PROGRAM #Aiaascitech

9–13 JANUARY 2017 GRAPEVINE, TX

Addressing Full Spectrum Disruptions Across the Global Aerospace Community

PROGRAM www.aiaa-SciTech.org #aiaaSciTech

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© 2014 LOCKHEED MARTIN CORPORATION VC377_164 Executive Steering Committee AIAA SciTech Forum Welcome Welcome to the 2017 AIAA Science and Technology Forum and Exposition (AIAA SciTech Forum) – the world’s largest event for aerospace research, development, and technology! Only here will you find the diversity of topics, caliber of speakers, and level of discourse about issues that directly impact your work, your career, and your industry – we are confident you will leave Grapevine prepared to shape the future of aerospace in new and exciting ways. Chuck Gustafson Jill Marlowe By bringing together 11 aerospace science and technology conferences, and by attracting attendees The Aerospace NASA Langley from across academia, industry, and government, AIAA SciTech will give you an unparalleled Corporation Research Center opportunity to hear from industry thought leaders, interact with your peers, and begin the inspired exchange of ideas that so often leads to breakthroughs in our community. Our organizing committee has worked hard over the past year to ensure that our plenary sessions examine some of the most critical issues facing aerospace today, especially the role that disruption plays in our community for better or worse. The five plenary sessions will explore the factors driving today’s disruptive environment, the disruptive business model, presidential transitions, technology breakthroughs that will transform aerospace, and how we can build a next-generation workforce that is second to none.

The Forum 360 program dives even deeper into a diverse range of issues, including the CREATE modeling and simulation environment, a historical look at NASA Langley Research Center, Pamela Melroy Darryll Pines the future of the aerospace workforce, geoengineering to mitigate climate change, space traffic DARPA University of Maryland management, UAS integration, managing change during the development of disruptive technologies, and the NASA Innovative Advanced Concepts program.

The forum’s technical sessions will provide unique opportunities to learn how your peers are tackling the pressing challenges that face the advancement of aerospace technology and science. Whatever session you attend, you will gain actionable, future-focused insights that will enable you to begin thinking about how you will use your talents and skills to advance the state of the art in aerospace.

While you are with us this week, be sure to attend our networking events, which provide unique opportunities to connect, collaborate, and exchange ideas. It is often those conversations that lead to Robie Robbie Robertson groundbreaking collaboration. They also provide rich networking opportunities as you continue to build your career, and as you seek out colleagues and students with similar interests. Samanta Roy Air Force Research Lockheed Martin Laboratory Also, be sure to spend some time in our Exposition Hall. Over 50 companies and organizations are Corporation waiting to show you their innovative products and services, and with the wide variety of technology on display, you are sure to see something that captivates your imagination.

AIAA SciTech Forum offers every aerospace professional, regardless of the role you play in our community, an opportunity to explore important topics at every level and to gain insights into technologies and industry sectors that are intersecting with aerospace in heretofore unimaginable ways – all in one place. We are excited to offer you this program, and we thank you for making the choice to be with us this week.

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

2017 AIAA SciTech Forum General Chair Computer Systems Propellants and Combustion Robie Samanta Roy, Lockheed Martin Chiping Li, Air Force Office of Scientific Tim Lieuwen, Georgia Institute of Technology Corporation Research Sensor Systems and Information Fusion Forum 360 Chair Design Engineering Domenico Accardo, University of Naples Robbie Robertson, Air Force Research Lisa Saam, ATA Engineering, Inc. Laboratory Small Satellites Digital Avionics Jeremy Straub, University of North Dakota Forum 360 Deputy Chair Douglas Abernathy, Lockheed Martin Martiqua Post, U.S. Air Force Academy Corporation Society and Aerospace Technology Jarret Lafleur, Sandia National Laboratories Young Professional Chair Fluid Dynamics Samantha Alberts, Purdue University Steve Karman, Pointwise, Inc. Software Christoph Torens, DLR Forum Technical Chairs Gas Turbine Engines Terry Morris, NASA Langley Research Center Scott Drennan, Convergent Science, Inc. Space Exploration Surendra Sharma, NASA Ames Research Richard Ruff, MathWorks Green Engineering Center Tarek Abdel-Salam, East Carolina University Ben Thacker, Southwest Research Institute Space Operations and Support Ground Test Shirley Tseng, Tseng, LLC Forum Deputy Technical Chairs Rajan Kumar, Florida State University Kevin Melcher, NASA Glenn Research Space Resources Utilization Symposium Center Guidance, Navigation, and Control Julie Kleinhenz, NASA Glenn Research Jason Hui, BAE Systems Center Gregory Odegard, Michigan Technological University High-Speed Air-Breathing Propulsion Spacecraft Structures Dan Paxson, NASA Glenn Research Center Matthew Santer, Imperial College London Subrata Roy, University of Florida

Eric Silk, NASA Goddard Space Flight Center History Structural Dynamics Dick Hallion, Science and Technology Policy Zahra Sotoudeh, Rensselaer Polytechnic Technical Discipline Chairs Institute, IDA Institute Adaptive Structures Information and Command & Control Structures Edward White, The Boeing Company Systems John Zipay, NASA Johnson Space Center Aeroacoustics Mike Sotak, Kratos Defense and Security Student Paper Competition – AD&S Eric Nesbitt, The Boeing Company Solutions Olesya Zhupanska, University of Arizona Aerodynamic Measurement Technology Intelligent Systems Survivability Bharathram Ganapathisubramani, Amanda Lampton, Systems Technology, Inc. Steven Broussard, The Boeing Company University of Southampton Materials Aerospace Education Mohammad Naraghi, Texas A&M University Systems Engineering John Hsu, California State University, Long K. Ravindra, St. Louis University Meshing Visualization and Computational Beach Air Breathing Propulsion Systems Integration Environments Terrestrial Energy Eric Loth, University of Virginia Andrew Lofthouse, U.S. Air Force Academy Ahsan Choudhuri, University of Texas at El Aircraft Design Modeling and Simulation Technologies Paso Cees Bil, RMIT University Peter Grant, University of Toronto Institute for Aerospace Studies Thermophysics Applied Aerodynamics Micah Howard, Sandia National Laboratories Dennis Finley, Lockheed Martin Aeronautics Multi-Disciplinary Design Optimization Frode Engelsen, Boeing Research and Unique and Transformational Flight Systems Atmospheric Flight Mechanics Technology Virginia Stouffer, LMI Timur Alexeev, University of California Non-Deterministic Approaches Unmanned Systems Communications Systems Barron Bichon, Southwest Research Institute Richard Stansbury, Embry-Riddle Denise Ponchak, NASA Glenn Research Aeronautical University Center Plasmadynamics and Lasers Marco Panesi, University of Illinois at Wind Energy Symposium Urbana-Champaign Matthew Churchfield, National Renewable Energy Laboratory www.aiaa-SciTech.org 4 #aiaaSciTech IntroContents

Welcome 3

Organizing Committee 4

Forum Overview 8

Sponsors and Supporters 10

Pre-Forum Activities 11

Keynote Speakers and Plenary Sessions 12 www.twitter.com/aiaa

Forum 360 13 www.facebook.com/AIAAfan

Special Sessions and Events 16 www.youtube.com/AIAATV

Educational Events 19 www.linkedin.com/companies/aiaa

Networking Events 21 www.flickr.com/aiaaevents

Recognition Events 22 instagram.com/AIAAerospace

Exposition Hall 25 livestream.com/AIAAVideo/SciTech2017

Exhibitors 28 Join the conversation! Join the Q&A General Information 36 #aiaaSciTech aiaa.cnf.io

Author and Session Chair Information 38 On-Site Wi Fi Information Network Name: AIAASciTech Committee Meetings and Events 39 Password: scitech17

Sessions at a Glance 44

AIAA is the world’s largest aerospace professional society, Session Detail Matrix 57 serving a diverse range of more than 30,000 individual members from 88 countries, and nearly 100 corporate members. AIAA members help make the world safer, Author and Session Chair Index 176 more connected, more accessible, and more prosperous. For more information, visit www.aiaa.org, or follow us on Twitter @AIAA. Venue Map 196 www.aiaa-SciTech.org 5 #aiaaSciTech Get Your Conference Info on the Go!

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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 “2017 AIAA SciTech http://download.abstractcentral. Forum” See the surrounding area and com/aiaa-mst17/index.htm the Gaylord Texan • Once downloaded, you can bookmark Connect to Twitter the site to access it later or add a link 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 Forum with conferences i/o!

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NO DOWNLOADING REQUIRED! IntroForum Overview

SATURDAY/SUNDAY MONDAY TUESDAY 7–8 January 9 January 10 January 0730 hrs Speakers’ Briefing Speakers’ Briefing

0800 hrs Opening Plenary Panel Keynote 0830 hrs

0900 hrs Networking Coffee Break Networking Coffee Break

0930 hrs NDA Lecture 1000 hrs ASC Lecture Continuing Education Forum 360 and Special Forum 360 1030 hrs Courses Technical Presentation Technical Sessions and 1100 hrs Sessions Workshops 1130 hrs 0800–1700 hrs 1200 hrs Saturday and Sunday (See p. 11 for more information) 1230 hrs Durand Lecture for Public Recognition Luncheon: Celebrating Networking Lunch Networking 1300 hrs Service and Luncheon Achievements in Aerospace Sciences On Own Lunch on Own and Information Systems 1330 hrs

1400 hrs Exposition Hall Open SCS Lecture 1430 hrs (Ice Cream and Panel Forum 360 Forum 360 Break 1500 hrs 1530–1600 Technical Technical hrs) Networking Coffee Networking Coffee 1530 hrs Sessions Sessions Meet the Employers Break Break in Exposition Hall Sunday 1600 hrs

1630 hrs Rising Leaders Leadership International Student Exchange and 1700 hrs Conference Student Briefing Speed Mentoring AIAA Town Hall Sunday Meeting (Governance 1730 hrs and Open Access) Dryden Lecture in Research 1800 hrs 1830 hrs Student Welcome Reception Sunday Associate Fellows Opening Reception in the Exposition Hall 1900 hrs All students welcome Reception Rising Leaders Hall opens at 1815 hrs in Aerospace 1930 hrs Reception

2000 hrs

2030 hrs AIAA Associate Fellows Dinner 2100 hrs Career Workshop: Tools to Ensure Your Career (Tickets will occur 0930–1230 hrs and 1400–1600 Required) Success 2130 hrs hrs. See p. 19 for more information. 2200 hrs

2230 hrs

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

WEDNESDAY THURSDAY FRIDAY 11 January 12 January 13 January 0730 hrs Speakers’ Briefing Speakers’ Briefing Speakers’ Briefing

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

1000 hrs Forum Forum 360 360 1030 hrs Technical Technical Sessions 1100 hrs Sessions Technical Exposition Exposition Sessions 1130 hrs Hall Open Hall Open Hall opens Hall opens 1200 hrs at 0845 hrs at 0845 hrs Recognition Luncheon: 1230 hrs Celebrating Achievements Rising Networking in Aerospace Design/ Networking Lunch Leaders 1300 hrs Luncheon in Exposition Hall Coffee Structures and Aerospace Keynote On Own Break in Literature Speaker and Exposition Hall 1330 hrs Box Lunch 1530-1600 hrs 1400 hrs

1430 hrs Forum Forum 360 360 1500 hrs Technical Technical Sessions Sessions 1530 hrs Diversity Networking Coffee Break and Inclusion in 1600 hrs the Workplace

1630 hrs Corporate 1700 hrs Member and Exhibitor 1730 hrs Reception Women at SciTech 1800 hrs Social SDM Hour and Lecture 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 IntroSponsors and Supporters

AIAA would like to thank the following organizations for their support of the 2017 AIAA SciTech Forum:

Premier Sponsor

Executive Sponsor

Livestream Sponsor Student Reception Sponsors

Wedneday Networking Rising Leaders in Aerospace Lanyard Sponsor Coffee Break Sponsor Keynote Speaker and Lunch Sustaining Small Business Sponsor

Supporting Sponsors

High-Voltage Amplifiers Media Sponsor Electrostatic Voltmeters ESD Products

www.aiaa-SciTech.org 10 #aiaaSciTech IntroPre-Forum Activities Continuing Education Offerings Stay at the top of your game with AIAA’s continuing education offerings. You will leave with invaluable knowledge and solutions that you can put to immediate use. Courses Workshops 7–8 January, 0800–1700 hrs Texas 1 7–8 January, 0800–1700 hrs Texas 3 NEW COURSE! Introduction to Shock-Wave/ 2nd AIAA Sonic Boom Prediction Workshop Boundary-Layer Interactions This workshop will cover both the state of the art for (Instructor: Holger Babinsky) predicting near-field sonic boom signatures with CFD as well as propagation of the near-field pressures to the ground. This new course introduces the basics of shock-wave/ boundary-layer interactions (SBLIs). Exercises during the course reinforce the key learning points and enable feedback. Professionals and students new to, or wishing to move into, Sunday, 8 January applications/research areas affected by SBLIs and who need a 1500–1700 hrs Grapevine B thorough introduction should take this course. Meet the Employers AIAA’s Meet the Employers event offers students and young 7–8 January, 0800–1700 hrs Texas 5 professional attendees the opportunity to meet AIAA corporate members. This is a fun and dynamic environment where Six-Degrees-of-Freedom Modeling of Missile and students and professionals interact with organizations regarding Aircraft Simulations employment opportunities. (Instructor: Peter Zipfel) The first hour will consist of 8-minute briefs where participating This course takes you into the inner workings of six-degrees- companies/organizations will present an organizational overview of-freedom modeling—from aerodynamics and propulsion, to and opportunities available. The second hour will be roundtable guidance and control. Engineers tasked to employ, modify, or meet-and-greet sessions, with organizations hosting a table and develop detailed aerospace vehicle simulations and to conduct attendees switching every 10 minutes. performance evaluations would find this course invaluable. Following the event, AIAA will hold its Student Welcome Reception. There is no charge to participate in either the recruiting event or the reception. All students and young 7–8 January, 0800–1700 hrs Texas 4 professionals are invited to attend. No RSVP is required. Liquid Atomization, Spray, and Fuel Injection in Aircraft Gas Turbine Engines 1800–1930 hrs Mission Plaza (Instructor: Bruce Chehroudi) Student Welcome Reception This course provides an understanding of the processes of AIAA SciTech has one of the largest gatherings of students liquid atomization and spray formation and relates of any of the AIAA forums. Come meet fellow students who this understanding to fuel injection systems and emission you are sure to see again throughout the week. Many Student of pollutants in modern engines. Engineers working on the Award winners and presenters will be in attendance. AIAA design of components for high efficiency and performance of Executive Director Sandy Magnus will address the attendees, combustion engines will highly benefit from this course. as will a representative from the corporate sponsors. Members of the AIAA Board of Directors and the Technical Activities Committee will also be in attendance. Take 8 January, 0800–1700 hrs Texas 2 advantage of this chance to meet key members of AIAA and learn about opportunities that are available. NEW COURSE! Hypersonics Test (Instructor: Dan Marren) Sponsored by: This new course introduces the concept of hypersonic flight and describes the critical physics that is encountered at this unique and formidable speed regime. Anyone in the engineering field who has an interest in high-speed systems would benefit from taking this course.

www.aiaa-SciTech.org 11 #aiaaSciTech IntroKeynote 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, 9 January Thursday, 12 January 0800–0900 hrs Texas Ballroom A&B 0800–0900 hrs Texas Ballroom A&B Setting the Landscape — Factors Driving Today’s Disruptive Technology Developments — Disruptive Environment Breakthroughs that will Transform Aerospace Moderator: Robie Samanta Roy, Vice President, Technology Moderator: Samantha Marquart Brainard, Ph.D. Candidate, Strategy & Innovation, Lockheed Martin Corporation George Washington University Panelists: Panelists: Chuck Beames, Consultant Danette Allen, Senior Technologist for Intelligent Flight Carissa Christensen, Managing Partner, The Tauri Group Systems, NASA Langley Research Center David Whelan, Vice President, Engineering & Chief Neil Gershenfeld, Director, The Center for Bits and Atoms, Technologist, Boeing Defense, Space & Security, The Massachusetts Institute of Technology Boeing Company Rob High, Vice President and Chief Technology Officer, IBM George Whitesides, CEO, Virgin Galactic and The Watson Spaceship Company Robert Lutwak, Program Manager, Microsystems Technology Office, DARPA

1700–1830 hrs Texas Ballroom C AIAA Town Hall Meeting (Governance and Open Access) 1730–1930 hrs Texas Ballroom C This session will include important updates about AIAA’s Women at SciTech Social Hour and Keynote governance transition and open access for journal publication. Speaker: Mary “Missy” Cummings, Professor, Pratt School Please attend to learn more about these items and to of Engineering, Duke University, and Director, Humans and understand why they are important to you. Autonomy Laboratory, Duke Robotics Speakers: Governance: James Maser, AIAA President Friday, 13 January Open Access: Frank Lu, Vice President, Publications 0800–0900 hrs Texas Ballroom A&B Tuesday, 10 January Next-Generation Workforce Moderators: Darryll Pines, Dean, A. James Clark School of 0800–0900 hrs Texas Ballroom A&B Engineering and Nariman Farvardin Professor of Aerospace Innovation to Enable NASA’s Journey to Mars Engineering, University of Maryland Speaker: Dava Newman, Deputy Administrator, NASA Panelists: Curt Carlson, Founder & CEO, The Practice of Innovation Wednesday, 11 January Ben Marchionna, Lead System Integration & Test Engineer, SkySpecs 0800–0900 hrs Texas Ballroom A&B Jaiwon Shin, Associate Administrator, Aeronautics Research Disruptive Policy Issues — Presidential Transitions Mission Directorate, NASA Moderator: Ann Zulkosky, Director, NASA Programs, Dennis Todd, Vice President, Engineering – Services and Washington Operations, Lockheed Martin Space Systems Support, Boeing Commercial Airplanes Company Graham Warwick, Technology Managing Editor, Aviation Week & Space Technology Panelists: Russell Chew, Senior Advisor, NEXA Capital Partners Lt. Gen. Henry “Trey” Obering III, United States Air Force (Ret.), Executive Vice President, Booz Allen Hamilton Dorothy Robyn, Independent Consultant/Writer; Former Commissioner, GSA, Public Buildings Service; Former Deputy Under Secretary of Defense (Installations and Environment) Courtney Stadd, Washington Operations, Business Development, TIP Technologies www.aiaa-SciTech.org 12 #aiaaSciTech IntroForum 360

Tuesday, 10 January 0930–1130 hrs Texas Ballroom C Future of the Aerospace Industry and Workforce Needs Moderator: Michael D. Griffin, Chairman and CEO, Schafer Corporation Panelists: These conversations will cover a spectrum of C. Douglas Ebersole, Executive Director, Air Force timely topics including programs, systems, policy, Research Laboratory operations, applications, platforms and more! Kevin Parsons, Director, Innovation and Transformation, Northrop Grumman Corporation Robie Samanta Roy, Vice President, Technology Strategy & Monday, 9 January Innovation, Lockheed Martin Corporation 0930–1130 hrs Texas Ballroom C Kenneth Sanger, Vice President and General Manager, 787 CREATE: Enabling Innovation Through Airplane Development, Boeing Commercial Airplanes Computational Prototypes and Supercomputers Lisa Teague, Director, Research and Technology Strategy, Rolls-Royce Corporation Moderator: Paul Nielsen, Director and CEO, Software Engineering Institute, Carnegie Mellon University Panelists: 1400–1600 hrs Texas Ballroom C Edward Kraft, Technical Advisor, Air Force Test Center, Air Geoengineering to Mitigate Climate Change — Force Materiel Command, United States Air Force Is There a Role for Aerospace? Robert L. Meakin, CREATE Air Vehicle Project Manager, High Performance Computing Modernization Program, Moderator: Marty Bradley, Technical Fellow, The Boeing Company Department of Defense Panelists: Scott A. Morton, CREATE, Kestrel Principal Software Martin Bunzi, Professor, Department of Philosophy, Rutgers Developer, High Performance Computing Modernization University Program, Department of Defense William Burns, Co-Director, Forum for Climate Engineering Robert Narducci, Technical Fellow, The Boeing Company Assessment, American University Douglass Post, Associate Director, High Performance Timothy Langenkamp, Partner, Sidley & Austin Computing Modernization Program, Department of Defense Doug MacMartin, Research Professor, Computing + Brian Smith, Lockheed Martin Fellow, ADP Program and Mathematical Sciences, California Institute of Technology, and Technology Integration, Lockheed Martin Aeronautics Senior Research Associate, Department of Mechanical and Aerospace Engineering, Cornell University 1400–1600 hrs Texas Ballroom C NASA Langley Centennial – A Storied Legacy, A Soaring Future Moderator: James R. Hansen, Professor of History & Director, The University Honors College, Auburn University Panelists: Jeremiah Creedon, Center Director 1996–2002 Delma Freeman, Center Director 2002–2003 Roy Bridges, Center Director 2003–2005 Lesa Roe, Center Director 2005–2014 Congratulations to NASA Langley Steve Jurczyk, Center Director 2014–2015 Research Center on its 100th anniversary! David Bowles, Center Director 2015–present Celebrate with AIAA and NASA during the opening of the Exposition Hall, 10 January at 1830 hrs. www.aiaa-SciTech.org 13 #aiaaSciTech

PANTONE 288 C C: 100 M: 80 Y: 6 K: 32 R: 0 G: 45 B: 114

PANTONE 117 C C:6 M: 27 Y: 100 K: 12 R: 201 G: 151 B: 0

IntroForum 360

Wednesday, 11 January Thursday, 12 January 0930–1130 hrs Texas Ballroom C 0930–1130 hrs Texas Ballroom C Space Traffic Management Managing Change During the Development of Moderator: Moriba Jah, Director, Space Object Behavioral Disruptive Technologies Sciences, University of Arizona Moderator: Joycelyn Harrison, Program Manager, Air Force Panelists: Office of Scientific Research Travis Blake, Senior Manager, Advanced Technology Center, Panelists: Lockheed Martin Space Systems Company Irene Gregory, Senior Technologist for Advanced Control P.J. Blount, Adjunct Professor, Mississippi School of Law Theory and Applications, NASA Langley Research Center Mike Gazarik, Vice President, Engineering, Ball Aerospace Rob High, Vice President and Chief Technology Officer, IBM Donald Greiman, Vice President & General Manager, Watson Commercial Space Situational Awareness, Schafer Corporation Steven Huybrechts, Chief of Staff, Applied Minds LLC Lt. Gen. Susan Helms, United States Air Force (ret.) Robert Lutwak, Program Manager, Microsystems Technology George Nield, Associate Administrator, Commercial Space Office, DARPA Transportation, FAA 1400–1600 hrs Texas Ballroom C 1400–1600 hrs Texas Ballroom C NASA Innovative Advanced Concepts (NIAC): Transitioning Your Idea from the Lab to Flight Test Enabling Missions from Venus to Alpha Centauri Moderator: Chris Cotting, Flight Sciences Technical Expert, Moderator: Alvin Yew, Program Manager, NASA Innovative United States Air Force Test Pilot School Advanced Concepts, Space Technology Mission Directorate, Panelists: NASA Albion Bowers, Chief Scientist, NASA Armstrong Flight Panelists: Research Center Geoffrey Landis, Scientist, NASA Glenn Research Center James “Buddy” Denham, Senior Scientific Technical Manager, Mason Peck, Associate Professor, Mechanical and Aerospace Aeromechanics Division, Naval Air Systems Command Engineering, Cornell University Bill Gray, Chief Pilot, United States Air Force Test Pilot School Jonathan Sauder, Technologist, Technology Infusion Group, John S. Langford, Chairman and Chief Executive Officer, NASA Jet Propulsion Laboratory Aurora Flight Sciences Corporation Shawn Whitcomb, Systems Engineer, Advanced Development Programs, Lockheed Martin Corporation Craig Woolsey, Professor of Aerospace and Ocean Engineering, Virginia Polytechnic Institute and State University

www.aiaa-SciTech.org 14 #aiaaSciTech ForumIntro 360

Rising Leaders are graduate students and professionals who are 35 and younger. They are the people who will become the leaders of tomorrow, the inventors of the next great things, and the RISING people who will accept the mantle from those who have forged the way thus far. LEADERS The Rising Leaders in Aerospace multidimensional program features a leadership exchange/ inAEROSPACE speed mentoring, panel session, Q&A with top industry leaders, and multiple opportunities for networking. These exciting and energetic activities aimed at rising leaders in the industry will provide access to top aerospace leaders and their perspectives, with subject matter relevant to your career stage.

Monday, 9 January Wednesday, 11 January 1900–2030 hrs Mission Plaza 1500–1700 hrs Grapevine A Reception Diversity and Inclusion in the Workplace The reception will kick off the Rising Leaders in Aerospace events The AIAA Young Professional Committee and the Diversity and is a perfect opportunity for young leaders to mingle with Working Group have teamed up on this program. It will begin others that will be participating in AIAA SciTech as an attendee, with a presentation on diversity in the workplace. A discussion presenter, or veteran professional. Come meet other participants of how things are changing and what can be expected as you in a casual environment, all rising leaders are welcome. enter the workforce will be presented. Everyone will interact with diversity in the workplace. Hear some ideas on what you can expect to see and what you may be able to influence. Tuesday, 10 January There will then be a discussion of what the AIAA Diversity 1600–1730 hrs Grapevine A and Inclusion Plan entails: current state, challenges, and goals. Through facilitation and audience participation we Leadership Exchange and Speed Mentoring hope to elicit inputs from different perspectives: AIAA national, technical and program committees, regions, sections, Young professionals and students can speak with top leaders campuses, and corporations. Help be a part of forging AIAA’s of AIAA and the aerospace industry. They will provide insight diversity plan and its response to diversity in the aerospace and information about their careers and how they navigated industry. to where they are now. Top professionals from government, academia, and industry will be participating. Get sage advice from people who want to help the next generation of aerospace professionals succeed. Thursday, 12 January 1230–1400 hrs Grapevine A Mentors include: Nancy Andersen, Johns Hopkins University Applied Rising Leaders Speaker and Box Lunch Physics Laboratory Allen Arrington, NASA Glenn Research Center A New Era in Aviation Brad Belcher, Rolls-Royce Corporation Presenter: Jaiwon Shin, Associate Administrator, Aeronautics Terry Burress, Lockheed Martin Corporation Research Mission Directorate Ferdinand Grosveld, Northrop Grumman Corporation Mr. Shin co-chairs the National Science & Technology Basil Hassan , Sandia National Laboratories Council’s Aeronautics Science & Technology Subcommittee. Timothy Hinerman, Blue Origin He has worked at several NASA centers and has great insight on many different aspects of the industry. Come hear what his Sandra Magnus, AIAA thoughts are for rising leaders in the industry. Benjamin Marchionna, Skyspecs A limited number of box lunches will be available on a first- Jill Marlowe, NASA Langley Research Center come, first-served basis. James Maser, Pratt & Whitney Dimitri Mavris, Georgia Institute of Technology Sponsored by: David Riley, The Boeing Company Al Romig, National Academy of Engineering John Rose, The Boeing Company Tony Springer, NASA Headquarters Rob Vermeland, Lockheed Martin Aeronautics Woodrow Whitlow, Cleveland State University www.aiaa-SciTech.org 15 #aiaaSciTech IntroSpecial Sessions and Events

Monday, 9 January Tuesday, 10 January 1230–1400 hrs Texas Ballroom A&B 1730–1830 hrs Texas Ballroom C Durand Lecture for Public Service and Luncheon Dryden Lecture in Research NSF’s 10 Big Ideas: Understanding Science, Maturation of Active Flow Control Concepts for Discovering Breakthroughs, and In uencing Improved Aircra Performance Public Policy Israel J. Wygnanski, Professor, Aerospace Engineering, France A. Córdova, Director, National Science Foundation University of Arizona The Durand Lecture, named in honor of William F. Durand, The Dryden Lecture in Research, named in honor of Dr. is presented to showcase notable achievements by a scientific Hugh L. Dryden who was one of America’s most prominent or technical leader whose contributions have led directly aeronautical engineers, showcases research scientists and to the understanding and application of the science and engineers. The lecture emphasizes the great importance of technology of aeronautics and astronautics for the betterment basic and applied research to the advancement in aeronautics of mankind. Lunch will be provided to the first 200 guests on and astronautics, and is open to attendees and the general a first-come, first-served basis. The lecture will be presented public. after lunch and is open to all attendees at that time. Sponsored by: Wednesday, 11 January 1500–1700 hrs Grapevine A 0930–1700 hrs Pecos 1, Pecos 3, Longhorn D Diversity and Inclusion in the Workplace The AIAA Young Professional Committee and the Diversity AIAA Foundation International Student Conference Working Group have teamed up on this program. It will begin The first-place winners of the AIAA Regional Student with a presentation on diversity in the workplace. A discussion Conferences, which took place in the spring, will gather of how things are changing and what can be expected as you to present their research to a team of judges made up of enter the workforce will be presented. Everyone will interact professional members in the industry. The students will have with diversity in the workplace. Hear some ideas on what you four consecutive sessions in the categories of Undergraduate, can expect to see and what you may be able to influence. Masters, Team, and Community Outreach. There will then be a discussion of what the AIAA Diversity and Inclusion Plan entails: current state, challenges, and goals. Through facilitation and audience participation we Reception: 1830–1915 hrs Texas Ballroom Foyer (no ticket needed) hope to elicit inputs from different perspectives: AIAA Dinner: 1930–2230 hrs Texas Ballroom A&B (ticket required) national, technical and program committees, regions, sections, campuses, and corporations. Help be a part of forging AIAA’s 2017 Associate Fellows Recognition Ceremony diversity plan and its response to diversity in the aerospace and Dinner industry. Each year, the Institute recognizes exemplary professionals for their accomplishments in engineering or scientific work, outstanding merit and contributions to the art, science, or 1630–1800 hrs Exposition Hall; Longhorn E&F technology of aeronautics or astronautics. Please support your colleagues and join us for the induction of the 2017 Corporate Member & Exhibitor Reception Associate Fellows. The reception is open to all who would like to congratulate the newest members of the Class of 2017. Tickets to this celebrated event are available on a first-come, first-served basis and can be purchased for $100 via the AIAA SciTech Forum registration form, or onsite (based on availability).

www.aiaa-SciTech.org 16 #aiaaSciTech IntroSpecial Sessions and Events

Wednesday, 11 January 1700-1830 Dallas 5 Emerging Technologies Identiﬁcation Session The AIAA Emerging Technologies Committee (ETC) identifies emerging technologies, programs, and trends that AIAA should be infusing into its activities. The committee would like to leverage the wisdom of the SciTech crowd to expand its list of topics and to identify high priority areas we should be looking to grow into. Please join the ETC for a relaxed, social brainstorming session that will allow you to voice your opinion about the most important emerging areas you think the Institute should be watching. Thursday, 12 January 1730–1930 hrs Texas Ballroom C Women at SciTech Social Hour and Keynote e Workplace of the Future: Technology Traps and Leadership Challenges Speaker: Mary “Missy” Cummings, Professor, Pratt School of Engineering, Duke University, and Director, Humans and Autonomy Laboratory, Duke Robotics

www.aiaa-SciTech.org 17 #aiaaSciTech UP HERE WE DON’T HEAR “NO.” WE DON’T UNDERSTAND “CAN’T,” AND “IMPOSSIBLE” ISN’T IN OUR VOCABULARY. UP HERE IT’S ABOUT POSSIBILITIES. IT’S ABOUT A WORKING LABORATORY SET TO TEMPERATURES OF 380 DEGREES BELOW ZERO. IT’S ABOUT A FRONT-ROW SEAT TO THE BIRTH OF OUR UNIVERSE AND EVERY LIFE-SUSTAINING EXOPLANET THEREAFTER. IT’S ABOUT LOOKING UP AND KNOWING THERE IS NO LIMIT BECAUSE IF THERE’S ONE THING WE’VE LEARNED FROM THE PAST, IT’S THAT WE AS HUMANS HAVE ALWAYS UNDERESTIMATED THE POSSIBILITIES OF THE FUTURE. IT’S ABOUT PINPOINT PRECISION AND THE CONFIDENCE IN KNOWING WE’RE READY FOR THE SURPRISES THE UNIVERSE ALWAYS PROVIDES IN SUCH AN AMBITIOUS UNDERTAKING. UP HERE IT’S ABOUT PERFORMANCE.

www.northropgrumman.com/space

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, 10 January

0900–1430 hrs Longhorn D Mustang 4 Generation STEM: Discovering Aerospace Career Workshop: Tools to Ensure Your through Experience Career Success Hosted by the Lockeed Martin Corporation and the AIAA Career success in the aerospace field relies more than on Foundation, Generation STEM will be a day filled with fun just technical knowledge. You will also benefit from strong and interactive educational STEM experiences for middle networks, mentoring opportunities, and interviewing skills school students. to name a few. This workshop addresses ways that both those Generation STEM is designed to engage and stimulate entering the workforce and those with more experience can students by allowing them to participate in mini design manage their career path effectively. competitions and challenges, view engaging demonstrations 0930–1000 hrs from various aerospace companies, learn more about aerospace careers, and discover aerospace findings that are Networking Eectively impacting everyday life. Networking is a vital skillset to help advance your career. Conference attendees are encouraged to stop by during This panel session will highlight how to network effectively the afternoon program to inspire, encourage, or guide the and include a discussion on how to balance new technologies students. Or just come to observe the activities and take ideas while building personal connections. back to your section. Moderator: Michael Mohr, Student, Iowa State University Stop in for a few minutes or hang out for the afternoon. Networking Introduction Presentation: Michael Mohr Panel on Networking: Edward Burnett, Senior Technical Fellow, Lockheed Martin Corporation Networking Challenge Activity: Michael Mohr

1000–1115 hrs Getting the Most from Mentoring How do you find the right mentorship relationship? How do you ensure you are getting the most out of the mentorship? This session will include best practices in mentoring and explore how to build a strong partnership between mentee and mentor so that both sides benefit from the process with real-life experiences and observations. Moderator: Angela Trego, Assistant Professor, Utah Valley University, and Structures Director, Practical Aeronautics, Inc. Panelists: Kevin Melcher, Team Lead, Systems Health Management Methods for Space Exploration, NASA Glenn Research Center (Northern Ohio Section, mentor) Abigail Sevier,(Northern Ohio section, mentee) Brett Anderson, Senior Management Leader, Boeing Defense and Space (mentor)

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

Tuesday, 10 January (continued) Wednesday, 11 January

Mustang 4 1800–1930 hrs Texas Ballroom D Career Workshop: Tools to Ensure Your Design/Build/Fly (DBF) Discussion Career Success In recent years the popularity of and excitement surrounding the AIAA Foundation/Textron Aviation/Raytheon Missile 1130–1230 hrs Systems DBF has been growing by leaps and bounds. In the last three years over 100 teams and universities have shown Navigating Your Career When the interest in participating each year. And over 600 students have Unexpected Happens shown up onsite each year to participate in the flyoff. What happens when something goes wrong in your career and The organizers of the competition would love to hear your how can you make the most of opportunities? How do you input on how the competition can or should grow over the navigate unplanned career changes? How can you expect the coming years. They are inviting people who have participated unexpected? During this panel discussion, individuals well in the past, people participating this year, and students known in their fields will share their stories. and faculty who might like to participate in the future to Moderator: Jeff Jepson, Senior Systems Engineer I, GNC / join us for a discussion focusing on the competition’s past Guidance Design & Performance, Raytheon Missile Systems success and future growth. AIAA and the organizers would like to continue this success and expand to be an amazing Panelists: competition for even more teams. It may take a few iterations Jill Marlowe, Research Director, NASA Langley Research Center of the competition to implement some ideas that come forth, Laura McGill, Vice President, Engineering, Raytheon Missile but don’t miss this opportunity to provide your meaningful Systems input into this unique competition. Darryll Pines, Dean, A. James Clark School of Engineering Please note this discussion is about the competition as a whole and Nariman Farvardin Professor of Aerospace and will not address this year’s rules or previous year’s rules/ Engineering, University of Maryland results.

1400–1530 hrs Interviewing to Make an Impression Panel discussion during which HR and hiring managers will address the different aspects of recruiting process within an organization. Moderator: Eric Best, Control Systems Design and Analysis – EV41, Skill Lead, Jacobs ESSSA Group Panelists: Samantha Magill, Special Projects, Inclusion & Diversity, Honda Aircraft Company Cara Lundquist, Director, Talent Acquisition, Lockheed Martin Aeronautics Company Drew Robbins, Senior Manager, F-35 Utilities and Subsystems, Lockheed Martin Aeronautics Company

1530–1600 hrs Networking Eectively (continued) An interactive opportunity to share your experiences with the networking assignment given at the start of the workshop and hear what others learned from it. Moderator: Michael Mohr, Student, Iowa State University Panelist: Jenna Eppink, NASA Networking Activity Results www.aiaa-SciTech.org 20 #aiaaSciTech IntroNetworking 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 Welcome Reception Ice Cream Break in the Exposition Hall Sunday, 8 January Mission Plaza Tuesday, 10 January 1800–1930 hrs 1530–1600 hrs AIAA SciTech has one of the largest gatherings of students All attendees are welcome! of any of the AIAA forums. Come meet fellow students who you are sure to see again throughout the week. Many Student Award winners and presenters will be in attendance. AIAA Welcome Reception Executive Director Sandy Magnus will address the attendees, as will a representative from the corporate sponsors. Tuesday, 10 January Exposition Hall; Longhorn E & F 1815–2000 hrs Members of the AIAA Board and the Technical Activities Committee will also be in attendance. Take advantage of A welcome reception will be held on Tuesday, 10 January, this chance to meet key members of AIAA and learn about in the Exposition Hall. Take this opportunity to engage new opportunities that are available. contacts and refresh old ones. A ticket for the reception is required and included in the registration fee where indicated. Sponsored by: Additional tickets for guests may be purchased upon registration or on site, as space is available.

Coffee Breaks Luncheon in the Exposition Hall Wednesday, 11 January Exposition Hall; Longhorn E & F Coffee breaks allow even more time for making new contacts, 1230–1400 hrs continuing discussions from sessions, visiting the Exposition Hall, or checking emails and voicemails to keep in touch with A ticket is required and included in the registration fee where the office while you are at the forum. Coffee breaks will be indicated. located in the following locations and times:

Monday, 9 January 0700, 0900 and 1530 hrs; Meeting #AiaaSciTech Tweet Up Room Foyers Wednesday, 11 January Texas Station Sports Bar & Grill 1730 hrs (inside the Gaylord) Tuesday, 10 January 0700 and 0900 hrs; Meeting Room Foyers and 1530 hrs; Exposition Hall Sponsored by: Women at SciTech Social Hour and Keynote Thursday, 12 January Texas Ballroom C 1730–1930 hrs Women are underrepresented in the engineering sciences and Wednesday, 11 January 0700 hrs; Meeting Room Foyers and industry, and this event will provide an opportunity to meet 0900, 1530 hrs; Exposition Hall informally, network, discuss experiences and identify women Sponsored by: who are leaders in their fields for possible special recognition by AIAA. The speaker for the event will be Mary “Missy” Cummings of Duke University. There is no charge to attend this event and all attendees are welcome. Thursday, 12 January 0700 and 1530 hrs; Meeting Room Foyers and 0900 hrs; Exposition Hall Friday, 13 January 0700 and 0900 hrs; Meeting Room Foyers

www.aiaa-SciTech.org 21 #aiaaSciTech Recognition Events

For over 75 years, AIAA has been a champion to make sure that aerospace professionals are recognized for their contributions. Join with us throughout AIAA SciTech Forum as AIAA celebrates 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, 9 January Tuesday, 10 January 0930–1030 hrs Texas Ballroom D 0930–1130 hrs Texas Ballroom D Non-Deterministic Approaches Lecture Adaptive Structures Lecture and Special A Perspective on Model Uncertainty Presentation Ali Mosleh, Distinguished Professor, Evelyn Knight Chair in Requirements for Morphing from an Airplane Engineering, University of California, Los Angeles Perspective Speaker: Robert D. Gregg, Chief Aerodynamicist, Boeing 1400–1530 hrs Texas Ballroom D Commercial Airplanes Special Presentation: Spacecraft Structures Lecture and Panel Remembrance of the Contributions of Dr. Friedrich Straub Bridging the Gap from Technology to Space ight 1230–1400 hrs Texas Ballroom A&B Moderator: Mark Thomson, Chief Engineer, Northrop Grumman Astro Aerospace Recognition Luncheon: Celebrating Achievements Panelists: in Aerospace Sciences and Information Systems Hiraku Sakmoto, Associate Professor, Tokyo Institute of Join colleagues and friends to celebrate innovations and Technology achievements! A ticket for the luncheon is required and Jeanette Domber, Payload Systems Engineer, Ball Aerospace included in the registration fee where indicated. Additional tickets for guests may be purchased upon registration as space Roberta Ewart, Chief Scientist, Space and Missile Systems is available. Center, Air Force Space Command The following awards will be presented: Reception: 1830–1915 hrs Texas Ballroom Foyer Aerospace Software Engineering Award Dinner: 1930–2230 hrs Texas Ballroom A&B Lyle N. Long Distinguished Professor of Aerospace Engineering, 2017 Associate Fellows Recognition Ceremony Computational Sciences and Mathematics and Dinner The Pennsylvania State University University Park, Pennsylvania Each year, the Institute recognizes exemplary professionals for their accomplishments in engineering or scientific work, “For inspiration, innovation, and enormous dedication to outstanding merit and contributions to the art, science, or modernizing aerospace engineering education and research over technology of aeronautics or astronautics. Please support several decades.” your colleagues and join us for the induction of the 2017 de Florez Award For Flight Simulation Associate Fellows. The reception is open to all who would like to congratulate the newest members of the Class of Joseph F. Horn 2017. Tickets to this celebrated event are available on a first- Professor of Aerospace Engineering come, first-served basis and can be purchased for $100 via The Pennsylvania State University the AIAA SciTech Forum registration form, or onsite (based University Park, Pennsylvania on availability). “For pioneering contributions to rotorcraft flight simulation and education, including piloted ship-board landing and real-time simulation of coupled flight dynamics, ship-air wake modeling, and acoustics.”

www.aiaa-SciTech.org 22 #aiaaSciTech IntroRecognition Events

Tuesday, 10 January (continued) Intelligent Systems Best Paper AIAA 2016-2133, “Review of Proactive Safety Metrics for J. Leland Atwood Award Rotorcraft Operations and Improvements Using Model-Based John L. Crassidis Parameter Synthesis and Data Fusion,” Alexia Payan, Alek Gavrilovski, Hernando Jimenez, and Dimitri Mavris, Georgia CUBRC Professor in Space Situational Awareness Institute of Technology. Director, Center for Multisource Information Fusion University at Buffalo Modeling and Simulation Technologies Best Paper Amherst, New York AIAA 2016-1180, “Development of Spatial Disorientation “For your commitment to excellence in aerospace engineering Demonstration Scenarios for Commercial Pilot Training,” education.” David H. Klyde, Amanda Lampton, and Philip Schultze, Systems Technologies, Inc. Lawrence Sperry Award Announcement of Student Paper Competition Winners Karen T. Berger Aerospace Engineer Aerothermodynamics Branch NASA Langley Research Center Wednesday, 11 January Hampton, Virginia 1800–1900 hrs Texas Ballroom C “For outstanding contributions to hypersonic boundary layer transition through supporting Space Shuttle in-orbit damage Structures, Structural Dynamics, and Materials Lecture assessment and leading the Shuttle Boundary Layer Transition Flight Experiment Project.” Challenges in Integrated Computational Materials Mechanics and Control of Flight Award Engineering of Aerospace Composites Robert E. Skelton Anthony M. Waas, Boeing-Egtvedt Endowed Chair; Professor of Aerostructures; Chair, William E. Boeing Department of TEES Distinguished Professor Texas A&M University Aeronautics and Astronautics, University of Washington College Station, Texas “For lasting contributions at the interfaces of mechanics and Thursday, 12 January control of flight and leading the world in analysis, design, modeling and control of tensegrity structures.” 1200–1400 hrs Texas Ballroom A&B Abe M. Zarem Award for Distinguished Achievement— Recognition Luncheon—Celebrating Achievements Astronautics in Aerospace Design/Structures and Aerospace Christopher T. Lyne Literature Vanderbilt University Speaker: Walt Downing, Executive Vice President, Southwest Nashville, Tennessee Research Institute “Design and Test of a 10N Hydrogen-Peroxide Join colleagues and friends to celebrate innovations and Monopropellant Thruster” achievements! A ticket for the luncheon is required and included Abe M. Zarem Educator Award—Astronautics in the registration fee where indicated. Additional tickets for guests may be purchased upon registration as space is available. Amrutur V. Anilkumar Professor, Department of Mechanical Engineering The following awards will be presented: Vanderbilt University Nashville, Tennessee AIAA-ASC James H. Starnes Jr. Award Anthony M. Waas Flow Control Conference Best Paper Boeing-Egtvedt Endowed Chair AIAA 2016-4081, “Aerodynamic Flow Control of Wake University of Washington Dynamics Coupled to a Moving Bluff Body,” Thomas J. Seattle, Washington Lambert, Bojan Vukasinovic, and Ari Glezer, Georgia Institute of Technology. “For impactful contributions to experimental, analytical and computational aspects of composite structural mechanics, Guidance, Navigation and Control Best Paper commitment to mentoring the next generation, and service to AIAA 2016-2099, “Stability Augmentation and Active Flutter the field.” Suppression of a Flexible Flying-Wing Drone,” David K. Schmidt, University of Colorado-Colorado Springs.

continued www.aiaa-SciTech.org 23 #aiaaSciTech IntroRecognition Events

Thursday, 12 January (continued) Pendray Aerospace Literature Award Ashwani K. Gupta Ashley Award for Aeroelasticity Distinguished University Professor Charbel Farhat Department of Mechanical Engineering Vivian Church Hoff Professor of Aircraft Structures University of Maryland Chairman, Department of Aeronautics and Astronautics College Park, Maryland Stanford University “For exemplary contributions to the aerospace literature Stanford, California especially on swirl flows and high temperature combustion “For recent development of powerful reduced-order models that technology and for his services as book series editor and associate have revolutionized computational aeroelasticity and fluid- editor of journals.” structure interaction by allowing the simulation of complete ASME/Boeing Best Paper Award practical aircraft configurations.” AIAA 2016-0936, “A Coupled Electromechanical Peridynamics Children’s Literature Award Framework For Modeling Carbon Nanotube Reinforced Andrea Beaty Polymer Composites,” Naveen Prakash and Gary Seidel, Virginia Polytechnic Institute and State University. Children’s Author For the book: “Rosie Revere, Engineer” Collier Research Hypersizer/AIAA Structures Best Paper AIAA 2016-0733, “Effect of Notch on the Failure Response History Manuscript Award of Oxide/Oxide Ceramic Composites,” Dianyun Zhang, Layne Karafantis University of Connecticut; Pascal Meyer, University of Museum Curator, Modern Military Aircraft Michigan; and Anthony Waas, University of Washington. Smithsonian National Air & Space Museum Announcement of Student Competition Winners Washington, D.C. For the manuscript: “Under Control: Constructing the Nerve Centers of the Cold War”

www.aiaa-SciTech.org 24 #aiaaSciTech IntroExposition Hall

The Exposition Hall, located in Longhorn E & F, 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 Video Drone Rafﬂe

Tuesday, 10 January 1300–1630 hrs Enter to win a video drone! Complete the raffle ticket (behind Opening Reception* 1815–2000 hrs your registration badge) and drop it in the boxes in the Wednesday, 11 January 0845–1630 hrs Exposition Hall, or drop in a business card. Winner will be notified by email and does not need to be present to win. Luncheon* 1230–1400 hrs Thursday, 12 January 0845–1400 hrs

*A ticket is required to attend.

AIAA Pavilion Stop by the AIAA Pavilion, located in the Exposition Hall, AIAA Foundation to browse publications and merchandise, learn about your membership benefits, and meet AIAA staff. With our Match a Million program, AIAA will match gifts to the Foundation up to $1 million, doubling the 30% Off All Books at AIAA SciTech Forum impact of every donation. AIAA Publications is offering a special show discount on all When you donate to the AIAA Foundation you are investing titles featured at AIAA SciTech Forum. Attendees can take in the next generation of aerospace professionals through advantage of a 30% discount off the list price of all books for innovative, educational programs and recognition. An sale at the AIAA Bookstore located in the AIAA Pavilion. investment that will ensure the continuation of our industry’s This show special will only be available during the forum! leadership and contributions to global advancement. Take advantage of these super savings and visit the AIAA Bookstore! In addition, be sure and stop by the booth and check out the silent auction as there are some really cool aerospace items up Meet the Author Sessions for bid!

Thomas R. Yechout Introduction to Aircraft Flight Mechanics, 2nd Edition Tuesday, 10 January AIAA Exposition Hall Pavilion Opening Reception, 1815–2000 hrs

Daniel P. Raymer Aircraft Design, 5th Edition and RDSW in Student Wednesday, 11 January AIAA Exposition Hall Pavilion Luncheon, 1230–1400 hrs

www.aiaa-SciTech.org 25 #aiaaSciTech ExpositionIntro Hall

AIAA PAVILION EXHIBITOR LOUNGE /SALES OFFICE

Cradle North America 328 427 ciences

225 326 National Research Jama Phoenix Council of Software Integration CANADA 224 323 423 424 523 524 623 624 GRW • MathWorks Kamatics • RWG 321 322 421 521 522 Convergent Vision Calspan Hadland Kulite Semiconductor Research Corporation Imaging Science Products 219 220 319 420 519 520 619 dSpace Alpha Inc. Space 217 318 417 617 618 LaVision 215 316 415 Cambridge NUMECA University Press SG 414 513 USA 213 214 313 ANSYS 614 NAFEMS 412 511 ESTECO 211 212 311 Boeing 512 611 612 j2 PCB Piezotronics Inc. 209 310 610

Nanovea Northrop Grumman NASA Corporation 207 Langley Siemens AIAA North 100th Texas Chapter 406 205 206 305 506 606 IC2 203 304

ENTRANCE

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Exhibitors by Booth Number (êindicates AIAA Corporate Members)

305 Aerion Technologies (formerly Desktop 512 Lockheed Martin ê ê Aeronautics) 521 MathWorks 205 AIAA North Texas Chapter 322 Metacomp Technologies 323 Airborne Systems ê 212 NAFEMS 618 Alpha Space 207 NANOVEA 412 ANSYS, Inc. 406 NASA 225 Aurora Flight Sciences ê 506 NASA Langley 100th 414 BETA CAE Systems USA Inc. 417 National Academies of Sciences, Engineering, 310 Boeing Technology Services ê and Medicine 319 Calspan Systems Corporation 423 National Institute of Aerospace (NIA) ê 519 Cambridge Flow Solutions 326 National Reconnaissance Office (NRO) 213 Cambridge University Press 524 National Research Council of Canada 421 Computational Engineering International (CEI) 206 Northrop Grumman Corporation 219 Convergent Science 614 NUMECA-USA, Inc. 427 Cradle North America 611 Office of Naval Research 318 Cray Inc. 610 PCB Piezotronics Inc. 215 Dantec Dynamics, Inc. 624 Phoenix Integration Inc. 211 DARcorporation ê 513 Photron 617 dSPACE Inc. ê 420 Pointwise, Inc. ê 313 Ennova-CFD 523 Polytec Inc. 612 ESTECO 214 SG 321 Granta Design 606 Siemens 522 GRW • Kamatics • RWG 424 SmartUQ 520 Hadland Imaging 328 Space Electronics 415 Hypersizer - Collier Research Corporation ê 311 Tecplot, Inc. ê 203 IC2 511 Tri Models, Inc. 304 Intelligent Light ê 220 Vision Research 209 j2 Aircraft Dynamics Ltd. 224 TSI, Inc. 623 Jama Software 217 XFlow CFD ê 619 Kulite Semiconductor Products, Inc. 316 LaVision, Inc.

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Aerion Technologies (formerly Desktop Aeronautics) 305 ANSYS, Inc. 412 1900 Embarcadero Road 2600 ANSYS Drive Suite 101 Canonsburg, PA 15317 Palo Alto, CA 94303 www.ansys.com www.desktopaero.com [email protected] [email protected] If you’ve ever seen a rocket launch, flown on an airplane, Aerion Technologies (formerly Desktop Aeronautics) creates driven a car, used a computer, touched a mobile device, crossed tools for aerodynamic design and analysis of aerospace a bridge, or put on wearable technology, chances are you’ve vehicles. Our flagship product, GoCart, is an intuitive aerial used a product where ANSYS software played a critical role vehicle design tool built around NASA’s renowned Cartesian in its creation. ANSYS is the global leader in engineering Euler CFD solver, Cart3D. Our customer list includes the simulation. We help the world’s most innovative companies major players from the aerospace and defense industry. deliver radically better products to their customers by offering the best and broadest portfolio of engineering simulation software. AIAA North Texas Chapter 205 1 Lockheed Blvd. PO Box 748, MZ 1527 Aurora Flight Sciences 225 Attn: James Sergeant 9950 Wakeman Drive Fort Worth, TX 76101 Manassas, VA 20110 info.aiaa.org/Regions/SC/North_Texas/default.aspx www.aurora.aero [email protected] Aurora Flight Sciences has over 25 years developing The North Texas Section is one of the largest and dynamic innovative, highly capable unmanned aircraft for national sections in AIAA with 800 professional and student members. security requirements. From our Optionally Piloted Centaur, to our 5-day endurance Orion RPA, and our new DARPA VTOL X-Plane Technology Demonstrator, Aurora delivers! Airborne Systems 323 Contact us for an in-depth discussion of our solutions. Aurora 5800 Magnolia Avenue is currently hiring – “Come Build The Future With Us” Pennsauken, NJ 08109 www.airborne-sys.com [email protected] BETA CAE Systems USA, Inc. 414 Airborne Systems is the world leader in the design, 29800 Middlebelt Road development, fabrication, test and integration of Entry Descent Suite #100 and Landing Systems (EDLS), including parachutes systems, Farmington Hills, MI 48334 www.ansa-usa.com Air Bag Landing Attenuation systems, Inflatable Aerodynamic [email protected] Decelerators. We provide EDLS systems for various aircraft and spacecraft and is leading the development of new BETA CAE Systems is an engineering services company that technologies including Inflatable Aerodynamic Decelerators. distributes & supports the industry leading ANSA & META software. ANSA is a CAE pre-processing and morphing tool for FE & CFD Analysis, for full-model build, from CAD to Alpha Space 618 solver input file, in one integrated environment. 930 Gemini Ave Houston, TX 77058 www.alphaspace.com Boeing Technology Services 310 Alpha Space is a woman-owned company serving the 7755 E. Marginal Way S Mail Code 1W-02 research community with unparalleled access to/from the ISS. Seattle, WA 98108 Alpha Space owns and operates MISSE, a flight facility affixed www.boeing.com/bts to the exterior of the ISS where experiments endure extreme levels of solar and charged-particle radiation, atomic oxygen, Boeing Technology Services provides access to testing facilities, hard vacuum, and extreme temperatures. The MISSE platform equipment and technical expertise that have produced some yields accelerated and accurate testing for experiments ranging of today’s most innovative products. No other company from space suits, components and flight hardware to car paint can provide the same range of competitively-priced, high- and electronics. quality testing capabilities. Timely, accurate, consistent and repeatable test results can be the differentiators that produce sales. Capitalize on access to proven expertise and resources in aerodynamics, propulsion, acoustics, environmental, electromagnetics, structures, metrology, simulation and materials.

www.aiaa-SciTech.org 28 #aiaaSciTech Exhibitors Calspan Systems Corporation 319 Convergent Science 219 703 City Center Blvd. 1619 Common Ste 1204 Newport News, VA 23606 New Braunfels, TX 78132 www.calspan.com convergecfd.com [email protected] Calspan-Force Measurement Systems develops state of the art internal and external type balances, and model position Convergent Science specializes in modeling flow, spray, / motion control systems. Our expert staff specializes in the heat transfer and combustion using our CONVERGE CFD development, analysis, design, fabrication, instrumentation, software. CONVERGE generates an orthogonal mesh calibration and integration of balances and model positioning automatically at runtime even for complicated and moving systems. Our Force type balances offer unique capabilities that geometries. CONVERGE is ideally suited to model all aspects other types of balances do not. of gas turbine combustion including flame shape, emissions, wall temperatures, lean blowout, ignition and flashback. Cambridge Flow Solutions 519 Compass House Cradle North America, Inc. 427 VIsion Park 50 Chestnut Street, Suite A-214 Histon Beavercreek, OH 45440 Cambridge, Cambs UK CD24 www.cradle-cfd.com 9AD [email protected] www.cambridgeﬂowsolutions.com admin@cambridgeﬂowsolutions.com Software Cradle is a leading provider of Computational Fluid Dynamics (CFD) software including SC/Tetra (general Cambridge Flow Solutions conducts strategic, long-term purpose unstructured mesh), scSTREAM (general purpose research with Development Partners. Our work is focussed on Cartesian mesh), and HeatDesigner (Cartesian mesh for BOXER – a fully scalable simulation environment coupling an electronics). Since inception in 1984, Cradle has established advanced digital geometry model, mesh generation and CFD itself as a major innovator that is advancing the role of – aimed at complex, real-world, conjugate applications. CFS simulation in engineering design. markets BOXERmesh and advanced higher-order LES. Cray, Inc. 318 Cambridge University Press 213 901 Fifth Avenue Suite 1000 1 Liberty Plaza Seattle, WA 981642 20th Floor www.cray.com New York, NY 10006 [email protected] www.cambridge.org Global supercomputing leader Cray builds innovative systems [email protected] and solutions enabling researchers in academia, government, Cambridge University Press’ publishing in books and journals and industry to meet existing and future simulation and combines state-of-the-art content with the highest standards of analytics challenges. scholarship, writing and production. Visit our stand to browse new titles, available at 20% discount, and to pick up sample copies of our journals. Visit our website to find out more Dantec Dynamics, Inc. 215 about what we do: www.cambridge.org/academic. 750 Blue Point Road Holtsville, NY 11742 www.dantecdynamics.com Computational Engineering International 421 [email protected] 2166 N. Salem Street Dantec Dynamics develops and manufactures measurement Apex, NC 27523 systems that determine physical properties in fluids and in www.ensight.com solid structures. We deliver turnkey as well as customized [email protected] solutions with user-friendly software. Furthermore, our clients CEI makes EnSight the leading CFD post-processor for large benefit from superior technical application support worldwide. complex data. You gain accurate measurement results easily and quickly which help you accelerate the pace of discovery, innovation, EnSight is easy to use. At SciTech 2017 we will be quality control or NDT. demonstrating the new EnSight 10.2. We will also be privately demonstrating the new software, Nexus, a browser-based tool for processing design studies, parameter studies, organizing a company or department CAE workflow, and generating reports.

www.aiaa-SciTech.org 29 #aiaaSciTech IntroExhibitors

DARcorporation 211 Granta Design 321 1440 Wakarusa Drive 300 Rustat House Suite 500 62 Clifton Road Lawrence, KS 66049 Cambridge, Cambridgeshire UK www.darcorp.com CB1 7EG [email protected] www.grantadesign.com [email protected] DARcorporation has been offering aeronautical engineering software and consulting services since 1991. Our projects Granta helps hundreds of engineering enterprises to manage include single/multi-engine propeller and jet powered aircraft, materials information. Working closely with world-leading Business Jets, Very Light Jets (VLJ), Kit, LSA and Experimental aerospace organizations to help them develop and apply material intelligence, making better materials decisions, saving aircraft, VTOL aircraft, UAVs for civil and military time and money, and reducing risk as they optimize products applications and hybrid air/ground vehicles. and services. Granta also provides supporting resources to thousands of university educators worldwide teaching materials or related engineering topics to the next generation dSPACE Inc. 617 of engineers, scientists, and industrial designers about 50131 Pontiac Trail materials, processes, and sustainability. Wixom, MI 48393-2020 www.dspaceinc.com [email protected] GRW • Kamatics • RWG 522 dSPACE is the world’s leading provider of hardware and 1330 Blue Hills Ave software tools for developing and testing sophisticated Bloomﬁeld, CT 06002 electronic control systems. dSPACE tools are used in high- www.kaman.com/engineered performance engine development, navigation systems, [email protected] propulsion, real-time flight maneuver simulation and other GRW, Kamatics & RWG have been designing, testing, and applications. Learn more at www.dspaceinc.com. manufacturing the highest performing, self-lubricating and high-precision bearings and flight critical parts in the industry, excelling under the most demanding conditions. We work Ennova-CFD 313 hand-in-hand with our customers to design and implement 2150 Allston Way application specific bearing solutions that offer an increase in Suite 250 performance, reliability, and extended service life. Berkeley, CA 94704 www.ennova-cfd.com [email protected] Hadland Imaging 520 Leading edge grid generation software for computational Hadland Imaging West fluid dynamics (CFD). Automated mesh generation for 1414 Soquel Ave unstructured, structured and hybrid grids for internal and Suite #200 external flows. Santa Cruz CA 95062 Hadland Imaging East 10 Park Place ESTECO 612 Suite 507 39555 Orchard Hill Place Butler, NJ 07405 Novi, MI 48375 www.hadlandimaging.com www.esteco.com [email protected] Hadland Imaging - visible & infrared high-speed cameras with offices in California & New Jersey. We are the North American ESTECO is a pioneer in numerical optimization solutions, representatives of the Shimadzu HPV-X2 camera (10million specializing in the research and development of engineering FPS) iXcameras, Highest Resolution in Industry, 2048x1536 software for all stages of the simulation-driven design process. up to 500k FPS and the Full Line of FLIR high-speed and HD ESTECO’s top-class products, modeFRONTIER and VOLTA, Infrared Cameras. www.HadlandImaging.com are used worldwide, helping companies increase efficiency in design simulation and accelerate product innovation.

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HyperSizer® - Collier Research Corporation 415 Jama Software 623 760 Pilot House Dr. Ste. A 135 SW Taylor St. #200 Newport News, VA 2366 Portland, OR 97204 www.hypersizer.com www.jamasoftware.com [email protected] [email protected] Collier Research Corporation provides software solutions, Jama Software is the definitive system of record and action for methods research, and consulting services for the aerospace, product development. The company’s modern requirements wind energy, high speed rail, automotive, and shipbuilding and test management solution helps enterprises accelerate industries with its broad range of structural capabilities. development time, mitigate risk, slash complexity and verify Our company’s flagship product, HyperSizer performs design, regulatory compliance. More than 600 product-centric stress analysis, and detail sizing optimization for vehicles organizations, including NASA, Thales, and Caterpillar have fabricated with composite or traditional metallic materials. On used Jama to modernize their process for bringing complex average, the software reduces the weight of structures by 20-40%. products to market. The company is headquartered in Portland, Oregon. IC2 203 Kulite Semiconductor Products, Inc. 619 4647 NW 6th Street Suite A One Willow Tree Road Gainesville, FL 32609 Leonia, NJ 0765 www.thinkic2.com www.kulite.com [email protected] [email protected] IC2 is a developer and manufacturer of MEMS sensors and Kulite manufactures miniature high frequency pressure instrumentation, primarily for aerodynamic and aeroacoustic transducers, flight qualified pressure transducers, wind measurements. IC2 was founded in 2001 to develop high‐ tunnel engine pressure probes and turbine blade implants, performance, technologically disruptive instrumentation which are used in the development and manufacture of systems. IC2 technologies include MEMS microphones, direct helicopters, business jets, commuters, commercial and military measurement shear‐stress sensors, dynamic pressure sensors, aircraft. They are designed to operate with electromechanical acoustic arrays, and adaptive acoustic liners. indicators, ECU, FADEC and EICAS systems and other aircraft circuits, and are considered the most reliable aircraft pressure Intelligent Light 304 transducers available. 301 Route 17 North Rutherford, NJ 07070 LaVision, Inc. 316 www.ilight.com [email protected] 211 W. Michigan Avenue, Suite100 Intelligent Light provides post-processing, data management Ypilanti, MI 48197 and big data visualization capabilities for CFD. Thousands of www.lavision.com FOCUS ON IMAGING users rely on the industry leading FieldView Sofware and our [email protected] custom engineering services to maximize their productivity and LaVision provides integrated imaging systems to scientific, effectiveness. Let us help you eliminate bottlenecks and achieve industrial and educational markets. LaVision has extensive breakthrough results. experience in optical techniques such as 2-D, stereo, and tomographic particle image velocimetry, gaseous and liquid laser induced fluorescence, shadowgraphy for multi-phase flows, j2 Aircraft Dynamics Ltd. 209 digital image correlation for deformation/strain, high-speed and Daresbury Innovation Centre ultra-high-speed imaging, and intensified camera systems. Keckwick Lane Daresbury, Cheshire WA4 4FS Lockheed Martin 512 United Kingdom www.j2aircraft.com 1011 Lockheed Way [email protected] Palmdale, CA 935997 www.lockheedmartin.com/ J2 Aircraft Dynamics Ltd continues to provide commercial off us/aeronautics/skunkworks.html the shelf aircraft design, analysis and modelling software tools [email protected] built on a single fully supported Framework. Users of j2 software The Skunk Works is focused on the critical aircraft for can analyze a much wider array of options/trade-offs rapidly tomorrow. Advanced technology solutions draw on our world- from conceptual design through to detailed engineering stages class capabilities in conceptual design, systems engineering unlocking more value. J2 validated aircraft models can be ‘flown’ and integration, complex project management, software in desktop to Full Mission Simulators from conceptual design development and rapid prototyping. onwards, accelerating the move to certification. www.aiaa-SciTech.org 31 #aiaaSciTech IntroExhibitors

MathWorks 521 NASA 406 3 Apple Hill Drive 300 E Street Southwest Natick, MA 01760 Washington, DC 20546 www.mathworks.com www.nasa.gov The MATLAB and Simulink product families are fundamental [email protected] applied math and computational tools adopted by more than Since its inception in 1958, the National Aeronautics and Space 5000 universities and colleges. MathWorks products help Administration (NASA) has sought to reach for new heights prepare students for careers in industry, where the tools are and reveal the unknown so that what we do and learn will widely used for data analysis, mathematical modeling, and benefit all humankind. NASA’s priorities are: Earth Right Now algorithm development in collaborative research and new – Your Planet is Changing. We’re on It; Aeronautics– We’re product development. with You When You Fly; International Space Station – Off the Earth, For the Earth; Journey to Mars; Solar System and Beyond; and Technology Powering Exploration. For more Metacomp Technologies 322 information, visit us at: www.nasa.gov. 28632 Roadside Drive, Suite 255 Agoura Hills, CA 91301 www.metacomptech.com NASA Langley Research Center 506 [email protected] Mail Stop 151 Metacomp Technologies develops and disseminates simulation Hampton, VA 23681-2199 software and services in multiple physics areas. ICMP www.nasa.gov/specials/nasalangley100/ (Integral Computational Multi-Physics) is our unified NASA Langley Research Center celebrates vision for Multi-Physics simulations which simplifies the its Centennial on July 17, 2017. For a century, our employees complexities of the individual disciplines. ICMP provides a have been leading innovators in aerospace research and single environment for Mesh Generation, CFD and Structural development. Today, we are building on this storied legacy Analyses, and Visualization of results. of innovation as we continue to conduct groundbreaking research. As we soar into the future, our work will focus on PANTONE 288 C C: 100 M: 80 Y: 6 K: 32 issues that matter to Americans: being able to fly safelyR: 0 G: 45and B: 114 NAFEMS 212 affordably, protecting and preserving our planet, and getting PANTONE 117 C C:6 M: 27 Y: 100 K: 12 130 N Prospect Street humans to Mars. R: 201 G: 151 B: 0 Suite D Granville, OH 43023 www.nafems.org National Academies of Sciences, 417 [email protected] Engineering, and Medicine NAFEMS is a not-for-profit organization aimed at promoting 500 Fifth Street NW best practices and fostering education and awareness in the Washington, DC 20001 engineering analysis community. In line with its objectives to www.nationalacademies.org/rap promote the effective use of simulation technologies, NAFEMS [email protected] is continually seeking to create awareness of new analysis The National Academies of Sciences, Engineering, and methodologies, deliver education and training, and stimulate Medicine conducts the NRC Research Associateship Programs the adoption of best practices and standards by offering a that offer awards for postdoctoral, senior, and graduate platform for continuous professional development. research in US federal laboratories and affiliated institutions. Awards include competitive stipends, relocation, professional NANOVEA 207 travel and a health insurance plan. Complete information and online applications are on the website. 6 Morgan Suite 156 Irvine, CA 92618 www.nanovea.com National Institute of Aerospace (NIA) 423 [email protected] 100 Exploration Way Hampton, VA 23666 Firmly aligned with its vision, Nanovea aims to simplify www.nianet.org advanced measurement technologies to stimulate materials engineering for the common good. Ease of use, advanced The National Institute of Aerospace (NIA) is a non-profit automation and the dedication to superior accuracy are research and graduate education institute created to conduct the driving forces behind its full range of 3D Profilometers, leading-edge aerospace and atmospheric research, develop Mechanical Testers and Tribometers. new technologies for the nation and help inspire the next generation of scientists and engineers.

www.aiaa-SciTech.org 32 #aiaaSciTech IntroExhibitors

National Reconnaissance Office (NRO) 326 Office of Naval Research 611 14675 Lee Road 875 North Randolph Street Chantilly, VA 21051 Arlington, VA 22203 https://acq.westﬁelds.net www.onr.navy.mil [email protected] [email protected] NRO’s Director’s Innovation Initiative invests in advanced The Office of Naval Research’s Naval technologies, fosters innovation, and provides funding to Air Warfare and Weapons division supports the Navy’s power improve our capabilities. It presents an opportunity for projection needs, fostering the technology development of developers not traditionally associated with the NRO to naval aircraft, structures, propulsion, autonomy, energetics, participate in building the NRO of the 21st Century. directed energy and electric weapons. Visit us at Booth #309.

National Research Council of Canada 524 PCB Piezotronics 610 [email protected] 3425 Walden Avenue Depew, NY 14043 www.nrc-cnrc.gc.ca/eng/solutions/ www.pcb.com/aerospace facilities/wind_tunnel_index.html [email protected] The National Research Council of Canada (NRC) Aerospace PCB Piezotronics Inc. is a designer and manufacturer of portfolio offers several wind tunnels located in Ottawa, microphones, vibration, pressure, force, torque, load, and Ontario (Canada). Clients have access to our 5 ft trisonic, strain sensors, as well as the pioneer of ICP® technology. This 6 × 9 ft, 30 ft low-speed, altitude icing, and 10 × 20 ft icing instrumentation is used for flight testing, wind tunnels, modal wind tunnels. These facilities are used to support industry, analysis, satellite testing and acoustics for cabin noise. PCB® government, and university clients as part of NRC’s stands behind their products with valuable services, including Aeronautical Product Development Technologies program. a 24-hour SensorLine, a global distribution network, and the Projects are normally of a customized nature, and extensive industry’s only commitment to Total Customer Satisfaction. efforts are applied to derive innovative approaches in instrumentation, software and operations. Phoenix Integration Inc. 624 1715 Pratt Drive Northrop Grumman Corporation 206 Suite 2000 2980 Fairview Park Drive Blacksburg VA 24060 USA Falls Church, Virginia www.phoenix-int.com www.northropgrumman.com/media [email protected] [email protected] We are the framework for Model-Based Engineering. With Northrop Grumman is a leading global security company ModelCenter® by Phoenix Integration you can integrate your providing innovative systems, products and solutions in engineering simulation tools, explore your product designs, autonomous systems, cyber, C4ISR, strike, and logistics and and organize your engineering knowledge. Achieve a true modernization to government and commercial customers Model-Based Engineering development process with Phoenix worldwide. Through its research, development, design and Integration’s easy-to-use, flexible set of software applications. demonstration activities, the company is helping its customers Shorten design cycles, reduce errors and development costs, all solve their hardest mission problems, particularly those related while improving product performance and quality. to protecting freedom and advancing human discovery. Photron 513 NUMECA-USA, Inc. 614 9520 Padgett Street, 110 1044 Larkin Street San Diego, CA 92126 San Francisco, CA 94109 www.photron.com www.numeca.com [email protected] [email protected] Photron’s varied product range makes it the first choice for NUMECA offers grid generation, CFD tools, and consulting designers, manufacturers, R&D and test engineers to solve targeted to the aerospace industry. NUMECA’s software their most challenging motion problems. Photron’s digital and engineering services cover a wide range of aerospace camera systems can capture thousands of high resolution flow analyses including: passenger aircraft, full aircraft images for playback and analysis. Markets include military, configurations, transonic, supersonic, and hypersonic flows, automotive, broadcast, particle image velocimetry (PIV), aircraft cabins, wing-box fuel tanks and high-lift devices. digital image correlation (DIC), ballistics testing, and more.

www.aiaa-SciTech.org 33 #aiaaSciTech IntroExhibitors Pointwise, Inc. 420 Siemens 606 213 South Jennings Avenue 60 Boradhollow Road Fort Worth, TX 76104 Melville, NY 11747 www.pointwise.com www.siemens.com/mdx [email protected] [email protected] Pointwise, Inc. is solving the top problem facing engineering Siemens PLM Software (www.siemens.com/mdx) is a leading analysts today: mesh generation for computational fluid global provider of simulation software with a vision for dynamics. Manufacturing firms and research organizations Multidisciplinary Design eXploration. Our simulation tools, use Pointwise’s mesh generation software to create the “digital including STAR-CCM+®, allow engineers to discover better geometry” enabling computer simulation of a product’s designs, faster across a wide range of disciplines including performance in a fluid environment. Further information can Computational Fluid Dynamics, Computational Solid be obtained from pointwise.com. Mechanics, heat transfer, particle dynamics, and reacting flow.

Polytec Inc. 523 SmartUQ 424 10245 E. Washington Avenue 16400 Bake Parkway Suite 210 Irvine, CA 92656 Quantify Every Uncertainty. www.polytec.com Madison, WI 53703 [email protected] www.smartuq.com [email protected] At Polytec, we believe that there is a need to measure vibrations SmartUQ software provides breakthrough analytics and in a non-contact manner. Polytec has addressed this need by uncertainty quantification solutions for simulation and testing. designing optical measurement systems. Polytec is the market Using advanced statistics and stochastic methods, SmartUQ leader for non-contact, laser based vibration measurement allows engineers to quickly analyze high-dimensional or Big instrumentation since more than 45 years. Polytec vibrometers Data, understand the probabilities of all what-if scenarios, are utilized in the aerospace field for Engine Testing, accelerate simulation cycles, easily calibrate models, and create Material and Fatigue Testing, Experimental Modal Analysis, innovative designs with greater confidence. Ground Vibration Testing and Shock Testing to name a few applications. Space Electronics 328 SG 214 81 Fuller Way 6A Aigiidon Street Berlin, CT 06037 Athens, Attica Greece 11853 www.space-electronics.com www.sg-incorp.com [email protected] [email protected] Space Electronics is the world’s leading manufacturer of SG Company provides integrated engineering solutions aerospace mass properties measurement instruments. Our for air/space-based earth monitoring systems, develops success is based on our instruments providing the highest special techniques for UAS (Unmanned Aerial Systems) measurement accuracy along with extraordinary reliability. earth observation applications in various disciplines and Space Electronics also manufactures a wide range of igniter offers customized structural technical infrastructure studies. circuit testing products for use in electro-explosive devices. SG-Space & Ground Engineering Solutions has extensive Our Multi-Channel Weapon System Circuit Testers feature experience in UAS earth monitoring systems such as high extreme safety to guarantee that test current remains less than resolution mapping, digital elevation modeling (3D-model one one-thousandth of a device’s firing current. production/DEM), continuous monitoring of natural disasters, environmental pollution and in technical studies for infrastructure projects such as underground constructions and tunnels studies.

www.aiaa-SciTech.org 34 #aiaaSciTech IntroExhibitors Tecplot, Inc 311 Vision Research, Inc. 220 3535 Factoria Blvd SE #550 100 Dey Road Bellevue, WA 98006 Wayne, New Jersey 07470 www.tecplot.com www.phantomhighspeed.com [email protected] [email protected] Tecplot specializes in visual data analysis tools that boost your Vision Research designs and productivity, integrate into your workflows and cut time in manufactures a broad range understanding CFD, simulation or experimental results. Fast, of high-speed digital imaging reliable, easy-to-use and memory efficient, Tecplot software systems that are used in all military, industry, academic and helps you understand and communicate your results to others. entertainment sectors. Marketing under the Phantom® brand, For over 35 years, and with thousands of aerospace customers our cameras allow you to analyze physical phenomena when worldwide, Tecplot has become the trusted name in visual data it’s too fast to see, and too important not to™. For additional analysis. information regarding Vision Research, please visit www. phantomhighspeed.com. Tri Models Inc. 511 XFlow CFD 217 5191 Oceanus Drive Huntington Beach, CA 92649 40 Chellis Street www.trimodels.com White River Junction, VT 05001 [email protected] www.xflowusa.com info@xflowusa.com. Tri Models is the Premier supplier of Wind Tunnel Models & Ground Test hardware for the global aerospace community. XFlow™ CFD is the next-generation, meshless CFD package for We play a vital role in the development of new systems for the modeling external aerodynamics of fixed-wing and rotorcraft airframe companies. Whether you have a new program or are aircraft. XFlow supports complex motion of complicated refining an existing vehicle, Tri Models can help. moving parts to model dynamic effects of control surface motion in flight, high-lift (take-off and landing) configurations and/or separation of munitions or separable stores. TSI, Inc. 224 500 Cardigan Road Shoreview, MN 55126 www.tsi.com fl[email protected] For over 50 years, TSI has been providing a complete line of fluid diagnostics systems for air/gas flow research including: Particle Image Velocimetry, TR-Volumetric PIV, Laser Doppler Velocimetry and Hot Wire Anemometry. These systems can be used for measuring supersonic to low speed flows, giving details of the fluid statistics.

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AIAA Registration Hours Twitter Contest Sunday, 8 January 1500–1900 hrs Ready, Set, Tweet... Monday, 9 January – Thursday, 12 0700–1700 hrs Are you ready to win your very own iPad Mini? How about a January Visa gift card for $50, or even $100? All you have to do is start Friday, 13 January 0700–1300 hrs tweeting during the conference with #AiaaSciTech. Prizes: Wi-Fi Internet Access On Site First Place Prize: iPad Mini AIAA is providing limited Wi-Fi service for attendees to use Second Place Prize: $100 VISA gift card while on site. To keep this service available and optimized for Third Place Prize: $50 VISA gift card all attendees, please do not download files larger than 2MB, create multiple sessions across multiple devices, or download Twitter Contest Rules multiple files in one session. To enter our Twitter contest, tweet during AIAA SciTech Network Name: AIAASciTech Forum between 9–13 January 2017. Be sure to include the “#AiaaSciTech” tag. The user with the most tweets wins. Password: scitech17 Tweets must be substantive in nature and directly related 1. View Available Wireless Networks to conference sessions, speakers, events and the aerospace community. Retweets and quoting other users’ tweets do 2. Connect to “AIAASciTech” Network not qualify. If you are not able to attend AIAA SciTech, you 3. Enter the Password scitech17 are still eligible to participate by viewing sessions on our 4. Open your Web Browser, begin surfing Livestream channel and tweeting about them. The contest will end and the winners will be announced at 0930 hrs on 13 For assistance, please call our Meeting Room Internet Support January. at 817.205.8888. You must be at least 18 years old to participate. When you accept the prize, you’re consenting to our use of your AIAA Livestream Channel information (name, profile, photo) to announce you as a winner. We retain the right to use them in the future on our Visit www.livestream.com/aiaa to view selected keynotes, website or any other communication platform. plenaries, and Forum 360 sessions. Share the link with Finally, the “legalese”: Contest is void where prohibited. All colleagues who couldn’t attend the conference so they can prizes are delivered “as-is” and “with all faults.” AIAA is not watch live or view later. responsible for human or mechanical errors that adversely affect or delay your entry in the contest, or for force majeure Sponsored by: events that force the interruption or cancellation of this contest. No purchase necessary to win. Stay Fit at SciTech Certiﬁcate of Attendance Stay fit while at SciTech with your fellow attendees! Join AIAA staff on Tuesday, 10 January, and Thursday, 12 January, at Certificates of Attendance are available for attendees who 0600 hrs at the Gaylord Registration Lobby by the Cocoa Bean request documentation at the forum itself. Beginning Express for a 1–2-mile jog to start off your day! All levels are Wednesday, 11 January, you will be able to create and print welcome! your certificate at the AIAA Registration and Information Center. AIAA offers this service to better serve the needs of Concessions the professional community. Claims of hours or applicability toward professional education requirements are the The Gaylord Texan will provide breakfast and lunch for responsibility of the participant. purchase in the Longhorn Marble Foyer located on the Convention Center side; Level 1. Breakfast will be offered Monday to Thursday from 0715 – 0815 hrs. Lunch will be offered Monday, Tuesday and Thursday from 1230 – 1400 hrs.

www.aiaa-SciTech.org 36 #aiaaSciTech IntroGeneral Information

Conference Proceedings AIAA Foundation Proceedings for the forum will be For more than 20 years, the AIAA Foundation has being available online. The cost is included providing resources that support students and educators at both in the registration fee where indicated. the K–12 and university level. The AIAA Foundation’s initiatives Online proceedings will be available on include K–12 STEM education programs including classroom Monday, 9 January. grants and hands-on activities, college scholarships, design competitions, student conferences, and recognition awards. If Instructions to Access Proceedings: you would like to join our generous donors with a gift, please 1. To view proceedings, visit www.aiaa.org >ARC>Meeting Papers. visit us at the AIAA Pavilion in the Exposition Hall. 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 toolbar in the upper-right corner of the page: i. By paper number: Click the “Paper Number” link, select the conference year, and enter the paper number. Young Professional Guide for Gaining ii. Use the Search textbox to find papers by author, Management Support title, or keyword. The Advanced Search link provides Young professionals have the unique opportunity to meet and additional search information and options. learn from some of the most important people in the business 2. All manuscript files submitted by four days prior to the by attending conferences and participating in AIAA activities. conference are currently in the proceedings. Files submitted A detailed online guide, published by the AIAA Young after that date, both original and revised manuscripts, will Professional Committee, is available to help you gain support not be available until the final proceedings update, which and financial backing from your company. The guide explains may take up to 15 business days after the last day of the the benefits of participation, offers recommendations, and conference. provides an example letter for seeking management support 3. Direct any questions concerning access to proceedings and/ and funding, and shows you how to get the most out of your or ARC to [email protected]. participation. The online guide can be found on the AIAA website at www.aiaa.org/YPGuide. Manuscript Revisions 5. Manuscript revision is open for all presenting authors from 0900 hrs Eastern Time, Monday, 9 January through Badge Policy 2000 hrs Eastern Time, Wednesday, 25 January. Revisions submitted during this period are limited to minor changes AIAA forum badges are provided to those attendees who only (e.g., typos and the like). Changes to content are not have paid for a registration to the event (and must be worn permitted. at all times to participate in all forum activities). Badges are not provided at the registration desk for committee meetings. 6. Revisions submitted for manuscripts already online will In order to obtain a SciTech badge, one must register for the not refresh until after the proceedings have been updated, forum. which may take up to 15 business days after the last day of the conference. Nondiscriminatory Practices Employment Opportunities AIAA accepts registrations irrespective of race, creed, sex, AIAA members can post and browse resumes, browse job color, physical handicap, and national or ethnic origin. listings, and access other online employment resources by visiting the AIAA Career Center at careercenter.aiaa.org. Restrictions Membership Photos, video, or audio recording of sessions or exhibits, as well as the unauthorized sale of AIAA-copyrighted material, is AIAA is your vital lifelong link to the collective creativity and prohibited. brainpower of the aerospace profession and a champion for its achievements. Students who are not yet members may apply their registration fee toward their first year’s student member dues.

www.aiaa-SciTech.org 37 #aiaaSciTech GeneralIntro Information

Author and Session Chair Information

Speakers’ Brieﬁngs in Session Rooms Audiovisual Authors who are presenting papers will meet with session Each session room will be preset with the following: one chairs and co-chairs in their session rooms for a short LCD projector, one screen, one microphone and sound 30-minute briefing on the day of their sessions to exchange bios system (if necessitated by room size), and one laser pointer. and review final details prior to the session. Please attend on Laptop computers will also be provided. You may also use the day of your session(s). Laptops preloaded with the Speaker your own computer. Any additional audiovisual equipment Briefing preparation slides will be provided in each session requested onsite will be at cost to the presenter. Please note room. Speaker’s Briefing schedule is as follows: that AIAA does not provide security in the session rooms and Monday, 9 January – Friday, 13 January: 0730 hrs recommends that items of value not be left unattended. Specs for the laptops provided in each session room: Speakers’ Practice Room Operating System: Windows 10 Software: Office 2016 Speakers who wish to practice their presentations may do so 3) USB Ports (2 USB 3.0, 1 USB 2.0) in the Texas Reg A room located on the Convention Center 1) Card Reader side next to Texas Ballroom A. A sign-up sheet will be posted 1) Mini Display Port in front of the door. In consideration of others, please limit Processor: 3rd Generation Intel® Core™ i7-3520M (3.50 GHz, practice time to 30-minute increments. 4MB L3, 1333MHz FSB) Session Chair Reports Storage: 500GB (5400rpm) All session chairs are asked to complete a session chair report to “No Paper, No Podium” and “No Podium, No Paper” Policy evaluate their session for future planning. AIAA has partnered If a written paper is not submitted by the final manuscript with Canvas Solutions to provide an electronic Session Chair deadline, authors will not be permitted to present the paper at Report form. You can download the FREE mobile app in the forum. Also, if the paper is not presented at the forum, it your App Store, AppWorld, or Marketplace by searching for will be withdrawn from the proceedings. It is the responsibility “Canvas Solutions, Inc.” The mobile app is free, so please be of those authors whose papers or presentations are accepted to sure to download it. Detailed instructions will be provided in ensure that a representative attends the conference to present the session rooms. If you do not have a tablet or a smartphone, the paper. These policies are intended to improve the quality of simply use the report form as a guide and enter your session the program for attendees. chair report information at the session chair reporting computer station located on site near the AIAA registration Journal Publication area. Report data will be collected and used for future planning purposes, including session topics and room allocations. Please Authors of appropriate papers are encouraged to submit submit your session chair report electronically by Friday, 13 them for possible publication in one of the Institute’s archival January. journals: AIAA Journal; Journal of Aircraft; Journal of Air Transportation; Journal of Guidance, Control, and Dynamics; Journal of Propulsion and Power; Journal of Spacecraft and Rockets; Journal of Thermophysics and Heat Transfer; or Journal of Aerospace Information Systems. You may now submit your paper online at http://mc.manuscriptcentral.com/aiaa.

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www.aiaa-SciTech.org 38 #aiaaSciTech IntroCommittee Meetings and Events

Time Title Location Sunday, 8 January 0900-1200 TAC TC/PC Chair Training Grapevine 1 0900-1200 TAC Director/Deputy Director Training Grapevine 2 1200-1700 TAC Workshop Grapevine A 1430-1500 APATC Liaisons Subcommittee Pecos 3 1500-1600 APATC Education Subcommittee Del Rio 1 1500-1600 APATC Honors and Awards Subcommittee Mustang 1 1500-1600 APATC Publicity and Publications Subcommittee Pecos 4 1500-1600 APATC Membership and Nominations Subcommittee Hotel Suite 6333 1500-1600 APATC Planning Subcommittee Hotel Suite 6355 1600-1700 APATC Technical Activities Meeting Mustang 1 1600-1700 GTTC Steering Committee Grapevine 5 1600-1800 SRTC Subcommittee Dallas 1 1700-1800 FDTC High-Order Methods/Algorithms DG Appaloosa 2 1700-1800 GTTC Introduction/Overview Grapevine 5 1700-1800 APATC Steering Committee Hotel Suite 6355 1700-1800 HEP Workshop Debrief & Planning Pecos 3 1700-1900 Journal of Spacecraft and Rockets Editors and Advisory Board Del Rio 1 1730-2030 Structures TC Appaloosa 3 1800-1900 GTTC Program Subcommittee Grapevine 5 1800-2100 TAC Aerospace Design and Structures Group Meeting Pecos 4 1800-2100 TAC Program Committees Group Meeting Del Rio 3 1800-2100 TAC Engineering and Technology Management Group Meeting Palomino 3 1800-2100 TAC Information Systems Group Meeting Pecos 2 1800-2100 Atmospheric Flight Mechanics TC Appaloosa 4 1800-2200 Applied Aerodynamics TC Mustang 4 1900-2000 GTTC Conferences Subcommittee Grapevine 5 1900-2030 FDTC Steering Committee Hotel Suite 6333 1900-2200 TAC Propulsion and Energy Group Meeting Mustang 5 1900-2200 FDTC Transition DG Mustang 2 1900-2200 TAC Aircraft and Atmospheric Systems Group Meeting Palomino 1 1900-2200 TAC Space and Missiles Group Meeting Del Rio 2 1930-2130 Academic Affairs Committee Meeting Pecos 1 2000-2100 GTTC Membership Subcommittee Grapevine 5 2000-2200 AMTTC Conferences Subcommittee Bluebonnet Boardroom Monday, 9 January 0800-1200 Sub-Team #1 Governance Austin 5 0900-1000 ABPTCs Steering Committee Texas 5 0900-1600 GTTC Internal Balance WG Grapevine A 0930-1130 Journals Subcommittee Del Rio 1 0930-1600 National Institute of Aerospace Technical Advisory Committee Meeting Del Rio 3 1000-1100 HSABPTC Steering Committee Bluebonnet Boardroom 1000-1100 INPSITC (ABPSI) Meeting Del Rio 2 1030-1200 RAC I Hotel Suite 6333 www.aiaa-SciTech.org 39 #aiaaSciTech IntroCommittee Meetings and Events

Time Title Location Monday, 9 January (continued) 1100-1200 HSABPTC Meeting Pecos 4 1100-1200 PAW Meeting Hotel Suite 6355 1100-1200 GTETC Meeting Del Rio 2 1100-1200 Books Subcommittee Primrose Boardroom 1100-1500 Systems Engineering TC Mustang 5 1200-1400 TAC Aerospace Sciences Group Meeting Pecos 2 1200-1700 Governance Retreat Mustang 4 1300-1400 ABPTCs Conference & Communications Subcommittee Pecos 4 1300-1500 Education Series Advisory Board Bluebonnet Boardroom 1300-1530 Transformational Flight PC Del Rio 2 1400-1500 ABPTCs Honors and Awards Subcommittee Pecos 1 1400-1600 GTTC Future of Ground Testing WG Pecos 3 1500-1600 HSABPTC WG Pecos 4 1500-1600 ABPTCs Student Engine Design Competition Del Rio 1 1500-1700 GTTC Standards Subcommittee Hotel Suite 6333 1500-1700 Progress Series Editorial Advisory Board Primrose Boardroom 1530-1630 2017 AIAA AVIATION Forum Technical Program Committee Longhorn D 1600-1700 ABPTCs Student Leader Networking Event Pecos 1 1600-1800 Journal of Aircraft Editors and Advisory Board Mustang 5 1630-1730 GEPC Conference Subcommittee Del Rio 2 1630-1800 History TC Pecos 2 1700-1800 FDTC Low Re DG Pecos 4 1700-1800 ABPTCs Working Groups Austin 5 1700-1800 FDTC Turbulent Model Benchmarking DG Texas 2 1700-1830 AIAA Town Hall Meeting (Governance and Open Access) Texas C 1700-1900 APATC Low Boom DG Del Rio 1 1700-1900 Career and Professional Development Committee Ft. Worth 7 1700-1900 AIAA Journal Editors and Advisory Board Pecos 3 1700-2000 Computer Systems TC Del Rio 3 1730-1830 GEPC Leadership Team Del Rio 2 1730-1930 SCSTC Handbook Author's Meeting Palomino 1 1800-1900 GTTC Publications Subcommittee Hotel Suite 6333 1800-1930 FDTC Fundamentals of Flow Phenomena Subcommittee Dallas 6 1800-1930 FDTC Flow Control and Fluid Applications Subcommittee Ft. Worth 2 1800-2000 AMTTC Awards Subcommittee Primrose Boardroom 1800-2030 FDTC CFD Methods Subcommittee Ft. Worth 1 1800-2100 Small Satellite TC Pecos 1 1800-2100 Flight Testing TC Bluebonnet Boardroom 1800-2200 NASA's 2040 Vision Study Texas 3 1830-2030 Michigan Aerospace Engineering Alumni Reception Grapevine A 1830-2200 Propellants and Combustion TC Grapevine D 1830-2200 University of Illinois Alumni Reception Austin 3 1900-2000 GTTC Awards Subcommittee Hotel Suite 6333 www.aiaa-SciTech.org 40 #aiaaSciTech IntroCommittee Meetings and Events

Time Title Location Monday, 9 January (continued) 1900-2030 APATC Collaborative Experiments & Computations DG Dallas 1 1900-2100 Penn State Department of Aerospace Engineering 2017 Alumni Reception Riverwalk Terrace 1900-2200 ABPTCs Meeting Mustang 4 1900-2200 Aircraft Design TC Grapevine 1 1900-2200 Solid Rockets TC Austin 5 1900-2200 Space Resources TC Dallas 3 1930-2100 APATC Flow Control Applications & Impacts DG Dallas 4 2000-2100 GTTC Education and Student Activities Subcommittee Hotel Suite 6333 Tuesday, 10 January 0730-0900 International Activities Committee Del Rio 3 0730-0900 Finance Committee Del Rio 2 0830-1000 Publications Ethical Standards Subcommittee Pecos 1 0830-1200 2018 Associate Fellows Committee Kick-off Meeting Bluebonnet Boardroom 0900-1200 Governance Retreat Del Rio 2 0900-1700 GTTC Dual Flow Reference Nozzle WG - Day 1 Pecos 4 1000-1100 Publications Awards Subcommittee Primrose Boardroom 1000-1200 TAC New Initiatives Subcommittee Pecos 3 1000-1200 CASE Planning Meeting Del Rio 1 1100-1200 Journal of Propulsion and Power Editors and Advisory Board Pecos 2 1100-1200 P&E Group Coordination Meeting Mustang 5 1300-1400 ASME Structures and Materials TC Mustang 5 1300-1500 Student Activities Committee Meeting Pecos 1 1300-1500 GTTC Uncertainty Analysis WG Pecos 2 1400-1600 AIAA Standards Executive Council (SEC) Meeting Primrose Boardroom 1400-1700 TAC Executive Board Pecos 3 1400-1700 DETC Subcommittee Hotel Suite 6333 1400-1900 Region & Section Activities Committee Del Rio 2 1500-1600 TPTC Best Paper Subcommittee Grapevine Reg C 1500-1700 GTTC Statistically Defensible Test Methods Focus Group Texas D 1500-1700 Aerospace Cybersecurity Working Group Del Rio 3 1500-1700 Journal of Thermophysics and Heat Transfer Editors and Advisory Board Hotel Suite 6355 1600-1700 TPTC Awards Subcommittee Green Room Stage Right 1600-1700 TPTC Education Subcommittee Pecos 2 1600-1800 Emerging Technologies Committee Meeting Del Rio 1 1700-1800 TPTC Conferences Subcommittee Primrose Boardroom 1700-1800 TPTC Publicity Subcommittee Austin 6 1700-1900 Computational Fluid Dynamics CoS Austin 5 1700-2200 Digital Avionics TC Bluebonnet Boardroom 1730-1830 FDTC LES DG Hotel Suite 6333 1730-1830 FDTC Solver Technology for Turbulent Flow DG Ft. Worth 3 1730-2030 Green Engineering PC Mustang 5 1800-1900 TPTC Publications Subcommittee San Antonio 3 www.aiaa-SciTech.org 41 #aiaaSciTech IntroCommittee Meetings and Events

Time Title Location Tuesday, 10 January (continued) 1800-1900 TPTC Nominations Subcommittee San Antonio 6 1800-1900 FDTC Low Speed Flow Control DG Pecos 3 1800-1900 FDTC Non-Equilibrium DG Texas 1 1800-1900 FDTC Modal Decomposition DG Dallas 2 1800-2100 Design Engineering TC Pecos 4 1800-2100 Intelligent Systems TC Grapevine 2 1800-2200 GNCTC Student Paper Competition Palomino 2 1830-2200 Software TC Hotel Suite 6355 1900-2000 FDTC High Speed Flow Control DG Hotel Suite 6333 1900-2000 FDTC Fluid-Structure Interaction DG Dallas 7 1900-2030 Meet the Skunk Works - Recruiting and Information Session Texas 2 1900-2100 Plasmadynamics and Lasers TC Pecos 1 1900-2200 Adaptive Structures TC Ft. Worth 2 1900-2200 Unmanned Systems PC Pecos 2 1900-2200 Thermophysics TC Texas 4 1900-2200 Aeroacoustics TC Del Rio 3 1900-2200 Aerospace Department Chair Association (ADCA) Grapevine A 1900-2200 Pressure Gain Combustion PC Dallas 5 1900-2200 Meshing, Visualization and Computational Environments TC Dallas 6 1900-2300 Aerodynamic Measurement Technology TC Grapevine 1 1930-2130 Recent Events in the Evolution of NASA’s Aerosciences Capability Texas C 1930-2230 Materials TC Texas 1 1930-2230 Structures TC Texas 3 Wednesday, 11 January 0800-1200 GTTC Dual Flow Reference Nozzle WG - Day 2 Hotel Suite 6355 0830-1200 Honors and Awards Committee Mustang 5 0900-1200 Publications Committee Del Rio 2 0900-1600 GTTC Wind Tunnel Flow Quality WG Pecos 3 1000-1100 SciTech 2018 Technical Program Committee Planning Meeting Mustang 4 1000-1100 RAC IV Meeting Primrose Boardroom 1000-1400 Public Policy Committee Meeting Pecos 2 1000-1600 Technical Activities Committee Longhorn D 1100-1400 Space Operations and Support TC Del Rio 3 1200-1330 GNCTC Undergraduate Conference Experience Hotel Suite 6333 1300-1700 GTTC ONR WG Mustang 4 1330-1630 Foundation Board of Trustees Del Rio 1 1330-1630 Region & Section Activities Committee Pecos 4 1400-1600 FDTC Active Flow Control Documentation Project Mustang 5 1400-1600 Journal Editors in Chief and CrossMark Workshop Hotel Suite 6355 1430-1630 Corporate Member Committee Meeting Del Rio 2 1600-1800 Publications Review Subcommittee Pecos 2 1600-1800 Journal of Guidance, Control, and Dynamics Editors and Advisory Board Pecos 1 www.aiaa-SciTech.org 42 #aiaaSciTech IntroCommittee Meetings and Events

Time Title Location Wednesday, 11 January (continued) 1630-1800 LM Aeronautics Meeting Longhorn D 1700-1800 FDTC Mixing Layer Control DG Bluebonnet Boardroom 1700-1800 AMTTC Nominations Subcommittee Primrose Boardroom 1700-1830 APATC Missile & Projectile Aeroprediction DG Mustang 5 1700-1830 Emerging Technologies Identification Session Dallas 5 1700-1900 Plasma Aerodynamics DG Pecos 3 1700-2000 Energy Optimized Aircraft and Equipment Systems PC Del Rio 3 1700-2000 Pointwise Meet & Greet Dallas 6 1730-1900 APATC CFD Transition Modeling DG Austin 1 1800-1900 FDTC Future of Fluids Pecos 4 1800-1930 Design/Build/Fly Discussion Texas D 1800-2000 AMTTC Update Presentation/Student Event Texas 3 1800-2000 SETC Digital Systems Integration WG Palomino 3 1800-2000 APATC Aeropropulsive Interactions DG Del Rio 2 1800-2100 V/STOL Aircraft Systems TC Hotel Suite 6355 1800-2100 Spacecraft Structures TC Mustang 4 1830-2000 AIAA Publications--Book Authors Appreciation Reception Del Rio 1 1830-2130 Survivability TC Pecos 1 1830-2130 Multidisciplinary Design Optimization TC Ft. Worth 7 1830-2200 NPAT Mini-Facility User's Meeting (FUM) Grapevine 3 1900-2000 HyTASP PC Steering Committee Primrose Boardroom 1900-2200 Society and Aerospace Technology TC Bluebonnet Boardroom 1900-2200 Fluid Dynamics TC Texas 2 1900-2200 ASME Wind Energy TC Mustang 5 1900-2200 Non-Deterministic Approaches TC Grapevine 1 1900-2200 Space Logistics TC Pecos 2 1900-2200 Terrestrial Energy Systems TC Palomino 2 1900-2200 Structural Dynamics TC Mustang 2 1930-2130 Alumni and Friends of UC Appaloosa 1 2000-2200 HyTASP PC Texas 5 Thursday, 12 January 0800-1200 GTTC Future of Ground Test WG Pecos 1 0900-1200 Board of Directors Meeting Longhorn D 0900-1700 AIAA Resource Working Group Pecos 2 1200-1600 GTTC WT Model Attitude and Deformation Measurement WG Mustang 5 1300-1700 GTTC Industry WG Del Rio 1 1415-1545 HEP Workshop Results & Recommendations Mustang 4 1530-1630 RAC V Meeting Bluebonnet Boardroom 1730-2030 Ground Testing TC Texas 6 1800-2000 APATC Rotorcraft Simulations & Performance Predictions DG Texas 1 1800-2300 Guidance, Navigation and Control TC Grapevine 1 1900-2200 MVCE Meshing Subcommittee Del Rio 3 1900-2200 Modeling and Simulation TC Pecos 3 www.aiaa-SciTech.org 43 #aiaaSciTech IntroSessions at a Glance

Abbreviation Title Date Start Time End Time Location Aeroacoustics 7-AA-1 Aeroacoustics Jet Noise I 9-Jan 0930 hrs 1230 hrs Grapevine B 60-AA-2 Aeroacoustics Jet Noise II 9-Jan 1400 hrs 1700 hrs Grapevine B 69-APA-8/AA-3 Special Session: Low Boom Activities II 9-Jan 1400 hrs 1700 hrs Dallas 6 119-AA-4 Computational Aeroacoustics I 10-Jan 0930 hrs 1230 hrs Grapevine B 173-AA-5 Aeroacoustics Jet Noise III 10-Jan 1400 hrs 1700 hrs Grapevine B 234-AA-6 Computational Aeroacoustics II 11-Jan 0930 hrs 1230 hrs Grapevine B 235-AA-7 Aeroacoustics - Advanced Measurement and Experiment 11-Jan 0930 hrs 1230 hrs Grapevine 3 288-AA-8 Aeroacoustics - Fan Noise, Open Rotor 11-Jan 1400 hrs 1700 hrs Grapevine B 289-AA-9 Aeroacoustics - Airframe and Community Noise 11-Jan 1400 hrs 1700 hrs Grapevine 3 Air Breathing Propulsion Systems Integration 344-ABPSI-1 High-Speed Inlets and Scramjets 12-Jan 0930 hrs 1230 hrs Dallas 1 399-ABPSI-2 Inlet Distortion and Characterization 12-Jan 1400 hrs 1700 hrs Dallas 1 456-ABPSI-3 Nozzles and Propulsion Design 13-Jan 0930 hrs 1300 hrs Dallas 1 Aircraft Design 8-ACD-1 Aircraft Design Tools and Methods I 9-Jan 0930 hrs 1230 hrs San Antonio 1 9-ACD-2 Unmanned Aircraft Design I 9-Jan 0930 hrs 1230 hrs San Antonio 3 61-ACD-3 Aircraft Design Tools and Methods II 9-Jan 1400 hrs 1700 hrs San Antonio 1 62-ACD-4 Unmanned Aircraft Design II 9-Jan 1400 hrs 1700 hrs San Antonio 3 120-ACD-5 Aircraft Design Tools and Methods III 10-Jan 0930 hrs 1230 hrs San Antonio 1 174-ACD-6 Aircraft Design Tools and Methods IV 10-Jan 1400 hrs 1700 hrs San Antonio 1 290-ACD-7 Electric Aircraft Design 11-Jan 1400 hrs 1700 hrs San Antonio 5 345-ACD-8 Innovative Aircraft Design Concepts I 12-Jan 0930 hrs 1230 hrs Grapevine 3 400-ACD-9 Innovative Aircraft Design Concepts II 12-Jan 1400 hrs 1700 hrs Grapevine 3 401-ACD-10 CADWG: Concept Design Tools and Processes for Manufacturing and 12-Jan 1400 hrs 1700 hrs San Antonio 4 Certification of Aircraft 457-ACD-11 Special Purpose Aircraft 13-Jan 0930 hrs 1300 hrs Pecos 3 Atmospheric Flight Mechanics 10-AFM-1 Aeroservoelastic (ASE) Control, Modeling, Simulation, and 9-Jan 0930 hrs 1230 hrs Grapevine 5 Optimization 63-AFM-2 Launch Vehicle, Atmospheric Entry, Hypersonic Flight and Aeroassist 9-Jan 1400 hrs 1700 hrs Grapevine 5 Technology I 121-AFM-3 Launch Vehicle, Atmospheric Entry, Hypersonic Flight and Aeroassist 10-Jan 0930 hrs 1230 hrs Grapevine 5 Technology II 175-AFM-4 Flight Test and System Identification I 10-Jan 1400 hrs 1700 hrs Grapevine 5 236-AFM-5 Flight Test and System Identification II 11-Jan 0930 hrs 1230 hrs Grapevine 5 291-AFM-6 Aircraft Flight Dynamics, Handling Qualities, and Performance I 11-Jan 1400 hrs 1700 hrs Grapevine 5 346-AFM-7 Special Session: Performance Adaptive Aeroelastic Wing 12-Jan 0930 hrs 1230 hrs Grapevine 4 347-AFM-8 Aircraft Flight Dynamics, Handling Qualities, and Performance II 12-Jan 0930 hrs 1230 hrs Grapevine 5 402-AFM-9 Small/Mini/Micro Aerial Vehicles 12-Jan 1400 hrs 1700 hrs Grapevine 4 403-AFM-10 Aircraft Flight Dynamics, Handling Qualities, and Performance III 12-Jan 1400 hrs 1700 hrs Grapevine 5 458-AFM-11 Aircraft Flight Dynamics, Handling Qualities, and Performance IV 13-Jan 0930 hrs 1300 hrs Grapevine 5 459-AFM-12 Aerodynamic Prediction Methods 13-Jan 0930 hrs 1300 hrs Grapevine 4

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Abbreviation Title Date Start Time End Time Location Aerodynamic Measurement Technology 11-AMT-1 Velocimetry: Applications I 9-Jan 0930 hrs 1230 hrs Grapevine 6 12-AMT-2 Temperature Measurements and Applications 9-Jan 0930 hrs 1230 hrs Grapevine 4 64-AMT-3 Velocimetry: Development and Implementation Challenges 9-Jan 1400 hrs 1700 hrs Grapevine 6 65-AMT-4 Laser Tagging and Fluorescence Techniques 9-Jan 1400 hrs 1700 hrs Grapevine 4 122-AMT-5 Velocimetry: Applications II 10-Jan 0930 hrs 1230 hrs Grapevine 6 123-AMT-6 Wall-Based Sensors and Applications 10-Jan 0930 hrs 1230 hrs Grapevine D 124-AMT-7/GT-3 Force Measurements 10-Jan 0930 hrs 1230 hrs Grapevine 4 176-AMT-8 Pressure Determination Techniques and Applications 10-Jan 1400 hrs 1700 hrs Grapevine 6 237-AMT-9 Deformation, Displacement, and Object-Tracking Measurements 11-Jan 0930 hrs 1230 hrs Grapevine D 260-GT-6/AMT-10 Test Technique and Data Analysis Improvements at the NASA Ames 11-Jan 0930 hrs 1230 hrs Ft. Worth 6 Unitary Plan Wind Tunnels I (Invited) 312-GT-7/AMT-11 Test Technique and Data Analysis Improvements at the NASA Ames 11-Jan 1400 hrs 1700 hrs Ft. Worth 6 Unitary Plan Wind Tunnels II (Invited) 348-AMT-12 Launch Vehicle Buffet (Invited) 12-Jan 0930 hrs 1230 hrs Grapevine 2 349-AMT-13 Rayleigh Scattering Measurements 12-Jan 0930 hrs 1230 hrs Grapevine B 404-AMT-14 Simultaneous and/or Multidimensional Measurements 12-Jan 1400 hrs 1700 hrs Grapevine B Applied Aerodynamics 13-APA-1 Aerodynamic Design: Analysis, Methodologies and Optimization 9-Jan 0930 hrs 1230 hrs Dallas 1 Techniques I 14-APA-2 Special Session: Low Boom Activities I 9-Jan 0930 hrs 1230 hrs Dallas 2 15-APA-3 Environmentally Friendly/Efficient Aerodynamics and Enabling 9-Jan 0930 hrs 1230 hrs Dallas 3 Technology I 16-APA-4 Propeller/Rotorcraft/Wind Turbine Aerodynamics I: Coaxial and Open 9-Jan 0930 hrs 1230 hrs Dallas 4 Rotor 47-SD-1/APA-46 Special Session: Aerothermoelasticity of, and Dynamic Response in, 9-Jan 0930 hrs 1230 hrs Appaloosa 2 High Speed Vehicles and in High Speed Flow I 101-SD-4/APA-47 Special Session: Aerothermoelasticity of, and Dynamic Response in, 9-Jan 1400 hrs 1700 hrs Appaloosa 2 High Speed Vehicles and in High Speed Flow II 66-APA-5 Hypersonic Aerodynamics 9-Jan 1400 hrs 1700 hrs Dallas 2 67-APA-6 Airfoil/Wing/Configuration Aerodynamics I 9-Jan 1400 hrs 1700 hrs Dallas 3 68-APA-7 Special Session: CFD Applied to Real World Problems 9-Jan 1400 hrs 1700 hrs Dallas 4 69-APA-8/AA-3 Special Session: Low Boom Activities II 9-Jan 1400 hrs 1700 hrs Dallas 6 70-APA-9 Environmentally Friendly/Efficient Aerodynamics and Enabling 9-Jan 1400 hrs 1700 hrs Dallas 1 Technology II 71-APA-10 Special Session: CREATE-AV HPC Multiphysics I 9-Jan 1400 hrs 1700 hrs Dallas 5 125-APA-11 Flow Control Applications and Demonstrations (Active and Passive) I 10-Jan 0930 hrs 1230 hrs Dallas 1 126-APA-12 Aerodynamic/Propulsive Interactions - Panel Discussion 10-Jan 0930 hrs 1130 hrs Dallas 3 127-APA-13 Unsteady Aerodynamics I 10-Jan 0930 hrs 1230 hrs Dallas 2 128-APA-14 Bio-Inspired Flows 10-Jan 0930 hrs 1230 hrs Dallas 4 129-APA-15 Low Speed, Low Reynolds Number Aerodynamics 10-Jan 0930 hrs 1230 hrs Dallas 5 177-APA-16 Aerodynamic Design: Analysis, Methodologies, and Optimization 10-Jan 1400 hrs 1700 hrs Dallas 3 Techniques II 178-APA-17 Flow Control Applications and Demonstrations (Active and Passive) II 10-Jan 1400 hrs 1700 hrs Dallas 1 179-APA-18 Unsteady Aerodynamics II 10-Jan 1400 hrs 1700 hrs Dallas 2 180-APA-19 Aerodynamic Design: Design Tools and Propeller Integration 10-Jan 1400 hrs 1700 hrs Dallas 4 www.aiaa-SciTech.org 45 #aiaaSciTech IntroSessions at a Glance

Abbreviation Title Date Start Time End Time Location Applied Aerodynamics (continued) 181-APA-20 Propeller/Rotorcraft/Wind Turbine Aerodynamics II: Low-Rn 10-Jan 1400 hrs 1700 hrs Dallas 5 Propellers 238-APA-21 Flow Control Applications and Demonstrations (Active and Passive) III 11-Jan 0930 hrs 1230 hrs Dallas 1 239-APA-22 Unsteady Aerodynamics III 11-Jan 0930 hrs 1230 hrs Dallas 2 240-APA-23/FD-31 Vortical Flows & Wake Control 11-Jan 0930 hrs 1230 hrs Dallas 3 241-APA-24 DPW-6 Results and Comparisons I 11-Jan 0930 hrs 1230 hrs Dallas 4 242-APA-26 Special Session: CREATE-AV HPC Multiphysics II 11-Jan 0930 hrs 1230 hrs Dallas 5 292-APA-27 Special Session: CREATE-AV HPC Multiphysics III 11-Jan 1400 hrs 1700 hrs Dallas 1 293-APA-28 Special Session: Sensitivity Analysis and Uncertainty Quantification 11-Jan 1400 hrs 1700 hrs Dallas 2 Evaluation for Realistic Problems I 294-APA-29 Weapons Aerodynamics 11-Jan 1400 hrs 1700 hrs Dallas 3 295-APA-30 DPW-6 Results and Comparisons II 11-Jan 1400 hrs 1700 hrs Dallas 4 296-APA-31 High Angle-of-Attack Aerodynamics 11-Jan 1400 hrs 1630 hrs Dallas 5 297-APA-32 Aerodynamic Results from Ground Test or Flight Test 11-Jan 1400 hrs 1630 hrs Dallas 6 350-APA-33 Aerodynamic Design: Transonic/Supersonic 12-Jan 0930 hrs 1230 hrs Ft. Worth 2 351-APA-34 Aerodynamic-Structural Dynamic Interactions I 12-Jan 0930 hrs 1230 hrs Dallas 5 352-APA-35 Airfoil/Wing/Configuration Aerodynamics II: Multifidelity Methods 12-Jan 0930 hrs 1230 hrs Dallas 3 353-APA-36 Applied CFD I: Boundary Layer and Solver Methodologies 12-Jan 0930 hrs 1230 hrs Dallas 4 354-APA-37 Special Session: Simulation of Rotor in Hover I 12-Jan 0930 hrs 1230 hrs Dallas 2 355-APA-38 Transonic/Supersonic Aerodynamics 12-Jan 0930 hrs 1230 hrs Dallas 6 405-APA-39 Aerodynamic-Structural Dynamic Interactions II 12-Jan 1400 hrs 1700 hrs Dallas 5 406-APA-40 Special Session: Sensitivity Analysis and Uncertainty Quantification 12-Jan 1400 hrs 1700 hrs Ft. Worth 3 Evaluation for Realistic Problems II 407-APA-41 Airfoil/Wing/Configuration Aerodynamics III: Airfoil and Wing 12-Jan 1400 hrs 1700 hrs Dallas 3 Optimization 408-APA-42 Applied CFD II: Configuration Evaluation 12-Jan 1400 hrs 1700 hrs Dallas 4 409-APA-43 Special Session: Simulation of Rotor in Hover II 12-Jan 1400 hrs 1700 hrs Dallas 2 410-APA-44/FD-53 Special Session: Sensitivity Analysis of High-Fidelity Rotorcraft 12-Jan 1400 hrs 1700 hrs Dallas 6 Computations 460-APA-45 Special Session: Simulation of Rotor in Hover III 13-Jan 0930 hrs 1300 hrs Dallas 2 Adaptive Structures 17-ASC-1 Adaptive and Morphing Aircraft and Aeroelasticity 9-Jan 0930 hrs 1230 hrs Palomino 3 72-ASC-2 Adaptive and Morphing Aircraft and Aeroelasticity, Adaptive Skins, 9-Jan 1400 hrs 1700 hrs Palomino 3 Biomimetics 182-ASC-3 Smart and Multifunctional Materials 10-Jan 1400 hrs 1700 hrs Palomino 3 411-ASC-4 Smart and Multifunctional Materials, Structural Health Monitoring 12-Jan 1400 hrs 1700 hrs Palomino 3 and Damage Detection and Integrity 356-ASC-5 Active Noise and Vibration Control, Smart Sensor and Actuator Device 12-Jan 0930 hrs 1230 hrs Palomino 3 Design 461-ASC-6 Modeling, Simulation, and Optimization of Adaptive Structures, 13-Jan 0930 hrs 1300 hrs Palomino 3 Space and Planetary Systems and Subsystems Computer Systems 18-CMS-1 Communication Systems 9-Jan 0930 hrs 1230 hrs Ft. Worth 1 Digital Avionics 19-DA-1 Digital Avionics 9-Jan 0930 hrs 1230 hrs Grapevine 1 www.aiaa-SciTech.org 46 #aiaaSciTech IntroSessions at a Glance

Abbreviation Title Date Start Time End Time Location Design Engineering 73-EDU-2/DE-1 Advancing Aerospace Education I 9-Jan 1400 hrs 1700 hrs Dallas 7 130-DE-2 Innovative Aerospace Designs, Processes, and Tools 10-Jan 0930 hrs 1230 hrs Palomino 3 243-DE-3 Design Processes and Tools 11-Jan 0930 hrs 1230 hrs Palomino 3 Education 73-EDU-2/DE-1 Advancing Aerospace Education I 9-Jan 1400 hrs 1700 hrs Dallas 7 131-EDU-3 Advancing Aerospace Education II 10-Jan 0930 hrs 1230 hrs Dallas 7 244-EDU-1 Educating the Engineer of the 2030 11-Jan 0930 hrs 1230 hrs Grapevine A Fluid Dynamics 21-FD-1 Boundary Layer Stability and Transition I 9-Jan 0930 hrs 1230 hrs Texas 1 22-FD-2 Cartesian and Overset CFD Methods 9-Jan 0930 hrs 1230 hrs Texas 2 23-FD-3 CFD Applications 9-Jan 0930 hrs 1230 hrs Texas 3 24-FD-4 CFD Methods for Compressible Flows I 9-Jan 0930 hrs 1230 hrs Texas 4 25-FD-6 Experiments and Numerical Simulations of Shock Dominated Flows 9-Jan 0930 hrs 1230 hrs Austin 1 26-FD-7 Low-Re and Bio-Inspired Flows I: Applications 9-Jan 0930 hrs 1230 hrs Grapevine C 75-FD-8 Boundary Layer Stability and Transition II 9-Jan 1400 hrs 1700 hrs Texas 1 76-FD-9 CFD Methods for Compressible Flows II 9-Jan 1400 hrs 1700 hrs Texas 4 77-FD-11 RANS/LES for High-Speed Flows 9-Jan 1400 hrs 1700 hrs Texas 3 78-FD-12 Special Session: CRM High-Lift Project 9-Jan 1400 hrs 1700 hrs Texas 6 79-FD-13 Synthetic Jets 9-Jan 1400 hrs 1630 hrs Texas 2 80-FD-14 Low-Re and Bio-Inspired Flows II: Unsteady Wings 9-Jan 1400 hrs 1700 hrs Grapevine C 133-FD-15 High-Order Methods I 10-Jan 0930 hrs 1230 hrs Texas 1 134-FD-16 High-Speed Flows I 10-Jan 0930 hrs 1230 hrs Texas 2 135-FD-17 Honoring Gino Moretti 10-Jan 0930 hrs 1230 hrs Texas 3 136-FD-18 Modeling and Optimization Methods 10-Jan 0930 hrs 1230 hrs Texas 4 137-FD-19 Numerical Simulations of Shock Boundary Layer Interactions 10-Jan 0930 hrs 1230 hrs Texas 5 138-FD-20 RANS/LES Applications 10-Jan 0930 hrs 1230 hrs Texas 6 139-FD-22 Low-Re and Bio-Inspired Flows III: Wing Analysis and Design 10-Jan 0930 hrs 1230 hrs Grapevine C 184-FD-23 CFD Methods on Unstructured Meshes 10-Jan 1400 hrs 1700 hrs Austin 1 185-FD-24 High-Order Methods II 10-Jan 1400 hrs 1700 hrs Texas 2 186-FD-25 High-Speed Flows II 10-Jan 1400 hrs 1700 hrs Texas 3 187-FD-26 RANS/LES Modeling of Jet Flows 10-Jan 1400 hrs 1700 hrs Texas 4 188-FD-27 Novel CFD Methods 10-Jan 1400 hrs 1700 hrs Texas 5 189-FD-28 Shock Boundary Layer Interactions I 10-Jan 1400 hrs 1700 hrs Texas 1 190-FD-29 Stability and Transition over Cones 10-Jan 1400 hrs 1700 hrs Texas 6 191-FD-30 Experimental Aerodynamics 10-Jan 1400 hrs 1700 hrs Grapevine C 240-APA-23/FD-31 Vortical Flows & Wake Control 11-Jan 0930 hrs 1230 hrs Dallas 3 246-FD-32 RANS and LES Methods 11-Jan 0930 hrs 1230 hrs Texas 3 247-FD-33 Shock Boundary Layer Interactions II 11-Jan 0930 hrs 1230 hrs Texas 1 248-FD-34 Special Session: Low Reynold's Number Flows 11-Jan 0930 hrs 1230 hrs Texas 2 249-FD-35 Turbulence Modeling: RANS/LES 11-Jan 0930 hrs 1230 hrs Texas 4 250-FD-36 Unsteady Measurements 11-Jan 0930 hrs 1230 hrs Texas 5 251-FD-37 LES 11-Jan 0930 hrs 1230 hrs Texas 6 252-FD-38 Other Topics in Fluid Dynamics I 11-Jan 0930 hrs 1230 hrs Grapevine C www.aiaa-SciTech.org 47 #aiaaSciTech IntroSessions at a Glance

Abbreviation Title Date Start Time End Time Location Fluid Dynamics (continued) 299-FD-39 CFD Methods for Fast Computing 11-Jan 1400 hrs 1700 hrs Texas 6 300-FD-41 Special Session: Wall Models for Large Eddy Simulation 11-Jan 1400 hrs 1700 hrs Texas 2 301-FD-42 Transition Open Forum 11-Jan 1400 hrs 1700 hrs Texas 3 302-FD-43 Turbulent, Compressible CFD Applications and Validations 11-Jan 1400 hrs 1700 hrs Texas 4 303-FD-44 CFD Modeling 11-Jan 1400 hrs 1700 hrs Texas 5 304-FD-45 Other Topics in Fluid Dynamics II 11-Jan 1400 hrs 1700 hrs Grapevine C 414-FD-5 Experimental Measurements in Stability and Transition 12-Jan 1400 hrs 1700 hrs Grapevine 2 359-FD-46 Boundary Layer Separation Control 12-Jan 0930 hrs 1230 hrs Texas 1 360-FD-47 Internal Flow Control 12-Jan 0930 hrs 1230 hrs Texas 2 361-FD-48 Boundary Layers and Shear Layers I 12-Jan 0930 hrs 1230 hrs Texas 4 362-FD-49 Multiphase Flows I 12-Jan 0930 hrs 1230 hrs Texas 3 363-FD-50 Reacting Flows 12-Jan 0930 hrs 1230 hrs Texas 5 364-FD-51 Cavity Flows 12-Jan 0930 hrs 1230 hrs Texas 6 365-FD-52 LES/DES Simulations 12-Jan 0930 hrs 1230 hrs Grapevine C 410-APA-44/FD-53 Special Session: Sensitivity Analysis of High-Fidelity Rotorcraft 12-Jan 1400 hrs 1700 hrs Dallas 6 Computations 415-FD-54 Static and Dynamic Stall Control 12-Jan 1400 hrs 1700 hrs Texas 1 416-FD-55 Jet-Based Flow Control 12-Jan 1400 hrs 1700 hrs Texas 2 417-FD-56 Boundary Layers and Shear Layers II 12-Jan 1400 hrs 1700 hrs Texas 4 418-FD-57 Multiphase Flows II 12-Jan 1400 hrs 1700 hrs Texas 3 419-FD-58 Vortex Flows 12-Jan 1400 hrs 1700 hrs Texas 5 420-FD-59 Turbulence and Transition 12-Jan 1400 hrs 1700 hrs Texas 6 462-FD-10 Flow Stability Analysis 13-Jan 0930 hrs 1230 hrs Pecos 4 463-FD-60 Control of High Speed Flows 13-Jan 0930 hrs 1300 hrs Texas 1 464-FD-61 Jet Flow Experiments 13-Jan 0930 hrs 1300 hrs Texas 2 465-FD-62 Multiphase Flows III 13-Jan 0930 hrs 1300 hrs Texas 3 Green Engineering 27-GEPC-1 Hybrid Wing Body 9-Jan 0930 hrs 1230 hrs Texas 6 81-GEPC-2 Hybrid Propulsion Concept Development for Transport Class Aircraft 9-Jan 1400 hrs 1700 hrs Texas 5 Guidance, Navigation, and Control 253-GNC-1 Missile Intercept and Evasion Guidance 11-Jan 0930 hrs 1230 hrs Austin 1 254-GNC-2 Loss of Control and Protections 11-Jan 0930 hrs 1230 hrs Austin 6 255-GNC-3 Aircraft GNC Control Applications 11-Jan 0930 hrs 1230 hrs Grapevine 4 256-GNC-4 Navigation Methods 11-Jan 0930 hrs 1230 hrs Austin 2 257-GNC-5 Spacecraft and Launch Controls 11-Jan 0930 hrs 1230 hrs Grapevine 6 258-GNC-6 Control of Micro Air Vehicles 11-Jan 0930 hrs 1230 hrs Austin 4 259-GNC-7 Spacecraft Robotics 11-Jan 0930 hrs 1230 hrs Austin 5 305-GNC-8 Missile GNC 11-Jan 1400 hrs 1700 hrs Austin 1 306-GNC-9 Trajectory Optimization 11-Jan 1400 hrs 1700 hrs Grapevine D 307-GNC-10 Adaptive Control for Aircraft GNC 11-Jan 1400 hrs 1700 hrs Austin 6 308-GNC-11 Aircraft GNC Control Methods 11-Jan 1400 hrs 1700 hrs Austin 5 309-GNC-12 Estimation and Tracking Methods 11-Jan 1400 hrs 1700 hrs Austin 2 310-GNC-13 Spacecraft and Launch Guidance 11-Jan 1400 hrs 1700 hrs Grapevine 6 www.aiaa-SciTech.org 48 #aiaaSciTech IntroSessions at a Glance

