The Largest Event for Aerospace Research, Development, and Technology

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5–9 JANUARY 2015 KISSIMMEE, FL

FINAL PROGRAM www.aiaa-SciTech.org #aiaaSciTech

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© 2014 LOCKHEED MARTIN CORPORATION VC377_164 Executive Steering Committee AIAA SciTech 2015 Welcome We are excited to welcome you to the AIAA Science and Technology Forum and Exposition 2015 — the largest event for aerospace research, development, and technology in the world. We are confident that you will be informed, inspired, and motivated, as you take part in shaping the future of aerospace! Robert Braun Rich Christiansen Georgia Institute of Sierra Lobo, Inc. Over the coming days you will have the opportunity to hear from thought leaders in Technology our community, learn about the latest technical breakthroughs, collaborate with an unparalleled group of peers, and gain knowledge and insight with each session and event that you attend.

Our organizing committee has worked hard to ensure that our plenary sessions will examine the most critical issues in aerospace today: investment trends and strategies for science and technology policy and R&D; how globalization will impact the aerospace economy; the future of aerospace design; climate change and the use of big data to gain a better understanding of Earth’s climate cycles; and how best to John Evans George Lesieutre construct the future workforce. Lockheed Martin The Pennsylvania Corporation State University As always, our panel discussions will build on the themes and discussions of each day’s opening plenary session, adding a layer of content and context that will enhance the value of your forum experience. These discussions will also give you time to interact with industry leaders in more intimate settings, enabling meaningful communication, and stimulating greater insight into the critical issues of the day.

We also have built a premier technical program that is second to none in terms of the scope, breadth, and depth of the cutting-edge aerospace research being presented— material that you will be unable to find anywhere else. We thank the Technical Tom Shih James Shields Program Committee for working so hard to assemble this program. Purdue University Draper Laboratory AIAA SciTech 2015 will energize, enlighten, and illuminate your continuing efforts to advance the state of the art in aerospace engineering, science, and technology development. The forum will launch what we know will be an amazing year of discovery and innovation, and we are happy that you made the choice to be here with us this week to take part in this most important gathering.

John Tracy The Boeing Company AIAA SciTech 2015 is proud to feature the following conferences: 23rd AIAA/AHS Adaptive 17th AIAA Non-Deterministic Structures Conference Approaches Conference 53rd AIAA Aerospace Sciences Meeting 8th Symposium on Space Resource Utilization AIAA Atmospheric Flight Mechanics Conference 2nd AIAA Spacecraft Structures Conference AIAA Infotech @ Aerospace 56th AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference AIAA Guidance, Navigation, and Control Conference 33rd Wind Energy Symposium AIAA Modeling and Simulation Technologies Conference www.aiaa-SciTech.org 3 #aiaaSciTech IntroOrganizing Committee

SciTech 2015 Forum General Chair Applied Aerodynamics Non-Deterministic Approaches George Lesieutre, The Pennsylvania State Doug Lacy, The Boeing Company Markus P. Rumpfkeil, University of Dayton University Atmospheric Flight Mechanics Plasmadynamics and Lasers Forum 360 Chair Francis Priolo, Millenium Engineering Joseph Wang, University of Southern Edward Kraft, Air Force Test Center, Arnold California Air Force Base Communications Systems Jim Dragonas Dimarogonas, The MITRE Propellants and Combustion International Chair Corporation Chris Cadou, University of Maryland Jürgen Quest, European Transonic Windtunnel Computer Systems Sensor Systems Joe Collins, Naval Research Laboratory Dan Clancy, Lockheed Martin Aeronautics Membership Chair Company Luisella Giulicchi, European Space Agency Design Engineering E. Russ Althof, Raytheon Missile Systems Small Satellites Public Policy Chair Jeremy Straub, University of North Dakota John Rose, The Boeing Company Digital Avionics Jim Rankin, University of Arkansas Society and Aerospace Technology Young Professional Chair Steve Justice, Georgia Center of Innovation Fluid Dynamics for Aerospace Benjamin Marchionna, Lockheed Martin Jesse Little, University of Arizona Software Recognition Chair Gas Turbine Engines Stephen Blanchette, Software Engineering Dave Throckmorton, Northrop Grumman Jason Smith, General Electric Aviation Institute Education Chair Green Engineering Space Resources Utilization Symposium K. Ravindra (Ravi), Saint Louis University Franz-Josef Kahlen, University of Cape Town Julie Kleinhenz, NASA Glenn Research Forum Technical Chairs Center Ground Test D. Brett Ridgely, Raytheon Missile Systems Roman Paryz, NASA Langley Research Space Operations and Support John Kosmatka, University of California, San Center Shirley Tseng Diego Guidance, Navigation, and Control Spacecraft Structures Chris Tschan, The Aerospace Corporation John Reed, United Launch Alliance Jon Hinkle, ILC Dover

Forum Deputy Technical Chairs High Speed Air Breathing Propulsion Structural Dynamics Brad Burchett, Rose-Hulman Institute of Ronald R. Springer, Johns Hopkins Anubhav Datta, NASA Ames Research Technology University Applied Physics Laboratory Center

Richard Ruff, MathWorks History Structures William P. Barry, NASA Alex Selvarathinam, Lockheed Martin Jeanette L. Domber, Ball Aerospace & Technologies Corporation Information and Command & Control Systems Survivability Mike Sotak, Kratos Defense & Security Julian Rimoli, Georgia Institute of Technical Discipline Chairs Solutions Technology

Adaptive Structures Intelligent Systems Systems Engineering David McGowan, NASA Langley Research Kevin Kochersberger, Virginia Polytechnic John Hsu, California State University, Long Center Institute and State University Beach

Aeroacoustics Materials Terrestrial Energy Lysbeth S. Lieber, Honeywell Aerospace John Matlik, Rolls-Royce Ryo Amano, University of Wisconsin– Milwaukee Aerodynamic Measurement Technology Meshing, Visualization, and Computational Philippe (Phil) Lavoie, University of Toronto Environments Thermophysics Alina Alexeenko, Purdue University Air Breathing Propulsion Systems Integration Hugh Thornburg, High Technology Services Group, Engility Corporation Charles Gaharan, Lockheed Martin Unmanned Systems Aeronautics Modeling and Simulation Technologies Richard Stansbury, Embry-Riddle Aeronautical University Aircraft Design Dan Keating, Draper Labs Gil Crouse, Sierra Nevada Corporation Multi-Disciplinary Design Optimization Wind Energy Symposium Timothy Takahashi, Arizona State University D. Todd Griffith, Sandia National Laboratories www.aiaa-SciTech.org 4 #aiaaSciTech IntroContents

Welcome 3

Organizing Committee 4

Contents 5

Forum Overview 7

Sponsors and Supporters 10

Keynote Speakers and Plenary Sessions 11 www.twitter.com/aiaa

Forum 360 12 www.facebook.com/AIAAfan Special Sessions and Events 15 www.youtube.com/AIAATV Educational Events 16 www.linkedin.com/companies/aiaa Networking Events 17 www.flickr.com/aiaaevents Recognition Events 18 www.google.com/+aiaaorg Exposition Hall 21 new.livestream.com/AIAAVideo/SciTech2015 Exhibitors 24

General Information 32 Join the conversation! #aiaaSciTech Author and Session Chair Information 34

Committee Meetings and Events 35 On-Site Wi Fi Information Network Name: AIAA2015 Sessions at a Glance 41 Password: scitech2015

Session Detail Matrix 54

Author and Session Chair Index 175 AIAA is the world’s largest technical society dedicated to the global aerospace profession. With more than 35,000 individual members worldwide, and one hundred Venue Information 193 corporate members, AIAA brings together industry, academia, and government to advance engineering and science in aviation, space, and defense. Venue Map 194 www.aiaa.org

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 “AIAA SciTech 2015” http://download.abstractcentral. See the surrounding area and com/aiaa-mst15/index.htm the Gaylord Palms. • 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 IntroForum Overview Plenary Panels and Keynotes Get the big picture from industry, academia, and government leaders when they share their perspectives on the new challenges, future opportunities, and emerging trends in the global aerospace industry. Plenary sessions examine some of the most critical issues in aerospace today. Forum 360 These conversations build on the themes and discussions of each day’s opening plenary session, adding a layer of content and context that enhances the value of your forum experience. They also give you time to interact with industry leaders in more intimate settings, enabling meaningful communication, and stimulating greater insight into subjects like big data analytics, advanced manufacturing effects on design, climate change and defense —just to name a few. Technical Program This is the nuts and bolts, quite literally. The technical program contains more than 2,000 technical papers from about 800 government, academic, and private institutions in 40 countries reporting on the latest in aerospace research, and offering scores of opportunities for collaboration and discussion on about 300 high-impact topics. This week you will:

u Present recent advances before a knowledgeable international audience u Educate customers and providers on the latest research and product developments u Learn about the latest technology and research in the field from industry experts u Discover what lies ahead as senior industry leaders discuss their program and business challenges during keynote and panel sessions u Network to engage new contacts and refresh old ones u Recognize significant achievements from within the community

www.aiaa-SciTech.org 7 #aiaaSciTech IntroForum Overview

SATURDAY/SUNDAY MONDAY TUESDAY 3–4 January 5 January 6 January 0700 hrs Networking Coffee 0730 hrs Speakers’ Briefing Speakers’ Briefing

0800 hrs Opening Keynote Keynote 0830 hrs

0900 hrs Networking Break Networking Break in Exposition Hall

0930 hrs SSC Lecture ASC Lecture 1000 hrs Forum 360 Forum 360 1030 hrs Technical Technical Exposition 1100 hrs Sessions Sessions Hall Open

1130 hrs Continuing Education Courses 1200 hrs and 1230 hrs Workshop Recognition Luncheon: Celebrating Durand Lecture and Luncheon Networking Lunch 1300 hrs 0815–1700 hrs Achievments in Aerospace Sciences Hall Closed On Own Sponsored by Lockheed Martin and Information Systems 1330 hrs

1400 hrs NDA Lecture 1430 hrs Exposition Forum 360 Forum 360 1500 hrs Hall Open Technical Technical 1530 hrs Networking Break Networking Break Sessions Sessions 1600 hrs Rising Leaders Speed Geek 1630 hrs (1600–1715 hrs) Hall Closed 1700 hrs

1730 hrs Dryden Lecture 1800 hrs Rising Leaders Sunday Reception 1830 hrs Associate Student Reception Fellows 1900 hrs Reception Reception in Exposition Hall

1930 hrs

2000 hrs

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

2200 hrs

2230 hrs

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

WEDNESDAY THURSDAY FRIDAY 7 January 8 January 9 January 0700 hrs

0730 hrs Speakers’ Briefing Speakers’ Briefing Speakers’ Briefing

0800 hrs Plenary Panel Plenary Panel Keynote 0830 hrs

0900 hrs Networking Break in Exposition Hall Networking Break in Exposition Hall Networking Break

0930 hrs

1000 hrs Forum 360 Forum 360 Exposition 1030 hrs Hall Technical Technical Open Sessions Sessions 1100 hrs Technical Sessions

1130 hrs

1200 hrs Recognition Rising Exposition Luncheon: Leaders 1230 hrs Hall Celebrating Achievements Luncheon/ in Aerospace Networking Panel 1300 hrs Luncheon in Exposition Hall Open Design/Structures Lunch On Own and Literary 1330 hrs Excellence

1400 hrs

1430 hrs Forum 360 Forum 360 1500 hrs Technical Networking Technical 1530 hrs Networking Break Sessions Break Sessions 1600 hrs Rising Leaders Corporate 1630 hrs Leadership Member Exchange Reception 1700 hrs (1615–1745 hrs) 1730 hrs Women 1800 hrs at SciTech Happy Hour 1830 hrs SDM Lecture and Keynote 1900 hrs

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 AIAA SciTech 2015

Premier Sponsor and Durand Lecture and Public Policy Luncheon Sponsor

Supporting Sponsors

Livestream Sponsor Student Reception Sponsor

Crean & Associates Aerospace Consultants

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

Get the big picture on space/aviation/propulsion and energy/science and technology/defense from the leading authorities in the field during these high-level discussions and presentations. Monday, 5 January Thursday, 8 January 0800-0900 hrs Osceola Ballroom CD 0800-0900 hrs Osceola Ballroom CD Opening Keynote Plenary Panel Science and Technology Policy Diversity & Inclusion in the Aerospace Workforce Robie Samanta-Roy, Vice President, Technology and Moderator: Sandra H. Magnus, Executive Director, American Innovation, Lockheed Martin Corporation Institute of Aeronautics and Astronautics Panelists: Wesley Harris, Charles Stark Draper Professor of Aeronautics & Tuesday, 6 January Astronautics, Massachusetts Institute of Technology 0800-0900 hrs Osceola Ballroom CD Julio Navarro, Senior Technical Fellow, The Boeing Company Alton Romig, Vice President, Advanced Development Tuesday Morning Keynote Programs, The Skunk Works, Lockheed Martin Aeronautics Tom Shih, Professor and Head of Aeronautics and Astronautics, International Trends in Aerospace: Purdue University Up, Up and Away? To Where? Yvette Weber, Director C-5 Program, United States Air Force James N. Miller, President, Adaptive Strategies, LLC Friday, 9 January Wednesday, 7 January 0800-0900 hrs Osceola Ballroom CD 0800-0900 hrs Osceola Ballroom CD Friday Morning Keynote Plenary Panel Entrepreneurial Aerospace e Future of Design George Whitesides, CEO, Virgin Galactic and The Spaceship Moderator: Richard Christiansen, Vice President, Company Sierra Lobo, Inc. Panelists: Juan Alonso, Associate Professor, Department of Aeronautics, Stanford University Robert Liebeck, Senior Technical Fellow, The Boeing Company Mark Maughmer, Professor of Aerospace Engineering, The Pennsylvania State University

www.aiaa-SciTech.org 11 #aiaaSciTech IntroForum 360 Tuesday, 6 January 0930-1130 hrs Osceola Ballroom B Improving Business Skills and Business Processes for the Aerospace Technical Community Moderator: Andy White, Director, University of Tennessee Aerospace & Defense Business Institute Panelists: These conversations will cover a spectrum of Jeff Babione, Vice President and Deputy GM, Joint Strike Fighter Program, Lockheed Martin Corporation timely topics including programs, systems, policy, Robert Lightfoot, Associate Administrator, NASA operations, applications, platforms and more! Alex Miller, William B. Stokely Chair in Management and former Associate Dean, UT Haslam College of Business Administration Bobby Smart, Deputy Assistant Secretary, Air Force Acquisition Monday, 5 January Integration 0930–1130 hrs Osceola Ballroom B

U.S. Government Aerospace 1400–1600 hrs Osceola Ballroom B Technology Roadmaps Big Data Analytics in Aerospace Moderators: Mark Lewis, Director, IDA Science & Technology Policy Institute Moderator: Ashok Srivastava, Chief Data Scientist, Verizon Panelists: Panelists: Thomas Beutner, Head, Naval Air Warfare and Weapons, Eric Feron, Professor, School of Aerospace Engineering, Office of Naval Research Georgia Institute of Technology Dennis Filler, Director, FAA William J. Hughes Technical John Kelly, Technical Lead, Data Analytics Initiatives, Center Corporate Engineering, Technology, & Operations, Lockheed Martin Corporation David Miller, Chief Technologist, NASA Melanie Lorang, Associate Technical Fellow, The Boeing Robie Samanta-Roy, Vice President, Technology and Company Innovation, Lockheed Martin Corporation Nikunj Oza, Leader, Data Sciences Group, NASA Ames Morley Stone, Chief Technologist, Air Force Research Research Center Laboratory, Wright-Patterson AFB

1400–1600 hrs Osceola Ballroom B Wednesday, 7 January Climate Change and National Security 0930–1130 hrs Osceola Ballroom B Moderator: John Lanicci, Professor, Embry-Riddle Aeronautical University Advanced Manufacturing and its Impact on the Panelists: Design Process of the Future Chad Briggs, Strategy Director, Global Interconnections, LLC Moderator: Graeme Kennedy, Assistant Professor, School of Aerospace Engineering, Georgia Institute of Technology Roger Handberg, Professor, Political Science, College of Sciences, Prelaw Advisor , University of Central Florida Panelists: Peter Jacques, Associate Professor, Department of Political Steven Betza, Corporate Director, Advanced Manufacturing and Science, University of Central Florida Development, Lockheed Martin Corporation Cathy Snyder, Vice President, Energy & Environment, Lockheed Andrew Bicos, Director, Manufacturing Technology Domain, Martin Corporation Enterprise Technology Strategy, Office of the CTO, The David Titley, Director, Center for Solutions to Weather and Boeing Company Climate Risk, The Pennsylvania State University David Rosen, Morris M. Bryan, Jr. Professor and Associate Chair for Administration, The George W. Woodruff School of Mechanical Engineering, Georgia Institute of Technology Mark Shaw, Additive Programs Leader, GE Aviation Arthur Weiss, Executive Director, Defense Advanced Programs, Aerojet Rocketdyne (continued) www.aiaa-SciTech.org 12 #aiaaSciTech ForumIntro 360

Wednesday, 7 January (continued) 1400–1600 hrs Osceola Ballroom B 1400–1600 hrs Osceola Ballroom B The Digital System Model - The New Frontier in NASA Research Plans for Assured Autonomy for Aerospace & Defense Acquisition Aviation Transformation Moderator: Sanjay Garg, Chief, Intelligent Control and Moderator: Edward Kraft, Technical Advisor, Aerospace Autonomy Branch, NASA Glenn Research Center Ground Testing, Air Force Test Center, Arnold Air Force Base Panelists: Kristen Baldwin, Principal Deputy, Office of the Deputy Assistant Secretary of Defense for Systems Engineering John Cavolowsky, Program Director, Airspace Operations and Jeffery Holland , Director of Research and Development and Safety Program, Aeronautics Research Mission Directorate, Chief Scientist, Director of the U.S. Army Engineer Research National Aeronautics and Space Administration and Development Center, U.S. Army Corps of Engineers Jay Dryer, Program Director, Advanced Air Vehicles Program, David Walker, Deputy Assistant Secretary of the Air Force for Aeronautics Research Mission Directorate, National Science, Technology, and Engineering, Office of the Assistant Aeronautics and Space Administration Secretary of the Air Force for Acquisition Robert Pearce, Director – Strategy, Architecture and Analysis, Aeronautics Research Mission Directorate, National Aeronautics and Space Administration Doug Rohn, Program Director, Transformative Aeronautics Thursday, 8 January Concepts Program, Aeronautics Research Mission Directorate, 0930–1130 hrs Osceola Ballroom B National Aeronautics and Space Administration Ed Waggoner, Program Director, Integrated Aviation Systems Aerospace Vehicles Technology Trends Program, Aeronautics Research Mission Directorate, National Aeronautics and Space Administration Moderator: Alton Romig, Vice President, Advanced Development Programs, The Skunk Works, Lockheed Martin Aeronautics Panelists: Frank L. Culbertson, Jr., Executive Vice President and General Manager, Advanced Programs Group, Orbital Sciences Corporation Eric Schrock, Deputy – Technology and Product Innovation, Lockheed Martin Aeronautics John Tracy, Chief Technology Officer and Senior Vice President, Engineering, Operations, and Technology, The Boeing Company Steve Weiner, Chief Engineer, Sikorsky Innovations

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

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

Sunday, 4 January Wednesday, 7 January 1900–2100 hrs Wrecker’s Sports Bar 1615–1745 hrs Osceola Ballroom A Meet and Greet Leadership Exchange and Speed Networking This will be a casual event in the sports bar. A small section A networking event for young aerospace leaders, age 35 and will be reserved so that you can come and meet other people under. who will be participating in the Rising Leaders in Aerospace Mentors include: activities throughout the week. All food and beverages will be at your own expense, but it will be a great way to meet people Allen Arrington, Sierra Lobo, Inc. in a relaxed environment. Kathleen Atkins, Lockheed Martin Corporation Jay Dryer, NASA Headquarters Sanjay Garg, NASA Glenn Research Center Wes Harris, Massachusetts Institute of Technology Monday, 5 January Jeffery Holland, U.S. Army Corps of Engineers 1800–1900 hrs Osceola Ballroom A Tom Irvine, AIAA Reception Sandy Magnus, AIAA Dimitri Mavris, Georgia Institute of Technology The reception will kick off the Rising Leaders in Aerospace Laura McGill, Raytheon Company events and is a perfect opportunity for young leaders to mingle with others who will be participating at AIAA SciTech 2015 as Robert Pearce, NASA Headquarters attendee, presenter, or veteran professional. Come meet other Tom Shih, Purdue University participants in a casual environment. You’re bound to see them Clayton Smith, General Atomics again at Speed Geek, the Leadership Exchange, or the Young Annalisa Weigel, Panoptes Systems Corporation Professional Panel.

Thursday, 8 January Tuesday, 6 January 1200–1330 hrs Osceola Ballroom A 1600–1715 hrs Osceola Ballroom A How to Plan and Achieve Long-Term Speed Geek Career Success A half-dozen or more speakers provide a 5-minute overview Drs. Romig and Tracy have had amazing and fruitful careers on a particular, diverse technical topic with 5 additional in aerospace. In this session they will give the attendees an minutes of questions. Small groups travel from speaker to overview of their careers, discuss major career crossroad speaker over the course of the event in a structured way such decisions they had to make, discuss how career paths may be that, at the end of the event, you’ve been briefed and interacted different for young professionals today, and provide insight with speakers in a small group setting on a variety of subjects. on how to be successful in your career. They will also provide career planning tips and answer questions from the audience. Presenters: Alton Romig, Vice President, Advanced Development Programs, The Skunk Works, Lockheed Martin Aeronautics John Tracy, Chief Technology Officer and Senior Vice President, Engineering, Operations, and Technology, The Boeing Company

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

Monday, 5 January Tuesday, 6 January 1230–1400 hrs Osceola Ballroom CD 1730–1830 hrs Osceola Ballroom CD Durand Lecture for Public Service and Dryden Lecture in Research Public Policy Luncheon Aeroacoustics Making an Impact in Public Service Ann P. Dowling, President, Royal Academy of Engineering, Michael W. Wynne, Former Secretary of the Air Force, Senior London, England Advisor to the President of The Stevens Institute The luncheon is first-come, first-served. Thursday, 8 January 1730–1930 hrs Osceola Ballroom B Sponsored by: Women at SciTech Happy Hour and Keynote Stephanie Bednarek, Government Affairs Manager, SpaceX Women are underrepresented in the engineering sciences and Monday, 5 January industry, and this event will provide an opportunity to meet Reception: 1830–1930 Osceola Foyer informally, network, discuss experiences and identify women Dinner: 1930–2230 Osceola Ballroom C who are leaders in their fields for possible special recognition by AIAA. There is no charge to attend this event. 2015 Associate Fellows Recognition Ceremony and Dinner (Ticketed Event) Please support your colleagues, and join us for the induction of AIAA Associate Fellows – Class of 2015. Tickets are available on a first-come, first-served basis and can be purchased via the AIAA SciTech 2015 registration form or onsite based on availability. Business attire is requested.

1630–1800 hrs Osceola Ballroom B Complex Aerospace Systems Exchange (CASE) Panel Discussion Moderator: Thomas Irvine, Managing Director, Content Development, American Institute of Aeronautics and Astronautics Panelists: David Dress, Deputy Director for Space Technology, Space Technology and Exploration Directorate, NASA Langley Research Center Laura McGill, Deputy Vice President – Engineering, Raytheon Missile Systems Mark Melanson, Manager, Integrated Operations Labs & Technical Services, Lockheed Martin Aeronautics Sophia Bright, Senior Manager, The Boeing Company

www.aiaa-SciTech.org 15 #aiaaSciTech IntroEducational Events AIAA is committed to keeping aerospace professionals at their technical best, and provides an ongoing source of learning, community, professional connections, and career development. Gain the knowledge you need to excel in your field or to move confidently into a new one. Learn how to interact with students and teachers, and help inspire the next generation of aerospace leaders.

Monday, 5 January Tuesday, 6 January

St. George Room 112 and 114 1400–1700 hrs St. George 106 International Student Conference Veriﬁcation and Validation Best Practices for Come see the leaders of tomorrow as the first-place winners of Integrated Computational Materials Engineering the Regional Student Papers Conferences compete to be best This tutorial will benefit a broad cross section of ICME overall in their category. stakeholders, such as materials researchers, educators, design International Student Conference Sponsored by the AIAA and manufacturing engineers, and program managers who Foundation seek to understand how to assess the accuracy of computational • 0900–1230 hrs—Undergraduate Division materials science and engineering simulations. There is no • 1000–1200 hrs—Community Outreach Division charge to attend this session. • 1400–1730 hrs—Masters Division • 1400–1730 hrs—Team Division

www.aiaa-SciTech.org 16 #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. AIAA Student Welcome Reception Welcome Reception Sunday, 4 January Orange Blossom Ballroom Tuesday, 6 January Exposition Hall 1800-1930 hrs 1830–2000 hrs Mingle with your peers and hear from AIAA Executive Take this opportunity to engage new contacts and refresh old Director Sandy Magnus. This reception provides you with the ones. A ticket for the reception is required and included in the opportunity to meet your fellow students and learn more about registration fee where indicated. Additional tickets for guests the opportunities available to you as an AIAA student member. may be purchased upon registration or on site, as space is available. Sponsored by: Luncheon in the Exposition Hall Wednesday, 7 January Exposition Hall Networking Coffee Breaks 1230–1400 hrs Coffee breaks allow even more time for making new contacts, A ticket is required and included in the registration fee continuing discussions from sessions, visiting the Exposition where indicated. Hall, or checking emails and voicemails to keep in touch with the office while you are at the forum. Coffee breaks will be located in the following locations and times: Infotech@Aerospace Meet and Greet Monday, 5 January 0900, 1530 hrs; Osceola Lobby Wednesday, 7 January Osceola 1 Tuesday, 6 January 0900, 1530 hrs; Exposition Hall 1830–2000 hrs Wednesday, 7 January 0900, 1530 hrs; Exposition Hall Thursday, 8 January 0900 hrs; Exposition Hall Women at SciTech Happy Hour and Keynote 1530 hrs; Osceola Lobby Thursday, 8 January Osceola Ballroom B Friday, 9 January 0900 hrs; Osceola Lobby 1730–1930 hrs Women are underrepresented in the engineering sciences and industry, and this event will provide an opportunity to meet informally, network, discuss experiences and identify women who are leaders in their fields for possible special recognition by AIAA. There is no charge to attend this event.

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

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, 5 January Tuesday, 6 January 0930–1030 hrs Osceola Ballroom A 0900–1100 hrs St. George 106 Spacecraft Structures Lecture AIAA Foundation Student Awards Breakfast (By Invitation Only) Advanced Solar Arrays for NASA Electric Propulsion Missions This awards breakfast is by invitation only. The winners of the AIAA Foundation International Student Conference will be Tom Kerslake, Power System Engineer, NASA Glenn Research announced. Also the recipients of the following awards will be Center, Cleveland, Ohio recognized by Steve Gorrell, Vice President, Education: Fanny Besem, Orville and Wilbur Wright Graduate Award 1400–1500 hrs Osceola Ballroom A Giuseppe Cataldo, Orville and Wilbur Wright Graduate Award Non-Deterministic Approaches Lecture Armando Gomez-Farias, Zarem Award for Distinguished e Building Block Approach in the 21st Century — Achievement e Role of ICME & UQ Arturo Montoya, Zarem Award for Distinguished Achievement (Faculty Advisor) Rolland Dutton, Chief, Manufacturing and Industrial Technologies Division, AFRL/RXM, Wright-Patterson AFB 0930–1030 hrs Osceola Ballroom A Reception: 1830–1930 hrs Osceola Foyer Adaptive Structures Lecture Dinner: 1930–2230 hrs Osceola Ballroom C Micro Aerial Vehicles (MAV): Challenges and 2015 Associate Fellows Recognition Ceremony Opportunities and Dinner Inderjit Chopra, Alfred Gessow and Distinguished University A ticket for the dinner is required and not included in the Professor, University of Maryland registration fee. Additional tickets for guests may be purchased upon registration or on site, as space is available. 1230–1400 hrs Osceola Ballroom CD Recognition Luncheon—Celebrating Achievements in Aerospace Sciences and Information Systems A ticket for the luncheon is required and included in the registration fee where indicated. Additional tickets for guests may be purchased upon registration or on site, as space is available. The following awards will be presented: Aerospace Software Engineering Award Karen Gundy-Burlet Flight Software Lead LADEE NASA Ames Research Center Moffett Field, California “For over thirty years of significant research and innovations in the software engineering simulations of computational fluid dynamics and efficient spacecraft flight control software.”

(continued) www.aiaa-SciTech.org 18 #aiaaSciTech IntroRecognition Events

deFlorez Award For Flight Simulation Certiﬁcate of Merit for Best Papers: Cleve Moler Atmospheric Flight Mechanics Best Paper Chief Mathematician, Chairman and Co-Founder “Robust Modal Filtering and Control of the X-56A Model MathWorks with Simulated Fiber Optic Sensor Failures,” AIAA 2014-2053, Natick, Massachusetts Peter Suh and Alexander Chin, NASA Dryden Flight Research “For significant impact to the science of flight simulation Center; and Dimitri N Mavris, Georgia Institute of Technology. through development of computational algorithms underlying Modeling & Simulation Best Papers an environment now used widely to create multi-domain models “Frequency-Domain Method for Automated Simulation and operational software.” Updates based on Flight Data,” AIAA 2014-0472, Eugene Faculty Advisor Award Morelli, NASA Langley Research Center and Jared Cooper, Baron Associates. Joseph Majdalani Chair, Department of Aerospace Engineering “An Evaluation of Several Stall Models for Commercial Auburn University Transport Training,” AIAA 2014-1002, Jeffrey Schroeder, FAA; Auburn, Alabama Judith Burki-Cohen, USDOT-RITA-Volpe Center; David Shikany, The Boeing Company; David Gingras, Bihrle Applied “For unwavering devotion to student success in the AIAA Research Inc.; and Paul Desrochers, Test Pilot, Inc. Southeast Region yielding eight regional and two national AIAA awards, with eight-out-of-eight best papers within five years.” Intelligent Systems Best Paper “Robust Trajectory Planning for Autonomous Parafoils J. Leland Atwood Award under Wind Uncertainty,” AIAA 2013-4584, Brandon Luders, John Valasek Ian Sugel, and Jonathan How, Massachusetts Institute of Professor, Aerospace Engineering Technology. Texas A&M University Announcement of Student Competition Winners: College Station, Texas Atmospheric Flight Mechanics Student Paper “For outstanding contributions to the aerospace profession and Guidance, Navigation, and Control Student Paper deep commitment to the education and professional development of aerospace engineering students.” Intelligent Systems Student Paper Lawrence Sperry Award Jeremy T. Pinier LaRC SLS Lead for Aerosciences Wednesday, 7 January Configuration Aerodynamics Branch NASA Langley Research Center 1800–1900 hrs Osceola Ballroom B Hampton, Virginia “For significant technical accomplishments and leadership in the Structures, Structural Dynamics and aerodynamic design and development of the next U.S. crew and Materials Lecture heavy-lift launch vehicles.” Sustained Service Award Aerospace Structural Design and Safety: Do We Need David Klyde Fewer Tests or More? Vice President, Research and Engineering Services Raphael Haftka, Distinguished Professor, University of Florida System Technology, Inc. Hawthorne, California “For nearly two decades of service to AIAA including technical committee leadership, distinguished lecturer, journal associate editor, and corporate member advisory committee.”

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

Thursday, 8 January Pendray Aerospace Literature Award Antony Jameson 1200–1400 hrs Osceola Ballroom CD Thomas V. Jones Professor of Engineering Department of Aeronautics and Astronautics Recognition Luncheon—Celebrating Achievements Stanford University in Aerospace Design/Structures and Literary Stanford, California Excellence “For seminal and high-impact research papers in the field of computational fluid dynamics and aerodynamic optimization.” Commercial Spaceight: What Has Changed Certificate of Merit for Best Papers: Speaker: Christopher J. Ferguson, Director, Crew and Mission ASME/Boeing Best Paper Systems, Commercial Crew Program, Boeing Space Exploration “In-Flight Aeroelastic Stability of the Thermal Protection A ticket for the luncheon is required and included in the System on the NASA HIAD, Part I: Linear Theory” AIAA registration fee where indicated. Additional tickets for guests 2014-1520, Benjamin Goldman and Earl Dowell, Duke may be purchased upon registration or on site, as space is University; and Robert Scott, NASA Langley Research Center. available. Collier Research Hypersizer/AIAA Structures Best Paper The following awards will be presented: “Internally Reinforced Adhesively Bonded Metal to Composite Walter J. and Angeline H. Crichlow Trust Prize Joints,” AIAA 2014-1530, Stephen Clay, Air Force Research Laboratory and Vipul Ranatunga, Miami University. Satya N. Atluri Distinguished Professor, Mechanical and Aerospace Spacecraft Structures Best Paper Engineering, The Henry Samueli School of Engineering “Testing and Application of Numerically Determined and Director, Center For Aerospace Research and Education Expandable and Foldable Space Structures” AIAA 2014-1511, University of California-Irvine Daniel Kling, Jonathan Hinkle, Ryan Cook and Cliff Willey, Irvine, California ILC Dover; and William Doggett, NASA Langley Research “For lasting contributions to airframe structural integrity and Center. durability analysis using novel computational methods (MLPG meshless methods) and micromechanics of materials genome.” Announcement of Student Competition Winners: Children’s Literature Award Jefferson Goblet Student Paper Award Margaret A. Weitekamp The Harry H. and Lois G. Hilton Student Paper Curator, Space History Department Award in Structures Smithsonian National Air and Space Museum Lockheed Martin Student Paper Award in Structures Washington, D.C. American Society for Composites Student Paper “Pluto’s Secret: An Icy World’s Tale of Discovery” in Composites Award History Manuscript Award Southwest Research Institute Student Paper Award in Non- Frederick Johnsen Deterministic Approaches Former U.S. Air Force Historian and Retired Director of the Air Force Flight Test Center Museum Edwards Air Force Base, California “Sweeping Forward” Gardner-Lasser Aerospace History Literature Award Dennis R. Jenkins Aerospace Historian Cape Canaveral, Florida “Dressing For Altitude”

www.aiaa-SciTech.org 20 #aiaaSciTech IntroExposition Hall

The Exposition Hall is the hub of activity during this event—from seeing exhibitor displays to enjoying networking breaks and other functions. All the 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. The Exposition Hall is located on the lower level of the Convention Center, two floors below AIAA registration.

Exposition Hall Hours Tuesday, 6 January 0900–1230 hrs 1400–1600 hrs Reception* 1830–2000 hrs Wednesday, 7 January 0900–1600 hrs Luncheon* 1230–1400 hrs Thursday, 8 January 0900–1200 hrs

*A ticket is required to attend.

AIAA Pavilion Stop by the AIAA Pavilion, located in the Exposition Hall, to browse publications and merchandise, learn about your membership benefits, and meet AIAA staff. 30% Off All Books at AIAA SciTech 2015 AIAA Publications is offering a special discount on all titles featured at AIAA SciTech 2015. Attendees can take advantage of a 30% discount off the list price of all books for sale at the AIAA Bookstore located in the AIAA Pavilion. This special offer will only be available during the forum! Take advantage of these super savings and visit the AIAA Bookstore!

Meet the Author Sessions Thomas R. Yechout Introduction to Aircraft Flight Mechanics, 2E Tuesday, 6 January AIAA Pavilion Opening Reception

Daniel P. Raymer Aircraft Design, 5E and RDSWin Student AIAA Pavilion Wednesday, 7 January AM Networking Coffee Break Exposition Hall Luncheon

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AIAA Spirit Dunmore MSC Software Collier Higher Orbits Central Florida FlexSys Aerosystems Corp. IDT Section 124 223 224 323 324 423 424 523 Hanley Cambridge Convergent Granta ARi/Okazaki MathWorks Micro Craft Triumph Innovations Flow SG Science Solutions Design 122 221 222 321 322 421 422 521 522 CEI ANSYS 320 419 Dantec Dynamics Sabalcore Boeing NIA 517418 Software Quantel Tetra Cambridge Cradle USA Research ATK CFD Show 116 215 216 315 316 415 416 515 Ofﬁce Holloman NRC High Speed Pointwise SmartUQ Test Track Nat Acad 114 213 314 413 Tri ViGYAN Aerosoft Models Exhibitor 212 311 412 Springer Air Force Desktop Lounge Photron NRO Reserve Aeronautics Metacomp 210 309 CD- 410 509 NASA adapco 409 LaVision FlackTek Airborne BETA CAE Tecplot Systems 108 207 208 307 308 407 408 507

UCRI Lockheed Kamatics/ Cray NASA RWG Martin 104 203 Intelligent 404 503 ONR Skunk Light Applied NUMECA USC ® dSPACE Dynamics ONR Works International 102 201 202 302 402 501 502 ENTRANCE

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Exhibitors by Booth Number

311 Aerosoft, Inc 202 Lockheed Martin Skunk Works® 523 AIAA Central Florida Section 122 MathWorks 507 Airborne Systems 207 Metacomp Technologies 419 ANSYS, Inc. 221 Micro Craft, Inc 501 Applied Dynamics International (ADI) 124 MSC Software 522 ARi/Okazaki 108 NASA/Kennedy Space Center Public Affairs 415 ATK 104 NASA Space Technology Mission Directorate 407 BETA CAE Systems USA, Inc. 315 National Institute of Aerospace (NIA) 216 Boeing Technology Services 309 National Reconnaissance Office (NRO) 421 Cambridge Flow Solutions Ltd. 314 National Research Council of the National 416 Cambridge University Press Academies 308 CD-adapco 102 NUMECA USA, Inc. 320 Computational Engineering International 502/503 Office of Naval Research 222 Convergent Science, Inc. 210 Photron 503 Cray 213 Pointwise, Inc. 418 Dantec Dynamics, Inc. 215 Quantel, USA 410 Desktop Aeronautics, Inc. 517 Sabalcore Computing Inc. 402 dSPACE 413 SmartUQ 324 DUNMORE Corporation 116 Software Cradle 515 Ennova-CFD 521 SG — Space and Ground Engineering Solutions 307 FlackTek 323 Spirit Aerosystems 224 FlexSys 509 Springer 422 Granta Design 408 Tecplot, Inc. 322 Hanley Innovations 316 Tetra Research Corporation 423 Higher Orbits 412 Tri Models, Inc. 114 Holloman High Speed Test Track 321 Triumph Aerospace Systems — Newport News 223 HyperSizer® - Collier Research Corporation 409 United States Air Force Reserve 424 Integrated Design Tools, Inc (IDT) 203 University of Cincinnati Research Institute (UCRI) 302 Intelligent Light 201 University of Southern California (USC) 404 Kamatics/RWG 212 ViGYAN, Inc. 208 LaVision, Inc.

www.aiaa-SciTech.org 23 #aiaaSciTech Exhibitors Aerosoft, Inc. 311 Applied Dynamics International 501 2000 Kraft Drive, Suite 1400 Applied Dynamics International Blacksburg, VA 24060 Ann Arbor, MI 48101 www.aerosoftinc.com www.adi.com [email protected] [email protected] AeroSoft specializes in high-fidelity numerical algorithms for Applied Dynamics helps companies make better use of aerodynamic simulation and design. Services include licensing, simulation assets through all stages of product development, training and support of GASP, our premier structured and verification testing, demonstration, training, and maintenance. unstructured flow solver, as well as detailed analysis of Our user base includes more than 50% of the Fortune 500 customer applications and customized solutions. Come by and aerospace and defense companies and extends into marine, see what’s new with GASP version 5.2. power systems, oil & gas, and the automotive industry.

AIAA Central Florida Section 523 ARi / Okazaki 522 1082 West Riviera Blvd 381 ARi Court Oviedo, FL 32765 Addison, IL 60101 info.aiaa.org/Regions/SE/CF/default.aspx www.ariindustries.com [email protected] The Central Florida Section of the American Institute of Aeronautics and Astronautics is dedicated to furthering We are a leading designer and manufacturer of temperature the interests, activities, and technical programs of local sensors and heaters for applications ranging from -269 C professional, students and educators within the aerospace to +2200 C. Our metal sheath mineral insulated products community. withstand harsh environments and used in gas turbine engines, satellite thrusters, and rocket fuel engines. Airborne Systems 507 5800 Magnolia Avenue ATK 415 Pennsauken, NJ 08109 77 Raynor Avenue www.airborne-sys.com Ronkonkoma, NY 11779 [email protected] www.ATK.com Airborne Systems is a world leader in the design, development, ATK is a premier aerospace, defense and fabrication, test and integration of Entry Descent and commercial products company. Its Ronkonkoma, New York Landing Systems (EDLS), including parachutes systems, Air location is a world-class facility that features extensive test Bag Landing Attenuation systems, Inflatable Aerodynamic cell and wind tunnel infrastructure to address technology development for high speed propulsion, combustion systems Decelerators. We provide EDLS systems for various aircraft and related technologies. and spacecraft and are leading the development of new technologies including Inflatable Aerodynamic Decelerators. BETA CAE Systems USA, Inc. 407 ANSYS, Inc. 419 29800 Middlebelt Road Suite #100 2600 ANSYS Drive Farmington Hills, MI 48334 Cannonsburg, PA 15317 www.ansa-usa.com www.ansys.com [email protected] [email protected] BETA CAE Systems is an engineering services company that ANSYS, Inc. develops and globally markets engineering distributes & supports the industry leading ANSA & META simulation software used by designers and engineers software. ANSA is a CAE pre-processing tool for FE & CFD across the aerospace and defense industry. Our open and Analysis, for full-model build, from CAD to solver input file, flexible simulation solutions enable users to simulate design in one integrated environment. performance using an open platform for fast, efficient and cost-effective product development.

www.aiaa-SciTech.org 24 #aiaaSciTech Exhibitors Boeing Technology Services 216 Computational Engineering International 320 7755 E. Marginal Way S 2166 N. Salem Street Mail Code 1W-02 Apex, NC 27523 Seattle, WA 98108 www.ceisoftware.com www.boeing.com/bts [email protected] Boeing is the world’s leading aerospace company, and EnSight is a data visualization software used in CFD & FEA. employs more than 169,000 people around the world. EnSight is easy to learn, has a powerful calculator, Python Boeing Technology Services (BTS) is the point of access to scripting, batch and interactive usage & high quality graphics. more than 500 testing facilities across the US. BTS contracts New in EnSight 10.1 is case comparison, native polyhedral with companies, educational institutions, and government support, improved HPC model support, much faster particle organizations for use of Boeing laboratories. rendering and many more enhancements.

Cambridge Flow Solutions Ltd. 421 Convergent Science, Inc. 222 Compass House 6400 Enterprise Lane Vision Park Madison, WI 53719 Histon www.convergecfd.com Cambridge, Cambridgshire, [email protected] UK CB24 9AD www.cambridgeﬂowsolutions.com/ Convergent Science, Inc. is a world leader in Computational info@cambridgeﬂowsolutions.com Fluid Dynamics (CFD). The flagship product, CONVERGE™, is shifting the paradigm toward predictive CFD. The Cambridge Flow Solutions develops advanced mesh generation groundbreaking technology removes the user defined mesh and CFD software, specifically tailored to high performance computing. It is the power behind highly efficient higher- and implements an innovative new process that fully couples order LES solver technology, and behind BOXERMesh, the the automated mesh with the solver at runtime. advanced, easy-to-use parallel mesh generation system that delivers significant capability and productivity benefits. Cray 503 901 Fifth Avenue Suite 1000 Cambridge University Press 416 Seattle, WA 981642 32 Avenue of the Americas www.cray.com New York, NY 10013 [email protected] www.cambridge.org/us/academic Global supercomputing leader Cray builds innovative systems [email protected] and solutions enabling researchers in academia, government, Cambridge’s publishing in books and journals combines state- and industry to meet existing and future simulation and of-the-art content with the highest standards of scholarship, analytics challenges. writing and production. Visit our stand to browse new titles, available at a 20% discount, and to pick up sample issues of our journals. Visit our website to see everything we do: www. Dantec Dynamics, Inc. 418 cambridge.org/us/academic. 750 Blue Point Road Holtville, NY 11742 www.dantecdynamics.com CD-adapco 308 [email protected] 60 Broadhollow Road Dantec Dynamics is a leading developer and supplier of Melville, NY 11747 advanced measurement systems for fluid mechanics, solid www.cd-adapco.com mechanics, microfluidics, spray analysis and combustion [email protected] technology. Our products include: PIV, CTA, LDA, PDA, CD-adapco is the world’s largest independent CFD focused PLIF, DIC, and more. Measurement data include velocity, provider of engineering simulation software, support and turbulence, particle size, concentration, temperature, services. We have over 30 years of experience in engineering combustion species, strain/stress and vibration. simulation. The scope of our activities extends well beyond software development to encompass a wide range of CAE engineering services in both CFD and FEA.

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Desktop Aeronautics Inc. 410 Flacktek 307 1900 Embarcadero Road 1708 Highway 11 Bldg. G Suite 101 Landrum, SC 29356 Palo Alto, CA 94303 www.flacktek.net www.desktopaero.com sharon@flacktec.net [email protected] The FlackTek SpeedMixer is an advanced tool for mixing, Desktop Aeronautics is a software company and the distributor grinding/milling and dispersing. This Non-Invasive of NASA’s Cartesian Euler CFD code: Cart3D. Our flagship MixingTM technology removes air bubbles while product, GoCart, gives users easy access Cart3D’s capabilities homogenizing the sample in a matter of seconds, and there and addresses the diverse aspects of aerodynamics & vehicle is ABSOLUTELY NO CLEANUP! The SpeedMixer can be design. Users can quickly run analyses, do trade studies, and used to process any combination of powders, pastes, putties, build databases. Explore your design space. and liquids in batches ranging from 1g to 5Kg. Please visit our booth to learn how a SpeedMixer can benefit your R&D, quality control and specialty productions. dSPACE 402 50131 Pontiac Trail Wixom, MI 48393-2020 FlexSys 224 www.dspaceinc.com 2205 Commonwealth [email protected] Suite D dSPACE is the world’s leading provider of hardware and software Ann Arbpr, MI 48105 tools for developing and testing sophisticated electronic control www.flxsys.com systems. For over 20 years, dSPACE’s high-quality, off-the-shelf flexinfo@flxsys.com software and hardware tools have empowered engineers to FlexSys is the world-leader in variable geometry wings that design and innovate, while dramatically reducing development offer significant reduction in fuel-burn, noise and stresses. times and cost. Learn more by visiting: www.dspaceinc.com. Our pioneering design methods enable lightweight, reliable and cost-effective seamless shape-adaptive control surfaces. A Gulfstream business-jet retrofitted with FlexFoil(TM) DUNMORE Corporation 324 technology is undergoing flight testing at NASA. 145 Wharton Road Bristol, PA 19007

www.dunmore.com R Granta Design 422 [email protected] 300 Rustat House DUNMORE is a manufacturer of engineered films and tapes 62 Clifton Road for aerospace, supplying multilayer insulation materials to Cambridge, Cambridgeshire UK the aerospace industry for over twenty-five years. With a CB1 7EG www.grantadesign.com highly technical product base of over 400 certified products, [email protected] DUNMORE is the trusted source for engineered aerospace films and tapes. Granta Design is the materials information technology leader. Our materials data and information management solutions help aerospace enterprises to: manage data on composites, metals, and plastics; enable better materials decisions; reduce Ennova-CFD 515 regulatory and environmental risk; and provide materials 2150 Allston Way support for design, analysis, and simulation. Suite 250 Berkeley, CA 94704 www.ennova-cfd.com Hanley Innovations 322 [email protected] 505 Spring Lake Road Leading edge grid generation software for computational Ocala, FL 34472 fluid dynamics (CFD). Automated mesh generation for www.hanleyinnovations.com unstructured, structured and hybrid grids for internal and [email protected] external flows. Stallion 3D with HIST The ONLY truly automatic, All-In-One, 3D Navier-Stokes/Euler analysis software that runs on your Windows PC. Bring a STL file to watch Stallion 3D set-up your arbitrary geometry in seconds.

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Higher Orbits 423 Intelligent Light 302 32 Upshur Road 301 Route 17 N. 7th Floor Annapolis, MD 21402 Rutherford, NJ 07070 www.higherorbits.org www.ilight.com [email protected] [email protected] Higher Orbits strives to launch students to higher Intelligent Light provides post-processing, data management levels of performance, leadership and teamwork by using and big data visualization capability for CFD. Thousands of the wonder of spaceflight to ignite a passion for Science, users rely on the industry leading FieldView software and our Technology, Engineering & Math (STEM). Mankind’s journey custom engineering services to maximize their productivity into space serves as an ideal launchpad to excite students of all ages about STEM, Leadership and working to fulfill their and effectiveness. Let us help you eliminate bottlenecks and dreams and ambitions. achieve breakthrough results.

Holloman High Speed Test Track 114 Kamatics/RWG 404 1521 Test Track Road 1330 Blue Hills Ave Holloman AFB, NM 88330 Bloomﬁeld, CT 06002 www.holloman.af.mil www.kaman.com/engineered [email protected] [email protected] The Holloman High Speed Test Track is a DoD test facility that For decades, Kamatics (USA) and RWG have been designing, provides an efficient means of evaluating customer systems testing, and manufacturing the highest performing bearings through world-class technical photo and electronic data and flight critical parts in the industry, excelling under the collection while minimizing risk and cost. Rocket sled test most demanding conditions. environments include hypersonic impact, egress, calibrated rain, and a magnetic levitation capability. LaVision, Inc. 208

® 211 W. Michigan Avenue, Suite 100 HyperSizer - Collier Research Corporation 223 Ypsilanti, MI 48197 760 Pilot House Dr. Ste. A www.lavisioninc.com Newport News, VA 23606 [email protected] www.hypersizer.com LaVision provides integrated imaging systems to scientific, [email protected] industrial and education markets. LaVision has extensive As Collier Research Corporation’s flagship product, HyperSizer experience in optical techniques such as 2-D, stereo and Software performs design, stress analysis, and detail sizing tomographic particle image velocimetry, gaseous and liquid optimization for aerospace vehicles fabricated with composite laser induced fluorescence, shadography for multi-phase flows, or metallic materials. On average, the software reduces the digital image correlation for deformation/strain, high-speed weight of structures by 20-40%, an exceptional achievement for and ultra-high-speed imaging, and intensified camera systems. aerostructures.

® Integrated Design Tools, Inc. (IDT) 424 Lockheed Martin Skunk Works 202 1011 Lockheed Way 1W Mountain St. #3 Palmdale, CA 935997 Pasadena, CA 91106 www.lockheedmartin.com/ www.idtvision.com us/aeronautics/skunkworks.html [email protected] [email protected] Integrated Design Tools, Inc. (IDT) began in 1997 with the The Skunk Works is focused on the critical aircraft for purpose of providing digital imaging solutions for scientific tomorrow. Advanced technology solutions draw on our world- and industrial communities. Our standard is excellence class capabilities in conceptual design, systems engineering supported by our team of leading scientists in the fields of and integration, complex project management, software applied physics, imaging sensors, digital camera design and development and rapid prototyping. software. While high-speed digital imaging is our specialty, IDT also offers highly integrated systems that include data acquisition and signal synchronization modules. The product lines embrace industry standards such as high-speed USB and Gigabit Ethernet to supply plug-and-play instruments that are reliable, cost-effective, and easy to use.

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MathWorks 122 NASA/Kennedy Space Center Public Affairs 108 3 Apple Hill Drive Kennedy Space Center 32899 Natick, MA 01760 ksc-exhibits@nasa.gov www.mathworks.com Find out what is going on at NASA/Kennedy Space MathWorks is the leading developer of mathematical Center! Stop by our booth # 108! computing software. Engineers and scientists worldwide rely on its products to accelerate the pace of discovery, innovation, and development. For more information visit www.mathworks. NASA Space Technology Mission Directorate 104 com. 300 E St. SW Washington, D.C. 20024 Metacomp Technologies 207 www.nasa.gov/spacetech 28632 Roadside Drive, Suite 255 NASA’s Space Technology Mission Directorate rapidly Agoura Hills, CA 91301 develops, demonstrates, and infuses revolutionary, high-payoff www.metacomptech.com technologies through transparent, collaborative partnerships, [email protected] expanding the boundaries of the aerospace enterprise. Metacomp Technologies develops CFD++, for simulating compressible and incompressible fluids, unsteady and steady flows, regimes from very low speeds to high hypersonic National Institute of Aerospace 315 speeds, laminar and turbulent flows, multiphase effects, 100 Exploration Way cavitation effects, various thermal effects, overset meshes with Hampton, VA 23666 rigid-body-dynamics, conjugate heat transfer capabilities. www.NIAnet.org [email protected] The National Institute of Aerospace (NIA) is a non-profit Micro Craft, Inc. 221 research and graduate education institute created to conduct 207 Big Springs Ave. innovative aerospace and atmospheric research, develop Tullahoma, TN 37388 new technologies for the nation and help inspire the next www.microcraft.aero generation of scientists and engineers. [email protected] Micro Craft, Inc. is a 100% Employee Owned Small Business located in Tullahoma, Tennessee. We produce flight hardware National Reconnaissance Office (NRO) 309 for a wide variety of aircraft, wind tunnel models and space 14675 Lee Road flight hardware. We possess excellent capabilities in design Chantilly, VA 21051 and test engineering services. dii.westﬁeld.net [email protected] MSC Software 124 The National Reconnaissance Office’s Director’s 4675 MacArthur Court Innovation Initiative invests in advanced technologies, Suite 900 fosters innovation, and provides seed funding to push the Newport Beach, CA 92660 boundaries of technology to dramatically improve our satellite www.mscsoftware.com reconnaissance capabilities. It presents an opportunity for developers not traditionally associated with the NRO to MSC Software makes products that enable engineers to validate and optimize their designs using virtual prototypes. participate in building the National Reconnaissance Office of Customers in almost every part of manufacturing use our the 21st century. software to complement, and in some cases even replace the physical prototype “build and test” process that has traditionally been used in product design.

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National Research Council of 314 Pointwise, Inc. 213 the National Academies 213 S. Jennings Avenue 500 Fifth Street, NW Fort Worth, TX 76104 Washington, DC 20001 www.pointwise.com www.nationalacademies.org/rap [email protected] [email protected] Pointwise, Inc. is solving the top problems facing engineering The National Research Council of the National Academies analysts today: mesh generation for computational fluid offers awards for graduate, postdoctoral and senior research dynamics. Manufacturing firms and research organizations use in US federal laboratories and affiliated institutions. Awards Pointwise’s mesh generation software to seamlessly bridge the include generous stipends, relocation, professional travel and gap between CAD and computational fluid dynamics analysis. a health insurance plan. Complete information and online Find more information at pointwise.com. applications are on the Website. Quantel, USA 215 NUMECA USA, Inc. 102 601 Haggerty Lane 1044 Larkin Street Bozeman, MT 59715 San Francisco, CA 94109 www.quantel-laser.com www.numeca.com [email protected] [email protected] Quantel is a recognized expert in the manufacturing of Based on the most advanced technology, NUMECA software solid-state laser systems for scientific, military and industrial is focused on innovation in CFD and recognized for its applications. We provide technologically advanced laser application-driven features and interface, optimal solutions, systems to help you to achieve your specific goals: pulsed multi-physics models, high accuracy, speed, and general user- solid-state lasers, tunable dye lasers, high power laser diodes. friendliness. Our worldwide teams continuously improve our Quantel also provides manufacturers and optical users software to turn your product design into a real success. worldwide with industry leading laser damage testing.

Office of Naval Research 502 Sabalcore Computing Inc. 517 875 North Randolph Street 3153 Skyway Circle Arlington, VA 22203 Suite 105 www.onr.navy.mil Melbourne, FL 32934 [email protected] Where Data www.sabalcore.com Becomes Discovery ™ The Office of Naval Research’s Naval [email protected] Air Warfare and Weapons division supports the Navy’s power High Performance Computing in the Cloud - Rent CPUs by projection needs, fostering the technology development of the hour - Sabalcore provides easy to use high performance naval aircraft, structures, propulsion, autonomy, energetics, computing (HPC) services in the Cloud. Formed in 2000 as directed energy and electric weapons. Visit us at Booth #502. the first company to provide on-demand high performance computing services, Sabalcore brings 15 years of experience to help its customers achieve success. Photron 210 9520 Padgett Street, Suite 110 San Diego, CA 92126 SmartUQ 413 www.photron.com 1245 E. Washington Ave [email protected] Suite 210 Madison, WI 53703 Photron has fifty years’ experience in manufacturing a high- www.smartuq.com speed video cameras for slow motion analysis of events [email protected] occurring to fast to understand. Systems include highly light SmartUQ uses cutting-edge analytics to accelerate simulation, sensitive mega pixel to 21,000 frames per second (fps) cameras, saving time and costs for industries that make simulation- high-G imagers for hostile environments, miniature remote based decisions. To learn more about our modern design head cameras to high definition high-speed cameras. of experiments, fast meta-modeling, design optimization, calibration, sensitivity analysis and uncertainty quantification features, visit SmartUQ.com.

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Software Cradle 116 Tecplot, Inc 408 70 Birch Alley, Suite 240 3535 Factoria Blvd SE, Suite 550 Beavercreek, OH 45440 Bellevue, WA 98006 www.cradle-cfd.com 425-653-1200 X236 (phone) [email protected] 425-653-9200 (fax) www.tecplot.com Software Cradle is a leading provider of Computational Fluid [email protected] Dynamics (CFD) software including SC/Tetra (unstructured mesh), scSTREAM (Cartesian mesh), and HEAT Designer Tecplot delivers CFD post-processing software that allows (Cartesian mesh for electronics). Since inception in 1984, engineers and scientists to discover, analyze, and understand Cradle has established itself as a major innovator for advancing information in complex data, and to effectively communicate the role of simulation in engineering design. the results. For over 30 years, and with thousands of users worldwide, Tecplot has become a trusted name in data visualization. SG – Space & Ground Engineering Solutions 521 6A Aigiidon Street Athens, Attica, Greece 11853 Tetra Research Corporation 316 www.sg-incorp.com 420 Park Ave. West [email protected] Princeton, IL 61356 www.tetraresearch.com SG Company provides integrated engineering solutions [email protected] for air/space-based earth monitoring systems and develops special techniques for UAS (Unmanned Aerial Systems) earth Tetra Research specializes in Loci/CHEM development and observation applications in various disciplines. applications. Loci/CHEM is a unique CFD software tool used by NASA and industry partners for stage separation, solid motor ignition and other multi-disciplinary analyses. Spirit Aerosystems 323 We provide support, customized development and training P.O. Box 780008 services to allow you to make the most productive use of Loci/ Wichita, KS 67278 CHEM. www.spiritaero.com Spirit AeroSystems, Inc. is one Tri Models Inc. 412 of the largest non-OEM designers and manufacturers of aerostructures for commercial, military and business/regional 5191 Oceanus Drive Huntington Beach, CA 92649 jets in the world. Spirit offers a wide variety of test capabilities www.trimodels.com including acoustic, vibration, material static/fatigue, and full [email protected] scale structures testing. Tri Models is the Premier supplier of Wind Tunnel Models & Ground Test hardware for the global aerospace community. Springer 509 We play a vital role in the development of new systems for the 233 Spring Street airframe companies. Whether you have a new program or are New York, NY 10013 refining an existing vehicle, Tri Models can help. www.springer.com [email protected] Triumph Aerospace Systems—Newport News 321 We are proud to be the publisher of choice for numerous books, valued by researchers globally, and high-quality 703 Middle Ground Boulevard Newport News, VA 23606 journals. Come and browse our key titles! Get 20% off print www.triumphgroup.com/companies books and eBooks – and learn about MyCopy (a printed eBook /triumpn-aeros-ace-systems-newport-news for $24.99). Meet our Senior Editor Silvia Schilgerius to discuss [email protected] your publishing proposal. Ensure maximum readership for your work, too! Springer, your partner in publishing. Find all Triumph Aerospace Systems - Newport News is an industry offers online @ springer.com/aiaa. leader in the engineering and manufacture of complex aerospace hardware and force measurement systems (balances) for wind tunnel, ground test, and flight applications.

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United States Air Force Reserve 409

UCRI 203 51 Goodman Drive ML 0663 Cincinnati, OH 45221 www.ucri.org UNIVERSITY of CINCINNATI [email protected] RESEARCH INSTITUTE UCRI is an independent not-for-profit 501(c)(3) organization which serves for the University of Cincinnati (UC). UCRI makes it easy for the industry partners to connect with UC on business ideas, research projects, resource needs and other industry essentials.

University of Southern California 201 3650 McClintock Ave. OHE 106 Los Angeles, CA 90089 http://viterbi.usc.edu/GAPP [email protected] The USC Viterbi School of Engineering offers 40+ graduate programs entirely online through the Distance Education Network (DEN@Viterbi). Programs include the M.S. in Astronautical Engineering which encompasses the dynamic and cutting-edge field of advanced space technology, with a unique focus on spacecraft engineering.

ViGYAN, Inc. 212 30 Research Drive Hampton, VA 23666 www.vigyan.com [email protected] ViGYAN provides aerospace and engineering research and development services to NASA, other Government agencies, and corporations. We have expertise in wind tunnel testing and systems, operating the ViGYAN Wind Tunnel in Hampton, Virginia, now approved as an accredited ISO 17025 laboratory by the American Association for Laboratory Accreditation (A2LA). ViGYAN is ISO 9001 certified.

www.aiaa-SciTech.org 31 #aiaaSciTech IntroGeneral Information

AIAA Registration and Information Center Hours Conference Proceedings The AIAA Registration and Information Center will be located Proceedings for the forum will be available online. The cost on the ballroom level of the Convention Center. is included in the registration fee where indicated. Online Sunday, 4 January 1500–1900 hrs proceedings will be available on Monday, 5 January. Monday, 5 January –Thursday, 8 January 0700–1730 hrs Instructions to Access Proceedings: 1. To view proceedings, visit www.aiaa.org >ARC>Meeting Papers. Friday, 9 January 0700–1300 hrs a. Log in with the link at the top right of the page. b. Select the appropriate conference from the list. Wi-Fi Internet Access On Site c. Search for individual papers with the Quick Search toolbar AIAA is providing limited Wi-Fi service for attendees to use in the upper-right corner of the page: while on site. To keep this service available and optimized for i. By paper number: Click the Paper Number link, select all attendees, please do not download files larger than 2MB, the conference year, and enter the paper number. create multiple sessions across multiple devices, or download multiple files in one session. If you receive an error message ii. Use the Search textbox to find papers by author, title, or that an AIAA server is blocking your current IP address, please keyword. The Advanced Search link provides additional inform the AIAA registration desk. search information and options. 2. All manuscript files submitted by four days prior to the conference are currently in the proceedings. Files submitted AIAA Livestream Channel after that date, both original and revised manuscripts, will not be available until the final proceedings update, which Visit www.livestream.com/aiaa to view selected keynotes, may take up to 15 business days after the last day of the plenaries, and Forum 360 sessions. Share the link with conference. colleagues who couldn’t attend the conference so they can watch live or view later. AIAA SciTech 2015 Livestream 3. Direct any questions concerning access to proceedings and/ channel is sponsored by Airbus. or ARC to [email protected]. Manuscript Revisions Sponsored by: 1. Manuscript revision is open for all presenting authors from 0900 hrs Eastern Time, Monday, 5 January through 2000 hrs Eastern Time, Wednesday, 21 January. 2. Revisions submitted for manuscripts already online will not refresh until after the proceedings have been updated, which may take up to 15 business days after the last day of the conference.

Certiﬁcate of Attendance Certificates of Attendance are available for attendees who request documentation at the forum itself. Please request your copy at the AIAA Registration and Information Center. AIAA offers this service to better serve the needs of the professional community. Claims of hours or applicability toward professional education requirements are the responsibility of the participant.

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Employment Opportunities Badge Policy AIAA members can post and browse resumes, browse job AIAA forum badges are provided to those attendees who have listings, and access other online employment resources by paid for a registration to the event (and must be worn at all visiting the AIAA Career Center at http://careercenter.aiaa.org. times to participate in all forum activities). Badges are not provided for committee meetings. In order to obtain a badge, one must register for the event. Membership AIAA is your vital lifelong link to the collective creativity and brainpower of the aerospace profession and a champion for its Nondiscriminatory Practices achievements – and nonmembers who pay the full conference AIAA accepts registrations irrespective of race, creed, gender, registration fee will receive their first year’s AIAA membership color, sexual orientation, physical handicap, and national or at no additional cost! Students who are not yet members may ethnic origin. apply their registration fee toward their first year’s student member dues. (Free membership is not included in discounted group-rate registration.) Restrictions Photography or the video or audio recording of sessions or Young Professional Guide for Gaining exhibits, as well as the unauthorized sale of AIAA-copyrighted Management Support material, is prohibited. Young professionals have the unique opportunity to meet and learn from some of the most important people in the business International Trafﬁc in Arms Regulations (ITAR) by attending conferences and participating in AIAA activities. A detailed online guide, published by the AIAA Young AIAA speakers and attendees are reminded that some Professional Committee, is available to help you gain support topics discussed in the conference could be controlled and financial backing from your company. The guide explains by the International Traffic in Arms Regulations (ITAR). the benefits of participation, offers recommendations, and U.S. nationals (U.S. citizens and permanent residents) are provides an example letter for seeking management support responsible for ensuring that technical data they present and funding, and shows you how to get the most out of your in open sessions to non-U.S. nationals in attendance or in participation. The online guide can be found on the AIAA conference proceedings are not export restricted by the ITAR. website at www.aiaa.org/YPGuide. U.S. nationals are likewise responsible for ensuring that they do not discuss ITAR export-restricted information with non-U.S. nationals in attendance.

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Author and Session Chair Information

Speakers’ Brieﬁngs in Session Rooms Audiovisual Authors who are presenting papers will meet with session chairs Each session room will be preset with the following: one and co-chairs in their session rooms for a short 30-minute LCD projector, one screen, one microphone and sound briefing on the day of their sessions to exchange bios and review system (if necessitated by room size), and one laser pointer. final details prior to the session. Please attend on the day of Laptop computers will also be provided. You may also use your session(s). Laptops preloaded with the Speaker Briefing your own computer. Any additional audiovisual equipment preparation slides will be provided in each session room. requested onsite will be at cost to the presenter. Please note Speaker’s Briefing schedule is as follows: that AIAA does not provide security in the session rooms and Monday, 5 January–Friday, 9 January: 0730 hrs recommends that items of value not be left unattended. Speakers’ Practice Room “No Paper, No Podium” and “No Podium, No Paper” Policy Speakers who wish to practice their presentations may do so in Osceola Reg rooms 3 and 4, and Sun Reg rooms 3 and 4. A If a written paper is not submitted by the final manuscript sign-up sheet will be posted on the door. In consideration of deadline, authors will not be permitted to present the paper at others, please limit practice time to 30-minute increments. the forum. Also, if the paper is not presented at the forum, it will be withdrawn from the proceedings. It is the responsibility Session Chair Reports of those authors whose papers or presentations are accepted to ensure that a representative attends the conference to present All session chairs are asked to complete a session chair report to the paper. These policies are intended to improve the quality of evaluate their session for future planning. AIAA has partnered the program for attendees. with Canvas Solutions to provide an electronic Session Chair Report form. You can download the FREE mobile app in Journal Publication your App Store, AppWorld, or Marketplace by searching for “Canvas Solutions, Inc.” The mobile app is free, so please be AIAA has prior publication rights to any paper presented sure to download it. Detailed instructions will be provided in at its conferences. Authors who are seeking the opportunity the session rooms. If you do not have a tablet or a smartphone, for peer-reviewed publication are encouraged to submit simply use the report form as a guide and enter your session their papers for consideration by one of the Institute’s chair report information at the session chair reporting computer archival journals: AIAA Journal; Journal of Aircraft; Journal station located on site near the AIAA registration area. Report of Guidance, Control, and Dynamics; Journal of Propulsion data will be collected and used for future planning purposes, and Power; Journal of Spacecraft and Rockets; Journal of including session topics and room allocations. Please submit Thermophysics and Heat Transfer; or Journal of Aerospace your session chair report electronically by Friday, 9 January. Information Systems. You may now submit your paper online at http://mc.manuscriptcentral.com/aiaa

AIAA is the world’s largest technical society dedicated to the global aerospace profession. With more than 35,000 individual members worldwide, and 100 corporate members, AIAA brings together industry, academia, and government to advance engineering and science in aviation, space, and defense. American Institute of Aeronautics and Astronautics 1801 Alexander Bell Drive, Suite 500 Reston, VA 20191-4344 703.264.7500 or 800.639.AIAA (2422) Fax: 703.264.7657 [email protected] www.aiaa.org

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Time Title Location Saturday, 3 January 2015 0800-1700 hrs Aircraft and Rotorcraft System Identification Daytona 1 0800-1700 hrs Third International Workshop on High Order CFD Methods Daytona 2 0800-1700 hrs Best Practices in Wind Tunnel Testing Miami 1 Sunday, 4 January 2015 0800-1700 hrs Aircraft and Rotorcraft System Identification Daytona 1 0800-1700 hrs Third International Workshop on High Order CFD Methods Daytona 2 0800-1700 hrs Best Practices in Wind Tunnel Testing Miami 1 0900-1200 hrs TAC Director/Deputy Director Training Tallahassee 3 0900-1200 hrs TAC TC/PC Chair Training Osceola Ballroom 1/2 1200-1700 hrs TAC Workshop Osceola Ballroom 3/4 1430-1500 hrs APATC Liaisons Subcommittee Sanchez Boardroom 1500-1600 hrs APATC Education Subcommittee Sanchez Boardroom 1500-1600 hrs APATC Honors & Awards Subcommittee St George 102 1500-1600 hrs APATC Membership & Nominations Subcommittee Emerald 5 1400-1500 hrs GTTC Steering Subcommittee St George 112 1500-1600 hrs GTTC New Member and Mentors Meeting St George 112 1500-1600 hrs APATC Planning Subcommittee Emerald 7 1500-1600 hrs APATC Publicity & Publications Subcommittee Hemingway Boardroom 1600-1700 hrs GTTC Introduction/Overview St George 112 1600-1700 hrs APATC Technical Activities Subcommittee Sanchez Boardroom 1700-1800 hrs APATC Steering Committee Sanchez Boardroom 1700-1800 hrs GTTC Program Subcommittee St George 112 1730-2030 hrs Structures TC St George 108 1800-1930 hrs Student Reception Orange Blossom Ballroom 1800-2100 hrs Applied Aerodynamics TC St George 114 1800-2100 hrs Atmospheric Flight Mechanics TC St George 104 1800-1900 hrs GTTC Publications Subcommittee St George 112 1800-2200 hrs GNC Graduate Student Paper Competition Tallahassee 2 1830-2100 hrs GNCTC Undergraduate Conference Experience Emerald 2 1900-2100 hrs FDTC Transition DG St George 106 1900-2100 hrs TAC Aerospace Design & Structures Group Meeting Sanchez Boardroom 1900-2100 hrs TAC Aircraft & Atmospheric Systems Group Meeting Hemingway Boardroom 1900-2100 hrs TAC Engineering & Technology Management Group Meeting St George 102 1900-2200 hrs TAC Program Committees Group Meeting Emerald 4 1900-2100 hrs TAC Propulsion & Energy Group Meeting Emerald 1 1900-2100 hrs TAC Space & Missiles Group Meeting Emerald 3 1900-2000 hrs GTTC Conferences Subcommittee St George 112 2000-2200 hrs TAC Information Systems Group Meeting Emerald 5

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Time Title Location Monday, 5 January 2015 0800-1600 hrs Governance Workshop St George 108 0900-1000 hrs ABPTCs Steering Committee St George 106 0900-1600 hrs National Institute of Aerospace Suite 6095 1000-1100 hrs ABPSITC Meeting St George 106 1000-1100 hrs GTETC Meeting St George 102 1000-1100 hrs HSABPTC Meeting St George 104 1100-1400 hrs Academic Affairs Committee St George 102 1100-1200 hrs PDLTC Steering Committee Sanchez Boardroom 1200-1300 hrs ABPTCs Conference Subcommittee St George 106 1230-1400 hrs Durand Lecture in Public Service / Public Policy Luncheon Osceola Ballroom CD 1230-1400 hrs FDTC Steering Committee Sanchez Boardroom 1300-1500 hrs Education Series Editorial Advisory Board Hemingway Boardroom 1400-1700 hrs Honors and Awards Committee St George 104 1400-1500 hrs ABPTCs Honors and Awards Subcommittee St George 106 1500-1600 hrs FDTC Free Shear and Mixing Layer Control DG Hemingway Boardroom 1500-1700 hrs Progress Series Editorial Advisory Board Sanchez Boardroom 1500-1600 hrs ABPTCs Education Subcommittee St George 106 1600-1800 hrs Space Operations & Support TC Hemingway Boardroom 1600-1700 hrs ABPTCs Communications Subcommittee St George 106 1630-1730 hrs FDTC Flow Control Technology: Barriers/Challenges to Tech Transition DG Suite 5095 1630-1730 hrs AMTTC New Member Orientation Suite 6123 1700-1800 hrs ABPTCs Membership Subcommittee St George 106 1700-1900 hrs ABPTCs Working Group Suite 6095 1730-1830 hrs FDTC Turbulence Modeling Benchmarks WG Sanibel 3 1730-1900 hrs APATC Validation of Numerical Models DG Osceola Ballroom 5 1800-1900 hrs FDTC Future of Fluids SC Sanchez Boardroom 1800-1900 hrs Rising Leaders in Aerospace Reception Osceola Ballroom A 1830-2230 hrs Associate Fellows Reception/Dinner Osceola Foyer/Osceola Ballroom C 1830-2000 hrs AMTTC Award Subcommittee Suite 5095 1830-1930 hrs GTTC Committee on Standards Miami 2 1830-2130 hrs Aerospace @ Illinois Alumni Reception St George 114 1900-2030 hrs Penn State Alumni Reception Marlin Dock 1900-2130 hrs Propellants & Combustion TC Emerald 8 1900-2200 hrs Terrestrial Energy Systems TC St George 106 1900-2100 hrs FDTC Fundamentals of Flow Phenomena Subcommittee Emerald 6 1900-2100 hrs FDTC CFD Methods Subcommittee St George 102 1900-2200 hrs TAC Aerospace Sciences Group Meeting St George 108 1900-2100 hrs SDTC Aeroelastic Prediction Workshop Meeting Emerald 4 1900-2100 hrs FDTC Flow Control and Fluid Applications SC Emerald 5 1900-2100 hrs ABPTCs Group Meeting Miami 1 1930-2030 hrs GTTC Awards Subcommittee Miami 2 2030-2130 hrs GTTC Education and Student Activities Subcommittees Miami 2

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Time Title Location Tuesday, 6 January 2015 0700-1000 hrs GTTC Dual Reference Nozzle WG St George 112 0800-1500 hrs GTTC WT Model Attitude and Deformation Measurement WG St George 114 0800-1600 hrs GTTC Internal Balance WG Gainesville 2 0800-1200 hrs Public Policy Committee St George 108 0800-1000 hrs 2016 Associate Fellows Committee St George 102 0800-1700 hrs Systems Engineering TC Palm Beach 0800-0945 hrs RAC V Meeting Suite 6095 0800-0930 hrs Audit Committee Meeting Hemingway Boardroom 0800-1000 hrs Books Subcommittee Sanchez Boardroom 0900-1100 hrs ISC Award Brunch St George 106 0900-1000 hrs SRTC Subcommittee St George 104 0930-1130 hrs Finance Committee Meeting Orange Blossom Ballroom 1000-1100 hrs SciTech 2016 Executive Steering Committee Clearwater 1000-1230 hrs RAC I Meeting Sanchez Boardroom 1000-1100 hrs RAC IV Meeting Suite 6095 1000-1200 hrs Solid Rockets TC St George 104 1000-1200 hrs International Activities Committee St George 112 1000-1100 hrs TAC PEG Operations Group Hemingway Boardroom 1100-1200 hrs TAC PEG Technical Products Group St George 102 1115-1430 hrs RAC II Meeting Suite 6095 1200-1300 hrs Compensation Committee Sales Boardroom 1200-1400 hrs Education Activities Committee Hemingway Boardroom 1400-1700 hrs Board of Directors Meeting Orange Blossom Ballroom 1400-1700 hrs Aircraft Design TC St George 104 1500-1600 hrs TPTC Best Paper Subcommittee Suite 6095 1500-1730 hrs Aerospace Cybersecurity WG St George 114 1500-1600 hrs TPTC Awards Subcommittee St George 102 1500-1700 hrs Journal of Thermophysics and Heat Transfer Editorial Advisory Board Hemingway Boardroom 1600-1800 hrs GTTC FoGT Experimental and Computational Aero Development St George 102 1600-1700 hrs TPTC Publications Subcommittee Suite 6095 1600-1700 hrs TPTC Conference Subcommittee Suite 6123 1600-1700 hrs Book Authors Reception St George 106 1600-1700 hrs GEPC Conference Subcommittee Sanchez Boardroom 1600-1715 hrs Rising Leaders in Aerospace-Speed Geek Osceola Ballroom A 1700-1900 hrs AIAA Ethics Committee Gainesville 2 1700-1800 hrs TPTC Nominations Subcommittee Suite 6123 1700-1800 hrs TPTC Education Subcommittee Suite 5095 1700-1800 hrs GEPC Leadership Team Sanchez Boardroom 1730-2000 hrs SCSTC Publications Subcommittee Hemingway Boardroom 1730-1930 hrs APATC Aerodynamic Design Optimization DG St George 112 1730-1830 hrs Dryden Lecture in Research Osceola Ballroom CD

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Time Title Location Tuesday, 6 January 2015 (continued) 1800-1900 hrs TPTC Publicity Subcommittee Suite 5095 1800-2200 hrs Sensor Systems and Information Fusion TC Naples 1 1800-2130 hrs Software TC St George 114 1830-2100 hrs SciTech 2015 Executive Dinner (by invitation only) Old Hickory Steakhouse 1830-2130 hrs Pressure Gain Combustion PC Osceola Ballroom 1 1830-2130 hrs Legal Aspects of Aeronautics and Astronautics Sanchez Boardroom 1830-2130 hrs History TC Sanibel 1 1830-2130 hrs Survivability TC Miami 2 1830-2130 hrs ASME Wind Energy TC Miami 1 1900-2200 hrs Aerodynamics Technical Working Group Emerald 2 1900-2100 hrs CFD Committee on Standards Palm Beach 1900-2100 hrs Career and Professional Development Committee Suite 5095 1900-2200 hrs Small Satellite TC Sanibel 3 1900-2200 hrs Unmanned Systems PC St George 102 1900-2200 hrs Aerodynamic Measurement Technology TC Sarasota 1/2 1900-2200 hrs Materials TC Osceola Ballroom 2 1900-2200 hrs Fluid Dynamics TC Osceola Ballroom 5/6 1900-2200 hrs Plasmadynamics and Lasers TC St George 108 1900-2200 hrs Meshing, Visualization and Computational Environments TC Maimi 3 1900-2200 hrs Aeroacoustics TC St George 106 1900-2200 hrs Thermophysics TC Orange Blossom Ballroom 1900-2100 hrs CASE 2015 Planning Meeting Naples 2 1900-2200 hrs Aerospace Department Chair Association (ADCA) Meeting Sun Ballroom C 1900-2100 hrs Embry-Riddle Alumni Reception Captiva 1/2 1930-2200 hrs Adaptive Structures TC Naples 3 1930-2200 hrs Structures TC Osceola Ballroom 3/4 Wednesday, 7 January 2015 0700-1330 hrs Region & Section Activities Committee (RAC) St George 104 0700-1200 hrs GTTC Dual Flow Reference Nozzle WG- Day 2 Gainesville 2 0800-0930 hrs Standards Executive Council (SEC) Suite 6095 0800-1200 hrs GTTC FoGT WG St George 114 0800-1000 hrs Journals Subcommittee Hemingway Boardroom 0900-1200 hrs Student Activities Committee St George 112 0900-1200 hrs TAC Executive Board St. George 106 0930-1230 hrs DETC Subcommittees Sanchez Boardroom 0930-1130 hrs Foundation Board of Trustees St George 102 1000-1100 hrs SciTech 2016 Technical Program Committee Clearwater 1000-1300 hrs Journals Editors-in-Chief Hemingway Boardroom 1200-1700 hrs Lockheed Meeting Suite 6123 1200-1500 hrs EOAESPC Leadership Team St George 102 1200-1500 hrs EOAESPC Leadership Team St George 102

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Time Title Location Wednesday, 7 January 2015 (Continued) 1300-1500 hrs Aircraft Electric Propulsion Path Forward Sanchez Boardroom 1300-1500 hrs Publications Planning and Review Subcommittee Hemingway Boardroom 1300-1600 hrs Corporate Member Committee St George 114 1400-1800 hrs Design Engineering TC Suite 6095 1400-1700 hrs IDC St George 112 1400-1600 hrs AIAA Journal Editorial Advisory Board St George 106 1400-1500 hrs HyTASPPC Steering Meeting Gainesville 2 1400-1700 hrs TAC New Initiatives Subcommittee St George 104 1500-1700 hrs LM Aeronautics Company Meeting Palm Beach 1500-1700 hrs HyTASP PC Gainesville 2 1500-1700 hrs Publications Ethical Standards Subcommittee Sanchez Boardroom 1600-1730 hrs Corporate Member/Exhibitor Reception (by invitation only) Exhibit Hall 1600-1800 hrs Emerging Technologies Committee Clearwater 1600-1800 hrs Journal of Aircraft Editorial Advisory Board St George 106 1615-1745 hrs Rising Leaders in Aerospace-Leadership Exchange Osceola Ballroom A 1700-1815 hrs Reception Honoring 2015 Crichlow Prize Recipient (by invitation only) St George 108 1730-1800 hrs TPTC New Member Meeting Suite 6123 1730-1930 hrs APATC Low Boom DG Miami 3 1730-2000 hrs Green Engineering PC St George 114 1730-1830 hrs AMTTC Nominations Subcommittee Sanchez Boardroom 1730-1800 hrs GNCTC New Member Orientation St George 102 1730-1830 hrs FDTC Large Eddy Simulation DG St George 104 1730-1830 hrs FDTC Nonequilibrium Flows DG St George 112 1730-1830 hrs FDTC Student Outreach SC Suite 5095 1800-2000 hrs APATC Rotorcraft Simulations & Performance Predictions DG St George 106 1800-2100 hrs V/STOL Aircraft Systems TC Gainesville 2 1800-2000 hrs UK Reception Osceola Ballroom 6 1830-1930 hrs FDTC Low Re Aerodynamics DG Emerald 7 1830-2200 hrs Guidance, Navigation and Control TC Sun Ballroom B 1830-2130 hrs Society and Aerospace Technology TC Destin 2 1830-2030 hrs AMTTC Update Presentation/Student Event Osceola Ballroom 3/4 1830-1930 hrs APATC Missile & Projectile Aeroprediction DG St George 112 1830-2000 hrs ISG Meeting and Greet Osceola Ballroom 1 1830-1930 hrs Sneak Peak Into The Skunk Works Orange Blossom Ballroom 1900-2100 hrs Intelligent Light Captiva 1/2 1900-2030 hrs University of Cincinnati College of Engineering and Naples 1/2 Applied Science Reception 1900-2030 hrs FDTC Solver Technology for Turbulent Flows DG St George 104 1900-2030 hrs University of Michigan Reception Sanibel 3 1900-2100 hrs ASME Structures and Materials TC Daytona 2

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Time Title Location Wednesday, 7 January 2015 (Continued) 1900-2200 hrs Spacecraft Structures TC Tallahassee 1/2 1900-2000 hrs APATC Low Reynolds Number Aerodynamic Modeling & Test DG St George 102 1900-2200 hrs Non-Deterministic Approaches TC Sanibel 1/2 1900-2200 hrs Structural Dynamics TC Sun Ballroom A 2000-2200 hrs Intelligent Systems TC Osceola Ballroom 2 Thursday, 8 January 2015 0700-1200 hrs GTTC Wind Tunnel Flow Quality WG St George 102 0800-1700 hrs Lockheed Meeting Hemingway Boardroom 0800-1200 hrs Publications Committee St George 108 0800-1200 hrs GTTC Uncertainty Analysis WG St George 112 0900-1600 hrs Technical Activities Committee St George 114 1200-1330 hrs Rising Leaders in Aerospace Luncheon Panel Osceola Ballroom A 1200-1400 hrs V/STOL Aircraft Systems TC/Transformational Flight PC Joint Meeting Sanchez Boardroom 1230-1330 hrs FDTC SBLI Shock Boundry Layer Interaction DG Daytona 1 1300-1500 hrs AIAA/Boeing Partnership Meeting St. George 102 1500-1700 hrs Journal of Guidance, Control and Dynamics Editorial Advisory Board Gainesville 2 1730-2000 hrs SCSTC High Strain Composites Subcommittee Hemingway Boardroom 1730-2030 hrs Ground Testing TC Osceola Ballroom A 1800-2100 hrs Modeling and Simulation TC St George 102 1830-2130 hrs Transformational Flight PC Gainesville 2 1830-2030 hrs PDLTC Plasma Aerodynamics DG St George 104 1900-2200 hrs Information and Command and Control Systems TC St George 108

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Abbreviation Title Date Start Time End Time Location Aeroacoustics AA-1 Computational Aeroacoustics I 5-Jan 0930 hrs 1230 hrs Miami 2 AA-2 Jet Noise Measurements I 5-Jan 1400 hrs 1730 hrs Miami 2 AA-3 Computational Aeroacoustics II 6-Jan 0930 hrs 1230 hrs Miami 2 AA-4 Jet Noise Prediction I 6-Jan 0930 hrs 1230 hrs Sun Ballroom C AA-5 Jet Noise Measurements II 6-Jan 1400 hrs 1730 hrs Miami 2 AA-6 General Acoustics 6-Jan 1400 hrs 1730 hrs Sun Ballroom C AA-7 Jet Noise Prediction II 7-Jan 0930 hrs 1230 hrs Miami 2 AA-8 Airframe Noise and Shielding 7-Jan 1400 hrs 1730 hrs Miami 2 Air Breathing Propulsion Systems Integration ABPSI-1 Propulsion Integration and Controls 8-Jan 0930 hrs 1230 hrs Emerald 2 ABPSI-2 Inlets and Nozzles 8-Jan 1400 hrs 1730 hrs Emerald 2 Aircraft Design ACD-1 Aircraft Design Optimization 6-Jan 0930 hrs 1230 hrs Naples 3 ACD-2 High Speed Aircraft Design 7-Jan 0930 hrs 1230 hrs Tallahassee 2 ACD-3 Aircraft Design Tools 7-Jan 0930 hrs 1230 hrs Naples 3 ACD-4 Conceptual Aircraft Design Working Group (CADWG21) 8-Jan 0930 hrs 1230 hrs Naples 3 Panel: How much fidelity in conceptual aircraft design? ACD-5 Propulsion Integration for Aircraft Design 8-Jan 1400 hrs 1730 hrs Emerald 8 ACD-6 Aircraft Design Methodology 8-Jan 1400 hrs 1730 hrs Osceola Ballroom 3 ACD-7 Transport Aircraft Design 9-Jan 0930 hrs 1300 hrs Osceola Ballroom 3 ACD-8 Aircraft Design Case Studies 9-Jan 0930 hrs 1300 hrs Osceola Ballroom 4 Atmospheric Flight Mechanics AFM-1 AFM Best Student Paper Competition I 5-Jan 0930 hrs 1230 hrs Captiva 1 AFM-2 Aircraft Flight Dynamics, Handling Qualities and 5-Jan 0930 hrs 1230 hrs Captiva 2 Performance I AFM-3 AFM Best Student Paper Competition II 5-Jan 1400 hrs 1730 hrs Captiva 1 AFM-4 Aircraft Flight Dynamics, Handling Qualities and 5-Jan 1400 hrs 1730 hrs Captiva 2 Performance II AFM-5 Aerodynamic Prediction Methods 6-Jan 0930 hrs 1230 hrs Captiva 2 AFM-6 Atmospheric Entry, Hypersonic Flight and Aeroassist 6-Jan 0930 hrs 1230 hrs Captiva 1 Technology AFM-7 AFM Best Student Paper Competition III 6-Jan 1400 hrs 1730 hrs Captiva 1 AFM-8 Aircraft Flight Dynamics, Handling Qualities and 6-Jan 1400 hrs 1730 hrs Captiva 2 Performance III AFM-9 Launch Vehicle, Missile, and Projectile Flight Mechanics I 7-Jan 0930 hrs 1230 hrs Captiva 2 AFM-10 Air Launch to Orbit (Invited) 7-Jan 0930 hrs 1230 hrs Sun Ballroom B AFM-11 Flight Test and System Identification 8-Jan 0930 hrs 1230 hrs Captiva 1 AFM-12 MAV, UAV and Aeroservoelastic Vehicles 8-Jan 1400 hrs 1730 hrs Captiva 1 AFM-13 Seven Axioms of Good Engineering (Invited Session) 8-Jan 1400 hrs 1700 hrs Captiva 2 AFM-15 Launch Vehicle, Missile, and Projectile Flight Mechanics II 9-Jan 0930 hrs 1230 hrs Captiva 2

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Abbreviation Title Date Start Time End Time Location Aerodynamic Measurement Technology AMT-1 Pressure Sensitive Paint (PSP) and Novel Measurement 5-Jan 0930 hrs 1230 hrs Tallahassee 1 Techniques AMT-2 Laser Diagnostics for Reacting Flows 6-Jan 0930 hrs 1230 hrs Tallahassee 1 AMT-3 Novel Diagnostics in Reacting Flows 7-Jan 0930 hrs 1230 hrs Tallahassee 1 AMT-4 Laser Based Aerodynamic Diagnostic Tools 7-Jan 1400 hrs 1730 hrs Tallahassee 1 AMT-5 Aerodynamic Diagnostics Tool for High Speed Flows 8-Jan 0930 hrs 1230 hrs Tallahassee 1 AMT-6/GT-7 Background-Oriented Schlieren: Recent Advancements 8-Jan 1400 hrs 1730 hrs Sun Ballroom C and Applications in Ground Test Facilities AMT-7 Spectroscopy and Schlieren 8-Jan 1400 hrs 1730 hrs Tallahassee 1 AMT-8 Aerodynamic Diagnostics Tool for Supersonic and 9-Jan 0930 hrs 1300 hrs Tallahassee 1 Hypersonic Flows AMT-9 Aerodynamic Surface Measurements 9-Jan 0930 hrs 1300 hrs Tallahassee 2 Applied Aerodynamics APA-1 Aerodynamic Design: Analysis, Methodologies & 5-Jan 0930 hrs 1230 hrs Destin 1 Optimization Techniques I APA-2 Icing or Roughness Effects on Vehicle Aerodynamics I 5-Jan 0930 hrs 1230 hrs Destin 2 APA-3 Special Session: Low Reynolds Number Flight at a 5-Jan 0930 hrs 1230 hrs Naples 1 Crossroads APA-4 Special Session: CREATE-AV High Performance 5-Jan 0930 hrs 1230 hrs Naples 2 Computing Multiphysics Applications of Full-up Air Vehicles I APA-5 Aerodynamic Testing: Wind Tunnel & Flight Testing I 5-Jan 1400 hrs 1730 hrs Destin 1 APA-6 Aerodynamic-Structural Dynamics Interaction I 5-Jan 1400 hrs 1730 hrs Destin 2 APA-7 Unsteady Aerodynamics 5-Jan 1400 hrs 1730 hrs Naples 1 APA-8 Special Session: Aerodynamic Design Optimization of 5-Jan 1400 hrs 1730 hrs Naples 2 Benchmark Cases I APA-9/NDA-1 Frontiers of Uncertainty Management for Complex 5-Jan 1500 hrs 1730 hrs Osceola Ballroom 5 Aerospace Systems APA-10 Icing or Roughness Effects on Vehicle Aerodynamics II 6-Jan 0930 hrs 1230 hrs Destin 2 APA-11 Other Topics in Applied Aerodynamics 6-Jan 0930 hrs 1230 hrs Destin 1 APA-12 High-Angle-of-Attack, High-lift and Vortical Flow 6-Jan 0930 hrs 1230 hrs Sun Ballroom A Aerodynamics APA-13 Special Session: CREATE-AV High Performance 6-Jan 0930 hrs 1230 hrs Naples 2 Computing Multiphysics Applications of Full-up Air Vehicles II APA-14 Special Session: Space Launch System (SLS) I 6-Jan 0930 hrs 1230 hrs Naples 1 APA-15 Aerodynamic Design: Analysis, Methodologies & 6-Jan 1400 hrs 1730 hrs Destin 1 Optimization Techniques II APA-16 Aerodynamic-Structural Dynamics Interaction II 6-Jan 1400 hrs 1730 hrs Destin 2 APA-17 Airfoil/Wing/Configuration Aerodynamics I 6-Jan 1400 hrs 1730 hrs Naples 2 APA-18 Special Session: Space Launch System (SLS) II 6-Jan 1400 hrs 1730 hrs Naples 1 APA-19/FD-19 Flow Control: Fluidic Oscillators 6-Jan 1400 hrs 1730 hrs Sun Ballroom A APA-20 Propeller/Rotorcraft/Wind Turbine Aerodynamics I 7-Jan 0930 hrs 1230 hrs Naples 2 APA-21 Airfoil/Wing/Configuration Aerodynamics II 7-Jan 0930 hrs 1230 hrs Destin 2

