APA-25 Murman, S., 180-FD-22, 229-APA-23/FD-27, Nalci, M., 252-MST-7 Nichols, J., 378-APA-37, 467-WE-12 Oates, W., 53-TP-2, 144-MAT-4 Morimoto, T., 353-MAT-9 284-FD-35, 331-APA-33, 431-AMT-9 Nanda, J., 124-CMS-1/CPS-1 Nichols, R., 122-APA-14, 228-APA-22, 278-APA-28 Obabko, A., 285-FD-36 Morlier, J., 438-DSC-6 Murphey, T., 298-MAT-8, 314-STR-10 Nandi, T., 107-WE-1 Nickol, C., 185-GEPC-3, 223-ACD-4, 224-ACD-5 Obata, R., 155-SRE-2 Morr, D., 435-APA-44 Murphy, D., 206-SCS-2, 363-SCS-5, 413-SCS-6 Naohiko, B., 428-ACD-13 Nie, S., 405-MST-12 Obayashi, S., 329-AMT-7, 376-AFM-13 Author/Session Chair Index Obraczka, K., 312-SEN-2 Ostermann, F., 73-FD-13 Pant, K., 259-SD-7 Paxson, D., 28-HSABP-1, 168-ABPSI-4, 192-GTE-6, Phillips, N., 63-APA-6/FD-7 Ochi, Y., 20-GNC-1 Osteroos, R., 355-MST-11 Pant, T., 411-PC-17 255-PC-9/GTE-9, 351-HSABP-6 Phillips, T., 180-FD-22 Ochs, B., 93-PC-4, 306-PC-13 Ostrowski, D., 211-TP-6 Papadakis, G., 107-WE-1, 279-APA-29, 444-FD-59 Payan, A., 453-IS-13 Phong, V., 115-AA-3 Ochs, S., 59-ABPSI-2/GEPC-2 Ota, T., 377-AMT-8 Papamoschou, D., 115-AA-3 Payne, M., 33-MAT-1 Piana, M., 201-MST-5 Odegard, G., 33-MAT-1, 199-MAT-6 Othman, M., 210-TES-5 Papapetrou, V., 49-STR-1 Pearl, J., 435-APA-44 Piatak, D., 119-APA-11, 245-GT-5 Oe, H., 371-WE-9 Othmer, C., 386-FD-48 Pape, O., 289-GEPC-4 Pechlivanoglou, G., 213-WE-4 Pieri, D., 196-IS-5 Oefelein, J., 411-PC-17 Otsuki, M., 242-GNC-21 Pappa, R., 363-SCS-5, 413-SCS-6 Peck, J., 461-SD-14 Pierre, D., 9-AMT-1, 19-FD-6 Ogawa, H., 414-SD-12 Overton, N., 386-FD-48 Paquin, L., 128-FD-16 Peck, M., 154-SD-6, 290-GNC-24, 308-SATS-3, Pillsbury, T., 233-ASC-3 Ogino, Y., 128-FD-16, 241-FD-33, 283-FD-34 Owen, L., 129-FD-17, 385-FD-47 Parambil, N., 157-STR-5 446-GNC-38 Pinchak, M., 41-PDL-1 Oh, H., 36-MST-1 Owens, L., 15-FD-2 Paranjape, A., 291-GNC-25 Pecora, R., 233-ASC-3, 281-ASC-4 Pineda, E., 157-STR-5, 208-STR-6, 367-STR-12 Oh, S., 18-FD-5 Oyama, A., 8-AFM-2, 72-FD-12, 403-IS-11 Paredes, P., 15-FD-2, 182-FD-24 Peet, Y., 280-APA-30, 421-WE-10 Pineda, S., 442-FD-57 Ohata, R., 344-GNC-29 Ozawa, S., 152-SCS-1 Paris, A., 355-MST-11 Peeters, D., 417-STR-14 Piness, J., 199-MAT-6 Ohnishi, N., 128-FD-16, 241-FD-33 Ozawa, T., 369-TP-9 Parise, T., 39-PC-1 Pei, C., 285-FD-36 Pinier, J., 119-APA-11, 173-APA-16 Ohno, D., 398-GTE-13 Ozdemir, H., 161-WE-2 Park, C., 105-TP-4, 187-GNC-17, 253-NDA-4, Pei, J., 308-SATS-3 Pinkerman, C., 275-AFM-9 Oka, Y., 141-HSABP-2 Ozgen, S., 68-ASC-1 355-MST-11, 455-MST-15 Peigin, S., 330-APA-32 Pinon-Fischer, O., 88-MDO-2, 273-ACD-6 Okai, K., 103-TES-3 Pabon, R., 240-FD-32 Park, G., 310-SD-8, 333-APA-35/FD-41 Peinke, J., 318-WE-7 Pinsky, L., 308-SATS-3 Okasinski, J., 87-MAT-3 Pachter, M., 447-GNC-39 Park, J., 35-MDO-1, 286-FD-37, 432-APA-41 Pellegrino, S., 206-SCS-2, 258-SCS-3, 413-SCS-6, Pinto, J., 54-UMS-1 Okuizumi, N., 309-SCS-4 Pack, S., 457-PC-18 Park, M., 12-APA-3, 174-APA-17, 184-FD-26/APA-21 460-SCS-7 Piponniau, S., 9-AMT-1, 19-FD-6 Okutsu, M., 46-SEO-1, 337-EDU-1 Pack Melton, L., 387-FD-49 Park, S., 89-MST-3, 187-GNC-17, 251-MST-6, Pelletier, D., 285-FD-36, 340-FD-44, 404-MDO-8 Pisano, A., 377-AMT-8 Ol, M., 63-APA-6/FD-7, 280-APA-30, 287-FD-38 Padilha, B., 279-APA-29 346-GNC-31, 355-MST-11 Peltier, S., 340-FD-44 Pitt, D., 66-APA-9, 415-SD-13, 438-DSC-6 Oldani, A., 94-PC-5 Padron, A., 147-NDA-2 Parker, R., 53-TP-2, 119-APA-11 Pena, D., 439-FD-54 Pittman, C., 199-MAT-6 Oliva, E., 312-SEN-2 Page, G., 349-GTE-12 Parker, W., 84-ISC-3 Peng, J., 118-AFM-5 Pitz, R., 93-PC-4, 256-PC-10 Olivari, M., 251-MST-6 Page, J., 82-GTE-3 Parsani, M., 229-APA-23/FD-27 Peng, T., 156-STR-4 Pizzella, M., 131-FD-19 Oliveira, A., 33-MAT-1 Paielli, R., 395-GNC-35 Parschau, C., 33-MAT-1 Peng, W., 357-NDA-6 Pizzo, M., 105-TP-4