Abbreviation Title Date Start Time End Time Location Guidance, Navigation, and Control (continued) 311-GNC-14 Control of Innovative Micro Air Vehicle Configurations 11-Jan 1400 hrs 1700 hrs Austin 4 366-GNC-15 Airflow Mechanosensing for Aircraft Navigation and Control 12-Jan 0930 hrs 1230 hrs Grapevine 1 367-GNC-16 Verification and Validation of Adaptive Systems I 12-Jan 0930 hrs 1230 hrs Austin 2 368-GNC-17 Entry, Descent and Landing GNC Technology I 12-Jan 0930 hrs 1230 hrs Austin 4 369-GNC-18 Control Theory, Analysis and Design I 12-Jan 0930 hrs 1230 hrs Austin 5 370-GNC-19 Missile Guidance 12-Jan 0930 hrs 1230 hrs Austin 1 371-GNC-20 Predictive Control Methods 12-Jan 0930 hrs 1230 hrs Grapevine D 372-GNC-21 Spacecraft and Launch Navigation 12-Jan 0930 hrs 1230 hrs Grapevine 6 373-GNC-22 Aerospace Robotics Control 12-Jan 0930 hrs 1230 hrs Austin 6 421-GNC-23 Verification and Validation of Adaptive Systems II 12-Jan 1400 hrs 1700 hrs Austin 2 422-GNC-24 Elastic Aircraft and Load Alleviation 12-Jan 1400 hrs 1700 hrs Austin 1 423-GNC-25 ATM and Operations 12-Jan 1400 hrs 1700 hrs Grapevine D 424-GNC-26 Spacecraft and Launch Trajectory and Planning 12-Jan 1400 hrs 1700 hrs Grapevine 6 425-GNC-27 Control Theory, Analysis and Design II 12-Jan 1400 hrs 1700 hrs Austin 5 426-GNC-28 Aerospace Robotics Guidance and Navigation 12-Jan 1400 hrs 1700 hrs Austin 6 466-GNC-29 Verification and Validation of Adaptive Systems III 13-Jan 0930 hrs 1300 hrs Austin 2 467-GNC-30 Entry, Descent and Landing GNC Technology II 13-Jan 0930 hrs 1300 hrs Austin 4 468-GNC-31 Spacecraft and Launch Estimation and Sensors 13-Jan 0930 hrs 1300 hrs Grapevine 6 469-GNC-32 Emerging Micro Air Vehicle Capabilities 13-Jan 0930 hrs 1300 hrs Austin 5 470-GNC-33 Aerospace Robotics 13-Jan 0930 hrs 1300 hrs Austin 6 471-GNC-34 Intelligent and Cooperative Control in AE Applications 13-Jan 0930 hrs 1300 hrs Austin 1 Ground Testing 28-GT-1 Design, Calibration and Performance of Ground Test Facilities and 9-Jan 0930 hrs 1230 hrs Ft. Worth 6 Subsystems 82-GT-2 Experimental and Computational Fluid Dynamics Studies 9-Jan 1400 hrs 1700 hrs Ft. Worth 6 83-GT-11 High Reynolds Number Aerodynamics and Testing (Invited) 9-Jan 1400 hrs 1700 hrs Austin 1 124-AMT-7/GT-3 Force Measurements 10-Jan 0930 hrs 1230 hrs Grapevine 4 140-GT-4 Advances in Test Techniques and Test Management 10-Jan 0930 hrs 1230 hrs Ft. Worth 6 192-GT-5 Design, Calibration and Performance of Ground Test Facilities 10-Jan 1400 hrs 1700 hrs Ft. Worth 6 260-GT-6/AMT-10 Test Technique and Data Analysis Improvements at the NASA Ames 11-Jan 0930 hrs 1230 hrs Ft. Worth 6 Unitary Plan Wind Tunnels I (Invited) 312-GT-7/AMT-11 Test Technique and Data Analysis Improvements at the NASA Ames 11-Jan 1400 hrs 1700 hrs Ft. Worth 6 Unitary Plan Wind Tunnels II (Invited) 374-GT-8 Real-Time Control, Data Acquisition and Analysis 12-Jan 0930 hrs 1230 hrs Ft. Worth 6 375-GT-9 Selected Papers from the 10th International Symposium on Strain- 12-Jan 0930 hrs 1230 hrs San Antonio 5 Gauge Balances Held at CARDC (Invited) Gas Turbine Engines 29-GTE-1 Turbomachinery Technologies 9-Jan 0930 hrs 1230 hrs Ft. Worth 2 84-GTE-2 New Engine Architectures I 9-Jan 1400 hrs 1700 hrs Ft. Worth 2 141-GTE-3 Experimental Tools 10-Jan 0930 hrs 1230 hrs Austin 5 193-GTE-4 Combustion Technologies, Emissions I 10-Jan 1400 hrs 1700 hrs San Antonio 4 194-GTE-5 Numerical Tools I 10-Jan 1400 hrs 1700 hrs Grapevine 3

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Abbreviation Title Date Start Time End Time Location Gas Turbine Engines (continued) 261-GTE-6 Combustion Technologies, Emissions II 11-Jan 0930 hrs 1230 hrs San Antonio 4 313-GTE-7 Advanced Turbine Cooling I 11-Jan 1400 hrs 1700 hrs San Antonio 4 376-GTE-8 Advanced Turbine Cooling II 12-Jan 0930 hrs 1230 hrs San Antonio 4 427-GTE-9/PGC-6 Pressure Gain Combustion for Gas Turbines 12-Jan 1400 hrs 1700 hrs Grapevine C 472-GTE-10 New Engine Architectures II 13-Jan 0930 hrs 1300 hrs Grapevine 2 473-GTE-11 Numerical Tools II 13-Jan 0930 hrs 1300 hrs Grapevine 3 History 30-HIS-1 History of Aerospace 9-Jan 0930 hrs 1230 hrs Dallas 7 High Speed Air Breathing Propulsion 31-HSABP-1 Scramjet Design and Optimization 9-Jan 0930 hrs 1230 hrs San Antonio 4 85-HSABP-2 Scramjet Combustors 9-Jan 1400 hrs 1700 hrs San Antonio 4 142-HSABP-3 Computational Investigations of Scramjets 10-Jan 0930 hrs 1230 hrs San Antonio 4 195-HSABP-4/PGC-3 Pressure Gain Combustion - Rotating Detonation Engines I 10-Jan 1400 hrs 1700 hrs Ft. Worth 3 262-HSABP-5/PGC-4 Pressure Gain Combustion - Rotating Detonation Engines II 11-Jan 0930 hrs 1230 hrs Ft. Worth 3 314-HSABP-6/PGC-5 Pressure Gain Combustion - Rotating Detonation Engines III 11-Jan 1400 hrs 1700 hrs Ft. Worth 3 377-HSABP-7 Experimental Investigations of Scramjets 12-Jan 0930 hrs 1230 hrs Ft. Worth 3 474-HSABP-9/PGC-8 Pressure Gain Combustion - Rotating and Pulse Detonation Engines 13-Jan 0930 hrs 1300 hrs San Antonio 2 Information and Command & Control Systems 315-ICC-1 Information and Command and Control Systems 11-Jan 1400 hrs 1700 hrs Ft. Worth 2 Intelligent Systems 86-IS-1 Student Paper Competition 9-Jan 1400 hrs 1700 hrs Ft. Worth 1 143-IS-2 Run-Time Assurance for Adaptive and Intelligent Systems (Invited) 10-Jan 0930 hrs 1230 hrs Ft. Worth 1 196-IS-3 Learning, Reasoning, and Data Driven Systems 10-Jan 1400 hrs 1700 hrs Ft. Worth 1 263-IS-4 Adaptive and Intelligent Control Systems 11-Jan 0930 hrs 1230 hrs Ft. Worth 1 316-IS-5 Integrated Systems Health Management (ISHM) 11-Jan 1400 hrs 1530 hrs Ft. Worth 1 317-IS-6 Human Automation Interaction 11-Jan 1400 hrs 1700 hrs Ft. Worth 1 378-IS-7 Establishing Trust in Autonomous Systems 12-Jan 0930 hrs 1100 hrs Ft. Worth 1 396-IS-8 New Developments in ISHM for NASA Ground, Launch, and Flight 12-Jan 1100 hrs 1230 hrs Ft. Worth 1 Systems 428-IS-9 Probabilistic Rule-Based Systems 12-Jan 1400 hrs 1700 hrs Ft. Worth 1 International Student Conference 32-ISC-1 International Student Conference-Undergraduate Category 9-Jan 0930 hrs 1300 hrs Pecos 1 33-ISC-2 International Student Conference-Masters Category 9-Jan 0930 hrs 1300 hrs Longhorn Hall D

34-ISC-3 International Student Conference-Team Category 9-Jan 0930 hrs 1230 hrs Pecos 3 87-ISC-4 International Student Conference-Community Outreach Category 9-Jan 1400 hrs 1700 hrs Longhorn Hall D

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Abbreviation Title Date Start Time End Time Location Materials 36-MAT-1 Multifunctional Materials I 9-Jan 0930 hrs 1230 hrs Palomino 2 89-MAT-2 Multifunctional Materials II 9-Jan 1400 hrs 1700 hrs Palomino 1 90-MAT-3 Materials Testing and Characterization 9-Jan 1400 hrs 1700 hrs Palomino 2 145-MAT-4 Multiscale Modeling and Materials Design 10-Jan 0930 hrs 1230 hrs Palomino 2 197-MAT-5 Nanostructured Materials 10-Jan 1400 hrs 1700 hrs Palomino 2 318-MAT-6 Fatigue and Fracture 11-Jan 1400 hrs 1700 hrs Palomino 2 333-SUR-2/MAT-7 Materials/Materials for Survivability 11-Jan 1400 hrs 1700 hrs Palomino 3 379-MAT-8 Materials for Additive Manufacturing 12-Jan 0930 hrs 1230 hrs Palomino 2 Multidisciplinary Design Optimization 37-MDO-1 Aircraft Design Optimization I 9-Jan 0930 hrs 1230 hrs Mustang 1 57-TP-13/MDO-13 Hyperloop and Future High-Speed Transportation Concepts 9-Jan 0930 hrs 1230 hrs Dallas 5 38-MDO-2 Multifidelity Optimization 9-Jan 0930 hrs 1230 hrs Mustang 2 91-MDO-3 Aerodynamic Shape Optimization 9-Jan 1400 hrs 1700 hrs Mustang 1 146-MDO-4 Aeroelastic Optimization 10-Jan 0930 hrs 1230 hrs Mustang 1 150-NDA-2/MDO-5 Optimization Under Uncertainty I 10-Jan 0930 hrs 1230 hrs Mustang 2 198-MDO-6 Aero-Structures Optimization 10-Jan 1400 hrs 1700 hrs Mustang 1 264-MDO-7 Aircraft Design Optimization II 11-Jan 0930 hrs 1230 hrs Mustang 1 319-MDO-8 Topology and Structural Optimization 11-Jan 1400 hrs 1700 hrs Mustang 1 320-MDO-9 Emerging Methods and Algorithms in Optimization 11-Jan 1400 hrs 1700 hrs Mustang 3 380-MDO-10 Integrated Computational Materials Engineering (ICME) 12-Jan 0930 hrs 1230 hrs Mustang 1 429-MDO-11 Aircraft Design Optimization III 12-Jan 1400 hrs 1700 hrs Mustang 1 475-MDO-12/NDA-10 Optimization Under Uncertainty II 13-Jan 0930 hrs 1300 hrs Mustang 1 Modeling and Simulation Technologies 147-MST-1 Modeling and Simulation of Aeroelasticity and Structural Dynamics 10-Jan 0930 hrs 1230 hrs San Antonio 3 148-MST-2 Modeling and Simulation of Uninhabited Aerial Vehicles I 10-Jan 0930 hrs 1230 hrs San Antonio 2 199-MST-3 Modeling and Simulation of Air Traffic Management I 10-Jan 1400 hrs 1700 hrs San Antonio 3 200-MST-4 Modeling and Simulation of Uninhabited Aerial Vehicles II 10-Jan 1400 hrs 1700 hrs San Antonio 2 265-MST-5 Aviation Simulation Scenario Development I 11-Jan 0930 hrs 1230 hrs San Antonio 2 266-MST-6 Human Factors, Perception, Cueing I 11-Jan 0930 hrs 1230 hrs San Antonio 1 267-MST-7 Modeling and Simulation of Air Traffic Management II 11-Jan 0930 hrs 1230 hrs San Antonio 3 321-MST-8 Aviation Simulation Scenario Development II 11-Jan 1400 hrs 1700 hrs San Antonio 2 322-MST-9 Human Factors, Perception, Cueing II 11-Jan 1400 hrs 1700 hrs San Antonio 1 323-MST-10 Modeling and Simulation of Air Traffic Management III 11-Jan 1400 hrs 1700 hrs San Antonio 3 381-MST-11 Model and Simulation Design, Development, Testing, and Validation 12-Jan 0930 hrs 1230 hrs San Antonio 1 382-MST-12 Modeling and Simulation of Space Vehicle Dynamics, Systems, and 12-Jan 0930 hrs 1230 hrs Ft. Worth 7 Environments 383-MST-14 Modeling and Simulation of Uninhabited Aerial Vehicles III 12-Jan 0930 hrs 1230 hrs San Antonio 2 430-MST-15 Modeling and Simulation of Air Vehicle Dynamics, Systems, and 12-Jan 1400 hrs 1700 hrs San Antonio 1 Environments 431-MST-16 Modeling and Simulation in Education/Special Topics in Modeling and 12-Jan 1400 hrs 1700 hrs Ft. Worth 7 Simulation 432-MST-17 Modeling and Simulation Integration and Architectures 12-Jan 1400 hrs 1700 hrs Ft. Worth 6 476-MST-18 Modeling and Simulation of Propulsion Systems 13-Jan 0930 hrs 1300 hrs Ft. Worth 6

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Abbreviation Title Date Start Time End Time Location Meshing, Visualization, and Computational Environments 39-MVC-1 Visualization/Geometry Representation 9-Jan 0930 hrs 1230 hrs Grapevine 3 92-MVC-2 1st AIAA Geometry and Mesh Generation Workshop/High Lift 9-Jan 1400 hrs 1700 hrs Grapevine D Prediction Workshop 149-MVC-3 Meshing Techniques 10-Jan 0930 hrs 1230 hrs Grapevine 3 201-MVC-4 Computational Environments and the NASA CFD Vision 2030 Goals 10-Jan 1400 hrs 1700 hrs Grapevine D 477-MVC-5 Solution Adaptive Meshing and Error Estimation 13-Jan 0930 hrs 1300 hrs Palomino 1 Non-Deterministic Approaches 93-NDA-1 Reliability Analysis Methods and Applications 9-Jan 1400 hrs 1700 hrs Mustang 2 150-NDA-2/MDO-5 Optimization Under Uncertainty I 10-Jan 0930 hrs 1230 hrs Mustang 2 151-NDA-3 Uncertainty Quantification I 10-Jan 0930 hrs 1230 hrs Mustang 3 202-NDA-4 Special Session: Non-Deterministic Approaches for Integrated 10-Jan 1400 hrs 1700 hrs Mustang 2 Computational Materials Engineering 268-NDA-5 Special Session: DARPA Efficient Quantification of Uncertainty in 11-Jan 0930 hrs 1230 hrs Mustang 2 Physical Systems (EQUiPS) Program I 269-NDA-6 Special Session: Non-Deterministic Approaches for Aerospace Human- 11-Jan 0930 hrs 1230 hrs Mustang 3 in-the-Loop Related Missions 324-NDA-7 Special Session: DARPA Efficient Quantification of Uncertainty in 11-Jan 1400 hrs 1700 hrs Mustang 2 Physical Systems (EQUiPS) Program II 384-NDA-8 Special Session: Uncertainty Quantification and Management for the 12-Jan 0930 hrs 1230 hrs Mustang 2 Digital Thread and Twin 433-NDA-9 Model Calibration, Verification, and Validation 12-Jan 1400 hrs 1700 hrs Mustang 2 475-MDO-12/NDA-10 Optimization Under Uncertainty II 13-Jan 0930 hrs 1300 hrs Mustang 1 478-NDA-11 Uncertainty Quantification II 13-Jan 0930 hrs 1300 hrs Mustang 2 Space Operations and Support 325-OPS-1 Intelligent and Autonomous Systems for Improving Space Operation 11-Jan 1400 hrs 1700 hrs Grapevine 4 Pressure Gain Combustion 94-PC-5/PGC-2 Pressure Gain Combustion Detonative Propulsion Physics 9-Jan 1400 hrs 1700 hrs Ft. Worth 3 195-HSABP-4/PGC-3 Pressure Gain Combustion - Rotating Detonation Engines I 10-Jan 1400 hrs 1700 hrs Ft. Worth 3 262-HSABP-5/PGC-4 Pressure Gain Combustion - Rotating Detonation Engines II 11-Jan 0930 hrs 1230 hrs Ft. Worth 3 314-HSABP-6/PGC-5 Pressure Gain Combustion - Rotating Detonation Engines III 11-Jan 1400 hrs 1700 hrs Ft. Worth 3 427-GTE-9/PGC-6 Pressure Gain Combustion for Gas Turbines 12-Jan 1400 hrs 1700 hrs Grapevine C 474-HSABP-9/PGC-8 Pressure Gain Combustion - Rotating and Pulse Detonation Engines 13-Jan 0930 hrs 1300 hrs San Antonio 2 Propellants and Combustion 40-PC-2 Combustion Modeling and Simulation I 9-Jan 0930 hrs 1230 hrs San Antonio 6 41-PC-3 Alternate Aviation Fuels I 9-Jan 0930 hrs 1230 hrs San Antonio 5 42-PC-4 Combustion Diagnostics I: Applications 9-Jan 0930 hrs 1230 hrs San Antonio 2 94-PC-5/PGC-2 Pressure Gain Combustion Detonative Propulsion Physics 9-Jan 1400 hrs 1700 hrs Ft. Worth 3 95-PC-6 Combustion Modeling and Simulation II 9-Jan 1400 hrs 1700 hrs San Antonio 6 96-PC-7 Alternate Aviation Fuels II 9-Jan 1400 hrs 1700 hrs San Antonio 5 97-PC-8 Combustion Diagnostics II: Spectroscopy and Absorption 9-Jan 1400 hrs 1700 hrs San Antonio 2 98-PC-9 Advanced Combustion Concepts I 9-Jan 1400 hrs 1700 hrs Grapevine 3 152-PC-10 Detonations, Explosions, and Supersonic Combustion 10-Jan 0930 hrs 1230 hrs Ft. Worth 3 153-PC-11 Combustion Modeling and Simulation III 10-Jan 0930 hrs 1230 hrs San Antonio 6 154-PC-12 Chemical Kinetics for Multi-Component Fuels 10-Jan 0930 hrs 1230 hrs San Antonio 5 203-PC-13 Combustion Dynamics I 10-Jan 1400 hrs 1700 hrs Dallas 7 www.aiaa-SciTech.org 52 #aiaaSciTech IntroSessions at a Glance

Abbreviation Title Date Start Time End Time Location Propellants and Combustion (continued) 204-PC-14 Spray and Droplet Combustion 10-Jan 1400 hrs 1700 hrs Grapevine 4 205-PC-15 Solid Rockets 10-Jan 1400 hrs 1700 hrs San Antonio 6 206-PC-16 Combustion Chemistry 10-Jan 1400 hrs 1700 hrs San Antonio 5 270-PC-17 Combustion Dynamics II 11-Jan 0930 hrs 1230 hrs Dallas 7 271-PC-18 Super-Critical Combustion 11-Jan 0930 hrs 1230 hrs San Antonio 6 272-PC-19 Model Validation for Propulsion Workshop: Opening Session 11-Jan 0930 hrs 1230 hrs San Antonio 5 326-PC-20 Combustion Dynamics III 11-Jan 1400 hrs 1700 hrs Dallas 7 385-PC-22 Combustion Dynamics IV 12-Jan 0930 hrs 1230 hrs Dallas 7 386-PC-23 Model Validation for Propulsion Workshop I 12-Jan 0930 hrs 1230 hrs San Antonio 6 434-PC-24 Advanced Combustion Concepts II 12-Jan 1400 hrs 1700 hrs Grapevine 1 435-PC-25 Turbulent Combustion: Flow/Chemistry interactions 12-Jan 1400 hrs 1700 hrs Dallas 7 436-PC-26 Soot/Pyrolysis 12-Jan 1400 hrs 1700 hrs Ft. Worth 2 437-PC-27 Model Validation for Propulsion Workshop II 12-Jan 1400 hrs 1700 hrs San Antonio 6 438-PC-28 Shock Tubes 12-Jan 1400 hrs 1700 hrs Austin 4 439-PC-29 Laminar Flames I 12-Jan 1400 hrs 1700 hrs San Antonio 3 479-PC-30 Flame Stabilization/Blow Out 13-Jan 0930 hrs 1300 hrs San Antonio 1 480-PC-31 Jets in Cross-Flow 13-Jan 0930 hrs 1300 hrs Austin 3 481-PC-32 Laminar Flames II 13-Jan 0930 hrs 1300 hrs San Antonio 3 482-PC-33 Combustor Advances Enabled by Advanced Manufacturing 13-Jan 0930 hrs 1130 hrs Grapevine 1 483-PC-34 Model Validation for Propulsion Workshop: Closing Session 13-Jan 0930 hrs 1230 hrs Palomino 2 Plasmadynamics and Lasers 43-PDL-1 Plasma Aerodynamics I 9-Jan 0930 hrs 1230 hrs Ft. Worth 4 99-PDL-2 Plasma Aerodynamics II 9-Jan 1400 hrs 1700 hrs Ft. Worth 4 155-PDL-3 Diagnostics for Plasmas and Gases I 10-Jan 0930 hrs 1230 hrs Ft. Worth 4 207-PDL-4 Diagnostics for Plasmas and Gases II 10-Jan 1400 hrs 1700 hrs Ft. Worth 4 208-PDL-5 Computational Methods 10-Jan 1400 hrs 1700 hrs Ft. Worth 5 273-PDL-6 Plasma-Based Flow Control: Lessons Learned and Prospects I (Invited) 11-Jan 0930 hrs 1230 hrs Ft. Worth 4 274-PDL-7 Plasma and Laser Physics I 11-Jan 0930 hrs 1230 hrs Ft. Worth 5 327-PDL-8 Plasma-Based Flow Control: Lessons Learned and Prospects II 11-Jan 1400 hrs 1700 hrs Ft. Worth 4 (Invited) 328-PDL-9 Plasma and Laser Propulsion 11-Jan 1400 hrs 1700 hrs Ft. Worth 5 387-PDL-10 DBD Plasma Actuators I 12-Jan 0930 hrs 1230 hrs Ft. Worth 4 388-PDL-11 Plasma Assisted Combustion and Ignition I 12-Jan 0930 hrs 1230 hrs Ft. Worth 5 440-PDL-12 DBD Plasma Actuators II 12-Jan 1400 hrs 1700 hrs Ft. Worth 4 441-PDL-13 Diagnostics and Experimental Techniques 12-Jan 1400 hrs 1700 hrs Ft. Worth 5 484-PDL-14 Plasma and Laser Physics II 13-Jan 0930 hrs 1300 hrs Ft. Worth 5 485-PDL-15 Plasma Assisted Combustion and Ignition II 13-Jan 0930 hrs 1300 hrs Ft. Worth 4 Small Satellites 44-SATS-1 Small Satellite Missions 9-Jan 0930 hrs 1230 hrs Austin 4 45-SATS-2 Small Satellite Subsystems 9-Jan 0930 hrs 1230 hrs Austin 6 100-SATS-3 Small Satellite Software and Systems 9-Jan 1400 hrs 1700 hrs Austin 6 156-SATS-4 Small Satellite Mission Design 10-Jan 0930 hrs 1230 hrs Austin 6 209-SATS-5 Small Satellites - Fusion 10-Jan 1400 hrs 1700 hrs Austin 6 www.aiaa-SciTech.org 53 #aiaaSciTech IntroSessions at a Glance

Abbreviation Title Date Start Time End Time Location Spacecraft Structures 46-SCS-1 Deployable Booms and Flexures 9-Jan 0930 hrs 1230 hrs Palomino 1 157-SCS-2 Small Satellite Deployable Structures 10-Jan 0930 hrs 1230 hrs Palomino 1 210-SCS-3 Quantitative Determination of the Behavior of Deployable Structures 10-Jan 1400 hrs 1700 hrs Palomino 1 275-SCS-4 Membrane-Based Deployable Systems 11-Jan 0930 hrs 1230 hrs Palomino 1 329-SCS-5 Deployable Apertures and Novel Structural Concepts 11-Jan 1400 hrs 1700 hrs Palomino 1 Structural Dynamics 47-SD-1/APA-46 Special Session: Aerothermoelasticity of, and Dynamic Response in, 9-Jan 0930 hrs 1230 hrs Appaloosa 2 High Speed Vehicles and in High Speed Flow I 48-SD-2 Special Topics in Structural Dynamics and Aeroelasticity I 9-Jan 0930 hrs 1230 hrs Appaloosa 3 49-SD-3 Special Session: Aeroelastic Prediction I 9-Jan 0930 hrs 1230 hrs Appaloosa 4 101-SD-4/APA-47 Special Session: Aerothermoelasticity of, and Dynamic Response in, 9-Jan 1400 hrs 1700 hrs Appaloosa 2 High Speed Vehicles and in High Speed Flow II 102-SD-5 Special Topics in Structural Dynamics and Aeroelasticity II 9-Jan 1400 hrs 1700 hrs Appaloosa 3 103-SD-6 Special Session: Aeroelastic Prediction II 9-Jan 1400 hrs 1700 hrs Appaloosa 4 158-SD-7 Piezoelectric Materials for Active and Passive Vibration Control 10-Jan 0930 hrs 1230 hrs Appaloosa 2 159-SD-8 Vehicle and Component Response to Gust, Impact, and Thermal Loads 10-Jan 0930 hrs 1230 hrs Appaloosa 3 160-SD-9 Special Session: Aeroelastic Prediction III 10-Jan 0930 hrs 1230 hrs Appaloosa 4 211-SD-10 Computational Aero-, Servo-, Thermo- Elasticity 10-Jan 1400 hrs 1700 hrs Appaloosa 2 212-SD-11 Structural Health Monitoring and Prognosis, Model Uncertainty 10-Jan 1400 hrs 1700 hrs Appaloosa 3 213-SD-12 Special Session: Aeroelastic Prediction IV 10-Jan 1400 hrs 1700 hrs Appaloosa 4 276-SD-13 Flutter and Aeroelastic Analysis I 11-Jan 0930 hrs 1230 hrs Appaloosa 2 277-SD-14 Dynamic Testing Techniques and System Identification I 11-Jan 0930 hrs 1230 hrs Appaloosa 3 278-SD-15 Dynamics and Structural Dynamics of Launch Vehicles 11-Jan 0930 hrs 1230 hrs Appaloosa 4 330-SD-16 Aeroelastic Analysis 11-Jan 1400 hrs 1700 hrs Appaloosa 2 331-SD-17 Large-Deformation Nonlinear Dynamics, Flexible Multibody 11-Jan 1400 hrs 1700 hrs Appaloosa 3 Dynamics, Contact/Constraint Modeling 332-SD-18 Flutter and Aeroelastic Analysis II 11-Jan 1400 hrs 1700 hrs Appaloosa 4 389-SD-19 Special Session: Adaptive Aeroelastic Wing Shaping Control I 12-Jan 0930 hrs 1230 hrs Appaloosa 2 390-SD-20 Dynamic Loads, Response, Vibration, and Stability of Aerospace 12-Jan 0930 hrs 1230 hrs Appaloosa 3 Vehicles I 391-SD-21 Reduced Order Modeling 12-Jan 0930 hrs 1230 hrs Appaloosa 4 442-SD-22 Special Session: Adaptive Aeroelastic Wing Shaping Control II 12-Jan 1400 hrs 1700 hrs Appaloosa 2 443-SD-23 Dynamic Loads, Response, Vibration, and Stability of Aerospace 12-Jan 1400 hrs 1700 hrs Appaloosa 3 Vehicles II 444-SD-24 Dynamic Testing Techniques and System Identification II 12-Jan 1400 hrs 1700 hrs Appaloosa 4 486-SD-25 Active/Passive Vibration Control, Isolation, Stability Augmentation, 13-Jan 0930 hrs 1300 hrs Appaloosa 3 Damping 487-SD-26 Structural Dynamic Modeling of Beams, Cables, Membranes, Plates 13-Jan 0930 hrs 1300 hrs Appaloosa 4 and Shells Systems Engineering

161-SE-1 Systems Engineering I 10-Jan 0930 hrs 1230 hrs Dallas 6 214-SE-2 Systems Engineering II 10-Jan 1400 hrs 1700 hrs Dallas 6

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

Abbreviation Title Date Start Time End Time Location Sensor Systems 162-SEN-1 Novel Aerospace Sensor Systems 10-Jan 0930 hrs 1230 hrs Ft. Worth 2 215-SEN-2 Fusion of Networked Sensor and Systems 10-Jan 1400 hrs 1700 hrs Ft. Worth 2 279-SEN-3 Applications of Sensor and Information Fusion 11-Jan 0930 hrs 1230 hrs Ft. Worth 2 Software Systems 50-SOF-1 Verification vs Certification for Software Intense Systems 9-Jan 0930 hrs 1230 hrs Ft. Worth 7 104-SOF-2 Formal Methods for Software Verification 9-Jan 1400 hrs 1630 hrs Ft. Worth 7 163-SOF-3 Open Systems Architecture - Best Practices, Verification, and Security 10-Jan 0930 hrs 1230 hrs Ft. Worth 7 216-SOF-4 Software Challenges in Aerospace 10-Jan 1400 hrs 1700 hrs Ft. Worth 7 Space Resources Utilization 51-SRE-1 ISRU Technologies 9-Jan 0930 hrs 1230 hrs Ft. Worth 5 105-SRE-2 ISRU Mission Concepts 9-Jan 1400 hrs 1700 hrs Ft. Worth 5 164-SRE-3 Resource Harvesting 10-Jan 0930 hrs 1230 hrs Ft. Worth 5 Structures 52-STR-1 Composite Damage and Failure Prediction Methods I 9-Jan 0930 hrs 1230 hrs Mustang 3 53-STR-2 Aircraft Structural Design, Test and Analysis 9-Jan 0930 hrs 1230 hrs Appaloosa 1 106-STR-3 Other Topics in Structures I 9-Jan 1400 hrs 1700 hrs Mustang 3 107-STR-4 Composite Structure Design, Test and Analysis 9-Jan 1400 hrs 1700 hrs Appaloosa 1 165-STR-5 Composite Damage and Failure Prediction Methods II 10-Jan 0930 hrs 1230 hrs Appaloosa 1 217-STR-6 Buckling, Fatigue and Fracture of Structures I 10-Jan 1400 hrs 1700 hrs Mustang 3 218-STR-7 Composite Laminate and Structures Optimization 10-Jan 1400 hrs 1700 hrs Appaloosa 1 280-STR-8 Buckling, Fatigue and Fracture of Structures II 11-Jan 0930 hrs 1230 hrs Appaloosa 1 392-STR-10 Challenges in the Design of Joined Wings and Structural Joints 12-Jan 0930 hrs 1230 hrs Appaloosa 1 445-STR-11 Other Topics in Structures II 12-Jan 1400 hrs 1700 hrs Appaloosa 1 488-STR-12 Failure Analysis and Prediction 13-Jan 0930 hrs 1300 hrs Appaloosa 1 Survivability 281-SUR-1 Survivability 11-Jan 0930 hrs 1230 hrs Palomino 2 333-SUR-2/MAT-7 Materials/Materials for Survivability 11-Jan 1400 hrs 1700 hrs Palomino 3 Terrestrial Energy 393-TES-1 Fossil Fuel Power Technologies I 12-Jan 0930 hrs 1230 hrs Mustang 3 446-TES-2 Fossil Fuel Power Technologies II 12-Jan 1400 hrs 1700 hrs Mustang 3 447-TES-3 Emerging Energy Technologies I 12-Jan 1400 hrs 1700 hrs Palomino 1 489-TES-4 Emerging Energy Technologies II 13-Jan 0930 hrs 1300 hrs Mustang 3 Thermophysics 55-TP-1 Aerothermodynamics I 9-Jan 0930 hrs 1230 hrs Austin 2 57-TP-13/MDO-13 Hyperloop and Future High-Speed Transportation Concepts 9-Jan 0930 hrs 1230 hrs Dallas 5 56-TP-2 Heat Transfer I 9-Jan 0930 hrs 1230 hrs Austin 3 108-TP-3 Ablation 9-Jan 1400 hrs 1700 hrs Austin 2 109-TP-4 Experimental Heat Transfer 9-Jan 1400 hrs 1700 hrs Austin 3 166-TP-5 Aerothermodynamics II 10-Jan 0930 hrs 1230 hrs Austin 2 167-TP-6 Heat Transfer II 10-Jan 0930 hrs 1230 hrs Austin 3 219-TP-7 Thermal Protection Systems 10-Jan 1400 hrs 1700 hrs Austin 2 220-TP-8 Heat Pipes/Other Thermophysics Topics 10-Jan 1400 hrs 1700 hrs Austin 3 www.aiaa-SciTech.org 55 #aiaaSciTech SessionsIntro at a Glance

Abbreviation Title Date Start Time End Time Location Thermophysics (continued) 282-TP-9 Aerothermodynamics III 11-Jan 0930 hrs 1230 hrs Austin 3 334-TP-10 Nonequilibrium Radiation 11-Jan 1400 hrs 1700 hrs Austin 3 394-TP-11 Nonequilibrium Flows and Radiation 12-Jan 0930 hrs 1230 hrs Austin 3 448-TP-12 Direct Simulation Monte Carlo Methods 12-Jan 1400 hrs 1700 hrs Austin 3 Unmanned Systems 58-UMS-1 UAS Integration into Urban Environments 9-Jan 0930 hrs 1230 hrs Grapevine 2 110-UMS-2 Special Session: Safe Autonomous Urban Flight I 9-Jan 1400 hrs 1700 hrs Grapevine 1 168-UMS-4 Special Session: Safe Autonomous Urban Flight II 10-Jan 0930 hrs 1230 hrs Grapevine 1 169-UMS-5 UAS Autonomy and Path Planning I 10-Jan 0930 hrs 1230 hrs Grapevine 2 221-UMS-6 UAS Self-Separation and Collision Avoidance I 10-Jan 1400 hrs 1700 hrs Grapevine 1 222-UMS-7 UAS Safety and Certification/UAS Autonomy and Planning II 10-Jan 1400 hrs 1700 hrs Grapevine 2 283-UMS-8 UAS Self-Separation and Collision Avoidance II 11-Jan 0930 hrs 1230 hrs Grapevine 1 284-UMS-9 UAS Technologies and Applications I 11-Jan 0930 hrs 1230 hrs Grapevine 2 335-UMS-10 UAS Technologies and Applications II 11-Jan 1400 hrs 1700 hrs Grapevine 2 Wind Energy 111-WE-1 Wind Turbine Aeroelastics and Wakes 9-Jan 1400 hrs 1700 hrs Austin 4 170-WE-2 Wind Turbine Extreme Loads Analysis 10-Jan 0930 hrs 1230 hrs Austin 4 223-WE-3 Wind Turbine Airfoils and Aerodynamics Investigations 10-Jan 1400 hrs 1700 hrs Austin 4 224-WE-4 Offshore Wind Energy Applications 10-Jan 1400 hrs 1700 hrs Austin 5 285-WE-5 Atmospheric Inflow and Turbulence for Wind Energy 11-Jan 0930 hrs 1230 hrs Texas D 286-WE-6 Wind Turbine Structural Dynamics and Damage 11-Jan 0930 hrs 1230 hrs Ft. Worth 7 336-WE-8 Wind Turbine Rotor and Blade Innovations 11-Jan 1400 hrs 1700 hrs Ft. Worth 7 395-WE-9 Wind Energy Control and Optimization I 12-Jan 0930 hrs 1230 hrs Texas D 449-WE-10 Wind Energy Control and Optimization II 12-Jan 1400 hrs 1700 hrs Texas D 490-WE-11 Computational Methods for Wind Turbine Aerodynamics 13-Jan 0930 hrs 1300 hrs Dallas 7

www.aiaa-SciTech.org 56 #aiaaSciTech Sunday Sunday, 8 January 2017 1-NW-1 Meet the Employers Grapevine B 1500 - 1700 hrs Sunday, 8 January 2017 2-NW-2 Student Welcome Reception Mission Plaza 1800 - 1930 hrs All students welcome Monday Monday, 9 January 2017 3-NW-3 Monday Early Morning Networking Coffee Break Session Room Foyers 0700 - 0730 hrs Monday, 9 January 2017 4-SB-1 Monday Morning Speakers’ Brieﬁng Session Rooms 0730 - 0800 hrs Monday, 9 January 2017 5-PLNRY-1 Monday Morning Plenary: Setting the Landscape - Factors Driving Today’s Disruptive Environment Texas A & B 0800 - 0900 hrs Moderator: Robie Samanta Roy, Vice President, Technology Strategy & Innovation, Lockheed Martin Corporation

Panelists:

57 Chuck Beames Carissa Christensen David Whelan George Whitesides Consultant Managing Partner Vice President, Engineering & Chief Technologist CEO The Tauri Group Boeing Defense, Space & Security Virgin Galactic and The Spaceship Company The Boeing Company

Monday, 9 January 2017 6-NW-4 Monday Morning Networking Coffee Break Session Room Foyers 0900 - 0930 hrs Monday, 9 January 2017 7-AA-1 Aeroacoustics Jet Noise I Grapevine B Chaired by: K. AHUJA, Georgia Institute of Technology and A. LYRINTZIS 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2017-0001 AIAA-2017-0002 AIAA-2017-0003 AIAA-2017-0004 AIAA-2017-0005 AIAA-2017-0006 Modeling of Noise Reduction in Temperature effects on the Mach wave suppression by a pair An Investigation of Effects of Jet Investigation of Isolated and Flow and Noise Characteristics Complex Multistream Jets aerodynamic and acoustic fields of of subsonic helical modes in a Temperature on Twin-Jet Flow and Installed Three-Stream Jets from of Under- and Over-expanded D. Papamoschou, University of California, a rectangular supersonic jet supersonic jet Acoustic Fields Offset Nozzles Supersonic Rectangular Jets Irvine, Irvine, CA R. Gojon, Royal Institute of Technology (KTH), D. Watanabe, University of Toyama, J. Cluts, C. Kuo, M. Samimy, Ohio State V. Phong, D. Papamoschou, University of R. Johnson, K. Viswanath, A. Corrigan, K. Stockholm, Sweden; F. Baier, E. Gutmark, Toyama, Japan; H. Maekawa, University of University, Columbus, OH California, Irvine, Irvine, CA Kailasanath, Naval Research Laboratory, University of Cincinnati, Cincinnati, OH; M. Electro-Communications, Chofu, Japan Washington, D.C.; P. Mora , F. Baier, University Mihaescu, Royal Institute of Technology (KTH), of Cincinnati, Cincinnati, OH; et al. Stockholm, Sweden Monday, 9 January 2017 8-ACD-1 Aircraft Design Tools and Methods I San Antonio 1 Chaired by: R. VOS, TU Delft fac. Aerospace Engineering and J. MERRET, Gulfstream Aerospace Corporation 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2017-0007 AIAA-2017-0008 AIAA-2017-0009 AIAA-2017-0010 An Introduction to the Impact of Generalized Methodology for Sizing Initial Weight Estimate of Advanced A Business-Driven Optimization Pilot Techniques Upon “Certified” Unconventional Propulsion and Transport Aircraft Concepts Methodology Applied to Commercial Field Performance Configuration Aircraft Considering Aeroelastic Effects Aviation Programs T. Takahashi, D. Wood, Arizona State G. Bucsan, K. Collins, D. Mavris, Georgia G. P. Chiozzotto, German Aerospace Center F. Burgaud, M. Pokhrel, D. Mavris, Georgia University, Tempe, AZ; L. Bays, DragonFly Institute of Technology, Atlanta, GA (DLR), Göttingen, Germany Institute of Technology, Atlanta, GA Aeronautics, LLC, Kennesaw, GA Monday, 9 January 2017 9-ACD-2 Unmanned Aircraft Design I San Antonio 3 Chaired by: Z. MIAN, United Technologies Research Center and D. WELLS, NASA Langley Research Center 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2017-0011 AIAA-2017-0012 AIAA-2017-0013 AIAA-2017-0014 AIAA-2017-0015 A Variable Forward-Sweep Wing Design, Construction, and Flight Conceptual Design of a Man- Design Methodology for Small Scale Robust Design of Small-Scale Design for Enhanced Perching in Testing of the World’s Fastest Micro- Portable Ornithopter Unmanned Quadrotors Unmanned Helicopter for Hover Micro Aerial Vehicles Scale Quadcopter A. Moodie, A. Gallaher, Army Aviation J. Winslow, V. Hrishikeshavan, I. Chopra, Performance using Taguchi Method Z. Manchester, Harvard University, R. Bramlette, T. Johnston, R. Barrett- and Missile Research Development and University of Maryland, College Park, A. D. R., R. Ganguli, D. Harursampath, Cambridge, MA; J. Lipton, Massachusetts Gonzalez, University of Kansas, Lawrence, Engineering Center, Redstone Arsenal, AL College Park, MD Indian Institute of Science, Bengaluru, Institute of Technology, Cambridge, MA; R. Lawrence, KS India; P. Friedmann, University of Michigan, Wood, S. Kuindersma, Harvard University, Ann Arbor, Ann Arbor, MI Cambridge, MA Monday, 9 January 2017 58 10-AFM-1 Aeroservoelastic (ASE) Control, Modeling, Simulation, and Optimization Grapevine 5 Chaired by: T. ALEXEEV, University of California, San Diego and A. DA RONCH, University of Southampton 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2017-0016 AIAA-2017-0017 AIAA-2017-0018 AIAA-2017-0019 AIAA-2017-0020 AIAA-2017-0021 Multidimensional discrete gust loads Control surface modelling for fast Real Time Modal Identification of a Aeroservoelastic Modeling of Body Redesign of a Human Powered Impact of Rotor Blade Aeroelasticity of a large civil flexible aircraft simulation of large flexible aircraft Flexible Unmanned Aerial Vehicle Freedom Flutter for Control System Aircraft using the Boxplane Concept on Rotorcraft Flight Dynamics G. Dussart, M. Lone, S. Guo, Cranfield A. Pontillo, G. Dussart, M. Lone, D. P. Schulze, B. Danowsky, P. Yang, Systems Design A. Collazo Garcia, L. Gonzalez-Linero, S. Weber, Airbus, Kidlington, United University, Cranfield, United Kingdom Fleischmann, Cranfield University, Cranfield, Technology, Inc., Hawthorne, CA; C. Harris, J. Ouellette, NASA Armstrong Flight Embry-Riddle Aeronautical University, Kingdom; L. Ramos Valle, X. Barral, D. United Kingdom; E. Coetzee, Airbus, Air Force Test Center, Edwards AFB, CA Research Center, Edwards, CA Daytona Beach, FL Hayes, M. Lone, A. Cooke, Cranfield Bristol, United Kingdom University, Cranfield, United Kingdom Monday, 9 January 2017 11-AMT-1 Velocimetry: Applications I Grapevine 6 Chaired by: K. LOWE, Virginia Tech and P. LAVOIE, University of Toronto 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2017-0022 AIAA-2017-0023 AIAA-2017-0024 AIAA-2017-0025 AIAA-2017-0026 Three-Component Velocity Comparison of stereo-PIV and “Postage-Stamp PIV:” Small Velocity Two-Dimensional Krypton Tagging FLEET Velocimetry Measurements on Measurements in a Turbine Engine plenoptic-PIV measurements on the Fields at 400 kHz for Turbulence Velocimetry (KTV) Investigation of a Transonic Airfoil Exhaust wake of a cylinder in NASA ground Spectra Measurements Shock Wave/Turbulent Boundary- R. Burns, P. Danehy, NASA Langley T. Jenkins, C. Hess, R. Morgan, MetroLaser, test facilities. S. Beresh, J. Henfling, R. Spillers, Sandia Layer Interaction Research Center, Hampton, VA Inc., Laguna Hills, CA; J. Seitzman, S. T. Fahringer, B. Thurow, Auburn University, National Laboratories, Albuquerque, NM M. Mustafa, M. Hunt, N. Parziale, Stevens Adusumilli, Georgia Institute of Technology, Auburn, AL; W. Humphreys, S. Bartram, NASA Institute of Technology, Hoboken, NJ; M. Atlanta, GA Langley Research Center, Hampton, VA Smith, Aerospace Testing Alliance, Silver Spring, MD; E. Marineau, Arnold Engineering Development Complex, Silver Spring, MD Monday, 9 January 2017 12-AMT-2 Temperature Measurements and Applications Grapevine 4 Chaired by: C. DEDIC, Iowa State University and J. MILLER, USAF/AFRL/RQTC 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2017-0027 AIAA-2017-0028 AIAA-2017-0029 AIAA-2017-0030 AIAA-2017-0031 AIAA-2017-0032 Temperature measurements in a wall Spatially correlated temperature, See-through-wall Radar REMPI for Investigation of energy distributions Two-Beam Femtosecond Rotational Femtosecond Chirped-Probe-Pulse stabilized steady flame using CARS oxygen, and fuel measurements Spatially Localized Temperature behind a microscale gas-phase CARS for One-Dimensional Coherent Anti-Stokes Raman K. Sesha Giri, D. Lacoste, King Abdullah in a plasma-assisted hydrogen Measurements in a Well-Stirred detonation tube using hybrid fs/ Thermometry in a Turbulent, Scattering Thermometry of Nitrogen University of Science and Technology, Thuwal, diffusion flame by one-dimensional Reactor ps coherent anti-Stokes Raman Sooting Jet Flame in a Piloted Spray Burner Saudi Arabia; J. Damazo, E. Kwon, The Boeing fs/ps rotational CARS imaging Y. Wu, M. Gragston, Z. Zhang, University scattering D. Richardson, S. Roy, Spectral Energies, L. Thomas, Purdue University, West Lafayette, Company, Seattle, WA; W. Roberts, King J. Retter, G. Elliott, University of Illinois, Urbana- of Tennessee, Knoxville, Knoxville, TN; R. C. Dedic, J. Michael, Iowa State University, LLC, Dayton, OH; J. Gord, Air Force IN; A. Lowe, University of Sydney, Sydney, Abdullah University of Science and Technology, Champaign, Urbana, IL; S. Kearney, Sandia Stachler, J. Heyne, S. Stouffer, University Ames, IA; T. Meyer, Purdue University, West Research Laboratory, Wright-Patterson Australia; A. Satija, R. Lucht, Purdue University, Thuwal, Saudi Arabia National Laboratories, Albuquerque, NM of Dayton, Dayton, OH; et al. Lafayette, IN AFB, OH; S. Kearney, Sandia National West Lafayette, IN; A. Masri, University of Laboratories, Albuquerque, NM Sydney, Sydney, Australia Monday, 9 January 2017 13-APA-1 Aerodynamic Design: Analysis, Methodologies and Optimization Techniques I Dallas 1 Chaired by: N. HALL, Lockheed Martin and K. KONTIS, University of Glasgow 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2017-0033 AIAA-2017-0034 AIAA-2017-0035 AIAA-2017-0036 AIAA-2017-0037 Wing Optimization using Dual Numerical Investigation of the Efficient variable-fidelity multi-point Three-Dimensional Subdivision An Efficient Reduced-Order-Model Number Automatic Differentiation Effect of Geometric Design aerodynamic shape optimization Parameterisation for Aerodynamic for Accurate Projection of Adjoint in MachUp Parameters on Swirl Brake based on hierarchical kriging Shape Optimisation Sensitivities J. Hodson, D. Hunsaker, R. Spall, Utah Performance M. Huang, X. Yang, Northwestern D. Masters, University of Bristol, Bristol, United A. Kaminsky, R. Djeddi, K. Ekici, University State University, Logan, UT N. Matula, P. Cizmas, Texas A&M Polytechnical University, Xi’an, China; X. Kingdom; N. Taylor, MBDA, Bristol, United of Tennessee, Knoxville, Knoxville, TN University, College Station, TX Peng, Midea Global Innovation Center, Kingdom; T. Rendall, C. Allen, University of FoShan, China Bristol, Bristol, United Kingdom 59 Monday, 9 January 2017 14-APA-2 Special Session: Low Boom Activities I Dallas 2 Chaired by: K. WAITHE, Boom Technology Inc and G. CARRIER, ONERA/DAAP 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2017-0038 AIAA-2017-0039 AIAA-2017-0040 AIAA-2017-0041 AIAA-2017-0042 AIAA-2017-0043 Near Field Sonic Boom Analysis with Wing Planform Optimization Impact of Aeroelastic Uncertainties Nozzle Plume/Shock Interaction Sonic Computational Evaluations of Retroreflective Background- HUNS3D Solver Method for Low-Boom and Low- on Sonic Boom Signature of a Boom Test Results from the NASA Experimental Data for Sonic Oriented Schlieren Imaging Results B. Ma, G. Wang, J. Ren, Z. Ye, Drag Aircraft Commercial Supersonic Transport Ames 9- by 7-Foot Supersonic Wind Boom Models with Nozzle Jet Flow from the NASA Ames Plume-Shock Northwestern Polytechnical University, Y. Kasuga, University of Tokyo, Kashiwa, Configuration Tunnel Interactions Interaction Test Xi’an, China; G. Zha, University of Miami, Japan; K. Yoshida, Japan Aerospace M. Nikbay, National Institute of Aerospace, D. Durston, S. Cliff, M. Denison, D. Dalle, J. Jensen, M. Denison, Science and N. Smith, AerospaceComputing, Inc., Coral Gables, FL Exploration Agency (JAXA), Chofu, Japan; Hampton, VA; B. Stanford, T. West, NASA NASA Ames Research Center, Moffett Field, Technology Corporation, Moffett Field, Moffett Field, CA; D. Durston, J. Heineck, H. Ishikawa, ASIRI Corporation, Chiyoda, Langley Research Center, Hampton, VA; CA; R. Castner, NASA Glenn Research Center, CA; S. Cliff, NASA Ames Research Center, NASA Ames Research Center, Moffett Japan S. Rallabhandi, National Institute of Cleveland, OH; A. Elmiligui, NASA Langley Moffett Field, CA Field, CA Aerospace, Hampton, VA Research Center, Hampton, VA; et al. Monday, 9 January 2017 15-APA-3 Environmentally Friendly/Efficient Aerodynamics and Enabling Technology I Dallas 3 Chaired by: G. DALE, U.S. Air Force Research Laboratory and P. MCCLURE, Lockheed Martin Aeronautics 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2017-0044 AIAA-2017-0045 AIAA-2017-0046 AIAA-2017-0047 AIAA-2017-0048 AIAA-2017-0049 Prospects for the Application of Viscous Drag Measurements on Development of an Elastomeric Riblet Microfabrication Method for Design and Testing of Conventional Evaluation of Structured Roughness Practical Drag Reduction Technologies Non-Smooth Surfaces Balance for Evaluation of Drag Drag Reduction Riblets and 3-D Riblets with for Separation Control and Drag to Legacy Transport Aircraft J. Naughton, E. DeMillard, University of Reduction Materials H. Bilinsky, MicroTau Pty., Ltd., Sydney, Streamwise Variable Height Reduction W. Felder, Stevens Institute of Technology, Wyoming, Laramie, Laramie, WY; G. Dale, J. Crafton, J. Webb, R. Forlines, Innovative Australia P. McClure, B. Smith, W. Baker, P. Yagle, B. Smith, W. Baker, P. Yagle, Lockheed Hoboken, NJ; G. Dale, Air Force Research Air Force Research Laboratory, Wright- Scientific Solutions, Inc., Dayton, OH Lockheed Martin Corporation, Fort Worth, TX Martin Aeronautics Company, Fort Worth, Laboratory, Dayton, OH; C. Cash, Ohio Patterson AFB, OH TX Aerospace Institute, Cleveland, OH; M. Chang, General Atomics, Palmdale, CA Monday, 9 January 2017 16-APA-4 Propeller/Rotorcraft/Wind Turbine Aerodynamics I: Coaxial and Open Rotor Dallas 4 Chaired by: J. RAULEDER, Technical University of Munich and R. RAMAMURTI, Naval Research Laboratory 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2017-0050 AIAA-2017-0051 AIAA-2017-0052 AIAA-2017-0053 Real-Time Simulation of Dynamic Application of Vortex Methods Computations of Torque-Balanced Initial Development of Physics- Inflow Using Rotorcraft Flight to Coaxial Rotor Wake and Load Coaxial Rotor Flows Based Aeroanalysis Methods for Dynamics Coupled With a Lattice- Calculations S. Yoon, W. Chan, T. Pulliam, NASA Ames Open Rotor Conceptual Design Boltzmann Based Fluid Simulation P. Singh, P. Friedmann, University of Research Center, Moffett Field, CA T. Quackenbush, A. Boschitsch, M. Yu, J. Bludau, J. Rauleder, L. Friedmann, M. Michigan, Ann Arbor, Ann Arbor, MI Continuum Dynamics, Inc., Ewing, NJ Hajek, Technical University of Munich, Munich, Germany Monday, 9 January 2017 17-ASC-1 Adaptive and Morphing Aircraft and Aeroelasticity Palomino 3 Chaired by: D. MCGOWAN, NASA Langley Research Center and R. BOTEZ, Ecole de Technologie Superieure 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2017-0054 AIAA-2017-0055 AIAA-2017-0056 AIAA-2017-0057 AIAA-2017-0058 AIAA-2017-0059 Design optimization toward a shape A novel span-wise morphing trailing Aerodynamic Step Input Response Experimental Verification of a Semi- Novel growing micro unmanned air Design, Analysis and Experimental memory alloy-based bio-inspired edge concept of Electro-Active Membrane Wings Active Piezoelectric Pitch Link for vehicle: sizing process and spanning Testing of a Morphing Wing morphing wing Q. Ai, P. Weaver, University of Bristol, I. Barbu, R. de Kat, B. Ganapathisubramani, Helicopter Vibration Attenuation actuation J. Martinez, Technical University of Madrid, P. Leal, R. Petterson, D. Hartl, Texas A&M Bristol, United Kingdom University of Southampton, Southampton, M. Clementino, University of São Paulo, A. Quintana, M. Hassanalian, A. Abdelkefi, Madrid, Spain; D. Scopelliti, Technical University, College Station, TX United Kingdom São Carlos, Brazil; F. Nitzsche, Carleton New Mexico State University, Las Cruces, NM University of Turin, Turin, Italy; C. Bil, R. University, Ottawa, Canada; C. De Marqui, Carrese, P. Marzocca, RMIT University, University of São Paulo, São Carlos, Brazil Melbourne, Australia Monday, 9 January 2017 60 18-CMS-1 Communication Systems Ft. Worth 1 Chaired by: D. PONCHAK, NASA Glenn Research Center 0930 hrs 1000 hrs 1030 hrs AIAA-2017-0060 AIAA-2017-0061 AIAA-2017-0062 Performance Based Link Restart Investigating Encrypted IEEE Achieving Agreement In Three Concept for Aeronautical 802.15.4 and DigiMesh Rounds With Bounded-Byzantine Telecommunications Network (ATN) Communications for Small Faults Performance Improvement Unmanned Systems M. Malekpour, NASA Langley Research D. Zeng, J. Gonda, MITRE Corporation, M. Leccadito, B. Yemaneberhane, C. Center, Hampton, VA McLean, VA Nimo, T. Bakker, R. Klenke, Virginia Commonwealth University, Richmond, VA Monday, 9 January 2017 19-DA-1 Digital Avionics Grapevine 1 Chaired by: D. ABERNATHY, Lockheed Martin Aeronautics and M. UIJT DE HAAG, Ohio University 0930 hrs 1000 hrs 1030 hrs AIAA-2017-0063 AIAA-2017-0064 AIAA-2017-0065 Exploring a Model Predictive A Tripartite Concept of a Remote- Experience with Sensed and Derived Control Law to Design Four- Copilot Center for Commercial Angle of Attack Estimation Systems Dimensional Trajectories for Interval Single-Pilot Operations in a General Aviation Airplane Management D. Schmid, B. Korn, German Aerospace B. Jackson, K. Hoffler, Adaptive Aerospace X. Bai, Rutgers University, Piscataway, NJ; Center (DLR), Braunschweig, Germany Group, Inc., Hampton, VA; D. Sizoo, W. L. Weitz, MITRE Corporation, McLean, VA Ryan, Federal Aviation Administration, Kansas City, MO Monday, 9 January 2017 20-F360-1 CREATE: Enabling Innovation Through Computational Prototypes and Supercomputers Texas C 0930 - 1130 hrs Moderator: Paul Nielsen, Director and Chief Executive Officer, Software Engineering Institute, Carnegie Mellon University

Panelists: Edward Kraft Robert L. Meakin Scott A. Morton Robert Narducci Douglass Post Brian Smith Technical Advisor, Air Force Test Center CREATE Air Vehicles Project Manager CREATE, Kestrel Principal Software Developer Technical Fellow Chief Scientist Fellow, ADP Program and Technology Air Force Material Command High Performance Computing High Performance Computing The Boeing Company High Performance Computing Integration U.S. Air Force Modernization Program Modernization Program Modernization Program Lockheed Martin Aeronautics Department of Defense Department of Defense Department of Defense

Monday, 9 January 2017 21-FD-1 Boundary Layer Stability and Transition I Texas 1 Chaired by: A. SESCU, Mississippi State University and P. PAREDES, NASA Langley Research Center 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2017-0066 AIAA-2017-0067 AIAA-2017-0068 AIAA-2017-0069 AIAA-2017-0070 Transient Growth and Streak Direct Numerical Simulation of Boundary-Layer Transition Non-Equilibrium Effects on the Real gas effects on receptivity to Instabilities on a Hypersonic Blunt Hypersonic Turbulent Boundary Layers Measurements in the Boeing/AFOSR Stability of a Mach 10 Flat-Plate kinetic fluctuations Body inside an Axisymmetric Nozzle Mach-6 Quiet Tunnel Boundary Layer L. Edwards, A. Tumin, University of Arizona, P. Paredes, M. Choudhari, F. Li, NASA J. Huang, C. Zhang, L. Duan, Missouri K. Gray, B. Chynoweth, J. Edelman, G. X. Wang, University of Alabama, Tucson, Tucson, AZ Langley Research Center, Hampton, VA University of Science and Technology, Rolla, McKiernan, M. Wason, S. Schneider, Tuscaloosa, Tuscaloosa, AL MO; M. Choudhari, NASA Langley Research Purdue University, West Lafayette, IN Center, Hampton, VA Monday, 9 January 2017 22-FD-2 Cartesian and Overset CFD Methods Texas 2 61 Chaired by: M. GALBRAITH and J. BENEK, Air Force Research Lab AFRL/RQ 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2017-0071 AIAA-2017-0072 AIAA-2017-0073 AIAA-2017-0074 Isolating Flow-field Discontinuities An Effcient, High-Order, Hybrid Optimal multi-block mesh Validation of High-Order Methods while Preserving Monotonicity and Unstructured and Adaptive generation for CFD of Three-Dimensional Strand Grids High-order Accuracy on Cartesian Cartesian Mesh Approach for Z. Ali, P. Dhanasekaran, P. Tucker, R. with an Overset Cartesian Grid Meshes External Aerodynamics Watson, Cambridge University, Cambridge, D. Work, Y. Yanagita, A. Katz, Utah State N. Mundis, ERC, Inc., Edwards AFB, CA; C. K. Puri, S. Frankel, Technion--Israel Institute United Kingdom; S. Shahpar, Rolls-Royce University, Logan, UT Lietz, Sierra Lobo, Inc., Edwards AFB, CA; of Technology, Haifa, Israel Group plc, Derby, United Kingdom K. Brown, V. Sankaran, Air Force Research Laboratory, Edwards AFB, CA Monday, 9 January 2017 23-FD-3 CFD Applications Texas 3 Chaired by: K. SREENIVAS, SimCenter: Center for Excellence in Applied Computational Science and Engineering and L. WANG, National Institute of Aerospace 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2017-0075 AIAA-2017-0076 AIAA-2017-0077 AIAA-2017-0078 AIAA-2017-0079 AIAA-2017-0080 Frequency Domain Approach for Application of Exact Error Transport Stabilized Finite Elements in FUN3D Numerical Investigation of Recent Advances in Scaling Up A Non-Linear Harmonic Balance Transonic Aerodynamic Modelling Equations and Adjoint Error W. Anderson, NASA Langley Research Helicopter Blade Section Complex Fluid-Structure Interaction Method for Turbomachinery Applied to a Viscous Wing Estimation to AIAA Workshops Center, Hampton, VA; J. Newman, Undergoing Time-Periodic Motions Simulations Applications A. Poncet-Montanges, D. Jones, A. J. Derlaga, M. Park, NASA Langley Univerisity of Tennessee at Chattanooga, G. Wen, A. Gross, New Mexico State R. Lohner, F. Mut, F. Camelli, George G. Cvijetic, H. Jasak, University of Zagreb, Gaitonde, J. Cooper, University of Bristol, Research Center, Hampton, VA Chattanooga, TN; S. Karman, Pointwise, University, Las Cruces, NM Mason University, Fairfax, VA; J. Baum, O. Zagreb, Croatia; G. Contento, G. Lupieri, Bristol, United Kingdom; Y. Lemmens, Inc., Fort Worth, TX Soto, F. Togashi, Applied Simulations, Inc., University of Trieste, Trieste, Italy Siemens, Leuven, Belgium McLean, VA; et al. Monday, 9 January 2017 24-FD-4 CFD Methods for Compressible Flows I Texas 4 Chaired by: R. SINGH, General Electric Global Research and H. NISHIKAWA, National Institute of Aerospace 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2017-0081 AIAA-2017-0082 AIAA-2017-0083 AIAA-2017-0084 AIAA-2017-0085 Hyperbolic Navier-Stokes Method An hp-Adaptive Unstructured Finite An Oscillation-Suppressing Inviscid Entropy stable Discontinuous Finite-Element Formulation of a for High-Reynolds-Number Volume Solver for Compressible Compressible Flow Solver Based Galerkin Scheme for the Jacobian-free Solver for Supersonic Boundary Layer Flows Aerodynamic Flows on a CE/SE Inspired Second-Order compressible Navier-Stokes Viscous Flows on Hybrid Grids H. Nishikawa, Y. Liu, National Institute of A. Jalali, C. Ollivier Gooch, University of Spacetime Cell-Vertex Scheme Equations S. Gao, W. Habashi, M. Fossati, McGill Aerospace, Hampton, VA British Columbia, Vancouver, Canada S. Tu, Q. Pang, Jackson State University, M. Zakerzadeh, G. May, RWTH Aachen University, Montréal, Canada; D. Isola, G. Jackson, MS University, Aachen, Germany Baruzzi, ANSYS, Inc., Montréal, Canada Monday, 9 January 2017 25-FD-6 Experiments and Numerical Simulations of Shock Dominated Flows Austin 1 Chaired by: J. LARSSON, University of Maryland and M. GAMBA, University of Michigan 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2017-0086 AIAA-2017-0087 AIAA-2017-0088 AIAA-2017-0089 AIAA-2017-0090 AIAA-2017-0091 Dimensionless scaling of heat- Unsteadiness characteristics and Periodic forcing of a shock train in Simulation of Blast Wave Characteristics of Self-Sustained- On The Interaction of Oblique release-induced planar shock waves three-dimensional leading shock Mach 2.0 flow Propagation and Mushroom Cloud Shock Pulsation around a Forward- Shocks and Laminar Mixing Layers in near-critical CO2 structure of a Mach 2.0 shock train R. Hunt, J. Driscoll, M. Gamba, University formation by a Bomb Explosion Facng Concave with Spike D. Martinez-Ruiz, National Center for Scientific M. Migliorino, C. Scalo, Purdue University, R. Hunt, J. Driscoll, M. Gamba, University of Michigan, Ann Arbor, Ann Arbor, MI J. Kim, BOOLT Simulation Technology, T. Mizukaki, Tokai University, Hiratsuka, Research (CNRS), Marseille, France; C. Huete, West Lafayette, IN of Michigan, Ann Arbor, Ann Arbor, MI Seoul, South Korea Japan; K. Yamada, Japan Aerospace Charles III University of Madrid, Leganes, Exploration Agency (JAXA), Sagamihara, Spain; A. Sanchez, F. Williams, University of Japan California, San Diego, La Jolla, CA Monday, 9 January 2017 26-FD-7 Low-Re and Bio-Inspired Flows I: Applications Grapevine C 62 Chaired by: M. GREEN, Syracuse University and K. MULLENERS, EPFL 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2017-0092 AIAA-2017-0093 AIAA-2017-0094 AIAA-2017-0095 AIAA-2017-0096 Nonlinear Hydrodynamic Effects of Altitude on the Flight Wake Structure Induced by Seal Singularity Methods for Modeling The effects of advance ratio and Interaction in Fish Swimming Performance of Monarch Butterflies Whisker: Effects of Cross-section Airfoil Flows with Dynamic Stall and blade number on the forward flight M. Khalid, I. Akhtar, National University C. Kang, M. Sridhar, D. Landrum, Y. Rotation Angle Fast Flap Deflections efficiency of cycloidal rotor of Sciences and Technology, Rawalpindi, Nakamura, University of Alabama, A. Rinehart, W. Zhang, Cleveland State N. Laws, B. Epps, Dartmouth College, Y. Hu, G. Wang, H. Zhang, Northwestern Pakistan; H. Dong, University of Virginia, Huntsville, Huntsville, AL; H. Aono, Tokyo University, Cleveland, OH; V. Shyam, NASA Hanover, NH; A. Medina, M. Ol, Air Force Polytechnical University, Xi’an, China; Charlottesville, Charlottesville, VA; H. University of Science, Tokyo, Japan Glenn Research Center, Cleveland, OH Research Laboratory, Wright-Patterson J. Liu, Xi’an Jiaotong University, Xi’an, Imtiaz, National University of Sciences and AFB, OH China; X. Yang, B. Zhu, Northwestern Technology, Rawalpindi, Pakistan Polytechnical University, Xi’an, China Monday, 9 January 2017 27-GEPC-1 Hybrid Wing Body Texas 6 Chaired by: D. CHAN, NASA-Langley Research Center and R. PLUMLEY 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2017-0097 Oral Presentation AIAA-2017-0098 AIAA-2017-0099 AIAA-2017-0100 AIAA-2017-0101 Revolutionary Configurations: Recent Progress Towards the Transonic Semispan Aerodynamic Hybrid Wing Body Performance Powered Low Speed Testing of the Structural Layout of a Hybrid Wing Technology Convergence Point Lockheed Martin Hybrid Wing Body Testing of the Hybrid Wing Body with Validation at the National Transonic Hybrid Wing Body Body Transport R. Plumley, C. Zeune, Air Force Research Airlifter Concept Over Wing Nacelles in the National Facility A. Wick, J. Hooker, C. Clark, Lockheed J. Action, Lockheed Martin Corporation, Laboratory, Wright-Patterson AFB, OH A. Wick, J. Hooker, Lockheed Martin Transonic Facility A. Wick, J. Hooker, J. Walker, Lockheed Martin Corporation, Marietta, GA; R. Marietta, GA Corporation, Marietta, GA D. Chan, NASA Langley Research Center, Martin Corporation, Marietta, GA; D. Chan, Plumley, C. Zeune, Air Force Research Hampton, VA; J. Hooker, A. Wick, Lockheed NASA Langley Research Center, Hampton, Laboratory, Wright-Patterson AFB, OH Martin Corporation, Marietta, GA; R. Plumley, VA; R. Plumley, C. Zeune, Air Force C. Zeune, M. Ol, Air Force Research Laboratory, Research Laboratory, Wright-Patterson Wright-Patterson AFB, OH; et al. AFB, OH Monday, 9 January 2017 28-GT-1 Design, Calibration and Performance of Ground Test Facilities and Subsystems Ft. Worth 6 Chaired by: J. MICOL, NASA-Langley Research Center and M. RIVERS, NASA Langley Research Center 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2017-0102 AIAA-2017-0103 AIAA-2017-0104 AIAA-2017-0105 AIAA-2017-0106 AIAA-2017-0107 AFRL Ludwieg Tube Initial Performance The Supersonic Combustion Facility Design, Build, and Test of a Thrust Design fabrication and Estimating Balance Uncertainty By Assessment of calibration data R. Kimmel, M. Borg, J. Jewell, K. Lam, Air ACT-2 Test Stand performances of a closed circuit Monte Carlo Simulation on a High- using the JAXA automatic balance Force Research Laboratory, Wright-Patterson D. Baccarella, Q. Liu, T. Lee, University of J. Mondragon, J. Hubbard, University of subsonic wind tunnel Speed Parallel architecture. calibration machine AFB, OH; R. Bowersox, R. Srinivasan, Texas Illinois, Urbana-Champaign, Urbana, IL; H. Do, Maryland, College Park, College Park, MD E. Rubino, T. Ioppolo, Southern Methodist P. Bidgood, Council for Scientific and M. Kohzai, N. Sudani, Japan Aerospace A&M University, College Station, TX; et al. Seoul National University, Seoul, South Korea University, Dallas, TX Industrial Research, Pretoria, South Africa Exploration Agency (JAXA), Tokyo, Japan Monday, 9 January 2017 29-GTE-1 Turbomachinery Technologies Ft. Worth 2 Chaired by: S. SUBRAMANIAN, QuEST Global, Inc. 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2017-0108 AIAA-2017-0109 AIAA-2017-0110 AIAA-2017-0111 Computational Investigation of A Computational Study of From Conceptual 1D Design Towards Using of low-pressure compressor to Secondary Flow Structures in Low Combustor Dilution Flow Interaction Full 3D Optimization of a Highly design the concept of the air brake Pressure Turbines with Turbine Vanes Loaded Turbine Stage system J. Sharpe, P. Bear, M. Wolff, Wright K. Muirhead, S. Lynch, Pennsylvania State P. Juangphanich, C. De Maesschalck, G. Popov, O. Baturin, Y. Novikova, E. State University, Dayton, OH; C. Marks, University, University Park, PA G. Paniagua, Purdue University, West Goriachkin, A. Novikov, Samara University, R. Sondergaard, Air Force Research Lafayette, IN Samara, Russia Laboratory, Wright-Patterson AFB, OH Monday, 9 January 2017 30-HIS-1 History of Aerospace Dallas 7 Chaired by: R. HALLION 63 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2017-0112 AIAA-2017-0113 AIAA-2017-0114 AIAA-2017-0115 Flight Since the ‘Great War’- Reflections and Perspectives Germany and the Invention of the The Sky Was No Limit: The Story Let No New Improvement Pass Nevada Military Aviation and the Chaired by Richard P. Hallion, Florida Poly All-Metal Cantilever Airplane, 1915- of Claire Egtvedt and the Boeing Us By: The History of the Kirsten- Cold War Panelists: 1925: A Historical Review Company Boeing Engineering Company L. Cuevas, University of Nevada, Las Vegas, R. Hallion, Florida Polytechnic University, J. Lee, The Boeing Company, Seattle, WA J. Lee, The Boeing Company, Seattle, WA; Las Vegas, NV Mark J. Lewis John Tylko Lakeland, FL A. Bruckner, University of Washington, Past President, AIAA and Aurora Flight Sciences Seattle, Seattle, WA Director, Science & Technology Policy of the Institute for Defense Analyses Cam Martin James Hansen NASA Armstrong Flight Research Center Department of History, Auburn University

Monday, 9 January 2017 31-HSABP-1 Scramjet Design and Optimization San Antonio 4 Chaired by: T. SMITH, Boeing Engineering Operations & Technology and A. DRAKE, Orbital Sciences Corporation 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2017-0116 AIAA-2017-0117 AIAA-2017-0118 AIAA-2017-0119 AIAA-2017-0120 AIAA-2017-0121 Reducing Edney Type-IV Cowl The Design and Performance Modeling an Active and Passive Transient computational fluid The Effects of Scaling on the Design Pressure Control of Cold Air Testing Shock-On-Lip Heating Via Leading Evaluation of Scramjets Derived Thermal Protection System for a dynamic modeling of baffled tube and Performance of the Brayton- Plant with Delay Resistant Closed- Edge Geometry Optimization from Quasi-1D Flowfields Hypersonic Vehicle ram accelerator Gluhareff Pressure Jet Engine loop Reference Model Adaptive P. Rodi, Lockheed Martin Corporation, F. Ferguson, I. Osei Dwumah, M. Dhanasar, C. Marley, J. Driscoll, University of N. Daneshvaran, C. Knowlen, University of R. Bramlette, R. Barrett-Gonzalez, C. Control Houston, TX North Carolina A&T State University, Michigan, Ann Arbor, Ann Arbor, MI Washington, Seattle, Seattle, WA Depcik, University of Kansas, Lawrence, A. Alan, Y. Yildiz, Bilkent University, Greensboro, NC Lawrence, KS; I. Gluhareff, Gluhareff Ankara, Turkey; U. Poyraz, ROKETSAN Helicopters, San Francisco, CA Missile Industries, Inc., Ankara, Turkey Monday, 9 January 2017 32-ISC-1 International Student Conference-Undergraduate Category Pecos 1 Chaired by: L. HANSEN, HRP Systems, Inc. 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs 1230 hrs AIAA-2017-2004 AIAA-2017-2005 AIAA-2017-2006 AIAA-2017-2007 AIAA-2017-2008 AIAA-2017-2009 AIAA-2017-2010 Design and Test of a Radio- Simultaneous Orbital and Attitude Development of a New Wind Tunable Bistability of Origami-based Subsonic Aerodynamic Evaluation Performance Measurements of Development of a Diaphragmless, Frequency Electrothermal Thruster Propagation of Satellites in Measurement Tool based on a Mechanical Metamaterials of Heat Shield Roughness Effects on Meso-Scale Cyclodial Rotors in Miniature, Liquid-Piston Shock Tube A. Cervelloni, J. Kepron, Worcester Low-Earth Orbit using CUDA for Hovering Drone M. Lee, University of Washington, Seattle, the SpaceX Dragon Crew Capsule Hover R. McCormack, University of New South Polytechnic Institute, Worcester, MA Aerodynamics Simulation D. Pendleton, W. Zhang, Cleveland State Seattle, WA D. Kirkpatrick, C. McGinley, U.S. Air Force B. Himmelberg, M. Benedict, Texas A&M Wales at the Australian Defence Force K. Omar, University of Alabama, Huntsville, University, Cleveland, OH Academy, Colorado Springs, CO University, College Station, TX Academy, Canberra, Australia Huntsville, AL Monday, 9 January 2017 33-ISC-2 International Student Conference-Masters Category Longhorn Hall D Chaired by: S. CORBETS, Lockheed Martin Corporation 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs 1230 hrs AIAA-2017-2011 AIAA-2017-2012 AIAA-2017-2013 AIAA-2017-2014 AIAA-2017-2015 AIAA-2017-2016 AIAA-2017-2017 Magnetically Levitating Low-Friction Transmission Spectroscopy of Mission Planning for Information Development and Flight Testing of a Evaluating Nonlinear Reduced Design and Experimental Early and Robust Detection of Test Stand for the Measurement Electric Propulsion Sputtered Plumes Gathering Using Solar-Powered Meso-Scale Cyclopter Order Models’ Ability to Predict Investigation of a Continuously Oscillatory Failure Cases (OFC) in of Micro-Thruster Performance from Small Bodies Unmanned Ground Vehicles C. Runco, M. Benedict, Texas A&M Dynamic Snap Through of Curved Rotating Detonation Engine Initiated the Flight Control System: A Data Characteristics T. Leps, C. Hartzell, University of Maryland, N. Kingry, Y. Liu, Iowa State University, University, College Station, TX Structures by Azimuthally Sequential Sparking Driven Technique A. Patel, University of Alabama, Huntsville, College Park, College Park, MD Ames, IA C. VanDamme, M. Allen, University of and Radial Injection of Reactants S. Urbano, Higher Institute of Aeronautics Huntsville, AL Wisconsin, Madison, Madison, WI J. Boening, J. Heath, University of and Space, Toulouse, France Washington, Seattle, Seattle, WA Monday, 9 January 2017

64 34-ISC-3 International Student Conference-Team Category Pecos 3 Chaired by: J. CORBETS 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2017-2018 AIAA-2017-2019 AIAA-2017-2020 AIAA-2017-2021 AIAA-2017-2022 High Altitude Atmospheric Research Attenuation of Vortex Noise In-Situ Sample Collection Tool Project ELSA: Europa Lander for Design, Construction, and Flight of Balloon Generated by UAV Propellers at Low Design and Analysis Science Acquisition a High Power Rocket Vehicle and A. Blum, A. Dymit, M. Grohs, T. Smeddal, Reynolds Numbers A. Case, P. DeTrempe, S. Macenski, D. Combs, G. Frank, S. Grandone, C. Hall, Autonomous Payload Norwich University, Northﬁeld, VT N. Intravartolo, T. Sorrells, N. Ashkharian, University of Illinois, Urbana-Champaign, D. Johnson, T. Luke, University of Colorado, D. Hunter, W. Hill, University of Alabama, R. Kim, University of Southern California, Urbana, IL Boulder, Boulder, CO; et al. Huntsville, Huntsville, AL Los Angeles, CA Monday, 9 January 2017 35-LEC-1 Non-Deterministic Approaches Lecture Texas D 0930 - 1030 hrs A Perspective on Model Uncertainty Ali Mosleh Distinguished Professor, Evelyn Knight Chair in Engineering University of California, Los Angeles Monday, 9 January 2017 36-MAT-1 Multifunctional Materials I Palomino 2 Chaired by: R. FERTIG, University of Wyoming and G. SEIDEL, Virginia Polytechnic Institute and State Universit 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2017-0122 AIAA-2017-0123 AIAA-2017-0124 AIAA-2017-0125 AIAA-2017-0126 Application of Piezoresistive Characterization of Hybrid Investigation of the Effects of Porosity Developing a Numerical Scheme to Coupled Electromechanical Nanocomposite Binders for Real Carbon Fiber Composites using on the Overall Thermomechanical Capture the Piezoresistivity of CNF/ Peridynamic Modeling of Strain Time Embedded Sensing of Strain Photoluminescence Spectroscopy Properties of Graded Metal-Ceramic CNTs Hybrid Nanoﬁbers and Damage Sensing in Granular and Damage in Energetic Materials A. Selimov, R. Hoover, Q. Fouliard, A. Manero, Composites J. Cai, M. Naraghi, Texas A&M University, Energetic Materials E. Sengezer, G. Seidel, Virginia Polytechnic University of Central Florida, Orlando, FL; P. P. Deierling, University of Iowa, Iowa City, Iowa College Station, TX N. Prakash, G. Seidel, Virginia Polytechnic Institute and State University, Blacksburg, VA Dackus, D. Carolan, Imperial College London, City, IA; O. Zhupanska, University of Arizona, Institute and State University, Blacksburg, VA London, United Kingdom; et al. Tucson, Tucson, AZ; C. Pasiliao, Air Force Research Laboratory, Eglin AFB, FL Monday, 9 January 2017 37-MDO-1 Aircraft Design Optimization I Mustang 1 Chaired by: E. ALYANAK, AFRL/RQVC and B. STANFORD, NASA Langley Research Center 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2017-0127 AIAA-2017-0128 AIAA-2017-0129 AIAA-2017-0130 Aircraft Design Optimization for Multidisciplinary Aerodynamic Delaunay-based optimization in CFD A Discrete Adjoint Approach for Jet- Commercial Air Travel Under Multi- Shape Optimization of a Composite leveraging multivariate adaptive Flap Interaction Noise Reduction Domain Uncertainties Blended Wing Body Aircraft polyharmonic splines (MAPS) B. Zhou, T. Albring, N. Gauger, Technical S. Roy, W. Crossley, N. Davendralingam, C. Boozer, M. Van Tooren, University of S. Alimohammadi, P. Beyhaghi, T. Bewley, University of Kaiserslautern, Kaiserslautern, P. Govindaraju, Purdue University, West South Carolina, Columbia, Columbia, SC; University of California, San Diego, San Germany; C. Ilario da Silva, T. Economon, Lafayette, IN A. Elham, Delft University of Technology, Diego, CA J. Alonso, Stanford University, Stanford, CA Delft, The Netherlands

65 Monday, 9 January 2017 38-MDO-2 Multifidelity Optimization Mustang 2 Chaired by: S. CHOI, Virginia Tech and A. KO, Phoenix Integration, Inc. 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2017-0131 AIAA-2017-0132 AIAA-2017-0133 AIAA-2017-0134 AIAA-2017-0135 AIAA-2017-0136 Comparison of Unifed and Multilevel-Multifidelity Acceleration Bayesian Low-Fidelity Correction Automated Selection of Low-Fidelity Simple Alternative to Bayesian A Multi-Objective Multi-Fidelity Sequential-Approximate Approaches of PDE-Constrained Optimization Approach to Multi-Fidelity Models for Rapid Aerodynamic Multi-Fidelity Surrogate Framework framework for global optimization to Multifdelity Optimization J. Monschke, M. Eldred, Sandia National Aerospace Design Shape Optimization Using Physics- C. Park, R. Haftka, N. Kim, University of S. Kontogiannis, A. Savill, T. Kipouros, D. Bryson, M. Rumpfkeil, University of Laboratories, Albuquerque, NM C. Fischer, R. Grandhi, Wright State Based Surrogates Florida, Gainesville, Gainesville, FL Cranfield University, Cranfield, United Dayton, Dayton, OH University, Dayton, OH; P. Beran, Air Force S. Koziel, Reykjavik University, Reykjavik, Kingdom Research Laboratory, Wright-Patterson Iceland; L. Leifsson, Iowa State University, AFB, OH Ames, IA Monday, 9 January 2017 39-MVC-1 Visualization/Geometry Representation Grapevine 3 Chaired by: J. MASTERS, ATA and K. VOGIATZIS, ENGILITY 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2017-0137 AIAA-2017-0138 AIAA-2017-0139 AIAA-2017-0140 DNS Study on Three Vortex The Creation of a Static BRep Model Using Design-Parameter Sensitivities in A Thermodynamic Application Identification Methods Given a Cloud of Points Adjoint-Based Design Environments Program Interface for CFD and Y. Dong, Y. Yang, C. Liu, University of J. Dannenhoffer, Syracuse University, J. Dannenhoffer, Syracuse University, Syracuse, Analysis Texas, Arlington, Arlington, TX Syracuse, NY NY; R. Haimes, Massachusetts Institute of G. Power, C. Robinson, J. Morris, R. Bond, Technology, Cambridge, MA Aerospace Testing Alliance, Arnold AFB, TN Monday, 9 January 2017 40-PC-2 Combustion Modeling and Simulation I San Antonio 6 Chaired by: V. RAMAN, University of Michigan and H. IM, King Abdullah University of Science and Technology 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2017-0141 AIAA-2017-0142 AIAA-2017-0143 AIAA-2017-0144 Turbulent Mixing and Combustion Large-Eddy Simulation of the Numerical framework for Interface Tracking Simulations of of Supercritical Coflowing and HIFiRE Direct Connect Rig Scramjet transcritical real-fluid reacting Liquid Oxygen/Gaseous Hydrogen Transverse Jets Combustor flow simulations using the flamelet Coaxial Combustions at Subcritical S. Chong, V. Raman, University of Z. Vane, G. Lacaze, J. Oefelein, Sandia progress variable approach Pressures Michigan, Ann Arbor, Ann Arbor, MI National Laboratories, Livermore, CA P. Ma, D. Banuti, Stanford University, H. Tani, Y. Umemura, Y. Daimon, Japan Stanford, CA; J. Hickey, University of Aerospace Exploration Agency (JAXA), Waterloo, Waterloo, Canada; M. Ihme, Tsukuba, Japan Stanford University, Stanford, CA Monday, 9 January 2017 41-PC-3 Alternate Aviation Fuels I San Antonio 5 Chaired by: M. GUPTA and M. COLKET, United Technologies Research Center 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2017-0145 AIAA-2017-0146 AIAA-2017-0147 AIAA-2017-0148 AIAA-2017-0149 AIAA-2017-0150 Year 2 of the National Jet Fuels Reference Jet Fuels for Combustion Non-premixed Ignition of Spray Characteristics and Flame Flame Spread Measurements of Investigation of Engine Combustion Program: Towards a Testing Alternative Jet Fuels Structure of Jet A and Alternative Alternative Aviation fuels Performance at Altitude Using Streamlined Alternative Jet Fuels J. Edwards, Air Force Research Laboratory, B. Sforzo, S. Wei, J. Seitzman, Georgia Jet Fuels V. Goyal, R. Lucht, J. Gore, Purdue Selected Alternative Fuels for the Certification Process Wright-Patterson AFB, OH Institute of Technology, Atlanta, GA E. Mayhew, C. Mitsingas, B. McGann, University, West Lafayette, IN National Jet Fuels Combustion J. Heyne, University of Dayton, Dayton, OH; M. University of Illinois, Urbana-Champaign, Program Colket, Self, Avon, CT; M. Gupta, A. Jardines, Urbana, IL; T. Hendershott, S. Stouffer, P. Canteenwalla, W. Chishty, National Federal Aviation Administration, Washington, University of Dayton, Dayton, OH; P. Research Council Canada, Ottawa, Canada D.C.; J. Moder, NASA Glenn Research Center, Wrzesinski, Air Force Research Laboratory, 66 Cleveland, OH; J. Edwards, Air Force Research Wright-Patterson AFB, OH; et al. Laboratory, Wright-Patterson AFB, OH; et al. Monday, 9 January 2017 42-PC-4 Combustion Diagnostics I: Applications San Antonio 2 Chaired by: C. CADOU, University of Maryland and B. EMERSON 0930 hrs 1000 hrs 1030 hrs 1100 hrs Oral Presentation AIAA-2017-0151 AIAA-2017-0152 AIAA-2017-0153 Invited Review: Continuing High-speed chemiluminescence Simultaneous High Speed (5 kHz) Experimental and Numerical Study Advances in High-Speed, measurements of alternative jet Fuel-PLIE, OH-PLIF and Stereo of Chemiluminescence Characteristics Multidimensional Imaging fuels at engine relevant ambient PIV Imaging of Pressurized Swirl- in Premixed Counterflow Flames of J. Gord, Air Force Research Laboratory, conditions Stabilized Flames using Liquid Fuels Methane based Fuel blends Wright-Patterson AFB, OH J. Temme, V. Coburn, C. Kweon, Army I. Chterev, N. Rock, H. Ek, B. Emerson, J. Y. Liu, G. Vourliotakis, Y. Hardalupas, A. Taylor, Research Laboratory, Aberdeen Proving Seitzman, T. Lieuwen, Georgia Institute of Imperial College London, London, United Ground, MD Technology, Atlanta, GA; et al. Kingdom Monday, 9 January 2017 43-PDL-1 Plasma Aerodynamics I Ft. Worth 4 Chaired by: S. LEONOV, University of Notre Dame and L. RAJA, University of Texas at Austin 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2017-0154 AIAA-2017-0155 AIAA-2017-0156 AIAA-2017-0157 AIAA-2017-0158 AIAA-2017-0159 Measurement of Plasma Induced Numerical Study of Acceleration of Measurement of Velocity Induced Nonequilibrium Radiation NO in Experimental Investigation of the Characterization of the Formation Flow Perturbations Affecting a Mach the Hydrogen Ions in the Penning by a Propagating Arc Magneto- Shocked Air Internal Structure and Dynamic Process of Cathodic-Arc-Jet in 4.5 Corner Separation Zone Discharge at Pressures Around 1 hydrodynamic Plasma Actuator S. Surzhikov, Russian Academy of Behavior of the Rail Plasma Atmospheric Pressure Gas B. Hedlund, A. Houpt, S. Gordeyev, S. Torr Y. Choi, M. Gray, J. Sirohi, L. Raja, Sciences, Moscow, Russia; P. Kozlov, Actuator Arc I. Kronhaus, L. van Rossum, Technion--Israel Leonov, University of Notre Dame, Notre S. Surzhikov, Russian Academy of University of Texas, Austin, Austin, TX Moscow State University, Moscow, Russia M. Gray, Y. Choi, J. Sirohi, L. Raja, Institute of Technology, Haifa, Israel Dame, IN Sciences, Moscow, Russia University of Texas, Austin, Austin, TX Monday, 9 January 2017 44-SATS-1 Small Satellite Missions Austin 4 Chaired by: J. STRAUB, North Dakota University 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2017-0160 AIAA-2017-0161 AIAA-2017-0162 AIAA-2017-0163 AIAA-2017-0164 SRMSAT-2: Study of the Lunar Development of a Low-Flying Preliminary analysis of ‘BALLET’ - Nanosat Orbit Raising and Development of an Earth Smallsat Sub-Surface and Deep-Space CubeSat Mission for F-Region Ballistic Lunar Low Energy Transfer Rendezvous Using a Continuous- Flight Test to Demonstrate Viability Environment Using a Micro-Satellite Characterization design for SRMSAT-2 Thrust Controller of Mars Aerocapture Platform J. Black, A. Wolosik, Virginia Polytechnic A. Prakash, K. Barad, SRM University, K. Zhang, N. Gatsonis, J. Blandino, M. M. Werner, B. Woollard, A. Tadanki, R. K. Barad, A. Mody, S. Namdeo, A. Institute and State University, Blacksburg, VA Chennai, India Demetriou, Worcester Polytechnic Institute, Braun, Georgia Institute of Technology, Ratheesh, K. Naik, SRM University, Worcester, MA Atlanta, GA; R. Lock, A. Nelessen, Jet Chennai, India Propulsion Laboratory, California Institute of Technology, Pasadena, CA; et al. Monday, 9 January 2017 45-SATS-2 Small Satellite Subsystems Austin 6 Chaired by: A. SANTANGELO 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2017-0165 AIAA-2017-0166 AIAA-2017-0167 AIAA-2017-0168 AIAA-2017-0169 AIAA-2017-0170 Attitude Determination and Control CubeSat Attitude Determination Development of Stereo Camera System Validation of a Low-Cost Avionics Hall Effect Thruster Characterization Thrust Coefficient Losses in System Design for Srmsat-2: A Using Low-Cost Sensors and for Accurate Observation of Deployable Package for Small Spacecraft via Through Potential, Magnetic, and Additively Manufactured Low Thrust Micro Class Lunar Orbiter Magnetic Field Time Derivative Membranes onboard CubeSat Rocket-Based Field Tests Optical Measurements Nozzles A. Mody, T. Sharma, P. Tekriwal, G. A. Walker, M. Kumar, University of Y. Shimoda, K. Watanabe, N. Sakamoto, T. M. Sorgenfrei, D. Kemp, NASA Ames N. Hyatt, Air Force Institute of Technology, C. Tommila, C. Hartsfield, Air Force Institute Subraminian, A. Ratheesh, K. Barad, SRM Cincinnati, Cincinnati, OH Kuratomi, N. Hidaka, WEL Research Company, Research Center, Moffett Field, CA; A. Wright-Patterson AFB, OH of Technology, Wright-Patterson AFB, OH University, Chennai, India Ltd., Ichihara, Japan; M. Ogawa, Tokyo Harness, University of Colorado, Boulder, Institute of Technology, Meguro, Japan; et al. Boulder, CO; M. Nehrenz, NASA Ames Research Center, Moffett Field, CA 67 Monday, 9 January 2017 46-SCS-1 Deployable Booms and Flexures Palomino 1 Chaired by: M. SILVER, MIT Lincoln Laboratory 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2017-0171 AIAA-2017-0172 AIAA-2017-0173 AIAA-2017-0174 AIAA-2017-0175 AIAA-2017-0176 TRAC Boom Structural Mechanics Characterization of Ultra-Thin A Multifunctional Tape Spring Boom Experimental and Analytical Deployment Dynamics of Self- Design and Testing of a Space T. Murphey, D. Turse, L. Adams, Roccor, Composite Triangular Rollable and with Embedded Gas Lines and Characterization of a Slit-LockTM deployable Truss Structure Deployable Mechanism LLC, Longmont, CO Collapsible Booms Flexible Printed Circuit Boards Composite Boom Consisting of Bi-convex Booms Q. Chen, Z. Yao, Y. Hou, H. Fang, C. Leclerc, L. Wilson, S. Pellegrino, A. Brinkmeyer, J. Reveles, V. Gurusamy, Oxford A. Rakow, Composite Technology A. Tamura, S. Inoue, D. Kawarabayashi, M. Shanghai YS Information Technology California Institute of Technology, Space Systems, Oxford, United Kingdom; A. Development, Inc., Lafayette, CO; J. Banik, Yamazaki, Y. Miyazaki, Nihon University, Company, Ltd., Shanghai, China Pasadena, CA Pirrera, P. Weaver, University of Bristol, Bristol, Air Force Research Laboratory, Kirtland AFB, Funabashi, Japan United Kingdom; M. Lawton, Oxford Space NM; G. Sanford, C. Griffee, LoadPath, LLC, Systems, Oxford, United Kingdom Albuquerque, NM Monday, 9 January 2017 47-SD-1/APA-46 Special Session: Aerothermoelasticity of, and Dynamic Response in, High Speed Vehicles and in High Speed Flow I Appaloosa 2 Chaired by: J. MCNAMARA, The Ohio State University and N. FALKIEWICZ, MIT Lincoln Laboratory 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2017-0177 AIAA-2017-0178 AIAA-2017-0179 AIAA-2017-0180 AIAA-2017-0181 AIAA-2017-0182 Interplay of Surface Deformation Rapid Simulation of a Hypersonic A Construction of Thermal Basis Full and Reduced Order Nonlinear Geometric Thermoelastic Multi-Discipline Modeling of and Shock-Induced Separation in Vehicle Through Singular Value Functions for Coupled Structural - Aerothermoelastic Modeling of Response of Structures with Complete Hypersonic Vehicles Using Shock/Boundary Layer Interactions Decomposition Thermal Reduced Order Models Built- Up Aerospace Panels in High- Uncertain Thermal and Structural CFD Surrogates K. Brouwer, A. Gogulapati, J. McNamara, R. Klock, C. Cesnik, University of Michigan, R. Murthy, X. Wang, A. Matney, M. Speed Flows Properties E. Dreyer, B. Grier, J. McNamara, Ohio Ohio State University, Columbus, OH Ann Arbor, Ann Arbor, MI Mignolet, Arizona State University, A. Gogulapati, K. Brouwer, Ohio State P. Song, X. Wang, A. Matney, R. Murthy, State University, Columbus, OH; R. Klock, Tempe, AZ University, Columbus, OH; X. Wang, R. M. Mignolet, Arizona State University, C. Cesnik, University of Michigan, Ann Murthy, Arizona State University, Tempe, Tempe, AZ Arbor, Ann Arbor, MI AZ; J. McNamara, M. Mignolet, Ohio State University, Columbus, OH Monday, 9 January 2017 48-SD-2 Special Topics in Structural Dynamics and Aeroelasticity I Appaloosa 3 Chaired by: D. KUMAR, MSC Software and K. SINGH, Miami Univeristy 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2017-0183 AIAA-2017-0184 AIAA-2017-0185 AIAA-2017-0186 AIAA-2017-0187 Elastic Deformations Control of Optimizing Stiffness and Damping Integration of Structural Uncertainty Investigation of UAS Ingestion into Investigation of UAS Ingestion Highly Flexible Aircraft in Trimmed of Filled Cellular Lattice Structures and Robust Control High-Bypass Engines, Part 1: Bird into High-Bypass Engines, Part 2: Flight and Gust Encounter using Response Surface Methods H. Briggs, ATA Engineering, Inc., San Diego, CA; vs. Drone Parametric Drone Study L. Yagil, D. Raveh, M. Idan, Technion--Israel M. DiPalma, F. Gandhi, Rensselaer D. Kammer, University of Wisconsin, Madison, Y. Song, B. Horton, J. Bayandor, Virginia K. Schroeder, Y. Song, B. Horton, J. Institute of Technology, Haifa, Israel Polytechnic Institute, Troy, NY Madison, WI; A. White, D. Schwartz, ATA Polytechnic Institute and State University, Bayandor, Virginia Polytechnic Institute and Engineering, Inc., San Diego, CA Blacksburg, VA State University, Blacksburg, VA Monday, 9 January 2017 49-SD-3 Special Session: Aeroelastic Prediction I Appaloosa 4 Chaired by: A. SCOTTI, Pilatus Aircraft Ltd and E. BLADES, ATA Engineering, Inc. 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2017-0188 AIAA-2017-0189 AIAA-2017-0190 AIAA-2017-0191 AIAA-2017-0192 Plans and Suggestions of a Analysis of Resolved Turbulent Scales Numerical Investigations of the Investigating the transonic flutter Aeroelastic Simulations Using ANSYS Verification Case to the AIAA of Motion in Aeroelastic Problems Benchmark Supercritical Wing in boundary of the Benchmark Multiphysics Software Aeroelastic Prediction Workshop M. Righi, Zürich University of Applied Sciences, Transonic Flow Supercritical Wing B. Sasanapuri, K. Zore, E. Bish, ANSYS, C. Spode, E. Molina, R. Silva, Technological Winterthur, Switzerland; A. Da Ronch, F. P. Chwalowski, J. Heeg, R. Biedron, NASA J. Heeg, P. Chwalowski, NASA Langley Inc., Pune, India Institute of Aeronautics (ITA), São José Mazzacchi, University of Southampton, Langley Research Center, Hampton, VA Research Center, Hampton, VA dos Campos, Brazil; C. Silva, Stanford Southampton, United Kingdom University, Stanford, CA Monday, 9 January 2017 50-SOF-1 Verification vs Certification for Software Intense Systems Ft. Worth 7 68 0930 - 1230 hrs Panelists: Natasha Neogi Kristin Rozier Virginie Wiels André Platzer National Institute of Aerospace Iowa State University ONERA/DTIM Carnegie Mellon University

Monday, 9 January 2017 51-SRE-1 ISRU Technologies Ft. Worth 5 Chaired by: L. GERTSCH, Missouri University of Science and Technology 0930 hrs 1000 hrs 1030 hrs 1100 hrs Oral Presentation AIAA-2017-0193 AIAA-2017-0194 AIAA-2017-0195 The Advanced Explorations Systems Measurement of Cohesion in Meteoroid Impact Detection for Robotic Ultrasonic Pulse Velocity ISRU Technology Development Asteroid Regolith Materials Exploration of Asteroids (MIDEA): A Sensing for Planetary Material Project J. Kleinhenz, J. Gaier, D. Waters, NASA Small Satellite Concept for Asteroid Characterization and Exploration D. Linne, NASA Glenn Research Center, Glenn Research Center, Cleveland, OH; Characterization Objectives Cleveland, OH; G. Sanders, NASA Johnson R. Harvey, Z. Zeszut, B. Carreno, Case N. Lee, S. Close, Stanford University, T. Evans, West Virginia Robotic Technology Space Center, Houston, TX; S. Starr, NASA Western Reserve University, Cleveland, Stanford, CA Center, Fairmont, WV; D. Goodman, West Kennedy Space Center, Cape Canaveral, OH; et al. Virginia University, Morgantown, WV; M. FL; N. Suzuki, NASA Headquarters, Campbell, C. Panther, West Virginia Robotic Washington, D.C.; T. O’Malley, NASA Glenn Technology Center, Fairmont, WV; A. Research Center, Cleveland, OH Noble, B. Mishra, West Virginia University, Morgantown, WV Monday, 9 January 2017 52-STR-1 Composite Damage and Failure Prediction Methods I Mustang 3 Chaired by: I. RAJU, NASA-Langley Research Center and C. BISAGNI, TU Delft 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2017-0196 AIAA-2017-0197 AIAA-2017-0198 AIAA-2017-0199 AIAA-2017-0200 AIAA-2017-0201 Data Requirements for Progressive Peridynamic Modeling of Thermo- Fracture-Based Mesh Size Exploration of Surrogate Models Intra-inter Crack Band Model A Physics-Based Combined Creep Damage Analysis of Composite Oxidative Damage Evolution in a Requirements for Matrix Cracks in for Inverse Identification of (I2CBM) for Progressive Damage and Fatigue Methodology for Fiber- Structures Composite Lamina Continuum Damage Mechanics Models Delamination Cracks in Composites and Failure Analysis of Joints Reinforced Polymer Composites C. Rouseau, S. Engelstad, Lockheed Martin E. Madenci, University of Arizona, Tucson, F. Leone, C. Davila, NASA Langley Research using Electrical Resistance A. Joseph, P. Davidson, A. Waas, University F. Bhuiyan, R. Fertig, University of Corporation, Fort Worth, TX; S. Clay, Tucson, AZ; S. Oterkus, University of Center, Hampton, VA; G. Mabson, M. Tomography of Washington, Seattle, Seattle, WA Wyoming, Laramie, Laramie, WY Air Force Research Laboratory, Wright- Strathclyde, Glasgow, United Kingdom Ramnath, The Boeing Company, Seattle, P. Diaz Montiel, L. Escalona, S. Patterson AFB, OH WA; I. Hyder, The Boeing Company, North Venkataraman, San Diego State University, Charleston, SC San Diego, CA Monday, 9 January 2017 53-STR-2 Aircraft Structural Design, Test and Analysis Appaloosa 1 Chaired by: P. MURTHY, NASA Glenn Research Center and B. BEDNARCYK, NASA Glenn Research Center 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2017-0202 AIAA-2017-0203 AIAA-2017-0204 AIAA-2017-0205 AIAA-2017-0206 AIAA-2017-0207 Aeroelastic Optimization of Structural Design Exploration of an Study for Effectiveness of Idealized Structural Loads Analysis of a Honeycomb Core Buckling Due to Determination of Load paths in Generalized Tube and Wing Aircraft Electric Powered Multi-propulsor Theory for Fuselage Section Hybrid Wing Body Transport Transverse Compression Plates and Shells Using Load Path Concepts using HCDstruct Version 2.0 Wing Configuration Through Finite Element Analysis B. Flansburg, Lockheed Martin Corporation, H. Soliman, R. Kapania, Virginia Function J. Quinlan, F. Gern, NASA Langley Research J. Moore, S. Cutright, J. Viken, NASA C. Sachdeva, PEC University of Technology, Marietta, GA Polytechnic Institute and State University, K. Gharibi, J. Hurley, A. Tamijani, Embry- Center, Hampton, VA Langley Research Center, Hampton, VA Chandigarh, India; J. Miglani, Virginia Blacksburg, VA Riddle Aeronautical University, Daytona Polytechnic Institute and State University, Beach, FL Blacksburg, VA; S. Padhee, Indian Institute of Technology, Ropar, Ropar, India 69 Monday, 9 January 2017 54-TFPC-1 Unique and Transformational Flight Dallas 6 Chaired by: B. SEELEY, Sustainable Aviation Foundation, Inc. and M. PATTERSON, NASA Langley Research Center 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2017-0208 AIAA-2017-0209 AIAA-2017-0210 AIAA-2017-0211 Regional Sky Transit III: The Comparison of Aero-Propulsive A Modular Unmanned Aerial System Analytical Forms of the Range Primacy of Noise Performance Predictions For Missions Requiring Distributed Performance of Hybrid and Electric B. Seeley, Sustainable Aviation Foundation, for Distributed Propulsion Aerial Presence or Payload Delivery Turboprop Aircraft, for Design Inc., Santa Rosa, CA Configurations M. Patterson, J. Quinlan, W. Fredericks, Optimization Studies. N. Borer, J. Derlaga, K. Deere, M. Carter, NASA Langley Research Center, Hampton, M. Marwa, B. Martos, S. Martin, R. S. Viken, M. Patterson, NASA Langley VA; E. Tse, Georgia Institute of Technology, Anderson, Embry-Riddle Aeronautical Research Center, Hampton, VA; et al. Atlanta, GA; I. Bakhle, Purdue University, University, Daytona Beach, FL West Lafayette, IN Monday, 9 January 2017 55-TP-1 Aerothermodynamics I Austin 2 Chaired by: R. BOND, Arnold Engineering Development Complex 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2017-0212 AIAA-2017-0213 AIAA-2017-0214 AIAA-2017-0215 Study of the Afterbody Radiation Novel Approach for CO2 State-To- Numerical Investigation and Modeling Laser Attenuation in during Mars Entry in an Expansion State Modeling and Application to Modeling of Thermoacoustic Shock Reacting Flows Using Adaptive Tube Multidimensional Entry Flows Waves Finite Elements S. Gu, R. Morgan, T. McIntyre, University A. Sahai, B. Lopez, University of Illinois, P. Gupta, C. Scalo, Purdue University, West P. Bauman, T. Adowski, State University of of Queensland, Brisbane, Australia Urbana-Champaign, Urbana, IL; C. Lafayette, IN; G. Lodato, National Institute New York, Buffalo, NY Johnston, NASA Langley Research Center, of Applied Sciences (INSA), Saint-Étienne- Hampton, VA; M. Panesi, University of du-Rouvray, France Illinois, Urbana-Champaign, Urbana, IL Monday, 9 January 2017 56-TP-2 Heat Transfer I Austin 3 Chaired by: M. KIO, National Space Research & Development Agency and G. SCHNEIDER, University of Waterloo 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2017-0216 AIAA-2017-0217 AIAA-2017-0218 AIAA-2017-0219 AIAA-2017-0220 Characterization of a Method for Investigation of the Effects of Shear Numerical Investigation on the EHD-Enhanced Heat Transfer in a Numerical Studies on Direct Contact Inverse Heat Conduction Using Real on Arc-Electrode Erosion Using a Infrared Signature of Shock Vector Vertical Tube Condensation (DCC) of Subsonic and Simulated Thermocouple Data Modified Arc-Electrode Mass Loss Controlling Nozzle Y. Birhane, Addis Ababa University, Addis Vapor/Gas Jets in Subcooled M. Pizzo, Old Dominion University, Norfolk, Model W. Cheng, L. Zhou, J. Shi, Z. Wang, Ababa, Ethiopia; S. Lin, National Taiwan Flowing Liquid VA; D. Glass, NASA Langley Research B. Webb, Aerospace Testing Alliance, Arnold Northwestern Polytechnical University, University of Science and Technology, J. K N, A. Roy, P. Ghosh, Indian Institute of Center, Hampton, VA AFB, TN; J. Sheeley, National Aerospace Xi’an, China Taipei, Taiwan; F. Lai, University of Technology Kharagpur, Kharagpur, India Solutions, LLC, Arnold AFB, TN Oklahoma, Norman, Norman, OK Monday, 9 January 2017 57-TP-13/MDO-13 Hyperloop and Future High-Speed Transportation Concepts Dallas 5 Chaired by: C. PEKARDAN and J. CHIN, NASA Glenn Research Center 0930 hrs 1000 hrs 1030 hrs 1100 hrs Oral Presentation Oral Presentation Oral Presentation AIAA-2017-0221 Hyperloop: Transforming The Way Past and Future Ground Level Hyperloop Commercial Feasibility Conceptual Sizing and Feasibility We Move Aeronautics: Hyperloop Technology Analysis: A High Level Economic Study for a Magnetic Plane Concept J. Giegel, C. Karla, K. Hosseini, Hyperloop Convergence Overview K. Decker, Georgia Institute of Technology, One, Los Angeles, CA J. Chin, NASA Glenn Research Center, C. Taylor, Department of Transportation, Atlanta, GA; J. Chin, NASA Glenn Research Cleveland, OH Cambridge, MA Center, Cleveland, OH; A. Peng, Yale University, New Haven, CT; C. Summers, University of Washington, Seattle, Seattle, WA; G. Nguyen, Georgia Institute of Technology, Atlanta, GA; A. Oberlander, 70 Brown University, Providence, RI; et al. Monday, 9 January 2017 58-UMS-1 UAS Integration into Urban Environments Grapevine 2 Chaired by: M. LOGAN, NASA Langley Research Center 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2017-0222 AIAA-2017-0223 AIAA-2017-0224 AIAA-2017-0225 AIAA-2017-0226 Fail-Safe Navigation for Concept of Operations (ConOps) for A Modular Design Approach to A Requirements, Platform Impact of Varied Power Setting on Autonomous Urban Multicopter Traffic Management of Unmanned Reconfigurable Unmanned Aerial Specifications, and System Thrust of Multi-Rotor VTOL sUAS in Flight Aircraft Systems (TM-UAS) in Urban Vehicle Architectures for Future Unmanned Ground Effect C. Ochoa, E. Atkins, University of Michigan, Environment V. Maldonado , P. Sarker, University of Traffic Management Systems G. Eberhart, J. Wilhelm, Ohio University, Ann Arbor, Ann Arbor, MI M. Mohamed Salleh, K. Low, Nanyang Texas, San Antonio, San Antonio, TX; S. A. Vetrella, R. Fontanella, G. Fasano, D. Athens, OH Technological University, Singapore, Chowdhury, State University of New York, Accardo, S. Rosario, L. Angrisani, University Singapore Buffalo, NY of Naples “Federico II”, Naples, Italy Monday, 9 January 2017 59-LUNCH-1 Durand Lecture for Public Service and Luncheon Texas A & B 1230 - 1400 hrs NSF’s 10 Big Ideas: Understanding Science, Discovering Breakthroughs, and Influencing Public Policy

France A. Córdova Director National Science Foundation

First Come, First Serve Seating for 200 Monday, 9 January 2017 60-AA-2 Aeroacoustics Jet Noise II Grapevine B Chaired by: P. MORRIS, Pennsylvania State University and W. SCHUSTER, Honeywell International, Inc. 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2017-0227 AIAA-2017-0228 AIAA-2017-0229 AIAA-2017-0230 AIAA-2017-0231 AIAA-2017-0232 Near-field and Far-field Event Near-Field Acoustic Radiations in a The Near-Field Acoustics of The Very Near Pressure Field of Nearfield Characterization of Low Sound Propagation of a Mach 0.75 Associations in Supersonic Jet Flow Two-Stream Supersonic Jet Flow Supersonic Single and Dual Single- and Multi-Stream Jets Supersonic Single Expansion Ramp Jet in Crossflow G. Starke, J. Lewalle, M. Glauser, Syracuse P. Kan, Syracuse University, Syracuse, NY; C. Impinging Jets with Correlations to D. Papamoschou, V. Phong, University of Nozzles with Extended Ramps P. Souza, O. de Almeida, Federal University University, Syracuse, NY Ruscher, Spectral Energies, LLC, Dayton, OH; Far-Field Noise California, Irvine, Irvine, CA B. Malla, E. Gutmark, University of of Uberlândia, Uberlândia, Brazil; C. Ilario J. Lewalle, M. Glauser, Syracuse University, S. Hromisin, L. Myers, P. Morris, D. Cincinnati, Cincinnati, OH da Silva, Embraer, São José dos Campos, Syracuse, NY; S. Gogineni, Spectral Energies, McLaughlin, Pennsylvania State University, Brazil LLC, Dayton, OH; B. Kiel, Air Force Research University Park, PA Laboratory, Wright-Patterson AFB, OH Monday, 9 January 2017 61-ACD-3 Aircraft Design Tools and Methods II San Antonio 1 Chaired by: D. LEVY, Textron Aviation and D. BENCHERGUI, Bombardier Inc 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2017-0233 AIAA-2017-0234 AIAA-2017-0235 AIAA-2017-0236 AIAA-2017-0237 AIAA-2017-0238 Selection of Future Technologies SUAVE: An Open-Source Environment Optimizing Engine Placement on Modeling the Propeller Slipstream Local class shape transformation Utilization of Geometry Definition during Aircraft Conceptual Design Enabling Unconventional Vehicle an Aircraft Wing using Bio-mimetic Effect on Lift and Pitching Moment parameterization (l-CST) for airfoils Tools in Aircraft Design: Need for C. Jouannet, K. Amadori, E. Bäckström, Designs through Higher Fidelity optimization and FlightStreamTM T. Bouquet, R. Vos, Delft University of G. Mura, N. Qin, University of Sheffield, Paradigm Shift Saab, Linköping, Sweden T. MacDonald, E. Botero, J. Vegh, A. Variyar, V. Ahuja, R. Hartfield, J. Burkhalter, Technology, Delft, The Netherlands Sheffield, United Kingdom L. Iqbal, National University of Sciences J. Alonso, Stanford University, Stanford, CA; Research in Flight, Auburn, AL and Technology, Islamabad, Pakistan T. Orra, Embraer, São José dos Campos, Brazil; et al.