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Abbreviation Title Date Start Time End Time Location Applied Aerodynamics (continued) APA-22 Flow Control Applications & Demonstrations 7-Jan 0930 hrs 1230 hrs Naples 1 (Active & Passive) I APA-23 Special Session: CREATE-AV High Performance 7-Jan 0930 hrs 1230 hrs Destin 1 Computing Multiphysics Applications of Full-up Air Vehicles III APA-24 Special Session: Low Boom Activities I 7-Jan 0930 hrs 1230 hrs Miami 3 APA-25 Aerodynamic Testing: Wind Tunnel & Flight Testing II 7-Jan 1400 hrs 1730 hrs Destin 1 APA-26 Applied CFD & Numerical Correlations with Experimental 7-Jan 1400 hrs 1730 hrs Destin 2 Data I APA-27 Flow Control Applications & Demonstrations (Active & 7-Jan 1400 hrs 1730 hrs Naples 1 Passive) II APA-28 Special Session: Simulation of Rotor in Hover - Rotorcraft 7-Jan 1400 hrs 1730 hrs Naples 2 DG I APA-29 Special Session: Low Boom Activities II 7-Jan 1400 hrs 1730 hrs Miami 3 APA-30 Aerodynamic Design: Analysis, Methodologies & 8-Jan 0930 hrs 1230 hrs Naples 1 Optimization Techniques III APA-31 Propeller/Rotorcraft/Wind Turbine Aerodynamics II 8-Jan 0930 hrs 1230 hrs Naples 2 APA-32 Applied CFD & Numerical Correlations with Experimental 8-Jan 0930 hrs 1230 hrs Destin 1 Data II APA-33 High-Angle-of-Attack & High-lift Aerodynamics 8-Jan 0930 hrs 1230 hrs Sun Ballroom A APA-34 Special Session: CREATE-AV High Performance 8-Jan 0930 hrs 1230 hrs Destin 2 Computing Multiphysics Applications of Full-up Air Vehicles IV APA-35 Hypersonic Aerodynamics 8-Jan 1400 hrs 1730 hrs Destin 1 APA-36 Flow Control Applications & Demonstrations (Active & 8-Jan 1400 hrs 1730 hrs Naples 1 Passive) III APA-37 Special Session: Simulation of Rotor in Hover - Rotorcraft 8-Jan 1400 hrs 1730 hrs Naples 2 DG II APA-38 Special Session: Aerodynamic Design Optimization of 8-Jan 1400 hrs 1730 hrs Destin 2 Benchmark Cases II APA-39 Weapons Aerodynamics: Missile/Projectile/Guided- 9-Jan 0930 hrs 1230 hrs Naples 1 Munitions, Carriage & Store Separation APA-40 Applied CFD & Numerical Correlations with Experimental 9-Jan 0930 hrs 1230 hrs Destin 2 Data III APA-41 Low speed, Low Reynolds Number & VSTOL/STOL 9-Jan 0930 hrs 1300 hrs Naples 3 Aerodynamics APA-42 Transonic & Supersonic Aerodynamics 9-Jan 0930 hrs 1230 hrs Naples 2 APA-43 Special Session: Aerodynamic Design Optimization of 9-Jan 0930 hrs 1300 hrs Destin 1 Benchmark Cases III

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Abbreviation Title Date Start Time End Time Location Adaptive Structures AS-1 Aerodynamics of Adaptive Structures 5-Jan 1400 hrs 1730 hrs Osceola Ballroom 6 AS-2 Shape Memory Alloy Applications 6-Jan 1030 hrs 1230 hrs Osceola Ballroom 6 AS-3 Morphing Applications 6-Jan 1400 hrs 1730 hrs Osceola Ballroom 6 AS-4 Compliant Structures 7-Jan 0930 hrs 1230 hrs Osceola Ballroom 6 AS-5 Adaptive Actuation 7-Jan 1400 hrs 1730 hrs Osceola Ballroom 6 AS-6 Space Applications 8-Jan 0930 hrs 1230 hrs Osceola Ballroom 6 AS-7 Smart and Multifunctional Materials Applications 8-Jan 1400 hrs 1730 hrs Osceola Ballroom 6 Computer Systems CMS-1 High Performance and Embedded Computing 9-Jan 0930 hrs 1230 hrs Osceola Ballroom 2 Technologies for Aerospace Digital Avionics DA-1 Digital Avionics 6-Jan 1400 hrs 1730 hrs Osceola Ballroom 3 Design Engineering DE-1 Design Engineering 6-Jan 0930 hrs 1230 hrs Sarasota 2 DE-2 Design Education/Design Process 6-Jan 1400 hrs 1730 hrs Sarasota 2 DE-3 Wildlife Conservation UAV Challenge (wcUAVc) 8-Jan 0930 hrs 1230 hrs Sun Ballroom D Education EDU-1 Advancing Aerospace Education I 8-Jan 0930 hrs 1200 hrs Emerald 6 Fluid Dynamics FD-1 Bio-Inspired Flow 5-Jan 0930 hrs 1230 hrs Daytona 1 FD-2 CFD Methods I 5-Jan 0930 hrs 1230 hrs Sanibel 1 FD-3 Discontinuous Galerkin Methods for Turbulent Flows 5-Jan 0930 hrs 1230 hrs Daytona 2 FD-4 Experimental and Numerical Investigations of Blunt 5-Jan 0930 hrs 1230 hrs Sanibel 2 Leading Edge Separation for a 53 Degree Swept Diamond Wing (STO AVT-183) I (Invited) FD-5 Shock-Dominated Flows I 5-Jan 0930 hrs 1230 hrs Sanibel 3 FD-7 Boundary Layer Transition: Roughness and 3D Flow 5-Jan 1400 hrs 1730 hrs Tallahassee 1 Effects FD-8 CFD Methods II 5-Jan 1400 hrs 1730 hrs Sanibel 1 FD-9 Experimental and Numerical Investigations of Blunt 5-Jan 1400 hrs 1730 hrs Sanibel 2 Leading Edge Separation for a 53 Degree Swept Diamond Wing (STO AVT-183) II (Invited) FD-10 High-Order Methods I 5-Jan 1400 hrs 1730 hrs Daytona 1 FD-11 Jet Flows and Control 5-Jan 1400 hrs 1730 hrs Daytona 2 FD-12/PDL-1 Plasma Flow Control 5-Jan 1400 hrs 1730 hrs Sun Ballroom A FD-13 RANS/LES Applications 5-Jan 1400 hrs 1730 hrs Sanibel 3 FD-14 CFD Methods III 6-Jan 0930 hrs 1230 hrs Sanibel 1 FD-15 Discontinuous Galerkin Methods I 6-Jan 0930 hrs 1230 hrs Sanibel 2 FD-16 Experiments in Energy Exchange in High Speed Flows 6-Jan 0930 hrs 1230 hrs Daytona 1 (Invited) FD-17 Shock-Dominated Flows II 6-Jan 0930 hrs 1230 hrs Sanibel 3 FD-18 Stability and Transition Modeling 6-Jan 0930 hrs 1230 hrs Daytona 2 FD-20 Actuators and Active Flow Control 6-Jan 1400 hrs 1730 hrs Tallahassee 2 www.aiaa-SciTech.org 44 #aiaaSciTech IntroSessions at a Glance

Abbreviation Title Date Start Time End Time Location Fluid Dynamics (continued) FD-21 CFD Methods IV 6-Jan 1400 hrs 1730 hrs Sanibel 1 FD-22 Discontinuous Galerkin Methods II 6-Jan 1400 hrs 1730 hrs Sanibel 2 FD-23 Flow Control (Fundamentals and Technology) I 6-Jan 1400 hrs 1730 hrs Sanibel 3 FD-24 High-Order Methods II 6-Jan 1400 hrs 1730 hrs Daytona 1 FD-25 Hypersonic Boundary Layer Transition I 6-Jan 1400 hrs 1730 hrs Tallahassee 1 FD-26 Jets, Plumes, & Reacting Flows 6-Jan 1400 hrs 1730 hrs Daytona 2 FD-28 Current Challenges for Computational Fluid Dynamics, 7-Jan 0930 hrs 1230 hrs Sun Ballroom A Industry and Government Interests I (Invited) FD-29 Flow Control (Fundamentals and Technology) II 7-Jan 0930 hrs 1230 hrs Sanibel 3 FD-30 Hypersonic Flows 7-Jan 0930 hrs 1230 hrs Daytona 1 FD-31 Unsteady Flow I 7-Jan 0930 hrs 1230 hrs Sun Ballroom 6 FD-32 CFD Methods V 7-Jan 1400 hrs 1730 hrs Sanibel 2 FD-33 Current Challenges for Computational Fluid Dynamics, 7-Jan 1400 hrs 1730 hrs Sun Ballroom A Industry and Government Interests II (Invited) FD-34 Flow Control (Fundamentals and Technology) III 7-Jan 1400 hrs 1700 hrs Sanibel 3 FD-35 Fundamental Vortex Flows and Channel Flows 7-Jan 1400 hrs 1730 hrs Tallahassee 2 FD-36 Multiphase Flows 7-Jan 1400 hrs 1730 hrs Daytona 2 FD-37 Turbulence Modeling I 7-Jan 1400 hrs 1730 hrs Captiva 2 FD-38 Unsteady Flow II 7-Jan 1400 hrs 1730 hrs Sun Ballroom 6 FD-39 Wing Aerodynamics I 7-Jan 1400 hrs 1730 hrs Daytona 1 FD-40 Swept and 3D Shock Boundary Layer Interactions 8-Jan 0930 hrs 1230 hrs Daytona 1 FD-41 Turbulence 8-Jan 0930 hrs 1230 hrs Tallahassee 3 FD-42 Turbulence Modeling II 8-Jan 0930 hrs 1230 hrs Sanibel 3 FD-43 Turbulent Flow Solutions for NACA 0012 and Other Test 8-Jan 0930 hrs 1230 hrs Sanibel 2 Cases from the Turbulence Model Resource Website: Residual and Grid Convergence I (invited) FD-44 Unsteady Flow III 8-Jan 0930 hrs 1230 hrs Sun Ballroom 6 FD-45/PDL-9 DBD Plasma Actuators 8-Jan 1400 hrs 1730 hrs Sun Ballroom A FD-46 Hypersonic Boundary Layer Transition II 8-Jan 1400 hrs 1730 hrs Sanibel 3 FD-47 Overset/Deforming/Moving Meshes 8-Jan 1400 hrs 1730 hrs Daytona 2 FD-48 Turbulent Flow Solutions for NACA 0012 and Other Test 8-Jan 1400 hrs 1730 hrs Sanibel 2 Cases from the Turbulence Model Resource Website: Residual and Grid Convergence II (Invited) FD-49 Wing Aerodynamics II 8-Jan 1400 hrs 1730 hrs Daytona 1 FD-50 CFD Solution Adaptation & Optimization 9-Jan 0930 hrs 1300 hrs Miami 2 FD-51/PDL-12 Plasma Actuators and Flow Control 9-Jan 0930 hrs 1300 hrs Sun Ballroom A FD-52 Separated Flows 9-Jan 0930 hrs 1230 hrs Sanibel 2 FD-53 Shear Layers 9-Jan 0930 hrs 1230 hrs Tallahassee 3 FD-54 Shock Boundary Layer Interaction 9-Jan 0930 hrs 1300 hrs Daytona 2 FD-55 Turbulence Modeling III 9-Jan 0930 hrs 1300 hrs Sanibel 3 FD-56 Turbulent Boundary Layers 9-Jan 0930 hrs 1230 hrs Daytona 1 FD-57 New and Revolutionary Approaches in High Speed Flow 5-Jan 0930 hrs 1230 hrs Sun Ballroom A Turbulence Modeling FD-58 Transition Open Forum 9-Jan 0930 hrs 1300 hrs Sun Ballroom C www.aiaa-SciTech.org 45 #aiaaSciTech IntroSessions at a Glance

Abbreviation Title Date Start Time End Time Location Green Engineering GEPC-1 N+3 Configuration Concepts and Enabling Technologies 5-Jan 0930 hrs 1230 hrs Sun Ballroom C in NASA's Fixed Wing Project GEPC-2 Status/Progress of Environmentally Responsible Aviation 5-Jan 1400 hrs 1730 hrs Sun Ballroom C Project GEPC-3 NASA Transformational Tools and Technologies (T3) 8-Jan 0930 hrs 1230 hrs Sun Ballroom C Project Recent Modeling Advances GEPC-4/SAT-1 Green Engineering/Society and Aerospace Technology 7-Jan 1400 hrs 1730 hrs Sun Ballroom C Guidance, Navigation, and Control GNC-1 Aerospace Robotics and Autonomous/Unmanned Systems 5-Jan 0930 hrs 1200 hrs Sun Ballroom 3 I GNC-2 Flight Experience of Cassini Spacecraft Attitude Control at 5-Jan 0930 hrs 1230 hrs Miami 1 Saturn GNC-3 GNC Sensor Systems I 5-Jan 0930 hrs 1230 hrs Sun Ballroom 4 GNC-4 Missile Guidance I 5-Jan 0930 hrs 1230 hrs Sun Ballroom 6 GNC-5 Novel Navigation, Estimation, and Tracking Methods I 5-Jan 0930 hrs 1230 hrs Sun Ballroom 5 GNC-6 Aerospace Robotics and Autonomous/Unmanned Systems 5-Jan 1400 hrs 1730 hrs Sun Ballroom 3 II GNC-7 Lander Technology Development at NASA I 5-Jan 1400 hrs 1730 hrs Miami 1 GNC-8 GNC Sensor Systems II 5-Jan 1400 hrs 1730 hrs Sun Ballroom 4 GNC-9 Missile Guidance II 5-Jan 1400 hrs 1700 hrs Sun Ballroom 6 GNC-10 Novel Navigation, Estimation, and Tracking Methods II 5-Jan 1400 hrs 1730 hrs Sun Ballroom 5 GNC-11 Aerospace Robotics and Autonomous/Unmanned Systems 6-Jan 0930 hrs 1230 hrs Sun Ballroom 3 III GNC-12 Advances in GN&C of Multi-Agent Autonomous Systems 6-Jan 0930 hrs 1230 hrs Miami 1 GNC-13 Guidance and Control of Autonomous/Unmanned Systems 6-Jan 0930 hrs 1230 hrs Sun Ballroom 5 GNC-14 Adaptive Control of Flight Vehicles 6-Jan 0930 hrs 1230 hrs Sun Ballroom 4 GNC-15 Missile Guidance III 6-Jan 0930 hrs 1230 hrs Sun Ballroom 6 GNC-16 Aerospace Robotics and Autonomous/Unmanned Systems 6-Jan 1400 hrs 1700 hrs Sun Ballroom 3 IV GNC-17 Lander Technology Development at NASA II 6-Jan 1400 hrs 1730 hrs Miami 1 GNC-18 Control and Diagnostics of Air Vehicles and UAVs 6-Jan 1400 hrs 1730 hrs Sun Ballroom 4 GNC-19 Missile Autopilot and Integrated Control 6-Jan 1400 hrs 1730 hrs Sun Ballroom 6 GNC-20 Spacecraft Guidance, Navigation, and Control I 6-Jan 1400 hrs 1700 hrs Sun Ballroom 5 GNC-21 Advances in UAS Technologies I 7-Jan 0930 hrs 1230 hrs Miami 1 GNC-22 Trajectory Planning and Optimization I 7-Jan 0930 hrs 1230 hrs Sun Ballroom 3 GNC-23 Optimization Based Methods for Estimation and Control 7-Jan 0930 hrs 1230 hrs Sun Ballroom 4 of Flight Vehicles GNC-24 Spacecraft Guidance, Navigation, and Control II 7-Jan 0930 hrs 1230 hrs Sun Ballroom 5 GNC-25 Robust and Fault Tolerant Control 7-Jan 1400 hrs 1730 hrs Miami 1 GNC-26 Trajectory Planning and Optimization II 7-Jan 1400 hrs 1700 hrs Sun Ballroom 3 GNC-27 Nonlinear Control of Aircraft/UAV 7-Jan 1400 hrs 1730 hrs Sun Ballroom 4 GNC-28 Guidance, Navigation and Control Concepts in Air Traffic 7-Jan 1400 hrs 1730 hrs Sun Ballroom 2 Control Systems I GNC-29 Spacecraft Guidance, Navigation, and Control III 7-Jan 1400 hrs 1730 hrs Sun Ballroom 5 GNC-30 Advances in UAS Technologies II 8-Jan 0930 hrs 1230 hrs Miami 1 www.aiaa-SciTech.org 46 #aiaaSciTech IntroSessions at a Glance

Abbreviation Title Date Start Time End Time Location Guidance, Navigation, and Control (continued) GNC-31 Loss of Control Mitigation and Recovery 8-Jan 0930 hrs 1230 hrs Sun Ballroom 3 GNC-32 Guidance, Navigation and Control Concepts in Air Traffic 8-Jan 0930 hrs 1030 hrs Sun Ballroom 4 Control Systems II GNC-33 Mini/Micro Air Vehicle GNC I 8-Jan 0930 hrs 1230 hrs Sun Ballroom 4 GNC-34 Spacecraft Guidance, Navigation, and Control IV 8-Jan 0930 hrs 1230 hrs Sun Ballroom 5 GNC-35 Novel Algorithms in Aircraft GNC 8-Jan 1400 hrs 1730 hrs Sun Ballroom 3 GNC-36 Robust Control of Uncertain Flight Systems 8-Jan 1400 hrs 1730 hrs Miami 1 GNC-37 Mini/Micro Air Vehicle GNC II 8-Jan 1400 hrs 1730 hrs Sun Ballroom 6 GNC-38 Space Exploration and Transportation GNC 8-Jan 1400 hrs 1730 hrs Sun Ballroom 4 GNC-39 Spacecraft Guidance, Navigation, and Control V 8-Jan 1400 hrs 1700 hrs Sun Ballroom 5 GNC-40 Intelligent Systems in GNC 9-Jan 0930 hrs 1230 hrs Miami 1 GNC-41 Design and Analysis of Aircraft Control Laws 9-Jan 0930 hrs 1230 hrs Sun Ballroom 6 GNC-42 Control of Satellites, Spacecrafts and Missiles 9-Jan 0930 hrs 1230 hrs Sun Ballroom 3 GNC-43 Multi-Vehicle Control 9-Jan 0930 hrs 1230 hrs Sun Ballroom 4 GNC-44 Spacecraft Guidance, Navigation, and Control VI 9-Jan 0930 hrs 1230 hrs Sun Ballroom 5 Ground Testing GT-1 New Capabilities in Ground Test Facilities I 5-Jan 0930 hrs 1230 hrs Miami 3 GT-2 The NASA CRM Model & High Reynolds Number 6-Jan 0930 hrs 1230 hrs Miami 3 Aerodynamics and Testing (Invited) GT-3 ETW Test on Separated Wing Flow within the EU FP7 7-Jan 0930 hrs 1230 hrs Sanibel 1 ESWIRP Project (Invited) GT-4 Hypersonic Test Capabilities I (Invited) 7-Jan 1400 hrs 1730 hrs Sanibel 1 GT-5 High Reynolds Number Aerodynamics and Testing 8-Jan 0930 hrs 1230 hrs Sanibel 1 (Invited) GT-6 Unique or Innovative Uses of Existing GTF and Support 8-Jan 0930 hrs 1230 hrs Miami 3 Systems GT-8 Hypersonic Test Capabilities II (Invited) 8-Jan 1400 hrs 1730 hrs Sanibel 1 GT-9 International Symposium on Strain-Gage Balances 8-Jan 1400 hrs 1730 hrs Miami 3 (Invited) GT-10 New Capabilities in Ground Test Facilities II 9-Jan 0930 hrs 1300 hrs Sanibel 1 GT-11 Advances in Test Techniques, Test Management, & EFD/ 9-Jan 0930 hrs 1300 hrs Miami 3 CFD Integration Gas Turbine Engines GTE-1 Gas Turbine Combustion I 5-Jan 0930 hrs 1230 hrs Emerald 1 GTE-2 Film Cooling 5-Jan 1400 hrs 1730 hrs Emerald 1 GTE-3 Engine Systems I 6-Jan 0930 hrs 1230 hrs Emerald 1 GTE-4 Engine Systems II 6-Jan 1400 hrs 1730 hrs Emerald 1 GTE-5 Gas Turbine Combustion II 7-Jan 0930 hrs 1230 hrs Emerald 1 GTE-6 Compressors 7-Jan 1400 hrs 1730 hrs Emerald 1 GTE-7 Gas Turbine Combustion III 8-Jan 0930 hrs 1230 hrs Emerald 1

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Abbreviation Title Date Start Time End Time Location History HIS-1 Topics in Aerospace History 5-Jan 0930 hrs 1230 hrs Tallahassee 2 HIS-2 The NACA Centennial: An Assessment 6-Jan 0930 hrs 1130 hrs Tallahassee 2 High Speed Air Breathing Propulsion HSABP-1 High Speed Inlets 5-Jan 0930 hrs 1230 hrs Emerald 8 HSABP-2 Premixed High Speed Combustion (Invited) 5-Jan 1400 hrs 1730 hrs Emerald 8 HSABP-3 Pressure Gain Combustion - Rotating Detonation Engines 6-Jan 0930 hrs 1230 hrs Emerald 3 I HSABP-4 Numerical Analysis of High Speed Air-Breathing 6-Jan 0930 hrs 1230 hrs Emerald 8 Propulsion HSABP-5 Pressure Gain Combustion - Rotating Detonation Engines 6-Jan 1400 hrs 1730 hrs Emerald 3 II HSABP-6 High Speed Air-Breathing Combustors I 6-Jan 1400 hrs 1730 hrs Emerald 8 HSABP-7 Pressure Gain Combustion - Rotating Detonation Engines 7-Jan 0930 hrs 1230 hrs Emerald 3 III HSABP-8 High Speed Air-Breathing Combustors II 7-Jan 0930 hrs 1230 hrs Emerald 8 HSABP-9/GTE-8 Pressure Gain Combustion - Pulse Detonation Engines 7-Jan 1400 hrs 1730 hrs Emerald 3 Information and Command & Control Systems ICC-1 C2 and Beyond: A Look into the Future of Complex 6-Jan 0930 hrs 1230 hrs Osceola Ballroom 2 Aerospace Command and Control Systems Intelligent Systems IS-1 Intelligent Systems Special Session-Student Paper 5-Jan 0930 hrs 1230 hrs Osceola Ballroom 3 Competition IS-2 Augmenting Adaptive Algorithms for Aircraft Control I 5-Jan 0930 hrs 1230 hrs Osceola Ballroom 2 IS-3 Intelligent Collaborative Control of Multi-Agent Systems 5-Jan 1400 hrs 1730 hrs Osceola Ballroom 2 IS-4 Making Aerospace Operations Intelligent 5-Jan 1400 hrs 1730 hrs Osceola Ballroom 1 IS-5 Invited Panel Discussion - Autonomy Research for Civil 6-Jan 0930 hrs 1230 hrs Osceola Ballroom 3 Aviation: Toward a New Era of Flight IS-6 Realizing the Potential for Genetic Fuzzy Systems 6-Jan 1400 hrs 1730 hrs Osceola Ballroom 1 IS-7 Intelligent Interactions between Humans and Machines 7-Jan 0930 hrs 1230 hrs Osceola Ballroom 3 IS-8 Model-Based Systems and Software Engineering for 7-Jan 0930 hrs 1230 hrs Osceola Ballroom 2 Complex Aerospace Systems IS-9 Invited Panel Discussion - Roadmap for Intelligent Systems 7-Jan 1400 hrs 1700 hrs Osceola Ballroom 3 IS-10 Big Data & Analytics in Aerospace 8-Jan 0930 hrs 1230 hrs Osceola Ballroom 3 IS-11 Augmenting Adaptive Algorithms for Aircraft Control II 8-Jan 0930 hrs 1230 hrs Osceola Ballroom 1 IS-12 Enhancing Safety using Systems Health Management 8-Jan 1400 hrs 1730 hrs Osceola Ballroom 1 IS-13 Intelligent System Approach to Quadcopter Obstacle 9-Jan 0930 hrs 1230 hrs Osceola Ballroom 1 Avoidance International Student Conference ISC-1 International Student Conference (Undergraduate 5-Jan 0900 hrs 1230 hrs St. George 112 Category) ISC-2 International Student Conference (Masters Category) 5-Jan 1400 hrs 1730 hrs St. George 112 ISC-3 International Student Conference (Team Category) 5-Jan 1400 hrs 1730 hrs St. George 114 ISC-4 International Student Conference (Community Outreach 5-Jan 0930 hrs 1230 hrs St. George 114 Category)

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Abbreviation Title Date Start Time End Time Location Materials MAT-1 Nanostructured Materials I 5-Jan 0930 hrs 1230 hrs Sarasota 1 MAT-2 Advanced Materials and Processes 5-Jan 0930 hrs 1230 hrs Sarasota 2 MAT-3 ICME Applications - Residual Stress Modeling and 5-Jan 1400 hrs 1730 hrs Sarasota 1 Measurement MAT-4 Multi-Scale Modeling of Materials 5-Jan 1400 hrs 1730 hrs Sarasota 2 MAT-5 ICME Panel 6-Jan 0930 hrs 1230 hrs Sun Ballroom D MAT-6 Nanostructured Materials II 6-Jan 0930 hrs 1200 hrs Sarasota 1 MAT-7 Fatigue & Fracture I 6-Jan 1400 hrs 1730 hrs Sarasota 1 MAT-8 Constitutive Modeling & Metallics 7-Jan 0930 hrs 1230 hrs Sarasota 1 MAT-9 Materials Testing & Characterization I 7-Jan 0930 hrs 1230 hrs Sarasota 2 MAT-10 Materials & Design for Additive Manufacturing 7-Jan 1400 hrs 1730 hrs Sarasota 1 MAT-11 Fatigue & Fracture II 7-Jan 1400 hrs 1730 hrs Sarasota 2 MAT-12 Fatigue & Fracture III 8-Jan 0930 hrs 1230 hrs Sarasota 1 MAT-13 Materials Testing & Characterization II 8-Jan 0930 hrs 1230 hrs Sarasota 2 Multidisciplinary Design Optimization MDO-1 MDO: Aircraft Systems Design Applications 5-Jan 0930 hrs 1230 hrs Sarasota 3 MDO-2 MDO: Fundamental Algorithms & Processes I 5-Jan 0930 hrs 1230 hrs Osceola Ballroom 5 MDO-3 MDO: Wing Design Applications 5-Jan 1400 hrs 1730 hrs Sarasota 3 MDO-4 MDO: Supersonic Applications 6-Jan 0930 hrs 1230 hrs Sarasota 3 MDO-5 MDO: Fundamental Algorithms & Processes II 6-Jan 1400 hrs 1730 hrs Sarasota 3 MDO-6 MDO: AeroStructure Design I 7-Jan 0930 hrs 1230 hrs Sarasota 3 MDO-7 MDO: Decision Making/Value Driven Design 7-Jan 1400 hrs 1730 hrs Sarasota 3 MDO-8 MDO: AeroStructure Design II 8-Jan 0930 hrs 1230 hrs Sarasota 3 MDO-9 MDO: General Applications 8-Jan 1400 hrs 1730 hrs Sarasota 3 Modeling and Simulation Technologies MST-1 Air Traffic Management I 5-Jan 0930 hrs 1230 hrs Sun Ballroom 1 MST-2 Hardware In the Loop Simulation 5-Jan 0930 hrs 1230 hrs Sun Ballroom 2 MST-4 Modeling of Space Systems and Dynamics 5-Jan 1400 hrs 1730 hrs Sun Ballroom 2 MST-5 Air Traffic Management II 6-Jan 0930 hrs 1230 hrs Sun Ballroom 1 MST-6 Human Factors, Perception, and Cueing 6-Jan 0930 hrs 1230 hrs Sun Ballroom 2 MST-7 Model Design and Development 6-Jan 1400 hrs 1730 hrs Sun Ballroom 1 MST-8 Multi-Domain Modeling and Simulation 6-Jan 1400 hrs 1730 hrs Sun Ballroom 2 MST-9 Modeling of Vehicle Dynamics I 7-Jan 0930 hrs 1230 hrs Sun Ballroom 1 MST-10 Motion Systems, Visual Systems, Image Generation 7-Jan 0930 hrs 1230 hrs Sun Ballroom 2 MST-11 MST Panel: Flight Simulation Training Device 7-Jan 1400 hrs 1700 hrs Sun Ballroom 1 Qualification Testing MST-12 Modeling of Vehicle Dynamics II 8-Jan 0930 hrs 1230 hrs Sun Ballroom 1 MST-13 Model and Simulation Verification and Validation 8-Jan 0930 hrs 1230 hrs Sun Ballroom 2 MST-14 Unmanned Aerial Systems 8-Jan 1400 hrs 1730 hrs Sun Ballroom 1 MST-15 Special Topics in Modeling and Simulation 8-Jan 1400 hrs 1730 hrs Sun Ballroom 2 MST-16 Modeling of Vehicle Dynamics III 9-Jan 0930 hrs 1230 hrs Sun Ballroom 1

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Abbreviation Title Date Start Time End Time Location Meshing, Visualization, and Computational Environments MVC-2 Grid Quality Metrics Related to Solution Accuracy 5-Jan 1400 hrs 1730 hrs Gainesville 2 Including Real-World Configurations MVC-4 Meshing Techniques, Including Surface and Volume Grids, 6-Jan 1400 hrs 1730 hrs Naples 3 and Moving/Deforming Meshes MVC-5 Visualization for Feature Detection, Integration 7-Jan 1400 hrs 1730 hrs Naples 3 Techniques and Frameworks, and Multi-Scale Models MVC-6 Solution Adaptive Meshing, Error Estimation and 9-Jan 0930 hrs 1230 hrs Sun Ballroom D Uncertainty Quantification Techniques Non-Deterministic Approaches NDA-3 Uncertainty Quantification and Management I 6-Jan 0930 hrs 1230 hrs Osceola Ballroom 5 NDA-4 Optimization under Uncertainty 6-Jan 1400 hrs 1730 hrs Osceola Ballroom 5 NDA-5 Random Fatigue, Fracture and Life Prediction 7-Jan 0930 hrs 1230 hrs Osceola Ballroom 5 NDA-6 Model Verification and Validation & Optimization under 7-Jan 1400 hrs 1730 hrs Osceola Ballroom 5 Uncertainty NDA-7 Uncertainty Quantification and Management II 8-Jan 0930 hrs 1230 hrs Osceola Ballroom 5 NDA-8 Non-Deterministic Methods 8-Jan 1400 hrs 1730 hrs Osceola Ballroom 5 Propellants and Combustion PC-1 Plasma Assisted Combustion I: AFOSR MURI Reports 5-Jan 0930 hrs 1230 hrs Emerald 2 PC-2 Advanced Combustion Concepts I 5-Jan 0930 hrs 1230 hrs Emerald 3 PC-3 Spray and Droplet Combustion I 5-Jan 0930 hrs 1230 hrs Emerald 5 PC-4 Turbulent Combustion I 5-Jan 0930 hrs 1230 hrs Emerald 7 PC-5 Plasma Assisted Combustion II: AFOSR MURI Reports 5-Jan 1400 hrs 1730 hrs Emerald 2 PC-6 Combustion Chemistry 5-Jan 1400 hrs 1730 hrs Emerald 3 PC-7 Spray and Droplet Combustion II 5-Jan 1400 hrs 1730 hrs Emerald 5 PC-8 Turbulent Combustion II 5-Jan 1400 hrs 1730 hrs Emerald 7 PC-9 Advanced Combustion Concepts II 6-Jan 0930 hrs 1230 hrs Emerald 5 PC-10 Turbulent Combustion III 6-Jan 0930 hrs 1230 hrs Emerald 7 PC-11 Heterogeneous Combustion and Propellants 6-Jan 1400 hrs 1730 hrs Emerald 5 PC-12 Turbulent Combustion IV 6-Jan 1400 hrs 1730 hrs Emerald 7 PC-13 Advanced Combustion Concepts III 7-Jan 0930 hrs 1230 hrs Emerald 5 PC-14 Combustion Diagnostics 7-Jan 0930 hrs 1230 hrs Emerald 7 PC-15 Turbulent Combustion Models, their Foundations and 7-Jan 1400 hrs 1730 hrs Emerald 2 Major Assumptions PC-16 Laminar Flames 7-Jan 1400 hrs 1730 hrs Emerald 7 PC-17 Detonations, Explosions, and Supersonic Combustion I 8-Jan 0930 hrs 1230 hrs Emerald 3 PC-18 Rocket and Air-Breathing Combustion I 8-Jan 0930 hrs 1230 hrs Emerald 7 PC-19 Detonations, Explosions, and Supersonic Combustion II 8-Jan 1400 hrs 1730 hrs Emerald 3 PC-20 Rocket and Air-Breathing Combustion II 8-Jan 1400 hrs 1730 hrs Emerald 7

www.aiaa-SciTech.org 50 #aiaaSciTech IntroSessions at a Glance

Abbreviation Title Date Start Time End Time Location Plasmadynamics and Lasers PDL-2 Aero-Optics 6-Jan 0930 hrs 1230 hrs Emerald 2 PDL-3 Diagnostics and Experimental Techniques 6-Jan 1400 hrs 1730 hrs Emerald 2 PDL-5 Plasma & Laser Physics I 7-Jan 1400 hrs 1730 hrs Emerald 5 PDL-6 Astronautical Plasma Dynamics 7-Jan 1400 hrs 1730 hrs Emerald 8 PDL-7 Plasma & Laser Propulsion 8-Jan 0930 hrs 1230 hrs Emerald 5 PDL-8 Computational Methods 8-Jan 0930 hrs 1230 hrs Emerald 8 PDL-11 Plasma & Laser Physics II 8-Jan 1400 hrs 1730 hrs Emerald 4 PDL-13 Plasma & Laser Technology 7-Jan 0930 hrs 1230 hrs Emerald 2 Small Satellites SATS-1 Small Satellites - Technologies I 6-Jan 1400 hrs 1730 hrs Miami 3 SATS-2 Small Satellites - Missions 8-Jan 0930 hrs 1230 hrs Captiva 2 SATS-3 Small Satellites - Fusion 8-Jan 1400 hrs 1730 hrs Naples 3 SATS-4 Small Satellites - Technologies II 9-Jan 0930 hrs 1300 hrs Osceola Ballroom 5 Space Operations OPS-1 Space Operations 8-Jan 1400 hrs 1730 hrs Emerald 1 Spacecraft Structures SCS-1 Spacecraft Booms and Trusses 5-Jan 1100 hrs 1230 hrs Osceola Ballroom 4 SCS-2 Solar Sails and Tensioned Membranes 5-Jan 1400 hrs 1730 hrs Osceola Ballroom 4 SCS-3 Packaging and Deployment of Spacecraft Structures 6-Jan 0930 hrs 1230 hrs Osceola Ballroom 4 SCS-4 Composite Material for Spacecraft Structures 6-Jan 1400 hrs 1730 hrs Osceola Ballroom 4 SCS-6 Analysis of Lightweight Spacecraft Structures 7-Jan 0930 hrs 1230 hrs Osceola Ballroom 4 SCS-7 Spacecraft Antennas and Apertures 7-Jan 1400 hrs 1730 hrs Osceola Ballroom 4 SCS-8 Inflatable Space Structures 8-Jan 0930 hrs 1230 hrs Osceola Ballroom 4 SCS-9 Test and Qualification of Spacecraft Structures 8-Jan 1400 hrs 1730 hrs Osceola Ballroom 4 Structural Dynamics SD-1 Computational Aeroelasticity 5-Jan 0930 hrs 1230 hrs Tampa 2 SD-2 Large-deformation Nonlinear Dynamics 5-Jan 0930 hrs 1230 hrs Tampa 3 SD-3 Vehicle/Component Dynamic Environment and Loads 5-Jan 0930 hrs 1230 hrs Osceola Ballroom 6 SD-4 Flutter, LCO and Aeroelastic Tailoring 5-Jan 1400 hrs 1730 hrs Tampa 2 SD-5 Energy Harvesting, Health Monitoring and 5-Jan 1400 hrs 1730 hrs Tampa 3 Multifunctional Structures SD-6 Supersonic/Hypersonic Systems I 6-Jan 0930 hrs 1230 hrs Tampa 2 SD-7 Cable/Beam Modeling I 6-Jan 0930 hrs 1230 hrs Tampa 3 SD-8 Special Session: Transformative Technologies for High- 6-Jan 1400 hrs 1730 hrs Tampa 2 Speed/High-Efficiency Next-Gen Rotorcraft I SD-9 Cable/Beam Modeling II 7-Jan 0930 hrs 1230 hrs Tampa 3 SD-10 Special Session: Adaptive Aeroelastic Wing Shaping 7-Jan 1400 hrs 1730 hrs Sun Ballroom D Control I SD-11 Special Session: Transformative Technologies for High- 7-Jan 1400 hrs 1730 hrs Tampa 2 Speed/High-Efficiency Next-Gen Rotorcraft II SD-12 Flutter, LCO and Aeroelastic Instabilities 7-Jan 1400 hrs 1730 hrs Tampa 3 SD-13/GEPC-5 Special Session: Subsonic Ultra Green Aircraft Research 7-Jan 0930 hrs 1230 hrs Sun Ballroom C (SUGAR) Truss Braced Wing Aeroelasticity www.aiaa-SciTech.org 51 #aiaaSciTech IntroSessions at a Glance

Abbreviation Title Date Start Time End Time Location Structural Dynamics (continued) SD-14 Supersonic/Hypersonic Systems II 8-Jan 0930 hrs 1230 hrs Tampa 2 SD-15 Active and Passive Damping Systems 8-Jan 0930 hrs 1230 hrs Tampa 3 SD-16 Special Session: Adaptive Aeroelastic Wing Shaping 8-Jan 1400 hrs 1730 hrs Sun Ballroom D Control II SD-17 Gust and Turbulence Loads 8-Jan 1400 hrs 1730 hrs Tampa 1 SD-18 Active Aeroelastic Control 8-Jan 1400 hrs 1730 hrs Tampa 2 SD-19 Test and Evaluation and System Identification 8-Jan 1400 hrs 1730 hrs Tampa 3 SD-20 Plate/Shell Modeling 9-Jan 0930 hrs 1300 hrs Sarasota 3 SD-21 Computational Reduced Order Models 9-Jan 0930 hrs 1300 hrs Tampa 2 SD-22 Advanced Measurement Techniques 9-Jan 0930 hrs 1230 hrs Tampa 3 Systems Engineering SE-1 Systems Engineering I 8-Jan 0930 hrs 1230 hrs Miami 2 SE-2 Systems Engineering II 8-Jan 1400 hrs 1730 hrs Miami 2 Sensor Systems SEN-1 Information Fusion 5-Jan 0930 hrs 1230 hrs Osceola Ballroom 1 SEN-2 Novel Sensor Systems 7-Jan 1400 hrs 1730 hrs Osceola Ballroom 1 Software Systems SOF-1 Software Challenges in Aerospace Workshop I 8-Jan 0930 hrs 1230 hrs Osceola Ballroom 2 SOF-2 Software Challenges in Aerospace Workshop II 8-Jan 1400 hrs 1730 hrs Osceola Ballroom 2 Space Resources Utilization SRE-1 Lunar Resource Utilization 7-Jan 0930 hrs 1230 hrs Daytona 2 SRE-2 ISRU for Mars and Beyond 8-Jan 0930 hrs 1230 hrs Daytona 2 Structures STR-1 Special Sessions in Honor of Prof. Harry H. Hilton I 5-Jan 0930 hrs 1230 hrs Sun Ballroom D STR-2 ICME for Structures 5-Jan 0930 hrs 1230 hrs Tampa 1 STR-3 Space Structures 5-Jan 0930 hrs 1230 hrs Tallahassee 3 STR-4 Special Session: Composite Laminate Optimization 5-Jan 1400 hrs 1730 hrs Sun Ballroom D STR-5 Aircraft Structural Design 5-Jan 1400 hrs 1730 hrs Tampa 1 STR-6 Failure Analysis and Prediction I 5-Jan 1400 hrs 1730 hrs Tallahassee 3 STR-7 Special Session: Challenges in the Design of Joined Wings I 6-Jan 0930 hrs 1230 hrs Tampa 1 STR-8 Special Sessions in Honor of Prof. Harry H. Hilton II 6-Jan 0930 hrs 1230 hrs Tallahassee 3 STR-9 Special Session: Impact Damage in Composites 6-Jan 1400 hrs 1730 hrs Sun Ballroom D STR-10 Advanced Structures 6-Jan 1400 hrs 1730 hrs Tampa 1 STR-11 Failure Analysis and Prediction II 6-Jan 1400 hrs 1730 hrs Tallahassee 3 STR-12 Special Session: Challenges in the Design of Joined Wings II 7-Jan 0930 hrs 1230 hrs Tampa 1 STR-13 Special Sessions in Honor of Prof. Harry H. Hilton III 7-Jan 0930 hrs 1230 hrs Tallahassee 3 STR-14 Design, Test and Analysis I 7-Jan 1400 hrs 1730 hrs Tampa 1 STR-15 Structural Stability 7-Jan 1400 hrs 1730 hrs Tallahassee 3 STR-17 Design, Test and Analysis II 8-Jan 1400 hrs 1730 hrs Sarasota 1 STR-18 Special Session: USAF Benchmarking of Composite 8-Jan 1400 hrs 1730 hrs Tallahassee 3 Damage Prediction Methods STR-19 Special Session: Structural Joints & Repair I 8-Jan 1400 hrs 1730 hrs Sarasota 2 www.aiaa-SciTech.org 52 #aiaaSciTech IntroSessions at a Glance

Abbreviation Title Date Start Time End Time Location Structures (continued) STR-20 Special Session: Structural Joints & Repair II 9-Jan 0930 hrs 1300 hrs Sarasota 2 STR-21 Finite Element Analysis 9-Jan 0930 hrs 1300 hrs Sarasota 1 Survivability SUR-1 Air and Space Survivability 6-Jan 1400 hrs 1730 hrs Tampa 3 Terrestial Energy TES-1 Thermal and Fluid Behavior in Power Systems 7-Jan 1400 hrs 1730 hrs Captiva 1 TES-2 Clean and Alternative Fuels 8-Jan 0930 hrs 1230 hrs Tallahassee 2 TES-3 Energy Efficiency and Waste Reduction 8-Jan 1400 hrs 1730 hrs Tallahassee 2 TES-4 Topics in Terrestrial Energy 9-Jan 0930 hrs 1230 hrs Tampa 1 Thermophysics TP-1 Aerothermodynamics I 5-Jan 0930 hrs 1230 hrs Sun Ballroom B TP-2 Cryogenics 5-Jan 1400 hrs 1730 hrs Miami 3 TP-3 Nonequilibrium Flows and Radiation I 5-Jan 1400 hrs 1730 hrs Sun Ballroom B TP-4 Heat Pipes/Heat Transfer I 6-Jan 0930 hrs 1230 hrs Sun Ballroom B TP-5 Nonequilibrium Flows and Radiation II 6-Jan 1400 hrs 1730 hrs Sun Ballroom B TP-6 Heat Transfer II 7-Jan 0930 hrs 1230 hrs Captiva 1 TP-7 Ablation and Surface Catalysis 7-Jan 1400 hrs 1730 hrs Sun Ballroom B TP-8 DSMC and Non-Continuum Flows 8-Jan 0930 hrs 1230 hrs Sun Ballroom B TP-9 NASA Entry Systems Modeling Project 8-Jan 1400 hrs 1730 hrs Sun Ballroom B TP-10 Aerothermodynamics II/Other Thermophysics Topics 9-Jan 0930 hrs 1300 hrs Sun Ballroom 2 TP-11 University Space Systems Programs and Microgravity 9-Jan 0930 hrs 1230 hrs Sun Ballroom B Flight Activities Unmanned Systems UMS-1 UAS Integration: Detect and Avoid Technologies 5-Jan 1400 hrs 1730 hrs Osceola Ballroom 3 UMS-2 Unmanned Systems: Technologies and Applications I 6-Jan 0930 hrs 1230 hrs Osceola Ballroom 1 UMS-3 UAS Sensor Technologies 6-Jan 1400 hrs 1730 hrs Osceola Ballroom 2 UMS-4 UAS Airspace Integration: Policies and Guidelines 7-Jan 0930 hrs 1230 hrs Osceola Ballroom 1 UMS-5 Unmanned Systems: Technologies and Applications II 7-Jan 1400 hrs 1730 hrs Osceola Ballroom 2 Wind Energy WE-1 Wind Energy Aerodynamics and Aeroacoustics I 5-Jan 0930 hrs 1230 hrs Emerald 4 WE-2 Wind Farm and Turbine Wake Interactions I 5-Jan 0930 hrs 1230 hrs Emerald 6 WE-3 Wind Energy Blade and Turbine Design 5-Jan 1400 hrs 1730 hrs Emerald 6 WE-4 Wind Energy Aerodynamics and Aeroacoustics II 5-Jan 1400 hrs 1730 hrs Emerald 4 WE-5 Vertical Axis Wind Turbine (VAWT) Research 6-Jan 0930 hrs 1230 hrs Emerald 4 WE-6 Wind Farm and Turbine Wake Interactions II 6-Jan 0930 hrs 1230 hrs Emerald 6 WE-7 Wind Energy Aerodynamics and Aeroacoustics III 6-Jan 1400 hrs 1730 hrs Emerald 6 WE-8 Wind Energy Materials, Mechanics, and Sensing 6-Jan 1400 hrs 1730 hrs Emerald 4 WE-9 Offshore Wind Energy Systems 7-Jan 0930 hrs 1230 hrs Emerald 4 WE-10 Wind Turbine Loads, Control, and Dynamics 7-Jan 0930 hrs 1230 hrs Emerald 6 WE-11 Wind Turbine Aeroelasticity and Structural Dynamics 7-Jan 1400 hrs 1730 hrs Emerald 4 WE-12 Wind Energy Atmospheric Physics and Inflow 7-Jan 1400 hrs 1730 hrs Emerald 6 WE-13 Wind Energy Innovative Concepts 8-Jan 0930 hrs 1230 hrs Emerald 4 www.aiaa-SciTech.org 53 #aiaaSciTech Monday Monday, 5 January 2015 1-PLNRY-1 Opening Keynote Osceola Ballroom CD 0800 - 0900 hrs Robie Samanta-Roy Vice President, Technology and Innovation Lockheed Martin Corporation Monday, 5 January 2015 2-ISC-1 International Student Conference (Undergraduate Category) St. George 112 Chaired by: C. TAVARES, The Boeing Company 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2015-0001 AIAA-2015-0002 AIAA-2015-0003 AIAA-2015-0004 AIAA-2015-0005 AIAA-2015-0006 AIAA-2015-0007 Martian RHOVER Feasibility Study Satellite Formation Control using Manufacturing of Triaxial Quasi- The Design, Fabrication, and Colorimetric hydrogel-based Signiﬁcance of Constituent Aerodynamic Testing and J. Fuentes, R. Pankaja Kaluarachchi, Differential Drag three-dimensional Composite Evaluation of Millimeter Wave microﬂuidic assay system Chemical age on Solid Rocket Development of Sunswift eVe Cornell University, Ithaca, NY S. Omar, J. Wersinger, Auburn University, Materials Lenses for Beamed Energy to monitor malnutrition in a Propellant Regression Rates S. Ambrose, University of New South Auburn, AL G. Peterson, D. Liu, Michigan State Applications microgravity environment D. Dulin, G. Gibson, Arizona State Wales, New South Wales, Australia University, East Lansing, MI S. Sloan, University of Colorado, Colorado J. Tsosie, New Mexico Institute of Mining University, Tempe, AZ Springs, Colorado Springs, CO and Technology, Socorro, NM Monday, 5 January 2015 3-AA-1 Computational Aeroacoustics I Miami 2 Chaired by: W. EVERSMAN, Missouri University of Science and Technology

54 0930 hrs 1000 hrs 1030 hrs AIAA-2015-0008 AIAA-2015-0009 AIAA-2015-0010 A Computational Study of Flow Hybrid RANS/LES Acoustics Prediction Numerical Study of Synthetic-Jet Within Cavities with Complex in Supersonic Weapons Cavity Actuation Effect on Leading and Geometric Features R. Harris, E. Sheta, CFD Research Trailing Edge Noise M. Barone, S. Arunajatesan, Sandia Corporation, Huntsville, AL; E. Luke, L. Nguyen, V. Golubev, R. Mankbadi, National Laboratories, Albuquerque, NM Mississippi State University, Mississippi M. Sansone, Embry-Riddle Aeronautical State, MS; L. Ukeiley, University of University, Daytona Beach, FL Florida, Gainesville, Gainesville, FL Monday, 5 January 2015 4-AFM-1 AFM Best Student Paper Competition I Captiva 1 Chaired by: B. BURCHETT, Rose-Hulman Institute of Technology 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2015-0011 AIAA-2015-0012 AIAA-2015-0013 AIAA-2015-0014 Effect of Trail Aircraft Size on Sweet Lagrangian Flow Structures Around Evaluation of Hovering Thrust Rapid Modeling of Ablative Shape Spot Location for a Conventional a Flapping Wing Performance of Shrouded Rotors Change for Conceptual Hypersonic Aircraft Pair in Formation M. MacFarlane, J. Humbert, University of for Multi-rotor UAVs to Reduce Mission Design W. Okolo, A. Dogan, University of Texas, Maryland, College Park, College Park, MD Weight H. Saranathan, P. Geldermans, M. Grant, Arlington, Arlington, TX; W. Blake, Air H. Otsuka, K. Nagatani, K. Yoshida, Purdue University, West Lafayette, IN Force Research Laboratory, Wright- Tohoku University, Sendai, Japan Patterson AFB, OH Monday, 5 January 2015 5-AFM-2 Aircraft Flight Dynamics, Handling Qualities and Performance I Captiva 2 Chaired by: K. SHWEYK, Boeing Engineering Operations & Technology and R. LIND, University of Florida 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2015-0015 AIAA-2015-0016 AIAA-2015-0017 AIAA-2015-0018 AIAA-2015-0019 AIAA-2015-0020 Program to Calculate the Computational Analysis of the Experiment Design for Complex NTSB Investigation of an Icing- Piloted Simulation Handling Qualities Controllability Analysis of a Mass- Performance of Airplanes Driven Blade Number Effect on the VTOL Aircraft with Distributed Related Aerodynamic Stall Incident Assessment of a Business Jet Fly-By- Actuated Airplane by a Fixed-Pitch Propeller Performance of a Ducted Propeller Propulsion and Tilt Wing and Pilot Response Wire Flight Control System S. Erturk, A. Dogan, University of Texas, P. Boschetti, P. Gonzalez, E. Cardenas, C. Echavarria, S. Poroseva, University of New P. Murphy, NASA Langley Research Center, M. Moler, D. Crider, R. Cox, National T. Berger, University Affiliated Research Arlington, Arlington, TX Simón Bolívar University, Naiguata, Mexico, Albuquerque, Albuquerque, NM Hampton, VA; D. Landman, Old Dominion Transportation Safety Board, Washington, DC Center, Moffett Field, CA; M. Tischler, Venezuela, Bolivarian Republic of University, Norfolk, VA Army Aviation and Missile Research Development and Engineering Center, Moffett Field, CA; S. Hagerott, C. Eckhart, Cessna Aircraft Company, Wichita, KS Monday, 5 January 2015 6-AMT-1 Pressure Sensitive Paint (PSP) and Novel Measurement Techniques Tallahassee 1 Chaired by: C. KLEIN, DLR - German Aerospace Center and T. LIU, Western Michigan University 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2015-0021 AIAA-2015-0022 AIAA-2015-0023 AIAA-2015-0024 AIAA-2015-0025 AIAA-2015-0026 Dynamic Response Characteristics Global Skin-Friction Measurements Application of Temperature and Application of PSP Technique Unsteady PSP Measurement of Determining Aerodynamic of Polymer/Ceramic Pressure- Using Particle Image Surface Flow Pressure Sensitive Paints to DLR to Near-Field Sonic Boom Transonic Buffet on a Wing Characteristics of an Unmanned Sensitive Paint Visualization and a Luminescent Hypersonic Facilities: “lessons learned” Measurements in a Ballistic Range Y. Sugioka, D. Numata, K. Asai, Tohoku Aerial Vehicle using a 3D Scanning A. Pandey, J. Gregory, Ohio State Oil-Film W. Beck, C. Klein, U. Henne, J. Martinez D. Numata, K. Asai, K. Ohtani, Tohoku University, Sendai, Japan; S. Koike, K. Technique University, Columbus, OH N. Husen, Purdue University, West Schramm, A. Wagner, K. Hannemann, University, Sendai, Japan Nakakita, S. Koga, Japan Aerospace O. Dantsker, University of Illinois, Urbana- Exploration Agency (JAXA), Chofu, Japan 55 Lafayette, IN; T. Liu, Western Michigan German Aerospace Center (DLR), Champaign, Urbana, IL University, Kalamazoo, MI; J. Sullivan, Göttingen, Germany; et al. Purdue University, West Lafayette, IN Monday, 5 January 2015 7-APA-1 Aerodynamic Design: Analysis, Methodologies & Optimization Techniques I Destin 1 Chaired by: C. ROSEMA, US Army AMRDEC and E. WHALEN, Boeing Engineering Operations & Technology 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2015-0027 AIAA-2015-0028 AIAA-2015-0029 AIAA-2015-0030 AIAA-2015-0031 Lift and Drag Measurements of a A Fast Approach to Model the Multi-Fidelity Multi-Disciplinary Application of Simplified Numerical Flight Dynamics Modeling of a Gull-Wing Configuration Aircraft Effects of Propeller Slipstream on Propeller/Rotor Analysis and and Analytical Methods for Rapid Supersonic Aircraft Concept T. Davis, G. Spedding, University of Wing Load Distribution Design Analysis in Atmospheric Entry K. Biber, Bartin University, Bartin, Turkey Southern California, Los Angeles, CA C. Agostinelli, S. Simeone, University N. Nigam, A. Tyagi, P. Chen, Intelligent Vehicle Design of Bristol, Bristol, United Kingdom; A. Automation, Inc., Rockville, MD; J. Alonso, W. Hinman, S. Wilson, C. Johansen, Rampurawala, Airbus, Bristol, United F. Palacios, Stanford University, Stanford, University of Calgary, Calgary, Canada Kingdom; C. Allen, University of Bristol, CA; M. Ol, Air Force Research Laboratory, Bristol, United Kingdom; F. Zhu, University Wright-Patterson AFB, OH; et al. of Sheffield, Sheffield, United Kingdom Monday, 5 January 2015 8-APA-2 Icing or Roughness Effects on Vehicle Aerodynamics I Destin 2 Chaired by: J. GEORGE, Metrolaser Inc. and S. MORRIS, Engineering Systems, Inc. 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2015-0032 AIAA-2015-0033 AIAA-2015-0034 AIAA-2015-0035 Feasibility Study of a Hybrid Ice High-Speed Imaging to Quantify Optimization of the Morphogenetic An Experimental Investigation on Protection System Based on Passive the Transient Ice Accretion Process Approach for In-flight Icing the Unsteady Heat Transfer Process Removal of Residual Ice on a NACA 0012 Airfoil M. Butnarasu, W. Habashi, M. Fossati, Over an Ice Accreting NACA 0012 T. Strobl, Airbus, Munich, Germany; D. R. Waldman, Y. Liu, K. Zhang, H. Hu, Iowa McGill University, Montréal, Canada Airfoil Thompson, Mississippi State University, State University, Ames, IA H. Hu, Y. Liu, R. Waldman, Iowa State Columbus, MS; M. Hornung, Technical University, Ames, IA University of Munich, Munich, Germany Monday, 5 January 2015 9-APA-3 Special Session: Low Reynolds Number Flight at a Crossroads Naples 1 Chaired by: M. CHANG, Lockheed Martin Aeronautics and D. FINLEY, Lockheed Martin Aeronautics 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2015-0036 AIAA-2015-0037 Oral Presentation AIAA-2015-0038 Safety-guaranteed Flight Test Mission-Driven Design and Simulation and control of unsteady Unsteady Aerodynamics of Low Environment for Micro Air Vehicles Fabrication of Fixed-, Flapping-, separated flows over wings at low Reynolds Number Flight D. Lee, J. Han, Korea Advanced Institute and Rotary-Wing Micro Air Vehicles Reynolds number L. Bernal, H. Yu, University of Michigan, of Science and Technology, Daejeon, B. Pipenberg, M. Maughmer, Pennsylvania T. Colonius, California Institute of Ann Arbor, Ann Arbor, MI South Korea State University, University Park, PA Technology, Pasadena, CA Monday, 5 January 2015

56 10-APA-4 Special Session: CREATE-AV High Performance Computing Multiphysics Applications of Full-up Air Vehicles I Naples 2 Chaired by: N. HARIHARAN, CREATE-AV and T. SHAFER, NAVAIR 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2015-0039 AIAA-2015-0040 AIAA-2015-0041 AIAA-2015-0042 AIAA-2015-0043 AIAA-2015-0044 Kestrel Current Capabilities and Cartesian Adaptive Mesh Aeroelastic Simulations with Modal HPCMP CREATE™-AV and the Firebolt c2.0 - Unstructured Grid Application of 3D Strand Solver to Future Direction for Fixed Wing Refinement with the HPCMP and Finite-Element Structural Air Force Digital Thread Navier-Stokes Code for Airframe/ Rotorcraft Hover Aircraft Simulations CREATE™-AV Kestrel Solver Solvers Using CREATE-AV/Kestrel v5 E. Kraft, Air Force Research Laboratory, Propulsion Integration A. Wissink, Army Aviation and Missile S. Morton, CREATE Kestrel Team, Eglin T. Eymann, U.S. Air Force, Eglin AFB, S. Lamberson, Secure Mission Solutions, Wright-Patterson AFB, OH R. Nichols, D. McDaniel, University of Research Development and Engineering AFB, FL FL; R. Nichols, University of Alabama, North Charleston, SC; B. Hallissy, Naval Air Alabama, Birmingham, Birmingham, AL; T. Center, Moffett Field, CA; J. Sitaraman, Birmingham, Birmingham, AL; T. Tuckey, Systems Command, Patuxent River, MD Tuckey, CREATE Kestrel Team, Eglin AFB, FL; University of Wyoming, Laramie, Laramie, U.S. Air Force, Eglin AFB, FL; D. McDaniel, R. Koomullil, Y. Ito, University of Alabama, WY; A. Katz, Utah State University, University of Alabama, Birmingham, Birmingham, Birmingham, AL; J. Klepprt, Logan, UT Birmingham, AL Aerospace Testing Alliance, Arnold AFB, TN Monday, 5 January 2015 11-FD-1 Bio-Inspired Flow Daytona 1 Chaired by: K. GRANLUND, Air Force Research Laboratory and M. GREEN, Syracuse University 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2015-0045 AIAA-2015-0046 AIAA-2015-0047 AIAA-2015-0048 Insect Kinematics in Trimmed Experimental study of kinematics Three-Dimensional Separated Flow Effects of grooves on the formation Flight at Low Reynolds Numbers and fluid structure interaction of on a Flat Plate with Leading-Edge of the LEV of an impulsively-started Using CFD gravity driven falling plates Serrations flat plate C. Badrya, J. Baeder, University of R. Tian, F. Shu, New Mexico State M. Sakai, Y. Sunada, K. Rinoie, University R. Wahidi, A. Lang, J. Wilroy, University of Maryland, College Park, College Park, MD University, Las Cruces, NM of Tokyo, Tokyo, Japan Alabama, Tuscaloosa, Tuscaloosa, AL Monday, 5 January 2015 12-FD-2 CFD Methods I Sanibel 1 Chaired by: H. LUO, North Carolina State University and K. MOHSENI, University of Florida 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2015-0049 AIAA-2015-0050 AIAA-2015-0051 AIAA-2015-0052 AIAA-2015-0053 AIAA-2015-0054 Launch Environment Water Flow Towards the Implementation of Observable Euler Equations for Advanced Optimizations of An Development of Robust Cryogenic Subgrid Model for Shear Rate in Simulation Using Smoothed Particle Wind Turbine Simulations on Many- Inviscid Regularized Two Phase Implicit Navier-Stokes Solver on Cavitation Modeling Capability in Multiphase Simulations Hydrodynamics Core Systems Flow Simulation GPGPU an Advanced CFD Solver P. Zhang, K. Mohseni, University of Florida, B. Vu, J. Berg, M. Harris, NASA Kennedy I. Venetis, N. Nikoloutsakos, E. D. Lipinski, K. Mohseni, University of L. Luo, J. Edwards, H. Luo, F. Mueller, S. Thakur, J. Wright, Streamline Numerics, Gainesville, Gainesville, FL Space Center, Cape Canaveral, FL; A. Gallopoulos, J. Ekaterinaris, University of Florida, Gainesville, Gainesville, FL North Carolina State University, Raleigh, Inc., Gainesville, FL; C. Segal, University of Crespo, University of Vigo, Vigo, Spain Patras, Patras, Greece NC Florida, Gainesville, Gainesville, FL Monday, 5 January 2015 13-FD-3 Discontinuous Galerkin Methods for Turbulent Flows Daytona 2 Chaired by: P. PERSSON, Tsinghua University and M. GALBRAITH 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2015-0055 AIAA-2015-0056 AIAA-2015-0057 AIAA-2015-0058 AIAA-2015-0059 AIAA-2015-0060 A discontinuous Galerkin method Evaluation of a Discontinuous Galerkin A Fourth Order Accurate Cellwise Turbulent Flow Simulations with the A high-order Discontinuous Using LES in a Discontinuous for implicit LES of moderate Implementation of RANS and Spalart Relaxation Implicit Discontinuous High-Order DG Solver Aghora Galerkin Chimera method for Galerkin method with constant and Reynolds number flows Allmaras Turbulence Model Galerkin Scheme for Solving RANS F. Renac, M. de la Llave Plata, E. Martin, laminar and turbulent flows dynamic SGS models C. Carton de Wiart, K. Hillewaert, Cenaero, C. Schrock, J. Benek, Air Force Research Equations J. Chapelier, V. Couaillier, ONERA, M. Wurst, M. Kessler, E. Kraemer, M. Brazell, M. Brazell, M. Stoellinger, D. Gosselies, Belgium Laboratory, Wright-Patterson AFB, OH; H. Asada, Tohoku University, Sendai, Japan; Châtillon, France University of Stuttgart, Stuttgart, Germany Mavriplis, University of Wyoming, Laramie, M. Galbraith, Massachusetts Institute of K. Yasue, Japan Aerospace Exploration Agency Laramie, WY Technology, Cambridge, MA; R. Knapke, M. (JAXA), Chofu, Japan; Y. Ogino, K. Sawada, Turner, University of Cincinnati, Cincinnati, OH Tohoku University, Sendai, Japan 57 Monday, 5 January 2015 14-FD-4 Experimental and Numerical Investigations of Blunt Leading Edge Separation for a 53 Degree Swept Diamond Wing (STO AVT-183) I (Invited) Sanibel 2 Chaired by: S. HITZEL, Airbus Defence & Space , Military Aircraft and R. CUMMINGS, US Air Force Academy 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2015-0061 AIAA-2015-0062 AIAA-2015-0063 AIAA-2015-0064 AIAA-2015-0065 AIAA-2015-0066 A Reduced-Complexity Numerical and Theoretical Leading-Edge Roughness Effects Experimental Analyses on the Flow Incompressible flow calculations of Numerical Investigations of Flow Investigation of Blunt Leading-Edge Considerations for the Design of the on the Flow Separation Onset Field Characteristics of the AVT- blunt leading edge separation for Separation on the AVT-183 53 Degree Separation Motivated by UCAV AVT-183 Diamond-Wing Experimental of the AVT-183 Diamond Wing 183 Diamond Wing Configuration a 53 degree swept diamond wing Swept Diamond Wing Configuration Aerodynamics (Invited) Investigations (Invited) Configuration (Invited) (Invited) (Invited) D. Daniel, Aerospace Testing Alliance, J. Luckring, NASA Langley Research O. Boelens, National Aerospace Laboratory A. Hövelmann, F. Knoth, C. Breitsamter, A. Hövelmann, M. Grawunder, A. Buzica, M. Visonneau, E. Guilmineau, National Arnold AFB, TN; D. Malloy, Arnold Center, Hampton, VA; O. Boelens, National (NLR), Amsterdam, The Netherlands; J. Technical University of Munich, Garching, C. Breitsamter, Technical University of Center for Scientific Research (CNRS), Engineering Development Complex, Arnold Aerospace Laboratory (NLR), Amsterdam, Luckring, NASA Langley Research Center, Germany Munich, Garching, Germany Nantes, France; S. Toxopeus, Maritime AFB, TN; D. Reasor, 412th Test Wing, The Netherlands Hampton, VA; S. Deck, ONERA, Meudon, Research Institute Netherlands (MARIN), Edwards AFB, CA; C. Morris, Aerospace France Wageningen, The Netherlands Testing Alliance, Arnold AFB, TN Monday, 5 January 2015 15-FD-5 Shock-Dominated Flows I Sanibel 3 Chaired by: P. ORKWIS, University of Cincinnati and D. LEVIN, Pennsylvania State University 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2015-0067 AIAA-2015-0068 AIAA-2015-0069 AIAA-2015-0070 Shock Wave-Boundary-Layer Numerical Investigation of On the Drag Efficiency of Study of Shock-Shock Interactions Interactions in Subsonic Intakes at Transonic Airfoil Buffet Suppression Counterjets in Low Supersonic Flow for a Double Wedge Configuration High Incidence Z. Zhang, Northwestern Polytechnical R. Lohner, George Mason University, Using the SUGAR Code T. Makuni, H. Babinsky, University of University, Xi’an, China; K. Qu, City Fairfax, VA; J. Baum, Applied Simulations, S. Sawant, B. Korkut, D. Levin, Cambridge, Cambridge, United Kingdom; University of New York, New York, NY Inc., McLean, VA Pennsylvania State University, University M. Slaby, C. Sheaf, Rolls-Royce Group plc, Park, PA Derby, United Kingdom Monday, 5 January 2015 16-FD-57 New and Revolutionary Approaches in High Speed Flow Turbulence Modeling Sun Ballroom A 0930 - 1230 hrs Chaired by: R. PONNAPPAN and G. BLAISDELL, Purdue University Organized by Daniel Bodony, University of Illinois

Aerothermodynamics and Turbulence-Transition Programs - AFOSR Overview The Effect of Compressibility on Shear Flow Instabilities in High-Speed Flows Low-dimensional modeling of a transitional and turbulent boundary layer Ivett Leyva Sharath S. Girimaji Taraneh Sayadi Emerging Experiments in Compressible Cavity Flows Laminar-Turbulent Transition of Hypersonic Boundary Layer Affected by Surface Roughness The effect of strong wall-cooling on high-speed turbulent boundary layers Steven Beresh Xiaolin Zhong Johan Larsson Vortex ring and shock interaction in a supersonic turbulent boundary layer Chaoqun Liu

Monday, 5 January 2015 17-GEPC-1 N+3 Configuration Concepts and Enabling Technologies in NASA’s Fixed Wing Project Sun Ballroom C Chaired by: R. WAHLS, NASA-Langley Research Center and N. MADAVAN, NASA-Ames 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs Oral Presentation Oral Presentation Oral Presentation Oral Presentation AIAA-2015-0071 Final Results of the Subsonic Ultra Development and Assessment of the Power Balance Assessment of BLI Boundary Layer Ingestion Benefit Engine Architecture for High Green Aircraft Research (SUGAR) Conceptual Design for an Advanced Benefits for Civil Aircraft of the D8 Subsonic Transport Efficiency at Small Core Size Study Civil Transport: An Industry-NASA- A. Huang, D. Hall, A. Uranga, E. Greitzer, A. Uranga, M. Drela, E. Greitzer, N. W. Lord, G. Suciu, J. Chandler, K. Hasel, M. Bradley, The Boeing Company, University Collaborative Enterprise Massachusetts Institute of Technology, Titchener, M. Lieu, N. Siu, Massachusetts Pratt & Whitney, East Hartford, CT Long Beach, CA; C. Droney, The Boeing A. Uranga, E. Greitzer, M. Drela, Cambridge, MA Institute of Technology, Cambridge, MA; et al. 58 Company, Huntington Beach, CA Massachusetts Institute of Technology, Cambridge, MA Monday, 5 January 2015 18-GNC-1 Aerospace Robotics and Autonomous/Unmanned Systems I Sun Ballroom 3 Chaired by: L. POLLINI, University of Pisa; M. BALAS, Embry-Riddle Aeronautical University and Y. CHENG, Mississippi State University 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2015-0072 AIAA-2015-0073 AIAA-2015-0074 AIAA-2015-0075 AIAA-2015-0076 Optimal Airborne Trajectories for Centrifugally Stiffened Rotor: A Vision-Based Proportional Human-In-The-Loop Control of Neural Network Based Control of Data Collection from Wireless A Complete Derivation and Navigation Guidance Law for UAS Guided Airdrop Systems an Airplane UAV using Radial Basis Sensor Networks by Direct Simulation of the Inner Loop Sense and Avoid M. Cacan, M. Ward, E. Scheuermann, M. Functions Collocation Methods Controller M. Clark, Z. Kern, R. Prazenica, Embry- Costello, Georgia Institute of Technology, S. Bhandari, J. Novak, California N. Jodeh, R. Cobb, Air Force Institute of J. Selfridge, University of Virginia, Riddle Aeronautical University, Daytona Atlanta, GA Polytechnic State University, Pomona, CA Technology, Wright-Patterson AFB, OH; R. Charlottesville, Charlottesville, VA Beach, FL Livermore, Air Force Research Laboratory, Wright-Patterson AFB, OH Monday, 5 January 2015 19-GNC-2 Flight Experience of Cassini Spacecraft Attitude Control at Saturn Miami 1 Chaired by: T. BURK, Jet Propulsion Laboratory and J. WEBSTER, Jet Propulsion Laboratory 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs Video Presentation AIAA-2015-0077 AIAA-2015-0078 AIAA-2015-0079 AIAA-2015-0080 Ring World 3 - The Latest Cassini Attitude and Articulation Inflight Characterization of the Titan Density Reconstruction Using Precise Pointing for Radioscience Discoveries of the Cassini Mission Control Subsystem Fault Protection Cassini Spacecraft Propellant Slosh Radiometric and Cassini Attitude Occultations and Radar Mapping at Saturn Challenges During Saturn Proximal and Structural Frequencies Control Flight Data during the Cassini Mission at Saturn Produced by the Jet Propulsion Laboratory, Orbits J. Stupik, A. Lee, Jet Propulsion L. Andrade, T. Burk, F. Pelletier, Jet T. Burk, Jet Propulsion Laboratory, Pasadena, CA. D. Bates, Jet Propulsion Laboratory, California Laboratory, California Institute of Propulsion Laboratory, California Institute California Institute of Technology, Institute of Technology, Pasadena, CA Technology, Pasadena, CA of Technology, Pasadena, CA Pasadena, CA Monday, 5 January 2015 20-GNC-3 GNC Sensor Systems I Sun Ballroom 4 Chaired by: S. FROST, NASA-Ames Research Center and S. RAMASAMY, RMIT University 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2015-0081 AIAA-2015-0082 AIAA-2015-0083 AIAA-2015-0084 AIAA-2015-0085 AIAA-2015-0086 Sensitivity Analysis of Model-based Covariance Analysis of Sensors for Biomimetic optical sensor for Analysis of the Accuracy of MEMS Innovative Navigation and Sensitivity Analysis of an Synthetic Air Data Estimators Wind Field Estimation by Small real-time aircraft wing deflection Magnetometers in Small UAS for Guidance System for Small-to- Automated Formation Flight Based F. Lie, D. Gebre-Egziabher, University of Unmanned Aircraft measurement use in State Estimation Medium Size Unmanned Aircraft on GPS and Transmission Data Minnesota, Minneapolis, Minneapolis, MN J. Elston, B. Argrow, University of Colorado, S. Frost, NASA Ames Research Center, Moffett T. Nichols, J. Elston, B. Argrow, University using Low-Cost Sensors Specifications Boulder, Boulder, CO; M. Stachura, Black Swift Field, CA; C. Wright, M. Khan, University of of Colorado, Boulder, Boulder, CO S. Ramasamy, RMIT University, M. Kilic, M. Meiboom, Technical University Technologies, Boulder, CO Wyoming, Laramie, Laramie, WY Melbourne, Australia of Braunschweig, Braunschweig, Germany Monday, 5 January 2015 21-GNC-4 Missile Guidance I Sun Ballroom 6 Chaired by: A. RATNOO and J. LAFLEUR, Sandia National Laboratories 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2015-0087 AIAA-2015-0088 AIAA-2015-0089 AIAA-2015-0090 AIAA-2015-0091 AIAA-2015-0092 Velocity To Be Gained Guidance Exo-Atmospheric Mid-Course Near-Optimal Minimum Time Intercept Angle Guidance Under Look Angle Constrained Precision Munition Guidance and for a Generic 2D Course Correcting Guidance Guidance under a Spatial Angular Time Varying Speed Impact Angle Control Based on Moving Target Position Estimation Fuze S. Gutman, S. Rubinsky, Technion--Israel Constraint in Atmospheric Flight I. Taub, Israel Aerospace Industries, Ltd., Proportional Navigation S. Sreeja, Indian Institute of Technology P. Strömbäck, J. Robinson, Swedish Institute of Technology, Haifa, Israel N. Indig, J. Z. Ben-Asher, E. Sigal, Ben-Gurion Airport, Israel K. Erer, ROKETSAN Missiles Industries, Inc., Bombay, Mumbai, India Defense Research Agency (FOI), Technion--Israel Institute of Technology, Ankara, Turkey; R. Tekin, ASELSAN, Inc., Stockholm, Sweden Haifa, Israel Ankara, Turkey; M. Ozgoren, Middle East Technical University, Ankara, Turkey

59 Monday, 5 January 2015 22-GNC-5 Novel Navigation, Estimation, and Tracking Methods I Sun Ballroom 5 Chaired by: N. AHMED, CNRS & Université Paris-Sud and W. WHITACRE, Draper Laboratory 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2015-0093 AIAA-2015-0094 AIAA-2015-0095 AIAA-2015-0096 AIAA-2015-0097 Orbit Estimation Of A Continuously Line of Sight Alignment Algorithms Bio-Inspired Absolute Heading In-motion Alignment of Inertial A Monocular Vision-aided Inertial Thrusting Satellite Using Variable for Future Gravity Missions Sensing Based on Atmospheric Navigation System with Doppler Navigation System with Improved Dimension Filters F. Ales, P. Gath, U. Johann, Airbus, Scattering Speed Measurements Numerical Stability G. Goff, J. Black, Air Force Institute of Friedrichshafen, Germany; C. Braxmaier, J. Ashkanazy, J. Humbert, University of K. Bimal Raj, A. Joshi, Indian Institute of D. Magree, E. Johnson, Georgia Institute Technology, Wright-Patterson AFB, OH; University of Bremen, Bremen, Germany Maryland, College Park, College Park, MD Technology Bombay, Mumbai, India of Technology, Atlanta, GA J. Beck, Air Force Research Laboratory, Wright-Patterson AFB, OH Monday, 5 January 2015 23-GT-1 New Capabilities in Ground Test Facilities I Miami 3 Chaired by: G. SYDNOR, NASA Langley Research Center and R. RHEW, NASA-Langley Research Center 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs Oral Presentation Oral Presentation Oral Presentation Oral Presentation Oral Presentation Oral Presentation Historical Overview and Recent New Model Roll Mechanism (MRM) Acoustic Testing Upgrades at the COBRA Data System Upgrades Moving Belt for Ground Proximity Transforming Testing Capabilities at Improvements at the NASA Glenn for the Boeing Transonic Wind LLF at GRC Simulation Upgrade at the LLF the Ames UPWT Research Center 8x6/9x15 Wind Tunnel (BTWT) G. Eitelberg, DNW, Marknesse, The J. Panek, NASA Glenn Research Center, G. Eitelberg, DNW, Marknesse, The J. Bell, NASA Ames Research Center, Tunnel Complex D. Belter, The Boeing Company, Seattle, Netherlands Cleveland, OH Netherlands Moffett Field, CA J. Dussling, NASA Glenn Research Center, WA Cleveland, OH Monday, 5 January 2015 24-GTE-1 Gas Turbine Combustion I Emerald 1 Chaired by: S. SUBRAMANIAN, QuEST Global, Inc. 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2015-0098 AIAA-2015-0099 AIAA-2015-0100 AIAA-2015-0101 AIAA-2015-0102 NOx Emissions Performance Updates to Simulation of a Single- Optimization of Ultra Compact Numerical Investigation of the Early-Stage Design Optimization of and Correlation Equations for a Element Lean-Direct Injection Combustor Flow Path Splits Entropy Wave Generator Test a Turbofan for Low NOx Emissions Multipoint LDI Injector Combustor Using Arbitrary A. Cottle, M. Polanka, Air Force Institute of Case Using Multirate Impedance at Off-Design Operating Conditions Z. He, C. Chang, C. Follen, NASA Glenn Polyhedral Meshes Technology, Wright-Patterson AFB, OH Boundary Conditions L. Zilhão, J. Melo De Sousa, Technical Research Center, Cleveland, OH C. Wey, N. Liu, NASA Glenn Research J. Lourier, B. Noll, M. Aigner, German University of Lisbon, Lisbon, Portugal Center, Cleveland, OH Aerospace Center (DLR), Stuttgart, Germany Monday, 5 January 2015 25-HIS-1 Topics in Aerospace History Tallahassee 2 Chaired by: W. BARRY, NASA HQ 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2015-0103 AIAA-2015-0104 AIAA-2015-0105 AIAA-2015-0106 The First Aerial Raid From Portugal First Aerial South Atlantic Night Flight Is Not Improbable. Octave The Earliest Russian Wind Tunnels to Macau Crossing Chanute Combines Civil Engineering A. Gorbushin, TsAGI, Moscow, Russia F. Neves, J. Barata, A. Silva, University of F. Neves, J. Barata, A. Silva, University of With Aeronautics Beira Interior, Covilha, Portugal Beira Interior, Covilha, Portugal S. Short, National Soaring Museum, Elmira, NY Monday, 5 January 2015 26-HSABP-1 High Speed Inlets Emerald 8 60 Chaired by: G. PANIAGUA, von Karman Institute and D. KIRK, Florida Institute of Technology 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2015-0107 AIAA-2015-0108 AIAA-2015-0109 AIAA-2015-0110 AIAA-2015-0111 AIAA-2015-0112 Numerical and Experimental Viscous Effects and Truncation HIFiRE-6 Unstart Conditions at Flight test of a rugged scramjet- Flow Visualization and Fluctuating Experimental investigation of Research of Mass Addition in Inlet Effects in Axisymmetric Busemann Off-Design Mach Numbers inlet temperature and velocity Pressure Measurements in an a Mach 4 shock-wave turbulent at High Velocities SCRamjet Intakes E. Stephen, S. Hoenisch, C. Riggs, M. Waddel, sensor Internal Compression Inlet boundary layer interaction near an V. Vinogradov, A. Makarov, I. Potekhina, A. Flock, A. Guelhan, German Aerospace U.S. Air Force Academy, Colorado Springs, CO; J. Kurtz, M. Aizengendler, Y. Krishna, P. H. Tabanli, K. Yuceil, Istanbul Technical expansion corner V. Stepanov, Central Institute of Aviation Center (DLR), Cologne, Germany M. Bolender, Air Force Research Laboratory, Walsh, S. O’Byrne, University of New University, Istanbul, Turkey A. SathiaNarayanan, S. Verma, National Motors, Moscow, Russia Wright-Patterson AFB, OH; T. McLaughlin, U.S. South Wales at the Australian Defence Aerospace Laboratories, Bangalore, India Air Force Academy, Colorado Springs, CO Force Academy, Canberra, Australia Monday, 5 January 2015 27-IS-1 Intelligent Systems Special Session-Student Paper Competition Osceola Ballroom 3 Chaired by: S. CHUNG, University of Illinois at Urbana-Champaign 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2015-0113 AIAA-2015-0114 AIAA-2015-0115 AIAA-2015-0116 AIAA-2015-0117 Human Agent Interfaces as a Key Mixed-Initiative Interaction in A Constrained Markov Decision Signal Source Localization Using Adaptive Algorithms for Element for the Dialog between Manned-Unmanned-Teaming Process for Flight Safety Partially Observable Markov Autonomous Data-Ferrying in Human Crews and Cognitive Mission Planning: Design and Assessment and Management Decision Processes Nonstationary Environments Automation Evaluation of a Prototype S. Balachandran, E. Atkins, University of L. Dressel, M. Kochenderfer, Stanford A. Axelrod, G. Chowdhary, Oklahoma Y. Brand, A. Schulte, University of the German F. Schmitt, A. Schulte, University of the Michigan, Ann Arbor, Ann Arbor, MI University, Stanford, CA State University, Stillwater, OK Federal Armed Forces, Munich, Germany German Federal Armed Forces, Munich, Germany Monday, 5 January 2015 28-IS-2 Augmenting Adaptive Algorithms for Aircraft Control I Osceola Ballroom 2 Chaired by: N. NGUYEN, NASA-Ames Research Center 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2015-0118 AIAA-2015-0119 AIAA-2015-0120 AIAA-2015-0121 AIAA-2015-0122 Adaptive Linear Quadratic Gaussian Optimal Filter Design for a Performance Oriented Adaptive Demand-side energy management Bayesian Modeling for Decentralized Optimal Control Modiﬁcation for Discrete-Time Formulation of L1- Architectures with Guaranteed using an adaptive control strategy UAV Control and Task Allocation Flutter Suppression of Adaptive Wing Adaptive Control Bounds for aggregate thermostatic loads S. Hening, P. Regueiro, A. Rodriguez, M. N. Nguyen, S. Swei, NASA Ames Research H. Jafarnejadsani, N. Hovakimyan, B. Gruenwald, T. Yucelen, Missouri M. Ghanavati, A. Chakravarthy, Wichita Teodorescu, University of California, Santa Center, Moffett Field, CA University of Illinois, Urbana-Champaign, University of Science and Technology, State University, Wichita, KS Cruz, Santa Cruz, CA; N. Nguyen, C. Ippolito, Urbana, IL Rolla, MO; M. Fravolini, University of NASA Ames Research Center, Moffett Field, CA Perugia, Perugia, Italy Monday, 5 January 2015 29-ISC-4 International Student Conference (Community Outreach Category) St. George 114 Chaired by: R. ANDINO, AIAA-American Institute of Aeronautics and Astronautics 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs Oral Presentation Oral Presentation Oral Presentation Oral Presentation Oral Presentation Oral Presentation New Mexico State University Integrated Middle School UB UAV Community Outreach Engineers on Deck MSU Space Cowboys Outreach USAFA STEM Outreach for Community Outreach with Educational Outreach Program B. Bergh, T. Lutz, A. Lyons, M. West, M. C. Shields, R. Swasey, Brigham Young A. Sanford, Mississippi State University, Advancing Aeronautical and University Nanosat Program J. Gong, C. Reynolds, University of Majji, University of Buffalo, Buffalo, NY University, Provo, UT Starkville, MS Astronautical Engineering C. Barberan, New Mexico State University, Michigan, Ann Arbor, Ann Arbor, MI T. Hudson, U.S. Air Force Academy, Las Cruces, NM Colorado Springs, CO Monday, 5 January 2015

61 30-LEC-1 Spacecraft Structures Lecture: Advanced Solar Arrays for NASA Electric Propulsion Missions Osceola Ballroom A 0930 - 1030 hrs Thomas Kerslake Power System Engineer NASA Glenn Research Center Monday, 5 January 2015 31-MAT-1 Nanostructured Materials I Sarasota 1 Chaired by: G. ODEGARD, Michigan Technological University; S. ROY, The University of Alabama and B. WARDLE, Massachusettes Institute of Technology 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2015-0123 AIAA-2015-0124 AIAA-2015-0125 AIAA-2015-0126 AIAA-2015-0127 AIAA-2015-0128 Microstructure and High Through- Molecular dynamics of SWNT/ Fracture Toughness of Aligned Experimental Characterization Interlaminar Shear Strength An interphase design strategy thickness Thermal Conductivity Epoxy nanocomposites Carbon Nanotube Polymer of Damage Evolution in Carbon Investigation of Aligned Carbon for multifunctional polymer of Graphite Fiber Composite for N. Fasanella, V. Sundararaghavan, Nanocomposites Nanotube-Polymer Nanocomposites Nanotube-Reinforced Prepreg nanocomposites using multiscale Structural Applications University of Michigan, Ann Arbor, Ann S. Wicks, A. Vazquez, B. Wardle, E. Sengezer, G. Seidel, Virginia Polytechnic Composite Interfaces method A. Hao, S. Wang, J. Horne, M. Yang, R. Arbor, MI Massachusetts Institute of Technology, Institute and State University, Blacksburg, VA D. Lewis, B. Wardle, Massachusetts J. Choi, H. Shin, M. Cho, Seoul National Liang, Florida State University, Tallahassee, Cambridge, MA Institute of Technology, Cambridge, MA University, Seoul, South Korea FL; J. Koo, KAI, LLC, Austin, TX Monday, 5 January 2015 32-MAT-2 Advanced Materials and Processes Sarasota 2 Chaired by: D. POWELL and A. AVILA, Universidade Federal de Minas Gerais 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2015-0129 Oral Presentation AIAA-2015-0130 AIAA-2015-0131 Micromechanical modeling of Developing Strong and Tough Controlling Microstructure and Sapphire Laser Machining Modeling metal-ceramic composites for high Junctions in Carbon Fiber Polymer Deformation with and Experimental Validation temperature applications Composites via Hybridization with Polarized Light in Liquid Crystal for High Temperature Pressure P. Deierling, O. Zhupanska, University of Iowa, Electrospun Polymer Nanofibers Polymer Networks Transducer Development Iowa City, Iowa City, IA; C. Pasiliao, Air Force M. Naraghi, S. Hong, Texas A&M J. Bin, W. Oates, Florida State University, W. Oates, P. Woerner, Florida State Research Laboratory, Eglin AFB, FL University, College Station, TX Tallahassee, FL University, Tallahassee, FL Monday, 5 January 2015 33-MDO-1 MDO: Aircraft Systems Design Applications Sarasota 3 Chaired by: T. TAKAHASHI, Arizona State University and E. ALYANAK, AFRL/RQVC 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2015-0132 AIAA-2015-0133 AIAA-2015-0134 AIAA-2015-0135 AIAA-2015-0136 AIAA-2015-0137 Multi-Disciplinary Optimization of a Aircraft Trajectory Optimisation Value-Driven Design of Non- Rapid Development of Bespoke A modular adjoint approach to Integrated Global Wing and Local Near Sonic Airliner using Wind Forecasting Data Commercial Systems using Bargain Sensorcraft: A Proposed Design Loop aircraft mission analysis and Panel Optimization of Aircraft Wing V. Mirochnitchenko, M. Swann, D. Stallngs, Z. Assaad, M. Moore, C. Bil, A. Eberhard, Modeling C. Paulson, A. Sobester, J. Scanlan, optimization Q. Liu, M. Jrad, S. Mulani, R. Kapania, M. Merrell, D. Miller, T. Takahashi, Arizona RMIT University, Melbourne, Australia E. Goetzke, C. Bloebaum, B. Mesmer, University of Southampton, Southampton, J. Kao, J. Hwang, J. Martins, University of Virginia Polytechnic Institute and State State University, Tempe, AZ Iowa State University, Ames, IA United Kingdom Michigan, Ann Arbor, Ann Arbor, MI University, Blacksburg, VA Monday, 5 January 2015 34-MDO-2 MDO: Fundamental Algorithms & Processes I Osceola Ballroom 5 62 Chaired by: A. KO, Phoenix Integration, Inc. and J. PARRISH, Boeing Research and Technology 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2015-0138 AIAA-2015-0139 AIAA-2015-0140 AIAA-2015-0141 AIAA-2015-0142 AIAA-2015-0143 Discrete Adjoint Formulation for Simple and inexpensive algorithm Stress Constrained Optimization Approximation of the Pareto Surface Graph Coarsening Method for KKT Multifidelity Optimization using Continuum Sensitivity Analysis for surrogate filtering using SLP Level Set Topology via a Hybrid of Scalarization Method Matrices Arising from Orthogonal Statistical Surrogate Modeling M. Kulkarni, R. Canfield, M. Patil, Virginia S. Choze, F. Viana, General Electric Optimization and Evolutionary Algorithm Collocation Methods for Optimal for Non-Hierarchical Information Polytechnic Institute and State University, Company, Niskayuna, NY C. Brampton, P. Dunning, H. Kim, T. Erfani, University College London, London, Control Problems Sources Blacksburg, VA University of Bath, Bath, United Kingdom United Kingdom; H. Samami, University B. Senses, T. Davis, A. Rao, University of R. Lam, Massachusetts Institute of of Leicester, Leicester, United Kingdom; R. Florida, Gainesville, Gainesville, FL Technology, Cambridge, MA; D. Allaire, Erfani, Manchester Metropolitan University, Texas A&M University, College Station, Manchester, United Kingdom; S. Utyuzhnikov, TX; K. Willcox, Massachusetts Institute of University of Manchester, Manchester, United Technology, Cambridge, MA Kingdom Monday, 5 January 2015 35-MST-1 Air Traffic Management I Sun Ballroom 1 Chaired by: J. SCHROEDER, Federal Aviation Administration 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2015-0144 AIAA-2015-0145 AIAA-2015-0146 AIAA-2015-0147 AIAA-2015-0148 Modeling of Complex and Diverse Analysis of the Impact of Improving Aircraft Collision Risk Trajectory Analysis for Accident A Speech-Enabled Simulation Aircraft Trajectories with the Performance Model Accuracy on 4D Estimation using the Cross-Entropy Investigation Interface Agent for Airspace System Trajectory Synthesizer Generalized Trajectory Optimization Method D. Crider, National Transportation Safety Assessments Profile Interface M. Battipede, G. Sirigu, M. Cassaro, P. Gili, Y. Kim, M. Kochenderfer, Stanford Board, Washington, DC H. Lu, V. Cheng, Optimal Synthesis, Inc., Los A. Lee, NASA Ames Research Center, Technical University of Turin, Turin, Italy University, Stanford, CA Altos, CA; D. Ballinger, NASA Ames Research Moffett Field, CA; M. Wu, M. Abramson, Center, Moffett Field, CA; A. Fong, J. Nguyen, University of California, Santa Cruz, Optimal Synthesis, Inc., Los Altos, CA; S. Moffett Field, CA Jones, SimPhonics, Inc., Tampa, FL; et al. Monday, 5 January 2015 36-MST-2 Hardware In the Loop Simulation Sun Ballroom 2 Chaired by: S. KOWALCHUK, Sandia National Laboratories 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2015-0149 AIAA-2015-0150 AIAA-2015-0151 AIAA-2015-0152 AIAA-2015-0153 Rapid Prototyping of Hardware FLINT - a highly-flexible HWIL Distributed Hardware-In- Developing and Testing ECUs for Pitch Axis Control for a Guided Using Real-Time HWIL Simulation solution for GPU accelerated scene Loop Simulations for multiple Electric Drives Projectile in a Wind Tunnel-based Environments generation and sensor modeling Autonomous Aerial Vehicles A. Himmler, dSPACE GmbH, Paderborn, Hardware-In-the-Loop Setup J. Torres, M. Schrempp, S. Kowalchuk, J. Grimes, W. Herald, MacAulay Brown, S. Hangal, B. Tak, H. Arya, Indian Institute Germany; M. Muli, dSPACE, Inc., Wixom, MI G. Strub S. Theodoulis, V. Gassmann, S. Sandia National Laboratories, Inc., Shalimar, FL; R. Thompson, Air Force of Technology Bombay, Mumbai, India Dobre, French-German Research Institute Albuquerque, NM Research Laboratory, Eglin AFB, FL of Saint-Louis (ISL), Saint-Louis, France; M. Basset, University of Upper Alsace, Mulhouse, France Monday, 5 January 2015 37-PANEL-1 U.S. Government Aerospace Technology Roadmaps Osceola Ballroom B 0930 - 1130 hrs Moderator: Mark Lewis, Director, IDA Science & Technology Policy Institute Panelists: Thomas Beutner Dennis Filler David Miller Robie Samanta-Roy Morley Stone Head, Naval Air Warfare and Weapons Director, FAA William J. Hughes Technical Center Chief Technologist Vice President,Technology and Innovation Chief Technologist, Air Force Research Laboratory Office of Naval Research NASA Lockheed Martin Corporation Wright-Patterson AFB