Oliver, J., 153-SD-5 Pak, C., 260-SEN-1 Parsons, T., 162-WE-3 Penhallegon, W., 343-GNC-28 Plastinin, E., 204-PC-8 Oliver M, O., 227-AMT-5 Paku, H., 151-SATS-1 Parwana, H., 449-GNC-41 Penn, J., 252-MST-7 Plemmons, D., 9-AMT-1 Oliviu, S., 233-ASC-3 Palacios, F., 43-SD-1, 330-APA-32 Paryz, R., 137-GT-3 Peraire, J., 283-FD-34 Plesniak, M., 388-FD-50 Ollar, J., 88-MDO-2 Palacios, J., 272-AA-6 Parziale, N., 339-FD-43 Peral, E., 151-SATS-1 Plötner, K., 89-MST-3 Olles, J., 227-AMT-5 Palacios, R., 43-SD-1, 154-SD-6, 259-SD-7, 383-DSC-5 Pascarella, D., 89-MST-3 Peralta, A., 353-MAT-9 Plumley, R., 137-GT-3 Ollivier Gooch, C., 180-FD-22, 356-MVC-1 Palaszewski, B., 155-SRE-2 Paschalidis, N., 151-SATS-1, 205-SATS-2 Pereira, D., 415-SD-13 Poggie, J., 71-FD-11, 95-PDL-3, 241-FD-33 Olson, E., 170-ACD-3, 273-ACD-6 Palazotto, A., 43-SD-1, 102-STR-3, 157-STR-5, Paschereit, C., 73-FD-13, 127-FD-15, 213-WE-4, Pereira, J., 397-GT-8 Pogorelov, A., 130-FD-18 Ombrello, T., 41-PDL-1, 93-PC-4, 141-HSABP-2, 198-MAT-5, 316-SUR-2 246-GTE-8, 379-APA-38, 390-FD-52 Perez, B., 392-GNC-32 Poinot, M., 407-MVC-2 204-PC-8, 257-PDL-7 Paley, D., 293-GNC-27 Pasiliao, C., 102-STR-3, 167-AA-4, 282-DSC-3, Perez, R., 90-NDA-1, 253-NDA-4 Poirel, D., 332-APA-34 Omidshafiei, S., 297-IS-7 Paliwoda, M., 42-PDL-2 287-FD-38, 332-APA-34, 433-APA-42 Perez-Arancibia, N., 7-AFM-1 Polagye, B., 14-FD-1/APA-5 Ono, D., 377-AMT-8 Palla, A., 41-PDL-1 Pass, J., 401-SAT-1 Perez Rocha, A., 189-GNC-19 Polanka, M., 28-HSABP-1, 168-ABPSI-4, 192-GTE-6, Onural, D., 212-UMS-4 Palm, T., 315-STR-11 Patallo, E., 384-EDU-2 Péron, S., 439-FD-54 193-GTE-7, 294-GTE-10, 296-HSABP-5, 451-GTE-15 Oostdyk, R., 453-IS-13 Palma, R., 299-MDO-6 Pate, D., 17-FD-4 Perrotta, G., 442-FD-57 Pollini, L., 251-MST-6, 446-GNC-38 Opgenoord, M., 299-MDO-6 Palumbo, R., 89-MST-3 Patel, D., 315-STR-11 Persson, P., 17-FD-4, 370-WE-8 Polsky, S., 378-APA-37 Oppenheimer, M., 190-GNC-20, 394-GNC-34/ACD-12 Palwankar, M., 315-STR-11 Patil, G., 101-SOF-3 Pervan, B., 466-UMS-11 Poncet-Montanges, A., 336-DSC-4 Ordoukhanian, E., 99-SE-2 Pan, D., 198-MAT-5 Patil, M., 249-MAT-7, 250-MDO-5, 259-SD-7, Peter, J., 90-NDA-1, 277-APA-27, 407-MVC-2 Ponder, J., 347-GT-7 Orhan, E., 430-AFM-15 Pan, K., 40-PC-2, 224-ACD-5 429-AFM-14 Peterson, D., 141-HSABP-2, 239-FD-31, 402-HSABP-7 Ponnurangam, C., 371-WE-9 Orkwis, P., 71-FD-11, 439-FD-54 Panda, K., 283-FD-34 Patrick, R., 37-MST-2 Peterson, J., 393-GNC-33 Ponnusamy, S., 406-MST-13 Orphee, C., 21-GNC-2 Pandare, A., 283-FD-34 Patterson, A., 78-GNC-8 Peterson, M., 206-SCS-2 Ponomarev, A., 204-PC-8 Orr, M., 224-ACD-5 Pandey, A., 431-AMT-9 Patterson, M., 169-ACD-2 Peterson, W., 157-STR-5 Pool, D., 20-GNC-1, 302-MST-10 Ortiz, R., 353-MAT-9 Pandiya, N., 351-HSABP-6 Patton, C., 360-PC-15, 411-PC-17 Petit, X., 410-PC-16 Poole, D., 121-APA-13, 279-APA-29, 330-APA-32 Ortiz Gómez, N., 135-GNC-14 Pandya, M., 184-FD-26/APA-21 Paul, L., 340-FD-44 Petrilli, J., 226-AFM-8, 301-MST-9 Pope, A., 312-SEN-2 Oruc, I., 454-MST-14 Panerai, F., 317-TP-8 Paul, M., 174-APA-17 Pfifer, H., 375-AFM-12 Pope, K., 105-TP-4, 464-TP-11 Oshima, R., 329-AMT-7 Panesi, M., 104-TP-3, 369-TP-9 Paulsen, G., 48-SRE-1 Pfitzner, M., 359-PC-14 Popescu, A., 315-STR-11 Oskay, C., 208-STR-6 Pang, Z., 414-SD-12 Pavlov, L., 314-STR-10 Pham, S., 71-FD-11 Popov, A., 233-ASC-3 Osman, A., 455-MST-15 Paniagua, G., 27-GTE-2, 82-GTE-3, 192-GTE-6, 193-GTE-7 Pavone, M., 291-GNC-25 Phan, A., 266-UMS-6 Popov, N., 257-PDL-7, 361-PDL-10 Ossmann, D., 243-GNC-22 Pankonien, A., 335-ASC-5 Pavuluri, S., 151-SATS-1, 308-SATS-3 Phan, C., 315-STR-11 Popov, P., 94-PC-5, 410-PC-16 Osterberg, N., 31-ISC-2 Panourgias, K., 284-FD-35 Phan, N., 344-GNC-29, 353-MAT-9, 368-STR-13 Popova, M., 446-GNC-38 Author/Session Chair Index Poquet, T., 170-ACD-3 Qidwai, S., 239-FD-31 Rampurawala, A., 311-SD-9 Rendall, T., 121-APA-13, 279-APA-29, 311-SD-9, Robbins, D., 156-STR-4 Porter, R., 9-AMT-1 Qin, C., 268-WE-6 Ramsey, J., 231-APA-25 330-APA-32 Roberts, D., 67-APA-10 Post, D., 122-APA-14 Qin, N., 64-APA-7, 121-APA-13, 439-FD-54 Ranade, P., 240-FD-32 Rennie, M., 245-GT-5 Roberts, R., 145-MDO-3 Post, M., 380-APA-39 Qin, T., 133-GNC-12 Ranatunga, V., 463-STR-17 Renze, K., 225-AFM-7 Roberts, S., 152-SCS-1 Potsdam, M., 122-APA-14 Qin, X., 100-SEO-2 Rangarajan, A., 455-MST-15 Resmini, A., 90-NDA-1 Roberts, W., 30-ISC-1, 192-GTE-6 Pourhashem, H., 5-AA-1 Qu, K., 239-FD-31 Ranjan, R., 458-PC-19 Resor, B., 318-WE-7 Robertson, C., 135-GNC-14 Pourshafiee, A., 312-SEN-2 Qu, Q., 17-FD-4, 183-FD-25, 378-APA-37, 380-APA-39 Rankin, B., 28-HSABP-1, 255-PC-9/GTE-9, 294-GTE-10, Retter, J., 42-PDL-2, 95-PDL-3 Robeson, M., 262-STR-8 Povitsky, A., 17-FD-4 Quest, J., 25-GT-1, 81-GT-2, 137-GT-3 306-PC-13, 351-HSABP-6, 411-PC-17 Reu, P., 10-AMT-10/SD-15 Robinson, J., 415-SD-13 Powell, D., 298-MAT-8 Quevedo, S., 262-STR-8 Ransom, D., 147-NDA-2 Reuter, C., 94-PC-5, 256-PC-10 Robinson, S., 380-APA-39 Powell, O., 141-HSABP-2 Quimby, D., 103-TES-3 Ransom, J., 87-MAT-3, 144-MAT-4 Reuter, R., 145-MDO-3, 200-MDO-4 Roca, X., 283-FD-34 Power, G., 407-MVC-2 Quinlan, J., 49-STR-1 Ranuzzi, G., 457-PC-18 Rexroat, J., 465-TP-12 Rockwell, R., 93-PC-4, 141-HSABP-2, 377-AMT-8 Powers, R., 5-AA-1, 167-AA-4 Quinn, M., 12-APA-3, 67-APA-10, 280-APA-30 Rao, A., 196-IS-5, 453-IS-13 Reyes, M., 364-SD-10 Rockwood, M., 444-FD-59 Prabakar, M., 13-APA-4, 227-AMT-5 Quix, H., 137-GT-3, 397-GT-8 Rapski, J., 275-AFM-9 Reynolds, T., 329-AMT-7 Rodi, P., 194-HSABP-3 Prabhakar, N., 190-GNC-20 Quon, E., 379-APA-38 Rashid, A., 401-SAT-1 Rhew, R., 347-GT-7 Rodriguez, S., 422-WE-11 Prabhakar, P., 262-STR-8 Radespiel, R., 66-APA-9, 232-APA-26, 339-FD-43, Rasmussen, C., 312-SEN-2 Ribert, G., 93-PC-4, 410-PC-16 Rodriguez y Martin, M., 22-GNC-3 Prabhu, D., 61-AFM-4, 211-TP-6, 317-TP-8 389-FD-51, 391-FD-53 Rassaian, M., 417-STR-14, 463-STR-17 Ricci, J., 48-SRE-1 Roe, P., 180-FD-22 Prach, A., 292-GNC-26 Radestock, M., 281-ASC-4 Ratheesh, A., 205-SATS-2, 308-SATS-3 Ricci, S., 281-ASC-4, 311-SD-9 Roentsch, B., 387-FD-49 Prakash, N., 199-MAT-6 Radhakrishnan, K., 305-PC-12 Rathinam, S., 365-SEN-3 Ricciardi, J., 302-MST-10 Roeting, W., 124-CMS-1/CPS-1 Prasad, R., 250-MDO-5 Raffius, T., 441-FD-56 Ratnoo, A., 136-GNC-15, 448-GNC-40 Riccobene, L., 281-ASC-4 Roger, M., 15-FD-2 Prats, X., 345-GNC-30/ACD-10 Rafi, M., 345-GNC-30/ACD-10, 346-GNC-31 Rattan, K., 47-SOF-1 Rich, J., 459-PDL-13 Rogers, J., 76-GNC-6, 118-AFM-5, 344-GNC-29, Pratt, A., 399-GTE-14 Rafter, M., 124-CMS-1/CPS-1 Rauleder, J., 176-APA-20, 381-APA-40 Richard, L., 315-STR-11 448-GNC-40 Pratt, D., 300-MST-8 Ragab, S., 259-SD-7 Rausch, R., 119-APA-11 Richards, N., 188-GNC-18 Rogers, M., 229-APA-23/FD-27 Prause, J., 130-FD-18 Rageb, A., 103-TES-3 Raveh, D., 311-SD-9, 383-DSC-5 Richardson, D., 255-PC-9/GTE-9 Rogers, S., 173-APA-16 Prazenica, R., 106-UMS-2, 189-GNC-19, 190-GNC-20, Raghavan, S., 298-MAT-8, 364-SD-10 Ravindra, K., 337-EDU-1 Richardson, T., 171-AFM-6, 293-GNC-27, 327-AFM-10 Roget, B., 122-APA-14, 228-APA-22, 338-FD-42