71 Monday, 9 January 2017 62-ACD-4 Unmanned Aircraft Design II San Antonio 3 Chaired by: M. LOGAN, NASA Langley Research Center and D. CARTER, Air Force Research Laboratory 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2017-0239 AIAA-2017-0240 AIAA-2017-0241 AIAA-2017-0242 AIAA-2017-0243 AIAA-2017-0244 Defining a conceptual design for Conceptual design and analysis of The Trim Condition of a Hovering The Analysis and Design of a Design and Flight Testing of Optimizing Endurance and Stability a tilt-rotor micro air vehicle for a separation flight for an unmaned Insect-like Flapping-wing Micro Air Highly-Gyroscopic VTOL MAV a Convertible Quadcopter for of a Modular UAV Design well-defined mission air vehicle to five micro air vehicles Vehicle in Asymmetric Condition L. Whitcher, E. Johnson, Georgia Institute Maximum Flight Speed C. Larsen, Chalmers University of Technology, R. Salazar, M. Hassanalian, A. Abdelkefi, M. Hassanalian, A. Abdelkefi, New Mexico D. Ha, J. Kim, S. Choi, J. Han, Korea of Technology, Atlanta, GA R. Bramlette, R. Barrett-Gonzalez, University of Göteborg, Sweden; S. Paul, University at New Mexico State University, Las Cruces, State University, Las Cruces, NM Advanced Institute of Science and Kansas, Lawrence, Lawrence, KS Buffalo, Buffalo, NY; A. Svensson, Chalmers NM Technology, Daejeon, South Korea University of Technology, Göteborg, Sweden; S. Chowdhury, University at Buffalo, Buffalo, NY Monday, 9 January 2017 63-AFM-2 Launch Vehicle, Atmospheric Entry, Hypersonic Flight and Aeroassist Technology I Grapevine 5 Chaired by: K. DORSETT, Lockheed Martin Aeronautics and S. DUTTA, NASA Langley Research Center 1400 hrs 1430 hrs 1500 hrs 1530 hrs AIAA-2017-0245 AIAA-2017-0246 AIAA-2017-0247 AIAA-2017-0248 Comparison of the Effects of Velocity A Gauss Pseudospectral Collocation Optimal Hypersonic Trajectory Hypersonic Trajectory Optimization and Range Triggers on Trajectory for Rapid Trajectory Prediction and Strategies for Supersonic by Sequential Semidefinite Dispersions for the Mars 2020 Mission Guidance Retropropulsion at Mars Programming S. Dutta, D. Way, NASA Langley Research B. Burchett, Rose-Hulman Institute of C. Lorenz, Z. Putnam, University of Illinois, Z. Wang, M. Grant, Purdue University, West Center, Hampton, VA Technology, Terre Haute, IN Urbana-Champaign, Urbana, IL Lafayette, IN Monday, 9 January 2017 64-AMT-3 Velocimetry: Development and Implementation Challenges Grapevine 6 Chaired by: C. SLABAUGH, Purdue University and M. REEDER, Air Force Institute of Technology 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2017-0250 AIAA-2017-0251 AIAA-2017-0252 AIAA-2017-0253 AIAA-2017-0254 AIAA-2017-0255 Dynamic Leading Edge Stagnation Instrument for In-Flight Boundary Measurements of Ship Air Wake Validation of PSV for Turbulence PIV/BOS Synthetic Image Generation Particle Size Measurements in an Point Determination Utilizing an Layer Rake Measurements Using Airborne Anemometers Measurements and Modeling in Variable Density Environments for Arcjet Erosion Test Facility Array of Hot-Film Sensors with R. Westphal, R. Schelley, California C. Mallon, B. Muthig, K. Gamagedara, K. J. Harris , Z. Berger , C. Truong, S. Hinkle, Error Analysis and Experiment Design D. Plemmons, N. Galyen, Arnold Engineering Unknown Calibration Polytechnic State University, San Luis Patil, C. Friedman, T. Lee, George Washington Pennsylvania State University, University L. Rajendran, B. Singh, Purdue University, West Development Complex, Arnold AFB, TN J. Ellsworth, NASA Armstrong Flight Obispo, San Luis Obispo, CA; D. Frame, University, Washington, D.C.; et al. Park, PA Lafayette, IN; M. Giarra, Virginia Polytechnic Research Center, Edwards, CA Self, Richland, WA Institute and State University, Blacksburg, VA; S. Bane, P. Vlachos, Purdue University, West Lafayette, IN Monday, 9 January 2017 65-AMT-4 Laser Tagging and Fluorescence Techniques Grapevine 4 Chaired by: P. DANEHY, NASA Langley Research Center and T. JENKINS, MetroLaser Inc 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs AIAA-2017-0256 AIAA-2017-0257 AIAA-2017-0258 AIAA-2017-0259 AIAA-2017-0260 Characterizing the accuracy of Modeling of the FLEET Filament Mixture Fraction Imaging Using Sodium two-photon laser-induced Examination of NO Tag Formation FLEET velocimetry using comparison Interaction with a Nonuniform Femtosecond TPLIF of Krypton fluorescence characterization with for Unseeded Molecular Tagging with hot wire anemometry Gas Flow Y. Wang, W. Kulatilaka, Texas A&M nanosecond and femtosecond Velocimetry Y. Zhang, R. Miles, Princeton University, M. New-Tolley, M. Shneider, R. Miles, University, College Station, TX excitation W. Bearden, C. Hall, R. Pitz, Vanderbilt Princeton, NJ Princeton University, Princeton, NJ J. Michael, K. Zhu, C. Dedic, Iowa State University, Nashville, TN University, Ames, IA Monday, 9 January 2017 72 66-APA-5 Hypersonic Aerodynamics Dallas 2 Chaired by: M. CONWAY, The Aerospace Corporation and K. VANDEN, USAF 1400 hrs 1430 hrs 1500 hrs 1530 hrs AIAA-2017-0261 AIAA-2017-0262 AIAA-2017-0263 AIAA-2017-0264 A Demonstration of Hypersonic The Investigation of Shock-Wave Aerodynamic Heating Prediction of Comparisons of Measured and Pitching Control in the TUSQ Interaction with Aerodynamic an Inflatable Reentry Vehicle in a Modeled Aero-thermal Distributions for Hypersonic Wind Tunnel Models Hypersonic Wind Tunnel Complex Hypersonic Configurations D. Buttsworth, N. Stern, R. Choudhury, M. Kotov, I. Kryukov, L. Ruleva, S. M. Matsunaga, Y. Takahashi, N. Oshima, D. Sagerman, M. Rumpfkeil, University of University of Southern Queensland, Solodovnikov, Russian Academy of Hokkaido University, Sapporo, Japan; K. Dayton, Dayton, OH; B. Hellman, N. Dasque, Toowoomba, Australia Sciences, Moscow, Russia Yamada, Japan Aerospace Exploration Air Force Research Laboratory, Wright-Patterson Agency (JAXA), Sagamihara, Japan AFB, OH Monday, 9 January 2017 67-APA-6 Airfoil/Wing/Configuration Aerodynamics I Dallas 3 Chaired by: M. GHOREYSHI, United States Air Force Academy and K. MULLENERS, EPFL 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs AIAA-2017-0265 AIAA-2017-0266 AIAA-2017-0267 AIAA-2017-0268 AIAA-2017-0269 Modified Lee’s Transonic Buffet Critical Mach Number Prediction on Effects of Speed on Coupled Sweep Part II: Winglet Design and Composite Analysis and Mechanism Inspired with Fast- Swept Wings and Camber in Morphing Wings Optimization for a Low-speed Characterization of Exhaust Effects framing Focusing-schlieren J. Kirkman, T. Takahashi, Arizona State L. Gamble, A. Moosavian, D. Inman, Subsonic UAV Wing on Aerodynamic Behavior of a Visualization University, Tempe, AZ University of Michigan, Ann Arbor, Ann J. Masud, Z. Toor, Air University, Islamabad, Supersonic Aircraft T. Kouchi, S. Yamaguchi, Y. Yamashita, S. Arbor, MI Pakistan; F. Akram, National University J. Masud, A. Sayani, Z. Toor, Air University, Yanase, Okayama University, Okayama, of Sciences and Technology, Islamabad, Islamabad, Pakistan Japan; S. Koike, Japan Aerospace Pakistan; Z. Abbas, U. Ahsun, King Saud Exploration Agency (JAXA), Chofu, Japan University, Riyadh, Saudi Arabia Monday, 9 January 2017 68-APA-7 Special Session: CFD Applied to Real World Problems Dallas 4 Chaired by: M. JURKOVICH, US Air Force and P. MORGAN, Ohio Aerospace Institute 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2017-0270 AIAA-2017-0271 AIAA-2017-0272 AIAA-2017-0273 AIAA-2017-0274 AIAA-2017-0275 Studies on Aircraft Store with Applications of Computational Fluid AEDC Computational Modeling and Analysis of height stability and The Shock Characteristics of a Two CFD Modeling of US Army UAVs Rotating Tail Dynamics in Support of Aircraft Simulation Support to Integrated dynamic characteristics of a WIG craft Blade Turbofan System using NASA’s OVERFLOW CFD Code R. Kumar, M. Qumar, Defence Research Instrumentation Installations Test and Evaluation (IT&E) L. Chen, X. Liu, Nanjing University of A. Soueidan, R. LeBeau, Saint Louis Z. Hall, Army Aviation and Missile Research and Development Organisation, Bengaluru, K. Bhamidipati, C. Vatcher, U.S. Air Force, R. Knapke, Arnold Engineering Aeronautics and Astronautics, Nanjing, China University, St. Louis, MO Development and Engineering Center, India; V. T, ANSYS, Inc., Bengaluru, India Edwards, CA; J. Lechniak, NASA Armstrong Development Complex, Arnold AFB, TN Redstone Arsenal, AL Flight Research Center, Edwards, CA; D. Reasor, Air Force Research Laboratory, Eglin AFB, FL Monday, 9 January 2017 69-APA-8/AA-3 Special Session: Low Boom Activities II Dallas 6 Chaired by: L. BANGERT, NASA Langley Research Center and L. OZOROSKI, NASA Langley Research Center 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2017-0276 AIAA-2017-0277 AIAA-2017-0278 AIAA-2017-0279 AIAA-2017-0280 AIAA-2017-0281 DLR Simulations of the First AIAA Prediction, Minimization and Numerical Evauation of Effect of Characteristic Scales of Atmospheric Effects of Uncertainties in Comparing anisotropic adaptive Sonic Boom Prediction Workshop Propagation of Sonic Boom from Atmospheric Turbulence on Sonic Boom Turbulence Responsible for Sonic Atmospheric Turbulence and strategies on the 2nd AIAA sonic Cases Supersonic Bodies Observed in D-SEND#2 Flight Test Boom Propagation Weather Predictions on Sonic Boom boom workshop geometry J. Kirz, R. Rudnik, German Aerospace J. Li, J. Krampf, J. Mitchell, R. Agarwal, M. Kanamori, T. Takahashi, Y. Naka, Y. H. Takahashi, Japan Aerospace Exploration K. Fujino, R. Kikuchi, K. Shimoyama, S. A. Loseille, L. Frazza, F. Alauzet, French Center (DLR), Braunschweig, Germany Washington University in St. Louis, St. Makino, H. Takahashi, Japan Aerospace Agency (JAXA), Kakuda, Japan; M. Kanamori, Obayashi, Tohoku University, Sendai, Institute for Research in Computer Science Louis, MO Exploration Agency (JAXA), Chofu, Japan; H. Y. Naka, Y. Makino, Japan Aerospace Japan; Y. Makino, Japan Aerospace and Control (INRIA), Saclay, France Ishikawa, ASIRI Corporation, Chiyoda, Japan Exploration Agency (JAXA), Chofu, Japan Exploration Agency (JAXA), Chofu, Japan Monday, 9 January 2017 73 70-APA-9 Environmentally Friendly/Efficient Aerodynamics and Enabling Technology II Dallas 1 Chaired by: W. FELDER, Stevens Institute of Technology and E. FELTROP, Textron Aviation 1400 hrs 1430 hrs 1500 hrs 1530 hrs AIAA-2017-0282 AIAA-2017-0283 AIAA-2017-0284 AIAA-2017-0285 Designing Superhydrophobic Drag Reduction using Hairy Rotorcraft Fuselage Drag Reduction Drag Reduction Initial Conditions Coatings for Aircraft Drag Chemical Coating on NACA 0012 Using Dielectric Barrier Discharge on Various Legacy Fleet Aircraft: Avoidance Airfoil in Turbulent Airflow Plasma Actuators Surface Roughness Measurements C. Ellis-Terrell, V. Poenitzsch, G. Musgrove, M. Hasegawa, H. Sakaue, University of D. Coleman, SURVICE Engineering, Eglin A. Moyes, H. Kostak, C. Cox, T. Kocian, J. Simpson, R. Wei, K. Coulter, Southwest Notre Dame, Notre Dame, IN AFB, FL; F. Thomas, University of Notre W. Saric, H. Reed, Texas A&M University, Research Institute, San Antonio, TX Dame, Notre Dame, IN College Station, TX; et al. Monday, 9 January 2017 71-APA-10 Special Session: CREATE-AV HPC Multiphysics I Dallas 5 Chaired by: N. HARIHARAN, CREATE-AV and R. MEAKIN 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2017-0286 AIAA-2017-0287 AIAA-2017-0288 AIAA-2017-0289 AIAA-2017-0290 AIAA-2017-0291 CFD Based Model Building of the An Assessment of the Dual Mesh Progress in Strand Mesh Generation Results from HPCMP CREATETM-AV Full Potential Revisited: A Medium Creating High-Fidelity CFD Geometry F-16XL Static and Dynamic Loads Paradigm Using Different Near- and Domain Connectivity for Dual- COFFE and KCFD Solvers for the Fidelty Aerodynamic Analysis Tool Using CREATE-AV DaVinci 4.0 Using Kestrel Body Solvers in Helios Mesh CFD simulations 6th AIAA Drag Prediction Workshop M. Galbraith, S. Allmaras, R. Haimes, W. McGough, B. Smith, ASRC Federal S. Morton, CREATE Kestrel Team, Lorton, A. Wissink, Army Aviation and Missile J. Sitaraman, Parallel Geometric Algorithms Cases Massachusetts Institute of Technology, Inuteq LLC, Beltsville, MD VA; D. McDaniel, University of Alabama, Research Development and Engineering LLC, Sunnyvale, CA; V. Lakshminarayan, B. J. Erwin, R. Glasby, University of Cambridge, MA Birmingham, Birmingham, AL Center, Moffett Field, CA; B. Jayaraman, Roget, Science and Technology Corporation, Tennessee, Knoxville, Knoxville, TN; S. NASA Ames Research Center, Moffett Moffett Field, CA; A. Wissink, Army Karman, Pointwise, Inc., Fort Worth, TX; Field, CA; J. Sitaraman, Parallel Geometric Aviation and Missile Research Development D. Stefanski, University of Tennessee, Algorithms LLC, Moffett Field, CA and Engineering Center, Moffett Field, CA Knoxville, Knoxville, TN Monday, 9 January 2017 72-ASC-2 Adaptive and Morphing Aircraft and Aeroelasticity, Adaptive Skins, Biomimetics Palomino 3 Chaired by: G. REICH and H. SODANO, University of Michigan, Ann Arbor 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs AIAA-2017-0292 AIAA-2017-0293 AIAA-2017-0294 AIAA-2017-0295 AIAA-2017-0296 Design of Self-Twisting Rotor Shape Adaptation of Wing Smart Morphing Wing: Optimization Smart structures for wind energy Effects of birds’ wing color on their Blades for High-Speed Compound Structures by Chiral Structures of Distributed Piezoelectric turbines flight performance for biomimetics Rotorcraft Undergoing Elastic Instability Actuation H. Monner, O. Huxdorf, M. Pohl, J. purposes E. Ward, I. Chopra, A. Datta, University of F. Runkel, G. Molinari, Swiss Federal A. Henry, Purdue University, West Riemenschneider, German Aerospace M. Hassanalian, H. Abdelmoula, S. Ben Maryland, College Park, College Park, MD Institute of Technology, Zürich, Switzerland; Lafayette, IN; G. Molinari, Swiss Federal Center (DLR), Braunschweig, Germany; Ayed, A. Abdelkefi, New Mexico State A. Arrieta, Purdue University, West Institute of Technology, Zürich, Switzerland; T. Homeyer, M. Hölling, University of University, Las Cruces, NM Lafayette, IN; P. Ermanni, Swiss Federal A. Arrieta, Purdue University, West Oldenburg, Oldenburg, Germany Institute of Technology, Zürich, Switzerland Lafayette, IN Monday, 9 January 2017 73-EDU-2/DE-1 Advancing Aerospace Education I Dallas 7 Chaired by: H. BRIGGS, ATA Engineering, Inc. 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs AIAA-2017-0297 AIAA-2017-0298 AIAA-2017-0299 AIAA-2017-0300 AIAA-2017-0301 Applying the IMPULSE Method to Teaching Product Design & Use of a Full-motion Flight Turbopump Design, Build, and Electronic Controller Design and Second and Fourth Year Aerospace Development and Aircraft Design Simulator for Teaching Aircraft Testing at Purdue University Fabrication for Full-Scale Helicopter Engineering Courses Courses Together : Lessons to Share Performance and Dynamics E. Abdou, A. Carvalhar, M. Klein, S. Otto, Flight Simulator at CCSU C. Merrett, Carleton University, Ottawa, L. Iqbal, National University of Sciences J. Dannenhoffer, M. Green, Syracuse R. White, J. Harry, Purdue University, West D. Broderick, F. Wei, J. Ciccio, M. Bufalini, Canada and Technology, Islamabad, Pakistan University, Syracuse, NY Lafayette, IN; et al. Central Connecticut State University, New Britain, CT Monday, 9 January 2017 74 74-F360-2 NASA Langley Centennial—A Storied Legacy, A Soaring Future Texas C 1400 - 1600 hrs Moderator: James R. Hansen, Professor of History and Director, The University Honors College, Auburn University

Panelists: Jeremiah Creedon Delma Freeman Roy Bridges Lesa Roe Steve Jurczyk David Bowles Center Director 1996-2002 Center Director 2002-2003 Center Director 2003-2005 Center Director 2005-2014 Center Director 2014-2015 Center Director 2015-present

Monday, 9 January 2017 75-FD-8 Boundary Layer Stability and Transition II Texas 1 Chaired by: D. RIZZETTA, USAF/RQVA and R. GRAVES, Air Force Research Laboratory 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2017-0302 AIAA-2017-0303 AIAA-2017-0304 AIAA-2017-0305 AIAA-2017-0306 AIAA-2017-0307 Effect of Freestream Turbulence Roughness induced transition in low Effect of Compressibility on Plasma- Stereo Particle Velocimetry Stereo Particle Image Velocimetry On the Mechanics and Control of on Laminar Separation Bubbles pressure turbines Based Transition Control for a Wing Measurements of Transition Measurements of Transition Boundary Layer Transition induced by and Flow Transition on an SD7003 A. Sengupta, N. Vadlamani, P. Tucker, with Leading-Edge Excrescence Downstream of a Backward-Facing Downstream of a Foward-Facing Step Discrete Roughness Elements Airfoil at Low Reynolds Numbers University of Cambridge, Cambridge, D. Rizzetta, M. Visbal, Air Force Research Step in a Swept-Wing Boundary Layer in a Swept-Wing Boundary Layer S. Suryanarayanan, D. Goldstein, University of J. Zilli, D. Sutton, P. Lavoie, University of United Kingdom Laboratory, Wright-Patterson AFB, OH J. Eppink, C. Yao, NASA Langley Research J. Eppink, NASA Langley Research Center, Texas, Austin, Austin, TX; G. Brown, Princeton Toronto, Toronto, Canada Center, Hampton, VA Hampton, VA University, Princeton, NJ; A. Berger, E. White, Texas A&M University, College Station, TX Monday, 9 January 2017 76-FD-9 CFD Methods for Compressible Flows II Texas 4 Chaired by: S. SHERER, AFRL/RQVA and B. AHRABI, University of Wyoming 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2017-0308 AIAA-2017-0309 AIAA-2017-0310 AIAA-2017-0311 AIAA-2017-0312 AIAA-2017-0313 Weighted Upwinding Compact Large Eddy Simulations of Wall- Reconstructed Discontinuous Development of Discontinuous Edge-Based Finite Element Modeling A Gaskinetic Model For Background Scheme for Shock Capturing Mounted Cylinder in Supersonic Galerkin Methods for Diffusion Galerkin method for Hypersonic of Electromagnetic Effects in the Flow Effects On Rarefied Jet Flow H. Aldujaly, Y. Yang, C. Liu, University of Flow Using OVERFLOW Using a First-Order Hyperbolic Heating Prediction Hypersonic Regime C. Cai, Michigan Technological University, Texas, Arlington, Arlington, TX S. Sherer, P. Morgan, M. Visbal, Air Force System Formulation E. Ching, Y. Lv, M. Ihme, Stanford W. Zhang, W. Habashi, McGill University, Houghton, MI Research Laboratory, Wright-Patterson AFB, OH J. Lou, X. Liu, H. Luo, North Carolina State University, Stanford, CA Montréal, Canada; N. Ben Salah, L’École University, Raleigh, NC; H. Nishikawa, National Nationale Supérieure des Ingénieurs de Institute of Aerospace, Hampton, VA Tunis, Tunis, Tunisia; M. Fossati, University of Strathclyde, Glasgow, United Kingdom; D. Isola, G. Baruzzi, ANSYS, Montreal, Canada Monday, 9 January 2017 77-FD-11 RANS/LES for High-Speed Flows Texas 3 Chaired by: C. BARNES, AFRL/RQVA and D. GONZALEZ, Naval Surface Warfare Center 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs AIAA-2017-0314 AIAA-2017-0315 AIAA-2017-0316 AIAA-2017-0317 AIAA-2017-0318 Characterizing and Improving High-Mach-Number Turbulence Large-Eddy Simulation of a Turbulence Modeling of High Speed Transition and turbulence in a wall- Predictive Accuracy in Shock-Turbulent Modeling using Machine Learning and Compressible Mixing Layer and the Compressible Flows bounded channel flow at high Mach Boundary Layer Interactions Using Direct Numerical Simulation Database Significance of Inflow Turbulence S. Shuai, T. Wray, R. Agarwal, Washington number Data-driven Models J. Huang, L. Duan, Missouri University of M. Mankbadi, J. DeBonis, N. Georgiadis, NASA University in St. Louis, St. Louis, MO S. Pradhan, Indian Institute of Science, A. Singh, K. Duraisamy, S. Pan, University Science and Technology, Rolla, MO; J. Wang, Glenn Research Center, Cleveland, OH Bengaluru, India of Michigan, Ann Arbor, Ann Arbor, MI R. Sun, H. Xiao, Virginia Polytechnic Institute and State University, Blacksburg, VA 75 Monday, 9 January 2017 78-FD-12 Special Session: CRM High-Lift Project Texas 6 Chaired by: J. LIN, NASA-Langley Research Center and E. WHALEN, Boeing 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs AIAA-2017-0319 AIAA-2017-0320 AIAA-2017-0321 Oral Presentation AIAA-2017-0322 CRM High Lift Model for Wind Computational Fluid Dynamics System-Level Trade Studies for Traverse Actuation Method for Development of an Active Flow Tunnel Testing: an Active Flow Analyses for the High-Lift Common Transonic Transports with Active High Lift Control Technique for an Airplane Control Perceptive Research Model Using the USM3D Flow Control (AFC) Enhanced High- A. Shmilovich, Y. Yadlin, The Boeing High-Lift Configuration J. Lin, S. Viken, L. Pack Melton, M. Andino, and FUN3D Flow Solvers Lift Systems Company, Huntington Beach, CA A. Shmilovich, Y. Yadlin, E. Dickey, P. M. Koklu, J. Hannon, NASA Langley M. Rivers, C. Hunter, V. Vatsa, NASA P. Hartwich, P. Camacho, K. El-Gohary, A. Hartwich, A. Khodadoust, The Boeing Research Center, Hampton, VA Langley Research Center, Hampton, VA Gonzales, E. Lawson, A. Shmilovich, The Company, Huntington Beach, CA Boeing Company, Huntington Beach, CA Monday, 9 January 2017 79-FD-13 Synthetic Jets Texas 2 Chaired by: D. BRZOZOWSKI, The Boeing Company and S. JEE, Gwangju Institute of Science and Technology 1400 hrs 1430 hrs 1500 hrs 1530 hrs AIAA-2017-0323 AIAA-2017-0324 AIAA-2017-0325 AIAA-2017-0326 Novel Design of a Synthetic Jet Reduction of Skin Friction Drag in Effects of vortex-induced velocity Effects of Synthetic Jet Actuator Actuator for Flow Control a Turbulent Boundary Layer Using on the streamwise evolution of (SJA) on Flow Topology of Blunt- K. Bauer, Saarland University, Saarbrücken, Circular Synthetic Jets synthetic jets in cross-flow Edged UTM VFE2 Wing Model Germany; C. Karch, A. Heilmann, M. E. Spinosa, S. Zhong, University of T. Berk, G. Gomit, B. Ganapathisubramani, S. Mat, M. Abdullah, M. Dahalan, M. Said, Blechschmidt, Airbus, Munich, Germany Manchester, Manchester, United Kingdom University of Southampton, Southampton, S. Mansor, A. Abdul-Latif, University of United Kingdom Technology, Johor Bahru, Malaysia; et al. Monday, 9 January 2017 80-FD-14 Low-Re and Bio-Inspired Flows II: Unsteady Wings Grapevine C Chaired by: M. OL, US Air Force Reseach Laboratory 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs AIAA-2017-0327 AIAA-2017-0328 AIAA-2017-0329 AIAA-2017-0330 AIAA-2017-0331 Proper Orthogonal Decomposition Marsbee - Can a Bee Fly on Mars? Quasi-steady versus Navier- Low Reynolds Number Surge Analytical Aerodynamic Model of Analysis of Flapping Hovering Wings J. Bluman, C. Kang, D. Landrum, F. Stokes Solutions of Flapping Wing Response of a Flat Plate Wing at 90 Spanwise Flexible Flapping Wings in C. Li, Ohio State University, Columbus, OH; Fahimi, B. Mesmer, University of Alabama, Aerodynamics Degrees Incidence Forward Flight J. Wang, H. Dong, University of Virginia, Huntsville, Huntsville, AL J. Salmon, J. Bluman, C. Kang, University S. Corkery, R. Stevens, H. Babinsky, D. Kodali, C. Kang, University of Alabama, Charlottesville, Charlottesville, VA of Alabama, Huntsville, Huntsville, AL University of Cambridge, Cambridge, Huntsville, Huntsville, AL; H. Aono, Tokyo United Kingdom University of Science, Katsushika, Japan Monday, 9 January 2017 81-GEPC-2 Hybrid Propulsion Concept Development for Transport Class Aircraft Texas 5 Chaired by: N. MADAVAN, NASA-Ames Research Center and A. PROVENZA 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs Oral Presentation Oral Presentation Oral Presentation Oral Presentation Oral Presentation Oral Presentation Conceptual Design and Performance High Speed, High Frequency Air- 10 MW Ring Motor for Aircraft SiC MW Converter for Hybrid Ultra-light Highly Efficient MW-Class Modular and Scalable High Evaluation of a Parallel Hybrid Gas core Machine and Drive Power Propulsion Cryogenically-Cooled Inverter Efficiency Power Inverters for Electric Geared Turbofan for N+3 K. Haran, University of Illinois, Urbana- C. Cantemir, Ohio State University, D. Zhang, General Electric Company, S. Liu, The Boeing Company, Seattle, WA Extreme Power Density Applications Single Aisle Aircraft Champaign, Urbana, IL Columbus, OH Niskayuna, NY R. Pilawa-Podgurski, University of Illinois, C. Lents, United Technologies Corporation, Urbana-Champaign, Urbana, IL East Hartford, CT Monday, 9 January 2017 82-GT-2 Experimental and Computational Fluid Dynamics Studies Ft. Worth 6 Chaired by: C. JORGENS, The Boeing Company and A. CHOU, NASA Langley Research Center 76 1400 hrs 1430 hrs 1500 hrs AIAA-2017-0332 AIAA-2017-0333 AIAA-2017-0334 High-speed Wind Tunnel Test of Air Data System Calibration Numerical Analysis of Water-cooling the CAE-AVM in DNW-HST for CFD Methodology over Cylindrical Bodies Deflector for a High-power Rocket Validation Purposes A. Karns, J. Strike, R. Kumar, Florida State Engine Test Stand R. Gebbink, German-Dutch Wind Tunnels, University, Tallahassee, FL; B. Dickinson, Air M. Li, T. Luo, R. Liu, S. Yang, Beijing Marknesse, The Netherlands; G. Wang, M. Force Research Laboratory, Eglin AFB, FL Institute of Aerospace Testing Technology, Zhong, Chinese Aeronautical Establishment, Beijing, China Beijing, China Monday, 9 January 2017 83-GT-11 High Reynolds Number Aerodynamics and Testing (Invited) Austin 1 Chaired by: H. QUIX, European Transonic Windtunnel and R. PARYZ 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs Oral Presentation AIAA-2017-0335 AIAA-2017-0336 Oral Presentation Oral Presentation Oral Presentation Productivity Improvements at the Investigation of a Pressure Sensitive Application of Carbon Nanotubes Velocity measurements in unseeded Development of Shape Memory High Reynolds Testing of a Sweeping European Transonic Windtunnel Paint Technique for ETW (Invited) and Temperature Sensitive Paint cryogenic flows using FLEET (Invited) Alloy Based Active Wind Tunnel Jet Configuration in a Semi-Span (Invited) D. Yorita, Y. Deisuke, V. Ondruss, U. for the Detection of Boundary P. Danehy, R. Burns, NASA Langley Models and Cryogenic Testing at Supercritical Wing (Invited) H. Quix, European Transonic Windtunnel, Beifuss, German Aerospace Center (DLR), Layer Transition under Cryogenic Research Center, Hampton, VA European Transonic Windtunnel G. Jones, W. Milholen, D. Chan, S. Cologne, Germany Cologne, Germany; A. Hensch, J. Quest, Conditions (Invited) (ETW) and NASA Langley Transonic Goodliff, L. Pack Melton, NASA Langley European Transonic Windtunnel, Cologne, C. Klein, U. Henne, Y. Deisuke, V. Ondruss, Cryogenic Tunnel (TCT) (Invited) Research Center, Hampton, VA Germany; et al. U. Beifuss, A. Hensch, German Aerospace T. Calkins, M. Sleppy, B. Griffiths, The Center (DLR), Göttingen, Germany; et al. Boeing Company, Seattle, WA Monday, 9 January 2017 84-GTE-2 New Engine Architectures I Ft. Worth 2 Chaired by: M. RICKLICK, Embry Riddle Aeronautical University 1400 hrs 1430 hrs 1500 hrs AIAA-2017-0337 AIAA-2017-0338 Oral Presentation Continued Analysis of an Inverse A Parametric Study of Hybrid Emission free propulsion system Brayton Cycle Based UAV Propulsion Electric Gas Turbine Propulsion as a with an hydrogen fuel cell hybrid System Function of Aircraft Size Class and for a 4 seater aircraft J. Wilhite, K. Yellugari, E. Gutmark, Technology Level J. Kallo, German Aerospace Center (DLR), University of Cincinnati, Cincinnati, OH J. Gladin, C. Perullo, J. Tai, D. Mavris, Stuttgart, Germany Georgia Institute of Technology, Atlanta, GA Monday, 9 January 2017 85-HSABP-2 Scramjet Combustors San Antonio 4 Chaired by: J. EDWARDS and J. FULTON 1400 hrs 1430 hrs 1500 hrs 1530 hrs AIAA-2017-0339 AIAA-2017-0340 AIAA-2017-0341 AIAA-2017-0342 Hybrid Reynolds-Averaged and Large- Radiance of Select Species in a Three-Dimensional Visualization of Pressure Treatment in the Flamelet Eddy Simulations of Combustion in a Scramjet Cavity Flow and Flame in a Model Scramjet Modeling of Turbulent Supersonic Supersonic Cavity Flameholder S. Okhovat, T. Ombrello, M. Resor, in Mach 4.5 Flows Combustion D. Peterson, Innovative Scientific Solutions, Air Force Research Laboratory, Wright- Q. Liu, D. Baccarella, T. Lee, University of F. Ladeinde, Z. Lou, Stony Brook University, Inc., Dayton, OH; E. Hassan, Air Force Research Patterson AFB, OH Illinois, Urbana-Champaign, Urbana, IL; Stony Brook, NY Laboratory, Wright-Patterson AFB, OH C. Carter, Air Force Research Laboratory, Wright-Patterson AFB, OH; H. Do, Seoul National University, Seoul, South Korea Monday, 9 January 2017 77 86-IS-1 Student Paper Competition Ft. Worth 1 Chaired by: K. MELCHER, NASA Glenn Research Center and T. YUCELEN, Missouri University of Science & Technology 1400 hrs 1430 hrs 1500 hrs AIAA-2017-0343 AIAA-2017-0344 AIAA-2017-0345 Towards Adaptive Training of Human Automation Interaction Flight Deck Mode Confusion Agent-Based Sparring Partners for Issue Detection Using a Generalized Detection using Intent-based Fighter Pilots Fuzzy Hidden Markov Model Probabilistic Model Checking B. Israelsen, N. Ahmed, University of H. Lyu, J. Suraj Nandiganahalli, I. Hwang, J. Suraj Nandiganahalli, S. Lee, I. Hwang, Colorado, Boulder, Boulder, CO; K. Center, Purdue University, West Lafayette, IN Purdue University, West Lafayette, IN R. Green, Orbit Logic, Inc., Greenbelt, MD; W. Bennett, Air Force Research Laboratory, Wright-Patterson AFB, OH Monday, 9 January 2017 87-ISC-4 International Student Conference-Community Outreach Category Longhorn Hall D Chaired by: R. DOWDY 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs Oral Presentation Oral Presentation Oral Presentation Oral Presentation Oral Presentation UAH AIAA Community Outreach AIAA-UT Arlington Student Branch Daedalus Astronautics at ASU: Physics behind Light and Black Aero Outreach Program A. Scharfenberg, K. Dutour, University of Community Outreach: Fort Worth Outreach Program Holes using Darth Vader’s A. Phillips, U.S. Air Force Academy, Alabama, Huntsville, Huntsville, AL Regional Science Fair W. Templeton, Arizona State University, Lightsaber Colorado Springs, CO I. Marks, University of Texas, Arlington, Tempe, AZ S. Raghu, Pennsylvania State University, Arlington, TX University Park, PA Monday, 9 January 2017 88-LEC-2 Spacecraft Structures Lecture and Panel Texas D 1400 - 1530 hrs

Bridging the Gap from Technology to Spaceﬂight Mark Thomson Chief Engineer Northrop Grumman Astro Aerospace Panelists: Hiraku Sakmoto Jeanette Domber Roberta Ewart Associate Professor Payload Systems Engineer Chief Scientist, Space and Missile Systems Center Tokyo Institute of Technology Ball Aerospace Air Force Space Command

Monday, 9 January 2017 89-MAT-2 Multifunctional Materials II Palomino 1 Chaired by: S. ARNOLD, NASA Glenn Research Center and M. NARAGHI, Texas A & M university 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs AIAA-2017-0347 AIAA-2017-0348 AIAA-2017-0349 AIAA-2017-0350 AIAA-2017-0351 Ablative Polymer Nanocomposites – Multiscale Modeling of Effective Size dependent modeling 3D Printed Strain Gauge Geometry Galvanic Series of Recent Aerospace Further Review Piezoresistivity and Damage Response of electrostatically actuated and Orientation for Embedded Materials in Salt Water J. Koo, M. Natali, KAI, LLC, Austin, TX; K. in Nanocomposite Bonded Explosives functionally graded nanobeams Sensing T. Morimoto, Japan Aerospace Exploration Schellhase, B. Lisco, J. Langston, University K. Talamadupula, A. Chaurasia, G. Seidel, M. Shaat, A. Abdelkeﬁ, New Mexico State J. Gooding, T. Fields, University of Missouri, Agency (JAXA), Mitaka, Japan of Texas, Austin, Austin, TX Virginia Polytechnic Institute and State University, Las Cruces, NM Kansas City, Kansas City, MO University, Blacksburg, VA

78 Monday, 9 January 2017 90-MAT-3 Materials Testing and Characterization Palomino 2 Chaired by: R. NAIK, Pratt & Whitney and J. RANSOM, NASA-Langley Research Center 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs AIAA-2017-0352 AIAA-2017-0353 AIAA-2017-0354 AIAA-2017-0355 AIAA-2017-0356 Landing Gear Design Impact on Performance and Wear Tests of High Strain Rate Material Non-Destructive Evaluation of Defects Insitu Ablation and Thermal Sensing Aircraft Tire Life Icephobic Nanocoatings to Prevent Characterization of Al 7075-T651 in Polymer Matrix Composites for of a 3D Carbon/Phenolic Composite A. Zakrajsek, 96 TG/OL-ACL Landing Gear Ice Accretion on Aerofoils by Modified Taylor Impact Test and Aerospace Applications Using X-ray for Computer Modeling and Test Facility, Wright-Patterson AFB, OH; R. Z. Janjua, B. Turnbull, J. Liu, X. Hou, Velocity Interferometry Talbot-Lau Interferometry and Micro CT Simulation Vogel, Air Force Life Cycle Management K. Choi, University of Nottingham, L. Kesemen, TUBITAK, Ankara, Turkey; A. S. Senck, University of Applied Sciences, Wels, B. Lisco, J. Lewis, C. Kassem, K. Moser, Center, Wright-Patterson AFB, OH; S. Nottingham, United Kingdom Kayran, Middle East Technical University, Austria; M. Scheerer, Aerospace & Advanced J. Koo, University of Texas, Austin, Austin, Naboulsi, Air Force Research Laboratory, Ankara, Turkey Composites GmbH, Wiener Neustadt, Austria; TX; M. Berdoyes, Airbus, Le Haillan, Wright-Patterson AFB, OH; M. Bohun, V. Revol, Swiss Center for Electronics and France; et al. 96 TG/OL-ACL Landing Gear Test Facility, Microtechnology (CSEM), Alpnach Dorf, Wright-Patterson AFB, OH Switzerland; K. Dobes, RUAG Group, Vienna, Austria; B. Plank, J. Kastner, University of Applied Sciences, Wels, Austria Monday, 9 January 2017 91-MDO-3 Aerodynamic Shape Optimization Mustang 1 Chaired by: J. GRAY, NASA Glenn Research Center and F. ENGELSEN, The Boeing Company 1400 hrs 1430 hrs 1500 hrs 1530 hrs AIAA-2017-0357 AIAA-2017-0358 AIAA-2017-0359 AIAA-2017-0360 An Efficient Parallel Overset Simulation-based Design Aerodynamic Shape Optimization Objective Function and Constraints Method for Aerodynamic Shape Optimization by Adaptive Field Using Symbolic Sensitivity Analysis for Robust Transonic Aerofoil Optimization Correction of Multi-fidelity Models A. Elham, Delft University of Technology, Optimization G. Kenway, A. Mishra, N. Secco, K. L. Leifsson, Iowa State University, Ames, Delft, The Netherlands D. Poole, C. Allen, T. Rendall, University of Duraisamy, J. Martins, University of IA; S. Koziel, Reykjavik University, Bristol, Bristol, United Kingdom Michigan, Ann Arbor, Ann Arbor, MI Reykjavik, Iceland Monday, 9 January 2017 92-MVC-2 1st AIAA Geometry and Mesh Generation Workshop/High Lift Prediction Workshop Grapevine D Chaired by: J. CHAWNER, Pointwise, Inc. and T. MICHAL, Boeing Engineering Operations & Technology 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs AIAA-2017-0361 AIAA-2017-0362 AIAA-2017-0363 AIAA-2017-0364 Panel Generation of Mixed Element Best Practices on Overset Structured Mesh Generation for the NASA Mesh generation for high-lift Lessons Learned from Generating Baseline Meshes for 3rd AIAA High Lift Prediction Workshop

Unstructured Meshes for the 3rd Mesh Generation for the High-Lift High Lift Common Research Model geometry conﬁguration using The objective of the moderated discussion is to evaluate the utility of the meshing guidelines and the geometry models provided by High Lift Prediction Workshop CRM Geometry (HL-CRM) Capstone the workshop organizers; assess the capability to adhere to these guidelines; identify the best practices and current shortcomings; P. Li, J. Gallegos, T. Michal, The Boeing W. Chan, NASA Ames Research Center, E. Gantt, C. Woeber, N. Wyman, Pointwise, S. Dey, Naval Research Laboratory, and ﬁnally, review and document the required/desired capabilities and lessons learned. It is hoped that the technical interchange Company, St. Louis, MO Moffett Field, CA Inc., Fort Worth, TX Washington, D.C.; R. Aubry, B. Karamete, between the meshing community, simulation practitioners, researchers, and software developers will help to illuminate the path for E. Mestreau, J. Dean, Sotera Defense geometry and mesh generation research and tool development to meet future workshop requirements.

Solutions, Herndon, VA Moderated by: Hugh Thornburg, Engility

Panelists: Ed Alyanak William Jones Jeffrey Slotnick Carl Ollivier-Gooch AFRL NASA The Boeing Company UBC

Monday, 9 January 2017 93-NDA-1 Reliability Analysis Methods and Applications Mustang 2 Chaired by: S. MULANI, The University of Alabama and Y. LING 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs AIAA-2017-0365 AIAA-2017-0366 AIAA-2017-0367 AIAA-2017-0368 AIAA-2017-0369 Improved Neumann Expansion A New Approach of Mixed Uncertainty Adaptively Sampling Multi-Fidelity Reliability Analysis Considering Tail Uncertainty Aggregation in Method Using Partial Bivariate Quantification and its application Probabilistic Functions with Adjoints Dependence over Space and Time Reliability Analysis Subspaces to structural analysis with corrosion A. Wendorff, J. Alonso, Stanford University, Z. Hu, S. Mahadevan, Vanderbilt University, S. Nannapaneni, Z. Hu, S. Mahadevan, H. Bae, Wright State University, Dayton, degradation Stanford, CA; B. Whitehead, S. Bieniawski, Nashville, TN Vanderbilt University, Nashville, TN The Boeing Company, Seattle, WA 79 OH C. Xie, G. Li, F. Wei, F. Wang, China Academy of Engineering Physics, Mianyang, China Monday, 9 January 2017 94-PC-5/PGC-2 Pressure Gain Combustion Detonative Propulsion Physics Ft. Worth 3 Chaired by: J. HOKE, Innovative Scientific Solutions Incorporated and T. OMBRELLO, Air Force Research Laboratory 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2017-0370 AIAA-2017-0371 AIAA-2017-0372 AIAA-2017-0373 AIAA-2017-0374 AIAA-2017-0375 Mid-Infrared Imaging of an Optically Design & Development of a Deflagration-to-Detonation Effects of Lateral Relief of Effect of Equivalence Ratio and Self-Excited, Multi-kHz Dynamics in Accessible Non-Premixed Hydrogen-Air Hypersonic Combustor for Oblique Transition in Nitrous Oxide-Ethylene Detonation in a Thin Channel Turbulence Fluctuations on the a Linear, Semi-Bounded Detonation Rotating Detonation Engine Detonation Wave Stabilization Mixtures and its Application to K. Cho, J. Codoni, B. Rankin, Air Force Propagation of Detonations Channel B. Rankin, Air Force Research Laboratory, J. Sosa, K. Ahmed, University of Central Pulsed Propulsion Systems Research Laboratory, Wright-Patterson D. Masselot, R. Fiévet, V. Raman, University of K. Schwinn, B. Kan, S. Sardeshmukh, Wright-Patterson AFB, OH; J. Codoni, K. Cho, Florida, Orlando, FL P. Bangalore Venkatesh, T. Graziano, AFB, OH; J. Hoke, Innovative Scientific Michigan, Ann Arbor, Ann Arbor, MI R. Gejji, S. Heister, C. Slabaugh, Purdue J. Hoke, Innovative Scientific Solutions, Inc., S. Bane, S. Meyer, Purdue University, Solutions, Inc., Dayton, OH; F. Schauer, University, West Lafayette, IN Dayton, OH; F. Schauer, Air Force Research West Lafayette, IN; M. Grubelich, Sandia Air Force Research Laboratory, Wright- Laboratory, Wright-Patterson AFB, OH National Laboratories, Albuquerque, NM Patterson AFB, OH Monday, 9 January 2017 95-PC-6 Combustion Modeling and Simulation II San Antonio 6 Chaired by: M. ANAND, Rolls-Royce Corp and C. LI, Air Force Office of Scientific Research 1400 hrs 1430 hrs 1500 hrs 1530 hrs AIAA-2017-0376 AIAA-2017-0377 AIAA-2017-0378 AIAA-2017-0379 Droplet Flame Generated Manifolds Grid Convergence Studies of Bluff Exploration of POD-Galerkin Large Eddy Simulations of a Premixed for use in Large Eddy Simulations of Body Stabilized Turbulent Premixed Techniques for Developing Reduced Jet Combustor Using Flamelet- Two-phase Reacting Flows Combustion Order Models of Nonlinear Euler Generated Manifolds: Effects of Heat P. DesJardin, B. Bojko, State University of A. Comer, Air Force Institute of Equations Loss and Subgrid-Scale Models New York, Buffalo, NY Technology, Wright-Patterson AFB, OH; S. C. Huang, W. Anderson, C. Merkle, Purdue F. Hernandez Perez, B. Lee, H. Im, King Sardeshmukh, Purdue University, West University, West Lafayette, IN Abdullah University of Science and Technology, Lafayette, IN; B. Rankin, M. Harvazinski, Thuwal, Saudi Arabia; A. Fancello, A. Donini, J. V. Sankaran, Air Force Research Laboratory, van Oijen, Eindhoven University of Technology, Wright-Patterson AFB, OH Eindhoven, The Netherlands; et al. Monday, 9 January 2017 96-PC-7 Alternate Aviation Fuels II San Antonio 5 Chaired by: M. ROQUEMORE and S. VASU, University of Central Florida 1400 hrs 1430 hrs 1500 hrs 1530 hrs AIAA-2017-0380 AIAA-2017-0381 AIAA-2017-0382 AIAA-2017-0383 Impacts of Fuel Properties on Jet Fuel Thermal Stability Investigation of Combustion Emissions The effect of fuel composition on Combustor Performance, Operability Investigations using Ellipsometry from Conventional and Alternative swirling kerosene flames and Emissions Characteristics L. Nash, University of Central Florida, Aviation Fuels in a Well-Stirred Reactor J. Sidey, P. Allison, E. Mastorakos, E. Corporan, J. Edwards, Air Force Research Orlando, FL; J. Klettlinger, NASA Glenn R. Stachler, J. Heyne, S. Stouffer, University of Cambridge, Cambridge, Laboratory, Wright-Patterson AFB, OH; S. Research Center, Cleveland, OH; S. Vasu, University of Dayton, Dayton, OH; J. United Kingdom Stouffer, M. DeWitt, Z. West, C. Klingshirn, University of Central Florida, Orlando, FL Miller, M. Roquemore, Air Force Research University of Dayton, Dayton, OH; et al. Laboratory, Wright-Patterson AFB, OH 80 Monday, 9 January 2017 97-PC-8 Combustion Diagnostics II: Spectroscopy and Absorption San Antonio 2 Chaired by: J. TISHKOFF, Air Force Office of Scientific Research and C. DENNIS, Naval Air Warfare Center 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs AIAA-2017-0384 AIAA-2017-0385 AIAA-2017-0386 AIAA-2017-0387 AIAA-2017-0388 Sensitivity, Stability, and Precision Characterization of Emissions from Infrared Absorption Measurements Spectrally resolved measurements Spectroscopic Characterization of of Quantitative ns-LIBS-Based Fuel- Metalized Energetic Formulations of Saturated Vapor-Phase Jet A-1 of absorption of broadband UV Reactions Involving Counter-WMD Air Ratio Measurements for High- Using Laser-Induced Breakdown P. Chang, J. Li, C. Teo, L. Li, B. Khoo, light-emitting diodes by combustion Simulants Pressure Methane-Air Flames Spectroscopy National University of Singapore, radicals N. Niemiec, K. Campbell, T. Sikes, E. M. Gragston, Y. Wu, Z. Zhang, University of M. O’Neil, N. Niemiec, A. Demko, E. Singapore, Singapore L. White, M. Gamba, University of Petersen, W. Kulatilaka, Texas A&M Tennessee, Knoxville, Knoxville, TN; P. Hsu, Petersen, W. Kulatilaka, Texas A&M Michigan, Ann Arbor, Ann Arbor, MI University, College Station, TX A. Patnaik, S. Roy, Spectral Energies, LLC, University, College Station, TX Dayton, OH; et al. Monday, 9 January 2017 98-PC-9 Advanced Combustion Concepts I Grapevine 3 Chaired by: R. PITZ, Vanderbilt University and Y. HARDALUPAS, Imperial College London 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs Oral Presentation AIAA-2017-0389 AIAA-2017-0390 AIAA-2017-0391 AIAA-2017-0392 Opportunities and Challenges in Power Loss Pathways and Energy Design Strategy for Product A Model for Plasma-Combustion Inert state of fuel tank during Miniature Combustion Systems Balance of a Small Four-Stroke Internal Migration from a Circumferential Coupling and its Effect on the aircraft ascent C. Cadou, University of Maryland, College Combustion Engine Combustion Cavity Ignition of a Dielectric-Barrier M. Frank, D. Drikakis, University of Park, College Park, MD J. Blantin, J. Ausserer, M. Polanka, Air Force E. Hornedo Rodriquez, A. Cottle, C. Discharge Actuated Hydrogen Jet Strathclyde, Glasgow, United Kingdom Institute of Technology, Wright-Patterson AFB, Schmiedel, B. Bohan, M. Polanka, Air L. Massa, Virginia Polytechnic Institute and OH; P. Litke, Air Force Research Laboratory, Force Institute of Technology, Wright- State University, Blacksburg, VA; J. Freund, Wright-Patterson AFB, OH; J. Baranski, Patterson AFB, OH; L. Goss, Innovative University of Illinois, Urbana-Champaign, Innovative Scientific Solutions, Inc., Dayton, OH Scientific Solutions, Inc., Dayton, OH Urbana, IL Monday, 9 January 2017 99-PDL-2 Plasma Aerodynamics II Ft. Worth 4 Chaired by: S. BANE, Purdue University- Sch of Aero and Astro 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs Oral Presentation AIAA-2017-0394 AIAA-2017-0395 AIAA-2017-0396 AIAA-2017-0397 Quasi-DC Discharge in Supersonic Characterization of a 50kW A Comparison Between Corona Quantitative Mean Flow Measurements Characterization of Transient Airflow Inductively Coupled Plasma Torch and DBD Plasma Actuators for Downstream of a Plasma Actuated Grid Operation of a Quasi-DC Electrical S. Leonov, University of Notre Dame, Notre for Testing of Ablative Thermal Separation Control on an Airfoil P. Audier, N. Benard, National Center for Discharge in Supersonic Flow Dame, IN Protection Materials F. Messanelli, M. Belan, Technical Scientific Research (CNRS), Poitiers, France; A. Houpt, B. Hedlund, S. Leonov, S. Elliot, B. Greene, N. Clemens, P. Varghese, University of Milan, Milan, Italy A. Mizuno, University of Toyohashi, Toyohashi, University of Notre Dame, Notre Dame, IN; University of Texas, Austin, Austin, TX; S. Japan; E. Moreau, National Center for Scientific T. Ombrello, C. Carter, Air Force Research Bouslog, S. Del Papa, NASA Johnson Space Research (CNRS), Poitiers, France Laboratory, Wright-Patterson AFB, OH Center, Houston, TX Monday, 9 January 2017 100-SATS-3 Small Satellite Software and Systems Austin 6 Chaired by: A. SANTANGELO 1400 hrs 1430 hrs 1500 hrs 1530 hrs AIAA-2017-0398 AIAA-2017-0399 AIAA-2017-0400 AIAA-2017-0401 Autonomous Real-Time Optimal The Implementation of ‘App on Probabilistic Methods for 4The LinkStar System, A Globalstar Control and Tracking for Micro- Demand’ Functionality for CubeSats Nanosatellite Systems Engineering: Based Radio And Flight System For Satellite Proximity Operations and Other Small Satellites and Its A Lasercom Case Study Satellites In LEO – Architecture And K. Nastasi, D. Thomas, K. Tetreault, J. Application to Educational Applications E. Clements, K. Cahoy, Massachusetts Test Results Black, Virginia Polytechnic Institute and C. Hansen, J. Straub, University of North Institute of Technology, Cambridge, MA A. Santangelo, sci_Zone, Inc., Rio Rancho, NM State University, Blacksburg, VA Dakota, Grand Forks, Grand Forks, ND Monday, 9 January 2017 81 101-SD-4/APA-47 Special Session: Aerothermoelasticity of, and Dynamic Response in, High Speed Vehicles and in High Speed Flow II Appaloosa 2 Chaired by: J. MCNAMARA, The Ohio State University and N. FALKIEWICZ, MIT Lincoln Laboratory 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs AIAA-2017-0402 AIAA-2017-0403 AIAA-2017-0404 AIAA-2017-0405 AIAA-2017-0406 Fluid-Structure Interactions on a Big Data Algorithms and Study on Shock-Induced Panel High Speed Vehicle Fluid-Structure- Aeroelastic Stability of High-Speed Slender Cone under Quiet Flow Workflow Needed to Assess Highly Flutter in 3-D Inviscid Flow Jet Interaction Analysis and Cylindrical Vehicles Conditions at Mach 6 Maneuverable, Flexible Vehicles N. Boyer, J. McNamara, Ohio State Modeling R. Klock, C. Cesnik, University of Michigan, K. Casper, Sandia National Laboratories, A. Vanderwyst, V. Sharma, C. Martin, University, Columbus, OH; C. Barnes, M. R. Kitson, C. Cesnik, University of Ann Arbor, Ann Arbor, MI Albuquerque, NM Leidos, Eglin AFB, FL Visbal, Air Force Research Laboratory, Michigan, Ann Arbor, Ann Arbor, MI Wright-Patterson AFB, OH Monday, 9 January 2017 102-SD-5 Special Topics in Structural Dynamics and Aeroelasticity II Appaloosa 3 Chaired by: K. SPAK, Exponent and S. RAGHAVAN, University of Central Florida 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs AIAA-2017-0407 AIAA-2017-0408 AIAA-2017-0409 AIAA-2017-0410 AIAA-2017-0411 Stick Model Development of Aircraft Optimized Angular Acceleration Entropy for Nonconservative Entropy for Nonlinear Oscillators 3D-Printed Wind Tunnel Flutter Structures for Dynamic Analysis Profile of Flexible Satellite for Vibrating Systems D. Tufano, Z. Sotoudeh, Rensselaer Model U. Hayirli, Turkish Aerospace Industries, Minimum Residual Vibration D. Tufano, Z. Sotoudeh, Rensselaer Polytechnic Institute, Troy, NY A. Pankonien, G. Reich, N. Lindsley, B. Inc., Ankara, Turkey; A. Kayran, Middle Z. Hou, Y. Geng, S. Huang, Harbin Institute Polytechnic Institute, Troy, NY Smyers, Air Force Research Laboratory, East Technical University, Ankara, Turkey of Technology, Harbin, China Wright-Patterson AFB, OH Monday, 9 January 2017 103-SD-6 Special Session: Aeroelastic Prediction II Appaloosa 4 Chaired by: J. HEEG, NASA-Langley Research Center and K. GRIFFIN, Southwest Research Institute 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2017-0412 AIAA-2017-0413 AIAA-2017-0414 AIAA-2017-0415 AIAA-2017-0416 AIAA-2017-0417 Uncertainty Analysis of Flutter Aeroelastic Analysis of a Distributed Accurate Rational Function Flutter Boundary Prediction for a Aeroelastic Response of the AGARD Aeroelastic Analysis of High Aspect Predictions With Focus on the Electric Propulsion Wing Approximation for Time-Domain Flying-Wing Model Exhibiting Body 445.6 Wing with Freeplay Nonlinearity Ratio Wings Using Joined 3D Finite AGARD 445.6 Wing S. Massey, C. Wieseman, B. Stanford, Gust Analysis Freedom Flutter R. Carrese, N. Joseph, P. Marzocca, RMIT Elements and Variational Asymptotic S. Wu, E. Livne, University of Washington, J. Heeg, NASA Langley Research Center, Z. Wang, P. Chen, ZONA Technology, Inc., C. Huang, Z. Wu, C. Yang, Y. Dai, Beihang University, Bundoora, Australia; O. Levinski, Beam Models Seattle, Seattle, WA Hampton, VA Scottsdale, AZ University, Beijing, China Department of Defence, Melbourne, Australia H. Hoseini, D. Hodges, Georgia Institute of Technology, Atlanta, GA Monday, 9 January 2017 104-SOF-2 Formal Methods for Software Verification Ft. Worth 7 Chaired by: E. ATKINS, University of Michigan and J. PAUNICKA, Boeing 1400 hrs 1430 hrs 1500 hrs 1530 hrs Oral Presentation Oral Presentation AIAA-2017-0418 AIAA-2017-0419 Towards the Validation and Verification TOIF: Extending Static Code Analysis Formal Framework and Models for Towards Intelligent System Health of Complex Aerospace Systems Coverage Validation and Verification of Software- Management using Runtime (Invited) B. Calloni, Lockheed Martin Corporation, Intensive Aerospace Systems Monitoring M. Davies, NASA Ames Research Center, Fort Worth, TX S. Guarro, M. Yau, ASCA, Inc., Redondo Beach, C. Torens, F. Adolf, German Aerospace Moffett Field, CA; T. Kahsai, Carnegie Mellon CA; U. Ozguner, T. Aldemir, A. Kurt, M. Hejase, Center (DLR), Braunschweig, Germany; University, Moffett Field, CA; C. Teubert, Stinger Ohio State University, Columbus, OH; et al. P. Faymonville, S. Schirmer, Saarland Ghaffarian Technologies, Inc., Moffett Field, CA University, Saarbrücken, Germany Monday, 9 January 2017 105-SRE-2 ISRU Mission Concepts Ft. Worth 5 82 Chaired by: D. LINNE, NASA Glenn 1400 hrs 1430 hrs 1500 hrs 1530 hrs AIAA-2017-0421 AIAA-2017-0422 AIAA-2017-0423 AIAA-2017-0424 Solar System Exploration An Integrated Economics Model for An ISRU propellant production Design Study of a Mars Ascent Augmented by In-Situ Resource ISRU in Support of a Mars Colony-- system for a fully fueled Mars Vehicle for Sample Return Using Utilization: Human Planetary Base Initial Results Report Ascent Vehicle In-Situ Generated Propellant Issues for Mercury and Saturn R. Shishko, R. Fradet, Jet Propulsion J. Kleinhenz, NASA Glenn Research Center, G. Landis, S. Oleson, NASA Glenn Research B. Palaszewski, NASA Glenn Research Laboratory, California Institute of Cleveland, OH; A. Paz, NASA Johnson Center, Cleveland, OH; T. Packard, Vantage Center, Cleveland, OH Technology, Pasadena, CA; S. Saydam, Space Center, Houston, TX Partners, Cleveland, OH; D. Linne, J. C. Tapia-Cortez, A. Dempster, J. Coulton, Woytach, M. Martini, NASA Glenn Research University of New South Wales, Sydney, Center, Cleveland, OH; et al. Australia; et al. Monday, 9 January 2017 106-STR-3 Other Topics in Structures I Mustang 3 Chaired by: B. WILLIS, Jacobs Technology and S. CLAY, Air Force Research Laboratory 1400 hrs 1430 hrs 1500 hrs 1530 hrs AIAA-2017-0425 AIAA-2017-0426 AIAA-2017-0427 AIAA-2017-0428 Node-dependent kinematics, refined Evaluation of Strain Measurement Shape Sensing of Aerospace Structures Electromagnetic Modeling of Large zig-zag and multi-line beam theories Devices for Inflatable Structures by Coupling Isogeometric Analysis and Phased Arrays of Structurally for the analysis of composite structures D. Litteken, NASA Johnson Space Center, Inverse Finite Element Method Embedded Waveguides E. Carrera, M. Filippi, A. Pagani, E. Zappino, Houston, TX A. Kefal, E. Oterkus, University of Strathclyde, N. Albertson, R. Canfield, Virginia Polytechnic Technical University of Turin, Turin, Italy Glasgow, United Kingdom Institute and State University, Blacksburg, VA Monday, 9 January 2017 107-STR-4 Composite Structure Design, Test and Analysis Appaloosa 1 Chaired by: M. SCHULTZ, NASA Langley Research Center and V. RANATUNGA, Air Force Research Laboratory 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2017-0429 AIAA-2017-0430 AIAA-2017-0431 AIAA-2017-0432 AIAA-2017-0433 AIAA-2017-0434 Automation of Composite Failure Repeated Impact Response of Continuum Decohesive Finite Hybrid Laminates for Efficient Effects of Size and Location of a On the Contact Force Measurement Analysis for Fiber Breaks Woven Carbon Composites at Room Element Modeling of Fiber- Composite Bolted Joints Circular Cutout on Buckling and Failure for Small Mass Impact of Composite J. Miglani, Virginia Polytechnic Institute and Arctic Temperatures Reinforced Polymer Composites: M. Falugi, Air Force Research Laboratory, of a Cylindrical Shell in Bending Laminate and the Delamination and State University, Blacksburg, VA; C. A. Castellanos, P. Prabhakar, University of Mesh-Objectivity and Sensitivity Wright-Patterson AFB, OH M. Celebi, National Defense University, Event Identification Sachdeva, PEC University of Technology, Texas, El Paso, El Paso, TX Studies Istanbul, Turkey; Z. Gürdal, B. Tatting, Z. Yu, W. Ye, J. Xia, Shanghai Jiao Tong Chandigarh, India; S. Padhee, Indian N. Nguyen, A. Waas, University of University of South Carolina, Columbia, University, Shanghai, China Institute of Technology, Ropar, India Washington, Seattle, Seattle, WA Columbia, SC; A. Blom-Schieber, M. Rassaian, S. Wanthal, The Boeing Company, Seattle, WA Monday, 9 January 2017 108-TP-3 Ablation Austin 2 Chaired by: A. MARTIN, University of Kentucky and E. STERN, NASA Ames Research Center 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs AIAA-2017-0435 AIAA-2017-0436 AIAA-2017-0437 AIAA-2017-0438 AIAA-2017-0439 Temporally and Spatially Resolved Spatially Resolved Measurements of Investigation of Pyrolyzing Ablators High fidelity and multi-scale Development of a Coupled Elastic Emission of Pyrolizing Species from Simulated Pyrolysis Gases Using a Gas Injection Probe thermal response modeling of an Solver for Ablation Problems a Carbon Phenolic Ablator R. Herrmann-Stanzel, L. Allen, J. Meyers, N. Martin, J. Meyers, D. Fletcher, University Avcoat-like TPS. R. Fu, H. Weng, J. Wenk, A. Martin, J. Meyers, C. Tillson, D. Fletcher, University D. Fletcher, University of Vermont, of Vermont, Burlington, Burlington, VT; D. S. Sawant, Z. Li, D. Levin, University of University of Kentucky, Lexington, of Vermont, Burlington, Burlington, VT Burlington, Burlington, VT Dang, I. Boyd, University of Michigan, Ann Illinois, Urbana-Champaign, Urbana, IL Lexington, KY Arbor, Ann Arbor, MI Monday, 9 January 2017 83 109-TP-4 Experimental Heat Transfer Austin 3 Chaired by: D. PYTEL, Lockheed Martin Space Systems and S. AKKERMAN, WVU 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs AIAA-2017-0440 AIAA-2017-0441 AIAA-2017-0442 AIAA-2017-0443 AIAA-2017-0444 Experimental analysis of Carbon Development of Bakelite-Based An Experimental Study on the Visualization and Thermometry in Stagnation Temperature Measurements Monoxide production within a high Temperature Sensitive Paint Dynamics of Water Droplets Hypersonic Wedge and Leading- in a Shock-Tunnel Facility using Laser- temperature ablative boundary layer for High Speed Wind Tunnel Impingement onto a Goose Feather Edge Separated Flows Induced Grating Spectroscopy S. McGuire, C. Laux, National Center for Applications L. Ma, H. Li, H. Hu, Iowa State University, T. Kaseman, L. Le Page, S. O’Byrne, C. Selcan, T. Sander, F. Koroll, C. Mundt, Scientific Research (CNRS), Châtenay-Malabry, S. Claucherty, H. Sakaue, University of Ames, IA S. Gai, University of New South Wales, University of the German Federal Armed France Notre Dame, Notre Dame, IN Canberra, Australia Forces, Neubiberg, Germany Monday, 9 January 2017 110-UMS-2 Special Session: Safe Autonomous Urban Flight I Grapevine 1 Chaired by: K. KRISHNAKUMAR, NASA-Ames Research Center, TI and C. IPPOLITO, NASA Ames Research Center 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs AIAA-2017-0445 AIAA-2017-0446 AIAA-2017-0447 AIAA-2017-0448 AIAA-2017-0449 Safe Autonomous Flight Environment Towards A Computational Developing a Generalized Trajectory 3D LiDAR SLAM Integration with GPS/ Concepts of Airspace Structures and (SAFE50) for the Notional Last “50 ft” Framework for Autonomous Modeling Framework for Small INS for UAVs in Urban GPS-Degraded System Analysis for UAS Traffic flows of Operation of “55 lb” Class of UAS Decision-Making in Unmanned UAS Performance in the Presence Environments for Urban Areas K. Krishnakumar, P. Kopardekar, C. Ippolito, J. Aerial Vehicles of Wind S. Hening, C. Ippolito, K. Krishnakumar, V. D. Jang, Korea Advanced Institute of Science Melton, V. Stepanyan, S. Sankararaman, NASA S. Sankararaman, NASA Ames Research S. D’Souza, NASA Ames Research Center, Stepanyan, NASA Ames Research Center, and Technology, Daejeon, South Korea; C. Ames Research Center, Moffett Field, CA; et al. Center, Moffett Field, CA Moffett Field, CA Moffett Field, CA; M. Teodorescu, University of Ippolito, S. Sankararaman, V. Stepanyan, California, Santa Cruz, Santa Cruz, CA NASA Ames Research Center, Moffett Field, CA Monday, 9 January 2017 111-WE-1 Wind Turbine Aeroelastics and Wakes Austin 4 Chaired by: J. JONKMAN, National Renewable Energy Laboratory 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2017-0450 AIAA-2017-0451 AIAA-2017-0452 AIAA-2017-0453 AIAA-2017-0454 AIAA-2017-0455 Design Tool for Aeroelastic Analysis Experiments on Dynamic Aeroelastic Evaluation and comparison of Benchmarking of a Free Vortex Development of FAST.Farm: A New Uncertainty Quantification of Wind of Wind Turbine Blades Based on Response of Wind Turbine Blades two codes for aeroelastic VAWT Wake Model for Prediction of Wake Multi-Physics Engineering Tool for Turbine Wake Measurements with a Geometrically Exact Beam Theory R. Long, E. White, Texas A&M University, simulation Interactions Wind-Farm Design and Analysis Scanning Lidar and Lifting Surface Method College Station, TX D. Marten, I. Paraschivoiu, École K. Shaler, K. Kecskemety, J. McNamara, J. Jonkman, J. Annoni, G. Hayman, T. Herges, D. Maniaci, B. Naughton, Sandia J. Chen, X. Shen, P. Liu, X. Zhu, Z. Du, Polytechnique de Montréal, Montréal, Ohio State University, Columbus, OH B. Jonkman, A. Purkayastha, National National Laboratories, Albuquerque, NM; Shanghai Jiao Tong University, Shanghai, Canada; J. Saverin, J. Wendler, G. Renewable Energy Laboratory, Golden, CO S. Schreck, M. Churchfield, A. Clifton, China Pechlivanoglou, C. Paschereit, Technical National Renewable Energy Laboratory, University of Berlin, Berlin, Germany Boulder, CO; et al. Monday, 9 January 2017 112-NW-5 Monday Afternoon Networking Coffee Break Session Room Foyers 1530 - 1600 hrs Monday, 9 January 2017 113-PLNRY-2 AIAA Town Hall Meeting Texas C 1700 - 1830 hrs (Governance and Open Access)

James Maser Frank Lu AIAA President AIAA Vice President, Publications

Monday, 9 January 2017 84 114-NW-6 Rising Leaders in Aerospace Reception Mission Plaza 1900 - 2030 hrs All attendees welcome Tuesday Tuesday, 10 January 2017 115-NW-7 Tuesday Early Morning Networking Coffee Break Session Room Foyers 0700 - 0730 hrs Tuesday, 10 January 2017 116-SB-2 Tuesday Morning Speakers’ Briefing Session Rooms 0730 - 0800 hrs Tuesday, 10 January 2017 117-PLNRY-3 Tuesday Morning Plenary: Disruptive Business Models Texas A & B 0800 - 0900 hrs Innovation to Enable NASA’s Journey to Mars Dava Newman Deputy Administrator NASA Tuesday, 10 January 2017 118-NW-8 Tuesday Morning Networking Coffee Break Session Room Foyers 0900 - 0930 hrs Tuesday, 10 January 2017 119-AA-4 Computational Aeroacoustics I Grapevine B Chaired by: S. ARUNAJATESAN, Sandia National Labs and K. AHUJA, Georgia Institute of Technology 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2017-0456 AIAA-2017-0457 AIAA-2017-0458 AIAA-2017-0459 AIAA-2017-0460 Validating a Monotonically- Large Eddy Simulation of the Flight Numerical Investigations of Bio- Evaluating Source Terms of the Towards Impedance Integrated Large Eddy Simulation Effects on Single Stream Heated Inspired Blade Designs to Reduce Generalized Acoustic Analogy using Characterization of Carbon-Carbon Code for Subsonic Jet Acoustics Jets Broadband Noise in Aircraft Engines the Jet Engine Noise REduction Ultrasonically Absorptive Coatings D. Ingraham, J. Bridges, NASA Glenn Z. Wang, I. Naqavi, P. Tucker, University of and Wind Turbines (JENRE) Code via the Inverse Helmholtz Problem Research Center, Cleveland, OH Cambridge, Cambridge, United Kingdom A. Bodling, B. Agrawal, A. Sharma, Iowa State S. Leib, Ohio Aerospace Institute, Cleveland, D. Patel, P. Gupta, C. Scalo, Purdue University, Ames, IA; I. Clark, W. Alexander, W. OH; D. Ingraham, J. Bridges, NASA Glenn University, West Lafayette, IN; T. Devenport, Virginia Polytechnic Institute and Research Center, Cleveland, OH Rothermel, M. Kuhn, German Aerospace State University, Blacksburg, VA Center (DLR), Stuttgart, Germany Tuesday, 10 January 2017 120-ACD-5 Aircraft Design Tools and Methods III San Antonio 1 Chaired by: W. ANEMAAT, DARcorporation and M. ORR, Boeing Commercial Airplanes 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2017-0461 AIAA-2017-0462 AIAA-2017-0463 AIAA-2017-0464 AIAA-2017-0465 AIAA-2017-0466 Effect of Non-Consistent Mesh Requirements Analysis for Design Design and Optimization Evaluating the Rationale for Folding Continuing the Development of a Semi-Analytical Composite Oval Movements and Sensitivities on a Optimization of Aerobatic Aircraft of Unconventional Aircraft Wing Tips Comparing the Exergy Physics-Based Weight (PBWeight) Fuselage Weight Estimation Discrete Adjoint Based Aerodynamic D. Sarojini, K. Collins, D. Mavris, Georgia Configurations with Aeroelastic and Breguet Approaches Prediction Tool for Conceptual M. Roelofs, R. Vos, Delft University of Optimization Institute of Technology, Atlanta, GA Constraints D. Hayes, M. Lone, J. Whidborne, Cranfield Design: Build 1 Technology, Delft, The Netherlands G. Mura, B. Hinchliffe, N. Qin, University A. Variyar, T. Economon, J. Alonso, University, Cranfield, United Kingdom; E. T. Winter, B. Scheneman, J. Marquez, J. Sidhu, of Sheffield, Sheffield, United Kingdom; J. Stanford University, Stanford, CA Coetzee, Airbus, Bristol, United Kingdom M4 Engineering, Inc., Long Beach, CA Brezillon, Airbus, Toulouse, France

85 Tuesday, 10 January 2017 121-AFM-3 Launch Vehicle, Atmospheric Entry, Hypersonic Flight and Aeroassist Technology II Grapevine 5 Chaired by: J. JEWELL, Air Force Research Laboratory and B. JOLLY, USAF 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2017-0467 AIAA-2017-0468 AIAA-2017-0469 AIAA-2017-0470 AIAA-2017-0471 Guidance Scheme for Modulation of Aerobraking in the Cislunar Design of a Novel Hypersonic Planetary Probe Entry Atmosphere Node Control and Numerical Drag Devices to Enable Return from Economy Inflatable Aerodynamic Decelerator Estimation Using Synthetic Air Data Optimization of Aerogravity-Assist Low Earth Orbit N. Campbell, B. Argrow, University of for Mars Entry, Descent, and System Trajectories S. Dutta, A. Bowes, A. Dwyer Cianciolo, Colorado, Boulder, Boulder, CO; J. Ralph, Landing C. Karlgaard, Analytical Mechanics J. Hess, E. Mooij, Delft University of C. Glass, NASA Langley Research Center, United Launch Alliance, Centennial, CO N. Skolnik, H. Kamezawa, L. Li, G. Associates, Inc., Hampton, VA; M. Technology, Delft, The Netherlands Hampton, VA; R. Powell, Analytical Rossman, B. Sforzo, R. Braun, Georgia Schoenenberger, NASA Langley Research Mechanics Associates, Inc., Hampton, VA Institute of Technology, Atlanta, GA Center, Hampton, VA Tuesday, 10 January 2017 122-AMT-5 Velocimetry: Applications II Grapevine 6 Chaired by: K. CASPER, Sandia National Laboratories and J. WAGNER, Sandia National Laboratories 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2017-0472 AIAA-2017-0473 AIAA-2017-0474 AIAA-2017-0475 AIAA-2017-0476 Optical Flow for Flight and Wind Challenges of Optical Flow Analysis in Particle Image Velocimetry Particle- Resonance Dynamics in Compressible A tomographic PIV and TSP Study Tunnel Background Oriented Supersonic Jets Response Study in the AFRL Mach Cavity Flows using Time-Resolved of Leading-Edge Structures on Stall Schlieren Imaging D. Lim, J. Wu, X. Wei, T. New, Nanyang 3 Tunnel Particle Image Velocimetry and Behaviors of NACA0015 N. Smith, AerospaceComputing, Inc., Technological University, Singapore, Singapore; P. Gulotta, M. Reeder, C. Hoskins, Air Force Pressure Sensitive Paint A. Stolt, J. Estevadeordal, Y. Zhang, North Moffett Field, CA; J. Heineck, E. Schairer, Y. Cui, National University of Singapore, Institute of Technology, Wright-Patterson J. Wagner, S. Beresh, K. Casper, E. DeMauro, Dakota State University, Fargo, ND NASA Ames Research Center, Moffett Singapore, Singapore; S. Shi, Shanghai Jiao AFB, OH; B. Hagen, Air Force Research S. Arunajatesan, Sandia National Laboratories, Field, CA Tong University, Shanghai, China Laboratory, Wright-Patterson AFB, OH Albuquerque, NM Tuesday, 10 January 2017 123-AMT-6 Wall-Based Sensors and Applications Grapevine D Chaired by: M. GAMBA, University of Michigan and D. PLEMMONS, Aerospace Testing Alliance (ATA) 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2017-0477 AIAA-2017-0478 AIAA-2017-0479 AIAA-2017-0480 AIAA-2017-0481 Fabrication and Characterization of Characterization of a Hydraulically Aerodynamic Flow Sensing with Heat Flux Measurements on the The Luminescent Oil-Film Flow- a Flush-Mount MEMS Piezoelectric Smooth Wall Shear Stress Sensor for Elastic Microfence Structures Impingement Surface of a Jet Tagging (LOFFT) Skin-Friction Meter Dynamic Pressure Sensor and Low-Speed Wind Tunnel Applications A. Saini, T. Kim, Z. Cui, North Carolina State Operating at an Inclined Angle Applied to FAITH Hill Associated Package for Aircraft D. Mills, Interdisciplinary Consulting University, Raleigh, NC; B. Schuessler, F. J. Crafton, S. Stanfield, S. Palluconi, N. Husen, Purdue University, West Fuselage Arrays Corporation, Gainesville, FL; C. Barnard, M. Palmieri, NASA Langley Research Center, Innovative Scientific Solutions, Inc., Lafayette, IN; T. Liu, Western Michigan T. Reagan, University of Florida, Gainesville, Sheplak, University of Florida, Gainesville, Hampton, VA; Y. Lin, National Institute of Dayton, OH; T. Lui, J. Montefort, Western University, Kalamazoo, MI; J. Sullivan, Gainesville, FL; J. Meloy, J. Underbrink, The Gainesville, FL Aerospace, Hampton, VA; et al. Michigan University, Kalamazoo, MI Purdue University, West Lafayette, IN Boeing Company, Seattle, WA; M. Sheplak, University of Florida, Gainesville, Gainesville, FL Tuesday, 10 January 2017 124-AMT-7/GT-3 Force Measurements Grapevine 4 Chaired by: N. ULBRICH, Jacobs Technology and G. JONES, NASA-Langley Research Center 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2017-0482 AIAA-2017-0483 AIAA-2017-0484 AIAA-2017-0485 AIAA-2017-0486 Six-Axis Thruster Characterization A Universal Threshold for the Pre-Test Assessment of the Upper Developing a Wall Interference Effects Force Test in a Large-Scale Shock Technique for Small Satellites Assessment of Load and Output Bound of the Drag Coefficient Correction Technique for High-Lift and Tunnel R. Elandt, S. Aslan, M. Peck, Cornell Residuals of Strain-Gage Balance Repeatability of a Wind Tunnel Rotor Configurations in the National Y. Wang, Y. Liu, C. Luo, Z. Jiang, Chinese University, Ithaca, NY Data Model Full-Scale Aerodynamics Complex Academy of Sciences, Beijing, China N. Ulbrich, T. Volden, Jacobs, Moffett Field, CA N. Ulbrich, A. L’Esperance, Jacobs, Moffett P. Goulding, C. Nykamp, B. Bartow, National Field, CA Full-Scale Aerodynamics Complex, Moffett Field, CA 86 Tuesday, 10 January 2017 125-APA-11 Flow Control Applications and Demonstrations (Active and Passive) I Dallas 1 Chaired by: L. UKEILEY, University of Florida and B. OSBORNE, The Boeing Company 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2017-0487 AIAA-2017-0488 AIAA-2017-0489 AIAA-2017-0490 AIAA-2017-0491 AIAA-2017-0492 Experimental Study on Delayed Effects of Feedback Channels Transonic Buffet Control by Numerical Investigation on the Active Flow Separation Control The Wavy Leading Edge Performance Feedback Flow Control around a and Coanda Surfaces on the Tangential Jet Blowing Oblique Shock and High-speed Applied at Wing-Pylon Junction for a Very Thick Airfoil NACA0015 Airfoil using PSJA Performance of Sweeping Jet V. Soudakov, A. Petrov, A. Potapchik, K. Vortex Rings Interaction of a Wing Section in Landing A. de Paula, Technological Institute of K. Ogawara, M. Nomoto, Y. Taguchi, H. Actuator. Abramova, TsAGI, Zhukovsky, Russia Y. Dong, X. Dong, Y. Yang, C. Liu, Configuration Aeronautics (ITA), São José dos Campos, Shingin, Yamaguchi University, Ube, Japan B. Slupski, K. Kara, Khalifa University, Abu University of Texas, Arlington, Arlington, TX P. Vrchota, Aerospace Research and Test Brazil; J. Meneghini, University of São Paulo, Dhabi, United Arab Emirates Establishment (VZLÚ), Prague, Czech São Paulo, Brazil; V. Kleine, R. Girardi , Republic Technological Institute of Aeronautics (ITA), São José dos Campos, Brazil Tuesday, 10 January 2017 126-APA-12 Aerodynamic/Propulsive Interactions - Panel Discussion Dallas 3 0930 - 1130 hrs Panelists: Andrew Wick Frank Lu Paul Hagseth John Latz Brant Ginn Lockheed Martin Aeronautics University of Texas at Arlington Lockheed Martin Aeronautics Northrop Grumman Lockheed Martin Aeronautics Tuesday, 10 January 2017 127-APA-13 Unsteady Aerodynamics I Dallas 2 Chaired by: S. MUPPIDI and J. RAULEDER, Technical University of Munich 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2017-0493 AIAA-2017-0494 AIAA-2017-0495 AIAA-2017-0496 AIAA-2017-0497 Time domain analytical unsteady Transonic Buffet Simulation over NASA- Wall-modeled Large-Eddy Unsteady base pressure analysis of Dynamic Mode Decomposition of High aerodynamic modelling for finite CRM by Unsteady-FaSTAR Code Simulation of Transonic Buffet typical missile configuration in the Reynolds Number Supersonic Jet Flows wings T. Ishida, A. Hashimoto, Y. Ohmichi, T. Aoyama, over a Supercritical Airfoil at high presence of jet S. Yamouni, Technological Institute of J. Boutet, G. Dimitriadis, University of Japan Aerospace Exploration Agency (JAXA), Reynolds Number V. M, V. N S, V. S B, National Aerospace Aeronautics (ITA), São José dos Campos, Liège, Liège, Belgium Chofu, Japan; K. Takekawa, Ryoyu Systems Y. Fukushima, S. Kawai, Tohoku University, Laboratories, Bengaluru, India Brazil; C. Junqueira-Junior, J. Azevedo, Company, Ltd., Nagoya, Japan Sendai, Japan Aeronautics and Space Institute (IAE), São José dos Campos, Brazil; W. Wolf, University of Campinas, Campinas, Brazil Tuesday, 10 January 2017 128-APA-14 Bio-Inspired Flows Dallas 4 Chaired by: V. BHAGWANDIN, US Army Research Laboratory and P. ANSELL, University of Illinois at Urbana-Champaign 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2017-0498 AIAA-2017-0499 AIAA-2017-0500 AIAA-2017-0501 Experimental and Numerical Results of Forward flight capabilities and Reduction of Pitching Moment Free Flight Observations and a Flapping Wing Four Bar Mechanism performances of bio-inspired Generation of a Quadrotor UAV in Aerodynamic Analysis for M. Senol, Middle East Technical University, flapping wing nano air vehicles Gust with Slant Rotors Biologically-Inspired Optimization Ankara, Turkey; K. Arikan, Atilim University, M. Hassanalian, G. Throneberry, A. H. Otsuka, K. Nagatani, Tohoku University, C. Griffin, P. Browning, S. Hamburg, J. Ankara, Turkey; D. Kurtulus, Middle East Abdelkefi, New Mexico State University, Sendai, Japan Cox, W. Huebsch, West Virginia University, Technical University, Ankara, Turkey Las Cruces, NM Morgantown, WV; E. Katzner, Peregrine Fund, Boise, ID; et al.

87 Tuesday, 10 January 2017 129-APA-15 Low Speed, Low Reynolds Number Aerodynamics Dallas 5 Chaired by: C. TILMANN, AFRL/RQV and L. WANG, National Institute of Aerospace 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2017-0502 AIAA-2017-0503 AIAA-2017-0504 AIAA-2017-0505 A New Gust Generator for a Low Low Reynolds Number Aerodynamic Dynamic Measurement of Forces PIV Investigation of Self-Adaptive Speed Wind Tunnel: Design and Characteristics of Near Space Solar and Moments with the Motion Test Flap on Low Aspect Ratio Wings Commissioning Unmanned Aerial Vehicle Apparatus A. Durai, I. Singh, S. P, National Aerospace K. Wood, R. Cheung, T. Richardson, J. L. Feng, China Academy of Aerospace J. Sellers, A. Bower, I. Maatz, M. Reeder, Laboratories, Bengaluru, India Cooper, University of Bristol, Bristol, United Aerodynamics, Beijing, China Air Force Institute of Technology, Wright- Kingdom; O. Darbyshire, C. Warsop, BAE Patterson AFB, OH Systems, Bristol, United Kingdom Tuesday, 10 January 2017 130-DE-2 Innovative Aerospace Designs, Processes, and Tools Palomino 3 Chaired by: G. CREARY, NASA-Langley Research Center and N. HINES, Boeing Commercial Airplanes 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2017-0506 AIAA-2017-0507 AIAA-2017-0508 AIAA-2017-0509 AIAA-2017-0510 Automated Wingbox Structure Active Subspaces of Airfoil Shape Structural Optimization Study of Design and Manufacturing of Flapping Analysis of 3D Printed Titanium Generation Through MATLAB Parameterizations the D8 Double-Bubble Composite Wing Mechanisms for Micro Air Rocket Nozzle J. Qian, University of Sydney, Sydney, Z. Grey, P. Constantine, Colorado School of Fuselage Vehicles T. Fritz, W. Huebsch, West Virginia Australia Mines, Golden, CO J. Chambers, B. Yutko, R. Singh, C. Church, M. Balta, Technical University of Catalunya, University, Morgantown, WV; J. Wilhelm, Aurora Flight Sciences, Manassas, VA Terrassa, Spain; K. Ahmed, German University Ohio University, Athens, OH in Cairo, Cairo, Egypt; P. Wang, J. McCarthy, H. Taha, University of California, Irvine, Irvine, CA Tuesday, 10 January 2017 131-EDU-3 Advancing Aerospace Education II Dallas 7 Chaired by: R. LEBEAU, Saint Louis University 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2017-0511 AIAA-2017-0512 AIAA-2017-0513 AIAA-2017-0514 AIAA-2017-0515 AIAA-2017-0516 Building a Mechatronics Design The AUSS FIREfly: A Distributed Employing Unmanned Aircraft Design and Flight Testing of an Monarch Madness: A Cross-curricular Developing a Successful Course Around Quadcopters Sensing and Co-ordination Platform Systems to Actively Engage Experimental Aircraft for Green Approach to Elementary STEM Undergraduate Aerospace Engineering T. Fields, University of Missouri, Kansas for First-Year Engineering Education Students and Build Local Aerospace Leveraged Energy Education Program within an ME Department City, Kansas City, MO D. Yeo, D. Paley, University of Maryland, Infrastructure D. Landrum, K. Schikore, R. Longchamps, K. Benson, Cherokee Elementary School, framework – a 20-year Perspective College Park, College Park, MD M. Hatfield, University of Alaska, University of Alabama, Huntsville, Guntersville, AL; D. Landrum, C. Kang, J. Kosmatka, University of California, La Jolla, Fairbanks, Fairbanks, AK Huntsville, AL University of Alabama, Huntsville, Huntsville, AL La Jolla, CA Tuesday, 10 January 2017 132-F360-3 Future of the Aerospace Industry and Workforce Needs Texas C 0930 - 1130 hrs Moderator: Michael D. Griffin, Chairman and CEO, Schafer Corporation

Panelists: C. Doug Ebersole Kevin Parsons Robie Samanta Roy Kenneth Sanger Lisa Teague Executive Director Director, Innovation and Transformation Vice President, Technology Strategy and Innovation Vice President and General Manager Director, Research and Technology Strategy Air Force Research Laboratory Northrop Grumman Corporation Lockheed Martin Corporation 787 Airplane Development Rolls-Royce Corporation Boeing Commercial Airplanes

Tuesday, 10 January 2017 133-FD-15 High-Order Methods I Texas 1 Chaired by: R. GLASBY, University of Tennessee and J. ERWIN, University of Tennessee

88 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2017-0517 AIAA-2017-0518 AIAA-2017-0519 AIAA-2017-0520 AIAA-2017-0521 Scalable Solution Strategies for New Very High-Order Multilayer A High-Order Flux Reconstruction/ A New High-order Spectral High-Order Flux Reconstruction on Stabilized Finite-Element Flow Compact Schemes with Spectral-Like Correction Procedure via Difference Method for Simulating Stretched and Warped Meshes Solvers on Unstructured Meshes Resolution for Flow Simulations Reconstruction Method for Shock Compressible Flows on Unstructured W. Trojak, R. Watson, P. Tucker, University B. Reza Ahrabi, D. Mavriplis, M. Brazell, Z. Bai, X. Zhong, University of California, Capturing with Space-Time Grids with Mixed Elements of Cambridge, Cambridge, United Kingdom University of Wyoming, Laramie, Laramie, WY Los Angeles, Los Angeles, CA Extension Time Stepping and M. Li, George Washington University, Adaptive Mesh Reﬁnement Washington, D.C.; Z. Qiu, Northwestern X. Zhang, C. Liang, J. Yang, George Polytechnical University, Xi’an, China; Washington University, Washington, D.C. C. Liang, George Washington University, Washington, D.C.; M. Sprague, National Renewable Energy Laboratory, Golden, CO Tuesday, 10 January 2017 134-FD-16 High-Speed Flows I Texas 2 Chaired by: J. SEIDEL, USAF Academy and E. STEPHEN 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2017-0522 AIAA-2017-0523 AIAA-2017-0524 AIAA-2017-0525 AIAA-2017-0526 AIAA-2017-0527 Stereoscopic PIV Measurements of a Mach 3 Boundary Layer Turbulent spots induced by pairs of Wall Pressure Unsteadiness on the Investigation of Secondary Motion Dynamic Mode Decomposition applied Supersonic Axisymmetric Base Flow Measurement over a Flat Plate roughness elements in a blunt-body Aft Deck of a Planar Multi-stream in High Speed Flow to a Detached-Eddy Simulation of J. Favale, R. Hortensius, G. Elliott, J. Using the PIV and IR Thermography hypersonic boundary layer Supersonic Nozzle B. Rice, Air Force Research Laboratory, Separated Nozzle Flow Dutton, University of Illinois, Urbana- Techniques O. Taylor, P. Bruce, Imperial College C. Tinney, University of Texas, Austin, Arnold AFB, TN; N. Bisek, Air Force R. Larusson, M. Olander Burak, N. Andersson, Champaign, Urbana, IL H. Lee, Y. Kim, Y. Byun, S. Park, Konkuk London, London, United Kingdom Austin, TX Research Laboratory, Wright-Patterson Chalmers University of Technology, Göteborg, University, Seoul, South Korea AFB, OH; S. Peltier, J. Hofferth, Air Force Sweden; J. Östlund , GKN Aerospace Engine Research Laboratory, Arnold AFB, TN Systems, Trollhättan, Sweden Tuesday, 10 January 2017 135-FD-17 Honoring Gino Moretti Texas 3 0930 - 1230 hrs

0930-1000 hrs Gino Moretti: A Man for All Seasons, Manny Salas 1100-1120 hrs The Result of the Gino’s Teaching at Sapienza University of Rome, Marcello Onofri 1000-1020 hrs Gino as a Mentor, Frank Marconi 1120-1140 hrs Capturing Some Fond Memories of Gino in a Fitting Manner, Sukumar Chakravarthy 1020-1030 hrs Remarks from Phil Roe, Nicholas DiZinno 1140-1200 hrs A Renaissance Man: Personality & Generosity of a Dear Friend, Maurizio Pandolfi 1030-1050 hrs The Maestro of Gas Dynamics, Bob MacCormack 1200-1230 hrs On Shock Fitting and Shock Capturing Methods for DNS and LES Computations, Helen Yee 1050-1100 hrs Remarks from Pat Sforza, Nicholas DiZinno Tuesday, 10 January 2017 136-FD-18 Modeling and Optimization Methods Texas 4 Chaired by: K. FIDKOWSKI, University of Michigan and P. BLONIGAN, NASA Ames Research Center 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2017-0528 AIAA-2017-0529 AIAA-2017-0530 AIAA-2017-0531 AIAA-2017-0532 An ODE-based Wall Model for Unsteady Output-Based Adaptation Tensor-Product Summation-by-Parts Parameter Estimation for a A non-intrusive algorithm for Turbulent Flow Simulations Using Continuous-in-Time Adjoints Operators Turbulent Buoyant Jet using sensitivity analysis of chaotic flow M. Berger, New York University, New York, K. Fidkowski, University of Michigan, Ann D. Del Rey Fernández, P. Boom, M. Approximate Bayesian Computation simulations NY; M. Aftosmis, NASA Ames Research Arbor, Ann Arbor, MI Shademan, D. Zingg, University of Toronto, J. Christopher, C. Lapointe, N. Wimer, T. P. Blonigan, NASA Ames Research Center, Center, Moffett Field, CA Toronto, Canada Hayden, I. Grooms, G. Rieker, University of Moffett Field, CA; Q. Wang, Massachusetts Colorado, Boulder, Boulder, CO; et al. Institute of Technology, Cambridge, MA; E. Nielsen, NASA Langley Research Center, Hampton, VA; B. Diskin, National Institute of Aerospace, Hampton, VA 89 Tuesday, 10 January 2017 137-FD-19 Numerical Simulations of Shock Boundary Layer Interactions Texas 5 Chaired by: N. BISEK, Air Force Reseach Laboratory and D. GONZALEZ, Naval Surface Warfare Center 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2017-0533 AIAA-2017-0534 AIAA-2017-0535 AIAA-2017-0536 Turbulence Structure and Large- Numerical Simulations of a On the Effect of Test Section Aspect Shock Wave Laminar Boundary Scale Unsteadiness in Shock-Wave / Cylinder-Induced Shock Wave/ Ratio for Shock Wave - Boundary Layer Interaction at a Hypersonic Boundary Layer Interaction Boundary Layer Interaction Layer Interactions Flow Over a Blunt Fin-Plate Junction K. Porter, J. Poggie, Purdue University, S. Lindörfer, C. Combs, P. Kreth, J. M. Pizzella, S. Warning, M. McQuilling, M. Mortazavi, D. Knight, Rutgers West Lafayette, IN Schmisseur, University of Tennessee, Saint Louis University, St. Louis, MO; A. University, Piscataway, NJ Tullahoma, Tullahoma, TN Purkey, R. Scharnhorst, M. Mani, The Boeing Company, St. Louis, MO; et al. Tuesday, 10 January 2017 138-FD-20 RANS/LES Applications Texas 6 Chaired by: A. SESCU, Mississippi State University and J. DUDEK, NASA Glenn Research Center 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2017-0537 AIAA-2017-0538 AIAA-2017-0539 AIAA-2017-0540 AIAA-2017-0541 Aero-Optic Calculations of A Wall-Resolved Large-Eddy Performance Assessment of High- Simulation of an ethylene flame Evaluation of Full Reynolds Stress Spherical Turret at Transonic Flow Simulation of Flow Separation Over Order Large Eddy Simulation and with turbulence, soot and radiation Turbulence Models in Fun3D E. Arad, M. Weidenfeld, Rafael Advanced NASA Wall-Mounted Hump Immersed Boundary Method for modeling. J. Dudek, NASA Glenn Research Center, Defense Systems, Ltd., Haifa, Israel A. Uzun, National Institute of Aerospace, Rotorcraft Hover S. Golder, J. Doom, South Dakota State Cleveland, OH; J. Carlson, NASA Langley Hampton, VA; M. Malik, NASA Langley Y. Delorme, S. Frankel, Technion--Israel Institute University, Brookings, SD Research Center, Hampton, VA Research Center, Hampton, VA of Technology, Haifa, Israel; R. Jain, R. Strawn, NASA Ames Research Center, Moffett Field, CA Tuesday, 10 January 2017 139-FD-22 Low-Re and Bio-Inspired Flows III: Wing Analysis and Design Grapevine C Chaired by: D. GARMANN, Air Force Research Laboratory and J. JAWORSKI, Lehigh University 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2017-0542 AIAA-2017-0543 AIAA-2017-0544 AIAA-2017-0545 AIAA-2017-0546 Review of Fluid Dynamic and Low Reynolds number wake Steady and Unsteady Fluid- Vorticity Production at the Leading Computational Analysis of Thin Acoustic Performance of Biologically modification using a Gurney flap Structure Interactions with Edge of Flat Plates at High Incidence airfoils Under Low-Reynolds Inspired Passive Flow Control M. Gopalakrishnan Meena, K. Taira, Florida Compliant Membrane Wings F. Manar, A. Jones, University of Maryland, Number Flow Using Block- Trailing Edge Devices for Design State University, Tallahassee, FL; K. Asai, G. Alon Tzezana, K. Breuer, Brown College Park, College Park, MD Structured Cartesian Mesh Applications Tohoku University, Sendai, Japan University, Providence, RI D. Iioka, F. Kazuki, M. Okamoto, D. T. Wolfe, Naval Surface Warfare Center, Sasaki, Kanazawa Institute of Technology, Philadelphia, PA Hakusan, Japan; K. Shimoyama, S. Obayashi, Tohoku University, Sendai, Japan Tuesday, 10 January 2017 140-GT-4 Advances in Test Techniques and Test Management Ft. Worth 6 Chaired by: D. LEWIS, Aerospace Testing Alliance (ATA) and P. KELLY, Aerospace Testing Alliance (ATA) 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2017-0547 AIAA-2017-0548 AIAA-2017-0549 AIAA-2017-0550 Determining Products of Inertia for Development Trends and Flexible FPGA based Hardware In High-Speed Schlieren and 10-Hz Kr Small Scale UAVs Innovations in Aerospace System the Loop Simulator for Control, PLIF for the new AFRL Mach-6 Ludwieg J. Lorenzetti, Purdue University, West Testing Using the Example of Fault-Tolerant and Cyber-Physical Tube Hypersonic Wind Tunnel Lafayette, IN; L. Bañuelos, California High-Lift Systems K. Lam, Spectral Energies, LLC, Dayton, Polytechnic State University, San Luis K. Jandaurek, RWTH Aachen University, T. Bakker, M. Leccadito, R. Klenke, Virginia OH; J. Pickles, V. Narayanaswamy, North Obispo, San Luis Obispo, CA; R. Clarke, O. Aachen, Germany; M. Johst, FFT Production Commonwealth University, Richmond, VA Carolina State University, Raleigh, NC; Murillo, A. Bowers, NASA Armstrong Flight Systems Corporation, Bremen, Germany C. Carter, R. Kimmel, Air Force Research Research Center, Edwards, CA Laboratory, Wright-Patterson AFB, OH 90 Tuesday, 10 January 2017 141-GTE-3 Experimental Tools Austin 5 Chaired by: S. LYNCH, Penn State 0930 hrs 1000 hrs 1030 hrs AIAA-2017-0551 AIAA-2017-0552 AIAA-2017-0553 An Experimental Study of Dynamic Trends in JetCAT Microturbojet- Time-resolved schlieren POD and Ice Accretion Process on Aero- Compressor Efficiency aft deck pressure correlations on engine Spinners N. Grannan, Innovative Scientific Solutions, complex supersonic jet nozzles L. Li, H. Hu, Iowa State University, Inc., Dayton, OH; M. McClearn, P. Litke, M. Berry, A. Magstadt, M. Ali, Syracuse Ames, IA Air Force Research Laboratory, Wright- University, Syracuse, NY; C. Ruscher, Patterson AFB, OH; J. Hoke, Innovative Spectral Energies, LLC, Dayton, OH; M. Scientific Solutions, Inc., Dayton, OH; F. Glauser, Syracuse University, Syracuse, Schauer, Air Force Research Laboratory, NY; S. Gogineni, Spectral Energies, LLC, Wright-Patterson AFB, OH Dayton, OH Tuesday, 10 January 2017 142-HSABP-3 Computational Investigations of Scramjets San Antonio 4 Chaired by: O. POWELL and D. MUSIELAK, University of Texas at Arlington 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2017-0554 AIAA-2017-0555 AIAA-2017-0556 AIAA-2017-0557 AIAA-2017-0558 AIAA-2017-0559 Isolator Dynamics and Heat Release Dynamic Hybrid RANS/LES Simulations Studies on Leading Edge Detection Dynamical Features of a Supersonic Numerical Simulation about Mixing Large-Eddy Simulation of a Dual- during Unstart of a Dual-Mode of Axisymmetric Scramjet Component in Mechanically- and Combustion- Multistream Nozzle with an Aft-Deck Characteristics of an Inlet-Fueled Mode Scramjet Combustor Using Scramjet Flowpaths Generated Shock Trains in Dual- C. Stack, D. Gaitonde, Ohio State Scramjet Engine non-Adiabatic Flamelet Modeling L. Riley, Ohio State University, Columbus, T. Palmer, P. Shah, A. Robinson, ATA Mode Scramjet Engines University, Columbus, OH J. Kim, O. Kwon, Korea Advanced Institute T. Aksu, S. Uslu, TOBB University of OH; M. Hagenmaier, J. Donbar, Air Force Engineering, Inc., San Diego, CA; D. Walters, F. Ladeinde, SUNY Korea, Incheon, South of Science and Technology, Daejeon, Economics and Technology, Ankara, Turkey Research Laboratory, Wright-Patterson AFB, E. Luke, Mississippi State University, Starkville, Korea; Z. Lou, Stony Brook University, South Korea OH; D. Gaitonde, Ohio State University, MS; E. Hassan, Air Force Research Laboratory, Stony Brook, NY; D. Kim, R. Das, Andong Columbus, OH Wright-Patterson AFB, OH; et al. National University, Andong, South Korea Tuesday, 10 January 2017 143-IS-2 Run-Time Assurance for Adaptive and Intelligent Systems (Invited) Ft. Worth 1 Chaired by: E. WONG, NASA Glenn Research Center 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2017-0560 AIAA-2017-0561 AIAA-2017-0562 AIAA-2017-0563 AIAA-2017-0564 The Introduction of Software Certifiable Runtime Assurance of Validation of Convex Optimization Reducing V&V Cost of Flight Critical Military Airworthiness Certification Runtime Protection for Autonomous Distributed Real-Time Systems Algorithms and Credible Systems: Myth or Reality of Autonomous Air Vehicles with Aerospace Systems S. Chaki, D. de Niz, Carnegie Mellon Implementation for Model G. Brat, NASA Ames Research Center, Adaptive Controllers J. Schierman, M. DeVore, N. Richards, University, Pittsburgh, PA Predictive Control Moffett Field, CA M. Dillsaver, M. Clark, Air Force Research Barron Associates, Inc., Charlottesville, VA; E. Feron, R. Cohen, Georgia Institute Laboratory, Wright-Patterson AFB, OH; X. M. Clark, Air Force Research Laboratory, of Technology, Atlanta, GA; G. Davy, P. Zhang, Wright State University, Dayton, OH Wright-Patterson AFB, OH Garoche, ONERA, Toulouse, France Tuesday, 10 January 2017 144-LEC-3 Adaptive Structures Lecture and Special Presentation Texas D 0930 - 1130 hrs Requirements for Morphing from an Airplane Perspective Robert D. Gregg Chief Aerodynamicist Boeing Commercial Airplanes

Special Presentation Remembrance of the Contributions of Dr. Friedrich Straub Tuesday, 10 January 2017 145-MAT-4 Multiscale Modeling and Materials Design Palomino 2 91 Chaired by: J. MATLIK, Rolls-Royce Corp and G. ODEGARD 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2017-0565 AIAA-2017-0566 AIAA-2017-0567 AIAA-2017-0568 Multiscale Elasto-Plastic and Failure Elasto-plastic deformation Tsai-Wu Analysis of a Thin-Walled Peridynamics for Predicting Pit-to- Analysis of Metal Matrix Composite mechanisms of thermoset glassy 3D-Printed Polylactic Acid (PLA) Crack Transition H. Sertse, W. Yu, Purdue University, West polymers depending on the Structural Bracket D. De Meo, L. Russo, E. Oterkus, University Lafayette, IN structural characteristic of hardener: R. Chen, A. Ramachandran, C. Liu, F. of Strathclyde, Glasgow, United Kingdom; A molecular dynamics study Chang, D. Senesky, Stanford University, D. Gunasegaram, I. Cole, Commonwealth H. Park, B. Kim, J. Choi, M. Cho, Seoul Stanford, CA Scientific and Industrial Research National University, Seoul, South Korea Organisation (CSIRO), Clayton, Australia Tuesday, 10 January 2017 146-MDO-4 Aeroelastic Optimization Mustang 1 Chaired by: M. BHATIA, Mississippi State University and A. NING, BYU 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2017-0569 AIAA-2017-0570 AIAA-2017-0571 AIAA-2017-0572 AIAA-2017-0573 Optimal Sizing and Placement SpaRibs Geometry Parameterization Conceptual Design of Complex Aeroservoelastic Optimisation of an Similarity Maximization of a Scaled of Control Surfaces for Active for Wings with Multiple Sections Transonic Aircraft Configurations Aerofoil with Active Compliant Flap Aeroelastic Flight Demonstrator via Aeroservoelastic Control using Single Design Space with Flutter Prediction via Reparametrisation and Variable Multidisciplinary Optimization R. Brown, K. Singh, Miami University, S. De, M. Jrad, D. Locatelli, R. Kapania, R. Gupta, J. Schetz, R. Kapania, Virginia Selection J. Mas Colomer, N. Bartoli, T. Lefebvre, S. Oxford, OH; R. Kolonay, Air Force Research Virginia Polytechnic Institute and State Polytechnic Institute and State University, J. Broughton-Venner, A. Wynn, R. Palacios, Dubreuil, ONERA, Toulouse, France; J. Martins, Laboratory, Wright-Patterson AFB, OH University, Blacksburg, VA; M. Baker, M4 Blacksburg, VA Imperial College London, London, United University of Michigan, Ann Arbor, Ann Arbor, Engineering, Inc., Long Beach, CA Kingdom MI; E. Benard, Higher Institute of Aeronautics and Space, Toulouse, France; et al. Tuesday, 10 January 2017 147-MST-1 Modeling and Simulation of Aeroelasticity and Structural Dynamics San Antonio 3 Chaired by: A. ELMILIGUI, NASA Langley Research Center and P. ZAAL, NASA Ames Research Center 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2017-0574 AIAA-2017-0576 AIAA-2017-0577 AIAA-2017-0578 User subroutine for fatigue Effects of Engine Placement on Modelling Framework for Handling Structural system identification using modeling of wing structure of Nonlinear Aeroelastic Gust Response Qualities Analysis of Flexible degree of freedom-based reduction flapping micro air vehicle of High-Aspect-Ratio Wings Aircraft method and sensor selection algorithm H. Abdelmoula, M. Hassanalian, A. P. Mardanpour, E. Izadpanahi, S. Rastkar, V. Portapas, S. Yusuf, M. Lone, Cranfield H. Sung, Seoul National University, Seoul, Abdelkefi, New Mexico State University, Florida International University, Miami, FL; University, Cranfield, United Kingdom; E. South Korea; S. Chang, Korea Atomic Energy Las Cruces, NM D. Hodges, Georgia Institute of Technology, Coetzee, Airbus, Bristol, United Kingdom Research Institute (KAERI), Daejeon, South Atlanta, GA Korea; M. Cho, Seoul National University, Seoul, South Korea Tuesday, 10 January 2017 148-MST-2 Modeling and Simulation of Uninhabited Aerial Vehicles I San Antonio 2 Chaired by: D. KEATING, The Charles Stark Draper Laboratory, Inc. and D. GINGRAS, Bihrle Applied Research Inc. 0930 hrs 1000 hrs 1030 hrs AIAA-2017-0579 AIAA-2017-0580 AIAA-2017-0581 Longitudinal Aerodynamic Modeling, Simulation, and Control Modelling wing wake and tail-wake Coefficients of Hydra Technologies of Modular Vertical Lift Air Vehicles interaction of a clap-and-peel UAS-S4 from Geometrical Data B. Anderson, J. Warner, J. Rogers, Georgia flapping-wing MAV M. Segui, M. Kuitche, R. Botez, University Institute of Technology, Atlanta, GA S. Armanini, Delft University of Technology, of Québec, Montréal, Canada Delft, The Netherlands; J. Caetano, Portuguese Air Force Academy, Sintra, Portugal; C. de Visser, G. de Croon, Delft University of Technology, Delft, The Netherlands 92 Tuesday, 10 January 2017 149-MVC-3 Meshing Techniques Grapevine 3 Chaired by: N. WYMAN, Pointwise, Inc. and C. BRUNER, Sandia National Laboratories 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2017-0582 AIAA-2017-0583 AIAA-2017-0584 AIAA-2017-0585 AIAA-2017-0586 AIAA-2017-0587 Stitching and Deformation of Non- CFD Simulation of a Quad-Rotor Automatic high-order mesh On a robust boundary layer mesh Efficient and Exact Mesh An Automatic Parallel Octree overlapping Meshes for Unsteady UAV with Rotors in Motion Explicitly generation with Spring-Field and generation process Deformation using Multi-Scale RBF Grid Generation Software with an Rotorcraft Aerodynamics Modeled Using an LBM Approach with vector-adding:3D domain mesh D. Marcum, Mississippi State University, Interpolation Extensible Solver Framework and a M. Nathoo, W. Habashi, M. Fossati, McGill Adaptive Refinement generation Starkville, MS; F. Alauzet, A. Loseille, L. Kedward, C. Allen, T. Rendall, University Focus on Urban Simulation University, Montréal, Canada S. Thibault, Extendsive, Inc., White River T. Liu, University of Tennessee, French Institute for Research in Computer of Bristol, Bristol, United Kingdom E. Hereth, K. Sreenivas, L. Taylor, Junction, VT; D. Holman, S. Garcia, G. Trapani, Chattanooga, Chattanooga, TN; C. Hilbert, Science and Control (INRIA), Saclay, France D. Nichols, University of Tennessee, Next Limit Dynamics, Madrid, Spain Branch Technology, Chattanooga, TN Chattanooga, Chattanooga, TN Tuesday, 10 January 2017 150-NDA-2/MDO-5 Optimization Under Uncertainty I Mustang 2 Chaired by: J. GRAY, NASA Glenn Research Center and R. GRANDHI, Wright State University 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2017-0588 AIAA-2017-0589 AIAA-2017-0590 AIAA-2017-0591 AIAA-2017-0592 Effective Operations of Extinction- A Decision-Support Methodology Horsetail Matching for Optimization Probabilistic Characterization of Probabilistic pipe strength and Reignition with Simple Control of and Framework to Make Risk/Value Under Probabilistic, Interval and Composite-Aluminum Cocured Joints toughness estimation through Oxidizer Flux on a Single-Stage Trade-Offs in a Business-Driven Mixed Uncertainties N. Phelps, S. TerMaath, University of information fusion with Bayesian Sounding Hybrid Rocket Environment L. Cook, J. Jarrett, University of Cambridge, Tennessee, Knoxville, Knoxville, TN updating K. Chiba, University of Electro-Communications, F. Burgaud, J. Durand, D. Mavris, Georgia Cambridge, United Kingdom; K. Willcox, S. Dahire, Y. Liu, Y. Jiao, Arizona State Tokyo, Japan; M. Kanazaki, Tokyo Institute of Technology, Atlanta, GA Massachusetts Institute of Technology, University, Tempe, AZ Metropolitan University, Tokyo, Japan; T. Cambridge, MA Shimada, Japan Aerospace Exploration Agency (JAXA), Sagamihara, Japan Tuesday, 10 January 2017 151-NDA-3 Uncertainty Quantification I Mustang 3 Chaired by: H. BAE, Wright State University and N. KIM, University of Florida 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2017-0593 AIAA-2017-0594 AIAA-2017-0595 AIAA-2017-0596 AIAA-2017-0597 AIAA-2017-0598 Non-Deterministic Kriging Efficient Global Sensitivity Confidence Interval of Bayesian Numerical Analysis of Uncertainty in Higher-order moments of Efficient Integration Method for Framework for Responses with Analysis for Time-Dependent, Network and Global Sensitivity Crack Growth Prediction in Repaired generalized polynomial chaos Uncertainty Quantification Mixed Uncertainty Multidisciplinary Models Analysis Aluminum Alloys expansions for intrusive and non- S. Mulani, University of Alabama, D. Clark, H. Bae, Wright State University, E. DeCarlo, S. Mahadevan, Vanderbilt S. Bae, N. Kim, C. Park, University of B. Heng, S. TerMaath, University of intrusive uncertainty quantification Tuscaloosa, Tuscaloosa, AL; R. Walters, Dayton, OH University, Nashville, TN; B. Smarslok, Florida, Gainesville, Gainesville, FL Tennessee, Knoxville, Knoxville, TN E. Savin, ONERA, Châtillon, France; B. Virginia Polytechnic Institute and State Air Force Research Laboratory, Wright- Faverjon, Insa-Lyon, Villeurbanne, France University, Blacksburg, VA Patterson AFB, OH; D. Sparkman, Universal Technology Corporation, Dayton, OH Tuesday, 10 January 2017 152-PC-10 Detonations, Explosions, and Supersonic Combustion Ft. Worth 3 Chaired by: C. BROPHY, Naval Postgraduate School and T. JACKSON, University of Florida 0930 hrs 1000 hrs 1030 hrs AIAA-2017-0599 AIAA-2017-0600 AIAA-2017-0601 An Experimental Investigation of Uncertainty Quantification in the Numerical Simulation of Supersonic Fast Hydrogen-Air Flames and Simulation of Explosive Particle Premixed Turbulent Combustion Detonations Using a Turbulence Dispersal using an Eulerian/ T. Nielsen, J. Edwards, North Carolina State Generating Facility Lagrangian Formulation University, Raleigh, NC J. Chambers, K. Ahmed, University of M. Akiki, T. Gallagher, G. Hannebique, S. Central Florida, Orlando, FL Menon, Georgia Institute of Technology, Atlanta, GA

93 Tuesday, 10 January 2017 153-PC-11 Combustion Modeling and Simulation III San Antonio 6 Chaired by: J. OEFELEIN, Sandia National Laboratories and G. BORGHESI 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2017-0602 AIAA-2017-0603 AIAA-2017-0604 AIAA-2017-0605 AIAA-2017-0606

Hybrid Multi-Timescale and Direct Numerical Simulations of NOx Effect of the turbulence modeling Comparison of Flamelet/Progress- LES Simulation of the Cambridge G-Scheme Method for Efficient formation in spatially developing in large-eddy simulations of Variable and Finite-Rate Chemistry Stratified Flame Using Optimized Modeling with Detailed Chemical turbulent premixed Bunsen flames nonpremixed flames undergoing LES Models in a Preconditioning Virtual Mechanisms Kinetics with mixture inhomogeneity extinction and reignition Scheme R. Mercier, Safran Group, Magny-les- W. Sun, T. Grenga, Y. Ju, Princeton S. Luca, A. Attili, F. Bisetti, King Abdullah E. Gonzalez, A. Dasgupta, CSE, Inc., Columbia, S. Yang, X. Wang, V. Yang, W. Sun, H. Hameaux, France; M. Cailler, B. Fiorina, University, Princeton, NJ University of Science and Technology, MD; S. Arshad, M. Oevermann, Chalmers Huo, Georgia Institute of Technology, École Centrale Paris, Châtenay-Malabry, Thuwal, Saudi Arabia University of Technology, Göteborg, Sweden Atlanta, GA France Tuesday, 10 January 2017 154-PC-12 Chemical Kinetics for Multi-Component Fuels San Antonio 5 Chaired by: J. HEYNE, University of Dayton and V. KATTA, Innovative Scientific Solutions Incorporated 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2017-0607 AIAA-2017-0608 AIAA-2017-0609 AIAA-2017-0610 AIAA-2017-0611 AIAA-2017-0612 A Comparative Study of Combustion Evaluation of Kinetics Models for On the Development of General Species Selectivity Ratios from Temperature Jump Pyrolysis Studies Pyrolysis of RP-2 and Surrogate Fuels Chemistry of Conventional and JP-8 in Predicting Unsteady Flames Surrogate Composition Calculations Thermal Pyrolysis of Jet Fuels of RP-2 Fuel in a Jet Stirred Reactor Coupled with Alternative Jet Fuels with Hybrid V. Katta, Innovative Scientific Solutions, for Chemical and Physical Properties in a Microflow Tube Reactor: O. Pryor, University of Central Florida, Synchrotron Photo Ionization Mass Chemistry Approach Inc., Dayton, OH; W. Roquemore, Air Force D. Bell, J. Heyne, University of Dayton, Dayton, Experimental and Modeling Effor Orlando, FL; S. Chambreau, G. Vaghjiani, Spectrometry R. Xu, D. Chen, K. Wang, H. Wang, Research Laboratory, Wright-Patterson OH; S. Won, F. Dryer, F. Haas, Princeton H. Chelliah, M. Rahimi, U. Shrestha, K. Air Force Research Laboratory, Edwards G. Barari, Embry-Riddle Aeronautical University, Stanford University, Stanford, CA AFB, OH University, Princeton, NJ; S. Dooley, University Dang, University of Virginia, Charlottesville, AFB, CA; S. Vasu, University of Central Prescott, AZ; D. Popolan-Vaida, Lawrence of Limerick, Limerick, Ireland Charlottesville, VA Florida, Orlando, FL Berkeley National Laboratory, Berkeley, CA; S. Vasu, University of Central Florida, Orlando, FL Tuesday, 10 January 2017 155-PDL-3 Diagnostics for Plasmas and Gases I Ft. Worth 4 Chaired by: K. XU, University of Alabama in Huntsville 0930 hrs 1030 hrs 1130 hrs Oral Presentation Oral Presentation Oral Presentation Rayleigh and Raman Scattering Techniques and Application to Plasmas Microwave plasma diagnostic techinques Cavity Ring-Down Spectroscopy Plasma Diagnostics C. Limbach, Texas A&M University, College Station, TX A. Shashurin, Purdue University, West Lafayette, IN A. Yalin, Colorado State University, Fort Collins, CO Tuesday, 10 January 2017 156-SATS-4 Small Satellite Mission Design Austin 6 Chaired by: J. STRAUB, North Dakota University 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2017-0613 AIAA-2017-0614 AIAA-2017-0615 AIAA-2017-0616 AIAA-2017-0617 Time-optimal Slew Maneuver Using Safe, Failure-Tolerant CubeSat Navigation Analysis of WSB Low BRICSat-D Flight Experiment: A Nano-Satellite System for Single Gimbal Control Moment Gyro Docking Using Passive Magnetic Energy Lunar Transfer for SRMSAT-2 Demonstrating the Feasibility of Atmospheric Monitoring and Ground for Small Agile satellites Mechanisms K. Barad, T. Sharma, SRM University, Low Cost Diagnostic Missions Imaging M. Elkhayat, Y. Elhalwagy, A. ElRaffie, G. K. Doyle, M. Peck, Cornell University, Chennai, India D. Wenberg, J. Pittman, M. Lange, B. C. Sachdeva, PEC University of Technology, Elnashar, Egyptian Armed Forces, Cairo, Ithaca, NY Keegan, E. Hanlon, J. Kang, U.S. Naval Chandigarh, India; M. Gupta, Georgia Egypt Academy, Annapolis, MD; et al. Institute of Technology, Atlanta, GA Tuesday, 10 January 2017 157-SCS-2 Small Satellite Deployable Structures Palomino 1 Chaired by: S. BRADFORD, Jet Propulsion Laboratory and J. BLACK, Virginia Tech 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2017-0618 AIAA-2017-0619 AIAA-2017-0620 AIAA-2017-0621 AIAA-2017-0622 AIAA-2017-0623 Micro-gravity Testing of Boom- Membrane Deployment de-orbit From Prototype to Flight: Qualifying Flight Qualification Testing of a Meter- Composite Tube Flexures at Structural Optimization of

94 Membrane Integrated Deployable System by convex tapes a Ka-band Parabolic Deployable class CubeSat Deployable Boom Nanosatellite Scale Composite Spring Tape Hinges Structures for Micro-satellites N. Tada, S. Inoue, Y. Miyazaki, M. Antenna (KaPDA) for CubeSats J. Fulton, University of Colorado, Boulder, M. Santer, Imperial College London, C. Qian, Q. Chen, Y. Hou, H. Fang, H. Furuya, K. Yashima, T. Yokomatsu, H. Yamazaki, Nihon University, Funabashi, J. Sauder, N. Chahat, B. Hirsch, R. Hodges, Boulder, CO; S. Jeon, LoadPath, LLC, London, United Kingdom Shanghai YS Information Technology Sakamoto, Tokyo Institute of Technology, Japan Jet Propulsion Laboratory, California Albuquerque, NM; T. Murphey, Roccor, LLC, Company, Ltd., Shanghai, China Yokohama, Japan; A. Watanabe, Sakase Institute of Technology, Pasadena, CA; Y. Longmont, CO Adtech Company, Ltd., Fukui, Japan Rahmat-Samii, University of California, Los Angeles, Los Angeles, CA; E. Peral, Jet Propulsion Laboratory, California Institute of Technology, Pasadena, CA; et al. Tuesday, 10 January 2017 158-SD-7 Piezoelectric Materials for Active and Passive Vibration Control Appaloosa 2 Chaired by: D. JOHNSON, NASA Glenn Research Center and C. BARNES, AFRL/RQVA 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2017-0624 AIAA-2017-0625 AIAA-2017-0626 AIAA-2017-0627 AIAA-2017-0628 AIAA-2017-0629 Highly Flexible Piezoelectric Analytical modeling and On the potential of monostable Cross-sectional Stress Analysis of Necessity of accurate estimation On the Energy Harvesting Potential Multifunctional Wings for Adaptive effectiveness of low-frequency piezomagnetoelastic energy harvesting Smart Beam Energy Harvesters of the galloping force for efficient of an Airfoil-Based Piezoaeroelastic Vibration Control and Energy piezoelectric energy harvesters with from vortex-induced vibrations N. Hosking, Z. Sotoudeh, Rensselaer design of energy harvesters Harvester from Coupled Pitch- Harvesting dual magnetic forces R. Naseer, New Mexico State University, Las Polytechnic Institute, Troy, NY U. Javed, A. Abdelkefi, New Mexico State Plunge-Leadlag Vibrations N. Tsushima, W. Su, University of Alabama, S. Zimmerman, H. Abdelmoula, A. Cruces, NM; H. Dai, Huazhong University of University, Las Cruces, NM Y. Wu, D. Li, J. Xiang, Beihang University, Tuscaloosa, Tuscaloosa, AL Abdelkefi, New Mexico State University, Science and Technology, Wuhan, China; A. Beijing, China Las Cruces, NM Abdelkefi, New Mexico State University, Las Cruces, NM; L. Wang, Huazhong University of Science and Technology, Wuhan, China Tuesday, 10 January 2017 159-SD-8 Vehicle and Component Response to Gust, Impact, and Thermal Loads Appaloosa 3 Chaired by: W. SILVA, NASA-Langley Research Center and M. PATIL, Virginia Tech 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2017-0630 AIAA-2017-0631 AIAA-2017-0632 AIAA-2017-0633 AIAA-2017-0634 AIAA-2017-0635 Testing of Wing-Tip Spring Device Finite Element Simulation of Three A Doublet-Lattice Method Correction Spacecraft Pyroshock Attenuation in A Gust Reconstruction Framework Wind Tunnel Tests of Whirl Flutter for Gust Loads Alleviation Full-Scale Crash Tests for Cessna Approach for High Fidelity Gust Three Parts Applied to a Nonlinear Reduced Order Aeroelastic Demonstrator R. Cheung, A. Castrichini, J. Cooper, 172 Aircraft Loads Analysis V. Babuska, S. Gomez, S. Smith, C. Model of a Wing Typical Section J. Cecrdle, P. Malinek, O. Vich, Aerospace University of Bristol, Bristol, United B. Mason, J. Warren, NASA Langley C. Valente, Siemens, Leuven, Belgium; C. Hammetter, Sandia National Laboratories, S. Simeone, University of Bristol, Bristol, Research and Test Establishment (VZLÚ), Kingdom Research Center, Hampton, VA Wales, D. Jones, A. Gaitonde, J. Cooper, Albuquerque, NM; D. Murphy, University of United Kingdom; A. Da Ronch, University of Prague, Czech Republic University of Bristol, Bristol, United Georgia, Athens, GA Southampton, Southampton, United Kingdom; Kingdom; Y. Lemmens, Siemens, Leuven, T. Rendall, University of Bristol, Bristol, United Belgium Kingdom Tuesday, 10 January 2017 160-SD-9 Special session: Aeroelastic Prediction III Appaloosa 4 Chaired by: D. GRIFFITH and C. SPODE, Embraer S/A 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2017-0636 AIAA-2017-0637 AIAA-2017-0638 AIAA-2017-0639 AIAA-2017-0640 Gust and Ground Loads Integration Static and Dynamic Aeroelastic Towards a Hybrid Time-Frequency Tiltrotor Whirl-Flutter Stability Overset Grid Simulations for the for Aircraft Landing Loads Validation of a Flexible Forward Domain Approach for Time-Variant Predictions using Comprehensive Second AIAA Aeroelastic Prediction Prediction Swept Composite Wing Buffeting Flows Analysis Workshop A. Castrichini, J. Cooper, University of M. Ritter, J. Dillinger, Y. Meddaikar, F. Roizner, M. Karpel, Technion--Israel A. Kreshock, Army Research Laboratory, J. Housman, C. Kiris, NASA Ames Research Bristol, Bristol, United Kingdom; T. Benoit, German Aerospace Center (DLR), Institute of Technology, Haifa, Israel; R. Hampton, VA; H. Yeo, Army Aviation Center, Moffett Field, CA Y. Lemmens, Siemens, Leuven, Belgium Göttingen, Germany Carrese, P. Marzocca, RMIT University, and Missile Research Development and Melbourne, Australia Engineering Center, Moffett Field, CA

95 Tuesday, 10 January 2017 161-SE-1 Systems Engineering I Dallas 6 Chaired by: J. EILER, Stellar Solutions, Inc. and D. DRESS, NASA Langley Research Center 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2017-0641 AIAA-2017-0642 AIAA-2017-0643 AIAA-2017-0644 First Steps in Implementing Weapon Quantifying Negotiations and Initial Exploiting Pessimism for Fault Tree Contract-Based Byzantine Resilience System Sustainment Model Bids through a Weighted Analytical Completeness in Spacecraft Swarms C. Vono, Self, Ogden, UT Hierarchy Process A. Wille, F. Holzapfel, Technical University M. Sievers, Jet Propulsion Laboratory, D. Tinker, D. Watkins, Vanderbilt University, of Munich, Munich, Germany California Institute of Technology, Nashville, TN; R. Choate, Western Kentucky Pasadena, CA; A. Madni, University of University, Bowling Green, KY Southern California, Los Angeles, CA Tuesday, 10 January 2017 162-SEN-1 Novel Aerospace Sensor Systems Ft. Worth 2 Chaired by: D. ACCARDO, University of Naples 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2017-0645 AIAA-2017-0646 AIAA-2017-0647 AIAA-2017-0648 Airborne Active Sensing for Pipeline Distributed High Temperature Error Sensitivity Analysis of Small Estimating the Attitude of an Leak Survey Measurement for Monitoring Bleed Air UAS Wind-Sensing Systems Unmanned Aerial Vehicle through J. Bartholomew, P. Lyman, C. Weimer, L. Lines and other Aircraft Structures T. Nichols, B. Argrow, University of Multiple Low-Cost Ultrasonic Range Ruppert, Ball Aerospace & Technologies E. Templeton, M. Davis, J. Pedrazzani, Colorado, Boulder, Boulder, CO; D. Sensors Corporation, Boulder, CO O. Ohanian, Luna Innovations, Inc., Kingston, Air Force Research Laboratory, R. Salguero, M. Rhudy, Pennsylvania State Blacksburg, VA Dayton, OH University, Reading, PA Tuesday, 10 January 2017 163-SOF-3 Open Systems Architecture - Best practices, Veriﬁcation, and Security Ft. Worth 7 0930 - 1230 hrs Come and hear from experienced OSA practitioners about various aspects of their own OSA efforts that were challenging or risky and which mitigation approaches emerged.