Monday, 5 January 2015

63 38-PC-1 Plasma Assisted Combustion I: AFOSR MURI Reports Emerald 2 Chaired by: J. TISHKOFF and W. LEMPERT, Vanderbilt University 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2015-0154 AIAA-2015-0155 AIAA-2015-0156 AIAA-2015-0157 AIAA-2015-0158 AIAA-2015-0159 An Overview or the AFOSR Plasma Challenges in Understanding and Plasma assisted combustion: Atmospheric Pressure Plasma Based Plasma Assisted Combustion Non-Equilibrium Plasma-Assisted Assisted Combustion MURI Program Predictive Modeling of Plasma kinetic studies and new combustion Flame Control and Diagnostics Mechanism for Small Hydrocarbons Flow Reactor Studies of Highly W. Lempert, Ohio State University, Assisted Combustion technology R. Miles, Princeton University, Princeton, A. Starikovskiy, Princeton University, Diluted Reactive Mixtures Columbus, OH I. Adamovich, W. Lempert, J. Sutton, Ohio Y. Ju, J. Lefkowitz, T. Wada, X. Yang, S. Won, NJ Princeton, NJ N. Tsolas, K. Togai, R. Yetter, Pennsylvania State University, Columbus, OH Princeton University, Princeton, NJ; W. Sun, State University, University Park, PA Georgia Institute of Technology, Atlanta, GA Monday, 5 January 2015 39-PC-2 Advanced Combustion Concepts I Emerald 3 Chaired by: M. ANAND, Rolls-Royce Corp 0930 hrs 1000 hrs AIAA-2015-0160 AIAA-2015-0161 Oxygen-rich Combustion of A Electro-chemical propulsion for Porous Cylindrical Burner space exploration K. Pan, S. Chen, National Taiwan A. Ingenito, A. Agresta, University of Rome University, Taipei, Taiwan “La Sapienza”, Rome, Italy; R. Andriani, Technical University of Milan, Milan, Italy; F. Gamma, University of Rome “La Sapienza”, Rome, Italy Monday, 5 January 2015 40-PC-3 Spray and Droplet Combustion I Emerald 5 Chaired by: B. CHEHROUDI, European Research Council (ERC) and J. BELLAN, Jet Propulsion Laboratory 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2015-0162 AIAA-2015-0163 AIAA-2015-0164 AIAA-2015-0165 AIAA-2015-0166 A priori and a posteriori analyses Simulation of Subcritical Primary Ray tracing analysis of realistic Exploration of Gas Phase Properties Modeling the Diffusion to of multi-species turbulent mixing Atomization in a Rule-Based CFD atomizing jet geometries for optical in Aerated-Liquid Jets Using X-Ray Kinetically Controlled Burning layers at supercritical-p conditions Framework Using Stochastic Modeling connectivity applications Fluorescence Transition of Micron-Sized G. Borghesi, California Institute of S. Thakur, M. Kumar, University of Florida, G. Charalampous, N. Soulopoulos, Y. K. Lin, Taitech, Inc., Beavercreek, OH; Aluminum Particles Technology, Pasadena, CA; J. Bellan, Jet Gainesville, Gainesville, FL; E. Luke, Mississippi Hardalupas, Imperial College London, C. Carter, S. Smith, Air Force Research B. Bojko, P. DesJardin, State University of Propulsion Laboratory, California Institute State University, Mississippi State, MS London, United Kingdom Laboratory, Wright-Patterson AFB, OH; A. New York, Buffalo, NY of Technology, Pasadena, CA Kastengren, Argonne National Laboratory, Chicago, IL Monday, 5 January 2015 41-PC-4 Turbulent Combustion I Emerald 7 Chaired by: T. LIEUWEN, Georgia Institute of Technology and J. OEFELEIN, Sandia National Laboratories 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2015-0167 AIAA-2015-0168 AIAA-2015-0169 AIAA-2015-0170 Large-eddy simulation of a turbulent Measurements of Premixed Propagation of Premixed Flame Characterization of the sooting ﬂame in a swirling combustor Turbulent Combustion Regimes of Kernels in High Speed Channel Temperature and Velocity Field H. Koo, V. Raman, University of Texas, Austin, High Reynolds Number Flames Flows with Moderate Turbulence Structure in Turbulent Premixed Austin, TX; M. Mueller, Princeton University, J. Temme, T. Wabel, A. Skiba, J. Driscoll, N. Grady, R. Pitz, Vanderbilt University, Jet Flames Princeton, NJ; K. Geigle, German Aerospace University of Michigan, Ann Arbor, Ann Nashville, TN; S. Menon, B. Ochs, D. P. Allison, H. Shen, T. McManus, J. Sutton, Center (DLR), Stuttgart, Germany Arbor, MI Scarborough, T. Slais, Georgia Institute of Ohio State University, Columbus, OH

64 Technology, Atlanta, GA Monday, 5 January 2015 42-SD-1 Computational Aeroelasticity Tampa 2 Chaired by: K. GRIFFIN, Southwest Research Institute and B. GLAZ, U. S. Army Research Laboratory (APG) 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2015-0171 AIAA-2015-0172 AIAA-2015-0173 AIAA-2015-0174 AIAA-2015-0175 Numerical Study of the Transonic Adjoint-Based h-adaptive Aeroelastic Stability Predictions of Forced and Aeroelastic Response Accelerated convergence of static Limit Cycle Oscillation Phenomenon Calculation of Generalized a Business Jet Landing Gear Door of Bird-Damaged Fan Blades - A aeroelasticity using low-fidelity on the F-16 Fighter Aircraft Aerodynamic Forces using High Fidelity Fluid-Structure Comparison and Its Implications aerodynamics D. Raveh, Technion--Israel Institute of M. Bhatia, P. Beran, Air Force Research Interaction Tools E. Muir, P. Friedmann, University of K. Jovanov, R. De Breuker, Delft University Technology, Haifa, Israel; M. Iovnovich, Laboratory, Wright-Patterson AFB, OH E. Blades, A. Cornish, ATA Engineering, Michigan, Ann Arbor, Ann Arbor, MI of Technology, Delft, The Netherlands D. Michaels, M. Adar, Israeli Air Force, Tel Inc., Huntsville, AL Aviv, Israel Monday, 5 January 2015 43-SD-2 Large-deformation Nonlinear Dynamics Tampa 3 Chaired by: D. JOHNSON, NASA Glenn Research Center and W. SCHNEIDER, Lockheed Martin Aeronautics 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2015-0176 AIAA-2015-0177 AIAA-2015-0178 AIAA-2015-0179 AIAA-2015-0180 AIAA-2015-0181 An Enhanced Modal Approach for Reduced order modeling of loads Nonlinear Aeroelastic Modeling and Nonlinear Aeroservoelastic Analysis Nonlinear Model Updating of a Limit-cycle Oscillations of a Large Deformation Modeling of and deformation of a flexible Analysis of Flexible Wind Turbine of Flexible Aircraft Described by Cantilevered Plate and a Stiffened pretensed Membrane Strip Wing-Like Structures flapping wing Blades Large Finite-Element Models Skin Panel from a Lynx Helicopter A. Drachinsky, D. Raveh, Technion--Israel M. Ritter, German Aerospace Center (DLR), J. Tran, J. Sirohi, University of Texas, W. Su, W. Song, University of Alabama, Y. Wang, A. Wynn, R. Palacios, Imperial M. Allen, University of Wisconsin, Institute of Technology, Haifa, Israel Göttingen, Germany; C. Cesnik, University Austin, Austin, TX; H. Gao, M. Wei, New Tuscaloosa, Tuscaloosa, AL College London, London, United Kingdom Madison, Madison, WI; B. Weekes, of Michigan, Ann Arbor, Ann Arbor, MI; W. Mexico State University, Las Cruces, NM University of Bristol, Bristol, United Krüger, German Aerospace Center (DLR), Kingdom Göttingen, Germany Monday, 5 January 2015 44-SD-3 Vehicle/Component Dynamic Environment and Loads Osceola Ballroom 6 Chaired by: A. SCOTTI, Pilatus Aircraft Ltd and J. MCNAMARA, The Ohio State University 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2015-0182 AIAA-2015-0183 AIAA-2015-0184 AIAA-2015-0185 AIAA-2015-0186 Analytical Prediction and Test Integrated Flight Dynamics and Static and Dynamic Buckling of Integrated Flexible Dynamic PyPAD: A Multidisciplinary Correlation of Spacecraft Cavity Aeroelasticity of Flexible Aircraft with a DAEDALOS Composite Panel Maneuver Loads Models based on Framework for Preliminary Acoustic Environment Application to Swept Flying Wings Including Material Damping Aerodynamic Influence Coefficients Airframe Design D. Inoyama, R. Agarwal, T. Stoumbos, R. Simpson, R. Palacios, Imperial College M. Dalenbring, U. Falk, A. Zdunek, Swedish of a 3D Panel Method L. Travaglini, S. Ricci, G. Bindolino, Orbital Sciences Corporation, Dulles, VA London, London, United Kingdom; Defense Research Agency (FOI), Stockholm, T. Kier, German Aerospace Center (DLR), Technical University of Milan, Milan, Italy P. Goulart, Swiss Federal Institute of Sweden; C. Bisagni, R. Vescovini, Technical Wessling, Germany Technology, Zürich, Switzerland University of Milan, Milan, Italy Monday, 5 January 2015 45-SEN-1 Information Fusion Osceola Ballroom 1 Chaired by: T. FREY, Lockheed Martin Aeronautics 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2015-0187 AIAA-2015-0188 AIAA-2015-0189 AIAA-2015-0190 AIAA-2015-0191 Increasing the Convergence Rate of Consensus based Heuristic Multipath Routing and Sensor- Autonomous Flight Path Planning A Constrained Altruistic Method for the Extended Kalman Filter Algorithm for Distributed Sensor Wireless Scheduling to Reduce for Traffic Monitoring in Wireless Balancing Tracking Responsibility in M. Rhudy, Lafayette College, Easton, PA Management Latency and Packet Loss over Sensor Networks a Distributed Fusion Network K. Neema, D. DeLaurentis, Purdue Tactical Wireless Networks N. Jodeh, R. Cobb, Air Force Institute of T. Frey, Lockheed Martin Corporation, Fort University, West Lafayette, IN R. Tuggle, PeopleTec, Huntsville, AL Technology, Wright-Patterson AFB, OH Worth, TX Monday, 5 January 2015

65 46-STR-1 Special Sessions in Honor of Prof. Harry H. Hilton I Sun Ballroom D Chaired by: C. BELDICA, University of Illinois-NCSA and R. SULLIVAN, Mississippi State University 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2015-0192 AIAA-2015-0193 AIAA-2015-0194 AIAA-2015-0195 AIAA-2015-0196 AIAA-2015-0197 Creep Buckling of Viscoelastic Time to Flutter of a Viscoelastic Large-Strain Viscoelastic Generalized Unified Formulation Vibration Mitigation in Composite Nonlinear Structural Analysis of a Columns Modeled using Anelastic Goland Wing Constitutive Models for Thin Shell Element for Functionally Plates using an Electromagnetic Icosahedron and Its Application to Displacement Fields C. Merrett, Carleton University, Ottawa, Polyethylene Films Graded Variable-Stiffness Composite Field Lighter Than Air Vehicles Under an G. Lesieutre, Pennsylvania State Canada J. Li, K. Kwok, S. Pellegrino, California Laminates and Aeroelastic Applications D. Chernikov, P. Krokhmal, O. Zhupanska, Internal Vacuum University, University Park, PA Institute of Technology, Pasadena, CA L. Demasi, Y. Ashenafi, R. Cavallaro, San University of Iowa, Iowa City, Iowa City, IA A. Palazotto, Air Force Institute of Diego State University, San Diego, CA Technology, Wright-Patterson AFB, OH Monday, 5 January 2015 47-STR-2 ICME for Structures Tampa 1 Chaired by: S. ENGELSTAD, Lockheed Martin Aeronautics; S. ARNOLD, University of Heidelberg, Germany and J. DUSTIN, GE-Aviation 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2015-0198 AIAA-2015-0199 AIAA-2015-0200 AIAA-2015-0201 AIAA-2015-0202 Integrated Computational Recent Progress in Implementation Experiences With Materials Structure Genome: Fill the Gap Microstructural Influence on Materials Engineering for Airframe of ICME for Metallic Materials in Information Management Systems between Materials Genome and Deformation and Fatigue Life of Composite Structure Applications the Airframe Industry For ICME: The Importance Of Structural Analysis Composites Using the Generalized S. Engelstad, R. Koon, J. Action, Lockheed R. Glamm, D. Rosenbladt, E. Pripstein, J. Metadata W. Yu, Purdue University, West Lafayette, Method of Cells Martin Corporation, Marietta, GA; J. Riga, Cotton, The Boeing Company, Seattle, WA W. Marsden, S. Warde, E. Cope, D. IN S. Arnold, P. Murthy, B. Bednarcyk, E. Lockheed Martin Corporation, Cherry Debon, Granta Design, Cambridge, United Pineda, NASA Glenn Research Center, Hill, NJ; A. Waas, University of Michigan, Kingdom Cleveland, OH Ann Arbor, Ann Arbor, MI; D. Robbins, AutoDesk, Inc., Laramie, WY; et al. Monday, 5 January 2015 48-STR-3 Space Structures Tallahassee 3 Chaired by: J. DOMBER, Ball Aerospace & Technologies Corporation and A. CHATTOPADHYAY, Arizona State University 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2015-0203 AIAA-2015-0204 AIAA-2015-0205 AIAA-2015-0206 AIAA-2015-0207 A technique to evaluate on-orbit Finite Element Analysis of the MOIRE Strongback Thermal Design and Testing of Deployable Blossoming of Coiled Deployable thermal deformation for large Inflatable Re-Entry Vehicle Stability Analysis and Test Results Carbon Fiber Booms for CubeSat Booms precise structures in ASTRO-H Experiment (IRVE) D. Waller, J. Domber, Ball Aerospace & Non-Gossamer Applications A. Hoskin, University of Surrey, Guildford, T. Kawano, K. Ishimura, K. Minesugi, L. Li, K. Gonyea, R. Braun, Georgia Technologies Corporation, Boulder, CO; S. West, C. White, C. Celestino, S. United Kingdom Japan Aerospace Exploration Agency Institute of Technology, Atlanta, GA B. Belnap, R. Rynders, ATK, Magna, Philpott, M. Pankow, North Carolina State (JAXA), Sagamihara, Japan; K. Omagari, UT; R. Schweickart, Ball Aerospace & University, Raleigh, NC NEC Corporation, Fuchu, Japan; K. Tanaka, Technologies Corporation, Boulder, CO Nippi Corporation, Yokohama, Japan Monday, 5 January 2015 49-TP-1 Aerothermodynamics I Sun Ballroom B Chaired by: M. BORG, Air Force Research Laboratory and T. SCHWARTZENTRUBER, University of Minnesota 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2015-0208 AIAA-2015-0209 AIAA-2015-0210 AIAA-2015-0211 AIAA-2015-0212 AIAA-2015-0213 Aerothermal Environment and Boundary Layer Transition and Trip LES Computation of Turbulent Heat Numerical Investigation of Tangential Blowing to a Supersonic NASA Langley Experimental Thermal Response of Supersonic Effectiveness on an Apollo Capsule Flux on Reentry Capsule Afterbody Geometric Effects of Stardust Flow on a Blunted Nose Aerothermodynamic Contributions Inflatable Decelerators in the JAXA High Enthalpy Shock with Forced Transition Return Capsule Heat Shield I. Egorov, E. Vasilevskii, A. Novikov, I. to Slender and Winged Hypersonic S. Muppidi, ERC, Inc., Moffett Field, CA; Tunnel (HIEST) Facility T. Ishihara, Y. Ogino, N. Ohnishi, Tohoku H. Weng, A. Martin, University of Ezhov, TsAGI, Zhukovsky, Russia Vehicles R. Tanimoto, Jet Propulsion Laboratory, L. Kirk, R. Lillard, NASA Johnson Space University, Sendai, Japan; H. Tanno, Japan Kentucky, Lexington, Lexington, KY S. Berry, K. Berger, NASA Langley California Institute of Technology, Center, Houston, TX; J. Olejniczak, NASA Aerospace Exploration Agency (JAXA), Research Center, Hampton, VA

66 Pasadena, CA; D. Bose, C. Tang, NASA Ames Research Center, Moffett Field, CA; Kakuda, Japan Ames Research Center, Moffett Field, CA; I. H. Tanno, Japan Aerospace Exploration Clark, Jet Propulsion Laboratory, California Agency (JAXA), Kakuda, Japan Institute of Technology, Pasadena, CA Monday, 5 January 2015 50-WE-1 Wind Energy Aerodynamics and Aeroacoustics I Emerald 4 Chaired by: M. CHURCHFIELD, National Renewable Energy Laboratory and A. MITTAL, The University of Tennessee at Chattanooga 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2015-0214 AIAA-2015-0215 AIAA-2015-0216 AIAA-2015-0217 AIAA-2015-0218 Modeling Wind Turbine Tower and Development and Validation of a New Improvements to the Actuator Line Modeling and Simulation of a Validation of a High-Order Implicit Nacelle Effects within an Actuator Blade Element Momentum Skewed- Modeling for Wind Turbines 3MW Wind Turbine Blade for LES Solver for the Simulation of a Line Model Wake Model within AeroDyn A. Mittal, K. Sreenivas, L. Taylor, Determination and Analysis of Flow Low-Reynolds-Number Vertical-Axis M. Churchfield, S. Lee, National A. Ning, Brigham Young University, Provo, UT; L. Hereth, University of Tennessee, Characteristics Wind Turbine Renewable Energy Laboratory, Golden, CO; G. Hayman, R. Damiani, J. Jonkman, National Chattanooga, Chattanooga, TN A. Raina, K. Wetzel, Wetzel Engineering, S. Kanner, P. Persson, University of S. Schmitz, Z. Wang, Pennsylvania State Renewable Energy Laboratory, Golden, CO Inc., Austin, TX; S. Farokhi, University of California, Berkeley, Berkeley, CA University, University Park, PA Kansas, Lawrence, Lawrence, KS Monday, 5 January 2015 51-WE-2 Wind Farm and Turbine Wake Interactions I Emerald 6 Chaired by: J. BAKER, Frontier Wind and F. GRASSO, Energy Research Center of the Netherlands (ECN) 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2015-0219 AIAA-2015-0220 AIAA-2015-0221 AIAA-2015-0222 AIAA-2015-0223 AIAA-2015-0224 Preliminary Field Test of the Wind A Study of Intensified Wake Deflection System Identification of a Wind On the feasibility of using porous discs Turbulent mixing in wind Computational Simulation of the Turbine Wake Imaging System by Multiple Yawed Turbines based on Turbine Array for wind tunnel simulations of wind turbine and actuator disc wakes: Interaction Between Tandem Wind T. Herges, D. Maniaci, D. Bossert, R. Large Eddy Simulations J. Annoni, K. Howard, P. Seiler, M. Guala, farm power variation with turbine experiments and POD analysis Turbines with Offset Schmitt, B. Naughton, Sandia National L. Luo, North Carolina State University, University of Minnesota, Minneapolis, layout L. Lignarolo, D. Ragni, C. Simao Ferreira, K. Sreenivas, A. Mittal, L. Hereth, Laboratories, Albuquerque, NM Raleigh, NC; N. Srivastava, P. Ramaprabhu, Minneapolis, MN R. Theunissen, C. Allen, University of Bristol, G. van Bussel, Delft University of L. Taylor, University of Tennessee, University of North Carolina, Charlotte, Bristol, United Kingdom; P. Housley, SSE Technology, Delft, The Netherlands Chattanooga, Chattanooga, TN Charlotte, NC Renewables, Bristol, United Kingdom Monday, 5 January 2015 52-SCS-1 Spacecraft Booms and Trusses Osceola Ballroom 4 Chaired by: J. BLANDINO, Virginia Military Institute and J. HINKLE, ILC Dover 1100 hrs 1130 hrs 1200 hrs AIAA-2015-0225 AIAA-2015-0226 AIAA-2015-0227 Application of a Novel Long-Reach Embedding High Performance Simulation of Locking Space Truss Manipulator Concept to Asteroid Electrical Conductors in Space-Based Deployments Redirect Missions Deployable Composite Structures D. Van Dyne, A. Jennings, J. Black, Air J. Dorsey, W. Doggett, T. Jones, NASA Langley B. Davis, W. Francis, M. Hulse, P. Keller, Force Institute of Technology, Wright- Research Center, Hampton, VA; B. King, D. Campbell, G. Freebury, Roccor, LLC, Patterson AFB, OH Northrop Grumman Corporation, Hampton, VA Louisville, CO

67 Monday, 5 January 2015 53-LUNCH-1 Durand Lectureship and Public Policy Luncheon Osceola Ballroom CD 1230 - 1400 hrs Making an Impact in Public Service Michael W. Wynne Former Secretary of the Air Force Senior Advisor to the President of The Stevens Institute Monday, 5 January 2015 54-AA-2 Jet Noise Measurements I Miami 2 Chaired by: K. AHUJA, Georgia Institute of Technology 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2015-0228 AIAA-2015-0229 AIAA-2015-0230 AIAA-2015-0231 AIAA-2015-0232 AIAA-2015-0233 Turbulence Measurements of An Empirical Jet-Surface Interaction Characterization of a Supersonic Noise Reduction in Supersonic Jets Exploring Physics and Control of Investigation of a Heated Rectangular Nozzles with Bevel Noise Model with Temperature and Rectangular Jet over a Range of from Rectangular Convergent- Twin Supersonic Circular Jets Supersonic Jet Chevrons Nozzle J. Bridges, M. Wernet, NASA Glenn Nozzle Aspect Ratio Effects Test Conditions Divergent Nozzles J. Cluts, C. Kuo, M. Samimy, Ohio State P. Mora, J. Kastner, E. Gutmark, Research Center, Cleveland, OH C. Brown, NASA Glenn Research Center, G. Valentich, T. Davis, R. Kumar, F. Alvi, R. Powers, D. McLaughlin, P. Morris, University, Columbus, OH University of Cincinnati, Cincinnati, OH; K. Cleveland, OH Florida State University, Tallahassee, FL; Pennsylvania State University, University Kailasanath, Naval Research Laboratory, M. Alphonso, C. Harris, Northrop Grumman Park, PA Washington, DC Corporation, Redondo Beach, CA Monday, 5 January 2015 55-AFM-3 AFM Best Student Paper Competition II Captiva 1 Chaired by: M. GRANT, Purdue University 1400 hrs 1430 hrs AIAA-2015-0234 AIAA-2015-0235 Black-box LTI modelling of flapping- Aerodynamic Modeling and wing micro aerial vehicle dynamics Optimization of Sideslip Perching S. Armanini, C. de Visser, G. de Croon, Maneuver Delft University of Technology, Delft, The M. Alikhan, T. Go, Florida Institute of Netherlands Technology, Melbourne, FL Monday, 5 January 2015 56-AFM-4 Aircraft Flight Dynamics, Handling Qualities and Performance II Captiva 2 Chaired by: D. OWENS, NASA-Langley Research Center and M. COTTING, US Air Force Test Pilot School 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2015-0236 AIAA-2015-0237 AIAA-2015-0238 AIAA-2015-0239 AIAA-2015-0240 AIAA-2015-0241 Subset Simulation for Estimating Symmetric Steady Flapping Flight Brain Control of Horizontal Exposing Unique Pilot Behaviors Model Order Reduction for Control Improved Models for the Ground Small Failure Probabilities of of Bird-Scale Aircraft, Using Airplane Motion - A Comparison of from Flight Test Data Design of Flexible Free-Flying Aircraft Handling Assessment of Navy an Aerial System Subject to Bifurcation and Continuation Two Approaches D. Klyde, P. Schulze, P. Thompson, N. Tantaroudas, University of Liverpool, Aircraft Atmospheric Turbulences Method T. Fricke, Technical University of Munich, Systems Technology, Inc., Hawthorne, CA Liverpool, United Kingdom; A. Da Ronch, D. Klyde, T. Myers, A. Lampton, Systems D. Löbl, F. Holzapfel, Technical University A. Paranjape, McGill University, Montréal, Munich, Germany; V. Paixão, N. Loureiro, University of Southampton, Southampton, Technology, Inc., Hawthorne, CA; M. of Munich, Garching, Germany Canada R. Costa, Champalimaud Center for the United Kingdom; K. Badcock, University of Draper-Donley, M. Bishop, Naval Air Unknown, Lisbon, Portugal; F. Holzapfel, Liverpool, Liverpool, United Kingdom; Y. Systems Command, Patuxent River, MD Technical University of Munich, Munich, Wang, R. Palacios, Imperial College London, Germany London, United Kingdom 68 Monday, 5 January 2015 57-APA-5 Aerodynamic Testing: Wind Tunnel & Flight Testing I Destin 1 Chaired by: G. GATLIN and J. LIN, NASA-Langley Research Center 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs AIAA-2015-0242 AIAA-2015-0243 AIAA-2015-0244 AIAA-2015-0245 AIAA-2015-0246 AIAA-2015-0247 AIAA-2015-0248 Unsteady Pressures on a Generic Investigation of the Unique Aerodynamic Evaluation of a Investigation of Model Scale on Wind Tunnel Testing of Scaled Cascade Test in 6x6 Inch Evaluating an Experimental Capsule Shape Stability Characteristics of the NASA Capsule Shaped Projectile during Wind Tunnel Measurements of Ship Unconventional Airships Docking Flow Duct Streamlined Fairing for a Diverter J. Ross, N. Burnside, NASA Ames Research Maraia Reentry Vehicle Free Flight Testing with Ballistic Air Loads and Air Wake In-Flight and Conceptual Design of J. Locke, Spirit AeroSystems, Inc., Less Supersonic Inlet (DSI) Center, Moffett Field, CA J. Hunt, C. Shannon, T. Yechout, U.S. Air Range N. Rosenfeld, K. Kimmel, A. Sydney, Naval Docking Mechanism Wichita, KS Equipped Aircraft Force Academy, Colorado Springs, CO A. Ishida, H. Nagai, Tohoku University, Surface Warfare Center, Bethesda, MD A. Kaluvan, Imperial College London, J. Masud, O. Khan, Air University, Sendai, Japan; H. Tanno, T. Komuro, London, United Kingdom; P. Marzocca, Islamabad, Pakistan Japan Aerospace Exploration Agency Clarkson University, Potsdam, NY; A. (JAXA), Kakuda, Japan Ceruti, University of Bologna, Bologna, Italy; W. Lacarbonara, University of Rome “La Sapienza”, Rome, Italy Monday, 5 January 2015 58-APA-6 Aerodynamic-Structural Dynamics Interaction I Destin 2 Chaired by: J. AZEVEDO and L. UKEILEY, University of Florida 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs AIAA-2015-0249 AIAA-2015-0250 AIAA-2015-0251 AIAA-2015-0252 AIAA-2015-0253 AIAA-2015-0254 AIAA-2015-0255 Aeroelastic Response of a Finite Aeroelastic Response of a Finite Comprehensive Simulation Evaluation On an innovative approach to Static Aeroelastic Predictions for Aerodynamic Performance Fluid Structure Interaction on a Span NACA 0018 Wing Part 1: Span NACA 0018 Wing Part 2: of the AGARD 445.6 Weakened account for gust aerodynamic non- Complex Aircraft Configurations with of Flexible Flapping Wings at Flexible Micro Air Vehicle Experimental Measurements Computational Simulations Model #3 from a Test and Evaluation linearities in an industrial context CFD/CSD Coupling Methodology Bumblebee Scale in Hover Flight J. Chen, N. Qin, University of Sheffield, J. Farnsworth, S. Corbett, J. Seidel, T. C. Fagley, J. Seidel, T. McLaughlin, U.S. Perspective D. Quero-Martin, German Aerospace Center G. Wang, H. Mian, Northwestern Polytechnical M. Sridhar, C. Kang, University of Sheffield, United Kingdom McLaughlin, U.S. Air Force Academy, Air Force Academy, Colorado Springs, CO J. Lechniak, K. Bhamidipati, D. Reasor, U.S. (DLR), Göttingen, Germany; G. Jenaro- University, Xi’an, China; X. Shan, J. Lee, Alabama, Huntsville, Huntsville, AL Colorado Springs, CO Air Force, Edwards AFB, CA; K. Margosian, Rabadan, Airbus, Hamburg, Germany Beijing Aeronautical Science and Technology California State University, Monterey Bay, CA; Research Institute, Beijing, China C. Pasiliao, U.S. Air Force, Eglin AFB, FL Monday, 5 January 2015 59-APA-7 Unsteady Aerodynamics Naples 1 Chaired by: K. VANDEN, USAF and V. BHAGWANDIN, US Army Research Laboratory 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2015-0256 AIAA-2015-0257 AIAA-2015-0258 AIAA-2015-0259 AIAA-2015-0260 AIAA-2015-0261 Numerical Investigation of the Propulsion Theory of Flapping Implications of boundary layer An Attempt to Improve Prediction Reduced-Order Modeling of Unsteady Force and Flow Features Aerodynamics of an Airfoil in Airfoils, Comparison with establishment on convective heat Capability of Transonic Buffet Using Continuous-Time State-Space of Single and Tandem Wheels Mutational Ground Effect Computational Fluid Dynamics transfer experiments URANS Unsteady Aerodynamics S. Spagnolo, X. Zhang, Z. Hu, O. Stalnov, Q. Qu, P. Zuo, W. Wang, P. Liu, Beihang D. Hunsaker, W. Phillips, Utah State J. Saavedra, S. Lavagnoli, G. Paniagua, T. Izumi, Y. Ogino, K. Sawada, Tohoku E. Gillebaart, R. De Breuker, Delft D. Angland, University of Southampton, University, Beijing, China; R. Agarwal, University, Logan, UT von Kármán Institute for Fluid Dynamics, University, Sendai, Japan University of Technology, Delft, The Southampton, United Kingdom Washington University in St. Louis, St. Rhode-Saint-Genèse, Belgium Netherlands

69 Louis, MO Monday, 5 January 2015 60-APA-8 Special Session: Aerodynamic Design Optimization of Benchmark Cases I Naples 2 Chaired by: S. NADARAJAH and S. LEDOUX, Boeing Engineering Operations & Technology 1400 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs Oral Presentation AIAA-2015-0262 AIAA-2015-0263 AIAA-2015-0264 AIAA-2015-0265 A Study Based on the AIAA Aerodynamic Design Optimization Discussion Aerodynamic Shape Optimization Gradient-Based Single and Multi- Multipoint Aerodynamic Shape Application of Physics-Based Surrogate Group Test Cases Using Adjoint Methods of Benchmark Problems Using points Aerodynamic Optimizations Optimization Investigations of the Models to Benchmark Aerodynamic A. Jameson, Stanford University, Stanford, CA; J. Vassberg, The Boeing Company, Long Jetstream with the elsA Software Common Research Model Wing Shape Optimization Problems Beach, CA C. Lee, D. Koo, K. Telidetzki, H. Buckley, M. Meheut, D. Destarac, S. Ben Khelil, G. Kenway, D. Burdette, J. Martins, L. Leifsson, S. Koziel, Y. Tesfahunegn, H. Gagnon, T. Reist, University of Toronto, G. Carrier, A. Dumont, J. Peter, ONERA, University of Michigan, Ann Arbor, Ann Reykjavik University, Reykjavik, Iceland; S. Toronto, Canada; et al. Meudon, France Arbor, MI Hosder, J. Gramanzini, Missouri University of Science and Technology, Rolla, MO Monday, 5 January 2015 61-AS-1 Aerodynamics of Adaptive Structures Osceola Ballroom 6 Chaired by: I. CHOPRA, University of Maryland and M. BALAS, Embry-Riddle Aeronautical University 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs AIAA-2015-0266 AIAA-2015-0267 AIAA-2015-0268 AIAA-2015-0269 AIAA-2015-0270 AIAA-2015-0271 AIAA-2015-0272 Adaptive Vortex Generator Electro-aeromechanical modelling A framework for the aeroelastic Numerical and experimental Adaptive Kagome Lattices for Near Aerodynamic Characterization of Unsteady aerodynamic Structures for the Reduction of and feedback control of actuated analysis and design of generic investigation of aero-structural Wall Turbulence Suppression a Continuous Trailing Edge Flap optimization of the camber of a Turbulent Separation membrane wings morphing wings characteristics and performance of J. Bird, M. Santer, J. Morrison, Imperial Design morphing airfoil for rotorcraft M. Garland, M. Santer, J. Morrison, S. Buoso, R. Palacios, Imperial College N. Werter, R. De Breuker, Delft University distributed compliance morphing College London, London, United Kingdom T. Mapes, M. Agate, NASA Langley blades Imperial College London, London, United London, London, United Kingdom of Technology, Delft, The Netherlands wings Research Center, Hampton, VA A. Cortesi, F. Fusi, G. Quaranta, Technical Kingdom G. Molinari, A. Arrieta, P. Ermanni, Swiss University of Milan, Milan, Italy Federal Institute of Technology, Zürich, Switzerland Monday, 5 January 2015 62-FD-7 Boundary Layer Transition: Roughness and 3D Flow Effects Tallahassee 1 Chaired by: B. WHEATON, The Johns Hopkins University Applied Physics Laboratory and K. CASPER, Sandia National Laboratories 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs AIAA-2015-0273 AIAA-2015-0274 AIAA-2015-0275 AIAA-2015-0276 AIAA-2015-0277 AIAA-2015-0278 AIAA-2015-0279 The Interaction of a Backward-Facing Direct Numerical Simulation of A Study of the Impact of Wide- Pressure Gradient Effect on Experimental Investigation of the Freestream Effects on Boundary Analysis of Crossflow Instability on Step and Crossflow Instabilities in Roughness-Induced Transition in Range Roughness Elements on Boundary Layers over Surface Effect of Wall Suction on Cross-Flow Layer Disturbances for HIFiRE-5 HIFiRE-5 using Direct Numerical Boundary-Layer Transition the VKI Mach 6 Tunnel Gortler Instabilities Excrescences: Parametric Study Absolute Instability in a Rotating M. Borg, R. Kimmel, Air Force Research Simulation J. Eppink, NASA Langley Research Center, R. Chaudhry, P. Subbareddy, I. Nompelis, A. Sescu, R. Pendyala, J. Haywood, J. Haywood, A. Sescu, Mississippi State Disk Boundary Layer Laboratory, Wright-Patterson AFB, OH; D. Dinzl, G. Candler, University of Hampton, VA; R. Wlezien, Iowa State G. Candler, University of Minnesota, Mississippi State University, Mississippi University, Mississippi State, MS; M. J. Ho, T. Corke, E. Matlis, University of J. Hofferth, R. Bowersox, Texas A&M Minnesota, Twin Cities, Minneapolis, MN University, Ames, IA; R. King, M. Choudhari, Minneapolis, Minneapolis, MN State, MS; M. Visbal, Air Force Research Visbal, Air Force Research Laboratory, Notre Dame, Notre Dame, IN University, College Station, TX; C. Mai, NASA Langley Research Center, Hampton, VA Laboratory, Wright-Patterson AFB, OH Wright-Patterson AFB, OH United States Air Force, Eglin AFB, FL Monday, 5 January 2015 63-FD-8 CFD Methods II Sanibel 1 Chaired by: H. LUO, Vanderbilt University and R. DAVIS, University of California Davis 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs AIAA-2015-0280 AIAA-2015-0281 AIAA-2015-0282 AIAA-2015-0283 AIAA-2015-0284 AIAA-2015-0285 AIAA-2015-0286 Computation of the Tangent-Linear Structural Dynamics Solution hp-adaptive time integration for A Tensor Decomposition Method for Comparison of Artificial Dissipation On The Extension of SLAU Scheme CFD for prediction of flow Solution for LCO-Converged Procedure for Multi-Discipline ALE simulation of Fluid-Structure High Dimensional Fokker-Planck and Filtering Schemes for Time- to Compressible Two-Fluid Models separation on aircraft tail surfaces Nonlinear Flows Fluid/Structure/Thermal Interaction problems Equation Modeling Polymeric Accurate Simulations Z. Hosseinzadeh-Nik, J. Regele, A. A. Masi, University of Cambridge, S. Xu, J. Hückelheim, M. Gugala, J. Simulation A. Hay, S. Etienne, D. Pelletier, A. Liquids A. Edoh, A. Karagozian, University of Passalaqua, Iowa State University, Cambridge, United Kingdom; J. Benton, Müller, Queen Mary University of London, J. Zorn, R. Davis, University of California, Garon, École Polytechnique de Montréal, Y. Sun, M. Kumar, University of Florida, California, Los Angeles, Los Angeles, Ames, IA Airbus, Bristol, United Kingdom; P. Tucker, London, United Kingdom Davis, Davis, CA Montréal, Canada Gainesville, Gainesville, FL CA; C. Merkle, Purdue University, West University of Cambridge, Cambridge, Lafayette, IN United Kingdom 70 Monday, 5 January 2015 64-FD-9 Experimental and Numerical Investigations of Blunt Leading Edge Separation for a 53 Degree Swept Diamond Wing (STO AVT-183) II (Invited) Sanibel 2 Chaired by: A. RIZZI, KTH Royal Institute Technology and J. LUCKRING, NASA-Langley Research Center 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2015-0287 AIAA-2015-0288 AIAA-2015-0289 AIAA-2015-0290 AIAA-2015-0291 AIAA-2015-0292 Applicability of Hybrid RANS/LES Numerical Analysis of Incipient Vortex Development on the AVT-183 Numerical study of blunt leading edge CFD Study of Vortex Separation Vortical Flow Prediction of the Models in Predicting Separation Onset Separation on 53-Deg Swept Diamond Wing Configuration - separation on a 53 degree swept Phenomena on Blunt Diamond AVT-183 Diamond Wing of the AVT-183 Diamond Wing Diamond Wing Numerical and Experimental Findings diamond wing (STO AVT-183) using Wing M. Ghoreyshi, K. Ryszka, R. Cummings, D. Reasor, 412th Test Wing, Edwards AFB, CA; N. Frink, NASA Langley Research Center, S. Hitzel, Airbus, Manching, Germany; O. the Edge and Cobalt flow solvers M. Tomac, A. Rizzi, Royal Institute of A. Lofthouse, U.S. Air Force Academy, D. Malloy, Arnold Engineering Development Hampton, VA Boelens, National Aerospace Laboratory H. Edefur, M. Tormalm, Swedish Defense Technology (KTH), Stockholm, Sweden Colorado Springs, CO Complex, Arnold AFB, TN; D. Daniel, (NLR), Amsterdam, The Netherlands; A. Research Agency (FOI), Stockholm, Sweden; Aerospace Testing Alliance, Arnold AFB, TN Hövelmann, Technical University of Munich, R. Nangia, Self, Bristol, United Kingdom Garching, Germany Monday, 5 January 2015 65-FD-10 High-Order Methods I Daytona 1 Chaired by: C. LIANG, George Washington University and X. GAO, Colorado State Univ 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2015-0293 AIAA-2015-0294 AIAA-2015-0295 AIAA-2015-0296 AIAA-2015-0297 AIAA-2015-0298 Results and Conclusions of the Higher-Order Methods for Implementation of Turbulence Hybrid Spectral Difference/ A High-Order Finite-Volume Method A Fourth-Order Scheme for the European Project IDIHOM on Compressible Turbulent Flows Using Models to High-Order Spectral Embedded MPWENO Method for for Compressible Flows on Moving Compressible Navier-Stokes High-Order Methods for Industrial Entropy Variables Difference Method Conservation Laws Tetrahedral Grids Equations Aerodynamic Applications L. Diosady, S. Murman, NASA Ames H. Fan, J. Gao, Beihang University, J. Choi, University of Maryland, College M. Charest, T. Canfield, N. Morgan, J. X. Gao, S. Guzik, Colorado State N. Kroll, T. Leicht, C. Hirsch, F. Bassi, C. Research Center, Moffett Field, CA Beijing, China Park, College Park, MD Waltz, J. Wohlbier, Los Alamos National University, Fort Collins, CO Johnston, K. Sorensen, German Aerospace Laboratory, Los Alamos, NM Center (DLR), Braunschweig, Germany; et al. Monday, 5 January 2015 66-FD-11 Jet Flows and Control Daytona 2 Chaired by: D. GAITONDE, The Ohio State University and C. PASCHEREIT, Technical University of Berlin 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2015-0299 AIAA-2015-0300 AIAA-2015-0301 AIAA-2015-0302 AIAA-2015-0303 AIAA-2015-0304 Active Control of Mach 0.9 Jet LES Simulation of Forced High- Contrasting Modal Decompositions of The influence of the inner shear Effects of Shear Layer Manipulation Measurement and Prediction of Using High Frequency Excitation Speed Jet Flow Fields with & without Control layer on the suppression of the on Noise Emissions of a Turbulent Hot Streak Profiles Generated by P. Upadhyay, T. Davis, F. Alvi, Florida State J. Kim, BOOLTS Simulation Systems, D. Gonzalez, Naval Surface Warfare global mode in heated swirling jets Jet Flame Axially Opposed Dilution Jets University, Tallahassee, FL Seoul, South Korea Center, Indian Head, MD; A. Mohan, D. L. Rukes, M. Sieber, K. Oberleithner, C. H. Nawroth, C. Paschereit, Technical R. Prenter, A. Ameri, J. Bons, Ohio State Gaitonde, Ohio State University, Columbus, Nayeri, C. Paschereit, Technical University University of Berlin, Berlin, Germany University, Columbus, OH OH; M. Lewis, Science and Technology of Berlin, Berlin, Germany Policy Institute, Washington, DC Monday, 5 January 2015 67-FD-12/PDL-1 Plasma Flow Control Sun Ballroom A Chaired by: D. RIZZETTA, USAF and T. MCLAUGHLIN, US Air Force Academy 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2015-0305 AIAA-2015-0306 AIAA-2015-0307 AIAA-2015-0308 AIAA-2015-0309 AIAA-2015-0310 Plasma-Based Control of Transition Numerical Investigation on the Design Exploration of a DBD LES of Separated-flow Controlled Parametric investigation on plasma Active flow control by means of on a Wing with Leading-Edge Efficiency of a Plasma Actuator for Plasma Actuator for Massive by DBD Plasma Actuator around streamwise vortex generators with MHD plasma actuator on a NACA Excrescence Turbine Applications Separation Control NACA 0015 over Reynolds Number flow around the bluff body 23012 Airfoil Model D. Rizzetta, M. Visbal, Air Force Research G. Bell, H. Ogawa, S. Watkins, RMIT T. Watanabe, H. Aono, T. Tatsukawa, T. Range of 10^4-10^6 J. Yoon, J. Han, Korea Advanced Institute I. Moralev, V. Bityurin, A. Klimov, P. Laboratory, Wright-Patterson AFB, OH University, Melbourne, Australia Nonomura, A. Oyama, K. Fujii, Japan M. Sato, Japan Aerospace Exploration of Science and Technology, Daejeon, Kazanskiy, Russian Academy of Sciences, Aerospace Exploration Agency (JAXA), Agency (JAXA), Kanagawa, Japan; South Korea Moscow, Russia Sagamihara, Japan K. Okada, Ryoyu Systems Company,

71 Ltd., Nagoya, Japan; H. Aono, Japan Aerospace Exploration Agency (JAXA), Kanagawa, Japan; K. Asada, University of Tokyo, Kanagawa, Japan; A. Yakeno, T. Nonomura, Japan Aerospace Exploration Agency (JAXA), Kanagawa, Japan; et al. Monday, 5 January 2015 68-FD-13 RANS/LES Applications Sanibel 3 Chaired by: N. GEORGIADIS, NASA Glenn Research Center and J. AHMAD, NASA 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs AIAA-2015-0311 AIAA-2015-0312 AIAA-2015-0313 AIAA-2015-0314 AIAA-2015-0315 AIAA-2015-0316 AIAA-2015-0317 RANS and LES/RANS Simulations of Use of Symbolic Regression for OpenFOAM Simulations of Evaluation of Industry Flow Past Tandem Circular Cylinders Revisiting Turbulence Model Validation Numerical Accuracy in RANS Flow Over an Dynamically Pitching construction of Reynolds-stress Atmospheric-Entry Capsules in the Standard Turbulence Models at High Reynolds Numbers using for High-Mach Number Axisymmetric Computations of High-Lift Naca0012 Airfoil damping functions for Hybrid Subsonic Regime on an Axisymmetric Supersonic Overset Grids in OpenFOAM Compression Corner Flows Multi-element Airfoil and Aicraft J. Ke, J. Edwards, North Carolina State RANS/LES B. Nikaido, Science and Technology Compression Corner H. Gopalan, Union College, Schenectady, N. Georgiadis, NASA Glenn Research Center, Configurations University, Raleigh, NC J. Weatheritt, R. Sandberg, University Corporation, Moffett Field, CA; S. Murman, J. DeBonis, NASA Glenn Research Center, NY; R. Jaiman, National University of Cleveland, OH; C. Rumsey, NASA Langley D. Drikakis, P. Tsoutsanis, A. Antoniadis, of Southampton, Southampton, United J. Garcia, NASA Ames Research Center, Cleveland, OH Singapore, Singapore, Singapore; D. Research Center, Hampton, VA; G. Huang, Cranfield University, Cranfield, United Kingdom Moffett Field, CA Chandar, Agency for Science, Technology Wright State University, Dayton, OH Kingdom and Research, Singapore, Singapore Monday, 5 January 2015 69-GEPC-2 Status/Progress of Environmentally Responsible Aviation Project Sun Ballroom C Chaired by: F. COLLIER, NASA-Langley Research Center and G. BEZOS O’CONNOR, NASA Langley Research Center 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs Oral Presentation Oral Presentation Oral Presentation Oral Presentation Panel Discussion Status of ERA Airframe Technology Environmentally Responsible Status of ERA Vehicle System Assessment of System Level Technical Demonstrators Aviation: Status of Propulsion Integration Technology Demonstrators Performance and Impact of NASA’s P. Davis, D. Jegley, NASA Langley Technology Demonstrators J. Flamm, H. Fernandez, M. Khorrami, NASA Environmentally Responsible Aviation Research Center, Hampton, VA; T. Rigney, K. Suder, D. Van Zante, M. Celestina, C. Langley Research Center, Hampton, VA; K. (ERA) Project’s Integrated Technology NASA Armstrong Flight Research Center, Hughes, C. Lee, NASA Glenn Research James, NASA Ames Research Center, Moffett Demonstrations (ITDs) Edwards, CA Center, Cleveland, OH Field, CA; R. Thomas, NASA Langley Research C. Nickol, NASA Langley Research Center, Center, Hampton, VA Hampton, VA Monday, 5 January 2015 70-GNC-6 Aerospace Robotics and Autonomous/Unmanned Systems II Sun Ballroom 3 Chaired by: J. SASIADEK, Carleton University and D. PEREZ 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2015-0318 AIAA-2015-0319 AIAA-2015-0320 AIAA-2015-0321 AIAA-2015-0322 AIAA-2015-0323 CubeSat Autonomous Rendezvous Optimal Power Descent Guidance Dynamics and Control of Flexible Long-range Navigation using Solar Methods for Modeling Tensegrity M-MRAC for SPHERES Simulation with 6-DoF Line of Sight Constraints Manipulators Using Variable-Speed Panels Characteristics and Angle- Dynamics in LEO V. Stepanyan, University of California, E. Lightsey, A. Fear, University of Texas, via Unit Dual Quaternions Control Moment Gyros of-Arrival for Planetary Rover M. Rye, C. Sultan, Virginia Polytechnic Santa Cruz, Santa Cruz, CA; J. Barlow, Austin, Austin, TX U. Lee, M. Mesbahi, University of Q. Hu, Beijing Institute of Technology, Cooperating with Landers Institute and State University, Blacksburg, Stinger Ghaffarian Technologies, Inc., Washington, Seattle, Seattle, WA Beijing, China; Z. Wang, Beihang T. Ishida, M. Takahashi, Keio University, VA Moffett Field, CA; K. Krishnakumar, NASA University, Beijing, China; J. Zhang, Beijing Yokohama, Japan Ames Research Center, Moffett Field, CA Institute of Technology, Beijing, China 72 Monday, 5 January 2015 71-GNC-7 Lander Technology Development at NASA I Miami 1 Chaired by: J. CARSON, NASA Jet Propulsion Laboratory and E. ROBERTSON, NASA Johnson Space Center 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs AIAA-2015-0324 AIAA-2015-0325 AIAA-2015-0326 AIAA-2015-0327 AIAA-2015-0328 AIAA-2015-0329 AIAA-2015-0330 Developing Autonomous Precision Interfacing and Verifying ALHAT Flight testing a Real-Time Hazard Simulations of the Hazard Lidar Sensor Performance in Closed- Advancing Lidar Sensors Morpheus Lander Roll Control Landing and Hazard Avoidance Safe Precision Landing Systems Detection System for Safe Lunar Detection System for Approach Loop Flight Testing of the Morpheus Technologies for Next Generation System and Wind Modeling Technology from Concepts with the Morpheus Vehicle Landing on the Rocket-Powered Trajectories of the Morpheus Lunar Rocket-Propelled Lander to a Lunar- Landing Missions E. Gambone, NASA Johnson Space Center, through Terrestrially Flight-Tested J. Carson, R. Hirsh, J. Busa, NASA Morpheus Vehicle Lander Like Hazard Field F. Amzajerdian, NASA Langley Research Houston, TX Prototypes Johnson Space Center, Houston, TX; C. N. Trawny, A. Huertas, M. Luna, C. M. Luna, A. Huertas, N. Trawny, C. V. Roback, NASA Langley Research Center, Center, Hampton, VA; D. Pierrottet, C. Epp, E. Robertson, J. Carson, NASA Villalpando, K. Martin, N. Trawny, Jet Villalpando, K. Martin, J. Carson, Jet Villalpando, K. Martin, W. Wilson, Jet Hampton, VA; D. Pierrottet, Coherent Coherent Applications, Inc., Hampton, VA; Johnson Space Center, Houston, TX Propulsion Laboratory, California Institute Propulsion Laboratory, California Institute Propulsion Laboratory, California Institute Applications, Inc., Hampton, VA; F. G. Hines, V. Roback, L. Petway, B. Barnes, of Technology, Pasadena, CA; et al. of Technology, Pasadena, CA; et al. of Technology, Pasadena, CA; et al. Amzajerdian, B. Barnes, NASA Langley NASA Langley Research Center, Hampton, Research Center, Hampton, VA; A. Bulyshev, VA; et al. Analytical Mechanics Associates, Inc., Hampton, VA; G. Hines, NASA Langley Research Center, Hampton, VA; et al. Monday, 5 January 2015 72-GNC-8 GNC Sensor Systems II Sun Ballroom 4 Chaired by: S. STARIN, NASA-Goddard Space Flight Center and T. LIM, US Naval Academy 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2015-0331 AIAA-2015-0332 AIAA-2015-0333 AIAA-2015-0334 AIAA-2015-0335 AIAA-2015-0336 A New Method for Calibrating an Design and Development of a Laser Feature Detection for Pose Tool for Optimizing Star Tracker Improvement of Infrared Horizon LIRIS demonstrator on ATV5: a Angular Accelerometer Using a Fine Pointing Sensor Estimation and IMU Configuration Detector Using Two-dimensional step beyond for European non High-Precision Calibration Table F. Ales, P. Gath, U. Johann, Airbus, T. Lim, M. ODowd, P. Ramos, U.S. Naval E. Hariton, A. Swank, NASA Glenn Infrared Temperature Distribution cooperative navigation system D. Jatiningrum, P. Lu, C. de Visser, Q. Chu, Friedrichshafen, Germany; O. Mandel, Academy, Annapolis, MD Research Center, Cleveland, OH Model B. Cavrois, A. Vergnol, A. Donnard, P. M. Mulder, Delft University of Technology, Karlsruhe Institute of Technology, L. Xu, H. Chen, Tsinghua University, Casiez, Airbus Defence and Space, Les Delft, The Netherlands Karlsruhe, Germany; C. Braxmaier, Beijing, China Mureaux, France; O. Mongrard, ESA, University of Bremen, Bremen, Germany Noordwijk, The Netherlands Monday, 5 January 2015 73-GNC-9 Missile Guidance II Sun Ballroom 6 Chaired by: M. IDAN, Technion - Israel Institute of Technology and A. VANDERWYST, Raytheon Missile Systems 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs AIAA-2015-0337 AIAA-2015-0338 AIAA-2015-0339 AIAA-2015-0340 AIAA-2015-0341 Cooperative Aircraft Defense from an Bounded Differential Game Lateral Interception of Optimal Paths for Lateral An SDRE Based Differential Game Attacking Missile using Proportional Guidance Law with Dual Control Maneuvering Targets Using Dubins Interception of Moving Targets Approach for Maneuvering Target Navigation Systems for Agile Missiles Paths using a Dubins Approach Interception E. Garcia, D. Casbeer, Air Force Research D. Taur, Chungshan Institute of Science G. Akhil. Ratnoo, D. Ghose, Indian Institute G. Akhil, A. Ratnoo, D. Ghose, Indian R. Bardhan, D. Ghose, Indian Institute of Laboratory, Wright-Patterson AFB, OH; K. and Technology, Taipei, Taiwan of Science, Bangalore, India Institute of Science, Bangalore, India Science, Bangalore, India Pham, Air Force Research Laboratory, Kirtland AFB, NM; M. Pachter, Air Force Institute of

73 Technology, Wright-Patterson AFB, OH Monday, 5 January 2015 74-GNC-10 Novel Navigation, Estimation, and Tracking Methods II Sun Ballroom 5 Chaired by: N. AHMED, CNRS & Université Paris-Sud and M. KUMAR, University of Florida 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2015-0342 AIAA-2015-0343 AIAA-2015-0344 AIAA-2015-0345 AIAA-2015-0346 AIAA-2015-0347 Automated 3D Digital A Novel IEG Strategy for Realistically Line of Sight Rate Estimation for Calibration of Atmospheric Density Position Based Visual Servoing in Multiple UAV Target Tracking Using Reconstruction of Fiber Reinforced Modeled Seeker-less Interceptors Guided Projectiles with Strapdown Model Using Orbital Data of an Indoor Simulation Platform Consensus-Based Distributed High Polymer Composites S. Gour, D. Ghose, Indian Institute of Science, Seekers Multiple Satellites H. Zhu, H. Liu, University of Toronto, Degree Cubature Information Filter W. Whitacre, Draper Laboratory, Bangalore, India; V. Aki, Defence Research & J. Maley, Army Research Laboratory, Y. Ren, J. Shan, York University, Toronto, Toronto, Canada T. Sun, M. Xin, University of Missouri, Cambridge, MA; M. Czabaj, NASA Langley Development Organisation, Bangalore, India Aberdeen Proving Ground, MD Canada Columbia, Columbia, MO Research Center, Hampton, VA Monday, 5 January 2015 75-GTE-2 Film Cooling Emerald 1 Chaired by: S. SUBRAMANIAN, QuEST Global, Inc. 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs AIAA-2015-0348 AIAA-2015-0349 AIAA-2015-0350 AIAA-2015-0351 AIAA-2015-0352 Development of Novel Internal Experimental and Numerical Study Effects of Hole Conﬁguration, Surface Rib Shape Effects on Heat Transfer An Experimental Study of Cooling Geometry for Gas Turbine of Deposition in Pin Fin Arrays with Curvature, and Mach Number on Film Performance in Internal Cooling Compressibility Effects on the Film Blades Impingement Cooling Jets Cooling in Fuel Rich Environments Passages Cooling Effectiveness Using PSP I. Ranade, E. Guillen, D. Bystry-Wells, J. D. Zagnoli, R. Prenter, A. Ameri, J. Bons, A. Lynch, A. Shewhart, M. Polanka, J. Y. Dai, J. Tyacke, P. Tucker, University of and PIV Techniques Gutierrez, Y. Mehta, A. Dias dos Santos, Ohio State University, Columbus, OH Rutledge, Air Force Institute of Technology, Cambridge, Cambridge, United Kingdom H. Hu, W. Zhou, B. Johnson, Iowa State Embry-Riddle Aeronautical University, Wright-Patterson AFB, OH University, Ames, IA Daytona Beach, FL; et al. Monday, 5 January 2015 76-HSABP-2 Premixed High Speed Combustion (Invited) Emerald 8 Chaired by: J. MCDANIEL, University of Virginia and C. GOYNE, University of Virginia 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs AIAA-2015-0353 Oral Presentation AIAA-2015-0354 Oral Presentation AIAA-2015-0355 AIAA-2015-0356 AIAA-2015-0357 Development of a Premixed Thermal and Chemical Kinetic Nitric Oxide PLIF Visualization of Coherent Anti-Stokes Raman Velocimetry Using Graphite Tracer Large Eddy Simulation of Direct Measurement of Combustion Combustion Capability for Dual-Mode Analysis of a High-speed Reacting Simulated Fuel-Air Mixing in a Spectroscopy (CARS) in a Dual- Particles in a Scramjet Flowpath High-Speed, Premixed Ethylene Efﬁciency of a Dual-Mode Scramjet Scramjet Experiments (Invited) Flow in a Variable Area Duct Dual-Mode Scramjet (Invited) Mode Scramjet with Premixed (Invited) Combustion (Invited) via TDLAT and SPIV (Invited) R. Rockwell, C. Goyne, H. Chelliah, J. (Invited) L. Cantu, E. Gallo, A. Cutler, George Fueling (Invited) J. Kirik, C. Goyne, J. McDaniel, R. K. Ramesh, J. Edwards, North Carolina K. Busa, B. Rice, J. McDaniel, C. Goyne, McDaniel, University of Virginia, Charlottesville, M. Rahimi, H. Chelliah, University of Washington University, Hampton, VA; B. E. Gallo, L. Cantu, A. Cutler, George Rockwell, R. Johnson, H. Chelliah, State University, Raleigh, NC; C. Goyne, R. Rockwell, University of Virginia, Charlottesville, VA; J. Edwards, North Carolina Virginia, Charlottesville, Charlottesville, VA Bathel, P. Danehy, NASA Langley Research Washington University, Hampton, VA; P. University of Virginia, Charlottesville, J. McDaniel, University of Virginia, Charlottesville, Charlottesville, VA; J. State University, Raleigh, NC; A. Cutler, George Center, Hampton, VA; R. Rockwell, Danehy, NASA Langley Research Center, Charlottesville, VA Charlottesville, Charlottesville, VA Edwards, North Carolina State University, Washington University, Hampton, VA; et al. University of Virginia, Charlottesville, Hampton, VA; R. Rockwell, C. Goyne, Raleigh, NC Charlottesville, VA; et al. University of Virginia, Charlottesville, Charlottesville, VA; et al. Monday, 5 January 2015 77-IS-3 Intelligent Collaborative Control of Multi-Agent Systems Osceola Ballroom 2 Chaired by: K. KOCHERSBERGER, Virginia Polytechnic Institute and State University and A. YUCEL, Lockheed Martin Aeronautics 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs AIAA-2015-0358 AIAA-2015-0359 AIAA-2015-0360 AIAA-2015-0361 AIAA-2015-0362 Decentralized Message Passing for Coordinating Groups of Sensing Sensor Resource Management to An Intelligent, Heuristic Path Intelligent Water Drops Algorithm for Minimum Sensor Cover Based on Platforms in Dynamic, Uncertain Support UAS Integration into the Planner for Multiple Agent Coordinating Activities Between Cluster Belief Propagation Environments National Airspace System Unmanned Air Systems Spacecraft in a Communications- D. Jang, H. Choi, Korea Advanced Institute I. Sledge, K. Mohseni, University of N. Hanlon, K. Cohen, E. Kivelevitch, C. Crispin, A. Sobester, University of Denied Environment

74 of Science and Technology, Daejeon, Florida, Gainesville, Gainesville, FL University of Cincinnati, Cincinnati, OH Southampton, Southampton, United J. Straub, University of North Dakota, South Korea Kingdom Grand Forks, Grand Forks, ND Monday, 5 January 2015 78-IS-4 Making Aerospace Operations Intelligent Osceola Ballroom 1 Chaired by: C. BOWMAN, Novira Therapeutics 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs AIAA-2015-0363 AIAA-2015-0364 AIAA-2015-0365 AIAA-2015-0366 AIAA-2015-0367 AIAA-2015-0368 AIAA-2015-0369 Surveillance for Intelligent Emergency Multiobjective Design Exploration Abnormal Orbital Event Detection, GPS Scintillation Outage Prediction Helicopter Mission Assignment in A Scented Receding Horizon A Cascading Fuzzy Logic Controller Response Robotic Aircraft (SIERRA)- of a Many-objective Space Characterization, and Prediction C. Bowman, Data Fusion & Neural Disaster Relief Based on Particle Approach to the Mars Surveyor to the Mars Surveyor Competition VTOL Aircraft for Emergency Response Trajectory Problem for Low-Thrust C. Bowman, Data Fusion & Neural Networks, Broomfield, CO Swarm Optimization Competition A. Stubblebine, S. Higgins, T. Deshpande, B. Brown, W. Wei, University of Cincinnati, Spacecraft Using MOEA with Large Networks, Broomfield, CO A. Andreeva-Mori, K. Kobayashi, M. S. Higgins, A. Stubblebine, T. Deshpande, E. Kivelevitch, University of Cincinnati, Cincinnati, OH; R. Ozburn, West Virginia Populations Shindo, Japan Aerospace Exploration E. Kivelevitch, University of Cincinnati, Cincinnati, OH Division of Forestry, Farmington, WV; M. T. Tatsukawa, T. Watanabe, A. Oyama, K. Agency (JAXA), Tokyo, Japan Cincinnati, OH Kumar, University of Toledo, Toledo, OH; K. Fujii, Japan Aerospace Exploration Agency Cohen, University of Cincinnati, Cincinnati, OH (JAXA), Sagamihara, Japan Monday, 5 January 2015 79-ISC-2 International Student Conference (Masters Category) St. George 112 Chaired by: J. CORBETS 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs AIAA-2015-0370 AIAA-2015-0371 AIAA-2015-0372 AIAA-2015-0373 AIAA-2015-0374 AIAA-2015-0375 AIAA-2015-0376 Characterization of Rotor Wake in Comparison of Numerical Methods Complex Lamellar Helical Solution Particle In Cell (PIC) Algorithm Aerial Deployed Unfolding Ground Testing of Active Thermal Theoretical and Numerical Approaches Ground Effect to Determine the Effect of Non- for Cyclonically Driven Hybrid Advancement for Plasma Modelling Autonomous Glider System Tiles for Impact Load Identification on an G. Perrotta, University of Maryland, Equilibrium in Flows from the Rocket Engines of an Ion Thruster Discharge A. Smith, University of Nevada, Reno, R. Delaney, H. Dumm, University of New Aerospace Structure Correlation with College Park, College Park, MD Laminar to Turbulent Regime J. Fleischmann, J. Majdalani, Auburn Chamber Reno, NV Mexico, Albuquerque, Albuquerque, NM Experimental Data R. Bosworth, University of Colorado, University, Auburn, AL T. Godar, J. Menart, Wright State G. Fabbi, University of Rome “La Colorado Springs, Colorado Springs, CO University, Dayton, OH Sapienza”, Rome, Italy Monday, 5 January 2015 80-ISC-3 International Student Conference (Team Category) St. George 114 Chaired by: L. HANSEN, HRP Systems, Inc. 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2015-0377 AIAA-2015-0378 AIAA-2015-0379 AIAA-2015-0380 AIAA-2015-0381 AIAA-2015-0382 Experimental and Computational Analysis of Different Design Estimating Landing and Take-off Passive Turbulence Generating Grid L-Dominance: A New Mechanism Design of a Cost Effective Thrust Investigation of a Dual-Bell Nozzle Strategies to Improve Single Blade Cycle Parameters Using MATLAB Arrangements in a Turbine Cascade Combining ε-Dominance and Pareto Stand for Introducing Thrust and K. Davis, E. Fortner, M. Heard, H. Performance in Rotorcrafts J. Varney, P. Motevalli, D. Katsaduros, M. Wind Tunnel Knee Exploitation in Evolutionary Impulse McCallum, H. Putzke, Worcester L. Gilkey, C. Echavarria, S. Gomez, Prall, M. Johnson, Purdue University, West C. Wiese, M. McClearn, G. Allevato, K. Multi-objective Optimization E. Hopping, M. Murdy, N. Stepp, Polytechnic Institute, Worcester, MA University of New Mexico, Albuquerque, Lafayette, IN Rouser, U.S. Air Force Academy, Colorado B. Hancock, T. Nysetvold, C. Mattson, University of Alabama, Huntsville, Albuquerque, NM Springs, CO Brigham Young University, Provo, UT Huntsville, AL Monday, 5 January 2015 81-LEC-2 Non-Deterministic Approaches Lecture: The Building Block Approach in the 21st Century - The Role of ICME & UQ Osceola Ballroom A 1400 - 1500 hrs Chaired by: E. TUEGEL, USAF and M. RUMPFKEIL, University of Dayton Rolland Dutton Chief, Manufacturing and Industrial Technologies Division AFRL/RXM, Wright-Patterson AFB Monday, 5 January 2015 82-MAT-3 ICME Applications - Residual Stress Modeling and Measurement Sarasota 1 Chaired by: J. MATLIK, Rolls-Royce Corp and V. VENKATESH 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs 75 AIAA-2015-0383 AIAA-2015-0384 AIAA-2015-0385 AIAA-2015-0386 AIAA-2015-0387 AIAA-2015-0388 AIAA-2015-0389 Uncertainty Quantification in Residual Stress Modeling and Probabilistic Modeling of Bulk The Impact of Forging Residual Residual Stress Measurements Repeatability of Residual Stress The Effect of Stochastically Varying ICMSE: Application to Metal Alloys Uncertainty Quantification Residual Stresses Stress on Fatigue in Aluminum for Model Validation As Applied Measurements Creep Parameters on Residual Stresses G. Cai, S. Mahadevan, Vanderbilt R. Shankar, W. Wu, J. Yang, J. Oh, J. McFarland, V. Bhamidipati, R. McClung, D. Ball, Lockheed Martin Corporation, Fort in the United States Air Force A. DeWald, Hill Engineering, LLC, Rancho in Ceramic Matrix Composites University, Nashville, TN Scientific Forming Technologies Southwest Research Institute, San Worth, TX; M. James, R. Bucci, J. Watton, Foundational Engineering Problem Cordova, CA E. Pineda, B. Bednarcyk, NASA Glenn Corporation, Columbus, OH Antonio, TX; M. James, J. Watton, Alcoa Alcoa Technical Center, Alcoa Center, PA; Program on ICME of Bulk Residual Research Center, Cleveland, OH; S. Mital, Technical Center, Alcoa Center, PA; M. Hill, A. DeWald, M. Hill, Hill Engineering, LLC, Stress in Ni Rotors University of Toledo, Toledo, OH; S. Arnold, Hill Engineering, LLC, Rancho Cordova, Rancho Cordova, CA; et al. C. Iuliana, V. Venkatesh, Pratt & Whitney, NASA Glenn Research Center, Cleveland, OH CA; et al. East Hartford, CT Monday, 5 January 2015 83-MAT-4 Multi-Scale Modeling of Materials Sarasota 2 Chaired by: S. ROY, The University of Alabama and G. SEIDEL, Virginia Polytechnic Institute and State Universit 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2015-0390 AIAA-2015-0391 AIAA-2015-0392 AIAA-2015-0393 AIAA-2015-0394 AIAA-2015-0395 A Multiscale Model Coupling Prediction of Progressive Damage A Micromechanics Approach to Concurrent Multiscale Modeling A Micromechanical Approach to Effect of Material Variability Molecular Dynamics Simulations and at the Fiber/Matrix Scale Using Homogenizing Damageable of Coupling between Continuum Imperfect Interface Analysis of on Progressive Damage and Micromechanics to Study the Behavior Cohesive Zone Elements Elastoplastic Heterogeneous Damage and Piezoresistivity in Heterogeneous Materials Micromechanics of Composite of CNT-Enhanced Nanocomposites M. Ballard, J. Whitcomb, Texas A&M Materials CNT-Polymer Nanocomposites H. Sertse, W. Yu, Purdue University, West Materials N. Subramanian, A. Rai, S. Datta, B. Koo, University, College Station, TX L. Zhang, W. Yu, Purdue University, West X. Ren, G. Seidel, Virginia Polytechnic Lafayette, IN J. Johnston, C. Heitland, A. A. Chattopadhyay, Arizona State University, Lafayette, IN Institute and State University, Blacksburg, Chattopadhyay, Arizona State University, Tempe, AZ VA Tempe, AZ Monday, 5 January 2015 84-MDO-3 MDO: Wing Design Applications Sarasota 3 Chaired by: T. TAKAHASHI, Arizona State University and F. ENGELSEN, The Boeing Company 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs AIAA-2015-0396 AIAA-2015-0397 AIAA-2015-0398 AIAA-2015-0399 AIAA-2015-0400 Self-Designing Parametric Design Implications of Elliptical Adaptive Shape Control for Beyond Quasi-Analytical Methods Airfoil Optimization Based on Rapid Geometries Planform Wings Aerodynamic Design for Preliminary Structural Sizing and Transition Prediction A. Sobester, University of Southampton, D. Dulin, T. Takahashi, Arizona State G. Anderson, Stanford University, Stanford, Weight Estimation of Lifting Surfaces X. Wang, J. Cai, C. Liu, Z. Hu, Southampton, United Kingdom University, Tempe, AZ CA; M. Aftosmis, NASA Ames Research A. Elham, Delft University of Technology, Delft, Northwestern Polytechnical University, Center, Moffett Field, CA The Netherlands; M. van Tooren, University of Xi’an, China South Carolina, Columbia, Columbia, SC Monday, 5 January 2015 85-MST-4 Modeling of Space Systems and Dynamics Sun Ballroom 2 Chaired by: D. CARTMELL, Boeing Engineering Operations & Technology and B. BIRKMIRE, Air Force Research Laboratory 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2015-0401 AIAA-2015-0402 AIAA-2015-0403 AIAA-2015-0404 AIAA-2015-0405 AIAA-2015-0406 A New Approach to Simulating the Design of a Programmable Star Formation Flying Constant Low- Using the DIMMACSS-PSG Modeling and Design of a A Framework for Calibrating Trajectory of Solar Sail Spacecraft Tracker-Based Reference System thrust Control Model Based on Intelligent Robotic Middleware to Communication and Navigation Angular Accelerometers using a Using the Finite Element Method for a Simulated Spacecraft Relative Orbit Elements Control Real-World and Simulated Satellite Constellation for the Lunar Motion Simulator A. Karwas, R. Taghavi, University of W. Grunwald, E. Swenson, Air Force X. Wang, Y. Rao, C. Han, Y. Shi, Beihang Multi-Agent Systems South Pole D. Jatiningrum, C. de Visser, M. van Kansas, Lawrence, Lawrence, KS Institute of Technology, Wright-Patterson University, Beijing, China S. Walker, J. Shan, York University, M. Surratt, M. Kezirian, University of Paassen, M. Mulder, Delft University of AFB, OH Toronto, Canada Southern California, Los Angeles, CA Technology, Delft, The Netherlands Monday, 5 January 2015

76 86-MVC-2 Grid Quality Metrics Related to Solution Accuracy Including Real-World Conﬁgurations Gainesville 2 Chaired by: K. BRYDEN, Ames Laboratory 1400 hrs 1430 hrs 1500 hrs AIAA-2015-0407 AIAA-2015-0408 The Path to and State of Geometry and Meshing in 2030 Grid Quality and Resolution Effects On the quantiﬁcation of errors of Current and emerging trends in HPC are providing transformational capabilities for Simulation Based Research and Development and Simulation Based Design. Numerous efforts are underway to provide on the Aerodynamic Modeling of a pre-processing effort reducing Exascale systems in the next decades. HPC architectures are rapidly evolving and the tools and methods need to keep pace with both the scale and the evolving HW architecture. Emerging HPC capabilities Parachute Canopies contact meshing approach provide potential for simulation of increasingly complex, multi-scale and multi-disciplinary applications for discovery, design and evaluation of aerospace systems. The computational mesh, along with the M. Ghoreyshi, J. Seidel, U.S. Air Force A. Keskin, Rolls-Royce Group plc, Derby, geometry that it represents, has a considerable impact on the quality, stability, and amount of resources required to complete numerical simulations. Extreme-scale environments require increased levels of Academy, Colorado Springs, CO; K. United Kingdom; M. Kober, E. Stelldinger, process automation and reliability not currently available in state-of-the-art mesh generation tools. These shortcomings make geometry modeling and mesh generation a pacing bottleneck for the future. Bergeron, Army Research, Development A. Kuehhorn, Cottbus University, Cottbus, The goal of the proposed panel is to provide technical interchange to help illuminate the path for geometry and mesh generation as a supporting element of the NASA CFD 2030 Vision. and Engineering Command, Natick, MA; A. Germany; H. Boehm, A. Hornig, Dresden Moderator: Hugh Thornburg Jirasek, A. Lofthouse, R. Cummings, U.S. University of Technology, Dresden, Air Force Academy, Colorado Springs, CO Germany; et al. Panelists: John Dannenhoffer John Chawner Nigel Taylor Syracuse University Pointwise, Inc. MBDA Jeffrey Slotnick Saikat Dey William Jones The Boeing Company Naval Research Laboratory NASA Langley Research Cener Monday, 5 January 2015 87-PANEL-2 Climate Change and National Security Osceola Ballroom B 1400 - 1600 hrs Moderator: John Lanicci, Professor, Embry-Riddle Aeronautical University

Panelists: Chad Briggs Roger Handberg Peter Jacques David Titley Cathy Snyder Strategy Director Professor, Political Science, College of Sciences Prelaw Adviser Associate Professor, Department of Political Science Director, Center for Solutions to Weather and Climate Risk Vice President, Energy & Environment Global Interconnections, LLC University of Central Florida University of Central Florida Pennsylvania State University Lockheed Martin Washington Operations

Monday, 5 January 2015 88-PC-5 Plasma Assisted Combustion II: AFOSR MURI Reports Emerald 2 Chaired by: C. LI, Air Force Ofﬁce of Scientiﬁc Research and W. LEMPERT, Vanderbilt University 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2015-0409 AIAA-2015-0410 AIAA-2015-0411 AIAA-2015-0412 Oral Presentation Panel Discussion Multi-Scale Modeling of Plasma- Plasma assisted ignition of Parametric study of plasma-assisted High-pressure nanosecond Nanosecond Repetitively Pulsed Panelists: Assisted Ignition and Combustion combustible mixtures. Effect of ignition in combustible mixtures discharges for plasma-assisted Discharges in Plasma-Assisted Igor Adamovich Andrey Starikovskiy Richard Miles S. Nagaraja, V. Yang, Georgia Institute of N. Alexandrov, I. Kosarev, S. Kindysheva, electronically excited O(1D) atoms combustion Combustion Ohio State University Princeton University Princeton University Technology, Atlanta, GA and vibrationally excited molecules Moscow Institute of Physics and Technology, S. Starikovskaia, École Polytechnique, C. Laux, École Centrale de Paris, Paris, N. Popov, Moscow State University, Moscow, Russia; A. Starikovskiy, Princeton Paris, France France Rich Yetter Yiguang Ju Vigor Yang Moscow, Russia University, Princeton, NJ Penn State University Princeton University Georgia Tech

Monday, 5 January 2015 89-PC-6 Combustion Chemistry Emerald 3 77 Chaired by: P. KOURDIS, California Institute of Technology 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs AIAA-2015-0413 AIAA-2015-0414 AIAA-2015-0415 AIAA-2015-0416 AIAA-2015-0417 AIAA-2015-0418 AIAA-2015-0419 Simulations of a Micro-Reactor Modeling Gas Dynamic Effects in Hydrocarbon Emissions from a WSR HP-Mech: A High Pressure Kinetic The Effects of Non-Uniform High-Pressure Fuel Pyrolysis Unsteady Rans Simulation of for the Study of the Unimolecular Shock-Tubes for Reaction Kinetics Near Lean Blow-Off Mechanism for C2 Flames with Boundary Temperatures in Ignition Investigation Using a Microflow an Enclosed, Turbulent Reacting Decomposition of Large Fuel Measurements D. Blunck, Oregon State University, Exhaust Gas Dilution Delay Time Measurements from Tube Reactor Methane Jet with the Premixed Molecules K. Grogan, Q. Wang, M. Ihme, Stanford Corvallis, OR; S. Zeppieri, United J. Santner, X. Yang, D. Chen, Q. Wang, Heated Rapid Compression Machine U. Shrestha, G. Simms, H. Chelliah, CMC Method Q. Guan, G. Ellison, J. Daily, University of University, Stanford, CA Technologies Corporation, East Hartford, Y. Ju, Princeton University, Princeton, Experiments University of Virginia, Charlottesville, S. Vasu, University of Central Florida, Colorado, Boulder, Boulder, CO CT; J. Gross, S. Stouffer, University of NJ; X. Shen, University of Science and C. Allen, J. Neuman, Marquette University, Charlottesville, VA Orlando, FL Dayton, Dayton, OH; M. Colket, United Technology of China, Hefei, China Milwaukee, WI Technologies Corporation, East Hartford, CT Monday, 5 January 2015 90-PC-7 Spray and Droplet Combustion II Emerald 5 Chaired by: Y. HARDALUPAS, Imperial College London 1400 hrs 1430 hrs 1500 hrs 1530 hrs AIAA-2015-0420 AIAA-2015-0421 AIAA-2015-0422 AIAA-2015-0423 Multi-Scale Simulation of Aspects of droplet grouping in Hypergolic Ignition and Flame A Computational Study of Internal Primary Breakup in Gas-Assisted polydisperse spray diffusion flames Structures of Hydrazine Spray/ Flows in a Heated Water-Oil Atomization J. Greenberg, Technion--Israel Institute of Gaseous Nitrogen Tetroxide Co- Emulsion Droplet Y. Ling, S. Zaleksi, Pierre and Marie Curie Technology, Haifa, Israel; D. Katoshevski, flowing Jets J. Sim, H. Im, S. Chung, King Abdullah University, Paris, France Ben-Gurion University of the Negev, H. Tani, Japan Aerospace Exploration Agency University of Science and Technology, Beer-Sheva, Israel (JAXA), Tsukuba, Japan; H. Terashima, Thuwal, Saudi Arabia University of Tokyo, Tokyo, Japan; M. Koshi, Yokohama National University, Yokohama, Japan; Y. Daimon, Japan Aerospace Exploration Agency (JAXA), Tsukuba, Japan Monday, 5 January 2015 91-PC-8 Turbulent Combustion II Emerald 7 Chaired by: G. BORGHESI and J. O`CONNOR, Pennsylvania State University 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs AIAA-2015-0424 AIAA-2015-0425 AIAA-2015-0426 AIAA-2015-0427 AIAA-2015-0428 AIAA-2015-0429 AIAA-2015-0430 Spatiotemporal Characterization of Proper Orthogonal Decomposition Influence of Fuel Stratification on Measurement of 3D Rayleigh Modeling the Response of Turbulent Stability Analysis of Reacting Effect of Ignition Chemistry on Flame-Vortex Interactions in Bluff- Analysis of a Turbulent Swirling Turbulent Flame Propagation Index fields in helically-perturbed Flames to Harmonic Forcing Wakes: Flow and Density Turbulent Premixed Flames of Body Stabilized Turbulent Premixed Self-Excited Premixed Flame M. Hassanaly, V. Raman, University of swirl flames using doubly-phase- L. Humphrey, V. Acharya, Georgia Institute Asymmetry Effects n-Heptane and iso-Octane Flames Using Simultaneous High- A. Kypraiou, A. Dowling, E. Mastorakos, Texas, Austin, Austin, TX; M. Colket, conditioned chemiluminescence of Technology, Atlanta, GA; D. Shin, B. Emerson, S. Jagtap, T. Lieuwen, S. Won, S. Nakane, C. Reuter, Princeton Repetition-Rate OH-PLIF and PIV University of Cambridge, Cambridge, United Technologies Corporation, East tomography University of Southampton, Southampton, Georgia Institute of Technology, Atlanta, University, Princeton, NJ; B. Windom, A. Caswell, Air Force Research Laboratory, United Kingdom; N. Karimi, University of Hartford, CT B. Geraedts, S. Yang, University of United Kingdom; T. Lieuwen, Georgia GA University of Colorado, Colorado Springs, Wright-Patterson AFB, OH; B. Rankin, B. Glasgow, Glasgow, United Kingdom Toronto, Toronto, Canada; C. Arndt, Institute of Technology, Atlanta, GA Colorado Springs, CO; Y. Ju, Princeton Huelskamp, Innovative Scientific Solutions, Institute for Combustion Technology, University, Princeton, NJ Inc., Dayton, OH; N. Jiang, Spectral German Aerospace Center, Stuttgart, Energies, LLC, Dayton, OH; A. Lynch, V. Germany; A. Steinberg, University of Belovich, Air Force Research Laboratory, Toronto, Toronto, Canada Wright-Patterson AFB, OH; et al. Monday, 5 January 2015 92-SCS-2 Solar Sails and Tensioned Membranes Osceola Ballroom 4 Chaired by: R. PAPPA, NASA Langley Research Center and J. BANIK, USAF 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2015-0431 AIAA-2015-0432 AIAA-2015-0433 AIAA-2015-0434 AIAA-2015-0435 AIAA-2015-0436 Recent Advances in Heliogyro Solar Empirical Modeling for Sail Structural and Attitude Dynamics Deployment Testing of the De-Orbit Nonlinear Torsional Dynamics and Deformation Properties of Solar Sail Structural Dynamics, Stability, Membrane Dynamics by Fusing and Control of a Solar Sail using Sail Flight Hardware Control of Heliogyro Solar Sail Sail IKAROS Membrane with

78 and Control Research Measurement Data and Numerical Two Degrees of Freedom Tip Vanes M. Hillebrandt, S. Meyer, M. Zander, C. Blades Nonlinear Finite Element Analyses W. Wilkie, J. Warren, L. Horta, K. Lyle, Analysis M. Choi, C. Damaren, University of Huehne, German Aerospace Center (DLR), D. Guerrant, D. Lawrence, University of Y. Satou, O. Mori, N. Okuizumi, Y. J. Juang, NASA Langley Research Center, M. Yamazaki, Nihon University, Chiba, Toronto, Toronto, Canada Braunschweig, Germany Colorado, Boulder, Boulder, CO Shirasawa, Japan Aerospace Exploration Hampton, VA; S. Gibbs, Duke University, Japan Agency (JAXA), Sagamihara, Japan; H. Durham, NC; et al. Furuya, H. Sakamoto, Tokyo Institute of Technology, Yokohama, Japan Monday, 5 January 2015 93-SD-4 Flutter, LCO and Aeroelastic Tailoring Tampa 2 Chaired by: W. SCHNEIDER, Lockheed Martin Aeronautics and R. SCOTT, NASA-Langley Research Center 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs AIAA-2015-0437 AIAA-2015-0438 AIAA-2015-0439 AIAA-2015-0440 AIAA-2015-0441 AIAA-2015-0442 AIAA-2015-0443 Plans and example results for the 2nd Transonic Flutter Characteristics of Aeroelastic Tailoring using Rib/ On the Interpretation of Bending- Morphing Wing Design for Fixed Prediction of Wing Flutter Analysis of the Transonic Flutter of AIAA Aeroelastic Prediction Workshop Advanced Fighter Wings Spar Orientations: Experimental Torsion Coupling for Swept, Non- Wing Aircraft Boundary Using High Fidelity Supersonic Transport Wings J. Heeg, P. Chwalowski, NASA Langley O. Bendiksen, University of California, Los Investigation Homogenous Wings J. Yang, P. Sartor, J. Cooper, R. Nangia, Delayed Detached Eddy Simulation E. Mellquist, The Aerospace Corporation, El Research Center, Hampton, VA; D. Raveh, Angeles, Los Angeles, CA G. Francois, J. Cooper, P. Weaver, O. Stodieck, J. Cooper, P. Weaver, University of Bristol, Bristol, United J. Gan, H. Im, X. Chen, G. Zha, University Segundo, CA; O. Bendiksen, University of Technion--Israel Institute of Technology, Haifa, University of Bristol, Bristol, United University of Bristol, Bristol, United Kingdom of Miami, Coral Gables, FL; C. Pasiliao, Air California, Los Angeles, Los Angeles, CA Israel; M. Dalenbring, A. Jirasek, Swedish Kingdom Kingdom Force Research Laboratory, Eglin AFB, FL Defense Research Agency (FOI), Stockholm, Sweden Monday, 5 January 2015 94-SD-5 Energy Harvesting, Health Monitoring and Multifunctional Structures Tampa 3 Chaired by: W. WELSH, Sikorsky Aircraft Corporation and H. KIM, Boeing Defense, Space & Security 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs AIAA-2015-0444 AIAA-2015-0445 AIAA-2015-0446 AIAA-2015-0447 AIAA-2015-0448 Modeling of Highly Flexible Performance Analysis and Harvesting at the Margins: A Study Detecting Damage in a UAV Composite Damage Characterization Using Multifunctional Wings for Energy Parametric Design of an Airfoil-Based of Harvesting Away from Optimal Wing Spar Using Distributed Fiber Matching Pursuit with a Guided Harvesting Piezoaeroelastic Energy Harvester Conditions Optic Strain Sensors Wave Simulation Library W. Su, N. Tsushima, University of Y. Wu, D. Li, J. Xiang, Beihang University, T. Hynds, J. Kauffman, University of B. Martins, J. Kosmatka, University of M. Obenchain, C. Cesnik, University of Alabama, Tuscaloosa, Tuscaloosa, AL Beijing, China Central Florida, Orlando, FL California, San Diego, La Jolla, CA Michigan, Ann Arbor, Ann Arbor, MI Monday, 5 January 2015 95-STR-4 Special Session: Composite Laminate Optimization Sun Ballroom D Chaired by: M. RASSAIAN, Boeing Engineering Operations & Technology and A. BLOM, The Boeing Company 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2015-0449 AIAA-2015-0450 AIAA-2015-0451 AIAA-2015-0452 AIAA-2015-0453 AIAA-2015-0454 Maximizing Buckling Load Optimisation of Variable Stiffness Optimal Postbuckling Design of Mass Optimisation of Variable Level Set Optimization for Steered Optimization of Composite Plates Factors of Fiber-Placed Composite Composites with Ply Drops Variable Angle Tow Composites Angle Tow, Variable Thickness Fiber Composites with Spatially Varying Fiber Paths Cylindrical Shells by Particle Swarm D. Peeters, M. Abdalla, Delft University of using Lamination Parameters Panels with Static Failure and C. Brampton, H. Kim, University of Bath, for Thermal Buckling Optimization Technology, Delft, The Netherlands G. Raju, S. White, Z. Wu, P. Weaver, Buckling Constraints Bath, United Kingdom A. Duran, N. Fasanella, V. S. Guldu, A. Kayran, Middle East Technical University of Bristol, Bristol, United R. Groh, P. Weaver, University of Bristol, Sundararaghavan, A. Waas, University of University, Ankara, Turkey Kingdom Bristol, United Kingdom Michigan, Ann Arbor, Ann Arbor, MI Monday, 5 January 2015 96-STR-5 Aircraft Structural Design Tampa 1 79 Chaired by: M. WOLFF, Gulfstream Aerospace Corporation and P. MARDANPOUR 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2015-0455 AIAA-2015-0456 AIAA-2015-0457 AIAA-2015-0458 AIAA-2015-0459 AIAA-2015-0460 Topology Optimization of Methodology for Conceptual Design Structural Loads Analysis of a Reliability Based Structural Design Full Scale Aircraft Drop Test Analytical Evaluation of Composite Composite Structures for with Composite Stiffened Skin Carrier Onboard Delivery Aircraft using Continuum Sensitivity Program for the F-35C Carrier Laminates with Scored Balsa Multifunctional Behavior A. Noevere, A. Wilhite, Georgia Institute of B. Flansburg, Lockheed Martin Analysis Variant A. Tran, K. Wetzel, Wetzel Engineering, D. Seifert, M. Patil, G. Seidel, Virginia Technology, Atlanta, GA Corporation, Marietta, GA M. Kulkarni, R. Canfield, Virginia D. Norwood, R. Chichester, Lockheed Inc., Austin, TX; R. Hale, University of Polytechnic Institute and State University, Polytechnic Institute and State University, Martin Corporation, Fort Worth, TX Kansas, Lawrence, Lawrence, KS Blacksburg, VA Blacksburg, VA Monday, 5 January 2015 97-STR-6 Failure Analysis and Prediction I Tallahassee 3 Chaired by: S. RUSSELL, Triumph Aerostructures; J. MIN, NASA Glenn Research Center and M. CHO, Seoul National University 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs AIAA-2015-0461 AIAA-2015-0462 AIAA-2015-0463 AIAA-2015-0464 AIAA-2015-0465 AIAA-2015-0466 AIAA-2015-0467 A novel two-parameter linear Computational Techniques for A Micromechanical Approach Tensile Response of Oxide/Oxide Ordinary-State Based Peridynamic Progressive Damage and Failure Comparative Studies of Residual elastic constitutive model for bond the Thermostructural Analysis of to Static Failure Prediction of Woven Ceramic Composites Truss Element Prediction of Open Hole Tension and Stress Effects on Fatigue Crack based peridynamics Composites Heterogeneous Materials D. Zhang, P. Meyer, A. Waas, University of M. Dorduncu, A. Borut, E. Madenci, Open Hole Compression Specimens Growth of Welded Aluminum N. Prakash, G. Seidel, Virginia Polytechnic V. Goyal, The Aerospace Corporation, El H. Sertse, W. Yu, Purdue University, West Michigan, Ann Arbor, Ann Arbor, MI University of Arizona, Tucson, Tucson, AZ A. Joseph, A. Waas, University of Michigan, Structures under Block Spectrum Institute and State University, Blacksburg, VA Segundo, CA Lafayette, IN Ann Arbor, Ann Arbor, MI; W. Ji, Ulsan National Loading Institute of Science and Technology, Ulsan, S. Alireza, E. Fang, X. Liu, J. Lua, Korea (the Republic of); E. Pineda, NASA Global Engineering and Materials, Inc., Glenn Research Center, Cleveland, OH; S. Princeton, NJ Liguore, S. Wanthal, The Boeing Company, St. Louis, MO Monday, 5 January 2015 98-TP-2 Cryogenics Miami 3 Chaired by: H. MA, University of Missouri and E. SILK, NASA-Goddard Space Flight Center 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2015-0468 AIAA-2015-0469 AIAA-2015-0470 AIAA-2015-0471 AIAA-2015-0472 AIAA-2015-0473 Numerical Simulation of the Liquid RANS Modeling of Transcritical and Models for Cyrogenic Cavitation in Thermodynamic Effect on Backflow Cryogenic Loop Heat Pipe for Zero- Numerical Modeling of the Nitrogen Chilldown of a Vertical Tube Supercritical Nitrogen Jets Rotating Turbomachinery Vortex Cavitation Boil-Off Cryogen Storage Transient Chilldown Process of a S. Darr, H. Hu, R. Shaeffer, J. Chung, E. Antunes, A. Silva, J. Barata, University J. Schwille, D. Jackson, The Aerospace A. Tsunoda, Y. Ito, Tokyo Institute of D. Zakar, R. Baldauff, Naval Research Cryogenic Propellant Transfer Line University of Florida, Gainesville, Gainesville, of Beira Interior, Covilha, Portugal Corporation, El Segundo, CA Technology, Yokohama, Japan; N. Tani, Laboratory, Washington, DC; T. Hoang, J. Hartwig, J. Vera, NASA Glenn Research FL; J. Hartwig, NASA Glenn Research Center, Japan Aerospace Exploration Agency (JAXA), TTH Research, Inc., Laurel, MD Center, Cleveland, OH Cleveland, OH; A. Majumdar, NASA Marshall Tsukuba, Japan; T. Nagasaki, Tokyo Institute of Space Flight Center, Huntsville, AL Technology, Yokohama, Japan Monday, 5 January 2015 99-TP-3 Nonequilibrium Flows and Radiation I Sun Ballroom B Chaired by: M. PANESI, University of Illinois at Urbana Champaign and J. BURT, Universal Technology Corporation 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs AIAA-2015-0474 AIAA-2015-0475 AIAA-2015-0476 AIAA-2015-0477 AIAA-2015-0478 AIAA-2015-0479 AIAA-2015-0480 Direct simulation of rovibrational State-to-State Kinetic Model for a State-to-State Modeling of CO for State Specific Modeling of Energy Nonequilibrium Radiation Modeling Sensitivity of State-Specific Dissociation and Energy transfer study excitation and dissociation in Viscous Radiating Hypersonic Flow Mars Entry Applications Transfer and Chemical Reactions in for a Low Enthalpy Hypersonic Dissociation Cross Sections to O3 of N2-N and N2-N2 interactions by molecular nitrogen using an ab E. Josyula, Air Force Research Laboratory, R. Macdonald, A. Munafò, University of Shocks using High Fidelity Models Shock Layer Potential Energy Surfaces using rovibrational and coarse-grained initio potential energy surface Wright-Patterson AFB, OH; J. Burt, Ohio Illinois, Urbana-Champaign, Urbana, IL; C. T. Zhu, Z. Li, N. Parsons, D. Levin, J. Burt, E. Josyula, Air Force Research M. Kulakhmetov, A. Alexeenko, Purdue state-to-state models P. Valentini, I. Nompelis, T. Aerospace Institute, Wright-Patterson AFB, OH; Johnston, NASA Langley Research Center, Pennsylvania State University, University Laboratory, Wright-Patterson AFB, OH University, West Lafayette, IN A. Munafò, University of Illinois, Urbana- Schwartzentruber, University of Minnesota, E. Kustova, Saint Petersburg State University, Hampton, VA; M. Panesi, University of Park, PA Champaign, Urbana, IL; R. Jaffe, D. Minneapolis, Minneapolis, MN Saint Petersburg, Russia; P. Vedula, University Illinois, Urbana-Champaign, Urbana, IL Schwenke, NASA Ames Research Center, of Oklahoma, Norman, Norman, OK