420-UMS-10 Ragheb, A., 231-APA-25 Ravine, J., 33-MAT-1 Richer, T., 244-GNC-23, 327-AFM-10 Rohrschneider, R., 446-GNC-38 Price, H., 46-SEO-1 Ragni, D., 221-AA-5, 267-WE-5, 459-PDL-13 Raymer, D., 273-ACD-6, 275-AFM-9 Richter, K., 231-APA-25 Roidl, B., 239-FD-31 Price, N., 202-NDA-3 Raheja, A., 24-GNC-5 Raza, S., 293-GNC-27 Rickey, M., 329-AMT-7 Rojas, J., 54-UMS-1 Priess, S., 392-GNC-32 Rahman, M., 341-FD-45 Reasor, D., 228-APA-22 Rico, J., 201-MST-5 Rojo, R., 221-AA-5 Prigent, S., 183-FD-25 Rahmat-Samii, Y., 151-SATS-1 Redifer, M., 185-GEPC-3 Riddick, J., 310-SD-8 Rokhsaz, K., 311-SD-9 Princen, N., 6-ABPSI-1/GEPC-1, 59-ABPSI-2/GEPC-2 Rahn, C., 310-SD-8 Reed, D., 119-APA-11 Riddick, S., 188-GNC-18 Rolling, A., 117-ACD-1 Prinzel, L., 312-SEN-2 Rai, M., 72-FD-12 Reed, H., 128-FD-16, 182-FD-24, 308-SATS-3, Riedel, U., 39-PC-1 Roman, D., 6-ABPSI-1/GEPC-1, 59-ABPSI-2/GEPC-2 Priolo, F., 429-AFM-14 Rais-Rohani, M., 147-NDA-2, 299-MDO-6 321-FD-60, 376-AFM-13 Rife, J., 101-SOF-3 Romano, M., 187-GNC-17 Pritchard, J., 378-APA-37 Raj, P., 223-ACD-4, 273-ACD-6, 282-DSC-3 Reed, J., 133-GNC-12, 242-GNC-21, 290-GNC-24 Rigby, K., 420-UMS-10 Romanyszyn, A., 363-SCS-5 Pritchett, A., 22-GNC-3, 301-MST-9 Raja, L., 459-PDL-13 Reed, S., 117-ACD-1 Riggins, B., 170-ACD-3 Romero, J., 388-FD-50 Pröbsting, S., 221-AA-5 Rajasegar, R., 41-PDL-1 Reed, W., 223-ACD-4 Riley, J., 386-FD-48 Romero, S., 70-FD-9 Prosser, D., 455-MST-15 Rajendran, L., 257-PDL-7, 431-AMT-9 Reeger, J., 160-UMS-3 Riley, L., 402-HSABP-7 Romero, V., 90-NDA-1 Proulx, R., 186-GNC-16 Rajmohan, N., 405-MST-12 Regan, C., 375-AFM-12 Riley, Z., 234-DSC-1 Romero Martín, J., 135-GNC-14 Pruett, B., 172-AMT-4 Rajput, P., 64-APA-7 Rege, A., 230-APA-24 Rimoli, J., 264-SUR-1, 316-SUR-2 Roozeboom, N., 333-APA-35/FD-41, 431-AMT-9 Pryor, O., 39-PC-1 Raju, I., 49-STR-1, 263-STR-9 Reich, G., 249-MAT-7, 281-ASC-4, 329-AMT-7, Ringertz, U., 438-DSC-6 Roper, R., 343-GNC-28 Przekop, A., 462-STR-16 Raju, N., 227-AMT-5 335-ASC-5, 414-SD-12 Ringuette, M., 63-APA-6/FD-7 Roquemore, W., 39-PC-1, 94-PC-5 Pulliam, T., 18-FD-5, 176-APA-20, 333-APA-35/FD-41 Ramakrishnan, R., 82-GTE-3 Reichl, K., 310-SD-8 Rinoie, K., 224-ACD-5 Rorie, R., 212-UMS-4 Pumroy, D., 84-ISC-3 Ramamurthy, A., 178-DE-2 Reichman, B., 399-GTE-14 Rios, J., 312-SEN-2 Rose, D., 125-DE-1 Purkey, A., 131-FD-19 Raman, G., 221-AA-5 Reid, B., 206-SCS-2 Ritter, M., 364-SD-10, 383-DSC-5 Rosema, C., 13-APA-4, 334-APA-36 Putambekar, P., 205-SATS-2 Raman, V., 94-PC-5, 222-ABPSI-5, 294-GTE-10, Reikher, A., 210-TES-5 Ritter, S., 168-ABPSI-4 Rosenthal, J., 308-SATS-3 Puterbaugh, S., 82-GTE-3 451-GTE-15, 457-PC-18 Rein, K., 255-PC-9/GTE-9 Ritterbush, M., 201-MST-5 Ross, A., 43-SD-1 Putheenveed, S., 340-FD-44 Ramanujam, G., 161-WE-2 Rein, M., 174-APA-17 Ritz, S., 37-MST-2 Ross, B., 363-SCS-5 Putnam, D., 77-GNC-7 Ramasawmy, D., 337-EDU-1 Reinholtz, C., 420-UMS-10 Rivey, J., 144-MAT-4 Ross, I., 186-GNC-16 Putnam, Z., 8-AFM-2, 61-AFM-4, 430-AFM-15 Ramcke, T., 359-PC-14 Reis, R., 247-HIS-2, 337-EDU-1 Rizo-Patron, S., 414-SD-12 Ross, J., 431-AMT-9 Pyne, K., 84-ISC-3 Rame, E., 464-TP-11 Remark, B., 317-TP-8 Rizvi, F., 146-MST-4 Ross, M., 43-SD-1 Pytel, D., 52-TES-2/TP-1 Ramesh, K., 14-FD-1/APA-5 Remotigue, M., 356-MVC-1 Rizzetta, D., 69-FD-8, 389-FD-51 Ross, R., 382-ASC-6 Qi, J., 37-MST-2 Ramezani, A., 291-GNC-25 Ren, J., 88-MDO-2, 182-FD-24, 330-APA-32 Rizzi, A., 174-APA-17, 277-APA-27 Rossetti, J., 407-MVC-2 Qian, D., 422-WE-11 Ramos García, N., 370-WE-8 Ren, X., 157-STR-5 Rizzi, F., 48-SRE-1 Rossi, A., 7-AFM-1 Author/Session Chair Index Rossman, G., 317-TP-8 Sadeghirad, A., 157-STR-5 Santer, M., 206-SCS-2, 279-APA-29, 332-APA-34, Schinwald, C., 89-MST-3 Scott, R., 438-DSC-6 Rotea, M., 371-WE-9, 422-WE-11, 467-WE-12 Saeed, T., 441-FD-56 433-APA-42 Schmidt, B., 128-FD-16 Scott-Emuakpor, O., 87-MAT-3, 144-MAT-4, 157-STR-5, Rothlsiberger, C., 224-ACD-5 Saeki, N., 242-GNC-21 Santiago, F., 260-SEN-1 Schmidt, D., 375-AFM-12, 447-GNC-39 198-MAT-5, 202-NDA-3 Roughen, K., 415-SD-13 Safdar, U., 26-GTE-1 Santos, P., 68-ASC-1 Schmidt, H., 127-FD-15 Seaford, M., 119-APA-11 Rouhi Youssefi, M., 74-FD-14 Safdari, M., 249-MAT-7 Sanyal, A., 77-GNC-7 Schmidt, M., 274-ACD-7 Seager, C., 440-FD-55 Rouse, M., 462-STR-16 Sagliano, M., 186-GNC-16, 449-GNC-41 Sanz-Douglass, G., 418-STR-15 Schmidt, S., 48-SRE-1 Sears, D., 211-TP-6 Rouser, K., 84-ISC-3 Saha, D., 76-GNC-6 Saracino, D., 355-MST-11 Schmieder, W., 464-TP-11 Secheli, G., 258-SCS-3 Roush, T., 48-SRE-1 Sahawneh, L., 420-UMS-10 Saracoglu, B., 82-GTE-3, 192-GTE-6, 193-GTE-7, Schminder, J., 37-MST-2 Seckin, S., 19-FD-6 Rousseau, C., 208-STR-6, 262-STR-8 Sahin, M., 68-ASC-1 248-HSABP-4, 349-GTE-12 Schmisseur, J., 465-TP-12 Sedky, G., 377-AMT-8 Rousso, A., 204-PC-8 Sahni, O., 72-FD-12, 236-FD-28 Saraf, A., 430-AFM-15 Schmit, R., 443-FD-58 Seers, P., 73-FD-13 Rovey, J., 41-PDL-1, 42-PDL-2, 151-SATS-1, Sahu, J., 432-APA-41 Saranathan, H., 8-AFM-2 Schmitt, L., 393-GNC-33 Seidel, G., 34-MAT-2, 87-MAT-3, 199-MAT-6, 249-MAT-7 181-FD-23/PDL-6 Said, A., 103-TES-3 Sardeshmukh, S., 360-PC-15, 411-PC-17 Schmitt, R., 318-WE-7 Seidel, J., 69-FD-8, 334-APA-36, 348-GTE-11 Rowley, C., 237-FD-29, 299-MDO-6, 442-FD-57 Saijo, M., 128-FD-16 Sarhaddi, D., 414-SD-12 Schmitz, S., 161-WE-2 Seifert, A., 123-APA-15 Roy, A., 177-ASC-2, 192-GTE-6 Saiki, H., 106-UMS-2 Saric, W., 376-AFM-13 Schneider, D., 259-SD-7 Seifert, D., 249-MAT-7 Roy, C., 180-FD-22 Saini, P., 92-PC-3 Sarigulklijn, M., 325-ACD-8 Schneider, G., 318-WE-7, 390-FD-52, 458-PC-19 Seiler, P., 134-GNC-13, 375-AFM-12, 467-WE-12 Roy, S., 33-MAT-1, 95-PDL-3, 255-PC-9/GTE-9, Saito, T., 377-AMT-8 Sarigul-Klijn, N., 60-AFM-3, 325-ACD-8 Schneider, S., 75-FD-20, 224-ACD-5 Seitz, A., 168-ABPSI-4 257-PDL-7, 354-MDO-7, 412-PDL-12 Saito, Y., 102-STR-3 Sarkar, P., 370-WE-8, 422-WE-11 Schneider, T., 207-SE-3 Sekimoto, S., 181-FD-23/PDL-6 Royalty, C., 221-AA-5, 272-AA-6 Sakai, S., 133-GNC-12 Sartor, P., 336-DSC-4 Schneider, W., 461-SD-14 Sekula, M., 119-APA-11, 245-GT-5, 397-GT-8, Roychoudhury, I., 453-IS-13 Sakai, T., 53-TP-2 Sasaki, T., 21-GNC-2 Schneiders, J., 31-ISC-2, 227-AMT-5 454-MST-14 Roza, M., 251-MST-6 Sakamoto, H., 152-SCS-1, 258-SCS-3, 309-SCS-4, Sasiadek, J., 189-GNC-19 Schnell, R., 25-GT-1, 81-GT-2 Sekulic, D., 419-TP-10 Rozov, V., 72-FD-12 460-SCS-7 Sasidharan Nair, U., 5-AA-1, 238-FD-30 Schoegl, I., 377-AMT-8, 419-TP-10 Selig, M., 176-APA-20, 231-APA-25, 309-SCS-4 Rucco, A., 190-GNC-20 Sakamoto, N., 309-SCS-4 Sasoh, A., 71-FD-11 Scholz, P., 12-APA-3, 389-FD-51, 391-FD-53 Selim, O., 210-TES-5 Ruch, H., 31-ISC-2 Sakaue, H., 431-AMT-9 Sassanis, V., 115-AA-3 Schönherr, T., 459-PDL-13 Selimov, A., 298-MAT-8 Rudenko, A., 281-ASC-4 Sako, B., 118-AFM-5 Sathyan, A., 297-IS-7 Schönweitz, D., 25-GT-1, 81-GT-2 Sell, B., 255-PC-9/GTE-9