Panelists: Peter Mehlitz Ron Kohl Bryce Meyer Misty Davies NASA Ames Research Center R. J. Kohl and Associates Software Engineering Institute NASA Ames Research Center

Tuesday, 10 January 2017 164-SRE-3 Resource Harvesting Ft. Worth 5 Chaired by: J. KLEINHENZ, NASA Glenn Research Center 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2017-0649 AIAA-2017-0650 AIAA-2017-0651 AIAA-2017-0652 In-situ Nitrogen Harvesting for the The Use of Lithium Fuel with Initial Design and Analysis of a Producing Volatiles from Asteroid Titan Submarine Planetary In Situ Oxidizers System Extracting and Collecting Simulants: Preliminary Results P. Meyerhofer, Case Western Reserve T. Baker, T. Miller, M. Paul, J. Peters, Water from Temporarily Captured L. Gertsch, Missouri University of Science and University, Cleveland, OH; J. Hartwig, NASA Pennsylvania State University, University Orbiters Technology, Rolla, MO; A. Abbud-Madrid, C. Glenn Research Center, Cleveland, OH Park, PA S. Nomura, M. Tomooka, R. Funase, Dreyer, Colorado School of Mines, Golden, CO; University of Tokyo, Bunkyo, Japan R. Jedicke, A. Krot, University of Hawaii, Hilo, Hilo, HI; D. Linne, NASA Glenn Research Center, Cleveland, OH; et al. Tuesday, 10 January 2017 165-STR-5 Composite Damage and Failure Prediction Methods II Appaloosa 1 Chaired by: S. ENGELSTAD, Lockheed Martin Aeronautics and S. WANTHAL, The Boeing Company 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs 96 AIAA-2017-0653 AIAA-2017-0654 AIAA-2017-0655 AIAA-2017-0656 AIAA-2017-0657 AIAA-2017-0658 A Numerical Study on the Edgewise A nonlocal constitutive model for A Multiscale Fatigue Damage Peridynamic Augmented XFEM An Integrated Crack Initiation and Multiscale Damage Development in Compression Strength of Sandwich damageable brittle and quasi-brittle Prediction for Notched Composite M. Dorduncu, A. Barut, E. Madenci, Propagation Module for Fatigue Polymer Composite Laminates Structures with Facesheet-Core materials Components University of Arizona, Tucson, Tucson, AZ; Damage Prediction of Composite N. Parambil, S. Gururaja, Indian Institute of Disbonds Z. Gao, L. Zhang, W. Yu, Purdue University, J. Xiao, X. Fang, J. Lua, Global Engineering and N. Phan, Naval Air Systems Command, Structures Science, Bengaluru, India A. Bergan, NASA Langley Research Center, West Lafayette, IN Materials, Inc., Princeton, NJ; R. Li, D. Zhang, Patuxent River, MD X. Cui, X. Fang, J. Lua, Global Engineering Hampton, VA University of Connecticut, Storrs, Storrs, CT and Materials, Inc., Princeton, NJ Tuesday, 10 January 2017 166-TP-5 Aerothermodynamics II Austin 2 Chaired by: D. HASH, NASA - ARC and M. BORG, Air Force Research Laboratory 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2017-0659 AIAA-2017-0660 AIAA-2017-0661 AIAA-2017-0662 AIAA-2017-0663 AIAA-2017-0664

State-resolved O2--N2 kinetic model Dissociation and internal excitation Quantal treatment of O2--Ar Evaluation of Eigenvalues for Numerical investigation of Double-Cone Flows in at hypersonic temperatures of molecular nitrogen due to N2-N vibrational relaxation at hypersonic the Analysis of Combustion and vibrational relaxation coupling with Nonequilibrium: Comparison of CFD D. Andrienko, I. Boyd, University of collisions using direct molecular temperatures Chemical Non-Equilibrium Flows turbulent mixing with Experimental Data Michigan, Ann Arbor, Ann Arbor, MI simulation I. Ulusoy, Georgia Institute of Technology, V. Naoumov, Central Connecticut State R. Fiévet, University of Michigan, Ann K. Vogiatzis, Engility Corporation, Dayton, M. Grover, N. Singh, T. Schwartzentruber, Atlanta, GA; D. Andrienko, I. Boyd, University, New Britain, CT; A. Abdullin, V. Arbor, Ann Arbor, MI; S. Voelkel, University OH; E. Josyula, Air Force Research University of Minnesota, Minneapolis, University of Michigan, Ann Arbor, Ann Kriukov, Kazan Federal University, Kazan, of Texas, Austin, Austin, TX; V. Raman, Laboratory, Wright-Patterson AFB, OH; P. Minneapolis, MN; R. Jaffe, NASA Ames Arbor, MI; R. Hernandez, Johns Hopkins Russia University of Michigan, Ann Arbor, Ann Vedula, University of Oklahoma, Norman, Research Center, Moffett Field, CA University, Baltimore, MD Arbor, MI; P. Varghese, University of Texas, Norman, OK Austin, Austin, TX Tuesday, 10 January 2017 167-TP-6 Heat Transfer II Austin 3 Chaired by: E. SHORT, Raytheon Company and S. SHERIF, University of Florida 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2017-0665 AIAA-2017-0666 AIAA-2017-0667 AIAA-2017-0668 Numerical Simulation of Heat Uniform Design Correlations for Development of a three- Model of Plume Flowfield from Transfer Flow-Field under Glaze Ice Accretion and Convective dimensional, unstructured material Oxy-Acetylene Torch Transcritical Condition Heat Transfer from an Airfoil response design tool N. Diaz, J. Langston, University of Texas, T. Toki, S. Teramoto, University of Tokyo, B. Peach, K. Pope, G. Naterer, Memorial J. Schulz, Analytical Mechanics Associates, Austin, Austin, TX; M. Salita, Salita Tokyo, Japan; K. Okamoto, University of University of Newfoundland, St. John’s, Inc., Mountain View, CA; E. Stern, NASA Consulting, Phoenix, AZ; F. Stefani, J. Koo, Tokyo, Kashiwa, Japan Canada Ames Research Center, Moffett Field, University of Texas, Austin, Austin, TX CA; S. Muppidi, G. Palmer, Analytical Mechanics Associates, Inc., Mountain View, CA; O. Schroeder, University of Kentucky, Lexington, Lexington, KY Tuesday, 10 January 2017 168-UMS-4 Special Session: Safe Autonomous Urban Flight II Grapevine 1 Chaired by: V. STEPANYAN, Universities Space Research Association and A. CHAKRABARTY 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2017-0669 AIAA-2017-0670 AIAA-2017-0671 AIAA-2017-0672 Guaranteed Model Reference Estimation, Navigation and Control An Integrated System for Proportional Navigation Based Adaptive Control Performance in of Multi-Rotor Drones in an Urban Autonomous Search and Track with Guidance Laws for UAV Obstacle the Presence of Actuator Failures Wind Field a small Unmanned Aerial Vehicle Avoidance in Complex Urban E. Arabi, B. Gruenwald, T. Yucelen, V. Stepanyan, Universities Space A. Chakrabarty, R. Morris, X. Environments University of South Florida, Tampa, FL; J. Research Association, Moffett Field, CA; Bouyssounouse, R. Hunt, NASA Ames M. Clark, R. Prazenica, Embry-Riddle Steck, Wichita State University, Wichita, KS K. Krishnakumar, NASA Ames Research Research Center, Moffett Field, CA Aeronautical University, Daytona Beach, FL 97 Center, Moffett Field, CA Tuesday, 10 January 2017 169-UMS-5 UAS Autonomy and Path Planning I Grapevine 2 Chaired by: J. WILHELM, Ohio University and K. KOCHERSBERGER, Virginia Polytechnic Institute and State University 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2017-0673 AIAA-2017-0674 AIAA-2017-0675 AIAA-2017-0676 AIAA-2017-0677 AIAA-2017-0678 Homography-Based State Vision Sensor Fusion for Model Predictive Control Based Receding Horizon-based RRT* Implementation & Flight Testing of Optimization of Dynamic Soaring Estimation for Autonomous UAV Autonomous Landing Dynamic Geofence System for Algorithm for a UAV Real-time Path the IMPACT System for Autonomous Maneuvers for a Morphing Capable Landing T. Nakamura, S. Haviland, D. Bershadsky, Unmanned Aerial Vehicles Planner ISR UAV A. Chavez, D. L’Heureux, N. Prabhakar, M. E. Johnson, Georgia Institute of Technology, S. Zhang, D. Wei, M. Huynh, J. Quek, H. Lee, D. Lee, D. Shim, Korea Advanced J. Boskovic, J. Jackson, R. Wise, Scientific I. Mir, A. Maqsood, National University Clark, W. Law, R. Prazenica, Embry-Riddle Atlanta, GA X. Ma, L. Xie, Nanyang Technological Institute of Science and Technology, Systems Company, Inc., Woburn, MA of Sciences and Technology, Islamabad, Aeronautical University, Daytona Beach, FL University, Singapore, Singapore Daejeon, South Korea Pakistan; S. Akhtar, College of Aeronautical Engineering, Risalpur, Pakistan Tuesday, 10 January 2017 170-WE-2 Wind Turbine Extreme Loads Analysis Austin 4 Chaired by: L. MANUEL, University of Texas at Austin 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs Oral Presentation Oral Presentation AIAA-2017-0679 AIAA-2017-0680 AIAA-2017-0681 AIAA-2017-0682 American perspective on wind European perspective on wind Adaptive Extreme Load Estimation Advances in the Assessment of Wind Wind Turbine Loads during the On Simulation of a Rear-Flank energy research aimed at reducing energy research aimed at reducing in Wind Turbines Turbine Operating Extreme Loads via Evening Transition Period Downburst with Non-Stationary the cost of wind energy through the cost of wind energy through Q. Pan, E. Byon, University of Michigan, More Efficient Calculation Approaches N. Lu, University of Texas, Austin, Turbulence and its Influence on advances in wind-plant flow physics advances in wind-plant flow physics Ann Arbor, Ann Arbor, MI P. Graf, R. Damiani, K. Dykes, J. Jonkman, Austin, TX; S. Basu, North Carolina Wind Turbine Extreme Loads D. Laird, P. Veers, National Renewable modeling and understanding National Renewable Energy Laboratory, State University, Raleigh, NC; L. Manuel, H. Nguyen, L. Manuel, University of Texas, Energy Laboratory, Golden, CO F. Rasmussen, Technical University of Golden, CO; A. Ning, Brigham Young University, University of Texas, Austin, Austin, TX Austin, Austin, TX Denmark, Roskilde, Denmark Provo, UT Tuesday, 10 January 2017 171-WKSP-1 Career Workshop I Mustang 4 0930 - 1230 hrs Tuesday, 10 January 2017 172-LUNCH-2 Recognition Luncheon: Celebrating Achievements in Aerospace Sciences and Information Systems Texas A & B 1230 - 1400 hrs Tuesday, 10 January 2017 173-AA-5 Aeroacoustics Jet Noise III Grapevine B Chaired by: J. MENDOZA, United Technologies Research Center and P. MORRIS, Pennsylvania State University 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2017-0683 AIAA-2017-0684 AIAA-2017-0685 AIAA-2017-0686 AIAA-2017-0687 AIAA-2017-0688 Further Development of Supersonic Modeling Jet Noise using Potential Acoustic mode and sources in a Wavepacket intermittency and its Flow and Noise from Septa Nozzles Ideal Gas Effects in Aeroacoustics Jet Noise Reduction Using Nozzle Flow and Simple Acoustic Sources supersonic jet role in turbulent jet noise K. Zaman, J. Bridges, NASA Glenn Research J. Joseph, C. Tinney, University of Texas, Fluidic Inserts C. Ruscher, S. Gogineni, Spectral Energies, S. Unnikrishnan, D. Gaitonde, Ohio State O. Schmidt, T. Colonius, California Institute Center, Cleveland, OH Austin, Austin, TX; N. Murray, University of J. Morgan, P. Morris, D. McLaughlin, C. LLC, Dayton, OH; D. Gaitonde, Ohio State University, Columbus, OH of Technology, Pasadena, CA; G. Brès, Mississippi, Oxford, Oxford, MS Prasad, Pennsylvania State University, University, Columbus, OH; B. Kiel, A. Giese, Cascade Technologies, Inc., Palo Alto, CA University Park, PA Air Force Research Laboratory, Wright- Patterson AFB, OH Tuesday, 10 January 2017 174-ACD-6 Aircraft Design Tools and Methods IV San Antonio 1 Chaired by: P. RAJ, Virginia Polytechnic Institute and State University and P. MARZOCCA 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2017-0689 AIAA-2017-0690 AIAA-2017-0691 AIAA-2017-0692 AIAA-2017-0693 AIAA-2017-0694 A Method of Static Aeroelastic A Design Optimization Technique for Certification Modeling of Composites An Innovative Total-Flight-Envelope A Single Digital Thread Approach to Dorsal Fin Design Method: A Low 98 Analysis Based on Three Dimension Multi-Robot Systems Fuselage, Considering Effect of Defects Approach to Teach Configuration Aircraft Detailed Design Cost Aerodynamic Solution to Aerodynamic Force and Aeroelastic J. Durand, F. Burgaud, K. Cooksey, D. from Fiber Placement Manufacturing Aerodynamics A. Gharbi, D. Sarojini, E. Kallou, D. Harper, Prevent Loss-of-Control Correction for Hypersonic Vehicles Mavris, Georgia Institute of Technology, Processes T. Takahashi, J. Kirkman, A. Verbin, Arizona V. Petitgenet, D. Rancourt, Georgia Institute W. Anemaat, A. Karwas, W. Liu, S. X. Wang, Z. Wan, C. Yang, Beihang Atlanta, GA F. Abdi, AlphaSTAR Corporation, Long Beach, State University, Tempe, AZ; M. Cotting, of Technology, Atlanta, GA; et al. Johnson, Design, Analysis and Research University, Beijing, China CA; Z. Gürdal, University of South Carolina, U.S. Air Force Test Pilot School, Edwards Corporation, Lawrence, KS Columbia, Columbia, SC; D. Huang, AlphaSTAR AFB, CA Corporation, Long Beach, CA Tuesday, 10 January 2017 175-AFM-4 Flight Test and System Identification I Grapevine 5 Chaired by: J. SEYMOUR, Lockheed Martin and J. GRAUER, NASA Langley Research Center 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs AIAA-2017-0695 AIAA-2017-0696 AIAA-2017-0697 AIAA-2017-0698 AIAA-2017-0699 Application of Multivariate Efficient Testing Combining Design Improved Persistent Excitation for In-Flight Thrust Measurement using Selected Aeroelastic Modeling Orthogonal Functions to Identify of Experiment and Learn-to-Fly Real Time Parameter Estimation On-Board Force Sensor Results from the X-56A Stiff Wing Aircraft Flutter Modes Strategies M. AlAbsi, T. Fields, University of Missouri, M. Bronz, H. Garcia de Marina, G. Configuration Flight Tests O. Chavez, S. Yusuf, M. Lone, Cranfield P. Murphy, J. Brandon, NASA Langley Kansas City, Kansas City, MO Hattenberger, French Civil Aviation J. Grauer, NASA Langley Research Center, University, Cranfield, United Kingdom Research Center, Hampton, VA University, Toulouse, France Hampton, VA; M. Boucher, NASA Armstrong Flight Research Center, Edwards, CA Tuesday, 10 January 2017 176-AMT-8 Pressure Determination Techniques and Applications Grapevine 6 Chaired by: J. CRAFTON, Innovative Scientific Solutions Incorporated and X. LIU, San Diego State University 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs AIAA-2017-0700 AIAA-2017-0701 AIAA-2017-0702 AIAA-2017-0703 AIAA-2017-0704 Mean and Fluctuating pressure Data Processing Tools for Dynamic Improvement of Signal-to- Improvement of Lifetime-based Pressure-Sensitive Paint estimation from snapshots of planar Pressure-Sensitive Paint Noise Ratio for Unsteady PSP PSP Technique for Industrial Wind Measurement under Transient PIV measurements J. Crafton, Innovative Scientific Solutions, Inc., Measurement Tunnel Tests Plasma in M=2 Airflow. J. Van der Kindere, R. de Kat, B. Dayton, OH; J. Gregory, Ohio State University, T. Noda, M. Kameda, Tokyo University D. Yorita, U. Henne, C. Klein, German T. Hayashi, A. Houpt, B. Hedlund, S. Ganapathisubramani, University of Columbus, OH; M. Sellers, Aerospace Testing of Agriculture and Technology, Koganei, Aerospace Center (DLR), Göttingen, Leonov, H. Sakaue, University of Notre Southampton, Southampton, United Alliance, Telluhoma, TN; W. Ruyten, Euclidean Japan; K. Nakakita, Japan Aerospace Germany Dame, Notre Dame, IN Kingdom Optics, Murfreesboro, SD Exploration Agency (JAXA), Chofu, Japan Tuesday, 10 January 2017 177-APA-16 Aerodynamic Design: Analysis, Methodologies, and Optimization Techniques II Dallas 3 Chaired by: J. LATZ, Northrop Grumman Aerospace Systems and B. MCGRATH, Johns Hopkins University Applied Physics Laboratory 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2017-0705 AIAA-2017-0706 AIAA-2017-0707 AIAA-2017-0708 AIAA-2017-0709 AIAA-2017-0710 Design Optimization by Manifold Adjoint-Based Nonlinear Output Short and slim nacelle design for An optimisation method for nacelle A successive gappy proper orthogonal Design of Airfoils in Unsteady Mapping Response Correction and Space Mapping for Accelerated ultra-high BPR engines design decomposition approach and its Viscous Flows Using Hierarchical Low-Fidelity Model Preconditioning Aerodynamic Shape Optimization M. Robinson, D. MacManus, K. Richards, M. Robinson, D. MacManus, A. application to inverse airfoil design Kriging Model L. Leifsson, Iowa State University, Ames, L. Leifsson, Iowa State University, Ames, Cranfield University, Cranfield, United Heidebrecht, Cranfield University, Cranfield, S. Li, Z. Gao, C. Gao, L. Zhou, Northwestern C. Song, W. Song, X. Yang, Northwestern IA; S. Koziel, Reykjavik University, IA; S. Koziel, Reykjavik University, Kingdom; C. Sheaf, Rolls-Royce Group plc, United Kingdom; N. Grech, Rolls-Royce Polytechnical University, Xi’an, China Polytechnical University, Xi’an, China Reykjavik, Iceland Reykjavik, Iceland Derby, United Kingdom Group plc, Derby, United Kingdom Tuesday, 10 January 2017 178-APA-17 Flow Control Applications and Demonstrations (Active and Passive) II Dallas 1 99 Chaired by: M. CALVERT, U.S. Army AMRDEC and J. CODER, University of Tennessee 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs AIAA-2017-0711 AIAA-2017-0712 AIAA-2017-0713 AIAA-2017-0714 AIAA-2017-0715 A Numerical Study on the Ability On the Separated Flow Using Pulsed Transonic Buffet Control by Plasma Diminution of transonic buffet Separation Control over a of Shock Control Bumps for Buffet Nanosecond DBD Plasma Actuators Actuator with Spark Discharge phenomenon by plasma actuators NACA0015 Airfoil Using Alleviation on an NACA0015 Airfoil V. Soudakov, TsAGI, Zhukovsky, Russia; A. Firsov, Y. Isaenkov, I. Moralev, Russian Nanosecond Pulsed Plasma Actuator R. Mayer, T. Lutz, E. Kraemer, University of Z. Zhao, Y. Cui, J. Li, J. Zheng, B. A. Sidorenko, A. Maslov, A. Budovsky, P. Academy of Sciences, Moscow, Russia; S. Y. Cui, Z. Zhao, J. Zheng, J. Li, B. Stuttgart, Stuttgart, Germany Khoo, National University of Singapore, Polivanov, O. Vishnyakov, Russian Academy Leonov, University of Notre Dame, Notre Dame, Khoo, National University of Singapore, Singapore, Singapore of Sciences, Novosibirsk, Russia IN; V. Soudakov, TsAGI, Zhukovsky, Russia Singapore, Singapore Tuesday, 10 January 2017 179-APA-18 Unsteady Aerodynamics II Dallas 2 Chaired by: M. GHOREYSHI, United States Air Force Academy and K. KONTIS, University of Glasgow 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs AIAA-2017-0716 AIAA-2017-0717 AIAA-2017-0718 AIAA-2017-0719 AIAA-2017-0720 Computational Study of Lift Effect of a Pitch-Oscillating Canard Motion induced unsteady Reduced Order Modeling of a Flow Effect of Reduced Frequency on Frequency Responses of Pitching on Lift Enhancement and Tip Vortex aerodynamic loads with Past a Cylinder using Sparse Coding Dynamic Stall of a Pitching Airfoil in Airfoils at Low Reynolds Numbers Mitigation development of vortical flow R. Deshmukh, J. McNamara, Ohio State a Turbulent Wake A. Rezaei, H. Taha, University of California, J. Vasile, Army Research Laboratory, S. Wiggen, C. Klein, U. Henne, R. Konrath, University, Columbus, OH A. Gandhi, Arizona State University, Tempe, AZ; Irvine, Irvine, CA Aberdeen Proving Ground, MD W. Sachs, B. Wrede, German Aerospace B. Merrill, Raytheon Company, Tucson, AZ; Y. Center (DLR), Göttingen, Germany; et al. Peet, Arizona State University, Tempe, AZ Tuesday, 10 January 2017 180-APA-19 Aerodynamic Design: Design Tools and Propeller Integration Dallas 4 Chaired by: E. FELTROP, Textron Aviation and O. KHAN, Tuskegee Univ 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2017-0721 AIAA-2017-0722 AIAA-2017-0723 AIAA-2017-0724 AIAA-2017-0725 AIAA-2017-0726 Aerodynamic Design, Analysis and Research on Airfoil Design Space Comparison of Experimental Data Aerodynamic Optimization of a Golf Theoretical Critical Height for Convergence Acceleration of Fluid Testing of Propellers for Small and the Application of Niching with Computations for a Propeller- Driver Using Computational Fluid Boundary Layer Transition on Airfoil Dynamics Solvers Using a Reduced- Unmanned Aerial Vehicles Techniques in Airfoil Design Driven Airplane Dynamics Leading Edges Order-Model W. Anemaat, M. Schuurman, W. Liu, A. C. Gao, Z. Gao, S. Li, Northwestern K. Biber, Bartin University, Bartin, Turkey K. Hanquist, University of Michigan, Ann R. Robison, E. Loth, University of Virginia, R. Djeddi, A. Kaminsky, K. Ekici, University Karwas, Design, Analysis and Research Polytechnical University, Xi’an, China Arbor, Ann Arbor, MI; K. Neitzel, Smart Charlottesville, Charlottesville, VA of Tennessee, Knoxville, Knoxville, TN Corporation, Lawrence, KS Blue Innovations, Wichita, KS Tuesday, 10 January 2017 181-APA-20 Propeller/Rotorcraft/Wind Turbine Aerodynamics II: Low-Rn Propellers Dallas 5 Chaired by: D. HUNSAKER, Utah State University and R. RAMAMURTI, Naval Research Laboratory 1400 hrs 1430 hrs AIAA-2017-0727 AIAA-2017-0728 An Experimental Study on the Navier-Stokes Equations based Flow Transient Ice Accretion Process over Simulations of Low Reynolds Number a Rotating UAV Propeller Propeller for Unmanned Aerial Vehicle L. Li, Z. Ning, H. Hu, Iowa State University, J. Liu, S. Luo, Central South University, Ames, IA Changsha, China Tuesday, 10 January 2017 182-ASC-3 Smart and Multifunctional Materials Palomino 3 Chaired by: R. JHA, Mississippi State University and A. CHATTOPADHYAY, Arizona State University

100 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs AIAA-2017-0729 AIAA-2017-0730 AIAA-2017-0731 AIAA-2017-0732 AIAA-2017-0733 Design of a Piezoelectric Energy On the nonlinear dynamics and A Finite Strain Constitutive Model Experimentation and Computational Test rig development Harvester by Using Cylinder as a performance of hybrid piezoelectric- for Martensitic Transformation in Analysis of an SMA-Based Slat-Cove and characterization of Bluff Body inductive energy harvesters subjected Shape Memory Alloys Based on Filler For Noise Reduction in a High magnetorheological elastomers A. Avsar, M. Sahin, Middle East Technical to vortex-induced vibrations Logarithmic Strain Lift Wing A. Martins, University of Victoria, Victoria, University, Ankara, Turkey U. Javed, H. Abdelmoula, A. Abdelkeﬁ, New L. Xu, T. Baxevanis, D. Lagoudas, Texas W. Scholten, R. Patterson, Texas A&M Canada; A. Fereidooni, National Research Mexico State University, Las Cruces, NM A&M University, College Station, TX University, College Station, TX; Q. Council Canada, Ottawa, Canada; A. Chapelon, ENISE, Saint-Etienne, France; D. Suleman, University of Victoria, Victoria, Hartl, T. Strganac, Texas A&M University, Canada; V. Wickramasinghe, National College Station, TX; T. Turner, NASA Research Council Canada, Ottawa, Canada Langley Research Center, Hampton, VA Tuesday, 10 January 2017 183-F360-4 Geoengineering to Mitigate Climate Change – Is there a Role for Aerospace? Texas C 1400 - 1600 hrs Moderator: Marty Bradley, Technical Fellow, The Boeing Company

Panelists: Martin Bunzi Will Burns Tracy Hester Doug MacMartin Professor, Department of Philosophy Co-Director, Forum for Climate Engineering Assessment Professor Research Professor, Computing + Mathematical Sciences at Rutgers University American University University of Houston Law Center California Institute of Technology/Mechanical and Aerospace Engineering at Cornell University Tuesday, 10 January 2017 184-FD-23 CFD Methods on Unstructured Meshes Austin 1 Chaired by: R. SINGH, General Electric Global Research and S. TU, Jackson State University 1400 hrs 1430 hrs 1500 hrs 1530 hrs AIAA-2017-0734 AIAA-2017-0735 AIAA-2017-0736 AIAA-2017-0737 Reconstruction Map Stability A Posteriori Stability Analysis and Output Error Correction and Mesh A Preconditioned Flux Reconstruction/ Analysis for Cell Centered Finite Improvement for Finite Volume Adaptation for Unstructured Mesh Correction Procedure via Volume Methods on Unstructured Methods on Unstructured Meshes Finite Volume Method Reconstruction Formulation for Meshes R. Zangeneh, C. Ollivier Gooch, University M. Sharbatdar, C. Ollivier Gooch, University Unsteady Low Mach Number Flows on R. Zangeneh, C. Ollivier Gooch, University of British Columbia, Vancouver, Canada of British Columbia, Vancouver, Canada Dynamic Unstructured Meshes of British Columbia, Vancouver, Canada L. Wang, M. Yu, University of Maryland, Baltimore County, Baltimore, MD Tuesday, 10 January 2017 185-FD-24 High-Order Methods II Texas 2 Chaired by: K. FIDKOWSKI, University of Michigan and G. MAY, RWTH Aachen 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs AIAA-2017-0738 AIAA-2017-0739 AIAA-2017-0740 AIAA-2017-0741 AIAA-2017-0742 Third-Order Inviscid and Second- High-order implicit discontinuous A Study of Efficiency of Implicit High- A Hybrid Adjoint/Error Transport Efficient and affordable high order, Order Hyperbolic Navier-Stokes Galerkin scheme for unsteady Order Spectral Difference Method Approach to Error Estimation, high fidelity Large Eddy Simulations Solvers for Three-Dimensional turbulent flows Implementations Adaptation, and Higher-Order Solutions for industrial level applications Unsteady Inviscid and Viscous Flows H. Asada, S. Kawai, Tohoku University, E. Jourdan, F. Moreira, C. Breviglieri, for Computational Fluid Dynamics Y. Lu, A. Demargne, Cambridge Flow Y. Liu, H. Nishikawa, National Institute of Sendai, Japan Technological Institute of Aeronautics (ITA), W. Tyson, C. Roy, Virginia Polytechnic Institute Solutions, Ltd., Cambridge, United Aerospace, Hampton, VA São José dos Campos, Brazil; J. Azevedo, and State University, Blacksburg, VA Kingdom; K. Liu, BoXeR Solutions KK, Aeronautics and Space Institute (IAE), São José Kobe, Japan; W. Dawes, Cambridge dos Campos, Brazil; Z. Wang, University of University, Cambridge, United Kingdom

101 Kansas, Lawrence, Lawrence, KS Tuesday, 10 January 2017 186-FD-25 High-Speed Flows II Texas 3 Chaired by: S. LAURENCE, University of Maryland, College Park and E. MARINEAU, AEDC/TSTT USAF White Oak 1400 hrs 1430 hrs 1500 hrs 1530 hrs AIAA-2017-0743 AIAA-2017-0744 AIAA-2017-0745 AIAA-2017-0746 Transient Startup Simulations for a Moving Grid Methods in High Thermo-Acoustic Effects in High- Numerical Simulation of Supersonic Large Mach 6 Quiet Ludwieg Tube Enthalpy Shock Simulations for Speed Compressible Transitional and Flow over Segmental-Conical Bodies J. Jewell, Air Force Research Laboratory, Electric Arc Shock Tube (EAST) Turbulent Boundary Layers N. Palchekovskaya, I. Egorov, TsAGI, Wright-Patterson AFB, OH; C. Huffman, T. Experiments at NASA Ames K. Ritos, I. Kokkinakis, D. Drikakis, University Zhukovsky, Russia Juliano, University of Notre Dame, Notre D. Chandel, G. Candler, University of of Strathclyde, Glasgow, United Kingdom; S. Dame, IN Minnesota, Minneapolis, Minneapolis, MN Spottswood, Air Force Research Laboratory, Wright Patterson AFB, OH Tuesday, 10 January 2017 187-FD-26 RANS/LES Modeling of Jet Flows Texas 4 Chaired by: B. SMITH, Lockheed Martin Aeronautics and M. MANKBADI, NASA Glenn Research Center 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs AIAA-2017-0747 AIAA-2017-0748 AIAA-2017-0749 AIAA-2017-0750 AIAA-2017-0751 OpenFOAM based numerical Adaptive Detached Eddy Simulation Modeling Open Jet Airfoil Numerical Investigation of Airfoil Simulations of impinging jets with a simulation study of an underexpanded of Jet in Cross Flow Interaction Using RANS and Hybrid Placement and Modiﬁcation in Open range of conﬁguration supersonic jet. Z. Yin, P. Durbin, Iowa State University, LES-RANS Jet Experiments D. Singh, J. Doom, South Dakota State B. Zang, V. U S, T. New, Nanyang Technological Ames, IA A. Sheikh-AlShabab, P. Tucker, University of A. Sheikh-AlShabab, P. Tucker, University of University, Brookings, SD University, Singapore, Singapore Cambridge, Cambridge, United Kingdom Cambridge, Cambridge, United Kingdom Tuesday, 10 January 2017 188-FD-27 Novel CFD Methods Texas 5 Chaired by: Z. WANG, University of Kansas and G. JACOBS, San Diego State Univ 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs AIAA-2017-0752 AIAA-2017-0753 AIAA-2017-0754 AIAA-2017-0755 AIAA-2017-0756 A Fast Panel Code for Complex Explicit Large Time Stepping with Line Box Relaxation Method Development of Machine Learning A convergent and accuracy Actuator Disk Flows A Second-Order Exponential Time and Multigrid Acceleration for Models for Turbulent Wall Pressure preserving limiter for the FR/CPR S. Gamme, G. de Oliveira, D. Ragni, Integrator Scheme for Unsteady Simulation of 2-D Jet Flow in a Fluctuations method Delft University of Technology, Delft, The and Steady Flows Channel J. Ling, Sandia National Laboratories, Y. Li, Z. Wang, University of Kansas, Netherlands; F. Lau, Technical University of S. Li, Beijing Computational Science J. Tang, Y. Yang, C. Liu, University of Texas, Livermore, CA; M. Barone, W. Davis, Lawrence, Lawrence, KS Lisbon, Lisbon, Portugal Research Center, Beijing, China; Z. Wang, Arlington, Arlington, TX Sandia National Laboratories, Albuquerque, University of Kansas, Lawrence, Lawrence, NM; K. Chowdhary, Sandia National KS; L. Ju, University of South Carolina, Laboratories, Livermore, CA; J. Fike, Sandia Columbia, Columbia, SC; L. Luo, Old National Laboratories, Albuquerque, NM Dominion University, Norfolk, VA Tuesday, 10 January 2017 189-FD-28 Shock Boundary Layer Interactions I Texas 1 Chaired by: J. LITTLE, The University of Arizona and J. POGGIE, Purdue University- Sch of Aero and Astro 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs AIAA-2017-0757 AIAA-2017-0758 AIAA-2017-0759 AIAA-2017-0760 AIAA-2017-0762 Role of Boundary-Layer on Effect of Test Article Geometry Three-Dimensional Flow Features Experimental Investigation of a Gortler-like vortices in the LES Data Unsteadiness on a Mach 2 Swept-Ramp on Shock Wave-Boundary Layer of Swept Impinging Oblique Shock/ Cylinder-Induced Transitional Shock of a Mach 7 STBLI Shock/Boundary-Layer Interaction Interactions in Rectangular Intakes Boundary-Layer Interactions Wave-Boundary Layer Interaction C. Helm, M. Martin, University of Using 50 kHz PIV I. Grossman, P. Bruce, Imperial College J. Threadgill, I. Stab, A. Doehrmann, E. Lash, C. Combs, P. Kreth, J. Schmisseur, Maryland, College Park, College Park, MD L. Vanstone, M. Saleem, S. Seckin, N. London, London, United Kingdom J. Little, University of Arizona, Tucson, University of Tennessee, Tullahoma,

102 Clemens, University of Texas, Austin, Austin, TX Tucson, AZ Tullahoma, TN Tuesday, 10 January 2017 190-FD-29 Stability and Transition over Cones Texas 6 Chaired by: M. TUFTS, AFRL/RQHF and M. BORG, Air Force Research Laboratory 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2017-0763 AIAA-2017-0764 AIAA-2017-0765 AIAA-2017-0766 AIAA-2017-0767 AIAA-2017-0768 Nonlinear Saturation versus Analysis of Windward Side Fundamental Resonance Breakdown Sharp Cone Boundary-Layer Preliminary Study of the Effect of PSE and Spatial Biglobal Instability Nonlinear Detuning: Quantification Hypersonic Boundary Layer for a Flared Cone at Mach 6 Transition and Stability at Mach 14 Environmental Disturbances on Analysis of Reduced Scale and Flight on a Mach 6 Flared Cone Transition on Blunted Cones at C. Hader, H. Fasel, University of Arizona, E. Marineau, G. Morraru, Arnold Hypersonic Crossflow Instability on HIFiRE-5 Geometry J. Kuehl, Baylor University, Waco, TX Angle of Attack Tucson, Tucson, AZ Engineering Development Complex, Silver the HIFiRE-5 Elliptic Cone T. Kocian, A. Moyes, D. Mullen, H. Reed, M. Tufts, R. Kimmel, Air Force Research Spring, MD; D. Daniel, Arnold Engineering I. Neel, A. Leidy, R. Bowersox, Texas A&M Texas A&M University, College Station, TX Laboratory, Wright-Patterson AFB, OH Development Complex, Arnold AFB, TN University, College Station, TX Tuesday, 10 January 2017 191-FD-30 Experimental Aerodynamics Grapevine C Chaired by: A. AHMED, Auburn University and M. OL, US Air Force Reseach Laboratory 1400 hrs 1430 hrs 1500 hrs 1530 hrs AIAA-2017-0769 AIAA-2017-0770 AIAA-2017-0771 AIAA-2017-0772 Effect of Velocity Ratio on the Flow Effects of Roughness on the Experimental Study of NACA Aerodynamic Characteristics of Field of a Spatially Oscillating Jet in Performance of Fluidic Oscillators Symmetric and Camber Airfoils at Lifting Body HYFLEX under High- Crossflow M. Hossain, R. Prenter, L. Agricola, R. Low Reynolds Numbers Temperature Real-Gas Conditio F. Ostermann, R. Woszidlo, C. Nayeri, C. Lundgreen, A. Ameri, J. Gregory, Ohio State E. Garcia, V. Durgesh, H. Johari, California H. Tanno, T. Komuro, K. Sato, K. Itoh, Paschereit, Technical University of Berlin, University, Columbus, OH; et al. State University, Northridge, CA Japan Aerospace Exploration Agency Berlin, Germany (JAXA), Kakuda, Japan; S. Shimazaki, M. Matsumoto, Japan Aerospace Exploration Agency (JAXA), Tsukuba, Japan; et al. Tuesday, 10 January 2017 192-GT-5 Design, Calibration and Performance of Ground Test Facilities Ft. Worth 6 Chaired by: T. WAYMAN, Gulfstream Aerospace Corporation and K. BUTLER, AEDC - Arnold Engineering Development Complex 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs AIAA-2017-0773 AIAA-2017-0774 AIAA-2017-0775 Oral Presentation AIAA-2017-0776 Assessing Wall Interference Effects Balance Evaluation and Installation- Development of a Model Double- Photogrammetric Measurement Developing a Semi-Span Wall on a Medium-Sized Rotor in the Checks using Dead Weight Roll- and Roll Mounting System for a Large Methods for the Static-aeroelasticity Interference Correction Capability National Full-Scale Aerodynamics Pitch-Polars. Transonic Wind Tunnel Deformation of a Flying Wing in the National Full-Scale Complex A. Burger, P. Bidgood, Council for Scientific D. Belter, A. Krynytzky, D. Holler, R. A. Shi, L. Jiang, B. Wan, Northwestern Aerodynamics Complex 40- by P. Goulding, C. Nykamp, B. Bartow, and Industrial Research, Pretoria, South Parrish, M. Fleming, K. Hanke, The Boeing Polytechnical University, Xi’an, China 80-foot Wind Tunnel National Full-Scale Aerodynamics Complex, Africa Company, Tukwila, WA; et al. P. Goulding, A. Tupis, National Full-Scale Moffett Field, CA Aerodynamics Complex, Moffett Field, CA Tuesday, 10 January 2017 193-GTE-4 Combustion Technologies, Emissions I San Antonio 4 Chaired by: S. DRENNAN, Convergent Science, Inc. 1400 hrs 1430 hrs 1500 hrs AIAA-2017-0777 AIAA-2017-0778 AIAA-2017-0779 Development and Testing of a Experimental investigation of the Combustion dynamic characteristics Variable Geometry Diffuser in an Effect of Air Diffusive injection on identification in a 9-point LDI Ultra-Compact Combustor premixing swirl flames combustor under choked outlet B. Bohan, M. Polanka, Air Force Institute of N. Syred, F. Hatem, A. Valera-Medina, P. boundary conditions Technology, Wright-Patterson AFB, OH; L. Goss, Bowen, Cardiff University, Cardiff, United Z. He, C. Chang, NASA Glenn Research Innovative Scientific Solutions, Inc., Dayton, OH Kingdom Center, Cleveland, OH Tuesday, 10 January 2017

103 194-GTE-5 Numerical Tools I Grapevine 3 Chaired by: E. KHALIL, Cairo University 1400 hrs 1430 hrs 1500 hrs 1530 hrs AIAA-2017-0780 AIAA-2017-0781 AIAA-2017-0782 AIAA-2017-0783 Modeling Thermoacoustic Rumble Effects of Liner Cooling Momentum A Critical Examination of a Stall Flutter Simulation of a Transonic and Screech in Bluff-body-stabilized on Combustor Performance Correlation-Based Transition Model Axial Compressor Stage Using a Fully Combustors A. Briones, S. Stouffer, University of for Low Pressure Turbines Coupled Fluid-Structure Interaction E. Gonzalez, Combustion Science & Dayton, Dayton, OH; K. Vogiatzis, Engility D. Lefas, J. Cui, P. Tucker, University of J. Gan, University of Miami, Coral Gables, Engineering, Inc., Columbia, MD Corporation, Chantilly, VA; B. Rankin, Cambridge, Cambridge, United Kingdom FL; H. Im, Honeywell International, Inc., Air Force Research Laboratory, Wright- Torrance, CA; G. Zha, University of Miami, Coral Patterson AFB, OH Gables, FL Tuesday, 10 January 2017 195-HSABP-4/PGC-3 Pressure Gain Combustion - Rotating Detonation Engines I Ft. Worth 3 Chaired by: D. FERGUSON, National Energy Technology Laboratory and V. TANGIRALA, General Electric 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs AIAA-2017-0784 AIAA-2017-0785 AIAA-2017-0786 AIAA-2017-0787 AIAA-2017-0788 Recent Developments in the Development of a Lab-Scale Further Experimentation of a Effectiveness of Detonation Engines Experimental Characterization of Research on Rotating-Detonation- Experimental Testing Platform for Premixed Rotating Detonation Engine for Power Production Centerbodiless RDE Emissions Wave Engines Rotating Detonation Engine Inlets I. Andrus, Air Force Research Laboratory, R. Bello, F. Lu, University of Texas, W. Stoddard, V. Anand, R. Driscoll, B. Dolan, K. Kailasanath, Naval Research Laboratory, C. Bedick, National Energy Technology Wright-Patterson AFB, OH; M. Polanka, Air Arlington, Arlington, TX A. St. George, R. Villalva Gomez, University of Washington, D.C. Laboratory, Morgantown, WV; A. Sisler, Force Institute of Technology, Wright-Patterson Cincinnati, Cincinnati, OH; et al. West Virginia University, Morgantown, WV; AFB, OH; F. Schauer, Air Force Research D. Ferguson, P. Strakey, National Energy Laboratory, Wright-Patterson AFB, OH; J. Technology Laboratory, Morgantown, WV Hoke, Innovative Scientific Solutions, Inc., Centerville, OH Tuesday, 10 January 2017 196-IS-3 Learning, Reasoning, and Data Driven Systems Ft. Worth 1 Chaired by: A. YUCEL, Lockheed Martin Aeronautics 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2017-0789 AIAA-2017-0790 AIAA-2017-0791 AIAA-2017-0792 AIAA-2017-0793 AIAA-2017-0794 Utilizing Energy Metrics and Density Estimation of Moving Hierarchically Structured Controllers Helicopter Engine State Estimation Kernel Function Evaluation For Extracting and Applying Knowledge Clustering Techniques to Identify Targets on a Road Network for Safe UAV Reinforcement via Cockpit Audio Analysis Gaussian Process Wind Regression with Adaptive Knowledge-Driven Anomalous General Aviation Y. Cao, University of Texas, San Antonio, San Learning Applications A. Vaidya, S. Shin, I. Hwang, Purdue E. Frew, A. Mills, S. Sheahan, University of Optimization to Architect an Earth Operations Antonio, TX; D. Casbeer, Air Force Research T. Mannucci, E. Van Kampen, C. de Visser, University, West Lafayette, IN Colorado, Boulder, Boulder, CO Observing Satellite System T. Puranik, H. Jimenez, D. Mavris, Georgia Laboratory, Wright-Patterson AFB, OH; N. Q. Chu, Delft University of Technology, N. Hitomi, H. Bang, D. Selva, Cornell Institute of Technology, Atlanta, GA Ahmed, University of Colorado, Boulder, Delft, The Netherlands University, Ithaca, NY Boulder, CO; D. Kingston, Air Force Research Laboratory, Wright-Patterson AFB, OH Tuesday, 10 January 2017 197-MAT-5 Nanostructured Materials Palomino 2 Chaired by: B. WARDLE, Massachusettes Institute of Technology and S. ROY, The University of Alabama 1400 hrs 1430 hrs 1500 hrs 1530 hrs AIAA-2017-0795 AIAA-2017-0796 AIAA-2017-0797 AIAA-2017-0798 Numerical and Experimental Effect of Templating Graphitization Finite element modeling of Experimental and Simulation Investigation of the Piezoresistive on Electrical Conductivity of nanoindentation for FG nanomaterials Studies on Magnetic Nanoparticle Behavior of Hybrid Carbon Nanotube Electrospun Carbon nanofiber accounting for surface effects using Assembly for Scalable Polymer Sheet - Graphene Nanocomposites J. Cai, M. Naraghi, Texas A&M University, user subroutine Nanocomposite Fabrication A. Gbaguidi, S. Namilae, D. Kim, Embry-Riddle College station, TX H. Abdelmoula, M. Shaat, A. Abdelkefi, New M. Spencer, D. Gao, N. Yamamoto, Aeronautical University, Daytona Beach, FL Mexico State University, Las Cruces, NM Pennsylvania State University, University Park, PA

104 Tuesday, 10 January 2017 198-MDO-6 Aero-Structures Optimization Mustang 1 Chaired by: J. MARTINS, University of Michigan and B. STANFORD, NASA Langley Research Center 1400 hrs 1430 hrs 1500 hrs 1530 hrs AIAA-2017-0799 AIAA-2017-0800 AIAA-2017-0801 AIAA-2017-0802 Coupled Multiphysics Analysis Integrated Aircraft Parametric CFD-based Aeroelastic Adjoint Toward Wing Aerostructural for Design of Advanced Exhaust Structural & Outer Mold Line Sensitivities for Flight Vehicle Weight Optimization Using Simultaneous Systems Geometry Modeling Software Minimization Using Sizing and Shape Analysis and Design Strategy P. Urbanczyk, J. Alonso, Stanford N. Love, R. Kapania, Virginia Polytechnic Design Variables A. Elham, Delft University of Technology, University, Stanford, CA; N. Nigam, X. Institute and State University, Blacksburg, Z. Zhang, ZONA Technology, Inc., Scottsdale, Delft, The Netherlands; M. Van Tooren, Qi, P. Chen, Intelligent Automation, Inc., VA; D. Allison, Optimal Flight Sciences, LLC, AZ; Q. Wang, Massachusetts Institute of University of South Carolina, Columbia, Rockville, MD Wright-Patterson AFB, OH Technology, Cambridge, MA; P. Chen, S. Yang, Columbia, SC Z. Wang, ZONA Technology, Inc., Scottsdale, AZ Tuesday, 10 January 2017 199-MST-3 Modeling and Simulation of Air Traffic Management I San Antonio 3 Chaired by: J. SCHROEDER, Federal Aviation Administration and P. ZAAL, NASA Ames Research Center 1400 hrs 1430 hrs 1500 hrs 1530 hrs AIAA-2017-0803 AIAA-2017-0804 AIAA-2017-0805 AIAA-2017-0806 Evaluation of Airport Capacity a EUROCONTROL tower simulator to ATC Procedures Modeling for Human-in-the-Loop Simulation of Optimization Measures validate SESAR Routing, guidance Capacity Estimation of Japanese Trajectory Based Operation Concept C. Schinwald, Munich Aerospace e.V., and Airport safety nets concepts Airspace for Remotely Piloted Aircraft System Munich, Germany; K. Plötner, Bauhaus M. Ellejmi, M. Bonnier, R. Lane, S. K. Kageyama, Electronic Navigation Integration Luftfahrt e.V., Ottobrunn, Germany; M. Dubuisson, EUROCONTROL, Brussels, Research Institute, Tokyo, Japan J. Kang, S. Kang, H. Oh, K. Choi, H. Lee, Hornung, Technical University of Munich, Belgium Inha University, Incheon, South Korea; H. Munich, Germany Jung, Korea Aerospace University, Goyang, South Korea; et al. Tuesday, 10 January 2017 200-MST-4 Modeling and Simulation of Uninhabited Aerial Vehicles II San Antonio 2 Chaired by: R. RUFF and D. KEATING, The Charles Stark Draper Laboratory, Inc. 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs AIAA-2017-0807 AIAA-2017-0808 AIAA-2017-0809 AIAA-2017-0810 AIAA-2017-0811 New Methodology for Longitudinal Sensitivity of Unmanned Aerial Model-based Implementation of Integration and Evaluation of Dynamic Modeling and Hardware- Flight Dynamics Modelling of Vehicle Model-Aided Navigation an Onboard STANAG 4586 Vehicle UAS Systems: Building a Virtual In-Loop Simulation for a Tail-Sitter the UAS-S4 Ehecatl towards its S. D’Urso, J. Gross, West Virginia Specific Module for an Air Vehicle Engineering Facility Unmanned Aerial Vehicle in Hovering Aerodynamics Estimation Modelling University, Morgantown, WV M. Hochstrasser, C. Krause, V. Schneider, F. N. Cameron, C. Patchett, K. Vikhorev, Flight M. Kuitche, M. Segui, R. Botez, G. Ghazi, Holzapfel, Technical University of Munich, K. Lai, L. Wong, D. Bowman, Virtual J. Sun, B. Li, L. Shen, Hong Kong Polytechnic University of Québec, Montréal, Canada Munich, Germany Engineering Centre, Warrington, United University, Hong Kong, Hong Kong; C. Chen, Kingdom Da-Yeh University, Changhua, Taiwan; C. Wen, Hong Kong Polytechnic University, Hong Kong, Hong Kong Tuesday, 10 January 2017 201-MVC-4 Computational Environments and the NASA CFD Vision 2030 Goals Grapevine D Chaired by: A. LOFTHOUSE, US Air Force Academy and E. DUQUE, Intelligent Light 1400 hrs 1430 hrs 1500 hrs 1530 hrs AIAA-2017-0812 AIAA-2017-0813 AIAA-2017-0814 Panel TM Trinity: DataManagement Scheme The HPCMP CREATE -AV Kestrel A Web-Based Database Approach to Panelists will discuss the goals of the NASA CFD Vision 2030 report as they pertain to Computational Environments. Computational Environments is the advancement in the and Performance Computational Environment and its CFD Post-Processing interaction, automation, and computational speed/efficiency of and between pre-processing, computational simulation execution and monitoring, and post-processing as well as D. Morton, Los Alamos National Laboratory, Relation to NASA’s CFD Vision 2030 G. Pullan, University of Cambridge, between computational simulations across multiple disciplines that increases fidelity and capability. In addition, the advancement in the management and comprehension of trends Los Alamos, NM D. McDaniel, T. Tuckey, S. Morton, CREATE Cambridge, United Kingdom across multiple solutions, summary of results, discovery of relationships, and management of large volumes of data involved with optimization is included. AV Team, Eglin AFB, FL Moderated by: Andrew Lofthouse, U.S. Air Force and Earl Duque, Intelligent Light

Panelists: 105 David Morton David McDaniel Jack Harris Ed Hoffman Los Alamos DoD HPCMP CREATE Engility Sandia

Tuesday, 10 January 2017 202-NDA-4 Special Session: Non-Deterministic Approaches for Integrated Computational Materials Engineering Mustang 2 Chaired by: B. BICHON, Southwest Research Institute and A. CHAUDHURI, Massachusetts Institute of Technology 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2017-0815 AIAA-2017-0816 AIAA-2017-0817 AIAA-2017-0818 AIAA-2017-0819 AIAA-2017-0820 Uncertainty Quantification of Non-Intrusive Stochastic Modeling Decomposed Multilevel Evaluation of a Simple UQ Approach Influence of Textile architecture on Micromechanical Finite Element Microstructural Properties due to to Account for Microstructure Optimization of a Nano-Enhanced to Compensate for Sparse Stress- Cure induced Stresses and post-cure Modeling of Fiber Epoxy Composites Experimental Variations Variability Sandwich Composite Plate under Strain Curve Data in Solid Mechanics Stiffness and Strength Containing Void Defects Part 1: P. Acar, V. Sundararaghavan, University of S. Niezgoda, M. Yuan, N. Galbincea, Ohio Epistemic Uncertainty Applications R. D’Mello, M. Maiaru, A. Waas, University Stiffness Analysis Michigan, Ann Arbor, Ann Arbor, MI State University, Columbus, OH; A. Salem, I. Dettwiller, M. Rais-Rohani, Mississippi V. Romero, J. Dampsey, B. Schroeder, J. of Washington, Seattle, Seattle, WA R. Spoonire, J. Goodsell, Purdue University, J. Shaffer, Materials Resources, LLC, State University, Mississippi State, MS Lewis, N. Breivik, G. Orient, Sandia National West Lafayette, IN Dayton, OH Laboratories, Albuquerque, NM; et al. Tuesday, 10 January 2017 203-PC-13 Combustion Dynamics I Dallas 7 Chaired by: A. STEINBERG, University of Toronto and R. ERICKSON 1400 hrs 1430 hrs 1500 hrs 1530 hrs AIAA-2017-0821 AIAA-2017-0822 AIAA-2017-0823 AIAA-2017-0824 Investigation of Self-Excited Driving Mechanisms of Liquid- Flame Quenching Dynamics of High Analysis of intermittent Combustion Instabilities Generated Propellant Rocket Longitudinal Velocity Flames in Rectangular Cross- thermoacoustic oscillations in an by Reactions held by a 2D Combustion Instability section Channels aeronautical gas turbine combustor Flameholder fed with Non-Uniform T. Nguyen, P. Popov, W. Sirignano, A. Mahuthannan, D. Lacoste, King Abdullah J. Cirtwill, S. Kheirkhah, P. Saini, Fuel Distributions University of California, Irvine, Irvine, CA University of Science and Technology, Thuwal, University of Toronto, Ontario, Canada; C. Brown, U. Mondragon, V. McDonell, Saudi Arabia; J. Damazo, E. Kwon, The Boeing K. Venkatesan, General Electric Company, Energy Research Consultants, Laguna Company, Seattle, WA; W. Roberts, King Niskayuna, NY; A. Steinberg, University of Hills, CA; B. Emerson, T. Lieuwen, Georgia Abdullah University of Science and Technology, Toronto, Ontario, Canada Institute of Technology, Atlanta, GA Thuwal, Saudi Arabia Tuesday, 10 January 2017 204-PC-14 Spray and Droplet Combustion Grapevine 4 Chaired by: J. GORE, Purdue University and T. NGUYEN, Aerojet Rocketdyne 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs AIAA-2017-0825 AIAA-2017-0826 AIAA-2017-0827 AIAA-2017-0828 AIAA-2017-0829 Exploration of Two-Phase Flow Hot Surface Ignition Temperatures Liquid Fuel Injection Strategy to Spray Measurements at Elevated Forced ignition of dispersions of Structures in Aerated-Liquid Jets of Hydrocarbon Fuels Reduce Sensitivity to Liquid Physical Pressures and Temperatures Using liquid fuel in turbulent air flow Using Beryllium Nozzles and X-Ray V. Goyal, A. Benhidjeb-Carayon, Purdue Properties Phase Doppler Anemometry P. de Oliveira, E. Mastorakos, University of Fluorescence Techniques University, West Lafayette, IN; R. C. Brown, B. Hickey, V. McDonell, Energy A. Bokhart, D. Shin, R. Gejji, P. Sojka, J. Cambridge, Cambridge, United Kingdom K. Lin, Taitech, Inc., Beavercreek, OH; A. Simmons, Georgia Institute of Technology, Research Consultants, Laguna Hills, CA; Gore, R. Lucht, Purdue University, West Kastengren, Argonne National Laboratory, Atlanta, GA; S. Meyer, J. Gore, Purdue E. Baldwin, D. Schmidt, University of Lafayette, IN; et al.

106 Argonne, IL; C. Carter, J. Donbar, Air Force University, West Lafayette, IN Massachusetts, Amherst, Amherst, MA Research Laboratory, Wright-Patterson AFB, OH Tuesday, 10 January 2017 205-PC-15 Solid Rockets San Antonio 6 Chaired by: M. COIL, Orbital Technologies Corporation and A. GNANASKANDAN 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs Oral Presentation AIAA-2017-0830 AIAA-2017-0831 AIAA-2017-0832 AIAA-2017-0833 Invited Review: Nanoenergetics: Temperature Sensitivity of AP/HTPB- The effects of AP particle size and Pulsed Microwave-Plasma Coupling Study of the Combustion of Pure Bio- Challenges and Future Directions Based Rocket Propellants Using a New concentration on ap/htpb composite to Composite Solid Propellants Derived Fuels and Bio-Derived Fuels R. Yetter, Pennsylvania State University, High-Pressure Strand Burner propellant burning rates S. Barkley, K. Zhu, T. Sippel, J. Michael, with Additives in Hybrid Propellant University Park, PA C. Dillier, A. Demko, J. Stahl, Texas A&M G. Morrow, E. Petersen, Texas A&M Iowa State University, Ames, IA Rocket Engine University, College Station, TX; D. Reid, Helicon University, College Station, TX V. Naoumov, N. Al Masoud, K. Sherman, Chemical Company, Orlando, FL; E. Petersen, M. Doolittle, M. Ziegler, D. Thorne, Central Texas A&M University, College Station, TX Connecticut State University, New Britain, CT Tuesday, 10 January 2017 206-PC-16 Combustion Chemistry San Antonio 5 Chaired by: W. SUN, Georgia Institute of Technology and Y. IKEDA, Imagineering, Inc. 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2017-0834 AIAA-2017-0835 AIAA-2017-0836 AIAA-2017-0837 AIAA-2017-0838 AIAA-2017-0839 A Uniﬁed Reduction of Elementary Automated Generation of Chemical Using Global Pathway Selection Consistent Syngas Chemical Kinetic Modeling of Cyclohexane Theoretical Analysis of the Explosion Kinetic Mechanisms for n-Alkanes, Mechanisms for Predicting Method to Understand Chemical Mechanism from Collaborative Data Oxidation Including PAH Formation Limits of Hydrogen-Oxygen System Highly-Branched Alkanes and Extinction Strain Rates with Kinetics Processing M. Abbasi, N. Slavinskaya, U. Riedel, A. Lidor, D. Weihs, E. Sher, Technion--Israel Cycloalkanes Applications in Flame Stabilization X. Gao, W. Sun, Georgia Institute of N. Slavinskaya, J. Starcke, M. Abbasi, A. German Aerospace Center (DLR), Stuttgart, Institute of Technology, Haifa, Israel J. Bellan, Jet Propulsion Laboratory, and Combustion Instabilitie Technology, Atlanta, GA Mirzayeva, U. Riedel, German Aerospace Germany California Institute of Technology, A. Grinberg Dana, S. Gudiyella, W. Green, Center (DLR), Stuttgart, Germany; Pasadena, CA; P. Kourdis, California S. Shanbhogue, D. Michaels, N. Chakroun, M. Frenklach, University of California, Institute of Technology, Pasadena, CA Massachusetts Institute of Technology, Berkeley, Berkeley, CA; et al. Cambridge, MA; et al. Tuesday, 10 January 2017 207-PDL-4 Diagnostics for Plasmas and Gases II Ft. Worth 4 Chaired by: K. XU, University of Alabama in Huntsville 1400 hrs 1500 hrs 1530 hrs Oral Presentation AIAA-2017-0840 AIAA-2017-0841 Thomson Scattering Techniques in High and Low Pressure Plasmas Atomic Oxygen Measurements Characterization of intermediate C. Limbach, Texas A&M University, College Station, TX in a Low Pressure DC and Pulsed reactions following femtosecond laser Discharge via Radar REMPI excitation in argon-nitrogen mixtures J. Sawyer, Y. Wu, Z. Zhang, University of Y. Zhang, M. Shneider, R. Miles, Princeton Tennessee, Knoxville, Knoxville, TN University, Princeton, NJ Tuesday, 10 January 2017 208-PDL-5 Computational Methods Ft. Worth 5 Chaired by: D. LEVIN, University of Illinois and M. PANESI, University of Illinois at Urbana Champaign 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs AIAA-2017-0842 AIAA-2017-0843 AIAA-2017-0844 AIAA-2017-0845 AIAA-2017-0846 Development of Particle-In-Cell Fully Implict Magneto- Effective Preconditioners A High-Order Finite-Volume Method Adjoint-based sensitivity analysis Solver for Numerical Simulation of hydrodynamics Simulations of for Maxwell’s equations on with Anisotropic AMR for Ideal MHD of ignition in a turbulent reactive Penning Discharge Coaxial Plasma Accelerators Unstructured Grids for Coupled Flows shear layer A. Dikalyuk, All-Russia Research Institute of V. Subramaniam, L. Raja, University of Plasma-EM Wave Modeling L. Freret, L. Ivan, University of Toronto, J. Capecelatro, University of Michigan, Ann Automatics, Moscow, Russia; S. Surzhikov, Texas, Austin, Austin, TX P. Panneer Chelvam, L. Raja, University of Toronto, Canada; H. De Sterck, Monash Arbor, Ann Arbor, MI; D. Bodony, J. Freund, Russian Academy of Sciences, Moscow, Texas, Austin, Austin, TX University, Melbourne, Australia; C. Groth, University of Illinois, Urbana-Champaign, Russia University of Toronto, Toronto, Canada Urbana, IL Tuesday, 10 January 2017 209-SATS-5 Small Satellites - Fusion Austin 6

107 Chaired by: J. STRAUB, North Dakota University 1400 hrs 1430 hrs 1500 hrs 1530 hrs AIAA-2017-0847 AIAA-2017-0848 AIAA-2017-0849 AIAA-2017-0850 Lunar Brightness Temperature and Expantion and Measurement of Spiral Ground Demonstration on the Testing and Evaluating Deployment Radiometer Design Folded Membrane by Small Satellite Autonomous Docking of Two 3U Profiles of the Canisterized Satellite S. Namdeo, K. Barad, SRM University, T. Miyashita, H. Yamakawa, Waseda CubeSats Using a Novel Permanent Dispenser (CSD) Chennai, India University, Tokyo, Japan; M. Natori, Japan Magnet Docking Mechanism S. Tullino, E. Swenson, Air Force Institute of Aerospace Exploration Agency (JAXA), J. Pei, NASA Langley Research Center, Technology, Wright-Patterson AFB, OH Kanagawa, Japan; N. Katsumata, Muroran Hampton, VA Institute of Technology, Tokyo, Japan Tuesday, 10 January 2017 210-SCS-3 Quantitative Determination of the Behavior of Deployable Structures Palomino 1 Chaired by: R. PAPPA, NASA Langley Research Center and J. FOOTDALE, Load Path, LLC 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs AIAA-2017-0851 AIAA-2017-0852 AIAA-2017-0853 AIAA-2017-0854 AIAA-2017-0855 An Evaluation of Structural Analysis Structural Analysis Methodology Large Area Membrane Apertures for Non-Axisymmetric Inflatable Inflatable Airlock: Seaming Methodologies for Space Deployable for Space Deployable Structures Space Applications, Fabrication and Pressure Structure (NAIPS) Full- Techniques of Highly Loaded Fabrics Structures using a High Performance Parallel Mechanical Testing Scale Pressure Test K. Shariff, NASA Johnson Space Center, M. Mobrem, L. Peterson, V. Cormarkovic, F. Nonlinear Finite Element Solver D. Beasley, Ball Aerospace & Technologies T. Jones, W. Doggett, J. Warren, J. Watson, Houston, TX Montazersadgh, Jet Propulsion Laboratory, L. Peterson, M. Mobrem, Jet Propulsion Corporation, Boulder, CO NASA Langley Research Center, Hampton, California Institute of Technology, Laboratory, California Institute of VA; K. Shariff, NASA Johnson Space Center, Pasadena, CA Technology, Pasadena, CA Houston, TX; A. Makino, NASA Ames Research Center, Moffett Field, CA; et al. Tuesday, 10 January 2017 211-SD-10 Computational Aero-, Servo-, Thermo- Elasticity Appaloosa 2 Chaired by: W. SCHNEIDER, Lockheed Martin Aeronautics and K. SPAK, Exponent 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2017-0856 AIAA-2017-0857 AIAA-2017-0858 AIAA-2017-0859 AIAA-2017-0860 AIAA-2017-0861 New Flutter Analysis Technique Optimal Actuation of Dielectric Identification and Analysis of Fundamental Understanding, Probabilistic Study of Integrally Update on UH-60A Rotor for Time-Domain Computational Membrane Wings using High- Aeroelastic Systems Accounting for the Prediction, and Validation of Bladed Rotor Blends using Performance and Loads Correlation Aeroelasticity Fidelity Fluid-Structure Modelling Combined Effects of Aerodynamic and Tiltrotor Dynamic Loads in Geometric Mistuning Models at High Advance Ratios using RCAS C. Pak, S. Lung, NASA Armstrong Flight R. Sanchez, R. Palacios, Imperial College Structural Nonlinearities Transition Flight Using RANS/FEA J. Beck, J. Brown, B. Runyon, O. Scott- G. Bowen-Davies, Science and Technology Research Center, Edwards, CA London, London, United Kingdom; T. M. Candon, R. Carrese, P. Marzocca, H. W. Staruk, A. Datta, University of Emuakpor, Air Force Research Laboratory, Corporation, Mountain View, CA; H. Economon, J. Alonso, Stanford University, Ogawa, RMIT University, Melbourne, Maryland, College Park, College Park, MD Wright-Patterson AFB, OH Yeo, Army Aviation and Missile Research Stanford, CA; T. Albring, N. Gauger, Australia; O. Levinski, Department of Defence, Development and Engineering Center, Technical University of Kaiserslautern, Melbourne, Australia; W. Silva, NASA Langley Moffett Field, CA Kaiserslautern, Germany Research Center, Hampton, VA; et al. Tuesday, 10 January 2017 212-SD-11 Structural Health Monitoring and Prognosis, Model Uncertainty Appaloosa 3 Chaired by: R. RUSOVICI, Florida Institute of Technology and T. BARTKOWICZ, Boeing Defense, Space & Security 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2017-0862 AIAA-2017-0863 AIAA-2017-0864 AIAA-2017-0865 AIAA-2017-0866 AIAA-2017-0867 Longitudinal Crack Damage The Development and use of Fighter Aircraft Buffet Load Accurate Strain Gage Limits Through Modal Modeling via Fiber Optic A Novel Computational Method Detection in a Beam Structure Using a Digital Twin Model for Tire Prediction using Nonlinear System Geometry Mistuning Modeling Strain Sensing for Applications in Modeling Wave propagation using Lamb Wave Based Finite Element Touchdown Health Monitoring Idenitication Algorithms D. Gillaugh, Air Force Research Laboratory, Structural Health Monitoring K-space method and Damage Simulation A. Zakrajsek, 96 TG/OL-ACL Landing Gear T. Minshall, Imperial College London, Wright-Patterson AFB, OH; A. Kaszynski, B. Martins, J. Kosmatka, University of Detection using Adjoint Method C. Park, Agency for Defense Development, Test Facility, Wright-Patterson AFB, OH; London, United Kingdom; M. Candon, R. Universal Technology Corporation, Dayton, California, San Diego, La Jolla, CA Q. Chang, Y. Liu, Arizona State University, Daejeon, South Korea; A. Palazotto, C. S. Mall, Air Force Institute of Technology, Carrese, P. Marzocca, RMIT University, OH; J. Brown, D. Johnston, Air Force Tempe, AZ Research Laboratory, Wright-Patterson 108 Hale, Air Force Institute of Technology, Wright-Patterson AFB, OH Melbourne, Australia; O. Levinski, Wright-Patterson AFB, OH Department of Defence, Melbourne, AFB, OH; J. Slater, Wright State University, Australia Wright-Patterson AFB, OH Tuesday, 10 January 2017 213-SD-12 Special Session: Aeroelastic Prediction IV Appaloosa 4 Chaired by: F. NITZSCHE, Carleton University and M. RIGHI, Zurich University of Applied Sciences 1400 hrs 1430 hrs 1500 hrs 1530 hrs AIAA-2017-0868 AIAA-2017-0869 AIAA-2017-0870 AIAA-2017-0871 Finite Volume Based Fluid-Structure Motion Magnication For Quantifying Development, Verification, and Modal Testing Method for Finite Interaction Solver Aeroelastic Modes From High-Speed Validation of a Fluid-Structure Element Validation in Small and R. Koomullil, M. Selim, D. McDaniel, Videos Interaction Capability and Axial Asymmetric Rotors University of Alabama, Birmingham, Y. Bao, Vanderbilt University, Nashville, Evaluation of Temporal Coupling G. Bin, University of Science and Birmingham, AL TN; P. Seshadri, University of Cambridge, Strategies Technology, Xiangtan, China; G. Wang, Cambridge, United Kingdom; S. E. Blades, A. Cornish, ATA Engineering, Inc., University of Alabama, Huntsville, Mahadevan, Vanderbilt University, Huntsville, AL Huntsville, AL; H. Li, X. Li, University of Nashville, TN Science and Technology, Xiangtan, China Tuesday, 10 January 2017 214-SE-2 Systems Engineering II Dallas 6 Chaired by: M. FRENCH, Rolls-Royce Corp and J. MATLIK, Rolls-Royce Corp 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs AIAA-2017-0872 AIAA-2017-0873 AIAA-2017-0874 AIAA-2017-0875 AIAA-2017-0876 A Collaborative Approach to Towards A Reasoning Framework Integrating ICME Practices into Design Digital Thread and Twin for Systems Digital Thread and Twin for Systems Complex Systems Engineering for Digital Clones Using the Digital Systems and Structural Analysis Engineering: Requirements to Engineering: Design to Retirement using a Web-based Visual Analytics Thread M. Sangid, Purdue University, West Lafayette, Design E. Tuegel, P. Kobryn, J. Zweber, R. Kolonay, Framework Z. Ben Miled, Indiana University-Purdue IN; J. Matlik, A. Keskin, Rolls-Royce Group J. Zweber, R. Kolonay, P. Kobryn, E. Tuegel, Air Force Research Laboratory, Wright- M. Diaz, D. Fullmer, S. Briceno, D. Mavris, University Indianapolis, Indianapolis, plc, Indianapolis, IN; B. Thacker, B. Bichon, Air Force Research Laboratory, Wright- Patterson AFB, OH Georgia Institute of Technology, Atlanta, GA IN; M. French, Rolls-Royce Group plc, Southwest Research Institute, San Antonio, Patterson AFB, OH Indianapolis, IN TX; D. Ball, Lockheed Martin Corporation, Fort Worth, TX; et al. Tuesday, 10 January 2017 215-SEN-2 Fusion of Networked Sensor and Systems Ft. Worth 2 Chaired by: T. FREY, Lockheed Martin Aeronautics 1400 hrs 1430 hrs 1500 hrs 1530 hrs AIAA-2017-0877 AIAA-2017-0878 AIAA-2017-0879 AIAA-2017-0880 Image and Information Fusion Implementation of a Distributed Autonomous Flight in GPS- A O(nm) Heuristic to the Experiments with a Software-Defined Flocking Algorithm with Obstacle Challenging Environments Hierarchical Maximum Concurrent Multi-Spectral Imaging System for Avoidance Capability for UAV Exploiting Multi-UAV Cooperation Flow Problem Aviation and Marine Sensor Networks Swarming and Vision-aided Navigation F. Vilas, E. Olinick, D. Matula, Southern S. Siewert, M. Vis, R. Claus, Embry-Riddle S. Iovino, A. Vetrella, G. Fasano, D. A. Vetrella, R. Opromolla, G. Fasano, D. Methodist University, Dallas, TX Aeronautical University, Prescott, AZ; R. Accardo, University of Naples “Federico Accardo, M. Grassi, University of Naples Krishnamurthy, S. Singh, A. Singh, University of II”, Naples, Italy; A. Savvaris, Cranfield “Federico II”, Naples, Italy Colorado, Boulder, Boulder, CO; et al. University, Cranfield, United Kingdom Tuesday, 10 January 2017 216-SOF-4 Software Challenges in Aerospace Ft. Worth 7 Chaired by: M. DAVIES, NASA-ARC-TI and J. MURPHY, NASA -Ames Research Center 1400 hrs 1430 hrs 1500 hrs 1530 hrs AIAA-2017-0881 AIAA-2017-0882 AIAA-2017-0883 AIAA-2017-0884 An ASTM Standard for Bounding A Quantitative and Risk Based Virtual Reality for Enhanced 3D Live Blackboxes: Requirements for Behavior of Adaptive Algorithms Framework for UAS Control System Astronaut Situational Awareness Tracking and Verifying Aircraft in for Unmanned Aircraft Operations Assurance During Robotic Operations in Space Motion (Invited) M. Hejase, A. Kurt, T. Aldemir, U. Ozguner, V. Goecks, G. Chamitoff, S. Borissov, A. Y. Yu, M. Yang, B. Nuseibeh, Open S. Cook, Northrop Grumman Corporation, Ohio State University, Columbus, OH; Probe, N. McHenry, N. Cluck, Texas A&M University, Milton Keynes, United Kingdom Raleigh-Durham, NC S. Guarro, M. Yau, ASCA, Inc., Redondo University, College Station, TX; et al. Beach, CA; et al.

109 Tuesday, 10 January 2017 217-STR-6 Buckling, Fatigue and Fracture of Structures I Mustang 3 Chaired by: L. HARDAWAY, Ball Aerospace & Technologies Corporation and L. FOSTER, Pratt & Whitney 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2017-0885 AIAA-2017-0886 AIAA-2017-0887 AIAA-2017-0888 AIAA-2017-0889 AIAA-2017-0890 Large Deflections of Nonlinear Probabilistic Buckling Analysis of Some Observations On Damage Mesoscale Simulation of Corrosion Modeling and characterization of Fatigue Assessment of a Helicopter Elastic and Viscoelastic Columns with Sandwich Composite Cylindrical Tolerance Analyses in Pressure Fatigue by An Integrated particulate nanocomposite micro- Rotor Blade Using Uniaxial and Follower Loads: the Elastica and Shells based on Measured Vessels Transgranular and Intergranular beams under axial compressive Multiaxial Fatigue Criteria Viscoelastica Problems Imperfections I. Raju, NASA Langley Research Center, Crack Growth Method loads A. Isik, O. Celik, Turkish Aerospace H. Hilton, University of Illinois, Urbana- C. Bisagni, Delft University of Technology, Hampton, VA; D. Dawicke, Analytical H. Yuan, W. Zhang, J. Kim, University M. Shaat, A. Abdelkefi, New Mexico State Industries, Inc., Ankara, Turkey Champaign, Urbana, IL; D. de Albuquerque, Delft, The Netherlands; M. Alfano, Technical Services & Materials, Inc., Hampton, VA; of Connecticut, Storrs, Storrs, CT; Y. Liu, University, Las Cruces, NM Federal University of ABC, São Paulo, Brazil University of Milan, Milan, Italy R. Hampton , Owl Analytics, Cupertino, CA Arizona State University, Tempe, AZ Tuesday, 10 January 2017 218-STR-7 Composite Laminate and Structures Optimization Appaloosa 1 Chaired by: P. AGGARWAL, NASA Marshall Space Flight Center and D. NORWOOD, Lockheed Martin Aeronautics 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs AIAA-2017-0891 AIAA-2017-0892 AIAA-2017-0893 AIAA-2017-0894 AIAA-2017-0895 Zig-Zag and Layerwise Models Optimal Design of a Composite Maximization of Ultimate Strength A new framework for optimization Stiffness Corrections for Overlaps for Variable-Stiffness Composite Plate with Practical Design and of Unidirectional Tapered Composite of variable stiffness plates and Gaps in Steered Composite Laminates Based on the Manufacturing Constraints Structures Considering Different D. Barazanchy, M. Van Tooren, University Panel Optimization Generalized Unified Formulation R. Taylor, D. Polaki, University of Texas, Failure Modes of South Carolina, Columbia, Columbia, SC; D. Lucas, M. Van Tooren, University of L. Demasi, E. Santarpia, San Diego State Arlington, Arlington, TX O. Celik, Middle East Technical University, A. Elham, Delft University of Technology, South Carolina, Columbia, Columbia, SC; University, San Diego, CA; R. Cavallaro, Ankara, Turkey; L. Parnas, TED University, Delft, The Netherlands A. Elham, Delft University of Technology, Charles III University of Madrid, Madrid, Ankara, Turkey Delft, The Netherlands Spain; G. Biagini, F. Vannucci, San Diego State University, San Diego, CA Tuesday, 10 January 2017 219-TP-7 Thermal Protection Systems Austin 2 Chaired by: M. HOWARD, Sandia National Laboratories 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs AIAA-2017-0896 AIAA-2017-0897 AIAA-2017-0898 AIAA-2017-0899 AIAA-2017-0900 Validation of Ablation Model of PICA Radiative Transfer in a Low Density Design Methodology for Flexible Ablation Sensor Unit for Flight Computational Analysis of Electron Using Fully Implicit Ablation and Ablative Material under Arcjet Flow Thermal Protection System Demonstration on HTV Small Recovery Transpiration Cooling for Hypersonic Thermal Response Program Conditions Insulation Configuration Selection Capsule Vehicles J. Langston, C. Wong, N. Diaz, F. Stefani, T. Horiuchi, T. Sakai, T. Suzuki, Nagoya G. Rossman, R. Braun, Georgia Institute of K. Fujita, T. Suzuki, T. Ozawa, Japan Aerospace K. Hanquist, I. Boyd, University of M. Salita, J. Koo, University of Texas, University, Nagoya, Japan; Y. Ishida, Japan Technology, Atlanta, GA Exploration Agency (JAXA), Tokyo, Japan; Michigan, Ann Arbor, Ann Arbor, MI Austin, Austin, TX Aerospace Exploration Agency (JAXA), T. Sakai, Tottori University, Tottori, Japan; Y. Tokyo, Japan Danzuka, Nagoya University, Nagoya, Japan; Y. Ishida, Japan Aerospace Exploration Agency (JAXA), Tokyo, Japan; et al. Tuesday, 10 January 2017 220-TP-8 Heat Pipes/Other Thermophysics Topics Austin 3 Chaired by: E. SILK, NASA-Goddard Space Flight Center 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs AIAA-2017-0901 AIAA-2017-0902 AIAA-2017-0903 AIAA-2017-0904 AIAA-2017-0905 Heat transfer characteristics of Experimental comparison of a Opto-Thermal Response Development of Universal Two- Estimates for Cryogenic Pump Falling Film over Horizontal Tubes- traditionally built versus additively Optimization in Laser Processing of Phase Heat Transfer Correlations for Transfer Functions A Numerical Study manufactured aircraft heat Composites Cryogenic Transfer Line Chilldown D. Jackson, J. Schwille, J. Gariffo, The A. Karmakar, S. Acharya, Illinois Institute of exchanger T. Godar, University of Dayton, Dayton, OH; J. Hartwig, NASA Glenn Research Center, Aerospace Corporation, Los Angeles, CA; Technology, Chicago, IL D. Saltzman, M. Bichnevicius, S. Lynch, B. Volk, W. Kennedy , G. Ehlert, Air Force Cleveland, OH; S. Darr, J. Chung, University Z. Spakovszky, Massachusetts Institute T. Simpson, T. Reutzel, C. Dickman, Research Laboratory, Wright-Patterson of Florida, Gainesville, Gainesville, FL of Technology, Boston, MA; C. Lettieri, AFB, OH Delft University of Technology, Delft, The

110 Pennsylvania State University, University Park, PA; et al. Netherlands; V. Wang, Massachusetts Institute of Technology, Boston, MA Tuesday, 10 January 2017 221-UMS-6 UAS Self-Separation and Collision Avoidance I Grapevine 1 Chaired by: G. LARSON, Retired and V. SCHULTZ, NASA Langley Research Center 1400 hrs 1430 hrs 1500 hrs 1530 hrs AIAA-2017-0906 AIAA-2017-0907 AIAA-2017-0908 AIAA-2017-0909 Radar-Assisted Three-Dimensional Experimental Evaluation of PICAS: A Well Clear Recommendation for Flight Test Results of the Collision Operating Detect and Avoid System An Electro-Optical Array for Non- Small UAS in High-Density, ADS-B- Avoidance System for a Fixed-Wing for Small Unmanned Aerial System Cooperative Collision Sensing on Enabled Airspace UAS using Stereoscopic Vision C. Ben, I. Martin, N. Voget, D. Moormann, Unmanned Aircraft Systems M. Duffield, T. McLain, Brigham Young S. Bhandari, A. Tan, J. Banuelos, K. Patel, M. RWTH Aachen University, Aachen, Germany C. Minwalla, K. Ellis, National Research University, Provo, UT Chae, J. Cratsley, California State Polytechnic Council Canada, Ottawa, Canada University, Pomona, Pomona, CA; et al. Tuesday, 10 January 2017 222-UMS-7 UAS Safety and Certification/UAS Autonomy and Planning II Grapevine 2 Chaired by: Z. MIAN, United Technologies Research Center 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs AIAA-2017-0910 AIAA-2017-0911 AIAA-2017-0912 AIAA-2017-0913 AIAA-2017-0914 Risk Informed Safety Case Sensitivity Analysis for Energy- System-level Performance Analysis Cooperative Estimation of Moving Characterization of Pilot Profiles Framework for Unmanned Aircraft Aware Path Optimization of a Closed-loop Sense and Avoid Target Position Using Unmanned Through Non-Parametric System Flight Software Certification A. Mills, S. Sheahan, E. Frew, University of System for Unmanned Vehicles in Aerial Vehicles Classification of Flight Data S. Guarro, M. Yau, ASCA, Inc., Redondo Colorado, Boulder, Boulder, CO the NAS K. Subbarao, P. Ru, University of Texas, F. Garcia Lorca, S. Gururajan, S. Belt, Saint Beach, CA; U. Ozguner, T. Aldemir, A. J. Jackson, J. Boskovic, D. Diel, Scientific Arlington, Arlington, TX Louis University, St. Louis, MO Kurt, M. Hejase, Ohio State University, Systems Company, Inc., Woburn, MA Columbus, OH; et al. Tuesday, 10 January 2017 223-WE-3 Wind Turbine Airfoils and Aerodynamics Investigations Austin 4 Chaired by: S. SCHRECK, NREL and J. NAUGHTON, University of Wyoming 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2017-0915 AIAA-2017-0916 AIAA-2017-0917 AIAA-2017-0918 AIAA-2017-0919 AIAA-2017-0920 Summary of the Blind Test Campaign Characterization of the Numerical and experimental An Experimental Study on Icing Turbulence Structure of the Swirling Understanding Unsteady Flow to predict the High Reynolds number carborundum used in rough airfoil study of the unsteady transitional Physics for Wind Turbine Icing Axisymmetric Turbulent Wake Physics of Two Types of Vertical Axis performance of DU00-W-210 airfoil surface tests and modelling with boundary layer on a wind turbine Mitigation M. Holmes, E. DeMillard, J. Naughton, Wind Turbines with a Fluid-Structure O. Ceyhan, ECN, Petten, The Netherlands; CFD. airfoil H. Guo, K. Zhang, R. Waldman, H. Hu, University of Wyoming, Laramie, Laramie, WY Interaction Approach O. Pires, X. Munduate, CENER, Pamplona, B. Mendez, A. Muñoz, O. Pires, X. D. Zhang, D. Cadel, E. Paterson, K. Lowe, Iowa State University, Ames, IA K. Liu, M. Yu, W. Zhu, University of Spain; N. Sorensen, Technical University of Munduate, CENER, Sarriguren, Spain Virginia Polytechnic Institute and State Maryland, Baltimore County, Baltimore, MD Denmark, Roskilde, Denmark; A. Schaffarczyk, University, Blacksburg, VA T. Reichstein, University of Kiel, Kiel, Germany; et al. Tuesday, 10 January 2017 224-WE-4 Offshore Wind Energy Applications Austin 5 Chaired by: F. RASMUSSEN 1400 hrs 1430 hrs 1500 hrs 1530 hrs AIAA-2017-0921 AIAA-2017-0922 AIAA-2017-0923 AIAA-2017-0924 Alternative Mooring Systems for a Optimised direct-drive generators for Tip and Hub Vortex Interaction Low Mass, Morphing Rotor for Very Large Offshore Wind Turbine the DTU 10MW Offshore Wind turbine and Stability Analysis of a Floating Extreme Scale Wind Turbines Supported by a Semi-Submersible L. Sethuraman, M. Maness, K. Dykes, Offshore Wind Turbine Rotor C. Noyes, C. Qin, E. Loth, University of Floating Platform National Renewable Energy Laboratory, S. Rodriguez, J. Jaworski, Lehigh Virginia, Charlottesville, Charlottesville, VA J. Liu, L. Manuel, University of Texas, Golden, CO University, Bethlehem, PA Austin, Austin, TX

111 Tuesday, 10 January 2017 225-WKSP-2 Career Workshop II Mustang 4 1400 - 1600 hrs Tuesday, 10 January 2017 226-NW-9 Tuesday Afternoon Networking Coffee Break Longhorn Hall E&F 1530 - 1600 hrs Tuesday, 10 January 2017 227-NW-10 Rising Leaders Leadership Exchange and Speed Mentoring Grapevine A 1600 - 1730 hrs Tuesday, 10 January 2017 228-LEC-4 Dryden Lecture in Research Texas C 1730 - 1830 hrs Maturation of Active Flow Control Concepts for Improved Aircraft Performance Israel J. Wygnanski Professor, Aerospace Engineering University of Arizona Tuesday, 10 January 2017 229-NW-11 Opening Reception in the Exposition Hall Longhorn Hall E&F 1830 - 2000 hrs *Doors open at 6:15pm Wednesday Wednesday, 11 January 2017 230-NW-12 Wednesday Early Morning Networking Coffee Break Session Room Foyers 0700 - 0730 hrs Wednesday, 11 January 2017 231-SB-3 Wednesday Morning Speakers’ Brieﬁng Session Rooms 0730 - 0800 hrs Wednesday, 11 January 2017 232-PLNRY-4 Wednesday Morning Plenary: Disruptive Policy Issues - Presidential Transitions Texas A & B 0800 - 0900 hrs Moderator: Ann Zulkosky, Director, NASA Programs, Washington Operations, Lockheed Martin Space Systems Company

Panelists: Russell Chew Lt. Gen. Henry “Trey” Obering III Dorothy Robyn Courtney Stadd Senior Advisor Executive Vice President Independent Consultant/Writer Washington Operations, Business Development NEXA Capital Partners Booz Allen Hamilton Former Commissioner, GSA, Public Buildings Service TIP Technologies Former Deputy Under Secretary of Defense (Installations and Environment)

Wednesday, 11 January 2017 233-NW-13 Wednesday Morning Networking Coffee Break Longhorn Hall E&F 0900 - 0930 hrs Wednesday, 11 January 2017 112 234-AA-6 Computational Aeroacoustics II Grapevine B Chaired by: A. LYRINTZIS and S. ARUNAJATESAN, Sandia National Labs 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2017-0925 AIAA-2017-0926 AIAA-2017-0927 AIAA-2017-0928 AIAA-2017-0929 AIAA-2017-0930 Direct numerical simulation of a Similarity Spectra Analysis in Highly Lagrangian Coherent Structures & Hybrid Pressure/Density-Based Towards Modeling Ultrasonic Investigation of Airship Motion temporally-developing subsonic Heated Supersonic Jets Using Large- Their Role in Jet Noise Generation Overset Discontinuous Galerkin Thermoacoustics with Bulk Viscosity Sensitivity to Geometric Parameters round jet and its sound field Eddy Simulations D. Gonzalez, Naval Surface Warfare Center, Method for Acoustics Prediction Effects D. Han, X. Wang, Shanghai Jiao Tong C. Bogey, École Centrale de Lyon, Lyon, J. Liu, K. Kailasanath, Naval Research Indian Head, MD; D. Gaitonde, Ohio State R. Harris, CFD Research Corporation, J. Lin, Stanford University, Stanford, CA; C. University, Shanghai, China; L. Yan, France Laboratory, Washington, D.C.; E. Gutmark, University, Columbus, OH; M. Lewis, Huntsville, AL Scalo, Purdue University, West Lafayette, University of Texas, Arlington, Arlington, University of Cincinnati, Cincinnati, OH Science and Technology Policy Institute, IN; L. Hesselink, Stanford University, TX; G. Yan, D. Duan, Shanghai Jiao Tong Washington, D.C. Stanford, CA University, Shanghai, China Wednesday, 11 January 2017 235-AA-7 Aeroacoustics - Advanced Measurement and Experiment Grapevine 3 Chaired by: C. BROWN, NASA Glenn and E. NESBITT, Boeing Commercial Airplanes 0930 hrs 1000 hrs 1030 hrs AIAA-2017-0931 AIAA-2017-0932 AIAA-2017-0933 Testing and Characterization Flow Measurements from a Supersonic Acoustic Detection of Faults and of Windscreen Design for UAS Rectangular Nozzle Exhausting Over a Degradation in a High-Bypass Mounted Airborne Acoustic Sensing Flat Surface Turbofan Engine During VIPR Phase J. Banks, J. Kidd, Oklahoma State F. Baier, P. Mora , E. Gutmark, University of III Testing University, Stillwater, OK Cincinnati, Cincinnati, OH; K. Kailasanath, Naval D. Boyle, NASA Armstrong Flight Research Research Laboratory, Washington, D.C. Center, Edwards, CA Wednesday, 11 January 2017 236-AFM-5 Flight Test and System Identification II Grapevine 5 Chaired by: J. SEYMOUR, Lockheed Martin and M. PHILLIPS, NASA 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2017-0934 AIAA-2017-0935 AIAA-2017-0936 AIAA-2017-0937 AIAA-2017-0938 AIAA-2017-0939 Low Speed Airship Control using Flight Test Techniques for A Comparison of Model-Based Cessna Citation X Stall Data Reduction Methods for Dutch- Post-flight Evaluation of the Reinforcement Learning and Expert Quantifying Pitch Rate and Angle of and Data-Driven Methods for Characteristics Identification from Roll Analysis Guidance and Control for D-SEND#2 Demonstrations Attack Rate Dependencies Aerodynamic Parameter Estimation Flight Data using Neural Networks J. Laguardia, D. Dutra, R. Pinto, Federal 2nd Drop Test O. Daskiran, B. Huff, A. Dogan, University J. Grauer, E. Morelli, D. Murri, NASA from Flight Data G. Ghazi, M. Bosne, Q. Sammartano, R. University of Minas Gerais, Belo Horizonte, J. Kawaguchi, H. Suzuki, T. Ninomiya, of Texas, Arlington, Arlington, TX Langley Research Center, Hampton, VA A. Kumar, A. Ghosh, Indian Institute of Botez, University of Québec, Montréal, Brazil H. Tomita, Japan Aerospace Exploration Technology Kanpur, Kanpur, India Canada Agency (JAXA), Tokyo, Japan Wednesday, 11 January 2017 237-AMT-9 Deformation, Displacement, and Object-Tracking Measurements Grapevine D Chaired by: H. HU, Iowa State University and T. IOPPOLO, Southern Methodist University 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2017-0940 AIAA-2017-0941 AIAA-2017-0942 AIAA-2017-0943 Non-contact photonic displacement Photogrammetry for Masking Quantification of Dynamic Droplet Surface State Measurement of sensor based on the morphology Particle Image Velocimetry Images Impact onto a Solid Surface by a Free-Flight Object by Motion- dependent resonances Near Moving Bodies using a Digital Image Projection Capturing Method E. Rubino, T. Ioppolo, Southern Methodist P. Nikoueeyan, J. Naughton, University of Technique M. Ishii, National Research Institute University, Dallas, TX Wyoming, Laramie, Laramie, WY H. Li, K. Zhang, R. Waldman, H. Hu, Iowa of Police Science, Kashiwa, Japan; H. State University, Ames, IA Isokawa, T. Miyazaki, University of Electro- Communications, Chofu, Japan; H. Sakaue, University of Notre Dame, Notre Dame, IN Wednesday, 11 January 2017 113 238-APA-21 Flow Control Applications and Demonstrations (Active and Passive) III Dallas 1 Chaired by: A. VANDERWYST, Leidos and B. MARPLES, Johns Hopkins University Applied Physics Laboratory 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2017-0944 AIAA-2017-0945 AIAA-2017-0946 AIAA-2017-0947 AIAA-2017-0948 Reduction of Drag on Commercial Large-Eddy Simulation of MVG Spectrum analysis of SWBLI under Frequency Response of Control of Low Speed Cavity Flow Using Trucks via Vehicle Modifications Controlled Oblique Shockwave/ ramp-type MVG control Aerodynamic Load Control through Streamwise Tabs at Leading Edge E. Worthington, M. Tuke, K. Powers, S. Boundary Layer Interaction Y. Yang, S. Tian, X. Dong, C. Liu, University Mini-tabs A. Sathianarayanan, L. Venkatakrishnan, Lee, Alfred University, Alfred, NY G. Yang, J. Fang, Beihang University, of Texas, Arlington, Arlington, TX D. Heathcote, D. Cleaver, I. Gursul, National Aerospace Laboratories, Bengaluru, Beijing, China; C. Liu, University of Texas, University of Bath, Bath, United Kingdom India; S. Sharma, Indian Institute of Technology Arlington, Arlington, TX; Y. Yao, Beihang Mumbai, Mumbai, India University, Beijing, China Wednesday, 11 January 2017 239-APA-22 Unsteady Aerodynamics III Dallas 2 Chaired by: D. HUNSAKER, Utah State University and B. CYBYK, Johns Hopkins University Applied Physics Laboratory 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2017-0949 AIAA-2017-0950 AIAA-2017-0951 AIAA-2017-0952 Numerical Study of Coherent Structures Exact aerodynamic force Unsteady Coupling Algorithm for Reduced order modeling of a Around a Re-entry Capsule using decomposition and dynamic force Lifting-Line Methods dynamically pitching NACA 0018 Proper Orthogonal Decomposition derivatives in non linear flows M. Parenteau, F. Plante, E. Laurendeau, Airfoil G. Morikami, Tokyo Metropolitan University, M. Ostieri, B. Mele, R. Tognaccini, École Polytechnique de Montréal, Montréal, F. Niel, National Center for Scientific Hino, Japan; Y. Ohmichi, Japan Aerospace University of Naples “Federico II”, Naples, Canada; M. Costes, ONERA, Meudon, Research (CNRS), Toulouse, France; C. Exploration Agency (JAXA), Chofu, Japan; K. Italy France Fagley, J. Seidel, T. McLaughlin, U.S. Air Ishiko, Asahikawa College, Asahikawa, Japan; Force Academy, Colorado Springs, CO M. Kanazaki, Tokyo Metropolitan University, Hino, Japan Wednesday, 11 January 2017 240-APA-23/FD-31 Vortical Flows & Wake Control Dallas 3 Chaired by: K. TAIRA, Florida State University and B. DETERT, Boeing Commercial Airplanes 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2017-0953 AIAA-2017-0954 AIAA-2017-0955 AIAA-2017-0956 AIAA-2017-0957 AIAA-2017-0958 Parametric Investigation of Afterbody Drag Reduction Using A Passive Method to Control the Wake Towards Simulating the Evolution Experimental Flight Test of Small Transition and turbulence in a Turbulent Mixing Layer Control Active Flow Control Flow behind a Circular Cylinder of Aircraft Wake Vortices with UAS Wake Vortex Encounters lid-driven cavity flow at high Mach using Ns-DBD Plasma Actuators R. Jackson, Z. Wang, I. Gursul, University W. Chen, D. Li, H. Li, Harbin Institute of OVERFLOW Z. Barbeau, J. Jacob, Oklahoma State number A. Singh, J. Little, University of Arizona, of Bath, Bath, United Kingdom Technology, Harbin, China; H. Hu, Iowa State D. Schauerhamer, S. Robinson, University University, Stillwater, OK S. Pradhan, Indian Institute of Science, Tucson, Tucson, AZ University, Ames, IA of California, Davis, Davis, CA Bengaluru, India Wednesday, 11 January 2017 241-APA-24 DPW-6 Results and Comparisons I Dallas 4 Chaired by: C. ROY, Virginia Tech and E. FELTROP, Textron Aviation 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2017-0959 AIAA-2017-0960 AIAA-2017-0961 AIAA-2017-0962 AIAA-2017-0963 AIAA-2017-0964 TAS Code, FaSTAR and Cflow Results Contributions to the 6th AIAA CFD Drag Comparison of Fixed and Adaptive DPW-6 Results Using FUN3D Exa PowerFLOW Simulations for Experimental Investigations on the for the Sixth Drag Prediction Prediction Workshop Using Structured Unstructured Grid Results for Drag With Focus on k-kL-MEAH2015 the Sixth AIAA Drag Prediction Common Research Model at ONERA- Workshop Grid Methods Prediction Workshop 6 Turbulence Model Workshop S1MA – Comparison with DPW Y. Ito, M. Murayama, A. Hashimoto, T. J. Coder, University of Tennessee, Knoxville, T. Michal, D. Babcock, The Boeing K. Abdol-Hamid, J. Carlson, C. Rumsey, B. Konig, A. Ribeiro, E. Fares, Exa Numerical Results Ishida, K. Yamamoto, T. Aoyama, Japan Knoxville, TN; T. Pulliam, NASA Ames Research Company, St. Louis, MO; D. Kamenetskiy, E. Lee-Rausch, M. Park, NASA Langley Corporation, Stuttgart, Germany A. Cartieri, D. Hue, Q. Chanzy, O. Atinault, Aerospace Exploration Agency (JAXA), Center, Moffett Field, CA; D. Hue, ONERA, The Boeing Company, Seattle, WA; J. Research Center, Hampton, VA ONERA, Modane, France Chofu, Japan; et al. Meudon, France; G. Kenway, University of Krakos, M. Mani, The Boeing Company, Michigan, Ann Arbor, Ann Arbor, MI; A. Sclafani, St. Louis, MO; R. Glasby, University of The Boeing Company, Alta Loma, CA Tennessee, Knoxville, Knoxville, TN; et al. Wednesday, 11 January 2017 114 242-APA-26 Special Session: CREATE-AV HPC Multiphysics II Dallas 5 Chaired by: N. HARIHARAN, CREATE-AV and S. MORTON, DoD HPCMP 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2017-0965 AIAA-2017-0966 AIAA-2017-0967 AIAA-2017-0968 AIAA-2017-0969 AIAA-2017-0970 CFD Analysis of the F/A-18E Super Feedback Flow Control on a Simulation of C-130 H/J Troop Forced Motions Design for CFD Analysis of a Maneuvering Results from HPCMP CREATETM-AV Hornet during Approach to a FlutteringWing using HPCMP Doors and Cargo Ramp Flow Fields Aerodynamic Identification and F/A-18E Super Hornet COFFE for 3-D Aircraft Configurations Generic Ship CREATE™-AV Kestrel K. Bergeron, Army Research, Development Modeling of a Generic Missile B. Green, D. Findlay, Naval Air Systems with Higher-Order Meshes Generated B. Green, S. Polsky, Naval Air Systems J. Seidel, C. Fagley, T. McLaughlin, U.S. Air and Engineering Command, Natick, MA; Configuration Command, Patuxent River, MD by Pointwise, Inc. Command, Patuxent River, MD Force Academy, Colorado Springs, CO M. Ghoreyshi, A. Lofthouse, U.S. Air Force J. Allen, University of Colorado, Colorado J. Erwin, R. Glasby, University of Tennessee, Academy, Colorado Springs, CO Springs, Colorado Springs, CO; M. Knoxville, Knoxville, TN; S. Karman, Pointwise, Ghoreyshi, A. Lofthouse, U.S. Air Force Inc., Fort Worth, TX; D. Stefanski, University of Academy, Colorado Springs, CO Tennessee, Knoxville, Knoxville, TN Wednesday, 11 January 2017 243-DE-3 Design Processes and Tools Palomino 3 Chaired by: J. CUTSHALL, Southwest Research Institute and T. HARRIS, Northrop Grumman 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2017-0971 AIAA-2017-0972 AIAA-2017-0973 AIAA-2017-0974 AIAA-2017-0975 AIAA-2017-0976 Whitespace Exploration: The Next Mining Multi-Objective Minimal Multifidelity, Multiscale System Survey of Technology Forecasting Uncertainty Propagation in Application of Design Thinking in Step in Searching the Design Space Commitment Decision Significance Modeling and Simulation Environment Techniques for Complex Systems Technology Valuation Process a Rapid Design Study to Further A. Ko, J. Daniel, W. Keel, A. Baines, via Cluster-and-Find-Changes P. Menegay, D. Notestein, SynaptiCAD, A. Smith, K. Collins, D. Mavris, Georgia F. Akram, National University of Sciences Autonomy Experimental Research Phoenix Integration, Blacksburg, VA N. Knerr, D. Selva, Cornell University, Blacksburg, VA; S. Cornford, S. Wall, Jet Institute of Technology, Atlanta, GA and Technology, Islamabad, Pakistan; D. A. McGowan, NASA Langley Research Ithaca, NY Propulsion Laboratory, California Institute of Mavris, Georgia Institute of Technology, Center, Hampton, VA; C. Bakula, NASA Technology, Pasadena, CA Atlanta, GA Glenn Research Center, Cleveland, OH Wednesday, 11 January 2017 244-EDU-1 Educating the Engineer of the 2030 Grapevine A 0930 - 1230 hrs Technology is advancing tremendously and at a pace that is unparalleled in human history – changing the landscape of human endeavors including the aerospace sector. In aerospace, we see reduced barriers to entry in new and exciting arenas and greatly increased complexity and demands on affordability in the more traditional areas. How should higher education nurture and prepare today’s and tomorrow’s aerospace engineers to meet the challenges and opportunities that await for them in 2030 and 2050? This panel brings together leaders in aerospace education to tell us how they see the future of aerospace and how higher education must educate today’s students to realize the incredible and still unwritten future that awaits for them to create and build.

Moderator: Tom Shih, Purdue University

Panelists: Penina Axelrad Rodney Bowersox George Lesieutre Mark Lewis Tasos Lyrintzis Achille Messac Vigor Yang University of Colorado Texas A&M University Pennsylvania State University University of Maryland Embry-Riddle Aeronautical University Howard University Georgia Institute of Technology

Wednesday, 11 January 2017 245-F360-5 Space Trafﬁc Management Texas C 0930 - 1130 hrs Moderator: Moriba Jah, Director, Space Object Behavioral Sciences, University of Arizona

Panelists: Travis Blake P.J. Blount Mike Gazarik Donald Greiman Lt. Gen. Susan Helms George Nield Senior Manager, Advanced Technology Adjunct Professor Vice President, Engineering Vice President & General Manager U.S. Air Force (ret.) Associate Administrator Center Lockheed Martin Space Systems Mississippi School of Law Ball Aerospace Commercial Space Situational Awareness Commercial Space Transportation Company Schaffer Corporation FAA

Wednesday, 11 January 2017 246-FD-32 RANS and LES Methods Texas 3 Chaired by: Q. WANG, MIT and C. REED, Lockheed Martin Corporation 115 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2017-0977 AIAA-2017-0978 AIAA-2017-0979 AIAA-2017-0980 AIAA-2017-0981 AIAA-2017-0982 Hybrid RANS/LES modelling with Anisotropic grid-adaptation in large A New DES Model Based on Wray- Integral formulation of under- Modeling and analysis of large- Discontinuous Galerkin-Monte Carlo improved downstream anisotropic eddy simulations of wall-bounded Agarwal Turbulence Model for resolved near-wall scales for coarse- eddy simulations of particle-laden Solver for Large Eddy Simulation of eddy viscosity model and free shear flows Simulation of Wall Boundeed Flows grid LES turbulent boundary layer flows Compressible Turbulent Flows W. Zhang, T. Shih, Purdue University, West S. Toosi, J. Larsson, University of Maryland, X. Han, T. Wray, R. Agarwal, Washington A. Marques, Q. Wang, Massachusetts M. Rahman, R. Samtaney, King Abdullah S. Sammak, A. Nouri, University of Pittsburgh, Lafayette, IN College Park, College Park, MD University in St. Louis, St. Louis, MO Institute of Technology, Cambridge, MA University of Science and Technology, Pittsburgh, PA; M. Brazell, D. Mavriplis, Thuwal, Saudi Arabia University of Wyoming, Laramie, Laramie, WY; P. Givi, University of Pittsburgh, Pittsburgh, PA Wednesday, 11 January 2017 247-FD-33 Shock Boundary Layer Interactions II Texas 1 Chaired by: I. LEYVA, AFOSR and P. MARTIN, University of Maryland 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2017-0983 AIAA-2017-0984 AIAA-2017-0985 AIAA-2017-0986 AIAA-2017-0987 AIAA-2017-0988 Experimental Study Exploring Corner Effects in Oblique Shock Single Camera 3D Measurement of Comparison of Unsteady Flow Unsteadiness in Swept-Compression- Frequency analysis of oblique shock Unsteadiness Length Scales in a Wave/ Boundary Layer Interactions a Shock Wave-Turbulent Boundary Similarities in Various Shock/ Ramp Shock/Turbulent-Boundary- wave boundary layer interaction Reflected Shock - Boundary Layer in Rectangular Channels Layer Interaction Boundary-Layer Interaction Layer Interactions N. Chaganti, B. Brooker, S. Olcmen, Interaction X. Xiang, H. Babinsky, University of J. Bolton, B. Thurow, Auburn University, Configurations M. Adler, D. Gaitonde, Ohio State University of Alabama, Tuscaloosa, P. Rabey, P. Bruce, Imperial College London, Cambridge, Cambridge, United Kingdom Auburn, AL; F. Alvi, N. Arora, Florida State J. Threadgill, University of Arizona, Tucson, University, Columbus, OH Tuscaloosa, AL; P. Kolhe, Indian Institute of London, United Kingdom University, Tallahassee, FL Tucson, AZ; P. Bruce, Imperial College Technology Sangareddy, Sangareddy, India London, London, United Kingdom Wednesday, 11 January 2017 248-FD-34 Special Session: Low Reynold’s Number Flows Texas 2 Chaired by: M. GREEN, Syracuse University and K. MULLENERS, EPFL 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2017-0989 Oral Presentation Oral Presentation Oral Presentation Oral Presentation Review of Vortex Identification Vortex formation and shedding Surface Signatures for Leading Edge Tracking the footprints of dynamic Investigating Aerodynamic Flows at Methods characterized by Lagrangian Vortex Shedding and Detachment stall vortices in the wing surface Low Angle of Attack Using a Hybrid B. Epps, Dartmouth College, Hanover, NH techniques from Unsteady Airfoils pressure Vortex Sheet/Point Vortex Model M. Green, Syracuse University, Syracuse, NY A. Gopalarathnam, A. Saini, S. Narsipur, A. K. Mulleners, Swiss Federal Institute of D. Darakananda, J. Eldredge, University of Suresh Babu, North Carolina State University, Technology, Lausanne, Switzerland California, Los Angeles, Los Angeles, CA; T. Raleigh, NC; K. Ramesh, University of Glasgow, Colonius, California Institute of Technology, Glasgow, United Kingdom Pasadena, CA; D. Williams, Illinois Institute of Technology, Chicago, IL Wednesday, 11 January 2017 249-FD-35 Turbulence Modeling: RANS/LES Texas 4 Chaired by: D. MCDANIEL, DoD HPCMP/CREATE Kestrel Team, Eglin Air Force Base and K. DURAISAMY, University of Michigan, Ann Arbor 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2017-0990 AIAA-2017-0991 AIAA-2017-0992 AIAA-2017-0993 AIAA-2017-0994 One-Equation Turbulence Model Dominant Structures Identification Dynamic Large Eddy Simulation: Augmentation of Turbulence Models LES and Hybrid RANS-LES of High Based on k/e of Three-Dimensional Turbulent Analysis of Stability and Realizability Using Field Inversion and Machine Reynolds Number Separated Flows M. Rahman, V. Vuorinen, Aalto University, Cavity Flow R. Mokhtarpoor, S. Heinz, M. Stoellinger, Learning R. Mokhtarpoor, S. Heinz, M. Stoellinger, Helsinki, Finland; R. Agarwal, Washington T. Rokita, J. Greenberg, R. Arieli, Technion-- University of Wyoming, Laramie, Laramie, WY; A. Singh, K. Duraisamy, Z. Zhang, University of Wyoming, Laramie, Laramie, University in St. Louis, St. Louis, MO; M. Larmi, Israel Institute of Technology, Haifa, Israel; P. Balakumar, NASA Langley Research Center, University of Michigan, Ann Arbor, Ann WY T. Siikonen, Aalto University, Helsinki, Finland Y. Levy, Israeli CFD Center, Caesarea, Israel Hampton, VA Arbor, MI Wednesday, 11 January 2017 116 250-FD-36 Unsteady Measurements Texas 5 Chaired by: O. STALNOV, Technical University of Berlin Germany and G. DIMITRIADIS, University of Liege 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2017-0995 AIAA-2017-0996 AIAA-2017-0997 AIAA-2017-0998 AIAA-2017-0999 AIAA-2017-1000 Direct Force Measurements During Unsteady Measurements for a Experimental Investigation of Static Oscillatory Plunging Motion Applied Unsteady Flow Physics of Airfoil Stable POD-Galerkin Reduced Order Transient Flow about Pitching Flat Periodically Plunging Airfoil Stall Hysteresis on an NACA 0012 to an Airfoil Near Stall Dynamic Stall Models for unsteady turbulent Plates N. Chiereghin, D. Cleaver, I. Gursul, Airfoil M. Agate, J. Little, University of Arizona, R. Gupta, P. Ansell, University of Illinois, incompressible flows H. Yu, Chung Cheng Institute of University of Bath, Bath, United Kingdom G. Hristov, P. Ansell, University of Illinois, Tucson, Tucson, AZ; A. Gross, New Mexico Urbana-Champaign, Urbana, IL N. Akkari, R. Mercier, Safran Group, Technology, National Defense University, Urbana-Champaign, Urbana, IL State University, Las Cruces, NM; H. Fasel, Magny-les-Hameaux, France; G. Lartigue, Taoyuan, Taiwan; L. Bernal, University of University of Arizona, Tucson, Tucson, AZ V. Moureau, CORIA, Rouen, France Michigan, Ann Arbor, Ann Arbor, MI Wednesday, 11 January 2017 251-FD-37 LES Texas 6 Chaired by: D. GARMANN, Air Force Research Laboratory and C. BARNES, AFRL/RQVA 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2017-1001 AIAA-2017-1002 AIAA-2017-1003 AIAA-2017-1004 AIAA-2017-1005 AIAA-2017-1006 Self-Sustained Pitch-Heave Investigation of the Unsteady Tip Large-Eddy Simulation over Preliminary Numerical and Large Eddy Simulation of Flow LES of a surging airfoil with large Oscillations and Gust Response of Vortex Structure on a NACA0012 a backward rounded ramp in Experimental Evaluation of Turbulent Interactions of a Finite-span streamwise oscillations an Airfoil at Transitional Reynolds Wing at Fixed Incidence presence of crossflow Mixing from Thin-Film Cooling Synthetic Jet on an Airfoil A. Kocher, R. Cummings, S. Tran, O. Sahni, Numbers D. Garmann, M. Visbal, Air Force Research A. Masi, J. Cui, P. Tucker, University of M. Borghi, P. Poinsatte, D. Thurman, NASA S. Tran, E. McGlynn, O. Sahni, Rensselaer Rensselaer Polytechnic Institute, Troy, NY C. Barnes, M. Visbal, Air Force Research Laboratory, Wright-Patterson AFB, OH Cambridge, Cambridge, United Kingdom Glenn Research Center, Cleveland, OH; W. Polytechnic Institute, Troy, NY Laboratory, Wright-Patterson AFB, OH Engblom, Embry-Riddle Aeronautical University, Daytona Beach, FL Wednesday, 11 January 2017 252-FD-38 Other Topics in Fluid Dynamics I Grapevine C Chaired by: M. MUNSON, U.S. Army Research Office and A. GROSS, New Mexico State University 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2017-1007 AIAA-2017-1008 AIAA-2017-1009 AIAA-2017-1010 AIAA-2017-1011 AIAA-2017-1012 Linearized Fluid Film Forces for Obtaining a Stable Galerkin ROM Numerical simulation of laser Numerical Investigation of Radial Natural Convection About an Demonstration of Leakage Flow Squeeze Film Dampers Executing in Presence of Shock-Vortex energy deposition near a wall Flow in Solar Chimney Power Plant Idealized Standing Human With and Distribution of an Axial Fan inside Small Amplitude Circular-Centered Interaction S. Ghosh, Indian Institute of Technology Collector Without Body Armor the Tip Clearance Gap Orbits in Aero-Engines E. Rezaian, M. Wei, New Mexico State Madras, Chennai, India M. Hasan, A. Gross, New Mexico State D. Mott, A. Kercher, A. Corrigan, Naval A. Gamil, J. Teixeira , A. A., Cranfield S. Hamzelouia, K. Behdinan, University of University, Las Cruces, NM University, Las Cruces, NM Research Laboratory, Washington, D.C. University, Bedford, United Kingdom; H. Toronto, Toronto, Canada Alhajeri, College of Technological Studies, Kuwait, Kuwait; F. Elasha, Coventry University, Coventry, United Kingdom Wednesday, 11 January 2017 253-GNC-1 Missile Intercept and Evasion Guidance Austin 1 Chaired by: A. RATNOO and B. BISWELL, Raytheon Missile Systems 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2017-1013 AIAA-2017-1014 AIAA-2017-1015 AIAA-2017-1016 AIAA-2017-1017 AIAA-2017-1018 Visibility Augmentation of the Near Optimal Evasion from A Cooperative Differential Game for An Energy Based Objective for Optimal Guidance for Active Aircraft Estimation Enhancement by Proportional Navigation Guidance Acceleration Estimating Pursuers Imposing a Relative Intercept Angle Solving an Optimal Missile Evasion Defense Against Homing Missiles Imposing a Relative Intercept Angle L. Tardioli, G. Franzini, L. Pollini, M. V. Shaferman, Technology University of V. Shaferman, Technical University Problem E. Garcia, Infoscitex Corporation, Wright- for Defending Missiles Innocenti, University of Pisa, Pisa, Italy Vienna, Vienna, Austria of Vienna, Vienna, Austria; T. Shima, R. Carr, R. Cobb, Air Force Institute of Patterson AFB, OH; D. Casbeer, M. Pachter, R. Fonod, T. Shima, Technion--Israel Technion--Israel Institute of Technology, Technology, Wright-Patterson AFB, OH Air Force Institute of Technology, Wright- Institute of Technology, Haifa, Israel Haifa, Israel Patterson AFB, OH Wednesday, 11 January 2017 117 254-GNC-2 Loss of Control and Protections Austin 6 Chaired by: A. CHAKRAVARTHY, Wichita State University and J. DONGMO 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2017-1019 AIAA-2017-1020 AIAA-2017-1021 AIAA-2017-1022 AIAA-2017-1023 AIAA-2017-1024 Compact Trackers with Exponential Performance Enhacement of Compact Stall Recovery Guidance Using an Laplace-Based Predictive Estimation Low Speed Protections for a A Flight Envelope Protection Method Observers Using Hybrid Control High Order Sliding Mode Controllers Energy Based Algorithm of Loss-of-Control Boundaries on a Commercial Airliner : a Practical Based on Potential Functions Rates for Flight Vehicles Loss-Of- for Post LOC Autonomous Recovery Of T. Lombaerts, S. Schuet, J. Kaneshige, K. Transport Aircraft Approach D. Sun, X. Li, H. Jafarnejadsani, N. Control Autonomous Recovery Flight Vehicles Using Optimal Control Shish, V. Stepanyan, NASA Ames Research K. Rajaram, M. Rafi, J. Steck, A. S. Oudin, Airbus, Toulouse, France Hovakimyan, University of Illinois, Urbana- J. Dongmo, JetMech, Inc., Nottingham, MD Modification Center, Moffett Field, CA Chakravarthy, Wichita State University, Champaign, Urbana, IL J. Dongmo, JetMech, Inc., Nottingham, MD Wichita, KS Wednesday, 11 January 2017 255-GNC-3 Aircraft GNC Control Applications Grapevine 4 Chaired by: J. HORN, The Pennsylvania State University 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2017-1025 AIAA-2017-1026 AIAA-2017-1027 AIAA-2017-1028 AIAA-2017-1029 Trajectory Shaping Autopilot-Guidance Enhancing Manual Flight Precision and Design of a Virtual Fighter Pilot and Aerial Vehicle Localization Using PIL Simulation of Integrated Design for Civil Autonomous Aerial Reducing Pilot Workload Using a New Simulation Environment for Unmanned Generic Landmarks Autopilot and Path Following Refueling Manual Control Augmentation System Combat Aerial Vehicles M. DeAngelo, J. Horn, Pennsylvania State Algorithms for MAVs Using Arduino A. Tsukerman, M. Weiss, T. Shima, Technion- for Energy Angle H. Shin, J. Lee, D. Shim, Korea Advanced University, University Park, PA Target -Israel Institute of Technology, Haifa, Israel; K. Schreiter, S. Müller, R. Luckner, D. Manzey, Institute of Science and Technology, Daejeon, K. Ibrahim, Zewail City of Science and D. Löbl, F. Holzapfel, Technical University of Technical University of Berlin, Berlin, Germany South Korea; D. You, Agency for Defense Technology, Cairo, Egypt; G. El-Bayoumi, A. Munich, Munich, Germany Development, Daejeon, South Korea Kassem, Cairo University, Cairo, Egypt Wednesday, 11 January 2017 256-GNC-4 Navigation Methods Austin 2 Chaired by: W. WHITACRE, Draper Laboratory and M. OPPENHEIMER, Air Force Research Laboratory 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2017-1030 AIAA-2017-1031 AIAA-2017-1032 AIAA-2017-1033 AIAA-2017-1034 AIAA-2017-1035 Lost in Space and Time Inertial Navigation Employing Wahba’s Problem: A Combined Utilization of INS Measurements into Spacecraft Pose Estimation using Robust Navigation of UAV using V. Adams, M. Peck, Cornell University, Common Frame Error Binary Search and Bisection Fixed-Point Smoothing Approach to Principal Component Analysis and a Inertial Sensors Aided by UWB and Ithaca, NY Representations Approach Mitigate the Disturbance Effect of Monocular Camera RTK GPS M. Whittaker, J. Crassidis, State University K. Turkoglu, E. Wahl, San Jose State Missile Initial Heading Errors on Missile J. Shi, S. Ulrich, Carleton University, K. Gryte, J. Hansen, T. Johansen, T. of New York, Amherst, NY University, San Jose, CA Terminal Guidance Performance Ottawa, Canada; S. Ruel, Neptec, Ottawa, Fossen, Norwegian University of Science G. Tanriverdi, M. Cavdaroglu, ASELSAN, Inc., Canada and Technology, Trondheim, Norway Ankara, Turkey Wednesday, 11 January 2017 257-GNC-5 Spacecraft and Launch Controls Grapevine 6 Chaired by: K. BOLLINO, U.S. Air Force and J. REED, United Launch Alliance, LLC 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2017-1036 AIAA-2017-1037 AIAA-2017-1038 AIAA-2017-1039 AIAA-2017-1906 Non-linear Control Law Design Super-Twisting Sliding Mode Three- Adaptive Nonlinear Control of Evolving Systems Approach to the A New Multi-position Calibration For Satellite Fixed Ground Target Axis Attitude Control of Spacecraft Autonomous Spacecraft Rendezvous Attitude Control of a Space-Debris Method for the Gyrowheel Using tracking Using Solar Radiation Pressure and Proximity Operations Removal Spacecraft Multiple Objective Particle Swarm H. Bel, A. Aly, A. Youssef, Y. Elhalwagy, K. Lee, Catholic Kwandong University, L. Sun, W. Huo, Z. Jiao, Beihang University, J. Habets, E. Mooij, Delft University of Optimization Algorithm Military Technical College, Cairo, Egypt Gangwon, South Korea Beijing, China Technology, Delft, The Netherlands; S. Frost, Y. Zhao, H. Zhao, X. Huo, Harbin Institute NASA Ames Research Center, Moffett Field, CA of Technology, Harbin, China Wednesday, 11 January 2017

118 258-GNC-6 Control of Micro Air Vehicles Austin 4 Chaired by: E. JOHNSON, Georgia Institute of Technology and Y. CAO, University of Texas, San Antonio 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2017-1040 AIAA-2017-1041 AIAA-2017-1042 AIAA-2017-1043 AIAA-2017-1044 AIAA-2017-1045 A strategy for robust precision Nonlinear Controller Design for A Tangential Guidance Logic for A Daisy-Chain Control Design for Integrated Guidance and Nonlinear Longitudinal Controller for control of an endbody being towed Transition Flight of a Fixed-Wing Virtual Target Based Path Following a Multirotor UAV with Direct Force Feedback Control of Underactuated Hand Launched MAV Based on by an orbiting UAV. UAV with Input Constraints S. Thakar, A. Ratnoo, Indian Institute of Capabilities Unmanned Aerial Vehicles in SE(3) Supertwisting Algorithm M. Merz, Norwegian University of Science Y. Kawakami, K. Uchiyama, Nihon Science, Bengaluru, India H. Mehmood, Delft University of Technology, S. Viswanathan, A. Sanyal, Syracuse S. Balajiwale, H. Arya, A. Joshi, Indian and Technology, Trondheim, Norway University, Chiba, Japan Delft, The Netherlands; E. Johnson, Georgia University, Syracuse, NY; M. Izadi, Texas Institute of Technology Bombay, Mumbai, Institute of Technology, Atlanta, GA A&M University, College Station, TX India Wednesday, 11 January 2017 259-GNC-7 Spacecraft Robotics Austin 5 Chaired by: S. LEE, Alfred University and H. LIU, University of Toronto 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2017-1046 AIAA-2017-1047 AIAA-2017-1048 AIAA-2017-1049 AIAA-2017-1050 Iterative Learning Control of Experimental Emulation of the Contact Dynamics and Control of Experimental Validation for Dynamics and Control of Polyhedral Spacecraft Proximity Operations Scaled Clohessy-Wiltshire Dynamics a Space Manipulator Capturing a Tethered Capture of Spinning Space Surface Robots with Control Moment Based on Conﬁdence Level on a Flat Air-bearing Testbed Rotating Object Debris Gyroscopes S. Ulrich, K. Hovell, Carleton University, M. Ciarcia, South Dakota State University, S. Wu, F. Mou, Tsinghua University, K. Hovell, S. Ulrich, Carleton University, D. Elliott, M. Peck, Cornell University, Ottawa, Canada Brookings, SD; R. Cristi, M. Romano, Naval Beijing, China; O. Ma, New Mexico State Ottawa, Canada Ithaca, NY Postgraduate School, Monterey, CA University, Las Cruces, NM Wednesday, 11 January 2017 260-GT-6/AMT-10 Test Technique and Data Analysis Improvements at the NASA Ames Unitary Plan Wind Tunnels I (Invited) Ft. Worth 6 Chaired by: J. ROSS, NASA Ames Research Center and K. JAMES 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs Oral Presentation AIAA-2017-1051 AIAA-2017-1052 AIAA-2017-1053 AIAA-2017-1054 AIAA-2017-1055 The NASA Ames Unitary Plan Wind Recent Advancements in the Model Deformation and Optical Stereo Photogrammetry Model Deformation Measurements Customer Guide to Pressure- Tunnels - A Facility Overview Infrared Flow Visualization System Angle of Attack Measurement Measurements of the Position and of the Truss-Braced Wing Aircraft Sensitive Paint Testing at NASA F. Kmak, NASA Ames Research Center, for the NASA Ames Unitary Plan System in the NASA Unitary Plan Attitude of a Nozzle-plume/Shock- in the NASA Ames 11-By 11-Ft Ames Unitary Plan Wind Tunnels Moffett Field, CA Wind Tunnels Wind Tunnel wave Interaction Model in the NASA Transonic Wind Tunnel N. Roozeboom, J. Baerny, NASA Ames T. Garbeff, NASA Ames Research Center, L. Kushner, AerospaceComputing, Inc., Ames 9- by 7- Ft Supersonic Wind B. Drain, L. Kushner, Aerospace Computing, Research Center, Moffett Field, CA Moffett Field, CA; J. Baerny, Jacobs, Mountain View, CA; E. Schairer, J. Heineck, Tunnel Inc., Mountain View, CA; E. Schairer, J. Moffett Field, CA J. Bell, NASA Ames Research Center, E. Schairer, NASA Ames Research Center, Heineck, NASA Ames Research Center, Moffett Field, CA Moffett Field, CA; L. Kushner, B. Drain, Moffett Field, CA AerospaceComputing, Inc., Moffett Field, CA; J. Heineck, D. Durston, NASA Ames Research Center, Moffett Field, CA Wednesday, 11 January 2017 261-GTE-6 Combustion Technologies, Emissions II San Antonio 4 Chaired by: S. JAMES, Honeywell Inc. 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2017-1056 AIAA-2017-1057 AIAA-2017-1058 AIAA-2017-1059 AIAA-2017-1060

Experimental Study on Lean Effects of CO2 additions on local Experimental study of the combustion Using LES Simulations to Predict On the Colorless Distributed Blowout of a High Temperature Rise ﬂame front structure in turbulent of kerosene and binary surrogate in Pilot Fuel Split Emissions Effects in Combustion Regime Combustor premixed ﬂames the model combustion chamber an Industrial Gas Turbine Combustor A. Khalil Hasan, A. Gupta, University of J. Suo, H. Yu, L. Zheng, Northwestern D. Han, A. Satija, J. Kim, R. Lucht, J. Gore, S. Matveev, I. Chechet, R. Zubrilin, V. with Automatic Meshing Maryland, College Park, College Park, MD

119 Polytechnical University, Xi’an, China Purdue University, West Lafayette, IN Abrashkin, S. Lukachev, S. Matveev, S. Drennan, G. Kumar, Convergent Science, Samara University, Samara, Russia Inc., New Braunfels, TX Wednesday, 11 January 2017 262-HSABP-5/PGC-4 Pressure Gain Combustion - Rotating Detonation Engines II Ft. Worth 3 Chaired by: D. PAXSON, NASA Glenn Research Center and S. CLAFLIN, Aerojet Rocketdyne 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2017-1061 AIAA-2017-1062 AIAA-2017-1063 AIAA-2017-1064 AIAA-2017-1065 Pressure Feedback in the Diffuser of Study on a Long-time Operation Evaluation of the unsteadiness Multi-beam Temperature Experimental Study of Rotating a Ram-RDE Propulsive Device Towards Rotating Detonation Rocket across nozzles downstream of Measurements in a Rotating Detonation Combustor Performance D. Schwer, Naval Research Laboratory, Engine Flight Demonstration rotating detonation combustors Detonation Engine Using H2O under Preheat and Back Pressure Washington, D.C.; T. Kaemming, Innovative K. Ishihara, J. Nishimura, K. Goto, S. J. Braun, J. Saavedra Garcia, G. Paniagua, Absorption Spectroscopy Operation Scientific Solutions, Inc., Dayton, OH; K. Nakagami, K. Matsuoka, J. Kasahara, Purdue University, West Lafayette, IN K. Rein, S. Roy, Spectral Energies, LLC, A. Roy, D. Ferguson, T. Sidwell, Kailasanath, Naval Research Laboratory, Nagoya University, Nagoya, Japan; et al. Dayton, OH; J. Hoke, Innovative Scientific B. O’Meara, P. Strakey, C. Bedick, Washington, D.C. Solutions, Inc., Dayton, OH; A. Caswell, National Energy Technology Laboratory, F. Schauer, J. Gord, Air Force Research Morgantown, WV; et al. Laboratory, Wright-Patterson AFB, OH Wednesday, 11 January 2017 263-IS-4 Adaptive and Intelligent Control Systems Ft. Worth 1 Chaired by: M. BALAS, Embry-Riddle Aeronautical University 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2017-1066 AIAA-2017-1067 AIAA-2017-1068 AIAA-2017-1069 AIAA-2017-1070 Parametrized Experience Exchange Gaussian Process-based Visual Intelligent Controller Selection for Human Demonstrations for Fast and Enhancement of Nonlinear Smooth in Expert – Fellow Swarm Robotic Servoing Framework for an Aerial Aggressive Quadrotor Manoeuvring Safe Exploration in Reinforcement Trackers Using Neural Network for System, Controller Performance Parallel Manipulator D. Molenkamp, E. Van Kampen, C. Learning Post LOC Autonomous Recovery of Context S. Cho, D. Shim, J. Kim, Korea Advanced de Visser, Q. Chu, Delft University of G. Schonebaum, J. Junell, E. Van Kampen, Flying Vehicles S. Amin, K. Ibrahem, A. Al-Naggar, A. Nabil, A. Institute of Science and Technology, Technology, Delft, The Netherlands Delft University of Technology, Delft, The J. Dongmo, JetMech, Inc., Nottingham, MD El-Sadek, M. Abdel-Galil, Zewail City of Science Daejeon, South Korea Netherlands and Technology, Giza, Egypt; et al. Wednesday, 11 January 2017 264-MDO-7 Aircraft Design Optimization II Mustang 1 Chaired by: T. TAKAHASHI, Arizona State University and G. KURUVILA, Boeing Research & Technology 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2017-1071 AIAA-2017-1072 AIAA-2017-1073 AIAA-2017-1074 Optimal design of insect wing shape Conceptual Design of a Blended- Multidisciplinary Design High-Performance Aircraft Through for hovering nano air vehicles Wing-Body Tilt-Arm Hybrid Optimization of Air-based Battery Innovative Development Process G. Throneberry, M. Hassanalian, A. Unmanned Aerial Vehicle Thermal Management System in and Methods Abdelkefi, New Mexico State University, R. Abnous, C. Zeng, S. Chowdhury, Electric Vehicles F. Daoud, Airbus, Manching, Germany Las Cruces, NM University at Buffalo, Buffalo, NY; V. M. Li, J. Zhang, University of Texas, Dallas, Maldonado , P. Mancuso, University of Richardson, TX Texas, San Antonio, San Antonio, TX Wednesday, 11 January 2017 265-MST-5 Aviation Simulation Scenario Development I San Antonio 2 Chaired by: U. DURAK, DLR-German Aerospace Center and S. JAFER, Embry-Riddle Aeronautical University 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs Introduction AIAA-2017-1075 AIAA-2017-1076 AIAA-2017-1077 AIAA-2017-1078 Panel Discussion Scenario Development Process at Using System Entity Structures to Creating Scenarios for Airport The Use of Data from Accident the Vertical Motion Simulator Model the Elements of a Scenario in a Management Simulations Involving Investigations in Development of S. Reardon, NASA Ames Research Center, Research Flight Simulator Independent Connected Simulators Simulator Training Scenarios Moffett Field, CA; E. Lewis, SAIC, Moffett U. Durak, I. Pruter, T. Gerlach, German R. Suikat, T. Stelkens-Kobsch, F. Stiekel, D. Crider, National Transportation Safety Field, CA; S. Beard, NASA Ames Research Aerospace Center (DLR), Braunschweig, H. Lenz, German Aerospace Center (DLR), Board, Washington, D.C. Center, Moffett Field, CA Germany; S. Jafer, Embry-Riddle Aeronautical Braunschweig, Germany University, Daytona Beach, FL; T. Pawletta, University of Wismar, Wismar, Germany; S. Hartmann, Clausthal University of Technology, 120 Clausthal-Zellerfeld, Germany Wednesday, 11 January 2017 266-MST-6 Human Factors, Perception, Cueing I San Antonio 1 Chaired by: F. CARDULLO, State University of NY and D. CARTMELL, Boeing Engineering Operations & Technology 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2017-1079 AIAA-2017-1080 AIAA-2017-1081 AIAA-2017-1082 AIAA-2017-1083 AIAA-2017-1084 Evaluation of a Steep Turn Spatial Evaluation of a Missed Approach/ Refinement of Objective Motion An Objective Method to Determine Experimental evaluation of haptic Assessing the severity of wake Disorientation Demonstration Go-Around Spatial Disorientation Cueing Criteria Based on Three the Fidelity of Rotorcraft Motion support systems for learning a encounters in various aircraft types in Scenario for Commercial Pilot Demonstration Scenario for Flight Tasks Platforms 2-DoF tracking task piloted flight simulations Training Commercial Pilot Training P. Zaal, San Jose State University, Moffett M. Jones, German Aerospace Center (DLR), G. D’Intino, M. Olivari, S. Geluardi, J. G. Van Baren, National Aerospace Laboratory D. Klyde, A. Lampton, P. Schulze, Systems A. Lampton, D. Klyde, P. Schulze, Systems Field, CA; J. Schroeder, Federal Aviation Braunschweig, Germany Venrooij, Max Planck Institute for Biological (NLR), Amsterdam, The Netherlands; V. Technology, Inc., Hawthorne, CA Technology, Inc., Hawthorne, CA Administration, Moffett Field, CA; W. Cybernetics, Tübingen, Germany; L. Pollini, Treve, F. Rooseleer, EUROCONTROL, Brussels, Chung, SAIC, Moffett Field, CA University of Pisa, Pisa, Italy; H. Buelthoff, Belgium; P. Van der Geest, B. Heesbeen, Max Planck Institute for Biological National Aerospace Laboratory (NLR), Cybernetics, Tübingen, Germany Amsterdam, The Netherlands Wednesday, 11 January 2017 267-MST-7 Modeling and Simulation of Air Traffic Management II San Antonio 3 Chaired by: B. APONSO, NASA Ames Research Center 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2017-1085 AIAA-2017-1086 AIAA-2017-1087 AIAA-2017-1088 Integrated Arrival-Departure-Surface- Severe-Weather Avoidance using Merging Optimization Method Feasibility Study on Constrained Enroute Air Traffic Optimization Bezier Curve-based Trajectory Application to Arrival Scheduling Optimal Trajectory Application in P. Dutta, Optimal Synthesis, Inc., Los Altos, Planning for Arrival Air Traffic Algorithm for Parallel Runways the Japanese Airspace CA; P. Sengupta, Swift Navigation, San Management D. Toratani, N. Wickramasinghe, E. Itoh, N. Wickramasinghe, M. Brown, H. Francisco, CA; J. Kwan, P. Menon, Optimal S. Izuta, M. Takahashi, Keio University, National Institute of Maritime, Port and Hirabayashi, S. Nagaoka, Electronic Synthesis, Inc., Los Altos, CA Yokohama, Japan Aviation Technology, Chofu, Japan Navigation Research Institute, Tokyo, Japan Wednesday, 11 January 2017 268-NDA-5 Special Session: DARPA Efficient Quantification of Uncertainty in Physical Systems (EQUiPS) Program I Mustang 2 Chaired by: F. FAHROO and P. BERAN, US Air Force Research Laboratory(AFRL/RQVC) 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2017-1089 AIAA-2017-1090 AIAA-2017-1091 AIAA-2017-1092 AIAA-2017-1093 AIAA-2017-1094 Global Sensitivity Analysis and Developing Design Insight Through An Inadequacy Formulation for an The game theoretic approach to Uncertainty Modeling using Mixture A Multi-Fidelity Collocation Method Quantification of Model Error for Large Active Subspaces Uncertain Flamelet Model Uncertainty Quantification, reduced Distributions for Decision-Based for Time-Dependent Parameterized Eddy Simulation in Scramjet Design Z. del Rosario, Stanford University, D. Sondak, T. Oliver, C. Simmons, R. Moser, order modeling and numerical analysis Design Problems X. Huan, C. Safta, K. Sargsyan, G. Geraci, Stanford, CA; P. Constantine, Colorado University of Texas, Austin, Austin, TX H. Owhadi, California Institute of V. Pandey, Oakland University, Rochester, MI X. Zhu, D. Xiu, University of Utah, Salt M. Eldred, Z. Vane, Sandia National School of Mines, Golden, CO; G. Iaccarino, Technology, Pasadena, CA Lake City, Salt Lake City, UT Laboratories, Livermore, CA; et al. Stanford University, Stanford, CA Wednesday, 11 January 2017 269-NDA-6 Special Session: Non-Deterministic Approaches for Aerospace Human-in-the-Loop Related Missions Mustang 3 Chaired by: E. SUHIR and W. GERSTENMAIER, NASA 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2017-1095 AIAA-2017-1096 AIAA-2017-1097 AIAA-2017-1098 AIAA-2017-1099 Electronics Probabilistic/Prognostics, A Method for the Integration of Accounting for the Speed-Accuracy And the Humans Saves the Day or Towards a Framework for Reliability a Qualification Paradigm Shift Real-time Probabilistic Approaches Trade-off in Quantifying Human-in- Maybe They Ruin It, The Importance and Safety Analysis of Complex with HITL for Astronaut Wellness in Human the-Loop Error Probabilities of Humans in the Loop Space Missions R. Ghaffarian, Jet Propulsion Laboratory, in the Loop Related Missions and A. Ahumada, B. Beard, NASA Ames D. DeMott, SAIC, Houston, TX; R. Boyer, J. Evans, F. Groen, NASA Headquarters, California Institute of Technology, Situations with Big Data Analytics Research Center, Moffett Field, CA; C. M. Bigler, NASA Johnson Space Center, Washington, D.C.; L. Wang, NASA Johnson Pasadena, CA C. McGregor, University of Ontario, Null, NASA Langley Research Center, Houston, TX Space Center, Houston, TX; R. Austin, A. Oshawa, Canada; O. Orlov, R. Baevsky, A. Hampton, VA Witulski, Vanderbilt University, Institute for Chernikova, V. Rusanov, Russian Academy Space and Defense Electronics, Nashville, of Sciences, Moscow, Russia TN; S. Cornford, Jet Propulsion Laboratory, California Institute of Technology, 121 Pasadena, CA; et al. Wednesday, 11 January 2017 270-PC-17 Combustion Dynamics II Dallas 7 Chaired by: E. BARBOUR, The Aerospace Corpation and K. MCMANUS, GE Global Research Center 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2017-1100 AIAA-2017-1101 AIAA-2017-1102 AIAA-2017-1103 Perturbation Dynamics in Turbulent Evaluating Combustion Instability in Self-induced transitions between stable The instability characteristics of lean Flames a Swirl-Stabilized Combustor Using and thermoacoustically excited states premixed hydrogen and syngas M. Hassanaly, V. Raman, University of Simultaneous Pressure, Temperature, in a model swirl-stabilized burner at flames stabilized on meso-scale Michigan, Ann Arbor, Ann Arbor, MI and Chemiluminescense Measurements elevated pressure bluff-body at High Repetition Rates I. Boxx, K. Geigle, German Aerospace Center Y. Kim, B. Lee, H. Im, King Abdullah J. Monfort, S. Stouffer, T. Hendershott, (DLR), Stuttgart, Germany; C. Carter, Air Force University of Science and Technology, University of Dayton, Dayton, OH; P. Research Laboratory, Wright-Patterson AFB, Thuwal, Saudi Arabia Wrzesinski, W. Foley, Air Force Research OH; M. Yang, J. Lewalle, B. Kumgeh, Syracuse Laboratory, Wright-Patterson AFB, OH; K. Rein, University, Syracuse, NY Spectral Energies, LLC, Beavercreek, OH Wednesday, 11 January 2017 271-PC-18 Super-Critical Combustion San Antonio 6 Chaired by: J. BELLAN, Jet Propulsion Laboratory and L. BAUWENS, University of Calgary 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs Oral Presentation AIAA-2017-1104 AIAA-2017-1105 AIAA-2017-1106 AIAA-2017-1107 AIAA-2017-1108 Invited Review:Supercritical Computational Modeling of Large Eddy Simulations of high Seven questions about supercritical Flow Dynamics of Gaseous Oxygen/ Numerical Simulation for Effects of Combustion Modeling and Supercritical and Transcritical Flows pressure jets: Effect of subgrid scale fluids - towards a new fluid state Kerosene Jet-Swirl Injectors at Pressure on Cryogenic Coaxial Jet Simulation: Recent Advances M. Harvazinski, Air Force Research Laboratory, modeling diagram Supercritical Conditions under Supercritical Pressure V. Yang, Georgia Institute of Technology, Edwards AFB, CA; G. Lacaze, J. Oefelein, A. Gnanaskandan, California Institute of D. Banuti, M. Raju, P. Ma, M. Ihme, Y. Li, X. Wang, L. Zhang, S. Yeh, V. Yang, T. Araki, D. Muto, Kyushu Institute of Atlanta, GA Sandia National Laboratories, Livermore, CA; Technology, Pasadena, CA; J. Bellan, Jet Stanford University, Stanford, CA; J. Hickey, Georgia Institute of Technology, Atlanta, GA Technology, Fukuoka, Japan; H. Terashima, S. Sardeshmukh, Purdue University, West Propulsion Laboratory, California Institute of University of Waterloo, Waterloo, Canada Hokkaido University, Sapporo, Japan; N. Lafayette, IN; V. Sankaran, Air Force Research Technology, Pasadena, CA Tsuboi, Kyushu Institute of Technology, Laboratory, Edwards AFB, CA Fukuoka, Japan Wednesday, 11 January 2017 272-PC-19 Model Validation for Propulsion Workshop: Opening Session San Antonio 5 0930 - 1230 hrs The Model Validation for Propulsion (MVP) workshop is an open forum, bringing together researchers and modelers to help improve our understanding and capabilities of modeling turbulent reacting flows in relevant aerospace propulsion systems. This session introduces the objectives of the workshop and is followed by a panel discussion on Validation Metrics and Experimental Interactions. Wednesday, 11 January 2017 273-PDL-6 Plasma-Based Flow Control: Lessons Learned and Prospects I (Invited) Ft. Worth 4 Chaired by: S. LEONOV, University of Notre Dame and J. POGGIE, Purdue University- Sch of Aero and Astro 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs Oral Presentation Oral Presentation Oral Presentation Oral Presentation Oral Presentation Oral Presentation Plasma Aerodynamics – Recent Applications of Plasma-Based Modeling Laser Discharge in Computational Modeling of Plasma- Turbulent Boundary Layer Drag Nanosecond Pulse Surface 122 Developments and Future Prospects Aerodynamic Flow Control for Quiescent Air Based Control in High-Speed Flow Reduction Through Plasma Streak Discharges for Control of Turbulent K. Choi, J. Kim, University of Nottingham, Understanding of Flow Physics D. Knight, N. Kianvashrad, Rutgers J. Poggie, Purdue University, West Transient Growth Instability Control Shear Flows Nottingham, United Kingdom M. Samimy, Ohio State University, University, New Brunswick, NJ; S. Lafayette, IN T. Corke, F. Thomas, A. Duong, R. J. Little, University of Arizona, Tucson, Columbus, OH Wilkinson, A. Chou, G. Herring, R. McGowan, University of Notre Dame, Notre Tucson, AZ Horne, NASA Langley Research Center, Dame, IN Hampton, VA Wednesday, 11 January 2017 274-PDL-7 Plasma and Laser Physics I Ft. Worth 5 Chaired by: L. RAJA, University of Texas at Austin and A. YALIN, Colorado State University 0930 hrs 1030 hrs 1100 hrs 1130 hrs Oral Presentation AIAA-2017-1109 AIAA-2017-1110 AIAA-2017-1111 The Development and Physics of High Power Lasers - Myths, Legends, and Kinetic Mechanism of Plasma NS Dielectric Barrier Discharge FEM Simulation of Laser-Induced Facts; From SDI to Tactical Battlefield Lasers - Reflections of a ‘Star Warrior’ Recombination in Methane, Ethane Development and Thrust Generation Plasma Breakdown Experiments for J. Horkovich, Schafer Corporation Military Aerospace, Albuquerque, NM and Propane after High-Voltage in 4-Electrode Geometry Combustion Applications Nanosecond Discharge A. Starikovskiy, Princeton University, A. Alberti, A. Munafò, A. Sahai, C. Pantano, A. Starikovskiy, Princeton University, Princeton, NJ M. Panesi, University of Illinois, Urbana- Princeton, NJ Champaign, Urbana, IL Wednesday, 11 January 2017 275-SCS-4 Membrane-Based Deployable Systems Palomino 1 Chaired by: J. MOORE and J. SAUDER, Jet Propulsion Laboratory 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2017-1112 AIAA-2017-1113 AIAA-2017-1114 AIAA-2017-1115 AIAA-2017-1116 AIAA-2017-1117 Data Driven Model for Efficient Investigation of the Deformation Verification of the Similarity Rules Vibration Response of Ultralight In-space Shape Measurement of Super Pressure Balloon with Prediction and Estimation of Spin and Stiffness of Spinning Solar Sail for Spin Deployment Membrane in Wrapped Spacecraft Structures Large Planar Structures Diamond-Shaped Net: A Numerical Type Membrane Space Structure Membrane of IKAROS the ground experiment J. Umali, Northrop Grumman Corporation, T. Talon, S. Pellegrino, California Institute Study of its Structural Characteristics Dynamics N. Okuizumi, Y. Satou, O. Mori, Japan Y. Tatematsu, T. Suzuki, M. Yamazaki, Y. Azusa, CA; L. Wilson, S. Pellegrino, of Technology, Pasadena, CA K. Nakashino, Tokai University, Kanagawa, M. Yamazaki, Nihon University, Chiba, Aerospace Exploration Agency (JAXA), Miyazaki, Nihon University, Funabashi, California Institute of Technology, Japan; Y. Saito, K. Goto, Japan Aerospace Japan Sagamihara, Japan; H. Sakamoto, Tokyo Japan Pasadena, CA Exploration Agency (JAXA), Kanagawa, Japan; Institute of Technology, Okayama, Japan; D. Akita, Tokyo Institute of Technology, Tokyo, H. Furuya, Tokyo Institute of Technology, Japan; T. Matsuo, Meiji University, Kanagawa, Yokohama, Japan Japan; K. Matsushima, Fujikura Parachute Company, Ltd., Hukushima, Japan; et al. Wednesday, 11 January 2017 276-SD-13 Flutter and Aeroelastic Analysis I Appaloosa 2 Chaired by: W. SU, University of Alabama, Tuscaloosa and H. KIM, Boeing Defense, Space & Security 0930 hrs 1000 hrs 1030 hrs AIAA-2017-1118 AIAA-2017-1119 AIAA-2017-1120 Panel Flutter Analysis and Optimization Active Flutter Suppression: State of Optimisation of an Aeroelastic of Composite Tow Steered Plates the Art and Technology Maturation Flutter Energy Harvester T. Guimaraes, Federal University of Uberlândia, Needs L. Grainger, D. Rezgui, D. Barton, Uberlândia, Brazil; S. Castro, Embraer, E. Livne, University of Washington, Seattle, University of Bristol, Bristol, United São José dos Campos, Brazil; D. Rade, Seattle, WA Kingdom Technological Institute of Aeronautics (ITA), São 123 José dos Campos, Brazil; C. Cesnik, University of Michigan, Ann Arbor, Ann Arbor, MI Wednesday, 11 January 2017 277-SD-14 Dynamic Testing Techniques and System Identification I Appaloosa 3 Chaired by: T. KINNEY, NASA-Kenndey Space Center and R. MALLA, University of Connecticut 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2017-1121 AIAA-2017-1122 AIAA-2017-1123 AIAA-2017-1124 AIAA-2017-1125 Evolution of the Laser Vibrometer Structural Dynamic Model Experimental Characterization Development of a Stress Limit Finite Element Model Updating for Structural Dynamic Testing Identification Using Time and Computational Modeling of Surface for Turbine Blades under using Adjoint Based Sensitivity J. Kosmatka, B. Martins, University of Transformation Method Nonlinear Dynamics for F-16 Multimode Forced Vibration for Use Analysis California, La Jolla, La Jolla, CA; M. Pineda, J. Wang, Beijing Institute of Structure & Substructures in Engine Testing R. Prasad, H. Kim, S. Choi, Virginia Polytec, Inc., Irvine, CA Environment, Beijing, China; F. Wei, Central A. Ricciardi, D. Coleman, C. Denegri, Air A. Kamaraj, V. Yadav, S. Venkataraman, Polytechnic Institute and State University, Connecticut State University, New Britain, CT Force SEEK EAGLE Office, Eglin AFB, FL San Diego State University, San Diego, CA Blacksburg, VA Wednesday, 11 January 2017 278-SD-15 Dynamics and Structural Dynamics of Launch Vehicles Appaloosa 4 Chaired by: B. WILLIS, Jacobs Technology and R. RUSOVICI, Florida Institute of Technology 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2017-1126 AIAA-2017-1127 AIAA-2017-1128 AIAA-2017-1129 AIAA-2017-1130 AIAA-2017-1131 Bending Vibration Monitoring Development of Three-dimensional Using Dispersed Modes During Experimental Investigations on Reduced Order Modeling of SLS Pre- Structural and Acoustic Boundary for Flexible Rockets through a Structural Analysis for Engine Model Correlation dynamic aeroelastic Stability of Burner to Enable Rapid Transient Condition Assessment for Vibro- Reference Strain Structure Nozzle Using Anisotropic Facet Shell E. Stewart, M. Hathcock, NASA Marshall Panels in the Transonic Domain Analysis Acoustic Analysis of Spacecraft N. Tsushima, W. Su, University of Alabama, Element Space Flight Center, Huntsville, AL J. Lübker, German Aerospace Center (DLR), A. Brown, A. Mulder, NASA Marshall Space Reflectors using Acoustic Boundary Tuscaloosa, Tuscaloosa, AL; M. Wolf, NASA S. Kim, H. Cho, H. Joo, S. Shin, Seoul Göttingen, Germany Flight Center, Huntsville, AL Element Method Kennedy Space Center, Cape Canaveral, FL; National University, Seoul, South Korea D. Inoyama, T. McQuigg, J. Francis, T. E. Griffin, a.i. solutions, Inc., Cape Canaveral, Stoumbos, Orbital ATK, Dulles, VA FL; J. Whittaker, NASA Kennedy Space Center, Cape Canaveral, FL; M. Dumoulin, a.i. solutions, Inc., Cape Canaveral, FL Wednesday, 11 January 2017 279-SEN-3 Applications of Sensor and Information Fusion Ft. Worth 2 Chaired by: D. ACCARDO, University of Naples 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2017-1132 AIAA-2017-1133 AIAA-2017-1134 AIAA-2017-1135 Cooperative Searching Strategies Real-Time Radar-Based Tracking Improving Inertial Attitude Prediction of Cognitive States during for Distributed Sensor Networks and State Estimation of Multiple Measurement Performance by Flight Simulation using Multimodal T. Frey, D. Faulk, Lockheed Martin Non-Conformant Aircraft Exploiting MEMS Gyros and Neural Psychophysiological Sensing Corporation, Fort Worth, TX B. Cook, T. Arnett, O. Macmann, M. Kumar, Thermal Calibration A. Harrivel, C. Stephens, R. Milletich, C. University of Cincinnati, Cincinnati, OH R. Fontanella, D. Accardo, University of Naples Heinich, M. Last, N. Napoli, NASA Langley “Federico II”, Naples, Italy; E. Caricati, S. Research Center, Hampton, VA; et al. Cimmino, MBDA, Bacoli, Italy; D. De Simone, G. Lucignano, GMA S.r.l., Giugliano, Italy Wednesday, 11 January 2017 280-STR-8 Buckling, Fatigue and Fracture of Structures II Appaloosa 1 Chaired by: M. WOLFF, Gulfstream Aerospace Corporation and J. MIN, NASA Glenn Research Center 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2017-1136 AIAA-2017-1137 AIAA-2017-1138 AIAA-2017-1139 AIAA-2017-1140 Investigation of Hybridization and Buckling Analysis of Stiffened Peridynamic Unit Cell Comparison of Finite Element Strain Peridynamic Modeling of Fatigue Architectural Effects on Tensile Panels Using Mechanics of Structure Homogenization Distribution to In Situ Strain Field of Damage in Notched Composite Response of Hybrid 3D Woven Genome E. Madenci, University of Arizona, Tucson, a Plastically-Deformed Plate Laminates Textile Composites using NCYL N. Liu, W. Yu, Purdue University, West Tucson, AZ; A. Barut, Global Engineering K. Knapp, A. Palazotto, Air Force Institute Y. Hu, E. Madenci, University of Arizona, Multiscale Method Lafayette, IN Research and Technologies, Tucson, AZ; of Technology, Wright-Patterson AFB, OH; Tucson, Tucson, AZ A. Waas, University of Washington, N. Phan, Naval Surface Warfare Center, O. Scott-Emuakpor, Air Force Research Seattle, Seattle, WA; D. Patel, University Patuxent River, MD Laboratory, Wright-Patterson AFB, OH