80 Moffett Field, CA; M. Panesi, University of Illinois, Urbana-Champaign, Urbana, IL Monday, 5 January 2015 100-UMS-1 UAS Integration: Detect and Avoid Technologies Osceola Ballroom 3 Chaired by: M. LOGAN, NASA Langley Research Center and R. STANSBURY, Embry-Riddle Aeronautical University 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs AIAA-2015-0481 AIAA-2015-0482 AIAA-2015-0483 AIAA-2015-0484 AIAA-2015-0485 AIAA-2015-0486 AIAA-2015-0487 Defining Well Clear for Unmanned Challenges and Solutions for Vision- Conflict Detection and Resolution Unmanned Aircraft System Sense Development of a Surrogate Real-Time Validation of an ADS-B Optimal UAS Path Planning for Aircraft Systems based Sense and Avoid System Architecture for Unmanned and Avoid Integrity and Continuity Autonomous Aircraft for Entry Based Aircraft Conflict Detection Convoy Overwatch S. Cook, MITRE Corporation, McLean, VA; G. Fasano, D. Accardo, A. Tirri, A. Moccia, Aerial Vehicles in Civil Airspace Risk for Non-Cooperatve Intruders in the NASA Airspace Operation System R. Livermore, Air Force Research D. Brooks, New Mexico State University, University of Naples “Federico II”, Naples, Y. Jenie, E. Van Kampen, J. Ellerbroek, J. M. Jamoom, M. Joerger, S. Khanafseh, Challenge M. Orefice, V. Di Vito, F. Corraro, Italian Laboratory, Wright-Patterson AFB, OH; R. Las Cruces, NM; R. Cole, Lincoln Laboratory, Italy; E. De Lellis, Italian Aerospace Hoekstra, Delft University of Technology, B. Pervan, Illinois Institute of Technology, R. Anderson, H. Moncayo, R. Prazenica, Aerospace Research Center (CIRA), Capua, Cobb, Air Force Institute of Technology, Massachusetts Institute of Technology, Research Center (CIRA), Capua, Italy Delft, The Netherlands Chicago, IL M. Mirmirani, A. Noriega, B. Burnett, Italy; G. Fasano, D. Accardo, University of Wright-Patterson AFB, OH Lexington, MA; D. Hackenberg, NASA Embry-Riddle Aeronautical University, Naples “Federico II”, Naples, Italy Headquarters, Washington, DC; V. Raska, Air Daytona Beach, FL; et al. Force Research Laboratory, Wright-Patterson AFB, OH Monday, 5 January 2015 101-WE-3 Wind Energy Blade and Turbine Design Emerald 6 Chaired by: D. GRIFFITH and C. KELLEY 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2015-0488 AIAA-2015-0489 AIAA-2015-0490 AIAA-2015-0491 AIAA-2015-0492 AIAA-2015-0493 Free-form Design of Low Induction Analysis of the Impact of Leading Horizontal-Axis Wind Turbine Wake Aero-Elastic Optimization of a 10 Effects of spanwise blade load Numerical Simulations of Subscale Rotors Edge Surface Degradation on Wind Sensitivity to Different Blade Load MW Wind Turbine distribution on wind turbine wake Wind Turbine Rotor Inboard Airfoils C. Bottasso, Technical University of Turbine Performance Distributions F. Zahle, C. Tibaldi, D. Verelst, R. Bitche, evolution at Low Reynolds Number Munich, Munich, Germany; A. Croce, L. C. Langel, R. Chow, O. Hurley, C. Van Dam, C. Kelley, D. Maniaci, B. Resor, Sandia C. Bak, Technical University of Denmark, X. Yang, A. Boomsma, F. Sotiropoulos, M. Blaylock, Sandia National Sartori, Technical University of Milan, University of California, Davis, Davis, CA; National Laboratories, Albuquerque, NM Roskilde, Denmark University of Minnesota, Minneapolis, Laboratories, Livermore, CA; D. Maniaci, Milan, Italy D. Maniaci, Sandia National Laboratories, Minneapolis, MN; B. Resor, D. Maniaci, B. Resor, Sandia National Laboratories, Albuquerque, NM; R. Ehrmann, Texas A&M C. Kelley, Sandia National Laboratories, Albuquerque, NM University, College Station, TX; et al. Albuquerque, NM Monday, 5 January 2015 102-WE-4 Wind Energy Aerodynamics and Aeroacoustics II Emerald 4 Chaired by: T. KIM, Technical University of Denmark 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2015-0494 AIAA-2015-0495 AIAA-2015-0496 AIAA-2015-0497 AIAA-2015-0498 AIAA-2015-0499 Non-conventional flat back thick Numerical Studies Of the Upstream Investigation of Wind Turbine AVATAR: AdVanced Aerodynamic Experimental Investigation of the Cross-Validation of Numerical airfoils for very large offshore Flow Field Around A Horizontal Axis Power Generation During Tools of lArge Rotors Wake Flow Field of a Model Wind and Experimental Studies of wind turbines Wind Turbine Atmospheric Icing by Multi- G. Schepers, Energy Research Center of Turbine Rotor with Tip Injection Transitional Airfoil Performance F. Grasso, O. Ceyhan, Energy Research H. Abedi, L. Davidson, Chalmers University Disciplinary Experimentation the Netherlands, Petten, The Netherlands A. Abdulrahim, E. Anik, O. Uzol, Middle A. Frere, K. Hillewaert, Cenaero, Gosselies, Center of the Netherlands, Petten, The of Technology, Göteborg, Sweden; S. P. Blasco, J. Palacios, S. Schmitz, East Technical University, Ankara, Turkey Belgium; H. Chivaee, R. Mikkelsen, Technical Netherlands Voutsinas, National Technical University of Pennsylvania State University, University University of Denmark, Copenhagen,

81 Athens, Athens, Greece Park, PA Denmark; P. Chatelain, Université catholique de Louvain, Louvain, Belgium Monday, 5 January 2015 103-APA-9/NDA-1 Frontiers of Uncertainty Management for Complex Aerospace Systems Osceola Ballroom 5 1500 - 1730 hrs Chaired by: R. GRAVES, Air Force Reseach Laboratory and P. MORGAN, Ohio Aerospace Institute This joint session between the NDA and APA technical committees is a unique forum with the goal of presenting a number of best practices associated with validation, verification, and uncertainty quantification from a work flow management perspective. Invited speakers in this session will communicate their approaches to validation, verification, and uncertainty quantification, and how the adoption of non-deterministic work flows has influenced their organizations, and their ability to deliver reliable aerospace system products. Panelists: Overview of Selected DOE/NNSA Predictive Science Initiatives: Integrated Uncertainty Quantification for Risk and Resource Management: Verification, Validation, and Uncertainty Propagation and Quantification for the Predictive Science Academic Alliance Program and the DAKOTA Project A NASA Langley Perspective Simulation Credibility AIAA-2015-0500 AIAA-2015-0501 AIAA-2015-0502 Michael Eldred Eric Walker Dean Eklund SANDIA NASA Langley AFRL/RQH

Tuesday Tuesday, 6 January 2015 104-PLNRY-2 International Trends in Aerospace: Up, Up and Away? To Where? Osceola Ballroom CD 0800 - 0900 hrs James N. Miller President Adaptive Strategies, LLC Tuesday, 6 January 2015 105-AA-3 Computational Aeroacoustics II Miami 2 Chaired by: J. GALLMAN, Gulfstream 0930 hrs 1000 hrs 1030 hrs AIAA-2015-0503 AIAA-2015-0504 AIAA-2015-0505 LES of jet ﬂow and noise with Implementation of a Sharp Immersed Synchronized Large-Eddy internal and external geometry Boundary Method in a 3-D Multi-block Simulations to track Native features Large Eddy Simulation Tool for Jet Perturbations in a Turbulent Jet J. Tyacke, P. Tucker, University of Aeroacoustics U. Sasidharan Nair, D. Gaitonde, Ohio Cambridge, Cambridge, United Kingdom N. Dhamankar, G. Blaisdell, Purdue University, State University, Columbus, OH West Lafayette, IN; A. Lyrintzis, Embry-Riddle Aeronautical University, Daytona Beach, FL Tuesday, 6 January 2015 106-AA-4 Jet Noise Prediction I Sun Ballroom C Chaired by: A. PILON, Lockheed Martin Aeronautics 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2015-0507 AIAA-2015-0508 AIAA-2015-0509 AIAA-2015-0510 AIAA-2015-0511 AIAA-2015-0512 Application of Synthetic Array Numerical Study of Noise Analysis of Converging-Diverging Numerical modelling of jets exiting Numerical Simulation of Supersonic 3-D Jet Noise Prediction for Techniques for Improved Simulations Characteristics in Overexpanded Beveled Nozzle Jets Using Large from the ASME and conical nozzles Twin-Jet Noise with High Order Separate Flow Nozzles with Pylon of Hot Supersonic Jet Noise Jet Flows Eddy Simulation with a Wall Model C. Bogey, O. Marsden, École Centrale, Finite Difference Scheme Interaction C. Nelson, A. Cain, Innovative Technology J. Liu, A. Corrigan, K. Kailasanath, Naval K. Aikens, G. Blaisdell, Purdue University, Ecully, France J. Gao, X. Xu, X. Li, Beihang University, X. Xu, J. He, X. Li, Beihang University, Applications Company, LLC, Chesterﬁeld, Research Laboratory, Washington, DC; N. West Lafayette, IN; A. Lyrintzis, Embry- Beijing, China Beijing, China; F. Hu, Old Dominion MO; R. Dougherty, OptiNav, Inc., Bellevue, Heeb, E. Gutmark, University of Cincinnati, Riddle Aeronautical University, Daytona University, Norfolk, VA WA; K. Brentner, P. Morris, Pennsylvania Cincinnati, OH Beach, FL

82 State University, University Park, PA Tuesday, 6 January 2015 107-ACD-1 Aircraft Design Optimization Naples 3 Chaired by: H. JIMENEZ, Georgia Institute of Technology 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2015-0513 AIAA-2015-0514 AIAA-2015-0515 AIAA-2015-0516 AIAA-2015-0517 Optimized Military Transport Evaluation of N+2 Technologies Comparison of Advanced Vehicle An Aircraft Conceptual Design Multirotor Configuration Feasibility Aircraft Design Through Multi- and Advanced Vehicle Concepts Concepts through Pareto-Optimal and Optimization Platform and Its Analysis and Optimal Design Based Objective Analysis of Fleet-Level J. Schutte, D. Mavris, Georgia Institute of Technology Sets Application for Nature Laminar on Moore-Penrose Pseudoinverse Metrics Under Demand Uncertainty Technology, Atlanta, GA C. Ingram, H. Jimenez, D. Mavris, Georgia Flow Aircraft Study Z. Hu, S. Yang, F. Xiong, Beijing Institute P. Govindaraju, W. Crossley, Purdue Institute of Technology, Atlanta, GA Y. Zhao, H. Chen, Y. Zhang, Tsinghua of Technology, Beijing, China University, West Lafayette, IN University, Beijing, China Tuesday, 6 January 2015 108-AFM-5 Aerodynamic Prediction Methods Captiva 2 Chaired by: F. PRIOLO, Millennium Engineering and Integration Company 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2015-0518 AIAA-2015-0519 AIAA-2015-0520 AIAA-2015-0521 AIAA-2015-0522 AIAA-2015-0523 Linear Computational Fluid Computational Analysis of a Flow Analytical Aerodynamic Force Kinetic Models and Gas Kinetic Trajectory Simulation of a Spinning Analytical Shock Standoff and Dynamic Analysis of Dynamic Around Two-Dimensional Streamlined and Moment Coefficients of Schemes for Hybrid Simulation of Projectile Based on Variable Step Shape Prediction with Validation for Ground Effect of a Wing in Sink Bodies with OpenFOAM Axisymmetric Objects in Rarefied Partially Rarefied Flows Size CFD/RBD Method Blunt Face Cylinder and Flare Maneuvers R. Habbit, A. Porteous, C. Echavarria, Flow S. Colonia, R. Steijl, G. Barakos, University G. Wang, Z. Zeng, Northwestern J. Martel, SURVICE Engineering, Fort G. Quijada, Simón Bolívar University, S. Poroseva, University of New Mexico, K. Hart, K. Simonis, B. Steinfeldt, R. of Liverpool, Liverpool, United Kingdom Polytechnical University, Xi’an, China; Q. Walton Beach, FL; B. Jolly, 96th Test Caracas, Venezuela; P. Boschetti, Simón Albuquerque, Albuquerque, NM; S. Murman, Braun, Georgia Institute of Technology, Suo, Nanjing University of Aeronautics and Wing, Eglin AFB, FL Bolívar University, Naiguata, Venezuela NASA Ames Research Center, Moffett Field, CA Atlanta, GA Astronautics, Jingdezhen, China Tuesday, 6 January 2015 109-AFM-6 Atmospheric Entry, Hypersonic Flight and Aeroassist Technology Captiva 1 Chaired by: M. BOLENDER, Air Force Research Lab 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2015-0524 AIAA-2015-0525 AIAA-2015-0526 AIAA-2015-0527 AIAA-2015-0528 A Comparison of Three Algorithms Spatial Parameterization of Blunt Coupled Inertial Navigation and Free Flight Investigation of The Flight Dynamics of the HIFiRE for Orion Drogue Parachute Body Dynamics under Parachutes Flush Air Data Sensing Algorithm Atmospheric Entry Capsules in Low Flight 6 Research Vehicle Release M. Hughes, Lockheed Martin Corporation, for Atmosphere Estimation Subsonic Flow D. Adamczak, M. Bolender, Air Force D. Matz, NASA Johnson Space Center, Littleton, CO C. Karlgaard, P. Kutty, Analytical Mechanics A. Preci, A. Guelhan, German Aerospace Research Laboratory, Wright-Patterson Houston, TX; R. Braun, Georgia Institute of Associates, Inc., Hampton, VA; M. Center (DLR), Cologne, Germany AFB, OH Technology, Atlanta, GA Schoenenberger, NASA Langley Research Center, Hampton, VA Tuesday, 6 January 2015 110-AMT-2 Laser Diagnostics for Reacting Flows Tallahassee 1 Chaired by: J. SUTTON, Ohio State University and D. PLEMMONS, Aerospace Testing Alliance (ATA) 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2015-0529 AIAA-2015-0530 AIAA-2015-0531 AIAA-2015-0532 AIAA-2015-0533 AIAA-2015-0534 Characterization of Inverse Pulsed Laser Diode for Use as a High-Speed 1D Raman/Rayleigh Techniques for Three-Dimensional Time Resolved Planar In situ Measurements of Ethylene Diffusion Flames by Planar Laser Light Source for Short-Exposure, Scattering Imaging in Turbulent Flame Reconstructions with a Measurements in the wake of and Methyl Radical by using the Induced Fluorescence of CO and OH High-Frame-Rate Flow Visualization H2/N2 Flames Plenoptic Camera a Reacting Jet Injected into a Radar REMPI technique D. Richardson, National Research Council, N. Parziale, Stevens Institute of K. Gabet Hoffmeister, F. Fuest, J. Sutton, J. Bolan, K. Johnson, B. Thurow, Auburn Swirling, Vitiated Crossflow at High Y. Wu, Z. Zhang, University of Tennessee, Dayton, OH; N. Jiang, S. Roy, Spectral Technology, Hoboken, NJ; B. Schmidt, P. Ohio State University, Columbus, OH University, Auburn, AL Pressure Knoxville, Knoxville, TN Energies, LLC, Dayton, OH; A. Lynch, Wang, H. Hornung, J. Shepherd, California P. Panda, M. Roa, R. Lucht, Purdue J. Gord, Air Force Research Laboratory, Institute of Technology, Pasadena, CA University, West Lafayette, IN

83 Wright-Patterson AFB, OH Tuesday, 6 January 2015 111-APA-10 Icing or Roughness Effects on Vehicle Aerodynamics II Destin 2 Chaired by: S. MORRIS, Engineering Systems, Inc. and D. O’BRIEN, US Army RDECOM 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2015-0535 AIAA-2015-0536 AIAA-2015-0537 AIAA-2015-0538 Two-Dimensional/Infinite Swept The Influence of Ice Accretion on Numerical Simulation of Hot Air Calculation and Analysis of Water Wing Ice Accretion Model the Aerodynamic Performance of a Anti-icing Charateristics of an Aero- Film Flow Characteristics on Anti-icing S. Bourgault-Cote, E. Laurendeau, École UAS Airfoil engine Strut Airfoil Surface Polytechnique de Montréal, Montréal, K. Szilder, W. Yuan, National Research W. Dong, J. Zhu, G. Lei, M. Zheng, Shanghai W. Dong, M. Zheng, G. Lei, J. Zhu, Shanghai Canada Council, Ottawa, Canada Jiao Tong University, Shanghai, China Jiao Tong University, Shanghai, China Tuesday, 6 January 2015 112-APA-11 Other Topics in Applied Aerodynamics Destin 1 Chaired by: G. GATLIN and P. VIJGEN, Boeing Commercial Airplanes 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2015-0539 AIAA-2015-0540 AIAA-2015-0541 AIAA-2015-0542 AIAA-2015-0543 AIAA-2015-0544 Flight Test Experiments on Discrete Assessment of the Potential for Forecast of Uncertainty-Based Experimental study of supersonic Efficient Flight Simulation Using Aerodynamic Study of Range Roughness Element Technology for Micro Energy Harvesting in a Analytics for a Data Acquisition Probe corner flow evolution in a rectangular Kriging Surrogate Model Based Extension Modification for a Laminar Flow Control Fixed-Wing MAV Configuration in the Presence of Cross Winds channel Aerodynamic Database Fighter Aircraft W. Saric, D. West, M. Tufts, H. Reed, D. Martos, J. Melo De Sousa, Technical R. Graves, Air Force Research Laboratory, R. Morajkar, J. Driscoll, M. Gamba, University N. Othman, M. Kanazaki, Tokyo J. Masud, O. Khan, Air University, Texas A&M University, College Station, TX University of Lisbon, Lisbon, Portugal Wright-Patterson AFB, OH of Michigan, Ann Arbor, Ann Arbor, MI Metropolitan University, Hino, Japan Islamabad, Pakistan Tuesday, 6 January 2015 113-APA-12 High-Angle-of-Attack, High-lift and Vortical Flow Aerodynamics Sun Ballroom A Chaired by: A. JONES, University of Maryland and M. CONWAY, The Aerospace Corporation 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2015-0545 AIAA-2015-0546 AIAA-2015-0547 AIAA-2015-0548 AIAA-2015-0550 AIAA-2015-0549 Mixing Flow Characteristics for a Initiation of Leading-Edge-Vortex Effect of Roll Orientation on the Improved Methodology for Aerodynamics and Flow Mechanics Aerodynamics of the F-15 At High Transverse Sonic Jet Injecting into a Formation on Finite Wings in Vortex Asymmetry on a Conical Predicting the Force on Stalled of a Two-Element Airfoil in Ground Angle of Attack Supersonic Crossflow Unsteady Flow Forebody Spinning Wings Effect S. Yang, P. Chen, ZONA Technology, Inc., E. Khali, Saad Dahleb University, Blida, Y. Hirato, M. Shen, North Carolina State J. Taligoski, A. Uzun, R. Kumar, Florida A. Ragheb, M. Selig, University of Illinois, Q. Qu, W. Wang, P. Liu, Beihang Scottsdale, AZ; X. Wang, M. Mignolet, Algeria; Y. Yao, University of the West of University, Raleigh, NC; S. Aggarwal, State University, Tallahassee, FL Urbana-Champaign, Urbana, IL University, Beijing, China; R. Agarwal, Arizona State University, Tempe, AZ; D. England, Bristol, United Kingdom Swifter Technology, LLC, Denville, NJ; A. Washington University in St. Louis, St. Pitt, The Boeing Company, St. Louis, MO Gopalarathnam, J. Edwards, North Carolina Louis, MO State University, Raleigh, NC Tuesday, 6 January 2015 114-APA-13 Special Session: CREATE-AV High Performance Computing Multiphysics Applications of Full-up Air Vehicles II Naples 2 Chaired by: N. HARIHARAN, CREATE-AV and D. MCDANIEL, University of Alabama at Birmingham 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2015-0551 AIAA-2015-0553 AIAA-2015-0554 AIAA-2015-0555 AIAA-2015-0556 AIAA-2015-0552 An Assessment of CREATE-AV An Industry Assessment of HPCMP Coaxial Rotor Wake and Prop Computational Fluid Dynamics Coupled Flight Simulator and CFD An Industry Assessment of HPCMP Kestrel for F-35 Aero/Performance CREATE-AV Helios Induction Impact on a Horizontal for the Aerodynamic Design and Calculations of Ship Airwake using CREATE-AV Kestrel Applications R. Narducci, The Boeing Company, Tail Using HPCMP CREATE™-AV Modeling of a Ram-Air Parachute Kestrel D. Stookesberry, The Boeing Company, B. Smith, Lockheed Martin Corporation, Philadelphia, PA Helios with Bleed-Air Actuators J. Forsythe, E. Lynch, S. Polsky, Naval Air St. Louis, MO Fort Worth, TX E. Reed, T. Egolf, Sikorsky Aircraft M. Ghoreyshi, U.S. Air Force Academy, Systems Command, Patuxent River, MD Corporation, Stratford, CT Colorado Springs, CO; K. Bergeron, Army

84 Research, Development and Engineering Command, Natick, MA; J. Seidel, A. Jirasek, A. Lofthouse, R. Cummings, U.S. Air Force Academy, Colorado Springs, CO Tuesday, 6 January 2015 115-APA-14 Special Session: Space Launch System (SLS) I Naples 1 Chaired by: J. BLEVINS, NASA Marshall Space Flight Center and J. PINIER, NASA Langley Research Center 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2015-0557 AIAA-2015-0558 AIAA-2015-0559 AIAA-2015-0560 AIAA-2015-0561 Overview of the Space Launch Initial Assessment of Space Launch Computational and Experimental An Empirical Non-TNT Approach to Space Launch System Ascent System Transonic Buffet System Transonic Unsteady Unsteady Pressures for Alternate Launch Vehicle Explosion Modeling Aerothermal Environments Environment Test Program Pressure Environment SLS Booster Nose Shapes J. Blackwood, Bangham Engineering, Methodology D. Piatak, M. Sekula, R. Rausch, J. M. Sekula, D. Piatak, R. Rausch, J. Florance, G. Brauckmann, C. Streett, W. Kleb, S. Huntsville, AL C. Morris, NASA Marshall Space Flight Florance, T. Ivanco, NASA Langley NASA Langley Research Center, Hampton, VA; Alter, K. Murphy, C. Glass, NASA Langley Center, Huntsville, AL Research Center, Hampton, VA J. Ramey, Jacobs, Hampton, VA Research Center, Hampton, VA Tuesday, 6 January 2015 116-DE-1 Design Engineering Sarasota 2 Chaired by: F. KAHLEN, University of Cape Town and S. ROWE, NASA Marshall Space Flight Center 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2015-0562 AIAA-2015-0563 AIAA-2015-0564 AIAA-2015-0565 Multi-Objective Hydrodynamic The process of validating Model An Intermeshing Rotor Helicopter Perching Feasibility of a Fixed Design Optimization of a and Software for applying Model- Design and Test Delta M-Wing MAV Centrifugal Pump Based Development (MBD) to F. Wei, E. Moore, A. Gates, Central D. Patel, University of Michigan, Ann M. Sagban, S. Gangadharan, Embry-Riddle embedded systems more fruitfully Connecticut State University, New Arbor, Ann Arbor, MI Aeronautical University, Daytona Beach, FL S. Mina, H. Oyori, IHI Corporation, Britain, CT Tomioka, Japan Tuesday, 6 January 2015 117-FD-14 CFD Methods III Sanibel 1 Chaired by: S. TU, Jackson State University and M. YU, University of Maryland, Baltimore County 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2015-0566 AIAA-2015-0567 AIAA-2015-0568 AIAA-2015-0569 AIAA-2015-0570 AIAA-2015-0571 Advanced Data Transfer Strategies Further Development of a Riemann- Wave-number Independent Finite-element Time Discretizations Homotopy Continuation for Source Term Discretization Effects for Overset Computational Methods solver Free Space-time Discontinuous Preconditioning for GMRES Time- for the Unsteady Euler Equations Correction Procedure via on the Accuracy of Finite Volume E. Quon, M. Smith, Georgia Institute of Galerkin Method for Compressible spectral Solvers N. Mundis, D. Mavriplis, University of Reconstruction - Discontinuous Schemes Technology, Atlanta, GA Magnetohydrodynamics (MHD) N. Mundis, D. Mavriplis, University of Wyoming, Laramie, Laramie, WY Galerkin (CPR-DG) Methods J. Thorne, A. Katz, Utah State University, Equations Wyoming, Laramie, Laramie, WY M. Yu, University of Maryland, Baltimore, Logan, UT H. Song, L. Ji, Beijing Institute of Baltimore, MD; Z. Wang, University of Technology, Beijing, China; Q. Pang, S. Tu, Kansas, Lawrence, Lawrence, KS Jackson State University, Jackson, MS Tuesday, 6 January 2015 118-FD-15 Discontinuous Galerkin Methods I Sanibel 2 Chaired by: E. JOHNSEN, University of Michigan and H. HUYNH, NASA Glenn Research Center 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2015-0572 AIAA-2015-0573 AIAA-2015-0574 AIAA-2015-0575 AIAA-2015-0576 A general and robust high-order Analysis of Discontinuous Galerkin A dissipative Filter for the A Reconstructed Discontinuous Three-Dimensional Discontinuous numerical framework for shock- Approaches for Advection-- Discontinuous Galerkin method Galerkin Method for the Galerkin h/p Adaptive Numerical capturing: entropy-bounding, shock Diffusion Problems K. Panourgias, University of Patras, Patras, Compressible Navier-Stokes Solutions for Compressible Flows detection and artiﬁcial viscosity L. Khieu, K. Fidkowski, E. Johnsen, Greece; J. Ekaterinaris, Embry-Riddle Equations on Hybrid Grids K. Panourgias, University of Patras, Patras, Y. Lv, Y. See, M. Ihme, Stanford University of Michigan, Ann Arbor, Ann Aeronautical University, Daytona Beach, FL H. Luo, L. Xuan, North Carolina State Greece; J. Ekaterinaris, Embry-Riddle University, Stanford, CA Arbor, MI University, Raleigh, NC; Y. Xia, Idaho Aeronautical University, Daytona Beach, FL

85 National Laboratory, Idaho Falls, ID Tuesday, 6 January 2015 119-FD-16 Experiments in Energy Exchange in High Speed Flows (Invited) Daytona 1 Chaired by: J. AUSTIN, University of Illinois at Urbana-Champaign and E. JOSYULA, Air Force Reseach Laboratory 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs Oral Presentation Oral Presentation AIAA-2015-0577 Oral Presentation AIAA-2015-0578 Oral Presentation Progress on the Basic Research Boundary-Layer Transition on a Measurements of Vibrational Measurements of Vibrational Flow characterization and Shock Wave- Boundary Layer Initiative for AFOSR on how energy Slender Cone in Hypervelocity Flow Energy Transfer and Its Effect on Non-equilibrium in Supersonic Jet boundary layer transition studies in Interaction In Hypervelocity Flow transfer mechanisms affect flow with Real Gas Effects (Invited) the Flow in a Plasma Wind Tunnel Mixing and Combustion (Invited) VKI hypersonic facilities (Invited) J. Austin, California Institute of Technology, properties around bodies going at J. Jewell, Air Force Research Laboratory, (Invited) H. Reising, T. Haller, N. Clemens, P. G. Grossir, D. Masutti, O. Chazot, von Pasadena, CA; A. Knisely, University of hypersonic speeds (Invited) Wright-Patterson AFB, OH M. Nishihara, S. Leonov, W. Lempert, J. Varghese, University of Texas, Austin, Kármán Institute for Fluid Dynamics, Illinois, Urbana-Champaign, Urbana, IL; J. Schmisseur, I. Leyva, Air Force Research Rich, I. Adamovich, Ohio State University, Austin, TX Rhode-Saint-Genèse, Belgium D. Levin, Pennsylvania State University, Laboratory, Edwards AFB, CA Columbus, OH University Park, PA Tuesday, 6 January 2015 120-FD-17 Shock-Dominated Flows II Sanibel 3 Chaired by: D. KNIGHT, Rutgers University 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2015-0579 AIAA-2015-0580 AIAA-2015-0581 AIAA-2015-0582 AIAA-2015-0583 AIAA-2015-0584 Physical Diffusion Cures the Assessment of CFD Capability for Numerical Prediction of Dynamics of Numerical Prediction of Dynamics Numerical Simulation of Energy LES for Prediction of Pressure Carbuncle Phenomenon High Enthalpy Non-Equilibrium Microwave Filament Interaction with of Interaction of Laser Discharge Deposition in a Viscous Supersonic Fluctuation for Supersonic Flow J. Powers, J. Bruns, A. Jemcov, University Flows with Strong Viscous-Inviscid Supersonic Combined Cylinder Bodies Plasma with a Hemisphere-Cylinder Flow Past a Hemisphere around a Truncated Cone of Notre Dame, Notre Dame, IN Interaction O. Azarova, Russian Academy of Sciences, in a Supersonic Flow M. Mortazavi, D. Knight, Rutgers S. Chern, G. Lobser, M. Schoonmaker, E. M. Rouhi Youssefi, D. Knight, Rutgers Moscow, Russia; D. Knight, Rutgers O. Azarova, Russian Academy of Sciences, University, Piscataway, NJ Heyde, United Launch Alliance, Denver, University, Piscataway, NJ University, New Brunswick, NJ Moscow, Russia; D. Knight, Rutgers CO; C. Liu, University of Texas, Arlington, University, New Brunswick, NJ Arlington, TX Tuesday, 6 January 2015 121-FD-18 Stability and Transition Modeling Daytona 2 Chaired by: E. WHITE, Texas A&M University and L. DECHANT, Sandia National Laboratories/Aerosciences 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2015-0585 AIAA-2015-0586 AIAA-2015-0587 AIAA-2015-0588 AIAA-2015-0589 AIAA-2015-0590 DNS Study on Role of Linearly Laminar Turbulent Intermittency A Comparison of a Local Application of the Amplification A General 3D Relation for Oblique A physics-Based Stress Model Unstable Modes in Flow Transition Models: Determination of Functional Correlation-Based Transition Factor Transport Transition Model to Shocks on Swept Ramps J. Rodio, North Carolina State University, J. Tang, Y. Yan, Y. Dong, C. Liu, University Behavior Using an Asymptotic Model Coupled with SA and SST the Shear Stress Transport Model N. Domel, Lockheed Martin Corporation, Raleigh, NC; X. Xiao, Corvid Technologies, of Texas, Arlington, Arlington, TX Differential Equation Argument Turbulence Models J. Coder, M. Maughmer, Pennsylvania Fort Worth, TX Inc., Mooresville, NC; H. Hassan, North L. DeChant, Sandia National Laboratories, J. Wang, C. Sheng, University of Toledo, State University, University Park, PA Carolina State University, Raleigh, NC Albuquerque, NM Toledo, OH Tuesday, 6 January 2015 122-GNC-11 Aerospace Robotics and Autonomous/Unmanned Systems III Sun Ballroom 3 Chaired by: J. SASIADEK, Carleton University and D. PEREZ 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2015-0591 AIAA-2015-0592 AIAA-2015-0593 AIAA-2015-0594 Two Dimensional Optimum Path Three-Dimensional Velocity Comprehensive Modeling and Tracking a Maneuvering Target Navigation for Autonomous Parafoil Obstacle Method for UAV Analysis of an Unmanned Coaxial with an Underactuated UAV in the Vehicles in High Altitude Ballooning Deconflicting Maneuvers Helicopter SE(3) Space S. Lee, Alfred University, Alfred, NY; Y. Jenie, E. Van Kampen, C. de Visser, J. X. Yuan, J. Zhu, Tsinghua University, D. Pylorof, E. Bakolas, University of Texas, J. Conner, A. Arena, Oklahoma State Ellerbroek, J. Hoekstra, Delft University of Beijing, China Austin, Austin, TX University, Stillwater, OK Technology, Delft, The Netherlands Tuesday, 6 January 2015

86 123-GNC-12 Advances in GN&C of Multi-Agent Autonomous Systems Miami 1 Chaired by: S. CHUNG, University of Illinois at Urbana-Champaign and N. HOVAKIMYAN, University of Illinois at Urbana-Champaign 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2015-0595 AIAA-2015-0596 AIAA-2015-0597 AIAA-2015-0598 AIAA-2015-0599 AIAA-2015-0600 Time-Critical Coordination of Attitude Control and Stabilization of Trajectory Generation using Spatial Collision Avoidance through Path Swarm Assignment and Trajectory Collision Avoidance: A Game Multiple UAVs with Absolute Spacecraft with a Captured Asteroid Pythagorean Hodograph Bezier Replanning using Bézier Curves Optimization Using Variable-Swarm, Theoretic Approach Temporal Constraints S. Bandyopadhyay, S. Chung, University Curves S. Mehdi, R. Choe, V. Cichella, N. Distributed Auction Assignment and S. Snyder, N. Hovakimyan, University of J. Puig, E. Xargay, R. Choe, N. of Illinois, Urbana-Champaign, Urbana, R. Choe, J. Puig, V. Cichella, E. Xargay, N. Hovakimyan, University of Illinois, Urbana- Model Predictive Control Illinois, Urbana-Champaign, Urbana, IL Hovakimyan, University of Illinois, Urbana- IL; F. Hadaegh, Jet Propulsion Laboratory, Hovakimyan, University of Illinois, Urbana- Champaign, Urbana, IL D. Morgan, S. Chung, University of Illinois, Champaign, Urbana, IL California Institute of Technology, Champaign, Urbana, IL Urbana-Champaign, Urbana, IL; F. Hadaegh, Pasadena, CA Jet Propulsion Laboratory, California Institute of Technology, Pasadena, CA Tuesday, 6 January 2015 124-GNC-13 Guidance and Control of Autonomous/Unmanned Systems Sun Ballroom 5 Chaired by: K. BOLLINO, AFOSR/EOARD and P. SHANKAR, California State Univ 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2015-0601 AIAA-2015-0602 AIAA-2015-0603 AIAA-2015-0604 AIAA-2015-0605 AIAA-2015-0606 SDRE Based Guidance and Flight Tight Formation Flight with Feasible A Fully Parameterizable A Kalman Filter Based Attitude Robust Flight Control System for a Design of Gain Scheduled Stability Control of Aircraft Formations Model Predictive Control Implementation of Autonomous Heading Reference System Using a Tilt Rotor UAV and Control Augmentation System O. Tekinalp, S. Kumbasar, Middle East F. Almeida, Aeronautics and Space Institute Take-off and Landing for a Fixed Low Cost Inertial Measurement Unit G. Di Francesco, E. D’Amato, M. Mattei, for Quad-Tilt-Wing UAV Technical University, Ankara, Turkey (IAE), São José dos Campos, Brazil Wing UAV M. Leccadito, T. Bakker, R. Niu, R. Klenke, Second University of Naples, Aversa, Italy H. Totoki, Y. Ochi, National Defense T. Carnes, T. Bakker, R. Klenke, Virginia Virginia Commonwealth University, Academy, Yokosuka, Japan; M. Sato, K. Commonwealth University, Richmond, VA Richmond, VA Muraoka, Japan Aerospace Exploration Agency (JAXA), Tokyo, Japan Tuesday, 6 January 2015 125-GNC-14 Adaptive Control of Flight Vehicles Sun Ballroom 4 Chaired by: S. SCHATZ, Institute of Flight System Dynamics and T. YUCELEN, Missouri University of Science & Technology 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2015-0607 AIAA-2015-0608 AIAA-2015-0609 AIAA-2015-0610 AIAA-2015-0611 AIAA-2015-0612 Output Feedback Concurrent Application of a Novel Scalability Adaptive Fault Tolerant Controller A Direct Uncertainty Minimization A Design, Analysis and Veriﬁcation An adaptive compensation strategy Learning Model Reference Adaptive Notion in Adaptive Control to Various Based on Quasi-Continuous High- Framework in Model Reference Framework for Adaptive Flight Control of control surfaces free-play Control Adaptive Control Frameworks Order Sliding Modes Adaptive Control M. Fravolini, University of Perugia, Perugia, A. Mannarino, Technical University of J. Quindlen, Massachusetts Institute S. Schatz, Technical University of Munich, J. Davila, National Polytechnic Institute, T. Yucelen, B. Gruenwald, Missouri Italy; T. Yucelen, B. Gruenwald, Missouri Milan, Milan, Italy of Technology, Cambridge, MA; G. Garching, Germany; T. Yucelen, B. Gruenwald, Mexico City, Mexico; J. Cieslak, D. Henry, University of Science and Technology, University of Science and Technology, Rolla, Chowdhary, Oklahoma State University, Missouri University of Science and Technology, A. Zolghadri, University of Bordeaux, Rolla, MO; J. Muse, Air Force Research MO; N. Nguyen, NASA Ames Research Stillwater, OK; J. How, Massachusetts Rolla, MO; F. Holzapfel, Technical University of Bordeaux, France; F. Bejarano, National Laboratory, Wright-Patterson AFB, OH Center, Moffett Field, CA; W. Daniel, Missouri Institute of Technology, Cambridge, MA Munich, Garching, Germany Polytechnic Institute, Mexico City, Mexico University of Science and Technology, Rolla, MO Tuesday, 6 January 2015 126-GNC-15 Missile Guidance III Sun Ballroom 6 Chaired by: S. THEODOULIS, French German Research Institute and R. TEKIN, ASELSAN Inc 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2015-0613 AIAA-2015-0614 AIAA-2015-0615 AIAA-2015-0616 AIAA-2015-0617 AIAA-2015-0618 A New Impact Time Control Blind Evasion by Random-Phase Satisfying Impact Angle Constraint Impact Time and Angle Control A Composite Guidance for Vertically Cooperative Attack of Multiple Guidance Law for Precise Time-on- Periodic Maneuvers with Field-of-View Limitations Guidance Launched Dual Range SAM with Missiles with Ideal-Line-of-Sight- Target Missile Strike R. Morgan, J. Riel, Raytheon Missile A. Ratnoo, Indian Institute of Science, S. kumar, D. Ghose, Indian Institute of Side Jet Controls Guidance M. Snyder, University of Central Florida, Systems, Tucson, AZ Bangalore, India Science, Bangalore, India D. Taur, Chungshan Institute of Science H. Li, Beijing Institute of Technology, Orlando, FL; R. Prazenica, Embry- and Technology, Taipei, Taiwan Beijing, China Riddle Aeronautical University, Daytona 87 Beach, FL; R. Hull, United Technologies Corporation, Orlando, FL Tuesday, 6 January 2015 127-GT-2 The NASA CRM Model & High Reynolds Number Aerodynamics and Testing (Invited) Miami 3 Chaired by: J. QUEST, ETW GmbH and W. KILGORE, NASA Langley Research Center 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2015-0619 AIAA-2015-0620 AIAA-2015-0621 AIAA-2015-0622 AIAA-2015-0623 Validation of Wing Deformation CFD-Aided Model Deformation Slotted Wall Interference Mach Stability Improvements A Description of the Development, Simulations for the NASA CRM Corrections of NASA Research Investigation in ETW using the Using an Existing Second Throat Capabilities, and Operational Status of Model using Fluid-Structure Model Wind Tunnel data NASA CRM model Capability at the National Transonic the Test SLATE Data Acquisition System Interaction Computations K. Yasue, M. Ueno, S. Koga, M. Kohzai, A. Gorbushin, S. Bosnyakov, S. Glazkov, Facility (Invited) at the National Transonic Facility S. Keye, German Aerospace Center (DLR), Japan Aerospace Exploration Agency A. Llysenkov, S. Matyash, A. Semenov, D. Chan, NASA Langley Research Center, C. Cramer, Sierra Lobo, Inc., Hampton, VA; Braunschweig, Germany (JAXA), Tokyo, Japan TsAGI, Zhukovsky, Russia; et al. Hampton, VA; S. Balakrishna, Jacobs, J. DeMoss, Analytical Services & Materials, Hampton, VA; E. Walker, NASA Langley Inc., Hampton, VA; J. Wright, M. Asay, S. Research Center, Hampton, VA; S. Simmons, L. Bobbitt, Jacobs, Hampton, VA Goodliff, Jacobs, Hampton, VA Tuesday, 6 January 2015 128-GTE-3 Engine Systems I Emerald 1 Chaired by: G. WELCH, NASA Glenn Research Center and M. RICKLICK, CATER: Center for Advanced Turbines & Energy Research 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2015-0624 AIAA-2015-0625 AIAA-2015-0626 AIAA-2015-0627 AIAA-2015-0628 AIAA-2015-0629 Optimization of Gas Turbine - Solid Inverted Gas Turbine Design and Preliminary Design Investigation Feasibility Study of an Inverse An Off-Design Analysis of an Advances of Turbomachinery Oxide Fuel Cell Systems for Aircraft Analysis of Electromagnetic Motors for Brayton UAV Propulsion System Inverse Brayton Cycle Based UAV Design Optimization Power Generation J. Wilson, M. Polanka, Air Force Institute Turbofan-Drive Assist N. Grannan, E. Gutmark, University of Propulsion System J. Page, R. Watson, Z. Ali, University of D. Waters, C. Cadou, University of of Technology, Wright-Patterson AFB, OH K. Okai, T. Shinohara, T. Himeno, T. Cincinnati, Cincinnati, OH N. Grannan, E. Gutmark, University of Cambridge, Cambridge, United Kingdom; Maryland, College Park, College Park, MD Watanabe, University of Tokyo, Tokyo, Cincinnati, Cincinnati, OH P. Hield, Rolls-Royce Group plc, Bristol, Japan; D. Masaki, T. Tagashira, Japan United Kingdom; P. Tucker, University of Aerospace Exploration Agency (JAXA), Cambridge, Cambridge, United Kingdom Tokyo, Japan; et al. Tuesday, 6 January 2015 129-HIS-2 The NACA Centennial: An Assessment Tallahassee 2 0930 - 1130 hrs Chaired by: T. CROUCH, National Air & Space Museum An invited panel discussion on the impact and inﬂuence of the National Advisory Committee for Aeronautics 100 years after the founding (March 3, 1915).

Roger Launius James Hansen Deborah Douglas William Barry NASM Auburn MIT NASA

Tuesday, 6 January 2015 130-HSABP-3 Pressure Gain Combustion - Rotating Detonation Engines I Emerald 3 88 Chaired by: D. MUSIELAK, University of Texas at Arlington and T. KAEMMING, Innovative Scientific Solutions Incorporated 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2015-0630 AIAA-2015-0631 AIAA-2015-0632 AIAA-2015-0633 AIAA-2015-0634 AIAA-2015-0635 Performance Evaluation of a Study of the Experimental Experimental Ignition Fuel Blending as a Means to Experimental Measurement of Development of a Rotating Rotating Detonation Engine with Performance of a Rotating Detonation Characteristics of a Rotating Achieve Initiation in a Rotating Detonation Cell Size in a Two- Detonation Engine Facility at the Conical-Shape Tail Engine with Nozzled Exhaust Flow Detonation Engine under Detonation Engine Dimensional Facility at High Pressures University of Cincinnati K. Ishihara, K. Matsuoka, J. Kasahara, Nagoya M. Fotia, Air Force Research Laboratory, Backpressured Conditions A. St. George, R. Driscoll, V. Anand, C. Babbie, P. King, Air Force Institute of A. St. George, R. Driscoll, D. Munday, University, Nagoya, Japan; A. Matsuo, Keio Wright-Patterson AFB, OH; T. Kaemming, J. M. Fotia, Air Force Research Laboratory, D. Munday, E. Gutmark, University of Technology, Wright-Patterson AFB, OH; E. Gutmark, University of Cincinnati, University, Yokohama, Japan; I. Funaki, Hoke, Innovative Scientific Solutions, Inc., Wright-Patterson AFB, OH; J. Hoke, Cincinnati, Cincinnati, OH C. Stevens, J. Hoke, F. Schauer, Air Force Cincinnati, OH Japan Aerospace Exploration Agency (JAXA), Dayton, OH; F. Schauer, Air Force Research Innovative Scientific Solutions, Inc., Research Laboratory, Wright-Patterson Sagamihara, Japan Laboratory, Wright-Patterson AFB, OH Dayton, OH; F. Schauer, Air Force Research AFB, OH Laboratory, Wright-Patterson AFB, OH Tuesday, 6 January 2015 131-HSABP-4 Numerical Analysis of High Speed Air-Breathing Propulsion Emerald 8 Chaired by: H. HASSAN, North Carolina State University and T. SMITH, Boeing Engineering Operations & Technology 0930 hrs 1000 hrs 1030 hrs AIAA-2015-0636 AIAA-2015-0637 AIAA-2015-0639 Simulating Turbulence and Mixing Hybrid Reynolds-Averaged / Performance Analysis of the in Supersonic Combustors Using Large Eddy Simulation of a Cavity Atlantis Dynamic Intake System Hybrid RANS/LES Flameholder; Assessment of S. Wilson, C. Johansen, University of D. Peterson, E. Hassan, Air Force Research Modeling Sensitivities Calgary, Calgary, Canada; V. Mravcak, Laboratory, Wright-Patterson AFB, OH R. Baurle, NASA Langley Research Center, Atlantis Research Labs Inc., Regina, Hampton, VA Canada Tuesday, 6 January 2015 132-ICC-1 C2 and Beyond: A Look into the Future of Complex Aerospace Command and Control Systems Osceola Ballroom 2 Chaired by: M. SOTAK, Kratos Defense and Security Solutions and J. MCEVER, The Johns Hopkins University Applied Physics Laboratory 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2015-0640 AIAA-2015-0641 AIAA-2015-0642 AIAA-2015-0643 AIAA-2015-0644 A System-of-Systems Approach Utilization of Wind Energy in Direct Adaptive Control for Infinite- MAR-CPS: Measurable Augmented A System-of-Systems Perspective for Assessing the Resilience of Optimal Guidance Strategies via Dimensional Symmetric Hyperbolic Reality for Prototyping Cyber- on Information Fusion Systems: Reconfigurable Command and Real-Time Control Methodologies Systems with Application to Physical Systems Architecture Representation and Control Networks K. Turkoglu, A. Mazzulla, San Jose State Controlled Wave-like Behavior S. Omidshafiei, A. Agha-Mohammadi, Y. Evaluation H. Tran, D. Mavris, Georgia Institute of University, San Jose, CA M. Balas, Embry-Riddle Aeronautical University, Chen, N. Üre, J. How, Massachusetts Institute A. Raz, D. DeLaurentis, Purdue University, Technology, Atlanta, GA Daytona Beach, FL; S. Frost, NASA Ames of Technology, Cambridge, MA; J. Vian, The West Lafayette, IN Research Center, Moffett Field, CA Boeing Company, Seattle, WA; et al. Tuesday, 6 January 2015 133-IS-5 Invited Panel Discussion - Autonomy Research for Civil Aviation: Toward a New Era of Flight Osceola Ballroom 3 0930 - 1230 hrs This panel will share their perspectives on autonomy research and development needs in civil aviation. Panelists represent a broad set of industrial and academic stakeholders in civil aviation with interests in manned and unmanned aircraft as well as air traffic management and National Airspace System operations. As members of the National Research Council (NRC) committee to develop a national research agenda for autonomy in civil aviation (released June 2014), panelists will each provide their views on the most critical autonomy barriers, research priorities, and potential benefits identified in this report followed by an open question and answer period with attendees. Panelists: Ella Atkins John-Paul Clarke Noah Flood Andrew Lacher University of Michigan Georgia Institute of Technology Delta Airlines MITRE

Tuesday, 6 January 2015

89 134-LEC-3 Adaptive Structures Lecture: Micro Aerial Vehicles (MAV): Challenges and Opportunities Osceola Ballroom A 0930 - 1030 hrs Chaired by: D. MCGOWAN, NASA Langley Research Center and E. WHITE, Boeing Engineering Operations & Technology

Inderjit Chopra Alfred Gessow and Distinguished University Professor University of Maryland Tuesday, 6 January 2015 135-MAT-5 ICME Panel Sun Ballroom D 0930 - 1230 hrs Chaired by: J. MATLIK, Rolls-Royce Corp; S. ARNOLD, University of Heidelberg, Germany and M. SANGID, Purdue University Integrating Computational Materials Engineering Practices into Design Systems and Structural Analysis - Requirements Definition & Implementation Opportunities Panelists: Charles Ward Dale Ball Steve Engelstad Ben Thacker H Alicia Kim Vasisht Venkatesh Joe Salvo Vikas Saraf Rob Gorham AFRL Lockheed Martin Lockheed Martin SouthwestResearch Institute Univeristy of Bath Pratt & Whitney GE Global Research ATI America Makes Coporation Corporation Tuesday, 6 January 2015 136-MAT-6 Nanostructured Materials II Sarasota 1 Chaired by: V. ROLLIN, Embry-Riddle Aeronautical University and D. POWELL 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2015-0645 AIAA-2015-0646 Oral Presentation AIAA-2015-0647 Graphene-Carbon Nanotubes Modeling of Fracture in Nano-Particle Aerospace Applications of Multiscale analysis of polymer Hybrids for Composite Materials Reinforced Polymers using the Nanomaterials for Sustainable nanocomposites considering A. Avila, G. Pereira, Federal University of Atomistic J-Integral Energy hyperelasto-plastic behavior Minas Gerais, Belo Horizonte, Brazil A. Akepati, S. Roy, V. Unnikrishnan, University S. Arepalli, National Institute of Aerospace, H. Shin, W. Kim, J. Ryu, S. Chang, M. Cho, of Alabama, Tuscaloosa, Tuscaloosa, AL Hampton, VA Seoul National University, Seoul, South Korea Tuesday, 6 January 2015 137-MDO-4 MDO: Supersonic Applications Sarasota 3 Chaired by: T. TAKAHASHI, Arizona State University and E. ALYANAK, AFRL/RQVC 0930 hrs 1000 hrs 1030 hrs AIAA-2015-0648 AIAA-2015-0649 AIAA-2015-0650 Multi-Parameter Performance High Fidelity, Nonlinear, Integrated Multi-Objective, Multidisciplinary Evaluation, the Next Step in Nozzle Installation Effects for Design Optimization of TSTO Space Conceptual Design Concept Numerical Propulsion System Planes with RBCC Engines Assessment Simulation T. Fujikawa, T. Tsuchiya, University of E. Alyanak, D. Allison, Air Force Research D. Allison, Optimal Flight Sciences, Tokyo, Bunkyo, Japan; S. Tomioka, Japan Laboratory, Wright-Patterson AFB, OH LLC, Dayton, OH; E. Alyanak, Air Force Aerospace Exploration Agency (JAXA), Research Laboratory, Wright-Patterson Kakuda, Japan AFB, OH; N. Bhagat, Universal Technology Corporation, Fairborn, OH 90 Tuesday, 6 January 2015 138-MST-5 Air Traffic Management II Sun Ballroom 1 Chaired by: J. SCHROEDER, Federal Aviation Administration 0930 hrs 1000 hrs 1030 hrs AIAA-2015-0651 AIAA-2015-0652 AIAA-2015-0653 Study on Validation and Application Continuous Descent Operation Arrival Metering Precision Study of Fuel-Burn Estimation Performance Improvement through T. Prevot, NASA Ames Research Center, Y. Nakamura, K. Kageyama, Electronic Flight Time Reduction Moffett Field, CA; J. Mercer, J. Homola, Navigation Research Institute, Tokyo, N. Takeichi, J. Ishihara, M. Sato, Nagoya S. Hunt, A. Gomez, N. Bienert, San Jose Japan University, Nagoya, Japan State University, Moffett Field, CA; et al. Tuesday, 6 January 2015 139-MST-6 Human Factors, Perception, and Cueing Sun Ballroom 2 Chaired by: F. CARDULLO, State University of NY 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2015-0654 AIAA-2015-0655 AIAA-2015-0656 AIAA-2015-0657 AIAA-2015-0658 Adaptive State Predictor Based Effects of False Tilt Cues on the An Algorithm to Improve Ground- Automatic Air Collision Avoidance Experimental Evaluation of RLS Human Operator Modeling on Training of Manual Roll Control Based Spatial Disorientation Training System Testing Algorithm for Identification of Longitudinal and Lateral Control Skills B. McGrath, University of Canberra, Canberra, C. Richardson, Air Force Test Center, Time-Varying Neuromuscular A. Trujillo, I. Gregory, NASA Langley P. Zaal, San Jose State University, San Australia; B. Lawson, Army Aeromedical Edwards AFB, CA; T. Hamilton, Air Force Response Research Center, Hampton, VA; L. Jose, CA; B. Sweet, NASA Ames Research Research Laboratory, Fort Rucker, AL; M. Life Cycle Management Center, Arlington, M. Olivari, F. Nieuwenhuizen, H. Bülthoff, Hempley, Northrop Grumman Corporation, Center, Moffett Field, CA Newman, National Aerospace Training and VA; T. Millet, M. Pacini, Air Force Test Max Planck for Biological Cybernetics, Hampton, VA Research Center (NASTAR), Southampton, Center, Edwards AFB, CA Tübingen, Germany; L. Pollini, University PA; A. Rupert, Army Aeromedical Research of Pisa, Pisa, Italy Laboratory, Fort Rucker, AL Tuesday, 6 January 2015 140-NDA-3 Uncertainty Quantification and Management I Osceola Ballroom 5 Chaired by: G. MODGIL, Rolls-Royce Corp and B. SMARSLOK, Air Force Reseach Laboratory 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2015-0659 AIAA-2015-0660 AIAA-2015-0661 AIAA-2015-0662 AIAA-2015-0663 AIAA-2015-0664 Calibration of Predictor Models Using Expected Information Gain Global Sensitivity Analysis for Using Bootstrap to Assess Sampling Uncertainty Quantification of a Uncertainty Quantification Using Multple Validation to Design Aerothermal Model System Response Prediction Using Uncertainty in Fatigue Crack Rectangular 5:1 Cylinder and Sensitivity Analysis of Experiments Calibration Experiments Auxiliary Variable Method Growth Life J. Witteveen, Center for Mathematics and Aeroservoelastic Stability for a L. Crespo, National Institute of Aerospace, D. Villanueva, Universal Technology C. Li, S. Mahadevan, Vanderbilt University, K. Bhachu, R. Haftka, N. Kim, University Computer Science (CWI), Amsterdam, Slender Flight Vehicle Hampton, VA; S. Kenny, D. Giesy, NASA Corporation, Dayton, OH; B. Smarslok, Nashville, TN of Florida, Gainesville, Gainesville, FL The Netherlands; P. Omrani, TNO, Delft, J. Tang, Z. Wu, C. Yang, Beihang Langley Research Center, Hampton, VA Air Force Research Laboratory, Wright- The Netherlands; A. Mariotti, M. Salvetti, University, Beijing, China Patterson AFB, OH University of Pisa, Pisa, Italy Tuesday, 6 January 2015 141-PANEL-3 Improving Business Skills and Business Processes for the Aerospace Technical Community Osceola Ballroom B 0930 - 1130 hrs Moderator: Andy White, Director, University of Tennessee Aerospace & Defense Business Institute Panelists: Jeff Babione Robert Lightfoot Alex Miller Bobby Smart Vice President and Deputy GM, Joint Strike Fighter Program Associate Administrator William B. Stokely Chair in Management and former Associate Dean Deputy Assistant Secretary Lockheed Martin Corporation NASA UT Haslam College of Business Administration Air Force Acquisition Integration

Tuesday, 6 January 2015 142-PC-9 Advanced Combustion Concepts II Emerald 5

91 Chaired by: W. SUN, Georgia Institute of Technology and R. PITZ, Vanderbilt University 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2015-0665 AIAA-2015-0666 AIAA-2015-0667 AIAA-2015-0668 AIAA-2015-0669 Low temperature oxidation of Plasma Assisted MILD Combustion On the Role of Translational Energy balance in surface nanosecond The Effect of Ozone Addition on methane in a nanosecond pulsed T. Wada, J. Lefkowitz, Y. Ju, Princeton Nonequilibrium for Hydrogen Air dielectric barrier discharge. Flame Propagation plasma discharge University, Princeton, NJ Plasma Assisted Ignition Plasma-assisted ignition of heavy X. Gao, Y. Zhang, S. Adusumilli, J. J. Lefkowitz, P. Guo, A. Rousso, Y. Ju, A. Starikovskiy, Princeton University, hydrocarbons at high pressures Seitzman, W. Sun, Georgia Institute of Princeton University, Princeton, NJ Princeton, NJ S. Shcherbanev, S. Stepanyan, École Technology, Atlanta, GA; T. Ombrello, Polytechnique, Palaiseau, France; M. Air Force Research Laboratory, Wright- Boumehdi, P. Desgroux, G. Vanhove, Lille Patterson AFB, OH; et al. University of Science and Technology, Lille, France; S. Starikovskaia, École Polytechnique, Palaiseau, France Tuesday, 6 January 2015 143-PC-10 Turbulent Combustion III Emerald 7 Chaired by: A. STEINBERG, University of Toronto and Y. JU, Princeton University 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2015-0670 AIAA-2015-0671 AIAA-2015-0672 AIAA-2015-0673 AIAA-2015-0674 High-Speed Measurements in Large Scale Dynamics and Statistics Simulation Using Flamelet Addition of Ammonia to a Bluff-Body Strain Effects in Partially Premixed Partially-Premixed Swirl Flames at of the Time-Varying Temperature Radiation Modeling Stabilized Flame and Its Effect on NOx Methane-air Jet Flames Elevated Temperature and Pressure Field in Turbulent Non-Premixed J. Doom, General Electric Company, Emissions and Static Stability W. Calhoon, K. Kemenov, Combustion C. Slabaugh, Purdue University, West Jet Flames Niskayuna, NY B. Huelskamp, Innovative Scientiﬁc Solutions, Research and Flow Technology, Inc., Lafayette, IN; I. Boxx, S. Werner, W. T. McManus, J. Sutton, Ohio State Inc., Dayton, OH; P. Gokulakrishnan, Huntsville, AL Meier, German Aerospace Center (DLR), University, Columbus, OH Combustion Science and Engineering, Inc., Stuttgart, Germany; R. Lucht, Purdue Columbia, MD; C. Klingshirn, University of University, West Lafayette, IN Dayton Research Institute, Dayton, OH; N. Kuprowicz, V. Belovich, Air Force Research Laboratory, Wright-Patterson AFB, OH Tuesday, 6 January 2015 144-PDL-2 Aero-Optics Emerald 2 Chaired by: M. STANEK, AFRL/RQVI and M. RENNIE, University of Notre Dame 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2015-0675 AIAA-2015-0676 AIAA-2015-0677 AIAA-2015-0678 AIAA-2015-0679 Airborne Aero-Optics Laboratory - Aero-Optical Investigation of Global Unsteady Pressure Fields Computation of the Aero-Optical A Latency-Tolerant Architecture for Transonic (AAOL-T) Transonic Flow Features And Shock Over Turrets In-Flight Effect of a Helicopter Rotor Wake Airborne Adaptive Optic Systems E. Jumper, S. Gordeyev, D. Cavalieri, P. Rollins, Dynamics on Hemisphere-On- N. De Lucca, S. Gordeyev, E. Jumper, Using Unsteady RANS and LES W. Burns, E. Jumper, S. Gordeyev, University of Notre Dame, Notre Dame, IN; M. Cylinder Turrets University of Notre Dame, Notre Dame, IN R. Kelly, A. Jemcov, M. Rennie, E. Jumper, University of Notre Dame, Notre Dame, IN Whiteley, MZA Associates Corporation, Dayton, N. De Lucca, S. Gordeyev, J. Morrida, E. University of Notre Dame, Notre Dame, IA; OH; M. Krizo, Air Force Institute of Technology, Jumper, University of Notre Dame, Notre M. Whiteley, D. Goorskey, MZA Associates Wright-Patterson AFB, OH Dame, IN Corporation, Dayton, OH Tuesday, 6 January 2015 145-SCS-3 Packaging and Deployment of Spacecraft Structures Osceola Ballroom 4 Chaired by: W. REYNOLDS, Air Force Research Laboratory and G. GRESCHIK, TentGuild Engineering Co 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2015-0680 AIAA-2015-0681 AIAA-2015-0682 AIAA-2015-0683 Wrapping Fold and Deployment An Examination of Crease Removal Wrapping Thick Membranes with A Basic Construction Concept for Characteristics of Boom-Membrane in Rigidizable Inﬂatable Metal- Slipping Folds Space Structure Systems Using Integrated Space Structures Polymer Laminate Cylinders M. Arya, N. Lee, S. Pellegrino, California Active Connecting Elements H. Sakamoto, H. Furuya, Tokyo Institute G. Secheli, A. Viquerat, V. Lappas, Institute of Technology, Pasadena, CA M. Natori, Self, Sagamihara, Japan; M. of Technology, Tokyo, Japan; Y. Satou, University of Surrey, Guildford, United Nagasawa, J. Yamada, A. Okuno, H. N. Okuizumi, M. Takai, M. Natori, Japan Kingdom Yamakawa, Waseda University, Shinjyuku, Aerospace Exploration Agency (JAXA), Japan; K. Higuchi, Muroran Institute of

92 Kanagawa, Japan Technology, Muroran, Japan Tuesday, 6 January 2015 146-SD-6 Supersonic/Hypersonic Systems I Tampa 2 Chaired by: B. GLAZ, U. S. Army Research Laboratory (APG) and N. FALKIEWICZ, MIT Lincoln Laboratory 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2015-0684 AIAA-2015-0685 AIAA-2015-0686 AIAA-2015-0687 AIAA-2015-0688 An Overview of the NASA High Speed Response of a Panel to Shock Loosely Coupled Time-Marching Rapid Prediction of Unsteady Characterization of Structural ASE Project: Aeroelastic Analyses of a Impingement: Modeling and of Fluid-Thermal-Structural Aeroelastic Loads in Shock- Response to Hypersonic Boundary Low-Boom Supersonic Conﬁguration Comparison with Experiments - Part 2 Interactions with Time-Accurate CFD Dominated Flows Layer Transition W. Silva, NASA Langley Research Center, A. Gogulapati, R. Deshmukh, J. McNamara, B. Miller, J. McNamara, Ohio State K. Brouwer, A. Crowell, J. McNamara, Ohio Z. Riley, R. Deshmukh, B. Miller, J. Hampton, VA; A. De La Garza, P. Zink, E. Ohio State University, Columbus, OH; V. University, Columbus, OH State University, Columbus, OH McNamara, Ohio State University, Bounajem, J. Johnson, Lockheed Martin Vyas, X. Wang, M. Mignolet, Arizona State Columbus, OH Corporation, Fort Worth, TX; M. Buonanno, University, Tempe, AZ; et al. Lockheed Martin Corporation, Palmdale, CA; et al. Tuesday, 6 January 2015 147-SD-7 Cable/Beam Modeling I Tampa 3 Chaired by: C. HEBERT, Sierra Nevada Corporation and Z. SOTOUDEH, Rensselaer Polytechnic Institute 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2015-0689 AIAA-2015-0690 AIAA-2015-0691 AIAA-2015-0692 AIAA-2015-0693 AIAA-2015-0694 Nonlinear Normal Modes in Finite Experimental and Theoretical Non-linear Sectional Analysis Nonlinear Geometric Reduced Investigation of a Dynamic Finite Application of Transfer Matrix Element Model Validation of Analysis of Cabled Beams of Composite Beams with Finite Order Model for the Response of a Element Model for the Nonlinear Approach to Modeling and Geometrically Nonlinear Flat and K. Spak, Virginia Polytechnic Institute and Deformation and Hyperelastic Beam with a Piezoelectric Actuator Response of Fatigue Cracked Decentralized Control of Lattice- Curved Beams State University, Blacksburg, VA; G. Agnes, Materials V. Vyas, X. Wang, A. Jain, M. Mignolet, Structures based Structures D. Ehrhardt, M. Allen, R. Kuether, Jet Propulsion Laboratory, California F. Jiang, W. Yu, Purdue University, West Arizona State University, Tempe, AZ P. Cooley, J. Slater, Wright State N. Cramer, University of California, Santa University of Wisconsin, Madison, Institute of Technology, Pasadena, CA; D. Lafayette, IN University, Dayton, OH Cruz, Santa Cruz, CA; S. Swei, K. Cheung, Madison, WI Inman, University of Michigan, Ann Arbor, NASA Ames Research Center, Moffett Ann Arbor, MI Field, CA; M. Teodorescu, University of California, Santa Cruz, Santa Cruz, CA Tuesday, 6 January 2015 148-STR-7 Special Session: Challenges in the Design of Joined Wings I Tampa 1 Chaired by: L. DEMASI, San Diego State University College of Engineering and A. PALAZOTTO, AFIT 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2015-0695 AIAA-2015-0696 AIAA-2015-0697 AIAA-2015-0698 AIAA-2015-0699 AIAA-2015-0700 Aerodynamic Optimization Trade Performance Based MDO of a Joined- Minimum Induced Drag Theorems Minimum Induced Drag Theorems Reduced Order Methods and Design of a prototype of light Study of a Box-Wing Aircraft Wing Regional Transport Aircraft (For for Joined Wings, Closed systems, for Joined Wings, Closed Systems, Algorithms for Structurally amphibious PrandtlPlane Conﬁguration Challenges in the Design of Joined and Generic Biwings: Theory and Generic Biwings: Results Nonlinear Joined Wings A. Frediani, University of Pisa, Pisa, Italy; H. Gagnon, D. Zingg, University of Wings SPECIAL SESSION) L. Demasi, San Diego State University, L. Demasi, San Diego State University, San N. Teunisse, P. Tiso, Delft University of V. Cipolla, SkyBox Engineering, Pisa, Italy; Toronto, Toronto, Canada A. Suleman, University of Victoria, Victoria, San Diego, CA; G. Monegato, Technical Diego, CA; G. Monegato, Technical University Technology, Delft, The Netherlands; L. F. Oliviero, University of Pisa, Pisa, Italy

93 Canada; F. Afonso, J. Vale, F. Lau, Technical University of Turin, Turin, Italy; A. Dipace, of Turin, Turin, Italy; E. Rizzo, SkyBox Demasi, R. Cavallaro, San Diego State University of Lisbon, Lisbon, Portugal University of Pisa, Pisa, Italy; R. Cavallaro, Engineering, Pisa, Italy; R. Cavallaro, San University, San Diego, CA San Diego State University, San Diego, CA Diego State University, San Diego, CA; A. Dipace, University of Pisa, Pisa, Italy Tuesday, 6 January 2015 149-STR-8 Special Sessions in Honor of Prof. Harry H. Hilton II Tallahassee 3 Chaired by: O. ZHUPANSKA, The University of Iowa; P. MARZOCCA, Clarkson University and R. SIERAKOWSKI, Air Force Reseach Laboratory 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2015-0701 AIAA-2015-0702 AIAA-2015-0703 AIAA-2015-0704 AIAA-2015-0705 AIAA-2015-0706 Molecular Dynamics and Finite On the Closed-Form Constitutive Multiscale Modeling of the Radar Flight Vehicle Structural Design Multiscale Modeling of a Further Results on the Use of Element Investigation of Polymer Relations for Damageable Elasto- Signature of a Composite Aircraft Processes for a Common Bulkhead Mechanophore-embedded Material Tailoring to Improve Interphase Effects on Effective Viscoplastic Materials K. Zhang, J. Jin, P. Geubelle, University of and an MPCV Spacecraft Adapter Nanocomposite for Damage Buckling Capacity of Elliptical Stiffness of Wavy Aligned Carbon L. Zhang, W. Yu, Purdue University, West Illinois, Urbana-Champaign, Urbana, IL P. Aggarwal, P. Hull, NASA Marshall Space Initiation Detection Composite Cylinders Nanotube Composites Lafayette, IN Flight Center, Huntsville, AL B. Koo, Y. Liu, A. Chattopadhyay, L. Dai, M. Hyer, Virginia Polytechnic Institute and Y. Atescan, Istanbul Technical University, Arizona State University, Tempe, AZ State University, Blacksburg, VA Istanbul, Turkey; C. Hadden, Michigan Technological University, Houghton, MI; B. Wardle, Massachusetts Institute of Technology, Cambridge, MA; G. Odegard, Michigan Technological University, Houghton, MI; H. Cebeci, Istanbul Technical University, Istanbul, Turkey Tuesday, 6 January 2015 150-TP-4 Heat Pipes/Heat Transfer I Sun Ballroom B Chaired by: E. SHORT, Raytheon Company and M. HOWARD, Sandia National Laboratories 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2015-0707 AIAA-2015-0708 AIAA-2015-0709 AIAA-2015-0710 AIAA-2015-0711 AIAA-2015-0712 Analytical Model for Transient Loop Non-Intrusive Fluid Flow Measurement Multiple-Evaporator Loop Heat Pipe On the Modelling of Evaporating Numerical Simulation of a Experimental Assessment of Heat Pipe Operation Method for Loop Heat Pipes T. Hoang, TTH Research, Inc., Clifton, VA; Sprays Impinging onto Solid stationery 3D Cooling Channel Vapour Chamber Heater Spreader T. Hoang, TTH Research, Inc., Clifton, VA; T. Hoang, TTH Research, Inc., Clifton, VA; J. Ku, NASA Goddard Space Flight Center, Surfaces using periodic condition Implementation in Avionic Cooling R. Baldauff, Naval Research Laboratory, R. Baldauff, K. Cheung, Naval Research Greenbelt, MD C. Rodrigues, J. Barata, A. Silva, University H. Alhajeri, College of Technological Studies, A. Jones, R. Chen, Loughborough Washington, DC; D. Mahony, Praxis, Inc., Laboratory, Washington, DC; D. Mahony, of Beira Interior, Covilha, Portugal Kuwait, Kuwait; A. Addali, Cranfield University, University, Loughborough, United Kingdom Alexandria, VA Praxis, Inc., Alexandria, VA Cranfield, United Kingdom Tuesday, 6 January 2015 151-UMS-2 Unmanned Systems: Technologies and Applications I Osceola Ballroom 1 Chaired by: B. ARGROW, University of Colorado Boulder 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2015-0713 AIAA-2015-0714 AIAA-2015-0715 AIAA-2015-0716 AIAA-2015-0717 AIAA-2015-0718 Motion Analysis of Captive Platform Control for Suppressing Roll Motion Autonomous Navigation of UAV Development of a Low-Cost Autonomous Navigation System Architecture, Development System Constructed from Airship of Outdoor Blimp Robots for through GPS-Denied Indoor Experimental Quadcopter Testbed of a Quadrotor in Indoor and Results of the Embry-Riddle and Tether Disaster Surveillance Environment with Obstacles using an Arduino controller for Environments for Surveillance and Aeronautical University Maritime K. Chiba, S. Satori, R. Mitsuhashi, H. Saiki, National Research Institute of Fire E. Schnipke, S. Reidling, J. Meiring, W. Video Surveillance Reconnaissance RobotX Platform Hokkaido University of Science, Sapporo, and Disaster, Chofu, Japan; T. Kobayashi, T. Jeffers, M. Hashemi, R. Tan, University of K. Turkoglu, A. Ji, San Jose State S. Bhandari, S. Viska, H. Shah, C. Chen, C. Hockley, T. Zuercher, C. Kennedy, G. Japan; J. Sasaki, R. Akiba, Hokkaido Fukao, T. Urakubo, Kobe University, Kobe, Toledo, Toledo, OH; et al. University, San Jose, CA G. Tonini, S. Kline, California Polytechnic Gamble, H. Patel, P. Currier, Embry-Riddle Aerospace Science and Technology Japan; K. Araiba, H. Amano, National Research State University, Pomona, CA Aeronautical University, Daytona Beach, Incubation Center, Sapporo, Japan Institute of Fire and Disaster, Chofu, Japan FL; et al. 94 Tuesday, 6 January 2015 152-WE-5 Vertical Axis Wind Turbine (VAWT) Research Emerald 4 Chaired by: D. GRIFFITH and C. SIMAO FERREIRA 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2015-0719 AIAA-2015-0720 AIAA-2015-0721 AIAA-2015-0722 AIAA-2015-0723 Combined structural optimization Post-stall airfoil performance and Efficient Aerodynamic Shape Airfoil optimization for stall regulated Dynamic Stall on Vertical Axis Wind and aeroelastic analysis of a vertical-axis wind turbines Optimization of VAWT Airfoil and vertical axis wind turbines Turbines Vertical Axis Wind Turbine J. Graham, J. Peiro, J. Rainbird, Imperial Its Validation C. Simao Ferreira, Delft University of D. Casteleim, G. Tescione, D. Ragni, B. Roscher, C. Simao Ferreira, L. Bernhammer, College London, London, United Kingdom W. Yamazaki, Y. Arakawa, Nagaoka Technology, Delft, The Netherlands; M. C. Simao Ferreira, Delft University of Delft University of Technology, Delft, The University of Technology, Nagaoka, Japan Barone, Sandia National Laboratories, Technology, Delft, The Netherlands Netherlands; H. Madsen, Technical University Albuquerque, NM; A. Zanon, Austrian Institute of Denmark, Roskilde, Denmark; D. Griffith, of Technology, Vienna, Austria; R. Kemp, Sandia National Laboratories, Albuquerque, Delft University of Technology, Delft, The NM; B. Stoevesandt, Fraunhofer, Oldenburg, Netherlands; P. Giannattasio, University of Germany Udine, Udine, Italy Tuesday, 6 January 2015 153-WE-6 Wind Farm and Turbine Wake Interactions II Emerald 6 Chaired by: D. MANIACI, Sandia National Laboratories and T. HERGES 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2015-0724 AIAA-2015-0725 AIAA-2015-0726 AIAA-2015-0727 AIAA-2015-0728 AIAA-2015-0729 A Comparison of the Dynamic Wake A Modeling Framework for Wind A Comparison of the NREL 5-MW Actuator Line Wind Turbine A Parabolic Method without Preliminary Study on Wake Meandering Model, Large-Eddy Farm Analysis: Wind Turbine Wake Wake Characteristics Using Both Simulations in Atmospheric Pressure Approximations for Wind Interaction Effects Using a Free Simulation, and Field Data at the Interactions SOWFA and OVERFLOW2 Turbulent Flows using Spectral Turbines Vortex Wake Model Egmond aan Zee Offshore Wind Plant A. Ghate, S. Lele, Stanford University, E. Anderson, R. Chow, C. Van Dam, Element Method A. Mittal, W. Briley, L. Taylor, K. Sreenivas, K. Shaler, J. McNamara, K. Kecskemety, M. Churchfield, S. Lee, P. Moriarty, National Stanford, CA University of California, Davis, Davis, CA T. Chatterjee, Y. Peet, Arizona State University of Tennessee, Chattanooga, Ohio State University, Columbus, OH Renewable Energy Laboratory, Golden, CO; Y. University, Tempe, AZ Chattanooga, TN Hao, M. Lackner, University of Massachusetts, Amherst, Amherst, MA; R. Barthelmie, Cornell University, Ithaca, NY; et al. Tuesday, 6 January 2015 154-AS-2 Shape Memory Alloy Applications Osceola Ballroom 6 Chaired by: D. LAGOUDAS, Texas A&M University and J. LENG 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2015-0730 AIAA-2015-0731 AIAA-2015-0732 AIAA-2015-0733 Development of a SMA-Based, Aero−structural Optimization Design and Testing of a Shape Development of a Twisting Wing Slat-Gap Filler for Airframe Noise of Shape Memory Alloy-based Memory Alloy Buoyancy Engine for Powered by a Shape Memory Alloy Reduction Wing Morphing via a Class/Shape Unmanned Underwater Vehicles Actuator T. Turner, NASA Langley Research Center, Transformation Approach A. Angilella, F. Gandhi, Rensselaer C. Stein, D. Hartl, L. Hodge, J. Mabe, Hampton, VA; D. Long, Analytical P. Leal, Federal University of Rio de Janeiro, Polytechnic Institute, Troy, NY; T. Miller, J. Herrington, R. Saunders, Texas A&M

95 Mechanics Associates, Inc., Hampton, VA Rio de Janeiro, Brazil; D. Hartl, C. Bertagne, Pennsylvania State University, University University, College Station, TX Texas A&M University, College Station, TX Park, PA Tuesday, 6 January 2015 155-LUNCH-2 Recognition Luncheon: Celebrating Achievements in Aerospace Sciences and Information Systems Osceola Ballroom CD 1230 - 1400 hrs Tuesday, 6 January 2015 156-AA-5 Jet Noise Measurements II Miami 2 Chaired by: C. BROWN, NASA Glenn Research Center 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2015-0734 AIAA-2015-0735 AIAA-2015-0736 AIAA-2015-0737 AIAA-2015-0738 AIAA-2015-0739 An Investigation of Transonic Measuring Jet Noise Source A Study of the Noise Source The Properties and Localizations of Comparison of Spatial and Investigation of “Loud” Modes in a Resonance in a Mach 2.2 Round Locations with Acoustic Mechanisms in an Excited Mach 0.9 Acoustic Sources of High Speed Jets Temporal Resolution on High Speed High-Speed Jet to Identify Noise- Convergent-Divergent Nozzle Beamforming Jet - Complementary Experimental P. Kan, J. Lewalle, Z. Berger, M. Glauser, Axisymmetric Jets Producing Events V. Dippold, K. Zaman, NASA Glenn N. Breen, K. Ahuja, Georgia Institute of and Computational Analysis Syracuse University, Syracuse, NY M. Berry, A. Magstadt, Z. Berger, P. Shea, Z. Berger, M. Berry, P. Shea, M. Glauser, Research Center, Cleveland, OH Technology, Atlanta, GA M. Crawley, R. Speth, M. Samimy, D. M. Glauser, Syracuse University, Syracuse, P. Kan, J. Lewalle, Syracuse University, Gaitonde, Ohio State University, Columbus, OH NY; C. Ruscher, Spectral Energies, LLC, Syracuse, NY; et al. Dayton, OH; et al. Tuesday, 6 January 2015 157-AA-6 General Acoustics Sun Ballroom C Chaired by: J. PETERS, Rolls-Royce Corp 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2015-0740 AIAA-2015-0741 AIAA-2015-0742 AIAA-2015-0743 AIAA-2015-0744 AIAA-2015-0745 Phase-Based Adaptive Estimation Assessment of Geometry and Normal Incidence Acoustic A Multi-Stage Surrogate Modeling Multiple Aircraft Approach Path Analysis of sonic boom propagation of Magnitude-Squared Coherence In-Flow Effects on Contra-Rotating Transmission Loss of Perforated Approach to Examine Vehicle-Level Optimization for Noise Abatement based on the KZK equation Between Turbofan Internal Sensors Open Rotor Broadband Noise Plates Subject to Bias Flow Technology Impacts at the Airport- Considering the Influence of J. Takeno, T. Misaka, K. Shimoyama, and Far-Field Microphone Signals Predictions V. Phong, D. Papamoschou, University of Level Meteorological Conditions on Sound S. Obayashi, Tohoku University, Sendai, J. Miles, NASA Glenn Research Center, N. Zawodny, D. Nark, D. Boyd, NASA California, Irvine, Irvine, CA J. Bernardo, C. Besson, H. Pfaender, J. Propagation Japan Cleveland, OH Langley Research Center, Hampton, VA Schutte, D. Mavris, Georgia Institute of A. Andreeva-Mori, H. Ishii, Japan Aerospace Technology, Atlanta, GA Exploration Agency (JAXA), Tokyo, Japan Tuesday, 6 January 2015 158-AFM-7 AFM Best Student Paper Competition III Captiva 1 Chaired by: F. PRIOLO, Millennium Engineering and Integration Company 1400 hrs 1430 hrs 1500 hrs 1530 hrs AIAA-2015-0746 AIAA-2015-0747 AIAA-2015-0748 AIAA-2015-0749 Suppression of Wing Rock in Quadrotor System Identification Non-Iterative Adaptive Limit and Wing Sensor Placement for Gust Slender Delta Wing by Horizontal Using the Multivariate Multiplex Control Margin Estimation with Disturbance Rejection Strakes B-Spline Concurrent Learning L. Castano, University of Maryland, S. Bakaul, Y. Wang, W. Guangxing, T. Visser, C. de Visser, E. Van Kampen, G. Gursoy, I. Yavrucuk, Middle East College Park, College Park, MD; S. Airoldi, Beihang University, Beijing, China Delft University of Technology, Delft, The Technical University, Ankara, Turkey T. McKenna, Aurora Flight Sciences, Netherlands Manassas, VA; J. Humbert, University of Maryland, College Park, College Park, MD 96 Tuesday, 6 January 2015 159-AFM-8 Aircraft Flight Dynamics, Handling Qualities and Performance III Captiva 2 Chaired by: D. MURRI, NASA Langley Research Center and B. ALSTROM, International Test Pilot School 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2015-0750 AIAA-2015-0751 AIAA-2015-0752 AIAA-2015-0754 AIAA-2015-0755 AIAA-2015-0756 Evaluation of Aircraft Model Upset The Effects of Stick Force Gradient Improved Obstacle Clearance Power Efficient Trim Solutions for Aircraft Input Prediction in the Wind Field Estimation and Its Behaviour Using Wind Tunnel on Pilot Mental Demand Capability of a Transport Aircraft Using the Hybrid Wing Body in Approach Presence of Spatially Varying Wind Utilization in Trajectory Prediction Manoeuvre Rig M. Bromfield, Coventry University, a Modified Climb-Out Flight Profile Conditions Field J. Kampoon, W. Okolo, S. Erturk, O. S. Araujo-Estrada, M. Lowenberg, S. Coventry, United Kingdom; G. Gratton, M. L. Bays, Aero Performance Engineering, LLC, D. Garmendia, D. Mavris, Georgia Institute J. Kampoon, W. Okolo, S. Erturk, O. Daskiran, A. Dogan, University of Texas, Neilld, University of Bristol, Bristol, Young, Brunel University, Uxbridge, United Kennesaw, GA; K. Halpin, Elite Electronic of Technology, Atlanta, GA Daskiran, A. Dogan, University of Texas, Arlington, Arlington, TX United Kingdom; M. Goman, De Montfort Kingdom Engineering, Inc., Downers Grove, IL Arlington, Arlington, TX University, Leicester, United Kingdom Tuesday, 6 January 2015 160-APA-15 Aerodynamic Design: Analysis, Methodologies & Optimization Techniques II Destin 1 Chaired by: J. LATZ, Northrop Grumman Aerospace Systems and G. ZHA, University of Miami 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs AIAA-2015-0757 AIAA-2015-0758 AIAA-2015-0759 AIAA-2015-0760 AIAA-2015-0761 AIAA-2015-0762 AIAA-2015-0763 Optimization of Waverider-Derived Shape Optimization of an Airfoil Surrogate-Based Airfoil Design Sensitivity Analysis for Uncertainty Review of Aerofoil Optimal Domain Element Shapes Multi-objective aerodynamic Crew Reentry Vehicles using a in Ground Effect for Application to with Multi-Level Optimization and Propagation and Robust Design Parameterisation Methods for for Free-Form Aerodynamic Shape optimization of supercritical Rapid Aerodynamics Analysis WIG Craft Adjoint Sensitivity D. Papadimitriou, C. Papadimitriou, Aerodynamic Shape Optimisation Control wing with substantial pressure Approach Y. He, Washington University in St. Louis, Y. Tesfahunegn, S. Koziel, L. Leifsson, University of Thessaly, Volos, Greece D. Masters, University of Bristol, Bristol, D. Poole, C. Allen, T. Rendall, University of constraints M. Lobbia, The Aerospace Corporation, El St. Louis, MO; Q. Qu, Beihang University, Reykjavik University, Reykjavik, Iceland United Kingdom; N. Taylor, MBDA, Bristol, Bristol, Bristol, United Kingdom Z. Tong, Y. Zhang, H. Chen, Tsinghua Segundo, CA Beijing, China; R. Agarwal, Washington United Kingdom; T. Rendall, C. Allen, D. Poole, University, Beijing, China University in St. Louis, St. Louis, MO University of Bristol, Bristol, United Kingdom Tuesday, 6 January 2015 161-APA-16 Aerodynamic-Structural Dynamics Interaction II Destin 2 Chaired by: C. PASILIAO, AFRL/RWWV and C. SHENG, University of Toledo 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2015-0764 AIAA-2015-0765 AIAA-2015-0766 AIAA-2015-0767 AIAA-2015-0768 AIAA-2015-0769 Combined translational and An Efficient Time-variant Fluid- Nonlinear Aeroelastic Analysis of Comparison of Viscous and Inviscid Wing Flutter Computation Using Coupling of the Edge CFD Solver rotational galloping of square Structure Interaction Analysis based High Aspect-Ratio Wings Using Unsteady Aerodynamic Loads for Modified Spectral Volume Method with External Solvers cylinders in cross-flow at low on Coupling in Frequency Domain Immersed Boundary Technique Aeroelastic Analyses for Hybrid Unstructured Mesh A. Jirasek, O. Amoignon, P. Eliasson, Reynolds numbers S. Yi, Korea Advanced Institute of Science and K. Gobal, R. Grandhi, Wright State R. Ihi, Technological Institute of Y. Sawaki, Tohoku University, Sendai, Swedish Defense Research Agency (FOI), B. Battaglia, Paris Institute of Technology, Technology, Daejeon, Korea (the Republic of); University, Dayton, OH Aeronautics (ITA), São José dos Campos, Japan; T. Haga, Japan Aerospace Stockholm, Sweden Palaiseau, France; S. Etienne, A. Hay, D. S. Choi, D. Im, Virginia Polytechnic Institute Brazil; J. Azevedo, Aeronautics and Space Exploration Agency (JAXA), Sagamihara, Pelletier, École Polytechnique de Montréal, and State University, Blacksburg, VA; D. Lee, Institute (IAE), São José dos Campos, Japan; Y. Ogino, K. Sawada, Tohoku Montréal, Canada Korea Advanced Institute of Science and Brazil University, Sendai, Japan Technology, Daejeon, South Korea Tuesday, 6 January 2015 162-APA-17 Airfoil/Wing/Configuration Aerodynamics I Naples 2 Chaired by: M. POST, USAF Academy and J. MURRAY, Sandia National Laboratories 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs AIAA-2015-0770 AIAA-2015-0771 AIAA-2015-0772 AIAA-2015-0773 AIAA-2015-0774 Surrogates for the Aerodynamic Computational Aerodynamic Conceptual Design of an Electric Computed Effect of Wing Tip Experimental and Numerical Coefficients of Supersonic Airfoils Analysis of Annular Wing Airplane Utilizing Co-Flow Jet Flow Configuration on Wing Load Research on Aerodynamic M. Ahmed, Military Technical College, Unmanned Aerial Vehicle Control Characteristics of a High Speed Characteristics of Rectangular Fin Cairo, Egypt A. Kanoria, K. Panchal, M. Damodaran, A. Lefebvre, G. Zha, University of Miami, Aircraft Mounted Vertically over the Wing Indian Institute of Technology Coral Gables, FL J. Masud, O. Khan, Air University, T. Omori, Y. Sunada, T. Imamura,

97 Gandhinagar, Ahmedabad, India Islamabad, Pakistan University of Tokyo, Bunkyo, Japan Tuesday, 6 January 2015 163-APA-18 Special Session: Space Launch System (SLS) II Naples 1 Chaired by: K. ABDOL-HAMID, NASA Langley Research Center and J. PINIER, NASA Langley Research Center 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2015-0775 AIAA-2015-0776 AIAA-2015-0777 AIAA-2015-0778 AIAA-2015-0779 AIAA-2015-0780 Space Launch System Liftoff Results from DES Simulations of Reduced-order Model for NASA CFD Simulations of the Aerodynamic Modeling and Development of an Aerodynamic and Transition Aerodynamic an SLS Variant at Liftoff Conditions Space Launch System Liftoff Space Launch System Ascent Database Development of the Database for the SLS Service Characterization in the NASA Langley with Comparison to Experiment Aerodynamics Aerodynamics and Booster Space Launch System Booster Module Panel Jettison Event 14x22’ Subsonic Wind Tunnel S. Krist, F. Ghaffari, NASA Langley H. Carlson, R. Verberg, Clear Science Separation Separation Utilizing Inviscid CFD and MATLAB J. Pinier, G. Erickson, J. Paulson, W. Tomek, Research Center, Hampton, VA Corporation, Harford, NY S. Rogers, D. Dalle, W. Chan, NASA Ames B. Pamadi, J. Pei, C. Gumbert, L. Green, L. Hall, M. Applebaum, W. Eppard, D. D. Bennett, NASA Langley Research Center, Research Center, Moffett Field, CA NASA Langley Research Center, Hampton, Purinton, NASA Marshall Space Flight Hampton, VA; J. Blevins, NASA Marshall Space VA; J. Housman, J. Onufer, NASA Ames Center, Huntsville, AL Flight Center, Huntsville, AL Research Center, Moffett Field, CA; et al. Tuesday, 6 January 2015 164-APA-19/FD-19 Flow Control: Fluidic Oscillators Sun Ballroom A Chaired by: E. WHALEN, Boeing Engineering Operations & Technology and D. LACY, Boeing Commercial Airplanes 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2015-0781 AIAA-2015-0782 AIAA-2015-0783 AIAA-2015-0784 AIAA-2015-0785 AIAA-2015-0786 Experimental Comparison between Experimental Investigation of Control of Separation on a Swept Performance Enhancement of Flow Separation Control on a Experimental Investigation of the the Flow Field of Two Common Compressibility Effects in a Fluidic Wing using Fluidic Oscillators a Full-Scale Vertical Tail Model Full-Scale Vertical Tail Model using Flow Field behind a Bluff Body Fluidic Oscillator Designs Oscillator P. Tewes, L. Taubert, University of Arizona, Equipped with Active Flow Control Sweeping Jet Actuators Equipped with Fluidic Oscillators F. Ostermann, Technical University of F. von Gosen, F. Ostermann, Technical Tucson, Tucson, AZ E. Whalen, The Boeing Company, Hazelwood, M. Andino, J. Lin, A. Washburn, NASA Langley H. Schmidt, Technical University of Berlin, Berlin, Berlin, Germany; R. Woszidlo, University of Berlin, Berlin, Germany; R. MO; D. Lacy, The Boeing Company, Everett, Research Center, Hampton, VA; E. Whalen, Berlin, Germany; R. Woszidlo, University University of Kansas, Lawrence, Lawrence, Woszidlo, University of Kansas, Lawrence, WA; J. Lin, M. Andino, A. Washburn, NASA The Boeing Company, Hazelwood, MO; of Kansas, Lawrence, Lawrence, KS; C. KS; C. Nayeri, C. Paschereit, Technical Lawrence, KS; C. Nayeri, C. Paschereit, Langley Research Center, Hampton, VA; E. Graff, California Institute of Technology, Nayeri, C. Paschereit, Technical University University of Berlin, Berlin, Germany Technical University of Berlin, Berlin, E. Graff, California Institute of Technology, Pasadena, CA; I. Wygnanski, University of of Berlin, Berlin, Germany Germany Pasadena, CA; et al. Arizona, Tucson, Tucson, AZ Tuesday, 6 January 2015 165-AS-3 Morphing Applications Osceola Ballroom 6 Chaired by: F. GANDHI, Rensselaer Polytechnic Inst and T. TURNER, NASA-Langley Research Center 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs AIAA-2015-0787 AIAA-2015-0788 AIAA-2015-0789 AIAA-2015-0790 AIAA-2015-0791 AIAA-2015-0792 AIAA-2015-0793 Extremely Anisotropic Multi-functional A Bi-Stable System for Rotor Span Efficient Active Rotor Concepts for Design and manufacturing of Experimental Evaluation of the Development and Testing of a New Concept Bi-stable Structure: Skin for Morphing Applications Extension in Rotary-Wing Micro In-Plane Noise Reduction morphing fan blades for experimental Morphing Leading Edge Concept Corrugated Skin for a Camber Adaptive Saddle-shaped Bi-stable F. Previtali, Swiss Federal Institute of Aerial Vehicles E. Corle, S. Schmitz, T. Yang, K. Brentner, investigations in a cascaded wind J. Sodja, M. Martinez, Delft University Morphing Aerofoil Panel Technology, Zürich, Switzerland; T. Delpero, A. M. Misiorowski, M. Pontecorvo, F. Gandhi, Pennsylvania State University, University tunnel of Technology, Delft, The Netherlands; J. R. Navaratne, Swansea University, J. Lee, J. Ryu, H. Lee, M. Cho, Seoul Bergamini, Empa, Dübendorf, Switzerland; A. Rensselaer Polytechnic Institute, Troy, NY Park, PA H. Monner, O. Huxdorf, J. Riemenschneider, Simpson, Fraunhofer, Valley, Germany; R. Swansea, United Kingdom National University, Seoul, South Korea Arrieta, P. Ermanni, Swiss Federal Institute of De Breuker, Delft University of Technology, 98 R. Keimer, German Aerospace Center (DLR), Technology, Zürich, Switzerland Braunschweig, Germany Delft, The Netherlands Tuesday, 6 January 2015 166-DA-1 Digital Avionics Osceola Ballroom 3 Chaired by: J. RANKIN, The University of Arkansas 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2015-0794 AIAA-2015-0795 AIAA-2015-0796 AIAA-2015-0797 AIAA-2015-0798 AIAA-2015-0799 Human-in-the-loop Evaluation of A Formally Verified Conflict TCAS Compatibility of Advanced Application of Unified Departure Developing an Attitude and Communication of Target Trajectory an Information Management and Detection Algorithm for Polynomial Airborne Separation Assurance Operation Spacing to a Large Hub Heading Reference System based and Wind Information to Improve Notification System to Improve Trajectories System Operations Airport on Advanced MEMS Gyros Airborne Interval Management Aircraft State Awareness A. Narkawicz, C. Munoz, NASA Langley H. Lenz, German Aerospace Center (DLR), G. Schwoch, German Aerospace Center A. Simonetti, D. Accardo, University of Spacing Performance P. Duan, Ohio University, Athens, OH; Research Center, Hampton, VA Braunschweig, Germany (DLR), Braunschweig, Germany Naples “Federico II”, Naples, Italy; D. L. Weitz, W. Penhallegon, B. Lascara, H. M. Yocius, University of Iowa, Iowa City, Domenico, P. Calcagni, Axitude S.r.l., Stassen, R. Katkin, MITRE Corporation, Iowa City, IA; M. Miltner, Ohio University, Giugliano, Italy McLean, VA Athens, OH; J. Engler, T. Schnell, University of Iowa, Iowa City, Iowa City, IA; M. Uijt De Haag, Ohio University, Athens, OH Tuesday, 6 January 2015 167-DE-2 Design Education/Design Process Sarasota 2 Chaired by: J. WANG, Kingston University and J. CUTSHALL, Southwest Research Institute 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs AIAA-2015-0800 AIAA-2015-0801 AIAA-2015-0802 AIAA-2015-0803 AIAA-2015-0804 Mars Mission Design Strategy Leveraging Open Standards and A Survey of Integrated Tools for Air A Survey of Integrated Tools for Air Formulation and Applications of a Board Game to Inspire STEM Credit-Card-Sized Linux Computers Vehicle Design, Part I Vehicle Design, Part II Probabilistic Pareto Chart Students in Embedded Control & Robotics H. Briggs, ATA Engineering, Inc., San H. Briggs, ATA Engineering, Inc., San K. Hart, B. Steinfeldt, R. Braun, Georgia R. Pidaparti, University of Georgia, Athens, Education Diego, CA Diego, CA Institute of Technology, Atlanta, GA Athens, GA T. Bewley, J. Strawson, S. Ostovari, University of California, San Diego, La Jolla, CA; H. Briggs, ATA Engineering, Inc., San Diego, CA Tuesday, 6 January 2015 168-FD-20 Actuators and Active Flow Control Tallahassee 2 Chaired by: P. MORGAN, Ohio Aerospace Institute and D. SCHATZMAN, Science and Technology Corporation 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2015-0806 AIAA-2015-0807 AIAA-2015-0808 AIAA-2015-0809 AIAA-2015-0810 AIAA-2015-0811 A Combined Type of a Flow Control Axisymmetric Synthetic Jets: Suction and Oscillatory Blowing High-Accuracy Simulations of Active Flow Control to Improve the Flow Control for NACA 4418Airfoil Actuator Composed of the Synthetic Modeling of the Far-field Interaction with Boundary Layers Robust LCO Control Using Synthetic Outer-Wing Performance during Using an “Active Slat” Jet and Vortex Generator Momentum Flux D. Schatzman, Science and Technology Jet Actuators Take-Off T. Tawfik, Petroleum Air Services, Cairo, Y. Ono, Y. Kameya, M. Motosuke, S. X. Xia, K. Mohseni, University of Florida, Corporation, Moffett Field, CA; J. Wilson, Army L. Nguyen, V. Golubev, W. Mackunis, C. Huehne, P. Scholz, Technical University Egypt; B. Elhadidi, M. Abdelrahman, Cairo Honami, Tokyo University of Science, Gainesville, Gainesville, FL Aviation and Missile Research Development N. Ramos, Embry-Riddle Aeronautical of Braunschweig, Braunschweig, Germany University, Giza, Egypt Niijuku, Japan and Engineering Center, Moffett Field, CA; L. University, Daytona Beach, FL; C. Pasiliao, Maron, V. Palei, A. Seifert, Tel Aviv University, Air Force Research Laboratory, Eglin