Rudenko, N., 379-APA-38 Sakovsky, M., 206-SCS-2 Sato, M., 20-GNC-1, 29-IS-1/ICC-1/DA-1, 377-AMT-8 Schottler, J., 318-WE-7 Sellers, D., 308-SATS-3 Rudnik, R., 12-APA-3 Saleem, A., 448-GNC-40 Satoh, Y., 258-SCS-3 Schrage, D., 454-MST-14 Sellers, M., 245-GT-5 Ruehl, K., 422-WE-11 Saleem, M., 19-FD-6 Satou, Y., 460-SCS-7 Schranner, F., 72-FD-12 Sellers, W., 450-GT-9 Ruess, M., 418-STR-15 Salehian, S., 167-AA-4 Sattelmayer, T., 246-GTE-8, 451-GTE-15, 458-PC-19 Schreck, S., 161-WE-2, 213-WE-4 Sells, H., 76-GNC-6 Ruetten, M., 279-APA-29 Salvoldi, M., 446-GNC-38 Sauder, J., 151-SATS-1, 206-SCS-2, 460-SCS-7 Schreiber, J., 371-WE-9 Selvarathinam, A., 262-STR-8 Ruf, J., 221-AA-5 Samaratunga, D., 382-ASC-6 Saunders, D., 211-TP-6 Schreyer, A., 9-AMT-1, 339-FD-43 Sengezer, E., 87-MAT-3 Rufer, S., 75-FD-20 Samareh, J., 46-SEO-1 Saussié, D., 76-GNC-6 Schröder, K., 418-STR-15 Sengupta, S., 238-FD-30 Ruff, K., 27-GTE-2 Samborsky, D., 162-WE-3 Savill, A., 121-APA-13 Schroeder, A., 25-GT-1, 81-GT-2 Senne, J., 363-SCS-5 Ruff, R., 300-MST-8 Samiei, E., 77-GNC-7 Savin, E., 90-NDA-1 Schroeder, J., 36-MST-1, 301-MST-9 Senocak, I., 72-FD-12, 129-FD-17 Rufino, G., 312-SEN-2 Samimy, M., 181-FD-23/PDL-6, 238-FD-30, Savoia, M., 48-SRE-1 Schroeder, K., 46-SEO-1 Senoguchi, A., 36-MST-1 Ruleva, L., 67-APA-10 276-AMT-6/PC-11/PDL-8 Sawada, H., 329-AMT-7 Schroeder, W., 129-FD-17, 130-FD-18, 239-FD-31 Sensmeier, M., 102-STR-3 Rumizen, M., 39-PC-1 Samir, K., 289-GEPC-4 Sawada, K., 241-FD-33, 283-FD-34, 284-FD-35, Schroll, M., 25-GT-1 Seo, Y., 24-GNC-5 Rumpfkeil, M., 64-APA-7, 253-NDA-4 Samper, T., 399-GTE-14 286-FD-37 Schuet, S., 437-DA-2 Serpelloni, E., 77-GNC-7 Rumsey, C., 184-FD-26/APA-21, 333-APA-35/FD-41 Samuel, A., 66-APA-9 Sawaki, Y., 283-FD-34 Schuh, M., 6-ABPSI-1/GEPC-1, 59-ABPSI-2/GEPC-2 Serrano Galiano, S., 183-FD-25 Runco, C., 266-UMS-6 Sanchez, A., 93-PC-4 Sawant, S., 104-TP-3 Schultz, M., 368-STR-13 Sertse, H., 156-STR-4, 198-MAT-5 Runyon, B., 144-MAT-4 Sanchez, R., 43-SD-1 Scarano, F., 31-ISC-2, 227-AMT-5 Schultz, V., 212-UMS-4, 420-UMS-10 Sescu, A., 115-AA-3, 167-AA-4, 240-FD-32 Rupp, C., 363-SCS-5 Sandberg, R., 183-FD-25, 287-FD-38 Scarborough, D., 93-PC-4 Schulze, M., 458-PC-19 Seshadri, B., 382-ASC-6 Rusak, Z., 286-FD-37, 390-FD-52 Saneholtz, N., 275-AFM-9 Schanz, D., 25-GT-1 Schulze, P., 251-MST-6, 429-AFM-14 Seufert, S., 46-SEO-1, 337-EDU-1 Ruscher, C., 115-AA-3, 348-GTE-11, 398-GTE-13 Sanetrik, M., 282-DSC-3 Scharnhorst, R., 131-FD-19 Schuster, M., 162-WE-3 Severance, K., 437-DA-2 Russell, G., 145-MDO-3 Sanfelice, R., 447-GNC-39 Schatz, S., 76-GNC-6 Schwartzentruber, T., 104-TP-3, 369-TP-9 Seweryn, K., 135-GNC-14, 189-GNC-19 Russell, S., 209-STR-7, 263-STR-9, 418-STR-15 Sangid, M., 87-MAT-3, 249-MAT-7, 409-MAT-10 Schauer, F., 27-GTE-2, 28-HSABP-1, 93-PC-4, 192-GTE-6, Schweizer, L., 363-SCS-5 Sexton, B., 415-SD-13 Russi, S., 247-HIS-2 Sankar, L., 65-APA-8 255-PC-9/GTE-9, 296-HSABP-5, 351-HSABP-6 Schwenke, D., 104-TP-3 Sexton, M., 6-ABPSI-1/GEPC-1, 59-ABPSI-2/GEPC-2 Rust, W., 418-STR-15 Sankaran, R., 411-PC-17 Schauerhamer, D., 380-APA-39 Schwetzler, D., 12-APA-3 Sezer, E., 252-MST-7 Rutledge, J., 193-GTE-7, 457-PC-18 Sankaran, V., 18-FD-5, 305-PC-12, 360-PC-15, Schenk, M., 258-SCS-3 Schwille, J., 464-TP-11 Shaat, M., 198-MAT-5, 199-MAT-6 Rybalko, M., 116-ABPSI-3 410-PC-16, 411-PC-17 Schetz, J., 50-STR-2, 170-ACD-3 Sciacchitano, A., 227-AMT-5 Shafer, T., 228-APA-22 Rybus, T., 189-GNC-19 Sankararaman, S., 253-NDA-4, 303-NDA-5, 453-IS-13 Scheuermann, E., 244-GNC-23 Scigliano, R., 367-STR-12, 405-MST-12 Shah, G., 301-MST-9 Ryle, S., 450-GT-9 Santana, C., 327-AFM-10 Schilling, T., 289-GEPC-4 Scime, E., 308-SATS-3 Shah, J., 29-IS-1/ICC-1/DA-1, 352-IS-9 Sabo, C., 83-IS-2 Santangelo, A., 124-CMS-1/CPS-1, 205-SATS-2 Schinetsky, P., 172-AMT-4 Sclafani, A., 66-APA-9, 121-APA-13 Shahbaz, M., 175-APA-18 Author/Session Chair Index Shahid, Z., 401-SAT-1 Shipman, J., 454-MST-14 Singh, J., 298-MAT-8, 430-AFM-15 Smith, S., 154-SD-6, 422-WE-11, 465-TP-12 Spiegel, S., 229-APA-23/FD-27 Shaler, K., 318-WE-7 Shirasawa, Y., 258-SCS-3 Singh, K., 44-SD-2, 154-SD-6 Smith, T., 248-HSABP-4 Spike, C., 237-FD-29 Shamsaei, Y., 458-PC-19 Shish, K., 437-DA-2 Singh, L., 190-GNC-20 Smyers, B., 329-AMT-7 Spillers, R., 10-AMT-10/SD-15, 172-AMT-4, 241-FD-33, Shan, J., 46-SEO-1, 146-MST-4, 355-MST-11 Shishkov, O., 441-FD-56 Singh, M., 213-WE-4 Snow, C., 432-APA-41 286-FD-37, 443-FD-58 Shan, X., 232-APA-26 Shivakumar, K., 199-MAT-6 Singh, R., 381-APA-40 Snyder, K., 23-GNC-4 Spink, J., 413-SCS-6 Shang, H., 100-SEO-2 Shively, J., 212-UMS-4 Singh, S., 193-GTE-7, 394-GNC-34/ACD-12 Snyder, M., 12-APA-3 Spirkovska, L., 453-IS-13 Shankar, U., 133-GNC-12, 242-GNC-21, 290-GNC-24 Shneider, M., 96-PDL-4, 361-PDL-10 Singha, A., 308-SATS-3 Snyder, P., 340-FD-44 Spirlet, G., 68-ASC-1 Shanor, R., 23-GNC-4 Shoda, T., 71-FD-11 Singhal, A., 181-FD-23/PDL-6 Snyder, R., 145-MDO-3 Spirnak, J., 432-APA-41 Shao, A., 207-SE-3 Short, E., 105-TP-4 Sinha, A., 415-SD-13 Snyder, S., 78-GNC-8 Spivey, N., 98-SD-4 Shao, Z., 290-GNC-24 Short, S., 247-HIS-2 Sinha, M., 225-AFM-7 Sobester, A., 194-HSABP-3, 297-IS-7 Spoor, M., 16-FD-3 Sharf, I., 80-GNC-10, 244-GNC-23 Shouse, D., 94-PC-5 Sinke, J., 34-MAT-2 Sodano, H., 298-MAT-8 Spotts, N., 130-FD-18 Shariff, K., 232-APA-26 Shrestha, E., 31-ISC-2 Sinsay, J., 88-MDO-2 Söderberg, R., 253-NDA-4 Sprague, M., 162-WE-3 Sharma, A., 167-AA-4, 268-WE-6 Shrivastava, P., 205-SATS-2 Siochi, E., 185-GEPC-3 Sodja, J., 68-ASC-1, 98-SD-4, 102-STR-3 Spring, J., 48-SRE-1 Sharma, B., 87-MAT-3 Shukla, H., 429-AFM-14 Sippel, T., 149-PC-6 Sofronsky, S., 87-MAT-3 Springer, R., 194-HSABP-3 Sharma, N., 54-UMS-1 Shula, B., 353-MAT-9 Sirignano, W., 94-PC-5, 340-FD-44, 410-PC-16 Soken, H., 133-GNC-12 Squire, T., 317-TP-8 Sharma, R., 136-GNC-15, 365-SEN-3 Shurupov, M., 361-PDL-10 Sirohi, J., 381-APA-40, 414-SD-12 Solodovnikov, S., 67-APA-10 Sreeja, S., 449-GNC-41 Shawky Mohamedy, A., 300-MST-8 Shuvo, M., 262-STR-8 Sisemore, C., 98-SD-4 Soltmann, L., 12-APA-3 Sreenivas, K., 82-GTE-3, 161-WE-2, 467-WE-12 Shcherbanev, S., 361-PDL-10 Shweyk, K., 275-AFM-9 Sisler, A., 192-GTE-6 Somavarapu, D., 404-MDO-8 Sridhar, B., 89-MST-3 Shea, P., 6-ABPSI-1/GEPC-1, 222-ABPSI-5, 348-GTE-11 Si, J., 283-FD-34 Sitaraman, H., 459-PDL-13 Son, M., 305-PC-12 Sridhar, M., 98-SD-4 Sheaf, C., 168-ABPSI-4 Siala, F., 179-FD-21 Sitaraman, J., 18-FD-5, 122-APA-14, 228-APA-22, Son, O., 63-APA-6/FD-7 Srinivasan, T., 420-UMS-10, 466-UMS-11 Shelley, E., 84-ISC-3 Siddle-Mitchell, S., 227-AMT-5 338-FD-42, 421-WE-10, 439-FD-54 Sondergaard, R., 26-GTE-1, 70-FD-9, 444-FD-59 St. George, A., 28-HSABP-1, 296-HSABP-5, Shelton, A., 97-SD-3, 282-DSC-3 Sideris, A., 410-PC-16 Sivaneri, V., 395-GNC-35 Song, H., 259-SD-7 351-HSABP-6 Shen, H., 157-STR-5, 435-APA-44 Sidey, J., 359-PC-14 Sivasubramanian, B., 340-FD-44 Song, P., 383-DSC-5 Stäblein, A., 213-WE-4 Shen, W., 161-WE-2 Sidor, A., 465-TP-12 Sivasubramanian, J., 131-FD-19, 182-FD-24 Song, S., 83-IS-2, 205-SATS-2 Stachowiak, S., 79-GNC-9