124 of Michigan, Ann Arbor, Ann Arbor, MI; C. Yen, Army Research Laboratory, Aberdeen Proving Ground, MD Wednesday, 11 January 2017 281-SUR-1 Survivability Palomino 2 Chaired by: S. BROUSSARD, The Boeing Co and M. SCHUCK, SURVICE Engineering Company 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2017-1141 AIAA-2017-1142 AIAA-2017-1143 AIAA-2017-1144 Research on Space Debris Protection Analysis of the Effects of Additive Additively Manufactured CFD Analysis and Shape and Removal Strategy Based on Manufacturing on the Material Penetrators Optimization of the Internal Space Station Platform Properties of 15-5PH Stainless Steel Z. Provchy, A. Palazotto, Air Force Institute Convective Cooling System of a M. Liu, China Academy of Space E. Lum, A. Palazotto, A. Dempsey, Air Force of Technology, Wright-Patterson AFB, OH Hypersonic Vehicle Technology (CAST), Beijing, China; Z. Zhu, Institute of Technology, Wright-Patterson K. Liu, D. Stelzer, Air Force Institute of York University, Toronto, Canada AFB, OH Technology, Wright-Patterson AFB, OH Wednesday, 11 January 2017 282-TP-9 Aerothermodynamics III Austin 3 Chaired by: D. KUNTZ, Sandia National Laboratories and W. FLAHERTY, MIT 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2017-1145 AIAA-2017-1146 AIAA-2017-1147 AIAA-2017-1148 AIAA-2017-1149 Benchmark EAST Experiments for Inviscid/Boundary-Layer Dependence of the Parameters of Computation of Rarefaction Effects Best Practices for Unstructured Grid Earth Re-Entry Aeroheating Approach for Shock Layer for Super-Orbital Space on a Blunt Body in Hypersonic Flow Shock Fitting A. Brandis, B. Cruden, Analytical Mechanics Integrated Vehicle Design Vehicles at Increasing of Entry Velocity G. Huang, R. Agarwal, Washington P. McCloud, NASA Johnson Space Center, Associates, Inc., Moffett Field, CA E. Lee, K. Wurster, NASA Langley Research S. Surzhikov, Russian Academy of University in St. Louis, St. Louis, MO Houston, TX Center, Hampton, VA Sciences, Moscow, Russia Wednesday, 11 January 2017 283-UMS-8 UAS Self-Separation and Collision Avoidance II Grapevine 1 Chaired by: M. LOGAN, NASA Langley Research Center and R. STANSBURY, Embry-Riddle Aeronautical University 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2017-1150 AIAA-2017-1151 AIAA-2017-1152 AIAA-2017-1153 AIAA-2017-1154 Autonomous Stereo Vision based Sense and Avoid for Small Small Aircraft Flight Encounters UAV Collision Detection and ADS-B Surveillance System Collision Avoid System for Small Unmanned Aircraft Systems Database for UAS Sense and Avoid Avoidance using ADS-B Sensor and Performance With Small UAS at Low UAV C. Dolph, National Institute of Aerospace, H. McClelland, C. Kang, C. Woolsey, Custom ADS-B Like Solution Altitudes Y. Lyu, Q. Pan, C. Zhao, J. Hu, Hampton, VA; M. Logan, L. Glaab, NASA Virginia Polytechnic Institute and State S. Bhandari, N. Curtis-Brown, I. Guzman, M. Guterres, S. Jones, G. Orrell, R. Strain, Northwestern Polytechnical University, Langley Research Center, Hampton, VA; University, Blacksburg, VA; A. Roberts, D. T. Sherman, J. Tellez, E. Gomez, California MITRE Corporation, McLean, VA Xi’an, China T. Vranas, National Institute of Aerospace, Buck, T. Cheney, Brigham Young University, State Polytechnic University, Pomona, Hampton, VA; R. McSwain, NASA Langley Provo, UT; et al. Pomona, CA Research Center, Hampton, VA; Z. Johns, National Institute of Aerospace, Hampton, VA Wednesday, 11 January 2017 284-UMS-9 UAS Technologies and Applications I Grapevine 2 Chaired by: O. ARIFF, University of Salford and S. SMITH, University of Kentucky 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2017-1155 AIAA-2017-1156 AIAA-2017-1158 AIAA-2017-1157 AIAA-2017-1159 3-D Mapping using LIDAR and Catalyzing Collaboration for Multi- Autonomous System for Rapid A Swarm-Intelligence Approach to Design of a Modular Offline Autonomous Unmanned Aerial Disciplinary UAS Development with Airfield Assessment Oil Spill Mapping using Unmanned Reconfigurable Unmanned Aerial Vehicle a Flight Campaign Focussed on M. Anderson, P. Pasque, C. Lane, J. Aerial Vehicles Vehicle C. Carreon-Limones, A. Rashid, P. Chung, Meteorology and Atmospheric Physics Pond, U.S. Air Force Academy, Colorado Z. Ball, P. Odonkor, S. Chowdhury, State B. Rinauto, S. Gupta, S. Chowdhury, State S. Bhandari, California State Polytechnic S. Smith, University of Kentucky, Lexington, Springs, CO University of New York, Buffalo, NY University of New York, Buffalo, NY; V. University, Pomona, Pomona, CA Lexington, KY; P. Chilson, University of Maldonado , University of Texas, San Oklahoma, Norman, Norman, OK; A. Houston, Antonio, San Antonio, TX 125 University of Nebraska, Lincoln, Lincoln, NE; J. Jacob, Oklahoma State University, Stillwater, OK Wednesday, 11 January 2017 285-WE-5 Atmospheric Inflow and Turbulence for Wind Energy Texas D Chaired by: M. CHURCHFIELD, National Renewable Energy Laboratory and P. VEERS, National Renewable Energy Laboratory 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2017-1160 AIAA-2017-1161 AIAA-2017-1162 AIAA-2017-1163 AIAA-2017-1164 AIAA-2017-1165 Large Eddy Simulation of Wind Flow Large eddy simulation of Numerical Modeling Framework for Development of a Wind Plant Large- Subfilter Scale Enrichment of Wind Incorporating realistic geophysical Over Complex Terrain: The Bolund atmospheric boundary layer flows Wind Turbine Analysis & Atmospheric Eddy Simulation with Measurement- Farm LES using discrete Fourier- effects of mean wind from LIDAR Hill Case over complex terrain with varying Boundary Layer Interaction Driven Atmospheric Inflow Gabor Modes measurements in Large Eddy R. Roy, M. Stoellinger, University of stability conditions M. Siddiqui, Norwegian University of Science E. Quon, M. Churchfield, S. Lee, National A. Ghate, S. Lele, Stanford University, Simulation of Wind Turbine Arrays Wyoming, Laramie, Laramie, WY Y. Han, M. Stoellinger, University of and Technology, Trondheim, Norway; A. Renewable Energy Laboratory, Golden, CO; L. Stanford, CA T. Chatterjee, N. Cherukru, Y. Peet, Wyoming, Laramie, Laramie, WY Rasheed, M. Tabib, SINTEF, Trondheim, Cheung, General Electric Company, Niskayuna, R. Calhoun, Arizona State University, Norway; T. Kvamsdal, Norwegian University of NY; S. Kern, General Electric Company, Munich, Tempe, AZ Science and Technology, Trondheim, Norway Germany Wednesday, 11 January 2017 286-WE-6 Wind Turbine Structural Dynamics and Damage Ft. Worth 7 Chaired by: D. GRIFFITH and D. CAIRNS, Montana State University 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2017-1166 AIAA-2017-1167 AIAA-2017-1168 AIAA-2017-1169 AIAA-2017-1170 Collapse of a 47-meter Composite Effect of Fiber Orientation of Effects of Fiber Misalignment on Multi-Dimensional Variational Mode Agile Airborne Wind Energy System Blade under Combined Bending and Bend-Twist Coupled Blades on the Composite Wind Turbine Rotor Decomposition Applied to Intrinsic Design with Birds Impact Detection Torsion during Full-scale Structural Structural Performance of the Wind Blades Vibration Mode Extraction for Bearing R. Albertani, A. Muschler, W. Maurer, Testing Turbine System W. Vanskike, R. Hale, University of Kansas, Crack Detection in Wind Turbines with Oregon State University, Corvallis, OR X. Chen, Chinese Academy of Sciences, O. Sener, T. Farsadi, A. Kayran, Middle East Lawrence, Lawrence, KS Large Speed Variation Beijing, China Technical University, Ankara, Turkey Z. Li, J. Yu, China University of Mining and Technology, Xuzhou, China; C. Hu, Iowa State University, Ames, IA; Z. Peng, University of New South Wales, Sydney, Australia Wednesday, 11 January 2017 287-LUNCH-3 Luncheon in the Exposition Hall Longhorn Hall E&F 1230 - 1400 hrs Wednesday, 11 January 2017 288-AA-8 Aeroacoustics - Fan Noise, Open Rotor Grapevine B Chaired by: S. RIZZI, NASA Langley Research Center and J. MENDOZA, United Technologies Research Center 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2017-1171 AIAA-2017-1172 AIAA-2017-1173 AIAA-2017-1174 AIAA-2017-1175 AIAA-2017-1176 Validating the Harmonic Balance Sound Radiation from a Rotor A Comparison of the Aerodynamic Acoustic Characterization of a Multi- Tractor Propeller–Pylon Interaction, Tractor Propeller-Pylon Interaction, Method for Turbomachinery Tonal Operating in the Wake of a Cylinder Performance and Aeroacoustic Rotor UAS as a First Step Towards Part I: Characterization of Unsteady Part II:Mitigation of Unsteady Pylon

126 Noise Predictions S. Glegg, J. Grant, Florida Atlantic Behavior of Commercial and Custom Noise Reduction Pylon Loading Loading by Application of Leading- D. Lindblad, N. Andersson, Chalmers University, Boca Raton, FL; W. Devenport, Designed Quadcopter Propellers J. Feight, S. Whyte, J. Jacob, R. Gaeta, R. de Vries, T. Sinnige, B. Della Corte, Edge Porosity University of Technology, Göteborg, W. Alexander, Virginia Polytechnic Institute C. Wisniewski, A. Byerley, U.S. Air Force Oklahoma State University, Stillwater, OK F. Avallone, D. Ragni, G. Eitelberg, Delft B. Della Corte, T. Sinnige, R. de Vries, F. Sweden and State University, Blacksburg, VA Academy, Colorado Springs, CO; K. Van University of Technology, Delft, The Avallone, D. Ragni, G. Eitelberg, Delft University Treuren, A. Hays, Baylor University, Waco, TX Netherlands; et al. of Technology, Delft, The Netherlands; et al. Wednesday, 11 January 2017 289-AA-9 Aeroacoustics - Airframe and Community Noise Grapevine 3 Chaired by: W. SCHUSTER, Honeywell International, Inc. and E. NESBITT, Boeing Commercial Airplanes 1400 hrs 1430 hrs 1500 hrs 1530 hrs AIAA-2017-1177 AIAA-2017-1178 AIAA-2017-1179 AIAA-2017-1180 Owl-Inspired Trailing Edge Noise Investigation of Passive Flow The HELINOIR Aeroacoustic Code Optimal Flight Trajectory to Treatments: Acoustic and Flow Control of Cavity Acoustics Using and its Application to Active/Passive Minimize Noise During Landing Measurements Dynamic Pressure-Sensitive Paint Helicopter Noise Reduction J. Udani, K. Mall, M. Grant, D. Sun, Purdue A. Millican, I. Clark, W. Devenport, Virginia J. Crafton, S. Stanfield, N. Rogoshchenkov, M. Chia, K. Duraisamy, P. Friedmann, A. University, West Lafayette, IN Polytechnic Institute and State University, Innovative Scientific Solutions, Inc., Padthe, University of Michigan, Ann Arbor, Blacksburg, VA Dayton, OH; R. Schmit, Air Force Research Ann Arbor, MI Laboratory, Wright-Patterson AFB, OH Wednesday, 11 January 2017 290-ACD-7 Electric Aircraft Design San Antonio 5 Chaired by: R. MCDONALD, California Polytechnic State University-San Luis Obispo and I. CHAKRABORTY, ASDL, Georgia Tech 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs AIAA-2017-1181 AIAA-2017-1182 AIAA-2017-1183 AIAA-2017-1184 AIAA-2017-1185 Design Space Investigation for a Development of Parametric Power Sizing, Integration and Performance Sparky Flapjack: Aircraft Design Sizing Methods for Aircraft of Small Electric General Aviation Generation and Distribution Evaluation of Hybrid Electric Inspirations from the Vought 173 Variable Propulsion System Airplane Subsystem Models at Conceptual Propulsion Subsystem Architectures D. Raymer, Conceptual Research Complexity C. Brooks, S. Salgueiro, Massachusetts Aircraft Design Stage G. Cinar, D. Mavris, Georgia Institute of Corporation, Playa del Rey, CA; M. Zhang, J. Vegh, T. MacDonald, A. Wendorff, J. Institute of Technology, Cambridge, MA G. Cinar, D. Mavris, Georgia Institute of Technology, Atlanta, GA; M. Emeneth, A. A. Rizzi, E. Raymer, Airinnova, Stockholm, Alonso, Stanford University, Stanford, CA Technology, Atlanta, GA; M. Emeneth, A. Schneegans, PACE America, Inc., Seattle, Sweden Schneegans, PACE America, Inc., Seattle, WA; C. Riediger, 328 Design GnbH, WA; Y. Fefermann, Safran Tech, Magny-Les- Wessling, Germany; Y. Fefermann, Safran Hameaux, France Tech, Magny-Les-Hameaux, France; et al. Wednesday, 11 January 2017 291-AFM-6 Aircraft Flight Dynamics, Handling Qualities, and Performance I Grapevine 5 Chaired by: H. CHEN, Beihang University and C. KARLGAARD, Analytical Mechanics Associates Inc 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs AIAA-2017-1186 AIAA-2017-1187 AIAA-2017-1188 AIAA-2017-1189 AIAA-2017-1190 Cyclic Blade Pitch Control for Small System Identification of a Multi- Handling Qualities Metrics for Small Measuring Atmospheric Winds from Uncertainty Analysis of Avian UAV Without a Swashplate rotor UAV Actuator VTOL UAVs in Precision and Agile Quadrotor Motion Approach to Remote Thermal J. Paulos, M. Yim, University of M. Cunningham, J. Hubbard, University of Maneuvering Tasks J. Gonzalez-Rocha, C. Woolsey, C. Updraft Detection for Unmanned Pennsylvania, Philadelphia, PA Maryland, College Park, College Park, MD M. Abdulrahim, J. Dee, J. Grzywna, Prioria Sultan, Virginia Polytechnic Institute and Aerial Vehicles Robotics, Inc., Gainesville, FL State University, Blacksburg, VA; S. de C. Pinkerman, T. O’Connell, A. Arena, Wekker, N. Rose, University of Virginia, Oklahoma State University, Stillwater, OK Charlottesville, Charlottesville, VA 127 Wednesday, 11 January 2017 292-APA-27 Special Session: CREATE-AV HPC Multiphysics III Dallas 1 Chaired by: N. HARIHARAN, CREATE-AV and A. WISSINK, US Army Aeroflightdynamics Directorate 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs Oral Presentation AIAA-2017-1191 AIAA-2017-1192 AIAA-2017-1193 AIAA-2017-1194 AIAA-2017-1195 On Changing Paradigms – Motive Kestrel Modeling and Simulation Results from HPCMP CREATETM-AV Development of a Dual-Mesh On the Accuracy and Convergence CREATE-AV DaVinci 4.0 Capabilities Resonant Catalysts, Sentient Flutter Evaluation for Fighter COFFE for 3-D Aircraft Configurations Computational Fluid Dynamics of a Hamiltonian-Strand Approach and DaVinci 5.0 Development Subroutines, and Multi-Disciplinary, Aircraft with Meshes Generated by HPCMP Platform for Internal Reacting Flows for Aerodynamic Flows J. Livingston, Riverside Research, Physics-Based Simulation Software J. Dubben, C. Lillian, Air Force SEEK EAGLE CREATE™-MG Capstone N. Mundis, M. Harvazinski, K. Brown, Y. Jung, B. Govindarajan, J. Baeder, Beavercreek, OH R. Meakin, HPCMP CREATE-AV, Lorton, VA Office, Eglin AFB, FL R. Glasby, J. Erwin, D. Stefanski, University C. Lietz, C. Umphrey, Air Force Research University of Maryland, College Park, of Tennessee, Knoxville, Knoxville, TN Laboratory, Edwards AFB, CA; J. Sitaraman, College Park, MD PGA, LLC, Sunnyvale, CA; et al. Wednesday, 11 January 2017 293-APA-28 Special Session: Sensitivity Analysis and Uncertainty Quantification Evaluation for Realistic Problems I Dallas 2 Chaired by: P. MORGAN, Ohio Aerospace Institute and M. JURKOVICH, US Air Force 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs AIAA-2017-1196 AIAA-2017-1197 AIAA-2017-1198 AIAA-2017-1199 AIAA-2017-1200 Overview of the AVT-191 Project Three-parameter uncertainty Meta-Model Results For Polynomial Scalable Uncertainty Taxonomy for Uncertainty Quantification in Internal to Assess Sensitivity Analysis and quantification for generic missile FG5 Chaos Method a Transonic Missile Flows Uncertainty Quantification Methods for J. Peter, ONERA, Châtillon, France; S. J. Doty, Doty Consulting Services, Dayton, R. Graves, Air Force Research Laboratory, R. Nigro, University of Mons, Mons, Belgium; Military Vehicle Design Goertz, German Aerospace Center (DLR), OH Wright-Patterson AFB, OH D. Wunsch, NUMECA International, Brussels, J. Benek, Air Force Research Laboratory, Braunschweig, Germany; R. Graves, Air Force Belgium; G. Coussement, University of Wright-Patterson AFB, OH; J. Luckring, NASA Research Laboratory, Wright-Patterson AFB, OH Mons, Mons, Belgium; C. Hirsch, NUMECA Langley Research Center, Hampton, VA International, Brussels, Belgium Wednesday, 11 January 2017 294-APA-29 Weapons Aerodynamics Dallas 3 Chaired by: C. PASILIAO, AFRL/RW and J. DOYLE, US Army AMRDEC 1400 hrs 1430 hrs 1500 hrs AIAA-2017-1201 AIAA-2017-1204 AIAA-2017-1205 Catastrophic Yaw of Triform and Trajectory Simulation of a Standard A Comparative Study of Prediction Cruciform Tailed Missiles Store and Generic Wing Pylon Techniques for Supersonic Missile J. Morote, P. Morote, National Institute using CFD Aerodynamic Coefficients at Incidence of Aerospace Technology (INTA), Madrid, J. Masud, O. Mahmood, Z. Toor, Air L. El mahdi, M. Ahmed, O. Mahmoud, O. Spain University, Islamabad, Pakistan Abdel Hameed, Military Technical College, Cairo, Egypt Wednesday, 11 January 2017 295-APA-30 DPW-6 Results and Comparisons II Dallas 4 Chaired by: J. VASSBERG, Boeing Engineering Operations & Technology and J. MORRISON, NASA Langley Research Center 1400 hrs 1430 hrs 1500 hrs 1600 hrs 1630 hrs AIAA-2017-1206 AIAA-2017-1207 AIAA-2017-1208 AIAA-2017-1209 Open Discussion Summary of Data from the Summary of Data from the Summary of Data from the Sixth AIAA CFD Drag Prediction Workshop: Statistical Analysis of CFD Solutions Sixth AIAA CFD Drag Prediction Sixth AIAA CFD Drag Prediction CRM Cases 2 to 5. from the Sixth AIAA Drag Prediction Workshop: Case 1 Code Verification Workshop: Case 5 (Coupled Aero- E. Tinoco, Self, Kent, WA; O. Brodersen, S. Keye, German Aerospace Center (DLR), Workshop C. Roy, Virginia Polytechnic Institute and Structural Simulation) Braunschweig, Germany; K. Laflin, Cessna Aircraft Company, Wichita, KS J. Derlaga, J. Morrison, NASA Langley State University, Blacksburg, VA S. Keye, German Aerospace Center (DLR), Research Center, Hampton, VA Braunschweig, Germany; D. Mavriplis, University of Wyoming, Laramie, Laramie, WY Wednesday, 11 January 2017

128 296-APA-31 High Angle-of-Attack Aerodynamics Dallas 5 Chaired by: N. HALL, Lockheed Martin and J. PINIER, NASA Langley Research Center 1400 hrs 1430 hrs 1500 hrs AIAA-2017-1210 AIAA-2017-1211 AIAA-2017-1212 Design of Airfoils to Mitigate Wake Analysis of Multi-Element Airfoil Computational Study of Aerodynamic Bursting High Lift Improvement by Efﬁcient Characteristics of Reusable Rocket at B. Pomeroy, M. Selig, University of Illinois, Upper Surface Suction High-Angle-of-Attack Urbana-Champaign, Urbana, IL L. Veldhuis, J. van Craenenbroeck, Delft T. Aogaki, K. Kitamura, Yokohama National University of Technology, Delft, The University, Kanagawa, Japan; S. Nonaka, Netherlands Japan Aerospace Exploration Agency (JAXA), Kanagawa, Japan Wednesday, 11 January 2017 297-APA-32 Aerodynamic Results from Ground Test or Flight Test Dallas 6 Chaired by: G. GATLIN, NASA Langley Research Center and A. VANDERWYST, Leidos 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs AIAA-2017-1213 AIAA-2017-1214 AIAA-2017-1215 AIAA-2017-1216 AIAA-2017-1217 Blockage Testing in the NASA Glenn Range and Endurance Estimation Low Cost Accurate Angle of Attack Wind Induced Forces on a Use of a Ring Wing Model to 225 Square Centimeter Supersonic for Low-Re Electric UAS System Hemispherical Observatory Dome investigate Factors affecting Wind Tunnel M. McCrink, J. Gregory, Ohio State B. Martos, Embry-Riddle Aeronautical with Open Shutter Doors Transition Measurement using A. Sevier, Case Western Reserve University, University, Columbus, OH University, Daytona Beach, FL; D. Rogers, T. Siefers, R. Frost, S. Lim, T. McLaughlin, U.S. Temperature Sensitive Paint and Cleveland, OH; D. Davis, NASA Glenn Research U.S. Naval Academy, Annapolis, MD Air Force Academy, Colorado Springs, CO Hot Films in Transonic Flow Center, Cleveland, OH; M. Schoenenberger, A. Ciarella, S. Lawson, Aircraft Research NASA Langley Research Center, Hampton, VA Association, Ltd., Bedford, United Kingdom Wednesday, 11 January 2017 298-F360-6 Transitioning Your Idea from the Lab to Flight Test Texas C 1400 - 1600 hrs Moderator: Chris Cotting, Flight Sciences Technical Expert, United States Air Force Test Pilot School

Panelists: Albion Bowers James “Buddy” Denham Bill Gray John S. Langford Shawn Whitcomb Craig Woolsey Chief Scientist Senior Scientiﬁc Technical Manager Chief Pilot Chairman and Chief Executive Ofﬁcer Systems Engineer, Advanced Development Professor of Aerospace and Ocean Engineering NASA Armstrong Flight Research Center Aeromechanics Division U.S. Air Force Test Pilot School Aurora Flight Sciences Corporation Programs Virginia Polytechnic Institute and State Naval Air Systems Command Lockheed Martin Corporation University

Wednesday, 11 January 2017 299-FD-39 CFD Methods for Fast Computing Texas 6 Chaired by: J. BORIS, US Naval Research Lab 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs AIAA-2017-1218 AIAA-2017-1220 AIAA-2017-1219 AIAA-2017-1221 AIAA-2017-1222

Improving the strong parallel Pleasingly Parallel Discontinuous An Order N log 2(N) Parallel Solver Implementing the Swept Time-Space Speed-Up of Colloidal Fluctuating scalability of CFD schemes via the Least Squares Spectral Element for Time Spectral Problems Decomposition Scheme for PDEs on Lattice Boltzmann Simulations swept domain decomposition rule Method for Laminar Incompressible D. Ramezanian, D. Mavriplis, University of the GPU through Discrete Approximations of M. Alhubail, Q. Wang, Massachusetts Flows with H-Reﬁnement Wyoming, Laramie, Laramie, WY D. Magee, K. Niemeyer, Oregon State Probability Distributions Institute of Technology, Cambridge, MA J. Hasbestan, J. Newman, A. Arabshahi, University, Corvallis, OR S. Coogan, G. Musgrove, H. Basagaoglu, University of Tennessee, Chattanooga, Southwest Research Institute, San Antonio, TX Chattanooga, TN Wednesday, 11 January 2017 300-FD-41 Special Session: Wall Models for Large Eddy Simulation Texas 2

129 Chaired by: N. BISEK, Air Force Reseach Laboratory and J. LARSSON, University of Maryland 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs Oral Presentation Oral Presentation Oral Presentation AIAA-2017-1223 Oral Presentation Oral Presentation Large eddy simulation with modeled Wall Modeling for Shock Turbulent Wall-Modeled Large Eddy Assessment of Wall-modeled LES Algorithmic and modeling Scale-Resolving Simulations and wall-stress: what to expect, recent Boundary Layer Interactions with Simulation of Separated Flows Strategies Within a Discontinuous- constraints for the application of their Impact on Scramjet Engine progress, and future directions Heat Transfer F. Cadieux, J. Sadique, X. Yang, R. Mittal, Galerkin Spectral-element LES to design Design and Development J. Larsson, University of Maryland, College J. Komives, Air Force Institute of C. Meneveau, Johns Hopkins University, Framework S. Bose, F. Ham, Cascade Technologies, R. Baurle, NASA Langley Research Center, Park, College Park, MD Technology, Wright-Patterson AFB, OH; Baltimore, MD C. Carton de Wiart, S. Murman, NASA Inc., Palo Alto, CA Hampton, VA G. Candler, University of Minnesota, Ames Research Center, Moffett Field, CA Minneapolis, Minneapolis, MN Wednesday, 11 January 2017 301-FD-42 Transition Open Forum Texas 3 1400 - 1700 hrs Wednesday, 11 January 2017 302-FD-43 Turbulent, Compressible CFD Applications and Validations Texas 4 Chaired by: J. CHAPELIER, Université de Rouen and S. LELE, Stanford University 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs AIAA-2017-1224 AIAA-2017-1225 AIAA-2017-1226 AIAA-2017-1227 AIAA-2017-1228 Finite-element solutions to the Triple Hill’s Vortex Synthetic Eddy Development and Validation of Stabilized Scale-Similarity Modeling Optimized high-order Spectral Reynolds Averaged Navier-Stokes Method for Turbulent Inflow a Lagrangian Droplet Tracking for Explicitly-Filtered Large-Eddy Difference schemes for the equations using a Spalart-Allmaras Conditions Algorithm in a Turbulent Simulations computation of aeroacoutics and Turbulence Model J. Haywood, A. Sescu, Mississippi State Combustion Solver A. Edoh, A. Karagozian, University of turbulence N. Burgess, Science and Technology University, Mississippi State, MS; J. Foster, C. Neal, S. Thakur, J. Wright, Streamline California, Los Angeles, Los Angeles, CA J. Chapelier, G. Lodato, CORIA, Rouen, Corporation, Moffett Field, CA; R. Glasby, M. Farthing, U.S. Army Corps of Engineers, Numerics, Inc., Gainesville, FL France J. Erwin, D. Stefanski, University of Vicksburg, MS Tennessee, Knoxville, Knoxville, TN; S. Allmaras, Massachusetts Institute of Technology, Cambridge, MA Wednesday, 11 January 2017 303-FD-44 CFD Modeling Texas 5 Chaired by: M. CONWAY, The Aerospace Corporation 1400 hrs 1430 hrs 1500 hrs 1530 hrs AIAA-2017-1229 AIAA-2017-1230 AIAA-2017-1231 AIAA-2017-1232 CFD Modelling of Kiel-Shrouded Modeling of Conventional Flaps at DNS of High Temperature Effects on Three-dimensional Numerical Temperature Probes High Deflection-Rate Compressible Isotropic Turbulence Simulation on Dispersion Process of B. Ubald, P. Tucker, University of A. Medina, M. Ol, Air Force Research G. Ramanathan, S. Ghosh, Indian Institute Unsteady High Pressure Hydrogen Cambridge, Cambridge, United Kingdom; Laboratory, Wright-Patterson AFB, OH; D. of Technology Madras, Chennai, India Jet Flow S. Shahpar, Rolls-Royce Group plc, Derby, Williams, X. An, Illinois Institute of Technology, N. Tsuboi, K. Fujimoto, D. Muto, Kyushu United Kingdom Chicago, IL; M. Hemati, University of Institute of Technology, Kitakyushu, Japan; Minnesota, Minneapolis, Minneapolis, MN M. Asahara, Gifu University, Gifu, Japan Wednesday, 11 January 2017 304-FD-45 Other Topics in Fluid Dynamics II Grapevine C Chaired by: Y. ZHANG, and J. ESTEVADEORDAL, Innovative Scientific Solutions Incorporated 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs AIAA-2017-1233 AIAA-2017-1234 AIAA-2017-1235 AIAA-2017-1236 AIAA-2017-1237 Numerical Study of Radial Approximate Analytical Models for Design of a Modular Vortex Tube BiGlobal Stability Analysis of Unsteady Performance Analysis of Labyrinth Deformation and Energy Conversion Turbulent Boundary Layer Wall Engine Air Particle Separator for Flow in Vaneless Diffuser of Centrifugal Seals Using Analytical Methods and in Head-on Collision of Two Equal- Pressure and Wall Shear Fluctuation the MQ-1 UAV Utilizing Additive Compressor Numerical Techniques size Droplets Spectra and Coherence Functions Manufacturing Technologies C. Hu, P. Liu, X. Zhu, Shanghai Jiao Tong J. Masud, A. Yar, Z. Sohail, H. Anwar, Z. Q. Qu, C. Ge, P. Liu, Beihang University, L. DeChant, J. Smith, M. Barone, Sandia R. Crumpacker, Ohio State University, University, Shanghai, China; H. Chen, National Toor, Air University, Islamabad, Pakistan Beijing, China; R. Agarwal, Washington National Laboratories, Albuquerque, NM Columbus, OH Laboratory of Engine Turbocharging Technology, University in St. Louis, St. Louis, MO Tianjin, China; Z. Du, Shanghai Jiao Tong University, Shanghai, China

130 Wednesday, 11 January 2017 305-GNC-8 Missile GNC Austin 1 Chaired by: S. WELLS, Raytheon Missile Systems and J. PARISH, Sandia National Laboratories 1400 hrs 1430 hrs 1500 hrs AIAA-2017-1238 AIAA-2017-1239 AIAA-2017-1240 Adaptive Roll Control of Guided Time-to-Go Prediction for Anti- Linearized Analysis of Azimuth Munitions with State Independent Ballistic Missile Midcourse Guidance Transfer of Strapdown INS for Vertical Uncertainty Parameterization G. Moon, M. Seo, S. Hong, S. Shim, M. and Slant Launch Applications N. Ovec, ROKETSAN Missile Industries, Tahk, Korea Advanced Institute of Science V. Bogala, C. RS, N. BHVS, Defence Research Inc., Ankara, Turkey; A. Kutay, Middle East and Technology, Daejeon, South Korea and Development Organisation, Hyderabad, Technical University, Ankara, Turkey India Wednesday, 11 January 2017 306-GNC-9 Trajectory Optimization Grapevine D Chaired by: J. RYAN, NASA-Dryden Flight Research Center and Y. MIYAZAWA, Kyushu University 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2017-1241 AIAA-2017-1242 AIAA-2017-1243 AIAA-2017-1244 AIAA-2017-1245 AIAA-2017-1246 Vertical and Horizontal Flight An Improved Online Reentry Maximizing Range Observability A Blended Performance Function Target tracking using Adaptive Optimal Arrival Time Assignment and Reference Trajectory Optimization Trajectory Planning and Tracking in Bearings-Only Rendezvous for Extremum-Seeking-Control of a coarse-to-fine Particle Filter Control Analysis using Air Traffic Data for a Commercial Aircraft Algorithm for Common Aero Guidance Formation Flight System D. Lee, S. Shim, M. Hwang, M. Tahk, for Tokyo International Airport A. Murrieta Mendoza, P. Mugnier, R. Botez, Vehicles P. Anjaly , A. Ratnoo, Indian Institute of J. Ryan, NASA Armstrong Flight Research Korea Advanced Institute of Science and Y. Higuchi, N. Kitazume, K. Tamura, T. University of Québec, Montréal, Canada Y. Wang, W. Zhou, Y. Pang, Dalian Science, Bengaluru, India Center, Edwards, CA Technology, Daejeon, South Korea Kozuka, Y. Miyazawa, Kyushu University, University of Technology, Dalian, China Fukuoka, Japan; M. Brown, Electronic Navigation Research Institute, Tokyo, Japan Wednesday, 11 January 2017 307-GNC-10 Adaptive Control for Aircraft GNC Austin 6 Chaired by: F. HOLZAPFEL and S. NIVISON, Air Force Research Lab 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs AIAA-2017-1247 AIAA-2017-1248 AIAA-2017-1249 AIAA-2017-1250 AIAA-2017-1251 L1 Augmentations for a Fixed Gain NDI-Based L1 Adaptive Control Improving Long-Term Learning Design and Evaluation of an L1 Helicopter Dynamic Model Controller on a Large Transport Design for a Generic Hypersonic of Model Reference Adaptive Adaptive Controller for NASA’s Identification by Conditional Aircraft Vehicle Model Controllers for Flight Applications: A Transport Class Model Attitude Hold Logic M. Wang, Harbin Institute of Technology, C. Qi, A. Jianliang, Fudan University, Sparse Neural Network Approach J. Dodenhöft, Technical University of S. Jung, D. Shim, Korea Advanced Institute Beijing, China; F. Holzapfel, F. Zhang, Shanghai, China S. Nivison, P. Khargonekar, University of Munich, Garching, Germany; R. Choe, K. of Science and Technology, Daejeon, South Technical University of Munich, Munich, Florida, Gainesville, Gainesville, FL Ackerman, University of Illinois, Urbana- Korea; E. Kim, Korea Aerospace Research Germany; S. Zhang, Harbin Institute of Champaign, Urbana, IL; F. Holzapfel, Institute (KARI), Daejeon, South Korea Technology, Beijing, China Technical University of Munich, Garching, Germany; N. Hovakimyan, University of Illinois, Urbana-Champaign, Urbana, IL Wednesday, 11 January 2017 308-GNC-11 Aircraft GNC Control Methods Austin 5 Chaired by: T. YUCELEN, Missouri University of Science & Technology and M. MCFARLAND, Orbital ATK 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2017-1252 AIAA-2017-1253 AIAA-2017-1254 AIAA-2017-1255 AIAA-2017-1256 AIAA-2017-1257 Decentralized LQT in a Limited An Anti-windup Fault Tolerant Intent Inference of Aircraft via Integrator-Augmented Robust Two-Time-Scale Slow and Fast State Angle of Attack and Load Factor Information Environment Control Scheme with Guaranteed Inverse Optimal Control Including Adaptive Control Design for Close Tracking of an F-16 Using Slow and Limiting in Fighter Aircraft using C. Robertson, A. Sinclair, Auburn University, Transient Performance for Tailless Second-order Optimality Condition Formation Flight Fast Controls Command Governors Auburn, AL; E. Doucette, Air Force Research Flying Wing Aircrafts N. Yokoyama, National Defense Academy, Q. Zhang, H. Liu, University of Toronto, D. Saha, J. Valasek, Texas A&M University, D. Simon, O. Härkegård, Saab, Linköping, Laboratory, Eglin AFB, FL W. Shuang, S. Zhang, X. Wu, Yokosuka, Japan Toronto, Canada College Station, TX Sweden; J. Löfberg, Linköping University, Linköping, Sweden

131 Nanjing University of Aeronautics and Astronautics, Nanjing, China; E. Van Kampen, Q. Chu, Delft University of Technology, Delft, The Netherlands Wednesday, 11 January 2017 309-GNC-12 Estimation and Tracking Methods Austin 2 Chaired by: W. WHITACRE, Draper Laboratory and N. AHMED 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2017-1258 AIAA-2017-1259 AIAA-2017-1260 AIAA-2017-1261 AIAA-2017-1262 AIAA-2017-1263 Application of Observability Analysis Gaussian Sum-Based Maneuvering Multiple-Model Adaptive Estimation Norm-Constrained Forward- Distributed Cubature Gaussian Efficient Nonlinear Actuator Fault to Space Object Tracking Target Tracking Using Unmanned for Measurements with Unknown Backward Smoothing Mixture Filters Reconstruction System A. Dianetti, State University of New York, Aerial Vehicle Time Delay S. Chee, J. Forbes, McGill University, B. JIa, Intelligent Fusion Technology, Inc., P. Lu, E. Van Kampen, Q. Chu, Delft Buffalo, NY; R. Weisman, Air Force Research C. Zhang, I. Hwang, Purdue University, K. Lee, E. Johnson, Georgia Institute of Montréal, Canada Germantown, MD; M. Xin, T. Sun, University of University of Technology, Delft, The Laboratory, Kirtland AFB, NM; J. Crassidis, State West Lafayette, IN Technology, Atlanta, GA Missouri, Columbia, Columbia, MO Netherlands University of New York, Buffalo, NY Wednesday, 11 January 2017 310-GNC-13 Spacecraft and Launch Guidance Grapevine 6 Chaired by: J. REED, United Launch Alliance, LLC and K. BOLLINO, U.S. Air Force 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2017-1264 AIAA-2017-1265 AIAA-2017-1266 AIAA-2017-1267 AIAA-2017-1268 AIAA-2017-1269 Adaptive Controllers for Spacecraft Re-entry Guidance for Path- An Optimal Explicit Guidance Explicit Constrained Terminal Spacecraft De-Orbit Point Targeting Autonomous Spacecraft Swarm Rendezvous based on nonlinear Constraint Tracking Algorithm for Terminal Descent Acceleration Optimal Guidance for using Aerodynamic Drag Formation Planning Using model with unknown parameters E. Mooij, Delft University of Technology, Phase of Lunar Soft Landing Three Dimensional Lunar Landing S. Omar, R. Bevilacqua, University of Artificial Field Based on Nonlinear K. Zhang, M. Demetriou, Worcester Delft, The Netherlands A. Banerjee, R. Padhi, Indian Institute of M. S, Indian Space Research Organisation, Florida, Gainesville, Gainesville, FL Bifurcation Dynamics Polytechnic Institute, Worcester, MA Science, Bengaluru, India Bengaluru, India; R. Padhi, Indian Institute H. Chen, J. Sun, Beihang University, of Science, Bengaluru, India Beijing, China; K. Li, Beijing Institute of Control Engineering, Beijing, China; M. Wang, Beihang University, Beijing, China Wednesday, 11 January 2017 311-GNC-14 Control of Innovative Micro Air Vehicle Configurations Austin 4 Chaired by: M. OPPENHEIMER, Air Force Research Laboratory and H. TAHA, University of California, Irvine 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2017-1270 AIAA-2017-1271 AIAA-2017-1272 AIAA-2017-1273 AIAA-2017-1274 AIAA-2017-1275 Manipulation of Wing Tip Vortices Wing Design and Testing for a Tailless Wing Flexibility Induced Control Wing Flexibility Induced Control Aerodynamic-Dynamic Interactions Aerodynamic-Dynamic Interactions on Low Aspect Ratio Wings using Flapping Wing Micro-Air Vehicle Reversal For Flapping Wing Reversal For Flapping Wing and Multi-Body Formulation of and Multi-Body Formulation of Winglet Control Surfaces M. Oppenheimer, Air Force Research Vehicles: Theoretical Analysis Vehicles: Observation and Flapping Wing Dynamics: Part I Flapping Wing Dynamics: Part II R. O’Donnell, K. Mohseni, University of Laboratory, Wright-Patterson AFB, OH; D. Sigthorsson, Infoscitex Corporation, Evaluation Modeling Trim and Stability Analysis Florida, Gainesville, Gainesville, FL D. Sigthorsson, Infoscitex Corporation, Dayton, OH; M. Oppenheimer, D. Doman, D. Sigthorsson, Infoscitex Corporation, A. Hassan, H. Taha, University of California, A. Hassan, H. Taha, University of California, Beavercreek, OH; D. Doman, I. Weintraub, Air I. Weintraub, Air Force Research Laboratory, Dayton, OH; M. Oppenheimer, D. Doman, Irvine, Irvine, CA Irvine, Irvine, CA Force Research Laboratory, Wright-Patterson Wright-Patterson AFB, OH I. Weintraub, Air Force Research Laboratory, AFB, OH Wright-Patterson AFB, OH Wednesday, 11 January 2017 312-GT-7/AMT-11 Test Technique and Data Analysis Improvements at the NASA Ames Unitary Plan Wind Tunnels II (Invited) Ft. Worth 6 Chaired by: N. BURNSIDE, NASA-Ames and K. LONG, Arc-Aox, Experimental Aerophyscis Branch 1400 hrs 1430 hrs 1500 hrs AIAA-2017-1277 AIAA-2017-1278 AIAA-2017-1279 Initial Testing of the Ames Unitary MiniWall Tool for Analyzing CFD and Development of a Hybrid Non– Short Static Pipe Wind Tunnel Large Data Sets Iterative and Neural Network M. Amaya, R. Flach, A. L’Esperance, NASA M. Schuh, J. Melton, NASA Ames Research Based Strain–Gage Balance Load Ames Research Center, Moffett Field, CA Center, Moffett Field, CA; P. Stremel, Calculation Method Science and Technology Corporation, A. Meade, A. Mokhtarzadeh, Rice University, Moffett Field, CA Houston, TX; K. James, K. Long, NASA Ames Research Center, Moffett Field, CA 132 Wednesday, 11 January 2017 313-GTE-7 Advanced Turbine Cooling I San Antonio 4 Chaired by: G. PANIAGUA, Purdue University 1400 hrs 1430 hrs 1500 hrs 1530 hrs AIAA-2017-1280 AIAA-2017-1281 AIAA-2017-1282 AIAA-2017-1283 Relating Film Cooling Performance Optimization of Film Cooling Hole Extended Surface Heat Transfer A Detailed Uncertainty Analysis of at Ambient and Near Engine Array Considering the Variation of Coefficients via Endwall Heat Transfer Experiments using Temperatures Turbine Inlet Temperature Profiles Temperature Measurements. Temperature Sensitive Paint C. Vorgert, R. Ashby, C. Schmiedel, M. S. Lee, Seoul National University, Seoul, Y. Pai, R. Fernandes, S. Fernandes, A. Prasad, M. Ricklick, Embry-Riddle Polanka, J. Rutledge, Air Force Institute of South Korea; D. Rhee, Korea Aerospace M. Ricklick, Embry-Riddle Aeronautical Aeronautical University, Daytona Beach, FL Technology, Wright-Patterson AFB, OH Research Institute (KARI), Daejeon, South University, Daytona Beach, FL Korea; Y. Kim, K. Yee, Seoul National University, Seoul, South Korea Wednesday, 11 January 2017 314-HSABP-6/PGC-5 Pressure Gain Combustion - Rotating Detonation Engines III Ft. Worth 3 Chaired by: K. KAILASANATH, Naval Research Laboratory and D. PAXSON, NASA Glenn Research Center 1400 hrs 1430 hrs 1500 hrs 1530 hrs AIAA-2017-1284 AIAA-2017-1285 AIAA-2017-1286 AIAA-2017-1287 Numerical Investigation on Burned Experimental Characterization Experimental Study of the Disk- Numerical study of oblique Gas Backflow in Liquid Fuel Purge of Heat Transfer Coefficients in a Shaped Rotating Detonation Turbine detonation initiations with chain- Method Rotating Detonation Engine Engine branching kinetics H. Watanabe, A. Matsuo, Keio University, S. Meyer, M. Polanka, Air Force Institute J. Higashi, S. Nakagami, K. Matsuoka, H. Teng, P. Yang, Z. Jiang, Chinese Yokohama, Japan; K. Matsuoka, J. of Technology, Wright-Patterson AFB, OH; J. Kasahara, Nagoya University, Nagoya, Academy of Sciences, Beijing, China Kasahara, Nagoya University, Chikusa, F. Schauer, R. Anthony, Air Force Research Japan; A. Matsuo, Keio University, Japan Laboratory, Wright-Patterson AFB, OH; C. Yokohama, Japan; I. Funaki, Japan Stevens, J. Hoke, Innovative Scientific Aerospace Exploration Agency (JAXA), Solutions, Inc., Dayton, OH; et al. Sagamihara, Japan; et al. Wednesday, 11 January 2017 315-ICC-1 Information and Command and Control Systems Ft. Worth 2 Chaired by: J. MCEVER, Johns Hopkins University Applied Physics Laboratory and M. SOTAK 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs AIAA-2017-1288 AIAA-2017-1289 AIAA-2017-1290 AIAA-2017-1291 AIAA-2017-1292 TowardsThe Design of An Intelligent Multivariable Direct Adaptive Stability VOSSCA Satellite Operation System Development of Command and Control System-of-Systems Architecture Aerospace Pursuit - Evasion Game And Command Augmentation of an S. Chusri, U. Khowsuwan, J. Plaidoung, P. Software for an In-Space 3D Printer Metrics for Information Fusion: A M. El-Arabaty, Misr International University, Air-Breathing Hypersonic Vehicle Pipitsunthonsan, Geo-Informatics and Space and Small Satellite Test Mission Network Theoretic Formulation Cairo, Egypt M. Balas, R. Aditya, Embry-Riddle Aeronautical Technology Development Agency, Chonburi, R. Barsotti, University of Texas, Dallas, A. Raz, D. DeLaurentis, Purdue University, University, Daytona Beach, FL; D. Doman, Thailand Dallas, TX; J. Straub, University of North West Lafayette, IN Air Force Research Laboratory, Wright- Dakota, Grand Forks, Grand Forks, ND Patterson AFB, OH; F. Franquiz, Embry-Riddle Aeronautical University, Daytona Beach, FL Wednesday, 11 January 2017 316-IS-5 Integrated Systems Health Management (ISHM) Ft. Worth 1 Chaired by: J. VALASEK, Texas A&M University 1400 hrs 1430 hrs 1500 hrs AIAA-2017-1293 AIAA-2017-1294 AIAA-2017-1295 Architectural Considerations Towards Spacecraft Health Monitoring Fault Management Metrics Automated Contingency Management Using a Biomimetic Fault Diagnosis S. Johnson, Dependable System for Unmanned Aircraft Scheme Technologies, Broomfield, CO; S. Ghoshal, H. Usach, Technical University of Valencia, D. Garcia, H. Moncayo, A. Perez Rocha, D. Haste, Qualtech Systems, Inc., Rocky Valencia, Spain; C. Torens, F. Adolf, German K. Rivera, Embry-Riddle Aeronautical Hill, CT; C. Moore, NASA Marshall Space Aerospace Center (DLR), Braunschweig, University, Daytona Beach, FL; M. Dupuis, Flight Center, Huntsville, AL Germany; J. Vila, Technical University of R. Mueller, NASA Kennedy Space Center, Valencia, Valencia, Spain Cape Canaveral, FL 133 Wednesday, 11 January 2017 317-IS-6 Human Automation Interaction Ft. Worth 1 Chaired by: N. NGUYEN, NASA-Ames Research Center 1400 hrs 1530 hrs 1600 hrs No Presentations AIAA-2017-1296 AIAA-2017-1297 A Human-System Interface Aviate, Navigate: Functional with Contingency Planning for Visualizations of Asymmetric Flight Collaborative Operations of Envelope Limits Unmanned Aerial Vehicles T. Rijndorp, C. Borst, C. de Visser, O. J. Mueller, C. Miller, U. Kuter, J. Rye, Stroosma, M. Mulder, M. van Paassen, J. Hamell, Smart Information Flow Delft University of Technology, Delft, The Technologies, Minneapolis, MN Netherlands Wednesday, 11 January 2017 318-MAT-6 Fatigue and Fracture Palomino 2 Chaired by: R. FERTIG, University of Wyoming and G. SEIDEL, Virginia Polytechnic Institute and State Universit 1400 hrs 1430 hrs 1500 hrs AIAA-2017-1298 AIAA-2017-1299 AIAA-2017-1300 Delamination Detection in Calibrating an equivalent initial Observation of the Constant Carbon Fiber Composites using flaw size distribution from da/dN Life Criterion for Turbine Engine Piezoresistive Nanocomposites and S-N data Component Design S. Chava, S. Choudhary, S. Namilae, I. Asher, G. Khan, L. Wang, Y. Ling, O. Scott-Emuakpor, T. George, C. Holycross, Embry-Riddle Aeronautical University, F. Viana, General Electric Company, B. Langley, Air Force Research Laboratory, Daytona Beach, FL Niskayuna, NY Wright-Patterson AFB, OH Wednesday, 11 January 2017 319-MDO-8 Topology and Structural Optimization Mustang 1 Chaired by: J. DEATON, Adjoint Technologies and A. NAJAFI, ANSYS, Inc. 1400 hrs 1430 hrs 1500 hrs 1530 hrs AIAA-2017-1301 AIAA-2017-1302 AIAA-2017-1303 AIAA-2017-1304 Topological Optimization of a Cuboct A Nonlinear Finite Element Analysis Aeroelastic Optimization of Wing Efficient Methods for Design And Truss Structure Using a Genetic Capability for the Optimization of Structure Using Curvilinear Spars, Analysis of Tow Steered Wing Algorithm Thermoelastic Structures Ribs, and Flutter Suppression Structures H. Jackson, NASA Ames Research Center, D. Neiferd, R. Grandhi, Wright State S. Doyle, M4 Engineering, Inc., Long M. Henson, Lockheed Martin Corporation, Moffett Field, CA University, Dayton, OH; P. Beran, Air Force Beach, CA Fort Worth, TX; B. Wang, University of Research Laboratory, Wright-Patterson AFB, Texas, Arlington, Arlington, TX OH; M. Bhatia, Mississippi State University, Mississippi State, MS Wednesday, 11 January 2017 320-MDO-9 Emerging Methods and Algorithms in Optimization Mustang 3 Chaired by: V. BALABANOV, Boeing Commercial Airplanes and D. ALLAIRE, Texas A&M University 1400 hrs 1430 hrs 1500 hrs 1530 hrs AIAA-2017-1305 AIAA-2017-1306 AIAA-2017-1307 AIAA-2017-1308 A Mixed Integer Efficient Global Spiral: A General Framework For Sub-space Metamodel-based Optimization of Aerospace Optimization Algorithm for the Parameter Sensitivity Analysis Multidisciplinary Optimization of an Structures under Uncertainty Simultaneous Aircraft Allocation- D. Makhija, Universal Technology Aircraft Wing subjected to Bird Strike using an Iterative Distribution Mission-Design Problem Corporation, Dayton, OH; P. Beran, J. Ollar, R. Jones, Altair Engineering, Inc., Evolutionary Algorithm S. Roy, Purdue University, West Lafayette, Air Force Research Laboratory, Wright- Leamington Spa, United Kingdom; V. I. Tartaruga, Siemens, Leuven, Belgium; M. IN; K. Moore, J. Hwang, J. Gray, NASA Patterson AFB, OH Toropov, Queen Mary University of London, Lowenberg, J. Cooper, P. Sartor, University Glenn Research Center, Cleveland, OH; W. London, United Kingdom of Bristol, Bristol, United Kingdom; Y.

134 Crossley, Purdue University, West Lafayette, Lemmens, Siemens, Leuven, Belgium IN; J. Martins, University of Michigan, Ann Arbor, Ann Arbor, MI Wednesday, 11 January 2017 321-MST-8 Aviation Simulation Scenario Development II San Antonio 2 Chaired by: U. DURAK, DLR-German Aerospace Center and S. JAFER, Embry-Riddle Aeronautical University 1400 hrs 1430 hrs 1500 hrs 1530 hrs AIAA-2017-1309 AIAA-2017-1310 AIAA-2017-1311 Panel Discussion Enhanced Scenario-Based Training Harmonizing the Scenario Graphical Specification of Flight for Unmanned Aircraft System Generation Process, Tools and Scenarios with Aviation Scenario Operational Missions Standards for Flight Simulators Defintion Language (ASDL) K. Rigby, N. Macchiarella, A. Mirot, Embry- J. Field, A. Gerretsen, R. Meiland, F. S. Jafer, B. Chhaya, Embry-Riddle Riddle Aeronautical University, Daytona Mohrmann, National Aerospace Laboratory Aeronautical University, Daytona Beach, FL; Beach, FL (NLR), Amsterdam, The Netherlands U. Durak, German Aerospace Center (DLR), Braunschweig, Germany Wednesday, 11 January 2017 322-MST-9 Human Factors, Perception, Cueing II San Antonio 1 Chaired by: D. CARTMELL, Boeing Engineering Operations & Technology and F. CARDULLO, State University of NY 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2017-1312 AIAA-2017-1313 AIAA-2017-1314 AIAA-2017-1315 AIAA-2017-1316 AIAA-2017-1317 Development of model-following Passive Haptics to Enhance Virtual Real-Time Performance Feedback A Hybrid-Systems Approach for Effects of Eye Parameters on Real Time Eye Tracking Interface control laws for helicopters to Reality Simulations in a Manually-Controlled Spacecraft Analyzing Pilot-Cockpit Interactions Human Controller Remnant and for Visual Monitoring of Radar achieve personal aerial vehicle’s R. Joyce, S. Robinson, University of Inspection Task B. Yang, S. Park, Optimal Synthesis, Inc., Los Control Behavior Controllers handling qualities California, Davis, Davis, CA J. Karasinski, S. Robinson, University of Altos, CA; J. Suraj Nandiganahalli, I. Hwang, A. Popovici, P. Zaal, San Jose State H. Wee, S. Lye, Nanyang Technological C. Gerboni, S. Geluardi, J. Venrooij, Max California, Davis, Davis, CA; P. Handley, K. Purdue University, West Lafayette, IN University, Moffett Field, CA; D. Pool, M. University, Singapore, Singapore; J. Planck Institute for Biological Cybernetics, Duda, Draper Laboratory, Cambridge, MA Mulder, Delft University of Technology, Pinheiro, Thales Group, Rungis, France Tübingen, Germany; A. Joos, W. Fichter, Delft, The Netherlands University of Stuttgart, Stuttgart, Germany; H. Buelthoff, Max Planck Institute for Biological Cybernetics, Tübingen, Germany Wednesday, 11 January 2017 323-MST-10 Modeling and Simulation of Air Traffic Management III San Antonio 3 Chaired by: J. SCHROEDER, Federal Aviation Administration 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2017-1318 AIAA-2017-1319 AIAA-2017-1320 AIAA-2017-1321 AIAA-2017-1322 AIAA-2017-1323 Automated Route Clustering for Air TFDM Departure Queue Estimation of Midair Collision A Study on Free Routing Considering An Elementary Algorithm for Arrival Traffic Scheduling Traffic Modeling Management - Effective Calibration Risk for Established on Required Interference of Air Traffic Flow Autonomous Air Terminal Merging Performance subject to Futuristic A. Bombelli, A. Segarra Torne, E. and Validation Strategies for High- Navigation Performance Procedures Y. Nakamura, K. Kageyama, Electronic and Interval Management Traffic Statistics Trumbauer, K. Mease, University of Fidelity Modeling C. Nichols, J. Walls, Federal Aviation Navigation Research Institute, Chofu, Japan; A. White, NASA Langley Research Center, N. Takeichi, Tokyo Metropolitan University, California, Irvine, Irvine, CA V. Shah, C. David, S. James, Noblis, Falls Administration, Washington, D.C. Y. Miyazawa, H. Matsuda, Kyushu University, Hampton, VA Hino, Japan Fukuoka, Japan 135 Church, VA Wednesday, 11 January 2017 324-NDA-7 Special Session: DARPA Efficient Quantification of Uncertainty in Physical Systems (EQUiPS) Program II Mustang 2 Chaired by: F. FAHROO and B. SMARSLOK, AFRL/RQH 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs AIAA-2017-1324 AIAA-2017-1325 AIAA-2017-1326 AIAA-2017-1327 AIAA-2017-1328 Information theory based metrics An Adaptive Sampling Approach for Predicting fracture patterns in Scalable Environment for A multi-fidelity framework for for the characterization and Solving PDEs with Uncertain Inputs simulations of brittle materials Quantification of Uncertainty investigating the performance of influence of reinforcing matrix and Evaluating Risk under variable load and material and Optimization in Industrial super-cavitating hydrofoils under phases in polymeric composites Z. Zou, Duke University, Durham, NC; strength Applications (SEQUOIA) uncertain flow conditions P. Bandaru, University of Calfornia, San D. Kouri, Sandia National Laboratories, M. Stoyanov, P. Seleson, C. Webster, Oak J. Alonso, Stanford University, Stanford, CA; L. Bonfiglio, P. Perdikaris, S. Brizzolara, Diego, La Jolla, CA; S. Pfeifer, General Albuquerque, NM; W. Aquino, Duke Ridge National Laboratory, Oak Ridge, TN M. Eldred, Sandia National Laboratories, Massachusetts Institute of Technology, Atomics, San Diego, CA University, Durham, NC Albuquerque, NM; P. Constantine, Colorado Cambridge, MA; G. Karniadakis, Brown School of Mines, Golden, CO; K. Duraisamy, University, Providence, RI University of Michigan, Ann Arbor, Ann Arbor, MI; C. Farhat, G. Iaccarino, Stanford University, Stanford, CA; et al. Wednesday, 11 January 2017 325-OPS-1 Intelligent and Autonomous Systems for Improving Space Operation Grapevine 4 Chaired by: S. BURLEIGH, Jet Propulsion Laboratory 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2017-1329 AIAA-2017-1330 AIAA-2017-1331 AIAA-2017-1332 AIAA-2017-1333 AIAA-2017-1334 Satellite Articulation Sensing using Configuration validation of a novel in- Optical Tracking and Collision Asteroid Planetary Defense and Satellite formation flight vision Reference Ground Station Design Computer Vision space propellant storage and transfer Avoidance System for GEO/MEO Redirection Mission Design navigation system for University Satellite Missions D. Curtis, R. Cobb, Air Force Institute of S. Gangadharan, Embry-Riddle Aeronautical Spacecraft Operators, in use at K. Turkoglu, J. Zhen, San Jose State R. Glebocki, M. Jacewicz, Warsaw with Varying Communication Technology, Wright-Patterson AFB, OH University, Daytona Beach, FL; D. Kirk, Florida Italian MoD University, San Jose, CA University of Technology, Warsaw, Poland Requirements Institute of Technology, Melbourne, FL A. D’Apolito, L. Rizzo, M. Argentiero, A. T. Choi, T. Stevenson, E. Lightsey, Georgia D’Antoni, G. Marino, D. D’Amato, Italian Institute of Technology, Atlanta, GA Ministry of Defence, Rome, Italy Wednesday, 11 January 2017 326-PC-20 Combustion Dynamics III Dallas 7 Chaired by: J. O`CONNOR, Pennsylvania State University and B. CHEHROUDI, European Research Council (ERC) 1400 hrs 1430 hrs 1500 hrs 1530 hrs AIAA-2017-1335 AIAA-2017-1336 AIAA-2017-1337 AIAA-2017-1338 A Study of Acoustic Forcing on Gas- Experimental Investigation of the Forced Response of Flames in a Extraction of response function from Centered Swirl-Coaxial Reacting Flows Ensemble-Averaged Turbulent Bluff-Body Stabilized Annular numerical simulations and their use M. Roa, Sierra Lobo, Inc., Edwards AFB, CA; Displacement Speed Combustor for longitudinal combustion intsbility S. Schumaker, D. Talley, Air Force Research L. Humphrey, T. Lieuwen, Georgia Institute P. Allison, E. Mastorakos, University of modeling Laboratory, Edwards AFB, CA; J. Bennewitz, of Technology, Atlanta, GA Cambridge, Cambridge, United Kingdom M. Frezzotti, F. Nasuti, University of Rome University of California, Los Angeles, Los “La Sapienza”, Rome, Italy; C. Huang, W. Angeles, CA Anderson, Purdue University, West Lafayette, IN Wednesday, 11 January 2017 136 327-PDL-8 Plasma-Based Flow Control: Lessons Learned and Prospects II (Invited) Ft. Worth 4 Chaired by: S. LEONOV, University of Notre Dame and J. POGGIE, Purdue University- Sch of Aero and Astro 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2017-1339 Oral Presentation Oral Presentation Oral Presentation Oral Presentation Oral Presentation Thermal perturbations generated by Thermal and Non-Thermal Effects in Electrohydrodynamic phenomena Plasma Guiding and Deflection of Plasma actuators as tools for Experimental Investigation of near-surface electric discharges and Plasma Aerodynamics in corona discharges and surface High Speed Projectiles understanding transitional flows Dynamic Stall Control by Plasma mechanisms of their interaction with S. Macheret, Purdue University, West plasma actuators for airflow control R. Miles, A. Starikovskiy, Princeton M. Kotsonis, Delft University of Technology, Actuators with Combined Energy/ the airflow Lafayette, IN E. Moreau, N. Benard, University of University, Princeton, NJ; C. Limbach, Delft, The Netherlands Momentum Action I. Adamovich, Ohio State University, Columbus, Poitiers, Poitiers, France Colorado State University, Fort Collins, CO A. Starikovskiy, Princeton University, OH; S. Leonov, University of Notre Dame, Princeton, NJ Notre Dame, IN; K. Frederickson, Ohio State University, Columbus, OH; J. Zheng, Y. Cui, B. Khoo, National University of Singapore, Singapore, Singapore Wednesday, 11 January 2017 328-PDL-9 Plasma and Laser Propulsion Ft. Worth 5 Chaired by: D. LEVIN, University of Illinois and T. MOELLER, University of Tennessee Space Institute 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs AIAA-2017-1340 AIAA-2017-1341 AIAA-2017-1342 AIAA-2017-1343 AIAA-2017-1344 High Temperature Millimeter-Wave Effect of solvents on Ethylammonium Static and Dynamic Stall Control at Particle Simulation of Electrodeless Multiple aperture approach to Permittivity Measurement Setup for nitrate nanostructure in the presence High Angle of Attack by NS pulsed Plasma Thruster with Rotating wavefront prediction for adaptive- Beamed Energy Heat Exchangers of an electric field Actuator in Burst Mode Magnetic Field optic applications M. Hilario, J. Wang, University of Southern N. Mehta, D. Levin, University of Illinois, A. Starikovskiy, Princeton University, D. Uchigasaki, N. Ohnishi, Tohoku M. Kemnetz, S. Gordeyev, University of California, Los Angeles, CA Urbana-Champaign, Urbana, IL Princeton, NJ University, Sendai, Japan Notre Dame, Notre Dame, IN Wednesday, 11 January 2017 329-SCS-5 Deployable Apertures and Novel Structural Concepts Palomino 1 Chaired by: H. FANG and J. BANIK, USAF 1400 hrs 1430 hrs 1500 hrs 1530 hrs AIAA-2017-1345 AIAA-2017-1346 AIAA-2017-1347 AIAA-2017-1348 Modular Foldable Surfaces: a The Straightness of Off-Radial A Study on the Design of Effect of grid geometry on mechanical Novel Approach based on Spatial Ribs with Preloaded Sheet Sections Deployable Cable-Panel Structure behavior of skin added lattice structure Mechanisms and Thin Shells Between - a Wrapped Array Design K. Seino, V. Parque, T. Miyashita, Waseda under axial compression Y. Wei, S. Pellegrino, California Institute of G. Greschik, TentGuild Engineering University, Shinjuku, Japan Y. Shimizu, T. Aoki, T. Yokozeki, University Technology, Pasadena, CA Company, Boulder, CO of Tokyo, Tokyo, Japan Wednesday, 11 January 2017 330-SD-16 Aeroelastic Analysis Appaloosa 2 Chaired by: P. TAYLOR, Gulfstream Aerospace Corporation and T. BARTKOWICZ, Boeing Defense, Space & Security 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs AIAA-2017-1349 AIAA-2017-1350 AIAA-2017-1351 AIAA-2017-1352 AIAA-2017-1353 Geometrical Nonlinear Aeroelastic High-fidelity Multipoint Aerostructural Nonlinear Aeroelastic Analysis of Geometrically-nonlinear effects in Nonlinear Aeroelasticity of Highly Stability Analysis and Active Control Optimization of a High Aspect Ratio Aircraft with Strut-Braced Highly lateral manoeuvres with coupled Flexible Joined-Wing Aircraft using with Piezoelectric Actuators of a Tow-steered Composite Wing Flexible Wings flight dynamics and aeroelasticity Unsteady Vortex-Lattice Method High-Aspect-Ratio Flexible Wing T. Brooks, University of Michigan, Ann Arbor, W. Su, University of Alabama, Tuscaloosa, S. Maraniello, R. Palacios, Imperial College W. Su, Y. Huang, J. Hammerton, University Y. Bi, C. Xie, C. Yang, Beihang University, Ann Arbor, MI; G. Kennedy, Georgia Institute of Tuscaloosa, AL London, London, United Kingdom of Alabama, Tuscaloosa, Tuscaloosa, AL Beijing, China Technology, Atlanta, GA; J. Martins, University of Michigan, Ann Arbor, Ann Arbor, MI Wednesday, 11 January 2017 331-SD-17 Large-Deformation Nonlinear Dynamics, Flexible Multibody Dynamics, Contact/Constraint Modeling Appaloosa 3

137 Chaired by: J. COOPER, University of Bristol and W. SILVA, NASA-Langley Research Center 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs AIAA-2017-1354 AIAA-2017-1355 AIAA-2017-1356 AIAA-2017-1357 AIAA-2017-1358 Evaluating NLROMs’ Ability to Worst Case Gust Prediction of Highly A Computational approach for Multi-Body Dynamics Simulation of Structural Bionic Design for Thin- Predict Dynamic Snap Through of a Flexible Wings vertical launch system by coupled Spacecraft Rendezvous Operations walled Energy Absorber Tube and Curved Beam in a Random Loading R. Cook, D. Calderon, M. Lowenberg, CFD/CSD with hybrid particle level- D. Inoyama, J. Francis, T. Stoumbos, Parametric Analysis Environment S. Nield, J. Cooper, University of Bristol, set method Orbital ATK, Dulles, VA Z. Feng, Z. Luo, J. Xiang, Beihang C. VanDamme, M. Allen, University of Bristol, United Kingdom; E. Coetzee, H. Cho, S. Shin, H. Joo, Seoul National University, Beijing, China Wisconsin, Madison, Madison, WI Airbus, Bristol, United Kingdom University, Seoul, South Korea Wednesday, 11 January 2017 332-SD-18 Flutter and Aeroelastic Analysis II Appaloosa 4 Chaired by: I. CHOPRA, University of Maryland and A. GREWAL, National Research Council Canada 1400 hrs 1430 hrs 1500 hrs 1530 hrs AIAA-2017-1359 AIAA-2017-1360 AIAA-2017-1361 AIAA-2017-1362 Bifurcations of limit-cycle oscillations of Aeroelastic Tailoring using the Spars A Recurrent Neural Network Higher Order Estimations of Load a two degree-of-freedom airfoil caused and Stringers Planform Geometry Controller for Gust Load Alleviation Factor from Derived Gust Velocity by aerodynamic non-linearities G. Francois, J. Cooper, P. Weaver, on a Transport Aircraft K. Rokhsaz, L. Kliment, Wichita State A. van Rooij, J. Nitzsche, German Aerospace University of Bristol, Bristol, United F. Fonte, P. Mantegazza, Technical University, Wichita, KS Center (DLR), Göttingen, Germany; R. Dwight, Kingdom University of Milan, Milan, Italy Delft University of Technology, Delft, The Netherlands Wednesday, 11 January 2017 333-SUR-2/MAT-7 Materials/Materials for Survivability Palomino 3 Chaired by: E. FAHRENTHOLD, University of Texas and G. ODEGARD 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs AIAA-2017-1363 AIAA-2017-1364 AIAA-2017-1365 AIAA-2017-1366 AIAA-2017-1367 Steady State and Transient Creep Simulation for Explosive Sensing Progressive Damage Analysis in Rapid Heat Generation using Development of New Thermal Responses of High Temperature Alloys Materials Design Composites Carbon Nanotubes Protection Systems Based on Silica/ R. Song, A. Muliana, Texas A&M University, E. Fahrenthold, J. Zhang, University of H. Sertse, W. Yu, Purdue University, West S. Loganathan, V. Rollin, D. Kim, Embry- Polysiloxane Composites College Station, TX; A. Palazotto, Air Force Texas, Austin, Austin, TX Lafayette, IN Riddle Aeronautical University, Daytona K. Schellhase, E. Liu, J. Koo, University of Institute of Technology, Wright-Patterson Beach, FL Texas, Austin, Austin, TX; J. Buffy, Dyna- AFB, OH Glass, Perrysburg, OH; R. Brushaber, Texas Research International, Austin, TX Wednesday, 11 January 2017 334-TP-10 Nonequilibrium Radiation Austin 3 Chaired by: A. BRANDIS, AMA Inc at NASA Ames and W. YUEN, The Hong Kong Polytechnic University 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs AIAA-2017-1368 AIAA-2017-1369 AIAA-2017-1370 AIAA-2017-1371 AIAA-2017-1372 Physico-Chemical Parameters Measurement of Carbon Dioxide Development of a Radiative Heating Impact of Non-Tangent-Slab On the development of a new Governing the Convective and Infrared Radiation in the Afterbody Margin Policy for Lunar Return Radiative Transport on Flowﬁeld- nonequilibrium chemistry model for

Radiative Heating from a CO2-based of a Mars entry Capsule Missions Radiation Coupling Mars entry mixture H. Takayanagi, A. Lemal, S. Nomura, K. B. Cruden, A. Brandis, Analytical Mechanics C. Johnston, NASA Langley Research R. Jaffe, D. Schwenke, G. Chaban, D. Y. Higuchi, Ryokoku University, Otsu, Fujita, Japan Aerospace Exploration Agency Associates, Inc., Moffett Field, CA; C. Center, Hampton, VA Prabhu, NASA Ames Research Center, Japan; L. Pierre, École Polytechnique, (JAXA), Tokyo, Japan Johnston, NASA Langley Research Center, Moffett Field, CA; C. Johnston, NASA Palaiseau, France; A. Lemal, S. Hampton, VA Langley Research Center, Hampton, VA; Matsuyama, K. Fujita, Japan Aerospace M. Panesi, University of Illinois at Urbana- Champaign, Urbana, IL

138 Exploration Agency (JAXA), Tokyo, Japan Wednesday, 11 January 2017 335-UMS-10 UAS Technologies and Applications II Grapevine 2 Chaired by: O. ARIFF, University of Salford 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs AIAA-2017-1373 AIAA-2017-1374 AIAA-2017-1375 AIAA-2017-1376 AIAA-2017-1377 Experimental Analysis of Forces Design of a Small UAS for Optimal Strategies for Temporal Feature Variation as an Small Unmanned Aircraft Systems During Take-Off of Birds Manipulation in Cluttered Indoor Meteorological Measurements with Efﬁcient Method for Real-Time for Project-Based Engineering J. Barata, T. Silva, F. Neves, A. Silva, Environments Unmanned Aircraft Video Summarization Captured Education University of Beira Interior, Covilha, D. Sun, R. Jones, T. Marinho, A. A. Avery, J. Jacob, Oklahoma State from Unmanned Aerial Systems P. Di Donato, National Civil Aviation Agency, Portugal Lakshmanan, A. Jones, N. Hovakimyan, University, Stillwater, OK B. Massinas, A. Doulamis, N. Doulamis, D. São José dos Campos, Brazil; P. Gaskell, E. University of Illinois, Urbana-Champaign, Paradissis, National Technical University of Atkins, University of Michigan, Ann Arbor, Urbana, IL Athens, Athens, Greece Ann Arbor, MI Wednesday, 11 January 2017 336-WE-8 Wind Turbine Rotor and Blade Innovations Ft. Worth 7 Chaired by: D. GRIFFITH and K. WETZEL, Wetzel Engineering, Inc. 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs AIAA-2017-1378 AIAA-2017-1379 AIAA-2017-1380 AIAA-2017-1381 AIAA-2017-1382 Wind Tunnel and Field Test Results Numerical analysis of noise Design of a Boundary-Layer Suction Bio-inspired Leading-Edge Effects of Gurney Flaps on the on Reducing Load Oscillations on reduction mechanisms on improved System for Trailing-Edge Noise Tubercles to Improve Fatigue Life in Performance of Diffuser Augmented Wind Turbine Blades using Synthetic trailing edge serrations using the Reduction of an Industrial Wind Horizontal Axis Wind Turbine Blades Wind Turbine Jets Lattice Boltzmann method Turbine B. Ng, T. New, Nanyang Technological V. Dighe, F. Avallone, J. Tang, G. van T. Rice, K. Taylor, M. Amitay, Rensselaer W. van der Velden, Delft University of B. Arnold, University of Stuttgart, Stuttgart, University, Singapore, Singapore; R. Bussel, Delft University of Technology, Polytechnic Institute, Troy, NY Technology, Delft, The Netherlands; S. Germany; C. Rautmann, Nordex Energy GmbH, Palacios, Imperial College London, London, Delft, The Netherlands Oerlemans, Siemens, Brande, Denmark Hamburg, Germany; T. Lutz, E. Kraemer, United Kingdom University of Stuttgart, Stuttgart, Germany Wednesday, 11 January 2017 337-NW-14 Diversity and Inclusion in the Workplace Grapevine A 1500 - 1700 hrs Wednesday, 11 January 2017 338-NW-15 Wednesday Afternoon Networking Coffee Break Longhorn Hall E&F 1530 - 1600 hrs Wednesday, 11 January 2017 339-LEC-5 Structures, Structural Dynamics, and Materials Lecture Texas C 1800 - 1900 hrs Challenges in Integrated Computational Materials Engineering of Aerospace Composites

Anthony M. Waas Boeing-Egtvedt Chair, Professor of Aerostructures Chair, William E Boeing Department of Aeronautics and Astronautics University of Washington Thursday Thursday, 12 January 2017 340-NW-16 Thursday Early Morning Networking Coffee Break Session Room Foyers 0700 - 0730 hrs Thursday, 12 January 2017 341-SB-4 Thursday Morning Speakers’ Brieﬁng Session Rooms

139 0730 - 0800 hrs Thursday, 12 January 2017 342-PLNRY-5 Thursday Morning Plenary: Disruptive Technology Developments - Breakthroughs that will Transform Aerospace Texas A & B 0800 - 0900 hrs Moderator: Samantha Marquart Brainard, Ph.D. Candidate, George Washington, University

Panelists: Danette Allen Neil Gershenfeld Rob High Robert Lutwak Senior Technologist for Intelligent Flight Systems Director, The Center for Bits and Atoms Vice President and Chief Technology Ofﬁcer Program Manager, Microsystems Technology Ofﬁce NASA Langley Research Center Massachusetts Institute of Technology IBM Watson DARPA

Thursday, 12 January 2017 343-NW-17 Thursday Morning Networking Coffee Break Longhorn Hall E&F 0900 - 0930 hrs Thursday, 12 January 2017 344-ABPSI-1 High-Speed Inlets and Scramjets Dallas 1 Chaired by: L. LEAVITT, N A S A and C. CHUCK, The Boeing Company 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2017-1383 AIAA-2017-1384 AIAA-2017-1385 AIAA-2017-1386 Vortex Generators in a Streamline- Trajectory Optimization using Shapeable Inlet Manifold for Research Developments on Rocket- Traced, External-Compression Indirect Methods and Parametric Hypersonic Scramjet Based Combined-Cycle Inlet in Supersonic Inlet Scramjet Cycle Analysis J. Maxwell, G. Goodwin, Naval Research Northwestern Polytechnical University E. Baydar, F. Lu, University of Texas, Arlington, J. Williams, K. Mall, M. Grant, Purdue Laboratory, Washington, D.C. L. Shi, Northwestern Polytechnical Arlington, TX; J. Slater, C. Trefny, NASA Glenn University, West Lafayette, IN University, Xi’an, China Research Center, Cleveland, OH Thursday, 12 January 2017 345-ACD-8 Innovative Aircraft Design Concepts I Grapevine 3 Chaired by: C. NICKOL, NASA Langley Research Center and W. CROSSLEY, Purdue University 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2017-1387 AIAA-2017-1388 AIAA-2017-1389 AIAA-2017-1390 Preliminary Design of an N+1 Cost-Driven Design of a Large Scale Development of an Improved Advanced Tube and Wing Aircraft Overwater Supersonic Commerical X-Plane Wing-Integrated Airborne Antenna for Year 2050 Timeframe Transport Aircraft J. Welstead, NASA Langley Research Array with Applications to Future P. Heinemann, Bauhaus Luftfahrt e.V., M. Mathieu, A. Marin, K. Stephenson, Center, Hampton, VA; P. Frederic, Tecolote Wing Sizing Taufkirchen, Germany; P. Panagiotou, Aristotle J. Beard, E. Castillo, C. Weddle-Weaver, Research, Inc., Santa Barbara, CA; M. E. Arnold, A. Patil, University of Kansas, University of Thessaloniki, Thessaloniki, Greece; Arizona State University, Tempe, AZ; et al. Frederick, S. Jacobson, NASA Armstrong Lawrence, Lawrence, KS P. Vratny, S. Kaiser, M. Hornung, Bauhaus Flight Research Center, Edwards, CA; J. Luftfahrt e.V., Taufkirchen, Germany; K. Berton, NASA Glenn Research Center, Yakinthos, Aristotle University of Thessaloniki, Cleveland, OH Thessaloniki, Greece Thursday, 12 January 2017 346-AFM-7 Special Session: Performance Adaptive Aeroelastic Wing Grapevine 4 Chaired by: B. DANOWSKY, Systems Technology, Inc. and S. KEYES 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2017-1391 AIAA-2017-1392 AIAA-2017-1393 AIAA-2017-1394 AIAA-2017-1395 mAEWing2: Conceptual Design and Multidisciplinary Design Analysis Finite Element Model Updating of A Control-Oriented System and A Newtonian Development of the System Test and Optimization of Performance Small Flexible Composite UAV Parameter Identification of a Small Mean-Axis Equations of Motion for C. Regan, University of Minnesota, Adaptive Aeroelastic Wings W. Zhao, N. Muthirevula, R. Kapania, Flexible Flying-Wing Aircraft Flexible Aircraft Minneapolis, Minneapolis, MN W. Zhao, M. Jrad, R. Gupta, R. Kapania, Virginia Polytechnic Institute and State B. Danowsky, Systems Technology, Inc., S. Keyes, P. Seiler, University of Minnesota, Virginia Polytechnic Institute and State University, Blacksburg, VA; A. Gupta, C. Hawthorne, CA; D. Schmidt, D.K. Schmidt & Minneapolis, Minneapolis, MN; D. Schmidt, University, Blacksburg, VA Regan, P. Seiler, University of Minnesota, Associates, Monument, CO; H. Pfifer, University D.K. Schmidt & Associates, Monument, CO Minneapolis, Minneapolis, MN of Nottingham, Nottingham, United Kingdom 140 Thursday, 12 January 2017 347-AFM-8 Aircraft Flight Dynamics, Handling Qualities, and Performance II Grapevine 5 Chaired by: I. CHAKRABORTY, ASDL, Georgia Tech and K. SHWEYK, Boeing Engineering Operations & Technology 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2017-1397 AIAA-2017-1398 AIAA-2017-1399 AIAA-2017-1400 AIAA-2017-1401 AIAA-2017-0249 Control Law Affect on Spin Handling Qualities Flight Test Dynamic Stability of the Boeing Gust Load Alleviation and Ride Comparison of free flight base Rapid Ascent-Entry Vehicle Mission

Characteristics of Aerodynamically Assessment of a Business Jet N zU CST-100 Quality Improvement with pressure measurements with CFD Optimization Using hp-Adaptive Asymmetric Aircraft P-β Fly-By-Wire Control System V. Aubuchon, D. Owens, NASA Langley Incremental Nonlinear Dynamic predictions Gaussian Quadrature Collocation S. Akhtar, National University of Sciences T. Berger, M. Tischler, Army Aviation and Missile Research Center, Hampton, VA; O. Carvajal, Inversion M. Albisser, S. Dobre, C. Berner, French- A. Miller, A. Rao, University of Florida, and Technology, Islamabad, Pakistan; B. Research Development and Engineering Center, The Boeing Company, Houston, TX; S. X. Wang, E. Van Kampen, Q. Chu, Delft German Research Institute of Saint-Louis Gainesville, Gainesville, FL Malik, J. Masud, Air University, Islamabad, Moffett Field, CA; S. Hagerott, Cessna Aircraft Lumb, The Boeing Company, Huntington University of Technology, Delft, The (ISL), Saint-Louis, France Pakistan Company, Wichita, KS; M. Cotting, J. Gresham, Beach, CA Netherlands J. George, U.S. Air Force Test Pilot School, Edwards AFB, CA; et al. Thursday, 12 January 2017 348-AMT-12 Launch Vehicle Buffet (Invited) Grapevine 2 Chaired by: J. ROSS, NASA Ames Research Center and J. PANDA, NASA Ames Research Center 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs Oral Presentation AIAA-2017-1402 AIAA-2017-1403 AIAA-2017-1404 AIAA-2017-1405 AIAA-2017-1406 Measuring Aerodynamic Buffet on Evaluation of Unsteady Experimental Visualizations of a Comparison of Transonic Buffet Inverse Force Determination on a Wavenumber-Frequency Spectra of a Generic Launch-Vehicle Using Pressure Sensitive Paint Use Generic Launch Vehicle Flow Field: Simulations with Unsteady PSP Small Scale Launch Vehicle Model Pressure Fluctuations on a Generic Unsteady Pressure-Sensitive Paint for Space Launch Vehicle Buffet Time-Resolved Shadowgraph and Measurements for a Hammerhead using a Dynamic Balance Space Vehicle Measured via Fast- J. Ross, NASA Ames Research Center, Determination Infrared Imaging Payload Fairing C. Ngo, Aerospace Computing, Inc., Moffett Response Pressure-Sensitive Paint Moffett Field, CA; M. Sellers, Quantitech, M. Sellers, M. Nelson, Quantitech, Arnold T. Garbeff, J. Panda, J. Ross, N. Smith, S. Murman, L. Diosady, P. Blonigan, NASA Field, CA; J. Powell, NASA Johnson Space J. Panda, N. Roozeboom, J. Ross, NASA Arnold AFB, TN; N. Roozeboom, J. Panda, AFB, TN; N. Burnside, N. Roozeboom, NASA Ames Research Center, Moffett Ames Research Center, Moffett Field, CA Center, Houston, TX; J. Ross, NASA Ames Ames Research Center, Moffett Field, CA D. Atler, NASA Ames Research Center, NASA Ames Research Center, Moffett Field, CA Research Center, Moffett Field, CA Moffett Field, CA; D. Piatak, NASA Langley Field, CA Research Center, Hampton, VA; et al. Thursday, 12 January 2017 349-AMT-13 Rayleigh Scattering Measurements Grapevine B Chaired by: B. BATHEL, NASA Langley Research Center and J. SUTTON, Ohio State University 0930 hrs 1000 hrs AIAA-2017-1407 AIAA-2017-1408 Measurement of Density in High Speed Quantitative 2D Temperature Shear Layers and Oblique Shocks using Imaging in Turbulent Nonpremixed Filtered Rayleigh Scattering Jet Flames using Filtered Rayleigh J. George, T. Jenkins, MetroLaser, Inc., Scattering Laguna Hills, CA; R. Miles, Princeton T. McManus, J. Sutton, Ohio State University, Princeton, NJ University, Columbus, OH Thursday, 12 January 2017 350-APA-33 Aerodynamic Design: Transonic/Supersonic Ft. Worth 2 Chaired by: C. TILMANN, AFRL/RQV and S. MUPPIDI 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2017-1409 AIAA-2017-1410 AIAA-2017-1411 AIAA-2017-1412 AIAA-2017-1413 AIAA-2017-1414 Drag polar prediction Restricted Snakes: a Flexible Validation of LS-FLOW for Reentry Enhanced Manoeuvrability of Delta- Utilizing Direct Numerical Simulations Robust Design of High Speed methodologies during aircraft Topology Parameterisation Method Capsule Unsteady Aerodynamic Canard Combat Aircraft by Vortex of Transition and Turbulence in Design Natural-Laminar-Flow Airfoil for design phases for Aerodynamic Optimisation Analysis Flow Control Optimization – Part 2 High Lift A. de Paula, F. Porto, Technological Institute A. Payot, T. Rendall, C. Allen, University of K. Fujimoto, Japan Aerospace Exploration S. Hitzel, Airbus, Manching, Germany M. Rai, NASA Ames Research Center, H. Zhao, Z. Gao, C. Wang, G. Yuan, of Aeronautics (ITA), São José dos Campos, Bristol, Bristol, United Kingdom Agency (JAXA), Tsukuba, Japan; T. Nambu, Moffett Field, CA Northwestern Polytechnical University, Brazil; M. Sousa, Federal University of Japan Aerospace Exploration Agency Xi’an, China Itajubá, Itajubá, Brazil (JAXA), Chofu, Japan; H. Negishi, Y. Watanabe, Japan Aerospace Exploration Agency (JAXA), Tsukuba, Japan

141 Thursday, 12 January 2017 351-APA-34 Aerodynamic-Structural Dynamic Interactions I Dallas 5 Chaired by: D. ABERNATHY, Lockheed Martin Aeronautics and R. DOWGWILLO, Boeing Engineering Operations & Technology 0930 hrs 1000 hrs 1030 hrs AIAA-2017-1415 AIAA-2017-1416 AIAA-2017-1417 A Drichlet/Neumann Strongly Stall Flutter Prediction and Improved Computational Approach for Coupled Iterative Method for Fluid Experimental Verification using a 3-D Realistic Insect-like Flapping Wing Structure Interaction of Parafoil Cyber-Physical Wing using Co-rotational Finite Elements Inflation Process C. Fagley, D. Broadbent, J. Seidel, T. H. Cho, Seoul National University, Seoul, South S. Nie, Y. Cao, Beihang University, Beijing, McLaughlin, U.S. Air Force Academy, Korea; N. Lee, Inha University, Incheon, South China Colorado Springs, CO Korea; S. Shin, Seoul National University, Seoul, South Korea; S. Lee, Inha University, Incheon, South Korea; S. Kim, Agency for Defense Development, Daejeon, South Korea Thursday, 12 January 2017 352-APA-35 Airfoil/Wing/Configuration Aerodynamics II: Multifidelity Methods Dallas 3 Chaired by: J. PINIER, NASA Langley Research Center and D. O’BRIEN, US Army RDECOM 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2017-1418 AIAA-2017-1419 AIAA-2017-1420 AIAA-2017-1421 AIAA-2017-1422 Surrogate Models for Surface Designing Wings with Fixed Twist Aerodynamic Shape Optimization of An Efficient Multistep ROM Method The Thickness Effect on Symmetrical Vorticity for Minimum Induced Drag Morphing Wings at Multiple Flight for Prediction of Flows over Airfoils Airfoil Flow Characteristics at low M. Carpenter, R. Hartfield, Auburn D. Hunsaker, W. Phillips, Utah State Conditions C. Cao, J. Cai, K. Qu, J. Li, Northwestern Reynolds number University, Auburn, AL; V. Ahuja, Research University, Logan, UT; J. Joo, Air Force D. Hunsaker, W. Phillips, Utah State Polytechnical University, Xi’an, China A. de Paula, V. Kleine, F. Porto, in Flight, Auburn, AL Research Laboratory, Dayton, OH University, Logan, UT; J. Joo, Air Force Technological Institute of Aeronautics (ITA), Research Laboratory, Dayton, OH São José dos Campos, Brazil Thursday, 12 January 2017 353-APA-36 Applied CFD I: Boundary Layer and Solver Methodologies Dallas 4 Chaired by: K. VANDEN, USAF and B. MARPLES, Johns Hopkins University Applied Physics Laboratory 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2017-1423 AIAA-2017-1424 AIAA-2017-1425 AIAA-2017-1426 AIAA-2017-1427 Oral Presentation CFD Investigation Using Bleed as a Numerical Study of the Numerical and Experimental Testing On the Stall Characteristics of Iced Interpolation Techniques for Requirements for Certification by Method of Active Flow Control Aerodynamics of DLR-F6 Wing-Body of a Morphing Upper Surface Wing Wings Data Reconstruction at Surface in Analysis and Implications for CFD D. Chang, D. Crowe, Air Force Institute of in Unbounded Flow Field and in Equipped with Conventional and A. Ribeiro, B. Konig, E. Fares, Exa Immersed Boundary Method R. Gregg-III, The Boeing Company, Technology, Wright-Patterson AFB, OH; Ground Effect Morphing Ailerons Corporation, Stuttgart, Germany A. Bharadwaj S, S. Ghosh, C. Joseph, Mukilteo, WA; J. Alonso, Stanford S. Sherer, Air Force Research Laboratory, N. Deng, Q. Qu, R. Agarwal, Washington A. Koreanschi, S. Oliviu, Y. Tondji, R. Botez, Indian Institute of Technology Madras, University, Stanford, CA Wright-Patterson AFB, OH University in St. Louis, St. Louis, MO University of Québec, Montréal, Canada Chennai, India Thursday, 12 January 2017 354-APA-37 Special Session: Simulation of Rotor in Hover I Dallas 2 Chaired by: N. HARIHARAN, CREATE-AV and R. NARDUCCI, Boeing Defense, Space & Security 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2017-1429 AIAA-2017-1430 AIAA-2017-1431 AIAA-2017-1432 Oral Presentation AIAA Standardized Hover Simulation: Comparison of Steady-State and Parameter Studies on the S-76 OVERFLOW Rotor Simulations Using On the breakdown of wake in Hover Performance Prediction Status Time-Dependent Solutions for the Rotor Using HELIOS Advanced Turbulence and Transition computed hover Navier-Stokes and Outstanding Issues S-76 Model-Scale Rotor in Hover J. Abras, Naval Air Systems Command, Modeling simulations N. Hariharan, CREATE AV Team, Lorton, R. Narducci, The Boeing Company, Patuxent River, MD; N. Hariharan, CREATE J. Coder, Pennsylvania State University, N. Hariharan, HPCMP CREATE-AV, Lorton, VA VA; R. Narducci, The Boeing Company, Philadelphia, PA AV Team, Lorton, VA University Park, PA Philadelphia, PA; E. Reed, A. Egolf, Sikorsky Aircraft Corporation, Stratford, CT Thursday, 12 January 2017

142 355-APA-38 Transonic/Supersonic Aerodynamics Dallas 6 Chaired by: J. LATZ, Northrop Grumman Aerospace Systems and M. CONWAY, The Aerospace Corporation 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2017-1433 AIAA-2017-1434 AIAA-2017-1435 AIAA-2017-1436 AIAA-2017-1437 AIAA-2017-1438 Computational Study of Supersonic High Resolution Numerical Schemes Onset of unsteadiness in aero- Numerical Investigation of Transonic Dynamic CFD Simulations of the Buffet Simulations with a Lattice- Flow Past Wall-Mounted Cylindrical and Supersonic Flow over a engine intakes at incidence Buffet on a Three-Dimensional Supersonic Inflatable Aerodynamic Boltzmann based Transonic Solver and Hemispherical Bodies Backward-Facing Step A. Coschignano, H. Babinsky, University of Wing using Incremental Mode Decelerator (SAID) Ballistic Range A. Ribeiro, B. Konig, D. Singh, E. Fares, P. Morgan, Ohio Aerospace Institute, Dayton, O. Khan, Tuskegee University, Tuskegee, Cambridge, Cambridge, United Kingdom Decomposition Tests Exa Corporation, Stuttgart, Germany; R. OH; S. Sherer, M. Visbal, Air Force Research AL; G. Arshed, National University of Y. Ohmichi, A. Hashimoto, Japan Aerospace J. Brock, E. Stern, M. Wilder, NASA Ames Zhang, P. Gopalakrishnan, Exa Corporation, Laboratory, Wright-Patterson AFB, OH Sciences and Technology, Karachi, Pakistan Exploration Agency (JAXA), Tokyo, Japan Research Center, Moffett Field, CA Boston, MA; et al. Thursday, 12 January 2017 356-ASC-5 Active Noise and Vibration Control, Smart Sensor and Actuator Device Design Palomino 3 Chaired by: J. KAUFFMAN, University of Central Florida and D. HARTL, Texas A&M University 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2017-1439 AIAA-2017-1440 AIAA-2017-1441 AIAA-2017-1442 AIAA-2017-1443 Resonance Frequency Detuning in Model Reference Adaptive Sliding Investigation of a Parallel Active Multi-fidelity Analysis and Liquid Metal Integration for Regions of High Modal Density Mode Control of a Laser Beam for Vibration Isolation Mount for Experimental Characterization Expedited Heating and Cooling G. Lopp, J. Kauffman, University of Central Jitter Correction Mitigating N/Rev Helicopter of Muscular-Skeletal Structures of Monolithic and Composite SMA Florida, Orlando, FL S. Samantaray, R. Padhi, Indian Institute of Vibrations Optimized via Genetic Programming Actuators Science, Bengaluru, India A. Fereidooni, S. Graham, E. Chen, V. D. Hartl, B. Bielefeldt, Texas A&M J. Mingear, A. Greer, B. Bielefeldt, D. Hartl, Wickramasinghe, National Research Council University, College Station, TX; G. Reich, Texas A&M University, College Station, TX Canada, Ottawa, Canada P. Beran, Air Force Research Laboratory, Wright-Patterson AFB, OH Thursday, 12 January 2017 357-EXPL-1 Habitation Systems Palomino 1 Chaired by: S. SHARMA, NASA Ames Research Center 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2017-1444 AIAA-2017-1445 AIAA-2017-1446 AIAA-2017-1447 AIAA-2017-1448 Design and Development of Analysis of a Radioisotope Thermal Lunar Environtmental and Generating Artificial Gravity on A Study in Selected Power Support Systems for Future Human Rocket Engine Construction Challenges and a Planetary Bodies Subsystems and Components of Extravehicular Activity J. Machado-Rodriguez, G. Landis, NASA Proposed Semi-Circular Frame R. White, Purdue University, West Space Electric Propulsion M. Miller, Georgia Institute of Technology, Glenn Research Center, Cleveland, OH Membrane Habitat Lafayette, IN A. Gohardani, International Rectifier HiRel Atlanta, GA; D. Coan, A. Abercromby, NASA F. O’Donnell, R. Malla, University of Products, El Segundo, CA Johnson Space Center, Houston, TX; K. Feigh, Connecticut, Storrs, Storrs, CT Georgia Institute of Technology, Atlanta, GA Thursday, 12 January 2017 358-F360-7 Managing Change During the Development of Disruptive Technologies Texas C 0930 - 1130 hrs Moderator: Jocelyn Harrison, Program Manager, Air Force Office of Scientific Research

Panelists: Irene Gregory Rob High Steven Huybrechts Robert Lutwak Samantha Magill Senior Technologist for Advanced Control Theory and Vice President and Chief Technology Ofﬁcer Chief of Staff Program Manager, Microsystems Technology Ofﬁce Special Projects, Inclusion & Diversity Applications IBM Watson Applied Minds LLC DARPA Honda Aircraft Company NASA Langley Research Center

Thursday, 12 January 2017 359-FD-46 Boundary Layer Separation Control Texas 1

143 Chaired by: J. LITTLE, The University of Arizona 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2017-1449 AIAA-2017-1450 AIAA-2017-1451 AIAA-2017-1452 Flow around Low Aspect Ratio Experimental Study of Discrete Jet Use of local periodic heating for Separation delay via hydro-acoustic Cylinders and their Applications Forcing for Flow Separation Control separation control on a NACA 0012 control of a NACA4412 airfoil in S. Gildersleeve, M. Amitay, Rensselaer on a Wall Mounted Hump airfoil pre-stalled conditions Polytechnic Institute, Troy, NY; D. Clingman, D. Borgmann, A. Pande, J. Little, C. Yeh, P. Munday, K. Taira, Florida State J. Bodart, G. Shelekhov, Higher Institute of The Boeing Company, Milton, WA University of Arizona, Tucson, Tucson, AZ; University, Tallahassee, FL Aeronautics and Space, Toulouse, France; R. Woszidlo, The Boeing Company, St. C. Scalo, Purdue University, Lafayette, IN; Louis, MO L. Joly, Higher Institute of Aeronautics and Space, Toulouse, France Thursday, 12 January 2017 360-FD-47 Internal Flow Control Texas 2 Chaired by: D. BRZOZOWSKI, The Boeing Company and B. VUKASINOVIC, Georgia Institute of Technology 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2017-1453 AIAA-2017-1454 AIAA-2017-1455 AIAA-2017-1456 Active Flow Control in a Cascade Experimental and Numerical Numerical Investigation of Fluidic Numerical Investigation of Low Thrust Reverser Investigation of Controlled Flow Oscillator Flow Control in an S-Duct Reynolds Number Flow in Turbine A. Gissen, The Boeing Company, St. Louis, MO; Distortion in a Subsonic Offset Diffuser Passage B. Vukasinovic, Georgia Institute of Technology, Diffuser by Trapped Vorticity M. Lakebrink, M. Mani, C. Winkler, The S. Romero Martinez, A. Gross, New Mexico Atlanta, GA; N. Packard, The Boeing Company, B. Vukasinovic, T. Burrows, A. Glezer, Boeing Company, St. Louis, MO State University, Las Cruces, NM Seattle, WA; D. Brzozowski, The Boeing Georgia Institute of Technology, Atlanta, Company, St. Louis, MO; A. Glezer, Georgia GA; M. Lakebrink, M. Mani, The Boeing Institute of Technology, Atlanta, GA Company, St. Louis, MO Thursday, 12 January 2017 361-FD-48 Boundary Layers and Shear Layers I Texas 4 Chaired by: Q. WANG, MIT and C. REED, Lockheed Martin Corporation 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2017-1457 AIAA-2017-1458 AIAA-2017-1459 AIAA-2017-1460 AIAA-2017-1461 AIAA-2017-1462 Development of Trip Line Sub- Observation of the development of Towards laminar flow control on Numerical Simulations of Active Cross-stream Contributions to Resonant growth of surface Region Approach for Flow Transition -vortex to hairpin vortex packet swept wings with AC-DBD plasma Flow Control for Highly Loaded Low- Wing Wake Free Shear Layers pressure fluctuation in hypersonic Modeling Y. Yang, S. Tian, C. Liu, University of Texas, actuators as active roughness Pressure Turbine Cascade Using Particle Image Velocimetry: boundary layer in shock tunnel D. Yeh, J. Slotnick, The Boeing Company, Arlington, Arlington, TX J. Serpieri, S. Yadala Venkata, M. Kotsonis, A. Gross, New Mexico State University, Las Challenges and Results K. Itoh, H. Tanno, T. Komuro, Japan Huntington Beach, CA Delft University of Technology, Delft, The Cruces, NM; C. Marks, R. Sondergaard, M. Memon, A. Altman, University of Aerospace Exploration Agency (JAXA), Netherlands Air Force Research Laboratory, Wright- Dayton, Dayton, OH Kakuda, Japan Patterson AFB, OH Thursday, 12 January 2017 362-FD-49 Multiphase Flows I Texas 3 Chaired by: J. HARTWIG, NASA Glenn Research Center and C. TSAI, Lockheed Martin Space Systems 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2017-1463 AIAA-2017-1464 AIAA-2017-1465 AIAA-2017-1466 AIAA-2017-1467 AIAA-2017-1468 Uncertainty Quantification of Longitudinal Wavelength of Pneumatic Transport of Drill Measurements of the Initial Transient Deformation and Breakup Numerical Simulation of a Droplet Experiments on a Small Number of Oscillating Liquid Sheet with Air Cuttings Under Venus Conditions Transient of a Dense Particle Curtain of a Droplet in Confined Shear Flow Impacting upon Films with Varied Explosively-Driven Particles Flow J. Lambert, J. Rabinovitch, Jet Propulsion Following Shock Wave Impingement Q. Qu, F. Liu, P. Liu, Beihang University, Liquid Properties K. Hughes, University of Florida, Gainesville, I. Oshima, A. Sou, R. Kawabata, Kobe Laboratory, California Institute of E. DeMauro, J. Wagner, S. Beresh, P. Beijing, China; R. Agarwal, Washington Y. Zhang, P. Liu, Q. Qu, F. Liu, Beihang Gainesville, FL; A. Diggs, D. Littrell, Air Force University, Kobe, Japan; K. Matsuura, Technology, Pasadena, CA Farias, A. Turpin, W. Sealy, Sandia National University in St. Louis, St. Louis, MO University, Beijing, China; R. Agarwal, Research Laboratory, Eglin AFB, FL; S. Japan Aerospace Exploration Agency Laboratories, Albuquerque, NM; et al. Washington University in St. Louis, St. Balachandar, R. Haftka, N. Kim, University of (JAXA), Chofu, Japan Louis, MO Florida, Gainesville, Gainesville, FL; et al.

144 Thursday, 12 January 2017 363-FD-50 Reacting Flows Texas 5 Chaired by: J. BORIS, US Naval Research Lab 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2017-1469 AIAA-2017-1470 AIAA-2017-1471 AIAA-2017-1472 AIAA-2017-1473 Non-Adiabatic Tabulation Methods Shock-Tube Boundary-Layer LES modeling of piloted jet flames The Impact of Global Parameters Simulation of turbulent reactive flows to predict Wall-Heat Loads in Rocket Growth Effects on Reflected-Shock with inhomogeneous inlets using of the Gas Mixture on Flow Field using a hybrid LES / PDF methodology Combustion Conditions in Bath Gases with and tabulated chemistry methods and Direct Combustion Noise of a - Advances in particle density control J. Zips, H. Müller, M. Pfitzner, University of without CO2 G. Maio, M. Cailler, B. Fiorina, École Turbulent Jet Flame for normalized variables the German Federal Armed Forces, Munich, J. Hargis, E. Petersen, Texas A&M Centrale Paris, Paris, France; R. Mercier, H. Nawroth, C. Paschereit, Technical J. Vedovoto, M. Damasceno, J. Guarato Germany University, College Station, TX Safran Group, Paris, France; V. Moureau, University of Berlin, Berlin, Germany de Freitas Santos, A. Silveira Neto, Federal CORIA, Rouen, France University of Uberlândia, Uberlândia, Brazil; R. Serfaty, CENPES-PETROBRAS, Rio de Janeiro, Brazil Thursday, 12 January 2017 364-FD-51 Cavity Flows Texas 6 Chaired by: A. AHMED, Auburn University 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2017-1474 AIAA-2017-1475 AIAA-2017-1476 AIAA-2017-1477 AIAA-2017-1478 Measurements of Finite-Span Flow Characteristics of Axisymmetric Spatial Distribution of Pressure Implicit Large-Eddy Simulation of a Pressure Rate of Strain, Pressure Complex Cavities Using PIV and Cavity Resonance in a Rectangular Cavity Supersonic Cavity Diffusion and Velocity Pressure High-Speed Pressure Sensitive Paint B. Brooker, N. Chaganti, R. Weiner, S. K. Casper, J. Wagner, S. Beresh, R. Spillers, D. Peterson, Innovative Scientific Solutions, Gradient Tensor Measurements in a E. DeMauro, K. Casper, S. Beresh, J. Olcmen, University of Alabama, Tuscaloosa, J. Henfling, Sandia National Laboratories, Inc., Dayton, OH; E. Hassan, Air Force Research Cavity Shear Layer Flow Wagner, J. Henfling, R. Spillers, Sandia Tuscaloosa, AL Albuquerque, NM Laboratory, Wright-Patterson AFB, OH X. Liu, San Diego State University, National Laboratories, Albuquerque, NM San Diego, CA; J. Katz, Johns Hopkins University, Baltimore, MD Thursday, 12 January 2017 365-FD-52 LES/DES Simulations Grapevine C Chaired by: N. BISEK, Air Force Reseach Laboratory and R. GOSSE, AFRL/RQH 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2017-1479 AIAA-2017-1480 AIAA-2017-1481 AIAA-2017-1482 AIAA-2017-1483 Numerical Investigation on the Effect Influence of the External Aeroshell Numerical Investigation of Spanwise Modeling of Three Dimensional Towards Predicting Dry Cable of Ground Proximity on the Transient on the HIFiRE-6 Internal Flow Path End Effects on Dynamic Stall of a Effects in Fuel Film Cooling Galloping using Detached Eddy Forces of Low Aspect Ratio Wings using High-Fidelity Simulations Pitching NACA 0012 Wing K. Brown, E. Coy, M. Harvazinski, V. Simulations B. Johnson, Hokkaido University, Sapporo, N. Bisek, Air Force Research Laboratory, M. Visbal, D. Garmann, Air Force Research Sankaran, Air Force Research Laboratory, X. Wu, A. Sharma, M. Jafari, P. Sarkar, Japan; M. Tsubokura, Kobe University, Kobe, Wright-Patterson AFB, OH Laboratory, Wright-Patterson AFB, OH Edwards AFB, CA Iowa State University, Ames, IA Japan Thursday, 12 January 2017 366-GNC-15 Airflow Mechanosensing for Aircraft Navigation and Control Grapevine 1 Chaired by: Y. XU, University of Central Florida and B. DICKINSON, Air Force Reseach Laboratory 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2017-1484 AIAA-2017-1485 AIAA-2017-1486 AIAA-2017-1487 AIAA-2017-1488 AIAA-2017-1489 Tip-Vortex Localization for Cross- Active Gust Alleviation using Active Camber Control of Flexible Bio-inspired Distributed Strain Fixed Wing Micro Aerial Vehicle Thin film flow sensor for unmanned Stream Position Control of a Multi- Artificial Hair Sensors and Airfoils using Artificial Hair Sensors and Airflow Sensing for Small Pitching Control Based on Flow Field aerial platforms Hole Probe Relative to a Stationary Feedforward Control W. Su, H. Spencer, University of Alabama, Unmanned Air Vehicle Flight Control Patterns L. Castano, A. Flatau, University of Wing in a Free-Jet Wind Tunnel K. Thapa Magar, University of Dayton, Tuscaloosa, Tuscaloosa, AL S. Araujo-Estrada, F. Salama, C. K. Thompson, Y. Xu, A. Mark, University of Maryland, College Park, College Park, MD; N. Lauer, D. Yeo, D. Paley, University of Dayton, OH; G. Reich, A. Pankonien, B. Greatwood, K. Wood, T. Richardson, S. Central Florida, Orlando, FL; B. Dickinson, Air J. Hubbard, National Institute of Aerospace, Maryland, College Park, College Park, MD Smyers, Air Force Research Laboratory, Windsor, University of Bristol, Bristol, Force Research Laboratory, Eglin AFB, FL Hampton, VA Wright-Patterson AFB, OH United Kingdom Thursday, 12 January 2017

145 367-GNC-16 Verification and Validation of Adaptive Systems I Austin 2 Chaired by: T. YUCELEN, Missouri University of Science & Technology and J. MUSE, AFRL/RQQA 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2017-1490 AIAA-2017-1491 AIAA-2017-1492 AIAA-2017-1493 AIAA-2017-1494 AIAA-2017-1495 Robust and Adaptive Output Model Reference Adaptive Control Observer-Based Feedback Adaptive Stability Analysis of Human- Adaptive Model Predictive Control Analysis of Simple Relay Feedback Feedback Control for Non-Minimum in the Presence of Actuator Control for Nonlinear Hypersonic Adaptive Controller Interactions of Uncertain Systems with Input Adaptive Control Phase Systems with Arbitrary Dynamics with Applications to the Vehicles T. Yucelen, University of South Florida, Tampa, Constraints Y. Yoon, E. Johnson, Georgia Institute of Relative Degree Input Time-Delay Problem D. Famularo, J. Valasek, Texas A&M FL; Y. Yildiz, Bilkent University, Ankara, Turkey; M. Yayla, A. Kutay, Middle East Technical Technology, Atlanta, GA E. Lavretsky, The Boeing Company, B. Gruenwald, T. Yucelen, University University, College Station, TX; J. Muse, M. R. Sipahi, Northeastern University, Boston, MA; University, Ankara, Turkey Huntington Beach, CA of South Florida, Tampa, FL; J. Muse, Bolender, Air Force Research Laboratory, E. Yousefi, Bilkent University, Ankara, Turkey; Air Force Research Laboratory, Wright- Wright Patterson AFB, OH N. Nguyen, NASA Ames Research Center, Patterson AFB, OH Moffett Field, CA Thursday, 12 January 2017 368-GNC-17 Entry, Descent and Landing GNC Technology I Austin 4 Chaired by: J. CARSON, NASA Jet Propulsion Laboratory and R. SOSTARIC, NASA-Johnson Space Center 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2017-1496 AIAA-2017-1497 AIAA-2017-1498 AIAA-2017-1499 AIAA-2017-1500 COBALT: Development of a Platform Evaluation of the Simple Safe Site Comparison of Factorization-based Linear Covariance Analysis for a Successive Convexification for Mars to Flight Test Lander GN&C Selection (S4) Hazard Detection Filtering for Landing Navigation Lunar Lander 6-DoF Powered Descent Landing Technologies on Suborbital Rockets Algorithm using Helicopter Field J. McCabe, Missouri University of Science J. Jang, S. Bhatt, M. Fritz, D. Woffinden, Guidance J. Carson, NASA Johnson Space Center, Test Data and Technology, Rolla, MO; A. Brown, Draper Laboratory, Houston, TX M. Szmuk, U. Eren, B. Acikmese, University of Houston, TX; C. Seubert, Jet Propulsion M. Luna, E. Almeida, G. Spiers, C. NASA Johnson Space Center, Houston, TX; Washington, Seattle, Seattle, WA Laboratory, California Institute of Technology, Villalpando, A. Johnson, N. Trawny, Jet K. DeMars, Missouri University of Science Pasadena, CA; F. Amzajerdian, NASA Langley Propulsion Laboratory, California Institute of and Technology, Rolla, MO; J. Carson, Research Center, Hampton, VA; C. Bergh, Technology, Pasadena, CA NASA Johnson Space Center, Houston, TX A. Kourchians, Jet Propulsion Laboratory, California Institute of Technology, Pasadena, CA; C. Restrepo, NASA Johnson Space Center, Houston, TX; et al. Thursday, 12 January 2017 369-GNC-18 Control Theory, Analysis and Design I Austin 5 Chaired by: A. NARANG-SIDDARTH, University of Washington and R. YEDAVALLI, The Ohio State University 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2017-1501 AIAA-2017-1502 AIAA-2017-1503 AIAA-2017-1504 AIAA-2017-1505 AIAA-2017-1506 Normal Form for Linear Infinite- Simple Adaptive Control System Optimal Trajectory Planning of Mismatch-Observer Based Model Resilient Control of Active-Passive Mesh Refinement Method for Dimensional Systems in Hilbert Space Design Trades Wheeled Mobile Robot Using Reference Adaptive Control Networked Multiagent Systems Optimal Control Problems with and Its Role in Direct Adaptive Control E. Mooij, Delft University of Technology, Nonlinear Receding Horizon for Transient Performance in the Presence of Persistent Discontinuous Control Profiles of Distributed Parameter Systems Delft, The Netherlands K. Turkoglu, M. Miller, San Jose State Improvement of Aircraft Disturbances Y. Agamawi, W. Hager, A. Rao, University M. Balas, Embry-Riddle Aeronautical University, University, San Jose, CA S. Kim, Y. Kim, Seoul National University, D. Tran, T. Yucelen, University of South of Florida, Gainesville, Gainesville, FL Daytona Beach, FL; S. Frost, NASA Ames Seoul, South Korea Florida, Tampa, FL; J. Peterson, Missouri Research Center, Moffett Field, CA University of Science and Technology, Rolla, MO Thursday, 12 January 2017 370-GNC-19 Missile Guidance Austin 1 Chaired by: S. KOWALCHUK, Sandia National Laboratories and R. TEKIN, ASELSAN Inc 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2017-1507 AIAA-2017-1508 AIAA-2017-1509 AIAA-2017-1510 Optimal Guidance With an in Route A Non-Switching Guidance Law Impact Angle Control Based on Nonlinear Robust Inscribed Angle Look-Angle Constraint for Impact Angle Constrained Feedback Linearization Guidance for Stationary Targets V. Shaferman, Technology University of Interception of Moving Targets R. Tekin, F. Holzapfel, Technical University S. Kumar, R. Tsalik, T. Shima, Technion-- Vienna, Vienna, Austria V. A, A. Ratnoo, Indian Institute of Science, of Munich, Munich, Germany Israel Institute of Technology, Haifa, Israel Bengaluru, India Thursday, 12 January 2017

146 371-GNC-20 Predictive Control Methods Grapevine D Chaired by: E. ATKINS, University of Michigan and V. STEPANYAN, Universities Space Research Association 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2017-1511 AIAA-2017-1512 AIAA-2017-1513 AIAA-2017-1514 AIAA-2017-1515 AIAA-2017-1516 Model Predictive Control Based Integral Nonlinear MPC for Fixed-wing UAV Stall Recovery Guidance Using Fast Application of Generalized Nonlinear System Finite-Time Cooperative Control of Unmanned Line-of-Sight Curved Path Following for Trajectory Tracking: Implementation Model Predictive Control Predictive Control to an Output Reachability for Flight Aerial Vehicles based on Nonlinear Unmanned Aerial Vehicle and Flight Experiments S. Schuet, T. Lombaerts, J. Kaneshige, K. Experimental Data-based Control given Uncertain Airspeed Model Predictive Control S. Zhao, X. Wang, D. Zhang, L. Shen, T. Stastny, A. Dash, R. Siegwart, Swiss Shish, V. Stepanyan, NASA Ames Research Aeroelastic System H. Rastgoftar, X. Ni, E. Atkins, University of P. Ru, K. Subbarao, University of Texas, National University of Defense Technology, Federal Institute of Technology, Zürich, Center, Moffett Field, CA W. Zhuang, Z. Wu, C. Yang, Beihang Michigan, Ann Arbor, Ann Arbor, MI Arlington, Arlington, TX Changsha, China Switzerland University, Beijing, China Thursday, 12 January 2017 372-GNC-21 Spacecraft and Launch Navigation Grapevine 6 Chaired by: J. REED, United Launch Alliance, LLC and K. BOLLINO, U.S. Air Force 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2017-1517 AIAA-2017-1518 AIAA-2017-1519 AIAA-2017-1520 AIAA-2017-1521 Orbit Injection Error Mitigation by Spacecraft Relative Navigation Multiple-Model Adaptive Estimation Space Object Data Association Relative Navigation in Asteroid Time-Differenced GPS Carrier Phase using Only Range-Rate for Star Identiﬁcation with Two Stars Using Spatial Pattern Recognition Missions: A Dual Quaternion Approach Observables-Aided Inertial Navigation Measurements S. Szklany, J. Crassidis, State University of Approaches B. Razgus, E. Mooij, Delft University of S. P V, D. Thomas, Defence Research and C. Kilic, J. Christian, West Virginia New York, Amherst, NY A. Kalur, P. Silversmith, J. Crassidis, State Technology, Delft, The Netherlands; D. Development Organisation, Hyderabad, India University, Morgantown, WV University of New York, Amherst, NY Choukroun, Ben-Gurion University of the Negev, Be’er Sheva, Israel Thursday, 12 January 2017 373-GNC-22 Aerospace Robotics Control Austin 6 Chaired by: A. DE RUITER, Ryerson University and S. ULRICH, Carleton University 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2017-1522 AIAA-2017-1523 AIAA-2017-1524 AIAA-2017-1525 AIAA-2017-1526 AIAA-2017-1527 Relative Motion Modeling and Trajectory-Driven Adaptive Nonlinear Adaptive Control of a Fixed- Pseudospectral Model Predictive Robust Control of Quadrotors using Dynamic Vehicle Routing with Control for a Quadrotor Landing on Control of Autonomous UAVs with Wing UAV using Multilayer Perceptrons Control under Partially Learned Neuro-Adaptive Control Augmented Indirect Communication via an Unmanned Vessel Disturbance Accommodation S. Bhandari, N. Patel, California State Dynamics with State Estimation Unattended Ground Sensors C. Jin, M. Zhu, L. Sun, Z. Zheng, Beihang D. Painter, N. Prabhakar, R. Prazenica, M. Polytechnic University, Pomona, Pomona, CA M. Gandhi, Y. Pan, E. Theodorou, Georgia G. Joshi, University of Illinois, Urbana- C. Olsen, D. Kunz, Air Force Institute of University, Beijing, China Balas, Embry-Riddle Aeronautical University, Institute of Technology, Atlanta, GA Champaign, Urbana, IL; R. Padhi, Indian Technology, Wright-Patterson AFB, OH Daytona Beach, FL Institute of Science, Bengaluru, India Thursday, 12 January 2017 374-GT-8 Real-Time Control, Data Acquisition and Analysis Ft. Worth 6 Chaired by: M. RHODE, NASA-Langley Research Center and S. SIMERLY, NASA Glenn Research Center 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2017-1528 AIAA-2017-1529 AIAA-2017-1530 AIAA-2017-1531 AIAA-2017-1532 Design and Development of a Upgrades to Common Data Modernization of the real time control Design, Fabrication, and Testing of Mathematical Modeling of Wind Control Scheme for the UC2AV: Acquisition System Software and data acquisition systems at the a B-Dot Probe in Arc Heaters Tunnels for Low Reynolds Number Unmanned Circulation Control Development for NASA’s Rocket National Research Council of Canada’s C. Rudolf, J. Sheeley, W. Scott, Arnold Unsteady Aerodynamic Testing Aerial Vehicle Propulsion Test Facilities and 1.5m Tri-Sonic Wind Tunnel Engineering Development Complex, Arnold M. Rennie, B. Catron, University of Notre C. Rosen, K. Kanistras, P. Saka, K. Software Reuse G. Burns, M. Sabbagh, S. Rutherford, Y. AFB, TN Dame, Notre Dame, IN; D. Williams, M. Valavanis, M. Rutherford, University of P. Hebert, A. Elliot, K. Mobbs, NASA Stennis Cronier, National Research Council Canada, Feroz, Illinois Institute of Technology, Denver, Denver, CO Space Center, Stennis Space Center, MS Ottawa, Canada Chicago, IL Thursday, 12 January 2017

147 375-GT-9 Selected Papers from the 10th International Symposium on Strain-Gauge Balances Held at CARDC (Invited) San Antonio 5 0930 - 1230 hrs

A Review of Wind Tunnel Balance Technologies with a Look Towards the Future Design, Manufacture and Commissioning of a New NLR 6-Component Rotating Shaft Design Concepts of Fatigue Tolerant Wind Tunnel Balances Devin Burns Balance for Propeller Tests at Delft University of Technology Henry Bennett NASA Langley Research Center Ruben Nahuis The Boeing Company Netherlands Aerospace Center (NLR) Strain Gauge Balance Optimization Platform Based on Web Service and Process Encapsulation Design, Calibration and Commissioning of a Small Cryogenic High Load Balance for ETW An Experimental Six Component Wind Tunnel Block Balance Using Fibre Sensors Xiang Guangwei Jennifer Semmelmann Francois Pieterse China Aerodynamic Research and Development Center European Transonic Wind Tunnel (ETW) University of Johannesburg

Thursday, 12 January 2017 376-GTE-8 Advanced Turbine Cooling II San Antonio 4 Chaired by: A. SURYANARAYANAN, FMC Technologies 0930 hrs 1000 hrs 1030 hrs AIAA-2017-1533 AIAA-2017-1534 AIAA-2017-1535 Variable Fidelity Optimization of U-turn Optimization of a Ribbed Impingement Heat Transfer Film Cooling Hole Arrangement Turbine Blade Cooling Channel Characteric of a Sweeping Jet Considering Internal Cooling Effects Using a Meshless Optimization R. Lundgreen, M. Hossain, R. Prenter, J. Y. Kim, S. Lee, Seoul National University, Technique Bons, J. Gregory, A. Ameri, Ohio State Seoul, South Korea; J. Kim, Hanyang F. Kiyici, S. Yilmazturk, E. Arican, Tusas University, Columbus, OH University, Seoul, South Korea; D. Rhee, Engine Industries, Inc., Eskisehir, Turkey; Korea Aerospace Research Institute (KARI), E. Costa, S. Porziani, D’Appolonia SpA, Daejeon, South Korea; K. Yee, Seoul Rome, Italy National University, Seoul, South Korea Thursday, 12 January 2017 377-HSABP-7 Experimental Investigations of Scramjets Ft. Worth 3 Chaired by: J. DONOHUE, United Technologies Research Center and S. ELIA, Northrop Grumman Corporation 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2017-1536 AIAA-2017-1537 AIAA-2017-1538 AIAA-2017-1539 Closed-Loop Control of Isolator Computational and Experimental The Effect of Pulsed Injection on the The Effects of Planar Symmetry Shock Trains in a Mach 2.2 Direct- Characterization of the Mach 6 Facility Entrainment into a Cavity Based and Radiative Heat Losses in a Connect Scramjet Nozzle Flow for the Enhanced Injection Flameholder in Supersonic Flow Three-Dimensional Transient CFD L. Vanstone, K. Hashemi, J. Lingren, M. and Mixing Project at NASA Langley L. Smith, T. Ombrello, S. Okhovat, Air Simulation of Right Angle Flow Akella, N. Clemens, University of Texas, Research Center Force Research Laboratory, Wright- Through a Brayton-Gluhareff Cycle Austin, Austin, TX; J. Donbar, Air Force T. Drozda, K. Cabell, NASA Langley Research Patterson AFB, OH Pressure Jet Engine Research Laboratory, Wright-Patterson AFB, Center, Hampton, VA; B. Passe, Analytical R. Bramlette, C. Depcik, R. Barrett- OH; et al. Mechanics Associates, Inc., Hampton, VA; Gonzalez, University of Kansas, Lawrence, R. Baurle, NASA Langley Research Center, Lawrence, KS Hampton, VA Thursday, 12 January 2017 378-IS-7 Establishing Trust in Autonomous Systems Ft. Worth 1 0930 - 1100 hrs Moderator: Andrew Lacher

Automation in many different forms is a routine part of our everyday lives. Automation systems are becoming increasingly autonomous in that they are often making and executing decisions with little human oversight (i.e., self-governing) leveraging algorithms that are increasingly complex and adaptive (i.e. non-deterministic and intelligent). As these systems mature, establishing and ensuring appropriate levels of human trust in these systems will be necessary. The panel will discuss several different perspectives on this issue for systems used in life-critical applications.