99 Tel Aviv, Israel; E. Arad, Rafael, Haifa, Israel AFB, FL Tuesday, 6 January 2015 169-FD-21 CFD Methods IV Sanibel 1 Chaired by: A. PROBST, DGLR 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs AIAA-2015-0812 AIAA-2015-0813 AIAA-2015-0814 AIAA-2015-0815 AIAA-2015-0816 AIAA-2015-0817 AIAA-2015-0818 Grid Convergence Study on a Finite Azure: An Advanced CFD Software The Performance Evaluation of an A Low-Dissipation Low-Dispersion Scale-Resolving Simulations with Investigation on Hypersonic A Verification Driven Process Volume Code NSAWET Suite Based on High-Resolution and Improved Finite Volume Method for Second-Order Scheme for a Low-Dissipation Low-Dispersion Aerodynamics Using Numerical and for Rapid Development of CFD Z. Li, H. Chen, Y. Zhang, S. Fu, Tsinghua High-Order Methods Solving the Navier Stokes Equation Unstructured Finite-Volume Flow Second-Order Scheme for Analytical Methods Software University, Beijing, China D. Drikakis, A. Antoniadis, P. Tsoutsanis, I. F. Ferguson, H. Mrema, M. Dhanasar, Solvers Unstructured Finite-Volume Flow W. Luo, D. Li, J. Xiang, Beihang University, M. Galbraith, S. Allmaras, D. Darmofal, Kokkinakis, Z. Rana, Cranfield University, North Carolina A&T State University, J. Löwe, A. Probst, T. Knopp, R. Kessler, Solvers Beijing, China Massachusetts Institute of Technology, Cranfield, United Kingdom Greensboro, NC German Aerospace Center (DLR), A. Probst, J. Löwe, S. Reuss, T. Knopp, R. Cambridge, MA Göttingen, Germany Kessler, German Aerospace Center (DLR), Göttingen, Germany Tuesday, 6 January 2015 170-FD-22 Discontinuous Galerkin Methods II Sanibel 2 Chaired by: J. EKATERINARIS, FORTH/IACM and K. FIDKOWSKI, University of Michigan 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs AIAA-2015-0819 AIAA-2015-0820 AIAA-2015-0821 AIAA-2015-0822 AIAA-2015-0823 High-order unstructured grid High-order Discontinuous Galerkin A mixed continuous/discontinuous OpenACC-based GPU Acceleration Discontinuous High-Order Finite- generation and Discontinuous Simulations on Moving Domains finite element discretization of the of a p-multigrid Discontinuous Volume/Finite-Element Method for Galerkin discretization applied to a using ALE Formulations and Local incompressible NS equations Galerkin Method for Compressible Inviscid Compressible Flows 3D high-lift configuration Remeshing and Projections N. Kyriazis, J. Ekaterinaris, Embry-Riddle Flows on 3D Unstructured Grids A. Ramezani, G. Stipcich, L. Remaki, R. Hartmann, T. Leicht, German Aerospace L. Wang, P. Persson, University of Aeronautical University, Daytona Beach, FL J. Lou, Y. Xia, L. Luo, H. Luo, J. Edwards, Basque Center for Applied Mathematics, Center (DLR), Braunschweig, Germany California, Berkeley, Berkeley, CA F. Mueller, North Carolina State University, Bilbao, Spain Raleigh, NC Tuesday, 6 January 2015 171-FD-23 Flow Control (Fundamentals and Technology) I Sanibel 3 Chaired by: D. MILLER, Lockheed Martin Aeronautics and F. ALVI, Florida State University 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2015-0824 AIAA-2015-0825 AIAA-2015-0826 AIAA-2015-0827 AIAA-2015-0828 AIAA-2015-0829 Flow Control of Unsteadiness in the Active flow control on an Ahmed Drag Reduction Control for Flow Unsteady Aerodynamic Loads Investigation of Flow Modifications Aircraft Carrier Burble Mitigation Wake of a Turbine Blade body - An experimental study over a Hump with Surface-Mounted Effected by Flow Control on a Induced by an Undulating Airfoil With Alternating Current Dielectric M. Irsch, RWTH Aachen University, Aachen, J. McNally, F. Alvi, Florida State University, Thermoacoustic Actuator Moving Axisymmetric Bluff Body Surface Barrier Discharge Plasma Actuators Germany; R. Davis, University of California, Tallahassee, FL; N. Mazellier, A. Kourta, C. Yeh, P. Munday, K. Taira, Florida State T. Lambert, B. Vukasinovic, A. Glezer, G. Spencer, J. Krofta, R. LeBeau, M. B. Munguia, N. Bui, B. Lewis, D. Richie, Davis, Davis, CA; J. Clark, Air Force Research University of Orléans, Orléans, France University, Tallahassee, FL; M. Munson, Georgia Institute of Technology, Atlanta, McQuilling, Saint Louis University, St. Ohio State University, Columbus, OH Laboratory, Wright-Patterson AFB, OH; G. Army Research Laboratory, Aberdeen GA Louis, MO Paniagua, von Kármán Institute for Fluid Proving Ground, MD Dynamics, Rhode-Saint-Genèse, Belgium Tuesday, 6 January 2015 172-FD-24 High-Order Methods II Daytona 1 Chaired by: W. DAWES, Cambridge University and A. KATZ 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2015-0830 AIAA-2015-0831 AIAA-2015-0832 AIAA-2015-0833 AIAA-2015-0834 AIAA-2015-0835 A High-Order Method for Solving Large-Eddy Simulation of a A conservative cutcell method Flow simulation system based on Aspects of the Flux Correction High-Order Methods for Three- Unsteady Incompressible Navier- Supersonic Jet using High-Order with adaptive mesh refinement high order space-time extension of Method for Solving the Navier- Dimensional Strand-Cartesian Grids Stokes Equations with Implicit Time Flux Reconstruction Scheme for large eddy simulation of flux reconstruction method Stokes Equations on Unstructured O. Tong, A. Katz, Utah State University, Stepping on Unstructured Grids T. Haga, S. Tsutsumi, S. Kawai, R. Takaki, compressible flows Y. Lu, University of Cambridge, Cambridge, Meshes Logan, UT; A. Wissink, J. Sitaraman, C. Cox, C. Liang, M. Plesniak, George Japan Aerospace Exploration Agency B. Muralidharan, S. Menon, Georgia United Kingdom; K. Liu, Tsinghua University, D. Work, A. Katz, Utah State University, Army Aviation and Missile Research Washington University, Washington, DC (JAXA), Sagamihara, Japan Institute of Technology, Atlanta, GA Beijing, China; W. Dawes, University of Logan, UT Development and Engineering Center,

100 Cambridge, Cambridge, United Kingdom Moffett Field, CA Tuesday, 6 January 2015 173-FD-25 Hypersonic Boundary Layer Transition I Tallahassee 1 Chaired by: L. DUAN, Missouri University of Science and Technology 1400 hrs 1430 hrs 1500 hrs AIAA-2015-0836 AIAA-2015-0837 AIAA-2015-0838 Acoustic Radiation from High-Speed Parametric study on stabilization of Linearized Navier-Stokes Turbulent Boundary Layers in a hypersonic boundary layer waves Simulations of the Spatial Stability Tunnel-like Environment using 2-D surface roughness of a Hypersonic Boundary-Layer on L. Duan, Missouri University of Science K. Fong, X. Wang, X. Zhong, University of a Flared Cone and Technology, Rolla, MO; M. Choudhari, California, Los Angeles, Los Angeles, CA L. Salemi, H. Fasel, University of Arizona, NASA Langley Research Center, Hampton, Tucson, Tucson, AZ VA; C. Zhang, Missouri University of Science and Technology, Rolla, MO Tuesday, 6 January 2015 174-FD-26 Jets, Plumes, & Reacting Flows Daytona 2 Chaired by: G. BLAISDELL, Purdue University and C. BOURASSA, GE Aviation 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs AIAA-2015-0840 AIAA-2015-0841 AIAA-2015-0842 AIAA-2015-0843 AIAA-2015-0844 Computational Fluid Dynamics Rocket Plume Modeling Implementation of Large-Eddy Simulation of Coaxial Large Eddy Simulation of Flame Simulation of United Launch C. Cai, New Mexico State University, Las Thermochemistry and Chemical LN2/GH2 Injection at Trans- and Flashback in Swirling Premixed Alliance Delta IV Hydrogen Plume Cruces, NM Kinetics in a GPU-based CFD Code Supercritical Conditions CH4/H2-Air Flames Mitigation Strategies B. Taylor, D. Schwer, A. Corrigan, Naval H. Müller, M. Pfitzner, University of the C. Lietz, V. Raman, University of Texas, S. Guimond, M. Ni, N. Voce, A. Kassab, Research Laboratory, Washington, DC German Federal Armed Forces, Munich, Austin, Austin, TX University of Central Florida, Orlando, Germany; J. Matheis, S. Hickel, Technical FL; S. Song, Z. Richards, United Launch University of Munich, Munich, Germany Alliance, Centennial, CO; et al. Tuesday, 6 January 2015 175-GNC-16 Aerospace Robotics and Autonomous/Unmanned Systems IV Sun Ballroom 3 Chaired by: J. SASIADEK, Carleton University and D. PEREZ 1400 hrs 1430 hrs 1500 hrs 1530 hrs AIAA-2015-0845 AIAA-2015-0846 AIAA-2015-0847 AIAA-2015-0848 Real-Time Guidance of Quadrotor Image-based Visual Servoing UAV Circumnavigation under Vision Based Obstacle Detection for Obstacle Mapping Using Vision Framework for a Multirotor UAV using a GPS-denied Environment: and Avoidance for UAVs Using System Sampling-based Path Planning Algorithms and Experiments Image Segmentation J. Park, Y. Kim, Seoul National University, S. Cho, D. Lee, D. Shim, Korea Advanced Y. Cao, D. Kingston, S. Rasmussen, P. Agrawal, A. Ratnoo, D. Ghose, Indian Seoul, South Korea Institute of Science and Technology, Air Force Research Laboratory, Wright- Institute of Science, Bangalore, India Daejeon, South Korea Patterson AFB, OH Tuesday, 6 January 2015 176-GNC-17 Lander Technology Development at NASA II Miami 1 Chaired by: J. CARSON, NASA Jet Propulsion Laboratory and N. TRAWNY, Jet Propulsion Laboratory 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs AIAA-2015-0849 AIAA-2015-0850 AIAA-2015-0851 AIAA-2015-0852 AIAA-2015-0853 Project Morpheus: Tailored Systems Interpolation-Enhanced Powered Real-Time Terrain Relative Navigation The Mighty Eagle Vertical Testbed APLNav: Development Status of an Engineering of a Terrestrial Flight Descent Guidance for Onboard Test Results from a Relevant M. Hannan, NASA Marshall Space Flight Onboard Passive Optical Terrain Testbed for Maturing NASA Lander Nominal, Off-Nominal, and Multi-X Environment for Mars Landing Center, Huntsville, AL; T. McGee, Johns Relative Navigation System Technologies Scenarios A. Johnson, Y. Cheng, J. Montgomery, Hopkins University Applied Physics Laboratory, T. McGee, P. Rosendall, A. Hill, W. Shyong, J. Devolites, J. Olansen, NASA Johnson D. Scharf, S. Ploen, Jet Propulsion N. Trawny, B. Tweddle, J. Zheng, Jet Columbia, MD; G. Chavers, J. Adam, L. T. Criss, C. Reed, Johns Hopkins University Space Center, Houston, TX Laboratory, California Institute of Propulsion Laboratory, California Institute Kennedy, J. Moore, NASA Marshall Space Applied Physics Laboratory, Laurel, MD; Technology, Pasadena, CA; B. Acikmese, of Technology, Pasadena, CA Flight Center, Huntsville, AL; et al. et al. University of Texas, Austin, Austin, TX 101 Tuesday, 6 January 2015 177-GNC-18 Control and Diagnostics of Air Vehicles and UAVs Sun Ballroom 4 Chaired by: A. KNOBLACH, DLR - German Aerospace Center and R. VENKATARAMAN, University of Minnesota 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2015-0854 AIAA-2015-0855 AIAA-2015-0856 AIAA-2015-0857 AIAA-2015-0858 AIAA-2015-0859 Maximizing the Efficiency of a UAV Necessary Conditions for Control Disturbance Observer-Based Model-Based Detection and Worst Case Analysis of a Saturated Aircraft Inertial Measurement Unit on Perimeter Patrol Effort Minimization of Euler- Control to Suppress Air Resonance Isolation of Rudder Faults for a Gust Loads Alleviation System Fault Identification with Application K. Kalyanam, Air Force Research Laboratory, Lagrange Systems for the EC135 ACT/FHS Research Small UAS A. Knoblach, German Aerospace Center to Real Flight Data Wright-Patterson AFB, OH; M. Pachter, Air A. L’Afflitto, W. Haddad, Georgia Institute Helicopter R. Venkataraman, P. Seiler, University of (DLR), Wessling, Germany; H. Pfifer, P. Lu, E. Van Kampen, Delft University of Force Institute of Technology, Wright-Patterson of Technology, Atlanta, GA S. Greiser, German Aerospace Center Minnesota, Minneapolis, Minneapolis, MN P. Seiler, University of Minnesota, Technology, Delft, The Netherlands AFB, OH; P. Chandler, Air Force Research (DLR), Braunschweig, Germany Minneapolis, Minneapolis, MN Laboratory, Wright-Patterson AFB, OH Tuesday, 6 January 2015 178-GNC-19 Missile Autopilot and Integrated Control Sun Ballroom 6 Chaired by: S. KOWALCHUK, Sandia National Laboratories and R. RATLIFF, Boeing Defense, Space & Security 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs AIAA-2015-0860 AIAA-2015-0861 AIAA-2015-0862 AIAA-2015-0863 AIAA-2015-0864 Missile Autopilot Design During Missile Guidance Law Considering Considerations on Boost Phase Lyapunov Based Nonlinear Impact Autopilot Design for Aerial Vehicles Boost Phase Using Robust Constraints on Impact Angle and Modeling and Guidance Command Angle Guidance Law for Stationary with Aerodynamic Surfaces and Backstepping Approach Terminal Angle of Attack Generation Targets Lateral Jets Using Explicit Hybrid S. Lee, Y. Kim, Seoul National University, H. Kim, H. Kim, Seoul National University, R. Tekin, ASELSAN, Inc., Ankara, Turkey; U. Ates, ROKETSAN Missiles Industries, MPC Seoul, Korea (the Republic of); G. Moon, Seoul, South Korea K. Erer, ROKETSAN Missiles Industries, Inc., Inc., Ankara, Turkey B. Yang, Y. Zhao, Y. Yao, Harbin Institute B. Jun, Agency for Defense Development, Ankara, Turkey of Technology, Harbin, China Daejeon, South Korea Tuesday, 6 January 2015 179-GNC-20 Spacecraft Guidance, Navigation, and Control I Sun Ballroom 5 Chaired by: F. MORA-CAMINO, ENAC and S. ULRICH, Carleton University 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2015-0865 AIAA-2015-0866 AIAA-2015-0867 AIAA-2015-0868 AIAA-2015-0869 AIAA-2015-0870 SEXTANT - Station Explorer for X-ray A Comparison of Thruster Assessing Nanosatellite Cluster On the development of a 6DoF GNC Preliminary Design and Prototyping Attitude Control of Upper Stage Timing and Navigation Technology Implementation Strategies for a Launch Scenarios framework for docking multiple of a Low-Cost Spacecraft Attitude with Gimbaled Thruster during J. Mitchell, M. Hassouneh, L. Winternitz, J. Deep Space Nanosatellite C. Wen, Beihang University, Beijing, small satellites Determination and Control Setup Orbit Transfer Valdez, S. Price, S. Semper, NASA Goddard M. Nehrenz, M. Sorgenfrei, NASA Ames China; P. Gurfil, Technion--Israel Institute of M. Nunes, University of Hawaii, Honolulu, K. Turkoglu, A. Gong, San Jose State Z. Wang, Beihang University, Beijing, Space Flight Center, Greenbelt, MD; et al. Research Center, Moffett Field, CA Technology, Haifa, Israel Honolulu, HI University, San Jose, CA China Tuesday, 6 January 2015 180-GTE-4 Engine Systems II Emerald 1 Chaired by: K. MILLSAPS, Naval Postgraduate School and A. GORDON, University of Central Florida 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs AIAA-2015-0871 AIAA-2015-0872 AIAA-2015-0873 AIAA-2015-0874 AIAA-2015-0875 Unsteady Particle Dynamics within A Novel Approach to Life Prediction Turbine Engine Performance Comparison of Thermal Barrier Three-Dimensional Numerical an Inertial Particle Separator Analysis of a Turbine Engine Blade Estimation Using Particle Filters Coating Stresses via High Energy Modeling of Tip Leakage Flow over P. Snyder, Rolls-Royce Group plc, to Disk Attachment B. Yang, P. Sengupta, P. Menon, Optimal X-Rays and Piezospectroscopy a Finite Blade Indianapolis, IN; E. Loth, D. Barone, S. Naboulsi, Air Force Research Laboratory, Synthesis, Inc., Los Altos, CA A. Manero, K. Knipe, University of Central O. Khan, M. Khan, Tuskegee University, University of Virginia, Charlottesville, Wright-Patterson AFB, OH Florida, Orlando, FL; C. Meid, J. Wischek, Tuskegee, AL Charlottesville, VA German Aerospace Center (DLR), Cologne, Germany; C. Lacdao, M. Smith, Cleveland State University, Cleveland, OH; et al.

102 Tuesday, 6 January 2015 181-HSABP-5 Pressure Gain Combustion - Rotating Detonation Engines II Emerald 3 Chaired by: V. TANGIRALA, General Electric and S. STANLEY, Aerojet Rocketdyne 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2015-0876 AIAA-2015-0877 AIAA-2015-0878 AIAA-2015-0879 AIAA-2015-0880 AIAA-2015-0881 Numerical Investigation of Experimental and Numerical Visualization of Rotating Numerical Investigation of Inlet Numerical Study of Heat Transfer Method of Characteristics Analysis Centerbodiless RDE Design Evaluation of Pressure Gain Detonation Waves in a Plane Injection in a Rotating Detonation in a Rotating Detonation Combustor of the Internal Flowfield in a Variations Combustion in a Rotating Combustor with a Cylindrical Wall Engine S. Randall, V. Anand, A. St. George, Rotating Detonation Engine W. Stoddard, E. Gutmark, University of Detonation Engine Injector R. Driscoll, V. Anand, A. St. George, E. Gutmark, University of Cincinnati, R. Fievisohn, K. Yu, University of Cincinnati, Cincinnati, OH B. Rankin, Innovative Scientific Solutions, S. Nakagami, K. Matsuoka, J. Kasahara, W. Stoddard, D. Munday, E. Gutmark, Cincinnati, OH Maryland, College Park, College Park, MD Inc., Dayton, OH; M. Fotia, National Research Nagoya University, Nagoya, Japan; A. University of Cincinnati, Cincinnati, OH Council, Dayton, OH; D. Paxson, NASA Glenn Matsuo, Keio University, Yokohama, Research Center, Cleveland, OH; J. Hoke, Japan; I. Funaki, Japan Aerospace Innovative Scientific Solutions, Inc., Dayton, Exploration Agency (JAXA), Sagamihara, OH; F. Schauer, Air Force Research Laboratory, Japan Wright-Patterson AFB, OH Tuesday, 6 January 2015 182-HSABP-6 High Speed Air-Breathing Combustors I Emerald 8 Chaired by: C. BRUNO, United Technologies Research Center and J. CASTRO, Pratt & Whitney-Rocketdyne 1400 hrs 1430 hrs 1500 hrs 1530 hrs AIAA-2015-0882 AIAA-2015-0883 AIAA-2015-0884 AIAA-2015-0885 Effects of Inlet Distortion on Cavity Response of a Mach 3 Cavity Numerical Investigation of Upstream Preliminary analysis of strategies Ignition in Supersonic Flow Flameholder to a Shock-Induced Fuel Injection through Porous Media for NOx reduction T. Ombrello, S. Peltier, C. Carter, Air Force Distortion for Scramjet Engines via Surrogate- A. Ingenito, A. Agresta, University of Rome Research Laboratory, Wright-Patterson S. Peltier, C. Carter, Air Force Research Assisted Evolutionary Algorithms “La Sapienza”, Rome, Italy; R. Andriani, AFB, OH Laboratory, Wright-Patterson AFB, OH H. Ogawa, RMIT University, Melbourne, Technical University of Milan, Milan, Australia; B. Capra, Queensland University Italy; F. Gamma, University of Rome “La of Technology, Brisbane, Australia; P. Lorain, Sapienza”, Rome, Italy University of New South Wales at the Australian Defence Force Academy, Canberra, Australia Tuesday, 6 January 2015 183-IS-6 Realizing the Potential for Genetic Fuzzy Systems Osceola Ballroom 1 Chaired by: K. COHEN, University of Cincinnati and N. ERNEST, University of Cincinnati 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs AIAA-2015-0886 AIAA-2015-0887 AIAA-2015-0888 AIAA-2015-0889 AIAA-2015-0890 Genetic Algorithm Based LQR for Genetic Fuzzy Approach for Control Multi-agent Cooperative Decision Enhanced Approaches to Solving Genetic Optimization of Fuzzy Attitude Control of a Magnetically and Task Planning Applications Making using Genetic Cascading the Multiple Traveling Salesman Logic Control for Coupled Dynamic Actuated CubeSat A. Sathyan, N. Ernest, K. Cohen, University Fuzzy Systems Problem Systems S. Kukreti, University of Cincinnati, of Cincinnati, Cincinnati, OH N. Ernest, University of Cincinnati, Cincinnati, N. Boone, A. Sathyan, K. Cohen, A. Janson, N. Stockton, K. Cohen,

103 Cincinnati, OH; A. Walker, P. Putman, OH; E. Garcia, Infoscitex Corporation, Dayton, University of Cincinnati, Cincinnati, OH University of Cincinnati, Cincinnati, OH Sierra Lobo, Inc., Milan, OH; K. Cohen, OH; D. Casbeer, Air Force Research Laboratory, University of Cincinnati, Cincinnati, OH Wright-Patterson AFB, OH; K. Cohen, University of Cincinnati, Cincinnati, OH; C. Schumacher, Air Force Research Laboratory, Wright-Patterson AFB, OH Tuesday, 6 January 2015 184-MAT-7 Fatigue & Fracture I Sarasota 1 Chaired by: D. POWELL and R. FERTIG, University of Wyoming 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs AIAA-2015-0891 AIAA-2015-0892 AIAA-2015-0893 AIAA-2015-0894 AIAA-2015-0895 Regression Study to Standardize Interlaminar and Intralaminar Oblique plies for steering through- Fatigue Life of Selective Laser Fatigue Behavior and Modeling for Piezoelectric Axial Fatigue Testing Dynamic Fracture Behaviors of thickness delamination migration in Melted and Hot Isostatically Thermoplastics O. Scott-Emuakpor, T. George, C. CFRP: An Investigation Using fibre reinforced polymers Pressed Ti-6Al-4v Absent of Surface R. Meyer, J. Simsiriwong, M. Lugo, N. Holycross, J. Beck, C. Cross, Air Force Digital Image Correlation and High- R. Luterbacher, R. Trask, I. Bond, Machining Shamsaei, Mississippi State University, Research Laboratory, Wright-Patterson Speed Photography University of Bristol, Bristol, United K. Rekedal, D. Liu, Air Force Institute of Mississippi State, MS AFB, OH R. Bedsole, H. Tippur, Auburn University, Kingdom Technology, Wright-Patterson AFB, OH Auburn, AL Tuesday, 6 January 2015 185-MDO-5 MDO: Fundamental Algorithms & Processes II Sarasota 3 Chaired by: A. KO, Phoenix Integration, Inc. and J. HICKEN, Rensselaer Polytechnic Institute 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2015-0896 AIAA-2015-0897 AIAA-2015-0898 AIAA-2015-0899 AIAA-2015-0900 AIAA-2015-0901 Application of Reduced Order Standard Particle Swarm Sequential Radial Basis Function Sensitivity Analysis Methods Simultaneous aircraft allocation Effectiveness Indicators for Techniques for Sensitivity Analysis Optimization on Source Seeking Optimization Strategy Using for Mitigating Uncertainty in and mission optimization using a Stopping Criteria based on to Multidisciplinary Aerospace Using Mobile Robots Support Vector Machine for Flight Engineering System Design modular adjoint approach Minimum Required Improvement Systems R. Zou, V. Kalivarapu, S. Bhattacharya, Vehicle Multidisciplinary Design Q. Curran, K. Willcox, Massachusetts J. Hwang, University of Michigan, Ann A. Chaudhuri, R. Haftka, University of J. Parrish, M. Rais-Rohani, J. Janus, E. Winer, J. Oliver, Iowa State University, Optimization Institute of Technology, Cambridge, MA Arbor, Ann Arbor, MI; S. Roy, Purdue Florida, Gainesville, Gainesville, FL Mississippi State University, Mississippi Ames, IA R. Shi, L. Liu, T. Long, X. Guo, L. Peng, University, West Lafayette, IN; J. Kao, State, MS Beijing Institute of Technology, Beijing, J. Martins, University of Michigan, Ann China Arbor, Ann Arbor, MI; W. Crossley, Purdue University, West Lafayette, IN Tuesday, 6 January 2015 186-MST-7 Model Design and Development Sun Ballroom 1 Chaired by: R. RUFF, Technical University Munich 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs AIAA-2015-0902 AIAA-2015-0903 AIAA-2015-0904 AIAA-2015-0905 AIAA-2015-0906 Development of an Aerodynamic Updating a finite element based Systemic modeling and design Flight Dynamics Modeling of a A Coupled Lateral/Directional Model for a Delta-Wing Equivalent structural model of a small flexible approach for morphing wing Body Freedom Flutter Vehicle for Flight Dynamics and Structural Model II (EQ-II) Aircraft aircraft aileron controller using Matlab/ Multidisciplinary Analyses Model for Flight Control Design W. Okolo, A. Dogan, University of Texas, A. Gupta, C. Moreno, H. Pfifer, B. Taylor, Simulink M. Leitner, A. Knoblach, T. Kier, German O. Juhasz, San Jose State University, Arlington, Arlington, TX; W. Blake, Air G. Balas, University of Minnesota, V. Jean-Baptiste, R. Botez, École de Aerospace Center (DLR), Wessling, Moffett Field, CA; M. Tischler, Army Aviation

104 Force Research Laboratory, Wright- Minneapolis, Minneapolis, MN Technologie Supérieure, Montréal, Canada Germany; C. Moreno, A. Kotikalpudi, and Missile Research Development and Patterson AFB, OH H. Pfifer, University of Minnesota, Engineering Center, Moffett Field, CA; S. Minneapolis, Minneapolis, MN; et al. Hagerott, D. Staples, J. Fuentealba, Cessna Aircraft Company, Wichita, KS Tuesday, 6 January 2015 187-MST-8 Multi-Domain Modeling and Simulation Sun Ballroom 2 Chaired by: A. ELMILIGUI, NASA Langley Research Center 1400 hrs 1430 hrs 1500 hrs AIAA-2015-0907 AIAA-2015-0908 AIAA-2015-0909 Development of a Reduced Modeling Systems-of-Systems Coupling between non-local particle Order Model to Study Rotor/Ship from Multiple Design Perspectives: and finite element methods Aerodynamic Interaction Agents, Interfaces, and E. Lin, H. Chen, Y. Liu, Arizona State N. Rajmohan, J. Zhao, C. He, Advanced Architectures University, Tempe, AZ Rotorcraft Technology, Inc., Sunnyvale, CA; D. Fry, R. Campbell, D. DeLaurentis, S. Polsky, Naval Air Systems Command, Purdue University, West Lafayette, IN Patuxent River, MD Tuesday, 6 January 2015 188-MVC-4 Meshing Techniques, Including Surface and Volume Grids, and Moving/Deforming Meshes Naples 3 Chaired by: J. MASTERS, Aerospace Testing Alliance (ATA) 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2015-0910 AIAA-2015-0911 AIAA-2015-0912 AIAA-2015-0913 AIAA-2015-0914 AIAA-2015-0915 A Survey of Overset Domain Advances in Parallelization An Overset Grid 2D/Infinite Mesh Manipulation for 3D Adaptive curvature control grid Alignment and orthogonality in Assembly Methods For Large Scale Oct-Tree Mesh Swept Wing URANS Solver Using Tetrahedral Meshes generation algorithms for complex anisotropic metric-based mesh C. Druyor, NASA Langley Research Center, Generation Recursive Cartesian Bucket Method J. Masters, Arnold Engineering glaze ice shapes RANS simulations adaptation Hampton, VA; S. Karman, University of M. O’Connell, NASA Langley Research A. Levesque, A. Pigeon, E. Laurendeau, Development Complex, Arnold AFB, TN K. Hasanzadeh Lashkajani, E. Laurendeau, A. Loseille, French National Institute Tennessee, Chattanooga, Chattanooga, Center, Hampton, VA; S. Karman, École Polytechnique de Montréal, I. Paraschivoiu, École Polytechnique de for Research in Computer Science and TN; W. Jones, NASA Langley Research University of Tennessee, Chattanooga, Montréal, Canada Montréal, Montréal, Canada Control (INRIA), Paris, France; D. Marcum, Center, Hampton, VA Chattanooga, TN Mississippi State University, Starkville, MS; F. Alauzet, French National Institute for Research in Computer Science and Control (INRIA), Paris, France Tuesday, 6 January 2015 189-NDA-4 Optimization under Uncertainty Osceola Ballroom 5 Chaired by: M. RAIS-ROHANI, Mississippi State University and E. TUEGEL, USAF 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2015-0916 AIAA-2015-0917 AIAA-2015-0918 AIAA-2015-0919 AIAA-2015-0920 AIAA-2015-0921 Investigating Uncertainty in Multi-fidelity Robust Aerodynamic Robust Aeroelastic Design of a Robust aerodynamic optimization Robust Optimization of a Wing Active Subspaces Applied to Range Capability versus Cost Decision- Design Optimization Under Mixed Composite Wing-Box of morphing airfoils for helicopter Under Structural and Material Safety Analysis and Optimization Making Uncertainty C. Scarth, P. Sartor, J. Cooper, P. Weaver, rotor blades Uncertainties F. Capristan, J. Alonso, Stanford University, E. Forster, P. Beran, R. Kolonay, Air Force H. Shah, S. Hosder, Missouri University University of Bristol, Bristol, United F. Fusi, G. Quaranta, A. Guardone, K. Boopathy, M. Rumpfkeil, University Stanford, CA

105 Research Laboratory, Wright-Patterson of Science and Technology, Rolla, MO; Kingdom; G. Silva, Embraer, São José dos Technical University of Milan, Milan, Italy; of Dayton, Dayton, OH; R. Kolonay, US AFB, OH; H. Bae, Wright State University, L. Leifsson, S. Koziel, Y. Tesfahunegn, Campos, Brazil P. Congedo, French National Institute for Air Force Research Laboratory, Wright- Dayton, OH Reykjavik University, Reykjavik, Iceland Research in Computer Science and Control Patterson AFB, OH (INRIA), Bordeaux, France Tuesday, 6 January 2015 190-PANEL-4 Big Data Analytics in Aerospace Osceola Ballroom B 1400 - 1600 hrs Moderator: Ashok Srivastava, Chief Data Scientist, Verizon Panelists: Eric Feron John Kelly Melanie Lorang Nikunj Oza Professor, School of Aerospace Engineering Technical Lead, Data Analytics Initiatives Associate Technical Fellow Leader, Data Sciences Group Georgia Institute of Technology Corporate Engineering, Technology, & Operations The Boeing Company NASA Ames Research Center Lockheed Martin Corporation Tuesday, 6 January 2015 191-PC-11 Heterogeneous Combustion and Propellants Emerald 5 Chaired by: T. JACKSON, University of Florida Gainesville and J. MURPHY, The Aerospace Corporation 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2015-0922 AIAA-2015-0923 AIAA-2015-0924 AIAA-2015-0925 AIAA-2015-0926 AIAA-2015-0927 Thermogravimetric Analysis of Combustion of Bio-derived Fuels 3D Printer for Paraffin Based Experimental characterization of Combustion characteristic of solid Fabrication and Thermophysical the Decomposition of a Paraffin With Additives and Research on the Hybrid Rocket Fuel Grains combustion regimes for micron- propellants used H2O Properties of Nickel-coated Particle/HTPB Fuel Grain for Losses of Unburned Fuel in Hybrid M. Creech, A. Crandell, N. Eisenhauer, S. sized aluminum powders T. Sasaki, K. Takahashi, T. Kuwahara, Aluminum Powder by Electroless Hybrid Rocket Motors Propellant Rocket Engines Marx, T. Busari, A. Link, Purdue University, R. Lomba, F. Halter, University of Orléans, Nihon University, Funabashi, Japan Plating K. Cardoso, Technological Institute of V. Naoumov, P. Skomin, P. Deptula, West Lafayette, IN; et al. Orléans, France; C. Chauveau, National S. Lee, W. Yoon, K. Noh, J. Lim, Yonsei Aeronautics (ITA), São José dos Campos, Central Connecticut State University, New Center for Scientific Research (CNRS), University, Seoul, Korea (the Republic Brazil; M. Nagamachi, Aeronautics and Britain, CT Orléans, France; S. Bernard, P. Gillard, C. of); D. Lee, C. Kim, Agency for Defense Space Institute (IAE), São José dos Mounaim-Rousselle, University of Orléans, Development, Daejeon, South Korea Campos, Brazil; E. Kawachi, Technological Orléans, France; et al. Institute of Aeronautics (ITA), São José dos Campos, Brazil; T. de Araújo, R. Nunes, Aeronautics and Space Institute (IAE), São José dos Campos, Brazil Tuesday, 6 January 2015 192-PC-12 Turbulent Combustion IV Emerald 7 Chaired by: E. MASTORAKOS, University of Cambridge and V. RAMAN, University of Texas at Austin 1400 hrs 1430 hrs 1500 hrs 1530 hrs AIAA-2015-0928 AIAA-2015-0929 AIAA-2015-0930 AIAA-2015-0931 Characteristics of Freely Experimental Study on the Flame Extinction Dynamics of Lean Study on Flame Response

106 Propagating Premixed Flame Interaction between Swirl-stabilized Premixed Bluff-Body Stabilized Characteristics under Transverse Kernels in Supersonic Turbulent Nozzles for Isothermal Flowfields Flames Pressure Excitations Channel Flows B. Dolan, R. Villalva Gomez, University M. Geikie, K. Ahmed, Old Dominion S. Seo, Y. Park, Hanbat National B. Ochs, D. Scarborough, S. Menon, of Cincinnati, Cincinnati, OH; H. Nawroth, University, Norfolk, VA University, Daejeon, South Korea Georgia Institute of Technology, Atlanta, Technical University of Berlin, Berlin, Germany; GA; N. Grady, R. Pitz, Vanderbilt University, S. Pack, United Technologies Corporation, Nashville, TN West Des Moines, IA; E. Gutmark, University of Cincinnati, Cincinnati, OH Tuesday, 6 January 2015 193-PDL-3 Diagnostics and Experimental Techniques Emerald 2 Chaired by: A. YALIN, Colorado State University 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs AIAA-2015-0932 AIAA-2015-0933 AIAA-2015-0934 AIAA-2015-0935 AIAA-2015-0937 Characterization of Dissociation Methods for Enhancing Radar Measurements of OH and H Electric Field Measurements in a Capillary nanosecond discharges and Gas Heating in Femtosecond REMPI Sensitivity number density distributions in a Dielectric Barrier Nanosecond Pulse as a tool for the measurement Laser Plasma with Planar Rayleigh S. McGuire, A. Dogariu, T. Chng, R. Miles, near-surface discharge at the liquid Discharge with Sub-nanosecond of quenching coefficients at high Scattering and Rayleigh Scattering Princeton University, Princeton, NJ water / water vapor interface Time Resolution specific energy deposition Polarimetry V. Petrishchev, Z. Yin, C. Winters, W. B. Goldberg, Ohio State University, Columbus, A. Klochko, A. Salmon, J. Lemainque, C. Limbach, R. Miles, Princeton University, Lempert, I. Adamovich, Ohio State OH; S. O’Byrne, University of New South École Polytechnique, Palaiseau, France; Princeton, NJ University, Columbus, OH Wales at the Australian Defence Force N. Popov, Moscow State University, Academy, Canberra, Australia; W. Lempert, Moscow, Russia; S. Starikovskaia, École Ohio State University, Columbus, OH Polytechnique, Palaiseau, France Tuesday, 6 January 2015 194-SATS-1 Small Satellites - Technologies I Miami 3 Chaired by: A. SANTANGELO and J. STRAUB, University of North Dakota 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs AIAA-2015-0938 AIAA-2015-0939 AIAA-2015-0940 Oral Presentation AIAA-2015-0941 Micro-Cathode Arc Thruster for Attitude Control System of a Cube A Practical Attitude Control System Crew Waste Water Electrical Modular Rapidly Manufactured Small Satellite Propulsion Satellite with Small Solar Sail using Control Moment Gyros for Propulsion System With Developed Small Satellite (MRMSS) M. Keidar, George Washington University, Y. Yoo, S. Koo, G. Kim, S. Kim, J. Suk, Nano-Satellite TSUBAME Arcjet Thruster G. Trinh, K. Cheung, NASA Ames Research Washington, DC Chungnam National University, Daejeon, T. Hao, Tokyo Institute of Technology, H. Tahara, Osaka Institute of Technology, Center, Moffett Field, CA Korea (the Republic of); J. Kim, University Tokyo, Japan; S. Matunaga, Japan Osaka, Japan; Y. Nogawa, Splije, LLC, of Glasgow, Glasgow, United Kingdom Aerospace Exploration Agency (JAXA), Tsukuba, Japan Sagamihara, Japan Tuesday, 6 January 2015 195-SCS-4 Composite Material for Spacecraft Structures Osceola Ballroom 4 Chaired by: M. SANTER, Imperial College London and S. BRADFORD, Jet Propulsion Laboratory 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs AIAA-2015-0942 AIAA-2015-0943 AIAA-2015-0944 AIAA-2015-0945 AIAA-2015-0946 AIAA-2015-0947 AIAA-2015-0948 High Strain Composites High Strain Composite Slit Tubes for Dual-Matrix Composite Wideband Preliminary Design of Deployable The Strain Energy Deployed High Simulation of Non-Synchronous Hysteresis modeling and control T. Murphey, High Strain Dynamics, Large Roll-Out Structures Antenna Structures for CubeSats Flexible Shell Reflector of an Expansion Outer Barrel Assembly Deployment of the Large system design for shape memory Phoenix, NY; W. Francis, B. Davis, Roccor, W. Francis, B. Davis, M. Hulse, P. Keller, M. Sakovsky, I. Maqueda Jimenez, C. X-band Satellite Payload M. Silver, Lincoln Laboratory, Deployable Hoop Truss Antenna alloy actuators LLC, Louisville, CO; J. Mejia-Ariza, L’Garde, D. Campbell, G. Freebury, Roccor, LLC, Karl, S. Pellegrino, California Institute of O. Soykasap, S. Karakaya, A. Gayretli, Massachusetts Institute of Technology, L. Liu, China Academy of Space Technology, I. Kim, J. Shan, York University, Toronto, Inc., Tustin, CA Louisville, CO Technology, Pasadena, CA; J. Costantine, Y. Akcin, Afyon Kocatepe University, Lexington, MA; P. Warren, Physical Beijing, China; J. Shan, York University, Canada California State University, Fullerton, CA Afyonkarahisar, Turkey Sciences, Inc., Andover, MA Toronto, Canada; C. Tao, China Academy of Space Technology, Beijing, China 107 Tuesday, 6 January 2015 196-SD-8 Special Session: Transformative Technologies for High-Speed/High-Efficiency Next-Gen Rotorcraft I Tampa 2 Chaired by: A. DATTA, Science & Technology Corporation and E. SMITH, Pennsylvania State University 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs AIAA-2015-0949 AIAA-2015-0950 AIAA-2015-0951 AIAA-2015-0952 AIAA-2015-0953 AIAA-2015-0954 AIAA-2015-0955 NASA Technology for Next Wind Tunnel Testing of an Aeromechanics of Slowed Rotors at Leading- and Trailing-Edge Multi-Plate Dry Clutch Design and Analysis of Pericyclic Mechanical Blast Attenuating Aircraft Structure Generation Vertical Lift Vehicles Instrumented Rotor at High High Advance Ratios Reversal of a Cambered Airfoil for Analysis for Dual Speed Rotorcraft Transmission with Straight Bevel Gears D. McCarthy, L. Chiu, The Boeing S. Gorton, NASA Langley Research Advance Ratio G. Bowen-Davies, I. Chopra, University of Stopped Rotors Applications T. Mathur, Pennsylvania State University, Company, Mesa, AZ; M. Robeson, Center, Hampton, VA; I. Lopez, NASA B. Berry, I. Chopra, University of Maryland, College Park, College Park, MD R. Niemiec, G. Jacobellis, F. Gandhi, H. Desmidt, University of Tennessee, University Park, PA; Z. Saribay, Turkish Army Aviation and Missile Research Glenn Research Center, Cleveland, OH; C. Maryland, College Park, College Park, MD Rensselaer Polytechnic Institute, Troy, NY Knoxville, Knoxville, TN; E. Smith, R. Bill, Aerospace Industries, Inc., Ankara, Turkey; R. Development and Engineering Center, Fort Theodore, NASA Ames Research Center, S. Rao, Pennsylvania State University, Bill, E. Smith, Pennsylvania State University, Eustis, VA Moffett Field, CA University Park, PA University Park, PA; H. Desmidt, University of Tennessee, Knoxville, Knoxville, TN Tuesday, 6 January 2015 197-STR-9 Special Session: Impact Damage in Composites Sun Ballroom D Chaired by: A. NAJAFI, ANSYS, Inc. and M. RASSAIAN, Boeing Engineering Operations & Technology 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2015-0956 AIAA-2015-0957 AIAA-2015-0958 AIAA-2015-0959 AIAA-2015-0960 AIAA-2015-0961 Face-on and Edge-on Impact Low-Velocity Impact Damage and Prediction of Low-velocity Impact An effective modeling strategy for Lagrange-based Modeling and Comparison of Delamination Response of Composite Laminates Delamination Crack Arrestment Damage in Sandwich Composite drop test analysis of composite Testing of Composite Structure Threshold Load Prediction of W. Ji, Ulsan National Institute of Science and with Translaminar Reinforcements Beams curved beam Impact Dynamics Composite Panels with Different Technology, Ulsan, Korea (the Republic of); V. Ranatunga, Miami University, J. Xie, S. Thorsson, J. Marek, A. Waas, D. Pham, Institute of High Performance A. Baeten, Augsburg University of Applied Thickness S. Sringeri, S. Thorsson, C. Kosztowny, A. Middletown, OH; S. Clay, Air Force University of Michigan, Ann Arbor, Ann Computing, Singapore, Singapore Sciences, Augsburg, Germany S. Gao, Z. Yu, H. Wang, Shanghai Jiao Waas, University of Michigan, Ann Arbor, Ann Research Laboratory, Wright-Patterson Arbor, MI Tong University, Shanghai, China Arbor, MI; M. Rassaian, The Boeing Company, AFB, OH Seattle, WA; et al. Tuesday, 6 January 2015 198-STR-10 Advanced Structures Tampa 1 Chaired by: J. ZIPAY, NASA-Johnson Space Center and P. GUSTAFSON, Western Michigan University 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs AIAA-2015-0962 AIAA-2015-0963 AIAA-2015-0964 AIAA-2015-0965 AIAA-2015-0966 Morphing structures: non-linear Damage Detection Threshold of Investigation the Finite Element Isogeometric Weak Coupling of Structural Characterization of composite shells with irregular Optically-Digitized Gas-Turbine Model and Impact Characteristics of Shell Structures Advanced Composite Tow-Steered planforms Engine Hardware Civil Aircraft Y. Guo, M. Ruess, Delft University of Shells with Large Cutouts E. Lamacchia, E. Eckstein, A. Pirrera, J. Wertz, C. Baudendistel, E. Henry, Y. Ren, Hunan University, Changsha, Technology, Delft, The Netherlands K. Wu, NASA Langley Research Center, P. Weaver, University of Bristol, Bristol, Universal Technology Corporation, China; J. Xiang, Z. Luo, J. Zheng, Beihang Hampton, VA; J. Turpin, Kansas Space United Kingdom Dayton, OH; J. Brown, Air Force Research University, Beijing, China Grant Consortium, Wichita, KS; N. Gardner, Laboratory, Wright-Patterson AFB, OH Analytical Services & Materials, Inc., Hampton, VA; B. Stanford, R. Martin, NASA Langley Research Center, Hampton, VA Tuesday, 6 January 2015 199-STR-11 Failure Analysis and Prediction II Tallahassee 3 Chaired by: S. SMELTZER, NASA Langely Research Center and P. MURTHY, NASA Glenn Research Center 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs AIAA-2015-0967 AIAA-2015-0968 AIAA-2015-0969 AIAA-2015-0970 AIAA-2015-0971 AIAA-2015-0972 AIAA-2015-0973 Modeling cure induced damage in The effect of free edges on inter- A novel two-scale progressive Fatigue Crack Initiation Analysis Damage Development 3D-RUC of Statistical Strength Determination Simulation of Distributed Co-Crack Fiber Reinforced Composites laminar performance of curved failure analysis method for of Roller Bearing Using Multiscale Polymer Matrix with Randomly of Carbon Fibres Using a Propagation in Cellular Automata R. D’Mello, M. Maiaru, A. Waas, laminates laminated fiber-reinforced modeling Distributed Fibers Generalized Weibull Model by Time Warp Synchronization University of Michigan, Ann Arbor, Ann T. Kim, T. Fletcher, T. Dodwell, R. Butler, R. composites M. Ghaffari, S. Xiao, University of Iowa, N. Parambil, S. Gururaja, Indian Institute H. Rajendran, P. Mohite, C. Upadhyay, Y. Park, D. Mavris, Georgia Institute of Arbor, MI; P. Prabhakar, University of Scheichl, University of Bath, Bath, United D. Zhang, D. Patel, A. Waas, University of Iowa City, Iowa City, IA of Science, Bangalore, India Indian Institute of Technology Kanpur, Technology, Atlanta, GA

108 Texas, El Paso, El Paso, TX Kingdom; J. Ankersen, GKN Aerospace Engine Michigan, Ann Arbor, Ann Arbor, MI Kanpur, India Systems, Bristol, United Kingdom; et al. Tuesday, 6 January 2015 200-SUR-1 Air and Space Survivability Tampa 3 Chaired by: J. RIMOLI, Georgia Institute of Technology and S. POROSEVA, The University of New Mexico 1400 hrs 1430 hrs 1500 hrs 1530 hrs AIAA-2015-0974 AIAA-2015-0975 AIAA-2015-0976 AIAA-2015-0977 Advanced Vertical Lift Aircraft Development of Methods for Topology Optimization of an Characterization of Spin Effects on Demonstrator: Design for Certification Characterization of Hydrodynamic Aircraft Wing Warhead Fragment Flyout Distance of a Hover Lift-Drive System Ram Cavity Dynamics D. Walker, D. Liu, Air Force Institute of J. Trombetta, M. Bennett, J. Hand, S. J. Silva-Martinez, W. Lee, A. Boshinski, A. Lingenfelter, D. Liu, Air Force Institute of Technology, Wright-Patterson AFB, OH Carpenter, D. Liu, Air Force Institute of Georgia Institute of Technology, Atlanta, GA Technology, Wright-Patterson AFB, OH Technology, Wright-Patterson AFB, OH Tuesday, 6 January 2015 201-TP-5 Nonequilibrium Flows and Radiation II Sun Ballroom B Chaired by: M. WINTER, University of Kentucky and D. HASH, NASA Ames Research Center 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs AIAA-2015-0978 AIAA-2015-0979 AIAA-2015-0980 AIAA-2015-0981 AIAA-2015-0982 AIAA-2015-0983 AIAA-2015-0984 Modeling of Non-equilibrium Nonequilibrium Plasma Flow Radiative Gasdynamics of Re-entry Measurements of Surface Sensitivity Analysis of Non- ‘Uncertainty Quantification Study Bluntness Effects on Hypersonic Plasmas in an Inductively Coupled Computation with Atomic and Space Vehicle of Large Size with Accommodation Coefficients for equilibrium Martian Entry Flow to of Non-Equilibrium Viscous Shock- Leading Edge Separation Plasma Facility Molecular State Transitions Superorbital Velocity Rarefied Aerodynamics Chemical and Thermal Modelling Layer’ A. Khraibut, S. Gai, A. Neely, University of W. Zhang, University of Illinois, Urbana- Y. Ogino, K. Totani, N. Ohnishi, Tohoku S. Surzhikov, Russian Academy of T. Ozawa, T. Suzuki, K. Fujita, Japan A. Preci, German Aerospace Center (DLR), T. Kino, K. Totani, T. Ishihara, Y. Ogino, N. New South Wales, Canberra, Australia Champaign, Urbana, IL; A. Lani, von Kármán University, Sendai, Japan Sciences, Moscow, Russia Aerospace Exploration Agency (JAXA), Cologne, Germany; M. Auweter-Kurtz, Ohnishi, Tohoku University, Sendai, Japan Institute for Fluid Dynamics, Rhode-Saint- Chofu, Japan German Aerospace Academy, Böblingen, Genèse, Belgium; M. Panesi, University of Germany Illinois, Urbana-Champaign, Urbana, IL Tuesday, 6 January 2015 202-UMS-3 UAS Sensor Technologies Osceola Ballroom 2 Chaired by: R. STANSBURY, Embry-Riddle Aeronautical University 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2015-0985 AIAA-2015-0986 AIAA-2015-0987 AIAA-2015-0988 AIAA-2015-0989 AIAA-2015-0990 From Radiosonde To Papersonde: Obstacle Avoidance System for SDAC-UAS: A Sensor Data Validation and Calibration of a High Autonomous Wall-Following Based A Ground Control Station for The Use of Conductive Inkjet Printing UAVs using Computer Vision Acquisition Unmanned Aerial Resolution Sensor in Unmanned Navigation of Unmanned Aerial Multivehicular Control and Data in the Massive Atmospheric Volume S. Bhandari, B. Richards, M. Gan, J. System for Flight State Monitoring Aerial Vehicles for Producing Vehicles in Indoor Environments Visualization Instrumentation System (MAVIS) Dayton, M. Enriquez, J. Liu, California and Aerodynamic Data Collection Images in the IR Range Utilizable A. Nemati, M. Sarim, M. Hashemi, M. S. Bhandari, M. Heid, A. Bettadapura, E. Project Polytechnic State University, Pomona, O. Dantsker, A. Louis, R. Mancuso, M. in Precision Agriculture Kumar, University of Toledo, Toledo, OH Ito, D. Tang, California Polytechnic State P. King, J. Scanlan, A. Sobester, University of CA; et al. Caccamo, M. Selig, University of Illinois, P. Jimenez Soler, D. Agudelo, University of University, Pomona, CA Southampton, Southampton, United Kingdom Urbana-Champaign, Urbana, IL San Buenaventura, Bogota, Colombia Tuesday, 6 January 2015 203-WE-7 Wind Energy Aerodynamics and Aeroacoustics III Emerald 6 Chaired by: E. WHITE, Texas A&M University and R. CHOW, University of California Davis 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2015-0991 AIAA-2015-0992 AIAA-2015-0993 AIAA-2015-0994 AIAA-2015-0995 AIAA-2015-0996 Flow Field Around a Serrated ECN-G1-21 Airfoil: Design and Aerodynamic Drag and Study of distributed roughness Aerodynamic Response of a Wind New airfoil family design for large Trailing Edge at Incidence Wind Tunnel Testing Aeroacoustic Noise Mitigation of effect over wind turbine airfoils Turbine Airfoil to Gurney Flap wind turbine blades C. Arce, LM Wind Power, Kolding, F. Grasso, Energy Research Center of the Flatback Airfoil with Spanwise performance using CFD Deployment M. Canal Vila, D. Miguel Alfaro, Alstom, Denmark; D. Ragni, S. Pröbsting, F. Netherlands, Petten, The Netherlands Wavy Trailing Edge B. Mendez, X. Munduate, CENER, P. Nikoueeyan, J. Strike, A. Magstadt, M. Barcelona, Spain Scarano, Delft University of Technology, S. Yang, J. Baeder, University of Maryland, Sarriguren, Spain Hind, J. Naughton, University of Wyoming, Delft, The Netherlands College Park, College Park, MD Laramie, Laramie, WY

109 Tuesday, 6 January 2015 204-WE-8 Wind Energy Materials, Mechanics, and Sensing Emerald 4 Chaired by: D. MILLER, Mechanical and Industrial Engineering 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2015-0997 AIAA-2015-0998 AIAA-2015-0999 AIAA-2015-1000 AIAA-2015-1001 AIAA-2015-1002 Fatigue Resistance of Wind Blade Development and Assessment Assessment of the Effect of Hybrid Development and Commissioning A Robust Algorithm to Detecting Evaluating the Aerodynamic Laminates Containing In-Plane of Advanced Inspection Methods GRFP-CFRP Usage in Wind Turbine of a Small / Mid-Size Wind Turbine Wind Turbine Blade Health Using Performance of Small Horizontal Waviness Flaws for Wind Turbine Blades Using a Blades on the Reduction of Fatigue Test Facility Vibro-Acoustic Modulation and Axis Wind Turbines D. Samborsky, D. Miller, D. Cairns, J. Focused WINDIE Experiment Damage Equivalent Loads in the D. Valyou, T. Arsenault, K. Janoyan, P. Sideband Spectral Analysis B. Wallace, D. McLaughlin, S. Stewart, Mandell, A. Lolatte, Montana State D. Roach, S. Neidigk, T. Rice, R. Duvall, J. Wind Turbine System Marzocca, Clarkson University, Potsdam, N. Myrent, D. Adams, Vanderbilt Pennsylvania State University, University University, Bozeman, MT Paquette, Sandia National Laboratories, O. Gözcü, T. Farsadi, C. Tola, A. Kayran, NY; N. Post, National Renewable Energy University, Nashville, TN; G. Rodriguez- Park, PA Albuquerque, NM Middle East Technical University, Ankara, Laboratory, Golden, CO; C. Grappasonni, Rivera, D. Ulybyshev, J. Vitek, Purdue Turkey University of Rome “La Sapienza”, Rome, University, West Lafayette, IN; E. Blanton, Italy; et al. Fiji Systems, Inc., South Bend, IN; et al. Tuesday, 6 January 2015 205-LEC-4 Dryden Lectureship in Research Osceola Ballroom CD 1730 - 1830 hrs Aeroacoustics Ann P. Dowling President Royal Academy of Engineering Tuesday, 6 January 2015 206-NW-1 Reception in the Exhibit Hall Exhibit Hall B/C 1830 - 2000 hrs Wednesday Wednesday, 7 January 2015 207-PLNRY-3 The Future of Design Osceola Ballroom CD 0800 - 0900 hrs Moderator: Richard Christiansen, Vice President, Sierra Lobo, Inc. Panelists: Juan Alonso Robert Liebeck Mark Maughmer Associate Professor, Department of Aeronautics Senior Technical Fellow Professor of Aerospace Engineering Stanford University The Boeing Company Pennsylvania State University

Wednesday, 7 January 2015 208-AA-7 Jet Noise Prediction II Miami 2 Chaired by: P. MORRIS, Pennsylvania State University 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2015-1003 AIAA-2015-1004 AIAA-2015-1005 AIAA-2015-1006 AIAA-2015-1007 The Prediction of Scattered Linear Analysis of Jet-Engine Core Empirical Source Strength Towards a Low-Cost Wavepacket Assessing Prediction and Reduction Broadband Shock-Associated Noise Noise Based upon High-Fidelity Correlations for RANS-Based Model of the Jet Noise Source Technique of Lift-off Acoustics Using S. Miller, NASA Langley Research Center, Combustor and Turbine Simulations Acoustic Analogy Methods D. Papamoschou, J. Xiong, F. Liu, Epsilon Flight Data Hampton, VA J. O’Brien, J. Kim, M. Ihme, Stanford M. Kube-McDowell, G. Blaisdell, Purdue University of California, Irvine, Irvine, CA S. Tsutsumi, Japan Aerospace Exploration University, Stanford, CA University, West Lafayette, IN; A. Lyrintzis, Agency (JAXA), Sagamihara, Japan; T. Embry-Riddle Aeronautical University, Ishii, Japan Aerospace Exploration Agency Daytona Beach, FL (JAXA), Chofu, Japan; K. Ui, Japan Aerospace Exploration Agency (JAXA), Tsukuba, Japan;

110 S. Tokudome, Japan Aerospace Exploration Agency (JAXA), Sagamihara, Japan; K. Wada, Science Service, Inc., Chuuou-ku, Japan Wednesday, 7 January 2015 209-ACD-2 High Speed Aircraft Design Tallahassee 2 Chaired by: S. KOMADINA, Northrop Grumman Aerospace Systems 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2015-1008 AIAA-2015-1009 AIAA-2015-1010 Oral Presentation Oral Presentation The Design, Analysis and On the Conceptual Design of A Design Space Exploration TU Delft Advanced Transonic TU Delft SMART, Winner AIAA Performance Evaluation of Waverider Forebody Geometries Methodology to Support Decisions Trainer, Winner AIAA Graduate Team Aircraft Design Waverider Configurations for K. Kontogiannis, A. Sobester, University under Evolving Requirements’ Undergraduate Individual Design Competition Hypersonic Vehicle Applications of Southampton, Southampton, United Uncertainty and its Application to Competition R. Klein, Delft University of Technology, F. Ferguson, N. Dasque, M. Dhanasar, Kingdom; N. Taylor, MBDA, Bristol, United Suborbital Vehicles S. van Schie, Delft University of Delft, The Netherlands North Carolina A&T State University, Kingdom C. Frank, O. Pinon-Fischer, D. Mavris, Technology, Delft, The Netherlands Greensboro, NC Georgia Institute of Technology, Atlanta, GA Wednesday, 7 January 2015 210-ACD-3 Aircraft Design Tools Naples 3 Chaired by: A. HAHN, NASA-Langley Research Center 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2015-1012 AIAA-2015-1013 AIAA-2015-1014 AIAA-2015-1015 AIAA-2015-1016 Oral Presentation Closing the Loop on Aircraft Artificial Neural Networks Applied Interactive Reconstruction of 3D Multi-section Wing Capability for Parametric Identification of Surface Demonstration of new Capabilities Conceptual Sizing using the Merlin to Airplane Design Models in the OpenVSP Parametric the Vehicle Sketch Pad Structural Regions in OpenVSP for Improved of OpenVSP v3.0.0 Flight Simulator N. Secco, B. Mattos, Technological Geometry Tool Analysis Module Engineering Analysis R. McDonald, California Polytechnic State A. Altman, University of Dayton, Dayton, OH Institute of Aeronautics (ITA), São José R. McDonald, California Polytechnic State A. Chaput, University of Texas, Austin, A. Gary, R. McDonald, California Polytechnic University, San Luis Obispo, CA dos Campos, Brazil University, San Luis Obispo, CA Austin, TX State University, San Luis Obispo, CA Wednesday, 7 January 2015 211-AFM-9 Launch Vehicle, Missile, and Projectile Flight Mechanics I Captiva 2 Chaired by: P. WERNERT, French-German Research Institute of Saint-Louis (ISL) 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2015-1017 AIAA-2015-1018 AIAA-2015-1019 AIAA-2015-1020 AIAA-2015-1021 Integration of Grid Fins for the An Improved Method to Calculate Robust Stability Evaluation of Euler-Lagrange Optimal Control for Elliptical Trajectory Guidance Optimal Design of Missile Systems the Nonlinear Rolling Moment Due the Space Launch System Control Symmetric Projectiles Law with Terminal Impact Angle T. Ledlow, J. Burkhalter, R. Hartfield, to Differential Fin Deflection of Design: A Singular Value Approach B. Burchett, A. Nash, Rose-Hulman Constraint Auburn University, Auburn, AL Canard Controlled Missiles J. Pei, NASA Langley Research Center, Institute of Technology, Terre Haute, IN T. Zhang, H. She, Beijing Institute of F. Moore, L. Moore, G. McGowan, Hampton, VA; J. Newsom, Analytical Technology, Beijing, China Aeroprediction, Inc., King George, VA Mechanics Associates, Inc., Hampton, VA Wednesday, 7 January 2015 212-AFM-10 Air Launch to Orbit (Invited) Sun Ballroom B 0930 - 1230 hrs Chaired by: J. DEL FRATE, NASA Dryden Flight Research Center and P. WILLIAMS-HAYES, NASA Armstrong Flight Research Center This session will focus on efforts to develop air-launch systems that place small satellites and payloads into low Earth orbit without the use of conventional ground-based launch systems. Speakers from the U.S. Air Force, Defense Advanced Research Projects Agency (DARPA), Federal Aviation Administration (FAA), Orbital Sciences Corporation, and National Aeronautics and Space Administration (NASA) efforts will brief results of past programs and discuss current progress. Following these informational briefings, a group of panelists will participate in a discussion with the audience. This session is intended to gather a community of practice and provide networking opportunities for attendees. Moderators: John F. Carter, Director, Exploration and Space Technology Missions, NASA Neil A. Armstrong Flight Research Center John Del Frate, Director, Advanced Planning and Partnerships, NASA Neil A. Armstrong Flight Research Center Invited Speakers: Doug Pearson Mitchell Burnside Clapp Jerry Budd Antonio Elias Michael S. Kelly U.S. Air Force (Gen, Retired) Program Manager Air Launch Development Project Manager Executive Vice President and Chief Technical Officer Chief Engineer, Office of Commercial Space Transportation 111 DARPA Tactical Technology Office NASA Neil A. Armstrong Flight Research Center Orbital Sciences Corporation Federal Aviation Administration

Wednesday, 7 January 2015 213-AMT-3 Novel Diagnostics in Reacting Flows Tallahassee 1 Chaired by: B. MA, GE Global Research Center and C. JOHANSEN, University of Calgary 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2015-1022 AIAA-2015-1023 AIAA-2015-1024 AIAA-2015-1025 Experimental Characterization Experimental study of transverse Multi-Beam, High-Repetition-Rate Quantitative Temperature Imaging of Decay Rates in Bluff-Body jet mapping using PLIF Thermometry in a Gas Turbine in Turbulent Non-Premixed Flames Stabilized Flames Using Sodium L. Thompson, G. Natsui, C. Velez, J. Combustor Test Rig using Time- Using Filtered Rayleigh Scattering Injection Kapat, S. Vasu, University of Central Division-Multiplexed Tunable Diode T. McManus, J. Sutton, Ohio State J. Monfort, University of Dayton, Dayton, Florida, Orlando, FL Lasers University, Columbus, OH OH; A. Caswell, V. Belovich, Air Force A. Caswell, Air Force Research Laboratory, Research Laboratory, Wright-Patterson Wright-Patterson AFB, OH; K. Rein, S. Roy, AFB, OH; B. Huelskamp, Innovative Spectral Energies, LLC, Dayton, OH; S. Scientific Solutions, Inc., Dayton, OH Stouffer, University of Dayton, Dayton, OH; A. Lynch, E. Corporan, Air Force Research Laboratory, Wright-Patterson AFB, OH; et al. Wednesday, 7 January 2015 214-APA-20 Propeller/Rotorcraft/Wind Turbine Aerodynamics I Naples 2 Chaired by: K. KARA, Khalifa University of Science, Technology & Research and C. SHENG, University of Toledo 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2015-1026 AIAA-2015-1027 AIAA-2015-1028 AIAA-2015-1029 AIAA-2015-1030 Analysis of propeller-airframe Computational Simulation Testing and Evaluation of Passively Experimental Feasibility Effect of Duct-Rotor Aerodynamic interaction effects through a of Pusher-Tractor Propeller Actuated Vanes Operating near Assessment of Counter-Rotating Interactions on Blade Design for combined numerical simulation and Configurations for Unmanned Air Propeller Tip Propellers for Stratospheric Airships Hover and Axial Flight wind-tunnel testing approach Vehicles W. Loh, J. Jacob, Oklahoma State P. Liu, Z. Tang, Y. Chen, H. Guo, Beihang B. Jimenez, Oak Ridge Institute for A. Gomariz-Sancha, M. Maina, A. Peace, U. Kaynak, TOBB University of Economics University, Stillwater, OK University, Beijing, China Science and Education, Aberdeen, MD; Aircraft Research Association, Ltd., and Technology, Ankara, Turkey R. Singh, Army Research Laboratory, Bedford, United Kingdom Aberdeen Proving Ground, MD Wednesday, 7 January 2015 215-APA-21 Airfoil/Wing/Configuration Aerodynamics II Destin 2 Chaired by: A. MCCOMAS, TLG Aerospace and J. LATZ, Northrop Grumman Aerospace Systems 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2015-1031 AIAA-2015-1032 AIAA-2015-1033 AIAA-2015-1034 AIAA-2015-1035 Demonstration of a Conceptual Numerical Study of Intermittent 3D stall-cells investigation on a Airfoil Designs for a Small and Simulation of a MW rotor equipped Design Tool for Multiple Lifting Laminar Bubble Bursting and NACA64418 Large Horizontal Axis Wind Turbine with vortex generators using CFD Elements Vortex Shedding on an NACA D. Ragni, C. Simao Ferreira, Delft D. Hall, Self, Mechanicsville, MD and an actuator shape model W. Bissonnette, G. Bramesfeld, Ryerson 64_3-618 Airfoil University of Technology, Delft, The N. Troldborg, N. Sørensen, F. Zahle, P. University, Toronto, Canada A. Jost, J. Zhang, Florida Institute of Netherlands Réthoré, Technical University of Denmark, Technology, Melbourne, FL Roskilde, Denmark

112 Wednesday, 7 January 2015 216-APA-22 Flow Control Applications & Demonstrations (Active & Passive) I Naples 1 Chaired by: B. CYBYK, The Johns Hopkins University Applied Physics Laboratory and J. GEORGE, Metrolaser Inc. 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2015-1036 AIAA-2015-1037 AIAA-2015-1038 AIAA-2015-1039 Plasma Flow Control on a Landing Analysis of the Near-Field of Dynamic Stall Alleviation for an Effect of Vertical Strakes on Gear Model an Asymmetrically Controlled SC1095 Airfoil using Synthetic Jets Suppression of Wing Rock in M. Wicks, F. Thomas, T. Corke, University Supersonic Round Jet S. Tran, A. Fisher, Rensselaer Polytechnic Slender Delta Wing of Notre Dame, Notre Dame, IN; C. D. Gonzalez, Naval Surface Warfare Institute, Troy, NY; D. Corson, Altair S. Bakaul, Military Institute of Science Nelson, M. Patel, A. Cain, Innovative Center, Indian Head, MD; D. Gaitonde, Engineering, Inc., Clifton Park, NY; O. and Technology, Dhaka, Bangladesh; Y. Technology Applications Company, LLC, Ohio State University, Columbus, OH; Sahni, Rensselaer Polytechnic Institute, Wang, W. Guangxing, Beihang University, Chesterﬁeld, MO M. Lewis, Science and Technology Policy Troy, NY Beijing, China Institute, Washington, DC Wednesday, 7 January 2015 217-APA-23 Special Session: CREATE-AV High Performance Computing Multiphysics Applications of Full-up Air Vehicles III Destin 1 Chaired by: N. HARIHARAN, CREATE-AV and R. JAIN, AFDD, US Army 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2015-1040 AIAA-2015-1041 AIAA-2015-1042 AIAA-2015-1043 Applications of CREATE-AV Dual Mesh CFD Solver Comparison Dynamic Modeling of an Aircraft A-10 Analysis Using HPCMP KestrelTM v5 with Cartesian of Low Mach Flow over the ROBIN Primary Thrusting Nozzle CREATETM-AV Kestrel Product Adaptive Mesh Reﬁnement Fuselage J. Masters, Arnold Engineering Utilizing the Firebolt Propulsion T. Shafer, Naval Air Systems Command, J. Abras, Naval Air Systems Command, Development Complex, Arnold AFB, TN Component Patuxent River, MD; T. Eymann, CREATE Patuxent River, MD; N. Hariharan, CREATE J. Klepper, R. Nichols, J. Jenkins, AEDC, AV Team, Eglin AFB, FL; J. Forsythe, AV Team, Lorton, VA Tullahoma, TN B. Hallissy, D. Hine, Naval Air Systems Command, Patuxent River, MD Wednesday, 7 January 2015 218-APA-24 Special Session: Low Boom Activities I Miami 3 Chaired by: L. BANGERT, NASA Langley Research Center and K. WAITHE, Gulfstream Aerospace Corporation 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2015-1044 AIAA-2015-1045 AIAA-2015-1046 AIAA-2015-1047 AIAA-2015-1048 Computational and Experimental Airframe-Nozzle-Plume Interactions Plume and Shock Interaction Effects Aerodynamic Shape Optimization Acoustically Induced Shock Study of Supersonic Nozzle Flow in the Context of Low Sonic Boom on Sonic Boom in the 1-foot by of a Two-Stream Supersonic Plug Oscillations of a Low-Boom Inlet and Shock Interactions Design 1-foot Supersonic Wind Tunnel Nozzle S. Candon, E. Loth, University of Virginia, M. Carter, A. Elmiligui, NASA Langley Research M. Wintzer, NASA Langley Research R. Castner, NASA Glenn Research Center, C. Heath, NASA Glenn Research Center, Charlottesville, Charlottesville, VA Center, Hampton, VA; S. Nayani, Analytical Center, Hampton, VA; R. Castner, NASA Cleveland, OH; S. Cliff, NASA Ames Cleveland, OH; E. Nielsen, M. Park, NASA Services & Materials, Inc., Hampton, VA; Glenn Research Center, Cleveland, OH Research Center, Moffett Field, CA; Langley Research Center, Hampton, VA; R. Castner, NASA Glenn Research Center, A. Elmiligui, C. Winski, NASA Langley J. Gray, NASA Glenn Research Center, Cleveland, OH; W. Bruce, University of Virginia, Research Center, Hampton, VA Cleveland, OH Charlottesville, Charlottesville, VA; J. Inskeep, West Virginia University, Morgantown, WV Wednesday, 7 January 2015 219-AS-4 Compliant Structures Osceola Ballroom 6 Chaired by: W. YU, Purdue University and R. BOTEZ 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2015-1049 AIAA-2015-1050 AIAA-2015-1051 AIAA-2015-1052 AIAA-2015-1053 AIAA-2015-1054 Design and Testing of a Compliant Variable Camber Compliant Wing Variable Camber Compliant Wing - Implementation of a Contact Chiral Morphing Wing Tip Design Active Camber Morphing Wings Mechanism-based Demonstrator for - Design Wind Tunnel Testing Model in a Topology Optimization and Test Based on Compliant Structures: an a Droop-Nose Morphing Device J. Joo, Air Force Research Laboratory, C. Marks, L. Zientarski, University of Method for the Design of Compliant C. Wales, R. Cheung, J. Cooper, University Aeroelastic Assessment S. Vasista, J. Riemenschneider, H. Wright-Patterson AFB, OH; C. Marks, L. Dayton, Dayton, OH; A. Culler, B. Hagen, Mechanisms for Thermal Control of Bristol, Bristol, United Kingdom A. De Gaspari, S. Ricci, L. Travaglini, L.

113 Monner, German Aerospace Center (DLR), Zientarski, University of Dayton, Dayton, Sierra Lobo, Inc., Wright-Patterson AFB, P. Thurier, G. Lesieutre, M. Frecker, J. Cavagna, Technical University of Milan, Milan, Braunschweig, Germany OH; A. Culler, Sierra Lobo, Inc., Wright- OH; B. Smyers, J. Joo, Air Force Research Adair, Pennsylvania State University, Italy; A. Antunes, F. Odaguil, Embraer, São Patterson AFB, OH Laboratory, Wright-Patterson AFB, OH University Park, PA José dos Campos, Brazil; et al. Wednesday, 7 January 2015 220-FD-28 Current Challenges for Computational Fluid Dynamics, Industry and Government Interests I (Invited) Sun Ballroom A Chaired by: H. HUYNH, NASA Glenn Research Center and N. KROLL, DLR - German Aerospace Center 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs Oral Presentation Oral Presentation Oral Presentation Oral Presentation Oral Presentation Oral Presentation Challenges for the Application of Current Challenges for Industrial Challenges to the use of CFD in the Current Challenges for CFD Towards an end to end integrated high CFD, past, present, and future CFD in a Production Aircraft Design Application of LES Turbulence Military Aircraft Industry (Invited) (Invited) order flow simulation system (Invited) (Invited) Environment (Invited) Models (Invited) B. Smith, Lockheed Martin Corporation, B. Glaz, Army Research Laboratory, W. Dawes, Y. Lu, Cambridge University, A. Jameson, Stanford University, Stanford, J. Vassberg, The Boeing Company, Long R. Bush, Pratt & Whitney, East Hartford, Fort Worth, TX Aberdeen Proving Ground, MD Cambridge, United Kingdom CA Beach, CA CT Wednesday, 7 January 2015 221-FD-29 Flow Control (Fundamentals and Technology) II Sanibel 3 Chaired by: D. WILLIAMS, Illinois Institute of Technology and J. BONS, Ohio State University 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2015-1055 AIAA-2015-1056 AIAA-2015-1057 AIAA-2015-1058 AIAA-2015-1059 AIAA-2015-1060 Control of a Model Secondary Flow Comparison of a Separated Flow Spatial Growth of the Spanwise Model Reduction and Analysis of Deep Control of Three-Dimensional Concept of Fluid Motion Scale Targeting Convective Instabilities Response to Localized and Global- Disturbance Induced by a Synthetic Dynamic Stall on a Plunging Airfoil Cavity Flow Using Leading-Edge Control and Its Realization S. Benton, J. Bons, Ohio State University, type Disturbances Jet on Separation Control over an using Dynamic Mode Decomposition Slot Blowing N. Yurchenko, National Academy of Columbus, OH B. Monnier, D. Williams, Illinois Institute Airfoil A. Mohan, Ohio State University, Columbus, B. George, L. Ukeiley, University of Sciences of Ukraine, Kiev, Ukraine of Technology, Chicago, IL; T. Weier, T. Y. Abe, University of Tokyo, Sagamihara, OH; M. Visbal, Air Force Research Laboratory, Florida, Gainesville, Gainesville, FL; Albrecht, Helmholtz-Zentrum Dresden- Japan; T. Nonomura, K. Fujii, Japan Wright-Patterson AFB, OH; D. Gaitonde, Ohio L. Cattafesta, K. Taira, Florida State Rossendorf, Dresden, Germany Aerospace Exploration Agency (JAXA), State University, Columbus, OH University, Tallahassee, FL Sagamihara, Japan Wednesday, 7 January 2015 222-FD-30 Hypersonic Flows Daytona 1 Chaired by: E. STEPHEN, Vanderbilt University and R. BOWERSOX, Texas A&M University 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2015-1061 AIAA-2015-1062 AIAA-2015-1063 AIAA-2015-1064 Gas flow in a generic inlet with Large-Eddy Simulation of a Three- Three dimensional vortex modes of Preliminary LES of Hypersonic blunted leading edges Dimensional Hypersonic Shock hypersonic steady-state flow on the Shock/Turbulent Boundary Layer V. Radchenko, V. Borovoy, V. Mosharov, Wave Turbulent Boundary Layer blunted bodies leading age Interactions A. Skuratov, I. Struminskaya, TsAGI, Interaction of a Single-Fin S. Drozdov, TsAGI, Zhukovsky, Russia C. Helm, M. Martin, University of Zhukovsky, Russia J. Fang, Beihang University, Beijing, China; Y. Maryland, College Park, College Park, MD Yao, University of the West of England, Bristol, United Kingdom; A. Zheltovodov, Russian Academy of Sciences, Novosibirsk, Russia; L. Lu, Beihang University, Beijing, China Wednesday, 7 January 2015 223-FD-31 Unsteady Flow I Sun Ballroom 6 Chaired by: R. GORDNIER, Air Force Reseach Laboratory and Z. YANG, Wright State University 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2015-1065 AIAA-2015-1066 AIAA-2015-1067 AIAA-2015-1068 AIAA-2015-1069 Streamwise oscillation of airfoils Streamwise-oriented vortex Implicit LES Computation of a Investigation of Incompressible Unsteady Aerodynamic Response into reverse flow interactions with a NACA0012 wing Vortical-Gust/Wing Interaction for Dynamic Stall Physics by Modeling: A Parameter-Varying K. Granlund, M. Ol, Air Force Research D. Garmann, M. Visbal, Air Force Research Transitional Flow Application of a Parametric Proper Approach Laboratory, Wright-Patterson AFB, OH; A. Laboratory, Wright-Patterson AFB, OH R. Gordnier, M. Visbal, Air Force Research Orthogonal Decomposition M. Hemati, S. Dawson, C. Rowley, Jones, University of Maryland, College Laboratory, Wright-Patterson AFB, OH D. Coleman, F. Thomas, S. Gordeyev, Princeton University, Princeton, NJ 114 Park, College Park, MD K. Heintz, T. Corke, University of Notre Dame, Notre Dame, IN Wednesday, 7 January 2015 224-GNC-21 Advances in UAS Technologies I Miami 1 Chaired by: S. CHUNG, University of Illinois at Urbana-Champaign and J. VALASEK, Texas A&M University 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2015-1070 AIAA-2015-1071 AIAA-2015-1072 AIAA-2015-1073 AIAA-2015-1074 Position Control for Free-Designed Source Localization For A Turbulent High Velocity Path Control of Synthesis and flight test of an Disturbance Rejection with Generic Multi Rotor Vehicle Systems Plume Model Using Bayesian Quadrotors automatic landing controller using Distributed Acceleration and Strain with Augmented L1 Adaptive Occupancy Grid Mapping J. Wang, T. Raffler, F. Holzapfel, Technical Quantitative Feedback Theory Sensing Control H. Abdelghaffar, C. Woolsey, Virginia University of Munich, Munich, Germany T. Woodbury, J. Valasek, Texas A&M G. Gremillion, L. Castano, J. Humbert, Z. Wang, F. Holzapfel, Technical University Polytechnic Institute and State University, University, College Station, TX University of Maryland, College Park, of Munich, Munich, Germany Blacksburg, VA College Park, MD Wednesday, 7 January 2015 225-GNC-22 Trajectory Planning and Optimization I Sun Ballroom 3 Chaired by: A. LAMPTON, Systems Technology, Inc. and F. HUGON, Gulfstream Aerospace Corporation 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2015-1075 AIAA-2015-1076 AIAA-2015-1077 AIAA-2015-1078 AIAA-2015-1079 AIAA-2015-1080 Dynamic Programming Trajectory Rapid Mission Planning for Aircraft Mobile Target Tracking Using an Multiresolution Aircraft Guidance Optimal Cruise Altitude for Aircraft Vulnerability of UAV Sense Optimization by Piecewise Linear Thermal Management Unmanned Aerial Vehicle with a in a Spatiotemporally-varying Thermal Management and Avoid to Exploitations: Approximation D. Doman, Air Force Research Laboratory, Non-Gimbaled Video Sensor Threat Field D. Doman, Air Force Research Laboratory, Non-Cooperative Trajectory A. Harada, H. Matsuda, Y. Miyazawa, Wright-Patterson AFB, OH L. Sun, D. Pack, University of Texas, San R. Cowlagi, Worcester Polytechnic Wright-Patterson AFB, OH Modifications Kyushu University, Fukuoka, Japan Antonio, San Antonio, TX Institute, Worcester, MA P. Pierpaoli, R. Zanforlin, A. Rahmani, University of Miami, Coral Gables, FL Wednesday, 7 January 2015 226-GNC-23 Optimization Based Methods for Estimation and Control of Flight Vehicles Sun Ballroom 4 Chaired by: Z. ZHAO, University of Calgary and A. RAO, University of Florida 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2015-1081 AIAA-2015-1082 AIAA-2015-1083 AIAA-2015-1084 AIAA-2015-1085 AIAA-2015-1086 Estimated Time of Arrival Prediction Modeling and Simulation of a Fish- Fault Detection and Isolation for A Split-Bernstein/MCMC Approach Utilizing the Algorithmic Impulsive Spacecraft Formation based on State-Dependent like Swimmer in an Ideal Flow with Air Data Sensors Using Real-Time to Probabilistically Constrained Differentiation Package ADiGator for Maneuvers with Optimal Firing Transition Hybrid Estimation Lateral-line Flow Sensors Moving Horizon Estimation Optimization Solving Optimal Control Problems Times Algorithm Y. Xu, K. Mohseni, University of Florida, Y. Wan, T. Keviczky, Delft University of Z. Zhao, M. Kumar, University of Florida, Using Direct Collocation L. Sobiesiak, C. Damaren, University of J. Wei, J. Lee, I. Hwang, Purdue Gainesville, Gainesville, FL Technology, Delft, The Netherlands Gainesville, Gainesville, FL M. Weinstein, M. Patterson, A. Rao, University Toronto, Toronto, Canada University, West Lafayette, IN of Florida, Gainesville, Gainesville, FL Wednesday, 7 January 2015 227-GNC-24 Spacecraft Guidance, Navigation, and Control II Sun Ballroom 5 Chaired by: K. BOLLINO, AFOSR/EOARD 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2015-1087 AIAA-2015-1088 AIAA-2015-1090 AIAA-2015-1091 AIAA-2015-1092 Flywheel Parameters and Fault-Tolerant Attitude Control Systems Generalized Dynamics of A An Integrated Steering Law Singularity Analysis of Control Configuration Skew Angle using Multi-Objective Optimization for Spacecraft with Plural MEDs and Considering Biased Loads and Moment Gyros on Gyroelastic Body Distribution for Variable Speed a Spacecraft Equipped with Control Attitude Control with DGVSCMGs via Singularity for Control Moment Q. Hu, Z. Wang, J. Zhang, Y. Jia, Beihang Control Moment Gyro Moment Gyros LPV Control Theory Gyroscopes University, Beijing, China; M. Liu, Z. Zhou, F. Liu, Harbin Institute of Technology, A. Noumi, M. Takahashi, Keio University, T. Sasaki, T. Shimomura, Osaka Prefecture Y. Nanamori, M. Takahashi, Keio China Academy of Space Technology, Harbin, China Yokohama, Japan; T. Kanzawa, M. Haruki, University, Sakai, Japan University, Yokohama, Japan Beijing, China Japan Aerospace Exploration Agency (JAXA), Tsukuba, Japan 115 Wednesday, 7 January 2015 228-GT-3 ETW Test on Separated Wing Flow within the EU FP7 ESWIRP Project (Invited) Sanibel 1 Chaired by: J. QUEST, ETW GmbH and R. PARYZ 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs Oral Presentation AIAA-2015-1093 AIAA-2015-1094 AIAA-2015-1095 AIAA-2015-1096 AIAA-2015-1097 ETW scientific Access in ESWIRP Comparison of the NASA Common Time-resolved Prediction and High-Speed PIV Applied to Wake Unsteady Wake Flow Analysis of Dynamic Measurements on the T. Lutz, University of Stuttgart, Stuttgart, Research Model European Transonic Measurement of the Wake past the of NASA CRM Model in ETW Under an Aircraft under low-speed Stall NASA CRM Model tested in ETW Germany; J. Quest, European Transonic Wind Tunnel Test Data to NASA Test CRM at high Reynolds number stall High Re-Number Stall Conditions Conditions using DES and PIV H. Quix, A. Hensch, European Transonic Windtunnel, Cologne, Germany; J. Godard, Data (Invited) conditions for Sub- and Transonic Speeds A. Waldmann, University of Stuttgart, Windtunnel, Cologne, Germany ONERA, Paris, France M. Rivers, NASA Langley Research T. Lutz, University of Stuttgart, Stuttgart, R. Konrath, German Aerospace Center Stuttgart, Germany Center, Hampton, VA; R. Rudnik, German Germany (DLR), Göttingen, Germany Aerospace Center (DLR), Braunschweig, Germany; J. Quest, European Transonic Windtunnel, Cologne, Germany Wednesday, 7 January 2015 229-GTE-5 Gas Turbine Combustion II Emerald 1 Chaired by: S. VASU, University of Central Florida 0930 hrs 1000 hrs 1030 hrs AIAA-2015-1098 AIAA-2015-1099 AIAA-2015-1100 The Effect of Fluid Mechanics on High-Speed Imaging of Combustion Ignition of Hydrogen-Air and the Temperature Evolution of Spark Oscillations in a Multiple Nozzle Methane-Air Mixtures by PS DBD Kernels Staged Combustor Plasma at Elevated Pressures S. Okhovat, D. Blunck, Oregon State B. Dolan, R. Villalva Gomez, University A. Starikovskiy, Princeton University, University, Corvallis, OR of Cincinnati, Cincinnati, OH; G. Zink, S. Princeton, NJ Pack, United Technologies Corporation, West Des Moines, IA; E. Gutmark, University of Cincinnati, Cincinnati, OH Wednesday, 7 January 2015 230-HSABP-7 Pressure Gain Combustion - Rotating Detonation Engines III Emerald 3 Chaired by: D. PAXSON, NASA Glenn Research Center and F. LU, University of Texas at Arlington 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2015-1101 AIAA-2015-1102 AIAA-2015-1103 AIAA-2015-1104 AIAA-2015-1105 Comparison of Numerically Comparison of Transient Response Statistical Treatment of Wave Experimental Investigation of a Experimental Analogue of a Pre- Simulated and Experimentally of Pressure Measurement Instability in Rotating Detonation Rotating Detonation Engine Injector Mixed Rotating Detonation Engine Measured Performance of a Techniques with Application to Combustors Temporal Response In Plane Flow Rotating Detonation Engin Detonation Waves V. Anand, A. St. George, R. Driscoll, A. Naples, J. Hoke, Innovative Scientific I. Andrus, P. King, Air Force Institute of D. Paxson, NASA Glenn Research Center, C. Stevens, Innovative Scientific Solutions, E. Gutmark, University of Cincinnati, Solutions, Inc., Dayton, OH; F. Schauer, Technology, Wright-Patterson AFB, OH; Cleveland, OH; M. Fotia, J. Hoke, Inc., Dayton, OH; M. Fotia, National Cincinnati, OH Air Force Research Laboratory, Wright- M. Fotia, F. Schauer, Air Force Research Innovative Scientific Solutions, Inc., Research Council, Dayton, OH; J. Hoke, Patterson AFB, OH Laboratory, Wright-Patterson AFB, OH; J. Dayton, OH; F. Schauer, Air Force Research Innovative Scientific Solutions, Inc., Hoke, Innovative Scientific Solutions, Inc., Laboratory, Wright-Patterson AFB, OH Dayton, OH; F. Schauer, Air Force Research Dayton, OH Laboratory, Wright-Patterson AFB, OH Wednesday, 7 January 2015 231-HSABP-8 High Speed Air-Breathing Combustors II Emerald 8 Chaired by: F. MALO-MOLINA, Air Force Reseach Laboratory and R. SPRINGER, The Johns Hopkins University Applied Physics Laboratory 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2015-1106 AIAA-2015-1107 AIAA-2015-1108 AIAA-2015-1109 Thrust Augmentation Optimisation Analysis of High Temperature Design Modifications of a Numerical investigation of high- through Supersonic After-Burning Deposition as Flow Control in a Supersonic Wind Tunnel for High pressure combustion in rocket engines in Scramjet Engine Nozzles via Supersonic Combustor Speed Mixing Research of a Novel using Flamelet/Progress-variable Surrogate-Assisted Evolutionary F. Malo-Molina, Air Force Research Injector in a Scramjet Combustor models 116 Algorithms Laboratory, Wright-Patterson AFB, OH L. Smith, S. Farokhi, University of Kansas, A. Coclite, Technical University of Milan, Bari, M. Candon, H. Ogawa, G. Dorrington, Lawrence, Lawrence, KS Italy; L. Cutrone, Italian Aerospace Research RMIT University, Melbourne, Australia Center (CIRA), Capua, Italy; G. Pascazio, P. De Palma, Technical University of Milan, Bari, Italy Wednesday, 7 January 2015 232-IS-7 Intelligent Interactions between Humans and Machines Osceola Ballroom 3 Chaired by: M. GOMBOLAY, MIT and J. SHAH, MIT - Massachusetts Institute of Technology 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2015-1110 AIAA-2015-1112 AIAA-2015-1113 AIAA-2015-1114 AIAA-2015-1111 Toward the Development of a Flight Envelope Information- Trajectory Prediction and Alerting Verifying Correctness of Designing a Human-Computer Low-Altitude Air Traffic Control Augmented Display for Enhanced for Aircraft Mode and Energy State Information in Flight-Deck User Cooperation Decision Planning Paradigm for Networks of Small, Pilot Situational Awareness Awareness Interface using Hybrid System System for Aircraft Carrier Deck Autonomous Unmanned Aerial K. Ackerman, E. Xargay, D. Talleur, R. K. Shish, Millennium Engineering and Observability Scheduling Vehicles Carbonari, A. Kirlik, N. Hovakimyan, Integration Company, Moffett Field, CA; B. Yang, P. Menon, Optimal Synthesis, Z. Zhang, S. Lin, R. Dong, Q. Zhu, Harbin A. Hutchins, M. Cummings, M. Aubert, S. University of Illinois, Urbana-Champaign, J. Kaneshige, D. Acosta, S. Schuet, NASA Inc., Los Altos, CA; I. Hwang, Purdue Engineering University, Harbin, China Uzumcu, Duke University, Durham, NC Urbana, IL; et al. Ames Research Center, Moffett Field, CA; T. University, West Lafayette, IN Lombaerts, German Aerospace Center (DLR), Wessling, Germany; L. Martin, San Jose State University, Moffett Field, CA; et al. Wednesday, 7 January 2015 233-IS-8 Model-Based Systems and Software Engineering for Complex Aerospace Systems Osceola Ballroom 2 Chaired by: M. INGHAM, Jet Propulsion Laboratory 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2015-1115 Oral Presentation AIAA-2015-1116 AIAA-2015-1117 Ontology and Modeling Patterns The Engineering Modeling System: Connecting Requirements to Intelligent Planning Systems for for State-Based Behavior A Model-Based Engineering Architecture and Analysis via Space Resiliency Representation Environment for Integrated Model-Based Systems Engineering P. Zetocha, R. Sivilli, Air Force Research J. Castet, M. Rozek, M. Ingham, N. Systems Engineering B. Cole, J. Jenkins, Jet Propulsion Laboratory, Kirtland AFB, NM; D. Rouquette, S. Chung, J. Jenkins, Jet C. Delp, D. Lam, C. Lee, B. Clement, S. Laboratory, California Institute of Surka, Applied Technology Associates, Propulsion Laboratory, California Institute Wong, Jet Propulsion Laboratory, California Technology, Pasadena, CA Albuquerque, NM of Technology, Pasadena, CA; et al. Institute of Technology, Pasadena, CA Wednesday, 7 January 2015 234-MAT-8 Constitutive Modeling & Metallics Sarasota 1 Chaired by: V. TOMAR, Purdue University and M. SANGID, Purdue University 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2015-1118 Oral Presentation AIAA-2015-1119 Oral Presentation AIAA-2015-1120 Modeling Rate Dependent Response Fractal Patterns in Mechanics of The effective elastic and fracture Numerical Modeling of Ice Behavior Experimental Investigation and of Shape Memory Alloys Using a Materials properties of particulate reinforced at High Strain Rates Modelling of Laser Machining of Thermo-Mechanical Continuum S. Kale, S. Koric, M. Ostoja-Starzewski, composites using a new non-local S. Balunna, T. Sain, North Carolina A&T Sapphire for High Temperature Phase Field Approach A. Saharan, University of Illinois, Urbana- particle method State University, Greensboro, NC Pressure Transducers B. Agboola, D. Lagoudas, Texas A&M Champaign, Urbana, IL H. Chen, Y. Liu, Arizona State University, J. Collins, W. Oates, Florida State University, College Station, TX Tempe, AZ University, Tallahassee, FL; M. Sheplak, D. Blood, University of Florida, Gainesville, 117 Gainesville, FL Wednesday, 7 January 2015 235-MAT-9 Materials Testing & Characterization I Sarasota 2 Chaired by: R. NAIK, Pratt & Whitney and D. JAWORSKE, NASA Glenn Research Center 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2015-1121 AIAA-2015-1122 AIAA-2015-1123 AIAA-2015-1124 AIAA-2015-1125 AIAA-2015-1126 Wave Amplification in Double A Versatile In-Situ Ablation Damage Mapping of Composites Particle Size Effect on Load Transfer Improved Aircraft Tire Life through Environmental Effects on Long Negative Elastic Metamaterials Recession and Thermal Sensor with Piezospectroscopic Coatings in Single Particle Composite Laboratory Tire Wear Testing and Term Displacement Data of Woven Y. Su, C. Sun, Purdue University, West Adaptable for Different Types of G. Freihofer, S. Raghavan, University of Samples via X-Ray Diffraction Computational Modeling Fabric Webbings Under Constant Lafayette, IN Ablatives Central Florida, Orlando, FL E. Durnberg, K. Knipe, G. Freihofer, I. A. Zakrajsek, 96 TG/OL-ACL Landing Gear Load for Inflatable Structures J. Koo, M. Natali, KAI, LLC, Austin, TX; B. Hanhan, University of Central Florida, Test Facility, Wright-Patterson AFB, OH; S. W. Kenner, NASA Langley Research Center, Lisco, E. Yao, O. Ezekoye, University of Orlando, FL; R. Feng, Canadian Light Naboulsi, Air Force Research Laboratory, Hampton, VA Texas, Austin, Austin, TX Source, Saskatoon, Canada; S. Raghavan, Wright-Patterson AFB, OH; M. Bohun, M. University of Central Florida, Orlando, FL Vogel, 96 TG/OL-ACL Landing Gear Test Facility, Wright-Patterson AFB, OH; B. Fiepke, R. Vogel, Air Force Life Cycle Management Center, Wright-Patterson AFB, OH; et al. Wednesday, 7 January 2015 236-MDO-6 MDO: AeroStructure Design I Sarasota 3 Chaired by: J. MARTINS, University of Michigan and V. BALABANOV, Boeing Commercial Airplanes 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2015-1127 AIAA-2015-1128 AIAA-2015-1129 AIAA-2015-1130 AIAA-2015-1131 AIAA-2015-1132 Aeroelastic Tailoring of Transport Level-Set Topology Optimization Aerostructural Design Optimization Time-dependent Aero-elastic Robust Design of Aeroelastically High-Fidelity Aerostructural Wings Including Transonic Flutter with Aeroelastic Constraints of an Adaptive Morphing Trailing Adjoint-based Aerodynamic Shape Tailored Composite Plates Using Optimization with Integrated Constraints P. Dunning, National Institute of Edge Wing Optimization of Helicopter Rotors a New Formulation of Anti- Geometry Parameterization and B. Stanford, C. Wieseman, NASA Langley Aerospace, Hampton, VA; B. Stanford, D. Burdette, G. Kenway, Z. Lyu, J. Martins, in Forward Flight Optimization and Optimization Mesh Movement Research Center, Hampton, VA; C. Jutte, NASA Langley Research Center, Hampton, University of Michigan, Ann Arbor, Ann A. Mishra, K. Mani, D. Mavriplis, J. S. Phelan, D. Mavris, Georgia Institute of Z. Zhang, S. Khosravi, D. Zingg, University Craig Technologies, Inc., Cape Canaveral, VA; H. Kim, University of Bath, Bath, Arbor, MI Sitaraman, University of Wyoming, Technology, Atlanta, GA of Toronto, Toronto, Canada FL United Kingdom Laramie, Laramie, WY Wednesday, 7 January 2015 237-MST-9 Modeling of Vehicle Dynamics I Sun Ballroom 1 Chaired by: D. GINGRAS, Bihrle Applied Research Inc. 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2015-1133 AIAA-2015-1134 AIAA-2015-1135 AIAA-2015-1136 AIAA-2015-1137 AIAA-2015-1138 Modeling of aircraft with time- Symmetric dual solutions and Rapid State Space Modeling Dynamic Modeling, Simulation An Integrated Modeling, Simulation Modeling, Analysis and Validation varying inertia properties nongreat-circle effect of out-of- Tool for Rectangular Wing and Safe Boundary Evaluation of and Analysis Environment for Coupled of a Small Airplane Flight Dynamics J. Han, G. Hong, Beihang University, plane equilibrium formation Aeroservoelastic Studies Catapult launch for Carrier-based Aircraft Subsystems to Facilitate A. Kamal, A. Aly, A. Elshabka, Military Beijing, China Y. Shi, C. Han, Beihang University, Beijing, P. Suh, NASA Armstrong Flight Research airplane Control Synthesis and Validation Technical College, Cairo, Egypt China Center, Edwards, CA; H. Conyers, NASA C. Jing, H. Zheng-Chun, China M. Yasar, InnoVital Systems, Inc., Stennis Space Center, Stennis Space Aerodynamics Research and Development Beltsville, MD; H. Kwatny, Drexel Center, MS; D. Mavris, Georgia Institute of Center, Mianyang, China University, Philadelphia, PA; G. Bajpai, 118 Technology, Atlanta, GA Techno-Sciences, Inc., Beltsville, MD Wednesday, 7 January 2015 238-MST-10 Motion Systems, Visual Systems, Image Generation Sun Ballroom 2 Chaired by: F. CARDULLO, State University of NY 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2015-1139 AIAA-2015-1140 AIAA-2015-1141 AIAA-2015-1142 Automatic Optimization of Motion Evolutionary System Identification State of the Art Flight Motion Aircraft Upset and Recovery Drive Algorithms using OMCT of Flight Motion Simulators Simulator Controller Simulation with the DLR Robot K. De Ridder, M. Roza, National Aerospace T. Vu, R. Thamm, Defence Science & T. Vu, R. Thamm, Defence Science & Motion Simulator Laboratory (NLR), Amsterdam, The Technology Organisation, Adelaide, Technology Organisation, Adelaide, Y. Nie, T. Bellmann, A. Labusch, G. Netherlands Australia Australia Looye, German Aerospace Center (DLR), Wessling, Germany; E. Van Kampen, Q. Chu, Delft University of Technology, Delft, The Netherlands Wednesday, 7 January 2015 239-NDA-5 Random Fatigue, Fracture and Life Prediction Osceola Ballroom 5 Chaired by: T. KRISHNAMURTHY, NASA-Langley Research Center and B. THACKER, Southwest Research Institue 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2015-1143 AIAA-2015-1144 AIAA-2015-1145 AIAA-2015-1146 Methods of Determining Equivalent A Fleet Risk Prediction Methodology Probabilistic fatigue life prediction Free vibration analysis of angle-ply Initial Flaw Size (EIFS) Distributions for Mistuned IBRs using Geometric of composite laminates using composite plates with uncertain Containing Suspended Data Mistuning Models Bayesian updating properties L. Domyancic, Southwest Research E. Henry, Wright State University, T. Peng, Y. Liu, Arizona State University, S. Adhikari, Swansea University, Swansea, Institute, San Antonio, TX Dayton, OH; J. Brown, Air Force Research Tempe, AZ United Kingdom Laboratory, Wright-Patterson AFB, OH; J. Slater, Wright State University, Dayton, OH Wednesday, 7 January 2015 240-PANEL-5 Advanced Manufacturing and its Impact on the Design Process of the Future Osceola Ballroom B 0930 - 1130 hrs Moderator: Graeme Kennedy, Assistant Professor, School of Aerospace Engineering, Georgia Institute of Technology Panelists: Steven Betza Andrew Bicos David Rosen Mark Shaw Arthur Weiss Corporate Director, Advanced Manufacturing & Director, Manufacturing Technology Domain Enterprise Morris M. Bryan, Jr. Professor and Associate Chair for Additive Programs Leader Executive Director, Defense Advanced Programs Development Technology Strategy, Office of the CTO Administration, The George W. Woodruff School of GE Aviation Aerojet Rocketdyne Lockheed Martin Corporation The Boeing Company Mechanical Engineering Georgia Institute of Technology