Shen, X., 464-TP-11 Sidwell, T., 192-GTE-6 Skelton, R., 394-GNC-34/ACD-12 Song, W., 175-APA-18, 330-APA-32, 411-PC-17, Stack, C., 440-FD-55 Shen, Y., 120-APA-12 Siefers, T., 379-APA-38 Skentzos, P., 124-CMS-1/CPS-1, 205-SATS-2 436-APA-45 Stackpoole, M., 298-MAT-8, 317-TP-8 Sheng, C., 65-APA-8 Sienz, J., 88-MDO-2 Skiba, A., 306-PC-13 Song, Y., 153-SD-5 Stadlmair, N., 246-GTE-8 Shenogin, S., 177-ASC-2 Sievers, M., 99-SE-2 Skinner, S., 35-MDO-1 Song, Z., 290-GNC-24 Stalnov, O., 337-EDU-1, 383-DSC-5 Shepard, J., 192-GTE-6 Sigthorsson, D., 190-GNC-20 Sklyanski, E., 46-SEO-1 Sorgenfrei, M., 76-GNC-6, 205-SATS-2 Stanfield, S., 431-AMT-9 Shepherd, J., 128-FD-16 Siikonen, T., 341-FD-45 Slabaugh, C., 246-GTE-8, 399-GTE-14 Sosa, J., 193-GTE-7 Stanford, B., 88-MDO-2, 235-DSC-2, 314-STR-10 Sheplak, M., 53-TP-2, 144-MAT-4, 240-FD-32, Silk, E., 465-TP-12 Slane, J., 355-MST-11 Sostaric, R., 23-GNC-4 Stanford, L., 463-STR-17 431-AMT-9 Siller, H., 25-GT-1 Slater, J., 116-ABPSI-3 Sotak, M., 29-IS-1/ICC-1/DA-1, 195-ICC-2 Stankowski, T., 168-ABPSI-4 Sheppard, B., 315-STR-11 Silton, S., 67-APA-10 Slavinskaya, N., 39-PC-1 Soteriou, M., 305-PC-12 Stansbury, R., 160-UMS-3, 420-UMS-10, 466-UMS-11 Sherer, S., 13-APA-4, 439-FD-54 Silva, C., 33-MAT-1 Sledge, I., 403-IS-11 Sotoudeh, Z., 44-SD-2, 98-SD-4, 280-APA-30, Stanton, J., 92-PC-3 Sheth, K., 89-MST-3 Silva, R., 120-APA-12 Slipchenko, M., 9-AMT-1 461-SD-14 Stapel, J., 20-GNC-1 Sheth, R., 335-ASC-5 Silva, W., 54-UMS-1, 282-DSC-3, 438-DSC-6 Slostad, J., 413-SCS-6 Soueidan, A., 138-GTE-4 Starikovskaia, S., 257-PDL-7, 361-PDL-10 Shi, J., 189-GNC-19 Silver, M., 152-SCS-1, 206-SCS-2 Slotnick, J., 120-APA-12 Soulaïmani, A., 180-FD-22 Starikovskiy, A., 41-PDL-1, 95-PDL-3, 96-PDL-4, Shi, K., 71-FD-11, 82-GTE-3 Sim, J., 233-ASC-3, 305-PC-12 Smaisim, G., 103-TES-3 Sousa, J., 190-GNC-20, 247-HIS-2 204-PC-8 Shi, L., 175-APA-18, 330-APA-32, 341-FD-45, 388-FD-50 Simao Ferreira, C., 161-WE-2, 267-WE-5, 370-WE-8 Smarslok, B., 90-NDA-1, 202-NDA-3, 253-NDA-4, Southward, S., 302-MST-10 Starin, S., 243-GNC-22, 344-GNC-29 Shi, X., 291-GNC-25 Simeone, S., 311-SD-9 303-NDA-5 Soykasap, O., 309-SCS-4, 460-SCS-7 Starke, J., 39-PC-1 Shibuya, K., 100-SEO-2 Simic, M., 325-ACD-8 Smeets, B., 314-STR-10 Soysal, S., 325-ACD-8 Starkey, R., 116-ABPSI-3 Shigeta, A., 155-SRE-2 Simmons, S., 245-GT-5 Smeur, E., 293-GNC-27 Spada, C., 170-ACD-3 Starr, B., 171-AFM-6 Shih, C., 221-AA-5 Simon, N., 157-STR-5, 315-STR-11 Smith, A., 376-AFM-13 Spakovszky, Z., 464-TP-11 Starr, M., 43-SD-1 Shih, T., 452-GTE-16 Simonian, S., 314-STR-10 Smith, B., 130-FD-18 Sparkman, D., 303-NDA-5 Starr, R., 228-APA-22 Shila, J., 451-GTE-15 Simpson, A., 83-IS-2 Smith, C., 62-AMT-2, 340-FD-44 Speakman, N., 171-AFM-6 Stassen, H., 343-GNC-28, 392-GNC-32 Shimmin, K., 145-MDO-3 Simpson, R., 259-SD-7 Smith, D., 274-ACD-7, 444-FD-59, 447-GNC-39 Spedding, G., 174-APA-17 Statnikov, V., 239-FD-31 Shimoda, Y., 309-SCS-4 Simsek, I., 325-ACD-8 Smith, E., 9-AMT-1, 266-UMS-6, 310-SD-8 Spencer, G., 127-FD-15 Stechmann, D., 255-PC-9/GTE-9 Shimomura, T., 21-GNC-2 Simsek, M., 177-ASC-2 Smith, K., 124-CMS-1/CPS-1, 152-SCS-1 Spencer, J., 420-UMS-10 Steck, J., 345-GNC-30/ACD-10, 346-GNC-31 Shimoyama, K., 376-AFM-13 Simsek, O., 430-AFM-15 Smith, L., 94-PC-5, 174-APA-17, 178-DE-2, 274-ACD-7 Spencer, M., 33-MAT-1 Steeger, S., 68-ASC-1 Shin, D., 172-AMT-4, 399-GTE-14 Sinclair, A., 135-GNC-14 Smith, M., 65-APA-8, 245-GT-5, 339-FD-43, 455-MST-15 Sperry, J., 80-GNC-10, 434-APA-43 Steele, K., 363-SCS-5 Shin, S., 177-ASC-2, 196-IS-5, 233-ASC-3 Singh, A., 95-PDL-3 Smith, P., 397-GT-8 Speth, R., 167-AA-4 Steeves, J., 152-SCS-1, 206-SCS-2 Shinozaki, N., 103-TES-3 Singh, B., 257-PDL-7 Smith, R., 385-FD-47 Spetzler, M., 20-GNC-1 Steffens, M., 146-MST-4 Author/Session Chair Index Steijl, R., 17-FD-4 Su, L., 362-PDL-11 Swieringa, K., 392-GNC-32 Tani, K., 222-ABPSI-5 Thienel, J., 21-GNC-2, 187-GNC-17 Stein, I., 33-MAT-1 Su, W., 154-SD-6, 235-DSC-2, 414-SD-12, 438-DSC-6 Swiler, L., 90-NDA-1 Tani, Y., 231-APA-25 Tholeti, S., 361-PDL-10 Stein, J., 382-ASC-6 Subbarao, K., 230-APA-24, 395-GNC-35 Syam, S., 359-PC-14 Tanno, H., 75-FD-20, 128-FD-16, 241-FD-33 Thomareis, N., 444-FD-59 Steinberg, A., 92-PC-3 Subbareddy, P., 126-FD-10 Sydney, A., 231-APA-25 Tao, T., 325-ACD-8, 374-ACD-11 Thomas, E., 422-WE-11 Steiner, T., 343-GNC-28 Subramanian, T., 207-SE-3 Sydney, N., 293-GNC-27 Tartabini, P., 171-AFM-6 Thomas, G., 300-MST-8 Steinfeldt, B., 401-SAT-1 Suchomel, C., 376-AFM-13 Syed, A., 422-WE-11 Tartaglia, V., 187-GNC-17 Thomas, J., 184-FD-26/APA-21, 239-FD-31 Stelzer, D., 264-SUR-1 Suchyta, C., 74-FD-14 Syred, N., 103-TES-3, 246-GTE-8 Tartaruga, I., 336-DSC-4 Thomas, M., 299-MDO-6 Stepanyan, V., 188-GNC-18, 293-GNC-27 Sudalagunta, P., 282-DSC-3 Szlatenyi, C., 279-APA-29 Tatsukawa, T., 403-IS-11 Thomas, R., 185-GEPC-3, 272-AA-6, 327-AFM-10 Stephan, J., 395-GNC-35 Suder, K., 82-GTE-3, 138-GTE-4 Szmuk, M., 79-GNC-9 Taubert, L., 387-FD-49 Thomas, S., 106-UMS-2 Stephan, S., 339-FD-43 Suess, L., 317-TP-8 Tabandeh, M., 237-FD-29 Taur, D., 449-GNC-41 Thompson, K., 440-FD-55 Stephens, C., 312-SEN-2 Sugahara, M., 361-PDL-10 Tabata, A., 231-APA-25 Taurino, A., 42-PDL-2 Thomsen, B., 80-GNC-10 Stephens, J., 245-GT-5 Sugawara, H., 371-WE-9 Tadghighi, H., 122-APA-14 Tavakoli, S., 195-ICC-2 Thomson, M., 151-SATS-1, 460-SCS-7 Stephens, S., 134-GNC-13 Sugioka, Y., 431-AMT-9 Tagai, R., 120-APA-12, 242-GNC-21 Taylor, A., 298-MAT-8 Thorn, C., 26-GTE-1 Stern, E., 211-TP-6, 317-TP-8 Suh, P., 259-SD-7 Taguchi, M., 67-APA-10 Taylor, B., 375-AFM-12, 452-GTE-16 Thorsson, S., 463-STR-17 Stern, T., 363-SCS-5 Suhey, J., 414-SD-12 Taha, H., 7-AFM-1, 20-GNC-1, 190-GNC-20, Taylor, J., 401-SAT-1 Threadgill, J., 19-FD-6 Sternberg, D., 344-GNC-29 Suhir, E., 357-NDA-6 292-GNC-26, 345-GNC-30/ACD-10 Taylor, K., 391-FD-53 Thul, D., 9-AMT-1 Stevens, C., 255-PC-9/GTE-9, 296-HSABP-5 Sujit, P., 54-UMS-1, 190-GNC-20 Tahir, F., 144-MAT-4, 198-MAT-5 Taylor, L., 161-WE-2, 467-WE-12 Thurow, B., 30-ISC-1, 227-AMT-5, Stevens, R., 63-APA-6/FD-7, 267-WE-5 Suk, J., 205-SATS-2 Tahmasian, S., 190-GNC-20 Taylor, N., 121-APA-13, 194-HSABP-3, 330-APA-32 276-AMT-6/PC-11/PDL-8, 307-PDL-9/FD-40 Stewart, D., 17-FD-4, 381-APA-40 Suleman, A., 170-ACD-3, 209-STR-7 Tahtali, M., 245-GT-5 Taylor, O., 241-FD-33 Tian, J., 102-STR-3 Stewart, E., 461-SD-14 Sullivan, J., 23-GNC-4, 431-AMT-9 Tai, J., 27-GTE-2 Taylor, P., 234-DSC-1 Tian, P., 136-GNC-15 Stewart, J., 60-AFM-3 Sullivan, R., 50-STR-2 Taira, K., 14-FD-1/APA-5, 286-FD-37, 342-FD-46 Taylor, R., 417-STR-14 Tian, Q., 107-WE-1 Stewart, V., 308-SATS-3 Sultan, C., 282-DSC-3 Takagi, S., 28-HSABP-1 Tekelioğlu, K., 212-UMS-4 Tian, S., 263-STR-9 Stieha, J., 465-TP-12 Sun, C., 77-GNC-7 Takahashi, A., 417-STR-14 Tekinalp, O., 292-GNC-26, 325-ACD-8, 430-AFM-15 Tian, Y., 239-FD-31 Stimpson, A., 352-IS-9 Sun, D., 134-GNC-13, 349-GTE-12 Takahashi, S., 131-FD-19, 265-TP-7 te Kloeze, I., 314-STR-10 Tibaldi, C., 213-WE-4, 268-WE-6, 371-WE-9