Panelists: Steve Cook Ella Atkins Katharine Sieck

148 Northrop Grumman University of Michigan Rand Corporation

Thursday, 12 January 2017 379-MAT-8 Materials for Additive Manufacturing Palomino 2 Chaired by: J. KOO, The University of Texas at Austin and S. WANTHAL, The Boeing Company 0930 hrs 1000 hrs 1030 hrs AIAA-2017-1540 AIAA-2017-1541 AIAA-2017-1542 A Holistic Process-Flow from Concept to Cooling System for 0.1 kN Thrust Real-time evolution of Selective Validation for Additive Manufacturing Micro-Engines: Concept Design Laser Melted (SLM) Inconel of Light-Weight, Optimized, Metallic Using Additive Manufacturing 718 with temperature through Components Suitable for Space Flight M. Ugolotti, M. Sharma, Z. Williams, M. synchrotron X-rays M. Orme, Morf3D, El Segundo, CA; M. Owen, J. Ouwerkerk, S. Balachandar, B. Sarley, A. Manero, J. Cotelo, University Gschweitl, M. Ferrari, RUAG Group, Zürich, University of Cincinnati, Cincinnati, OH; of Central Florida, Orlando, FL; J. Wischek, Switzerland; R. Vernon, Altair Engineering, et al. German Aerospace Center (DLR), Cologne, Inc., Irvine, CA; R. Yancey, Altair, Bothell, Germany; J. Okasinski, P. Kenesei, Argonne WA; F. Mouriaux, RUAG Group, Zürich, National Laboratory, Argonne, IL; et al. Switzerland; et al. Thursday, 12 January 2017 380-MDO-10 Integrated Computational Materials Engineering (ICME) Mustang 1 Chaired by: H. KIM and G. KENNEDY, Georgia Institute of Technology 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2017-1543 AIAA-2017-1544 AIAA-2017-1545 AIAA-2017-1546 AIAA-2017-1547 Integrated Computational Materials Stress Minimization Using The Level Application of Numerical Two-Dimensional Optimization of The Validation of a Genetically Engineering (ICME) Approaches to the Set Topology Optimization Optimisation to Support Engineering Functionally Graded Material Plates Inspired Aircaft Structural Design Design and Fabrication of Architected R. Picelli, S. Townsend, Cardiff University, Design Subjected to Buckling Constraints using an Additive Manufacturing Materials Cardiff, United Kingdom; C. Brampton, A. Keskin, Rolls-Royce Group plc, Derby, O. Hussien, S. Mulani, University of Technique C. Spadaccini2, J. Jackson, Lawrence Livermore University of Bath, Bath, United Kingdom; United Kingdom Alabama, Tuscaloosa, Tuscaloosa, AL M. Kobayashi, University of Hawaii, National Laboratory, Livermore, CA; S. Watts, J. Norato, University of Connecticut, Storrs, Manoa, Manoa, HI; J. Deaton, R. Reuter, D. Tortorelli, University of Illinois, Urbana- Storrs, CT; H. Kim, University of California, Air Force Research Laboratory, Wright- Champaign, Urbana, IL; J. Hopkins, University San Diego, San Diego, CA Patterson AFB, OH of California, Los Angeles, Los Angeles, CA; N. Fang, Massachusetts Institute of Technology, Cambridge, MA; et al. Thursday, 12 January 2017 381-MST-11 Model and Simulation Design, Development, Testing, and Validation San Antonio 1 Chaired by: D. CRIDER, National Transportation Safety Board and S. BEARD, NASA/ARC-AFS Aerospace Simulation R&D 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2017-1548 AIAA-2017-1549 AIAA-2017-1550 AIAA-2017-1551 AIAA-2017-1552 Parameter Identification through Development of Post-stall Flight Development and Validation of Matching of Aerodynamic databank Nonparametric Time-Varying Adaptive Optimal Estimation Models from Certification Flight Test a Flight-Identified Full-Envelope with Flight test data – Latero- Frequency Response Function A. Hebert, Engility Corporation, Shalimar, and Wind-tunnel Data Business Jet Simulation Model Using directional Dynamics Estimates for Aircrafts FL; S. Cafarelli, MacAulay Brown, Dayton, P. Grant, Z. Luo, S. Liu, G. Moszczynski, a Stitching Architecture M. Sousa, Federal University of Itajubá, T. Song, D. Lin, J. Wang, T. Jiang, Y. Yu, OH; P. Mackin, Engility Corporation, 149 University of Toronto, Toronto, Canada T. Berger, M. Tischler, Army Aviation and Missile Itajubá, Brazil; A. de Paula, F. Porto, Beijing Institute of Technology, Beijing, Shalimar, FL; J. Shaver, Air Force Research Research Development and Engineering Center, Technological Institute of Aeronautics China Laboratory, Eglin AFB, FL Moffett Field, CA; S. Hagerott, Cessna Aircraft (ITA), São José dos Campos, Brazil; S. Company, Wichita, KS; M. Cotting, W. Gray, Cunha Junior, Federal University of Itajubá, J. Gresham, U.S. Air Force Test Pilot School, Itajubá, Brazil Edwards AFB, CA; et al. Thursday, 12 January 2017 382-MST-12 Modeling and Simulation of Space Vehicle Dynamics, Systems, and Environments Ft. Worth 7 Chaired by: R. RUFF and D. KEATING, The Charles Stark Draper Laboratory, Inc. 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2017-1553 AIAA-2017-1554 AIAA-2017-1555 AIAA-2017-1556 AIAA-2017-1557 Microsatellite Simulation for Characterization of Multi-Antenna Interaction of a Robotic Servicing An open-source, stochastic, six- Modeling and Simulation of Constellation Research GNSS, Multi-Sensor Attitude Vehicle with Satellite Flexible Modes degrees-of-freedom rocket flight Aerobee-150A Sounding Rocket K. Leidig, J. Eickhoff, University of Determination for Stratospheric during Capture simulator, with a probabilistic U. Akcal, B. Yuksek, N. Ure, Istanbul Stuttgart, Stuttgart, Germany Balloon Platforms J. Brannan, Emergent Space Technologies, trajectory analysis approach Technical University, Istanbul, Turkey N. Tehrani, J. Gross, West Virginia Inc., Greenbelt, MD; C. Carignan, University of W. Eerland, S. Box, H. Fangohr, A. University, Morgantown, WV Maryland, College Park, College Park, MD Sobester, University of Southampton, Southampton, United Kingdom Thursday, 12 January 2017 383-MST-14 Modeling and Simulation of Uninhabited Aerial Vehicles III San Antonio 2 Chaired by: D. KLYDE, Systems Technology, Inc. 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2017-1558 AIAA-2017-1559 AIAA-2017-1560 AIAA-2017-1561 Flight Testing, Data Collection, Improving Model Fidelity For Dynamic Modeling and Simulation of A Modeling and Flight Control and System Identification of a a Small Quadcopter Through Quadcopter with Motor Dynamics Simulation of a Quadrotor Tailsitter Multicopter UAV Experimental Modeling A. Kim, P. Vivekanandan, P. McNamee, I. VTOL UAV S. Bhandari, P. Navarro, A. Ruiz, California P. Olejnik, B. Burchett, Rose-Hulman Sheppard, A. Blevins, A. Sizemore, University F. Zhang, X. Lyu, Y. Wang, H. Gu, Z. Li, State Polytechnic University, San Luis Institute of Technology, Terre Haute, IN of Kansas, Lawrence, Lawrence, KS Hong Kong University of Science and Obispo, Pomona, CA Technology, Hong Kong, China Thursday, 12 January 2017 384-NDA-8 Special Session: Uncertainty Quantification and Management for the Digital Thread and Twin Mustang 2 Chaired by: E. TUEGEL, U.S. Air Force Research Laboratory and T. KRISHNAMURTHY, NASA-Langley Research Center 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2017-1562 AIAA-2017-1563 AIAA-2017-1564 AIAA-2017-1565 AIAA-2017-1566 AIAA-2017-1567 Developing a Probabilistic Load Near Real Time Damage Diagnosis A diagnosis-prognosis feedback loop Information gain-based inspection A dynamic Bayesian network approach Probabilistic Damage Tolerance Spectrum for Fatigue Modeling Using Surrogate Modeling and High for improved performance under scheduling for fatigued aircraft for digital twin for Aviation Fleets Using a Kriging I. Asher, L. Wang, G. Khan, Y. Ling, Performance Computing uncertainties components C. Li, S. Mahadevan, Vanderbilt University, Surrogate Model F. Viana, General Electric Company, J. Warner, NASA Langley Research Center, P. Leser, J. Warner, NASA Langley Research Y. Ling, I. Asher, L. Wang, F. Viana, Nashville, TN; Y. Ling, L. Wang, General Electric J. Ocampo, St. Mary’s University, San Antonio, Niskayuna, NY Hampton, VA; M. Zubair, D. Ranjan, Old Center, Hampton, VA G. Khan, General Electric Company, Company, Niskayuna, NY; S. Choze, Alcoa TX; N. Crosby, H. Millwater, University of Texas, Dominion University, Norfolk, VA Niskayuna, NY Technical Center, Pittsburgh, PA San Antonio, San Antonio, TX Thursday, 12 January 2017 385-PC-22 Combustion Dynamics IV Dallas 7

150 Chaired by: D. TALLEY, and P. PALIES, CFD Research Corporation 0930 hrs 1000 hrs 1030 hrs AIAA-2017-1569 AIAA-2017-1570 AIAA-2017-1571 Transient Behavior of Kerosene Axial Evolution of Helical Flame and Development and Application of an Flames in a Bluff-Body Stabilized Swirl Flow Disturbances in a Transversely Energy Balance Analysis Tool for Combustor Forced Combustor Combustion P. Allison, J. Sidey, E. Mastorakos, University of T. Smith, C. Douglas, B. Emerson, T. Lieuwen, A. Pons Lorente, S. Sardeshmukh, C. Cambridge, Cambridge, United Kingdom Georgia Institute of Technology, Atlanta, GA Huang, W. Anderson, Purdue University, West Lafayette, IN Thursday, 12 January 2017 386-PC-23 Model Validation for Propulsion Workshop I San Antonio 6 Chaired by: A. COMER, Air Force Institute of Technology and V. SANKARAN, US Air Force/AFRL/RQRC 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2017-1572 AIAA-2017-1573 AIAA-2017-1574 AIAA-2017-1575 AIAA-2017-1576 On the Role of Chemical Kinetics MVP-Workshop Contribution: Developing Grid-Convergent A Comparative Study of Large Eddy LES reliability of the Volvo bluff- Modeling in the LES of Premixed Modeling of Volvo bluff body flame LES Simulations of Augmentor Simulation (LES) Combustion Models body stabilized ame dynamics Bluff Body and Backward-Facing experiment Combustion with Automatic Meshing applied to the Volvo Validation Rig D. Maestro, CERFACS, Toulouse, France; A. Step Combustors H. Wu, P. Ma, Y. Lv, M. Ihme, Stanford and Adaptive Mesh Refinement C. Fureby, Swedish Defense Research Ghani, Fluid Mechanics Institute of Toulouse N. Chakroun, S. Shanbhogue, G. Kewlani, University, Stanford, CA S. Drennan, G. Kumar, S. Liu, Convergent Agency (FOI), Stockholm, Sweden (IMFT), Toulouse, France; L. Gicquel, S. Taamallah, D. Michaels, A. Ghoniem, Science, Inc., New Braunfels, TX CERFACS, Toulouse, France; T. Poinsot, Massachusetts Institute of Technology, Fluid Mechanics Institute of Toulouse Cambridge, MA (IMFT), Toulouse, France Thursday, 12 January 2017 387-PDL-10 DBD Plasma Actuators I Ft. Worth 4 Chaired by: S. ROY, University of Florida and S. BANE, Purdue University- Sch of Aero and Astro 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2017-1577 AIAA-2017-1578 AIAA-2017-1579 AIAA-2017-1580 Stall Cell Formation over a Boeing Airfoil Optimisation for DBD PIV-based dynamic model of EHD Unsteady Joule Heating Energy Vertol VR-7 Airfoil Plasma Actuator in a Wind volume force produced by a surface Model for Nanosecond Pulsed DBD A. Ghassemi Isfahani, N. Webb, M. Samimy, Energy Environment: Design and dielectric barrier discharge Plasma Actuator Ohio State University, Columbus, OH Experimental Study N. Benard, University of Poitiers, J. Chae, S. Ahn, H. Kim, K. Kim, Seoul E. Batlle, Technical University of Catalonia, Futuroscope, France; S. Laizet, Imperial National University, Seoul, South Korea Terrassa, Spain; R. Pereira, M. Kotsonis, G. College London, London, United Kingdom; de Oliveira, Delft University of Technology, E. Moreau, University of Poitiers, Delft, The Netherlands Futuroscope, France Thursday, 12 January 2017 388-PDL-11 Plasma Assisted Combustion and Ignition I Ft. Worth 5 Chaired by: A. STARIKOVSKIY, Princeton University and J. POGGIE, Purdue University- Sch of Aero and Astro 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2017-1581 AIAA-2017-1582 AIAA-2017-1583 AIAA-2017-1584 AIAA-2017-1585 Hydrodynamic effects induced by Developing Multiphysics Simulations Effect of Translational OH Radical Measurements in Effects of DC electric fields on the nanosecond sparks in air and air/fuel of Swirl-Stabilized Plasma-Assisted Nonequilibrium and “Hot” Atoms Hydrogen-Air Mixtures at the combustion of a simplified multi- mixtures Combustion Reactions on Active Species Conditions of Strong Vibrational element injector S. Stepanyan, École Centrale Paris, Châtenay- J. Zimmerman, A. Palla, D. King, D. Carroll, CU Production in High-Voltage Pulsed Nonequilibrium P. Salvador, K. Xu, University of Alabama, Malabry, France; J. Hayashi, Osaka University, Aerospace, LLC, Champaign, IL; C. Mitsingas, Discharges C. Winters, Y. Hung, E. Jans, K. Huntsville, Huntsville, AL Suita, Japan; S. Lovascio, University of Bari, R. Rajasegar, University of Illinois, Urbana- A. Starikovskiy, Princeton University, Frederickson, I. Adamovich, Ohio State Bari, Italy; G. Stancu, C. Laux, École Centrale Champaign, Urbana, IL; et al. Princeton, NJ University, Columbus, OH

151 Paris, Châtenay-Malabry, France Thursday, 12 January 2017 389-SD-19 Special Session: Adaptive Aeroelastic Wing Shaping Control I Appaloosa 2 Chaired by: N. NGUYEN, NASA-Ames Research Center and B. STANFORD, NASA Langley Research Center 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2017-1586 AIAA-2017-1588 AIAA-2017-1589 AIAA-2017-1590 AIAA-2017-1591 Flexible Deflection Measurements A Flutter Suppression and Drag Multi-Objective Flight Control Decentralized Optimal Adaptive Development of a Refined Space using the SansEC Smart Sensor Optimization Approach for Flexible for Drag Minimization and Load Control Architectures for the VCCTEF Vehicle Rollout Forcing Function A. Menon, J. Whitford, Y. Kostogorova- Aircraft Alleviation of High-Aspect Ratio Aircraft G. James, J. Tucker, G. Valle, R. Grady, J. Beller, J. Steck, A. Chakravarthy, Wichita J. Boskovic, R. Wise, J. Jackson, Scientific Flexible Wing Aircraft A. Menon, A. Chakravarthy, J. Steck, Schliesing, NASA Johnson Space Center, State University, Wichita, KS Systems Company, Inc., Woburn, MA; N. N. Nguyen, NASA Ames Research Center, Wichita State University, Wichita, KS; N. Houston, TX; J. Fahling, Jacobs, Houston, Nguyen, NASA Ames Research Center, Moffett Field, CA; E. Ting, D. Chaparro, M. Nguyen, NASA Ames Research Center, TX; et al. Moffett Field, CA Drew, Stinger Ghaffarian Technologies, Inc., Moffett Field, CA Moffett Field, CA; S. Swei, NASA Ames Research Center, Moffett Field, CA Thursday, 12 January 2017 390-SD-20 Dynamic Loads, Response, Vibration, and Stability of Aerospace Vehicles I Appaloosa 3 Chaired by: C. HEBERT and A. DATTA, Science & Technology Corporation 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2017-1592 AIAA-2017-1593 AIAA-2017-1594 AIAA-2017-1595 AIAA-2017-1596 AIAA-2017-1597 Dynamic analysis of assembled aircraft Development and Implementation of Linear and Nonlinear Flutter State-space realizations of potential- Design and Modal Analysis of a Modal Characteristics of a structures with nonlinear joints a Hybrid Dynamic Force Measurement Analyses Using Dynamic Response flow unsteady aerodynamics with Unique Structure under an Internal Piezoelectric Shaker Table S. Hernandez, University of A Coruña, A System at AEDC Tunnel 9 Computations arbitrary kinematics Vacuum A. Palazotto, Air Force Institute of Coruña, Spain; E. Menga, Airbus, Madrid, J. Draper, S. Lee, University of Maryland, F. Roizner, M. Karpel, Technion--Israel R. Simpson, R. Palacios, S. Maraniello, Imperial J. Snyder, A. Palazotto, Air Force Institute Technology, Wright-Patterson AFB, OH Spain; P. Naveira, C. Lopez, A. Baldomir, College Park, College Park, MD; E. Marineau, Institute of Technology, Haifa, Israel College London, London, United Kingdom of Technology, Wright-Patterson AFB, OH M. Cid, University of A Coruña, A Coruña, Arnold Engineering Development Complex, Spain; et al. Silver Spring, MD Thursday, 12 January 2017 391-SD-21 Reduced Order Modeling Appaloosa 4 Chaired by: Z. SOTOUDEH, Cal Poly Pomona and R. PALACIOS, Imperial College London 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2017-1598 AIAA-2017-1599 AIAA-2017-1600 AIAA-2017-1601 Genetic Algorithm-Guided, Adaptive A Reduced Order Model of Corrected Mistuned Rotor Reduced Order An Aerothermoelastic Analysis Model Order Reduction of Flexible Aerodynamic Influence Coefficients Modeling with Surrogate-Modeled Framework Enhanced by Model Aircrafts for Aircraft Loads Analysis Airfoil Substructures Order Reduction With Applications J. Zhu, Y. Wang, K. Pant, CFD Research M. Verveld, T. Kier, German Aerospace E. Henry, J. Brown, Air Force Research D. Huang, T. Rokita, P. Friedmann, University of Corporation, Huntsville, AL; P. Suh, M. Center (DLR), Oberpfaffenhofen, Germany Laboratory, Wright-Patterson AFB, OH; J. Michigan, Ann Arbor, Ann Arbor, MI Brenner, NASA Armstrong Flight Research Beck, Universal Technology Corporation, Center, Edwards, CA Dayton, OH Thursday, 12 January 2017 392-STR-10 Challenges in the Design of Joined Wings and Structural Joints Appaloosa 1 Chaired by: L. DEMASI, San Diego State University College of Engineering and S. RUSSELL, Triumph Aerostructures 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2017-1602 AIAA-2017-1603 AIAA-2017-1604 AIAA-2017-1605 Analytical and Experimental Studies Physical based Multidisciplinary Honeycomb Core Failure Prediction Automatic Design and Sizing of on Delamination Arrest in Bolted- Optimization of Strut Braced Wing in Joint using Nonlinear Finite Inverted Joined-Wing Aircraft Bonded Composite Structures Configuration in a Distributed Element Analysis M. Kalinowski, Institute of Aviation, L. Richard, K. Lin, University of design environment A. Lyford, Orbital ATK, Dulles, VA; R. Warsaw, Poland Washington, Seattle, Seattle, WA X. Gu, P. Ciampa, B. Nagel, German Kapania, Virginia Polytechnic Institute Aerospace Center (DLR), Hamburg, and State University, Blacksburg, VA; T. Germany Stoumbos, Orbital ATK, Dulles, VA Thursday, 12 January 2017 152 393-TES-1 Fossil Fuel Power Technologies I Mustang 3 Chaired by: A. GUPTA, University of Maryland and H. KIM, Airliquide 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2017-1606 AIAA-2017-1607 AIAA-2017-1608 AIAA-2017-1609 AIAA-2017-1610 Heat Transfer Characterization of Impact of Confinement on a Swirl CARSOXY (CO2-Argon-Steam- Preliminary Computational Analysis Sorption Enhanced Steam a High Heat Flux Oxy-Fuel Direct Burner Flowfield OxyFuel) Combustion in Gas of Combustion in a Directly Heated Reforming of Methane using Power Extraction Combustor A. Khalil Hasan, J. Brooks, A. Gupta, Turbines for CCS Systems Supercritical Oxy-Fuel Combustor Calcium Looping L. Cabrera, J. Aboud, M. Hernandez, B. University of Maryland, College Park, N. Syred, M. Gutesha, A. Doboon, A. A. Badhan, A. Chowdhury, A. Choudhuri, N. C. Batini, K. Burra, A. Gupta, University of Lovich, A. Choudhuri, N. Love, University of College Park, MD Valera-Medina, P. Bowen, Cardiff University, Love, University of Texas, El Paso, El Paso, TX Maryland, College Park, College Park, MD Texas, El Paso, El Paso, TX Cardiff, United Kingdom Thursday, 12 January 2017 394-TP-11 Nonequilibrium Flows and Radiation Austin 3 Chaired by: C. JOHNSTON, NASA-Langley Research Center 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2017-1611 AIAA-2017-1612 AIAA-2017-1613 AIAA-2017-1614 Simulations of stagnation point Advanced Modeling of Non- Rarefaction Effects on Species Assessment of Degree of Steadiness radiative heating rates and spectral equilibrium Flows using a Maximum Diffusion through Nanoscales in Boundary Layer Shock- analysis of entry vehicles Entropy “Quadratic” Formulation M. Darbandi, M. Sabouri, Sharif University Interaction Flows J. Bonin, University of the German Federal M. Sharma, University of Illinois, Urbana- of Technology, Tehran, Iran; G. Schneider, O. Tumuklu, D. Levin, University of Illinois, Armed Forces, Munich, Germany; D. Champaign, Urbana, IL; Y. Liu, NASA University of Waterloo, Waterloo, Canada Urbana-Champaign, Urbana, IL Kliche, IABG, Munich, Germany; C. Mundt, Ames Research Center, Moffett Field, CA; University of the German Federal Armed M. Panesi, University of Illinois, Urbana- Forces, Munich, Germany Champaign, Urbana, IL Thursday, 12 January 2017 395-WE-9 Wind Energy Control and Optimization I Texas D Chaired by: P. VEERS, National Renewable Energy Laboratory and R. DAMIANI, NREL 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2017-1615 AIAA-2017-1616 AIAA-2017-1617 AIAA-2017-1618 AIAA-2017-1619 Large Eddy Simulation Analysis of Real time controlled wind turbine Development of a Mechanical Multivariable controller design Gradient Based Optimization of Wake Characteristics and Power wake simulator Passive Pitch System for a 500W verification for a Liberty wind turbine Wind Farms with Multiple Turbine Spectrum of a Wind Turbine Operating R. Castillo, Y. Wang, S. Pol, A. Swift, Horizontal Axis Wind Turbine D. Ossmann, University of Minnesota, Hub Heights in Yaw C. Westergaard, Texas Tech University, T. Poryzala, T. Kim, Technical University of Minneapolis, Minneapolis, MN; J. Theis, A. Stanley, J. Thomas, A. Ning, Brigham T. Kaushik, T. Chatterjee, Y. Peet, R. Calhoun, Lubbock, TX Denmark, Roskilde, Denmark Hamburg University of Technology, Hamburg, Young University, Provo, UT; K. Dykes, Arizona State University, Tempe, AZ Germany P. Fleming, National Renewable Energy Laboratory, Boulder, CO Thursday, 12 January 2017 396-IS-8 New Developments in ISHM for NASA Ground, Launch, and Flight Systems Ft. Worth 1 1100 - 1230 hrs Moderator: Kevin Melcher, Team Lead, Systems Health Management for Space Exploration, NASA Glenn Research Center, Intelligent Control and Autonomy Branch

During this session, participants will discuss key developments in NASA ground, launch, and flight systems that have occurred over the past 2-3 years. This will be followed by a dialogue with audience participants. Questions to be addressed by the panel include: 1. In your area of experience, what are the top 2-3 advances or developments in Systems Health Management or Fault Management? 2. How have or will these advances positively impacted NASA’s systems engineering development processes and set the stage for successful recent or future flights? 3. What are 1 or 2 key next steps toward advancing ISHM in your area of expertise (i.e., ground, launch, or flight systems)?

Panelists: Stephen B. Johnson Fernando Figueroa Gordon B. Aaseng Edmond Wong Lorraine Fesq President, Dependable System Technology, LLC Lead, Autonomous Operations and Systems, Engineering Computer Scientist, Intelligent Systems Division Technical Lead, Sensor Data Qualiﬁcation and Lead, NASA’s Fault Management Community of Analysis Lead, Mission and Fault Management and Test Directorate, Advanced Technology and Tech NASA Ames Research Center Consolidation for the Space Launch System Practice; Chief Technologist for Systems Engineering

153 NASA Space Launch System Program Transfer Division NASA Glenn Research Center and Formulation Division NASA Stennis Space Center NASA Jet Propulsion Laboratory

Thursday, 12 January 2017 397-LUNCH-4 Recognition Luncheon: Celebrating Achievements in Aerospace Design/Structures and Aerospace Literature Texas A & B 1200 - 1400 hrs Walter Downing Executive Vice President Southwest Research Institute Thursday, 12 January 2017 398-NW-18 Rising Leaders Keynote Speaker with Boxed Lunch Grapevine A 1230 - 1400 hrs A New Era in Aviation Jaiwon Shin NASA Associate Administrator, Aeronautics Research Mission Directorate Thursday, 12 January 2017 399-ABPSI-2 Inlet Distortion and Characterization Dallas 1 Chaired by: E. LOTH, University of Virginia and C. CHUCK, The Boeing Company 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs AIAA-2017-1621 AIAA-2017-1620 AIAA-2017-1622 AIAA-2017-1623 AIAA-2017-1624 Axial Extent of Flowfield Variation Swirling Flow Evolution Part Swirling Flow Evolution Part 2: Fan Rotor Flow Measurements in Design and Testing of a Small Pressure from the StreamVaneTM Swirl 1: Design and Stereo PIV StreamFlow 2D+t Model Validated a Turbofan Engine operating with Wave Supercharger for an Industrial Pattern Generation System Measurements at Select Planes with Stereo PIV Measurements Inlet Swirl Distortion Diesel Engine C. Nessler, D. Sanders, T. Janczeswki, M. T. Guimaraes Bucalo, Virginia Polytechnic W. Schneck, T. Guimaraes Bucalo, D. D. Frohnapfel, W. O’Brien, K. Lowe, M. Mataczynski, Air Force Research Laboratory, List, W. Copenhaver, Air Force Research Institute and State University, Blacksburg, VA; Frohnapfel, K. Lowe, W. O’Brien, Virginia Virginia Polytechnic Institute and State Wright-Patterson AFB, OH; D. Paxson, NASA Laboratory, Wright-Patterson AFB, OH W. Copenhaver, Air Force Research Laboratory, Polytechnic Institute and State University, University, Blacksburg, VA Glenn Research Center, Cleveland, OH; J. Hoke, Wright-Patterson AFB, OH; W. Schneck, K. Blacksburg, VA; W. Copenhaver, Air Force Innovative Scientific Solutions, Inc., Dayton, Lowe, W. O’Brien, Virginia Polytechnic Institute Research Laboratory, Wright-Patterson AFB, OH OH; F. Schauer, Air Force Research Laboratory, and State University, Blacksburg, VA Wright-Patterson AFB, OH Thursday, 12 January 2017 400-ACD-9 Innovative Aircraft Design Concepts II Grapevine 3 Chaired by: C. BIL, RMIT University and S. KOMADINA, Northrop Grumman Aerospace Systems 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs AIAA-2017-1625 AIAA-2017-1626 AIAA-2017-1627 AIAA-2017-1628 AIAA-2017-1629 Conceptual Design of Air Vehicles Impact of Cloud Encounter Mitigation Integrated Assessment of Active Cruise Speed Sensitivity Study for Loads Certification of the Cirrus with Hybrid Lift Concepts - A Design Procedures on Operational and Flow Control Architectures for Transonic Truss Braced Wing Aircraft SF50 Vision Jet® Space Exploration Economic Effectiveness of HLFC Aircraft Commercial Aircraft D. Wells, NASA Langley Research Center, R. Kelbe, N. Hill, T. Ladeinde, C. J. Hartmann, German Aerospace Center K. Wicke, F. Linke, A. Lau, K. Risse, German Y. Cai, Z. Gao, I. Chakraborty, S. Briceno, Hampton, VA Venkatasubban, Cirrus Aircraft, Duluth, MN (DLR), Hamburg, Germany Aerospace Center (DLR), Hamburg, Germany; D. Mavris, Georgia Institute of Technology, A. Pohya, B. Lührs, Hamburg University of Atlanta, GA Technology, Hamburg, Germany; et al. 154 Thursday, 12 January 2017 401-ACD-10 CADWG: Concept Design Tools and Processes for Manufacturing and Certification of Aircraft San Antonio 4 1400 - 1700 hrs Panelists: Peter Schmollgruber Neal Pfeiffer Luis Gonzalez-Linero Nicholas Borer ONERA Mooney International Embry-Riddle Aeronautical University NASA Langley Research Center

Thursday, 12 January 2017 402-AFM-9 Small/Mini/Micro Aerial Vehicles Grapevine 4 Chaired by: T. RICHARDSON, University of Bristol and K. SHWEYK, Boeing Engineering Operations & Technology 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2017-1630 AIAA-2017-1631 AIAA-2017-1632 AIAA-2017-1633 AIAA-2017-1634 AIAA-2017-1635 Performance Improvement of Small Flight Test Investigation of Stall/ Validation of Flight Power Modeling Sliding Mode Control of a Flight Testing and Preliminary Stability Analysis of Longitudinal UAVs Through Energy-Harvesting Spin Detection Techniques for a by Direct Measurement of a Biomimetic Flapping Wing Micro Air Analysis for Global System Dynamics of Hovering Flapping Within Atmospheric Gusts Flying Wing UAS Flapping Wing Aerial Vehicle Vehicle in Hover Identiﬁcation of Ornithopter MAVs/Insects N. Gavrilovic, E. Benard, P. Pastor, J. H. Chao, H. Flanagan, P. Tian, University J. Gerdes, Army Research Laboratory, J. Bluman, C. Kang, Y. Shtessel, University Dynamics Using On-board and A. Elsadek, Zewail City of Science Moschetta, Higher Institute of Aeronautics of Kansas, Lawrence, Lawrence, KS; S. Aberdeen Proving Ground, MD; S. Gupta, of Alabama, Huntsville, Huntsville, AL Off-board Data and Technology, Giza, Egypt; H. Taha, and Space, Toulouse, France Hagerott, Textron Aviation, Wichita, KS University of Southern California, Los S. Armanini, M. Karásek, C. de Visser, G. University of California, Irvine, Irvine, CA; Angeles, CA; H. Bruck, University of de Croon, M. Mulder, Delft University of G. El-Bayoumi, Cairo University, Giza, Egypt Maryland, College Park, College Park, MD Technology, Delft, The Netherlands Thursday, 12 January 2017 403-AFM-10 Aircraft Flight Dynamics, Handling Qualities, and Performance III Grapevine 5 Chaired by: A. LAMPTON, Systems Technology, Inc. and D. GINGRAS, Bihrle Applied Research Inc. 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2017-1636 AIAA-2017-1637 AIAA-2017-1638 AIAA-2017-1639 AIAA-2017-1640 AIAA-2017-1641 Trim Analyses of Mass-Actuated Dynamic Simulation and Control of Flight Performance Optimization of Airdata-Sensor-based Relative Position Novel Estimation of Pilot Assessment of a Scalogram-Based PIO Airplane in Steady-state Climb and Mass-Actuated Airplane a Multi-Lift Rotorcraft Formation Estimation for Receiver Aircraft in Performance Characteristics Metric with Flight Test Data Descent S. Erturk, A. Dogan, University of Texas, J. Enciu, J. Horn, Pennsylvania State Aerial Refueling E. Bachelder, San Jose State University, D. Klyde, P. Schulze, Systems Technology, S. Erturk, A. Dogan, University of Texas, Arlington, Arlington, TX University, University Park, PA H. Sevil, University of Texas, Arlington Research San Jose, CA; B. Aponso, NASA Ames Inc., Hawthorne, CA; R. Mello, Embraer, São Arlington, Arlington, TX Institute, Fort Worth, TX; A. Dogan, University Research Center, Moffett Field, CA José dos Campos, Brazil; D. Mitchell, Mitchell of Texas, Arlington, Arlington, TX Aerospace Research, Long Beach, CA Thursday, 12 January 2017 404-AMT-14 Simultaneous and/or Multidimensional Measurements Grapevine B Chaired by: S. KEARNEY, Sandia National Laboratories and B. THUROW, Auburn University 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs AIAA-2017-1642 AIAA-2017-1643 AIAA-2017-1644 AIAA-2017-1645 AIAA-2017-1646 Volumetric calibration of a plenoptic Visualization of an SBLI using Tomographic PIV Measurement A Plenoptic Multi-Color Imaging 3D OH LIF Measurements in a Lifted camera Plenoptic BOS in a Bluff Body Wake Utilizing an Pyrometer Flame E. Hall, T. Fahringer, B. Thurow, Auburn C. Clifford, J. Klemkowsky, B. Thurow, Auburn Asymmetric Camera Conguration P. Danehy, NASA Langley Research Center, B. Halls, P. Hsu, L. Ethan, S. Roy, Spectral University, Auburn, AL; D. Guildenbecher, University, Auburn, AL; N. Arora, F. Alvi, Florida and Least Squares Matching Hampton, VA; W. Hutchins, Warwick High Energies, LLC, Dayton, OH; T. Meyer, Sandia National Laboratories, Albuquerque, NM State University, Tallahassee, FL E. Fleischhauer, J. Dahlberg, P. Tkacik, School, Hampton, VA; T. Fahringer, B. Purdue University, West Lafayette, IN; S. Hellman, University of North Carolina, Thurow, Auburn University, Auburn, AL J. Gord, Air Force Research Laboratory, Charlotte, Charlotte, NC Wright-Patterson AFB, OH Thursday, 12 January 2017

155 405-APA-39 Aerodynamic-Structural Dynamic Interactions II Dallas 5 Chaired by: C. PASILIAO, AFRL/RW and D. FINLEY, Lockheed Martin Aeronautics 1400 hrs 1430 hrs 1500 hrs 1530 hrs AIAA-2017-1647 AIAA-2017-1648 AIAA-2017-1649 AIAA-2017-1650 Multiple Equilibrium Points of Airfoil Flutter Study of NACA 64A010 Numerical Study of Evolution of Air A High Efficiency Aeroelastic Flutter in Viscous Flow Airfoil Using URANS and e^N Pockets during Water Impact of a Analysis Method based on Rigid F. Marti, F. Liu, University of California, Transition Models Coupled with an Flat-Bottom Structure External Aerodynamic Force and Irvine, Irvine, CA Integral Boundary Layer Code Q. Qu, G. Ji, P. Liu, X. Wu, Beihang Elastic Correction by High-Order F. Marti, F. Liu, University of California, University, Beijing, China; R. Agarwal, Panel Method Irvine, Irvine, CA Washington University in St. Louis, St. Y. Liu, S. Zhu, Z. Wan, C. Yang, Beihang Louis, MO University, Beijing, China Thursday, 12 January 2017 406-APA-40 Special Session: Sensitivity Analysis and Uncertainty Quantification Evaluation for Realistic Problems II Ft. Worth 3 Chaired by: P. MORGAN, Ohio Aerospace Institute and R. GRAVES, Air Force Research Laboratory 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2017-1651 AIAA-2017-1652 AIAA-2017-1653 AIAA-2017-1654 AIAA-2017-1655 AIAA-2017-1656 Studies of Aeroelastic Uncertainty Aeroelastic Uncertainty Flutter Uncertainty Quantification Development and Assessment of Validation of Uncertainty Summary Findings from the AVT-191 Quantification for a Wind Tunnel Quantification Studies Using the S4T for the S4T Model Uncertainty Quantification Methods Quantification Methods for High- Project to Assess Sensitivity Analysis Model and Test Program – Wind Tunnel Model I. Tartaruga, J. Cooper, University of Bristol, for Ship Hydrodynamics Fidelity CFD of Ship Response in and Uncertainty Quantification Overview and Static Aeroelastic M. Nikbay, National Institute of Aerospace, Bristol, United Kingdom; G. Georgiou, F. Stern, S. Volpi, N. Gaul, K. Choi, Irregular Waves Methods for Military Vehicle Design Analysis Hampton, VA; J. Heeg, NASA Langley University of Liverpool, Liverpool, United University of Iowa, Iowa City, Iowa City, M. Diez, R. Broglia, D. Durante, A. Olivieri, J. Benek, Air Force Research Laboratory, A. Cunningham, Lockheed Martin Research Center, Hampton, VA Kingdom; H. Khodaparast, Swansea IA; M. Diez, R. Broglia, National Research E. Campana, National Research Council, Wright-Patterson AFB, OH; J. Luckring, NASA Corporation, Fort Worth, TX University, Swansea, United Kingdom Council, Rome, Italy; et al. Rome, Italy; F. Stern, University of Iowa, Langley Research Center, Hampton, VA Iowa City, Iowa City, IA Thursday, 12 January 2017 407-APA-41 Airfoil/Wing/Configuration Aerodynamics III: Airfoil and Wing Optimization Dallas 3 Chaired by: B. DETERT, Boeing Commercial Airplanes and J. CODER, University of Tennessee 1400 hrs 1430 hrs 1500 hrs AIAA-2017-1657 AIAA-2017-1658 AIAA-2017-1659 Studies on Wingtip Geometries by Study on Aerodynamics of Annular Aerodynamics of an Airfoil in Optimum Spanwise Lift Distribution Wing for Unmanned Aerial Vehicles Dynamic Ground Effect during Design Method M. Debiasi, Y. Cui, M. Damodaran, National Take-Off Y. Oda, K. Rinoie, University of Tokyo, University of Singapore, Singapore, Q. Qu, L. Huang, P. Liu, T. Hu, Beihang Bunkyo, Japan; T. Yuhara, Japan Aerospace Singapore; J. Dela Cruz, J. Tan, Temasek University, Beijing, China; R. Agarwal, Exploration Agency (JAXA), Mitaka, Japan Polytechnic, Singapore, Singapore; A. Washington University in St. Louis, St. Raut , Indian Institute of Technology Louis, MO Gandhinagar, Palaj, India; et al. Thursday, 12 January 2017 408-APA-42 Applied CFD II: Configuration Evaluation Dallas 4 Chaired by: J. AZEVEDO and R. DOWGWILLO, Boeing Engineering Operations & Technology 1400 hrs 1430 hrs 1500 hrs 1530 hrs AIAA-2017-1660 AIAA-2017-1661 AIAA-2017-1662 AIAA-2017-1663 Flow simulations of a high-speed Comparison between Wall-modeled Aerodynamic Analysis of a High Effect of the Impinging Height of train for investigating the ballast and Wall-resolved Large Eddy Maneuverability Airframe Utilizing Twin Jets in Tandem Through a flight Simulations for the prediction of Magnetic Resonance Velocimetry Crossflow J. Zhu, Z. Hu, U. Oza, University of boundary-layer separation around the and Reynolds-Averaged Navier- J. Barata, A. Silva, D. Vieira, University of Southampton, Southampton, United side mirror of a full-scale vehicle Stokes Simulations Beira Interior, Covilha, Portugal Kingdom K. Ambo, T. Yoshino, T. Kawamura, M. E. Youn, A. Waugh, Z. Livingston, M. Teramura, Honda Motor Company, Ltd., Benson, B. Van Poppel, C. VerHulst, U.S.

156 Haga, Japan; D. Philips, G. Brès, Cascade Military Academy, West Point, NY; et al. Technologies, Inc., Palo Alto, CA; et al. Thursday, 12 January 2017 409-APA-43 Special Session: Simulation of Rotor in Hover II Dallas 2 Chaired by: N. HARIHARAN, CREATE-AV and R. NARDUCCI, Boeing Defense, Space & Security 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs AIAA-2017-1664 AIAA-2017-1665 AIAA-2017-1666 AIAA-2017-1667 AIAA-2017-1668 Methods for Efficient Resolution of CFD Hover Predictions Including Accurate predictions of hovering Application of CREATE TM-AV Helios Standardized Post-Processing Vortical Structures of an S-76 Rotor Boundary-Layer Transition rotor flows using CFD in Engineering Environment: Hover and Visualization of Participants’ in Hover B. Vieira, M. Kinzel, M. Maughmer, A. Garcia, S. Colonia, G. Barakos, Prediction Assessment Simulations of a Rotor in Hover B. Lee, J. Hayes, B. Govindarajan, J. Pennsylvania State University, University University of Glasgow, Glasgow, United T. Wong, Army Research, Development E. Duque, M. Burklund, A. Toyoda, Baeder, University of Maryland, College Park, PA Kingdom and Engineering Command, Redstone Intelligent Light, Rutherford, NJ; N. Park, College Park, MD Arsenal, AL Hariharan, CREATE AV Team, Lorton, VA Thursday, 12 January 2017 410-APA-44/FD-53 Special Session: Sensitivity Analysis of High-Fidelity Rotorcraft Computations Dallas 6 Chaired by: L. WANG, National Institute of Aerospace and G. KENNEDY, Georgia Institute of Technology 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2017-1669 AIAA-2017-1670 AIAA-2017-1671 AIAA-2017-1672 AIAA-2017-1673 Oral Presentation Recent Advances in High-Fidelity Sensitivity Analysis of Adjoint-based derivative evaluation Sensitivity of Rotorcraft Hover Robust Acoustic Objective Functions The efficient use of CFD in Multidisciplinary Adjoint-Based Multidisciplinary Rotorcraft methods for flexible multibody Predictions to Mesh Resolution in and Sensitivities in Adjoint-Based Rotorcraft Optimization Optimization with the NSU3D Flow Simulations systems with rotorcraft applications Strand Grid Framework Design Optimizations T. Schwarz, M. Wentrup, G. Wilke, German Solver Framework L. Wang, B. Diskin, National Institute of K. Boopathy, G. Kennedy, Georgia Institute V. Lakshminarayan, Science and L. Lopes, NASA Langley Research Center, Aerospace Center (DLR), Braunschweig, D. Mavriplis, E. Fabiano, E. Anderson, Aerospace, Hampton, VA; R. Biedron, E. of Technology, Atlanta, GA Technology Corporation, Moffett Field, CA; Hampton, VA Germany University of Wyoming, Laramie, Laramie, WY Nielsen, NASA Langley Research Center, J. Sitaraman, Parallel Geometric Algorithms Hampton, VA; O. Bauchau, University of LLC, Sunnyvale, CA; A. Wissink, Army Maryland, College Park, College Park, MD Aviation and Missile Research Development and Engineering Center, Moffett Field, CA Thursday, 12 January 2017 411-ASC-4 Smart and Multifunctional Materials, Structural Health Monitoring and Damage Detection and Integrity Palomino 3 Chaired by: G. DAVIS, Jet Propulsion Laboratory and T. TURNER, NASA-Langley Research Center 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs AIAA-2017-1674 AIAA-2017-1675 AIAA-2017-1676 AIAA-2017-1677 AIAA-2017-1678 Effect of Triaxiality on Phase Structural Health Management of Assessment of Adhesively Bonded Structural Health Monitoring of Guided Wave Based Damage

Transformation in NI50.8TI Notched Damaged Aircraft Structures Using Joint Health Status using Wavelet Skin-Stiffener Structures Using Assessment in X-COR Composite Cylindrical Bars Digital Twin Concept Spectral Finite Element Method WSFE-based User Deﬁned Elements Sandwich Structures F. Phillips, S. Jape, T. Baxevanis, D. B. Seshadri , National Institute of Aerospace, N. Jayakody, R. Jha, A. Khalili, Mississippi in Abaqus G. Li, R. Neerukatti, A. Rajadas, A. Lagoudas, Texas A&M University, College Hampton, VA; T. Krishnamurthy, NASA Langley State University, Mississippi State, MS; D. A. Khalili, R. Jha, N. Jayakody, Mississippi Chattopadhyay, Arizona State University, Station, TX Research Center, Hampton, VA Samaratunga, The Aerospace Corporation, State University, Mississippi State, MS Tempe, AZ; D. Huff, The Boeing Company, El Segundo, CA Mesa, AZ Thursday, 12 January 2017 412-EXPL-2 Novel Concepts for Solar System Exploration Palomino 2 Chaired by: S. BAUER, NASA LaRC and S. SHARMA, NASA Ames Research Center 1400 hrs 1430 hrs AIAA-2017-1679 AIAA-2017-1680 Mission to the Gravitational Focus of Autoport Project: a Docking Station the Sun: A Critical Analysis for Planetary Exploration Drones G. Landis, NASA Glenn Research Center, A. Compagnin, A. Cenzato, E. Lungavia, N. Cleveland, OH Bagarello, A. Rossi, A. Reffo, University of Padova, Padova, Italy; et al. Thursday, 12 January 2017 413-F360-8 NASA Innovative Advanced Concepts (NIAC): Enabling Missions from Venus to Alpha Centauri Texas C

157 1400 - 1600 hrs Moderator: Alvin Yew, Program Manager, NASA Innovative Advanced Concepts, Space Technology Mission Directorate, NASA

Panelists: Geoff Landis Mason Peck Jonathan Sauder Scientist Associate Professor, Mechanical and Aerospace Engineering Technologist, Technology Infusion Group NASA Glenn Research Center Cornell University NASA Jet Propulsion Laboratory

Thursday, 12 January 2017 414-FD-5 Experimental Measurements in Stability and Transition Grapevine 2 Chaired by: K. CASPER, Sandia National Laboratories and D. BERRIDGE, Johns Hopkins University, Applied Physics Laboratory 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs AIAA-2017-1681 AIAA-2017-1682 AIAA-2017-1683 AIAA-2017-1684 AIAA-2017-1685 Measurements of Crossflow Global Heat Flux Measurement Using Hypersonic Boundary-Layer Dependence of Turbulent Spot Influence of Perturbations on Instability Modes for HIFiRE-5 at Temperature-Sensitive Paint in High- Transition Features from High- Initiation Rates on Hypersonic 3-D Hypersonic Shock Laminar Angle of Attack Enthalpy Shock Tunnel HIEST Speed Schlieren Images Boundary Layer Flow Parameters Boundary Interactions M. Borg, R. Kimmel, Air Force Research T. Nagayama, H. Nagai, Tohoku University, R. Kennedy, S. Laurence, University of S. Raghunath, University of Queensland, A. Leidy, I. Neel, R. Bowersox, Texas Laboratory, Wright-Patterson AFB, OH Sendai, Japan; H. Tanno, T. Komuro, Japan Maryland, College Park, College Park, MD; Brisbane, Australia; R. Narasimha, Jawaharlal A&M University, College Station, TX; Aerospace Exploration Agency (JAXA), M. Smith, E. Marineau, Arnold Engineering Nehru Centre for Advanced Scientific Research, J. Schmisseur, University of Tennessee, Kakuda, Japan Development Complex, Silver Spring, MD Bengaluru, India; D. Mee, University of Tullahoma, Tullahoma, TN Queensland, Brisbane, Australia Thursday, 12 January 2017 415-FD-54 Static and Dynamic Stall Control Texas 1 Chaired by: M. SAMIMY, The Ohio State University and M. VISBAL, USAF AFRL/RQVA 1400 hrs 1430 hrs 1500 hrs AIAA-2017-1687 AIAA-2017-1688 AIAA-2017-1689 Unsteady Flow Separation Control Experimental Study of Burst Ratio Numerical Simulation of Stall Flow over a NACA 0015 using NS-DBD Effect for Dielectric-Barrier-Discharge Control over NACA0012 Airfoil with Plasma Actuators Plasma Actuator for Separation Control Contour Bump A. Singhal, D. Castañeda, N. Webb, M. S. Sekimoto, Tokyo University of Science, L. Hao, Northwestern Polytechnical Samimy, Ohio State University, Columbus, Tokyo, Japan; N. Tanaka, Tohoku University, University, Xi’an, China OH Sendai, Japan; T. Nonomura, Japan Aerospace Exploration Agency (JAXA), Sagamihara, Japan; H. Nishida, Tokyo University of Agriculture and Technology, Koganei, Japan; K. Fujii, Tokyo University of Science, Tokyo, Japan Thursday, 12 January 2017 416-FD-55 Jet-Based Flow Control Texas 2 Chaired by: O. STALNOV, Technical University of Berlin Germany and R. WOSZIDLO, The Boeing Company 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs AIAA-2017-1690 AIAA-2017-1691 AIAA-2017-1692 AIAA-2017-1693 AIAA-2017-1694 Investigation of Crossflow Characterization of SaOB Actuators Nonlinear Interactions in Planar Jet Super-Lift Coefficient of Active Flow Numerical and Experimental Interaction of an Oscillating Jet Interacting With Flat Plate Flow with Direct Turbulence Scale Control Airfoil: What is the Limit? Study of the Co-Flow Jet Airfoil M. Hossain, R. Prenter, R. Lundgreen, L. Boundary Layers Excitation Y. Yang, G. Zha, University of Miami, Performance Enhancement Agricola, A. Ameri, J. Gregory, Ohio State J. Wilson, D. Schatzman, Army Aviation T. Kreutzfeldt, University of Maryland, Miami, FL S. Zhang, B. Song, X. Yang, J. Xu, University, Columbus, OH; et al. and Missile Research Development and College Park, College Park, MD; J. Hrynuk, C. Northwestern Polytechnical University, Engineering Center, Moffett Field, CA; A. Kroninger, B. Glaz, Army Research Laboratory, Xi’an, China 158 Seifert, Tel Aviv University, Tel Aviv, Israel; Aberdeen Proving Ground, MD; P. Hareesh, V. E. Arad, Rafael Advanced Defense Systems, Hrishikeshavan, University of Maryland, College Ltd., Haifa, Israel; L. Marom, N. Shay, Tel Park, College Park, MD; et al. Aviv University, Tel Aviv, Israel; et al. Thursday, 12 January 2017 417-FD-56 Boundary Layers and Shear Layers II Texas 4 Chaired by: J. SEIDEL, USAF Academy and T. MCLAUGHLIN, US Air Force Academy 1400 hrs 1430 hrs 1500 hrs 1530 hrs AIAA-2017-1695 AIAA-2017-1696 AIAA-2017-1697 AIAA-2017-1698 Analysis of Unstable Mode Structures in Turbulent Boundary Layer Response Influence of Streamline Adverse In-Flight Measurements of Low-Altitude Hypersonic Boundary Layer to Multiple Step Changes in Surface Pressure Gradients on the Structure of Marine Atmospheric Properties H. Tatematsu, Y. Ogino, N. Ohnishi, Tohoku Roughness a Mach 5 Turbulent Boundary Layer G. Brian, J. Dansie, Department of Defence, University, Sendai, Japan; H. Tanno, Japan J. George, MetroLaser, Inc., Laguna N. Tichenor, PM&AM Research, Bryan, TX; Fishermans Bend, Australia; D. Newman, Aerospace Exploration Agency (JAXA), Hills, CA; G. Byun, R. Simpson, Applied I. Neel, A. Leidy, R. Bowersox, Texas A&M Quantitative Aeronautics Pty., Ltd., Glebe, Kakuda, Japan University Research, Blacksburg, VA University, College Station, TX Australia; J. Gibard, Department of Defence, Fishermans Bend, Australia Thursday, 12 January 2017 418-FD-57 Multiphase Flows II Texas 3 Chaired by: C. TSAI, Lockheed Martin Space Systems and M. SOTERIOU, United Technologies Research Center 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs AIAA-2017-1700 AIAA-2017-1701 AIAA-2017-1702 AIAA-2017-1703 AIAA-2017-1704 Direct numerical simulation of noise Numerical Investigation on the A Numerical Parametric Study High Fidelity Simulation of the Direct numerical simulations suppression by water injection in Flow Structure of Gaseous Jet on the Air-Blast Atomization of a Impact of Pressure Conditions on of turbulent multiphase flows high-speed flows Horizontally Injected into Water for Planar Liquid Layer Liquid Jet in Crossflow Atomization undergoing evaporation J. Capecelatro, University of Michigan, Ann Underwater Propulsion R. Chiodi, O. Desjardins, Cornell University, X. Li, M. Soteriou, United Technologies J. Palmore, O. Desjardins, Cornell Arbor, Ann Arbor, MI; D. Buchta, University L. Shipeng , Y. Tang, X. Zhang, Z. Liu, Ithaca, NY Corporation, East Hartford, CT University, Ithaca, NY of Illinois, Urbana-Champaign, Urbana, IL N. Wang, Beijing Institute of Technology, Beijing, China Thursday, 12 January 2017 419-FD-58 Vortex Flows Texas 5 Chaired by: J. HARTWIG, NASA Glenn Research Center 1400 hrs 1430 hrs 1500 hrs 1530 hrs AIAA-2017-1705 AIAA-2017-1706 AIAA-2017-1707 AIAA-2017-1708 Better Insight into the Wingtip Integral Surface Analysis of Vortical A Computational Fluid Dynamics Proper Orthogonal Decomposition Vortex-Free Shear Layer Interaction Lobed Nozzle Flows Study of Swirling Flow Reduction by Analysis on the Hydrodynamic S. Gunasekaran, A. Altman, University of A. Gehrke, O. Wuensch, University of Using Anti-Vortex Baffle Effects of the Propulsor Geometries Dayton, Dayton, OH Kassel, Kassel, Germany; M. Ruetten, H. Yang, CFD Research Corporation, in Flapping Propulsion German Aerospace Center (DLR), Huntsville, AL P. Han, G. Liu, H. Dong, University of Göttingen, Germany Virginia, Charlottesville, Charlottesville, VA Thursday, 12 January 2017 420-FD-59 Turbulence and Transition Texas 6 Chaired by: B. WHEATON, JHU Applied Physics Laboratory 1400 hrs 1430 hrs 1500 hrs 1530 hrs AIAA-2017-1709 AIAA-2017-1710 AIAA-2017-1711 AIAA-2017-1712 Enhancement of the Amplification Uncertainty Quantification and Numerical Investigation of A Physics-Informed Machine Factor Transport Transition Modeling Sensitivity Analysis of SA Turbulence Transcritical-T Heat-and-Mass- Learning Approach of Improving Framework Model Coefficients in Two and Three Transfer Dynamics in Compressible RANS Predicted Reynolds Stresses J. Coder, Pennsylvania State University, Dimensions Turbulent Channel Flow J. Wang, J. Wu, H. Xiao, Virginia University Park, PA J. Schaefer, A. Cary, M. Mani, P. Spalart, K. Kim, Purdue University, West Lafayette, Polytechnic Institute and State University, The Boeing Company, St. Louis, MO IN; J. Hickey, University of Waterloo, Blacksburg, VA Waterloo, Canada; C. Scalo, Purdue University, West Lafayette, IN Thursday, 12 January 2017 159 421-GNC-23 Verification and Validation of Adaptive Systems II Austin 2 Chaired by: T. YUCELEN, Missouri University of Science & Technology and J. MUSE, AFRL/RQQA 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs AIAA-2017-1713 AIAA-2017-1714 AIAA-2017-1715 AIAA-2017-1716 AIAA-2017-1717 Robustness of Adaptive Control Model Reference Neuroadaptive Performance Optimizing Multi- Approaches to Real-time Predictive On the Stability of Adaptive Control Systems to Unmodeled Dynamics: A Control Revisited: How to Keep Objective Adaptive Control with Estimation of Loss-of-Control Events Systems in the presence of Control and Describing Function Viewpoint the System Trajectories on a Given Time-Varying Reference Model & Boundaries on Transport Aircraft State Dependent Unmodeled Dynamics H. Hussain, C. Sharma Subedi, A. Annaswamy, Compact Set Modification M. Rafi, J. Steck, A. Chakravarthy, Wichita K. Dogan, B. Gruenwald, T. Yucelen, Missouri Massachusetts Institute of Technology, E. Arabi, B. Gruenwald, T. Yucelen, N. Nguyen, K. Hashemi, NASA Ames State University, Wichita, KS; T. Yucelen, University of Science and Technology, Rolla, Cambridge, MA; E. Lavretsky, The Boeing University of South Florida, Tampa, FL; M. Research Center, Moffett Field, CA; T. University of South Florida, Tampa, FL MO; J. Muse, Air Force Research Laboratory, Company, Huntington Beach, CA Fravolini, University of Perugia, Perugia, Yucelen, E. Arabi, University of South Wright-Patterson AFB, OH Italy; N. Nguyen, NASA Ames Research Florida, Tampa, FL Center, Moffett Field, CA Thursday, 12 January 2017 422-GNC-24 Elastic Aircraft and Load Alleviation Austin 1 Chaired by: M. BALAS, Embry-Riddle Aeronautical University and A. CHAKRAVARTHY, Wichita State University 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs AIAA-2017-1718 AIAA-2017-1719 AIAA-2017-1720 AIAA-2017-1721 AIAA-2017-1722 Gust-Load Alleviation of a Flexible Optimal Control Allocation with Optimal Control Allocation with Gust Load Alleviation Control for a Optimal Decentralized Controller Aircraft using a Disturbance Observer Load Sensor Feedback for Active Load Sensor Feedback for Active Flexible Aircraft with Loss of Control with Output Feedback Design for an R. Caverly, University of Michigan, Ann Arbor, Load Suppression, Experiment Load Suppression, Flight Test Results Effectiveness Elastically Shaped Aircraft Concept Ann Arbor, MI; J. Forbes, McGill University, Development C. Miller, D. Goodrick, NASA Armstrong W. Fan, H. Liu, R. Kwong, University of W. Nobleheart, Nobleheart Products, LLC, Montréal, Canada; B. Danowsky, Systems C. Miller, D. Goodrick, NASA Armstrong Flight Research Center, Edwards, CA Toronto, Toronto, Canada Wichita, KS; N. Nguyen, NASA Ames Technology, Inc., Hawthorne, CA; P. Suh, NASA Flight Research Center, Edwards, CA Research Center, Moffett Field, CA Armstrong Flight Research Center, Edwards, CA Thursday, 12 January 2017 423-GNC-25 ATM and Operations Grapevine D Chaired by: J. KROZEL, The Innovation Laboratory and S. SANKARARAMAN, SGT Inc., NASA Ames Research Center 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2017-1723 AIAA-2017-1724 AIAA-2017-1725 AIAA-2017-1726 AIAA-2017-1727 AIAA-2017-1728 Eabling Technologies supporting Uncertainty Quantification in Airline Dispatcher Cost Situational A Framework for Wind Sensitivity Using Weather Translation and Just On Time – A Concept for iPad Oceanic Trajectory-Based Operations Trajectory Prediction for Aircraft Awareness Analysis for Trajectory Tracking. Machine Learning to Identify Enabled Timely Accurate Continuous P. Hruz, Metron Aviation, Inc., Dulles, VA; Operations J. Krozel, Innovation Laboratory, Inc., H. Escamilla, French Civil Aviation Similar Weather Impact Day Descent Operations J. Krozel, Innovation Laboratory, Inc., S. Sankararaman, M. Daigle, NASA Ames Portland, OR; W. Leber, C. Maccarone, University, Toulouse, France; H. Bouadi, J. Chen, R. Kicinger, Metron Aviation, H. Lenz, German Aerospace Center (DLR), Portland, OR; W. Leber, PASSUR Aerospace, Research Center, Moffett Field, CA PASSUR Aerospace, Stamford, CT École Militaire Polytechnique, Alger, Algeria; Inc., Dulles, VA; S. Schelling, J. Krozel, Braunschweig, Germany Stamford, CT; C. Cross, G. O’Keeffe, F. Mora-Camino, French Civil Aviation Innovation Laboratory, Inc., Portland, OR Metron Aviation, Inc., Dulles, VA University, Toulouse, France Thursday, 12 January 2017 424-GNC-26 Spacecraft and Launch Trajectory and Planning Grapevine 6 Chaired by: J. REED, United Launch Alliance, LLC and K. BOLLINO, U.S. Air Force 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs AIAA-2017-1729 AIAA-2017-1730 AIAA-2017-1731 AIAA-2017-1732 AIAA-2017-1733 A Study on Rendezvous Trajectory A General Approach for Calculating Using Solar Sails to Transfer to the Fuel-Optimal Rocket Landing with A Multi-Objective Planning Method Design Utilizing Invariant Manifolds Far-Field Orbital Rendezvous L5 Lagrange Point Aerodynamic Controls for Multi-Debris Active Removal of Cislunar Periodic Orbits Maneuvers A. Meras, C. Damaren, University of X. Liu, Beijing Institute of Technology, Mission in LEO S. Ueda, N. Murakami, T. Ikenaga, Japan M. Walsh, M. Peck, Cornell University, Toronto, Toronto, Canada Beijing, China Y. Liu, J. Yang, Northwestern Polytechnical Aerospace Exploration Agency (JAXA), Ithaca, NY University, Xi’an, China Sagamihara, Japan Thursday, 12 January 2017 425-GNC-27 Control Theory, Analysis and Design II Austin 5 160 Chaired by: R. YEDAVALLI, The Ohio State University and A. NARANG-SIDDARTH, University of Washington 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2017-1734 AIAA-2017-1735 AIAA-2017-1736 AIAA-2017-1737 AIAA-2017-1738 AIAA-2017-1739 A combined Averaging-Shooting Flutter Suppression for a Two Centralized Predictive Control Optimal Guidance with Additional Passivity-Based Magnetic Attitude Simultaneous Arrival Control Approach for the Trim Analysis of Degree of Freedom Aeroeslastic Allocation Scheme for V/STOL Thrust Controller For Various Flight Control with Impulsive Thrusting Algorithms for Weapon Target Hovering Insects/Flapping-Wing Wing Section: a Structured Aircrafts Tasks B. Vatankhahghadim, C. Damaren, Assignment Micro-Air-Vehicles H-infinity-Based Gain-Scheduling W. Xiangyang, Tsinghua University, Beijing, N. Indig, J. Ben-Asher, E. Sigal, Technion-- University of Toronto, Toronto, Canada K. Volle, J. Rogers, Georgia Institute of A. Hassan, H. Taha, University of California, Approach with Explicit Hidden China; B. Zhu, Nanjing University of Israel Institute of Technology, Haifa, Israel Technology, Atlanta, GA Irvine, Irvine, CA Coupling Terms Handling Science and Technology, Nanjing, China; H. Lhachemi, D. Saussie, G. Zhu, École Z. Cheng, J. Zhu, Tsinghua University, Polytechnique de Montréal, Montréal, Canada Beijing, China Thursday, 12 January 2017 426-GNC-28 Aerospace Robotics Guidance and Navigation Austin 6 Chaired by: H. LIU, University of Toronto and S. ULRICH, Carleton University 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2017-1740 AIAA-2017-1741 AIAA-2017-1742 AIAA-2017-1743 AIAA-2017-1744 AIAA-2017-1745 Autonomous Navigation with Acoustic Detection of UAS Technologies Robust detection and tracking of Neural Network Guidance for UAVs Dynamic Re-Plan of the Loyal Dynamic Visual Servoing of Obstacle Avoidance for Unmanned Using a Biologically-Inspired Wide- ground vehicles using UAV K. Julian, M. Kochenderfer, Stanford Wingman Optimal Control Problem a Rotary-wing Unmanned Aircraft Systems using MILP Band Integration Method H. Oliveira, University of Porto, Porto, Portugal; University, Stanford, CA C. Humphreys, R. Cobb, D. Jacques, J. Aerial Vehicle Without Velocity J. Devens, T. Bakker, R. Klenke, Virginia I. Movius, J. King, K. Barbor, M. Mondal, I. S. P B, Indraprastha Institute of Information Reeger, Air Force Institute of Technology, Measurement Commonwealth University, Richmond, VA Faruque, University of Maryland, College Park, Technology Delhi, New Delhi, India; J. Sousa, Wright-Patterson AFB, OH H. Xie, K. Low, Nanyang Technological College Park, MD University of Porto, Porto, Portugal University, Singapore, Singapore Thursday, 12 January 2017 427-GTE-9/PGC-6 Pressure Gain Combustion for Gas Turbines Grapevine C Chaired by: V. RAMAN, University of Michigan 1400 hrs 1430 hrs 1500 hrs 1530 hrs AIAA-2017-1746 AIAA-2017-1747 AIAA-2017-1748 AIAA-2017-1749 Numerical and Analytical RDE Implementation into an Open- Influence of Actively Controlled Heat Assessment of Incidence Loss and Assessment of a Coupled Rotating Loop T63 Gas Turbine Engine Release Timing on the Performance Shaft Work Production For Wave Detonation Engine and Turbine A. Naples, J. Hoke, Innovative Scientific and Operational Characteristics of a Rotor Combustor with Non-Axial Experiment Solutions, Inc., Dayton, OH; R. Battelle, Rotary Valve, Acoustically Resonant Channels D. Paxson, NASA Glenn Research Center, M. Wagner, F. Schauer, Air Force Research Pulse Combustor R. Jagannath, S. Bane, Purdue University, Cleveland, OH; A. Naples, Innovative Laboratory, Wright-Patterson AFB, OH J. Lisanti, W. Roberts, King Abdullah University West Lafayette, IN; M. Feyz, M. Nalim, Scientific Solutions, Inc., Dayton, OH of Science and Technology, Thuwal, Saudi Indiana University-Purdue University Arabia Indianapolis, Indianapolis, IN Thursday, 12 January 2017 428-IS-9 Probabilistic Rule-Based Systems Ft. Worth 1 Chaired by: F. ADOLF, DLR - German Aerospace Center 1400 hrs 1430 hrs 1500 hrs 1530 hrs AIAA-2017-1750 AIAA-2017-1751 AIAA-2017-1752 Panel: Challenges to Production Intelligent Aerospace Systems Safe and Autonomous UAV A Genetic Fuzzy Logic Based A Fuzzy-Logic-Based Solution to The panel will discuss why intelligent systems and algorithms are not experiencing more widespread use by the aerospace user community. The goal of the panel will be to: Navigation using Graph Policies Approach to Solving the Aircraft Dynamic Target Interception and a) identify the reasons why intelligent systems have not gained wider use in production aerospace vehicles, b) create the steps needed to facilitate such use, and c) including a) T. Mannucci, E. Van Kampen, C. de Visser, Conflict Resolution Problem Landing with a Small Multirotor and b) into the Autonomy Roadmap which has been written by the Intelligent Systems Technical Committee. Q. Chu, Delft University of Technology, A. Sathyan, University of Cincinnati, Aircraft Moderator: John Valasek, Texas A&M University Delft, The Netherlands Cincinnati, OH; N. Ernest, Psibernetix, Inc., N. Stockton, M. Kumar, K. Cohen, Cincinnati, OH; L. Lavigne, F. Cazaurang, University of Cincinnati, Cincinnati, OH Panelists: University of Bordeaux, Bordeaux, Jason Mukherjee Adrian Stoica Greg Tallant Kevin Wise

161 France; M. Kumar, K. Cohen, University of AeroVironment NASA Jet Propulsion Laboratory Lockheed Aeronautical Systems Company The Boeing Company Cincinnati, Cincinnati, OH Thursday, 12 January 2017 429-MDO-11 Aircraft Design Optimization III Mustang 1 Chaired by: J. ZHANG, The University of Texas at Dallas and S. CHOI, Virginia Tech 1400 hrs 1430 hrs 1500 hrs AIAA-2017-1753 AIAA-2017-1754 AIAA-2017-1755 Study of a Boundary Layer Variable-Fidelity Multidisciplinary Multi-Objective Aircraft Design Ingestion Configuration using a Design Optimization with Uncertain Optimization for Low External Noise Fully Coupled Propulsion-RANS Design Variable for Innovative and Fuel Burn Model Control Effector of Tailless Aircraft C. Ilario da Silva, T. Orra, Embraer, São J. Gray, NASA Glenn Research Center, J. Park, Virginia Polytechnic Institute and José dos Campos, Brazil; J. Alonso, Cleveland, OH; C. Mader, G. Kenway, J. State University, Blacksburg, VA; Y. Jo, Stanford University, Stanford, CA Martins, University of Michigan, Ann Arbor, Korea Advanced Institute of Science and Ann Arbor, MI Technology, Daejeon, South Korea; S. Choi, Virginia Polytechnic Institute and State University, Blacksburg, VA Thursday, 12 January 2017 430-MST-15 Modeling and Simulation of Air Vehicle Dynamics, Systems, and Environments San Antonio 1 Chaired by: D. CRIDER, National Transportation Safety Board 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs AIAA-2017-1756 AIAA-2017-1757 AIAA-2017-1758 AIAA-2017-1759 AIAA-2017-1760 Ventus – Towards a cost-effective A Tailless Fighter Aircraft Model Modeling of Flight Dynamics and Aerodynamic Lateral-Directional A Four-Stage One-Dimensional phenomenological post-stall for Control-Related Research and Pilot’s Handling of a Hang Glider Coefficients Modeling During Model for Rime, Mixed and Glaze aerodynamic model add-on for Development Y. Ochi, National Defense Academy, Aircraft Design Phases Ice Accretion on Aerofoils upset recovery training M. Niestroy, K. Dorsett, K. Markstein, Lockheed Yokosuka, Japan A. de Paula, F. Porto, Technological Institute Z. Janjua, B. Turnbull, S. Hibberd, K. Choi, M. Roza, R. Van der Ploeg, M. Laban, Martin Corporation, Fort Worth, TX of Aeronautics (ITA), São José dos Campos, University of Nottingham, Nottingham, Netherlands Aerospace Centre NLR, Brazil; M. Sousa, Federal University of United Kingdom Amsterdam, The Netherlands Itajubá, Itajubá, Brazil Thursday, 12 January 2017 431-MST-16 Modeling and Simulation in Education/Special Topics in Modeling and Simulation Ft. Worth 7 Chaired by: P. GRANT, University of Toronto and S. BEARD, NASA/ARC-AFS Aerospace Simulation R&D 1400 hrs 1430 hrs 1500 hrs 1530 hrs AIAA-2017-1761 AIAA-2017-1762 AIAA-2017-1763 AIAA-2017-1764 A Proposed Hardware in the Loop Design, Build and Integration of The Use of Modelling and Simulation Energy-Based Compressible Convective Gimbal Platform that Supports an a Low-Cost Self-Erecting Inverted to Give Students a HEADSTART into model Proper for Multiple field Applied Graduate Controls Course Pendulum Mechanism Aerospace Engineering Dynamic Investigation: A Bond Graph M. Smith, J. Reasoner, R. Fithen, Arkansas K. Turkoglu, B. Graham, San Jose State M. White, C. Dadswell, T. Fell, R. Coates, Approach on FSI Problems Technical University, Russellville, AR University, San Jose, CA University of Liverpool, Liverpool, United A. Zanj, F. He, Flinders University, Adelaide, Kingdom Australia; P. Breedveld, University of Twente, Enschede, The Netherlands Thursday, 12 January 2017 162 432-MST-17 Modeling and Simulation Integration and Architectures Ft. Worth 6 Chaired by: P. ZAAL, NASA Ames Research Center and A. ELMILIGUI, NASA Langley Research Center 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs AIAA-2017-1765 AIAA-2017-1766 AIAA-2017-1767 AIAA-2017-1768 AIAA-2017-1769 Schedule Failure Analysis within the The Horizon Simulation Framework A Virtual Laboratory for Aviation A Code Architecture to Streamline Integrated System Modeling in Horizon Simulation Framework v3.0 and Airspace Prognostics Research the Missile Simulation Life Cycle SysML for Small Satellites I. Lunsford, E. Mehiel, California M. Yost, E. Mehiel, California Polytechnic C. Kulkarni, C. Teubert, G. Gorospe, Stinger R. Sells, DESE Research, Inc., Huntsville, AL L. Walker, D. Thomas, University of Polytechnic State University, San Luis State University, San Luis Obispo, San Luis Ghaffarian Technologies, Inc., Moffett Field, Alabama, Huntsville, Huntsville, AL Obispo, San Luis Obispo, CA Obispo, CA CA; C. Quach, NASA Langley Research Center, Hampton, VA; E. Hogge, Northrop Grumman Corporation, Hampton, VA Thursday, 12 January 2017 433-NDA-9 Model Calibration, Verification, and Validation Mustang 2 Chaired by: L. DOMYANCIC, Southwest Research Institute and T. WEST, NASA Langley Research Center 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2017-1770 AIAA-2017-1771 AIAA-2017-1772 AIAA-2017-1773 AIAA-2017-1774 AIAA-2017-1775 Visualization of High Dimensional Identification and quantification Variance Reduction Estimation in Fuzzy Logic Controller Stability Design of Multi-Level Validation Bayesian Calibration of Spatially Turbulence Simulation Data using t-SNE of spatial variability in the Bayesian Inference Analysis Using a Satisfiability Experiments for Multi-Physics Systems Varying Model Parameters with J. Wu, J. Wang, H. Xiao, Virginia elastostatic properties of additively C. Li, S. Mahadevan, Vanderbilt University, Modulo Theories Approach D. Villanueva, Universal Technology High-Dimensional Response Polytechnic Institute and State University, manufactured components Nashville, TN T. Arnett, B. Cook, University of Cincinnati, Corporation, Wright-Patterson AFB, OH; B. P. Nath, Z. Hu, S. Mahadevan, Vanderbilt Blacksburg, VA; J. Ling, Sandia National M. Faes, D. Moens, Catholic University of Cincinnati, OH; M. Clark, Air Force Research Smarslok, Air Force Research Laboratory, University, Nashville, TN Laboratories, Livermore, CA Leuven, Leuven, Belgium Laboratory, Wright-Patterson AFB, OH; K. Wright-Patterson AFB, OH; G. Bartram, Rattan, Wright State University, Dayton, OH Universal Technology Corporation, Wright- Patterson AFB, OH Thursday, 12 January 2017 434-PC-24 Advanced Combustion Concepts II Grapevine 1 Chaired by: E. LYNCH, Aerojet Rocketdyne and L. SMITH, United Technologies Research Center 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs AIAA-2017-1776 AIAA-2017-1777 AIAA-2017-1778 AIAA-2017-1779 AIAA-2017-1780 The Effect of Ozonolysis Activated Study of Nanosecond Pulsed High Demonstration of swirl-controlled Investigations of Microwave Computations of a New Hydrogen- Autoignition on Jet Flame Dynamics Frequency Discharge Ignition in a 3D-printed mesoscale burner array Stimulation of Turbulent Flames with Oxygen Rocket Engine Based on X. Gao, W. Sun, Georgia Institute of Flowing Methane/Air Mixture using gaseous hydrocarbon fuels Implications to Gas Turbine Combustors Supermulti-jets Colliding with Pulse Technology, Atlanta, GA; T. Ombrello, C. J. Lefkowitz, T. Ombrello, Air Force Research C. Martin, R. Groetz, J. Yoo, State C. Fureby, Swedish Defense Research Agency R. Konagaya, K. Naitoh, T. Okamoto, K. Carter, Air Force Research Laboratory, Laboratory, Wright-Patterson AFB, OH University of New York, Buffalo, NY; T. Lee, (FOI), Stockholm, Sweden; A. Ehn, E. Nilsson, Tsuru, Waseda University, Tokyo, Japan Wright-Patterson AFB, OH University of Illinois, Urbana-Champaign, P. Petterson, M. Aldén, Lund University, Lund, Urbana, IL Sweden; T. Hurtig, Swedish Defense Research Agency (FOI), Stockholm, Sweden; et al. Thursday, 12 January 2017 435-PC-25 Turbulent Combustion: Flow/Chemistry interactions Dallas 7 Chaired by: I. BOXX, DLR - German Aerospace Center and E. MASTORAKOS, University of Cambridge 1400 hrs 1430 hrs 1500 hrs 1530 hrs AIAA-2017-1781 AIAA-2017-1782 AIAA-2017-1783 AIAA-2017-1784 Effect of Low-Temperature Turbulence effects on the chemical Reconfigurable Fan-Stirred Flame Turbulence-Flame Interaction in the Reactivity on the Turbulent pathways for premixed Methane/ Bomb with Optical Access Wrinkled and Corrugated Flamelet Combustion of n-Octane/iso-Octane Air flames A. Morones, V. Leon, E. Petersen, Texas Regimes Mixtures in a Reactor-Assisted D. Dasgupta, W. Sun, Georgia Institute of A&M University, College Station, TX M. Geikie, C. Engelmann, A. Morales, R. Turbulent Slot Burner Technology, Atlanta, GA; M. Day, Lawrence Schale, K. Ahmed, University of Central C. Reuter, S. Won, Y. Ju, Princeton Berkeley National Laboratory, Berkeley, CA; Florida, Orlando, FL University, Princeton, NJ T. Lieuwen, Georgia Institute of Technology, Atlanta, GA 163 Thursday, 12 January 2017 436-PC-26 Soot/Pyrolysis Ft. Worth 2 Chaired by: Y. JU, Princeton University and H. CHELLIAH, University of Virginia 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2017-1785 AIAA-2017-1786 AIAA-2017-1787 AIAA-2017-1788 AIAA-2017-1789 AIAA-2017-1790 Large Eddy Simulations of a Sooting Assessment of Differential Diffusion Experimental and Modeling Vortex Dynamics and Soot Detailed-Chemistry Study of Soot A computational study of soot Lifted Turbulent Jet-Flame Effects on Soot Evolution in Piloted Investigation of Pyrolytic Carbon Formation in a Dump Combustor Nano-Aerosol Formation in a formation in opposed-flow diffusion C. Eberle, German Aerospace Center (DLR), Non-premixed Turbulent Flames Deposition Relevant to Fuel Film V. Katta, Innovative Scientific Solutions, Inc., Stagnation-Point Reverse-Flow flame interacting with vortices Stuttgart, Germany; P. Gerlinger, University H. Lalit, J. Gore, H. Wang, Purdue Cooling in Rocket Engines Dayton, OH; W. Roquemore, Air Force Research Combustor P. Selvaraj, H. Im, King Abdullah University of Stuttgart, Stuttgart, Germany; M. University, West Lafayette, IN P. Gokulakrishnan, R. Joklik, C. Fuller, Laboratory, Wright-Patterson AFB, OH M. Darbandi, M. Saidi, M. Ghafourizadeh, of Science and Technology, Thuwal, Saudi Aigner, German Aerospace Center (DLR), Combustion Science & Engineering, Sharif University of Technology, Tehran, Arabia Stuttgart, Germany Inc., Columbia, MD; R. Vander Wal, J. Iran; G. Schneider, University of Waterloo, Abrahamson, Pennsylvania State University, Waterloo, Canada University Park, PA Thursday, 12 January 2017 437-PC-27 Model Validation for Propulsion Workshop II San Antonio 6 Chaired by: A. COMER, Air Force Institute of Technology and V. SANKARAN, US Air Force/AFRL/RQRC 1400 hrs 1430 hrs 1500 hrs 1530 hrs AIAA-2017-1791 AIAA-2017-1792 AIAA-2017-1793 AIAA-2017-1794 Grid Convergence in LES of Bluff Advanced LES Models for Turbulent Application of Detached Eddy Model Validation for Propulsion – Body Stabilized Flames Combustion Simulation to a Bluff Body Flame On the TFNS Subgrid Models for a V. Sankaran, United Technologies A. Potturi, Metacomp Technologies, Inc., Stabilizer in Duct Flow Bluff Body Stabilized Flame Corporation, East Hartford, CT; T. Gallagher, Agoura Hills, CA; J. Edwards, North Carolina J. West, C. Groth, University of Toronto, C. Wey, NASA Glenn Research Center, Georgia Institute of Technology, Atlanta, GA State University, Raleigh, NC Toronto, Canada Cleveland, OH Thursday, 12 January 2017 438-PC-28 Shock Tubes Austin 4 Chaired by: H. CHELLIAH, University of Virginia and J. MILLER, Air Force Reseach Laboratory 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs AIAA-2017-1795 AIAA-2017-1796 AIAA-2017-1797 AIAA-2017-1798 AIAA-2017-1799 Shock-Tube Studies of Tri-Ethyl- High-Speed Imaging of the Dynamics Shock-tube Time-history Shock Tube Measurements of Jet Instability Analysis of the Separated

Phosphate (TEP) Kinetics at High of H2/O2 Ignition at Low to Moderate Measurements of CO and H2O Using and Rocket Fuel Ignition Delay Boundary Layer in Shock Tubes Temperatures Temperatures in a Shock Tube IR Laser Absorption Times K. Grogan, M. Ihme, Stanford University, O. Mathieu, W. Kulatilaka, E. Petersen, E. Ninnemann, O. Pryor, S. Barak, B. C. Mulvihill, O. Mathieu, E. Petersen, Texas D. Davidson, J. Shao, T. Parise, R. Hanson, Stanford, CA Texas A&M University, College Station, TX Koroglu, J. Sosa, K. Ahmed, University of A&M University, College Station, TX Stanford University, Stanford, CA Central Florida, Orlando, FL; et al. Thursday, 12 January 2017 439-PC-29 Laminar Flames I San Antonio 3 Chaired by: W. KULATILAKA, Texas A & M University and E. BARBOUR, The Aerospace Corpation 1400 hrs 1430 hrs 1500 hrs 1530 hrs Oral Presentation AIAA-2017-1800 AIAA-2017-1801 AIAA-2017-1802 Invited Review: Progress and Response of Premixed Stoichiometric Major species measurements and Accuracy of plug-ow assumption in

challenges of plasma assisted CH4/O2/CO2 Flames to Strain; the Role simulation of partially-premixed, the analysis of laminar ow reactors: combustion of Chemistry and Transport cellular, tubular H2-air ﬂames an exploration of ideal operating Y. Ju, Princeton University, Princeton, NJ N. Chakroun, D. Michaels, S. Shanbhogue, D. Tinker, C. Hall, R. Pitz, Vanderbilt conditions A. Ghoniem, Massachusetts Institute of University, Nashville, TN H. Chelliah, M. Rahimi, University of Technology, Cambridge, MA Virginia, Charlottesville, Charlottesville, VA Thursday, 12 January 2017 440-PDL-12 DBD Plasma Actuators II Ft. Worth 4

164 Chaired by: J. ZIMMERMAN, CU Aerospace 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2017-1803 AIAA-2017-1804 AIAA-2017-1805 AIAA-2017-1806 AIAA-2017-1807 AIAA-2017-1808 Airfoil Stall Hysteresis Control with Influence of Voltage Waveform on Shock Wave/Boundary Layer Control Simulation of Reduced Air Plasma Modeling of a Sliding Nanosecond Improving the Performance of a DBD Plasma actuation Electrohydrodynamic Force in a Using Nanosecond Reptitively Pulsed Reactions for Nanosecond-Pulse Dielectric Barrier Discharge Actuator Plasma Actuator Model for DBD E. Batlle, R. Pereira, M. Kotsonis, Delft Dielectric-Barrier-Discharge Plasma Dielectric Barrier Discharges Dielectric Barrier Discharge for Flow Control and Multi-Encapsulated Electrode University of Technology, Delft, The Actuator K. Newnam, R. Jagannath, P. Stockett, S. Ahn, J. Chae, H. Kim, K. Kim, Seoul K. Kourtzanidis, L. Raja, University of Actuators Netherlands S. Sato, N. Ohnishi, Tohoku University, P. Wu, L. Rajendran, S. Bane, Purdue National University, Seoul, South Korea Texas, Austin, Austin, TX J. Laten, R. LeBeau, Saint Louis University, Sendai, Japan University, West Lafayette, IN St. Louis, MO Thursday, 12 January 2017 441-PDL-13 Diagnostics and Experimental Techniques Ft. Worth 5 Chaired by: R. MILES, Princeton University and K. XU, University of Alabama in Huntsville 1400 hrs 1430 hrs 1500 hrs 1530 hrs AIAA-2017-1809 AIAA-2017-1810 AIAA-2017-1811 AIAA-2017-1812 Development of a Femtosecond A parametric investigation of Electric Field Measurements in a Plasma Engine Performance Laser Electric Field Probe for Non- repetitively pulsed nanosecond Quasi-Two-Dimensional Ns Pulse Estimate by Optical Analysis of Species Dependent Measurements duration discharges in argon Discharge in Atmospheric Air Exhaust Plume B. Goldberg, A. Dogariu, Princeton R. Manoharan, T. Boyson, S. O’Byrne, M. Simeni Simeni, Ohio State University, D. M R, S. T. S., M. P, Indian Institute of University, Princeton, NJ; S. O’Byrne, University of New South Wales at the Columbus, OH; B. Goldberg, Princeton Science, Bengaluru, India University of New South Wales at the Australian Defence Force Academy, University, Princeton, NJ; C. Zhang, Chinese Australian Defence Force Academy, Canberra, Australia Academy of Sciences, Beijing, China; K. Canberra, Australia; R. Miles, Princeton Frederickson, W. Lempert, I. Adamovich, University, Princeton, NJ Ohio State University, Columbus, OH Thursday, 12 January 2017 442-SD-22 Special Session: Adaptive Aeroelastic Wing Shaping Control II Appaloosa 2 Chaired by: E. TING, SGT and B. STANFORD, NASA Langley Research Center 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs AIAA-2017-1813 AIAA-2017-1814 AIAA-2017-1815 AIAA-2017-1816 AIAA-2017-1817 Optimal Control Surface Layout for Computational Results for the KTH- Development of an Integrated Uncertainty Quantification of the LPV Model Development for a an Aeroservoelastic Wingbox NASA Wind-Tunnel Model Used for Nonlinear Aeroservoelastic Flight FUN3D-Predicted Flutter Boundary Flexible Wing Aircraft B. Stanford, NASA Langley Research Acquisition of Transonic Nonlinear Dynamic Model of the Truss-Braced on the NASA CRM A. Al-jiboory, G. Zhu, Michigan State Center, Hampton, VA Aeroelastic Data Wing Aircraft B. Stanford, S. Massey, NASA Langley University, East Lansing, MI; S. Swei, NASA W. Silva, P. Chwalowski, C. Wieseman, E. Ting, Stinger Ghaffarian Technologies, Research Center, Hampton, VA Ames Research Center, Moffett Field, CA; NASA Langley Research Center, Hampton, Inc., Moffett Field, CA; D. Chaparro, MORI W. Su, University of Alabama, Tuscaloosa, VA; D. Eller, U. Ringertz, Royal Institute of Associates, Inc., Moffett Field, CA; N. Nguyen, Tuscaloosa, AL; N. Nguyen, NASA Ames Technology (KTH), Stockholm, Sweden NASA Ames Research Center, Moffett Field, CA Research Center, Moffett Field, CA Thursday, 12 January 2017 443-SD-23 Dynamic Loads, Response, Vibration, and Stability of Aerospace Vehicles II Appaloosa 3 Chaired by: A. DATTA, Science & Technology Corporation and B. GLAZ, U. S. Army Research Laboratory (APG) 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs AIAA-2017-1818 AIAA-2017-1819 AIAA-2017-1820 AIAA-2017-1821 AIAA-2017-1822 Design and Wind Tunnel Test Validation Buffet Load Alleviation on the Fin of a Usage Analysis of BAe-146 Diffuse Acoustic Field Shaping in Challenges in Using Measured Data of Gust Load Alleviation Systems High Performance Training Aircraft Airtankers in USFS Service Acoustic Boundary Element Method to Assess Payload Stresses and S. Ricci, A. De Gaspari, L. Riccobene, F. Fonte, S. Ricci, J. Beretta, F. Fonte, Technical L. Kliment, K. Rokhsaz, Wichita State using Gradient Based Optimization Fatigue Life Technical University of Milan, Milan, Italy University of Milan, Milan, Italy; D. Monti, University, Wichita, KS Technique M. Baker, ATA Engineering, Inc., San Leonardo Company, Venegono Inferiore, Italy D. Inoyama, R. Agarwal, T. Stoumbos, Diego, CA Orbital ATK, Dulles, VA Thursday, 12 January 2017 165 444-SD-24 Dynamic Testing Techniques and System Identification II Appaloosa 4 Chaired by: M. BOESWALD, DLR - German Aerospace Center and S. SMITH, University of Kentucky 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2017-1823 AIAA-2017-1824 AIAA-2017-1825 AIAA-2017-1826 AIAA-2017-1827 AIAA-2017-1828 Flutter Flight Testing at Gulfstream Efficient ground vibration testing of Online Monitoring of Aircraft Modal Full-field Structural Dynamics by OMA Study on the Structural Flight Loads Analysis and Aerospace Using Advanced Signal aircraft based on output-only modal Parameters during Flight Test based Video Motion Manipulation Dynamic Properties of a Launcher Measurements of External Stores on Processing Techniques analysis during taxi on permanent Output-Only Modal Y. Yang, C. Farrar, D. Mascarenas, Los Alamos Vehicle Using Flight Data an Atmospheric Research Aircraft P. Taylor, Gulfstream Aerospace Corporation, Y. Govers, J. Sinske, J. Schwochow, G. Analysis National Laboratory, Los Alamos, NM M. Eugeni, G. Coppotelli, F. Mastroddi, W. Krueger, V. Handojo, T. Klimmek, Savannah, GA; R. Moreno, Altran, Madrid, Jelicic, R. Buchbach, J. Springer, German G. Jelicic, J. Schwochow, Y. Govers, J. Sinske, P. Gaudenzi, University of Rome “La German Aerospace Center (DLR), Spain; N. Banavara, R. Narisetti, L. Aerospace Center (DLR), Göttingen, R. Buchbach, J. Springer, German Aerospace Sapienza”, Rome, Italy; S. Muller, B. Göttingen, Germany Morgan, Gulfstream Aerospace Corporation, Germany; et al. Center (DLR), Göttingen, Germany Troclet, Airbus, Les Mureaux, France Savannah, GA Thursday, 12 January 2017 445-STR-11 Other Topics in Structures II Appaloosa 1 Chaired by: M. SENSMEIER, Embry-Riddle Aeronautical University and G. HRINDA, NASA-Langley Research Center 1400 hrs 1430 hrs 1500 hrs 1530 hrs AIAA-2017-1829 AIAA-2017-1830 AIAA-2017-1831 AIAA-2017-1832 Evaluation of Low Cost Additive Optimal Design of Curvilinearly A Micromechanics Based Processing Modeling Thin-Walled Beams using Manufacturing Techniques for Small Stiffened Shells Model for the Curing Response of 2D VAM Rocket Nozzles K. Singh, W. Zhao, R. Kapania, Virginia Triaxially Braided Textile Composites M. Gupta, D. Hodges, Georgia Institute of L. Kunka, J. Jacob, Oklahoma State Polytechnic Institute and State University, D. Zhang, W. Chen, University of Technology, Atlanta, GA University, Stillwater, OK Blacksburg, VA Connecticut, Storrs, Storrs, CT Thursday, 12 January 2017 446-TES-2 Fossil Fuel Power Technologies II Mustang 3 Chaired by: N. SYRED, Cardiff University and B. DAM, WoodWard 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs AIAA-2017-1833 AIAA-2017-1834 AIAA-2017-1835 AIAA-2017-1836 AIAA-2017-1837

Swirlers Effectiveness in Turbulent Study of High Intensity Turbluent Effect of N2-CO2 Mixture on Study on the Use of HiCOP Fuel for Study of Aeration by Using Transverse Jet Mixing Uniformity Flow Over a Backward Facing Entrainment and Emission in a High Gas Turbine Combustors Pulsating Air Flow T. Elgammal, R. Amano, University of Step Using 10kHz Particle Image Intensity Combustor H. Fujiwara, K. Okai, M. Makida, K. R. Amano, University of Wisconsin, Wisconsin, Milwaukee, Milwaukee, WI Velocimetry A. Said, E. Darby, A. Gupta, University of Shimodaira, T. Mizuno, Japan Aerospace Milwaukee, Milwaukee, WI; A. Alkhalidi, M. de la Torre, A. Acosta-Zamora, N. Love, Maryland, College Park, College Park, MD Exploration Agency (JAXA), Tokyo, Japan; German-Jordanian University, Amman, A. Choudhuri, University of Texas, El Paso, S. Noda, Environmental Energy, Tokyo, Jordan; A. Alkhafaji, University of El Paso, TX Japan; et al. Wisconsin, Milwaukee, Milwaukee, WI Thursday, 12 January 2017 447-TES-3 Emerging Energy Technologies I Palomino 1 Chaired by: S. SHERIF, University of Florida and A. VISHWANATH, GE 1400 hrs 1430 hrs 1500 hrs 1530 hrs AIAA-2017-1838 AIAA-2017-1839 AIAA-2017-1840 AIAA-2017-1841 Aircraft-Blended Winglet Slotted airfoils for increasing the Commercial Aircraft Cabins’ Effect of Raked Winglet on Aircraft Performance Analyses aerodynamic efﬁciency Ventilation Systems Performance E. Khalil, H. Helal, Cairo University, Cairo, S. Beyhaghi, R. Amano, University of E. Khalil, A. Azzazi, G. ElHarriri, T. E. Khalil, H. Helal, Cairo University, Cairo, Egypt; O. Abdellatif, Benha University, Cairo, Wisconsin, Milwaukee, Milwaukee, WI AbouDeif, Cairo University, Cairo, Egypt Egypt; O. Abdellatif, Benha University, Cairo, Egypt; G. ElHarriri, Cairo University, Cairo, Egypt Egypt; G. ElHarriri, Cairo University, Cairo, Egypt Thursday, 12 January 2017 448-TP-12 Direct Simulation Monte Carlo Methods Austin 3

166 Chaired by: K. STEPHANI, University of Illinois at Urbana-Champaign 1400 hrs 1430 hrs 1500 hrs 1530 hrs AIAA-2017-1842 AIAA-2017-1843 AIAA-2017-1844 AIAA-2017-1845 DSMC implementation of compact DSMC Acceleration Techniques DSMC Computations of Separation Detailed DSMC Surface Chemistry state-speciﬁc N2+O dissociation and Applied to Shock Heated and over a `Tick’ model in Hypersonic Modeling of the Oxidation of exchange models Recirculating Flows High Enthalpy Transitional Flows Carbon-Based Ablators I. Borges Sebastiao, H. Luo, M. N. Singh, S. Poovathingal, T. R. Prakash, S. Gai, S. O’Byrne, University K. Swaminathan Gopalan, A. Borner, K. Kulakhmetov, A. Alexeenko, Purdue Schwartzentruber, University of Minnesota, of New South Wales at the Australian Stephani, University of Illinois, Urbana- University, West Lafayette, IN Minneapolis, Minneapolis, MN Defence Force Academy, Canberra, Champaign, Urbana, IL; N. Mansour, NASA Australia Ames Research Center, Moffett Field, CA Thursday, 12 January 2017 449-WE-10 Wind Energy Control and Optimization II Texas D Chaired by: C. BOTTASSO, Technichse Universität München 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2017-1846 AIAA-2017-1847 AIAA-2017-1848 AIAA-2017-1849 AIAA-2017-1850 AIAA-2017-1851 Multi-ﬁdelity Optimization of Inverse Design of a Dual-Rotor Inverse Design of Horizontal Axis Propagation of Uncertainties Aerodynamic Shape Optimization of Modeling of Tethered Kite Apparent Horizontal Axis Wind Turbines Wind Turbine using a Prescribed Wind Turbine Blades Through Wind Turbine Models for Wind Turbine Blades for Reducing Velocity Dynamics Based on M. McWilliam, F. Zahle, C. Pavese, J. Wake Vortex Lattice Method B. Moghadassian, A. Sharma, Iowa State Robust Design Optimization Power Production Losses due to Ice Effective Attitude Tracking Blasques, Technical University of Denmark, A. Rosenberg, A. Sharma, Iowa State University, Ames, IA C. Bottasso, P. Bortolotti, J. Loganathan, Accretion H. Li, D. Olinger, M. Demetriou, Worcester Risø, Denmark University, Ames, IA Technical University of Munich, Munich, O. Yirtici, I. Tuncer, S. Ozgen, Middle East Polytechnic Institute, Worcester, MA Germany Technical University, Ankara, Turkey Thursday, 12 January 2017 450-NW-19 Thursday Afternoon Networking Coffee Break Session Room Foyers 1530 - 1600 hrs Thursday, 12 January 2017 451-NW-20 Women at SciTech Social Hour and Keynote Texas C 1730 - 1930 hrs Open to all attendees

The Workplace of the Future: Technology Traps and Leadership Challenges Mary “Missy” Cummings Professor, School of Engineering, Duke University Director, Humans and Autonomy Laboratory, Duke Robotics Friday Friday, 13 January 2017 452-NW-21 Friday Early Morning Coffee Break Session Room Foyers 0700 - 0730 hrs Friday, 13 January 2017 453-SB-5 Friday Morning Speakers’ Brieﬁng Session Rooms 0730 - 0800 hrs Friday, 13 January 2017 454-PLNRY-7 Friday Morning Plenary: Next-Generation Workforce Texas A & B 0800 - 0900 hrs Moderator: Darryll Pines, Dean, A. James Clark School of Engineering, University of Maryland

Panelists:

167 Curt Carlson Jaiwon Shin Dennis Todd Graham Warwick Founder & Chief Executive Ofﬁcer Associate Administrator, Aeronautics Mission Directorate Vice President, Engineering—Services and Support Technology Managing Editor The Practice of Innovation NASA Boeing Commercial Airplanes Aviation Week & Space Technology

Friday, 13 January 2017 455-NW-22 Friday Morning Networking Coffee Break Session Room Foyers 0900 - 0930 hrs Friday, 13 January 2017 456-ABPSI-3 Nozzles and Propulsion Design Dallas 1 Chaired by: E. LOTH, University of Virginia and L. LEAVITT, N A S A 0930 hrs 1000 hrs 1030 hrs AIAA-2017-1852 AIAA-2017-1853 AIAA-2017-1854 Performance Prediction of External Relating a Jet-Surface Interaction A Study of Engine Parameters and Nozzle with Clustered Entrance Experiment to a Commercial Shaft Configuration on Transport T. Isono, Tohoku University, Sendai, Supersonic Transport Aircraft Using Aircraft Performance Japan; S. Tomioka, N. Sakuranaka, Japan Numerical Simulations I. Garnica, T. Takahashi, Arizona State Aerospace Exploration Agency (JAXA), V. Dippold, D. Friedlander, NASA Glenn University, Tempe, AZ Kakuda, Japan Research Center, Cleveland, OH Friday, 13 January 2017 457-ACD-11 Special Purpose Aircraft Pecos 3 Chaired by: R. BARRETT and J. WELSTEAD, NASA Langley Research Center 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2017-1855 AIAA-2017-1856 AIAA-2017-1858 AIAA-2017-1859 AIAA-2017-1860 AIAA-2017-1857 Next-Generation Regional Jet Boarding and Turnaround Process Particle Swarm Optimization with Reconfigurable Internal Weapons Natural Laminar Flow Wing Design Wing-body junction redesign Transport Conceptual Design Assessment of Single- and Twin-Aisle Surrogate Modelling for Passive Carriage System for Small Fighter for a Low-Boom Supersonic Aircraft with CAD-based parametrization M. Benassi, C. Hrdina, E. Horton, E. Aircraft Vortex Generators Aircraft H. Ishikawa, ASIRI Corporation, Tokyo, including moving intersection Hadder, T. Takahashi, Arizona State M. Schmidt, Munich Aerospace e.V., J. Fox, C. Bil, R. Carrese, RMIT University, M. Anderson, K. Teope, U.S. Air Force Japan; Y. Ueda, Try-Angle, Inc., Tokyo, S. Xu, S. Timme, University of Liverpool, University, Tempe, AZ Taufkirchen, Germany; P. Heinemann, Melbourne, Australia Academy, Colorado Springs, CO Japan; N. Tokugawa, Japan Aerospace Liverpool, United Kingdom; O. Mykhaskiv, M. Hornung, Bauhaus Luftfahrt e.V., Exploration Agency (JAXA), Tokyo, Japan J. Mueller, Queen Mary University of Taufkirchen, Germany London, London, United Kingdom Friday, 13 January 2017 458-AFM-11 Aircraft Flight Dynamics, Handling Qualities, and Performance IV Grapevine 5 Chaired by: N. DEVARAKONDA, The Ohio State University and N. HALL, Lockheed Martin 0930 hrs 1000 hrs 1030 hrs AIAA-2017-1861 AIAA-2017-1862 AIAA-2017-1863 Non-Centroidal Equations of Motion Dynamic Soaring − Kinetic Energy Online Damage Case Identification for Flight Simulation and Inertial Speed for Database-driven Safe Flight G. Howe, Gulfstream Aerospace G. Sachs, B. Grüter, Technical University of Envelope Prediction System Corporation, Savannah, GA Munich, Garching, Germany Y. Zhang, C. de Visser, Q. Chu, Delft University of Technology, Delft, The Netherlands Friday, 13 January 2017 459-AFM-12 Aerodynamic Prediction Methods Grapevine 4

168 Chaired by: K. DORSETT, Lockheed Martin Aeronautics and M. PHILLIPS, NASA 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2017-1864 AIAA-2017-1865 AIAA-2017-1866 AIAA-2017-1867 AIAA-2017-1868 AIAA-2017-1869 Main Rotor Downwash Effect Flight Test Maneuver Design and Revised Indicial Aerodynamics Experimental and Numerical Calibration and accuracy Determination of Water Droplet on Separation Characteristics of Aerodynamic Parameter Estimation for Parametric Search and Design Investigation of Flight Dynamics of a determination of airdata system for Collection Efficiency: An Empirical External Stores for Single Use Autonomous Gliding Analysis Generic Lambda Wing Configuration a modern fighter aircraft Model O. Kapulu, Turkish Aerospace Industries, Air Vehicles A. Da Ronch, University of Southampton, D. Nelson, University of Colorado, Colorado S. Jain, K. C, Y. Yarlagadda, National A. Anttho, A. Mohiudeen, K. Kara, Khalifa Inc., Ankara, Turkey; O. Tekinalp, Middle V. Yavuztürk, E. Topbas, Ü. Kutluay, Southampton, United Kingdom; M. Righi, Springs, Colorado Springs, CO; J. Irving, Aerospace Laboratories, Bengaluru, University, Abu Dhabi, United Arab Emirates East Technical University, Ankara, Turkey TUBITAK, Ankara, Turkey; Y. Yazicioglu, Zürich University of Applied Sciences, BAE Systems, Warton, United Kingdom; M. India; A. Saraf, A. Goyal, Aeronautical Middle East Technical University, Ankara, Winterthur, Switzerland; M. Berci, Ghoreyshi, A. Jirasek, A. Lofthouse, U.S. Air Development Agency, Bengaluru, India Turkey University of Leeds, Leeds, United Kingdom Force Academy, Colorado Springs, CO Friday, 13 January 2017 460-APA-45 Special Session: Simulation of Rotor in Hover III Dallas 2 Chaired by: N. HARIHARAN, CREATE-AV and E. REED, Sikorsky Aircraft 0930 hrs 1000 hrs 1030 hrs AIAA-2017-1870 AIAA-2017-1871 AIAA-2017-1872 Application of Hover Prediction CFD Performance and Turbulence Measured Boundary Layer Methodologies to Anhedral Tip Transition Predictions on an Transition and Rotor Hover Shapes Installed Model-scale Rotor in Hover Performance at Model Scale L. Sankar, Georgia Institute of Technology, R. Jain, U.S. Army Aviation and Missile A. Overmeyer, P. Martin, Army Aviation Atlanta, GA Research Development and Engineering and Missile Research Development and Center, Moffett Field, CA Engineering Center, Hampton, VA Friday, 13 January 2017 461-ASC-6 Modeling, Simulation, and Optimization of Adaptive Structures, Space and Planetary Systems and Subsystems Palomino 3 Chaired by: D. DOYLE, USAF and J. JOO, AFRL/RQVC 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2017-1873 AIAA-2017-1874 AIAA-2017-1875 AIAA-2017-1876 AIAA-2017-1877 AIAA-2017-1878 A Finite Beam Element Framework Computational Modeling of a Modeling and Design of Shape BILL-E: Robotic Platform for Experimental Characterization of Design and Fabrication of a for Variable Stiffness Structures Mechanized Bench-Top Apparatus Memory Alloy-based Origami Locomotion and Manipulation of a Composite Morphing Radiator Composite Morphing Radiator Panel T. Macquart, A. Pirrera, P. Weaver, for Leading-Edge Slat Noise Structures with Smooth Folds Lightweight Space Structures Prototype in a Relevant Thermal Using High Conductivity Fibers University of Bristol, Bristol, United Treatment Device Prototypes E. Peraza Hernandez, D. Hartl, D. B. Jenett, Massachusetts Institute of Environment J. McQuien, C. Bertagne, J. Whitcomb, Kingdom T. Turner, J. Moore, NASA Langley Research Lagoudas, Texas A&M University, College Technology, Cambridge, MA; K. Cheung, NASA C. Bertagne, J. Whitcomb, D. Hartl, Texas A&M D. Hartl, Texas A&M University, College Center, Hampton, VA; D. Long, Analytical Station, TX Ames Research Center, Moffett Field, CA University, College Station, TX; L. Erickson, Station, TX; L. Erickson, NASA Johnson Mechanics Associates, Inc., Hampton, VA NASA Johnson Space Center, Houston, TX Space Center, Houston, TX Friday, 13 January 2017 462-FD-10 Flow Stability Analysis Pecos 4 Chaired by: G. RIGAS, Caltech and S. RAGHUNATH, The University of Queensland 0930 hrs 1000 hrs 1030 hrs AIAA-2017-1879 AIAA-2017-1880 AIAA-2017-1881 Bi-Global Stability Analysis of Secondary Stability Analysis of Stability of wall-bounded fows Compressible Channel Flow over Crossflow Vortices using BiGlobal using one-way spatial integration of Complex Impedance Walls Theory on PIV Base Flows Navier-Stokes equations I. Rahbari, C. Scalo, Purdue University, K. Groot, J. Serpieri, M. Kotsonis, Delft G. Rigas, T. Colonius, California Institute of West Lafayette, IN University of Technology, Delft, The Technology, Pasadena, CA; M. Beyar, The Netherlands; F. Pinna, von Kármán Institute for Boeing Company, Huntington Beach, CA Fluid Dynamics, Rhode-Saint-Genèse, Belgium Friday, 13 January 2017 169 463-FD-60 Control of High Speed Flows Texas 1 Chaired by: N. WEBB, The Ohio State University and C. CLIFFORD, Auburn University 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2017-1882 AIAA-2017-1883 AIAA-2017-1884 AIAA-2017-1885 The Effects of High-Frequency, LES Study on Unsteadiness of Shock Numerical and Experimental High-Speed Flow Mixing Supersonic Microjet Injection on a Boundary Layer Interaction Frequency Response of Plasma Using High-Frequency Pulsed High-Speed Cavity Flow X. Dong, Y. Yang, J. Tang, C. Liu, University Synthetic Jet Actuators Microactuators P. Kreth, University of Tennessee, of Texas, Arlington, Arlington, TX M. Chiatto, L. de Luca, University of Naples J. Solomon, Tuskegee University, Tuskegee, AL Tullahoma, Tullahoma, TN; F. Alvi, Florida “Federico II”, Naples, Italy State University, Tallahassee, FL Friday, 13 January 2017 464-FD-61 Jet Flow Experiments Texas 2 Chaired by: S. SILTON, US Army Research Laboratory and X. LIU, San Diego State University 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2017-1886 AIAA-2017-1887 AIAA-2017-1888 AIAA-2017-1889 AIAA-2017-1890 Simultaneous Planar PIV and sDIC Multi-Measurement Correlations Flow Field Characteristics of An Experimental Study of Time-Resolved Flow Field Measurements of an Axisymmetric in the Near-Field of a Complex Non-Axisymmetric Jets at High Momentum-Driven Unsteady Jets Measurements of Momentum Jet Flowing Across a Compliant Supersoinc Jet Using Time-Resolved Temperatures S. Artham, Z. Zhang, E. Gnanamanickam, Driven Pulsed, Transient Jets Surface Schlieren Imaging R. Vemula, G. Valentich, R. Kumar, Florida Embry-Riddle Aeronautical University, Z. Zhang, D. Seth, S. Artham, J. Leishman, R. Hortensius, J. Dutton, G. Elliott, A. Tenney, T. Coleman, J. Lewalle, M. Glauser, State University, Tallahassee, FL Daytona Beach, FL E. Gnanamanickam, Embry-Riddle University of Illinois, Urbana-Champaign, Syracuse University, Syracuse, NY; S. Gogineni, Aeronautical University, Daytona Beach, FL Urbana, IL Spectral Energies, LLC, Dayton, OH Friday, 13 January 2017 465-FD-62 Multiphase Flows III Texas 3 Chaired by: J. HARTWIG, NASA Glenn Research Center 0930 hrs 1000 hrs AIAA-2017-1891 AIAA-2017-1892 Spray-Wall Interactions Modeling Aerodynamic Breakup and Secondary A. Silva, C. Rodrigues, J. Barata, University Drop Formation for a Liquid Metal of Beira Interior, Covilha, Portugal Column in a Shock-Induced Cross-Flow Y. Chen, E. DeMauro, J. Wagner, Sandia National Laboratories, Albuquerque, NM; M. Arienti, Sandia National Laboratories, Livermore, CA; D. Guildenbecher, P. Farias, Sandia National Laboratories, Albuquerque, NM; et al. Friday, 13 January 2017 466-GNC-29 Verification and Validation of Adaptive Systems III Austin 2 Chaired by: T. YUCELEN, Missouri University of Science & Technology and J. MUSE, AFRL/RQQA 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2017-1893 AIAA-2017-1894 AIAA-2017-1895 AIAA-2017-1896 Sensor Blending with an Application Cost Detectability and Stability of Decentralized Adaptive Stabilization Nonlinear Adaptive Control of to Robust Direct Adaptive Control of Multiple Model-based Adaptive of Large-Scale Active-Passive Quadrotor UAVs with Run-Time a Non-minimum Phase Aircraft Controllers Using Data-Driven Modular Systems Safety Assurance M. Balas, A. Norriega, R. Anderson, Embry- Control Theory B. Gruenwald, E. Arabi, T. Yucelen, University R. Avram, X. Zhang, Wright State Riddle Aeronautical University, Daytona K. Dogan, K. Rajagopal, S. Balakrishnan, of South Florida, Tampa, FL; A. Chakravarthy, University, Dayton, OH; J. Muse, M. Clark, Beach, FL Missouri University of Science and Wichita State University, Wichita, KS; D. Air Force Research Laboratory, Wright- McNeely, S. Balakrishnan, Missouri University Patterson AFB, OH

170 Technology, Rolla, MO of Science and Technology, Rolla, MO Friday, 13 January 2017 467-GNC-30 Entry, Descent and Landing GNC Technology II Austin 4 Chaired by: J. CARSON, NASA Jet Propulsion Laboratory and P. LU, San Diego State University 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2017-1897 AIAA-2017-1898 AIAA-2017-1899 AIAA-2017-1900 AIAA-2017-1901 Synopsis of Precision Landing A Rigid Mid Lift-to-Drag Ratio Automated Re-entry System using Aerocapture Guidance for a Human Application of a Fully Numerical and Hazard Avoidance (PL&HA) Approach to Human Mars Entry, FNPEG Mars Mission Guidance to Mars Aerocapture Capabilities for Space Exploration Descent, and Landing W. Johnson, Intuitive Machines, Inc., K. Webb, P. Lu, Iowa State University, D. Matz, NASA Johnson Space Center, E. Robertson, NASA Johnson Space Center, R. Sostaric, C. Cerimele, E. Robertson, Houston, TX; P. Lu, San Diego State Ames, IA; A. Dwyer Cianciolo, NASA Houston, TX; P. Lu, San Diego State Houston, TX NASA Johnson Space Center, Houston, TX; University, San Diego, CA; S. Stachowiak, Langley Research Center, Hampton, VA University, San Diego, CA; G. Mendeck, J. Garcia, NASA Ames Research Center, NASA Johnson Space Center, Houston, TX R. Sostaric, NASA Johnson Space Center, Moffett Field, CA Houston, TX Friday, 13 January 2017 468-GNC-31 Spacecraft and Launch Estimation and Sensors Grapevine 6 Chaired by: K. BOLLINO, U.S. Air Force and S. STARIN, NASA-Goddard Space Flight Center 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2017-1902 AIAA-2017-1903 AIAA-2017-1904 AIAA-2017-1905 Recursive Inertia Estimation with Prediction of Lunar Reconnaissance Three-Axis Attitude Estimation Using Investigating Cross-Axis Sensitivity Semideﬁnite Programming Orbiter Reaction Wheel Assembly Rate-Integrating Gyroscopes and Misalignment in an Angular Z. Manchester, Harvard University, Angular Momentum Using J. Crassidis, State University of New York, Accelerometer Measurement Unit Cambridge, MA; M. Peck, Cornell Regression Analysis Amherst, NY; F. Markley, NASA Goddard D. Jatiningrum, C. de Visser, M. van Paassen, University, Ithaca, NY R. DeHart, NASA Goddard Space Flight Space Flight Center, Greenbelt, MD Q. Chu, M. Mulder, Delft University of Center, Greenbelt, MD Technology, Delft, The Netherlands Friday, 13 January 2017 469-GNC-32 Emerging Micro Air Vehicle Capabilities Austin 5 Chaired by: H. CHAO, University of Kansas and J. LANGELAAN, Pennsylvania State University 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2017-1907 AIAA-2017-1908 AIAA-2017-1909 AIAA-2017-1910 A Quasi Polar Local Occupancy Grid Dynamic Soaring in Finite-Thickness Control Strategies for Flight in Wake Encounter Simulation and Flight Approach for Vision-based Obstacle Wind Shears: an Asymptotic Extreme Turbulence Validation with UAV Close Formation Avoidance Solution M. Abdulrahim, A. Mohamed, S. Watkins, Flight J. Geng, J. Langelaan, Pennsylvania State G. Bousquet, M. Triantafyllou, J. Slotine, RMIT University, Melbourne, Australia P. Tian, A. He, H. Chao, Z. Zheng, University of University, University Park, PA Massachusetts Institute of Technology, Kansas, Lawrence, Lawrence, KS; Y. Gu, West Cambridge, MA Virginia University, Morgantown, WV Friday, 13 January 2017 470-GNC-33 Aerospace Robotics Austin 6 Chaired by: S. ULRICH, Carleton University and J. SASIADEK, Carleton University 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2017-1911 AIAA-2017-1912 AIAA-2017-1913 AIAA-2017-1914 AIAA-2017-1915 Quadcopter Experimental Experimental Validation of the Curvature Constrained Lyapunov Control of Departure and Approach Fixed Wing Aircraft Perching Evaluation of Nonlinear Dynamic Selective Velocity Obstacle method Vector Field for Stand-off Target Maneuvers of Tiltwing VTOL Aircraft M. Vedantam, S. Keshmiri, G. Garcia, W. Inversion Coupled with Fourier for Autonomous Collision Avoidance Tracking P. Hartmann, M. Schütt, D. Moormann, Huang, University of Kansas, Lawrence, Transform Regression C. Cheung, Y. Jenie, E. Van Kampen, A. Pothen, A. Ratnoo, Indian Institute of RWTH Aachen University, Aachen, Germany Lawrence, KS M. AlAbsi, T. Fields, University of Missouri, Delft University of Technology, Delft, The Science, Bengaluru, India Kansas City, Kansas CIty, MO Netherlands Friday, 13 January 2017 471-GNC-34 Intelligent and Cooperative Control in AE Applications Austin 1

171 Chaired by: I. WEINTRAUB and J. WARNER 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2017-1916 AIAA-2017-1917 AIAA-2017-1918 AIAA-2017-1919 AIAA-2017-1920 AIAA-2017-1921 Autonomous Flightworthiness An Optimal Aircraft Defense Strategy Game Theoretic Trajectory Grid-Free Search and Exploration Machine Learning Approach for Machine Learning for Efficient Determination for Modular Vertical for the Active Target Defense Scenario Negotiation Mechanism for Merging using Modified Cyclic Pursuit Finding Similar Weather-Impacted Sampling-Based Algorithms in Lift Vehicles I. Weintraub, E. Garcia, D. Casbeer, Air Air Traffic Management D. Mukherjee, Technion--Israel Institute of Situations in En Route Airspace Robust Multi-Agent Planning Under J. Warner, J. Rogers, Georgia Institute of Force Research Laboratory, Wright-Patterson S. Park, P. Menon, Optimal Synthesis, Inc., Technology, Haifa, Israel; D. Ghose, Indian S. Schelling, J. Krozel, Innovation Uncertainty Technology, Atlanta, GA AFB, OH; M. Pachter, Air Force Institute of Los Altos, CA Institute of Science, Bengaluru, India Laboratory, Inc., Portland, OR J. Quindlen, J. How, Massachusetts Technology, Wright-Patterson AFB, OH Institute of Technology, Cambridge, MA Friday, 13 January 2017 472-GTE-10 New Engine Architectures II Grapevine 2 Chaired by: M. ATTIA, Embry-Riddle Aeronautical University 0930 hrs 1000 hrs 1030 hrs AIAA-2017-1922 AIAA-2017-1923 AIAA-2017-1924 Development and Application of Cycle Selection and Sizing of a Single- Modeling and Design of a Partially GT-HEAT for the Electrically Variable Aisle Transport with the Electrically Electric Distributed Aircraft Engine(TM) Design Variable Engine(TM) (EVE) for Fleet Propulsion System with GT-HEAT D. Trawick, C. Perullo, Georgia Institute of Level Fuel Optimization J. Gladin, D. Trawick, C. Perullo, J. Tai, D. Technology, Atlanta, GA; M. Armstrong, D. C. Perullo, D. Trawick, Georgia Institute of Mavris, Georgia Institute of Technology, Snyder, Rolls-Royce Group plc, Indianapolis, Technology, Atlanta, GA; M. Armstrong, Atlanta, GA IN; J. Tai, D. Mavris, Georgia Institute of Rolls-Royce Group plc, Indiannapolis, IN; J. Technology, Atlanta, GA Tai, D. Mavris, Georgia Institute of Technology, Atlanta, GA Friday, 13 January 2017 473-GTE-11 Numerical Tools II Grapevine 3 Chaired by: M. RICKLICK, Embry Riddle Aeronautical University 0930 hrs 1000 hrs 1030 hrs AIAA-2017-1925 AIAA-2017-1926 AIAA-2017-1927 Numerical Simulation of Cascade Performance Modeling of Gas Effect of Gradient Reconstruction Flows Using Block-Structured Turbine Engines Using Inverse Method on Transonic Fan Cartesian Mesh Solution Methods Performance M. Koike, Kanazawa Institute of Technology, J. Delimont, C. Nolen, A. McClung, F. Carpenter, P. Cizmas, Texas A&M Hakusan, Japan; D. Sasaki, Kanazawa Institute Southwest Research Institute, San University, College Station, TX of Technology, Kanazawa, Japan; T. Misaka, K. Antonio, TX Shimoyama, S. Obayashi, Tohoku University, Sendai, Japan; K. Hirakawa, IHI Corporation, Nishitama, Japan; et al. Friday, 13 January 2017 474-HSABP-9/PGC-8 Pressure Gain Combustion - Rotating and Pulse Detonation Engines San Antonio 2 Chaired by: S. STANLEY, Aerojet Rocketdyne and T. KAEMMING, Innovative Scientific Solutions Incorporated 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2017-1928 AIAA-2017-1929 AIAA-2017-1930 AIAA-2017-1931 AIAA-2017-1932 AIAA-2017-1933 Experimental Study of the Ignition Study of Shock Wave Transmission Exergy analysis of pulse detonation High-Pressure Rotating Detonation Experimental Study of Liquid Oriented Jet In Crossflow Turbulence Process in Rotating Detonation Engines by Detonation Wave Interaction engine with linear power generator Engine Testing and Flameholding Injector Elements for Use in Generator for Confined Flame M. Fotia, J. Hoke, Innovative Scientific with Contact Discontinuity R. Bello, F. Lu, University of Texas, Analysis with Hydrogen and Natural Rotating Detonation Engines Acceleration in Moving Mixtures Solutions, Inc., Dayton, OH; F. Schauer, Air J. Peace, F. Lu, University of Texas, Arlington, Arlington, TX Gas W. Anderson, D. Lim, S. Heister, Purdue J. Lowe, M. Attia, Embry-Riddle Force Research Laboratory, Wright-Patterson Arlington, Arlington, TX D. Stechmann, S. Heister, S. Sardeshmukh, University, West Lafayette, IN Aeronautical University, Daytona Beach, FL AFB, OH Purdue University, West Lafayette, IN

172 Friday, 13 January 2017 475-MDO-12/NDA-10 Optimization Under Uncertainty II Mustang 1 Chaired by: D. ALLAIRE, Texas A&M University and A. CHAUDHURI, Massachusetts Institute of Technology 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2017-1934 AIAA-2017-1935 AIAA-2017-1936 AIAA-2017-1937 AIAA-2017-1938 AIAA-2017-1939 Design Optimization Under Optimal Approximations of Coupling Multifidelity, Multidisciplinary The relevance of reliability- Robust Aeroelastic Design Stochastic Design Optimization of Uncertainty Using the Multipoint in Multidisciplinary Models Uncertainty Quantification with based topology optimization in Optimization of Hypersonic Vehicle Microstructures with Utilization of a Approximation Method R. Baptista, Y. Marzouk, K. Willcox, Non-Intrusive Polynomial Chaos preliminary phases of aerospace with Uncertainties in Aerodynamic Linear Solver Y. Korolev, V. Toropov, Queen Mary Massachusetts Institute of Technology, T. West, C. Gumbert, NASA Langley structural design Loads, Heat Flux, and Structure P. Acar, S. Srivastava, V. Sundararaghavan, University of London, London, United Cambridge, MA; B. Peherstorfer, University Research Center, Hampton, VA C. Lopez, A. Baldomir, S. Hernandez, Z. Du, Z. Wan, Y. Dai, S. Zhu, C. Yang, University of Michigan, Ann Arbor, Ann Kingdom; S. Shahpar, Rolls-Royce Group of Wisconsin, Madison, Madison, WI University of A Coruña, A Coruña, Spain Beihang University, Beijing, China Arbor, MI plc, Derby, United Kingdom Friday, 13 January 2017 476-MST-18 Modeling and Simulation of Propulsion Systems Ft. Worth 6 Chaired by: S. KOWALCHUK, Sandia National Laboratories 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2017-1940 AIAA-2017-1941 AIAA-2017-1942 AIAA-2017-1943 AIAA-2017-1944 Design of a Transient Variable Cycle Cessna Citation X Engine Model Identification and Validation of the Design and Benchmarking of a Application of Immersed Boundary Turbine Engine Model for System Identification and Validation in Cessna Citation X Engine Component Network-In-the-Loop Simulation for Method with Wall Injection for Solid Integration with Controls the Cruise Regime from Flight Level Modeling with Flight Tests Use in a Hardware-In-the-Loop System Rocket Motor Internal Flow R. Buettner, R. Roberts, M. Wolff, Tests based on Neural Networks P. Bardela, R. Botez, University of Québec, E. Aretskin-Hariton, NASA Glenn Research T. Hirose, S. Ogawa, D. Sasaki, Kanazawa Wright State University, Dayton, OH; A. combined with Extended Great Montréal, Canada Center, Cleveland, OH; G. Thomas, N&R Institute of Technology, Hakusan, Japan; Behbahani, Air Force Research Laboratory, Deluge Algorithm Engineering, Inc., Parma Heights, OH; J. Y. Fukushima, S. Obayashi, Tohoku Wright-Patterson AFB, OH M. Zaag, R. Botez, University of Québec, Kratz, D. Culley, NASA Glenn Research Center, University, Katahira, Japan Montréal, Canada Cleveland, OH Friday, 13 January 2017 477-MVC-5 Solution Adaptive Meshing and Error Estimation Palomino 1 Chaired by: C. OLLIVIER GOOCH, University of British Columbia and W. JONES, NASA-Langley Research Center 0930 hrs 1000 hrs 1030 hrs AIAA-2017-1945 AIAA-2017-1946 AIAA-2017-1947 An Adaptive Conservative ALE Comparison of Anisotropic Mesh A Truncation Error Based Anisotropic Approach to Deal with Large Adaptation for Turbomachinery Flows Mesh Adaptation Metric for CFD Boundary Displacements in Three- G. Vivarelli, N. Qin, University of Sheffield, T. Phillips, C. Ollivier Gooch, University of Dimensional Inviscid Simulations Sheffield, United Kingdom; S. Shahpar, British Columbia, Vancouver, Canada B. Re, A. Guardone, Technical University of Rolls-Royce Group plc, Derby, United Milan, Milan, Italy; C. Dobrzynski, French Kingdom Institute for Research in Computer Science and Control (INRIA), Talence, France Friday, 13 January 2017 478-NDA-11 Uncertainty Quantification II Mustang 2 Chaired by: N. CHENNIMALAI KUMAR, General Electric Global Research Center and P. JOSHI, Heinkel Engineering GmbH 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2017-1948 AIAA-2017-1949 AIAA-2017-1950 AIAA-2017-1951 AIAA-2017-1952 AIAA-2017-1953 Construction of Multi-Fidelity Locally A Model Reification Approach Quantifying the Impact of Different A multifidelity multilevel Monte Uncertainty Analysis of Turbulence Value Driven Optimization in Optimized Surrogate Models for to Fusing Information from Model Discrepancy Formulations in Carlo method for uncertainty Model Closure Coefficients for Wall- an Uncertain Marketplace and Uncertainty Quantification Multifidelity Information Sources Coupled Multidisciplinary Systems propagation in aerospace Bounded Attached and Separated Quantifying Uncertainty with the M. Rumpfkeil, University of Dayton, W. Thomison, D. Allaire, Texas A&M S. Friedman, S. Ghoreishi, D. Allaire, Texas applications Flows Gini Coefficient Dayton, OH; K. Hanazaki, Nagaoka University, College Station, TX A&M University, College Station, TX G. Geraci, Stanford University, Stanford, A. Erb, S. Hosder, Missouri University of M. Wang, H. Kannan, C. Bloebaum, Iowa University of Technology, Niigata, Japan; CA; M. Eldred, Sandia National Science and Technology, Rolla, MO State University, Ames, IA P. Beran, Air Force Research Laboratory, Laboratories, Albuquerque, NM; G.