Wednesday, 7 January 2015 241-PC-13 Advanced Combustion Concepts III Emerald 5 Chaired by: L. SMITH, United Technologies Research Center 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2015-1147 AIAA-2015-1148 AIAA-2015-1149 AIAA-2015-1150 AIAA-2015-1151 AIAA-2015-1152 Enhanced Homogeneous Catalysis Optical Measurements of Density Numerical Modeling of Fuel Experimental Investigation on The Impact of Phase transitions on the An Evaluation of a PCM-based in a Monopropellant Microthruster and Species Concentration in a Low Pyrolysis and Oxidation in a Ignition limits of Plasma-assisted Flow Structure of Gaseous Jets power plant for Micro Aerial M. McDevitt, GreenScale Technologies, Reynolds Number Micro-Nozzle Flow Laminar Micro-ﬂow Tube Reactor Ignition in Propane-Air Mixture Injected into Water Vehicles (MAV) South Burlington, VT; D. Hitt, University of D. Rosenberg, B. Williams, S. Tuttle, M. Rahimi, R. Johnson, H. Chelliah, Y. Jinlu, H. Liming, D. Wei, Air Force X. Zhang, Y. Tang, J. Tang, S. Li, N. A. Lidor, D. Weihs, E. Sher, Technion--Israel Vermont, Burlington, Burlington, VT M. Osborn, Naval Research Laboratory, University of Virginia, Charlottesville, Engineering University, Xi’an, China Wang, Beijing Institute of Technology, Institute of Technology, Haifa, Israel Washington, DC; L. Williams, Praxis, Inc., Charlottesville, VA Beijing, China Alexandria, VA

119 Wednesday, 7 January 2015 242-PC-14 Combustion Diagnostics Emerald 7 Chaired by: C. CADOU, University of Maryland 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2015-1153 AIAA-2015-1154 AIAA-2015-1155 AIAA-2015-1156 AIAA-2015-1157 AIAA-2015-1158 A Method for Eliminating Beam Study of Swirl Stabilized Burner Characterization of Unsteady Methane Absorbance Quantitative Experimental Shock Tube/Laser Absorption Steering Error for the Modulated with Interchangeable Swirler Using Combustion Phenomena in a Measurements at Pressure/ and Model-based Imaging of Measurements of Jet Fuel Pyrolysis Absorption-Emission Thermometry Chirped-Probe-Pulse Femtosecond University Scale Rocket Combustor Temperature Conditions Associated Mid-Infrared Radiation from a and Oxidation Technique Coherent Anti-Stokes Raman A. Dasari, M. Gamba, University of With Hypersonic Flight Turbulent Luminous Flame Y. Zhu, R. Hanson, D. Davidson, Stanford E. Coy, Air Force Research Laboratory, Scattering for Thermometry and Michigan, Ann Arbor, Ann Arbor, MI D. Maqbool, C. Cadou, University of R. Kapaku, Purdue University, West Lafayette, University, Stanford, CA Edwards AFB, CA CH4 Concentration Measurements Maryland, College Park, College Park, MD IN; B. Rankin, Innovative Scientiﬁc Solutions, C. Dennis, D. Cruise, H. Mongia, G. Inc., Dayton, OH; M. Mueller, Princeton King, R. Lucht, Purdue University, West University, Princeton, NJ; H. Lalit, J. Gore, Lafayette, IN Purdue University, West Lafayette, IN Wednesday, 7 January 2015 243-PDL-13 Plasma & Laser Technology Emerald 2 Chaired by: J. DRAKES, Aerojet and R. WALTER, University of Texas at San Antonio 0930 hrs 1000 hrs AIAA-2015-1159 AIAA-2015-1160 Kinetics of NO Formation and Laser Pointing for Orbital Debris Decay in Nanosecond Pulse Mitigation Using Higher Order Sliding Discharges in Air-Fuel Mixtures Mode Control and Observation D. Burnette, I. Shkurenkov, I. Adamovich, Techniques W. Lempert, Ohio State University, A. Palosz, Gleason Research Associates, Columbus, OH Huntsville, AL; Y. Shtessel, R. Fork, University of Alabama, Huntsville, Huntsville, AL Wednesday, 7 January 2015 244-SCS-6 Analysis of Lightweight Spacecraft Structures Osceola Ballroom 4 Chaired by: J. FOOTDALE, Load Path, LLC and T. MURPHEY, Air Force Reseach Laboratory 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2015-1161 AIAA-2015-1162 AIAA-2015-1163 AIAA-2015-1164 AIAA-2015-1165 Stability of Skin Added Lattice Assessment of Existing Models Structural Design of with Multi- Analysis of Thermal-Mechanical Deployment Dynamic Analysis of a Structure for Honeycomb Homogenized Mission Space Exploration Vehicle Interactions of STEM Booms Tetrahedral Truss Reﬂector S. Yoshino, T. Aoki, T. Yokozeki, University Properties (MMSEV)/Human Airlock (HAL) J. Blandino, Virginia Military Institute, X. Wang, Y. Wang, H. Fang, Shanghai YS of Tokyo, Tokyo, Japan; K. Terashima, H. Soliman, R. Kapania, Virginia Concept Mission Lexington, VA Information Technology Company, Ltd., T. Kamita, Japan Aerospace Exploration Polytechnic Institute and State University, G. Hrinda, NASA Langley Research Center, Shanghai, China; P. Huang, Xi’an Institute Agency (JAXA), Tsukuba, Japan Blacksburg, VA Hampton, VA of Space Radio Technology, Xi’an, China; Z. Chen, MSC Software Corporation, Beijing, China Wednesday, 7 January 2015 245-SD-9 Cable/Beam Modeling II Tampa 3 Chaired by: C. HEBERT, Sierra Nevada Corporation 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2015-1166 AIAA-2015-1167 AIAA-2015-1168 AIAA-2015-1169 AIAA-2015-1170 A Novel Scheme to Accurately Free Vibration Analysis of an Improved Solution of Nonlinear Modeling and Dynamic Analysis of On the Nonlinear Dynamics Compute Higher Vibration Modes Integrally Stiffened Plate with Reduced-Order Models for Static a Cable Towed Decoy of Buckled Beams for Energy using the Ritz Method and a Two-point Plate-Strip Stiffeners using a Set of and Dynamic Response Prediction K. Liu, D. Li, J. Xiang, Y. Yan, Beihang Harvesting BVP Solver Static Timoshenko Beam Functions P. O’Hara, J. Hollkamp, Air Force Research University, Beijing, China S. Emam, United Arab Emirates University, P. Sudalagunta, C. Sultan, R. Kapania, L. N. Ahmad, R. Kapania, Virginia Polytechnic Laboratory, Wright-Patterson AFB, OH Al Ain, United Arab Emirates Watson, P. Raj, Virginia Polytechnic Institute Institute and State University, Blacksburg, VA

120 and State University, Blacksburg, VA Wednesday, 7 January 2015 246-SD-13/GEPC-5 Special Session: Subsonic Ultra Green Aircraft Research (SUGAR) Truss Braced Wing Aeroelasticity Sun Ballroom C Chaired by: R. SCOTT, NASA-Langley Research Center and C. FUNK 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2015-1171 AIAA-2015-1172 AIAA-2015-1173 AIAA-2015-1174 AIAA-2015-1175 AIAA-2015-1176 SUGAR Truss Braced Wing Full Aeroservoelastic Wind-Tunnel Test Nonlinear Aeroelastic Analysis of Aeroelastic Analysis of SUGAR Aeroelastic Analysis and Low-Weight Low-Drag Truss-Braced Scale Aeroelastic Analysis and of the SUGAR Truss Braced Wing SUGAR Truss-braced Wing (TBW) Truss-Braced Wing Wind-Tunnel Optimization of Flexible Wing Wing Design Using Variable Dynamically Scaled Wind Tunnel Wind-Tunnel Model Wind-tunnel Model (WTM) Under Model Using FUN3D and a Aircraft with a Novel Control Camber Continuous Trailing Edge Model Development R. Scott, NASA Langley Research Center, In-plane Loads Nonlinear Structural Model Effector Flaps T. Allen, The Boeing Company, Huntington Hampton, VA; T. Allen, The Boeing Company, W. Zhao, R. Kapania, J. Schetz, J. Coggin, R. Bartels, R. Scott, NASA Langley W. Mallik, R. Kapania, J. Schetz, Virginia P. Chen, Z. Zhou, S. Ghoman, ZONA Beach, CA; B. Sexton, The Boeing Huntington Beach, CA; M. Castelluccio, The Virginia Polytechnic Institute and State Research Center, Hampton, VA; T. Allen, Polytechnic Institute and State University, Technology, Inc., Scottsdale, AZ; N. Company, St. Louis, MO; M. Scott, Boeing Company, Seattle, WA; B. Sexton, University, Blacksburg, VA The Boeing Company, Huntington Beach, Blacksburg, VA Falkiewicz, The Boeing Company, NextGen Aeronautics, Torrance, CA The Boeing Company, St. Louis, MO; S. CA; B. Sexton, The Boeing Company, St. Huntington Beach, CA Claggett, The Boeing Company, Seattle, WA; Louis, MO J. Dykman, The Boeing Company, Huntington Beach, CA; et al. Wednesday, 7 January 2015 247-SRE-1 Lunar Resource Utilization Daytona 2 Chaired by: D. LINNE, NASA Glenn Research Center 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs Oral Presentation AIAA-2015-1177 AIAA-2015-1178 AIAA-2015-1179 AIAA-2015-1180 AIAA-2015-1181 Technologies and Techniques for Impact of Drilling Operations on Internal Combustion Engine Solar Thermite Reactions in the Mixtures Development of a Molten Regolith A Systematic Assessment of Lunar Prospecting: Results from Lunar Volatiles Capture: Thermal Independent Propulsion for the of Magnesium with Lunar and Electrolysis Reactor Model for Asteroid Redirection Methods for 2014 Field Testing Campaign Vacuum Tests Exploration of Permanently Shaded Martian Regolith Simulants Lunar In-Situ Resource Utilization” Resource Exploration M. Cross, University of Western Ontario, J. Kleinhenz, NASA Glenn Research Center, Lunar Craters A. Delgado, E. Shaﬁrovich, University of S. Schreiner, Massachusetts Institute of M. Bazzocchi, M. Emami, University of London, Canada Cleveland, OH; K. Zacny, Honeybee W. Platts, Groundhog GeoScience, Texas, El Paso, El Paso, TX Technology, Cambridge, MA; L. Sibille, J. Toronto, Toronto, Canada Robotics, Pasadena, CA; J. Smith, NASA LLC, Pinedale, WY; C. Dyess, American Dominguez, NASA Kennedy Space Center, Kennedy Space Center, Cape Canaveral, FL Performance Technologies, Kansas City, MO Cape Canaveral, FL; A. Sirk, University of Victoria, Victoria, Canada; J. Hoffman, Massachusetts Institute of Technology, Cambridge, MA; G. Sanders, NASA Johnson Space Center, Houston, TX Wednesday, 7 January 2015 248-STR-12 Special Session: Challenges in the Design of Joined Wings II Tampa 1 Chaired by: L. DEMASI, San Diego State University College of Engineering and A. PALAZOTTO, AFIT 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2015-1182 AIAA-2015-1183 AIAA-2015-1184 AIAA-2015-1185 AIAA-2015-1186 AIAA-2015-1187 for Challenges in the Design of For Challenges in the Design of PrandtlPlane Joined Wing: Body Amphibious PrandtlPlane: Design of an airfreight system Buckling Alleviation for Joined- Joined Wings Special Session: Joined Wings Special Session: Freedom Flutter, Limit Cycle Preliminary Design Aspects based on an innovative Wing Aircraft Comparison of Aeroelastic Stability Joined-wing Aircraft in the Twenty- Oscillation and Freeplay Studies Including Propellers Integration PrandtlPlane aircraft L. Lambert, J. Cooper, R. Nangia,

121 of Conventional and Joined-Wing First Century and Beyond R. Cavallaro, University of California, San and Ground Effect A. Frediani, F. Oliviero, University of Pisa, University of Bristol, Bristol, United Highly Flexible Aircraft Z. Sotoudeh, Rensselaer Polytechnic Diego, San Diego, CA; L. Demasi, San R. Cavallaro, San Diego State University, San Pisa, Italy; E. Rizzo, SkyBox Engineering, Kingdom Z. Sotoudeh, Rensselaer Polytechnic Institute, Troy, NY Diego State University, San Diego, CA; R. Diego, CA; M. Nardini, University of Pisa, Pisa, Pisa, Italy Institute, Troy, NY Bombardieri, A. Iannelli, University of Pisa, Italy; L. Demasi, San Diego State University, Pisa, Italy San Diego, CA; E. Santarpia, University of California, San Diego, San Diego, CA Wednesday, 7 January 2015 249-STR-13 Special Sessions in Honor of Prof. Harry H. Hilton III Tallahassee 3 Chaired by: M. HYER, University of Calgary and C. MERRETT, Carleton University 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2015-1188 AIAA-2015-1189 AIAA-2015-1190 AIAA-2015-1191 AIAA-2015-1192 A Multi-Objective Nonlinear Higher Order ZigZag Laminated Statistical Characterization of Multiscale Modeling of Ceramic For Special Session in Honor of Piezoaeroelastic Wing Solution Composite Shell Theory for Viscoelastic Modulus using a Matrix Composites Harry H. Hilton Manipulating for Energy Harvesting and Load Viscoelastic Behavior Spectrum Function Approach B. Bednarcyk, NASA Glenn Research Natural Frequencies with Tunable Alleviation: Modeling and Simulation N. Nguyen Sy, J. Lee, M. Cho, Seoul R. Sullivan, J. Simsiriwong, Mississippi Center, Cleveland, OH; S. Mital, University Spring Masses C. Bruni, G. Frulla, E. Cestino, Technical National University, Seoul, Korea (the State University, Mississippi State, MS of Toledo, Toledo, OH; E. Pineda, S. N. Hall, J. Hackel, J. Girard, Ball Aerospace University of Turin, Turin, Italy; P. Marzocca, Republic of) Arnold, NASA Glenn Research Center, & Technologies Corporation, Boulder, CO Clarkson University, Potsdam, NY Cleveland, OH Wednesday, 7 January 2015 250-TP-6 Heat Transfer II Captiva 1 Chaired by: D. PYTEL, Lockheed Martin Space Systems and A. HASHEMI, Lockheed Martin Space Systems 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2015-1193 AIAA-2015-1194 AIAA-2015-1195 AIAA-2015-1196 Effect of Airflow on Heat Transfer A numerical study of thermal Time-Accurate CFD Conjugate Development of a Full Scale of Air-to-Refrigerant Airfoil Heat effects on vortex-induced vibration Analysis of Transient Measurements Experimental and Simulation Tool Exchanger H. Wan, S. Patnaik, Air Force Research of the Heat-Transfer Coefficient for Environmental Control System Y. Ito, T. Goto, T. Nagasaki, Tokyo Institute Laboratory, Wright-Patterson AFB, OH; B. S. Sathyanarayanan, S. Ramachandran, T. Optimisation and Fault Detection of Technology, Yokohama, Japan Ervin, University of Cincinnati, Cincinnati, OH Shih, Purdue University, West Lafayette, IN T. Childs, A. Jones, R. Chen, Loughborough University, Loughborough, United Kingdom Wednesday, 7 January 2015 251-UMS-4 UAS Airspace Integration: Policies and Guidelines Osceola Ballroom 1 Chaired by: D. MARSHALL, New Mexico State Universtiy and S. COOK, The MITRE Corporation 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2015-1197 AIAA-2015-1198 AIAA-2015-1199 AIAA-2015-1200 AIAA-2015-1201 AIAA-2015-1202 An Alternative UAS Classification and Verification and Validation Learning and Predicting Pilot Improvements in UAV & their Dynamic Mobile Areas: Efficient Deployment of Multiple Analysis Approach for Integration into Considerations for UAS Test Sites Behavior in Uncontrolled Airspace applications opportunities for RPAS emergency RPAS - Approaches towards Optimal the National Airspace System to Facilitate Civil Certification of C. Lowe, J. How, Massachusetts Institute A. Rashid, Ghulam Ishaq Khan Institute management Mission Planning Techniques R. Stansbury, K. Rigby, J. Clifford, Embry-Riddle Remotely Piloted Aircraft of Technology, Cambridge, MA of Engineering Sciences and Technology, A. Joulia, T. Dubot, ONERA, Toulouse, J. Zillies, D. Geister, German Aerospace Aeronautical University, Daytona Beach, FL; L. Mutuel, CGH Technologies, Inc., Topi, Pakistan France Center (DLR), Braunschweig, Germany D. Rudolph, University of Florida, Gainesville, Washington, DC Gainesville, FL

122 Wednesday, 7 January 2015 252-WE-9 Offshore Wind Energy Systems Emerald 4 Chaired by: J. JONKMAN, National Renewable Energy Laboratory and F. WENDT 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2015-1203 AIAA-2015-1204 AIAA-2015-1205 AIAA-2015-1206 AIAA-2015-1207 AIAA-2015-1208 Wake Influence on Dynamic Verification of New Floating Verification of the new FAST v8 Optimization and Design of An Experimental Investigation on Surface Ice Effects on the Extreme Characteristics of Offshore Floating Capabilities in FAST v8 Capabilities for the Modeling of Fixed- a 105m Blade for a 10MW the Performance and the Wake and Fatigue Loading of Bottom Wind Turbines F. Wendt, A. Robertson, J. Jonkman, G. Bottom Offshore Wind Turbines Hurricane-Resilient Wind Turbine Characteristics of a Wind Turbine Fixed Offshore Wind Turbines M. Jeon, S. Lee, S. Lee, Seoul National Hayman, National Renewable Energy B. Barahona, J. Jonkman, R. Damiani, A. Raina, K. Lee, K. Wetzel, Wetzel Subjected to Surge Motion T. McCoy, A. Byrne, DNV GL, Seattle, WA University, Seoul, South Korea Laboratory, Golden, CO A. Robertson, G. Hayman, National Engineering, Inc., Pflugerville, TX H. Hu, M. Morteza Khosravi, P. Sarkar, Renewable Energy Laboratory, Golden, CO Iowa State University, Ames, IA Wednesday, 7 January 2015 253-WE-10 Wind Turbine Loads, Control, and Dynamics Emerald 6 Chaired by: S. FROST, NASA-Ames Research Center and P. SEILER, University of Minnesota 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2015-1209 AIAA-2015-1210 AIAA-2015-1211 AIAA-2015-1212 AIAA-2015-1213 Field Test Results from Lidar Measured LPV Active Power Control and Study on Controller Tuning of Wind Adaptive Individual Blade Pitch Wind Turbine Envelope Riding Yaw Control for Improved Power Robust Analysis for Wind Turbines Turbines with Backward Swept Control for Large Wind Turbines V. Petrovic, C. Bottasso, Technical Capture with the NREL Controls S. Wang, P. Seiler, University of Blades with LiDAR Measurement of Wind University of Munich, Munich, Germany Advanced Research Turbine Minnesota, Minneapolis, Minneapolis, MN C. Pavese, C. Tibaldi, T. Kim, Technical Speed A. Scholbrock, P. Fleming, A. Wright, National University of Denmark, Lyngby, Denmark K. Thapa Magar, M. Balas, Embry-Riddle Renewable Energy Laboratory, Golden, CO; Aeronautical University, Daytona Beach, FL C. Slinger, J. Medley, M. Harris, Zephir Lidar, Hollybush, United Kingdom Wednesday, 7 January 2015 254-LUNCH-3 Luncheon in the Exposition Hall Exhibit Hall B/C 1230 - 1400 hrs Wednesday, 7 January 2015 255-AA-8 Airframe Noise and Shielding Miami 2 Chaired by: R. THOMAS, NASA Langley Research Center 1400 hrs 1430 hrs 1500 hrs 1530 hrs AIAA-2015-1214 AIAA-2015-1215 AIAA-2015-1216 AIAA-2015-1217 Open Rotor Noise Shielding by System Noise Assessment of Noise Generation in Flow past a Computational Aeroacoustics Blended-Wing-Body Aircraft Blended-Wing-Body Aircraft with Full-Span Trailing-Edge Flap Analysis for Noise Minimization on Y. Guo, M. Czech, The Boeing Company, Open Rotor Propulsion W. Li, H. Liu, Shanghai Jiao Tong the G550 Nose Landing Gear Huntington Beach, CA; R. Thomas, NASA Y. Guo, The Boeing Company, Huntington University, Shanghai, China A. de Paula, Technological Institute of Langley Research Center, Hampton, VA Beach, CA; R. Thomas, NASA Langley Aeronautics (ITA), São José dos Campos, Research Center, Hampton, VA Brazil; R. Queiroz, Embraer, São José dos Campos, Brazil; J. Meneghini, University of São Paulo, São Paulo, Brazil Wednesday, 7 January 2015 256-AMT-4 Laser Based Aerodynamic Diagnostic Tools Tallahassee 1 Chaired by: S. KEARNEY, Sandia National Laboratories and B. THUROW, Auburn University 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs AIAA-2015-1218 AIAA-2015-1219 AIAA-2015-1220 AIAA-2015-1221 AIAA-2015-1222 AIAA-2015-1223 AIAA-2015-1224 Pulse-Burst PIV in a High-Speed Limitations on High-Spatial Simultaneous High-Resolution Comparing Tomographic Multi-parameter estimation for Particle Image Velocimetry An Experimental Investigation Wind Tunnel Resolution Measurements of kHz-Rate 2-D Conserved Scalar Reconstruction Algorithms for spatially-resolved measurement Applications Using Fluorescent on Supercooled Large Droplet 123 S. Beresh, S. Kearney, J. Wagner, Sandia Turbulence Using Femtosecond and 3-Component Velocity Field Plenoptic-PIV of two-component velocity using Dye-doped Particles Icing by using Molecular Tagging National Laboratories, Albuquerque, NM; Laser Tagging Measurements in Gas-Phase T. Fahringer, B. Thurow, Auburn University, absorption tomography B. Petrosky, K. Lowe, Virginia Polytechnic Thermometry Technique S. Roy, N. Jiang, M. Slipchenko, Spectral M. Edwards, C. Limbach, R. Miles, Turbulent Jets Auburn, AL M. Gamba, University of Michigan, Ann Institute and State University, Blacksburg, H. Hu, H. Li, F. Chen, Iowa State Energies, LLC, Dayton, OH; et al. Princeton University, Princeton, NJ; A. M. Papageorge, J. Sutton, Ohio State Arbor, Ann Arbor, MI VA; P. Bardet, George Washington University, Ames, IA Tropina, Kharkov National Automobile and University, Columbus, OH University, Washington, DC; P. Tiemsin, C. Highway University, Kharkov, Ukraine Wohl, P. Danehy, NASA Langley Research Center, Hampton, VA; et al. Wednesday, 7 January 2015 257-APA-25 Aerodynamic Testing: Wind Tunnel & Flight Testing II Destin 1 Chaired by: B. MCGRATH, JHU/Applied Physics Laboratory and J. FARNSWORTH, University of Colorado Boulder 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2015-1225 AIAA-2015-1226 AIAA-2015-1227 AIAA-2015-1228 AIAA-2015-1229 AIAA-2015-1230 Implementation of an innovative Stall Behavior of the HINVA KH- Experimental Study of Splitter Experimental Study on Aerodynamic Reynolds Number Effects on Flow Compressible Boundary ice crystal generation system to the A320-HA Highlift Model in ETW Plates for Use with Semispan Wing Characteristics of Blended-Wing-Body Topology Above Blunt-edged Delta Layer Turbulence Transition Icing Wind Tunnel Braunschweig N. Bier, R. Rudnik, German Aerospace Models by a Wake Integration Method Wing VFE-2 Configurations Measurements with In-depth A. Baumert, S. Bansmer, Technical Center (DLR), Braunschweig, Germany; J. Diebold, B. Woodard, University of M. Kashitani, Y. Suganuma, H. Date, National M. Said, S. Mat, S. Mansor, A. Abdul-Latif, thermocouples University of Braunschweig, Braunschweig, J. Quest, A. Rechlin, European Transonic Illinois, Urbana-Champaign, Urbana, IL; Defense Academy, Yokosuka, Japan; S. T. Mat Lazim, University of Technology, X. Zhao, China Academy of Aerospace Germany; M. Bacher, Neuschnee GmbH, Windtunnel, Cologne, Germany M. Monastero, Rensselaer Polytechnic Nakao, Nagasaki Institute of Applied Science, Malaysia, Johor Bahru, Malaysia Aerodynamics, Beijing, China Perchtoldsdorf, Austria Institute, Troy, NY; M. Bragg, University of Nagasaki, Japan; Y. Takita, National Defense Washington, Seattle, Seattle, WA Academy, Yokosuka, Japan; Y. Yamaguchi, Nagasaki Institute of Applied Science, Nagasaki, Japan Wednesday, 7 January 2015 258-APA-26 Applied CFD & Numerical Correlations with Experimental Data I Destin 2 Chaired by: M. JURKOVICH, US Air Force and J. DEBONIS, NASA Glenn Research Center 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs AIAA-2015-1231 AIAA-2015-1232 AIAA-2015-1233 AIAA-2015-1234 AIAA-2015-1235 A Numerical Study on Transitional Further Developments to a Local Effects of Step-Excrescence Location Helicopter Blade NACA 8H12 Fluid-Structure Interaction of a Flows by Means of a Correlation- Correlation Based Roughness Model on Swept-Wing Transition Performance Prediction with Laminar- Variable Camber Compliant Wing Based Transition Model for Boundary Layer Transition B. Crawford, G. Duncan, M. Tufts, W. Turbulent Transition Effects: Integral S. Miller, Air Force Research Laboratory, G. Halila, Technological Institute of Prediction Saric, H. Reed, Texas A&M University, Boundary-Layer and CFD Results Wright-Patterson AFB, OH; M. Rumpfkeil, Aeronautics (ITA), São José dos Campos, C. Langel, R. Chow, C. Van Dam, College Station, TX compared with Experimental Data University of Dayton, Dayton, OH; J. Joo, Brazil; E. Bigarella, Embraer, São José dos University of California, Davis, Davis, CA G. Silva, ATS4i Aero-Thermal Solutions for Air Force Research Laboratory, Wright- Campos, Brazil; J. Azevedo, Aeronautics Industry, São Paulo, Brazil; D. de Andrade, Patterson AFB, OH and Space Institute (IAE), São José dos Technological Institute of Aeronautics (ITA), Campos, Brazil São José dos Campos, Brazil; C. Rafael, Federal University of ABC, Santo André, Brazil; D. Pio, ATS4i Aero-Thermal Solutions for Industry, São Paulo, Brazil Wednesday, 7 January 2015 259-APA-27 Flow Control Applications & Demonstrations (Active & Passive) II Naples 1 Chaired by: C. TILMANN, Air Force Reseach Laboratory and L. UKEILEY, University of Florida 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2015-1236 AIAA-2015-1237 AIAA-2015-1238 AIAA-2015-1239 AIAA-2015-1240 AIAA-2015-1241 Experiments with Vortex Experimental Investigation of Effect of Vortex Generators on Experimental Study of Fillets to LES Study on Mechanism of The Use of Actuated Flexible Plates Generators applied to a Notchback Vortex Generator Effect on Two- Transonic Swept Wings Reduce Corner Effects in an Oblique Reduction of Shock Induced Flow for Adaptive Shock Control Bumps 124 Car Model and Three-Dimensional NASA Y. Ito, K. Yamamoto, K. Kusunose, S. Shock-Wave/Boundary-Layer Separation by MVG E. Jinks, P. Bruce, M. Santer, Imperial D. Wieser, C. Nayeri, C. Paschereit, Common Research Models Koike, K. Nakakita, M. Murayama, Japan Interaction Y. Yang, Y. Yan, C. Liu, University of Texas, College London, London, United Kingdom Technical University of Berlin, Berlin, S. Koike, K. Nakakita, T. Nakajima, Aerospace Exploration Agency (JAXA), S. Hirt, NASA Glenn Research Center, Arlington, Arlington, TX Germany S. Koga, M. Sato, H. Kanda, Japan Mitaka, Japan; et al. Cleveland, OH Aerospace Exploration Agency (JAXA), Chofu, Japan; et al. Wednesday, 7 January 2015 260-APA-28 Special Session: Simulation of Rotor in Hover - Rotorcraft DG I Naples 2 Chaired by: N. HARIHARAN, CREATE-AV and T. EGOLF, Sikorsky Aircraft Corporation 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs AIAA-2015-1242 AIAA-2015-1243 AIAA-2015-1244 AIAA-2015-1245 AIAA-2015-1246 AIAA-2015-1247 AIAA-2015-1248 Standardized Evaluation of S-76 Hover Performance Assessment Hover Predictions for the S-76 The Effects of Turbulence Modelings Assessment of S-76 Rotor Analysis of a Hovering Rotor using Predicting the Influence of Blade Rotor-in-hover: Summary of the of Several Tip Shapes using Rotor with Tip Shape Variation on CFD Simulations of S76 Aerodynamic Performance in Hover UT-GENCAS: A Modified Hybrid Tip Shape on Hovering Rotor first (2014) special session OVERFLOW using CREATE-AV Helios Hovering Rotor on Unstructured Mixed Meshes Navier-Stokes/Free-Wake Method Performance with Comprehensive N. Hariharan, CREATE AV Team, Lorton, R. Narducci, The Boeing Company, St. R. Jain, U.S. Army, Moffett Field, CA P. Anusonti-Inthra, University of Tennessee, J. Hwang, J. Choi, O. Kwon, Korea B. Min, B. Wake, United Technologies Analyses VA; T. Egolf, Sikorsky Aircraft Corporation, Louis, MO Tullahoma, Tullahoma, TN Advanced Institute of Science and Corporation, East Hartford, CT G. Whitehouse, D. Wachspress, T. Stratford, CT; L. Sankar, Georgia Institute Technology, Daejeon, South Korea Quackenbush, Continuum Dynamics, Inc., of Technology, Atlanta, GA Ewing, NJ Wednesday, 7 January 2015 261-APA-29 Special Session: Low Boom Activities II Miami 3 Chaired by: K. WAITHE, Gulfstream Aerospace Corporation and L. BANGERT, NASA Langley Research Center 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs AIAA-2015-1249 AIAA-2015-1250 AIAA-2015-1251 AIAA-2015-1252 AIAA-2015-1253 Analysis of a Low Boom Supersonic Unstructured Grids for Sonic Boom Sonic Boom Pressure Signature Near field Sonic Boom calculation Near Field Pressure Measurement Flying Wing Preliminary Design Analysis and Design Uncertainty Calculation and of Benchmark Cases around Free Flight 69 Degree J. Gan, G. Zha, Rush University, Miami, FL R. Campbell, NASA Langley Research Propagation to Ground Noise (Invited) J. Gan, G. Zha, University of Miami, Coral Swept Back Delta Wing Model Center, Hampton, VA; S. Nayani, Analytical E. Walker, J. Pinier, NASA Langley Research Gables, Coral Gables, FL A. Toyoda, A. Sasoh, T. Imaizumi, T. Services & Materials, Inc., Hampton, VA; Center, Hampton, VA; T. West, Missouri Ooyama, Nagoya University, Nagoya, M. Lynde, NASA Langley Research Center, University of Science and Technology, Rolla, Japan; M. Kanamori, T. Aoyama, Japan Hampton, VA MO; K. Bretl, Massachusetts Institute of Aerospace Exploration Agency (JAXA), Technology, Cambridge, MA Chofu, Japan Wednesday, 7 January 2015 262-AS-5 Adaptive Actuation Osceola Ballroom 6 Chaired by: A. CHATTOPADHYAY, Arizona State University and J. KAUFFMAN, University of Central Florida 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2015-1254 AIAA-2015-1255 AIAA-2015-1256 AIAA-2015-1257 AIAA-2015-1258 AIAA-2015-1259 Stiffness Control with Pneumatic Semi-Active Control of Torsional New methodology for the controller Galloping Piezoelectric Energy Optimal Resonance Frequency Design and Testing of a FMC Artificial Muscle Inclusions in a Vibrations Using a New Hybrid of an electrical actuator for Harvester with Bio-inspired Square Detuning Switch Trigger Actuated Morphing Aileron Cellular Honeycomb Unit Torsional Damper morphing a wing Bluff Body Determination Using Measurable E. Doepke, M. Philen, Virginia Polytechnic M. Pontecorvo, F. Gandhi, F. Foerster, E. Abouobaia, R. Bhat, R. Sedaghati, M. Tchatchueng Kammegne, S. Khan, R. F. Ewere, G. Wang, K. Frendi, University of Response Characteristics Institute and State University, Blacksburg, Rensselaer Polytechnic Institute, Troy, NY Concordia University, Montréal, Canada Botez, École de Technologie Supérieure, Alabama, Huntsville, Huntsville, AL G. Lopp, J. Kauffman, University of Central VA Montréal, Canada Florida, Orlando, FL 125 Wednesday, 7 January 2015 263-FD-32 CFD Methods V Sanibel 2 Chaired by: M. FOSSATI, McGill University and G. ZHA, University of Miami 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2015-1260 AIAA-2015-1261 AIAA-2015-1262 AIAA-2015-1263 AIAA-2015-1264 AIAA-2015-1265 Dynamic Mesh Deformation with Development of a Jacobian- Adjoint and Truncation Error Based Implicit Time Marching Methods Accuracy of Discretization Error A Primitive Variable Central Flux Radial Basis Functions for the Non- free Finite Element Solver for Adaptation for Finite Volume for Large-Scale High-Accuracy Estimation by the Error Transport Scheme for All Mach Number Flows Linear Frequency Domain Method Aerothermodynamic Design Schemes with Error Estimates Simulations of Compressible Flows Equation on Unstructured Meshes K. Shi, S. Morris, A. Jemcov, University of P. Tardif, S. Nadarajah, McGill University, M. Fossati, W. Habashi, S. Gao, P. Yin, J. Derlaga, T. Phillips, C. Roy, J. Y. Du, J. Ekaterinaris, Embry-Riddle G. Yan, C. Ollivier Gooch, University of Notre Dame, Notre Dame, IN Montréal, Canada McGill University, Montréal, Canada; D. Borggaard, Virginia Polytechnic Institute Aeronautical University, Daytona Beach, FL British Columbia, Vancouver, Canada Isola, G. Baruzzi, Newmerical Technologies and State University, Blacksburg, VA International, Montréal, Canada; et al. Wednesday, 7 January 2015 264-FD-33 Current Challenges for Computational Fluid Dynamics, Industry and Government Interests II (Invited) Sun Ballroom A Chaired by: H. HUYNH, NASA Glenn Research Center and N. KROLL, DLR - German Aerospace Center 1400 hrs 1430 hrs 1500 hrs 1530 hrs Oral Presentation Oral Presentation Oral Presentation Oral Presentation Status and challenges of CFD for Current challenges for CFD at Current Status and Challenges The Challenges of Present and aircraft design at Dassault Aviation Onera (Invited) in CFD at the DLR Institute of Future Industrial CFD (Invited) (Invited) V. Couaillier, ONERA, Châtillon, France Aerodynamics and Flow Technology C. Hirsch, NUMECA International, Brussels, M. Mallet, Dassault Group, Saint Cloud, France N. Kroll, German Aerospace Center (DLR), Belgium Braunschweig, Germany Wednesday, 7 January 2015 265-FD-34 Flow Control (Fundamentals and Technology) III Sanibel 3 Chaired by: M. VISBAL, USAF AFRL/RQVA and I. GURSUL, University of Bath 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2015-1266 AIAA-2015-1267 AIAA-2015-1268 AIAA-2015-1269 AIAA-2015-1270 AIAA-2015-1271 Flow Control on an Airfoil in Fully- Control of Dynamic Stall on Parametric Optimization of Control Post-Stall Lift Enhancement of a Experimental Investigation of the Wake Vortex Field of an Airfoil Reversed Condition with Actuation a Pitching Airfoil Using High- for a Post-Stall Airfoil Using Pulsed Flat Plate Airfoil by Suction Aerodynamic Lift Response of an Equipped with an Active Finite on Both Leading and Trailing Edges Frequency Actuation Jets Z. Wang, I. Gursul, J. Wu, University of Active Finite Gurney Flap Gurney Flap C. Clifford, M. Samimy, Ohio State M. Visbal, Air Force Research Laboratory, K. Hipp, S. Benton, M. Walker, J. Bons, Bath, Bath, United Kingdom A. Bach, R. Berg, Technical University of A. Bach, Technical University of Berlin, University, Columbus, OH Wright-Patterson AFB, OH Ohio State University, Columbus, OH Berlin, Berlin, Germany; G. Pechlivanoglou, Berlin, Germany; G. Pechlivanoglou, Smart Smart Blade GmbH, Berlin, Germany; C. Blade GmbH, Berlin, Germany; C. Nayeri, Nayeri, C. Paschereit, Technical University C. Paschereit, Technical University of of Berlin, Berlin, Germany Berlin, Berlin, Germany Wednesday, 7 January 2015 266-FD-35 Fundamental Vortex Flows and Channel Flows Tallahassee 2 Chaired by: J. AHMAD, NASA and Y. SEE, University of Michigan 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2015-1272 AIAA-2015-1273 AIAA-2015-1274 AIAA-2015-1275 AIAA-2015-1276 AIAA-2015-1277 Vortex force and lift induced drag Vortex structure of low-aspect-ratio Prediction of Turbulent Secondary An Experimental Study of Adverse Pressure Gradient Effects Investigation on Turbulence in compressible flows wings in sideslip Flows in Ducts Using Equilibrium Homogeneous Anisotropic in the Turbulent Kinetic Energy Characteristics of Channel Flow B. Mele, M. Ostieri, R. Tognaccini, A. DeVoria, K. Mohseni, University of Wall-Modeled LES Turbulence in Channel Flow Budget for Channel Flows over the Compliant Wall University of Naples “Federico II”, Naples, Florida, Gainesville, Gainesville, FL Z. Vane, S. Lele, Stanford University, T. Slais, B. Ochs, D. Scarborough, S. L. Schiavo, A. Jesus, Technological Institute N. Fujimatsu, Toyo University, Kawagoe, Italy Stanford, CA Menon, Georgia Institute of Technology, of Aeronautics (ITA), São José dos Japan Atlanta, GA; N. Grady, R. Pitz, Vanderbilt Campos, Brazil; J. Azevedo, Aeronautics

126 University, Nashville, TN and Space Institute (IAE), São José dos Campos, Brazil; W. Wolf, University of Campinas, Campinas, Brazil Wednesday, 7 January 2015 267-FD-36 Multiphase Flows Daytona 2 Chaired by: C. TSAI, Lockheed Martin Space Systems and J. KUHLMAN, West Virginia University 1400 hrs 1430 hrs 1500 hrs 1530 hrs AIAA-2015-1278 AIAA-2015-1279 AIAA-2015-1280 AIAA-2015-1281 Modelling of Drop Deformation Fruit Fly Impact Outcomes and Stress dependent slip boundary Spray Droplet Impingement onto a and Breakup Residue Components on an condition for single- and two-phase Smooth Flat Surface C. Rodrigues, J. Barata, A. Silva, University Aerodynamic Surface fluid flow on a substrate J. Kuhlman, J. Taylor, West Virginia of Beira Interior, Covilha, Portugal K. Krishnan, A. Milionis, M. Starr, E. Loth, J. Thalakkottor, K. Mohseni, University of University, Morgantown, WV University of Virginia, Charlottesville, Florida, Gainesville, Gainesville, FL Charlottesville, VA Wednesday, 7 January 2015 268-FD-37 Turbulence Modeling I Captiva 2 Chaired by: P. HAMLINGTON and Z. WANG, University of Kansas 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs AIAA-2015-1282 AIAA-2015-1283 AIAA-2015-1284 AIAA-2015-1285 AIAA-2015-1286 AIAA-2015-1287 AIAA-2015-1288 Wall - Distance - Free Modifications to A priori and a posteriori New Approaches in Turbulence and Autonomic Subgrid-Scale Closure CPR High-order Discretization of A Machine Learning Strategy Closure in Reduced-Order Model of Spalart - Allmaras Turbulence Model evaluations of subgrid stress Transition Modeling Using Data- for Large Eddy Simulations the RANS Equations with the SA to Assist Turbulence Model Burgers Equation M. Rahman, Aalto University, Helsinki, Finland; models with the Burgers’ equation driven Techniques R. King, P. Hamlington, University of Model Development H. Imtiaz, I. Akhtar, National University R. Agarwal, Washington University in St. Louis, Y. Li, Z. Wang, University of Kansas, K. Duraisamy, Z. Zhang, A. Singh, Colorado, Boulder, Boulder, CO; W. Dahm, C. Zhou, Z. Wang, University of Kansas, B. Tracey, Stanford University, Stanford, of Sciences and Technology, Rawalpindi, St. Louis, MO; M. Lampinen, T. Siikonen, Aalto Lawrence, Lawrence, KS University of Michigan, Ann Arbor, Ann Arizona State University, Tempe, AZ Lawrence, Lawrence, KS CA; K. Duraisamy, University of Michigan, Pakistan University, Helsinki, Finland Arbor, MI Ann Arbor, Ann Arbor, MI; J. Alonso, Stanford University, Stanford, CA Wednesday, 7 January 2015 269-FD-38 Unsteady Flow II Sun Ballroom 6 Chaired by: K. GRANLUND, Air Force Research Laboratory and Z. ZHANG, University of Tennessee 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs AIAA-2015-1289 AIAA-2015-1290 AIAA-2015-1291 AIAA-2015-1292 AIAA-2015-1293 AIAA-2015-1294 AIAA-2015-1295 Unsteady Behavior of a Pressure- Investigation of Low-Pressure Complex Geometry Effects on Acoustics of a Supersonic Cavity Response of a Store with Low-Frequency Unsteadiness in Bluff-body wake stability for Induced Turbulent Separation Turbine Endwall Flows: Simulations Subsonic Cavity Flows with a Generic Store Tunable Natural Frequencies in 3D Shock-Wave/Boundary-Layer unsteady inflow conditions Bubble and Experiments K. Casper, J. Wagner, S. Beresh, J. G. Robertson, R. Kumar, Florida State Compressible Cavity Flow Interactions in a Supersonic T. Cleaver, K. Granlund, A. Comer, A. J. Weiss, A. Mohammed-Taifour, A. Gross, New Mexico State University, Henfling, R. Spillers, B. Pruett, Sandia University, Tallahassee, FL; S. Doyle, M. Baker, J. Wagner, K. Casper, S. Beresh, J. Crossflow Briones, V. Belovich, Air Force Research Q. Schwaab, École de Technologie Las Cruces, NM; R. Sondergaard, Air Force National Laboratories, Albuquerque, NM K. Roughen, M4 Engineering, Inc., Long Henfling, R. Spillers, B. Pruett, Sandia D. Drikakis, Z. Rana, Cranfield University, Laboratory, Wright-Patterson AFB, OH Supérieure, Montréal, Canada Research Laboratory, Wright-Patterson Beach, CA; R. Johnson, Air Force Research National Laboratories, Albuquerque, NM Cranfield, United Kingdom AFB, OH Laboratory, Wright-Patterson AFB, OH Wednesday, 7 January 2015 270-FD-39 Wing Aerodynamics I Daytona 1 Chaired by: A. JONES, University of Maryland and K. TAIRA, Florida State University 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2015-1296 AIAA-2015-1297 AIAA-2015-1298 AIAA-2015-1299 AIAA-2015-1300 AIAA-2015-1301 Effect of Aspect Ratio and Leading Vortex Characterization and Force Three Dimensional Unsteady Wake Aerodynamic Comparison of Flat Direct Numerical Simulations of High fidelity simulations of and Trailing Edge Form on the Flow Production on Two- and Three- of a Trapezoidal Pitching Panel and Cambered Frames for Flexible Membrane Wings at Low Reynolds electroactive membrane wings Around an Impulsively Pitching Dimensional Wing Kinematics T. Rice, M. Green, Syracuse University, MAV Wings Number G. Cetraro, R. Sandberg, University of Flat Plate F. Manar, P. Mancini, A. Jones, University Syracuse, NY A. Wrist, Z. Zhang, D. Pepley, J. Hubner, S. Serrano Galiano, R. Sandberg, Southampton, Southampton, United O. Son, O. Cetiner, Istanbul Technical of Maryland, College Park, College University of Alabama, Tuscaloosa, University of Southampton, Southampton, Kingdom University, Istanbul, Turkey Park, MD Tuscaloosa, AL United Kingdom

127 Wednesday, 7 January 2015 271-GEPC-4/SAT-1 Green Engineering/Society and Aerospace Technology Sun Ballroom C Chaired by: R. JUSTICE, The Georgia Center of Innovation for Aerospace 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2015-1302 AIAA-2015-1303 AIAA-2015-1304 AIAA-2015-1305 AIAA-2015-1306 AIAA-2015-1307 Regenerative Electric Flight Model of Fast Pyrolysis of a Small Maple Seed Performance as a Wind Antares DLR H2 - Test bed for NASA Innovation Ecosystem: Role of UAVs in Daily Life Synergy and Integration of Dual Volume-Fraction of Biomass Within Turbine electric propulsion Innovation for Government A. Rashid, Z. Shahid, Ghulam Ishaq Khan role Machines an Gas of Transient Temperature J. Holden, T. Caley, M. Turner, University of J. Kallo, S. Flade, T. Stephan, J. Schirmer, Technology Institute of Engineering Sciences and J. Barnes, Pelican Aero Group, San and Pressure Cincinnati, Cincinnati, OH German Aerospace Center (DLR), J. Hardash, Booz Allen Hamilton, Los Angeles, Technology, Topi, Pakistan Pedro, CA N. Parziale, Stevens Institute of Stuttgart, Germany CA; A. Landegger, Booz Allen Hamilton, Technology, Hoboken, NJ Washington, DC; B. Decker, V. Thompson, NASA Headquarters, Washington, DC Wednesday, 7 January 2015 272-GNC-25 Robust and Fault Tolerant Control Miami 1 Chaired by: S. MEHTA, Vanderbilt University and F. HUGON, Gulfstream Aerospace Corporation 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2015-1308 AIAA-2015-1309 AIAA-2015-1310 AIAA-2015-1311 AIAA-2015-1312 AIAA-2015-1313 Disturbance Rejection using Micro- Diverging Engine Failure Paths on Fault Tolerant Control Design for Air Data Sensor Fault Detection and Active Fault-Tolerant Control Pilot-in-the-Loop Evaluation of a jet Actuators with a MPC Policy Standard Instrument Departures the Longitudinal Aircraft Dynamics Diagnosis with Application to Real System using Incremental Bio-Inspired Adaptive Fault Tolerant M. McCourt, University of Florida, B. Masson, M. Bain, J. Page, University of using Quantitative Feedback Flight Data Backstepping Approach Control System in a Motion Based Shalimar, Shalimar, FL; J. Klotz, University New South Wales, Sydney, Australia Theory P. Lu, L. Van Eykeren, E. Van Kampen, Q. P. Lu, E. Van Kampen, Delft University of Flight Simulator of Florida, Gainesville, Gainesville, FL; S. D. Ossmann, German Aerospace Center Chu, Delft University of Technology, Delft, Technology, Delft, The Netherlands A. Perez Rocha, H. Moncayo, Embry- Mehta, University of Florida, Shalimar, (DLR), Oberpfaffenhofen, Germany The Netherlands Riddle Aeronautical University, Daytona Shalimar, FL; J. Curtis, Air Force Research Beach, FL; A. Togayev, M. Perhinschi, Laboratory, Eglin AFB, FL D. Al Azzawi, West Virginia University, Morgantown, WV Wednesday, 7 January 2015 273-GNC-26 Trajectory Planning and Optimization II Sun Ballroom 3 Chaired by: D. DOMAN, Air Force Research Laboratory and P. SHANKAR, California State Univ 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs AIAA-2015-1314 AIAA-2015-1315 AIAA-2015-1316 AIAA-2015-1317 AIAA-2015-1318 Trajectory Design and Coverage Design of a Track Guidance An Optimal Control Approach to Lyapnov-Based Three-Dimensional Correlation between Flight Time and Control for Solar-Powered UAVs Algorithm for Formation Flight Aircraft Automatic Ground Collision Nonlinear Path-Following Guidance Fuel Consumption in Airliner Flight S. Vasisht, M. Mesbahi, University of of UAVs Avoidance Law Plan with Trajectory Optimization Washington, Seattle, Seattle, WA D. Lee, S. Kim, J. Suk, Chungnam A. Suplisson, R. Cobb, W. Baker, D. N. Cho, Y. Kim, Seoul National University, N. Wickramasinghe, M. Brown, S. National University, Daejeon, South Korea Jacques, Air Force Institute of Technology, Seoul, South Korea Fukushima, Y. Fukuda, Electronic Wright-Patterson AFB, OH Navigation Research Institute, Tokyo, Japan; A. Harada, Y. Miyazawa, Kyushu University, Fukuoka, Japan Wednesday, 7 January 2015 274-GNC-27 Nonlinear Control of Aircraft/UAV Sun Ballroom 4 Chaired by: M. SPETZLER, University of Washington and M. IDAN, Technion - Israel Institute of Technology 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs AIAA-2015-1319 AIAA-2015-1320 AIAA-2015-1321 AIAA-2015-1322 AIAA-2015-1323 Nonlinear H-infinity Control applied Continuation Analysis of Nonlinear Integrator-Backstepping Control Seeker Head Line-of-Sight Sliding Advanced Sliding Mode Online to a UAS in Trajectory Following Systems with Equality Constraints Design for Nonlinear Flight System Mode Control Training for Neural Network Flight G. Garcia, S. Keshmiri, University of on States, Parameters, and Dynamics G. Fursht, M. Idan, Technion--Israel Control Applications Kansas, Lawrence, Lawrence, KS Eigenvalues T. Tran, B. Newman, Old Dominion Institute of Technology, Haifa, Israel P. Schnetter, J. Kaste, Technical University of M. Spetzler, A. Narang-Siddarth, University University, Norfolk, VA Braunschweig, Braunschweig, Germany; T. of Washington, Seattle, Seattle, WA Krüger, Aerodata AG, Braunschweig, Germany 128 Wednesday, 7 January 2015 275-GNC-28 Guidance, Navigation and Control Concepts in Air Traffic Control Systems I Sun Ballroom 2 Chaired by: A. CHAKRAVARTHY, Wichita State University and X. BAI 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2015-1324 AIAA-2015-1325 AIAA-2015-1326 AIAA-2015-1327 AIAA-2015-1328 AIAA-2015-1329 Intent Based Trajectory Prediction The Application of Probability Flow Enhancing the Traffic Management Near-Optimal Conflict-Free Evaluation of Time Arrival Optimization Approaches to by Multiple Model Prediction and for Conflict Detection near Airports Advisor’s Schedule by Time Trajectory Generation in the Uncertainties Associated with the Single Airport Ground Hold Smoothing L. Pienaar, T. Jones, University of Advance Presence of Uncertainty NextGen FMS Capabilities Problem Y. Liu, X. Li, University of New Orleans, Stellenbosch, Stellenbosch, South Africa M. Wu, University of California, Santa Y. Matsuno, T. Tsuchiya, University of V. Vaddi, X. Bai, Optimal Synthesis, Inc., J. Cox, M. Kochenderfer, Stanford New Orleans, LA Cruz, Moffett Field, CA; H. Swenson, NASA Tokyo, Bunkyo, Japan Los Altos, CA; S. Park, Georgia Institute of University, Stanford, CA Ames Research Center, Moffett Field, CA Technology, Atlanta, GA Wednesday, 7 January 2015 276-GNC-29 Spacecraft Guidance, Navigation, and Control III Sun Ballroom 5 Chaired by: O. TEKINALP, Middle East Technical University and S. KOWALTSCHEK, European Space Agency 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2015-1330 AIAA-2015-1331 AIAA-2015-1332 AIAA-2015-1333 AIAA-2015-1334 AIAA-2015-1335 Receding-Horizon Unscented A Multi Sensor Based Integrated Star Position Estimation Interacting Multiple Model Autonomous Optical Navigation for Satellite Angular Velocity Kalman Filter using Successive Navigation for Pin-Point Landing Improvements for Accurate Star Estimation for Spacecraft Maneuver Earth-Observing Satellites using Estimation Based on Optical Flow Unscented Transformation for on Mars Tracker Attitude Estimation Detection and Characterization Coastline Matching Technique Spacecraft Attitude Estimation Z. Yu, R. Xu, P. Cui, Beijing Institute of T. Delabie, Catholic University of Leuven, S. Lee, I. Hwang, Purdue University, West M. Straub, J. Christian, West Virginia L. Kazemi, J. Enright, T. Dzamba, K. R. Hirasawa, Keio University, Yokohama, Technology, Beijing, China Heverlee, Belgium Lafayette, IN University, Morgantown, WV Raahemifar, Ryerson University, Toronto, Japan; Y. Nakajima, Japan Aerospace Canada Exploration Agency (JAXA), Tsukuba, Japan; M. Takahashi, Keio University, Yokohama, Japan Wednesday, 7 January 2015 277-GT-4 Hypersonic Test Capabilities I (Invited) Sanibel 1 Chaired by: K. BERGER, NASA-Langley Research Center and J. LAFFERTY, AEDC 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2015-1336 AIAA-2015-1337 AIAA-2015-1338 Oral Presentation AIAA-2015-1339 AIAA-2015-1340 Hypersonic Test Capabilities in NASA Langley Aerothermodynamics Modernization of Sandia’s Review of CUBRC LENS Hypersonic Testing Capabilities at The Hypervelocity Wind Tunnel No. Tunnels B and C at AEDC’s von Laboratory: Hypersonic Testing Hypersonic Wind Tunnel Hypervelocity Tunnels and Recent the NASA Ames Ballistic Ranges 9; Continued Excellence Through Karman Facility Capabilities S. Beresh, K. Casper, J. Wagner, J. Research and Testing Activities M. Wilder, NASA Ames Research Center, Improvement and Modernization M. Mills, Aerospace Testing Alliance, K. Berger, NASA Langley Research Center, Henfling, R. Spillers, B. Pruett, Sandia M. Holden, T. Wadhams, M. MacLean, A. Moffett Field, CA; D. Bogdanoff, ERC, Inc., J. Lafferty, Arnold Engineering Arnold AFB, TN Hampton, VA; K. Hollingsworth, S. Wright, National Laboratories, Albuquerque, NM Dufrene, CUBRC, Buffalo, NY Moffett Field, CA; C. Cornelison, NASA Development Complex, White Oak, MD Jacobs, Hampton, VA; S. Rufer, NASA Ames Research Center, Moffett Field, CA Langley Research Center, Hampton, VA Wednesday, 7 January 2015 278-GTE-6 Compressors Emerald 1 Chaired by: R. WEBSTER, University of Tennessee at Chattanooga 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs AIAA-2015-1341 AIAA-2015-1342 AIAA-2015-1343 AIAA-2015-1344 AIAA-2015-1345 Vane Wake Characterization Experimental and Computational Reduction of Rotor Forced Response Computational Simulation of the Validation and Simulation of a Small- Including Variability in a Multistage Study of Forced Response in a Using Stator Asymmetry in a Fan and Low-pressure Compressor Scale Pressure Wave Supercharger Compressor Multistage Axial Compressor Multistage Compressor Stages of the Energy Efficient M. Mataczynski, Air Force Research J. Methel, N. Smith, N. Key, Purdue D. Monk, W. Murray, N. Key, Purdue D. Monk, N. Key, Purdue University, West Engine Laboratory, Wright-Patterson AFB, OH; M. University, West Lafayette, IN University, West Lafayette, IN; R. Fulayter, Lafayette, IN; R. Fulayter, Rolls-Royce R. Webster, K. Sreenivas, C. Hilbert, Polanka, Air Force Institute of Technology, Rolls-Royce Group plc, Indianapolis, IN Group plc, Indianapolis, IN University of Tennessee, Chattanooga, Wright-Patterson AFB, OH; J. Nees, Innovative Chattanooga, TN Scientific Solutions, Inc., Dayton, OH; D.

129 Paxson, NASA Glenn Research Center, Cleveland, OH Wednesday, 7 January 2015 279-HSABP-9/GTE-8 Pressure Gain Combustion - Pulse Detonation Engines Emerald 3 Chaired by: K. KAILASANATH, Naval Research Laboratory and D. PAXSON, NASA Glenn Research Center 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs AIAA-2015-1346 AIAA-2015-1347 AIAA-2015-1348 AIAA-2015-1349 AIAA-2015-1350 AIAA-2015-1351 AIAA-2015-1352 10 kHz Mid-IR TDLAS of Detonation Development and Investigation of Experimental Study of Unsteady Thrust Optical Measurement of Detonation Effect of initial flow velocity on the Performance Model for Fully and Events with a Fiber-Coupled Laser an Air-Breathing, Pulse Detonation Magnetohydrodynamic Energy Characteristics of Pulse Detonation with a Focusing Schlieren Technique flame propagation in obstructed Partially Filled Pulse Detonation Diagnostic Engine-Crossover System Extraction from a Pulsed Engines C. Stevens, J. Hoke, Innovative Scientific channels Engine B. Sell, Innovative Scientific Solutions, R. Driscoll, A. St. George, V. Anand, Detonation Tube D. Joshi, F. Lu, University of Texas, Solutions, Inc., Dayton, OH; F. Schauer, J. Gray, J. Moeck, C. Paschereit, Technical R. Bello, F. Lu, University of Texas, Inc., Dayton, OH; M. Fotia, National D. Munday, E. Gutmark, University of K. Teope, P. King, Air Force Institute of Arlington, Arlington, TX Air Force Research Laboratory, Wright- University of Berlin, Berlin, Germany Arlington, Arlington, TX Research Council, Wright-Patterson Cincinnati, Cincinnati, OH Technology, Wright-Patterson AFB, OH; F. Patterson AFB, OH AFB, OH; A. Caswell, Air Force Research Schauer, Air Force Research Laboratory, Laboratory, Wright-Patterson AFB, OH; J. Wright-Patterson AFB, OH; J. Hoke, Hoke, Innovative Scientific Solutions, Inc., Innovative Scientific Solutions, Inc., Dayton, OH; F. Schauer, Air Force Research Dayton, OH Laboratory, Wright-Patterson AFB, OH Wednesday, 7 January 2015 280-IS-9 Invited Panel Discussion - Roadmap for Intelligent Systems Osceola Ballroom 3 1400 - 1700 hrs This invited session will discuss recent efforts focused towards developing a roadmap which charts a course for integrating Intelligent Systems into the aerospace technology. Presentations will include summaries of the discussions at the August 2014 Intelligent Systems Workshop in focus areas of Autonomy, Adaptive Control and Air Traffic Management. Moderator: Kelly Cohen, University of Cincinnati Panelists: Paul Zetocha Ella Atkins Nhan Ngugen Christine Belcastro Sam Adhikari Chris Tschan Air Force Research Laboratory University of Michigan NASA Ames NASA Langley Sysoft The Aerospace Corporation

Wednesday, 7 January 2015 281-MAT-10 Materials & Design for Additive Manufacturing Sarasota 1 Chaired by: J. KOO, The University of Texas at Austin; S. WANTHAL, The Boeing Company and T. CLEMENT, Raytheon 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs AIAA-2015-1353 AIAA-2015-1354 AIAA-2015-1355 AIAA-2015-1356 AIAA-2015-1357 Electrically Conductive Polyamide Fatigue Behavior of a Titanium Microstructural Features and Effect of Substrate Thickness on Reducing Production Costs of 11 Nanocomposites for Selective Alloy Additively Manufactured by a Mechanical Properties of 316L Micro-Hardness of Direct Laser E-Mobility Components by Using Laser Sintering: Properties Direct Deposition Method Stainless Steel fabricated by Laser Deposited Ti-6Al-4V Parts Polyjet 3D Printing Characterization N. Shamsaei, M. Lugo, D. Seely, S. Additive Manufacture G. Marshall, W. Young, S. Thompson, C. Reinders, RWTH Aachen University, B. Ong, H. Wu, J. Koo, University of Thompson, A. Sterling, Mississippi State D. Seely, N. Shamsaei, B. Patton, D. Seely, N. Shamsaei, Mississippi State Aachen, Germany Texas, Austin, Austin, TX University, Mississippi State, MS Mississippi State University, Starkville, MS University, Mississippi State, MS Wednesday, 7 January 2015

130 282-MAT-11 Fatigue & Fracture II Sarasota 2 Chaired by: S. ARNOLD, University of Heidelberg, Germany and J. DUSTIN, GE-Aviation 1400 hrs 1430 hrs 1500 hrs 1530 hrs AIAA-2015-1358 AIAA-2015-1359 AIAA-2015-1360 AIAA-2015-1361 Experimental and numerical Investigation of Cyclic Behavior and Combined Multiscale Creep Strain Multiscale Stochastic Analysis of monitoring of strain gradients in Structure-property Relations of a and Creep Rupture Modeling for FRP based on variability in fiber notched composites under tension 304 Stainless Steel Composite Materials volume fraction, epoxy stiffness loading M. Lugo, J. Pegues, N. Shamsaei, E. Jensen, R. Fertig, University of and strength B. Aidi, S. W.Case, Virginia Polytechnic Mississippi State University, Mississippi Wyoming, Laramie, Laramie, WY S. Sanei, E. Jensen, R. Fertig, University Institute and State University, Blacksburg, VA State, MS of Wyoming, Laramie, Laramie, WY Wednesday, 7 January 2015 283-MDO-7 MDO: Decision Making/Value Driven Design Sarasota 3 Chaired by: J. HICKEN, Rensselaer Polytechnic Institute and G. KENNEDY, Georgia Institute of Technology 1400 hrs 1430 hrs 1500 hrs 1530 hrs AIAA-2015-1362 AIAA-2015-1363 AIAA-2015-1364 AIAA-2015-1365 Sensitivity analysis of surrogate- Defining and Mitigating Organization Design in the Context Variable-Fidelity Design Using based methodology for real-time Requirements-Induced Value Gaps of Value-Driven Design Kriging Surrogate Model with structural assessment A. Abbas, University of Illinois, Urbana- B. Kwasa, C. Bloebaum, B. Mesmer, Iowa Fidelity Indicator L. Mainini, K. Willcox, Massachusetts Champaign, Urbana, IL; C. Bloebaum, B. State University, Ames, IA Y. Jo, Korea Advanced Institute of Science Institute of Technology, Cambridge, MA Mesmer, Iowa State University, Ames, IA and Technology, Daejeon, Korea (the Republic of); S. Choi, Virginia Polytechnic Institute and State University, Blacksburg, VA; D. Lee, Korea Advanced Institute of Science and Technology, Daejeon, South Korea Wednesday, 7 January 2015 284-MST-11 MST Panel: Flight Simulation Training Device Qualification Testing Sun Ballroom 1 1400 - 1700 hrs Chaired by: B. MAZZACAVALLO, The Boeing Company Flight training requires an accurate representation of a flying aircraft with the fidelity and realism to affect a positive standard of behavior in flight crews. Qualification Test Guides (QTGs) are the method currently used to ensure the device remains faithful to the original design and qualification data. Recent discussions at industry conferences and events have discussed the topic of alternative methods to discern changes in an Flight Simulation Training Devices (FSTDs) accurate modeling of an aircraft type and/ or impacts and changes to the training being performed. This panel brings together industry experts and will endeavor to highlight the current state of the art and expose opportunities to utilize research and design expertise, academia and other simulation expertise to help optimize and develop new solutions to validating the training simulator system while minimizing the touch labor required. The current tools are used as an initial validation and recurring - new solutions to both requirements will be explored. Moderator: Brandon Mazzacavallo, Senior Manager of Simulator Management Services/Flight Operations Support at Boeing Panelists: Kip Caudrey Eric Fuilla-Weishaupt Jim Knezevich The Boeing Company Airbus FAA National Simulator Program

Wednesday, 7 January 2015 285-MVC-5 Visualization for Feature Detection, Integration Techniques and Frameworks, and Multi-Scale Models Naples 3 Chaired by: R. DAVIS, University of California Davis 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs AIAA-2015-1366 AIAA-2015-1367 AIAA-2015-1368 AIAA-2015-1369 AIAA-2015-1370 Visualization and Post-Processing of Recent advances in the integration Analysis of Stable and Unstable Visualization and Quantiﬁcation Design Sensitivity Calculations Large Scale Engineering Applications of CFD into the missile concept Manifolds in Fluid Flows Using of Rotor Tip Vortices in Helicopter Directly on CAD-based Geometry using In-Situ Data Extracts and Proper design process Lagrangian Coherent Structures Flows J. Dannenhoffer, Syracuse University, Orthogonal Decomposition N. Taylor, MBDA, Filton, United Kingdom A. Ahmed, I. Akhtar, I. Aziz, National D. Kao, J. Ahmad, T. Holst, NASA Ames Syracuse, NY; R. Haimes, Massachusetts E. Duque, D. Hiepler, Intelligent Light, University of Sciences and Technology, Research Center, Moffett Field, CA Institute of Technology, Cambridge, MA

131 Rutherford, NJ; S. Gorrell, M. Jones, T. Blanc, Islamabad, Pakistan Brigham Young University, Provo, UT Wednesday, 7 January 2015 286-NDA-6 Model Verification and Validation & Optimization under Uncertainty Osceola Ballroom 5 Chaired by: H. BAE, Wright State University and J. BROWN 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs AIAA-2015-1371 AIAA-2015-1372 AIAA-2015-1373 AIAA-2015-1374 AIAA-2015-1375 AIAA-2015-1376 AIAA-2015-1377 Experimental Validation of an Locally-Optimized Covariance Validation of Geometric Mistuning Evaluation of Model Validation A Surrogate-based Adjustment Comparing Deterministic and Decomposition-based Evolutionary Optically Measured Geometric Kriging for Engineering Design Reduced-Order Models for Single and Techniques in the Presence of Factor Approach to Multi-Fidelity Non-deterministic Optimization for Aerodynamic Robust Optimization Mistuning Model Using a System ID Exploration Dual Flow-Path Integrally Bladed Aleatory and Epistemic Input Design Optimization Airfoil Shape Design with Multi-fidelity Point Collocation Approach D. Clark, H. Bae, Wright State University, Rotors Uncertainties C. Fischer, R. Grandhi, Wright State T. Kanno, W. Crossley, Purdue University, Non-intrusive Polynomial Chaos A. Kaszynski, J. Brown, J. Beck, Air Force Dayton, OH; R. Penmetsa, Air Force J. Beck, Air Force Research Laboratory, Wright- I. Voyles, C. Roy, Virginia Polytechnic University, Dayton, OH West Lafayette, IN P. Palar, T. Tsuchiya, University of Tokyo, Research Laboratory, Wright-Patterson Research Laboratory, Wright-Patterson Patterson AFB, OH; A. Kaszynski, Universal Institute and State University, Blacksburg, Tokyo, Japan; G. Parks, University of AFB, OH AFB, OH Technology Corporation, Beavercreek, OH; O. VA Cambridge, Cambridge, United Kingdom Scott-Emuakpor, J. Brown, Air Force Research Laboratory, Wright-Patterson AFB, OH Wednesday, 7 January 2015 287-PANEL-6 The Digital System Model - The New Frontier in Aerospace & Defense Acquisition Osceola Ballroom B 1400 - 1600 hrs Moderator: Edward Kraft, Technical Advisor, Aerospace Ground Testing, Air Force Test Center Panelists: Kristen Baldwin Jeffery Holland David Walker Principal Deputy Director of Research and Development and Chief Scientist Deputy Assistant Secretary of the Air Force for Science, Technology, and Engineering Office of the Deputy Assistant Secretary of Defense for Systems Engineering Director of the U.S. Army Engineer Research and Development Center Office of the Assistant Secretary of the Air Force for Acquisition US Army Corp of Engineers Wednesday, 7 January 2015 288-PC-15 Turbulent Combustion Models, their Foundations and Major Assumptions Emerald 2 Chaired by: C. LI, Air Force Office of Scientific Research 1400 hrs 1430 hrs 1530 hrs 1630 hrs Oral Presentation AIAA-2015-1378 AIAA-2015-1379 AIAA-2015-1380 Insights into Model Assumptions Advances in the Simulation of Turbulent Combustion Survey of Turbulent Combustion Models for Large-Eddy Simulations of An analysis of the basic assumptions of turbulent combustion models with and Road to Model Validation for J. Oefelein, Sandia National Laboratories, Livermore, CA Propulsive Flowfields emphasis on high-speed flows Turbulent Combustion J. Foster, Corvid Technologies, Inc., Mooresville, NC; R. Miller, Clemson University, E. Gonzalez, Combustion Science and Engineering, Inc., Columbia, MD; S. Menon, R. Ranjan, V. Sankaran, Air Force Research Clemson, SC Georgia Institute of Technology, Atlanta, GA; A. Kerstein, Self, Danville, CA Laboratory, Edwards AFB, CA Wednesday, 7 January 2015 289-PC-16 Laminar Flames Emerald 7 Chaired by: H. IM, King Abdullah University of Science and Technology and D. GLAZE, Sandia National Laboratories 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs AIAA-2015-1381 AIAA-2015-1382 AIAA-2015-1383 AIAA-2015-1384 AIAA-2015-1385 AIAA-2015-1386 AIAA-2015-1387 A Dynamic Fidelity Adaptive Multi-timescale and Correlated Towards direct simulations of Evaluation of Soot Models in Modeling flame propagation and Local Burning Rates and Heat Cool Flames Activated by Ozone Modeling Framework for Dynamic Adaptive Chemistry and counterflow flames with consistent Computing m-Xylene Jet Diffusion quenching in stratified mixtures Flux for Boundary Layer Diffusion Addition Combustion Systems Based on Transport Modeling of Flames in differential-algebraic boundary Flames V. Katta, Innovative Scientific Solutions, Flames under Forced Flow C. Reuter, S. Won, Y. Ju, Princeton Local Estimation of Model Accuracy n-Heptane/Air Mixtures conditions V. Katta, Innovative Scientific Solutions, Inc., Dayton, OH; S. Zeppieri, M. Colket, A. Singh, M. Gollner, University of University, Princeton, NJ Y. See, H. Wu, Q. Wang, M. Ihme, W. Sun, Y. Ju, Princeton University, P. Kourdis, California Institute of Technology, Inc., Dayton, OH; W. Wang, M. United Technologies Corporation, East Maryland, College Park, College Park, MD Stanford University, Stanford, CA Princeton, NJ Pasadena, CA; J. Bellan, K. Harstad, Jet Linevsky, S. Iyer, T. Litzinger, B. Santoro, Hartford, CT; W. Roquemore, Air Force Propulsion Laboratory, California Institute of Pennsylvania State University, University Research Laboratory, Wright-Patterson Technology, Pasadena, CA Park, PA; et al. AFB, OH

132 Wednesday, 7 January 2015 290-PDL-5 Plasma & Laser Physics I Emerald 5 Chaired by: R. MILES, Princeton University and K. XU, University of Alabama in Huntsville 1400 hrs 1430 hrs 1500 hrs 1530 hrs AIAA-2015-1388 AIAA-2015-1389 AIAA-2015-1390 AIAA-2015-1391 Reducing the Breakdown Threshold Arc breakdown in high-pressure Pre-breakdown processes in Active Particles Production by Pulsed in DC Microdischarges via Metal large gap sources using surface dielectric fluid in inhomogeneous Nanosecond Discharge in Ambient Air. Nanoparticle Seeding streamer based initiation pulsed electric fields Quenching of Electronically Excited J. Sawyer, Z. Zhang, University of M. Pachuilo, F. Stefani, R. Bengtson, M. Shneider, Princeton University, States of Nitrogen by O2 Molecules Tennessee, Knoxville, Knoxville, TN L. Raja, University of Texas, Austin, Princeton, NJ and O(3P) Atoms Austin, TX N. Popov, Moscow State University, Moscow, Russia Wednesday, 7 January 2015 291-PDL-6 Astronautical Plasma Dynamics Emerald 8 Chaired by: J. WANG, University of Southern California and H. USUI, Kobe University 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2015-1392 AIAA-2015-1393 AIAA-2015-1394 AIAA-2015-1395 AIAA-2015-1396 AIAA-2015-1397 Drag Measurements in a Simulated PIC Simulation on Plasma Flow Numerical Simulations of Electron Kinetic Characteristics Dynamics of Spacecraft Plume/ Plume Structure and Current- Low-Earth Orbit Environment Response to a Mesoscale Magnetic Spacecraft-Plasma Interactions on in Plasma Plumes: Fully Kinetic Magnetosphere Interactions in Voltage Characteristic Analysis for a C. Maldonado, A. Ketsdever, University Dipole in Space Lunar Surface Simulations Geostationary Earth Orbit Cathodic Plasma Contactor of Colorado, Colorado Springs, Colorado H. Usui, M. Umezawa, Y. Miyake, Kobe D. Han, J. Wang, University of Southern Y. Hu, J. Wang, University of Southern K. Stephani, University of Illinois, Urbana- Q. Xia, K. Xie, Beijing Institute of Technology, Springs, CO University, Kobe, Japan California, Los Angeles, CA California, Los Angeles, CA Champaign, Urbana, IL; I. Boyd, University Beijing, China; N. Guo, Y. Jia, Lanzhou of Michigan, Ann Arbor, Ann Arbor, MI University, Lanzhou, China; X. Liu, Z. Wu, Beijing Institute of Technology, Beijing, China Wednesday, 7 January 2015 292-SCS-7 Spacecraft Antennas and Apertures Osceola Ballroom 4 Chaired by: W. BELVIN, NASA-Langley Research Center and J. MOORE, ManTech Nexolve Corporation 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs AIAA-2015-1398 AIAA-2015-1399 AIAA-2015-1400 AIAA-2015-1401 AIAA-2015-1402 AIAA-2015-1403 AIAA-2015-1404 Telescoping Solar Array Concept Experimental Study of Reflector Energy-Efficient Active Reflectors Optimal Placement of Actuators The Mechanical Design of a Mesh Spin-Stabilized Membrane Antenna Thermal Distortion Testing of a for Achieving High Packaging Shape Control under Various with Improved Mechanical Stability and Sensors for Gyroelastic Body Ka-band Parabolic Deployable Structures 4-meter Microwave Reflector Efficiency Thermal Conditions S. Bradford, D. Hofmann, Jet Propulsion from the Controllability and Antenna (KaPDA) for CubeSats M. Delapierre, S. Pellegrino, California S. Bradford, Jet Propulsion Laboratory, M. Mikulas, National Institute of A. Inagaki, H. Sakamoto, Tokyo Institute Laboratory, California Institute of Observability Perspective J. Sauder, M. Thomson, Jet Propulsion Institute of Technology, Pasadena, CA California Institute of Technology, Aerospace, Hampton, VA; R. Pappa, J. of Technology, Tokyo, Japan; H. Tanaka, Technology, Pasadena, CA; D. Kochmann, Q. Hu, Beijing Institute of Technology, Laboratory, California Institute of Pasadena, CA Warren, G. Rose, NASA Langley Research National Defense Academy, Kanagawa, California Institute of Technology, Beijing, China; Z. Wang, Beihang Technology, Pasadena, CA Center, Hampton, VA Japan; K. Ishimura, Japan Aerospace Pasadena, CA University, Beijing, China; J. Zhang, Beijing Exploration Agency (JAXA), Kanagawa, Institute of Technology, Beijing, China; Y. Japan; M. Okuma, Tokyo Institute of Jia, Beihang University, Beijing, China; Technology, Tokyo, Japan M. Liu, Z. Zhou, China Academy of Space Technology, Beijing, China Wednesday, 7 January 2015 293-SD-10 Special Session: Adaptive Aeroelastic Wing Shaping Control I Sun Ballroom D Chaired by: N. NGUYEN, NASA-Ames Research Center and S. ANDERS, NASA Langley Research Center 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs AIAA-2015-1405 AIAA-2015-1406 AIAA-2015-1407 AIAA-2015-1408 AIAA-2015-1409 Aeroelastic Analysis of Wind Tunnel The design, construction, and Static Aeroelastic Modeling of a Multidisciplinary Drag Optimization Optimized Off-Design Performance Test Data of a Flexible Wing with tests of a concept aeroelastic Sub-Scale Wind Tunnel Model with of Reduced Stiffness Flexible Wing of Flexible Wings with Continuous a Variable Camber Continuous wind tunnel model of a high-lift Novel Flap Concept Aircraft With Variable Camber Trailing-Edge Flaps 133 Trailing Edge Flap (VCCTEF) variable camber continuous trailing E. Ting, Stinger Ghaffarian Technologies, Continuous Trailing Edge Flap D. Rodriguez, M. Aftosmis, M. Nemec, N. Nguyen, NASA Ames Research Center, edge flap (HL-VCCTEF) wing Inc., Moffett Field, CA; N. Nguyen, NASA S. Lebofsky, E. Ting, Stinger Ghaffarian NASA Ames Research Center, Moffett Moffett Field, CA; E. Ting, S. Lebofsky, configuration Ames Research Center, Moffett Field, Technologies, Inc., Moffett Field, CA; N. Field, CA; G. Anderson, Stanford Stinger Ghaffarian Technologies, Inc., N. Precup, M. Mor, E. Livne, University of CA; S. Lebofsky, Stinger Ghaffarian Nguyen, NASA Ames Research Center, University, Stanford, CA Moffett Field, CA Washington, Seattle, Seattle, WA Technologies, Inc., Moffett Field, CA Moffett Field, CA Wednesday, 7 January 2015 294-SD-11 Special Session: Transformative Technologies for High-Speed/High-Efficiency Next-Gen Rotorcraft II Tampa 2 Chaired by: E. SMITH, Pennsylvania State University and A. DATTA, Science & Technology Corporation 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2015-1411 AIAA-2015-1412 AIAA-2015-1413 AIAA-2015-1414 AIAA-2015-1415 AIAA-2015-1416 Aeromechanics of the Coaxial Transient Hub Loads and Blade Performance and Loads Prediction Advanced Composite Wings for Aeroelastic Optimization for High- Tube Compliance Effects on Fluidic Compound Helicopter Deformation of a Mach-Scale for a High Advance Ratio Coaxial Whirl Flutter Augmentation: Wind Speed, High-Efficiency Tiltrotors Flexible Matrix Composite Devices C. Zhang, AVX Aircraft Company, Benbrook, Coaxial Rotor in Hover Rotor Tunnel Model Design with Wing Extensions and Winglets for Rotorcraft Vibration Control TX; T. Quackenbush, Continuum Dynamics, C. Cameron, J. Sirohi, D. Uehara, J. Schmaus, I. Chopra, University of J. Zhang, E. Smith, Pennsylvania State S. Kambampati, J. Zhang, E. Smith, M. Krott, K. Miura, S. LaBarge, C. Rahn, Inc., Ewing, PA; H. Saberi, Advanced Rotorcraft University of Texas, Austin, Austin, TX Maryland, College Park, College Park, MD University, University Park, PA Pennsylvania State University, University E. Smith, Pennsylvania State University, Technology, Inc., Sunnyvale, CA; C. Sheng, Park, PA University Park, PA; P. Romano, Bell University of Toledo, Toledo, OH; T. Gaffey, Helicopter Textron, Inc., Hurst, TX AVX Aircraft Company, Benbrook, TX Wednesday, 7 January 2015 295-SD-12 Flutter, LCO and Aeroelastic Instabilities Tampa 3 Chaired by: J. COOPER, University of Bristol and W. WELSH, Sikorsky Aircraft Corporation 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs AIAA-2015-1417 AIAA-2015-1418 AIAA-2015-1419 AIAA-2015-1420 AIAA-2015-1421 AIAA-2015-1422 AIAA-2015-1423 The Influence of Steady Loading Store-Induced Limit Cycle Whirl Flutter Analysis with Propeller Effect of Embedded Control Surface A Modification to the Enhanced In-Flight Aeroelastic Stability of Nonlinear airfoil torsional response Parameters on Low-Pressure Oscillations due to Nonlinear Wing- Aerodynamic Derivatives Computed Actuators on Active Aeroelastic Correction Factor Technique to the Thermal Protection System induced by separated flows Turbine Flutter Store Attachment by Unsteady Vortex Lattice Method Control Correlate With Experimental Data on the NASA HIAD, Part II: F. Marques, D. Pereira, University of São J. Waite, R. Kielb, Duke University, M. Padmanabhan, Duke University, Z. Wang, P. Chen, ZONA Technology, Inc., R. Brown, K. Singh, Miami University, R. Moreno, F. von Knoblauch, R. Nonlinear Theory and Extended Paulo, São Carlos, Brazil; R. Vasconcellos, Durham, NC; S. Bittner, Leibniz University, Durham, NC; C. Pasiliao, Air Force Scottsdale, AZ Oxford, OH; R. Kolonay, Air Force Research Narisetti, P. Taylor, Gulfstream Aerospace Aerodynamics São Paulo State University, São Joao da Hannover, Germany Research Laboratory, Eglin AFB, FL; E. Laboratory, Wright-Patterson AFB, OH Corporation, Savannah, GA B. Goldman, E. Dowell, Duke University, Boa Vista, Brazil Dowell, Duke University, Durham, NC Durham, NC Wednesday, 7 January 2015 296-SEN-2 Novel Sensor Systems Osceola Ballroom 1 Chaired by: M. MAJJI, State University of New York at Buffalo 1400 hrs 1430 hrs 1500 hrs 1530 hrs AIAA-2015-1424 AIAA-2015-1425 AIAA-2015-1426 AIAA-2015-1427 Optical Flow Techniques for A Low-Cost System for Wind Performance Evaluation of 3D Model- Wing Shape Sensing from Wind-Velocity Sensing on a Small Field Estimation Through Sensor based Techniques for Autonomous Measured Strain Unmanned Aircraft System Networks and Aircraft Design Pose Initialization and Tracking C. Pak, NASA Armstrong Flight Research D. Pope, B. Argrow, D. Lawrence, University of R. Laurence, J. Elston, B. Argrow, University of R. Opromolla, G. Fasano, G. Rufino, M. Center, Edwards, CA Colorado, Boulder, Boulder, CO Colorado, Boulder, Boulder, CO Grassi, University of Naples “Federico II”, Naples, Italy