Stoddard, W., 28-HSABP-1 Sun, F., 37-MST-2 Takahashi, T., 88-MDO-2, 169-ACD-2, 170-ACD-3, Temme, J., 306-PC-13 Tigges, M., 79-GNC-9 Stoellinger, M., 341-FD-45, 389-FD-51 Sun, J., 331-APA-33 250-MDO-5, 274-ACD-7, 299-MDO-6, 326-ACD-9, Teng, T., 226-AFM-8 Tilmann, C., 67-APA-10, 329-AMT-7, 436-APA-45 Stohlman, O., 309-SCS-4 Sun, K., 384-EDU-2 334-APA-36, 436-APA-45 Tenney, A., 238-FD-30 Timilsina, R., 315-STR-11 Stöhr, M., 40-PC-2, 398-GTE-13 Sun, W., 41-PDL-1, 204-PC-8, 256-PC-10, 360-PC-15 Takahashi, Y., 129-FD-17 Teo, Z., 174-APA-17 Timme, S., 311-SD-9 Stoia, T., 223-ACD-4 Sun, Y., 286-FD-37 Takaki, R., 120-APA-12 Teodorescu, M., 83-IS-2, 312-SEN-2 Timmer, B., 35-MDO-1 Stokes, N., 67-APA-10 Sundaram, D., 105-TP-4 Takamatsu, L., 299-MDO-6 Teramoto, S., 120-APA-12 Tinapple, J., 172-AMT-4 Stone, C., 11-APA-2 Sundararaghavan, V., 33-MAT-1, 34-MAT-2, 249-MAT-7, Takatsuka, M., 154-SD-6 Terashima, H., 73-FD-13, 149-PC-6, 359-PC-14 Tinetti, A., 450-GT-9 Stone, D., 312-SEN-2 368-STR-13 Takayanagi, H., 159-TP-5 Terentjev, I., 249-MAT-7 Ting, E., 235-DSC-2 Storck, K., 37-MST-2 Sundararajan, V., 100-SEO-2 Takehana, R., 151-SATS-1 TerMaath, S., 315-STR-11 Tingey, E., 370-WE-8 Storms, B., 123-APA-15 Sung, T., 445-GNC-37 Takeichi, N., 89-MST-3 Terracol, M., 439-FD-54 Tinker, D., 256-PC-10 Stoumbos, T., 461-SD-14 Suqi, A., 446-GNC-38 Takekawa, K., 280-APA-30, 288-FD-39/APA-31 Tesfahunegn, Y., 88-MDO-2, 330-APA-32 Tinney, C., 221-AA-5, 399-GTE-14 Strahan, A., 23-GNC-4 Sur, R., 39-PC-1 Talamadupula, K., 199-MAT-6 Teubert, C., 243-GNC-22 Tishkoff, J., 150-PDL-5/PC-7/AMT-3, 350-HIS-4 Strakey, P., 192-GTE-6 Suraj Nandiganahalli, J., 29-IS-1/ICC-1/DA-1 Talley, D., 40-PC-2, 410-PC-16 Tezaur, R., 284-FD-35 Togai, K., 41-PDL-1 Stralka, D., 84-ISC-3 Suryawanshi, V., 144-MAT-4 Tam, C., 307-PDL-9/FD-40 Tezuka, A., 36-MST-1 Toghiani, H., 199-MAT-6 Stratemeier, D., 242-GNC-21 Surzhikov, S., 67-APA-10, 159-TP-5 Tamaki, Y., 129-FD-17, 236-FD-28 Thacker, B., 253-NDA-4 Tol, H., 387-FD-49 Straub, F., 281-ASC-4 Sussman, M., 285-FD-36 Tamaskar, S., 195-ICC-2 Thai, B., 406-MST-13 Tomac, M., 174-APA-17 Straub, J., 151-SATS-1, 205-SATS-2, 308-SATS-3 Sutcliffe, P., 245-GT-5 Tamba, T., 71-FD-11 Thakur, S., 390-FD-52 Tompkins, D., 6-ABPSI-1/GEPC-1, 59-ABPSI-2/GEPC-2 Strawson, J., 178-DE-2 Sutton, J., 93-PC-4, 276-AMT-6/PC-11/PDL-8 Tamijani, A., 49-STR-1, 367-STR-12 Thames, C., 47-SOF-1 Ton, C., 135-GNC-14, 293-GNC-27, 396-GNC-36 Streett, C., 229-APA-23/FD-27 Suzuki, S., 29-IS-1/ICC-1/DA-1 Tamunobere, O., 193-GTE-7 Thapa Magar, K., 329-AMT-7 Tong, M., 224-ACD-5 Stremel, P., 59-ABPSI-2/GEPC-2, 123-APA-15 Suzuki, T., 53-TP-2, 369-TP-9 Tan, W., 106-UMS-2 Tharp, J., 446-GNC-38 Tong, O., 288-FD-39/APA-31, 338-FD-42 Strom, B., 14-FD-1/APA-5 Swanson, G., 10-AMT-10/SD-15 Tan, Y., 69-FD-8 Thebault, P., 406-MST-13 Tong, W., 88-MDO-2 Strong, S., 210-TES-5 Swanson, T., 450-GT-9 Tanabe, Y., 371-WE-9 Theil, S., 449-GNC-41 Tong, Z., 332-APA-34 Stroosma, O., 20-GNC-1, 302-MST-10 Sweeney, C., 75-FD-20 Tanaka, H., 152-SCS-1 Theis, J., 375-AFM-12 Toor, Z., 121-APA-13 Strub, G., 396-GNC-36 Sweeney, L., 400-HIS-5 Tang, D., 20-GNC-1, 24-GNC-5 Thelen, A., 268-WE-6, 330-APA-32 Torens, C., 101-SOF-3 Stumfoll, J., 31-ISC-2 Sweet, N., 352-IS-9 Tang, J., 123-APA-15, 441-FD-56 Theodorou, E., 80-GNC-10, 187-GNC-17 Torf, J., 394-GNC-34/ACD-12 Stumpf, E., 169-ACD-2 Swei, S., 61-AFM-4, 83-IS-2, 233-ASC-3, 235-DSC-2 Tang, Y., 294-GTE-10 Theodoulis, S., 406-MST-13 Torisaka, A., 258-SCS-3 Stupik, J., 445-GNC-37 Swenson, E., 37-MST-2, 47-SOF-1, 146-MST-4, Tangirala, V., 402-HSABP-7 Theuerkauf, S., 255-PC-9/GTE-9 Toro, K., 347-GT-7 Sturla, G., 29-IS-1/ICC-1/DA-1 393-GNC-33 Tani, H., 149-PC-6, 359-PC-14 Thielk, S., 102-STR-3 Toropov, V., 88-MDO-2 Author/Session Chair Index Torres-Reyna, M., 327-AFM-10 Ueno, M., 380-APA-39 Vanstone, L., 19-FD-6 Viquerat, A., 258-SCS-3, 309-SCS-4, 314-STR-10 Wan, Z., 380-APA-39 Torstenbo, M., 420-UMS-10 Ugolotti, M., 71-FD-11 Van Tooren, M., 417-STR-14 Visbal, M., 13-APA-4, 15-FD-2, 69-FD-8, 70-FD-9, Wang, B., 418-STR-15 Totoki, H., 20-GNC-1 Uijt De Haag, M., 437-DA-2 Van Wijk, E., 464-TP-11 287-FD-38 Wang, C., 37-MST-2, 252-MST-7, 283-FD-34 Totpal, A., 179-FD-21 Ukeiley, L., 240-FD-32, 286-FD-37 Van Y, S., 46-SEO-1 Visconti, U., 233-ASC-3 Wang, D., 315-STR-11 Toyoda, A., 11-APA-2 Ulbrich, N., 329-AMT-7, 347-GT-7 van Zuijlen, A., 58-AA-2, 356-MVC-1 Visentin, G., 48-SRE-1 Wang, E., 376-AFM-13 Tozzi, A., 312-SEN-2 Ulrich, S., 21-GNC-2, 24-GNC-5, 80-GNC-10, 135- Vargas-Jimenez, J., 273-ACD-6 Vishnampet, R., 458-PC-19 Wang, G., 287-FD-38 Tran, J., 16-FD-3 GNC-14, 189-GNC-19, 252-MST-7 Varghese, P., 94-PC-5 Viswanath, K., 348-GTE-11 Wang, H., 357-NDA-6, 411-PC-17 Tran, S., 72-FD-12 Ulybyshev, Y., 100-SEO-2 Variyar, A., 273-ACD-6, 428-ACD-13 Vlachos, P., 257-PDL-7 Wang, J., 95-PDL-3, 127-FD-15, 178-DE-2, 222-ABPSI-5, Trapier, S., 438-DSC-6 Umemura, Y., 359-PC-14 Varma, S., 449-GNC-41 Voelkel, S., 94-PC-5 331-APA-33, 362-PDL-11, 449-GNC-41 Travaglini, L., 311-SD-9 Umphrey, C., 72-FD-12, 129-FD-17 Vasconcellos, R., 415-SD-13 Voevodin, A., 177-ASC-2 Wang, K., 307-PDL-9/FD-40 Trawny, N., 23-GNC-4, 79-GNC-9 Underwood, M., 392-GNC-32 Vasilaki, E., 83-IS-2 Vogel, R., 87-MAT-3 Wang, L., 237-FD-29, 356-MVC-1, 370-WE-8, Trease, B., 206-SCS-2 Ungwattanapanit, T., 417-STR-14 Vasile, M., 135-GNC-14 Vojisavljevic, V., 325-ACD-8 388-FD-50, 389-FD-51 Treve, V., 342-FD-46 Upadhyay, P., 115-AA-3 Vasko, T., 125-DE-1 Volden, T., 329-AMT-7 Wang, M., 307-PDL-9/FD-40 Tristanto, I., 349-GTE-12 Upadhyay, S., 136-GNC-15 Vassberg, J., 330-APA-32 Volk, B., 317-TP-8 Wang, N., 371-WE-9 Tritschler, J., 378-APA-37 Urbina, A., 43-SD-1 Vasu, S., 39-PC-1 Volle, K., 448-GNC-40 Wang, P., 99-SE-2, 147-NDA-2, 303-NDA-5 Troolin, D., 340-FD-44 Usenmez, S., 27-GTE-2 Vatsa, V., 387-FD-49 Vono, C., 207-SE-3 Wang, Q., 64-APA-7, 162-WE-3, 213-WE-4, Tropina, A., 96-PDL-4 Uslu, S., 139-GTE-5 Vaughn, W., 202-NDA-3 von Spakovsky, M., 223-ACD-4 250-MDO-5, 386-FD-48 Truax, R., 260-SEN-1 Uzol, O., 27-GTE-2, 107-WE-1 Vaught, S., 124-CMS-1/CPS-1 Vorobiev, A., 307-PDL-9/FD-40 Wang, R., 17-FD-4 Tsai, J., 312-SEN-2 Vaddi, V., 89-MST-3, 312-SEN-2 Veers, P., 162-WE-3 Vos, J., 277-APA-27, 439-FD-54 Wang, S., 39-PC-1, 390-FD-52 Tsai, K., 45-SE-1 Vahab, M., 285-FD-36 Vegh, J., 223-ACD-4, 273-ACD-6 Vos, R., 223-ACD-4, 273-ACD-6, 274-ACD-7, 374-ACD-11 Wang, V., 464-TP-11 Tsai, W., 419-TP-10 Valasek, J., 76-GNC-6, 77-GNC-7, 160-UMS-3, Vehorn, K., 50-STR-2 Voutsinas, S., 107-WE-1, 267-WE-5 Wang, X., 58-AA-2, 66-APA-9, 67-APA-10, 159-TP-5, Tschan, C., 403-IS-11 243-GNC-22, 394-GNC-34/ACD-12 Veiberman, R., 311-SD-9 Vradis, G., 70-FD-9 229-APA-23/FD-27, 265-TP-7, 383-DSC-5, 410-PC-16 Tsiotras, P., 187-GNC-17, 447-GNC-39 Valco, D., 94-PC-5 Veillard, A., 54-UMS-1 Vu, B., 338-FD-42 Wang, Y., 70-FD-9, 106-UMS-2, 151-SATS-1, Tsolas, N., 41-PDL-1 Valdes, J., 464-TP-11 Veklich, A., 95-PDL-3 Vukasinovic, B., 16-FD-3 154-SD-6, 209-STR-7, 259-SD-7, 386-FD-48,