173 Wright-Patterson AFB, OH Iaccarino, Stanford University, Stanford, CA Friday, 13 January 2017 479-PC-30 Flame Stabilization/Blow Out San Antonio 1 Chaired by: A. CASWELL, USAF AFRL/RQTC and S. SHANBHOGUE 0930 hrs 1000 hrs 1030 hrs AIAA-2017-1954 AIAA-2017-1955 AIAA-2017-1956 Lean Blowout and Ignition Large-Eddy Simulations of Fuel Parametric Study of Alternating Characteristics of Conventional and Effect on Gas Turbine Lean Blow-out Flow Patterns in Non-Reacting Surrogate Fuels Measured in a Swirl L. Esclapez, P. Ma, Stanford University, Multiple-Swirl Flows Stabilized Combustor Stanford, CA; E. Mayhew, University of B. Dolan, R. Villalva Gomez, E. Gutmark, S. Stouffer, T. Hendershott, J. Monfort, Illinois, Urbana-Champaign, Urbana, IL; University of Cincinnati, Cincinnati, OH University of Dayton, Dayton, OH; J. R. Xu, Stanford University, Stanford, CA; Diemer, Innovative Scientific Solutions, S. Stouffer, University of Dayton, Dayton, Inc., Dayton, OH; E. Corporan, P. OH; T. Lee, University of Illinois, Urbana- Wrzesinski, Air Force Research Laboratory, Champaign, Urbana, IL; et al. Wright-Patterson AFB, OH; et al. Friday, 13 January 2017 480-PC-31 Jets in Cross-Flow Austin 3 Chaired by: J. OEFELEIN, Sandia National Laboratories and V. ACHARYA, Georgia Institute of Technology 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2017-1957 AIAA-2017-1958 AIAA-2017-1959 AIAA-2017-1960 AIAA-2017-1961 Digital Holographic Analysis of the Structures and Temporal Evolution Filtered Rayleigh Scattering On the Ignition and the Combustion of Effect of orifice geometry on spray Breakup of Aerated Liquid Jets in of Liquid Jets in Supersonic Measurements of Liquid Nitrogen Supercritical Fuel Jet-In-Cross-Flow characteristics of liquid jet in cross Supersonic Crossflow Crossflow Jets in Subcritical and Supercritical K. Gottiparthi, R. Sankaran, Oak Ridge flow K. Sallam, Oklahoma State University, K. Lin, Taitech, Inc., Beavercreek, OH; M. Crossflows National Laboratory, Oak Ridge, TN; J. Y. Song, D. Hwang, K. Ahn, Chungbuk Stillwater, OK; K. Lin, Taitech, Inc., Lai, Wayne State University, Detroit, MI; A. Cross, General Electric Company, Oefelein, Sandia National Laboratories, National University, Cheongju, South Korea Beavercreek, OH; S. Hammack, C. Carter, T. Ombrello, C. Carter, Air Force Research Niskayuna, NY; J. Estevadeordal, North Livermore, CA Air Force Research Laboratory, Wright- Laboratory, Wright-Patterson AFB, OH Dakota State University, Fargo, ND; M. Patterson AFB, OH Masquelet, K. McManus, General Electric Company, Niskayuna, NY Friday, 13 January 2017 481-PC-32 Laminar Flames II San Antonio 3 Chaired by: D. GLAZE, Sandia National Laboratories and Y. JU, Princeton University 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2017-1962 AIAA-2017-1963 AIAA-2017-1964 AIAA-2017-1965 Laminar Flame Speeds of Dilute Effects of n-Alkane Chain Length on Effect of “prompt” dissociation of The effect of radiation on the

Triethyl Phosphate in H 2- and CH Cool Diffusion Flames formyl radical on high temperature dynamics of near limit cool flames C. Reuter, M. Lee, S. Won, Y. Ju, Princeton 4-Air Mixtures oxidation of formaldehyde in the and hot flames T. Sikes, N. Niemiec, W. Kulatilaka, E. University, Princeton, NJ study of 1,3,5-trioxane pressurized Y. Ju, Princeton University, Princeton, NJ; Petersen, Texas A&M University, College laminar flame speeds E. Lin, Princeton High School, Princeton, Station, TX H. Zhao, J. Fu, Y. Ju, Princeton University, NJ; C. Reuter, Princeton University,

174 Princeton, NJ Princeton, NJ Friday, 13 January 2017 482-PC-33 Combustor Advances Enabled by Advanced Manufacturing Grapevine 1 0930 - 1130 hrs Panelists: Andrew Ihnen Lance Smith Jeffrey Haynes Jean-Francois Rideau Naval Air Warfare Center UTRC Aerojet Rocketdyne Microturbo Safran

Friday, 13 January 2017 483-PC-34 Model Validation for Propulsion Workshop: Closing Session Palomino 2 0930 - 1230 hrs The Model Validation for Propulsion (MVP) workshop is an open forum, bringing together researchers and modelers to help improve our understanding and capabilities of modeling turbulent reacting flows in relevant aerospace propulsion systems. This session includes a panel discussion on Best Practices in Reacting Large Eddy Simulations and closes with an opportunity for participants to provide feedback for future workshop forums. Friday, 13 January 2017 484-PDL-14 Plasma and Laser Physics II Ft. Worth 5 Chaired by: J. ZIMMERMAN, CU Aerospace and M. PANESI, University of Illinois at Urbana Champaign 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs 1230 hrs AIAA-2017-1966 AIAA-2017-1967 AIAA-2017-1968 AIAA-2017-1969 AIAA-2017-1970 AIAA-2017-1971 AIAA-2017-1972 Numerical simulation of dissociation Progress in Development of a Experimental and Numerical Laser Induced “Counter” Convection Computational Studies of Positive Experiments on a Plasma-based Modeling of Dual-Pulse Laser kinetics in the Penning discharge Chemical CO Laser Driven by a Investigations of a Pulsed in Water and Negative Streamers in Bubbles Metamaterial at Microwave Ignition plasma using 2D modified drift- Chemical Reaction between Carbon Nanosecond Streamer Discharge M. Shneider, Princeton University, Suspended in Distilled Water Fequencies A. Tropina, Kharkiv National University, diffusion model Vapor and Oxygen in CO2 Princeton, NJ; V. Semak, Virtual Laser A. Sharma, D. Levko, L. Raja, University of E. Matlis, A. Hoffman, T. Corke, University Kharkiv, Ukraine; M. Shneider, R. Miles, S. Surzhikov, Russian Academy of E. Jans, K. Frederickson, M. Yurkovich, Z. M. Pachuilo, D. Levko, L. Raja, P. Varghese, Application Design, State College, PA Texas, Austin, Austin, TX of Notre Dame, Notre Dame, IN Princeton University, Princeton, NJ Sciences, Moscow, Russia; D. Storozhev, Eckert, J. Rich, I. Adamovich, Ohio State University of Texas, Austin, Austin, TX All-Russian Scientific Research Institute of University, Columbus, OH Automatics, Moscow, Russia Friday, 13 January 2017 485-PDL-15 Plasma Assisted Combustion and Ignition II Ft. Worth 4 Chaired by: A. STARIKOVSKIY, Princeton University and S. BANE, Purdue University- Sch of Aero and Astro 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2017-1973 AIAA-2017-1974 AIAA-2017-1975 AIAA-2017-1976 AIAA-2017-1977 Proper Orthogonal Decomposition Volumetric Plasma Discharge in a First experiments on plasma Laser Ignition of Propane-Air Mechanism of Plasma-Assisted for Flame Dynamics of Microwave Coaxial Electrode Configuration Using assisted supersonic combustion at Mixtures Using a Dual-Pulse Ignition for H2 and C1-C5 Plasma Assisted Swirl Stabilized Repetitively Pulsed Nanosecond LAERTE facility Technique Hydrocarbons Premixed flames Discharges A. Vincent-Randonnier, ONERA, Palaiseau, C. Dumitrache, R. VanOsdol, C. Limbach, A. Starikovskiy, Princeton University, R. Rajasegar, C. Mitsingas, E. Mayhew, R. Jagannath, K. Newnam, P. Stockett, P. Wu, France; S. Leonov, University of Notre A. Yalin, Colorado State University, Fort Princeton, NJ T. Lee, University of Illinois, Urbana- S. Bane, Purdue University, West Lafayette, IN; Dame, Notre Dame, IN; D. Packan, ONERA, Collins, CO Champaign, Urbana, IL; J. Yoo, State M. Nalim, Indiana University-Purdue University Palaiseau, France University of New York, Buffalo, NY Indianapolis, Indianapolis, IN Friday, 13 January 2017 486-SD-25 Active/Passive Vibration Control, Isolation, Stability Augmentation, Damping Appaloosa 3 Chaired by: W. WELSH, Sikorsky Aircraft Corporation and S. LIGUORE, Boeing Engineering Operations & Technology 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2017-1978 AIAA-2017-1979 AIAA-2017-1980 AIAA-2017-1981 AIAA-2017-1982 AIAA-2017-1983 Vibration Theory for Damping Modeling and Analysis of Damping Transient Analysis of Anti-symmetric Lattice-based Discrete Structure Multi-fidelity Modeling of Interfacial Characteristics and control of base- Control of 2D-deployable Linked Performance of Hard Coatings in Cross-Ply and Angle-Ply Laminated Modeling and Control for Large Micromechanics for Off-Aligned excited dynamical system through a Panel Structures in Space Turbomachinery Composite Plates Using Nurbs-Based Flexible Space Structure Applications Polymer/Carbon Nanotube vibration absorber energy harvester M. Takatsuka, Nagoya University, Nagoya, M. Tidball, J. Slater, Wright State Isogeometric Analysis N. Cramer, University of California, Santa Cruz, Nanocomposites H. Abdelmoula, New Mexico State Japan University, Dayton, OH; J. Brown, B. A. Gupta, A. Ghosh, Indian Institute of Santa Cruz, CA; S. Swei, K. Cheung, NASA R. Kopp, Pennsylvania State University, University, Las Cruces, NM; H. Dai, Langley, T. George, Air Force Research Technology Kharagpur, Kharagpur, India Ames Research Center, Moffett Field, CA; University Park, PA; B. Glaz, F. Gardea, Huazhong University of Science and Laboratory, Wright-Patterson AFB, OH D. Cellucci, Cornell University, Ithaca, NY; B. Army Research Laboratory, Aberdeen Technology, Wuhan, China; A. Abdelkefi,

175 Jenett, Massachusetts Institute of Technology, Proving Ground, MD; E. Smith, New Mexico State University, Las Cruces, Cambridge, MA; M. Teodorescu, University of Pennsylvania State University, University NM; L. Wang, Huazhong University of California, Santa Cruz, Santa Cruz, CA Park, PA Science and Technology, Wuhan, China Friday, 13 January 2017 487-SD-26 Structural Dynamic Modeling of Beams, Cables, Membranes, Plates and Shells Appaloosa 4 Chaired by: J. KOSMATKA, University of California, San Diego and J. SLATER, Wright State University 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2017-1984 AIAA-2017-1985 AIAA-2017-1986 AIAA-2017-1987 AIAA-2017-1988 Dynamic analysis of the continuous Random Eigenvalue Analysis for the Geometrically-exact, fully intrinsic Vibration of Long Rectangular An Investigation of Factors Affecting fluid-structure system based on Free Vibration of Rotating Beams analysis of pretwisted beams under Composite Plates and Buckling of such Vibration Comfort of Quayside Timoshenko model and considering Using Inverse Problem Approach distributed follower forces Plates under Shear and Axial loads Crane Cab damping K. Sarkar, R. Ganguli, D. Ghosh, Indian P. Mardanpour, E. Izadpanahi, S. Rastkar, H. Eslami, Embry-Riddle Aeronautical W. Li, Y. Li, H. Wang, L. Zhao, Shanghai X. Zhang, M. Zhu, H. Liang, Beihang Institute of Science, Bengaluru, India Florida International University, Miami, FL; University, Daytona Beach, FL; N. Khalili, Zhenhua Heavy Industry Company, Ltd., University, Beijing, China S. Fazelzadeh, Shiraz University, Shiraz, Gulfstream Aerospace Corporation, Shanghai, China Iran; D. Hodges, Georgia Institute of Savannah, GA; U. Gandi, Embry-Riddle Technology, Atlanta, GA Aeronautical University, Daytona Beach, FL Friday, 13 January 2017 488-STR-12 Failure Analysis and Prediction Appaloosa 1 Chaired by: S. DORMOHAMMADI, AlphaSTAR Corp. and G. MABSON, Boeing Engineering Operations & Technology 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2017-1989 AIAA-2017-1990 AIAA-2017-1991 AIAA-2017-1992 Numerical Investigation of Longer Stochastic multiscale approach Modeling of Bird Strike to a Micromechanics-Based Fatigue Life Life Combustion Chambers of Liquid to predict failure initiation and Composite Helicopter Rotor Blade Prediction of Composites Rocket Engines Based on Coupled progression in composite materials Z. Eren, S. Tataroglu, D. Balkan, Z. S. Arnold, P. Murthy, B. Bednarcyk, E. Thermal-fluid-structure Simulation S. Sanei, E. Barsotti, R. Fertig, University Mecitoglu, Istanbul Technical University, Pineda, NASA Glenn Research Center, H. Amakawa, H. Negishi, M. Nishimoto, S. of Wyoming, Laramie, Laramie, WY Istanbul, Turkey Cleveland, OH; S. Mital, University of Hori, Japan Aerospace Exploration Agency Toledo, Toledo, OH; P. Naghipour, Ohio (JAXA), Tsukuba, Japan Aerospace Institute, Brook Park, OH Friday, 13 January 2017 489-TES-4 Emerging Energy Technologies II Mustang 3 Chaired by: A. AGRAWAL, The University of Alabama and N. LOVE, The University of Texas El Paso 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2017-1993 AIAA-2017-1994 AIAA-2017-1995 AIAA-2017-1996 AIAA-2017-1997 Numerical Analysis of Air Thermal Comfort Analyses in Temperature Distributions in an Simulation of Air Flow Pattern Embedded Void Approach for Distribution Systems in Aircraft Naturally Ventilated Handball Arena Underground Road Tunnel: Effect of in a Room with Ceiling Mounted Nitride Based Multi-Junction passengers’ Cabins Utilizing CFD Techniques Car fire Heat Release Circulator Photovoltaic Cells E. Khalil, R. AbdelMaksoud, W. E. Khalil, A. Masoud, A. Ibrahim, E. ElBialy, W. Sweda, E. Khalil, O. Huzzayyin, Cairo E. Khalil, A. ElDegwy, Cairo University, S. Salah, T. Hatem, British University in AbdelMaksoud, A. Fahim, Cairo University, Cairo University, Cairo, Egypt University, Cairo, Egypt Cairo, Egypt Cairo, Cairo, Egypt; E. Khalil, Cairo University, Cairo, Egypt Cairo, Egypt; S. Bedair, North Carolina State University, Raleigh, NC; W. AbdelMaksoud, Cairo University, Cairo, Egypt Friday, 13 January 2017 490-WE-11 Computational Methods for Wind Turbine Aerodynamics Dallas 7 Chaired by: D. MANIACI, Sandia National Laboratories and J. SITARAMAN, University of WY 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2017-1998 AIAA-2017-1999 AIAA-2017-2000 AIAA-2017-2001 AIAA-2017-2002 AIAA-2017-2003 An Advanced Actuator Line Method Improving Airfoil Lift Prediction A Computationally-Efficient Panel Fast Multilevel Panel Method Development of a Partially Unsteady Interacting Boundary for Wind Energy Applications and G. Ramanujam, H. Ozdemir, Energy Code for Unsteady Airfoil Modelling for Wind Turbine Rotor Flow Stochastic Unsteady Aerodynamics Layer Method Beyond Research Center of the Netherlands, Petten, Including Dynamic Stall Simulations Model H. Ozdemir, Energy Research Center of the M. Churchfield, S. Schreck, National The Netherlands A. Gonzalez-Salcedo, M. Aparicio-Sanchez, A. van Garrel, C. Venner, H. Hoeijmakers, M. Lennie, J. Wendler, G. Pechlivanoglou, Netherlands, Petten, The Netherlands; A. Renewable Energy Laboratory, Golden, CO; X. Munduate, CENER, Sarriguren, Spain; University of Twente, Enschede, The C. Nayeri, C. Paschereit, Technical van Garrel, University of Twente, Enschede, L. Martinez, C. Meneveau, Johns Hopkins R. Palacios, J. Graham, Imperial College Netherlands University of Berlin, Berlin, Germany; D. The Netherlands; A. Koodly Ravishankara, University, Baltimore, MD; P. Spalart, The London, London, United Kingdom; O. Pires, Greenblatt, Technion--Israel Institute of Purdue University, West Lafayette, IN; F. Boeing Company, Seattle, WA CENER, Sarriguren, Spain; et al. Technology, Haifa, Israel Passalacqua, Technical University of Milan, 176 Milan, Italy; H. Seubers, Delft University of Technology, Delft, The Netherlands

Author/Session Chair Index A, V., 370-GNC-19 Abdullah, M., 79-FD-13 Acikmese, B., 368-GNC-17 Agate, M., 250-FD-36 Aigner, M., 436-PC-26 A., A., 252-FD-38 Abdul-Latif, A., 79-FD-13 Ackerman, K., 307-GNC-10 Aggarwal, P., 218-STR-7 Akcal, U., 382-MST-12 Abbas, Z., 67-APA-6 Abdullin, A., 166-TP-5 Acosta-Zamora, A., 446-TES-2 Agrawal, A., 489-TES-4 Akella, M., 377-HSABP-7 Abbasi, M., 206-PC-16 Abdulrahim, M., 291-AFM-6, 469-GNC-32 Action, J., 27-GEPC-1 Agrawal, B., 119-AA-4 Akhtar, I., 26-FD-7 Abbud-Madrid, A., 164-SRE-3 Abercromby, A., 357-EXPL-1 Adamovich, I., 327-PDL-8, 388-PDL-11, 441-PDL-13, Agricola, L., 191-FD-30, 416-FD-55 Akhtar, S., 169-UMS-5, 347-AFM-8 Abdel-Galil, M., 263-IS-4 Abernathy, D., 19-DA-1, 351-APA-34 484-PDL-14 Ahmed, A., 191-FD-30, 364-FD-51 Akiki, M., 152-PC-10 Abdel Hameed, O., 294-APA-29 Abnous, R., 264-MDO-7 Adams, L., 46-SCS-1 Ahmed, K., 94-PC-5/PGC-2, 130-DE-2, 152-PC-10, Akita, D., 275-SCS-4 Abdelkeﬁ, A., 17-ASC-1, 62-ACD-4, 72-ASC-2, 89-MAT-2, Aboud, J., 393-TES-1 Adams, V., 256-GNC-4 435-PC-25, 438-PC-28 Akkari, N., 250-FD-36 128-APA-14, 147-MST-1, 158-SD-7, 182-ASC-3, AbouDeif, T., 447-TES-3 Aditya, R., 315-ICC-1 Ahmed, M., 294-APA-29 Akkerman, S., 109-TP-4 197-MAT-5, 217-STR-6, 264-MDO-7, 486-SD-25 Abrahamson, J., 436-PC-26 Adler, M., 247-FD-33 Ahmed, N., 86-IS-1, 196-IS-3, 309-GNC-12 Akram, F., 67-APA-6, 243-DE-3 Abdellatif, O., 447-TES-3 Abramova, K., 125-APA-11 Adolf, F., 104-SOF-2, 316-IS-5, 428-IS-9 Ahn, K., 480-PC-31 Aksu, T., 142-HSABP-3 AbdelMaksoud, R., 489-TES-4 Abras, J., 354-APA-37 Adowski, T., 55-TP-1 Ahn, S., 387-PDL-10, 440-PDL-12 AlAbsi, M., 175-AFM-4, 470-GNC-33 AbdelMaksoud, W., 489-TES-4 Abrashkin, V., 261-GTE-6 Adusumilli, S., 11-AMT-1 Ahrabi, B., 76-FD-9 Alan, A., 31-HSABP-1 Abdelmoula, H., 72-ASC-2, 147-MST-1, 158-SD-7, Acar, P., 202-NDA-4, 475-MDO-12/NDA-10 Aftosmis, M., 136-FD-18 Ahsun, U., 67-APA-6 Alauzet, F., 69-APA-8/AA-3, 149-MVC-3 182-ASC-3, 197-MAT-5, 486-SD-25 Accardo, D., 58-UMS-1, 162-SEN-1, 215-SEN-2, Agamawi, Y., 369-GNC-18 Ahuja, K., 7-AA-1, 119-AA-4 Albertani, R., 286-WE-6 Abdi, F., 174-ACD-6 279-SEN-3 Agarwal, R., 69-APA-8/AA-3, 77-FD-11, 246-FD-32, Ahuja, V., 61-ACD-3, 352-APA-35 Alberti, A., 274-PDL-7 Abdol-Hamid, K., 241-APA-24 Acharya, S., 220-TP-8 249-FD-35, 282-TP-9, 304-FD-45, 353-APA-36, Ahumada, A., 269-NDA-6 Albertson, N., 106-STR-3 Abdou, E., 73-EDU-2/DE-1 Acharya, V., 480-PC-31 362-FD-49, 405-APA-39, 407-APA-41, 443-SD-23 Ai, Q., 17-ASC-1 Albisser, M., 347-AFM-8 Author/Session Chair Index Albring, T., 37-MDO-1, 211-SD-10 Anderson, W., 23-FD-3, 95-PC-6, 326-PC-20, Ashby, R., 313-GTE-7 Baldwin, E., 204-PC-14 Barut, A., 165-STR-5, 280-STR-8 Aldemir, T., 104-SOF-2, 216-SOF-4, 222-UMS-7 385-PC-22, 474-HSABP-9/PGC-8 Asher, I., 318-MAT-6, 384-NDA-8 Balkan, D., 488-STR-12 Baruzzi, G., 24-FD-4, 76-FD-9 Aldén, M., 434-PC-24 Andersson, N., 134-FD-16, 288-AA-8 Ashkharian, N., 34-ISC-3 Ball, D., 214-SE-2 Basagaoglu, H., 299-FD-39 Aldujaly, H., 76-FD-9 Andino, M., 78-FD-12 Aslan, S., 124-AMT-7/GT-3 Ball, Z., 284-UMS-9 Basu, S., 170-WE-2 Alexander, W., 119-AA-4, 288-AA-8 Andrienko, D., 166-TP-5 Atinault, O., 241-APA-24 Balta, M., 130-DE-2 Bathel, B., 349-AMT-13 Alexeenko, A., 448-TP-12 Andrus, I., 195-HSABP-4/PGC-3 Atkins, E., 58-UMS-1, 104-SOF-2, 163-SOF-3, Banavara, N., 444-SD-24 Batini, C., 393-TES-1 Alexeev, T., 10-AFM-1 Anemaat, W., 120-ACD-5, 174-ACD-6, 180-APA-19 335-UMS-10, 371-GNC-20 Bandaru, P., 324-NDA-7 Batlle, E., 387-PDL-10, 440-PDL-12 Alfano, M., 217-STR-6 Angrisani, L., 58-UMS-1 Atler, D., 348-AMT-12 Bane, S., 64-AMT-3, 94-PC-5/PGC-2, 99-PDL-2, Battelle, R., 427-GTE-9/PGC-6 Alhajeri, H., 252-FD-38 Anjaly, P., 306-GNC-9 Attia, M., 472-GTE-10, 474-HSABP-9/PGC-8 387-PDL-10, 427-GTE-9/PGC-6, 440-PDL-12, Baturin, O., 29-GTE-1 Alhubail, M., 299-FD-39 Annaswamy, A., 421-GNC-23 Attili, A., 153-PC-11 485-PDL-15 Bauchau, O., 410-APA-44/FD-53 Ali, M., 141-GTE-3 Annoni, J., 111-WE-1 Aubry, R., 92-MVC-2 Banerjee, A., 310-GNC-13 Bauer, K., 79-FD-13 Ali, Z., 22-FD-2 Ansell, P., 128-APA-14, 250-FD-36 Aubuchon, V., 347-AFM-8 Bang, H., 196-IS-3 Bauer, S., 412-EXPL-2 Alimohammadi, S., 37-MDO-1 Anthony, R., 314-HSABP-6/PGC-5 Audier, P., 99-PDL-2 Bangalore Venkatesh, P., 94-PC-5/PGC-2 Baum, J., 23-FD-3 Al-jiboory, A., 442-SD-22 Anttho, A., 459-AFM-12 Ausserer, J., 98-PC-9 Bangert, L., 69-APA-8/AA-3 Bauman, P., 55-TP-1 Alkhafaji, A., 446-TES-2 Anwar, H., 304-FD-45 Austin, R., 269-NDA-6 Banik, J., 46-SCS-1, 329-SCS-5 Baurle, R., 300-FD-41, 377-HSABP-7 Alkhalidi, A., 446-TES-2 Aogaki, T., 296-APA-31 Avallone, F., 288-AA-8, 336-WE-8 Banks, J., 235-AA-7 Bauwens, L., 271-PC-18 Allaire, D., 320-MDO-9, 475-MDO-12/NDA-10, Aoki, T., 329-SCS-5 Avery, A., 335-UMS-10 Banuelos, J., 221-UMS-6 Baxevanis, T., 182-ASC-3, 411-ASC-4 478-NDA-11 Aono, H., 26-FD-7, 80-FD-14 Avram, R., 466-GNC-29 Bañuelos, L., 140-GT-4 Bayandor, J., 48-SD-2 Allen, C., 13-APA-1, 91-MDO-3, 149-MVC-3, 350-APA-33 Aoyama, T., 127-APA-13, 241-APA-24 Avsar, A., 182-ASC-3 Banuti, D., 40-PC-2, 271-PC-18 Baydar, E., 344-ABPSI-1 Allen, J., 242-APA-26 Aparicio-Sanchez, M., 490-WE-11 Azevedo, J., 127-APA-13, 185-FD-24, 408-APA-42 Bao, Y., 213-SD-12 Bays, L., 8-ACD-1 Allen, L., 108-TP-3 Aponso, B., 267-MST-7, 403-AFM-10 Azzazi, A., 447-TES-3 Baptista, R., 475-MDO-12/NDA-10 Bear, P., 29-GTE-1 Allen, M., 33-ISC-2, 331-SD-17 Aquino, W., 324-NDA-7 Babcock, D., 241-APA-24 Barad, K., 44-SATS-1, 45-SATS-2, 156-SATS-4, Beard, B., 269-NDA-6 Allison, D., 198-MDO-6 Arabi, E., 168-UMS-4, 421-GNC-23, 466-GNC-29 Babinsky, H., 80-FD-14, 247-FD-33, 355-APA-38 209-SATS-5 Beard, J., 345-ACD-8 Allison, P., 96-PC-7, 326-PC-20, 385-PC-22 Arabshahi, A., 299-FD-39 Babuska, V., 159-SD-8 Barak, S., 438-PC-28 Beard, S., 265-MST-5, 381-MST-11, 431-MST-16

177 Allmaras, S., 71-APA-10, 302-FD-43 Arad, E., 138-FD-20, 416-FD-55 Baccarella, D., 28-GT-1, 85-HSABP-2 Barakos, G., 409-APA-43 Bearden, W., 65-AMT-4 Al Masoud, N., 205-PC-15 Araki, T., 271-PC-18 Bachelder, E., 403-AFM-10 Baranski, J., 98-PC-9 Beasley, D., 210-SCS-3 Almeida, E., 368-GNC-17 Araujo-Estrada, S., 366-GNC-15 Bäckström, E., 61-ACD-3 Barari, G., 154-PC-12 Beck, J., 211-SD-10, 391-SD-21 Al-Naggar, A., 263-IS-4 Arena, A., 291-AFM-6 Badhan, A., 393-TES-1 Barata, J., 335-UMS-10, 408-APA-42, 465-FD-62 Bedair, S., 489-TES-4 Alonso, J., 37-MDO-1, 61-ACD-3, 93-NDA-1, 120-ACD-5, Aretskin-Hariton, E., 476-MST-18 Bae, H., 93-NDA-1, 151-NDA-3 Barazanchy, D., 218-STR-7 Bedick, C., 195-HSABP-4/PGC-3, 262-HSABP-5/PGC-4 198-MDO-6, 211-SD-10, 290-ACD-7, 324-NDA-7, Argentiero, M., 325-OPS-1 Bae, S., 151-NDA-3 Barbeau, Z., 240-APA-23/FD-31 Bednarcyk, B., 53-STR-2, 488-STR-12 353-APA-36, 429-MDO-11 Argrow, B., 121-AFM-3, 162-SEN-1 Baeder, J., 292-APA-27, 409-APA-43 Barbor, K., 426-GNC-28 Behbahani, A., 476-MST-18 Alon Tzezana, G., 139-FD-22 Arican, E., 376-GTE-8 Baerny, J., 260-GT-6/AMT-10 Barbour, E., 270-PC-17, 439-PC-29 Behdinan, K., 252-FD-38 Altman, A., 361-FD-48, 419-FD-58 Arieli, R., 249-FD-35 Baevsky, R., 269-NDA-6 Barbu, I., 17-ASC-1 Beifuss, U., 83-GT-11 Alvi, F., 247-FD-33, 404-AMT-14, 463-FD-60 Arienti, M., 465-FD-62 Bagarello, N., 412-EXPL-2 Bardela, P., 476-MST-18 Bel, H., 257-GNC-5 Aly, A., 257-GNC-5 Ariff, O., 284-UMS-9, 335-UMS-10 Bai, X., 19-DA-1 Barkley, S., 205-PC-15 Belan, M., 99-PDL-2 Alyanak, E., 37-MDO-1 Arikan, K., 128-APA-14 Bai, Z., 133-FD-15 Barnard, C., 123-AMT-6 Bell, D., 154-PC-12 Amadori, K., 61-ACD-3 Armanini, S., 148-MST-2, 402-AFM-9 Baier, F., 7-AA-1, 235-AA-7 Barnes, C., 77-FD-11, 101-SD-4/APA-47, 158-SD-7, Bell, J., 260-GT-6/AMT-10 Amakawa, H., 488-STR-12 Armstrong, M., 472-GTE-10 Baines, A., 243-DE-3 251-FD-37 Bellan, J., 206-PC-16, 271-PC-18 Amano, R., 446-TES-2, 447-TES-3 Arnett, T., 279-SEN-3, 433-NDA-9 Baker, M., 146-MDO-4, 443-SD-23 Barone, M., 188-FD-27, 304-FD-45 Bello, R., 195-HSABP-4/PGC-3, 474-HSABP-9/PGC-8 Amaya, M., 312-GT-7/AMT-11 Arnold, B., 336-WE-8 Baker, T., 164-SRE-3 Barral, X., 10-AFM-1 Belt, S., 222-UMS-7 Ambo, K., 408-APA-42 Arnold, E., 345-ACD-8 Baker, W., 15-APA-3 Barrett, R., 457-ACD-11 Belter, D., 192-GT-5 Ameri, A., 191-FD-30, 376-GTE-8, 416-FD-55 Arnold, S., 89-MAT-2, 488-STR-12 Bakhle, I., 54-TFPC-1 Barrett-Gonzalez, R., 9-ACD-2, 31-HSABP-1, Ben, C., 221-UMS-6 Amin, S., 263-IS-4 Arora, N., 247-FD-33, 404-AMT-14 Bakker, T., 18-CMS-1, 140-GT-4, 426-GNC-28 62-ACD-4, 377-HSABP-7 Benard, E., 146-MDO-4, 402-AFM-9 Amitay, M., 336-WE-8, 359-FD-46 Arrieta, A., 72-ASC-2 Bakula, C., 243-DE-3 Barsotti, E., 488-STR-12 Benard, N., 99-PDL-2, 327-PDL-8, 387-PDL-10 Amzajerdian, F., 368-GNC-17 Arshad, S., 153-PC-11 Balabanov, V., 320-MDO-9 Barsotti, R., 315-ICC-1 Ben-Asher, J., 425-GNC-27 An, X., 303-FD-44 Arshed, G., 355-APA-38 Balachandar, S., 362-FD-49, 379-MAT-8 Bartholomew, J., 162-SEN-1 Benassi, M., 457-ACD-11 Anand, M., 95-PC-6 Artham, S., 464-FD-61 Balajiwale, S., 258-GNC-6 Bartkowicz, T., 212-SD-11, 330-SD-16 Ben Ayed, S., 72-ASC-2 Anand, V., 195-HSABP-4/PGC-3 Arunajatesan, S., 119-AA-4, 122-AMT-5, 234-AA-6 Balakrishnan, S., 466-GNC-29 Bartoli, N., 146-MDO-4 Benchergui, D., 61-ACD-3 Anderson, B., 148-MST-2 Arya, H., 258-GNC-6 Balakumar, P., 249-FD-35 Barton, D., 276-SD-13 Benedict, M., 32-ISC-1, 33-ISC-2 Anderson, E., 410-APA-44/FD-53 Asada, H., 185-FD-24 Balas, M., 263-IS-4, 315-ICC-1, 369-GNC-18, Bartow, B., 124-AMT-7/GT-3, 192-GT-5 Benek, J., 22-FD-2, 293-APA-28, 406-APA-40 Anderson, M., 284-UMS-9, 457-ACD-11 Asahara, M., 303-FD-44 373-GNC-22, 422-GNC-24, 466-GNC-29 Bartram, G., 433-NDA-9 Benhidjeb-Carayon, A., 204-PC-14 Anderson, R., 54-TFPC-1, 466-GNC-29 Asai, K., 139-FD-22 Baldomir, A., 390-SD-20, 475-MDO-12/NDA-10 Bartram, S., 11-AMT-1 Ben Miled, Z., 214-SE-2 Author/Session Chair Index Bennett, W., 86-IS-1 Bil, C., 17-ASC-1, 400-ACD-9, 457-ACD-11 Borgmann, D., 359-FD-46 Breviglieri, C., 185-FD-24 Burkhalter, J., 61-ACD-3 Bennewitz, J., 326-PC-20 Bilinsky, H., 15-APA-3 Boris, J., 299-FD-39, 363-FD-50 Brezillon, J., 120-ACD-5 Burklund, M., 409-APA-43 Benoit, T., 160-SD-9 Bin, G., 213-SD-12 Borissov, S., 216-SOF-4 Brian, G., 417-FD-56 Burleigh, S., 325-OPS-1 Ben Salah, N., 76-FD-9 Birhane, Y., 56-TP-2 Borner, A., 448-TP-12 Briceno, S., 214-SE-2, 400-ACD-9 Burns, G., 374-GT-8 Benson, K., 131-EDU-3 Bisagni, C., 52-STR-1, 217-STR-6 Borst, C., 317-IS-6 Bridges, J., 119-AA-4, 173-AA-5 Burns, R., 11-AMT-1, 83-GT-11 Benson, M., 408-APA-42 Bisek, N., 134-FD-16, 137-FD-19, 300-FD-41, Bortolotti, P., 449-WE-10 Briggs, H., 48-SD-2, 73-EDU-2/DE-1 Burnside, N., 312-GT-7/AMT-11, 348-AMT-12 Beran, P., 38-MDO-2, 268-NDA-5, 319-MDO-8, 365-FD-52 Boschitsch, A., 16-APA-4 Brinkmeyer, A., 46-SCS-1 Burra, K., 393-TES-1 320-MDO-9, 356-ASC-5, 478-NDA-11 Bisetti, F., 153-PC-11 Bose, S., 300-FD-41 Briones, A., 194-GTE-5 Burrows, T., 360-FD-47 Berci, M., 459-AFM-12 Bish, E., 49-SD-3 Boskovic, J., 169-UMS-5, 222-UMS-7, 389-SD-19 Brizzolara, S., 324-NDA-7 Butler, K., 192-GT-5 Berdoyes, M., 90-MAT-3 Biswell, B., 253-GNC-1 Bosne, M., 236-AFM-5 Broadbent, D., 351-APA-34 Buttsworth, D., 66-APA-5 Beresh, S., 11-AMT-1, 122-AMT-5, 362-FD-49, Black, J., 44-SATS-1, 100-SATS-3, 157-SCS-2 Botero, E., 61-ACD-3 Brock, J., 355-APA-38 Byerley, A., 288-AA-8 364-FD-51 Blades, E., 49-SD-3, 213-SD-12 Botez, R., 17-ASC-1, 148-MST-2, 200-MST-4, Broderick, D., 73-EDU-2/DE-1 Byon, E., 170-WE-2 Beretta, J., 443-SD-23 Blandino, J., 44-SATS-1 236-AFM-5, 306-GNC-9, 353-APA-36, 476-MST-18 Brodersen, O., 295-APA-30 Byun, G., 417-FD-56 Bergan, A., 165-STR-5 Blantin, J., 98-PC-9 Bottasso, C., 449-WE-10 Broglia, R., 406-APA-40 Byun, Y., 134-FD-16 Berger, A., 75-FD-8 Blasques, J., 449-WE-10 Bouadi, H., 423-GNC-25 Bronz, M., 175-AFM-4 C, K., 459-AFM-12 Berger, M., 136-FD-18 Blechschmidt, M., 79-FD-13 Boucher, M., 175-AFM-4 Brooker, B., 247-FD-33, 364-FD-51 Cabell, K., 377-HSABP-7 Berger, T., 347-AFM-8, 381-MST-11 Blevins, A., 383-MST-14 Bouquet, T., 61-ACD-3 Brooks, C., 290-ACD-7 Cabrera, L., 393-TES-1 Berger, Z., 64-AMT-3 Bloebaum, C., 478-NDA-11 Bouslog, S., 99-PDL-2 Brooks, J., 393-TES-1 Cadel, D., 223-WE-3 Bergeron, K., 242-APA-26 Blom-Schieber, A., 107-STR-4 Bousquet, G., 469-GNC-32 Brooks, T., 330-SD-16 Cadieux, F., 300-FD-41 Bergh, C., 368-GNC-17 Blonigan, P., 136-FD-18, 348-AMT-12 Boutet, J., 127-APA-13 Brophy, C., 152-PC-10 Cadou, C., 42-PC-4, 98-PC-9 Berk, T., 79-FD-13 Bludau, J., 16-APA-4 Bouyssounouse, X., 168-UMS-4 Broughton-Venner, J., 146-MDO-4 Caetano, J., 148-MST-2 Bernal, L., 250-FD-36 Blum, A., 34-ISC-3 Bowen, P., 193-GTE-4, 393-TES-1 Broussard, S., 281-SUR-1 Cafarelli, S., 381-MST-11 Berner, C., 347-AFM-8 Bluman, J., 80-FD-14, 402-AFM-9 Bowen-Davies, G., 211-SD-10 Brouwer, K., 47-SD-1/APA-46 Cahoy, K., 100-SATS-3 Berridge, D., 414-FD-5 Bodart, J., 359-FD-46 Bower, A., 129-APA-15 Brown, A., 278-SD-15, 368-GNC-17 Cai, C., 76-FD-9

178 Berry, M., 141-GTE-3 Bodling, A., 119-AA-4 Bowers, A., 140-GT-4 Brown, C., 203-PC-13, 204-PC-14, 235-AA-7 Cai, J., 36-MAT-1, 197-MAT-5, 352-APA-35 Bershadsky, D., 169-UMS-5 Bodony, D., 208-PDL-5 Bowersox, R., 28-GT-1, 190-FD-29, 414-FD-5, Brown, G., 75-FD-8 Cai, Y., 400-ACD-9 Bertagne, C., 461-ASC-6 Boening, J., 33-ISC-2 417-FD-56 Brown, J., 211-SD-10, 212-SD-11, 391-SD-21, Cailler, M., 153-PC-11, 363-FD-50 Berton, J., 345-ACD-8 Boeswald, M., 444-SD-24 Bowes, A., 121-AFM-3 486-SD-25 Cairns, D., 286-WE-6 Bevilacqua, R., 310-GNC-13 Bogala, V., 305-GNC-8 Bowman, D., 200-MST-4 Brown, K., 22-FD-2, 292-APA-27, 365-FD-52 Calderon, D., 331-SD-17 Bewley, T., 37-MDO-1 Bogey, C., 234-AA-6 Box, S., 382-MST-12 Brown, M., 267-MST-7, 306-GNC-9 Calhoun, R., 285-WE-5, 395-WE-9 Beyar, M., 462-FD-10 Bohan, B., 98-PC-9, 193-GTE-4 Boxx, I., 270-PC-17, 435-PC-25 Brown, R., 146-MDO-4 Calkins, T., 83-GT-11 Beyhaghi, P., 37-MDO-1 Bohun, M., 90-MAT-3 Boyd, I., 108-TP-3, 166-TP-5, 219-TP-7 Browning, P., 128-APA-14 Calloni, B., 104-SOF-2 Beyhaghi, S., 447-TES-3 Bojko, B., 95-PC-6 Boyer, N., 101-SD-4/APA-47 Bruce, P., 134-FD-16, 189-FD-28, 247-FD-33 Calvert, M., 178-APA-17 Bhagwandin, V., 128-APA-14 Bokhart, A., 204-PC-14 Boyer, R., 269-NDA-6 Bruck, H., 402-AFM-9 Camacho, P., 78-FD-12 Bhamidipati, K., 68-APA-7 Bolender, M., 367-GNC-16 Boyle, D., 235-AA-7 Bruckner, A., 30-HIS-1 Camelli, F., 23-FD-3 Bhandari, S., 221-UMS-6, 283-UMS-8, 284-UMS-9, Bollino, K., 257-GNC-5, 310-GNC-13, 372-GNC-21, Boyson, T., 441-PDL-13 Bruner, C., 149-MVC-3 Cameron, N., 200-MST-4 373-GNC-22, 383-MST-14 424-GNC-26, 468-GNC-31 Bradford, S., 157-SCS-2 Brushaber, R., 333-SUR-2/MAT-7 Campana, E., 406-APA-40 Bharadwaj S, A., 353-APA-36 Bolton, J., 247-FD-33 Bramlette, R., 9-ACD-2, 31-HSABP-1, 62-ACD-4, Bryson, D., 38-MDO-2 Campbell, K., 97-PC-8 Bhatia, M., 146-MDO-4, 319-MDO-8 Bombelli, A., 323-MST-10 377-HSABP-7 Brzozowski, D., 79-FD-13, 360-FD-47 Campbell, M., 51-SRE-1 Bhatt, S., 368-GNC-17 Bond, R., 39-MVC-1, 55-TP-1 Brampton, C., 380-MDO-10 Buchbach, R., 444-SD-24 Campbell, N., 121-AFM-3 Bhuiyan, F., 52-STR-1 Bonfiglio, L., 324-NDA-7 Brandis, A., 282-TP-9, 334-TP-10 Buchta, D., 418-FD-57 Candler, G., 186-FD-25, 300-FD-41 BHVS, N., 305-GNC-8 Bonin, J., 394-TP-11 Brandon, J., 175-AFM-4 Buck, D., 283-UMS-8 Candon, M., 211-SD-10, 212-SD-11 Bi, Y., 330-SD-16 Bonnier, M., 199-MST-3 Brannan, J., 382-MST-12 Bucsan, G., 8-ACD-1 Canfield, R., 106-STR-3 Biagini, G., 218-STR-7 Bons, J., 376-GTE-8 Brat, G., 143-IS-2 Budovsky, A., 178-APA-17 Canteenwalla, P., 41-PC-3 Biber, K., 180-APA-19 Boom, P., 136-FD-18 Braun, J., 262-HSABP-5/PGC-4 Buelthoff, H., 266-MST-6, 322-MST-9 Cantemir, C., 81-GEPC-2 Bichnevicius, M., 220-TP-8 Boopathy, K., 410-APA-44/FD-53 Braun, R., 44-SATS-1, 121-AFM-3, 219-TP-7 Buettner, R., 476-MST-18 Cao, C., 352-APA-35 Bichon, B., 202-NDA-4, 214-SE-2 Boozer, C., 37-MDO-1 Brazell, M., 133-FD-15, 246-FD-32 Bufalini, M., 73-EDU-2/DE-1 Cao, Y., 196-IS-3, 258-GNC-6, 351-APA-34 Bidgood, P., 28-GT-1, 192-GT-5 Borer, N., 54-TFPC-1 Breedveld, P., 431-MST-16 Buffy, J., 333-SUR-2/MAT-7 Capecelatro, J., 208-PDL-5, 418-FD-57 Biedron, R., 49-SD-3, 410-APA-44/FD-53 Borg, M., 28-GT-1, 166-TP-5, 190-FD-29, 414-FD-5 Breivik, N., 202-NDA-4 Burchett, B., 63-AFM-2, 383-MST-14 Cardullo, F., 266-MST-6, 322-MST-9 Bielefeldt, B., 356-ASC-5 Borges Sebastiao, I., 448-TP-12 Brenner, M., 391-SD-21 Burgaud, F., 8-ACD-1, 150-NDA-2/MDO-5, 174-ACD-6 Caricati, E., 279-SEN-3 Bieniawski, S., 93-NDA-1 Borghesi, G., 153-PC-11 Brès, G., 173-AA-5, 408-APA-42 Burger, A., 192-GT-5 Carignan, C., 382-MST-12 Bigler, M., 269-NDA-6 Borghi, M., 251-FD-37 Breuer, K., 139-FD-22 Burgess, N., 302-FD-43 Carlson, J., 138-FD-20, 241-APA-24 Author/Session Chair Index Carolan, D., 36-MAT-1 Chaban, G., 334-TP-10 Chen, X., 286-WE-6 Chuck, C., 344-ABPSI-1, 399-ABPSI-2 Coleman, D., 70-APA-9, 277-SD-14 Carpenter, F., 473-GTE-11 Chae, J., 387-PDL-10, 440-PDL-12 Chen, Y., 465-FD-62 Chung, J., 220-TP-8 Coleman, T., 464-FD-61 Carpenter, M., 352-APA-35 Chae, M., 221-UMS-6 Cheney, T., 283-UMS-8 Chung, P., 284-UMS-9 Colket, M., 41-PC-3 Carr, R., 253-GNC-1 Chaganti, N., 247-FD-33, 364-FD-51 Cheng, W., 56-TP-2 Chung, W., 266-MST-6 Collazo Garcia, A., 10-AFM-1 Carreno, B., 51-SRE-1 Chahat, N., 157-SCS-2 Cheng, Z., 425-GNC-27 Church, C., 130-DE-2 Collins, K., 8-ACD-1, 120-ACD-5, 243-DE-3 Carreon-Limones, C., 284-UMS-9 Chaki, S., 143-IS-2 Chennimalai Kumar, N., 478-NDA-11 Churchfield, M., 111-WE-1, 285-WE-5, 490-WE-11 Colonia, S., 409-APA-43 Carrera, E., 106-STR-3 Chakrabarty, A., 168-UMS-4 Chernikova, A., 269-NDA-6 Chusri, S., 315-ICC-1 Colonius, T., 173-AA-5, 248-FD-34, 462-FD-10 Carrese, R., 17-ASC-1, 103-SD-6, 160-SD-9, Chakraborty, I., 290-ACD-7, 347-AFM-8, 400-ACD-9 Cherukru, N., 285-WE-5 Chwalowski, P., 49-SD-3, 442-SD-22 Combs, C., 137-FD-19, 189-FD-28 211-SD-10, 212-SD-11, 457-ACD-11 Chakravarthy, A., 254-GNC-2, 389-SD-19, Cheung, C., 470-GNC-33 Chynoweth, B., 21-FD-1 Combs, D., 34-ISC-3 Carrier, G., 14-APA-2 421-GNC-23, 422-GNC-24, 466-GNC-29 Cheung, K., 461-ASC-6, 486-SD-25 Ciampa, P., 392-STR-10 Comer, A., 95-PC-6, 272-PC-19, 386-PC-23, Carroll, D., 388-PDL-11 Chakroun, N., 206-PC-16, 386-PC-23, 439-PC-29 Cheung, L., 285-WE-5 Ciarcia, M., 259-GNC-7 437-PC-27, 483-PC-34 Carson, J., 368-GNC-17, 467-GNC-30 Chambers, J., 130-DE-2, 152-PC-10 Cheung, R., 129-APA-15, 159-SD-8 Ciarella, A., 297-APA-32 Commo, S., 375-GT-9 Carter, C., 85-HSABP-2, 99-PDL-2, 140-GT-4, Chambreau, S., 154-PC-12 Chhaya, B., 321-MST-8 Ciccio, J., 73-EDU-2/DE-1 Compagnin, A., 412-EXPL-2 204-PC-14, 270-PC-17, 434-PC-24, 480-PC-31 Chamitoff, G., 216-SOF-4 Chia, M., 289-AA-9 Cid, M., 390-SD-20 Constantine, P., 130-DE-2, 268-NDA-5, 324-NDA-7 Carter, D., 62-ACD-4 Chan, D., 27-GEPC-1, 83-GT-11 Chiatto, M., 463-FD-60 Cimmino, S., 279-SEN-3 Contento, G., 23-FD-3 Carter, M., 54-TFPC-1 Chan, W., 16-APA-4, 92-MVC-2 Chiba, K., 150-NDA-2/MDO-5 Cinar, G., 290-ACD-7 Conway, M., 66-APA-5, 303-FD-44, 355-APA-38 Cartieri, A., 241-APA-24 Chandel, D., 186-FD-25 Chiereghin, N., 250-FD-36 Cirtwill, J., 203-PC-13 Coogan, S., 299-FD-39 Cartmell, D., 266-MST-6, 322-MST-9 Chang, C., 193-GTE-4 Chilson, P., 284-UMS-9 Cizmas, P., 13-APA-1, 473-GTE-11 Cook, B., 279-SEN-3, 433-NDA-9 Carton de Wiart, C., 300-FD-41 Chang, D., 353-APA-36 Chin, J., 57-TP-13/MDO-13 Claflin, S., 262-HSABP-5/PGC-4 Cook, L., 150-NDA-2/MDO-5 Carvajal, O., 347-AFM-8 Chang, F., 145-MAT-4 Ching, E., 76-FD-9 Clark, C., 27-GEPC-1 Cook, R., 331-SD-17 Carvalhar, A., 73-EDU-2/DE-1 Chang, M., 15-APA-3 Chiodi, R., 418-FD-57 Clark, D., 151-NDA-3 Cook, S., 216-SOF-4 Cary, A., 420-FD-59 Chang, P., 97-PC-8 Chishty, W., 41-PC-3 Clark, I., 119-AA-4, 289-AA-9 Cooke, A., 10-AFM-1 Casbeer, D., 196-IS-3, 253-GNC-1, 471-GNC-34 Chang, Q., 212-SD-11 Cho, H., 278-SD-15, 331-SD-17, 351-APA-34 Clark, M., 143-IS-2, 168-UMS-4, 169-UMS-5, Cooksey, K., 174-ACD-6 Case, A., 34-ISC-3 Chang, S., 147-MST-1 Cho, K., 94-PC-5/PGC-2 433-NDA-9, 466-GNC-29 Cooper, J., 23-FD-3, 129-APA-15, 159-SD-8, 160-SD-9,

179 Cash, C., 15-APA-3 Chanzy, Q., 241-APA-24 Cho, M., 145-MAT-4, 147-MST-1 Clarke, R., 140-GT-4 320-MDO-9, 331-SD-17, 332-SD-18, 406-APA-40 Casper, K., 101-SD-4/APA-47, 122-AMT-5, Chao, H., 402-AFM-9, 469-GNC-32 Cho, S., 263-IS-4 Claucherty, S., 109-TP-4 Copenhaver, W., 399-ABPSI-2 364-FD-51, 414-FD-5 Chaparro, D., 389-SD-19, 442-SD-22 Choate, R., 161-SE-1 Claus, R., 215-SEN-2 Coppotelli, G., 444-SD-24 Castañeda, D., 415-FD-54 Chapelier, J., 302-FD-43 Choe, R., 307-GNC-10 Clay, S., 52-STR-1, 106-STR-3 Corbets, J., 34-ISC-3 Castano, L., 366-GNC-15 Chapelon, Q., 182-ASC-3 Choi, J., 145-MAT-4 Cleaver, D., 238-APA-21, 250-FD-36 Corbets, S., 33-ISC-2 Castellanos, A., 107-STR-4 Chatterjee, T., 285-WE-5, 395-WE-9 Choi, K., 90-MAT-3, 199-MST-3, 273-PDL-6, Clemens, N., 99-PDL-2, 189-FD-28, 377-HSABP-7 Corke, T., 273-PDL-6, 484-PDL-14 Castillo, E., 345-ACD-8 Chattopadhyay, A., 182-ASC-3, 411-ASC-4 406-APA-40, 430-MST-15 Clementino, M., 17-ASC-1 Corkery, S., 80-FD-14 Castillo, R., 395-WE-9 Chaudhuri, A., 202-NDA-4, 475-MDO-12/NDA-10 Choi, S., 38-MDO-2, 62-ACD-4, 277-SD-14, 429-MDO-11 Clements, E., 100-SATS-3 Cormarkovic, V., 210-SCS-3 Castner, R., 14-APA-2 Chaurasia, A., 89-MAT-2 Choi, T., 325-OPS-1 Cliff, S., 14-APA-2 Cornford, S., 243-DE-3, 269-NDA-6 Castrichini, A., 159-SD-8, 160-SD-9 Chava, S., 318-MAT-6 Choi, Y., 43-PDL-1 Clifford, C., 404-AMT-14, 463-FD-60 Cornish, A., 213-SD-12 Castro, S., 276-SD-13 Chavez, A., 169-UMS-5 Chong, S., 40-PC-2 Clifton, A., 111-WE-1 Corporan, E., 96-PC-7, 479-PC-30 Caswell, A., 262-HSABP-5/PGC-4, 479-PC-30 Chavez, O., 175-AFM-4 Chopra, I., 9-ACD-2, 72-ASC-2, 332-SD-18 Clingman, D., 359-FD-46 Corrigan, A., 7-AA-1, 252-FD-38 Catron, B., 374-GT-8 Chawner, J., 92-MVC-2 Chou, A., 82-GT-2, 273-PDL-6 Close, S., 51-SRE-1 Coschignano, A., 355-APA-38 Cavallaro, R., 218-STR-7 Chechet, I., 261-GTE-6 Choudhari, M., 21-FD-1 Cluck, N., 216-SOF-4 Costa, E., 376-GTE-8 Cavdaroglu, M., 256-GNC-4 Chee, S., 309-GNC-12 Choudhary, S., 318-MAT-6 Cluts, J., 7-AA-1 Costes, M., 239-APA-22 Caverly, R., 422-GNC-24 Chehroudi, B., 326-PC-20 Choudhuri, A., 393-TES-1, 446-TES-2 Coan, D., 357-EXPL-1 Cotelo, J., 379-MAT-8 Cazaurang, F., 428-IS-9 Chelliah, H., 154-PC-12, 436-PC-26, 438-PC-28, Choudhury, R., 66-APA-5 Coates, R., 431-MST-16 Cotting, M., 174-ACD-6, 347-AFM-8, 381-MST-11 Cecrdle, J., 159-SD-8 439-PC-29 Choukroun, D., 372-GNC-21 Cobb, R., 253-GNC-1, 325-OPS-1, 426-GNC-28 Cottle, A., 98-PC-9 Celebi, M., 107-STR-4 Chen, C., 200-MST-4 Chowdhary, K., 188-FD-27 Coburn, V., 42-PC-4 Coulter, K., 70-APA-9 Celik, O., 217-STR-6, 218-STR-7 Chen, D., 154-PC-12 Chowdhury, A., 393-TES-1 Coder, J., 178-APA-17, 241-APA-24, 354-APA-37, Coulton, J., 105-SRE-2 Cellucci, D., 486-SD-25 Chen, E., 356-ASC-5 Chowdhury, S., 58-UMS-1, 62-ACD-4, 264-MDO-7, 407-APA-41, 420-FD-59 Coussement, G., 293-APA-28 Center, K., 86-IS-1 Chen, H., 291-AFM-6, 304-FD-45, 310-GNC-13 284-UMS-9 Codoni, J., 94-PC-5/PGC-2 Cox, C., 70-APA-9 Cenzato, A., 412-EXPL-2 Chen, J., 111-WE-1, 423-GNC-25 Choze, S., 384-NDA-8 Coetzee, E., 10-AFM-1, 120-ACD-5, 147-MST-1, Cox, J., 128-APA-14 Cerimele, C., 467-GNC-30 Chen, L., 68-APA-7 Christian, J., 372-GNC-21 331-SD-17 Coy, E., 365-FD-52 Cervelloni, A., 32-ISC-1 Chen, P., 103-SD-6, 198-MDO-6 Christopher, J., 136-FD-18 Cohen, K., 428-IS-9 Crafton, J., 15-APA-3, 123-AMT-6, 176-AMT-8, Cesnik, C., 47-SD-1/APA-46, 101-SD-4/APA-47, Chen, Q., 46-SCS-1, 157-SCS-2 Chterev, I., 42-PC-4 Cohen, R., 143-IS-2 289-AA-9 276-SD-13 Chen, R., 145-MAT-4 Chu, Q., 196-IS-3, 263-IS-4, 308-GNC-11, 309-GNC-12, Coil, M., 205-PC-15 Cramer, N., 486-SD-25 Ceyhan, O., 223-WE-3 Chen, W., 240-APA-23/FD-31, 445-STR-11 347-AFM-8, 428-IS-9, 458-AFM-11, 468-GNC-31 Cole, I., 145-MAT-4 Author/Session Chair Index Crassidis, J., 256-GNC-4, 309-GNC-12, 372-GNC-21, Damazo, J., 12-AMT-2, 203-PC-13 DeChant, L., 304-FD-45 Detert, B., 240-APA-23/FD-31, 407-APA-41 Doman, D., 311-GNC-14, 315-ICC-1 468-GNC-31 Damiani, R., 170-WE-2, 395-WE-9 Decker, K., 57-TP-13/MDO-13 DeTrempe, P., 34-ISC-3 Domyancic, L., 433-NDA-9 Cratsley, J., 221-UMS-6 Damodaran, M., 407-APA-41 de Croon, G., 148-MST-2, 402-AFM-9 Dettwiller, I., 202-NDA-4 Donbar, J., 142-HSABP-3, 204-PC-14, 377-HSABP-7 Creary, G., 130-DE-2 Dampsey, J., 202-NDA-4 Dedic, C., 12-AMT-2, 65-AMT-4 Devarakonda, N., 458-AFM-11 Dong, H., 26-FD-7, 80-FD-14, 419-FD-58 Crider, D., 265-MST-5, 381-MST-11, 430-MST-15 Danehy, P., 11-AMT-1, 65-AMT-4, 83-GT-11, 404-AMT-14 Dee, J., 291-AFM-6 Devenport, W., 119-AA-4, 288-AA-8, 289-AA-9 Dong, X., 125-APA-11, 238-APA-21, 463-FD-60 Cristi, R., 259-GNC-7 Daneshvaran, N., 31-HSABP-1 Deere, K., 54-TFPC-1 Devens, J., 426-GNC-28 Dong, Y., 39-MVC-1, 125-APA-11 Cronier, Y., 374-GT-8 Dang, D., 108-TP-3 De Gaspari, A., 443-SD-23 de Visser, C., 148-MST-2, 196-IS-3, 263-IS-4, 317-IS-6, Dongmo, J., 254-GNC-2, 263-IS-4 Crosby, N., 384-NDA-8 Dang, K., 154-PC-12 DeHart, R., 468-GNC-31 402-AFM-9, 428-IS-9, 458-AFM-11, 468-GNC-31 Donini, A., 95-PC-6 Cross, A., 480-PC-31 Daniel, D., 190-FD-29 Deierling, P., 36-MAT-1 DeVore, M., 143-IS-2 Donohue, J., 377-HSABP-7 Cross, C., 423-GNC-25 Daniel, J., 243-DE-3 Deisuke, Y., 83-GT-11 de Vries, R., 288-AA-8 Dooley, S., 154-PC-12 Crossley, W., 37-MDO-1, 320-MDO-9, 345-ACD-8 Dannenhoffer, J., 39-MVC-1, 73-EDU-2/DE-1 de Kat, R., 17-ASC-1, 176-AMT-8 de Wekker, S., 291-AFM-6 Doolittle, M., 205-PC-15 Crowe, D., 353-APA-36 Danowsky, B., 10-AFM-1, 346-AFM-7, 422-GNC-24 Dela Cruz, J., 407-APA-41 DeWitt, M., 96-PC-7 Doom, J., 138-FD-20, 187-FD-26 Cruden, B., 282-TP-9, 334-TP-10 Dansie, J., 417-FD-56 de la Torre, M., 446-TES-2 Dey, S., 92-MVC-2 Dorduncu, M., 165-STR-5 Crumpacker, R., 304-FD-45 Danzuka, Y., 219-TP-7 DeLaurentis, D., 315-ICC-1 Dhanasar, M., 31-HSABP-1 Dormohammadi, S., 488-STR-12 Cuevas, L., 30-HIS-1 Daoud, F., 264-MDO-7 Delimont, J., 473-GTE-11 Dhanasekaran, P., 22-FD-2 Dorsett, K., 63-AFM-2, 430-MST-15, 459-AFM-12 Cui, J., 194-GTE-5, 251-FD-37 Darakananda, D., 248-FD-34 Della Corte, B., 288-AA-8 Dianetti, A., 309-GNC-12 Doty, J., 293-APA-28 Cui, X., 165-STR-5 Darbandi, M., 394-TP-11, 436-PC-26 Delorme, Y., 138-FD-20 Diaz, M., 214-SE-2 Doucette, E., 308-GNC-11 Cui, Y., 122-AMT-5, 178-APA-17, 327-PDL-8, 407-APA-41 Darby, E., 446-TES-2 Del Papa, S., 99-PDL-2 Diaz, N., 167-TP-6, 219-TP-7 Douglas, C., 385-PC-22 Cui, Z., 123-AMT-6 Darbyshire, O., 129-APA-15 Del Rey Fernández, D., 136-FD-18 Diaz Montiel, P., 52-STR-1 Doulamis, A., 335-UMS-10 Culley, D., 476-MST-18 Da Ronch, A., 10-AFM-1, 49-SD-3, 159-SD-8, del Rosario, Z., 268-NDA-5 Dickey, E., 78-FD-12 Doulamis, N., 335-UMS-10 Cummings, R., 251-FD-37 459-AFM-12 de Luca, L., 463-FD-60 Dickinson, B., 82-GT-2, 366-GNC-15 Dowdy, R., 87-ISC-4 Cunha Junior, S., 381-MST-11 Darr, S., 220-TP-8 De Maesschalck, C., 29-GTE-1 Dickman, C., 220-TP-8 Dowgwillo, R., 351-APA-34, 408-APA-42 Cunningham, A., 406-APA-40 Das, R., 142-HSABP-3 Demargne, A., 185-FD-24 Di Donato, P., 335-UMS-10 Doyle, D., 461-ASC-6 Cunningham, M., 291-AFM-6 Dasgupta, A., 153-PC-11 De Marqui, C., 17-ASC-1 Diel, D., 222-UMS-7 Doyle, J., 294-APA-29

180 Curtis, D., 325-OPS-1 Dasgupta, D., 435-PC-25 DeMars, K., 368-GNC-17 Diemer, J., 479-PC-30 Doyle, K., 156-SATS-4 Curtis-Brown, N., 283-UMS-8 Dash, A., 371-GNC-20 Demasi, L., 218-STR-7, 392-STR-10 Diez, M., 406-APA-40 Doyle, S., 319-MDO-8 Cutright, S., 53-STR-2 Daskiran, O., 236-AFM-5 DeMauro, E., 122-AMT-5, 362-FD-49, 364-FD-51, Diggs, A., 362-FD-49 Drain, B., 260-GT-6/AMT-10 Cutshall, J., 243-DE-3 Dasque, N., 66-APA-5 465-FD-62 Dighe, V., 336-WE-8 Drake, A., 31-HSABP-1 Cvijetic, G., 23-FD-3 Datta, A., 72-ASC-2, 211-SD-10, 390-SD-20, 443-SD-23 De Meo, D., 145-MAT-4 Dikalyuk, A., 208-PDL-5 Draper, J., 390-SD-20 Cybyk, B., 239-APA-22 Davendralingam, N., 37-MDO-1 Demetriou, M., 44-SATS-1, 310-GNC-13, 449-WE-10 Dillier, C., 205-PC-15 Drennan, S., 193-GTE-4, 261-GTE-6, 386-PC-23 D. R., A., 9-ACD-2 David, C., 323-MST-10 DeMillard, E., 15-APA-3, 223-WE-3 Dillinger, J., 160-SD-9 Dress, D., 161-SE-1 D’Amato, D., 325-OPS-1 Davidson, D., 438-PC-28 Demko, A., 97-PC-8, 205-PC-15 Dillsaver, M., 143-IS-2 Drew, M., 389-SD-19 D’Antoni, A., 325-OPS-1 Davidson, P., 52-STR-1 DeMott, D., 269-NDA-6 Dimitriadis, G., 127-APA-13, 250-FD-36 Dreyer, C., 164-SRE-3 D’Apolito, A., 325-OPS-1 Davies, M., 50-SOF-1, 104-SOF-2, 216-SOF-4 Dempsey, A., 281-SUR-1 Diosady, L., 348-AMT-12 Dreyer, E., 47-SD-1/APA-46 D’Intino, G., 266-MST-6 Davila, C., 52-STR-1 Dempster, A., 105-SRE-2 DiPalma, M., 48-SD-2 Drikakis, D., 98-PC-9, 186-FD-25 D’Mello, R., 202-NDA-4 Davis, D., 297-APA-32 Denegri, C., 277-SD-14 Dippold, V., 456-ABPSI-3 Driscoll, J., 25-FD-6, 31-HSABP-1 D’Souza, S., 110-UMS-2 Davis, G., 411-ASC-4 Deng, N., 353-APA-36 Diskin, B., 136-FD-18, 410-APA-44/FD-53 Driscoll, R., 195-HSABP-4/PGC-3 D’Urso, S., 200-MST-4 Davis, M., 162-SEN-1 Denison, M., 14-APA-2 DiZinno, N., 135-FD-17 Drozda, T., 377-HSABP-7 Dackus, P., 36-MAT-1 Davis, W., 188-FD-27 de Niz, D., 143-IS-2 Djeddi, R., 13-APA-1, 180-APA-19 Dryer, F., 154-PC-12 Dadswell, C., 431-MST-16 Davy, G., 143-IS-2 Dennis, C., 97-PC-8, 482-PC-33 Do, H., 28-GT-1, 85-HSABP-2 Du, Z., 111-WE-1, 304-FD-45, 475-MDO-12/NDA-10 Dahalan, M., 79-FD-13 Dawes, W., 185-FD-24 de Oliveira, G., 188-FD-27, 387-PDL-10 Dobes, K., 90-MAT-3 Duan, D., 234-AA-6 Dahire, S., 150-NDA-2/MDO-5 Dawicke, D., 217-STR-6 de Oliveira, P., 204-PC-14 Doboon, A., 393-TES-1 Duan, L., 21-FD-1, 77-FD-11 Dahlberg, J., 404-AMT-14 Day, M., 435-PC-25 de Paula, A., 125-APA-11, 350-APA-33, 352-APA-35, Dobre, S., 347-AFM-8 Dubben, J., 292-APA-27 Dai, H., 158-SD-7, 486-SD-25 De, S., 146-MDO-4 381-MST-11, 430-MST-15 Dobrzynski, C., 477-MVC-5 Dubreuil, S., 146-MDO-4 Dai, Y., 103-SD-6, 475-MDO-12/NDA-10 de Albuquerque, D., 217-STR-6 Depcik, C., 31-HSABP-1, 377-HSABP-7 Dodenhöft, J., 307-GNC-10 Dubuisson, S., 199-MST-3 Daigle, M., 423-GNC-25 de Almeida, O., 60-AA-2 Derlaga, J., 23-FD-3, 54-TFPC-1, 295-APA-30 Doehrmann, A., 189-FD-28 Duda, K., 322-MST-9 Daimon, Y., 40-PC-2 Dean, J., 92-MVC-2 de Ruiter, A., 373-GNC-22 Dogan, A., 236-AFM-5, 403-AFM-10 Dudek, J., 138-FD-20 Dale, G., 15-APA-3 DeAngelo, M., 255-GNC-3 Deshmukh, R., 179-APA-18 Dogan, K., 421-GNC-23, 466-GNC-29 Dufﬁeld, M., 221-UMS-6 Dalle, D., 14-APA-2 Deaton, J., 319-MDO-8, 380-MDO-10 De Simone, D., 279-SEN-3 Dogariu, A., 441-PDL-13 Dumitrache, C., 485-PDL-15 Dam, B., 446-TES-2 Debiasi, M., 407-APA-41 DesJardin, P., 95-PC-6 Doggett, W., 210-SCS-3 Dumoulin, M., 278-SD-15 Damaren, C., 424-GNC-26, 425-GNC-27 DeBonis, J., 77-FD-11 Desjardins, O., 418-FD-57 Dolan, B., 195-HSABP-4/PGC-3, 479-PC-30 Duong, A., 273-PDL-6 Damasceno, M., 363-FD-50 DeCarlo, E., 151-NDA-3 De Sterck, H., 208-PDL-5 Dolph, C., 283-UMS-8 Dupuis, M., 316-IS-5 Author/Session Chair Index Duque, E., 201-MVC-4, 409-APA-43 218-STR-7 Fahling, J., 389-SD-19 Fiévet, R., 94-PC-5/PGC-2, 166-TP-5 Freund, J., 98-PC-9, 208-PDL-5 Durai, A., 129-APA-15 ElHarriri, G., 447-TES-3 Fahrenthold, E., 333-SUR-2/MAT-7 Fike, J., 188-FD-27 Frew, E., 196-IS-3, 222-UMS-7 Duraisamy, K., 77-FD-11, 91-MDO-3, 249-FD-35, Elia, S., 377-HSABP-7 Fahringer, T., 11-AMT-1, 404-AMT-14 Filippi, M., 106-STR-3 Frey, T., 215-SEN-2, 279-SEN-3 289-AA-9, 324-NDA-7 Elkhayat, M., 156-SATS-4 Fahroo, F., 268-NDA-5, 324-NDA-7 Findlay, D., 242-APA-26 Frezzotti, M., 326-PC-20 Durak, U., 265-MST-5, 321-MST-8 Ellejmi, M., 199-MST-3 Falkiewicz, N., 47-SD-1/APA-46, 101-SD-4/APA-47 Finley, D., 126-APA-12, 405-APA-39 Friedlander, D., 456-ABPSI-3 Durand, J., 150-NDA-2/MDO-5, 174-ACD-6 Eller, D., 442-SD-22 Falugi, M., 107-STR-4 Fiorina, B., 153-PC-11, 363-FD-50 Friedman, C., 64-AMT-3 Durante, D., 406-APA-40 Elliot, A., 374-GT-8 Famularo, D., 367-GNC-16 Firsov, A., 178-APA-17 Friedman, S., 478-NDA-11 Durbin, P., 187-FD-26 Elliot, S., 99-PDL-2 Fan, W., 422-GNC-24 Fischer, C., 38-MDO-2 Friedmann, L., 16-APA-4 Durgesh, V., 191-FD-30 Elliott, D., 259-GNC-7 Fancello, A., 95-PC-6 Fithen, R., 431-MST-16 Friedmann, P., 9-ACD-2, 16-APA-4, 289-AA-9, 391-SD-21 Durston, D., 14-APA-2, 260-GT-6/AMT-10 Elliott, G., 12-AMT-2, 134-FD-16, 464-FD-61 Fang, H., 46-SCS-1, 157-SCS-2, 329-SCS-5 Flach, R., 312-GT-7/AMT-11 Fritz, M., 368-GNC-17 Dussart, G., 10-AFM-1 Ellis, K., 221-UMS-6 Fang, J., 238-APA-21 Flaherty, W., 282-TP-9 Fritz, T., 130-DE-2 Dutour, K., 87-ISC-4 Ellis-Terrell, C., 70-APA-9 Fang, N., 380-MDO-10 Flanagan, H., 402-AFM-9 Frohnapfel, D., 399-ABPSI-2 Dutra, D., 236-AFM-5 Ellsworth, J., 64-AMT-3 Fang, X., 165-STR-5 Flansburg, B., 53-STR-2 Frost, R., 297-APA-32 Dutta, P., 267-MST-7 El mahdi, L., 294-APA-29 Fangohr, H., 382-MST-12 Flatau, A., 366-GNC-15 Frost, S., 257-GNC-5, 369-GNC-18 Dutta, S., 63-AFM-2, 121-AFM-3 Elmiligui, A., 14-APA-2, 147-MST-1, 432-MST-17 Fares, E., 241-APA-24, 353-APA-36, 355-APA-38 Fleischhauer, E., 404-AMT-14 Fu, J., 481-PC-32 Dutton, J., 134-FD-16, 464-FD-61 Elnashar, G., 156-SATS-4 Farhat, C., 324-NDA-7 Fleischmann, D., 10-AFM-1 Fu, R., 108-TP-3 Dwight, R., 332-SD-18 ElRafﬁe, A., 156-SATS-4 Farias, P., 362-FD-49, 465-FD-62 Fleming, M., 192-GT-5 Fujii, K., 415-FD-54 Dwyer Cianciolo, A., 121-AFM-3, 467-GNC-30 Elsadek, A., 402-AFM-9 Farrar, C., 444-SD-24 Fleming, P., 395-WE-9 Fujimoto, K., 303-FD-44, 350-APA-33 Dykes, K., 170-WE-2, 224-WE-4, 395-WE-9 El-Sadek, A., 263-IS-4 Farsadi, T., 286-WE-6 Fletcher, D., 108-TP-3 Fujino, K., 69-APA-8/AA-3 Dymit, A., 34-ISC-3 Emeneth, M., 290-ACD-7 Farthing, M., 302-FD-43 Foley, W., 270-PC-17 Fujita, K., 219-TP-7, 334-TP-10 Eberhart, G., 58-UMS-1 Emerson, B., 42-PC-4, 203-PC-13, 385-PC-22 Faruque, I., 426-GNC-28 Fonod, R., 253-GNC-1 Fujiwara, H., 446-TES-2 Eberle, C., 436-PC-26 Enciu, J., 403-AFM-10 Fasano, G., 58-UMS-1, 215-SEN-2 Fontanella, R., 58-UMS-1, 279-SEN-3 Fukushima, Y., 127-APA-13, 476-MST-18 Eckert, Z., 484-PDL-14 Engblom, W., 251-FD-37 Fasel, H., 190-FD-29, 250-FD-36 Fonte, F., 332-SD-18, 443-SD-23 Fuller, C., 436-PC-26 Economon, T., 37-MDO-1, 120-ACD-5, 211-SD-10 Engelmann, C., 435-PC-25 Faulk, D., 279-SEN-3 Footdale, J., 210-SCS-3 Fullmer, D., 214-SE-2

181 Edelman, J., 21-FD-1 Engelsen, F., 91-MDO-3 Favale, J., 134-FD-16 Forbes, J., 309-GNC-12, 422-GNC-24 Fulton, J., 85-HSABP-2, 157-SCS-2 Edoh, A., 302-FD-43 Engelstad, S., 52-STR-1, 165-STR-5 Faverjon, B., 151-NDA-3 Forlines, R., 15-APA-3 Funaki, I., 314-HSABP-6/PGC-5 Edwards, J., 41-PC-3, 85-HSABP-2, 96-PC-7, Eppink, J., 75-FD-8 Faymonville, P., 104-SOF-2 Fossati, M., 24-FD-4, 76-FD-9, 149-MVC-3 Funase, R., 164-SRE-3 152-PC-10, 437-PC-27 Epps, B., 26-FD-7, 248-FD-34 Fazelzadeh, S., 487-SD-26 Fossen, T., 256-GNC-4 Fureby, C., 386-PC-23, 434-PC-24 Edwards, L., 21-FD-1 Erb, A., 478-NDA-11 Fefermann, Y., 290-ACD-7 Foster, J., 302-FD-43 Furuya, H., 157-SCS-2, 275-SCS-4 Eerland, W., 382-MST-12 Eren, U., 368-GNC-17 Feigh, K., 357-EXPL-1 Foster, L., 217-STR-6 Gaeta, R., 288-AA-8 Egolf, A., 354-APA-37 Eren, Z., 488-STR-12 Feight, J., 288-AA-8 Fotia, M., 474-HSABP-9/PGC-8 Gai, S., 109-TP-4, 448-TP-12 Egorov, I., 186-FD-25 Erickson, L., 461-ASC-6 Felder, W., 15-APA-3, 70-APA-9 Fouliard, Q., 36-MAT-1 Gaier, J., 51-SRE-1 Ehlert, G., 220-TP-8 Erickson, R., 203-PC-13 Fell, T., 431-MST-16 Fox, J., 457-ACD-11 Gaitonde, A., 23-FD-3, 159-SD-8 Ehn, A., 434-PC-24 Ermanni, P., 72-ASC-2 Feltrop, E., 70-APA-9, 180-APA-19, 241-APA-24 Fradet, R., 105-SRE-2 Gaitonde, D., 142-HSABP-3, 173-AA-5, 234-AA-6, Eickhoff, J., 382-MST-12 Ernest, N., 428-IS-9 Feng, L., 129-APA-15 Frame, D., 64-AMT-3 247-FD-33 Eiler, J., 161-SE-1 Erturk, S., 403-AFM-10 Feng, Z., 331-SD-17 Francis, J., 278-SD-15, 331-SD-17 Galbincea, N., 202-NDA-4 Eitelberg, G., 288-AA-8 Erwin, J., 71-APA-10, 133-FD-15, 242-APA-26, Fereidooni, A., 182-ASC-3, 356-ASC-5 Francois, G., 332-SD-18 Galbraith, M., 22-FD-2, 71-APA-10 Ek, H., 42-PC-4 292-APA-27, 302-FD-43 Ferguson, D., 195-HSABP-4/PGC-3, Frank, G., 34-ISC-3 Gallagher, T., 152-PC-10, 437-PC-27 Ekici, K., 13-APA-1, 180-APA-19 Escalona, L., 52-STR-1 262-HSABP-5/PGC-4 Frank, M., 98-PC-9 Gallaher, A., 9-ACD-2 Elandt, R., 124-AMT-7/GT-3 Escamilla, H., 423-GNC-25 Ferguson, F., 31-HSABP-1 Frankel, S., 22-FD-2, 138-FD-20 Gallegos, J., 92-MVC-2 El-Arabaty, M., 315-ICC-1 Esclapez, L., 479-PC-30 Fernandes, R., 313-GTE-7 Franquiz, F., 315-ICC-1 Galyen, N., 64-AMT-3 Elasha, F., 252-FD-38 Eslami, H., 487-SD-26 Fernandes, S., 313-GTE-7 Franzini, G., 253-GNC-1 Gamagedara, K., 64-AMT-3 El-Bayoumi, G., 255-GNC-3, 402-AFM-9 Estevadeordal, J., 122-AMT-5, 304-FD-45, 480-PC-31 Feron, E., 143-IS-2 Fravolini, M., 421-GNC-23 Gamba, M., 25-FD-6, 97-PC-8, 123-AMT-6 ElBialy, E., 489-TES-4 Ethan, L., 404-AMT-14 Feroz, M., 374-GT-8 Frazza, L., 69-APA-8/AA-3 Gamble, L., 67-APA-6 ElDegwy, A., 489-TES-4 Eugeni, M., 444-SD-24 Ferrari, M., 379-MAT-8 Frederic, P., 345-ACD-8 Gamil, A., 252-FD-38 Eldred, M., 38-MDO-2, 268-NDA-5, 324-NDA-7, Evans, J., 269-NDA-6 Fertig, R., 36-MAT-1, 52-STR-1, 318-MAT-6, 488-STR-12 Frederick, M., 345-ACD-8 Gamme, S., 188-FD-27 478-NDA-11 Evans, T., 51-SRE-1 Feyz, M., 427-GTE-9/PGC-6 Fredericks, W., 54-TFPC-1 Gan, J., 194-GTE-5 Eldredge, J., 248-FD-34 Fabiano, E., 410-APA-44/FD-53 Fichter, W., 322-MST-9 Frederickson, K., 327-PDL-8, 388-PDL-11, Ganapathisubramani, B., 17-ASC-1, 79-FD-13, Elgammal, T., 446-TES-2 Faes, M., 433-NDA-9 Fidkowski, K., 136-FD-18, 185-FD-24 441-PDL-13, 484-PDL-14 176-AMT-8 El-Gohary, K., 78-FD-12 Fagley, C., 239-APA-22, 242-APA-26, 351-APA-34 Field, J., 321-MST-8 French, M., 214-SE-2 Gandhi, A., 179-APA-18 Elhalwagy, Y., 156-SATS-4, 257-GNC-5 Fahim, A., 489-TES-4 Fields, T., 89-MAT-2, 131-EDU-3, 175-AFM-4, Frenklach, M., 206-PC-16 Gandhi, F., 48-SD-2 Elham, A., 37-MDO-1, 91-MDO-3, 198-MDO-6, Fahimi, F., 80-FD-14 470-GNC-33 Freret, L., 208-PDL-5 Gandhi, M., 373-GNC-22 Author/Session Chair Index Gandi, U., 487-SD-26 Gerstenmaier, W., 269-NDA-6 Gojon, R., 7-AA-1 Grant, P., 381-MST-11, 431-MST-16 Gryte, K., 256-GNC-4 Gangadharan, S., 325-OPS-1 Gertsch, L., 51-SRE-1, 164-SRE-3 Gokulakrishnan, P., 436-PC-26 Grassi, M., 215-SEN-2 Grzywna, J., 291-AFM-6 Ganguli, R., 9-ACD-2, 487-SD-26 Ghaffarian, R., 269-NDA-6 Goldberg, B., 441-PDL-13 Grauer, J., 175-AFM-4, 236-AFM-5 Gschweitl, M., 379-MAT-8 Gantt, E., 92-MVC-2 Ghafourizadeh, M., 436-PC-26 Golder, S., 138-FD-20 Graves, R., 75-FD-8, 293-APA-28, 406-APA-40 Gu, H., 383-MST-14 Gao, C., 177-APA-16, 180-APA-19 Ghani, A., 386-PC-23 Goldstein, D., 75-FD-8 Gray, J., 91-MDO-3, 150-NDA-2/MDO-5, 320-MDO-9, Gu, S., 55-TP-1 Gao, D., 197-MAT-5 Gharbi, A., 174-ACD-6 Gomez, E., 283-UMS-8 429-MDO-11 Gu, X., 392-STR-10 Gao, S., 24-FD-4 Gharibi, K., 53-STR-2 Gomez, S., 159-SD-8 Gray, K., 21-FD-1 Gu, Y., 469-GNC-32 Gao, X., 206-PC-16, 434-PC-24 Ghassemi Isfahani, A., 387-PDL-10 Gomit, G., 79-FD-13 Gray, M., 43-PDL-1 Guarato de Freitas Santos, J., 363-FD-50 Gao, Z., 165-STR-5, 177-APA-16, 180-APA-19, Ghate, A., 285-WE-5 Gonda, J., 18-CMS-1 Gray, W., 381-MST-11 Guardone, A., 477-MVC-5 350-APA-33, 400-ACD-9 Ghazi, G., 200-MST-4, 236-AFM-5 Gonzales, A., 78-FD-12 Graziano, T., 94-PC-5/PGC-2 Guarro, S., 104-SOF-2, 216-SOF-4, 222-UMS-7 Garbeff, T., 260-GT-6/AMT-10, 348-AMT-12 Ghoniem, A., 386-PC-23, 439-PC-29 Gonzalez, D., 77-FD-11, 137-FD-19, 234-AA-6 Greatwood, C., 366-GNC-15 Gudiyella, S., 206-PC-16 Garcia, A., 409-APA-43 Ghoreishi, S., 478-NDA-11 Gonzalez, E., 153-PC-11, 194-GTE-5 Grech, N., 177-APA-16 Guildenbecher, D., 404-AMT-14, 465-FD-62 Garcia, D., 316-IS-5 Ghoreyshi, M., 67-APA-6, 179-APA-18, 242-APA-26, Gonzalez-Linero, L., 10-AFM-1 Green, B., 242-APA-26 Guimaraes, T., 276-SD-13 Garcia, E., 191-FD-30, 253-GNC-1, 471-GNC-34 459-AFM-12 Gonzalez-Rocha, J., 291-AFM-6 Green, M., 26-FD-7, 73-EDU-2/DE-1, 248-FD-34 Guimaraes Bucalo, T., 399-ABPSI-2 Garcia, G., 470-GNC-33 Ghose, D., 471-GNC-34 Gonzalez-Salcedo, A., 490-WE-11 Green, R., 86-IS-1 Gulotta, P., 122-AMT-5 Garcia, J., 467-GNC-30 Ghosh, A., 236-AFM-5, 486-SD-25 Gooding, J., 89-MAT-2 Green, W., 206-PC-16 Gumbert, C., 475-MDO-12/NDA-10 Garcia, S., 149-MVC-3 Ghosh, D., 487-SD-26 Goodliff, S., 83-GT-11 Greenberg, J., 249-FD-35 Gunasegaram, D., 145-MAT-4 Garcia de Marina, H., 175-AFM-4 Ghosh, P., 56-TP-2 Goodman, D., 51-SRE-1 Greenblatt, D., 490-WE-11 Gunasekaran, S., 419-FD-58 Garcia Lorca, F., 222-UMS-7 Ghosh, S., 252-FD-38, 303-FD-44, 353-APA-36 Goodrick, D., 422-GNC-24 Greene, B., 99-PDL-2 Guo, H., 223-WE-3 Gardea, F., 486-SD-25 Ghoshal, S., 316-IS-5 Goodsell, J., 202-NDA-4 Greer, A., 356-ASC-5 Guo, S., 10-AFM-1 Gariffo, J., 220-TP-8 Giarra, M., 64-AMT-3 Goodwin, G., 344-ABPSI-1 Gregg-III, R., 353-APA-36 Gupta, A., 261-GTE-6, 346-AFM-7, 393-TES-1, Garmann, D., 139-FD-22, 251-FD-37, 365-FD-52 Gibard, J., 417-FD-56 Gopalakrishnan, P., 355-APA-38 Gregory, J., 176-AMT-8, 191-FD-30, 297-APA-32, 446-TES-2, 486-SD-25 Garnica, I., 456-ABPSI-3 Gicquel, L., 386-PC-23 Gopalakrishnan Meena, M., 139-FD-22 376-GTE-8, 416-FD-55 Gupta, M., 41-PC-3, 156-SATS-4, 445-STR-11 Garoche, P., 143-IS-2 Giegel, J., 57-TP-13/MDO-13 Gopalarathnam, A., 248-FD-34 Grenga, T., 153-PC-11 Gupta, P., 55-TP-1, 119-AA-4

182 Gaskell, P., 335-UMS-10 Giese, A., 173-AA-5 Gord, J., 12-AMT-2, 42-PC-4, 262-HSABP-5/PGC-4, Greschik, G., 329-SCS-5 Gupta, R., 146-MDO-4, 250-FD-36, 346-AFM-7 Gatlin, G., 297-APA-32 Gildersleeve, S., 359-FD-46 404-AMT-14 Gresham, J., 347-AFM-8, 381-MST-11 Gupta, S., 284-UMS-9, 402-AFM-9 Gatsonis, N., 44-SATS-1 Gillaugh, D., 212-SD-11 Gordeyev, S., 43-PDL-1, 328-PDL-9 Grewal, A., 332-SD-18 Gürdal, Z., 107-STR-4, 174-ACD-6 Gaudenzi, P., 444-SD-24 Gingras, D., 148-MST-2, 403-AFM-10 Gore, J., 41-PC-3, 204-PC-14, 261-GTE-6, 436-PC-26 Grey, Z., 130-DE-2 Gursul, I., 238-APA-21, 240-APA-23/FD-31, 250-FD-36 Gauger, N., 37-MDO-1, 211-SD-10 Girardi, R., 125-APA-11 Goriachkin, E., 29-GTE-1 Grier, B., 47-SD-1/APA-46 Gururaja, S., 165-STR-5 Gaul, N., 406-APA-40 Gissen, A., 360-FD-47 Gorospe, G., 432-MST-17 Griffee, C., 46-SCS-1 Gururajan, S., 222-UMS-7 Gavrilovic, N., 402-AFM-9 Givi, P., 246-FD-32 Goss, L., 98-PC-9, 193-GTE-4 Griffin, C., 128-APA-14 Gurusamy, V., 46-SCS-1 Gbaguidi, A., 197-MAT-5 Glaab, L., 283-UMS-8 Gosse, R., 365-FD-52 Griffin, E., 278-SD-15 Guterres, M., 283-UMS-8 Ge, C., 304-FD-45 Gladin, J., 84-GTE-2, 472-GTE-10 Goto, K., 262-HSABP-5/PGC-4, 275-SCS-4 Griffin, K., 103-SD-6 Gutesha, M., 393-TES-1 Gebbink, R., 82-GT-2 Glasby, R., 71-APA-10, 133-FD-15, 241-APA-24, Gottiparthi, K., 480-PC-31 Griffith, D., 160-SD-9, 286-WE-6, 336-WE-8 Gutmark, E., 7-AA-1, 60-AA-2, 84-GTE-2, 234-AA-6, Gehrke, A., 419-FD-58 242-APA-26, 292-APA-27, 302-FD-43 Goulding, P., 124-AMT-7/GT-3, 192-GT-5 Griffiths, B., 83-GT-11 235-AA-7, 479-PC-30 Geigle, K., 270-PC-17 Glass, C., 121-AFM-3 Govers, Y., 444-SD-24 Grinberg Dana, A., 206-PC-16 Guzman, I., 283-UMS-8 Geikie, M., 435-PC-25 Glass, D., 56-TP-2 Govindarajan, B., 292-APA-27, 409-APA-43 Groen, F., 269-NDA-6 Ha, D., 62-ACD-4 Gejji, R., 94-PC-5/PGC-2, 204-PC-14 Glauser, M., 60-AA-2, 141-GTE-3, 464-FD-61 Govindaraju, P., 37-MDO-1 Groetz, R., 434-PC-24 Haas, F., 154-PC-12 Geluardi, S., 266-MST-6, 322-MST-9 Glaz, B., 416-FD-55, 443-SD-23, 486-SD-25 Goyal, A., 459-AFM-12 Grogan, K., 438-PC-28 Habashi, W., 24-FD-4, 76-FD-9, 149-MVC-3 Geng, J., 469-GNC-32 Glaze, D., 481-PC-32 Goyal, V., 41-PC-3, 204-PC-14 Grohs, M., 34-ISC-3 Habets, J., 257-GNC-5 Geng, Y., 102-SD-5 Glebocki, R., 325-OPS-1 Grady, R., 389-SD-19 Grooms, I., 136-FD-18 Hadder, E., 457-ACD-11 George, J., 347-AFM-8, 349-AMT-13, 417-FD-56 Glegg, S., 288-AA-8 Graf, P., 170-WE-2 Groot, K., 462-FD-10 Hader, C., 190-FD-29 George, T., 318-MAT-6, 486-SD-25 Glezer, A., 360-FD-47 Gragston, M., 12-AMT-2, 97-PC-8 Gross, A., 23-FD-3, 250-FD-36, 252-FD-38, 360-FD-47, Haftka, R., 38-MDO-2, 362-FD-49 Georgiadis, N., 77-FD-11 Gluhareff, I., 31-HSABP-1 Graham, B., 431-MST-16 361-FD-48 Hagen, B., 122-AMT-5 Georgiou, G., 406-APA-40 Gnanamanickam, E., 464-FD-61 Graham, J., 490-WE-11 Gross, J., 200-MST-4, 382-MST-12 Hagenmaier, M., 142-HSABP-3 Geraci, G., 268-NDA-5, 478-NDA-11 Gnanaskandan, A., 205-PC-15, 271-PC-18 Graham, S., 356-ASC-5 Grossman, I., 189-FD-28 Hager, W., 369-GNC-18 Gerboni, C., 322-MST-9 Godar, T., 220-TP-8 Grainger, L., 276-SD-13 Groth, C., 208-PDL-5, 437-PC-27 Hagerott, S., 347-AFM-8, 381-MST-11, 402-AFM-9 Gerdes, J., 402-AFM-9 Goecks, V., 216-SOF-4 Grandhi, R., 38-MDO-2, 150-NDA-2/MDO-5, 319-MDO-8 Grover, M., 166-TP-5 Haimes, R., 39-MVC-1, 71-APA-10 Gerlach, T., 265-MST-5 Goertz, S., 293-APA-28 Grandone, S., 34-ISC-3 Grubelich, M., 94-PC-5/PGC-2 Hajek, M., 16-APA-4 Gerlinger, P., 436-PC-26 Gogineni, S., 60-AA-2, 141-GTE-3, 173-AA-5, 464-FD-61 Grannan, N., 141-GTE-3 Gruenwald, B., 168-UMS-4, 367-GNC-16, 421-GNC-23, Hale, C., 212-SD-11 Gern, F., 53-STR-2 Gogulapati, A., 47-SD-1/APA-46 Grant, J., 288-AA-8 466-GNC-29 Hale, R., 286-WE-6 Gerretsen, A., 321-MST-8 Gohardani, A., 357-EXPL-1 Grant, M., 63-AFM-2, 289-AA-9, 344-ABPSI-1 Grüter, B., 458-AFM-11 Hall, C., 34-ISC-3, 65-AMT-4, 439-PC-29 Author/Session Chair Index Hall, E., 404-AMT-14 Hartsfield, C., 45-SATS-2 Heinz, S., 249-FD-35 Hodges, D., 103-SD-6, 147-MST-1, 445-STR-11, Hrdina, C., 457-ACD-11 Hall, N., 13-APA-1, 296-APA-31, 458-AFM-11 Hartwich, P., 78-FD-12 Heister, S., 94-PC-5/PGC-2, 474-HSABP-9/PGC-8 487-SD-26 Hrinda, G., 445-STR-11 Hall, Z., 68-APA-7 Hartwig, J., 164-SRE-3, 220-TP-8, 362-FD-49, Hejase, M., 104-SOF-2, 216-SOF-4, 222-UMS-7 Hodges, R., 157-SCS-2 Hrishikeshavan, V., 9-ACD-2, 416-FD-55 Hallion, R., 30-HIS-1 419-FD-58, 465-FD-62 Helal, H., 447-TES-3 Hodson, J., 13-APA-1 Hristov, G., 250-FD-36 Halls, B., 404-AMT-14 Hartzell, C., 33-ISC-2 Hellman, B., 66-APA-5 Hoeijmakers, H., 490-WE-11 Hromisin, S., 60-AA-2 Ham, F., 300-FD-41 Harursampath, D., 9-ACD-2 Hellman, S., 404-AMT-14 Hofferth, J., 134-FD-16 Hruz, P., 423-GNC-25 Hamburg, S., 128-APA-14 Harvazinski, M., 95-PC-6, 271-PC-18, 292-APA-27, Helm, C., 189-FD-28 Hoffler, K., 19-DA-1 Hrynuk, J., 416-FD-55 Hamell, J., 317-IS-6 365-FD-52 Hemati, M., 303-FD-44 Hoffman, A., 484-PDL-14 Hsu, P., 97-PC-8, 404-AMT-14 Hammack, S., 480-PC-31 Harvey, R., 51-SRE-1 Hendershott, T., 41-PC-3, 270-PC-17, 479-PC-30 Hogge, E., 432-MST-17 Hu, C., 286-WE-6, 304-FD-45 Hammerton, J., 330-SD-16 Hasan, M., 252-FD-38 Henfling, J., 11-AMT-1, 364-FD-51 Hoke, J., 94-PC-5/PGC-2, 141-GTE-3, Hu, H., 109-TP-4, 141-GTE-3, 181-APA-20, 223-WE-3, Hammetter, C., 159-SD-8 Hasbestan, J., 299-FD-39 Heng, B., 151-NDA-3 195-HSABP-4/PGC-3, 262-HSABP-5/PGC-4, 237-AMT-9, 240-APA-23/FD-31 Hampton, R., 217-STR-6 Hasegawa, M., 70-APA-9 Hening, S., 110-UMS-2 314-HSABP-6/PGC-5, 399-ABPSI-2, 427-GTE-9/PGC-6, Hu, J., 283-UMS-8 Hamzelouia, S., 252-FD-38 Hash, D., 166-TP-5 Henne, U., 83-GT-11, 176-AMT-8, 179-APA-18 474-HSABP-9/PGC-8 Hu, T., 407-APA-41 Han, D., 234-AA-6, 261-GTE-6 Hashemi, K., 377-HSABP-7, 421-GNC-23 Henry, A., 72-ASC-2 Holler, D., 192-GT-5 Hu, Y., 26-FD-7, 280-STR-8 Han, J., 62-ACD-4 Hashimoto, A., 127-APA-13, 241-APA-24, 355-APA-38 Henry, E., 391-SD-21 Hölling, M., 72-ASC-2 Hu, Z., 93-NDA-1, 408-APA-42, 433-NDA-9 Han, P., 419-FD-58 Hassan, A., 311-GNC-14, 425-GNC-27 Hensch, A., 83-GT-11 Holman, D., 149-MVC-3 Huan, X., 268-NDA-5 Han, X., 246-FD-32 Hassan, E., 85-HSABP-2, 142-HSABP-3, 364-FD-51 Henson, M., 319-MDO-8 Holmes, M., 223-WE-3 Huang, C., 95-PC-6, 103-SD-6, 326-PC-20, 385-PC-22 Han, Y., 285-WE-5 Hassanalian, M., 17-ASC-1, 62-ACD-4, 72-ASC-2, Hereth, E., 149-MVC-3 Holycross, C., 318-MAT-6 Huang, D., 174-ACD-6, 391-SD-21 Hanazaki, K., 478-NDA-11 128-APA-14, 147-MST-1, 264-MDO-7 Herges, T., 111-WE-1 Holzapfel, F., 161-SE-1, 200-MST-4, 255-GNC-3, Huang, G., 282-TP-9 Handley, P., 322-MST-9 Hassanaly, M., 270-PC-17 Hernandez, M., 393-TES-1 307-GNC-10, 370-GNC-19 Huang, J., 21-FD-1, 77-FD-11 Handojo, V., 444-SD-24 Haste, D., 316-IS-5 Hernandez, R., 166-TP-5 Homeyer, T., 72-ASC-2 Huang, L., 407-APA-41 Hanke, K., 192-GT-5 Hatem, F., 193-GTE-4 Hernandez, S., 390-SD-20, 475-MDO-12/NDA-10 Hong, S., 305-GNC-8 Huang, M., 13-APA-1 Hanlon, E., 156-SATS-4 Hatem, T., 489-TES-4 Hernandez Perez, F., 95-PC-6 Hooker, J., 27-GEPC-1 Huang, S., 102-SD-5 Hannebique, G., 152-PC-10 Hatfield, M., 131-EDU-3 Herring, G., 273-PDL-6 Hoover, R., 36-MAT-1 Huang, W., 470-GNC-33

183 Hannon, J., 78-FD-12 Hathcock, M., 278-SD-15 Herrmann-Stanzel, R., 108-TP-3 Hopkins, J., 380-MDO-10 Huang, Y., 330-SD-16 Hanquist, K., 180-APA-19, 219-TP-7 Hattenberger, G., 175-AFM-4 Hess, C., 11-AMT-1 Hori, S., 488-STR-12 Hubbard, J., 28-GT-1, 291-AFM-6, 366-GNC-15 Hansen, C., 100-SATS-3 Haviland, S., 169-UMS-5 Hess, J., 121-AFM-3 Horiuchi, T., 219-TP-7 Hue, D., 241-APA-24 Hansen, J., 256-GNC-4 Hayashi, J., 388-PDL-11 Hesselink, L., 234-AA-6 Horkovich, J., 274-PDL-7 Huebsch, W., 128-APA-14, 130-DE-2 Hansen, L., 32-ISC-1 Hayashi, T., 176-AMT-8 Heyne, J., 12-AMT-2, 41-PC-3, 96-PC-7, 154-PC-12 Horn, J., 255-GNC-3, 403-AFM-10 Huete, C., 25-FD-6 Hanson, R., 438-PC-28 Hayden, T., 136-FD-18 Hibberd, S., 430-MST-15 Horne, R., 273-PDL-6 Huff, B., 236-AFM-5 Hao, L., 415-FD-54 Hayes, D., 10-AFM-1, 120-ACD-5 Hickey, B., 204-PC-14 Hornedo Rodriquez, E., 98-PC-9 Huff, D., 411-ASC-4 Haran, K., 81-GEPC-2 Hayes, J., 409-APA-43 Hickey, J., 40-PC-2, 271-PC-18, 420-FD-59 Hornung, M., 199-MST-3, 345-ACD-8, 457-ACD-11 Huffman, C., 186-FD-25 Hardalupas, Y., 42-PC-4, 98-PC-9 Hayirli, U., 102-SD-5 Hidaka, N., 45-SATS-2 Hortensius, R., 134-FD-16, 464-FD-61 Hughes, K., 362-FD-49 Hardaway, L., 217-STR-6 Hayman, G., 111-WE-1 Higashi, J., 314-HSABP-6/PGC-5 Horton, B., 48-SD-2 Humphrey, L., 326-PC-20 Hareesh, P., 416-FD-55 Hays, A., 288-AA-8 Higuchi, Y., 306-GNC-9, 334-TP-10 Horton, E., 457-ACD-11 Humphreys, C., 426-GNC-28 Hargis, J., 363-FD-50 Haywood, J., 302-FD-43 Hilario, M., 328-PDL-9 Hosder, S., 478-NDA-11 Humphreys, W., 11-AMT-1 Hariharan, N., 71-APA-10, 242-APA-26, 292-APA-27, He, A., 469-GNC-32 Hilbert, C., 149-MVC-3 Hoseini, H., 103-SD-6 Hung, Y., 388-PDL-11 354-APA-37, 409-APA-43, 460-APA-45 He, F., 431-MST-16 Hill, N., 400-ACD-9 Hosking, N., 158-SD-7 Hunsaker, D., 13-APA-1, 181-APA-20, 239-APA-22, Härkegård, O., 308-GNC-11 He, Z., 193-GTE-4 Hill, W., 34-ISC-3 Hoskins, C., 122-AMT-5 352-APA-35 Harness, A., 45-SATS-2 Heath, J., 33-ISC-2 Hilton, H., 217-STR-6 Hossain, M., 191-FD-30, 376-GTE-8, 416-FD-55 Hunt, M., 11-AMT-1 Harper, D., 174-ACD-6 Heathcote, D., 238-APA-21 Himmelberg, B., 32-ISC-1 Hosseini, K., 57-TP-13/MDO-13 Hunt, R., 25-FD-6, 168-UMS-4 Harris, C., 10-AFM-1 Hebert, A., 381-MST-11 Hinchliffe, B., 120-ACD-5 Hou, X., 90-MAT-3 Hunter, C., 78-FD-12 Harris, J., 64-AMT-3 Hebert, C., 390-SD-20 Hines, N., 130-DE-2 Hou, Y., 46-SCS-1, 157-SCS-2 Hunter, D., 34-ISC-3 Harris, R., 234-AA-6 Hebert, P., 374-GT-8 Hinkle, S., 64-AMT-3 Hou, Z., 102-SD-5 Huo, H., 153-PC-11 Harris, T., 243-DE-3 Hedlund, B., 43-PDL-1, 99-PDL-2, 176-AMT-8 Hirabayashi, H., 267-MST-7 Houpt, A., 43-PDL-1, 99-PDL-2, 176-AMT-8 Huo, W., 257-GNC-5 Harrivel, A., 279-SEN-3 Heeg, J., 49-SD-3, 103-SD-6, 406-APA-40 Hirakawa, K., 473-GTE-11 Housman, J., 160-SD-9 Huo, X., 257-GNC-5 Harry, J., 73-EDU-2/DE-1 Heesbeen, B., 266-MST-6 Hirose, T., 476-MST-18 Houston, A., 284-UMS-9 Hurley, J., 53-STR-2 Hartﬁeld, R., 61-ACD-3, 352-APA-35 Heidebrecht, A., 177-APA-16 Hirsch, B., 157-SCS-2 Hovakimyan, N., 254-GNC-2, 307-GNC-10, 335-UMS-10 Hurtig, T., 434-PC-24 Hartl, D., 17-ASC-1, 182-ASC-3, 356-ASC-5, 461-ASC-6 Heilmann, A., 79-FD-13 Hirsch, C., 293-APA-28 Hovell, K., 259-GNC-7 Husen, N., 123-AMT-6 Hartmann, J., 400-ACD-9 Heineck, J., 14-APA-2, 122-AMT-5, 260-GT-6/AMT-10 Hitomi, N., 196-IS-3 How, J., 471-GNC-34 Hussain, H., 421-GNC-23 Hartmann, P., 470-GNC-33 Heinemann, P., 345-ACD-8, 457-ACD-11 Hitzel, S., 350-APA-33 Howard, M., 219-TP-7 Hussien, O., 380-MDO-10 Hartmann, S., 265-MST-5 Heinich, C., 279-SEN-3 Hochstrasser, M., 200-MST-4 Howe, G., 458-AFM-11 Hutchins, W., 404-AMT-14 Author/Session Chair Index Huxdorf, O., 72-ASC-2 Izadpanahi, E., 147-MST-1, 487-SD-26 Ji, G., 405-APA-39 Jouannet, C., 61-ACD-3 Karasinski, J., 322-MST-9 Huynh, M., 169-UMS-5 Izuta, S., 267-MST-7 JIa, B., 309-GNC-12 Jourdan, E., 185-FD-24 Karch, C., 79-FD-13 Huzzayyin, O., 489-TES-4 Jacewicz, M., 325-OPS-1 Jiang, L., 192-GT-5 Joyce, R., 322-MST-9 Karla, C., 57-TP-13/MDO-13 Hwang, D., 480-PC-31 Jackson, B., 19-DA-1 Jiang, T., 381-MST-11 Jrad, M., 146-MDO-4, 346-AFM-7 Karlgaard, C., 121-AFM-3, 291-AFM-6 Hwang, I., 86-IS-1, 196-IS-3, 309-GNC-12, 322-MST-9 Jackson, D., 220-TP-8 Jiang, Z., 124-AMT-7/GT-3, 314-HSABP-6/PGC-5 Ju, L., 188-FD-27 Karmakar, A., 220-TP-8 Hwang, J., 320-MDO-9 Jackson, H., 319-MDO-8 Jianliang, A., 307-GNC-10 Ju, Y., 153-PC-11, 435-PC-25, 436-PC-26, 439-PC-29, Karman, S., 23-FD-3, 71-APA-10, 242-APA-26 Hwang, M., 306-GNC-9 Jackson, J., 169-UMS-5, 222-UMS-7, 380-MDO-10, Jiao, Y., 150-NDA-2/MDO-5 481-PC-32 Karniadakis, G., 324-NDA-7 Hyatt, N., 45-SATS-2 389-SD-19 Jiao, Z., 257-GNC-5 Juangphanich, P., 29-GTE-1 Karns, A., 82-GT-2 Hyder, I., 52-STR-1 Jackson, R., 240-APA-23/FD-31 Jimenez, H., 196-IS-3 Julian, K., 426-GNC-28 Karpel, M., 160-SD-9, 390-SD-20 Iaccarino, G., 268-NDA-5, 324-NDA-7, 478-NDA-11 Jackson, T., 152-PC-10 Jin, C., 373-GNC-22 Juliano, T., 186-FD-25 Karwas, A., 174-ACD-6, 180-APA-19 Ibrahem, K., 263-IS-4 Jacob, J., 240-APA-23/FD-31, 284-UMS-9, 288-AA-8, Jirasek, A., 459-AFM-12 Junell, J., 263-IS-4 Kasahara, J., 262-HSABP-5/PGC-4, 314-HSABP-6/PGC-5 Ibrahim, A., 489-TES-4 335-UMS-10, 445-STR-11 Jo, Y., 429-MDO-11 Jung, H., 199-MST-3 Kaseman, T., 109-TP-4 Ibrahim, K., 255-GNC-3 Jacobs, G., 188-FD-27 Johansen, T., 256-GNC-4 Jung, S., 307-GNC-10 Kassem, A., 255-GNC-3 Idan, M., 48-SD-2 Jacobson, S., 345-ACD-8 Johari, H., 191-FD-30 Jung, Y., 292-APA-27 Kassem, C., 90-MAT-3 Ihme, M., 40-PC-2, 76-FD-9, 271-PC-18, 386-PC-23, Jacques, D., 426-GNC-28 Johns, Z., 283-UMS-8 Junqueira-Junior, C., 127-APA-13 Kastengren, A., 204-PC-14 438-PC-28 Jafari, M., 365-FD-52 Johnson, A., 368-GNC-17 Jurkovich, M., 68-APA-7, 293-APA-28 Kastner, J., 90-MAT-3 Iioka, D., 139-FD-22 Jafarnejadsani, H., 254-GNC-2 Johnson, B., 365-FD-52 Kaemming, T., 262-HSABP-5/PGC-4, Kasuga, Y., 14-APA-2 Ikeda, Y., 206-PC-16 Jafer, S., 265-MST-5, 321-MST-8 Johnson, D., 34-ISC-3, 158-SD-7 474-HSABP-9/PGC-8 Kaszynski, A., 212-SD-11 Ikenaga, T., 424-GNC-26 Jaffe, R., 166-TP-5, 334-TP-10 Johnson, E., 62-ACD-4, 169-UMS-5, 258-GNC-6, Kageyama, K., 199-MST-3, 323-MST-10 Katsumata, N., 209-SATS-5 Ilario da Silva, C., 37-MDO-1, 60-AA-2, 429-MDO-11 Jagannath, R., 427-GTE-9/PGC-6, 440-PDL-12, 309-GNC-12, 367-GNC-16 Kahsai, T., 104-SOF-2 Katta, V., 154-PC-12, 436-PC-26 Im, H., 40-PC-2, 95-PC-6, 194-GTE-5, 270-PC-17, 485-PDL-15 Johnson, R., 7-AA-1 Kailasanath, K., 7-AA-1, 195-HSABP-4/PGC-3, Katz, A., 22-FD-2 436-PC-26 Jain, R., 138-FD-20, 460-APA-45 Johnson, S., 174-ACD-6, 316-IS-5 234-AA-6, 235-AA-7, 262-HSABP-5/PGC-4, Katz, J., 364-FD-51 Imtiaz, H., 26-FD-7 Jain, S., 459-AFM-12 Johnson, W., 467-GNC-30 314-HSABP-6/PGC-5 Katzner, E., 128-APA-14 Indig, N., 425-GNC-27 Jalali, A., 24-FD-4 Johnston, C., 55-TP-1, 334-TP-10, 394-TP-11 Kaiser, S., 345-ACD-8 Kauffman, J., 356-ASC-5

184 Ingraham, D., 119-AA-4 James, G., 389-SD-19 Johnston, D., 212-SD-11 Kalinowski, M., 392-STR-10 Kaushik, T., 395-WE-9 Inman, D., 67-APA-6 James, K., 260-GT-6/AMT-10, 312-GT-7/AMT-11 Johnston, T., 9-ACD-2 Kallo, J., 84-GTE-2 Kawabata, R., 362-FD-49 Innocenti, M., 253-GNC-1 James, S., 261-GTE-6, 323-MST-10 Johst, M., 140-GT-4 Kallou, E., 174-ACD-6 Kawaguchi, J., 236-AFM-5 Inoue, S., 46-SCS-1, 157-SCS-2 Janczeswki, T., 399-ABPSI-2 Joklik, R., 436-PC-26 Kalur, A., 372-GNC-21 Kawai, S., 127-APA-13, 185-FD-24 Inoyama, D., 278-SD-15, 331-SD-17, 443-SD-23 Jandaurek, K., 140-GT-4 Jolly, B., 121-AFM-3 Kamaraj, A., 277-SD-14 Kawakami, Y., 258-GNC-6 Intravartolo, N., 34-ISC-3 Jang, D., 110-UMS-2 Joly, L., 359-FD-46 Kameda, M., 176-AMT-8 Kawamura, T., 408-APA-42 Ioppolo, T., 28-GT-1, 237-AMT-9 Jang, J., 368-GNC-17 Jones, A., 139-FD-22, 335-UMS-10 Kamenetskiy, D., 241-APA-24 Kawarabayashi, D., 46-SCS-1 Iovino, S., 215-SEN-2 Janjua, Z., 90-MAT-3, 430-MST-15 Jones, D., 23-FD-3, 159-SD-8 Kamezawa, H., 121-AFM-3 Kayran, A., 90-MAT-3, 102-SD-5, 286-WE-6 Ippolito, C., 110-UMS-2 Jans, E., 388-PDL-11, 484-PDL-14 Jones, G., 83-GT-11, 124-AMT-7/GT-3 Kaminsky, A., 13-APA-1, 180-APA-19 Kazuki, F., 139-FD-22 Iqbal, L., 61-ACD-3, 73-EDU-2/DE-1 Jape, S., 411-ASC-4 Jones, M., 266-MST-6 Kammer, D., 48-SD-2 Kearney, S., 12-AMT-2, 404-AMT-14 Irving, J., 459-AFM-12 Jardines, A., 41-PC-3 Jones, R., 320-MDO-9, 335-UMS-10 Kan, B., 94-PC-5/PGC-2 Keating, D., 148-MST-2, 200-MST-4, 382-MST-12 Isaenkov, Y., 178-APA-17 Jarrett, J., 150-NDA-2/MDO-5 Jones, S., 283-UMS-8 Kan, P., 60-AA-2 Kecskemety, K., 111-WE-1 Ishida, T., 127-APA-13, 241-APA-24 Jasak, H., 23-FD-3 Jones, T., 210-SCS-3 Kanamori, M., 69-APA-8/AA-3 Kedward, L., 149-MVC-3 Ishida, Y., 219-TP-7 Jatiningrum, D., 468-GNC-31 Jones, W., 477-MVC-5 Kanazaki, M., 150-NDA-2/MDO-5, 239-APA-22 Keegan, B., 156-SATS-4 Ishihara, K., 262-HSABP-5/PGC-4 Javed, U., 158-SD-7, 182-ASC-3 Jonkman, B., 111-WE-1 Kaneshige, J., 254-GNC-2, 371-GNC-20 Keel, W., 243-DE-3 Ishii, M., 237-AMT-9 Jaworski, J., 139-FD-22, 224-WE-4 Jonkman, J., 111-WE-1, 170-WE-2 Kang, C., 26-FD-7, 80-FD-14, 131-EDU-3, 283-UMS-8, Kefal, A., 106-STR-3 Ishikawa, H., 14-APA-2, 69-APA-8/AA-3, 457-ACD-11 Jayakody, N., 411-ASC-4 Joo, H., 278-SD-15, 331-SD-17 402-AFM-9 Kelbe, R., 400-ACD-9 Ishiko, K., 239-APA-22 Jayaraman, B., 71-APA-10 Joo, J., 352-APA-35, 461-ASC-6 Kang, J., 156-SATS-4, 199-MST-3 Kelly, P., 140-GT-4 Isik, A., 217-STR-6 Jedicke, R., 164-SRE-3 Joos, A., 322-MST-9 Kang, S., 199-MST-3 Kemnetz, M., 328-PDL-9 Isokawa, H., 237-AMT-9 Jee, S., 79-FD-13 Jorgens, C., 82-GT-2 Kanistras, K., 374-GT-8 Kemp, D., 45-SATS-2 Isola, D., 24-FD-4, 76-FD-9 Jelicic, G., 444-SD-24 Joseph, A., 52-STR-1 Kannan, H., 478-NDA-11 Kenesei, P., 379-MAT-8 Isono, T., 456-ABPSI-3 Jenett, B., 461-ASC-6, 486-SD-25 Joseph, C., 353-APA-36 Kapania, R., 53-STR-2, 146-MDO-4, 198-MDO-6, Kennedy, G., 330-SD-16, 380-MDO-10, Israelsen, B., 86-IS-1 Jenie, Y., 470-GNC-33 Joseph, J., 173-AA-5 346-AFM-7, 392-STR-10, 445-STR-11 410-APA-44/FD-53 Ito, Y., 241-APA-24 Jenkins, T., 11-AMT-1, 65-AMT-4, 349-AMT-13 Joseph, N., 103-SD-6 Kapulu, O., 459-AFM-12 Kennedy, R., 414-FD-5 Itoh, E., 267-MST-7 Jensen, J., 14-APA-2 Joshi, A., 258-GNC-6 Kara, K., 125-APA-11, 459-AFM-12 Kennedy, W., 220-TP-8 Itoh, K., 191-FD-30, 361-FD-48 Jeon, S., 157-SCS-2 Joshi, G., 373-GNC-22 Karagozian, A., 302-FD-43 Kenway, G., 91-MDO-3, 241-APA-24, 429-MDO-11 Ivan, L., 208-PDL-5 Jewell, J., 28-GT-1, 121-AFM-3, 186-FD-25 Joshi, P., 478-NDA-11 Karamete, B., 92-MVC-2 Kepron, J., 32-ISC-1 Izadi, M., 258-GNC-6 Jha, R., 182-ASC-3, 411-ASC-4 Josyula, E., 166-TP-5 Karásek, M., 402-AFM-9 Kercher, A., 252-FD-38 Author/Session Chair Index Kern, S., 285-WE-5 Kirk, D., 325-OPS-1 333-SUR-2/MAT-7, 379-MAT-8 Kulkarni, C., 432-MST-17 Lane, R., 199-MST-3 Kesemen, L., 90-MAT-3 Kirkman, J., 67-APA-6, 174-ACD-6 Koodly Ravishankara, A., 490-WE-11 Kumar, A., 236-AFM-5 Lange, M., 156-SATS-4 Keshmiri, S., 470-GNC-33 Kirkpatrick, D., 32-ISC-1 Koomullil, R., 213-SD-12 Kumar, D., 48-SD-2 Langelaan, J., 469-GNC-32 Keskin, A., 214-SE-2, 380-MDO-10 Kirz, J., 69-APA-8/AA-3 Kopardekar, P., 110-UMS-2 Kumar, G., 261-GTE-6, 386-PC-23 Langley, B., 318-MAT-6, 486-SD-25 Kewlani, G., 386-PC-23 Kitamura, K., 296-APA-31 Kopp, R., 486-SD-25 Kumar, M., 45-SATS-2, 279-SEN-3, 428-IS-9 Langston, J., 89-MAT-2, 167-TP-6, 219-TP-7 Keye, S., 295-APA-30 Kitazume, N., 306-GNC-9 Koreanschi, A., 353-APA-36 Kumar, R., 68-APA-7, 82-GT-2, 464-FD-61 Lapointe, C., 136-FD-18 Keyes, S., 346-AFM-7 Kitson, R., 101-SD-4/APA-47 Korn, B., 19-DA-1 Kumar, S., 370-GNC-19 Larmi, M., 249-FD-35 Khalid, M., 26-FD-7 Kiyici, F., 376-GTE-8 Koroglu, B., 438-PC-28 Kumgeh, B., 270-PC-17 Larsen, C., 62-ACD-4 Khalil, E., 194-GTE-5, 447-TES-3, 489-TES-4 Klein, C., 83-GT-11, 176-AMT-8, 179-APA-18 Korolev, Y., 475-MDO-12/NDA-10 Kunka, L., 445-STR-11 Larson, G., 221-UMS-6 Khalil Hasan, A., 261-GTE-6, 393-TES-1 Klein, M., 73-EDU-2/DE-1 Koroll, F., 109-TP-4 Kuntz, D., 282-TP-9 Larsson, J., 25-FD-6, 246-FD-32, 300-FD-41 Khalili, A., 411-ASC-4 Kleine, V., 125-APA-11, 352-APA-35 Kosmatka, J., 131-EDU-3, 212-SD-11, 277-SD-14, Kunz, D., 373-GNC-22 Lartigue, G., 250-FD-36 Khalili, N., 487-SD-26 Kleinhenz, J., 51-SRE-1, 105-SRE-2, 164-SRE-3 487-SD-26 Kuo, C., 7-AA-1 Larusson, R., 134-FD-16 Khan, G., 318-MAT-6, 384-NDA-8 Klemkowsky, J., 404-AMT-14 Kostak, H., 70-APA-9 Kuratomi, T., 45-SATS-2 Lash, E., 189-FD-28 Khan, O., 180-APA-19, 355-APA-38 Klenke, R., 18-CMS-1, 140-GT-4, 426-GNC-28 Kostogorova-Beller, Y., 389-SD-19 Kurt, A., 104-SOF-2, 216-SOF-4, 222-UMS-7 Last, M., 279-SEN-3 Khargonekar, P., 307-GNC-10 Klettlinger, J., 96-PC-7 Kotov, M., 66-APA-5 Kurtulus, D., 128-APA-14 Laten, J., 440-PDL-12 Kheirkhah, S., 203-PC-13 Kliche, D., 394-TP-11 Kotsonis, M., 327-PDL-8, 361-FD-48, 387-PDL-10, Kuruvila, G., 264-MDO-7 Latz, J., 177-APA-16, 355-APA-38 Khodadoust, A., 78-FD-12 Kliment, L., 332-SD-18, 443-SD-23 440-PDL-12, 462-FD-10 Kushner, L., 260-GT-6/AMT-10 Lau, A., 400-ACD-9 Khodaparast, H., 406-APA-40 Klimmek, T., 444-SD-24 Kouchi, T., 67-APA-6 Kutay, A., 305-GNC-8, 367-GNC-16 Lau, F., 188-FD-27 Khoo, B., 97-PC-8, 178-APA-17, 327-PDL-8 Klingshirn, C., 96-PC-7 Kourchians, A., 368-GNC-17 Kuter, U., 317-IS-6 Lauer, N., 366-GNC-15 Khowsuwan, U., 315-ICC-1 Klock, R., 47-SD-1/APA-46, 101-SD-4/APA-47 Kourdis, P., 206-PC-16 Kutluay, Ü., 459-AFM-12 Laurence, S., 186-FD-25, 414-FD-5 Kianvashrad, N., 273-PDL-6 Klyde, D., 266-MST-6, 383-MST-14, 403-AFM-10 Kouri, D., 324-NDA-7 Kvamsdal, T., 285-WE-5 Laurendeau, E., 239-APA-22 Kicinger, R., 423-GNC-25 Kmak, F., 260-GT-6/AMT-10 Kourtzanidis, K., 440-PDL-12 Kwan, J., 267-MST-7 Laux, C., 109-TP-4, 388-PDL-11 Kidd, J., 235-AA-7 K N, J., 56-TP-2 Kowalchuk, S., 370-GNC-19, 476-MST-18 Kweon, C., 42-PC-4 Lavigne, L., 428-IS-9 Kiel, B., 60-AA-2, 173-AA-5 Knapke, R., 68-APA-7 Koziel, S., 38-MDO-2, 91-MDO-3, 177-APA-16 Kwon, E., 12-AMT-2, 203-PC-13 Lavoie, P., 11-AMT-1, 75-FD-8