134 Wednesday, 7 January 2015 297-STR-14 Design, Test and Analysis I Tampa 1 Chaired by: W. YU, Purdue University and B. WILLIS, Boeing Defense, Space & Security 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs AIAA-2015-1428 AIAA-2015-1429 AIAA-2015-1430 AIAA-2015-1431 AIAA-2015-1432 AIAA-2015-1433 AIAA-2015-1434 Thermally Driven Morphing with Mechanical Properties and Fatigue Topology Optimization of Significance of Geometric Postbuckling Analysis of Composite Warping of Stiffened Composite Design and Evaluation of a Test Hybrid Laminates and Metal Matrix Behavior of 2D and 3D Woven PMC Additively-Manufactured, Lattice- Nonlinearity in the Design of Stiffened Panel under Shear Load Panels Due to Temperature Device for Thermal-Acoustical- Composites Airframe Structures at Elevated Reinforced Penetrative Warheads Thermally Loaded Structures K. Umezawa, T. Aoki, University of Tokyo, Changes in the Curing Process Mechanical Fatigue Experiments E. Eckstein, A. Pirrera, P. Weaver, Temperature H. Richards, D. Liu, Air Force Institute of J. Deaton, R. Grandhi, Wright State Tokyo, Japan A. Przekop, NASA Langley Research M. Sedlack, A. Jasmin, P. Lavandera, University of Bristol, Bristol, United M. Wilkinson, Air Force Research Technology, Wright-Patterson AFB, OH University, Dayton, OH Center, Hampton, VA A. Gordon, University of Central Florida, Kingdom Laboratory, Wright-Patterson AFB, OH; Orlando, FL; R. Penmetsa, Air Force M. Ruggles-Wrenn, Air Force Institute of Research Laboratory, Wright-Patterson Technology, Wright-Patterson AFB, OH AFB, OH Wednesday, 7 January 2015 298-STR-15 Structural Stability Tallahassee 3 Chaired by: C. BISAGNI and J. HEALD, Canadian Space Agnecy 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2015-1435 AIAA-2015-1436 AIAA-2015-1437 AIAA-2015-1438 AIAA-2015-1439 AIAA-2015-1440 Buckling Analysis of Axially Loaded Effect of Buckling Modes on the A Comparison of FEM and Semi- Buckling analysis and optimization Buckling and Postbuckling of Optimization of Damaged Corrugated Cylindrical Shells Fatigue Life and Damage Tolerance Analytical Method in the Buckling and of blade stiffened variable stiffness Unitized, Stiffened Composite Composite Plates Under Buckling X. Ning, S. Pellegrino, California Institute of Stiffened Structures Vibration of Non-Prismatic Columns panels Panels and Post buckling condition of Technology, Pasadena, CA C. Davila, NASA Langley Research Center, under Tip Force and Self-Weight B. Coburn, Z. Wu, P. Weaver, University of C. Kosztowny, A. Waas, University of in Hygrothermal Environment Hampton, VA; C. Bisagni, University of J. Cifuentes, R. Kapania, Virginia Bristol, Clifton, United Kingdom Michigan, Ann Arbor, Ann Arbor, MI employing an Inverse Hyperbolic California, San Diego, La Jolla, CA; C. Polytechnic Institute and State University, Shear Deformation Theory Rose, NASA Langley Research Center, Blacksburg, VA V. Sreehari, D. Maiti, Indian Institute of Hampton, VA Technology Kharagpur, Kharagpur, India Wednesday, 7 January 2015 299-TES-1 Thermal and Fluid Behavior in Power Systems Captiva 1 Chaired by: R. AMANO, University of Wisconsin-Milwaukee 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2015-1441 AIAA-2015-1442 AIAA-2015-1443 AIAA-2015-1444 AIAA-2015-1445 AIAA-2015-1446 On the Modeling of Thermal Study of Liquid Breakup Process in Energy Efficient Designs of Low Flow and Heat Transfer in a Rotating Modelling and Simulation on A Weave Design for Trailing-Edge Comfort in Heavy Truck Passengers Solid Rocket Motor Nozzle Carbon Buildings and Non-Rotating Wedge-Shaped Ingress into the Rim Seal and Cooling Cabins R. Amano, Y. Yen, M. Hamman, University E. Khalil, Cairo University, Cairo, Egypt; Cooling Passage with Ribs and Pin Fins Wheelspace of a Rotor-Stator A. Weaver, J. Liu, T. Shih, Purdue A. Omran, E. Khalil, Cairo University, of Wisconsin, Milwaukee, Glendale, WI W. Ajami, University of Technology MARA, I. Pardeshi, T. Shih, Purdue University, West Configuration University, West Lafayette, IN Cairo, Egypt Shah Allam, Malaysia Lafayette, IN; K. Bryden, Ames Laboratory, J. Liu, A. Weaver, T. Shih, Purdue Ames, IA; R. Ames, R. Dennis, National Energy University, West Lafayette, IN; C. Sangan, Technology Laboratory, Morgantown, WV; S. G. Lock, Bath University, Bath, United Ding, Beihang University, Beijing, China Kingdom Wednesday, 7 January 2015 300-TP-7 Ablation and Surface Catalysis Sun Ballroom B Chaired by: A. MARTIN, University of Kentucky and D. KUNTZ, Sandia National Laboratories 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs AIAA-2015-1447 AIAA-2015-1448 AIAA-2015-1449 AIAA-2015-1450 AIAA-2015-1451 AIAA-2015-1452 AIAA-2015-1453 Quantitative determination Conformal Phenolic Impregnated Molecular simulations of surface Microscale Simulations of In-Situ Measurement of Ablation Numerical Simulation of Regular Influence of Carbon Nitridation of species production from Carbon Ablator (C-PICA) Arcjet ablation using reaction probabilities Porous TPS Materials: Ablating Fronts of A Low Density Ablator Surface Patterns on Sublimating in a Nonequilibrium Finite-Rate the pyrolysis of the Phenolic Testing, Ablation and Thermal from molecular beam experiments Microstructures and Micro- With An Ablation Sensor Ablative Materials Ablation Model Impregnated Carbon Ablator (PICA) Response and realistic microstructure tomography T. Sakai, H. Nakazawa, Y. Dantsuka, K. L. Trevino, G. Candler, University of C. Alba, R. Greendyke, Air Force Institute H. Wong, J. Peck, J. Assif, Aerodyne F. Milos, M. Gasch, NASA Ames Research S. Poovathingal, T. Schwartzentruber, E. Stern, I. Nompelis, T. Schwartzentruber, Watanabe, Nagoya University, Nagoya, Minnesota, Minneapolis, Minneapolis, MN of Technology, Wright-Patterson AFB, OH; Research, Inc., Billerica, MA; J. Lachaud, Center, Moffett Field, CA University of Minnesota, Minneapolis, G. Candler, University of Minnesota, Japan; K. Kitagawa, Aichi Institute of J. Marschall, SRI International, Menlo 135 University of California, Santa Cruz, Minneapolis, MN; V. Murray, T. Minton, Minneapolis, Minneapolis, MN Technology, Toyota, Japan; K. Hirai, IHI Park, CA Moffett Field, CA; N. Mansour, NASA Ames Montana State University, Bozeman, MT Corporation, Tomioka, Japan; et al. Research Center, Moffett Field, CA Wednesday, 7 January 2015 301-UMS-5 Unmanned Systems: Technologies and Applications II Osceola Ballroom 2 Chaired by: R. PRAZENICA, Embry-Riddle Aeronautical University, Daytona Beach 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs AIAA-2015-1454 AIAA-2015-1455 AIAA-2015-1456 AIAA-2015-1458 AIAA-2015-1459

Experimental Design of a Flapping Development and Testing of an Optimizing Energy Efficiency of Search and Rescue using CO2 Plume Detection Using UAS Wing Micro Air Vehicle through Unmanned Aerial System with a Flapping Robotic Bird Through Unmanned Aerial Vehicles C. Brown, T. Mitchell, J. Jacob, Oklahoma Biomimicry of Bumblebees Micro-Fiber Composite Actuators Application of Evolutionary Algorithms S. Bhandari, A. Bettadapura, O. Dadian, State University, Stillwater, OK M. Thompson, J. Burnett, D. Ixtabalan, D. M. Chan, H. Moncayo, A. Perez Rocha, R. B. Perseghetti, J. Gallagher, Wright State M. Gan, J. Dayton, California Polytechnic Tran, A. Batra, A. Rodriguez, Arizona State Prazenica, D. Kim, B. Azizi, Embry-Riddle University, Dayton, OH; J. Goppert, S. State University, Pomona, CA University, Tempe, AZ; et al. Aeronautical University, Daytona Beach, FL Yantek, E. Matson, I. Hwang, Purdue University, West Lafayette, IN Wednesday, 7 January 2015 302-WE-11 Wind Turbine Aeroelasticity and Structural Dynamics Emerald 4 Chaired by: C. BOTTASSO, Technichse Universität München 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2015-1460 AIAA-2015-1461 AIAA-2015-1462 AIAA-2015-1463 AIAA-2015-1464 AIAA-2015-1465 Aeroelastic Modeling of Wind FAST Modular Framework for Wind Towards Multidisciplinary Wind Aeroelastic Time-Domain Prediction and Alleviation of Flutter BeamDyn: A High-Fidelity Wind Turbine Blades Using Harmonic Turbine Simulation: New Algorithms Turbine Design using High-Fidelity Simulation of SNL Smart Rotor in Swept Wind Turbine Blades Turbine Blade Solver in the FAST Balance and γ-Re_θt Transition and Numerical Examples Methods Experiment S. Larwood, University of the Pacific, Modular Framework Model M. Sprague, J. Jonkman, B. Jonkman, M. Imiela, F. Wienke, German Aerospace L. Bernhammer, R. De Breuker, G. van Stockton, CA Q. Wang, National Renewable Energy J. Howison, K. Ekici, University of National Renewable Energy Laboratory, Center (DLR), Braunschweig, Germany Kuik, Delft University of Technology, Delft, Laboratory, Golden, CO; N. Johnson, Tennessee, Knoxville, Knoxville, TN; J. Golden, CO The Netherlands Colorado School of Mines, Golden, CO; M. Thomas, Duke University, Durham, NC Sprague, J. Jonkman, National Renewable Energy Laboratory, Golden, CO Wednesday, 7 January 2015 303-WE-12 Wind Energy Atmospheric Physics and Inflow Emerald 6 Chaired by: S. SCHRECK, NREL and S. SCHMITZ, Pennsylvania State University 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs AIAA-2015-1466 AIAA-2015-1467 AIAA-2015-1468 AIAA-2015-1469 AIAA-2015-1470 AIAA-2015-1471 AIAA-2015-1472 The effect of stability on the Turbulent wind field Turbulent Flow and Heat Transport Real-Time Flow Prediction of Low- Comparing wall modeled LES Simulation of wind turbine wakes Development of CFD-based icing intermittent nature of atmospheric characterization and re-generation over a Two-dimensional Steep Hill: Level Atmospheric Turbulence and prescribed boundary layer on locally refined Cartesian grids model for wind turbines: A case winds based on pitot tube measurements Wind-tunnel Experiments R. Kikuchi, T. Misaka, S. Obayashi, Tohoku approach in infinite wind farm D. Angelidis, F. Sotiropoulos, University of study of ice sensor M. Sherry, University of Calgary, Calgary, mounted on a wind turbine W. Zhang, University of Minnesota, University Institute of Fluid Science, simulations Minnesota, Minneapolis, Minneapolis, MN M. Pedersen, Vattenfall Vindkraft, Fredericia, Canada M. Pedersen, T. Larsen, G. Larsen, H. Minneapolis, Minneapolis, MN; C. Markfort, Sendai, Japan H. Chivaee, R. Mikkelsen, Technical Denmark; C. Yin, Aalborg University, Aalborg, Madsen, Technical University of Denmark, F. Porte-Agel, Swiss Federal Institute of University of Denmark, Lyngby, Denmark Denmark; A. Billstein Andersson, Vattenfall

136 Roskilde, Denmark Technology, Lausanne, Switzerland Vindkraft, Fredericia, Denmark Wednesday, 7 January 2015 304-LEC-5 Structures, Structural Dynamics, and Materials Lecture: Aerospace Structural Design and Safety: Do We Need Fewer Tests or More? Osceola Ballroom B 1800 - 1900 hrs Raphael Haftka Distinguished Professor University of Florida Thursday Thursday, 8 January 2015 305-PLNRY-4 Diversity & Inclusion in the Aerospace Workforce Osceola Ballroom CD 0800 - 0900 hrs Moderator: Sandra H. Magnus, Executive Director, American Institute of Aeronautics and Astronautics Panelists: Wesley Harris Julio Navarro Alton Romig Tom Shih Yvette Weber Charles Stark Draper Professor of Aeronautics & Astronautics Senior Technical Fellow Vice President Professor and Head of Aeronautics and Astronautics Director C-5 Program Massachusetts Institute of Technology The Boeing Company Advanced Development Programs, The Skunk Works Purdue University United States Air Force Lockheed Martin Aeronautics Thursday, 8 January 2015 306-ABPSI-1 Propulsion Integration and Controls Emerald 2 Chaired by: R. SCHARNHORST, Boeing Defense, Space & Security and R. NICHOLS, The University of Alabama at Birmingham 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2015-1473 AIAA-2015-1474 AIAA-2015-1475 AIAA-2015-1476 Estimation of optimal flight altitude Dynamic Friction Measurements on Key Parameters Of Air Breathing Validation of an Integrated Airframe for an aircraft a Small Engine Test Bench Two-Stroke Combustion Engines For and Turbofan Engine Simulation for A. Singh, S. Dhawan, SRM University, K. Horn, A. Rowton, M. Polanka, Integration Into Small Scale UAVs Evaluation of Propulsion Control Chennai, India J. Ausserer, Air Force Institute of O. Ariff, E. Salami, F. Romli, Putra Modes Technology, Wright-Patterson AFB, OH; University, Serdang, Malaysia J. Litt, NASA Glenn Research Center, Cleveland, P. Litke, Air Force Research Laboratory, OH; Y. Liu, N&R Engineering, Inc., Parma Wright-Patterson AFB, OH; K. Grinstead, Heights, OH; T. Sowers, Vantage Partners, Innovative Scientific Solutions, Inc., LLC, Brook Park, OH; A. Owen, Self, North Dayton, OH Royalton, OH; T. Guo, NASA Glenn Research Center, Cleveland, OH Thursday, 8 January 2015 307-ACD-4 Conceptual Aircraft Design Working Group (CADWG21) Panel: How much fidelity in conceptual aircraft design? Naples 3 0930 - 1230 hrs Chaired by: T. TAKAHASHI, Arizona State University and W. ANEMAAT, DARcorporation Panelists: Jason Merret Colin Johnson Jason Welstead Shreekant Agrawal Ed Alyanak Arthur Rizzi Juan Alonso Gulfstream Aerospace Desktop Aeronautics NASA/LaRC Northrop Grumman Corporation AFRL/RVQC KTH Royal Institute of Technology Stanford University

137 Thursday, 8 January 2015 308-AFM-11 Flight Test and System Identification Captiva 1 Chaired by: B. LEONHARDT, DB Aircraft, LLC and J. GRAUER, NASA Langley Research Center 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2015-1477 AIAA-2015-1478 AIAA-2015-1479 AIAA-2015-1480 AIAA-2015-1481 High Angle of Attack Model Fuel State Reconstruction for Quadrotor 6-DOF HIL Simulation System Identification and Handling Flight test results of Observer/ Identification with Compressibility Maneuvering Aircraft and Verification Using a 6-axis Quality Analysis of a UAV from Kalman Filter Identification of the Effects E. Ozger, Ingolstadt University of Applied Load Cell Flight Test Data Pegasus unmanned vehicle J. Dias, Brazilian Air Force, São José dos Sciences, Ingolstadt, Germany T. Fields, G. King, University of Missouri, O. Simsek, Turkish Aerospace Industries, T. Woodbury, J. Valasek, F. Arthurs, Texas Campos, Brazil Kansas City, Kansas City, MO Inc., Ankara, Turkey; O. Tekinalp, Middle A&M University, College Station, TX East Technical University, Ankara, Turkey Thursday, 8 January 2015 309-AMT-5 Aerodynamic Diagnostics Tool for High Speed Flows Tallahassee 1 Chaired by: J. WAGNER, Sandia National Laboratories and S. ZAIDI, Agilent Technologies 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2015-1482 AIAA-2015-1483 AIAA-2015-1484 AIAA-2015-1485 AIAA-2015-1486 Gas-Phase Temperature Laser Doppler Velocimetry in Krypton Tagging Velocimetry for Method for spectra estimation from Application of a Focusing Schlieren Measurements at the Exhaust of Supersonic Round Jets Use in High-Speed Ground-Test high-speed experimental data at Deflectometry Velocimeter in a J85 Engine using Coherent Anti- A. Karns, R. Powers, D. McLaughlin, Facilities discrete points in time Supersonic Flow Stokes Raman Scattering Pennsylvania State University, University N. Parziale, Stevens Institute of A. Schreyer, L. Larchevêque, P. Dupont, J. Geerts, K. Yu, University of Maryland, A. Alexander, Aerospace Testing Alliance, Park, PA Technology, Hoboken, NJ; M. Smith, National Center for Scientific Research College Park, College Park, MD Arnold AFB, TN; P. Hsu, Spectral Energies, Aerospace Testing Alliance, Silver Spring, (CNRS), Marseille, France LLC, Dayton, OH; J. Wehrmeyer, Aerospace MD; E. Marineau, Arnold Engineering Testing Alliance, Arnold AFB, TN; S. Roy, Development Complex, Silver Spring, MD Spectral Energies, LLC, Dayton, OH; J. Gord, Air Force Research Laboratory, Wright-Patterson AFB, OH; J. Kriesel, Opto- Knowledge Systems, Inc., Torrance, CA Thursday, 8 January 2015 310-APA-30 Aerodynamic Design: Analysis, Methodologies & Optimization Techniques III Naples 1 Chaired by: A. VANDERWYST, Raytheon Missile Systems and K. DENISSEN, Sandia National Labs 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2015-1487 AIAA-2015-1488 AIAA-2015-1489 AIAA-2015-1490 Optimization of MVG Position for Using Mesh Adjoint for Shock Bump Multi-Winglets: Multi-Objective Effect of surface morphing on the Control of Shock Boundary Layer Deployment and Optimisation on Optimization of Aerodynamic Shapes wake structure and performance of 138 Interaction Transonic Wings S. Reddy, G. Dulikravich, A. Abdoli, pitching-rotating plates C. Liu, Y. Yang, Y. Yan, University of Texas, F. Zhu, N. Qin, University of Sheffield, Florida International University, Miami, Y. Ren, H. Dong, University of Virginia, Arlington, Arlington, TX Sheffield, United Kingdom FL; H. Sobieczky, Vienna University of Charlottesville, Charlottesville, VA Technology, Vienna, Austria Thursday, 8 January 2015 311-APA-31 Propeller/Rotorcraft/Wind Turbine Aerodynamics II Naples 2 Chaired by: M. CALVERT, U.S. Army AMRDEC and J. MURRAY, Sandia National Laboratories 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2015-1491 AIAA-2015-1492 AIAA-2015-1493 AIAA-2015-1494 AIAA-2015-1495 Fully Implicit Discrete Adjoint Tip Vortex Dynamics of a Pitching An Experimental Study of the Characterization of blade throw A Damage Assessment for Wind Methods Rotor Blade Tip Model Effects of Winglets and Serrations from a 2.3MW horizontal axis wind Turbine Blades from Heavy M. Biava, M. Woodgate, G. Barakos, C. Wolf, C. Merz, K. Richter, M. Raffel, on the Wake of a Wind Turbine turbine upon failure Atmospheric Particles University of Liverpool, Liverpool, United German Aerospace Center (DLR), V. Klimchenko, A. Jones, University of H. Chivaee, J. Sørensen, Technical G. Fiore, G. Camarinha Fujiwara, M. Selig, Kingdom Göttingen, Germany Maryland, College Park, College Park, MD University of Denmark, Lyngby, Denmark University of Illinois, Urbana-Champaign, Urbana, IL Thursday, 8 January 2015 312-APA-32 Applied CFD & Numerical Correlations with Experimental Data II Destin 1 Chaired by: E. FELTROP, The Cessna Aircraft Company and D. O’BRIEN, US Army RDECOM 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2015-1496 AIAA-2015-1497 AIAA-2015-1498 AIAA-2015-1499 AIAA-2015-1500 Detached Eddy Simulation for the Numerical Study of Ditching Effect of Tail Dihedral Angle on Numerical Simulation of the Integrated Aerodynamic Benefits of F-16XL Aircraft Configuration Characteristics of a Transport Lateral Directional Stability due to Flowfield around Airfoil with Distributed Propulsion A. Elmiligui, K. Abdol-Hamid, NASA Langley Aircraft by Global Moving Mesh Sideslip Angles Spoiler using the Higher Order A. Wick, J. Hooker, Lockheed Martin Research Center, Hampton, VA; E. Parlette, Q. Qu, M. Hu, H. Guo, P. Liu, Beihang N. Musa, S. Mansor, A. Ali, M. Che Spectral Difference Method Corporation, Marietta, GA; C. Zeune, ViGYAN, Inc., Hampton, VA University, Beijing, China; R. Agarwal, Man, University of Technology, Malaysia, M. Alhawwary, F. Owis, M. Abdelrahman, Air Force Research Laboratory, Wright- Washington University in St. Louis, St. Skudai, Malaysia Cairo University, Giza, Egypt Patterson AFB, OH Louis, MO Thursday, 8 January 2015 313-APA-33 High-Angle-of-Attack & High-lift Aerodynamics Sun Ballroom A Chaired by: A. SCLAFANI, Boeing Engineering Operations & Technology and J. AZEVEDO 0930 hrs 1000 hrs 1030 hrs AIAA-2015-1501 AIAA-2015-1502 AIAA-2015-1503 Time-Resolved Measurements of Geometrically-Exact Extension of Experimnetal Investigations of the Cellular Separation on a Stalling Theodorsen’s Frequency Response Lift Frequency Response at High Airfoil Model Angels of Attack K. Disotell, J. Gregory, Ohio State H. Taha, University of California, Irvine, Irvine, M. Zakaria, H. Taha, M. Hajj, Virginia University, Columbus, OH CA; Z. Yan, M. Hajj, Virginia Polytechnic Polytechnic Institute and State University, Institute and State University, Blacksburg, VA Blacksburg, VA Thursday, 8 January 2015 314-APA-34 Special Session: CREATE-AV High Performance Computing Multiphysics Applications of Full-up Air Vehicles IV Destin 2 Chaired by: N. HARIHARAN, CREATE-AV and J. FORSYTHE 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2015-1504 AIAA-2015-1505 AIAA-2015-1506 AIAA-2015-1507 AIAA-2015-1508 Static and Dynamic CFD Analysis of Investigation of Aeroelastic Flow A Flight Simulator for Agile Ensuring a smooth transition from CREATE-AV DaVinci 3.0 and a Generic Swept Wing UCAV Control of a Fluttering Wing with Fighter Aircraft and Nonlinear semi-structured surface boundary Capstone Integration E. Lynch, A. Crowell, J. Lee, Naval Air HPCMP CREATE™-AV Kestrel Aerodynamics layer mesh to fully unstructured G. Brooks, Secure Mission Solutions, North Systems Command, Patuxent River, MD C. Fagley, J. Seidel, T. McLaughlin, U.S. H. Carlson, R. Verberg, Clear Science anisotropic surface mesh Charleston, SC Air Force Academy, Colorado Springs, CO Corporation, Harford, NY R. Aubry, Naval Research Laboratory, Washington, DC Thursday, 8 January 2015 139 315-AS-6 Space Applications Osceola Ballroom 6 Chaired by: G. AGNES, Jet Propulsion Laboratory and R. BARRETT-GONZALEZ, The University of Kansas 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2015-1509 AIAA-2015-1510 AIAA-2015-1511 AIAA-2015-1512 A Morphing Radiator for High- Analysis of Highly Coupled The Spacecraft SHM Experiment, LQR Using Second Order Voctor Turndown Thermal Control of Thermal-Structural Responses in Part 1: Development for Space Form for a Membrane with Crewed Space Exploration Vehicles Morphing Radiative Bodies Flight Bimorph Actuators T. Cognata, Paragon Space Development C. Bertagne, D. Hartl, Texas A&M D. Doyle, S. Lee, J. Stein, Air Force I. Ferhat, C. Sultan, Virginia Polytechnic Corporation, Houston, TX; D. Hartl, Texas University, College Station, TX; T. Cognata, Research Laboratory, Kirtland AFB, NM; Institute and State University, Blacksburg, A&M University, College Station, TX; R. Paragon Space Development Corporation, S. Kessler, Metis Design Corporation, VA Sheth, C. Dinsmore, NASA Johnson Space Houston, TX Boston, MA Center, Houston, TX Thursday, 8 January 2015 316-DE-3 Wildlife Conservation UAV Challenge (wcUAVc) Sun Ballroom D 0930 - 1230 hrs Chaired by: L. SAAM, ATA Engineering, Inc. (HQ) and G. CREARY, NASA-Langley Research Center Moderator: Princess Aliyah Pandolfi, CEO - Kashmir World Foundation, wcUAVc Director Panelists: Jean Koster Samay Sigamani Toby Lankford Satyanarayanan Janakiraman Team AREND Team CruiseAders Team Aerial Vista Challenge Team SRM SCRO Thursday, 8 January 2015 317-EDU-1 Advancing Aerospace Education I Emerald 6 Chaired by: R. LEBEAU, Saint Louis University 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs Oral Presentation AIAA-2015-1513 AIAA-2015-1514 AIAA-2015-1515 AIAA-2015-1516 Empowering engineers through Undergraduate Research on A Massive Open Online Course in A Collaborative Conceptual Aircraft Forensic Engineering: Learning by structured online learning of CAE Peculiarities of the Combustion of Aerodynamics Design Environment for the Design Accident Teaching Investigation L. Bodnar, MSC Software Corporation, Ecologically Clean Paraffin Wax Fuels D. Darmofal, Massachusetts Institute of of Small-Scale UAVs in a Multi- Skills to Graduate Students using Newport Beach, CA in Hybrid Propellant Rocket Engines Technology, Cambridge, MA University Setting Real-Life Accident Simulations V. Naoumov, N. Al Masoud, P. Skomin, J. Becar, S. Gorrell, Brigham Young C. Rans, G. Saunders-Smits, M. P. Deptula, Central Connecticut State University, Provo, UT; B. Newill, Noesis Schuurman, Delft University of Technology, University, New Britain, CT Solutions, Carmel, IN Delft, The Netherlands Thursday, 8 January 2015 318-FD-40 Swept and 3D Shock Boundary Layer Interactions Daytona 1 Chaired by: J. LITTLE, The University of Arizona and J. AUSTIN, University of Illinois at Urbana-Champaign 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2015-1517 AIAA-2015-1518 AIAA-2015-1519 AIAA-2015-1520 Shock-Boundary Layer Interaction Large Eddy Simulation of A Three- Boundary layer separation in a 3D Study of Shock-shock interaction due to a Sharp Unswept Fin in a Dimensional Compression Ramp shock train for a double wedge configuration Mach 2 Flow Shock-Turbulent Boundary Layer R. Klomparens, M. Gamba, J. Driscoll, using a particle approach N. Arora, M. Ali, F. Alvi, Florida State Interaction University of Michigan, Ann Arbor, Ann O. Tumuklu, D. Levin, Pennsylvania State University, Tallahassee, FL D. Dawson, S. Lele, Stanford University, Arbor, MI University, University Park, PA; S. Gimelshein, Stanford, CA University of Southern California, Los Angeles, CA; J. Austin, University of Illinois, Urbana-

140 Champaign, Urbana, IL Thursday, 8 January 2015 319-FD-41 Turbulence Tallahassee 3 Chaired by: E. GUTMARK, University of Cincinnati 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2015-1521 AIAA-2015-1522 AIAA-2015-1523 AIAA-2015-1524 AIAA-2015-1525 Volumetric Three-Component Stereoscopic PIV measurements and Numerical Simulation of Pressure DNS Study on Hairpin Vortex Noise control of cavity flows for Measurements of Air Jet Flows of numerical simulation of turbulent Recovery and Distortion in an Aircraft Structure in Turbulence subsonic flows Different Diffuser Designs flow of liquid passing through Engine Intake Serpentine Diffuser with C. Liu, Y. Yan, H. Al-Dujaly, University of A. das Gupta, S. Roy, University of Florida, R. Wahidi, S. Olcmen, University of rectangular apertures in a narrow Vortex Generator Vanes Texas, Arlington, Arlington, TX Gainesville, Gainesville, FL Alabama, Tuscaloosa, Tuscaloosa, AL; W. annulus: influence of aperture B. Sasanapuri, ANSYS, Inc., Pune, India; Lai, TSI, Inc., Shoreview, MN shape on velocity field K. Kurbatskii, ANSYS, Inc., Lebanon, NH; Y. Perelstein, E. Gutmark, University of S. Kumar, ANSYS, Inc., Pune, India Cincinnati, Cincinnati, OH Thursday, 8 January 2015 320-FD-42 Turbulence Modeling II Sanibel 3 Chaired by: R. RANJAN, Georgia Institute of Technology and Y. SEE, University of Michigan 0930 hrs 1000 hrs AIAA-2015-1526 AIAA-2015-1527 Hybrid two-level large-eddy Turbulence Modeling for Realistic simulation of turbulent flow in a Computation of Internal Flow in channel, past a bump and around Liquid Ejector Pumps an inclined prolate spheroid J. Masud, M. Imran, Air University, R. Ranjan, S. Menon, Georgia Institute of Islamabad, Pakistan Technology, Atlanta, GA Thursday, 8 January 2015 321-FD-43 Turbulent Flow Solutions for NACA 0012 and Other Test Cases from the Turbulence Model Resource Website: Residual and Grid Convergence I (Invited) Sanibel 2 Chaired by: K. FIDKOWSKI, University of Michigan and W. ANDERSON, SimCenter at University of Tennessee at Chattanooga 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2015-1529 AIAA-2015-1530 Oral Presentation AIAA-2015-1531 AIAA-2015-1532 Oral Presentation High-Order Discontinuous Galerkin Application of a Higher-order Benchmark Turbulent Flow Finite-Element Solutions for High-Order Output-Based Adaptive A comparative study of grid Mesh Resolved Turbulent Flow Adaptive Method to RANS Test Simulations with a RANS High- Turbulent Flow over the NACA 0012 Simulations of Turbulent Flow in convergence and accuracy for Simulations of a NACA 0012 Airfoil Cases (Invited) order CPR Formulation (Invited) Airfoil (Invited) Two Dimensions (Invited) structured, unstructured and adaptive (Invited) Y. Hu, C. Wagner, S. Allmaras, M. C. Zhou, Z. Wang, University of Kansas, W. Anderson, J. Newman, L. Wang, M. Ceze, K. Fidkowski, University of grid discretizations in 2D (Invited) M. Brazell, D. Mavriplis, University of Galbraith, D. Darmofal, Massachusetts Lawrence, Lawrence, KS S. Kapadia, University of Tennessee, Michigan, Ann Arbor, Ann Arbor, MI D. Kamenetskiy, The Boeing Company, Wyoming, Laramie, Laramie, WY Institute of Technology, Cambridge, MA Chattanooga, Chattanooga, TN Seattle, WA Thursday, 8 January 2015 322-FD-44 Unsteady Flow III Sun Ballroom 6 Chaired by: Q. WANG, MIT and A. GROSS, New Mexico State University 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2015-1533 AIAA-2015-1534 AIAA-2015-1535 AIAA-2015-1536 AIAA-2015-1537 Development of a Navier-Stokes- Multiple Shooting Shadowing for Afterbody Effects on Axisymmetric An Analysis of the Unsteady Wake Eulerian and Lagrangian Methods Based Numerical method for Basic Sensitivity Analysis of Chaotic Base Flows Behind a Circular Cylinder using for Detecting Vortex Formation and State Perturbation Analysis Systems and Turbulent fluid flows V. Gentile, F. Schrijer, B. van Oudheusden, Lagrangian Coherent Structures Shedding S. Bhaumik, D. Gaitonde, M. Waindim, P. Blonigan, Q. Wang, Massachusetts F. Scarano, Delft University of Technology, M. Rockwood, M. Green, Syracuse Y. Huang, M. Green, Syracuse University, Ohio State University, Columbus, OH Institute of Technology, Cambridge, MA Delft, The Netherlands University, Syracuse, NY Syracuse, NY Thursday, 8 January 2015 323-GEPC-3 NASA Transformational Tools and Technologies (T3) Project Recent Modeling Advances Sun Ballroom C 141 Chaired by: D. WILLIAMS, NASA Langley Research Center and M. ROGERS, NASA Ames Research Center 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs Oral Presentation Oral Presentation Oral Presentation Oral Presentation Oral Presentation Oral Presentation NASA T3 Project and Modeling Test Cases for NASA’s Revolutionary Recent Developments in FUN3D: NASA’s Modelling and Simulation NASA’s Aeroacoustic Tools and Advances in Methods for Solving Vision Computational Aerosciences Entropy Stable DG-FEM Tools for Liquid-Fueled Turbulent Methods for Analysis of Aircraft Large Scale Design Problems J. Heidmann, NASA Glenn Research Technical Challenge (Invited) M. Carpenter, E. Nielsen, NASA Langley Combustion Noise Using Automatic Multidisciplinary Center, Cleveland, OH; D. Williams, NASA C. Rumsey, NASA Langley Research Center, Research Center, Hampton, VA; M. N. Liu, C. Wey, NASA Glenn Research S. Rizzi, L. Lopes, C. Burley, NASA Langley Derivatives with NASA’s OpenMDAO Langley Research Center, Hampton, VA; Hampton, VA; J. DeBonis, NASA Glenn Parsani, Oak Ridge Associated Universities, Center, Cleveland, OH Research Center, Hampton, VA J. Gray, NASA Glenn Research Center, M. Rogers, NASA Ames Research Center, Research Center, Cleveland, OH; M. Malik, Oak Ridge, TN Cleveland, OH Moffett Field, CA NASA Langley Research Center, Hampton, VA Thursday, 8 January 2015 324-GNC-30 Advances in UAS Technologies II Miami 1 Chaired by: F. HOLZAPFEL, Technische Universität München and N. HOVAKIMYAN, University of Illinois at Urbana-Champaign 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2015-1538 AIAA-2015-1539 AIAA-2015-1540 AIAA-2015-1541 Aerodynamic Parameter Open-Loop Quadrotor Flight Herding a Flock of Birds Verified Planar Formation Control Identification and Uncertainty Dynamics Identification in Approaching an Airport Using an Algorithms by Composition of Quantification for Small Unmanned Frequency Domain via Closed-Loop Unmanned Aerial Vehicle Primitives Aircraft Flight Testing S. Gade, University of Illinois, Urbana- L. Bobadilla, Florida International L. Hale, M. Patil, C. Roy, Virginia P. Niermeyer, T. Raffler, F. Holzapfel, Champaign, Urbana, IL; A. Paranjape, University, Miami, FL; T. Johnson, Polytechnic Institute and State University, Technical University of Munich, Munich, McGill University, Montréal, Canada; S. University of Texas, Arlington, Arlington, Blacksburg, VA Germany Chung, University of Illinois, Urbana- TX; A. LaViers, University of Virginia, Champaign, Urbana, IL Charlottesville, Charlottesville, VA Thursday, 8 January 2015 325-GNC-31 Loss of Control Mitigation and Recovery Sun Ballroom 3 Chaired by: F. ALMEIDA, Instituto de Aeronáutica e Espaço and P. SHANKAR, California State Univ 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2015-1542 AIAA-2015-1543 AIAA-2015-1544 AIAA-2015-1545 AIAA-2015-1546 Nonlinear Smooth Trackers with Loss-Of-Control Autonomous Preliminary Evaluation of the Recovery of an Aircraft from the Piloted Simulator Evaluation of Control Rates Constraints for Flight Recovery Regimes using SAFE-Cue Warning Display for Loss Loss of Control Using Open Final Maneuvering Envelope Information Aeronautical Vehicles Loss-Of- Feedback Linearization and High of Control Mitigation Time Dynamic Optimization and for Flight Crew Awareness Control Autonomous Recovery Order Sliding Mode Control with A. Lampton, D. Klyde, D. Lee, P. Schulze, Receding Horizon Control T. Lombaerts, German Aerospace Center J. Dongmo, JetMech.Inc., Parkville, MD Exponential Observers Systems Technology, Inc., Hawthorne, CA; G. Garcia, S. Keshmiri, W. Huang, University of (DLR), Oberpfaffenhofen, Germany; S. J. Dongmo, JetMech.Inc., Parkville, MD B. Cogan, NASA Armstrong Flight Research Kansas, Lawrence, Lawrence, KS Schuet, D. Acosta, J. Kaneshige, NASA Center, Edwards, CA Ames Research Center, Moffett Field, CA; K. Shish, Millennium Engineering and Integration Company, Moffett Field, CA Thursday, 8 January 2015 326-GNC-32 Guidance, Navigation and Control Concepts in Air Traffic Control Systems II Sun Ballroom 4 Chaired by: A. CHAKRAVARTHY, Wichita State University and X. BAI 0930 hrs 1000 hrs AIAA-2015-1547 AIAA-2015-1548 Remote Detection of Turbulence Detecting Convective Induced via ADS-B Turbulence via Total Lightning Sensing J. Krozel, Innovation Laboratory, Inc., J. Krozel, Innovation Laboratory, Inc., Portland, OR; R. Sharman, National Center Portland, OR; W. Deierling, R. Sharman, J. for Atmospheric Research, Boulder, CO Williams, National Center for Atmospheric

142 Research, Boulder, CO Thursday, 8 January 2015 327-GNC-33 Mini/Micro Air Vehicle GNC I Sun Ballroom 4 Chaired by: M. OPPENHEIMER, AFRL/RBCA and S. THEODOULIS, French German Research Institute 0930 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs No Presentations AIAA-2015-1549 AIAA-2015-1550 AIAA-2015-1551 AIAA-2015-1552 Experimental Measurements Effect of Wing Flexibility and Motor Roll Stability Regimes at Low A Geometric Control Approach for of Cycle Averaged Forces for a Dynamics on Split-Cycle Control of Reynolds Numbers the Longitudinal Flight Stability of Flapping Wing Vehicle Flapping Wing Vehicles M. Shields, K. Mohseni, University of Hovering Insects/FWMAVs M. Oppenheimer, Air Force Research S. Nogar, A. Serrani, A. Gogulapati, Florida, Gainesville, Gainesville, FL H. Taha, University of California, Irvine, Laboratory, Wright-Patterson AFB, OH; J. McNamara, Ohio State University, Irvine, CA I. Weintraub, D. Sigthorsson, General Columbus, OH Dynamics Information Technology, Dayton, OH; D. Doman, Air Force Research Laboratory, Wright-Patterson AFB, OH Thursday, 8 January 2015 328-GNC-34 Spacecraft Guidance, Navigation, and Control IV Sun Ballroom 5 Chaired by: D. ALAZARD, Institut Supérieur de l’Aéronautique et de l’Espace 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2015-1553 AIAA-2015-1554 AIAA-2015-1555 AIAA-2015-1556 Distributed Consensus-Based Evolutionary Optimization of Nonlinear Control to Maneuver a The Results of the AOCS Solutions Kalman Filter Estimation and Satellite Formation Topology Over Two-Craft Coulomb Formation at and Technologies study for the Control of Formation Flying a Region of Interest Libration Points Next Generation Gravity Mission Spacecraft: Simulation and D. Hinckley, D. Hitt, M. Eppstein, M. Gomroki, O. Tekinalp, Middle East A. Bacchetta, M. Buonocore, S. Cesare, S. Validation University of Vermont, Burlington, Technical University, Ankara, Turkey Dionisio, M. Parisch, Thales Group, Turin, T. Vu, A. Rahmani, University of Miami, Burlington, VT Italy; E. Canuto, Technical University of Coral Gables, FL Turin, Turin, Italy; et al. Thursday, 8 January 2015 329-GT-5 High Reynolds Number Aerodynamics and Testing (Invited) Sanibel 1 Chaired by: W. KILGORE, NASA Langley Research Center and J. QUEST, ETW GmbH 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2015-1557 AIAA-2015-1558 AIAA-2015-1559 AIAA-2015-1560 Oral Presentation Oral Presentation Influences of Models on the Unsteady Combination of Temperature Overview about the HINVA A320 Tracking the Nacelle Vortex above Facility Improvement and Data Testing of Laminar Wings at High Pressure Characteristics of the NASA Sensitive Paint and Carbon High Lift Flight Reynolds Number Aircraft Wing in the ETW at Real Optimization (FIDO) Efforts at the Reynolds Numbers National Transonic Facility Nanotubes for Transition Detection Test Campaign Mach- and Reynolds Numbers by NASA NTF W. Kühn, Airbus, Bremen, Germany G. Jones, NASA Langley Research Center, C. Klein, U. Henne, German Aerospace R. Rudnik, German Aerospace Center Means of PIV R. Paryz, E. Walker, NASA Langley Hampton, VA; S. Balakrishna, ViGYAN, Center (DLR), Göttingen, Germany (DLR), Braunschweig, Germany R. Konrath, German Aerospace Center Research Center, Hampton, VA Inc., Hampton, VA; J. DeMoss, Analytical (DLR), Göttingen, Germany Services & Materials, Inc., Hampton, VA; S. Goodliff, Jacobs, Hampton, VA Thursday, 8 January 2015 330-GT-6 Unique or Innovative Uses of Existing GTF and Support Systems Miami 3 Chaired by: V. CANACCI, Jacobs Technology 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2015-1561 AIAA-2015-1562 AIAA-2015-1563 AIAA-2015-1564 AIAA-2015-1565 Wind Tunnel Test On The Errors in Off-axis Loading of Development and Experimental An Experimental Four-Component Effects of Low Subsonic Wind Breakthrough Laminar Aircraft Off-the-shelf 6-Component Force Validation of a Dynamic Model for Optical Fibre Balance Tunnel Model Hardware Surface Demonstrator Europe In The Transducers: A Cautionary Tale Wind-Tunnel Heat Exchangers F. Pieterse, University of Johannesburg, Treatments on Drag DNW-LLF S. Gunasekaran, A. Altman, University of P. Sutcliffe, M. Rennie, E. Jumper, Johannesburg, South Africa A. Holup, N. Templon, B. Buerge, Wichita I. Philipsen, J. Postma, K. Artois, DNW, Dayton, Dayton, OH; M. Ol, Air Force Research University of Notre Dame, Notre Dame, IN State University, Wichita, KS Marknesse, The Netherlands Laboratory, Wright-Patterson AFB, OH 143 Thursday, 8 January 2015 331-GTE-7 Gas Turbine Combustion III Emerald 1 Chaired by: J. SMITH, GE Aviation 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2015-1566 AIAA-2015-1567 AIAA-2015-1568 AIAA-2015-1569 AIAA-2015-1570 Experimental Studies and Modeling A Finite-Volume Time-Domain Numerical Investigation of Flame Effects of Physical Modeling on Turbulent Premixed Flame of Acoustic Instabilities in a Gas Solver for Estimation of Combustion Shape Control by Dielectric Barrier Combustion Instability Predictions Ignition and Stabilization Using a Turbine Model Combustor Instabilities Discharge Actuators in a Single-Element Lean Direct Detonation Wave Y. Chen, J. Driscoll, University of Michigan, A. Jemcov, University of Notre Dame, C. Wang, H. Tsao, Yuan Ze University, Injection Gas Turbine Combustor W. Haw, P. King, Air Force Institute of Ann Arbor, Ann Arbor, MI Notre Dame, IN; E. Gonzalez, Combustion Chung, Taiwan C. Huang, R. Gejji, W. Anderson, Purdue Technology, Wright-Patterson AFB, OH; Science & Engineering, Inc., Columbia, MD University, West Lafayette, IN B. Rankin, J. Hoke, Innovative Scientific Solutions, Inc., Dayton, OH; F. Schauer, Air Force Research Laboratory, Wright- Patterson AFB, OH Thursday, 8 January 2015 332-IS-10 Big Data & Analytics in Aerospace Osceola Ballroom 3 Chaired by: A. SRIVASTAVA, NASA Ames Research Center and N. OZA, NASA-Ames 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs Oral Presentation AIAA-2015-1571 Oral Presentation Oral Presentation AIAA-2015-1572 AIAA-2015-1573 Visual Analytics at Boeing Multimodality in a Metroplex Data Mining for Aviation Safety Role of Big Data, Data Analytics, A Neural Network Approach to A Jump-Linear Model based D. Kasik, The Boeing Company, Seattle, WA Environment: A case study in the N. Oza, NASA Ames Research Center, and Networked Air Traffic Airport Management Sensitivity Study for Optimal Air San Francisco Bay Area Moffett Field, CA Management O. Milbredt, E. Grunewald, German Traffic Flow Management under A. Marzuoli, E. Feron, Georgia Institute of P. Kopardekar, NASA Ames Research Aerospace Center (DLR), Braunschweig, Weather Uncertainty Technology, Atlanta, GA; M. Hansen, A. Center, Moffett Field, CA Germany Y. Zhou, J. Xie, Y. Wan, University of Bayen, University of California, Berkeley, North Texas, Denton, TX Berkeley, CA; E. Boidot, Georgia Institute of Technology, Atlanta, GA Thursday, 8 January 2015 333-IS-11 Augmenting Adaptive Algorithms for Aircraft Control II Osceola Ballroom 1 Chaired by: N. NGUYEN, NASA-Ames Research Center 0930 hrs 1000 hrs AIAA-2015-1574 AIAA-2015-1575 Development of an Adaptive- Experimental Results for Adaptive, optimal Multi-Objective Optimal Control of a 2-DOF Optimization Algorithm Helicopter A. Abdollahi, G. Chowdhary, Oklahoma G. Atmeh, K. Subbarao, University of State University, Stillwater, OK Texas, Arlington, Arlington, TX Thursday, 8 January 2015 334-MAT-12 Fatigue & Fracture III Sarasota 1 Chaired by: G. SEIDEL, Virginia Polytechnic Institute and State Universit and S. WANTHAL, The Boeing Company 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2015-1576 AIAA-2015-1577 AIAA-2015-1578 AIAA-2015-1579 AIAA-2015-1580 In Situ Study of Strain Energy A Novel Method for the Cohesive Laws and Progressive A Phantom Paired Element Based A Microstructurally-Informed, Density at Notch Roots Using Manipulation of Damage and In- Damage Analysis of Composite Discrete Crack Network (DCN) Continuum-Level Life Prediction Model Digital Image Correlation Situ Repair of Composite T-Joints Bonded Joints, a Combined Toolkit for Residual Strength for Thermo-Acousto-Mechanically C. Holycross, M. Shen, Ohio State J. Cullinan, M. Wisnom, I. Bond, University Numerical/Experimental Approach Prediction of Laminated Composites Fatigued Ti-6242S and IN617 University, Columbus, OH; O. Scott- of Bristol, Bristol, United Kingdom D. Girolamo, National Institute of E. Fang, X. Cui, T. Zhang, X. Liu, J. Lua, A. Gordon, A. Owji, T. Bouchenot, Emuakpor, T. George, Air Force Research Aerospace, Hampton, VA; C. Davila, F. Global Engineering and Materials, Inc., University of Central Florida, Orlando, Laboratory, Wright-Patterson AFB, OH Leone, S. Lin, NASA Langley Research Princeton, NJ FL; R. Penmetsa, Air Force Research Center, Hampton, VA Laboratory, Wright-Patterson AFB, OH

144 Thursday, 8 January 2015 335-MAT-13 Materials Testing & Characterization II Sarasota 2 Chaired by: D. JAWORSKE, NASA Glenn Research Center and R. NAIK, Pratt & Whitney 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2015-1581 AIAA-2015-1582 AIAA-2015-1583 AIAA-2015-1584 Ablation, Thermal, and Strain Sensor Comparison Revisiting Mixed Mode Fracture in Design of Small-scale Ablative Morphological Properties of SiC for Improving Experimental Laminated Composites Using Edge Testing Apparatus with Sample Fibers Reinforced Ceramic Matrix Measurement of Hysteresis Energy Delamination Strength Testing Position and Velocity Control Composites O. Scott-Emuakpor, Air Force Research S. Sharma, P. Smith, Hexcel Corporation, L. Gutierrez, J. Reyes, S. Scott, A. Sada, J. T. Grantham, G. Tanner, R. Molina, N. Laboratory, Wright-Patterson AFB, OH; B. Dublin, CA Koo, University of Texas, Austin, Austin, TX Duong, J. Koo, University of Texas, Austin, Langley, Universal Technology Corporation, Austin, TX Dayton, OH; C. Holycross, T. George, B. Runyon, Air Force Research Laboratory, Wright-Patterson AFB, OH Thursday, 8 January 2015 336-MDO-8 MDO: AeroStructure Design II Sarasota 3 Chaired by: L. MAININI, Massachusetts Institute of Technology and J. MARTINS, University of Michigan 0930 hrs 1000 hrs 1030 hrs AIAA-2015-1585 AIAA-2015-1586 AIAA-2015-1587 Adaptive Sub-Space Multi-Objective Experimental Open-Source Conceptual Sizing Approximations in Trust-Regions Optimization with Multiple Models for the Hyperloop for Large Scale MDO problems Simultaneous Sampling for Passenger Pod J. Ollar, Altair Engineering, Inc., Flapping Wings J. Chin, J. Gray, NASA Glenn Research Leamington Spa, United Kingdom; V. A. Chaudhuri, R. Haftka, K. Chang, J. Center, Cleveland, OH Toropov, Queen Mary University of Van Hall, P. Ifju, University of Florida, London, London, United Kingdom; R. Gainesville, Gainesville, FL Jones, Altair Engineering, Inc., Leamington Spa, United Kingdom Thursday, 8 January 2015 337-MST-12 Modeling of Vehicle Dynamics II Sun Ballroom 1 Chaired by: D. GINGRAS, Bihrle Applied Research Inc. 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2015-1588 AIAA-2015-1589 AIAA-2015-1590 AIAA-2015-1591 AIAA-2015-1592 Modeling and Control Design for Design and Evaluation of a Semi- Design and Validation of a Modeling of the Longitudinal Dynamic Response Simulation of a New Spacecraft Concept for Empirical Piece-wise Exponential New Algorithm for the Online Dynamics of a Hang Glider Helicopter in Variable Wind Field Measuring Particles and Fields with Atmospheric Density Model for Computation of the Earth’s Y. Ochi, National Defense Academy, T. Liu, Y. Dai, G. Hong, Beihang University, Unprecedented Resolution and CubeSat Applications Magnetic Field Model Yokosuka, Japan Beijing, China Accuracy S. Kedare, S. Ulrich, Carleton University, F. Gulmammadov, Scientific and Y. Mao, D. Auslander, D. Pankow, University Ottawa, Canada Technological Research Council of Turkey of California, Berkeley, Berkeley, CA; K. Vega, (TÜBITAK), Ankara, Turkey Indiana University, Bloomington, IN; F. Mozer, P. Turin, University of California, Berkeley, Berkeley, CA Thursday, 8 January 2015 338-MST-13 Model and Simulation Verification and Validation Sun Ballroom 2 Chaired by: B. JACKSON, NASA-Langley Research Center 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2015-1593 AIAA-2015-1594 AIAA-2015-1595 AIAA-2015-1596 Verification and Validation Full Flight-Envelope Simulation Tuning of Airplane Flight Dynamic Modeling and Simulation of Spanning Models to Code and Piloted Fidelity Assessment Model Using Flight Testing Propeller Propulsion Model Using J. Abraham, MathWorks, Natick, MA of a Business Jet Using a Model A. Kamal, A. Aly, A. Elshabka, Military Wind Tunnel Stitching Architecture Technical College, Cairo, Egypt A. Kamal, A. Aly, A. Elshabka, Military 145 E. Tobias, San Jose State University, Technical College, Cairo, Egypt Moffett Field, CA; M. Tischler, Army Aviation and Missile Research Development and Engineering Center, Moffett Field, CA; T. Berger, University Affiliated Research Center, Moffett Field, CA; S. Hagerott, Cessna Aircraft Company, Wichita, KS Thursday, 8 January 2015 339-NDA-7 Uncertainty Quantification and Management II Osceola Ballroom 5 Chaired by: J. WITTEVEEN, Center for Mathematics and Computer Science (CWI) and V. ROMERO, Sandia National Laboratories 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2015-1597 AIAA-2015-1598 AIAA-2015-1599 AIAA-2015-1600 Towards Characterizing the Uncertainty Quantification of Designing Simulation Platforms For Investigating Model Uncertainty in Variability in the Loading Demands Composite Structures with Defects Uncertainty—an Example from an the Nonlinear Aeroelastic Response of an Unmanned Aerial Vehicle using Multilevel Monte Carlo Aerospace Supplier of Thin Panels S. Sankararaman, Stinger Ghaffarian Simulations A. Forslund, C. Levandowski, R. Söderberg, R. Perez, Universal Technology Technologies, Inc., Moffett Field, CA; K. R. Butler, T. Dodwell, University of Bath, Bath, Chalmers University of Technology, Göteborg, Corporation, Dayton, OH; B. Smarslok, Goebel, NASA Ames Research Center, United Kingdom; R. Haftka, N. Kim, University Sweden; J. Lööf, GKN Aerospace Engine Air Force Research Laboratory, Wright- Moffett Field, CA of Florida, Gainesville, Gainesville, FL; T. Kim, Systems, Trollhättan, Sweden; S. Knuts, Patterson AFB, OH; J. McNamara, Ohio S. Kynaston, University of Bath, Bath, United Massachusetts Institute of Technology, State University, Columbus, OH Kingdom; et al. Cambridge, MA; O. Isaksson, GKN Aerospace Engine Systems, Trollhättan, Sweden; et al. Thursday, 8 January 2015 340-PANEL-7 Aerospace Vehicles Technology Trends Osceola Ballroom B 0930 - 1130 hrs Moderator: Alton Romig, Vice President, Advanced Development Programs, The Skunk Works, Lockheed Martin Aeronautics Panelists: Frank L. Culbertson, Jr. Eric Schrock John Tracy Steve Weiner Executive Vice President and General Manager, Advanced Programs Group Deputy - Technology and Product Innovation Chief Technology Officer and Senior Vice President, Chief Engineer Orbital Sciences Corporation Lockheed Martin Aeronautics Engineering, Operations, and Technology Sikorsky Innovations The Boeing Company

Thursday, 8 January 2015 341-PC-17 Detonations, Explosions, and Supersonic Combustion I Emerald 3 Chaired by: C. BROPHY, Naval Postgraduate School and E. LYNCH, Aerojet Rocketdyne 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2015-1601 AIAA-2015-1602 AIAA-2015-1603 AIAA-2015-1604 Plasma-Assisted PDE and Physics of Heat-Release in Rotating Experimental Characterization of Imaging of OH* Chemiluminescence in Deflagration-to-Detonation Detonation Engines High-Frequency Heat Flux in a an Optically Accessible Nonpremixed Transition D. Schwer, K. Kailasanath, Naval Research Rotating Detonation Engine Rotating Detonation Engine A. Starikovskiy, Princeton University, Laboratory, Washington, DC S. Theuerkauf, F. Schauer, R. Anthony, B. Rankin, Innovative Scientific Solutions, Princeton, NJ Air Force Research Laboratory, Wright- Inc., Dayton, OH; D. Richardson, A. Patterson AFB, OH; J. Hoke, Innovative Caswell, Air Force Research Laboratory, Scientific Solutions, Inc., Dayton, OH Wright-Patterson AFB, OH; A. Naples, J. Hoke, Innovative Scientific Solutions, Inc., Dayton, OH; F. Schauer, Air Force Research

146 Laboratory, Wright-Patterson AFB, OH Thursday, 8 January 2015 342-PC-18 Rocket and Air-Breathing Combustion I Emerald 7 Chaired by: M. COIL, Orbital Technologies Corporation and T. NGUYEN, Aerojet Rocketdyne 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2015-1605 AIAA-2015-1606 AIAA-2015-1607 AIAA-2015-1608 AIAA-2015-1609 AIAA-2015-1610 Study of Liquid Breakup Processes Eigenvalue Analysis for the The Response of Cryogenic H2/ Comparison of a Structured-LES Investigation of Instability Boundary conditions treatment for in Solid Rocket Motors Prediction of Initial Growth Rates O2 Coaxial Jet Flames to Acoustic and an Unstructured-DES Code for Mechanisms in a Laboratory Scale supercritical ﬂows with tabulated R. Amano, Y. Yen, University of Wisconsin, of Thermoacoustic Instability in Disturbances Predicting Combustion Instabilities GH2/GO2 Combustor thermochemistry Milwaukee, Glendale, WI; T. Miller, A. Rocket Motors D. Forliti, Sierra Lobo, Inc., Edwards in a Longitudinal Mode Rocket L. White, A. Dasari, M. Gamba, University G. Ribert, X. Petit, P. Domingo, N. Vallée, Ebnit, M. Lightfoot, V. Sankaran, Air Force M. Schulze, T. Sattelmayer, Technical AFB, CA; A. Badakhshan, ERC, Inc., Combustor of Michigan, Ann Arbor, Ann Arbor, MI National Center for Scientiﬁc Research Research Laboratory, Edwards AFB, CA University of Munich, Munich, Germany Edwards AFB, CA; J. Wegener, University M. Harvazinski, D. Talley, V. Sankaran, (CNRS), Saint-Étienne-du-Rouvray, France of California, Los Angeles, Los Angeles, Air Force Research Laboratory, Edwards CA; I. Leyva, D. Talley, Air Force Research AFB, CA Laboratory, Edwards AFB, CA Thursday, 8 January 2015 343-PDL-7 Plasma & Laser Propulsion Emerald 5 Chaired by: G. WILLIAMS, Ohio Aerospace Institute and R. LITCHFORD, NASA 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2015-1611 AIAA-2015-1612 AIAA-2015-1613 AIAA-2015-1614 AIAA-2015-1615 W-Band Free-Space Dielectric Material Analyses of Ignition Thrust Measurement of Radio Numerical and Experimental A Detailed Comparison of Thermal Property Measurement Techniques for Processes of an Applied-Field Frequency Inductively Coupled Investigation of Nanosecond-Pulsed and Nanosecond Plasma Assisted

Beamed Energy Applications Magnetoplasmadynamic Thruster Plasma Thruster Plasma Activated C2H4/O2/Ar Ignition of Hydrogen-Air Mixtures M. Hilario, University of Southern M. Kong, H. Tang, W. Yang, Y. Xu, B. T. Kato, Y. Iwasaki, T. Fujino, University of Mixtures in a Low Temperature S. Yang, S. Nagaraja, W. Sun, V. Yang, California, Los Angeles, CA; B. Hoff, Wang, Beihang University, Beijing, China Tsukuba, Tsukuba, Japan; I. Funaki, Japan Flow Reactor Georgia Institute of Technology, Atlanta, Air Force Research Laboratory, Kirtland Aerospace Exploration Agency (JAXA), S. Yang, S. Nagaraja, V. Yang, W. Sun, GA AFB, NM; M. Young, Air Force Research Sagamihara, Japan Georgia Institute of Technology, Atlanta, Laboratory, Edwards AFB, CA GA; J. Lefkowitz, Y. Ju, Princeton University, Princeton, NJ Thursday, 8 January 2015 344-PDL-8 Computational Methods Emerald 8 Chaired by: S. ROY, University of Florida 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2015-1616 AIAA-2015-1617 AIAA-2015-1618 AIAA-2015-1619 Discontinuous Galerkin Method Master Equation Modeling of Influence of the Artificial Numerical Investigations of for Solving Magnetohydrodynamic Nanosecond Pulse Discharge in Permittivity on Particle-In-Cell Cathode Surface Streamer Equations Nitrogen in a Pin-to-Pin Geometry Simulation Method Discharges for High-Pressure Large A. das Gupta, S. Roy, University of Florida, Z. Eckert, I. Adamovich, Ohio State M. Li, H. Tang, J. Ren, Beihang University, Gap Arc Breakdown Gainesville, Gainesville, FL University, Columbus, OH Beijing, China A. Sharma, L. Raja, University of Texas, 147 Austin, Austin, TX Thursday, 8 January 2015 345-SATS-2 Small Satellites - Missions Captiva 2 Chaired by: A. SANTANGELO and J. STRAUB, University of North Dakota 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2015-1620 AIAA-2015-1621 Oral Presentation AIAA-2015-1623 AIAA-2015-1624 Flight of FRNCS-P and QuickSAT/ Three-Dimensional Numerical Study Employing Disruptive Business A Review of Impending Small In Search of Standards for the Xen on the SHARC CubeSat Mission of Linear Plug Micronozzles Practices In Space: Closing The Satellite Formation Flying Missions Operation of Small Satellites A. Santangelo, sci_Zone, Rio Rancho, NM J. Pearl, W. Louisos, D. Hitt, University of Business Case For Commercial Remote S. Bandyopadhyay, G. Subramanian, R. Foust, J. Straub, University of North Dakota, Vermont, Burlington, Burlington, VT Earth and Space Weather Sensing D. Morgan, S. Chung, University of Illinois, Grand Forks, Grand Forks, ND Using Micro-Satellite Constellations Urbana-Champaign, Urbana, IL; F. Hadaegh, W. Hosack, 406 Space Systems, Jet Propulsion Laboratory, California Institute of Bozeman, MT Technology, Pasadena, CA Thursday, 8 January 2015 346-SCS-8 Inflatable Space Structures Osceola Ballroom 4 Chaired by: H. FANG and J. HINKLE, ILC Dover 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2015-1625 AIAA-2015-1626 AIAA-2015-1627 AIAA-2015-1628 Creep Burst Testing of a Woven Analysis of Accelerometer Data Functional and Qualification Testing Analysis and Damage Sensitivity Inflatable Module from a Woven Inflatable Creep of the InflateSail Technology of Design Pathfinder for Inflatable M. Selig, G. Valle, G. James, NASA Johnson Burst Test Demonstrator Systems Space Center, Houston, TX; O. Oliveras, G. James, NASA Johnson Space Center, A. Viquerat, M. Schenk, V. Lappas, J. Fulcher, S. Smith, University of Kentucky, Jacobs, Houston, TX; T. Jones, W. Doggett, Houston, TX University of Surrey, Guildford, United Lexington, Lexington, KY; J. Baker, University NASA Langley Research Center, Hampton, VA Kingdom; B. Sanders, CGG Safety and of Kentucky, Paducah, Paducah, KY Systems, Klundert, The Netherlands Thursday, 8 January 2015 347-SD-14 Supersonic/Hypersonic Systems II Tampa 2 Chaired by: N. FALKIEWICZ, MIT Lincoln Laboratory and K. GRIFFIN, Southwest Research Institute 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2015-1629 AIAA-2015-1630 AIAA-2015-1631 AIAA-2015-1632 AIAA-2015-1633 Effects of Strain Hardening Panel Response Prediction Through Fluid-Thermal-Structural Interaction Investigation into Parallel Time Aeroservoelastic Response of A on Fluid-Thermal-Structural Reduced Order Models with Effects in Preliminary Design of Marching of Fluid-Thermal- Typical Lifting Type Reentry Vehicle Interactions Application to Hypersonic Aircraft High Speed Vehicles Structural Interactions Under Closed Loop Control J. LaFontaine, A. Gogulapati, B. Miller, M. Mignolet, Arizona State University, Z. Witeof, Leidos Corporation, Eglin M. LeVett, Z. Liang, B. Miller, J. A. Joshi, P. Mujumdar, Indian Institute of J. McNamara, Ohio State University, Tempe, AZ; A. Culler, Sierra Lobo, Inc., AFB, FL; C. Pasiliao, Air Force Research McNamara, Ohio State University, Technology Bombay, Mumbai, India; G. Columbus, OH Dayton, OH; J. McNamara, Ohio State Laboratory, Eglin AFB, FL Columbus, OH Chary, Vikram Sarabhai Space Centre, University, Columbus, OH; A. Matney, Thiruvananthapuram, India Arizona State University, Tempe, AZ; S. Spottswood, Air Force Research Laboratory, Wright-Patterson AFB, OH Thursday, 8 January 2015 348-SD-15 Active and Passive Damping Systems Tampa 3 Chaired by: S. RAGHAVAN, University of Central Florida and S. LIGUORE, Boeing Engineering Operations & Technology 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2015-1634 AIAA-2015-1635 AIAA-2015-1636 AIAA-2015-1637 AIAA-2015-1638 A Hybrid Magnetostrictive Passive Damping of Fuel Slosh Energy Dissipation in a Riveted Lap Investigation of Analytical Suppression of Aeroelastic Propellant Management Device for using a Suspended Pendulum Joint of Aircraft Structure under Modeling for Structural Damping Instability Due to Freeplay Active Slosh Damping in Spacecraft L. Paul, B. Sivasubramanian, J. Pinto, S. In-plane Tensile and Shear Loading Properties in Riveted Lap Joints Nonlinearity by a Nonlinear Energy B. Sivasubramanian, L. Paul, S. Gangadharan, Embry-Riddle Aeronautical J. Nishimuro, S. Suzuki, Waseda S. Machida, Japan Aerospace Exploration Sink

148 Krishnappa, S. Gangadharan, D. Kim, University, Daytona Beach, FL University, Tokyo, Japan; S. Machida, Agency (JAXA), Tokyo, Japan H. Chen, Zhejiang University, Hangzhou, Embry-Riddle Aeronautical University, T. Okada, Japan Aerospace Exploration China; Y. Lee, New Mexico State Daytona Beach, FL Agency (JAXA), Tokyo, Japan University, Las Cruces, NM Thursday, 8 January 2015 349-SE-1 Systems Engineering I Miami 2 Chaired by: J. EILER, Stellar Solutions, Inc. and D. DRESS, NASA Langley Research Center 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2015-1639 AIAA-2015-1640 AIAA-2015-1641 AIAA-2015-1642 AIAA-2015-1643 Extending Model Based Systems A concept of forecasting origin- Replacing Capabilities within a System- Future Passenger Air Traffic Threat Plane Method for Engineering for Complex Systems destination air passenger demand of-Systems: An Architectural Study on Modelling: Trend Analysis of the Developing Operational Rules of M. French, Rolls-Royce Group plc, between global city pairs using how to Simplify the National Airspace Passenger Air Travel Demand an Autonomous Anti-Air Defense Indianapolis, IN future socio-economic scenarios System Network System on a Warship against I. Terekhov, V. Gollnick, German Aerospace M. Levert, Federal Aviation Administration, R. Ghosh, I. Terekhov, German Aerospace Multiple Attacking Missiles Center (DLR), Hamburg, Germany Washington, DC; T. Ender, Georgia Institute Center (DLR), Hamburg, Germany S. Lee, J. Ahn, Korea Advanced Institute of of Technology, Atlanta, GA Science and Technology, Daejeon, South Korea Thursday, 8 January 2015 350-SOF-1 Software Challenges in Aerospace Workshop I Osceola Ballroom 2 Chaired by: K. FEIGH, Georgia Institute of Technology; M. DAVIES, NASA-Ames; J. MURPHY, NASA Ames Research Center and S. BLANCHETTE, Software Engineering Institute 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2015-1644 AIAA-2015-1645 AIAA-2015-1646 AIAA-2015-1647 AIAA-2015-1648 Slayer of Giants Using Formal Requirements and Seeking Meaningful Measures Message Latency Characterization of a RUMS - Realtime Visualization S. Blanchette, Carnegie Mellon University, Model-Checking for Verification For COTS-Intensive System Distributed Live, Virtual, Constructive and Evaluation of Live, Virtual, Pittsburgh, PA and Validation of an Unmanned Development Simulation Environment Constructive Simulation Data Rotorcraft L. Esker, M. Diep, F. Herman, Fraunhofer, J. Murphy, NASA Ames Research Center, G. Soler, S. Jovic, SAIC, Moffett Field, CA; C. Torens, F. Adolf, German Aerospace College Park, MD Moffett Field, CA; S. Jovic, N. Otto, SAIC, J. Murphy, NASA Ames Research Center, Center (DLR), Braunschweig, Germany Moffett Field, CA Moffett Field, CA Thursday, 8 January 2015 351-SRE-2 ISRU for Mars and Beyond Daytona 2 Chaired by: J. KLEINHENZ, NASA Glenn Research Center 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2015-1649 AIAA-2015-1650 AIAA-2015-1651 AIAA-2015-1652 AIAA-2015-1653 AIAA-2015-1654 Quantification of plume-soil Capability and Technology Integrated Systems Logistics in CIS- In-Space Propulsion, Logistics Feasibility of high speed Solar System Exploration interaction and excavation due to Performance Goals for the Next Step Lunar Space for 8th Space Resource Reduction, and Evaluation of Steam atmospheric flight on Venus Augmented by In-Situ Resource the Mars Science Laboratory Sky in Affordable Human Exploration Utilization Conference Reformer Kinetics: Problems and A. Ingenito, A. Agresta, University of Rome Utilization: Human Mercury and Crane Descent Phase of Space D. McAlister, Air Force Institute of Prospects “La Sapienza’’, Rome, Italy; R. Andriani, Saturn Exploration J. Vizcaino, Qualis Corporation, Huntsville, D. Linne, NASA Glenn Research Center, Technology, Wright-Patterson AFB, OH D. Jaworske, B. Palaszewski, M. Kulis, S. Technical University of Milan, Milan, B. Palaszewski, NASA Glenn Research AL; M. Mehta, NASA Marshall Space Flight Cleveland, OH; G. Sanders, NASA Johnson Gokoglu, NASA Glenn Research Center, Italy; F. Gamma, University of Rome “La Center, Cleveland, OH Center, Huntsville, AL Space Center, Houston, TX; K. Taminger, NASA Cleveland, OH Sapienza’’, Rome, Italy Langley Research Center, Hampton, VA Thursday, 8 January 2015 352-TES-2 Clean and Alternative Fuels Tallahassee 2 Chaired by: N. SYRED, Cardiff University 0930 hrs AIAA-2015-1655 Preliminary Results from a High Pressure Optical gas Turbine Combustor Model with 3D Viewing Capability N. Syred, S. Morris, P. Bowen, A. Valera- Medina, R. Marsh, Cardiff University, 149 Cardiff, United Kingdom Thursday, 8 January 2015 353-TP-8 DSMC and Non-Continuum Flows Sun Ballroom B Chaired by: D. GOLDSTEIN, University of Texas and J. BURT, Universal Technology Corporation 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2015-1656 AIAA-2015-1657 AIAA-2015-1659 AIAA-2015-1660 Coupled Rotational-Vibrational Effect of Injector Position on the Computation of Rarefied Near Continuum Gas Flows Excitation in Shock Waves using Mixing Performance in Micro/ Hypersonic Flows Using a Modified C. Cai, New Mexico State University, Las Trajectory-based Direct Simulation Nanomixers Form of the Conventional Burnett Cruces, NM Monte Carlo M. Darbandi, M. Sabouri, Sharif University Equations M. Grover, P. Valentini, T. of Technology, Tehran, Iran; G. Schneider, W. Zhou, W. Chen, Zhejiang University, Schwartzentruber, University of Minnesota, University of Waterloo, Waterloo, Canada Hangzhou, China; R. Agarwal, Washington Minneapolis, Minneapolis, MN University in St. Louis, St. Louis, MO Thursday, 8 January 2015 354-WE-13 Wind Energy Innovative Concepts Emerald 4 Chaired by: H. HU, Iowa State University and E. LOTH, University of Virginia 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2015-1661 AIAA-2015-1662 AIAA-2015-1663 AIAA-2015-1664 AIAA-2015-1665 Downwind Pre-Aligned Rotor for a Airfoil with morphing trailing edge A Comparative Study on the Experiments on Fairing Design for Numerical Investigation of 13.2 MW Wind Turbine for load reduction in wind turbines Aeromechanic Performances of a Wind Turbine Tower Aerodynamic Performance and E. Loth, University of Virginia, Charlottesville, T. Wolff, J. Seume, Leibniz University, a Twin-Rotor Wind Turbine and a K. O’Connor, E. Loth, University of Loads of a Novel Dual Rotor Wind Charlottesville, VA; B. Ichter, Stanford Hannover, Germany Single-Rotor Wind Turbine Virginia, Charlottesville, Charlottesville, Turbine University, Stanford, CA; A. Steele, Texas H. Hu, Z. Wang, A. Ozbay, W. Tian, A. VA; M. Selig, University of Illinois, Urbana- A. Rosenberg, B. Moghadassian, A. A&M University, College Station, TX; M. Selig, Sharma, Iowa State University, Ames, IA Champaign, Urbana, IL Sharma, H. Hu, Iowa State University, University of Illinois, Urbana-Champaign, Ames, IA Urban, IL; P. Moriarty, National Renewable Energy Laboratory, Golden, CO Thursday, 8 January 2015 355-LUNCH-4 Recognition Luncheon: Celebrating Achievements in Aerospace Design/Structures and Literary Excellence Osceola Ballroom CD 1200 - 1400 hrs

Commercial Spaceﬂight: What Has Changed? Christopher J. Ferguson Director, Crew and Mission Systems, Commercial Crew Program Boeing Space Exploration Thursday, 8 January 2015

150 356-ABPSI-2 Inlets and Nozzles Emerald 2 Chaired by: A. DELOT, ONERA and S. HIRT, NASA Glenn Research Center 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2015-1666 AIAA-2015-1667 AIAA-2015-1668 AIAA-2015-1669 AIAA-2015-1670 AIAA-2015-1671 The Design and Performance Benefits of Boundary Layer Pressure Based Comparison of Intake and Airframe Effect of Geometry on Exit Performance Evaluation of Evaluation of Hypersonic Inlets for Ingestion Propulsion Different Gas Turbine Ground Characterization through Composite Temperature from Serpentine Airframe-Integrated Aerospike Scramjet Applications K. Sabo, M. Drela, Massachusetts Institute Vortex Flows CFD Exhaust Nozzles Propulsion Systems in Off-Design F. Ferguson, M. Dhanasar, T. Lawrence, of Technology, Cambridge, MA J. Barata, P. Manquinho, A. Silva, J. Masud, O. Khan, S. Hassan, Air D. Crowe, C. Martin, Air Force Institute of Flight Conditions North Carolina A&T State University, University of Beira Interior, Covilha, University, Islamabad, Pakistan Technology, Wright-Patterson AFB, OH H. Takahashi, T. Tomita, S. Tomioka, Greensboro, NC; I. Blankson, NASA Glenn Portugal Japan Aerospace Exploration Agency Research Center, Cleveland, OH (JAXA), Kakuda, Japan Thursday, 8 January 2015 357-ACD-5 Propulsion Integration for Aircraft Design Emerald 8 Chaired by: E. DIGIROLAMO, Lockheed Martin Aeronautics 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs AIAA-2015-1672 AIAA-2015-1673 AIAA-2015-1674 AIAA-2015-1675 AIAA-2015-1676 AIAA-2015-1677 AIAA-2015-1678 Integrated Propeller-Wing Design Simplified Aerodynamics Models Flight Path and Wing Optimization Study of Electric Aircraft Recharged Modeling of Electric Motor Driven Multi-Disciplinary Impact of Engine Numerical Research on Exploration for Distributed to Predict the Effects of Upstream of Lithium-Air Battery Powered by Beamed Microwave Power Propellers for Conceptual Aircraft Parameters Upon Transport Aircraft Aerodynamic Efficiency of a VTOL Propulsion Concepts Propellers on Wing Lift Passenger Aircraft Y. Ozawa, N. Tanaka, IHI Corporation, Design Climb Fuel Consumption GFS UAV N. Borer, M. Moore, NASA Langley M. Patterson, M. Daskilewicz, B. German, J. Vegh, J. Alonso, Stanford University, Tomioka, Japan; H. Hakojima, Fuji-Imvac, R. McDonald, California Polytechnic State T. Takahashi, C. Gedeon, Arizona State Y. Zhang, L. Xu, H. Chen, Tsinghua Research Center, Hampton, VA Georgia Institute of Technology, Atlanta, GA Stanford, CA; T. Orra, C. Ilario da Silva, Yokohama, Japan University, San Luis Obispo, CA University, Tempe, AZ University, Beijing, China Embraer, São José dos Campos, Brazil Thursday, 8 January 2015 358-ACD-6 Aircraft Design Methodology Osceola Ballroom 3 Chaired by: C. BIL, RMIT University 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs AIAA-2015-1679 AIAA-2015-1680 AIAA-2015-1681 AIAA-2015-1682 AIAA-2015-1683 Semi-Empirical Prediction of A Practical Method for Uncertainty Alternative Energy Aircraft Range Integrating Subsystem Sizing Uncertainty Quantification for the Aircraft Low-Speed Aerodynamic Analysis in the Aircraft Conceptual Equations and Resulting Aircraft into the More Electric Aircraft Actuation Power Requirements of a Characteristics Design Phase Design Technology Extrapolation Conceptual Design Phase Hybrid Wing Body Configuration with E. Olson, NASA Langley Research Center, S. Van Haver, R. Vos, Delft University of D. Allison, A. Myklebust, Gestalt Technical T. Dendinger, E. Inclan, K. Handschuh, C. Electrically Actuated Flight Control Hampton, VA Technology, Delft, The Netherlands Institute, Blacksburg, VA Ingram, I. Chakraborty, E. Garcia, Georgia Surfaces Institute of Technology, Atlanta, GA; et al. D. Garmendia, I. Chakraborty, D. Mavris, Georgia Institute of Technology, Atlanta, GA Thursday, 8 January 2015 359-AFM-12 MAV, UAV and Aeroservoelastic Vehicles Captiva 1 Chaired by: K. CUNNINGHAM, NASA Langley Research Center 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2015-1684 AIAA-2015-1685 AIAA-2015-1686 AIAA-2015-1687 AIAA-2015-1688 AIAA-2015-1689 The Gust Resistant MAV - Experimental Development of Modal Matching for LPV Model Longitudinal and Directional Comparative Study of Wing’s A Bio-inspired UAV Leg-Foot Aerodynamic Measurements, a Rotorcraft UAV Downwash Reduction of Aeroservoelastic Vehicles Control Modeling for a Small Motion Patterns on Various Types of Mechanism for Landing, Grasping Performance Analysis, and Flight Model for Real-Time Disturbance J. Theis, Hamburg University of Powered Parafoil Aerial Vehicle Insects on Resemblant Flight Stages and Perching Tasks Tests Localization and Avoidance Technology, Hamburg, Germany; B. V. Devalla, O. Prakash, University of F. Neves, J. Barata, P. Manquinho, P. Xie, O. Ma, New Mexico State A. Zyluk, K. Sibilski, Air Force Institute of D. Yeo, E. Shrestha, D. Paley, University Takarics, H. Pfifer, G. Balas, University Petroleum and Energy Studies, Dehradun, University of Beira Interior, Covilha, University, Las Cruces, NM; Z. Zhao, Technology, Warsaw, Poland of Maryland, College Park, College Park, of Minnesota, Minneapolis, Minneapolis, India Portugal Beihang University, Beijing, China; L. MD; E. Atkins, University of Michigan, Ann MN; H. Werner, Hamburg University of Zhang, New Mexico State University, Las 151 Arbor, Ann Arbor, MI Technology, Hamburg, Germany Cruces, NM Thursday, 8 January 2015 360-AFM-13 Seven Axioms of Good Engineering (Invited Session) Captiva 2 1400 - 1700 hrs Chaired by: M. OGBURN, NASA Langley Research Center and P. WILLIAMS-HAYES, NASA Armstrong Flight Research Center This special session will include invited speakers who will review and participate in discussions related to the material presented in a popular case study-based course (“The Seven Axioms of Good Engineering”) that is offered at NASA. Panelists: Anthony Luscher Jeb S. Orr Ralph R. Basilio Matt Kohut Roger Forsgren Ed Hoffman Associate Professor, Department of Senior Member of the Technical Staff Project Manager KNP Communications APPEL Director Chief Knowledge Officer Mechanical and Aerospace Engineering Dynamic Systems and Control Orbiting Carbon Observatory-2 (OCO2) Project NASA Headquarters NASA Headquarters Ohio State University Charles Stark Draper Laboratory, Inc. Jet Propulsion Laboratory Case Study Learning and the Seven A Critical Analysis of the X-15 Flight 3-65 Truly Better the Second Time Around: The Axioms of Good Engineering Accident: Aircraft Systems, Human Factors, Application of OCO Lessons on OCO-2 and Flight Control Thursday, 8 January 2015 361-AMT-6/GT-7 Background-Oriented Schlieren: Recent Advancements and Applications in Ground Test Facilities Sun Ballroom C Chaired by: B. BATHEL, NASA Langley Research Center and M. CLEM, NASA Glenn Research Center 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs Oral Presentation Oral Presentation AIAA-2015-1690 AIAA-2015-1691 Oral Presentation Oral Presentation AIAA-2015-1692 Schlieren and Shadowgraphy Background-Oriented Schlieren Tomographic Background Development of Background- Application of Conebeam Development of 3D Background Background-Oriented Schlieren Developments at NASA Ames Applications in NASA Glenn Oriented Schlieren Applications for Oriented Schlieren for NASA Tomography to Background- Oriented Schlieren Imaging with a for Large-Scale and High-Speed Research Center (Invited) Research Center’s Ground Test Turbomachinery (Invited) Langley Research Center Ground Oriented Schlieren in a Large-Scale Plenoptic Camera (Invited) Aerodynamic Phenomena (Invited) J. Heineck, E. Schairer, NASA Ames Facilities (Invited) U. Hartmann, R. Adamczuk, J. Seume, Test Facilities (Invited) Transonic Wind Tunnel (Invited) B. Thurow, A. Bichal, Auburn University, T. Mizukaki, Tokai University, Hiratsuka, Research Center, Moffett Field, CA; L. M. Clem, M. Woike, NASA Glenn Research Leibniz University, Hannover, Germany B. Bathel, S. Borg, E. Walker, NASA K. Scott, J. Wehrmeyer, Aerospace Testing Auburn, AL Japan; B. Bathel, S. Borg, P. Danehy, NASA Kushner, AeroSpace Computing, Inc., Center, Cleveland, OH Langley Research Center, Hampton, VA; Alliance, Arnold AFB, TN Langley Research Center, Hampton, VA; Mountain View, CA; T. Garbeff, NASA Ames T. Mizukaki, Tokai University, Hiratsuka, S. Murman, NASA Ames Research Center, Research Center, Moffett Field, CA Japan Moffett Field, CA; T. Matsumura, National Institute of Advanced Industrial Science and Technology, Tsukuba, Japan; et al. Thursday, 8 January 2015 362-AMT-7 Spectroscopy and Schlieren Tallahassee 1 Chaired by: A. CUTLER, The George Washington University and T. ROSSMANN, Lafayette College 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2015-1693 AIAA-2015-1694 AIAA-2015-1695 AIAA-2015-1696 AIAA-2015-1697 AIAA-2015-1698 The Number Density of Ground Development of Combined Dual-Pump Two-color Polarization Spectroscopy Pressure Monitoring Using Hybrid Visualization of a Sweeping Jet Institutional Schlieren: A State Atomic Oxygen Measurement Vibrational and Pure-Rotational Technique for Probing Collisionally fs/ps Rotational CARS by Laser Speckle Retro-reflective Production-Level Wind Tunnel Test by High Sensitive Laser Absorption Coherent Anti-Stokes Raman Induced Resonances of Nitric Oxide S. Kearney, Sandia National Laboratories, Background Oriented Schlieren Measurement Spectroscopy using Forbidden Line Scattering (DPVCARS and PRCARS) A. Bhuiyan, A. Satija, S. Naik, R. Lucht, Albuquerque, NM; P. Danehy, NASA L. Kushner, Aerospace Computing, Inc., T. Garbeff, J. Heineck, T. McDevitt, L. 152 OI 630nm Systems and their Application to Purdue University, West Lafayette, IN Langley Research Center, Hampton, VA Mountain View, CA; J. Heineck, B. Storms, Kushner, NASA Ames Research Center, R. Morita, Shizuoka University, Laminar Counter-flow Flames R. Childs, NASA Ames Research Center, Moffett Field, CA Hamamatsu, Japan A. Satija, S. Yuan, R. Lucht, Purdue Moffett Field, CA University, West Lafayette, IN Thursday, 8 January 2015 363-APA-35 Hypersonic Aerodynamics Destin 1 Chaired by: M. CONWAY, The Aerospace Corporation and D.FINLEY, Lockheed Martin Aeronautics 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2015-1699 AIAA-2015-1700 AIAA-2015-1701 AIAA-2015-1702 AIAA-2015-1703 AIAA-2015-1704 Experimental Investigations of Integration of Optimized Leading Numerical Simulation of Radiating Sensitivity Analysis of a HIFiRE-6 Aerodynamic Response Shape Optimization of Aerodynamic Heating induced by Edge Geometries Onto Waverider Re-Entry Flows around Orbital Design Variant Using Minimum- Quantification of Complex Axisymmetric Bodies in Hypersonic Single and Double Side-jet on a Configurations Space Vehicle: Comparison with Resource Statistical Designs Hypersonic Configurations using Flow for Reducing Drag and Heat Blunted Cone P. Rodi, Lockheed Martin Corporation, Observed Data R. Graves, S. Sherer, Air Force Research Variable Fidelity Surrogate Transfer M. Taguchi, K. Mori, Nagoya University, Houston, TX S. Surzhikov, Russian Academy of Laboratory, Wright-Patterson AFB, OH Modeling C. Seager, R. Agarwal, Washington Nagoya, Japan; K. Kitamura, Yokohama Sciences, Moscow, Russia J. Tancred, M. Rumpfkeil, University of University in St. Louis, St. Louis, MO National University, Yokohama, Japan; Y. Dayton, Dayton, OH Nakamura, Chubu University, Kasugai, Japan Thursday, 8 January 2015 364-APA-36 Flow Control Applications & Demonstrations (Active & Passive) III Naples 1 Chaired by: J. FARNSWORTH, University of Colorado Boulder and G. ZHA, University of Miami 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2015-1705 AIAA-2015-1706 AIAA-2015-1707 AIAA-2015-1708 AIAA-2015-1709 AIAA-2015-1710 Numerical and Experimental Wind Topology of a Trailing Vortex Study on the Vortex Wake of an Effect of Piezoelectric Actuated Numerical Simulation of Transonic Flow Characteristics along an Active Tunnel and Flight Testing of Active Flow Field with Steady Circulation Airfoil Equipped with Flexible Winglets on the Tip Vortices Circulation Control Jets Equipped Contour Bump in Flow Control for Modified NACA Control Blowing Trailing Edge Fringe T. Guha, R. Kumar, Florida State M. Forster, R. Steijl, University of a Supersonic Freestream and Its 643-618 Airfoil A. Edstrand, L. Cattafesta, Florida State Z. Yang, Z. He, Wright State University, University, Tallahassee, FL Liverpool, Liverpool, United Kingdom Potential to be Applied on Transonic J. Dianics, D. Ohno, S. Fuggmann, J. Lay, University, Tallahassee, FL Dayton, OH; F. Chen, Shanghai Jiao Tong Aircraft for Drag Reduction: An D. Heim, H. Fasel, University of Arizona, University, Shanghai, China Experimental Study Tucson, Tucson, AZ K. Lo, H. Zare-Behtash, K. Kontis, University of Glasgow, Glasgow, United Kingdom Thursday, 8 January 2015 365-APA-37 Special Session: Simulation of Rotor in Hover - Rotorcraft DG II Naples 2 Chaired by: N. HARIHARAN, CREATE-AV and T. EGOLF, Sikorsky Aircraft Corporation 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2015-1711 AIAA-2015-1712 AIAA-2015-1713 AIAA-2015-1714 AIAA-2015-1715 AIAA-2015-1716 Comparison of CFD Hover Hover Performance Predictions for Evaluation of Rotor Hover High Order Evaluation of S-76 in S-76 Rotor Hover Predictions Using Assessment of Planform Effects on Predictions on the S-76 Rotor the S-76 Main Rotor Blade Performance With Differing Blade Hover Advanced Turbulence Models Rotor Hover Performance J. Abras, Naval Air Systems Command, A. Jimenez Garcia, G. Barakos, University Tip Shapes Using Carefree Hybrid L. Sankar, Georgia Institute of Technology, C. Sheng, J. Wang, Q. Zhao, University of L. Sankar, Georgia Institute of Technology, Patuxent River, MD; N. Hariharan, CREATE of Liverpool, Liverpool, United Kingdom Methodologies Atlanta, GA; N. Hariharan, CREATE AV Toledo, Toledo, OH Atlanta, GA; R. Marpu, CD-adapco, AV Team, Lorton, VA T. Ngaya, K. Jacobson, M. Smith, Georgia Team, Lorton, VA Orlando, FL; N. Hariharan, Naval Air Institute of Technology, Atlanta, GA; D. Warfare Center, Patuxent River, MD; 153 Wachspress, G. Whitehouse, Continuum T. Egolf, Sikorsky Aircraft Corporation, Dynamics, Inc., Ewing, NJ Bridgeport, CT Thursday, 8 January 2015 366-APA-38 Special Session: Aerodynamic Design Optimization of Benchmark Cases II Destin 2 Chaired by: J. MARTINS, University of Michigan and S. LEDOUX, Boeing Engineering Operations & Technology 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2015-1717 AIAA-2015-1718 AIAA-2015-1719 AIAA-2015-1720 AIAA-2015-1721 AIAA-2015-1722 A Study Based on the AIAA Aerodynamic Shape Optimization Aerodynamic Shape Optimization Direct Search Airfoil Optimization Evolutionary Optimization of Drag minimization of an isolated Aerodynamic Design Optimization of the Common Research Model Benchmarks with Error Control and Using Far-Field Drag Decomposition Benchmark Aerodynamic Cases airfoil in transonic inviscid flow by Discussion Group Test Cases Wing-Body-Tail Configuration Automatic Parameterization Results using Physics-based Surrogate means of genetic algorithms S. LeDoux, D. Young, S. Fugal, J. Elliott, S. Chen, Z. Lyu, G. Kenway, J. Martins, G. Anderson, Stanford University, Stanford, M. Gariepy, J. Trepanier, E. Petro, B. Models F. Fusi, G. Quaranta, A. Guardone, D. Kamenetskiy, R. Melvin, The Boeing University of Michigan, Ann Arbor, Ann CA; M. Nemec, M. Aftosmis, NASA Ames Malouin, C. Audet, S. LeDigabel, École E. Iuliano, Italian Aerospace Research Technical University of Milan, Milan, Italy; Company, Seattle, WA; et al. Arbor, MI Research Center, Moffett Field, CA Polytechnique de Montréal, Montréal, Center (CIRA), Capua, Italy P. Congedo, French National Institute for Canada; et al. Research in Computer Science and Control (INRIA), Bordeaux, France Thursday, 8 January 2015 367-AS-7 Smart and Multifunctional Materials Applications Osceola Ballroom 6 Chaired by: R. JHA, Mississippi State University and R. YOUNG, NASA-Langley Research Center 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs AIAA-2015-1723 AIAA-2015-1724 AIAA-2015-1725 AIAA-2015-1726 AIAA-2015-1727 AIAA-2015-1728 AIAA-2015-1729 Solid-State Ornithopter: A Computational Micromechanics Investigation of Aligned Conductive Wavelet Spectral Finite Element Wavelet spectral finite element Smart washers to measure bolt Structural Analysis of a Smart Feasibility Study Analysis of Damage Induced Polymer Nanocomposites for Based User-Defined Element in modeling for wave propagation in loads using magnetostrictive Fin Embedded with Single Crystal R. Bounthisane, E. Gumapas, F. Hauris, Piezoresistivity in Carbon Actuation of Bistable Laminates ABAQUS for Modeling Delamination adhesively bonded composite joints Galfenol Piezoelectric Actuators O. Bilgen, Old Dominion University, Nanotube-Polymer Nanocomposites J. Lee, Massachusetts Institute of Technology, in Composite Beams D. Samaratunga, R. Jha, Mississippi State G. Raghunath, B. Barkley, A. Flatau, I. Roh, S. Shin, Seoul National University, Norfolk, VA Under Cyclic Loading Conditions Cambridge, MA; C. Brampton, C. Bowen, A. Khalili, D. Samaratunga, R. Jha, University, Starkville, MS; G. Srinivasan, University of Maryland, College Park, Seoul, South Korea A. Chaurasia, X. Ren, G. Seidel, Virginia University of Bath, Bath, United Kingdom; B. Mississippi State University, Starkville, MS; Indian Institute of Science, Bangalore, College Park, MD Polytechnic Institute and State University, Wardle, Massachusetts Institute of Technology, G. Srinivasan, Indian Institute of Science, India Blacksburg, VA Cambridge, MA; H. Kim, University of Bath, Bangalore, India Bath, United Kingdom Thursday, 8 January 2015 368-FD-45/PDL-9 DBD Plasma Actuators Sun Ballroom A Chaired by: D. ASHPIS, NASA Glenn Research Center and L. ENLOE 1400 hrs 1430 hrs 1500 hrs 1530 hrs AIAA-2015-1730 AIAA-2015-1731 AIAA-2015-1732 AIAA-2015-1733 Effect of a thin-wire exposed An Out-of-Plane Velocity Examination of a Plasma Actuator Numerical Study of Three-dimensional electrode on plasma structure and Component in Dielectric Barrier Model Applied to DBD Actuators for Effects of Plasma Structure on Flow aerodynamic performance in a Discharge Actuator Flow Small Aircraft Applications Field around DBD Plasma Actuator DBD plasma actuator J. Kiser, K. Breuer, Brown University, J. Laten, R. LeBeau, Saint Louis University, H. Nishida, Tokyo University of Agriculture and R. Mangina, L. Enloe, M. Bliely, R. Providence, RI St. Louis, MO Technology, Koganei, Japan; T. Nonomura,