Tsuboi, N., 73-FD-13 Valdez, J., 399-GTE-14 Venkatachari, B., 229-APA-23/FD-27 Vukcevic, V., 18-FD-5 429-AFM-14, 441-FD-56 Tsushima, N., 154-SD-6 Valente, C., 336-DSC-4 Venkatapathy, E., 211-TP-6 Vynogradskyy, P., 387-FD-49 Wang, Z., 198-MAT-5, 236-FD-28, 250-MDO-5, Tsutsumi, S., 9-AMT-1, 120-APA-12 Valentich, G., 115-AA-3 Venkataraman, G., 334-APA-36 Waas, A., 157-STR-5, 208-STR-6, 262-STR-8, 338-FD-42, 341-FD-45, 388-FD-50, 391-FD-53, Tu, X., 386-FD-48 Valentini, P., 104-TP-3 Venkataraman, R., 134-GNC-13 368-STR-13, 463-STR-17 396-GNC-36, 414-SD-12, 440-FD-55 Tucker, A., 376-AFM-13 Valera-Medina, A., 103-TES-3, 246-GTE-8 Venkataraman, S., 315-STR-11, 349-GTE-12, Wabel, T., 306-PC-13 Wanthal, S., 87-MAT-3, 353-MAT-9 Tucker, J., 418-STR-15 Valero, E., 193-GTE-7 399-GTE-14, 418-STR-15 Wadhams, T., 81-GT-2 Ward, C., 35-MDO-1 Tucker, P., 26-GTE-1, 82-GTE-3, 389-FD-51, 452-GTE-16 van Bussel, G., 267-WE-5 Venkatesh, V., 249-MAT-7, 409-MAT-10, 433-APA-42 Wagner, D., 132-GNC-11, 292-GNC-26 Ward, D., 376-AFM-13 Tuckey, T., 278-APA-28 Van Dalen, G., 136-GNC-15 Venkateswaran, P., 306-PC-13 Wagner, J., 10-AMT-10/SD-15, 172-AMT-4, Ward, M., 244-GNC-23 Tudisco, P., 458-PC-19 Van Dam, C., 120-APA-12, 268-WE-6, 441-FD-56 Venrooij, J., 251-MST-6 227-AMT-5, 286-FD-37, 377-AMT-8, 443-FD-58 Warde, S., 353-MAT-9 Tuegel, E., 357-NDA-6 Vanden, K., 123-APA-15, 230-APA-24 Ventura, J., 187-GNC-17 Wahl, E., 404-MDO-8 Wardle, B., 33-MAT-1, 199-MAT-6 Tufano, D., 461-SD-14 Van den Broecke, J., 257-PDL-7 Venturi, S., 104-TP-3 Waindim, M., 131-FD-19, 386-FD-48 Warner, D., 353-MAT-9 Tuinstra, M., 183-FD-25 van der Horst, S., 370-WE-8 Veras, C., 337-EDU-1 Waithe, K., 334-APA-36, 435-APA-44 Warner, J., 344-GNC-29 Tulgestke, A., 40-PC-2 Vandermey, J., 328-AFM-11 Verhoeven, R., 345-GNC-30/ACD-10 Wake, B., 65-APA-8 Warnick, K., 420-UMS-10 Tumuklu, O., 104-TP-3, 440-FD-55 Van Der Veen, S., 34-MAT-2, 198-MAT-5 Vernekar, G., 101-SOF-3 Waldman, R., 105-TP-4 Warning, S., 131-FD-19 Tunçöz, I., 68-ASC-1 van der Velden, W., 58-AA-2 Vernis, P., 449-GNC-41 Walker, B., 149-PC-6 Warren, J., 199-MAT-6, 309-SCS-4, 460-SCS-7 Turkoglu, K., 37-MST-2, 201-MST-5, Vanderwyst, A., 97-SD-3, 282-DSC-3, 332-APA-34, Vetrella, A., 312-SEN-2 Walker, D., 76-GNC-6, 264-SUR-1, 392-GNC-32 Washabaugh, K., 386-FD-48 345-GNC-30/ACD-10, 404-MDO-8 381-APA-40 Vian, J., 297-IS-7 Walker, E., 202-NDA-3, 380-APA-39, 450-GT-9 Washburn, A., 191-GT-4 Turner, T., 335-ASC-5 van de Wiel, J., 370-WE-8 Vich, O., 415-SD-13 Walker, M., 387-FD-49 Watanabe, A., 309-SCS-4 Tursynbai, A., 39-PC-1 van Gils, P., 292-GNC-26 Vicroy, D., 6-ABPSI-1/GEPC-1, 59-ABPSI-2/GEPC-2 Walker, S., 135-GNC-14, 146-MST-4, 355-MST-11 Watanabe, H., 28-HSABP-1, 296-HSABP-5 Tuttle, S., 149-PC-6 Van Kampen, E., 20-GNC-1, 54-UMS-1, 76-GNC-6, Vidana, O., 52-TES-2/TP-1, 210-TES-5 Wall, A., 399-GTE-14, 452-GTE-16 Watanabe, K., 309-SCS-4 Tweddle, B., 79-GNC-9, 135-GNC-14 135-GNC-14, 212-UMS-4, 244-GNC-23, 292-GNC-26, Vijayachandran, A., 368-STR-13 Wallace, R., 378-APA-37 Watanabe, N., 236-FD-28 Tyacke, J., 452-GTE-16 293-GNC-27, 346-GNC-31, 376-AFM-13, 395-GNC-35 Vijayakumar, G., 107-WE-1 Wallner, E., 406-MST-13 Watanabe, S., 125-DE-1, 190-GNC-20, 376-AFM-13 Tyagi, A., 124-CMS-1/CPS-1, 306-PC-13 van Keulen, F., 200-MDO-4 Viken, S., 226-AFM-8 Walter, J., 245-GT-5 Watanabe, T., 103-TES-3, 403-IS-11 Uchiyama, K., 100-SEO-2, 151-SATS-1 van Kuik, G., 161-WE-2 Vila, L., 155-SRE-2 Walter, S., 116-ABPSI-3 Watanabe, Y., 54-UMS-1 Ueda, S., 222-ABPSI-5 van Muijden, J., 300-MST-8 Villalva Gomez, R., 246-GTE-8, 457-PC-18 Walter, U., 187-GNC-17 Watkins, J., 345-GNC-30/ACD-10 Uejima, K., 36-MST-1 van Oijen, J., 411-PC-17 Villanueva, D., 253-NDA-4 Walters, K., 239-FD-31 Watson, J., 125-DE-1, 309-SCS-4, 460-SCS-7 Uematsu, A., 152-SCS-1 van Paassen, M., 243-GNC-22, 302-MST-10 Vio, G., 200-MDO-4, 202-NDA-3, 433-APA-42 Wan, T., 434-APA-43 Watson, L., 282-DSC-3 Ueno, A., 435-APA-44 van Rooij, M., 232-APA-26 Viola, F., 467-WE-12 Wan, Y., 160-UMS-3 Watson, R., 395-GNC-35, 452-GTE-16 Author/Session Chair Index Wawrzinek, K., 389-FD-51 White, B., 48-SRE-1 Wissink, A., 18-FD-5, 122-APA-14, 228-APA-22, Xia, C., 123-APA-15, 232-APA-26 Yazdani, S., 418-STR-15 Weaver, P., 98-SD-4, 177-ASC-2, 263-STR-9, 314-STR-10 White, E., 335-ASC-5, 441-FD-56 338-FD-42 Xia, G., 341-FD-45 Yedavalli, R., 76-GNC-6 Webb, D., 460-SCS-7 White, M., 454-MST-14, 459-PDL-13 Witeof, Z., 97-SD-3, 282-DSC-3 Xia, X., 232-APA-26 Yee, K., 18-FD-5, 97-SD-3 Webb, K., 61-AFM-4 White, S., 211-TP-6, 298-MAT-8 Wittich, D., 286-FD-37, 307-PDL-9/FD-40 Xia, Y., 386-FD-48 Yee, P., 465-TP-12 Webb, N., 181-FD-23/PDL-6 Whitener, G., 84-ISC-3 Wlezien, R., 125-DE-1, 441-FD-56 Xiao, T., 439-FD-54 Yen, Y., 52-TES-2/TP-1, 103-TES-3 Weber, A., 160-UMS-3 Whitlock, B., 407-MVC-2 Woerner, P., 53-TP-2 Xiao, Y., 371-WE-9 Yeo, C., 106-UMS-2 Webster, J., 445-GNC-37 Whittaker, W., 23-GNC-4 Woicke, S., 242-GNC-21, 446-GNC-38 Xie, J., 160-UMS-3 Yeo, D., 293-GNC-27, 327-AFM-10 Webster, R., 82-GTE-3 Wick, A., 137-GT-3 Wojnar, C., 152-SCS-1 Xin, M., 7-AFM-1, 344-GNC-29 Yerkes, K., 300-MST-8 Wei, D., 54-UMS-1 Wicke, K., 289-GEPC-4 Wokoeck, R., 232-APA-26 Xing, F., 116-ABPSI-3 Yetter, R., 41-PDL-1, 150-PDL-5/PC-7/AMT-3 Wei, F., 125-DE-1 Wickham, A., 305-PC-12 Wolf, C., 231-APA-25 Xiong, J., 115-AA-3 Yi, S., 250-MDO-5, 272-AA-6 Wei, M., 237-FD-29, 374-ACD-11 Wickham, D., 305-PC-12 Wolf, J., 84-ISC-3 Xu, H., 130-FD-18 Yildiz, K., 259-SD-7 Weichselbaum, N., 10-AMT-10/SD-15 Wickramasinghe, N., 36-MST-1 Wolf, M., 414-SD-12 Xu, K., 412-PDL-12 Yildiz, Y., 212-UMS-4 Weimer, C., 446-GNC-38 Wiemer, D., 77-GNC-7 Wolfe, G., 233-ASC-3 Xuzhao, H., 342-FD-46 Yim, J., 363-SCS-5 Weintraub, I., 190-GNC-20 Wiese, C., 193-GTE-7 Wolff, M., 26-GTE-1, 49-STR-1, 145-MDO-3 Yachi, Y., 103-TES-3 Yin, Z., 40-PC-2 Weis, L., 308-SATS-3 Wiese, D., 292-GNC-26 Wollschlager, J., 156-STR-4 Yadav, V., 349-GTE-12, 399-GTE-14 Yoda, H., 125-DE-1 Weisberger, J., 53-TP-2 Wieser, D., 379-APA-38 Wolters, F., 81-GT-2 Yaggi, B., 48-SRE-1 Yoder, D., 333-APA-35/FD-41, 398-GTE-13 Weisman, R., 290-GNC-24 Wiggins, J., 199-MAT-6 Woltosz, W., 37-MST-2 Yakimenko, O., 60-AFM-3 Yodo, N., 99-SE-2 Weismiller, M., 149-PC-6 Wignall, T., 360-PC-15, 411-PC-17 Won, S., 256-PC-10 Yalin, A., 96-PDL-4, 362-PDL-11 Yoel, D., 160-UMS-3 Weiss, J., 443-FD-58 Wilcox, F., 173-APA-16 Wong, M., 30-ISC-1, 385-FD-47 Yamada, K., 377-AMT-8 Yokomatsu, T., 460-SCS-7 Weiss, M., 311-SD-9 Wild, J., 66-APA-9 Woo, G., 139-GTE-5 Yamaguchi, S., 377-AMT-8 Yokoyama, N., 186-GNC-16 Weit, C., 84-ISC-3 Wilhelm, J., 54-UMS-1 Woo, N., 363-SCS-5 Yamakawa, H., 258-SCS-3, 309-SCS-4 Yoo, Y., 205-SATS-2 Weitz, L., 343-GNC-28, 392-GNC-32 Wilhite, A., 49-STR-1 Wood, D., 224-ACD-5 Yamamoto, K., 169-ACD-2 Yoon, H., 134-GNC-13, 344-GNC-29 Welch, G., 26-GTE-1 Wilhite, J., 246-GTE-8, 351-HSABP-6 Woodgate, M., 176-APA-20 Yamamoto, M., 371-WE-9 Yoon, S., 176-APA-20, 186-GNC-16 Wells, D., 224-ACD-5 Wilkinson, C., 378-APA-37, 406-MST-13 Woodham, K., 223-ACD-4 Yamamoto, N., 33-MAT-1 Yorita, D., 137-GT-3