185 Kier, T., 391-SD-21 Knapp, K., 280-STR-8 Kozlov, P., 43-PDL-1 Kwon, O., 142-HSABP-3 Lavretsky, E., 367-GNC-16, 421-GNC-23 Kikuchi, R., 69-APA-8/AA-3 Knerr, N., 243-DE-3 Kozuka, T., 306-GNC-9 Kwong, R., 422-GNC-24 Law, W., 169-UMS-5 Kilic, C., 372-GNC-21 Knight, D., 137-FD-19, 273-PDL-6 Kraemer, E., 178-APA-17, 336-WE-8 L’Esperance, A., 124-AMT-7/GT-3, 312-GT-7/AMT-11 Laws, N., 26-FD-7 Kim, A., 383-MST-14 Knowlen, C., 31-HSABP-1 Krakos, J., 241-APA-24 L’Heureux, D., 169-UMS-5 Lawson, E., 78-FD-12 Kim, B., 145-MAT-4 Ko, A., 38-MDO-2, 243-DE-3 Krampf, J., 69-APA-8/AA-3 Laban, M., 430-MST-15 Lawson, S., 297-APA-32 Kim, D., 142-HSABP-3, 197-MAT-5, 333-SUR-2/MAT-7 Kobayashi, M., 380-MDO-10 Kratz, J., 476-MST-18 Lacaze, G., 40-PC-2, 271-PC-18 Lawton, M., 46-SCS-1 Kim, E., 307-GNC-10 Kobryn, P., 214-SE-2 Krause, C., 200-MST-4 Lacher, A., 378-IS-7 Leal, P., 17-ASC-1 Kim, H., 276-SD-13, 277-SD-14, 380-MDO-10, Kochenderfer, M., 426-GNC-28 Kreshock, A., 160-SD-9 Lacoste, D., 12-AMT-2, 203-PC-13 Leavitt, L., 344-ABPSI-1, 456-ABPSI-3 387-PDL-10, 393-TES-1, 440-PDL-12 Kocher, A., 251-FD-37 Kreth, P., 137-FD-19, 189-FD-28, 463-FD-60 Ladeinde, F., 85-HSABP-2, 142-HSABP-3 LeBeau, R., 68-APA-7, 131-EDU-3, 440-PDL-12 Kim, J., 25-FD-6, 62-ACD-4, 142-HSABP-3, 217-STR-6, Kochersberger, K., 169-UMS-5 Kreutzfeldt, T., 416-FD-55 Ladeinde, T., 400-ACD-9 Leber, W., 423-GNC-25 261-GTE-6, 263-IS-4, 273-PDL-6, 376-GTE-8 Kocian, T., 70-APA-9, 190-FD-29 Krishnakumar, K., 110-UMS-2, 168-UMS-4 Laﬂin, K., 295-APA-30 Leccadito, M., 18-CMS-1, 140-GT-4 Kim, K., 387-PDL-10, 420-FD-59, 440-PDL-12 Kodali, D., 80-FD-14 Krishnamurthy, R., 215-SEN-2 Lagoudas, D., 182-ASC-3, 411-ASC-4, 461-ASC-6 Lechniak, J., 68-APA-7 Kim, N., 38-MDO-2, 151-NDA-3, 362-FD-49 Kohzai, M., 28-GT-1 Krishnamurthy, T., 384-NDA-8, 411-ASC-4 Laguardia, J., 236-AFM-5 Leclerc, C., 46-SCS-1 Kim, R., 34-ISC-3 Koike, M., 473-GTE-11 Kriukov, V., 166-TP-5 Lai, F., 56-TP-2 Lee, B., 95-PC-6, 270-PC-17, 409-APA-43 Kim, S., 278-SD-15, 351-APA-34, 369-GNC-18 Koike, S., 67-APA-6 Kronhaus, I., 43-PDL-1 Lai, K., 200-MST-4 Lee, D., 169-UMS-5, 306-GNC-9 Kim, T., 123-AMT-6, 395-WE-9 Kokkinakis, I., 186-FD-25 Kroninger, C., 416-FD-55 Lai, M., 480-PC-31 Lee, E., 282-TP-9 Kim, Y., 134-FD-16, 270-PC-17, 313-GTE-7, Koklu, M., 78-FD-12 Krot, A., 164-SRE-3 Laird, D., 170-WE-2 Lee, H., 134-FD-16, 169-UMS-5, 199-MST-3 369-GNC-18, 376-GTE-8 Kolhe, P., 247-FD-33 Krozel, J., 423-GNC-25, 471-GNC-34 Laizet, S., 387-PDL-10 Lee, J., 30-HIS-1, 255-GNC-3 Kimmel, R., 28-GT-1, 140-GT-4, 190-FD-29, 414-FD-5 Kolonay, R., 146-MDO-4, 214-SE-2 Krueger, W., 444-SD-24 Lakebrink, M., 360-FD-47 Lee, K., 257-GNC-5, 309-GNC-12 King, D., 388-PDL-11 Komadina, S., 400-ACD-9 Krynytzky, A., 192-GT-5 Lakshmanan, A., 335-UMS-10 Lee, M., 32-ISC-1, 481-PC-32 King, J., 426-GNC-28 Komives, J., 300-FD-41 Kryukov, I., 66-APA-5 Lakshminarayan, V., 71-APA-10, 410-APA-44/FD-53 Lee, N., 51-SRE-1, 351-APA-34 Kingry, N., 33-ISC-2 Komuro, T., 191-FD-30, 361-FD-48, 414-FD-5 Kuehl, J., 190-FD-29 Lalit, H., 436-PC-26 Lee, S., 86-IS-1, 238-APA-21, 259-GNC-7, 285-WE-5, Kingston, D., 162-SEN-1, 196-IS-3 Konagaya, R., 434-PC-24 Kuhn, M., 119-AA-4 Lam, K., 28-GT-1, 140-GT-4 313-GTE-7, 351-APA-34, 376-GTE-8, 390-SD-20 Kinney, T., 277-SD-14 Konig, B., 241-APA-24, 353-APA-36, 355-APA-38 Kuindersma, S., 9-ACD-2 Lambert, J., 362-FD-49 Lee, T., 28-GT-1, 64-AMT-3, 85-HSABP-2, 434-PC-24, Kinzel, M., 409-APA-43 Konrath, R., 179-APA-18 Kuitche, M., 148-MST-2, 200-MST-4 Lampton, A., 266-MST-6, 403-AFM-10 479-PC-30, 485-PDL-15 Kio, M., 56-TP-2 Kontis, K., 13-APA-1, 179-APA-18 Kulakhmetov, M., 448-TP-12 Landis, G., 105-SRE-2, 357-EXPL-1, 412-EXPL-2 Lee-Rausch, E., 241-APA-24 Kipouros, T., 38-MDO-2 Kontogiannis, S., 38-MDO-2 Kulatilaka, W., 65-AMT-4, 97-PC-8, 438-PC-28, Landrum, D., 26-FD-7, 80-FD-14, 131-EDU-3 Lefas, D., 194-GTE-5 Kiris, C., 160-SD-9 Koo, J., 89-MAT-2, 90-MAT-3, 167-TP-6, 219-TP-7, 439-PC-29, 481-PC-32 Lane, C., 284-UMS-9 Lefebvre, T., 146-MDO-4 Author/Session Chair Index Lefkowitz, J., 434-PC-24 Liang, C., 133-FD-15 Liu, S., 81-GEPC-2, 381-MST-11, 386-PC-23 Lua, J., 165-STR-5 Mackin, P., 381-MST-11 Leib, S., 119-AA-4 Liang, H., 487-SD-26 Liu, T., 123-AMT-6, 149-MVC-3 Lübker, J., 278-SD-15 Macmann, O., 279-SEN-3 Leidig, K., 382-MST-12 Lidor, A., 206-PC-16 Liu, W., 174-ACD-6, 180-APA-19 Luca, S., 153-PC-11 MacManus, D., 177-APA-16 Leidy, A., 190-FD-29, 414-FD-5, 417-FD-56 Lietz, C., 22-FD-2, 292-APA-27 Liu, X., 68-APA-7, 76-FD-9, 176-AMT-8, 364-FD-51, Lucas, D., 218-STR-7 Macquart, T., 461-ASC-6 Leifsson, L., 38-MDO-2, 91-MDO-3, 177-APA-16 Lieuwen, T., 42-PC-4, 203-PC-13, 326-PC-20, 424-GNC-26, 464-FD-61 Lucht, R., 12-AMT-2, 41-PC-3, 204-PC-14, 261-GTE-6 Madavan, N., 81-GEPC-2 Leishman, J., 464-FD-61 385-PC-22, 435-PC-25, 482-PC-33 Liu, Y., 24-FD-4, 33-ISC-2, 42-PC-4, 124-AMT-7/GT-3, Lucignano, G., 279-SEN-3 Madenci, E., 52-STR-1, 165-STR-5, 280-STR-8 Lele, S., 285-WE-5, 302-FD-43 Lightsey, E., 325-OPS-1 150-NDA-2/MDO-5, 185-FD-24, 212-SD-11, Luckner, R., 255-GNC-3 Mader, C., 429-MDO-11 Lemal, A., 334-TP-10 Liguore, S., 486-SD-25 217-STR-6, 394-TP-11, 405-APA-39, 424-GNC-26 Luckring, J., 293-APA-28, 406-APA-40 Madni, A., 161-SE-1 Lemmens, Y., 23-FD-3, 159-SD-8, 160-SD-9, Lillian, C., 292-APA-27 Liu, Z., 418-FD-57 Lührs, B., 400-ACD-9 Maekawa, H., 7-AA-1 320-MDO-9 Lim, D., 122-AMT-5, 474-HSABP-9/PGC-8 Livingston, J., 292-APA-27 Lui, T., 123-AMT-6 Maestro, D., 386-PC-23 Lempert, W., 441-PDL-13 Lim, S., 297-APA-32 Livingston, Z., 408-APA-42 Lukachev, S., 261-GTE-6 Magee, D., 299-FD-39 Lennie, M., 490-WE-11 Limbach, C., 155-PDL-3, 207-PDL-4, 327-PDL-8, Livne, E., 103-SD-6, 276-SD-13 Luke, E., 142-HSABP-3 Magstadt, A., 141-GTE-3 Lents, C., 81-GEPC-2 485-PDL-15 Löbl, D., 255-GNC-3 Luke, T., 34-ISC-3 Mahadevan, S., 93-NDA-1, 151-NDA-3, 213-SD-12, Lenz, H., 265-MST-5, 423-GNC-25 Lin, D., 381-MST-11 Locatelli, D., 146-MDO-4 Lum, E., 281-SUR-1 384-NDA-8, 433-NDA-9 Leon, V., 435-PC-25 Lin, E., 481-PC-32 Lock, R., 44-SATS-1 Lumb, S., 347-AFM-8 Mahmood, O., 294-APA-29 Leone, F., 52-STR-1 Lin, J., 78-FD-12, 234-AA-6 Lodato, G., 55-TP-1, 302-FD-43 Luna, M., 368-GNC-17 Mahmoud, O., 294-APA-29 Leonov, S., 43-PDL-1, 99-PDL-2, 176-AMT-8, Lin, K., 204-PC-14, 392-STR-10, 480-PC-31 Löfberg, J., 308-GNC-11 Lundgreen, R., 191-FD-30, 376-GTE-8, 416-FD-55 Mahuthannan, A., 203-PC-13 178-APA-17, 273-PDL-6, 327-PDL-8, 485-PDL-15 Lin, S., 56-TP-2 Lofthouse, A., 201-MVC-4, 242-APA-26, 459-AFM-12 Lung, S., 211-SD-10 Maiaru, M., 202-NDA-4 Le Page, L., 109-TP-4 Lin, Y., 123-AMT-6 Logan, M., 58-UMS-1, 62-ACD-4, 283-UMS-8 Lungavia, E., 412-EXPL-2 Maio, G., 363-FD-50 Leps, T., 33-ISC-2 Lindblad, D., 288-AA-8 Loganathan, J., 449-WE-10 Lunsford, I., 432-MST-17 Makhija, D., 320-MDO-9 Leser, P., 384-NDA-8 Lindörfer, S., 137-FD-19 Loganathan, S., 333-SUR-2/MAT-7 Luo, C., 124-AMT-7/GT-3 Makida, M., 446-TES-2 Lettieri, C., 220-TP-8 Lindsley, N., 102-SD-5 Lohner, R., 23-FD-3 Luo, H., 76-FD-9, 448-TP-12 Makino, A., 210-SCS-3 Levin, D., 108-TP-3, 208-PDL-5, 328-PDL-9, 394-TP-11 Ling, J., 188-FD-27, 433-NDA-9 Lombaerts, T., 254-GNC-2, 371-GNC-20 Luo, L., 188-FD-27 Makino, Y., 69-APA-8/AA-3 Levinski, O., 103-SD-6, 211-SD-10, 212-SD-11 Ling, Y., 93-NDA-1, 318-MAT-6, 384-NDA-8 Lone, M., 10-AFM-1, 120-ACD-5, 147-MST-1, 175-AFM-4 Luo, S., 181-APA-20 Maldonado, V., 58-UMS-1, 264-MDO-7, 284-UMS-9

186 Levko, D., 484-PDL-14 Lingren, J., 377-HSABP-7 Long, D., 461-ASC-6 Luo, T., 82-GT-2 Malekpour, M., 18-CMS-1 Levy, D., 61-ACD-3 Linke, F., 400-ACD-9 Long, K., 312-GT-7/AMT-11 Luo, Z., 331-SD-17, 381-MST-11 Malik, B., 347-AFM-8 Levy, Y., 249-FD-35 Linne, D., 51-SRE-1, 105-SRE-2, 164-SRE-3 Long, R., 111-WE-1 Lupieri, G., 23-FD-3 Malik, M., 138-FD-20 Lewalle, J., 60-AA-2, 270-PC-17, 464-FD-61 Lipton, J., 9-ACD-2 Longchamps, R., 131-EDU-3 Lutz, T., 178-APA-17, 336-WE-8 Malinek, P., 159-SD-8 Lewis, D., 140-GT-4 Lisanti, J., 427-GTE-9/PGC-6 Lopes, L., 410-APA-44/FD-53 Lv, Y., 76-FD-9, 386-PC-23 Mall, K., 289-AA-9, 344-ABPSI-1 Lewis, E., 265-MST-5 Lisco, B., 89-MAT-2, 90-MAT-3 Lopez, B., 55-TP-1 Lye, S., 322-MST-9 Mall, S., 212-SD-11 Lewis, J., 90-MAT-3, 202-NDA-4 List, M., 399-ABPSI-2 Lopez, C., 390-SD-20, 475-MDO-12/NDA-10 Lyford, A., 392-STR-10 Malla, B., 60-AA-2 Lewis, M., 234-AA-6 Litke, P., 98-PC-9, 141-GTE-3 Lopp, G., 356-ASC-5 Lyman, P., 162-SEN-1 Malla, R., 277-SD-14, 357-EXPL-1 Leyva, I., 247-FD-33 Litteken, D., 106-STR-3 Lorenz, C., 63-AFM-2 Lynch, E., 434-PC-24 Mallon, C., 64-AMT-3 Lhachemi, H., 425-GNC-27 Little, J., 189-FD-28, 240-APA-23/FD-31, 250-FD-36, Lorenzetti, J., 140-GT-4 Lynch, S., 29-GTE-1, 141-GTE-3, 220-TP-8 Manar, F., 139-FD-22 Li, B., 200-MST-4 273-PDL-6, 359-FD-46 Loseille, A., 69-APA-8/AA-3, 149-MVC-3 Lyrintzis, A., 7-AA-1, 234-AA-6 Manchester, Z., 9-ACD-2, 468-GNC-31 Li, C., 80-FD-14, 95-PC-6, 384-NDA-8, 433-NDA-9 Littrell, D., 362-FD-49 Loth, E., 180-APA-19, 224-WE-4, 399-ABPSI-2, Lyu, H., 86-IS-1 Mancuso, P., 264-MDO-7 Li, D., 158-SD-7, 240-APA-23/FD-31 Liu, C., 39-MVC-1, 76-FD-9, 125-APA-11, 145-MAT-4, 456-ABPSI-3 Lyu, X., 383-MST-14 Manero, A., 36-MAT-1, 379-MAT-8 Li, F., 21-FD-1 188-FD-27, 238-APA-21, 361-FD-48, 463-FD-60 Lou, J., 76-FD-9 Lyu, Y., 283-UMS-8 Maness, M., 224-WE-4 Li, G., 93-NDA-1, 411-ASC-4 Liu, E., 333-SUR-2/MAT-7 Lou, Z., 85-HSABP-2, 142-HSABP-3 M, V., 127-APA-13 Mani, M., 137-FD-19, 241-APA-24, 360-FD-47, Li, H., 109-TP-4, 213-SD-12, 237-AMT-9, Liu, F., 362-FD-49, 405-APA-39 Lovascio, S., 388-PDL-11 Ma, B., 14-APA-2 420-FD-59 240-APA-23/FD-31, 449-WE-10 Liu, G., 419-FD-58 Love, N., 198-MDO-6, 393-TES-1, 446-TES-2, 489-TES-4 Ma, L., 109-TP-4 Maniaci, D., 111-WE-1, 490-WE-11 Li, J., 69-APA-8/AA-3, 97-PC-8, 178-APA-17, 352-APA-35 Liu, H., 259-GNC-7, 308-GNC-11, 422-GNC-24, Lovich, B., 393-TES-1 Ma, O., 259-GNC-7 Mankbadi, M., 77-FD-11, 187-FD-26 Li, K., 310-GNC-13 426-GNC-28 Low, K., 58-UMS-1, 426-GNC-28 Ma, P., 40-PC-2, 271-PC-18, 386-PC-23, 479-PC-30 Mannucci, T., 196-IS-3, 428-IS-9 Li, L., 97-PC-8, 121-AFM-3, 141-GTE-3, 181-APA-20 Liu, J., 26-FD-7, 90-MAT-3, 181-APA-20, 224-WE-4, Lowe, A., 12-AMT-2 Ma, X., 169-UMS-5 Manoharan, R., 441-PDL-13 Li, M., 82-GT-2, 133-FD-15, 264-MDO-7 234-AA-6 Lowe, J., 474-HSABP-9/PGC-8 Maatz, I., 129-APA-15 Mansor, S., 79-FD-13 Li, P., 92-MVC-2 Liu, K., 185-FD-24, 223-WE-3, 281-SUR-1 Lowe, K., 11-AMT-1, 223-WE-3, 399-ABPSI-2 Mabson, G., 52-STR-1, 488-STR-12 Mansour, N., 448-TP-12 Li, R., 165-STR-5 Liu, M., 281-SUR-1 Lowenberg, M., 320-MDO-9, 331-SD-17 Maccarone, C., 423-GNC-25 Mantegazza, P., 332-SD-18 Li, S., 177-APA-16, 180-APA-19, 188-FD-27 Liu, N., 280-STR-8 Lu, F., 195-HSABP-4/PGC-3, 344-ABPSI-1, Macchiarella, N., 321-MST-8 Manuel, L., 170-WE-2, 224-WE-4 Li, W., 487-SD-26 Liu, P., 111-WE-1, 304-FD-45, 362-FD-49, 405-APA-39, 474-HSABP-9/PGC-8 MacDonald, T., 61-ACD-3, 290-ACD-7 Manzey, D., 255-GNC-3 Li, X., 213-SD-12, 254-GNC-2, 418-FD-57 407-APA-41 Lu, N., 170-WE-2 Macenski, S., 34-ISC-3 Maqsood, A., 169-UMS-5 Li, Y., 188-FD-27, 271-PC-18, 487-SD-26 Liu, Q., 28-GT-1, 85-HSABP-2 Lu, P., 309-GNC-12, 467-GNC-30 Machado-Rodriguez, J., 357-EXPL-1 Maraniello, S., 330-SD-16, 390-SD-20 Li, Z., 108-TP-3, 286-WE-6, 383-MST-14 Liu, R., 82-GT-2 Lu, Y., 185-FD-24 Macheret, S., 327-PDL-8 Marcum, D., 149-MVC-3 Author/Session Chair Index Mardanpour, P., 147-MST-1, 487-SD-26 Mastorakos, E., 96-PC-7, 204-PC-14, 326-PC-20, McFarland, M., 308-GNC-11 Menon, A., 389-SD-19 Mitchell, J., 69-APA-8/AA-3 Marin, A., 345-ACD-8 385-PC-22, 435-PC-25 McGann, B., 41-PC-3 Menon, P., 267-MST-7, 471-GNC-34 Mitsingas, C., 41-PC-3, 388-PDL-11, 485-PDL-15 Marineau, E., 11-AMT-1, 186-FD-25, 190-FD-29, Mastroddi, F., 444-SD-24 McGinley, C., 32-ISC-1 Menon, S., 152-PC-10 Mittal, R., 300-FD-41 390-SD-20, 414-FD-5 Masud, J., 67-APA-6, 294-APA-29, 304-FD-45, McGlynn, E., 251-FD-37 Meras, A., 424-GNC-26 Miyashita, T., 209-SATS-5, 329-SCS-5 Marinho, T., 335-UMS-10 347-AFM-8 McGough, W., 71-APA-10 Mercier, R., 153-PC-11, 250-FD-36, 363-FD-50 Miyazaki, T., 237-AMT-9 Marino, G., 325-OPS-1 Mat, S., 79-FD-13 McGowan, A., 243-DE-3 Merkle, C., 95-PC-6 Miyazaki, Y., 46-SCS-1, 157-SCS-2, 275-SCS-4 Mark, A., 366-GNC-15 Mataczynski, M., 399-ABPSI-2 McGowan, D., 17-ASC-1 Merret, J., 8-ACD-1 Miyazawa, Y., 306-GNC-9, 323-MST-10 Markley, F., 468-GNC-31 Mathieu, M., 345-ACD-8 McGowan, R., 273-PDL-6 Merrett, C., 73-EDU-2/DE-1 Mizukaki, T., 25-FD-6 Marks, C., 29-GTE-1, 361-FD-48 Mathieu, O., 438-PC-28 McGrath, B., 177-APA-16 Merrill, B., 179-APA-18 Mizuno, A., 99-PDL-2 Marks, I., 87-ISC-4 Matlik, J., 145-MAT-4, 214-SE-2 McGregor, C., 269-NDA-6 Merz, M., 258-GNC-6 Mizuno, T., 446-TES-2 Markstein, K., 430-MST-15 Matlis, E., 484-PDL-14 McGuire, S., 109-TP-4 Mesmer, B., 80-FD-14 Mobbs, K., 374-GT-8 Marley, C., 31-HSABP-1 Matney, A., 47-SD-1/APA-46 McHenry, N., 216-SOF-4 Messanelli, F., 99-PDL-2 Mobrem, M., 210-SCS-3 Marom, L., 416-FD-55 Matsuda, H., 323-MST-10 McIntyre, T., 55-TP-1 Mestreau, E., 92-MVC-2 Moder, J., 41-PC-3 Marples, B., 238-APA-21, 353-APA-36 Matsumoto, M., 191-FD-30 McKiernan, G., 21-FD-1 Meyer, S., 94-PC-5/PGC-2, 204-PC-14, Mody, A., 44-SATS-1, 45-SATS-2 Marques, A., 246-FD-32 Matsunaga, M., 66-APA-5 McLain, T., 221-UMS-6 314-HSABP-6/PGC-5 Moeller, T., 328-PDL-9 Marquez, J., 120-ACD-5 Matsuo, A., 314-HSABP-6/PGC-5 McLaughlin, D., 60-AA-2, 173-AA-5 Meyer, T., 12-AMT-2, 404-AMT-14 Moens, D., 433-NDA-9 Marten, D., 111-WE-1 Matsuo, T., 275-SCS-4 McLaughlin, T., 239-APA-22, 242-APA-26, 297-APA-32, Meyerhofer, P., 164-SRE-3 Moghadassian, B., 449-WE-10 Marti, F., 405-APA-39 Matsuoka, K., 262-HSABP-5/PGC-4, 351-APA-34, 417-FD-56 Meyers, J., 108-TP-3 Mohamed, A., 469-GNC-32 Martin, A., 108-TP-3 314-HSABP-6/PGC-5 McManus, K., 270-PC-17, 480-PC-31 Mian, Z., 9-ACD-2, 222-UMS-7 Mohamed Salleh, M., 58-UMS-1 Martin, C., 101-SD-4/APA-47, 434-PC-24 Matsushima, K., 275-SCS-4 McManus, T., 349-AMT-13 Michael, J., 12-AMT-2, 65-AMT-4, 205-PC-15 Mohiudeen, A., 459-AFM-12 Martin, I., 221-UMS-6 Matsuura, K., 362-FD-49 McNamara, J., 47-SD-1/APA-46, 101-SD-4/APA-47, Michaels, D., 206-PC-16, 386-PC-23, 439-PC-29 Mohrmann, F., 321-MST-8 Martin, M., 189-FD-28 Matsuyama, S., 334-TP-10 111-WE-1, 179-APA-18 Michal, T., 92-MVC-2, 241-APA-24 Mohseni, K., 311-GNC-14 Martin, N., 108-TP-3 Matula, D., 215-SEN-2 McNamee, P., 383-MST-14 Micol, J., 28-GT-1 Mokhtarpoor, R., 249-FD-35 Martin, P., 247-FD-33, 460-APA-45 Matula, N., 13-APA-1 McNeely, D., 466-GNC-29 Miglani, J., 53-STR-2, 107-STR-4 Mokhtarzadeh, A., 312-GT-7/AMT-11

187 Martin, S., 54-TFPC-1 Matveev, S., 261-GTE-6 McQuien, J., 461-ASC-6 Migliorino, M., 25-FD-6 Molenkamp, D., 263-IS-4 Martinez, J., 17-ASC-1 Matz, D., 467-GNC-30 McQuigg, T., 278-SD-15 Mignolet, M., 47-SD-1/APA-46 Molina, E., 49-SD-3 Martinez, L., 490-WE-11 Maughmer, M., 409-APA-43 McQuilling, M., 137-FD-19 Mihaescu, M., 7-AA-1 Molinari, G., 72-ASC-2 Martinez-Ruiz, D., 25-FD-6 Maurer, W., 286-WE-6 McSwain, R., 283-UMS-8 Miles, R., 65-AMT-4, 207-PDL-4, 327-PDL-8, Moncayo, H., 316-IS-5 Martini, M., 105-SRE-2 Mavriplis, D., 133-FD-15, 246-FD-32, 295-APA-30, McWilliam, M., 449-WE-10 349-AMT-13, 441-PDL-13, 484-PDL-14 Mondal, M., 426-GNC-28 Martins, A., 182-ASC-3 299-FD-39, 410-APA-44/FD-53 Meade, A., 312-GT-7/AMT-11 Milholen, W., 83-GT-11 Mondragon, J., 28-GT-1 Martins, B., 212-SD-11, 277-SD-14 Mavris, D., 8-ACD-1, 84-GTE-2, 120-ACD-5, Meakin, R., 71-APA-10, 292-APA-27 Miller, A., 347-AFM-8 Mondragon, U., 203-PC-13 Martins, J., 91-MDO-3, 146-MDO-4, 198-MDO-6, 150-NDA-2/MDO-5, 174-ACD-6, 196-IS-3, 214-SE-2, Mease, K., 323-MST-10 Miller, C., 317-IS-6, 422-GNC-24 Monfort, J., 270-PC-17, 479-PC-30 320-MDO-9, 330-SD-16, 429-MDO-11 243-DE-3, 290-ACD-7, 400-ACD-9, 472-GTE-10 Mecitoglu, Z., 488-STR-12 Miller, J., 12-AMT-2, 96-PC-7, 438-PC-28 Monner, H., 72-ASC-2 Martos, B., 54-TFPC-1, 297-APA-32 Maxwell, J., 344-ABPSI-1 Meddaikar, Y., 160-SD-9 Miller, M., 357-EXPL-1, 369-GNC-18 Monschke, J., 38-MDO-2 Marwa, M., 54-TFPC-1 May, G., 24-FD-4, 185-FD-24 Medina, A., 26-FD-7, 303-FD-44 Miller, T., 164-SRE-3 Montazersadgh, F., 210-SCS-3 Marzocca, P., 17-ASC-1, 103-SD-6, 160-SD-9, Mayer, R., 178-APA-17 Mee, D., 414-FD-5 Milletich, R., 279-SEN-3 Montefort, J., 123-AMT-6 174-ACD-6, 211-SD-10, 212-SD-11 Mayhew, E., 41-PC-3, 479-PC-30, 485-PDL-15 Mehiel, E., 432-MST-17 Millican, A., 289-AA-9 Monti, D., 443-SD-23 Marzouk, Y., 475-MDO-12/NDA-10 Mazzacchi, F., 49-SD-3 Mehmood, H., 258-GNC-6 Mills, A., 196-IS-3, 222-UMS-7 Moodie, A., 9-ACD-2 Mascarenas, D., 444-SD-24 McCabe, J., 368-GNC-17 Mehta, N., 328-PDL-9 Mills, D., 123-AMT-6 Mooij, E., 121-AFM-3, 257-GNC-5, 310-GNC-13, Mas Colomer, J., 146-MDO-4 McCarthy, J., 130-DE-2 Meiland, R., 321-MST-8 Millwater, H., 384-NDA-8 369-GNC-18, 372-GNC-21 Masi, A., 251-FD-37 McClearn, M., 141-GTE-3 Melcher, K., 86-IS-1, 396-IS-8 Min, J., 280-STR-8 Moon, G., 305-GNC-8 Maslov, A., 178-APA-17 McClelland, H., 283-UMS-8 Mele, B., 239-APA-22 Mingear, J., 356-ASC-5 Moore, C., 316-IS-5 Mason, B., 159-SD-8 McCloud, P., 282-TP-9 Mello, R., 403-AFM-10 Minshall, T., 212-SD-11 Moore, J., 53-STR-2, 275-SCS-4, 461-ASC-6 Masoud, A., 489-TES-4 McClung, A., 473-GTE-11 Melton, J., 110-UMS-2, 312-GT-7/AMT-11 Minwalla, C., 221-UMS-6 Moore, K., 320-MDO-9 Masquelet, M., 480-PC-31 McClure, P., 15-APA-3 Memon, M., 361-FD-48 Mir, I., 169-UMS-5 Moormann, D., 221-UMS-6, 470-GNC-33 Masri, A., 12-AMT-2 McCormack, R., 32-ISC-1 Mendeck, G., 467-GNC-30 Mirot, A., 321-MST-8 Moosavian, A., 67-APA-6 Massa, L., 98-PC-9 McCrink, M., 297-APA-32 Mendez, B., 223-WE-3 Mirzayeva, A., 206-PC-16 Mora, P., 7-AA-1, 235-AA-7 Masselot, D., 94-PC-5/PGC-2 McDaniel, D., 71-APA-10, 201-MVC-4, 213-SD-12, Mendoza, J., 173-AA-5, 288-AA-8 Misaka, T., 473-GTE-11 Mora-Camino, F., 423-GNC-25 Massey, S., 103-SD-6, 442-SD-22 249-FD-35 Menegay, P., 243-DE-3 Mishra, A., 91-MDO-3 Morales, A., 435-PC-25 Massinas, B., 335-UMS-10 McDonald, R., 290-ACD-7 Meneghini, J., 125-APA-11 Mishra, B., 51-SRE-1 Moralev, I., 178-APA-17 Masters, D., 13-APA-1 McDonell, V., 203-PC-13, 204-PC-14 Meneveau, C., 300-FD-41, 490-WE-11 Mital, S., 488-STR-12 Moreau, E., 99-PDL-2, 327-PDL-8, 387-PDL-10 Masters, J., 39-MVC-1 McEver, J., 315-ICC-1 Menga, E., 390-SD-20 Mitchell, D., 403-AFM-10 Moreira, F., 185-FD-24 Author/Session Chair Index Morelli, E., 236-AFM-5 Mundt, C., 109-TP-4, 394-TP-11 Namilae, S., 197-MAT-5, 318-MAT-6 Nguyen, T., 203-PC-13, 204-PC-14 Nykamp, C., 124-AMT-7/GT-3, 192-GT-5 Moreno, R., 444-SD-24 Munduate, X., 223-WE-3, 490-WE-11 Nannapaneni, S., 93-NDA-1 Ni, X., 371-GNC-20 O`Connor, J., 326-PC-20 Morgan, J., 173-AA-5 Muñoz, A., 223-WE-3 Naoumov, V., 166-TP-5, 205-PC-15 Nichols, C., 323-MST-10 O’Brien, D., 352-APA-35 Morgan, L., 444-SD-24 Munson, M., 252-FD-38 Naples, A., 427-GTE-9/PGC-6 Nichols, D., 149-MVC-3 O’Brien, W., 399-ABPSI-2 Morgan, P., 68-APA-7, 76-FD-9, 293-APA-28, Muppidi, S., 127-APA-13, 167-TP-6, 350-APA-33 Napoli, N., 279-SEN-3 Nichols, T., 162-SEN-1 O’Byrne, S., 109-TP-4, 441-PDL-13, 448-TP-12 355-APA-38, 406-APA-40 Mura, G., 61-ACD-3, 120-ACD-5 Naqavi, I., 119-AA-4 Nickol, C., 345-ACD-8 O’Connell, T., 291-AFM-6 Morgan, R., 11-AMT-1, 55-TP-1 Murakami, N., 424-GNC-26 Naraghi, M., 36-MAT-1, 89-MAT-2, 197-MAT-5 Nie, S., 351-APA-34 O’Donnell, F., 357-EXPL-1 Mori, O., 275-SCS-4 Murayama, M., 241-APA-24 Narang-Siddarth, A., 369-GNC-18, 425-GNC-27 Niel, F., 239-APA-22 O’Donnell, R., 311-GNC-14 Morikami, G., 239-APA-22 Murillo, O., 140-GT-4 Narasimha, R., 414-FD-5 Nield, S., 331-SD-17 O’Keeffe, G., 423-GNC-25 Morimoto, T., 89-MAT-2 Murman, S., 300-FD-41, 348-AMT-12 Narayanaswamy, V., 140-GT-4 Nielsen, E., 136-FD-18, 410-APA-44/FD-53 O’Malley, T., 51-SRE-1 Morones, A., 435-PC-25 Murphey, T., 46-SCS-1, 157-SCS-2 Narducci, R., 354-APA-37, 409-APA-43 Nielsen, T., 152-PC-10 O’Meara, B., 262-HSABP-5/PGC-4 Morote, J., 294-APA-29 Murphy, D., 159-SD-8 Narisetti, R., 444-SD-24 Niemeyer, K., 299-FD-39 O’Neil, M., 97-PC-8 Morote, P., 294-APA-29 Murphy, J., 163-SOF-3, 216-SOF-4 Narsipur, S., 248-FD-34 Niemiec, N., 97-PC-8, 481-PC-32 Obayashi, S., 69-APA-8/AA-3, 139-FD-22, Morraru, G., 190-FD-29 Murphy, P., 175-AFM-4 Naseer, R., 158-SD-7 Niestroy, M., 430-MST-15 473-GTE-11, 476-MST-18 Morris, J., 39-MVC-1 Murray, N., 173-AA-5 Nash, L., 96-PC-7 Niezgoda, S., 202-NDA-4 Oberlander, A., 57-TP-13/MDO-13 Morris, P., 60-AA-2, 173-AA-5 Murri, D., 236-AFM-5 Nastasi, K., 100-SATS-3 Nigam, N., 198-MDO-6 Ocampo, J., 384-NDA-8 Morris, R., 168-UMS-4 Murrieta Mendoza, A., 306-GNC-9 Nasuti, F., 326-PC-20 Nigro, R., 293-APA-28 Ochi, Y., 430-MST-15 Morrison, J., 295-APA-30 Murthy, P., 53-STR-2, 488-STR-12 Natali, M., 89-MAT-2 Nikbay, M., 14-APA-2, 406-APA-40 Ochoa, C., 58-UMS-1 Morrow, G., 205-PC-15 Murthy, R., 47-SD-1/APA-46 Naterer, G., 167-TP-6 Nikoueeyan, P., 237-AMT-9 Oda, Y., 407-APA-41 Mortazavi, M., 137-FD-19 Muschler, A., 286-WE-6 Nath, P., 433-NDA-9 Nilsson, E., 434-PC-24 Odegard, G., 145-MAT-4, 333-SUR-2/MAT-7 Morton, D., 201-MVC-4 Muse, J., 367-GNC-16, 421-GNC-23, 466-GNC-29 Nathoo, M., 149-MVC-3 Nimo, C., 18-CMS-1 Odonkor, P., 284-UMS-9 Morton, S., 71-APA-10, 201-MVC-4, 242-APA-26 Musgrove, G., 70-APA-9, 299-FD-39 Natori, M., 209-SATS-5 Ning, A., 146-MDO-4, 170-WE-2, 395-WE-9 Oefelein, J., 40-PC-2, 153-PC-11, 271-PC-18, 480-PC-31 Moschetta, J., 402-AFM-9 Musielak, D., 142-HSABP-3 Naughton, B., 111-WE-1 Ning, Z., 181-APA-20 Oerlemans, S., 336-WE-8 Moser, K., 90-MAT-3 Mustafa, M., 11-AMT-1 Naughton, J., 15-APA-3, 223-WE-3, 237-AMT-9 Ninnemann, E., 438-PC-28 Oevermann, M., 153-PC-11

188 Moser, R., 268-NDA-5 Mut, F., 23-FD-3 Navarro, P., 383-MST-14 Ninomiya, T., 236-AFM-5 Ogawa, H., 211-SD-10 Moszczynski, G., 381-MST-11 Muthig, B., 64-AMT-3 Naveira, P., 390-SD-20 Nishida, H., 415-FD-54 Ogawa, M., 45-SATS-2 Mott, D., 252-FD-38 Muthirevula, N., 346-AFM-7 Nawroth, H., 363-FD-50 Nishikawa, H., 24-FD-4, 76-FD-9, 185-FD-24 Ogawa, S., 476-MST-18 Mou, F., 259-GNC-7 Muto, D., 271-PC-18, 303-FD-44 Nayeri, C., 191-FD-30, 490-WE-11 Nishimoto, M., 488-STR-12 Ogawara, K., 125-APA-11 Moureau, V., 250-FD-36, 363-FD-50 Myers, L., 60-AA-2 Neal, C., 302-FD-43 Nishimura, J., 262-HSABP-5/PGC-4 Ogino, Y., 417-FD-56 Mouriaux, F., 379-MAT-8 Mykhaskiv, O., 457-ACD-11 Neel, I., 190-FD-29, 414-FD-5, 417-FD-56 Nitzsche, F., 17-ASC-1, 213-SD-12 Oh, H., 199-MST-3 Movius, I., 426-GNC-28 Nabil, A., 263-IS-4 Neerukatti, R., 411-ASC-4 Nitzsche, J., 332-SD-18 Ohanian, O., 162-SEN-1 Moyes, A., 70-APA-9, 190-FD-29 Naboulsi, S., 90-MAT-3 Negishi, H., 350-APA-33, 488-STR-12 Nivison, S., 307-GNC-10 Ohmichi, Y., 127-APA-13, 239-APA-22, 355-APA-38 M R, D., 441-PDL-13 Nagai, H., 414-FD-5 Nehrenz, M., 45-SATS-2 Noble, A., 51-SRE-1 Ohnishi, N., 328-PDL-9, 417-FD-56, 440-PDL-12 Mueller, J., 317-IS-6, 457-ACD-11 Nagaoka, S., 267-MST-7 Neiferd, D., 319-MDO-8 Nobleheart, W., 422-GNC-24 Okai, K., 446-TES-2 Mueller, R., 316-IS-5 Nagatani, K., 128-APA-14 Neitzel, K., 180-APA-19 Noda, S., 446-TES-2 Okamoto, K., 167-TP-6 Mugnier, P., 306-GNC-9 Nagayama, T., 414-FD-5 Nelessen, A., 44-SATS-1 Noda, T., 176-AMT-8 Okamoto, M., 139-FD-22 Muirhead, K., 29-GTE-1 Nagel, B., 392-STR-10 Nelson, D., 459-AFM-12 Nolen, C., 473-GTE-11 Okamoto, T., 434-PC-24 Mukherjee, D., 471-GNC-34 Naghipour, P., 488-STR-12 Nelson, M., 348-AMT-12 Nomoto, M., 125-APA-11 Okasinski, J., 379-MAT-8 Mulani, S., 93-NDA-1, 151-NDA-3, 380-MDO-10 Naik, K., 44-SATS-1 Nesbitt, E., 235-AA-7, 289-AA-9 Nomura, S., 164-SRE-3, 334-TP-10 Okhovat, S., 85-HSABP-2, 377-HSABP-7 Mulder, A., 278-SD-15 Naik, R., 90-MAT-3 Nessler, C., 399-ABPSI-2 Nonaka, S., 296-APA-31 Okuizumi, N., 275-SCS-4 Mulder, M., 317-IS-6, 322-MST-9, 402-AFM-9, Naitoh, K., 434-PC-24 Neves, F., 335-UMS-10 Nonomura, T., 415-FD-54 Ol, M., 26-FD-7, 27-GEPC-1, 80-FD-14, 191-FD-30, 468-GNC-31 Najafi, A., 319-MDO-8 New, T., 122-AMT-5, 187-FD-26, 336-WE-8 Norato, J., 380-MDO-10 303-FD-44 Muliana, A., 333-SUR-2/MAT-7 Naka, Y., 69-APA-8/AA-3 Newman, D., 417-FD-56 Norriega, A., 466-GNC-29 Olander Burak, M., 134-FD-16 Mullen, D., 190-FD-29 Nakagami, S., 262-HSABP-5/PGC-4, Newman, J., 23-FD-3, 299-FD-39 Norwood, D., 218-STR-7 Olcmen, S., 247-FD-33, 364-FD-51 Mulleners, K., 26-FD-7, 67-APA-6, 248-FD-34 314-HSABP-6/PGC-5 Newnam, K., 440-PDL-12, 485-PDL-15 Notestein, D., 243-DE-3 Olejnik, P., 383-MST-14 Müller, H., 363-FD-50 Nakakita, K., 176-AMT-8 New-Tolley, M., 65-AMT-4 Nouri, A., 246-FD-32 Oleson, S., 105-SRE-2 Muller, S., 444-SD-24 Nakamura, T., 169-UMS-5 Ng, B., 336-WE-8 Novikov, A., 29-GTE-1 Olinger, D., 449-WE-10 Müller, S., 255-GNC-3 Nakamura, Y., 26-FD-7, 323-MST-10 Ngo, C., 348-AMT-12 Novikova, Y., 29-GTE-1 Olinick, E., 215-SEN-2 Mulvihill, C., 438-PC-28 Nakashino, K., 275-SCS-4 Nguyen, G., 57-TP-13/MDO-13 Noyes, C., 224-WE-4 Olivari, M., 266-MST-6 Munafò, A., 274-PDL-7 Nalim, M., 427-GTE-9/PGC-6, 485-PDL-15 Nguyen, H., 170-WE-2 N S, V., 127-APA-13 Oliveira, H., 426-GNC-28 Munday, P., 359-FD-46 Nambu, T., 350-APA-33 Nguyen, N., 107-STR-4, 317-IS-6, 367-GNC-16, Null, C., 269-NDA-6 Oliver, T., 268-NDA-5 Mundis, N., 22-FD-2, 292-APA-27 Namdeo, S., 44-SATS-1, 209-SATS-5 389-SD-19, 421-GNC-23, 422-GNC-24, 442-SD-22 Nuseibeh, B., 216-SOF-4 Olivieri, A., 406-APA-40 Author/Session Chair Index Oliviu, S., 353-APA-36 Padhee, S., 53-STR-2, 107-STR-4 Park, S., 134-FD-16, 322-MST-9, 471-GNC-34 Peral, E., 157-SCS-2 Plemmons, D., 64-AMT-3, 123-AMT-6 Ollar, J., 320-MDO-9 Padhi, R., 310-GNC-13, 356-ASC-5, 373-GNC-22 Parnas, L., 218-STR-7 Peraza Hernandez, E., 461-ASC-6 Plötner, K., 199-MST-3 Ollivier Gooch, C., 24-FD-4, 184-FD-23, 477-MVC-5 Padthe, A., 289-AA-9 Parque, V., 329-SCS-5 Perdikaris, P., 324-NDA-7 Plumley, R., 27-GEPC-1 Olsen, C., 373-GNC-22 Pagani, A., 106-STR-3 Parrish, R., 192-GT-5 Pereira, R., 387-PDL-10, 440-PDL-12 Poenitzsch, V., 70-APA-9 Omar, K., 32-ISC-1 Pai, Y., 313-GTE-7 Paryz, R., 83-GT-11 Perez, R., 401-ACD-10 Poggie, J., 137-FD-19, 189-FD-28, 273-PDL-6, Omar, S., 310-GNC-13 Painter, D., 373-GNC-22 Parziale, N., 11-AMT-1 Perez Rocha, A., 316-IS-5 327-PDL-8, 388-PDL-11 Ombrello, T., 85-HSABP-2, 94-PC-5/PGC-2, 99-PDL-2, Pak, C., 211-SD-10 Paschereit, C., 111-WE-1, 191-FD-30, 363-FD-50, Perullo, C., 84-GTE-2, 472-GTE-10 Pohl, M., 72-ASC-2 377-HSABP-7, 434-PC-24, 480-PC-31 Palacios, R., 146-MDO-4, 211-SD-10, 330-SD-16, 490-WE-11 Peter, J., 293-APA-28 Pohya, A., 400-ACD-9 Ondruss, V., 83-GT-11 336-WE-8, 390-SD-20, 391-SD-21, 490-WE-11 Pasiliao, C., 36-MAT-1, 294-APA-29, 405-APA-39 Peters, J., 164-SRE-3 Poinsatte, P., 251-FD-37 Oppenheimer, M., 256-GNC-4, 311-GNC-14 Palaszewski, B., 105-SRE-2 Pasque, P., 284-UMS-9 Petersen, E., 97-PC-8, 205-PC-15, 363-FD-50, Poinsot, T., 386-PC-23 Opromolla, R., 215-SEN-2 Palazotto, A., 212-SD-11, 280-STR-8, 281-SUR-1, Passalacqua, F., 490-WE-11 435-PC-25, 438-PC-28, 481-PC-32 Pokhrel, M., 8-ACD-1 Orient, G., 202-NDA-4 333-SUR-2/MAT-7, 390-SD-20 Passe, B., 377-HSABP-7 Peterson, D., 85-HSABP-2, 364-FD-51 Pol, S., 395-WE-9 Orlov, O., 269-NDA-6 Palchekovskaya, N., 186-FD-25 Pastor, P., 402-AFM-9 Peterson, J., 369-GNC-18 Polaki, D., 218-STR-7 Orme, M., 379-MAT-8 Paley, D., 131-EDU-3, 366-GNC-15 Patchett, C., 200-MST-4 Peterson, L., 210-SCS-3 Polanka, M., 98-PC-9, 193-GTE-4, 195-HSABP-4/PGC-3, Orr, M., 120-ACD-5 Palies, P., 385-PC-22 Patel, A., 33-ISC-2 Petitgenet, V., 174-ACD-6 313-GTE-7, 314-HSABP-6/PGC-5 Orra, T., 61-ACD-3, 429-MDO-11 Palla, A., 388-PDL-11 Patel, D., 119-AA-4, 280-STR-8 Petrov, A., 125-APA-11 Polivanov, P., 178-APA-17 Orrell, G., 283-UMS-8 Palluconi, S., 123-AMT-6 Patel, K., 221-UMS-6 Petterson, P., 434-PC-24 Pollini, L., 253-GNC-1, 266-MST-6 Osborne, B., 125-APA-11 Palmer, G., 167-TP-6 Patel, N., 373-GNC-22 Petterson, R., 17-ASC-1 Polsky, S., 242-APA-26 Osei Dwumah, I., 31-HSABP-1 Palmer, T., 142-HSABP-3 Paterson, E., 223-WE-3 Pfeifer, S., 324-NDA-7 Pomeroy, B., 296-APA-31 Oshima, I., 362-FD-49 Palmieri, F., 123-AMT-6 Patil, A., 345-ACD-8 Pfifer, H., 346-AFM-7 Poncet-Montanges, A., 23-FD-3 Oshima, N., 66-APA-5 Palmore, J., 418-FD-57 Patil, K., 64-AMT-3 Pfitzner, M., 363-FD-50 Ponchak, D., 18-CMS-1 Ossmann, D., 395-WE-9 Pan, Q., 170-WE-2, 283-UMS-8 Patil, M., 159-SD-8 Phan, N., 165-STR-5, 280-STR-8 Pond, J., 284-UMS-9 Ostermann, F., 191-FD-30 Pan, S., 77-FD-11 Patnaik, A., 97-PC-8 Phelps, N., 150-NDA-2/MDO-5 Pons Lorente, A., 385-PC-22 Ostieri, M., 239-APA-22 Pan, Y., 373-GNC-22 Patterson, M., 54-TFPC-1 Philips, D., 408-APA-42 Pontillo, A., 10-AFM-1

189 Östlund, J., 134-FD-16 Panagiotou, P., 345-ACD-8 Patterson, R., 182-ASC-3 Phillips, A., 87-ISC-4 Pool, D., 322-MST-9 Oterkus, E., 106-STR-3, 145-MAT-4 Panda, J., 348-AMT-12 Paul, M., 164-SRE-3 Phillips, F., 411-ASC-4 Poole, D., 91-MDO-3 Oterkus, S., 52-STR-1 Pande, A., 359-FD-46 Paul, S., 62-ACD-4 Phillips, M., 236-AFM-5, 459-AFM-12 Poovathingal, S., 448-TP-12 Otsuka, H., 128-APA-14 Pandey, V., 268-NDA-5 Paulos, J., 291-AFM-6 Phillips, T., 477-MVC-5 Pope, K., 167-TP-6 Otto, S., 73-EDU-2/DE-1 Panesi, M., 55-TP-1, 208-PDL-5, 274-PDL-7, Paunicka, J., 50-SOF-1, 104-SOF-2 Phillips, W., 352-APA-35 Popolan-Vaida, D., 154-PC-12 Oudin, S., 254-GNC-2 334-TP-10, 394-TP-11, 484-PDL-14 Pavese, C., 449-WE-10 Phong, V., 7-AA-1, 60-AA-2 Popov, G., 29-GTE-1 Ouellette, J., 10-AFM-1 Pang, Q., 24-FD-4 Pawletta, T., 265-MST-5 Piatak, D., 348-AMT-12 Popov, P., 203-PC-13 Ouwerkerk, J., 379-MAT-8 Pang, Y., 306-GNC-9 Paxson, D., 262-HSABP-5/PGC-4, 314-HSABP-6/PGC-5, Picelli, R., 380-MDO-10 Popovici, A., 322-MST-9 Ovec, N., 305-GNC-8 Paniagua, G., 29-GTE-1, 262-HSABP-5/PGC-4, 399-ABPSI-2, 427-GTE-9/PGC-6 Pickles, J., 140-GT-4 Portapas, V., 147-MST-1 Overmeyer, A., 460-APA-45 313-GTE-7 Payot, A., 350-APA-33 Pierre, L., 334-TP-10 Porter, K., 137-FD-19 Owen, M., 379-MAT-8 Pankonien, A., 102-SD-5, 366-GNC-15 Paz, A., 105-SRE-2 Pilawa-Podgurski, R., 81-GEPC-2 Porto, F., 350-APA-33, 352-APA-35, 381-MST-11, Owens, D., 347-AFM-8 Panneer Chelvam, P., 208-PDL-5 P B, S., 426-GNC-28 Pineda, E., 488-STR-12 430-MST-15 Owhadi, H., 268-NDA-5 Pant, K., 391-SD-21 Peace, J., 474-HSABP-9/PGC-8 Pineda, M., 277-SD-14 Poryzala, T., 395-WE-9 Oza, U., 408-APA-42 Pantano, C., 274-PDL-7 Peach, B., 167-TP-6 Pinheiro, J., 322-MST-9 Porziani, S., 376-GTE-8 Ozawa, T., 219-TP-7 Panther, C., 51-SRE-1 Pechlivanoglou, G., 111-WE-1, 490-WE-11 Pinier, J., 296-APA-31, 352-APA-35 Potapchik, A., 125-APA-11 Ozdemir, H., 490-WE-11 Papamoschou, D., 7-AA-1, 60-AA-2 Peck, M., 124-AMT-7/GT-3, 156-SATS-4, 256-GNC-4, Pinkerman, C., 291-AFM-6 Pothen, A., 470-GNC-33 Ozgen, S., 449-WE-10 Pappa, R., 210-SCS-3 259-GNC-7, 424-GNC-26, 468-GNC-31 Pinna, F., 462-FD-10 Potturi, A., 437-PC-27 Ozguner, U., 104-SOF-2, 216-SOF-4, 222-UMS-7 Paradissis, D., 335-UMS-10 Pedrazzani, J., 162-SEN-1 Pinto, R., 236-AFM-5 Powell, J., 348-AMT-12 Ozoroski, L., 69-APA-8/AA-3 Parambil, N., 165-STR-5 Peet, Y., 179-APA-18, 285-WE-5, 395-WE-9 Pipitsunthonsan, P., 315-ICC-1 Powell, O., 142-HSABP-3 P, M., 441-PDL-13 Paraschivoiu, I., 111-WE-1 Peherstorfer, B., 475-MDO-12/NDA-10 Pires, O., 223-WE-3, 490-WE-11 Powell, R., 121-AFM-3 P, S., 129-APA-15 Paredes, P., 21-FD-1 Pei, J., 209-SATS-5 Pirrera, A., 46-SCS-1, 461-ASC-6 Power, G., 39-MVC-1 P. Chiozzotto, G., 8-ACD-1 Parenteau, M., 239-APA-22 Pekardan, C., 57-TP-13/MDO-13 Pittman, J., 156-SATS-4 Powers, K., 238-APA-21 Pachter, M., 253-GNC-1, 471-GNC-34 Parise, T., 438-PC-28 Pellegrino, S., 46-SCS-1, 275-SCS-4, 329-SCS-5 Pitz, R., 65-AMT-4, 98-PC-9, 439-PC-29 Poyraz, U., 31-HSABP-1 Pachuilo, M., 484-PDL-14 Parish, J., 305-GNC-8 Peltier, S., 134-FD-16 Pizzella, M., 137-FD-19 Prabhakar, N., 169-UMS-5, 373-GNC-22 Packan, D., 485-PDL-15 Park, C., 38-MDO-2, 151-NDA-3, 212-SD-11 Pendleton, D., 32-ISC-1 Pizzo, M., 56-TP-2 Prabhakar, P., 107-STR-4 Packard, N., 360-FD-47 Park, H., 145-MAT-4 Peng, A., 57-TP-13/MDO-13 Plaidoung, J., 315-ICC-1 Prabhu, D., 334-TP-10 Packard, T., 105-SRE-2 Park, J., 429-MDO-11 Peng, X., 13-APA-1 Plank, B., 90-MAT-3 Pradhan, S., 77-FD-11, 240-APA-23/FD-31 Pack Melton, L., 78-FD-12, 83-GT-11 Park, M., 23-FD-3, 241-APA-24 Peng, Z., 286-WE-6 Plante, F., 239-APA-22 Prakash, A., 44-SATS-1 Author/Session Chair Index Prakash, N., 36-MAT-1 Rahmat-Samii, Y., 157-SCS-2 Reardon, S., 265-MST-5 Riemenschneider, J., 72-ASC-2 Rosen, C., 374-GT-8 Prakash, R., 448-TP-12 Rai, M., 350-APA-33 Reasoner, J., 431-MST-16 Rigas, G., 462-FD-10 Rosenberg, A., 449-WE-10 Prasad, A., 313-GTE-7 Rais-Rohani, M., 202-NDA-4 Reasor, D., 68-APA-7 Rigby, K., 321-MST-8 Ross, J., 260-GT-6/AMT-10, 348-AMT-12 Prasad, C., 173-AA-5 Raj, P., 174-ACD-6 Reed, C., 246-FD-32, 361-FD-48 Righi, M., 49-SD-3, 213-SD-12, 459-AFM-12 Rossi, A., 412-EXPL-2 Prasad, R., 277-SD-14 Raja, L., 43-PDL-1, 208-PDL-5, 274-PDL-7, Reed, E., 354-APA-37, 460-APA-45 Rijndorp, T., 317-IS-6 Rossman, G., 121-AFM-3, 219-TP-7 Prazenica, R., 168-UMS-4, 169-UMS-5, 373-GNC-22 440-PDL-12, 484-PDL-14 Reed, H., 70-APA-9, 190-FD-29, 301-FD-42 Riley, L., 142-HSABP-3 Rothermel, T., 119-AA-4 Prenter, R., 191-FD-30, 376-GTE-8, 416-FD-55 Rajadas, A., 411-ASC-4 Reed, J., 257-GNC-5, 310-GNC-13, 372-GNC-21, Rinauto, B., 284-UMS-9 Rouseau, C., 52-STR-1 Probe, A., 216-SOF-4 Rajagopal, K., 466-GNC-29 424-GNC-26 Rinehart, A., 26-FD-7 Roy, A., 56-TP-2, 262-HSABP-5/PGC-4 Provchy, Z., 281-SUR-1 Rajaram, K., 254-GNC-2 Reeder, M., 64-AMT-3, 122-AMT-5, 129-APA-15 Ringertz, U., 442-SD-22 Roy, C., 185-FD-24, 241-APA-24, 295-APA-30 Provenza, A., 81-GEPC-2 Rajasegar, R., 388-PDL-11, 485-PDL-15 Reeger, J., 426-GNC-28 Rinoie, K., 407-APA-41 Roy, R., 285-WE-5 Pruter, I., 265-MST-5 Rajendran, L., 64-AMT-3, 440-PDL-12 Reffo, A., 412-EXPL-2 Risse, K., 400-ACD-9 Roy, S., 12-AMT-2, 37-MDO-1, 97-PC-8, 197-MAT-5, Pryor, O., 154-PC-12, 438-PC-28 Raju, I., 52-STR-1, 217-STR-6 Regan, C., 346-AFM-7 Ritos, K., 186-FD-25 262-HSABP-5/PGC-4, 320-MDO-9, 387-PDL-10, Pullan, G., 201-MVC-4 Raju, M., 271-PC-18 Reich, G., 72-ASC-2, 102-SD-5, 356-ASC-5, 366-GNC-15 Ritter, M., 160-SD-9 404-AMT-14 Pulliam, T., 16-APA-4, 241-APA-24 Rakow, A., 46-SCS-1 Reichstein, T., 223-WE-3 Rivera, K., 316-IS-5 Roza, M., 430-MST-15 Puranik, T., 196-IS-3 Rallabhandi, S., 14-APA-2 Reid, D., 205-PC-15 Rivers, M., 28-GT-1, 78-FD-12 RS, C., 305-GNC-8 Puri, K., 22-FD-2 Ralph, J., 121-AFM-3 Rein, K., 262-HSABP-5/PGC-4, 270-PC-17 Rizzetta, D., 75-FD-8 Ru, P., 222-UMS-7, 371-GNC-20 Purkayastha, A., 111-WE-1 Ramachandran, A., 145-MAT-4 Ren, J., 14-APA-2 Rizzi, A., 290-ACD-7 Rubino, E., 28-GT-1, 237-AMT-9 Purkey, A., 137-FD-19 Ramamurti, R., 16-APA-4, 181-APA-20 Rendall, T., 13-APA-1, 91-MDO-3, 149-MVC-3, Rizzi, S., 288-AA-8 Rudnik, R., 69-APA-8/AA-3 Putnam, Z., 63-AFM-2 Raman, V., 40-PC-2, 94-PC-5/PGC-2, 166-TP-5, 159-SD-8, 350-APA-33 Rizzo, L., 325-OPS-1 Rudolf, C., 374-GT-8 P V, S., 372-GNC-21 270-PC-17, 427-GTE-9/PGC-6 Rennie, M., 374-GT-8 Roa, M., 326-PC-20 Ruel, S., 256-GNC-4 Pytel, D., 109-TP-4 Ramanathan, G., 303-FD-44 Resor, M., 85-HSABP-2 Roberts, A., 283-UMS-8 Ruetten, M., 419-FD-58 Qi, C., 307-GNC-10 Ramanujam, G., 490-WE-11 Restrepo, C., 368-GNC-17 Roberts, R., 476-MST-18 Ruff, R., 200-MST-4, 382-MST-12 Qi, X., 198-MDO-6 Ramesh, K., 248-FD-34 Retter, J., 12-AMT-2 Roberts, W., 12-AMT-2, 203-PC-13, 427-GTE-9/PGC-6 Ruiz, A., 383-MST-14 Qian, C., 157-SCS-2 Ramezanian, D., 299-FD-39 Reuter, C., 435-PC-25, 481-PC-32 Robertson, C., 308-GNC-11 Ruleva, L., 66-APA-5

190 Qian, J., 130-DE-2 Ramnath, M., 52-STR-1 Reuter, R., 380-MDO-10 Robertson, E., 467-GNC-30 Rumpfkeil, M., 38-MDO-2, 66-APA-5, 478-NDA-11 Qin, C., 224-WE-4 Ramos Valle, L., 10-AFM-1 Reutzel, T., 220-TP-8 Robinson, A., 142-HSABP-3 Rumsey, C., 241-APA-24 Qin, N., 61-ACD-3, 120-ACD-5, 477-MVC-5 Ranatunga, V., 107-STR-4 Reveles, J., 46-SCS-1 Robinson, C., 39-MVC-1 Runco, C., 33-ISC-2 Qiu, Z., 133-FD-15 Rancourt, D., 174-ACD-6 Revol, V., 90-MAT-3 Robinson, M., 177-APA-16 Runkel, F., 72-ASC-2 Qu, K., 352-APA-35 Ranjan, D., 384-NDA-8 Reza Ahrabi, B., 133-FD-15 Robinson, S., 240-APA-23/FD-31, 322-MST-9 Runyon, B., 211-SD-10 Qu, Q., 304-FD-45, 353-APA-36, 362-FD-49, Rankin, B., 94-PC-5/PGC-2, 95-PC-6, 194-GTE-5 Rezaei, A., 179-APA-18 Robison, R., 180-APA-19 Ruppert, L., 162-SEN-1 405-APA-39, 407-APA-41 Ransom, J., 90-MAT-3 Rezaian, E., 252-FD-38 Rock, N., 42-PC-4 Rusanov, V., 269-NDA-6 Quach, C., 432-MST-17 Rao, A., 347-AFM-8, 369-GNC-18 Rezgui, D., 276-SD-13 Rodi, P., 31-HSABP-1 Ruscher, C., 60-AA-2, 141-GTE-3, 173-AA-5 Quackenbush, T., 16-APA-4 Rasheed, A., 285-WE-5 Rhee, D., 313-GTE-7, 376-GTE-8 Rodrigues, C., 465-FD-62 Rusovici, R., 212-SD-11, 278-SD-15 Quek, J., 169-UMS-5 Rashid, A., 284-UMS-9 Rhew, R., 375-GT-9 Rodriguez, S., 224-WE-4 Russell, S., 392-STR-10 Quest, J., 83-GT-11 Rasmussen, F., 170-WE-2, 224-WE-4 Rhode, M., 374-GT-8 Roelofs, M., 120-ACD-5 Russo, L., 145-MAT-4 Quindlen, J., 471-GNC-34 Rassaian, M., 107-STR-4 Rhudy, M., 162-SEN-1 Rogers, D., 297-APA-32 Rutherford, M., 374-GT-8 Quinlan, J., 53-STR-2, 54-TFPC-1 Rastgoftar, H., 371-GNC-20 Ribeiro, A., 241-APA-24, 353-APA-36, 355-APA-38 Rogers, J., 148-MST-2, 425-GNC-27, 471-GNC-34 Rutherford, S., 374-GT-8 Quintana, A., 17-ASC-1 Rastkar, S., 147-MST-1, 487-SD-26 Ricci, S., 443-SD-23 Roget, B., 71-APA-10 Rutledge, J., 313-GTE-7 Quix, H., 83-GT-11 Ratheesh, A., 44-SATS-1, 45-SATS-2 Ricciardi, A., 277-SD-14 Rogoshchenkov, N., 289-AA-9 Ruyten, W., 176-AMT-8 Qumar, M., 68-APA-7 Ratnoo, A., 253-GNC-1, 258-GNC-6, 306-GNC-9, Riccobene, L., 443-SD-23 Roizner, F., 160-SD-9, 390-SD-20 Ryan, J., 306-GNC-9 Quon, E., 285-WE-5 370-GNC-19, 470-GNC-33 Rice, B., 134-FD-16 Rokhsaz, K., 332-SD-18, 443-SD-23 Ryan, W., 19-DA-1 Rabey, P., 247-FD-33 Rattan, K., 433-NDA-9 Rice, T., 336-WE-8 Rokita, T., 249-FD-35, 391-SD-21 Rye, J., 317-IS-6 Rabinovitch, J., 362-FD-49 Rauleder, J., 16-APA-4, 127-APA-13 Rich, J., 484-PDL-14 Rollin, V., 333-SUR-2/MAT-7 S, M., 310-GNC-13 Rade, D., 276-SD-13 Raut, A., 407-APA-41 Richard, L., 392-STR-10 Romano, M., 259-GNC-7 Saavedra Garcia, J., 262-HSABP-5/PGC-4 Raﬁ, M., 254-GNC-2, 421-GNC-23 Rautmann, C., 336-WE-8 Richards, K., 177-APA-16 Romero, V., 202-NDA-4 Sabbagh, M., 374-GT-8 Raghavan, S., 102-SD-5 Raveh, D., 48-SD-2 Richards, N., 143-IS-2 Romero Martinez, S., 360-FD-47 Sabouri, M., 394-TP-11 Raghu, S., 87-ISC-4 Raymer, D., 290-ACD-7 Richardson, D., 12-AMT-2 Rooseleer, F., 266-MST-6 Sachdeva, C., 53-STR-2, 107-STR-4, 156-SATS-4 Raghunath, S., 414-FD-5, 462-FD-10 Raymer, E., 290-ACD-7 Richardson, T., 129-APA-15, 366-GNC-15, 402-AFM-9 Roozeboom, N., 260-GT-6/AMT-10, 348-AMT-12 Sachs, G., 458-AFM-11 Ragni, D., 188-FD-27, 288-AA-8 Raz, A., 315-ICC-1 Ricklick, M., 84-GTE-2, 313-GTE-7, 473-GTE-11 Roquemore, M., 96-PC-7 Sachs, W., 179-APA-18 Rahbari, I., 462-FD-10 Razgus, B., 372-GNC-21 Riedel, U., 206-PC-16 Roquemore, W., 154-PC-12, 436-PC-26 Sadique, J., 300-FD-41 Rahimi, M., 154-PC-12, 439-PC-29 Re, B., 477-MVC-5 Riediger, C., 290-ACD-7 Rosario, S., 58-UMS-1 Safta, C., 268-NDA-5 Rahman, M., 246-FD-32, 249-FD-35 Reagan, T., 123-AMT-6 Rieker, G., 136-FD-18 Rose, N., 291-AFM-6 Sagerman, D., 66-APA-5 Author/Session Chair Index Saha, D., 308-GNC-11 Saraf, A., 459-AFM-12 Schikore, K., 131-EDU-3 Secco, N., 91-MDO-3 Shah, P., 142-HSABP-3 Sahai, A., 55-TP-1, 274-PDL-7 Sardeshmukh, S., 94-PC-5/PGC-2, 95-PC-6, Schinwald, C., 199-MST-3 Seckin, S., 189-FD-28 Shah, V., 323-MST-10 Sahin, M., 182-ASC-3 271-PC-18, 385-PC-22, 474-HSABP-9/PGC-8 Schirmer, S., 104-SOF-2 Seeley, B., 54-TFPC-1 Shahpar, S., 22-FD-2, 303-FD-44, Sahni, O., 251-FD-37 Sargsyan, K., 268-NDA-5 Schliesing, J., 389-SD-19 Segarra Torne, A., 323-MST-10 475-MDO-12/NDA-10, 477-MVC-5 Said, A., 446-TES-2 Saric, W., 70-APA-9 Schmid, D., 19-DA-1 Segui, M., 148-MST-2, 200-MST-4 Shaler, K., 111-WE-1 Said, M., 79-FD-13 Sarkar, K., 487-SD-26 Schmidt, D., 204-PC-14, 346-AFM-7 Seidel, G., 36-MAT-1, 89-MAT-2, 318-MAT-6 Shanbhogue, S., 206-PC-16, 386-PC-23, 439-PC-29, Saidi, M., 436-PC-26 Sarkar, P., 365-FD-52 Schmidt, M., 457-ACD-11 Seidel, J., 134-FD-16, 239-APA-22, 242-APA-26, 479-PC-30 Saini, A., 123-AMT-6, 248-FD-34 Sarker, P., 58-UMS-1 Schmidt, O., 173-AA-5 351-APA-34, 417-FD-56 Shao, J., 438-PC-28 Saini, P., 203-PC-13 Sarley, B., 379-MAT-8 Schmiedel, C., 98-PC-9, 313-GTE-7 Seifert, A., 416-FD-55 Sharbatdar, M., 184-FD-23 Saito, Y., 275-SCS-4 Sarojini, D., 120-ACD-5, 174-ACD-6 Schmisseur, J., 137-FD-19, 189-FD-28, 414-FD-5 Seiler, P., 346-AFM-7 Shariff, K., 210-SCS-3 Saka, P., 374-GT-8 Sartor, P., 320-MDO-9 Schmit, R., 289-AA-9 Seino, K., 329-SCS-5 Sharma, A., 119-AA-4, 365-FD-52, 449-WE-10, Sakai, T., 219-TP-7 Sasaki, D., 139-FD-22, 473-GTE-11, 476-MST-18 Schneck, W., 399-ABPSI-2 Seitzman, J., 11-AMT-1, 41-PC-3, 42-PC-4 484-PDL-14 Sakamoto, H., 157-SCS-2, 275-SCS-4 Sasanapuri, B., 49-SD-3 Schneegans, A., 290-ACD-7 Sekimoto, S., 415-FD-54 Sharma, M., 379-MAT-8, 394-TP-11 Sakamoto, N., 45-SATS-2 Sasiadek, J., 470-GNC-33 Schneider, G., 56-TP-2, 394-TP-11, 436-PC-26 Selcan, C., 109-TP-4 Sharma, S., 238-APA-21, 357-EXPL-1, 412-EXPL-2 Sakaue, H., 70-APA-9, 109-TP-4, 176-AMT-8, 237-AMT-9 Sathianarayanan, A., 238-APA-21 Schneider, S., 21-FD-1 Seleson, P., 324-NDA-7 Sharma, T., 45-SATS-2, 156-SATS-4 Sakuranaka, N., 456-ABPSI-3 Sathyan, A., 428-IS-9 Schneider, V., 200-MST-4 Selig, M., 296-APA-31 Sharma, V., 101-SD-4/APA-47 Salah, S., 489-TES-4 Satija, A., 12-AMT-2, 261-GTE-6 Schneider, W., 211-SD-10 Selim, M., 213-SD-12 Sharma Subedi, C., 421-GNC-23 Salama, F., 366-GNC-15 Sato, K., 191-FD-30 Schoenenberger, M., 121-AFM-3, 297-APA-32 Selimov, A., 36-MAT-1 Sharpe, J., 29-GTE-1 Salazar, R., 62-ACD-4 Sato, S., 440-PDL-12 Scholten, W., 182-ASC-3 Sellers, J., 129-APA-15 Shashurin, A., 155-PDL-3 Saleem, M., 189-FD-28 Satou, Y., 275-SCS-4 Schonebaum, G., 263-IS-4 Sellers, M., 176-AMT-8, 348-AMT-12 Shaver, J., 381-MST-11 Salem, A., 202-NDA-4 Sauder, J., 157-SCS-2, 275-SCS-4 Schreck, S., 111-WE-1, 223-WE-3, 490-WE-11 Sells, R., 432-MST-17 Shay, N., 416-FD-55 Salgueiro, S., 290-ACD-7 Saussie, D., 425-GNC-27 Schreiter, K., 255-GNC-3 Selva, D., 196-IS-3, 243-DE-3 Sheaf, C., 177-APA-16 Salguero, R., 162-SEN-1 Saverin, J., 111-WE-1 Schroeder, B., 202-NDA-4 Selvaraj, P., 436-PC-26 Sheahan, S., 196-IS-3, 222-UMS-7 Salita, M., 167-TP-6, 219-TP-7 Savill, A., 38-MDO-2 Schroeder, J., 199-MST-3, 266-MST-6, 323-MST-10 Semak, V., 484-PDL-14 Sheeley, J., 56-TP-2, 374-GT-8

191 Sallam, K., 480-PC-31 Savin, E., 151-NDA-3 Schroeder, K., 48-SD-2 Senck, S., 90-MAT-3 Sheikh-AlShabab, A., 187-FD-26 Salmon, J., 80-FD-14 Savvaris, A., 215-SEN-2 Schroeder, O., 167-TP-6 Sener, O., 286-WE-6 Shelekhov, G., 359-FD-46 Saltzman, D., 220-TP-8 Sawant, S., 108-TP-3 Schuck, M., 281-SUR-1 Senesky, D., 145-MAT-4 Shen, L., 200-MST-4, 371-GNC-20 Salvador, P., 388-PDL-11 Sawyer, J., 207-PDL-4 Schuessler, B., 123-AMT-6 Sengezer, E., 36-MAT-1 Shen, X., 111-WE-1 Samantaray, S., 356-ASC-5 Sayani, A., 67-APA-6 Schuet, S., 254-GNC-2, 371-GNC-20 Sengupta, A., 75-FD-8 Sheplak, M., 123-AMT-6 Samaratunga, D., 411-ASC-4 Saydam, S., 105-SRE-2 Schuh, M., 312-GT-7/AMT-11 Sengupta, P., 267-MST-7 Sheppard, I., 383-MST-14 Samimy, M., 7-AA-1, 273-PDL-6, 387-PDL-10, S B, V., 127-APA-13 Schultz, M., 107-STR-4 Senol, M., 128-APA-14 Sher, E., 206-PC-16 415-FD-54 Scalo, C., 25-FD-6, 55-TP-1, 119-AA-4, 234-AA-6, Schultz, V., 221-UMS-6 Sensmeier, M., 445-STR-11 Sherer, S., 76-FD-9, 353-APA-36, 355-APA-38 Sammak, S., 246-FD-32 359-FD-46, 420-FD-59, 462-FD-10 Schulz, J., 167-TP-6 Seo, M., 305-GNC-8 Sherif, S., 167-TP-6, 447-TES-3 Sammartano, Q., 236-AFM-5 Schaefer, J., 420-FD-59 Schulze, P., 10-AFM-1, 266-MST-6, 403-AFM-10 Serfaty, R., 363-FD-50 Sherman, K., 205-PC-15 Samtaney, R., 246-FD-32 Schaffarczyk, A., 223-WE-3 Schumaker, S., 326-PC-20 Serpieri, J., 361-FD-48, 462-FD-10 Sherman, T., 283-UMS-8 Sanchez, A., 25-FD-6 Schairer, E., 122-AMT-5, 260-GT-6/AMT-10 Schuster, W., 60-AA-2, 289-AA-9 Sertse, H., 145-MAT-4, 333-SUR-2/MAT-7 Shi, A., 192-GT-5 Sanchez, R., 211-SD-10 Schale, R., 435-PC-25 Schütt, M., 470-GNC-33 Sescu, A., 21-FD-1, 138-FD-20, 302-FD-43 Shi, J., 56-TP-2, 256-GNC-4 Sander, T., 109-TP-4 Scharfenberg, A., 87-ISC-4 Schuurman, M., 180-APA-19 Seshadri, B., 411-ASC-4 Shi, L., 344-ABPSI-1 Sanders, D., 399-ABPSI-2 Scharnhorst, R., 137-FD-19 Schwartz, D., 48-SD-2 Seshadri, P., 213-SD-12 Shi, S., 122-AMT-5 Sanders, G., 51-SRE-1 Schatzman, D., 416-FD-55 Schwartzentruber, T., 166-TP-5, 448-TP-12 Sesha Giri, K., 12-AMT-2 Shih, T., 246-FD-32 Sanei, S., 488-STR-12 Schauer, F., 94-PC-5/PGC-2, 141-GTE-3, Schwarz, T., 410-APA-44/FD-53 Seth, D., 464-FD-61 Shim, D., 169-UMS-5, 255-GNC-3, 263-IS-4, Sanford, G., 46-SCS-1 195-HSABP-4/PGC-3, 262-HSABP-5/PGC-4, Schwenke, D., 334-TP-10 Sethuraman, L., 224-WE-4 307-GNC-10 Sangid, M., 214-SE-2 314-HSABP-6/PGC-5, 399-ABPSI-2, Schwer, D., 262-HSABP-5/PGC-4 Seubers, H., 490-WE-11 Shim, S., 305-GNC-8, 306-GNC-9 Sankar, L., 460-APA-45 427-GTE-9/PGC-6, 474-HSABP-9/PGC-8 Schwille, J., 220-TP-8 Seubert, C., 368-GNC-17 Shima, T., 253-GNC-1, 255-GNC-3, 370-GNC-19 Sankaran, R., 480-PC-31 Schauerhamer, D., 240-APA-23/FD-31 Schwinn, K., 94-PC-5/PGC-2 Sevier, A., 297-APA-32 Shimada, T., 150-NDA-2/MDO-5 Sankaran, V., 22-FD-2, 95-PC-6, 271-PC-18, 272-PC-19, Scheerer, M., 90-MAT-3 Schwochow, J., 444-SD-24 Sevil, H., 403-AFM-10 Shimazaki, S., 191-FD-30 365-FD-52, 386-PC-23, 437-PC-27, 483-PC-34 Schelley, R., 64-AMT-3 Sclafani, A., 241-APA-24 Seymour, J., 175-AFM-4, 236-AFM-5 Shimizu, Y., 329-SCS-5 Sankararaman, S., 110-UMS-2, 423-GNC-25 Schellhase, K., 89-MAT-2, 333-SUR-2/MAT-7 Scopelliti, D., 17-ASC-1 Sforzo, B., 41-PC-3, 121-AFM-3 Shimoda, Y., 45-SATS-2 Santangelo, A., 45-SATS-2, 100-SATS-3 Schelling, S., 423-GNC-25, 471-GNC-34 Scott, W., 374-GT-8 Shaat, M., 89-MAT-2, 197-MAT-5, 217-STR-6 Shimodaira, K., 446-TES-2 Santarpia, E., 218-STR-7 Scheneman, B., 120-ACD-5 Scott-Emuakpor, O., 211-SD-10, 280-STR-8, 318-MAT-6 Shademan, M., 136-FD-18 Shimoyama, K., 69-APA-8/AA-3, 139-FD-22, Santer, M., 157-SCS-2 Schetz, J., 146-MDO-4 Scotti, A., 49-SD-3 Shaferman, V., 253-GNC-1, 370-GNC-19 473-GTE-11 Sanyal, A., 258-GNC-6 Schierman, J., 143-IS-2 Sealy, W., 362-FD-49 Shaffer, J., 202-NDA-4 Shin, D., 204-PC-14 Author/Session Chair Index Shin, H., 255-GNC-3 Singh, I., 129-APA-15 Song, P., 47-SD-1/APA-46 Stanley, S., 474-HSABP-9/PGC-8 Strike, J., 82-GT-2 Shin, S., 196-IS-3, 278-SD-15, 331-SD-17, 351-APA-34 Singh, K., 48-SD-2, 146-MDO-4, 445-STR-11 Song, R., 333-SUR-2/MAT-7 Stansbury, R., 283-UMS-8 Stroosma, O., 317-IS-6 Shingin, H., 125-APA-11 Singh, N., 166-TP-5, 448-TP-12 Song, T., 381-MST-11 Starcke, J., 206-PC-16 Su, W., 158-SD-7, 276-SD-13, 278-SD-15, 330-SD-16, Shipeng, L., 418-FD-57 Singh, P., 16-APA-4 Song, W., 177-APA-16 Starikovskiy, A., 274-PDL-7, 327-PDL-8, 328-PDL-9, 366-GNC-15, 442-SD-22 Shish, K., 254-GNC-2, 371-GNC-20 Singh, R., 24-FD-4, 130-DE-2, 184-FD-23 Song, Y., 48-SD-2, 480-PC-31 388-PDL-11, 485-PDL-15 Subbarao, K., 222-UMS-7, 371-GNC-20 Shishko, R., 105-SRE-2 Singh, S., 215-SEN-2 Sorensen, N., 223-WE-3 Starin, S., 468-GNC-31 Subramaniam, V., 208-PDL-5 Shmilovich, A., 78-FD-12 Singhal, A., 415-FD-54 Sorgenfrei, M., 45-SATS-2 Starke, G., 60-AA-2 Subramanian, S., 29-GTE-1 Shneider, M., 65-AMT-4, 207-PDL-4, 484-PDL-14 Sinnige, T., 288-AA-8 Sorrells, T., 34-ISC-3 Starr, S., 51-SRE-1 Subraminian, G., 45-SATS-2 Short, E., 167-TP-6 Sinske, J., 444-SD-24 Sosa, J., 94-PC-5/PGC-2, 438-PC-28 Staruk, W., 211-SD-10 Sudani, N., 28-GT-1 Shrestha, U., 154-PC-12 Sipahi, R., 367-GNC-16 Sostaric, R., 368-GNC-17, 467-GNC-30 Stastny, T., 371-GNC-20 Suh, P., 391-SD-21, 422-GNC-24 Shtessel, Y., 402-AFM-9 Sippel, T., 205-PC-15 Sotak, M., 315-ICC-1 Stechmann, D., 474-HSABP-9/PGC-8 Suhir, E., 269-NDA-6 Shuai, S., 77-FD-11 Sirignano, W., 203-PC-13 Soteriou, M., 418-FD-57 Steck, J., 168-UMS-4, 254-GNC-2, 389-SD-19, Suikat, R., 265-MST-5 Shuang, W., 308-GNC-11 Sirohi, J., 43-PDL-1 Soto, O., 23-FD-3 421-GNC-23 Suleman, A., 182-ASC-3 Shweyk, K., 347-AFM-8, 402-AFM-9 Sisler, A., 195-HSABP-4/PGC-3 Sotoudeh, Z., 102-SD-5, 158-SD-7, 391-SD-21 Stefani, F., 167-TP-6, 219-TP-7 Sullivan, J., 123-AMT-6 Shyam, V., 26-FD-7 Sitaraman, J., 71-APA-10, 292-APA-27, Sou, A., 362-FD-49 Stefanski, D., 71-APA-10, 242-APA-26, 292-APA-27, Sultan, C., 291-AFM-6 Siddiqui, M., 285-WE-5 410-APA-44/FD-53, 490-WE-11 Soudakov, V., 125-APA-11, 178-APA-17 302-FD-43 Summers, C., 57-TP-13/MDO-13 Sidey, J., 96-PC-7, 385-PC-22 Sizemore, A., 383-MST-14 Soueidan, A., 68-APA-7 Steinberg, A., 203-PC-13 Sun, D., 254-GNC-2, 289-AA-9, 335-UMS-10 Sidhu, J., 120-ACD-5 Sizoo, D., 19-DA-1 Sousa, J., 426-GNC-28 Stelkens-Kobsch, T., 265-MST-5 Sun, J., 200-MST-4, 310-GNC-13 Sidorenko, A., 178-APA-17 Skolnik, N., 121-AFM-3 Sousa, M., 350-APA-33, 381-MST-11, 430-MST-15 Stelzer, D., 281-SUR-1 Sun, L., 257-GNC-5, 373-GNC-22 Sidwell, T., 262-HSABP-5/PGC-4 Slabaugh, C., 64-AMT-3, 94-PC-5/PGC-2 Souza, P., 60-AA-2 Stepanyan, S., 388-PDL-11 Sun, R., 77-FD-11 Siefers, T., 297-APA-32 Slater, J., 212-SD-11, 344-ABPSI-1, 486-SD-25, Spadaccini2, C., 380-MDO-10 Stepanyan, V., 110-UMS-2, 168-UMS-4, 254-GNC-2, Sun, T., 309-GNC-12 Siegwart, R., 371-GNC-20 487-SD-26 Spak, K., 102-SD-5, 211-SD-10 371-GNC-20 Sun, W., 153-PC-11, 206-PC-16, 434-PC-24, 435-PC-25 Sievers, M., 161-SE-1 Slavinskaya, N., 206-PC-16 Spakovszky, Z., 220-TP-8 Stephani, K., 448-TP-12 Sundararaghavan, V., 202-NDA-4, Siewert, S., 215-SEN-2 Sleppy, M., 83-GT-11 Spalart, P., 420-FD-59, 490-WE-11 Stephen, E., 134-FD-16 475-MDO-12/NDA-10

192 Sigal, E., 425-GNC-27 Slotine, J., 469-GNC-32 Spall, R., 13-APA-1 Stephens, C., 279-SEN-3 Sung, H., 147-MST-1 Sigthorsson, D., 311-GNC-14 Slotnick, J., 361-FD-48 Sparkman, D., 151-NDA-3 Stephenson, K., 345-ACD-8 Suo, J., 261-GTE-6 Siikonen, T., 249-FD-35 Slupski, B., 125-APA-11 Spencer, H., 366-GNC-15 Stern, E., 108-TP-3, 167-TP-6, 355-APA-38 Suraj Nandiganahalli, J., 86-IS-1, 322-MST-9 Sikes, T., 97-PC-8, 481-PC-32 Smarslok, B., 151-NDA-3, 324-NDA-7, 433-NDA-9 Spencer, M., 197-MAT-5 Stern, F., 406-APA-40 Suresh Babu, A., 248-FD-34 Silk, E., 220-TP-8 Smeddal, T., 34-ISC-3 Spiers, G., 368-GNC-17 Stern, N., 66-APA-5 Suryanarayanan, A., 376-GTE-8 Silton, S., 464-FD-61 Smith, A., 243-DE-3 Spillers, R., 11-AMT-1, 364-FD-51 Stevens, C., 314-HSABP-6/PGC-5 Suryanarayanan, S., 75-FD-8 Silva, A., 335-UMS-10, 408-APA-42, 465-FD-62 Smith, B., 15-APA-3, 71-APA-10, 187-FD-26 Spinosa, E., 79-FD-13 Stevens, R., 80-FD-14 Surzhikov, S., 43-PDL-1, 208-PDL-5, 282-TP-9, Silva, C., 49-SD-3 Smith, E., 486-SD-25 Spode, C., 49-SD-3, 160-SD-9 Stevenson, T., 325-OPS-1 484-PDL-14 Silva, R., 49-SD-3 Smith, J., 304-FD-45 Spoonire, R., 202-NDA-4 Stewart, E., 278-SD-15 Sutton, D., 75-FD-8 Silva, T., 335-UMS-10 Smith, L., 377-HSABP-7, 434-PC-24 Spottswood, S., 186-FD-25 Stiekel, F., 265-MST-5 Sutton, J., 349-AMT-13 Silva, W., 159-SD-8, 211-SD-10, 331-SD-17, 442-SD-22 Smith, M., 11-AMT-1, 414-FD-5, 431-MST-16 Sprague, M., 133-FD-15 Stockett, P., 440-PDL-12, 485-PDL-15 Suzuki, H., 236-AFM-5 Silveira Neto, A., 363-FD-50 Smith, N., 14-APA-2, 122-AMT-5, 348-AMT-12 Springer, J., 444-SD-24 Stockton, N., 428-IS-9 Suzuki, N., 51-SRE-1 Silver, M., 46-SCS-1 Smith, S., 159-SD-8, 284-UMS-9, 444-SD-24 Sreenivas, K., 23-FD-3, 149-MVC-3 Stoddard, W., 195-HSABP-4/PGC-3 Suzuki, T., 219-TP-7, 275-SCS-4 Silversmith, P., 372-GNC-21 Smith, T., 31-HSABP-1, 385-PC-22 Sridhar, M., 26-FD-7 Stoellinger, M., 249-FD-35, 285-WE-5 Svensson, A., 62-ACD-4 Simeni Simeni, M., 441-PDL-13 Smyers, B., 102-SD-5, 366-GNC-15 Srinivasan, R., 28-GT-1 Stolt, A., 122-AMT-5 Swaminathan Gopalan, K., 448-TP-12 Simeone, S., 159-SD-8 Snyder, D., 472-GTE-10 Srivastava, S., 475-MDO-12/NDA-10 Storozhev, D., 484-PDL-14 Sweda, W., 489-TES-4 Simerly, S., 374-GT-8 Snyder, J., 390-SD-20 St. George, A., 195-HSABP-4/PGC-3 Stouffer, S., 12-AMT-2, 41-PC-3, 96-PC-7, 194-GTE-5, Swei, S., 389-SD-19, 442-SD-22, 486-SD-25 Simmons, C., 268-NDA-5 Sobester, A., 382-MST-12 Stab, I., 189-FD-28 270-PC-17, 479-PC-30 Swenson, E., 209-SATS-5 Simmons, R., 204-PC-14 Sodano, H., 72-ASC-2 Stachler, R., 12-AMT-2, 96-PC-7 Stoumbos, T., 278-SD-15, 331-SD-17, 392-STR-10, Swift, A., 395-WE-9 Simon, D., 308-GNC-11 Sohail, Z., 304-FD-45 Stachowiak, S., 467-GNC-30 443-SD-23 Syred, N., 193-GTE-4, 393-TES-1, 446-TES-2 Simpson, J., 70-APA-9 Sojka, P., 204-PC-14 Stack, C., 142-HSABP-3 Stoyanov, M., 324-NDA-7 Szklany, S., 372-GNC-21 Simpson, R., 390-SD-20, 417-FD-56 Soliman, H., 53-STR-2 Stahl, J., 205-PC-15 Strain, R., 283-UMS-8 Szmuk, M., 368-GNC-17 Simpson, T., 220-TP-8 Solodovnikov, S., 66-APA-5 Stalnov, O., 250-FD-36, 416-FD-55 Strakey, P., 195-HSABP-4/PGC-3, 262-HSABP-5/PGC-4 T, V., 68-APA-7 Sinclair, A., 308-GNC-11 Solomon, J., 463-FD-60 Stancu, G., 388-PDL-11 Straub, J., 44-SATS-1, 100-SATS-3, 156-SATS-4, T. S., S., 441-PDL-13 Singh, A., 77-FD-11, 215-SEN-2, 240-APA-23/FD-31, Sondak, D., 268-NDA-5 Stanﬁeld, S., 123-AMT-6, 289-AA-9 209-SATS-5, 315-ICC-1 Taamallah, S., 386-PC-23 249-FD-35 Sondergaard, R., 29-GTE-1, 361-FD-48 Stanford, B., 14-APA-2, 37-MDO-1, 103-SD-6, Strawn, R., 138-FD-20 Tabib, M., 285-WE-5 Singh, B., 64-AMT-3 Song, B., 416-FD-55 198-MDO-6, 389-SD-19, 442-SD-22 Stremel, P., 312-GT-7/AMT-11 Tada, N., 157-SCS-2 Singh, D., 187-FD-26, 355-APA-38 Song, C., 177-APA-16 Stanley, A., 395-WE-9 Strganac, T., 182-ASC-3 Tadanki, A., 44-SATS-1 Author/Session Chair Index Taguchi, Y., 125-APA-11 Temme, J., 42-PC-4 Tomita, H., 236-AFM-5 Turpin, A., 362-FD-49 Van Kampen, E., 196-IS-3, 263-IS-4, 308-GNC-11, Taha, H., 130-DE-2, 179-APA-18, 311-GNC-14, Templeton, E., 162-SEN-1 Tommila, C., 45-SATS-2 Turse, D., 46-SCS-1 309-GNC-12, 347-AFM-8, 428-IS-9, 470-GNC-33 402-AFM-9, 425-GNC-27 Templeton, W., 87-ISC-4 Tomooka, M., 164-SRE-3 Tyson, W., 185-FD-24 Vannucci, F., 218-STR-7 Tahk, M., 305-GNC-8, 306-GNC-9 Teng, H., 314-HSABP-6/PGC-5 Tondji, Y., 353-APA-36 Ubald, B., 303-FD-44 van Oijen, J., 95-PC-6 Tai, J., 84-GTE-2, 472-GTE-10 Tenney, A., 464-FD-61 Toor, Z., 67-APA-6, 294-APA-29, 304-FD-45 Uchigasaki, D., 328-PDL-9 VanOsdol, R., 485-PDL-15 Taira, K., 139-FD-22, 240-APA-23/FD-31, 359-FD-46 Teo, C., 97-PC-8 Toosi, S., 246-FD-32 Uchiyama, K., 258-GNC-6 van Paassen, M., 317-IS-6, 468-GNC-31 Takahashi, H., 69-APA-8/AA-3 Teodorescu, M., 110-UMS-2, 486-SD-25 Topbas, E., 459-AFM-12 Udani, J., 289-AA-9 Van Poppel, B., 408-APA-42 Takahashi, M., 267-MST-7 Teope, K., 457-ACD-11 Toratani, D., 267-MST-7 Ueda, S., 424-GNC-26 van Rooij, A., 332-SD-18 Takahashi, T., 8-ACD-1, 67-APA-6, 69-APA-8/AA-3, Teramoto, S., 167-TP-6 Torens, C., 50-SOF-1, 104-SOF-2, 316-IS-5 Ueda, Y., 457-ACD-11 van Rossum, L., 43-PDL-1 174-ACD-6, 264-MDO-7, 401-ACD-10, 456-ABPSI-3, Teramura, M., 408-APA-42 Toropov, V., 320-MDO-9, 475-MDO-12/NDA-10 Ugolotti, M., 379-MAT-8 Vanskike, W., 286-WE-6 457-ACD-11 Terashima, H., 271-PC-18 Tortorelli, D., 380-MDO-10 Uijt De Haag, M., 19-DA-1 Vanstone, L., 189-FD-28, 377-HSABP-7 Takahashi, Y., 66-APA-5 TerMaath, S., 150-NDA-2/MDO-5, 151-NDA-3 Townsend, S., 380-MDO-10 Ukeiley, L., 125-APA-11 Van Tooren, M., 37-MDO-1, 198-MDO-6, 218-STR-7 Takatsuka, M., 486-SD-25 Tetreault, K., 100-SATS-3 Toyoda, A., 409-APA-43 Ulbrich, N., 124-AMT-7/GT-3 Van Treuren, K., 288-AA-8 Takayanagi, H., 334-TP-10 Teubert, C., 104-SOF-2, 432-MST-17 Tran, D., 369-GNC-18 Ulrich, S., 256-GNC-4, 259-GNC-7, 373-GNC-22, Varghese, P., 99-PDL-2, 166-TP-5, 484-PDL-14 Takeichi, N., 323-MST-10 Thacker, B., 214-SE-2 Tran, S., 251-FD-37 426-GNC-28, 470-GNC-33 Variyar, A., 61-ACD-3, 120-ACD-5 Takekawa, K., 127-APA-13 Thakar, S., 258-GNC-6 Trapani, G., 149-MVC-3 Ulusoy, I., 166-TP-5 Vasile, J., 179-APA-18 Talamadupula, K., 89-MAT-2 Thakur, S., 302-FD-43 Trawick, D., 472-GTE-10 Umali, J., 275-SCS-4 Vassberg, J., 295-APA-30 Talley, D., 326-PC-20, 385-PC-22 Thapa Magar, K., 366-GNC-15 Trawny, N., 368-GNC-17 Umemura, Y., 40-PC-2 Vasu, S., 96-PC-7, 154-PC-12 Talon, T., 275-SCS-4 Theis, J., 395-WE-9 Trefny, C., 344-ABPSI-1 Umphrey, C., 292-APA-27 Vatankhahghadim, B., 425-GNC-27 Tamijani, A., 53-STR-2 Theodorou, E., 373-GNC-22 Treve, V., 266-MST-6 Underbrink, J., 123-AMT-6 Vatcher, C., 68-APA-7 Tamura, A., 46-SCS-1 Thibault, S., 149-MVC-3 Triantafyllou, M., 469-GNC-32 Unnikrishnan, S., 173-AA-5 Vatsa, V., 78-FD-12 Tamura, K., 306-GNC-9 Thomas, D., 100-SATS-3, 372-GNC-21, 432-MST-17 Troclet, B., 444-SD-24 Urbanczyk, P., 198-MDO-6 Vedantam, M., 470-GNC-33 Tan, A., 221-UMS-6 Thomas, F., 70-APA-9, 273-PDL-6 Trojak, W., 133-FD-15 Urbano, S., 33-ISC-2 Vedovoto, J., 363-FD-50 Tan, J., 407-APA-41 Thomas, G., 476-MST-18 Tropina, A., 484-PDL-14 Ure, N., 382-MST-12 Vedula, P., 166-TP-5

193 Tanaka, N., 415-FD-54 Thomas, J., 395-WE-9 Trumbauer, E., 323-MST-10 U S, V., 187-FD-26 Veers, P., 170-WE-2, 285-WE-5, 395-WE-9 Tang, J., 188-FD-27, 336-WE-8, 463-FD-60 Thomas, L., 12-AMT-2 Truong, C., 64-AMT-3 Usach, H., 316-IS-5 Vegh, J., 61-ACD-3, 290-ACD-7 Tang, Y., 418-FD-57 Thomison, W., 478-NDA-11 Tsai, C., 362-FD-49, 418-FD-57 Uslu, S., 142-HSABP-3 Veldhuis, L., 296-APA-31 Tangirala, V., 195-HSABP-4/PGC-3 Thompson, K., 366-GNC-15 Tsalik, R., 370-GNC-19 Uzun, A., 138-FD-20 Vemula, R., 464-FD-61 Tani, H., 40-PC-2 Thorne, D., 205-PC-15 Tse, E., 54-TFPC-1 Vadlamani, N., 75-FD-8 Venkatakrishnan, L., 238-APA-21 Tanno, H., 191-FD-30, 361-FD-48, 414-FD-5, 417-FD-56 Threadgill, J., 189-FD-28, 247-FD-33 Tsuboi, N., 271-PC-18, 303-FD-44 Vaghjiani, G., 154-PC-12 Venkataraman, S., 52-STR-1, 277-SD-14 Tanriverdi, G., 256-GNC-4 Throneberry, G., 128-APA-14, 264-MDO-7 Tsubokura, M., 365-FD-52 Vaidya, A., 196-IS-3 Venkatasubban, C., 400-ACD-9 Tapia-Cortez, C., 105-SRE-2 Thurman, D., 251-FD-37 Tsukerman, A., 255-GNC-3 Valasek, J., 308-GNC-11, 316-IS-5, 367-GNC-16 Venkatesan, K., 203-PC-13 Tardioli, L., 253-GNC-1 Thurow, B., 11-AMT-1, 247-FD-33, 404-AMT-14 Tsuru, K., 434-PC-24 Valavanis, K., 374-GT-8 Venner, C., 490-WE-11 Tartaruga, I., 320-MDO-9, 406-APA-40 Tian, P., 402-AFM-9, 469-GNC-32 Tsushima, N., 158-SD-7, 278-SD-15 Valente, C., 159-SD-8 Venrooij, J., 266-MST-6, 322-MST-9 Tataroglu, S., 488-STR-12 Tian, S., 238-APA-21, 361-FD-48 Tu, S., 24-FD-4, 184-FD-23 Valentich, G., 464-FD-61 Verbin, A., 174-ACD-6 Tatematsu, H., 417-FD-56 Tichenor, N., 417-FD-56 Tucker, J., 389-SD-19 Valera-Medina, A., 193-GTE-4, 393-TES-1 VerHulst, C., 408-APA-42 Tatematsu, Y., 275-SCS-4 Tidball, M., 486-SD-25 Tucker, P., 22-FD-2, 75-FD-8, 119-AA-4, 133-FD-15, Valle, G., 389-SD-19 Vernon, R., 379-MAT-8 Tatting, B., 107-STR-4 Tillson, C., 108-TP-3 187-FD-26, 194-GTE-5, 251-FD-37, 303-FD-44 Van Baren, G., 266-MST-6 Verveld, M., 391-SD-21 Taylor, A., 42-PC-4 Tilmann, C., 129-APA-15, 350-APA-33 Tuckey, T., 201-MVC-4 van Bussel, G., 336-WE-8 Vetrella, A., 58-UMS-1, 215-SEN-2 Taylor, C., 57-TP-13/MDO-13 Timme, S., 457-ACD-11 Tuegel, E., 214-SE-2, 384-NDA-8 van Craenenbroeck, J., 296-APA-31 Viana, F., 318-MAT-6, 384-NDA-8 Taylor, K., 336-WE-8 Ting, E., 389-SD-19, 442-SD-22 Tufano, D., 102-SD-5 VanDamme, C., 33-ISC-2, 331-SD-17 Vich, O., 159-SD-8 Taylor, L., 149-MVC-3 Tinker, D., 161-SE-1, 439-PC-29 Tufts, M., 190-FD-29 Vanden, K., 66-APA-5, 353-APA-36 Vieira, B., 409-APA-43 Taylor, N., 13-APA-1 Tinney, C., 134-FD-16, 173-AA-5 Tuke, M., 238-APA-21 Van der Geest, P., 266-MST-6 Vieira, D., 408-APA-42 Taylor, O., 134-FD-16 Tinoco, E., 295-APA-30 Tullino, S., 209-SATS-5 Van der Kindere, J., 176-AMT-8 Viken, J., 53-STR-2 Taylor, P., 330-SD-16, 444-SD-24 Tischler, M., 347-AFM-8, 381-MST-11 Tumin, A., 21-FD-1 Van der Ploeg, R., 430-MST-15 Viken, S., 54-TFPC-1, 78-FD-12 Taylor, R., 218-STR-7 Tishkoff, J., 97-PC-8 Tumuklu, O., 394-TP-11 van der Velden, W., 336-WE-8 Vikhorev, K., 200-MST-4 Tehrani, N., 382-MST-12 Tkacik, P., 404-AMT-14 Tuncer, I., 449-WE-10 Vander Wal, R., 436-PC-26 Vila, J., 316-IS-5 Teixeira, J., 252-FD-38 Togashi, F., 23-FD-3 Tupis, A., 192-GT-5 Vanderwyst, A., 101-SD-4/APA-47, 238-APA-21, Vilas, F., 215-SEN-2 Tekin, R., 370-GNC-19 Tognaccini, R., 239-APA-22 Turkoglu, K., 256-GNC-4, 325-OPS-1, 369-GNC-18, 297-APA-32 Villalpando, C., 368-GNC-17 Tekinalp, O., 459-AFM-12 Toki, T., 167-TP-6 431-MST-16 Vane, Z., 40-PC-2, 268-NDA-5 Villalva Gomez, R., 195-HSABP-4/PGC-3, 479-PC-30 Tekriwal, P., 45-SATS-2 Tokugawa, N., 457-ACD-11 Turnbull, B., 90-MAT-3, 430-MST-15 van Garrel, A., 490-WE-11 Villanueva, D., 433-NDA-9 Tellez, J., 283-UMS-8 Tomioka, S., 456-ABPSI-3 Turner, T., 182-ASC-3, 411-ASC-4, 461-ASC-6 Vincent-Randonnier, A., 485-PDL-15 Author/Session Chair Index Vis, M., 215-SEN-2 Wang, K., 154-PC-12 Wei, R., 70-APA-9 Wieseman, C., 103-SD-6, 442-SD-22 Wu, H., 386-PC-23 Visbal, M., 75-FD-8, 76-FD-9, 101-SD-4/APA-47, Wang, L., 23-FD-3, 129-APA-15, 158-SD-7, 184-FD-23, Wei, S., 41-PC-3 Wiggen, S., 179-APA-18 Wu, J., 122-AMT-5, 420-FD-59, 433-NDA-9 251-FD-37, 355-APA-38, 365-FD-52, 415-FD-54 269-NDA-6, 318-MAT-6, 384-NDA-8, Wei, X., 122-AMT-5 Wilder, M., 355-APA-38 Wu, P., 440-PDL-12, 485-PDL-15 Vishnyakov, O., 178-APA-17 410-APA-44/FD-53, 486-SD-25 Wei, Y., 329-SCS-5 Wilhelm, J., 58-UMS-1, 130-DE-2, 169-UMS-5 Wu, S., 103-SD-6, 259-GNC-7 Vishwanath, A., 447-TES-3 Wang, M., 307-GNC-10, 310-GNC-13, 478-NDA-11 Weidenfeld, M., 138-FD-20 Wilhite, J., 84-GTE-2 Wu, X., 308-GNC-11, 365-FD-52, 405-APA-39 Viswanath, K., 7-AA-1 Wang, N., 418-FD-57 Weihs, D., 206-PC-16 Wilke, G., 410-APA-44/FD-53 Wu, Y., 12-AMT-2, 97-PC-8, 158-SD-7, 207-PDL-4 Viswanathan, S., 258-GNC-6 Wang, P., 130-DE-2 Weimer, C., 162-SEN-1 Wilkinson, S., 273-PDL-6 Wu, Z., 103-SD-6, 371-GNC-20 Vivarelli, G., 477-MVC-5 Wang, Q., 136-FD-18, 198-MDO-6, 246-FD-32, Weiner, R., 364-FD-51 Willcox, K., 150-NDA-2/MDO-5, 475-MDO-12/NDA-10 Wuensch, O., 419-FD-58 Vivekanandan, P., 383-MST-14 299-FD-39, 361-FD-48 Weintraub, I., 311-GNC-14, 471-GNC-34 Wille, A., 161-SE-1 Wunsch, D., 293-APA-28 Vlachos, P., 64-AMT-3 Wang, V., 220-TP-8 Weisman, R., 309-GNC-12 Williams, D., 248-FD-34, 303-FD-44, 374-GT-8 Wurster, K., 282-TP-9 Voelkel, S., 166-TP-5 Wang, X., 21-FD-1, 47-SD-1/APA-46, 153-PC-11, Weiss, M., 255-GNC-3 Williams, F., 25-FD-6 Wyman, N., 92-MVC-2, 149-MVC-3 Vogel, R., 90-MAT-3 174-ACD-6, 234-AA-6, 271-PC-18, 347-AFM-8, Weitz, L., 19-DA-1 Williams, J., 344-ABPSI-1 Wynn, A., 146-MDO-4 Voget, N., 221-UMS-6 371-GNC-20 Wells, D., 9-ACD-2, 400-ACD-9 Williams, Z., 379-MAT-8 Xia, J., 107-STR-4 Vogiatzis, K., 39-MVC-1, 166-TP-5, 194-GTE-5 Wang, Y., 65-AMT-4, 124-AMT-7/GT-3, 306-GNC-9, Wells, S., 305-GNC-8 Willis, B., 106-STR-3, 278-SD-15 Xiang, J., 158-SD-7, 331-SD-17 Volden, T., 124-AMT-7/GT-3 383-MST-14, 391-SD-21, 395-WE-9 Welsh, W., 486-SD-25 Wilson, J., 416-FD-55 Xiang, X., 247-FD-33 Volk, B., 220-TP-8 Wang, Z., 56-TP-2, 63-AFM-2, 103-SD-6, 119-AA-4, Welstead, J., 345-ACD-8, 457-ACD-11 Wilson, L., 46-SCS-1, 275-SCS-4 Xiangyang, W., 425-GNC-27 Volle, K., 425-GNC-27 185-FD-24, 188-FD-27, 198-MDO-6, Wen, C., 200-MST-4 Wimer, N., 136-FD-18 Xiao, H., 77-FD-11, 420-FD-59, 433-NDA-9 Volpi, S., 406-APA-40 240-APA-23/FD-31 Wen, G., 23-FD-3 Windsor, S., 366-GNC-15 Xiao, J., 165-STR-5 Vono, C., 161-SE-1 Wanthal, S., 107-STR-4, 165-STR-5, 379-MAT-8 Wenberg, D., 156-SATS-4 Winkler, C., 360-FD-47 Xie, C., 93-NDA-1, 330-SD-16 Vorgert, C., 313-GTE-7 Ward, E., 72-ASC-2 Wendler, J., 111-WE-1, 490-WE-11 Winslow, J., 9-ACD-2 Xie, H., 426-GNC-28 Vos, R., 8-ACD-1, 61-ACD-3, 120-ACD-5 Wardle, B., 197-MAT-5 Wendorff, A., 93-NDA-1, 290-ACD-7 Winter, T., 120-ACD-5 Xie, L., 169-UMS-5 Vourliotakis, G., 42-PC-4 Warner, J., 148-MST-2, 384-NDA-8, 471-GNC-34 Weng, H., 108-TP-3 Winters, C., 388-PDL-11 Xin, M., 309-GNC-12 Vranas, T., 283-UMS-8 Warning, S., 137-FD-19 Wenk, J., 108-TP-3 Wischek, J., 379-MAT-8 Xiu, D., 268-NDA-5 Vratny, P., 345-ACD-8 Warren, J., 159-SD-8, 210-SCS-3 Wentrup, M., 410-APA-44/FD-53 Wise, R., 169-UMS-5, 389-SD-19 Xu, J., 416-FD-55

194 Vrchota, P., 125-APA-11 Warsop, C., 129-APA-15 Werner, M., 44-SATS-1 Wisniewski, C., 288-AA-8 Xu, K., 155-PDL-3, 207-PDL-4, 388-PDL-11, 441-PDL-13 Vukasinovic, B., 360-FD-47 Wason, M., 21-FD-1 West, J., 437-PC-27 Wissink, A., 71-APA-10, 292-APA-27, 410-APA-44/FD-53 Xu, L., 182-ASC-3 Vuorinen, V., 249-FD-35 Watanabe, A., 157-SCS-2 West, T., 14-APA-2, 433-NDA-9, 475-MDO-12/NDA-10 Witulski, A., 269-NDA-6 Xu, R., 154-PC-12, 479-PC-30 Waas, A., 52-STR-1, 107-STR-4, 202-NDA-4, 280-STR-8 Watanabe, D., 7-AA-1 West, Z., 96-PC-7 Woeber, C., 92-MVC-2 Xu, S., 457-ACD-11 Wagner, J., 122-AMT-5, 362-FD-49, 364-FD-51, Watanabe, H., 314-HSABP-6/PGC-5 Westergaard, C., 395-WE-9 Wofﬁnden, D., 368-GNC-17 Xu, Y., 366-GNC-15 465-FD-62 Watanabe, K., 45-SATS-2 Westphal, R., 64-AMT-3 Wolf, M., 278-SD-15 Yadala Venkata, S., 361-FD-48 Wagner, M., 427-GTE-9/PGC-6 Watanabe, Y., 350-APA-33 Wetzel, K., 336-WE-8 Wolf, W., 127-APA-13 Yadav, V., 277-SD-14 Wahl, E., 256-GNC-4 Waters, D., 51-SRE-1 Wey, C., 437-PC-27 Wolfe, T., 139-FD-22 Yadlin, Y., 78-FD-12 Waithe, K., 14-APA-2 Watkins, D., 161-SE-1 Whalen, E., 78-FD-12 Wolff, M., 29-GTE-1, 280-STR-8, 476-MST-18 Yagil, L., 48-SD-2 Waldman, R., 223-WE-3, 237-AMT-9 Watkins, S., 469-GNC-32 Wheaton, B., 420-FD-59 Wolosik, A., 44-SATS-1 Yagle, P., 15-APA-3 Wales, C., 159-SD-8 Watson, J., 210-SCS-3 Whidborne, J., 120-ACD-5 Won, S., 154-PC-12, 435-PC-25, 481-PC-32 Yakinthos, K., 345-ACD-8 Walker, A., 45-SATS-2 Watson, R., 22-FD-2, 133-FD-15 Whitacre, W., 256-GNC-4, 309-GNC-12 Wong, C., 219-TP-7 Yalin, A., 155-PDL-3, 274-PDL-7, 485-PDL-15 Walker, J., 27-GEPC-1 Watts, S., 380-MDO-10 Whitcher, L., 62-ACD-4 Wong, E., 143-IS-2 Yamada, K., 25-FD-6, 66-APA-5 Walker, L., 432-MST-17 Waugh, A., 408-APA-42 Whitcomb, J., 461-ASC-6 Wong, L., 200-MST-4 Yamaguchi, S., 67-APA-6 Wall, S., 243-DE-3 Way, D., 63-AFM-2 White, A., 48-SD-2, 323-MST-10 Wong, T., 409-APA-43 Yamakawa, H., 209-SATS-5 Walls, J., 323-MST-10 Wayman, T., 192-GT-5 White, E., 75-FD-8, 111-WE-1 Wood, D., 8-ACD-1 Yamamoto, K., 241-APA-24 Walsh, M., 424-GNC-26 Weaver, P., 17-ASC-1, 46-SCS-1, 332-SD-18, 461-ASC-6 White, L., 97-PC-8 Wood, K., 129-APA-15, 366-GNC-15 Yamamoto, N., 197-MAT-5 Walters, D., 142-HSABP-3 Webb, B., 56-TP-2 White, M., 431-MST-16 Wood, R., 9-ACD-2 Yamashita, Y., 67-APA-6 Walters, R., 151-NDA-3 Webb, J., 15-APA-3 White, R., 73-EDU-2/DE-1, 357-EXPL-1 Woollard, B., 44-SATS-1 Yamazaki, M., 46-SCS-1, 157-SCS-2, 275-SCS-4 Wan, B., 192-GT-5 Webb, K., 467-GNC-30 Whitehead, B., 93-NDA-1 Woolsey, C., 283-UMS-8, 291-AFM-6 Yamouni, S., 127-APA-13 Wan, Z., 174-ACD-6, 405-APA-39, 475-MDO-12/NDA-10 Webb, N., 387-PDL-10, 415-FD-54, 463-FD-60 Whitford, J., 389-SD-19 Work, D., 22-FD-2 Yan, G., 234-AA-6 Wang, B., 319-MDO-8 Weber, S., 10-AFM-1 Whittaker, J., 278-SD-15 Worthington, E., 238-APA-21 Yan, L., 234-AA-6 Wang, C., 350-APA-33 Webster, C., 324-NDA-7 Whittaker, M., 256-GNC-4 Woszidlo, R., 191-FD-30, 359-FD-46, 416-FD-55 Yanagita, Y., 22-FD-2 Wang, F., 93-NDA-1 Weddle-Weaver, C., 345-ACD-8 Whyte, S., 288-AA-8 Woytach, J., 105-SRE-2 Yanase, S., 67-APA-6 Wang, G., 14-APA-2, 26-FD-7, 82-GT-2, 213-SD-12 Wee, H., 322-MST-9 Wick, A., 27-GEPC-1 Wray, T., 77-FD-11, 246-FD-32 Yancey, R., 379-MAT-8 Wang, H., 154-PC-12, 436-PC-26, 487-SD-26 Wei, D., 169-UMS-5 Wicke, K., 400-ACD-9 Wrede, B., 179-APA-18 Yang, B., 322-MST-9 Wang, J., 77-FD-11, 80-FD-14, 277-SD-14, 328-PDL-9, Wei, F., 73-EDU-2/DE-1, 93-NDA-1, 277-SD-14 Wickramasinghe, N., 267-MST-7 Wright, J., 302-FD-43 Yang, C., 103-SD-6, 174-ACD-6, 330-SD-16, 381-MST-11, 420-FD-59, 433-NDA-9 Wei, M., 252-FD-38 Wickramasinghe, V., 182-ASC-3, 356-ASC-5 Wrzesinski, P., 41-PC-3, 270-PC-17, 479-PC-30 371-GNC-20, 405-APA-39, 475-MDO-12/NDA-10 Author/Session Chair Index Yang, G., 238-APA-21 Youseﬁ, E., 367-GNC-16 Zhang, W., 26-FD-7, 32-ISC-1, 76-FD-9, 217-STR-6, Yang, H., 419-FD-58 Youssef, A., 257-GNC-5 246-FD-32 Yang, J., 133-FD-15, 424-GNC-26 Yu, H., 250-FD-36, 261-GTE-6 Zhang, X., 133-FD-15, 143-IS-2, 418-FD-57, Yang, M., 216-SOF-4, 270-PC-17 Yu, J., 286-WE-6 466-GNC-29, 487-SD-26 Yang, P., 10-AFM-1, 314-HSABP-6/PGC-5 Yu, M., 16-APA-4, 184-FD-23, 223-WE-3 Zhang, Y., 65-AMT-4, 122-AMT-5, 207-PDL-4, Yang, S., 82-GT-2, 153-PC-11, 198-MDO-6 Yu, W., 145-MAT-4, 165-STR-5, 280-STR-8, 304-FD-45, 362-FD-49, 458-AFM-11 Yang, V., 153-PC-11, 271-PC-18 333-SUR-2/MAT-7 Zhang, Z., 12-AMT-2, 97-PC-8, 198-MDO-6, 207-PDL-4, Yang, X., 13-APA-1, 26-FD-7, 177-APA-16, Yu, Y., 216-SOF-4, 381-MST-11 249-FD-35, 464-FD-61 300-FD-41, 416-FD-55 Yu, Z., 107-STR-4 Zhao, C., 283-UMS-8 Yang, Y., 39-MVC-1, 76-FD-9, 125-APA-11, 188-FD-27, Yuan, G., 350-APA-33 Zhao, H., 350-APA-33, 257-GNC-5, 481-PC-32 238-APA-21, 361-FD-48, 416-FD-55, 444-SD-24, Yuan, H., 217-STR-6 Zhao, L., 487-SD-26 463-FD-60 Yuan, M., 202-NDA-4 Zhao, S., 371-GNC-20 Yao, C., 75-FD-8 Yucel, A., 196-IS-3 Zhao, W., 346-AFM-7, 445-STR-11 Yao, Y., 238-APA-21 Yucelen, T., 86-IS-1, 168-UMS-4, 308-GNC-11, Zhao, Y., 257-GNC-5 Yao, Z., 46-SCS-1 367-GNC-16, 369-GNC-18, 421-GNC-23, 466-GNC-29 Zhao, Z., 178-APA-17 Yar, A., 304-FD-45 Yuen, W., 334-TP-10 Zhen, J., 325-OPS-1 Yarlagadda, Y., 459-AFM-12 Yuhara, T., 407-APA-41 Zheng, J., 178-APA-17, 327-PDL-8 Yashima, K., 157-SCS-2 Yuksek, B., 382-MST-12 Zheng, L., 261-GTE-6 Yau, M., 104-SOF-2, 216-SOF-4, 222-UMS-7 Yurkovich, M., 484-PDL-14 Zheng, Z., 373-GNC-22, 469-GNC-32 Yavuztürk, V., 459-AFM-12 Yusuf, S., 147-MST-1, 175-AFM-4 Zhong, M., 82-GT-2 Yayla, M., 367-GNC-16 Yutko, B., 130-DE-2 Zhong, S., 79-FD-13 Yazicioglu, Y., 459-AFM-12 Zaag, M., 476-MST-18 Zhong, X., 133-FD-15 Ye, W., 107-STR-4 Zaal, P., 147-MST-1, 199-MST-3, 266-MST-6, Zhou, B., 37-MDO-1 Ye, Z., 14-APA-2 322-MST-9, 432-MST-17 Zhou, L., 56-TP-2, 177-APA-16

195 Yedavalli, R., 369-GNC-18, 425-GNC-27 Zahle, F., 449-WE-10 Zhou, W., 306-GNC-9 Yee, K., 313-GTE-7, 376-GTE-8 Zakerzadeh, M., 24-FD-4 Zhu, B., 26-FD-7, 425-GNC-27 Yeh, C., 359-FD-46 Zakrajsek, A., 90-MAT-3, 212-SD-11 Zhu, G., 425-GNC-27, 442-SD-22 Yeh, D., 361-FD-48 Zaman, K., 173-AA-5 Zhu, J., 391-SD-21, 408-APA-42, 425-GNC-27 Yeh, S., 271-PC-18 Zang, B., 187-FD-26 Zhu, K., 65-AMT-4, 205-PC-15 Yellugari, K., 84-GTE-2 Zangeneh, R., 184-FD-23 Zhu, M., 373-GNC-22, 487-SD-26 Yemaneberhane, B., 18-CMS-1 Zanj, A., 431-MST-16 Zhu, S., 405-APA-39, 475-MDO-12/NDA-10 Yen, C., 280-STR-8 Zappino, E., 106-STR-3 Zhu, W., 223-WE-3 Yeo, D., 131-EDU-3, 366-GNC-15 Zeng, C., 264-MDO-7 Zhu, X., 111-WE-1, 268-NDA-5, 304-FD-45 Yeo, H., 160-SD-9, 211-SD-10 Zeng, D., 18-CMS-1 Zhu, Z., 281-SUR-1 Yetter, R., 205-PC-15 Zeszut, Z., 51-SRE-1 Zhuang, W., 371-GNC-20 Yildiz, Y., 31-HSABP-1, 367-GNC-16 Zeune, C., 27-GEPC-1 Zhupanska, O., 36-MAT-1 Yilmazturk, S., 376-GTE-8 Zha, G., 14-APA-2, 194-GTE-5, 416-FD-55 Ziegler, M., 205-PC-15 Yim, M., 291-AFM-6 Zhang, C., 21-FD-1, 309-GNC-12, 441-PDL-13 Zilli, J., 75-FD-8 Yin, Z., 187-FD-26 Zhang, D., 81-GEPC-2, 165-STR-5, 223-WE-3, Zimmerman, J., 388-PDL-11, 440-PDL-12, 484-PDL-14 Yirtici, O., 449-WE-10 371-GNC-20, 445-STR-11 Zimmerman, S., 158-SD-7 Yokomatsu, T., 157-SCS-2 Zhang, F., 307-GNC-10, 383-MST-14 Zingg, D., 136-FD-18 Yokoyama, N., 308-GNC-11 Zhang, H., 26-FD-7 Zips, J., 363-FD-50 Yokozeki, T., 329-SCS-5 Zhang, J., 264-MDO-7, 333-SUR-2/MAT-7, 429-MDO-11 Zore, K., 49-SD-3 Yoo, J., 434-PC-24, 485-PDL-15 Zhang, K., 44-SATS-1, 223-WE-3, 237-AMT-9, Zou, Z., 324-NDA-7 Yoon, S., 16-APA-4 310-GNC-13 Zubair, M., 384-NDA-8 Yoon, Y., 367-GNC-16 Zhang, L., 165-STR-5, 271-PC-18 Zubrilin, R., 261-GTE-6 Yorita, D., 83-GT-11, 176-AMT-8 Zhang, M., 290-ACD-7 Zweber, J., 214-SE-2 Yoshida, K., 14-APA-2 Zhang, Q., 308-GNC-11 Yoshino, T., 408-APA-42 Zhang, R., 355-APA-38 Yost, M., 432-MST-17 Zhang, S., 169-UMS-5, 307-GNC-10, 308-GNC-11, You, D., 255-GNC-3 416-FD-55 Youn, E., 408-APA-42 IntroVENUE MAP

Convention Center, Ballroom Level

Convention Center, Exhibit Level

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Lone Star Tower (hotel side) Lobby Level

Lone Star Tower (hotel side) 3rd Floor

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Lone Star Tower (hotel side) 4th Floor

* Committee Meeting Rooms in hotel suites 6333 and 6355 are located on the 6th floor in the Gaylord on the hotel side.

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www.aiaa-SciTech.org 60 #aiaaSciTech 8–12 JANUARY 2018 GAYLORD PALMS, ORLANDO, FL SEE YOU NEXT YEAR Mark your calendars for the ﬁrst major aerospace event of 2018—AIAA Science and Technology Forum and Exposition—where engineers, researchers, students, and aerospace leaders from around the world share the most original perspectives, collaborate on stimulating ideas, and inﬂuence the future of aerospace. Technical conferences meeting as part of the 2018 AIAA SciTech Forum include:

• 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 • AIAA/AAS Space Flight Mechanics Meeting • 35th Wind Energy Symposium

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