Wells, M., 432-APA-41 Wilkinson, M., 315-STR-11 Woodruff, S., 333-APA-35/FD-41 Yamamoto, T., 403-IS-11 York, G., 80-GNC-10, 136-GNC-15, 201-MST-5, Wells, S., 449-GNC-41 Willcox, K., 299-MDO-6, 303-NDA-5 Woolley, B., 446-GNC-38 Yaman, Y., 68-ASC-1 275-AFM-9 Welsh, W., 414-SD-12 Williams, A., 464-TP-11 Woolsey, C., 190-GNC-20 Yamaoka, N., 406-MST-13 Yoshida, K., 435-APA-44 Welstead, J., 224-ACD-5 Williams, B., 149-PC-6, 397-GT-8 Worden, T., 221-AA-5 Yamashita, J., 231-APA-25 Yoshimura, A., 463-STR-17 Wen, B., 222-ABPSI-5 Williams, D., 16-FD-3, 84-ISC-3, 442-FD-57 Worth, N., 411-PC-17, 458-PC-19 Yamazaki, M., 146-MST-4 Youn, E., 432-APA-41 Wen, C., 384-EDU-2 Williams, F., 93-PC-4 Woszidlo, R., 73-FD-13, 127-FD-15 Yamazaki, W., 370-WE-8, 428-ACD-13 Young, D., 330-APA-32 Wendorff, A., 273-ACD-6, 299-MDO-6 Williams, J., 69-FD-8, 412-PDL-12 Wray, T., 130-FD-18, 239-FD-31 Yan, G., 180-FD-22 Young, J., 442-FD-57 Wereley, N., 233-ASC-3 Williams, M., 237-FD-29 Wrede, B., 25-GT-1 Yan, X., 42-PDL-2, 193-GTE-7 Young, S., 437-DA-2 Wermer, L., 96-PDL-4, 131-FD-19, 248-HSABP-4 Williams, S., 437-DA-2 Wriggers, P., 418-STR-15 Yan, Z., 259-SD-7 Youssef, A., 37-MST-2 Wermes, M., 12-APA-3 Williams, T., 314-STR-10 Wright, A., 371-WE-9 Yanagita, Y., 288-FD-39/APA-31, 338-FD-42 Yu, H., 230-APA-24, 395-GNC-35 Werner, S., 398-GTE-13 Williams-Hayes, P., 376-AFM-13 Wright, J., 390-FD-52 Yanase, S., 377-AMT-8 Yu, K., 248-HSABP-4, 255-PC-9/GTE-9, Wernet, M., 348-GTE-11 Williamson, A., 264-SUR-1 Wright, R., 367-STR-12 Yang, B., 251-MST-6 296-HSABP-5, 305-PC-12 Werter, N., 68-ASC-1, 98-SD-4, 417-STR-14 Willis, B., 461-SD-14 Wrist, A., 179-FD-21 Yang, C., 355-MST-11, 380-APA-39 Yu, M., 241-FD-33, 388-FD-50, 422-WE-11 Wertz, J., 207-SE-3 Wilson, D., 248-HSABP-4 Wroblewski, G., 121-APA-13 Yang, G., 13-APA-4, 331-APA-33 Yu, P., 183-FD-25 Wesseling, E., 452-GTE-16 Wilson, T., 336-DSC-4, 420-UMS-10 Wu, B., 181-FD-23/PDL-6 Yang, H., 151-SATS-1, 236-FD-28 Yu, T., 310-SD-8 Wessels, M., 387-FD-49 Winckelmans, G., 342-FD-46 Wu, C., 309-SCS-4 Yang, J., 144-MAT-4, 396-GNC-36 Yu, W., 156-STR-4, 161-WE-2, 198-MAT-5, 209-STR-7, Wessner, A., 237-FD-29 Wind, T., 41-PDL-1 Wu, H., 353-MAT-9, 462-STR-16 Yang, S., 41-PDL-1, 66-APA-9, 250-MDO-5 263-STR-9 West, T., 159-TP-5 Winer, E., 207-SE-3 Wu, K., 314-STR-10 Yang, V., 41-PDL-1, 105-TP-4, 410-PC-16 Yu, X., 243-GNC-22 Westfall, A., 404-MDO-8 Winski, C., 435-APA-44 Wu, L., 42-PDL-2, 181-FD-23/PDL-6 Yang, X., 151-SATS-1, 283-FD-34, 284-FD-35 Yu, Z., 243-GNC-22, 290-GNC-24 Wetzel, K., 267-WE-5 Winter, M., 317-TP-8, 419-TP-10 Wu, S., 259-SD-7, 311-SD-9, 461-SD-14 Yang, Y., 68-ASC-1, 70-FD-9, 123-APA-15, 127-FD-15, Yuan, H., 123-APA-15 Wey, C., 451-GTE-15 Winters, C., 62-AMT-2, 257-PDL-7 Wu, X., 100-SEO-2 149-PC-6, 368-STR-13, 405-MST-12 Yuan, W., 332-APA-34 Whalen, E., 16-FD-3, 185-GEPC-3 Wippich-Dienhart, R., 49-STR-1 Wu, Y., 62-AMT-2, 84-ISC-3 Yang, Z., 123-APA-15, 232-APA-26 Yuan, Z., 156-STR-4 Whelan, C., 337-EDU-1 Wirz, R., 268-WE-6 Wu, Z., 152-SCS-1, 189-GNC-19, 259-SD-7, 355-MST-11 Yao, H., 151-SATS-1 Yucel, A., 83-IS-2 Whidborne, J., 185-GEPC-3 Wischek, J., 87-MAT-3 Wukie, N., 439-FD-54 Yao, J., 405-MST-12 Yucelen, T., 29-IS-1/ICC-1/DA-1, 132-GNC-11, Whitacre, W., 262-STR-8, 297-IS-7, Wischt, R., 153-SD-5 Wutschitz, L., 129-FD-17 Yao, Y., 13-APA-4, 116-ABPSI-3, 405-MST-12 292-GNC-26, 393-GNC-33 345-GNC-30/ACD-10, 395-GNC-35 Wisda, D., 272-AA-6 Wygnanski, I., 387-FD-49 Yasin, R., 206-SCS-2 Yunis, I., 311-SD-9 Whitcher, L., 22-GNC-3 Wise, K., 20-GNC-1 Wynn, A., 154-SD-6 Yasky, R., 223-ACD-4 Yurchenko, N., 387-FD-49 Whitcomb, J., 335-ASC-5 Wise, R., 235-DSC-2 Xargay, E., 134-GNC-13 Yavrucuk, I., 27-GTE-2 Yurkovich, M., 459-PDL-13 Author/Session Chair Index Zaal, P., 37-MST-2, 302-MST-10 Zhou, E., 156-STR-4 Zachariah, M., 149-PC-6 Zhou, Y., 54-UMS-1, 76-GNC-6, 152-SCS-1, Zacny, K., 48-SRE-1, 189-GNC-19 293-GNC-27, 384-EDU-2 Zagorskiy, A., 41-PDL-1 Zhou, Z., 250-MDO-5 Zahle, F., 268-WE-6 Zhu, F., 154-SD-6 Zahr, M., 17-FD-4, 175-APA-18 Zhu, G., 76-GNC-6, 235-DSC-2 Zahradka, D., 339-FD-43 Zhu, H., 341-FD-45 Zakaria, M., 66-APA-9 Zhu, J., 244-GNC-23 Zakrajsek, A., 87-MAT-3 Zhu, M., 189-GNC-19 Zaloglu, B., 442-FD-57 Zhu, S., 133-GNC-12, 357-NDA-6, 368-STR-13 Zaman, K., 391-FD-53 Zhu, W., 161-WE-2, 422-WE-11 Zandian, A., 340-FD-44 Zhu, Y., 39-PC-1, 141-HSABP-2 Zare-Behtash, H., 35-MDO-1 Zhu, Z., 133-GNC-12, 151-SATS-1, 436-APA-45 Zarepoor, M., 43-SD-1 Zhuang, W., 355-MST-11 Zawodny, N., 272-AA-6 Zhupanska, O., 102-STR-3, 209-STR-7, 314-STR-10 Zemerick, S., 308-SATS-3 Ziaei-Rad, S., 374-ACD-11 Zettl, D., 282-DSC-3 Zidek, R., 77-GNC-7 Zewei, Z., 189-GNC-19 Zientarski, L., 281-ASC-4 Zha, G., 120-APA-12, 123-APA-15, 127-FD-15 Zilliac, G., 333-APA-35/FD-41 Zhai, Q., 239-FD-31 Zimmerman, J., 41-PDL-1 Zhai, J., 204-PC-8 Zingg, D., 277-APA-27 Zhang, A., 236-FD-28 Zinnecker, A., 300-MST-8 Zhang, C., 15-FD-2 Zipay, J., 263-STR-9, 367-STR-12 Zhang, D., 95-PDL-3, 157-STR-5 Zishka, E., 440-FD-55

Zhang, F., 394-GNC-34/ACD-12 Zong, Y., 149-PC-6 Zhang, H., 53-TP-2, 126-FD-10, 287-FD-38 Zwanenburg, P., 388-FD-50 Zhang, K., 240-FD-32 Zhang, L., 144-MAT-4 Zhang, M., 80-GNC-10, 277-APA-27, 380-APA-39 Zhang, P., 342-FD-46 Zhang, Q., 447-GNC-39 Zhang, R., 13-APA-4, 246-GTE-8, 399-GTE-14 Zhang, S., 265-TP-7 Zhang, T., 226-AFM-8, 422-WE-11 Zhang, W., 198-MAT-5 Zhang, X., 404-MDO-8 Zhang, Y., 9-AMT-1, 72-FD-12, 233-ASC-3, 252-MST-7, 286-FD-37, 330-APA-32, 332-APA-34, 430-AFM-15, 455-MST-15 Zhang, Z., 62-AMT-2, 222-ABPSI-5, 239-FD-31, 250-MDO-5, 362-PDL-11, 383-DSC-5 Zhao, J., 127-FD-15 Zhao, L., 118-AFM-5 Zhao, P., 95-PDL-3 Zhao, Q., 65-APA-8 Zhao, W., 104-TP-3, 314-STR-10, 375-AFM-12 Zhao, X., 19-FD-6 Zhao, Y., 244-GNC-23 Zhao, Z., 259-SD-7, 290-GNC-24 Zheng, J., 79-GNC-9 Zhongjiao, S., 118-AFM-5 Zhou, C., 65-APA-8, 388-FD-50, 454-MST-14 ITECHNICAL ZONES

AIAA SciTech 2016 Technical Zones Career Workshop Location The technical program, which consists of more than 2000 papers • Vista AB is located on the 32nd level of the Seaport Tower in over 10 technical tracks, has been placed within the hotel in Committee Meeting Rooms: zones to keep related session topics and technical conferences together. Please visit one of the zones to listen to a technical paper • Cityview A and B are located on the 32nd level of that is of interest to you! the Seaport Tower • Conference Parlors are located on the 7th floor of ZONE ADS: Aerospace Design and Structures the Harbor Tower • All other committee meeting rooms are located on the ZONE AS: Aerospace Sciences 2nd, 3rd, and 4th levels ZONE IS: Information Systems

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www.aiaa-SciTech.org 20961 #aiaaSciTech 9–13 JANUARY 2017 GRAPEVINE, TX SEE YOU NEXT YEAR Mark your calendars for the first major aerospace event of 2017—AIAA Science and Technology Forum and Exposition—where engineers, researchers, students, and aerospace leaders from around the world will share the most original perspectives, collaborate on stimulating ideas, and influence the future of aerospace FEATURING: • 25th AIAA/AHS Adaptive Structures Conference

• 55th AIAA Aerospace Sciences Meeting

• AIAA Atmospheric Flight Mechanics Conference

• AIAA Information Systems-AIAA Infotech @ Aerospace

• AIAA Guidance, Navigation, and Control Conference

• AIAA Modeling and Simulation Technologies Conference

• 19th AIAA Non-Deterministic Approaches Conference

• 58th AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference

• 10th Symposium on Space Resource Utilization

• 4th AIAA Spacecraft Structures Conference

• 35th Wind Energy Symposium

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