154 Cook, U.S. Air Force Academy, Colorado T. Abe, Japan Aerospace Exploration Agency Springs, CO (JAXA), Sagamihara, Japan Thursday, 8 January 2015 369-FD-46 Hypersonic Boundary Layer Transition II Sanibel 3 Chaired by: T. JULIANO, University of Notre Dame and T. WADHAMS, CUBRC 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs AIAA-2015-1734 AIAA-2015-1735 AIAA-2015-1736 AIAA-2015-1737 AIAA-2015-1738 Boundary Layer Instabilities Boundary-Layer Transition HIFiRE-1 Boundary-Layer Investigation of Mach 10 Boundary Transition Experiments on Blunt Generated by Freestream Laser Experiments in the Boeing/AFOSR Transition: Ground Test Results and Layer Stability of Sharp Cones Bodies with Distributed Roughness Perturbations Mach 6 Quiet Tunnel Stability Analysis at Angle-of-Attack, Part 1: in Hypersonic Free Flight in Carbon A. Chou, NASA Langley Research Center, G. McKiernan, B. Chynoweth, S. T. Juliano, R. Kimmel, Air Force Research Experiments Dioxide Hampton, VA; S. Schneider, Purdue Schneider, Purdue University, West Laboratory, Wright-Patterson AFB, OH; S. E. Marineau, G. Moraru, D. Lewis, J. M. Wilder, NASA Ames Research Center, University, West Lafayette, IN Lafayette, IN Willems, A. Guelhan, German Aerospace Norris, J. Lafferty, Arnold Engineering Moffett Field, CA; D. Reda, Self, Moffett Center (DLR), Cologne, Germany; R. Development Complex, Silver Spring, Field, CA; D. Prabhu, ERC, Inc., Moffett Wagnild, Sandia National Laboratories, MD; H. Johnson, GoHypersonic, Inc., Field, CA Albuquerque, NM Minneapolis, MN Thursday, 8 January 2015 370-FD-47 Overset/Deforming/Moving Meshes Daytona 2 Chaired by: K. DURAISAMY, Stanford University and D. MAVRIPLIS, University of Wyoming 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs AIAA-2015-1739 AIAA-2015-1740 AIAA-2015-1741 AIAA-2015-1742 AIAA-2015-1743 An Overset Mesh Approach for Adjoint-based Adaptation for Mesh deformation and shock A Simple, Efficient, High-Order High-Order Moving Overlapping 3D Mixed Element High Order the Correction Procedure via capturing techniques for high-order Accurate Sliding-mesh Interface Grid Methodology for Aerospace Discretizations Reconstruction Method on Hybrid simulation of unsteady compressible Approach to FR/CPR Method on Applications M. Brazell, D. Mavriplis, J. Sitaraman, Meshes flows on dynamic meshes Coupled Rotating and Stationary B. Merrill, Y. Peet, Arizona State University of Wyoming, Laramie, Laramie, L. Shi, Z. Wang, University of Kansas, A. Sheshadri, J. Crabill, Stanford Domains University, Tempe, AZ WY Lawrence, Lawrence, KS University, Stanford, CA B. Zhang, C. Liang, George Washington University, Washington, DC Thursday, 8 January 2015 371-FD-48 Turbulent Flow Solutions for NACA 0012 and Other Test Cases from the Turbulence Model Resource Website: Residual and Grid Convergence II (Invited) Sanibel 2 Chaired by: B. DISKIN, National Institute of Aerospace and F. PALACIOS, Stanford University 1400 hrs 1430 hrs 1500 hrs 1530 hrs AIAA-2015-1744 AIAA-2015-1745 AIAA-2015-1746 AIAA-2015-1747 Performance of a Newton-Krylov- RANS simulations on TMR test cases Grid Convergence for Turbulent Improved Convergence and Schur Algorithm for the Numerical and M6 wing with the Onera elsA Flows (Invited) Robustness of USM3D Solutions on Solution of the Steady Reynolds- flow solver (Invited) B. Diskin, National Institute of Aerospace, Mixed Element Grids (Invited) Averaged Navier-Stokes Equations V. Gleize, A. Dumont, J. Mayeur, D. Hampton, VA; J. Thomas, C. Rumsey, M. Pandya, NASA Langley Research Center, (Invited) Destarac, ONERA, Châtillon, France NASA Langley Research Center, Hampton, Hampton, VA; B. Diskin, National Institute of D. Brown, H. Buckley, M. Osusky, D. Zingg, VA; A. Schwoeppe, German Aerospace Aerospace, Hampton, VA; J. Thomas, N. Frink, University of Toronto, Toronto, Canada Center (DLR), Braunschweig, Germany NASA Langley Research Center, Hampton, VA 155 Thursday, 8 January 2015 372-FD-49 Wing Aerodynamics II Daytona 1 Chaired by: K. TAIRA, Florida State University and M. OL, US Air Force Reseach Laboratory 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2015-1748 AIAA-2015-1749 AIAA-2015-1750 AIAA-2015-1751 AIAA-2015-1752 AIAA-2015-1753 A Semi-Empirical Approach to Reduced-Order Two- and Three- The Lift Problem in Flapping Flow around an Oscillating Tandem- Fluid-Structure Interactions for Trends in Early Vortex Formation Modeling Lift Production Dimensional Vortex Modeling of Forward Flight at Low Reynolds Wing Power Generator Flexible and Rigid Tandem-Wings on a Wall-to-wall Plate in Pure P. Mancini, F. Manar, A. Jones, University Unsteady Separated Flows Numbers I. Fenercioglu, B. Zaloglu, Istanbul at Low Reynolds Numbers Plunge of Maryland, College Park, College J. Eldredge, D. Darakananda, University of T. Liu, Western Michigan University, Technical University, Istanbul, Turkey; M. R. Jones, D. Cleaver, I. Gursul, University S. Gunasekaran, A. Altman, University Park, MD California, Los Angeles, Los Angeles, CA Kalamazoo, MI; S. Wang, X. Zhang, Ashraf, J. Young, J. Lai, University of New of Bath, Bath, United Kingdom of Dayton, Dayton, OH; K. Granlund, G. He, Chinese Academy of Sciences, South Wales, Canberra, Australia; M. Air Force Research Laboratory, Wright- Beijing, China Platzer, AeroHydro Research & Technology Patterson AFB, OH Associates, Pebble Beach, CA Thursday, 8 January 2015 373-GNC-35 Novel Algorithms in Aircraft GNC Sun Ballroom 3 Chaired by: R. COWLAGI, Worcester Polytechnic Inst and F. HUGON, Gulfstream Aerospace Corporation 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs AIAA-2015-1754 AIAA-2015-1755 AIAA-2015-1756 AIAA-2015-1757 AIAA-2015-1758 AIAA-2015-1759 AIAA-2015-1760 Research on SINS/CNS Gaussian Adaptive Output Feedback Based A Selective Self-Locking Actuator SHERPA: a safe exploration Flight Control Using Physical Distance Fields Over Grid method Fundamental Control System Particle Filter Integrated Navigation on Closed-Loop Reference Models and Control Allocation Approach for algorithm for Reinforcement Dynamic Inversion for Aircraft Envelope Determination Design Issues for Scramjet-Powered Algorithm for Hypersonic Vehicle for Hypersonic Vehicles Thermal Load Minimization Learning controllers F. Zhang, F. Holzapfel, Technical University R. Helsen, E. Van Kampen, C. de Visser, Q. Hypersonic Vehicles Y. Yu, J. Xu, Z. Xiong, B. Liu, Nanjing D. Wiese, A. Annaswamy, Massachusetts D. Doman, M. Oppenheimer, W. Rone, T. Mannucci, E. Van Kampen, C. de Visser, of Munich, Munich, Germany Chu, Delft University of Technology, Delft, J. Echols, K. Puttannaiah, K. Mondal, University of Aeronautics and Astronautics, Institute of Technology, Cambridge, MA; Air Force Research Laboratory, Wright- Q. Chu, Delft University of Technology, The Netherlands A. Rodriguez, Arizona State University, Nanjing, China J. Muse, M. Bolender, Air Force Research Patterson AFB, OH Delft, The Netherlands Tempe, AZ Laboratory, Wright-Patterson AFB, OH; E. Lavretsky, The Boeing Company, Huntington Beach, CA Thursday, 8 January 2015 374-GNC-36 Robust Control of Uncertain Flight Systems Miami 1 Chaired by: P. LU, Delft University of Technology and J. SPEYER, UCLA 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs AIAA-2015-1761 AIAA-2015-1762 AIAA-2015-1763 AIAA-2015-1764 AIAA-2015-1765 Trajectory Optimization under Robustness and Tuning of Output Feedback Adaptive Control for Controller Synthesis for Periodic, Cyclic Control for Multiple Uncertainty based on Polynomial Incremental Backstepping Uncertain Systems with Unmodeled Linear-Distributed Parameter Satellite Cluster Flight Using Fixed Chaos Expansion Approach Dynamics and Input Uncertainty Systems: A Channel Flow Magnitude Thrust F. Xiong, Beijing Institute of Technology, P. Lu, E. Van Kampen, Q. Chu, Delft R. Chandramohan, Gulfstream Aerospace Application H. Zhang, P. Gurfil, Technion--Israel Beijing, China; Y. Xiong, Bank of America, University of Technology, Delft, The Corporation, Savannah, GA; A. Calise, Georgia S. Kang, J. Speyer, J. Kim, University of Institute of Technology, Haifa, Israel Charlotte, NC; B. Xue, Nvidia Corporation, Netherlands Institute of Technology, Atlanta, GA California, Los Angeles, Los Angeles, CA Santa Clara, CA Thursday, 8 January 2015 375-GNC-37 Mini/Micro Air Vehicle GNC II Sun Ballroom 6 Chaired by: S. CHUNG, University of Illinois at Urbana-Champaign and K. KOCHERSBERGER, Virginia Polytechnic Institute and State University 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs AIAA-2015-1766 AIAA-2015-1767 AIAA-2015-1768 AIAA-2015-1769 AIAA-2015-1770 Fast Actuator Fault Detection and Robust Tracking Control of a Robust Design of Transition Onboard Flow Sensing for Coordinated Standoff Flights for Reconfiguration for Multicopters Quadrotor in the Presence of Flight Control System with Input Downwash Detection and Multiple UAVs via Second-Order M. Frangenberg, J. Stephan, W. Fichter, Uncertainty and Non-vanishing Constraint Avoidance with a Small Quadrotor Sliding Modes University of Stuttgart, Stuttgart, Germany Disturbance R. Hatori, K. Uchiyama, Nihon University, Helicopter T. Yamasaki, National Defense Academy, C. Ton, National Research Council, Funabashi, Japan D. Yeo, N. Sydney, D. Paley, University Yokosuka, Japan; S. Balakrishnan, Missouri Shalimar, FL of Maryland, College Park, College Park, University of Science and Technology, Rolla, MD; D. Sofge, Naval Research Laboratory, MO; H. Takano, I. Yamaguchi, National

156 Washington, DC Defense Academy, Yokosuka, Japan Thursday, 8 January 2015 376-GNC-38 Space Exploration and Transportation GNC Sun Ballroom 4 Chaired by: U. SHANKAR, The Johns Hopkins University Applied Physics Laboratory and T. VAN ZWIETEN, NASA 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs AIAA-2015-1771 AIAA-2015-1772 AIAA-2015-1773 AIAA-2015-1774 AIAA-2015-1775 AIAA-2015-1776 AIAA-2015-1777 Optimal Aerocapture Guidance IMU-DM Integrated Navigation Analysis of Geometric Effects on Variable Memory Recurrent Neural In-Flight Suppression of a Destabilized Launch Vehicle Manual Steering Analysis of Orbit-Attitude Coupling P. Lu, Iowa State University, Ames, IA; and Terminal Reentry Guidance for Tightly-Integrated INS/Vision for Networks For Launch Vehicle F/A-18 Structural Mode Using the with Adaptive Augmenting Control: of Spacecraft Near Small Solar C. Cerimele, M. Tigges, D. Matz, NASA Accurate Guided Reentry Flight Lunar Descent Navigation Attitude Control Space Launch System Adaptive In-Flight Evaluations of Adverse System Bodies Johnson Space Center, Houston, TX S. Matsumoto, Y. Kondoh, T. Imada, Y. Park, H. Jeon, C. Park, Seoul National R. Sclafani, P. Shankar, California State Augmenting Control System Interactions Using a Piloted Aircraft G. Misra, A. Sanyal, New Mexico State Japan Aerospace Exploration Agency University, Seoul, South Korea University, Long Beach, CA J. Wall, NASA Marshall Space Flight Center, C. Hanson, C. Miller, NASA Armstrong University, Las Cruces, NM (JAXA), Tsukuba, Japan; S. Kobayashi, N. Huntsville, AL; C. Miller, C. Hanson, NASA Flight Research Center, Edwards, CA; T. Motoyama, Mitsubishi Group, Tsukuba, Armstrong Flight Research Center, Edwards, Van Zwieten, E. Gilligan, NASA Marshall Japan CA; T. Van Zwieten, J. Orr, E. Gilligan, NASA Space Flight Center, Huntsville, AL; J. Orr, Marshall Space Flight Center, Huntsville, AL Draper Laboratory, Huntsville, AL; J. Wall, Dynamic Concepts, Inc., Huntsville, AL Thursday, 8 January 2015 377-GNC-39 Spacecraft Guidance, Navigation, and Control V Sun Ballroom 5 Chaired by: S. KOWALTSCHEK, European Space Agency 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2015-1778 AIAA-2015-1779 AIAA-2015-1780 AIAA-2015-1781 AIAA-2015-1782 AIAA-2015-1783 Two-input two-output port model Simulation and Analysis of Satellite Spacecraft Adaptive Attitude Solar Pressure Variable Structure Satellite Attitude Control System Attitude Tracking Control of a for mechanical systems Dynamics with Flexible Wire Control with Application to Space Model Reference Adaptive Spacecraft Using Three-Dimensional Reaction Spacecraft by Two Reaction Wheels D. Alazard, University of Toulouse, Antennas and Nutation Damper Station Free-Flyer Robotic Capture Attitude Control in Elliptic Orbits Wheel H. Gui, S. Xu, Beihang University, Beijing, Toulouse, France; J. Perez, C. Cumer, T. Y. Hitachi, T. Kamiya, Y. Kusakawa, NEC J. Shi, S. Ulrich, Carleton University, K. Lee, Kwandong University, Gangneung, H. Watanabe, Nihon University, Funabashi, China Loquen, ONERA, Toulouse, France Corporation, Fuchu, Japan; S. Sakai, A. Ottawa, Canada; A. Allen, MDA, Korea (the Republic of); S. Singh, University Japan; K. Masuda, Toyota Motor Matsuoka, Japan Aerospace Exploration Brampton, Canada of Nevada, Las Vegas, Las Vegas, NV Corporation, Nagoya, Japan; K. Uchiyama, Agency (JAXA), Sagamihara, Japan Nihon University, Funabashi, Japan Thursday, 8 January 2015 378-GT-8 Hypersonic Test Capabilities II (Invited) Sanibel 1 Chaired by: J. LAFFERTY, AEDC and K. BERGER, NASA-Langley Research Center 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2015-1784 Oral Presentation Oral Presentation AIAA-2015-1785 AIAA-2015-1786 AIAA-2015-1787 Hypersonic Test Capabilities Recent Upgrades to the NASA Hypersonic Aero Propulsion Clean Design and Characterization of the Effects of Shock-Tube Cleanliness on Methods for Identifying Key at AEDC’s Aerodynamic and Langley 8-Foot High Temperature Air Testbed (HAPCAT): Development Michigan Hypersonic Expansion Slender-Body Hypersonic Instability Features in Schlieren Images Propulsion Test Unit Tunnel and Activation Status Tube Facility (MHExT) and Transition Studies at High- from Hypersonic Boundary-Layer G. Garrard, Aerospace Testing Alliance, S. Harvin, J. Curro, A. Fuchs, G. Mekkes, E. Tucker, W. Burﬁtt, Arnold Engineering Y. Abul-Huda, M. Gamba, University of Enthalpy Instability Experiments Arnold AFB, TN NASA Langley Research Center, Hampton, VA Development Complex, Arnold AFB, TN Michigan, Ann Arbor, Ann Arbor, MI N. Parziale, Stevens Institute of Technology, N. Shumway, S. Laurence, University of Hoboken, NJ; J. Jewell, Air Force Research Maryland, College Park, College Park, MD Laboratory, Wright-Patterson AFB, OH; I.

157 Leyva, Air Force Research Laboratory, Edwards AFB, CA; J. Shepherd, H. Hornung, California Institute of Technology, Pasadena, CA Thursday, 8 January 2015 379-GT-9 International Symposium on Strain-Gage Balances (Invited) Miami 3 Chaired by: R. RHEW, NASA-Langley Research Center and K. LYNN, NASA Langley Research Center 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2015-1788 AIAA-2015-1789 AIAA-2015-1790 Oral Presentation AIAA-2015-1791 AIAA-2015-1792 Design, Manufacturing, & Flexural Fillet Geometry Optimization Rotating Shaft Balances for CRORs Development of an In-Situ Load On the Application of Analogue Variable Acceleration Force Commissioning of a new NLR Half for Design of Force Transducers used T. Fetet, ONERA, Meudon, France System for Internal WT Balances Signal Integrated Circuits in a Calibration System (VACS) Model Balance for ETW in Aerodynamic Testing Including Prediction Intervals Refurbished Side Wall Balance T. Johnson, Institute for Defense Analyses, M. Wright, European Transonic K. Lynn, NASA Langley Research Center, S. Commo, NASA Langley Research P. Bidgood, Council for Scientific and Alexandria, VA Windtunnel, Cologne, Germany Hampton, VA Center, Hampton, VA Industrial Research, Pretoria, South Africa Thursday, 8 January 2015 380-IS-12 Enhancing Safety using Systems Health Management Osceola Ballroom 1 Chaired by: J. FIGUEROA, NASA Stennis Space Center 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2015-1793 AIAA-2015-1794 AIAA-2015-1795 AIAA-2015-1796 AIAA-2015-1797 AIAA-2015-1798 In-Flight Testing of a Bio-Inspired Application of Model-based Developing a Fault Management Verification of Functional Fault Application of an AIS to the problem An Off-Runway Emergency Approach for Assessment of an UAV Prognostics Framework to Pneumatic Guidebook for NASA’s Deep Space Models and the Use of Resource of through life health management of Landing Aid for a Small Aircraft Outside Bounds of Nominal Design Valves on Cryogenic Testbed Robotic Missions Efficient Verification Tools remotely piloted aircraft Experiencing Loss of Thrust I. Moguel, H. Moncayo, A. Perez Rocha, C. Kulkarni, Stinger Ghaffarian L. Fesq, R. Weitl, Jet Propulsion R. Bis, N&R Engineering, Inc., Cleveland, J. Pelham, I. Fan, I. Jennions, Cranfield P. Di Donato, National Civil Aviation Embry-Riddle Aeronautical University, Technologies, Inc., Moffett Field, CA; Laboratory, California Institute of OH; W. Maul, Vantage Partners, LLC, University, Cranfield, United Kingdom; J. Agency, São José dos Campos, Brazil; E. Daytona Beach, FL; M. Perhinschi, West M. Daigle, NASA Ames Research Center, Technology, Pasadena, CA Brook Park, OH McFeat, BAE Systems, London, United Atkins, University of Michigan, Ann Arbor, Virginia University, Morgantown, WV Moffett Field, CA; G. Gorospe, Stinger Kingdom Ann Arbor, MI Ghaffarian Technologies, Inc., Moffett Field, CA; K. Goebel, NASA Ames Research Center, Moffett Field, CA Thursday, 8 January 2015 381-MDO-9 MDO: General Applications Sarasota 3 Chaired by: S. CHOI and G. KENNEDY, Georgia Institute of Technology 1400 hrs 1430 hrs 1500 hrs 1530 hrs AIAA-2015-1799 AIAA-2015-1800 AIAA-2015-1801 AIAA-2015-1802 Large-scale Multi-material Multi-Objective Aeroacoustic Shape Adjoint - based Aeroacoustic Design Multi-Objective WindFarm Topology Optimization for Additive Optimization by Variable-Fidelity Optimization for Blade Vortex Optimization Simultaneously Manufacturing Models and Response Surface Interaction Noise Optimizing COE and Land Footprint G. Kennedy, Georgia Institute of Surrogates E. Fabiano, D. Mavriplis, J. Sitaraman, of Wind Farms under Different 158 Technology, Atlanta, GA L. Leifsson, S. Koziel, Reykjavik University, University of Wyoming, Laramie, Laramie, WY Land Plot Availability Reykjavik, Iceland; S. Hosder, Missouri W. Tong, Syracuse University, Syracuse, University of Science and Technology, NY; S. Chowdhury, A. Messac, Mississippi Rolla, MO State University, Mississippi State, MS Thursday, 8 January 2015 382-MST-14 Unmanned Aerial Systems Sun Ballroom 1 Chaired by: J. SHIN, The Aerospace Corporation 1400 hrs 1430 hrs 1500 hrs 1530 hrs AIAA-2015-1803 AIAA-2015-1804 AIAA-2015-1806 AIAA-2015-1807 System Identification, HIL and Dynamic Modeling and Analysis of Kinematic Modeling of Bat Wing Effects of Winglets on Small Flight Testing of an Adaptive a Single Tilt-Wing Unmanned Aerial Motion Using Articular Surface Unmanned Aerial Systems Controller on a Small Scale Vehicle Geometry C. Williams, J. Weaver, L. Fritz, A. Unmanned Aircraft J. Jeong, S. Yoon, S. Kim, J. Suk, M. Bender, A. Kurdila, R. Mueller, Virginia Blevins, University of Kansas, Lawrence, P. Kumar, J. Steck, Wichita State Chungnam National University, Daejeon, Polytechnic Institute and State University, Lawrence, KS University, Wichita, KS South Korea Blacksburg, VA Thursday, 8 January 2015 383-MST-15 Special Topics in Modeling and Simulation Sun Ballroom 2 Chaired by: B. JACKSON, NASA-Langley Research Center 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs AIAA-2015-1808 AIAA-2015-1809 AIAA-2015-1810 AIAA-2015-1811 AIAA-2015-1812 Requirements and Design A Symplectic Technique for Model Further Development of Verification Design Data Management in Design Variant Management in Challenges in Rotorcraft Flight Reduction of Wave Equations Check-cases for Six-Degree-of- Model-Based Design Model-Based Design Simulations for Research L. Peng, K. Mohseni, University of Florida, Freedom Flight Vehicle Simulations S. Mahapatra, P. Gotika, MathWorks, S. Mahapatra, P. Gotika, MathWorks, Applications Gainesville, Gainesville, FL B. Jackson, M. Madden, NASA Langley Natick, MA Natick, MA F. Viertler, M. Hajek, Technical University Research Center, Hampton, VA; R. Shelton, of Munich, Munich, Germany NASA Johnson Space Center, Houston, TX; M. Castro, D. Noble, NASA Armstrong Flight Research Center, Edwards, CA; C. Zimmerman, NASA Marshall Space Flight Center, Huntsville, AL Thursday, 8 January 2015 384-NDA-8 Non-Deterministic Methods Osceola Ballroom 5 Chaired by: C. ROY, Virginia Tech and W. YAMAZAKI, Nagaoka University of Technology 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs AIAA-2015-1813 AIAA-2015-1814 AIAA-2015-1815 AIAA-2015-1816 AIAA-2015-1817 AIAA-2015-1818 AIAA-2015-1819 Model and Data Uncertainty Effects Hypervolume-based Multi-Objective Aerodynamic Uncertainty Sequential Reliability Estimation Multi-Source Surrogate Modeling Sensitivity Analysis Methods for Uncertainty Quantification of State on Reliability Estimation Expected Improvement for Three- Quantification of Supersonic Biplane Correction (SREC) with Univariate with Bayesian Hierarchical Systems with Epistemic Uncertainties Boundaries in Thin Beam Buckling S. Nannapaneni, S. Mahadevan, Objective Functions Airfoil via Polynomial Chaos Approach Revolving Integration (URI) Regression L. Hale, M. Patil, C. Roy, Virginia Polytechnic Experiments Vanderbilt University, Nashville, TN J. Valenzuela-del Río, D. Mavris, Georgia Y. Suga, W. Yamazaki, Nagaoka University H. Bae, Wright State University, Dayton, S. Ghosh, R. Jacobs, D. Mavris, Georgia Institute and State University, Blacksburg, VA G. Bartram, R. Perez, R. Wiebe, B.

159 Institute of Technology, Atlanta, GA of Technology, Nagaoka, Japan OH Institute of Technology, Atlanta, GA Smarslok, Air Force Research Laboratory, Wright-Patterson AFB, OH Thursday, 8 January 2015 385-OPS-1 Space Operations Emerald 1 Chaired by: L. BRYANT, Jet Propulsion Laboratory 1400 hrs 1430 hrs AIAA-2015-1820 AIAA-2015-1822 A Commercial Transportation System Compact 4D Envelopes For Integrated For Robotic Lunar Exploration Air-and-Space Trafﬁc Management M. Tucker, D. Dolan, Moon Base Builders, T. Colvin, J. Alonso, Stanford University, Inc., Portland, OR Stanford, CA Thursday, 8 January 2015 386-PANEL-8 NASA Research Plans for Assured Autonomy for Aviation Transformation Osceola Ballroom B 1400 - 1600 hrs Moderator: Sanjay Garg, Chief, Intelligent Control and Autonomy Branch, NASA Glenn Research Center Panelists: John Cavolowsky Jay Dryer Robert Pearce Doug Rohn Ed Waggoner Program Director, Airspace Operations and Safety Program Program Director, Advanced Air Vehicles Program Director - Strategy, Architecture and Analysis Program Director, Transformative Aeronautics Concepts Program Program Director, Integrated Aviation Systems Program Aeronautics Research Mission Directorate Aeronautics Research Mission Directorate Aeronautics Research Mission Directorate Aeronautics Research Mission Directorate Aeronautics Research Mission Directorate NASA NASA NASA NASA NASA Thursday, 8 January 2015 387-PC-19 Detonations, Explosions, and Supersonic Combustion II Emerald 3 Chaired by: J. AUSTIN, University of Illinois at Urbana-Champaign and E. BARBOUR, The Aerospace Corpation 1400 hrs 1430 hrs 1500 hrs AIAA-2015-1823 Oral Presentation AIAA-2015-1824 Development of a High Fidelity Three-dimensional behavior in Numerical Investigation of Shock- RDE Simulation Capability oscillation mechanism of shock- Induced Combustion with Unsteady P. Cocks, A. Holley, C. Greene, M. Haas, induced combustion around a blunt Oscillation around Hypervelocity United Technologies Corporation, East projectile Conical Projectile Hartford, CT Y. Sakuragi, A. Matsuo, Keio University, K. Maeda, A. Matsuo, Keio university, Yokohama, Japan Yokohama, Japan Thursday, 8 January 2015 388-PC-20 Rocket and Air-Breathing Combustion II Emerald 7 Chaired by: T. OMBRELLO, Air Force Research Laboratory 1400 hrs 1430 hrs 1500 hrs AIAA-2015-1825 AIAA-2015-1826 AIAA-2015-1827 Effects of Injector Geometry on Co- Prediction of Combustion Instability A Three-Dimensional Analysis of Flowing Planar Jet Mixings under with Detailed Chemical Kinetics Swirl Injector Flow Dynamics at Supercritical Pressures S. Sardeshmukh, S. Heister, W. Anderson, Supercritical Conditions D. Muto, N. Tsuboi, Kyushu Institute Purdue University, West Lafayette, IN X. Wang, Georgia Institute of Technology, of Technology, Kitakyushu, Japan; H. Atlanta, GA; H. Huo, General Electric Company, Terashima, University of Tokyo, Bunkyo, Niskayuna, NY; Y. Wang, L. Zhang, V. Yang, Japan Georgia Institute of Technology, Atlanta, GA

160 Thursday, 8 January 2015 389-PDL-11 Plasma & Laser Physics II Emerald 4 Chaired by: H. LOWRY, Aerospace Testing Alliance (ATA) 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs AIAA-2015-1828 AIAA-2015-1829 AIAA-2015-1830 AIAA-2015-1831 AIAA-2015-1832 Laser Induced Fluorescence Thomson Scattering Measurements Measurement of the Vibrational Laser Ignition of Methane-Air Application of the Modified Drift- Measurements of Xenon Ion of Electron Density and Electron Distribution Function of Chemically Mixtures with a Rapid Compression Diffusion Theory to Study of the Velocity Distributions near Ceramic Temperature in a Nanosecond Pulse Produced Carbon Monoxide for the Machine Two-Dimensional Structure of the Surfaces Surface Discharge Development of a Chemical Carbon C. Dumitrache, M. Baumgardner, A. Penning Discharge S. Walsh, A. Yalin, Colorado State A. Roettgen, I. Shkurenkov, W. Lempert, Monoxide Laser Marchese, A. Yalin, Colorado State S. Surzhikov, Russian Academy of University, Fort Collins, CO I. Adamovich, Ohio State University, K. Frederickson, J. Rich, W. Lempert, University, Fort Collins, CO Sciences, Moscow, Russia Columbus, OH I. Adamovich, Ohio State University, Columbus, OH Thursday, 8 January 2015 390-SATS-3 Small Satellites - Fusion Naples 3 Chaired by: J. STRAUB, University of North Dakota 1400 hrs 1430 hrs 1500 hrs 1530 hrs AIAA-2015-1833 AIAA-2015-1834 AIAA-2015-1835 Small Satellites - Fusion Aerodynamics analyse and attitude Feasibility of Small Unmanned OpenOrbiter Mechanical Design: a This panel will provide a forum to discuss all aspects of small spacecraft development, missions and operations. It will commence with brief introductions of control design of ZJUCube for Spacecraft Launches via Low New Approach to the Design of a and presentations by the panelists, followed by several moderator questions and the opportunity for audience members to ask their own questions. QB50 project Acceleration Railguns Comprising 1-U CubeSat Moderator: Jeremy Straub - University of North Dakota T. Meng, D. Hu, B. Yang, Z. Jin, Zhejiang Helical Tracks B. Kading, University of North Dakota, Panelists: University, Hangzhou, China A. Hassan, University of Virginia, Grand Forks, Grand Forks, ND Charlottesville, Charlottesville, VA Jake Szatkowski John W. Conklin Andrew Santangelo Scott Palo United Launch Alliance University of Florida sci_Zone, Inc. University of Colorado Thursday, 8 January 2015 391-SCS-9 Test and Qualification of Spacecraft Structures Osceola Ballroom 4 Chaired by: G. DAVIS, Jet Propulsion Laboratory and S. PELLEGRINO, California Institute of Technology 1400 hrs 1430 hrs 1500 hrs AIAA-2015-1836 AIAA-2015-1837 AIAA-2015-1838 MOIRE Primary Diffractive Optical The Design and Test of the Testing the Deployment Element Structure Deployment GOSSAMER-1 Boom Deployment Repeatability of a Precision Testing Mechanisms Engineering Model Deployable Boom Prototype for the D. Waller, L. Campbell, J. Domber, D. M. Straubel, German Aerospace Center Proposed SWOT KaRIn Instrument Putnam, R. Thompson, Ball Aerospace & (DLR), Braunschweig, Germany; P. G. Agnes, J. Waldman, L. Peterson, Technologies Corporation, Boulder, CO Seefeldt, P. Spietz, German Aerospace R. Hughes, Jet Propulsion Laboratory, Center (DLR), Bremen, Germany; C. California Institute of Technology, Huehne, German Aerospace Center (DLR), Pasadena, CA Braunschweig, Germany Thursday, 8 January 2015 392-SD-16 Special Session: Adaptive Aeroelastic Wing Shaping Control II Sun Ballroom D Chaired by: N. NGUYEN, NASA-Ames Research Center and J. URNES, Boeing Engineering Operations & Technology 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2015-1839 AIAA-2015-1840 AIAA-2015-1841 AIAA-2015-1842 AIAA-2015-1843 AIAA-2015-1844 Aerodynamic Load Analysis of Aeroelasticity of Axially Loaded Comparison of Unsteady Active Control for Elastic Wing A Multi-Objective Flight Control LMI-based Multiobjective a Variable Camber Continuous Aerodynamic Structures for Truss- Aerodynamics Approximations for Structure Dynamic Modes Approach for Performance Optimization and Control of Trailing Edge Flap System on a Braced Wing Aircraft Time-Domain Representation of J. Urnes, J. Dykman, H. Truong, The Adaptive Aeroelastic Wing Flexible Aircraft Using VCCTEF Flexible Wing Aircraft N. Nguyen, NASA Ames Research Center, Frequency-Independent Aeroelastic Boeing Company, St. Louis, MO N. Nguyen, NASA Ames Research Center, S. Swei, NASA Ames Research Center, E. Ting, T. Dao, Stinger Ghaffarian Moffett Field, CA; E. Ting, Stinger State-Space Models Moffett Field, CA; E. Tal, Moffett Field, CA; G. Zhu, Michigan State 161 Technologies, Inc., Moffett Field, CA; N. Ghaffarian Technologies, Inc., Moffett E. Tal, Delft University of Technology, Delft, The University, East Lansing, MI; N. Nguyen, Nguyen, NASA Ames Research Center, Field, CA Netherlands; N. Nguyen, NASA Ames Research NASA Ames Research Center, Moffett Moffett Field, CA Center, Moffett Field, CA; E. Ting, Stinger Field, CA Ghaffarian Technologies, Inc., Moffett Field, CA Thursday, 8 January 2015 393-SD-17 Gust and Turbulence Loads Tampa 1 Chaired by: P. TAYLOR, Gulfstream Aerospace Corporation and H. KIM, Boeing Defense, Space & Security 1400 hrs 1430 hrs 1500 hrs 1530 hrs AIAA-2015-1845 AIAA-2015-1846 AIAA-2015-1847 AIAA-2015-1849 Flight Loads and Atmospheric Nonlinear Folding Wing-Tips for Efficient Prediction and Uncertainty Dynamic Response of Elastic Turbulence Analysis From a Fleet of Gust Loads Alleviation Propagation of Correlated Loads Aircrafts with Consideration of ASM/Lead Aircraft V. Hodigere Siddaramaiah, D. Calderon, I. Tartaruga, P. Sartor, J. Cooper, University Two-dimensional Discrete Gust A. Menon, L. Kliment, K. Rokhsaz, Wichita J. Cooper, University of Bristol, Bristol, of Bristol, Bristol, United Kingdom; S. Excitation State University, Wichita, KS; J. Nelson, B. United Kingdom; T. Wilson, Airbus, Bristol, Coggon, Airbus, Bristol, United Kingdom; Y. Cheng, Beihang University, Beijing, Terning, U.S. Forest Service, Boise, ID United Kingdom Y. Lemmens, Siemens, Leuven, Belgium China Thursday, 8 January 2015 394-SD-18 Active Aeroelastic Control Tampa 2 Chaired by: I. CHOPRA, University of Maryland and A. PALAZOTTO, AFIT 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2015-1850 AIAA-2015-1851 AIAA-2015-1852 AIAA-2015-1853 AIAA-2015-1854 AIAA-2015-1855 Variable Stiffness Technique for Aeroelastic System Control by a Experimental investigation of an Design Improvements of Smart Active Control on Helicopter Blades A Modified Receptance Method Turbomachinery using Shape Multiple Spoiler Actuation and MRAC autonomous flap for load alleviation Active Trailing-edge Flap for with a L-Shaped Gurney Flap for Active Control of a Nonlinear Memory Alloys Scheme L. Bernhammer, S. Navalkar, J. Sodja, R. De Rotating Test V. Motta, G. Quaranta, Technical University Aeroelastic System R. Wischt, N. Garafolo, University of M. Cassaro, M. Battipede, Technical University Breuker, Delft University of Technology, Delft, J. Kang, W. Eun, J. Lim, U. Visconti, S. of Milan, Milan, Italy C. Zhen, D. Li, J. Xiang, Beihang Akron, Akron, OH of Turin, Turin, Italy; P. Marzocca, G. Ahmadi, The Netherlands; M. Karpel, Technion--Israel Shin, Seoul National University, Seoul, University, Beijing, China Clarkson University, Potsdam, NY Institute of Technology, Haifa, Israel South Korea Thursday, 8 January 2015 395-SD-19 Test and Evaluation and System Identification Tampa 3 Chaired by: B. WILLIS, Boeing Defense, Space & Security and A. GREWAL, National Research Council Canada 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2015-1856 AIAA-2015-1857 AIAA-2015-1858 AIAA-2015-1859 AIAA-2015-1860 AIAA-2015-1861 Experimental Evaluation of Wind Design and Testing of an Active Preparatory Analyses and Correlation and Updating of an Design and Analysis of a Wind Fin-actuator System Modeling Turbine Rotor Tower Structural Aeroelastic Test Bench (AATB) Tests of W-WING Whirl Flutter Unmanned Aerial Vehicle Finite Tunnel Test Model System for and Experimental Validating for Dynamic Interaction for Unsteady Aerodynamic and Demonstrator Element Model Rolling Maneuver Load Alleviation Aeroelastic Research T. Arsenault, P. Marzocca, Clarkson University, Aeroelastic Experiments J. Cecrdle, J. Malecek, O. Vich, P. Malinek, S. Mezzapesa, M. Arras, G. Coppotelli, of Flying Wings R. Zhang, Z. Wu, C. Yang, Beihang Potsdam, NY; G. Coppotelli, University of J. Ertveldt, J. Schoukens, R. Pintelon, S. Aeronautical Research and Test Institute University of Rome “La Sapienza”, Rome, H. Yin, Z. Wu, C. Yang, Beihang University, Beijing, China Rome, Rome, Italy; A. Achuthan, Clarkson Vanlanduit, B. De Pauw, A. Rezayat, Vrije (VZLU), Prague, Czech Republic Italy; J. Miller, D. Valyou, P. Marzocca, University, Beijing, China University, Potsdam, NY; C. Grappasonni, Universiteit Brussel, Brussels, Belgium Clarkson University, Potsdam, NY University of Brussels, Brussels, Belgium Thursday, 8 January 2015 396-SE-2 Systems Engineering II Miami 2 Chaired by: M. BAILEY, Defense Acquisition University and D. DRESS, NASA Langley Research Center 1400 hrs 1430 hrs 1500 hrs 1530 hrs AIAA-2015-1862 AIAA-2015-1863 AIAA-2015-1864 AIAA-2015-1865 Adapting the Systems Engineering Decision Analysis Applied to Small Seeking an Open Framework for Report on the Science of Systems Paradigm to Revitalize Program Satellite Risk Management Systems Engineering in Aeronautics Engineering Workshop Control/Program Integration K. Gamble, E. Lightsey, University of and Astronautics P. Collopy, University of Alabama, Processes into USAF Complex Texas, Austin, Austin, TX V. Johnson, R. Voros, Textron Aviation, Huntsville, Huntsville, AL Systems Acquisition Programs Wichita, KS R. Flores, Embry-Riddle Aeronautical 162 University, Daytona Beach, FL Thursday, 8 January 2015 397-SOF-2 Software Challenges in Aerospace Workshop II Osceola Ballroom 2 Chaired by: S. BLANCHETTE, Software Engineering Institute; M. DAVIES, NASA-Ames; K. FEIGH, Georgia Institute of Technology and J. MURPHY, NASA Ames Research Center 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs AIAA-2015-1866 AIAA-2015-1867 AIAA-2015-1868 AIAA-2015-1869 AIAA-2015-1870 Verification of Real-Time Systems Dependability of Software of Trusting Outsourced Components In Maintenance Phase Considerations Wrap-Up Discussion using Statistical Model Checking Unknown Pedigree Flight Critical Systems for Onboard Flight Software S. Blanchette, Carnegie Mellon University, J. Hansen, L. Wrage, Carnegie Mellon S. Cook, MITRE Corporation, McLean, VA; F. Howar, T. Kahsai, NASA Ames Research Development Pittsburgh, PA; J. Murphy, M. Davies, University, Pittsburgh, PA A. Buttner, E. Lester, MITRE Corporation, Center, Moffett Field, CA; A. Gurfinkel, K. Gundy-Burlet, NASA Ames Research NASA Ames Research Center, Moffett Bedford, MA Carnegie Mellon University, Pittsburgh, PA; Center, Moffett Field, CA Field, CA C. Tinelli, University of Iowa, Iowa City, Iowa City, IA Thursday, 8 January 2015 398-STR-17 Design, Test and Analysis II Sarasota 1 Chaired by: G. MABSON, Boeing Engineering Operations & Technology and B. BEDNARCYK, NASA Glenn Research Center 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs AIAA-2015-1871 AIAA-2015-1872 AIAA-2015-1873 AIAA-2015-1874 AIAA-2015-1875 Development of the PRSEUS Multi- On the Study of PRSEUS - Structural Preliminary Weight Savings Damage Tolerant Novel Laminated Peridynamic Modeling of Defects in Bay Pressure Box for a Hybrid Integrity and Wing Design for Estimate for a Commercial Structures Composites Wing Body Vehicle General Aviation Aircraft Transport Wing Using Rod-stiffened M. Falugi, Air Force Research Laboratory, Y. Hu, E. Madenci, University of Arizona, D. Jegley, NASA Langley Research Center, S. Behl, R. Joshi, T. Surti, K. Ali, D. Kim, Stitched Composite Technology Wright-Patterson AFB, OH Tucson, Tucson, AZ; N. Phan, Naval Hampton, VA; A. Velicki, The Boeing A. Tamijani, Embry-Riddle Aeronautical A. Lovejoy, NASA Langley Research Center, Surface Warfare Center, Patuxent, MD Company, Huntington Beach, CA University, Daytona Beach, FL; et al. Hampton, VA Thursday, 8 January 2015 399-STR-18 Special Session: USAF Benchmarking of Composite Damage Prediction Methods Tallahassee 3 Chaired by: S. CLAY, Air Force Reseach Laboratory and S. ENGELSTAD, Lockheed Martin Aeronautics 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2015-1876 AIAA-2015-1877 AIAA-2015-1878 AIAA-2015-1879 AIAA-2015-1880 AIAA-2015-1881 Assessment of Composite Damage Assessment of Reduced Order Static Validation of Composite Application of Reduced Order Tensile and Compression Strength Multiscale Static Analysis of Notched Growth Tools for Aircraft Structure Homogenization for Damage Open Hole Analysis Technique Multiscale Homogenization to Prediction in Laminated Composites and Unnotched Laminates Using the - Part I Tolerant Design Principles (DTDP) for Standard and nonstandard ‘Assess and Quantify the Benefits by Using Discrete Damage Generalized Method of Cells S. Engelstad, J. Action, Lockheed Martin of Advanced Composite Aircraft Laminate -Part 1 of Applying Damage Tolerant Modeling L. Hansen, A. Waas, B. Stier, University Corporation, Marietta, GA; S. Clay, R. Structures F. Abdi, C. Godines, AlphaSTAR Corporation, Design Principles to Advanced E. Iarve, K. Hoos, M. Braginsky, E. of Michigan, Ann Arbor, Ann Arbor, MI; P. Holzwarth, Air Force Research Laboratory, A. Shojaei, Multiscale Design System, Long Beach, CA; L. Minnetyan, Clarkson Composite Aircraft Structures’ Zhou, University of Dayton, Dayton, Naghipour, S. Arnold, B. Bednarcyk, NASA Wright-Patterson AFB, OH; R. Dalgarno, D. LLC, New York, NY; J. Fish, Columbia University, Potsdam, NY M. Bogdanor, R. Crouch, C. Oskay, OH; D. Mollenhauer, Air Force Research Glenn Research Center, Cleveland, OH; et al. Robbins, AutoDesk, Inc., Laramie, WY University, New York, NY Vanderbilt University, Nashville, TN Laboratory, Wright-Patterson AFB, OH Thursday, 8 January 2015 400-STR-19 Special Session: Structural Joints & Repair I Sarasota 2 Chaired by: S. TERMAATH, University of Tennessee and D. NORWOOD, Lockheed Martin Aeronautics 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs AIAA-2015-1882 AIAA-2015-1883 AIAA-2015-1884 AIAA-2015-1885 AIAA-2015-1886 Flaw and Damage Tolerance of Adhesively Bonded Joint Modeling Thermo-mechanical Stresses in Modeling of Geometrically Graded A Variational Approach for Stress Redundant Adhesively Bonded Approaches using Linear Finite Single-Lap Composite Adhesive Multi-material Single-Lap Joints Analysis of Single-lap bonded Joints for Sandwich Structures Element Analysis Joints A. de Tejada Alvarez, S. Kumar, Masdar Joints under Mechanical and E. Lundgren, D. Patel, V. Goyal, C. Phan, The A. Lyford, T. Stoumbos, Orbital Sciences S. Kumar, Masdar Institute of Science Institute of Science and Technology, Abu Thermal Loads Aerospace Corporation, El Segundo, CA Corporation, Dulles, VA; R. Kapania, and Technology, Abu Dhabi, United Arab Dhabi, United Arab Emirates S. Kumar, S. Tampi, G. Pal, Masdar Virginia Polytechnic Institute and State Emirates Institute of Science and Technology, Abu 163 University, Blacksburg, VA Dhabi, United Arab Emirates Thursday, 8 January 2015 401-TES-3 Energy Efficiency and Waste Reduction Tallahassee 2 Chaired by: A. CHOUDHURI, University of Texas at El Paso 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs AIAA-2015-1887 AIAA-2015-1888 AIAA-2015-1889 AIAA-2015-1890 AIAA-2015-1891 Role of Benzene on Thermal Stage Analysis of Lift Force, Drag Force, Thermal Management in Energy Use of Algebraic-Stress Model Mathematical Modeling of Air Flow Performance in a Claus Process Side Force, Pitching Moment, Efficient Air Conditioned Buildings for determination of near-wall and Comfort in Places of Worship S. Ibrahim, University of Maryland, College Yawing Moment, and Rolling A. Fahim, Housing and Building National Reynolds-Stresses in turbulent flow E. Khalil, Cairo University, Cairo, Egypt Park, College Park, MD; A. Al Shoaibi, Moment Research Center, Cairo, Egypt; E. Khalil, over a flat plate Petroleum Institute, Abu Dhabi, United Arab R. Amano, Y. Yen, B. Sinkovec, University Cairo University, Cairo, Egypt R. Amano, S. Beyhaghi, University of Emirates; A. Gupta, University of Maryland, of Wisconsin, Milwaukee, Glendale, WI Wisconsin, Milwaukee, Glendale, WI College Park, College Park, MD Thursday, 8 January 2015 402-TP-9 NASA Entry Systems Modeling Project Sun Ballroom B Chaired by: M. WRIGHT, NASA Ames Research Center 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2015-1892 AIAA-2015-1893 AIAA-2015-1894 AIAA-2015-1895 AIAA-2015-1896 AIAA-2015-1897 An Overview of Technology Development of the US3D Code Radiative Heating for MSL Entry: Probabilistic Design Demonstration Electron-Impact Excitation Cross Measurements and Analysis of Investments in the NASA Entry for Advanced Compressible and Verification of Simulations from of a Flexible Thermal Protection Sections for Modeling Non- Mars Entry, Decent, and Landing Systems Modeling Project Reacting Flow Simulations Ground Test to Flight Data System for a Hypersonic Inflatable Equilibrium Gas Aerothermodynamics at Flight- M. Wright, NASA Ames Research Center, G. Candler, H. Johnson, I. Nompelis, B. Cruden, A. Brandis, T. White, ERC, Inc., Aerodynamic Decelerator W. Huo, Y. Liu, NASA Ames Research Duplicated Enthalpies in LENS-XX Moffett Field, CA; M. Hughes, NASA V. Gidzak, P. Subbareddy, University of Moffett Field, CA; D. Bose, NASA Ames S. Tobin, Northrop Grumman Corporation, Center, Moffett Field, CA; M. Panesi, Expansion Tunnel Langley Research Center, Hampton, VA; M. Minnesota, Minneapolis, Minneapolis, MN; Research Center, Moffett Field, CA Herndon, VA; J. Dec, NASA Langley University of Illinois, Urbana-Champaign, M. MacLean, A. Dufrene, Z. Carr, R. Barnhardt, NASA Ames Research Center, M. Barnhardt, ERC, Inc., Moffett Field, CA Research Center, Hampton, VA Urbana, IL; A. Wray, D. Carbon, NASA Parker, M. Holden, CUBRC, Buffalo, NY Moffett Field, CA; A. Calomino, NASA Ames Research Center, Moffett Field, CA Langley Research Center, Hampton, VA Friday Friday, 9 January 2015 403-PLNRY-5 Friday Morning Keynote Osceola Ballroom CD 0800 - 0900 hrs George Whitesides CEO Virgin Galactic and The Spaceship Company Friday, 9 January 2015 404-ACD-7 Transport Aircraft Design Osceola Ballroom 3 Chaired by: M. DRAKE, Boeing Commercial Airplanes 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2015-1898 AIAA-2015-1899 AIAA-2015-1900 AIAA-2015-1901 AIAA-2015-1902 Oral Presentation Transport Category Wing Weight Knowledge-Based Engineering The Right Single-Aisle for the Conceptual Design of a Mach 0.95 Variable Camber Impact on Aircraft KU Jayhawk Economic Turboprop Estimation Using A Optimizing Beam- Approach to the Finite Element Future Market Cruise N+1 Commercial Transport Mission Planning Transport, Winner AIAA Element Structural Formulation Analysis of the Oval Fuselage Concept T. Lammering, T. Schneider, Liebherr C. Langley, R. Burt, N. Patel, I. Martinez, F. Peter, K. Risse, F. Schueltke, E. Stumpf, Undergraduate Team Design T. Takahashi, T. Lemonds, Arizona State S. De Smedt, R. Vos, Delft University of Aerospace, Lindenberg, Germany; E. Stumpf, A. Leon, T. Takahashi, Arizona State RWTH Aachen University, Aachen, Competition University, Tempe, AZ Technology, Delft, The Netherlands RWTH Aachen University, Aachen, Germany University, Tempe, AZ Germany B. Basgall, University of Kansas, Lawrance, KS Friday, 9 January 2015 405-ACD-8 Aircraft Design Case Studies Osceola Ballroom 4 Chaired by: G. CROUSE, Sierra Nevada Corporation 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 164 AIAA-2015-1903 AIAA-2015-1904 AIAA-2015-1905 AIAA-2015-1906 AIAA-2015-1907 Design and Flight Test Study of a C-17 Conversion System for Fire Design of a Severe Storm Research Conceptual Study and Prototype Assessment of Potential Benefit of VTOL UAV Fighting Operations UAS Design of a Subsonic Transport UAV Formation Flight at Preliminary Z. Öznalbant, M. Kavsaoglu, Anadolu C. Bil, RMIT University, Melbourne, A. Avery, J. Jacob, Oklahoma State with VTOL Capabilities Aircraft Design Level University, Eskisehir, Turkey Australia University, Stillwater, OK K. Turkoglu, S. Najafi, San Jose State Y. Liu, K. Risse, K. Franz, E. Stumpf, RWTH University, San Jose, CA Aachen University, Aachen, Germany Friday, 9 January 2015 406-AFM-15 Launch Vehicle, Missile, and Projectile Flight Mechanics II Captiva 2 Chaired by: F. FRESCONI, US Army Research Lab 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2015-1908 AIAA-2015-1909 AIAA-2015-1910 AIAA-2015-1911 Calculating Expectation of Casualty Uncertainty Engagement Analysis Capturing the Global Feasible Guidance and Control of a Man for Hypersonic Reusable Launch of Exoatmospheric Interceptor Design Space for Launch Vehicle Portable Precision Munition Concept Vehicles Based on Reachable Set Model Ascent Trajectories F. Fresconi, Army Research Laboratory, J. Lechniak, C. Chinske, R. Carr, T. Jorris, C. Hua, L. Chen, Y. Zhang, G. Tang, M. Steffens, D. Mavris, S. Edwards, Georgia Aberdeen Proving Ground, MD; J. Rogers, U.S. Air Force, Edwards AFB, CA National University of Defense Technology, Institute of Technology, Atlanta, GA Georgia Institute of Technology, Atlanta, GA Changsha, China Friday, 9 January 2015 407-AMT-8 Aerodynamic Diagnostics Tool for Supersonic and Hypersonic Flows Tallahassee 1 Chaired by: K. LOWE, Virginia Tech and G. JOHNSTON, Texas A&M University 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2015-1912 AIAA-2015-1913 AIAA-2015-1914 AIAA-2015-1915 Measurements of Ablation-Products Model Deformation Measurements of Direct Measurements of Skin Development of Particle Image Transport in a Mach 5 Turbulent Sonic Boom Models in the NASA Ames Friction at AEDC Hypervelocity Velocimetry in a Mach 2.7 Wind Boundary Layer using Naphthalene 9- by 7- Ft Supersonic Wind Tunnel Wind Tunnel 9 Tunnel at AEDC White Oak PLIF E. Schairer, NASA Ames Research Center, R. Meritt, J. Schetz, Virginia Polytechnic J. Brooks, A. Gupta, University of C. Combs, N. Clemens, University of Moffett Field, CA; L. Kushner, Aerospace Institute and State University, Blacksburg, Maryland, College Park, College Park, MD; Texas, Austin, Austin, TX Computing, Inc., Mountain View, CA; T. VA; E. Marineau, D. Lewis, Arnold M. Smith, E. Marineau, Arnold Engineering Garbeff, J. Heineck, NASA Ames Research Engineering Development Complex, Silver Development Complex, Silver Spring, MD Center, Moffett Field, CA Spring, MD Friday, 9 January 2015 408-AMT-9 Aerodynamic Surface Measurements Tallahassee 2 Chaired by: T. IOPPOLO, Southern Methodist University and M. SHEPLAK, University of Florida 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs 1230 hrs AIAA-2015-1916 AIAA-2015-1917 AIAA-2015-1918 AIAA-2015-1919 AIAA-2015-1920 AIAA-2015-1921 AIAA-2015-1922 Error Source Studies of Direct Characterization of an Optical Investigation of a Photonic Wall Measuring Shear Stress with a Accuracy and Survivability of Bio-Inspired Air Data Sensing Probe High Temperature, High Frequency Measurement Skin Friction Sensors Moiré Wall Shear Stress Sensor for Pressure and Shear Stress Sensor Microfluidic Sensor to improve Distributed Fiber Optic Temperature for High Angles of Attack and Fiber Optic Strain Measurement R. Meritt, J. Donbar, Air Force Research Harsh Environments A. Zamanian, T. Ioppolo, Southern Aerodynamic Efficiency Sensors Sideslip System Laboratory, Wright-Patterson AFB, OH; N. D. Mills, University of Florida, Gainesville, Methodist University, Dallas, TX C. Hughes, American Nanofluidics, N. Abdul Rahim, M. Davis, L. Routhier, S. Farokhi, R. Taghavi, S. Keshmiri, University M. Davis, J. Pedrazzani, R. Hull, M. Molinaro, J. Schetz, Virginia Polytechnic Gainesville, FL; T. Chen, Interdisciplinary Altamonte Springs, FL; D. Dutta, Y. J. Chevalier, J. Bos, S. Kreger, Luna of Kansas, Lawrence, Lawrence, KS Castellucci, Luna Innovations, Inc., Institute and State University, Blacksburg, VA Consulting Corporation, Gainesville, FL; M. Bashirzadeh, K. Ahmed, S. Qian, Old Innovations, Inc., Blacksburg, VA; et al. Blacksburg, VA

165 Sheplak, University of Florida, Gainesville, Dominion University, Norfolk, VA Gainesville, FL Friday, 9 January 2015 409-APA-39 Weapons Aerodynamics: Missile/Projectile/Guided-Munitions, Carriage & Store Separation Naples 1 Chaired by: K. DENISSEN, Sandia National Labs and B. MCGRATH, JHU/Applied Physics Laboratory 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2015-1923 AIAA-2015-1924 AIAA-2015-1925 AIAA-2015-1926 AIAA-2015-1927 Effects of Turbulence Model on The Effect of Canard Interactions CFD Database for the Development Statistical Analysis of Jettison Influences of the gap between Prediction of Hot-Gas Lateral on Aerodynamic Performance of a of a Non-Linear Model for Rolling Ejection Scenarios all-movable rudders and the missile Jet Interaction in a Supersonic Fin-Stabilized Projectile Moment P. Reisenthel, D. Lesieutre, O. Quijano, body on flow fields Crossflow S. Silton, F. Fresconi, Army Research A. Nelson, G. McGowan, Corvid Technologies, Nielsen Engineering & Research, Inc., D. Li, J. Zhang, X. Guo, Northwestern J. DeSpirito, Army Research Laboratory, Laboratory, Aberdeen Proving Ground, MD Inc., Mooresville, NC; F. Moore, Aeroprediction, Santa Clara, CA Polytechnical University, Xi’an, China Aberdeen Proving Ground, MD Inc., King George, VA Friday, 9 January 2015 410-APA-40 Applied CFD & Numerical Correlations with Experimental Data III Destin 2 Chaired by: J. DEBONIS, NASA Glenn Research Center and K. VANDEN, USAF 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2015-1928 AIAA-2015-1929 AIAA-2015-1930 AIAA-2015-1931 Evaluation of Five Turbulence Models Application of a New One-Equation Simulation of Atmospheric-Entry Aerodynamics of Finite Cylinders in for Accurate Numerical Simulation of Turbulence Model Based on k-ω Capsules in the Subsonic Regime Quasi-Steady Flow 2D Slot Nozzle Ejector Closure to Flow in S-Ducts S. Murman, R. Childs, J. Garcia, NASA D. Prosser, M. Smith, Georgia Institute of C. Graham, R. Agarwal, Washington H. Xu, T. Wray, C. Fiola, R. Agarwal, Ames Research Center, Moffett Field, CA Technology, Atlanta, GA University in St. Louis, St. Louis, MO Washington University in St. Louis, St. Louis, MO Friday, 9 January 2015 411-APA-41 Low speed, Low Reynolds Number & VSTOL/STOL Aerodynamics Naples 3 Chaired by: M. OL, US Air Force Reseach Laboratory and P. VIJGEN, Boeing Commercial Airplanes 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs 1230 hrs AIAA-2015-1932 AIAA-2015-1933 AIAA-2015-1934 AIAA-2015-1935 AIAA-2015-1936 AIAA-2015-1937 AIAA-2015-1938 Enhancing Lift on a Flat Plate Open-Loop Flow Control At Low Aerodynamics of Low Reynolds Numerical Investigations of Ducted Analysis of the flow field around Outwash Measurements of a Dual Numerical Simulation of Twin using Vortex Pairs generated by Reynolds Numbers Using Periodic Number Axial Compressor Sections Fan Hover Performance for FIW the wing section of a FanWing Impinging Jet Scale Model Impinging jets in Tandem through Synthetic Jet Airfoil Morphing A. Maffioli, C. Hall, S. Melvin, University Applications aircraft under various flow L. Myers, D. McLaughlin, Pennsylvania a Crossflow X. Xia, K. Mohseni, University of Florida, G. Jones, M. Debiasi, Y. Bouremel, of Cambridge, Cambridge, United Kingdom C. Sheng, Q. Zhao, University of Toledo, conditions State University, University Park, PA D. Vieira, J. Barata, F. Neves, A. Silva, Gainesville, Gainesville, FL National University of Singapore, Toledo, OH; N. Bi, Naval Surface Warfare B. Saracoglu, G. Paniagua, von Kármán University of Beira Interior, Covilha, Singapore, Singapore; M. Santer, G. Center, Bethesda, MD Institute for Fluid Dynamics, Rhode-Saint- Portugal Papadakis, Imperial College London, Genèse, Belgium London, United Kingdom Friday, 9 January 2015 412-APA-42 Transonic & Supersonic Aerodynamics Naples 2 Chaired by: C. ROSEMA, US Army AMRDEC and E. FELTROP, The Cessna Aircraft Company 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2015-1939 AIAA-2015-1940 AIAA-2015-1941 AIAA-2015-1942 Reynolds-Averaged Navier-Stokes Numerical Prediction of Planar Investigations of Underexpanded A Numerical Study of High Mach Simulations of Shock Buffet on Half Shock Wave Interaction with a Moist Air Sonic Jets from and Low Reynolds Number Flow Wing-Body Configuration Cylindrical Body Axisymmetric Convergent Nozzles Around Airfoils F. Sartor, S. Timme, University of V. Bhagwandin, Army Research Laboratory, R. Mine, D. Ono, Y. Miyazato, University K. Wang, Z. Zhou, X. Xu, W. Gan, Liverpool, Liverpool, United Kingdom Aberdeen Proving Ground, MD of Kitakyushu, Kitakyushu, Japan Northwestern Polytechnical University, Xi’an, China 166 Friday, 9 January 2015 413-APA-43 Special Session: Aerodynamic Design Optimization of Benchmark Cases III Destin 1 Chaired by: D. ZINGG, University of Toronto and J. VASSBERG, Boeing Engineering Operations & Technology 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2015-1943 AIAA-2015-1944 AIAA-2015-1945 AIAA-2015-1946 AIAA-2015-1947 AIAA-2015-1948 Transonic Airfoils and Wings Design Application of OPTIMENGA_AERO Comparison of Inexact- and Large-scale aircraft design using Control Point-Based Aerodynamic Adjoint-Based Aerodynamic Using Inverse and Direct Methods to Constrained Aerodynamic Design Quasi-Newton Algorithms for SU2 Shape Optimization Applied to AIAA Optimization of Benchmark M. Zhang, A. Rizzi, Royal Institute of B. Epstein, Academic College of Tel Aerodynamic Shape Optimization F. Palacios, T. Economon, J. Alonso, ADODG Test Cases Problems Technology (KTH), Stockholm, Sweden; R. Aviv-Jaffa, Tel Aviv, Israel; S. Peigin, A. Dener, Rensselaer Polytechnic Institute, Stanford University, Stanford, CA D. Poole, C. Allen, T. Rendall, University of S. Nadarajah, McGill University, Montréal, Nangia, Nangia Aero Research Associates, OPTIMENGA-777, Moscow, Russia Troy, NY; G. Kenway, University of Bristol, Bristol, United Kingdom Canada Bristol, United Kingdom Michigan, Ann Arbor, Ann Arbor, MI; J. Hicken, Rensselaer Polytechnic Institute, Troy, NY; J. Martins, University of Michigan, Ann Arbor, Ann Arbor, MI Friday, 9 January 2015 414-CMS-1 High Performance and Embedded Computing Technologies for Aerospace Osceola Ballroom 2 Chaired by: C. LI, Air Force Office of Scientific Research 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2015-1949 AIAA-2015-1950 AIAA-2015-1951 AIAA-2015-1952 High-Performance Optimizations COTS Multicore Processors in MPI/Open-MP Hybridization of Multidisciplinary Simulation of the Unstructured Open-Source Avionics Systems: Challenges and Higher Order WENO Scheme for Acceleration using Multiple Shared- SU2 Suite Solutions the Incompressible Navier-Stokes Memory Graphical Processing Units T. Economon, S. Copeland, F. Palacios, J. D. de Niz, B. Andersson, L. Wrage, Equations J. Kemal, R. Davis, J. Owens, University of Alonso, Stanford University, Stanford, CA; Carnegie Mellon University, Pittsburgh, PA M. Selvam, K. Hoffmann, Wichita State California, Davis, Davis, CA G. Bansal, Intel Corporation, Hillsboro, OR University, Wichita, KS Friday, 9 January 2015 415-FD-50 CFD Solution Adaptation & Optimization Miami 2 Chaired by: M. NEAVES, Corvid Technologies and D. YOUNG, Raytheon Missile Systems 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2015-1953 AIAA-2015-1954 AIAA-2015-1956 AIAA-2015-1957 AIAA-2015-1958 AIAA-2015-1959 Time-averaged steady vs. unsteady Optimization with LES -- algorithms A Hybrid Petrov-Galerkin Method A Computational Approach to A Multi-Mesh CFD Technique for Analysis of a Turbine Flow Meter adjoint: a comparison for cases for dealing with sampling error of for Optimal Output Prediction Slosh Damping with Floating Adaptive Mesh Solutions Calibration Curve using CFD with mild unsteadiness turbulence statistics S. Kast, J. Dahm, K. Fidkowski, University Magnetoactive Micro-baffles C. Jackson, C. Roy, Virginia Polytechnic C. Tegtmeier, P. Anusonti-Inthra, University J. Hueckelheim, S. Xu, M. Gugala, J. C. Talnikar, P. Blonigan, Massachusetts of Michigan, Ann Arbor, Ann Arbor, MI V. Santhanam, M. Ricklick, D. Kim, S. Institute and State University, Blacksburg, VA of Tennessee, Tullahoma, Tullahoma, Müller, Queen Mary University of London, Institute of Technology, Cambridge, MA; J. Gangadharan, Embry-Riddle Aeronautical TN; J. Winchester, Arnold Engineering London, United Kingdom Bodart, University of Toulouse, Toulouse, University, Daytona Beach, FL Development Complex, Tullahoma, TN France; Q. Wang, Massachusetts Institute of Technology, Cambridge, MA Friday, 9 January 2015 416-FD-51/PDL-12 Plasma Actuators and Flow Control Sun Ballroom A Chaired by: J. LITTLE, The University of Arizona and I. ADAMOVICH, Ohio University 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2015-1960 AIAA-2015-1961 AIAA-2015-1962 AIAA-2015-1963 AIAA-2015-1964 The Effects of Laser Plasma Supersonic Cavity Control Using On the boundary and separated Dynamics of charge transfer and Experimental Study of a Discharge on a Separating Plasma Actuators flow using pulsed nanosecond DBD energy coupling in surface discharges Magnetohydrodynamic Plasma Boundary Layer N. Webb, M. Samimy, Ohio State plasma actuators on µsec to msec time scales Actuator in Quiescent Atmospheric Air A. Bright, Tufts University, Medford, MA; N. University, Columbus, OH Z. Zhao, J. Li, J. Zheng, B. Khoo, Y. S. Leonov, I. Adamovich, V. Petrishchev, Y. Choi, M. Gray, J. Sirohi, L. Raja, Tichenor, PM&AM Research, Tucson, AZ; R. Cui, National University of Singapore, Ohio State University, Columbus, OH University of Texas, Austin, Austin, TX Wlezien, Iowa State University, Ames, IA Singapore, Singapore 167 Friday, 9 January 2015 417-FD-52 Separated Flows Sanibel 2 Chaired by: H. FASEL and W. LIOU, Western Michigan University 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2015-1965 AIAA-2015-1966 AIAA-2015-1967 AIAA-2015-1968 Effect of Free-Stream Turbulence Implicit LES of turbulent, separated Flow Features of the Near Wake Prediction of Separation with a on the Structure and Dynamics of flow: wall-mounted hump of a Flat Plate With Turbulent Third-Order-Moment Model Laminar Separation Bubbles configuration Separating Boundary Layers M. Olsen, NASA Ames Research Center, S. Hosseinverdi, H. Fasel, University of S. Sekhar, N. Mansour, NASA Ames Research M. Rai, NASA Ames Research Center, Moffett Field, CA Arizona, Tucson, Tucson, AZ Center, Moffett Field, CA; D. Higuera Caubilla, Moffett Field, CA Institut Supérieur de l’Aéronautique et de l’Espace, Toulouse, France Friday, 9 January 2015 418-FD-53 Shear Layers Tallahassee 3 Chaired by: T. MCLAUGHLIN, US Air Force Academy and J. SEIDEL, USAF Academy 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2015-1969 AIAA-2015-1970 AIAA-2015-1971 AIAA-2015-1972 AIAA-2015-1973 Streamwise vortices in plane mixing Application of the Lattice Boltzmann DNS Study on the Evolution Spectral Scaling in a Supersonic Reynolds Number Effects on Airfoils layers originating from laminar or Method to Shear Layer Flows of Vortical Packets and Their Reattaching Shear Layer in Reverse Flow turbulent initial conditions B. Duda, E. Fares, Exa GmbH, Stuttgart, Interactions in Boundary Layer T. Leger, J. Poggie, Air Force Research A. Lind, L. Smith, University of Maryland, S. Hug, W. McMullan, S. Garrett, University of Germany; R. Kotapati, Exa Corporation, Y. Yan, C. Liu, University of Texas, Laboratory, Wright-Patterson AFB, OH College Park, College Park, MD; J. Leicester, Leicester, United Kingdom Burlington, MA Arlington, Arlington, TX Milluzzo, U.S. Naval Academy, Annapolis, MD; A. Jones, University of Maryland, College Park, College Park, MD Friday, 9 January 2015 419-FD-54 Shock Boundary Layer Interaction Daytona 2 Chaired by: N. BISEK, Air Force Reseach Laboratory and M. MCQUILLING, Saint Louis University 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2015-1974 AIAA-2015-1975 AIAA-2015-1976 AIAA-2015-1977 Transition Effect on Shock Wave Transition location effects on Sidewall Interaction of a Supersonic Unsteadiness in Shock Wave / Boundary Layer Interaction at normal shock wave--boundary Flow over a Compression Ramp Boundary Layer Interactions across M=1.47 layer interactions N. Bisek, Air Force Research Laboratory, Multiple Interaction Configurations P. Polivanov, A. Sidorenko, A. Maslov, Russian T. Davidson, H. Babinsky, University of Wright-Patterson AFB, OH J. Threadgill, P. Bruce, Imperial College Academy of Sciences, Novosibirsk, Russia Cambridge, Cambridge, United Kingdom London, London, United Kingdom Friday, 9 January 2015 420-FD-55 Turbulence Modeling III Sanibel 3 Chaired by: G. HUANG, Wright State University and Y. SEE, University of Michigan 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2015-1978 AIAA-2015-1979 AIAA-2015-1980 AIAA-2015-1981 AIAA-2015-1982 Investigation of hybrid RANS-LES Cut-Cell Method Based Large-Eddy High order LES for Supersonic Recent improvements in the Potential of the elliptic blending methods to understand their Simulation of a Tip-Leakage Vortex Backward-facing Step Flow with formulation of mode III of ZDES Reynolds stress model for use in predictive capabilities in flows with of an Axial Fan Turbulent Inflow (Zonal Detached Eddy Simulation) for hybrid RANS-LES methods separation A. Pogorelov, M. Meinke, W. Schroeder, S. Chern, G. Lobser, M. Schoonmaker, E. WMLES use at $Re_\theta > 10^4$ R. Roy, M. Stoellinger, University of N. Jain, J. Baeder, University of Maryland, RWTH Aachen University, Aachen, Heyde, United Launch Alliance, Denver, CO; C. N. Renard, S. Deck, ONERA, Meudon, France Wyoming, Laramie, Laramie, WY College Park, College Park, MD Germany; R. Kessler, German Aerospace Liu, University of Texas, Arlington, Arlington, TX Center (DLR), Göttingen, Germany Friday, 9 January 2015 168 421-FD-56 Turbulent Boundary Layers Daytona 1 Chaired by: J. POGGIE, USAF AFRL/RBAC 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2015-1983 AIAA-2015-1985 AIAA-2015-1986 AIAA-2015-1987 Compressible Turbulent Boundary An Approximate Turbulent Pressure Investigation of Numerical Schemes Implicit large-eddy simulations of Layer Simulations: Resolution Fluctuation Frequency Spectra for a for Direct Numerical Simulations of zero-pressure gradient, turbulent Effects and Turbulence Modeling Finite Supersonic Plate Supersonic Boundary Layers boundary layer J. Poggie, Air Force Research Laboratory, L. DeChant, J. Smith, Sandia National C. Morris, NASA Marshall Space Flight S. Sekhar, N. Mansour, NASA Ames Wright-Patterson AFB, OH Laboratories, Albuquerque, NM Center, Huntsville, AL Research Center, Moffett Field, CA Friday, 9 January 2015 422-FD-58 Transition Open Forum Sun Ballroom C 0930 - 1300 hrs Chaired by: H. REED, Texas A&M University Friday, 9 January 2015 423-GNC-40 Intelligent Systems in GNC Miami 1 Chaired by: M. BALAS, Embry-Riddle Aeronautical University and J. CONNOLLY, NASA Glenn Research Center 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2015-1988 AIAA-2015-1989 AIAA-2015-1990 AIAA-2015-1991 AIAA-2015-1992 Robust Three-Dimensional Aspects of Intuitive Control: Reinforcement Learning Applied Discrete Multiobjective Optimization Aircraft Energy Management: Collision Avoidance for Fixed-Wing Stabilize, Optimize, and Identify to a Quadrotor Guidance Law in Methodology applied to the Mixed Finite-time Optimal Control with Unmanned Aerial Systems P. Nuthi, K. Subbarao, University of Texas, Autonomous Flight Actuators Problem and Tested in a Dynamic Constraints T. Stastny, G. Garcia, S. Keshmiri, University of Arlington, Arlington, TX J. Junell, E. Van Kampen, C. de Visser, Q. Hardware-in-the-loop Rendezvous M. Yasar, InnoVital Systems, Inc., Kansas, Lawrence, Lawrence, KS Chu, Delft University of Technology, Delft, Simulator Beltsville, MD; H. Kwatny, Drexel The Netherlands W. Gomes, E. Marconi Rocco, National University, Philadelphia, PA; G. Bajpai, Institute for Space Research (INPE), São Techno-Sciences, Inc., Beltsville, MD José dos Campos, Brazil; T. Boge, F. Rems, H. Benninghoff, German Aerospace Center (DLR), Wessling, Germany Friday, 9 January 2015 424-GNC-41 Design and Analysis of Aircraft Control Laws Sun Ballroom 6 Chaired by: D. OSSMANN, DLR - German Aerospace Center and F. HUGON, Gulfstream Aerospace Corporation 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2015-1993 AIAA-2015-1994 AIAA-2015-1995 AIAA-2015-1996 AIAA-2015-1997 Control of Nonlinear Aerospace Nonlinear Flight Control Design for Integrator resetting for enforcing Kalman Filter Based Modification Hardware-In-Loop and Flight Testing Systems using Micro-Jet Actuators Longitudinal Dynamics constraints in aircraft flight control on Helicopter Adaptive Control of Modified State Observer Based S. Mehta, University of Florida, Shalimar, T. Tran, B. Newman, Old Dominion systems M. Okatan, G. Gursoy, I. Yavrucuk, Middle Adaptation for a General Aviation Shalimar, FL; W. Mackunis, Embry-Riddle University, Norfolk, VA K. McDonough, I. Kolmanovsky, University East Technical University, Ankara, Turkey Aircraft 169 Aeronautical University, Daytona Beach, of Michigan, Ann Arbor, Ann Arbor, MI V. Subba Reddiar Pappu, J. Steck, Wichita FL; M. McCourt, University of Florida, State University, Wichita, KS; B. Steele, Shalimar, Shalimar, FL; J. Curtis, Air Force Beechcraft Corporation, Wichita, KS; K. Research Laboratory, Eglin AFB, FL Rajagopal, S. Balakrishnan, Missouri University of Science and Technology, Rolla, MO Friday, 9 January 2015 425-GNC-42 Control of Satellites, Spacecrafts and Missiles Sun Ballroom 3 Chaired by: J. MIGNOT, CNES and J. THEIS, Hamburg University of Technology 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2015-1998 AIAA-2015-1999 AIAA-2015-2000 AIAA-2015-2001 AIAA-2015-2002 AIAA-2015-2003 Quaternion Error Based Optimal Nano-Satellite Transition Mode Orbital Pursuit-Evasion Hybrid Linear Parameter-Varying Feedback Control of a Nonlinear Adaptive Continuous Higher Attitude Control Applied to Pinpoint Attitude Determination and Control Spacecraft Controllers Feedforward Control: A Missile Non-Minimum Phase Missile with Order Sliding Mode Control of Air Landing J. Mignot, F. Viaud, French Space Agency W. Hafer, H. Reed, Texas A&M University, Autopilot Design Limited Modeling Information Breathing Hypersonic Missile for P. Ghiglino, V. Lappas, University of Surrey, (CNES), Toulouse, France College Station, TX J. Theis, Hamburg University of Technology, A. Narang-Siddarth, University of Maximum Target Penetration Guildford, United Kingdom Hamburg, Germany; H. Pfifer, University of Washington, Seattle, Seattle, WA; F. P. Yu, Y. Shtessel, University of Alabama, Minnesota, Minneapolis, Minneapolis, MN; Peter, F. Holzapfel, Technical University of Huntsville, Huntsville, AL; C. Edwards, A. Knoblach, F. Saupe, German Aerospace Munich, Munich, Germany University of Exeter, Exeter, United Center (DLR), Wessling, Germany; H. Werner, Kingdom Hamburg University of Technology, Hamburg, Germany Friday, 9 January 2015 426-GNC-43 Multi-Vehicle Control Sun Ballroom 4 Chaired by: T. YUCELEN, Missouri University of Science & Technology 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2015-2004 AIAA-2015-2005 AIAA-2015-2006 AIAA-2015-2007 AIAA-2015-2008 An Active-Passive Networked Market-Based Task Assignment for Distributed MIN-MAX Optimization Nonlinear Guidance of Unmanned Guidance Law Design For Two Flight Multiagent Systems Approach to Cooperative Timing Missions over Application to Time-optimal Aircraft Formations Vehicles Cooperative Interception Environment Surveillance Networks with Limited Connectivity Consensus: An Alternating O. Tekinalp, S. Ariyibi, Middle East W. Long, F. He, Y. Yao, Harbin Institute of J. Peterson, T. Yucelen, Missouri University G. Oh, Y. Kim, Seoul National University, Projection Approach Technical University, Ankara, Turkey Technology, Harbin, China of Science and Technology, Rolla, MO Seoul, Korea (the Republic of); J. Ahn, H. C. Hu, Z. Chen, Beihang University, Choi, Korea Advanced Institute of Science Beijing, China and Technology, Daejeon, South Korea Friday, 9 January 2015 427-GNC-44 Spacecraft Guidance, Navigation, and Control VI Sun Ballroom 5 Chaired by: L. MASSOTTI, European Space Agency (ESA) and D. PEREZ 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2015-2009 AIAA-2015-2010 AIAA-2015-2011 AIAA-2015-2012 AIAA-2015-2013 A Causality Free Computational Spacecraft Attitude Control under Sun Safe Mode Controller Design Optimal Low-Thrust Orbital Transfers A Linear Model for Low-Thrust Method for HJB Equations with Constrained Zones via Quadratically for LADEE for Rendezvous Between Active Spiral Orbits and Optimal Control Application to Rigid Body Satellites Constrained Quadratic Programming J. Fusco, S. Swei, R. Nakamura, NASA Spacecraft with Return Position D. Kolosa, J. Hudson, Western Michigan W. Kang, L. Wilcox, Naval Postgraduate C. Sun, R. Dai, Iowa State University, Ames, IA Ames Research Center, Moffett Field, CA Constraints University, Kalamazoo, MI School, Monterey, CA A. Dutta, Wichita State University, Wichita, KS Friday, 9 January 2015 170 428-GT-10 New Capabilities in Ground Test Facilities II Sanibel 1 Chaired by: T. WAYMAN, Gulfstream Aerospace Corporation and S. DUNN, Jacobs Technology 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2015-2014 AIAA-2015-2015 AIAA-2015-2016 AIAA-2015-2017 AIAA-2015-2018 AIAA-2015-2019 Development and Demonstration of Commissioning of a Polysonic Wind Low Power Plasma Facilities for Extension of LENS Shock Tunnel Development of the WVU 1.25s MOIRE Thermal Vacuum Structural A Free-to-Roll Rig in A Blow-down Tunnel at the Florida State University the Investigation of Gas-Surface Test Times and Lower Mach Number Reduced-Gravity Drop Tower Stability Testing Tri-sonic Wind Tunnel D. Van Every, S. Best, Aiolos Engineering Interaction at the University of Capability J. Kuhlman, K. Phillips, West Virginia D. Waller, J. Domber, C. Price, R. K. Xie, N. Chen, Q. Shen, China Academy Corporation, Toronto, Canada; J. Strike, R. Kentucky A. Dufrene, CUBRC, Buffalo, NY University, Morgantown, WV Schweickart, R. Thompson, K. Whiteaker, of Aerospace Aerodynamics, Beijing, China Kumar, Florida State University, Tallahassee, FL M. Winter, H. Koch, University of Ball Aerospace & Technologies Kentucky, Lexington, Lexington, KY Corporation, Boulder, CO Friday, 9 January 2015 429-GT-11 Advances in Test Techniques, Test Management, & EFD/CFD Integration Miami 3 Chaired by: J. MICOL, NASA-Langley Research Center 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2015-2020 AIAA-2015-2021 AIAA-2015-2022 AIAA-2015-2023 AIAA-2015-2024 AIAA-2015-2025 Strain Gage Loads Calibration Motive Methods of Heat Flux Numerical Study of the High-Speed Assessment of New Load Schedules Boundary Corrections for Wind Numerical Investigation of Wall Testing With Airbag Support for the Measurement in Stagnation Leg of a Wind Tunnel for the Machine Calibration of a Tunnel Testing of Large Ground Mounting Effects in Semi-Span Gulfstream III SubsoniC Research Ablation Test S. Nayani, W. Sellers, Analytical Services Force Balance Vehicles in Strong Crosswind Wind-Tunnel Tests Aircraft Testbed (SCRAT) H. Gao, L. Chen, D. Ou, China Academy of & Materials, Inc., Hampton, VA; S. N. Ulbrich, Jacobs, Moffett Field, CA; Conditions M. Bouriga, F. Morency, J. Weiss, École de W. Lokos, E. Miller, L. Hudson, A. Holguin, Aerospace Aerodynamics, Beijing, China Brynildsen, ViGYAN, Inc., Hampton, VA; J. R. Gisler, NASA Ames Research Center, C. Britcher, Old Dominion University, Technologie Supérieure, Montréal, Canada D. Neufeld, R. Haraguchi, NASA Armstrong Everhart, NASA Langley Research Center, Moffett Field, CA; R. Kew, Triumph Norfolk, VA; W. Mokhtar, Grand Valley Flight Research Center, Edwards, CA Hampton, VA Aerospace, San Diego, CA State University, Grand Rapids, MI Friday, 9 January 2015 430-IS-13 Intelligent System Approach to Quadcopter Obstacle Avoidance Osceola Ballroom 1 Chaired by: E. KIVELEVITCH, University of Cincinnati and A. YUCEL, Lockheed Martin Aeronautics 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2015-2026 AIAA-2015-2027 AIAA-2015-2028 AIAA-2015-2029 AIAA-2015-2030 AIAA-2015-2031 Laser-Guided Quadrotor Obstacle A Taxonomy of Intelligent Systems Location Determination of an Development of a Model based Target Detection using Image UAS Collision Avoidance, Avoidance E. Kivelevitch, University of Cincinnati, Unmanned Aerial Vehicle in a GPS- Fuzzy-PID Controller for the Processing Techniques Navigation, and Target Assignment A. Stubblebine, B. Feie, B. Redmond, Cincinnati, OH Denied, Hazard-Cluttered Indoor AeroQuad Cyclone Quad-copter J. Hartmann, B. Brown, S. in a Congested Airspace Using E. Kivelevitch, University of Cincinnati, Environment W. Wei, K. Cohen, University of Cincinnati, Mummidivarapu, E. Kivelevitch, University Fuzzy Logic Cincinnati, OH S. Sridhar, A. Sathyan, S. Kukreti, E. Cincinnati, OH of Cincinnati, Cincinnati, OH B. Cook, T. Arnett, B. Rich, E. Kivelevitch, Kivelevitch, University of Cincinnati, University of Cincinnati, Cincinnati, OH Cincinnati, OH Friday, 9 January 2015 431-MST-16 Modeling of Vehicle Dynamics III Sun Ballroom 1 Chaired by: D. CRIDER, National Transportation Safety Board 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2015-2032 AIAA-2015-2033 AIAA-2015-2034 AIAA-2015-2035 AIAA-2015-2036 Representative Post-Stall Modeling Application of SPRT based reset Geometry Based Quick Aircraft Model Based Analysis of Effective Model size for the of T-tail Regional Jet and Turboprop methods for damaged aircraft Modeling Method for Upset Precursors of Electromechanical prediction of the lateral control Aircraft for Flight Training parameter estimation Recovery Applications Servomechanism Failures envelope of damaged aircraft Simulator H. Koolstra, H. Damveld, J. Mulder, Y. Nie, E. Van Kampen, Q. Chu, Delft M. Battipede, M. Dalla Vedova, P. H. Koolstra, J. Mulder, Delft University of T. Teng, T. Zhang, P. Grant, University of Delft University of Technology, Delft, The University of Technology, Delft, The Maggiore, S. Romeo, Technical University Technology, Delft, The Netherlands Toronto, Toronto, Canada Netherlands Netherlands; T. Kier, G. Looye, German of Turin, Turin, Italy Aerospace Center (DLR), Wessling, Germany 171 Friday, 9 January 2015 432-MVC-6 Solution Adaptive Meshing, Error Estimation and Uncertainty Quantification Techniques Sun Ballroom D Chaired by: W. JONES, NASA-Langley Research Center 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2015-2037 AIAA-2015-2038 AIAA-2015-2039 AIAA-2015-2040 AIAA-2015-2041 AIAA-2015-2042 Anisotropic Norm-Oriented Mesh Adaptive Optimization-Based Metric-Based Anisotropic Mesh A Comparison Between Local Multigrid Strategies Coupled with An Anisotropic Adjoint-Based Adaptation for Compressible Flows Smoothing for Tetrahedral Meshes Adaptation for Three-Dimensional h-Refinement and a Novel Anisotropic Mesh Adaptation hp-Adaptive HDG Method for A. Loseille, A. Dervieux, F. Alauzet, French S. Karman, University of Tennessee, Time-Dependent Problems r-Refinement Method V. Menier, A. Loseille, F. Alauzet, French Compressible Turbulent Flow National Institute for Research in Computer Chattanooga, Chattanooga, TN Involving Moving Geometries J. Grisham, N. Vijayakumar, G. Liao, National Institute for Research in M. Woopen, G. May, RWTH Aachen Science and Control (INRIA), Le Chesnay, N. Barral, F. Alauzet, A. Loseille, French B. Dennis, F. Lu, University of Texas, Computer Science and Control (INRIA), University, Aachen, Germany France National Institute for Research in Computer Arlington, Arlington, TX Rocquencourt, France Science and Control (INRIA), Le Chesnay, France Friday, 9 January 2015 433-SATS-4 Small Satellites - Technologies II Osceola Ballroom 5 Chaired by: J. STRAUB, University of North Dakota 0930 hrs 1000 hrs 1030 hrs AIAA-2015-2043 AIAA-2015-2044 AIAA-2015-2045 Information-Driven Systems A CubeSat Mission and Orbit Selection Trade-Offs for LEO Engineering Study of a Formation Configuration Analysis for Locating Observation Microsatellites Flying Demonstration Mission using and Mapping Spot Beams of S. Mortazavi, Satellite Research Institute, Six CubeSats Geostationary Comm-Satellites Tehran, Iran G. Subramanian, R. Foust, D. Chen, S. Chan, J. LaSarge, J. Black, Air Force Institute of Y. Taleb, D. Rogers, University of Illinois, Technology, Wright-Patterson AFB, OH Urbana-Champaign, Urbana, IL; et al. Friday, 9 January 2015 434-SD-20 Plate/Shell Modeling Sarasota 3 Chaired by: Z. SOTOUDEH, Rensselaer Polytechnic Institute and A. SCOTTI, Pilatus Aircraft Ltd 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2015-2046 AIAA-2015-2047 AIAA-2015-2048 AIAA-2015-2049 AIAA-2015-2050 AIAA-2015-2051 Variational Asymptotic Modeling of A New Element for Mixed Plate Evaluating the Dynamic Behavior Finite Element Approach to the Static, Free Vibration Analysis of Nonlinear Membrane Inverse Finite Cosserat Elastic Plates Formulation and Analytically Predicted Vibration and Buckling Analysis of Curvilinearly Stiffened Cylindrical Element Model for Pliant Wings R. Kovvali, D. Hodges, Georgia Institute of Z. Sotoudeh, Rensselaer Polytechnic Displacements of Printed Circuit Curvilinearly Stiffened Plates Shells M. Alioli, P. Masarati, M. Morandini, Technology, Atlanta, GA Institute, Troy, NY Boards (PCBs) Using the “Smeared- P. Shi, Beijing Institute of Technology, Beijing, P. Shi, Beijing Institute of Technology, Technical University of Milan, Milan, Italy; Mass” & Fine Mesh Approach China; R. Kapania, Virginia Polytechnic Beijing, China; R. Kapania, Virginia T. Carpenter, R. Albertani, Oregon State A. Sayles, T. Stoumbos, Orbital Sciences Institute and State University, Blacksburg, Polytechnic Institute and State University, University, Corvallis, OR Corporation, Dulles, VA VA; C. Dong, Beijing Institute of Technology, Blacksburg, VA; C. Dong, Beijing Institute Beijing, China of Technology, Beijing, China Friday, 9 January 2015 435-SD-21 Computational Reduced Order Models Tampa 2 Chaired by: D. RAVEH, AIST and W. SU, University of Alabama, Tuscaloosa 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs 1230 hrs AIAA-2015-2052 AIAA-2015-2053 AIAA-2015-2054 AIAA-2015-2055 AIAA-2015-2056 AIAA-2015-2057 AIAA-2015-2058 Deterministic and Stochastic Partial Basis Identification for Reduced Reduced Order Modeling with Local Development of Aeroelastic and Aeroservoelastic Simulation Dynamic Aeroelastic Response of Tensegrity Structure Modal Analysis Linearization Approach for Nonlinear Order Modeling of Unsteady Flows Enrichments for Nonlinear Geometric Aeroservoelastic Reduced Order Considering Control System Highly Flexible Aircraft with Wing Using a Linear Perturbation Reduced Order Models of Structures Using Sparse Coding Vibration of a Notched Panel Models for Active Structural Control Component Uncertainty Camber Deformations Approach R. Perez, Universal Technology Corporation, R. Deshmukh, Z. Liang, A. Gogulapati, X. Wang, Arizona State University, Tempe, AZ; H. Song, J. Qian, Y. Wang, K. Pant, CFD S. Wu, E. Livne, University of Washington, W. Su, University of Alabama, Tuscaloosa, A. DiCarlo, MITRE Corporation, Bedford, Dayton, OH; B. Smarslok, Air Force Research J. McNamara, Ohio State University, R. Perez, Universal Technology Corporation, Research Corporation, Huntsville, AL; A. Seattle, Seattle, WA Tuscaloosa, AL MA; B. Knight, U.S. Air Force, Chantilly, VA Laboratory, Wright-Patterson AFB, OH; M. Columbus, OH; Z. Kolter, Carnegie Mellon Dayton, OH; G. Phlipot, M. Mignolet, Arizona Chin, M. Brenner, NASA Armstrong Flight

172 Mignolet, Arizona State University, Tempe, AZ University, Pittsburgh, PA State University, Tempe, AZ Research Center, Edwards, CA Friday, 9 January 2015 436-SD-22 Advanced Measurement Techniques Tampa 3 Chaired by: D. JOHNSON, NASA Glenn Research Center and B. WILLIS, Boeing Defense, Space & Security 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2015-2059 AIAA-2015-2060 AIAA-2015-2061 AIAA-2015-2062 Temporal Aliasing in High-Speed Experimental Validation of the Identification of the Smart Preliminary Investigation of Flight 3-Dimensional Digital Image Dynamic Inertia Measurement Spring properties from FRFs Loads of Single-Engine Air Tankers Correlation Vibration Measurement Method to find the Mass Properties measurements K. Rokhsaz, L. Kliment, Wichita State T. Beberniss, Air Force Research of an Iron Bird Test Article M. Arras, G. Coppotelli, University of Rome University, Wichita, KS Laboratory, Wright-Patterson AFB, OH; A. Chin, C. Herrera, N. Spivey, NASA “La Sapienza”, Rome, Italy; F. Nitzsche, D. Ehrhardt, University of Wisconsin, Armstrong Flight Research Center, D. Feszty, Carleton University, Ottawa, Madison, Madison, WI Edwards, CA; W. Fladung, D. Cloutier, ATA Canada Engineering, Inc., San Diego, CA Friday, 9 January 2015 437-STR-20 Special Session: Structural Joints & Repair II Sarasota 2 Chaired by: S. KUMAR and D. NORWOOD, Lockheed Martin Aeronautics 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs 1230 hrs AIAA-2015-2063 AIAA-2015-2064 AIAA-2015-2065 AIAA-2015-2066 AIAA-2015-2067 AIAA-2015-2068 AIAA-2015-2069 Experimental and Computational Investigation of Composite Patch Co-Simulation of Fatigue Crack Analytical and Experimental Practical Bonded Joint Stress Effect of Reinforcement Material Modeling of Stresses in an Evaluation of Out-of-Autoclave Modeling Techniques for Impact Growth and Delamination Evolution Studies on Delamination Arrest Analysis on the Properties of Pin-Reinforced Axisymmetric Composite Patch- Adhesively Bonded Repairs on Loading Conditions in Cracked Aluminum Plates Features in Aircraft Composite A. Selvarathinam, C. Rouseau, Lockheed Metal to Composite Joints Repair System Carbon/Epoxy Fuselage Skin S. TerMaath, A. Sproul, University of Repaired with a Composite Patch Structures Martin Corporation, Fort Worth, TX S. Clay, Air Force Research Laboratory, P. Upadhyaya, S. Kumar, G. Pal, U. Javed, F. Leone, NASA Langley Research Center, Tennessee, Knoxville, Knoxville, TN X. Cui, X. Liu, E. Fang, P. Liu, Global L. Richard, K. Lin, University of Wright-Patterson AFB, OH Masdar Institute of Science and Technology, Hampton, VA Engineering and Materials, Inc., Princeton, NJ Washington, Seattle, Seattle, WA Abu Dhabi, United Arab Emirates Friday, 9 January 2015 438-STR-21 Finite Element Analysis Sarasota 1 Chaired by: R. TAYLOR, Optimal Structures, LLC. and V. RANATUNGA, Air Force Research Laboratory 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2015-2070 AIAA-2015-2071 AIAA-2015-2072 AIAA-2015-2073 AIAA-2015-2074 Some Observations on the Current Enhanced first order shear A Refined Zigzag Element for Composite Beam Cross-Section Three Dimensional Progressive Status of Performing Finite Element deformation theory for the Modeling Sandwich Construction Analysis by a Single High-Order Failure Analysis of Laminated Analyses improved visco-elastic FEM analysis with Embedded Stiffeners Element Layer Composite Structures I. Raju, NASA Langley Research Center, of laminated composite plates M. Dorduncu, A. Borut, E. Madenci, P. Couturier, S. Krenk, Technical University A. Khan, R. Kapania, R. Batra, E. Johnson, Hampton, VA; K. Shivakumar, North Carolina J. Han, Seoul National University, Seoul, University of Arizona, Tucson, Tucson, AZ; of Denmark, Lyngby, Denmark Virginia Polytechnic Institute and State A&T State University, Greensboro, NC Korea (the Republic of); J. Kim, Kumoh A. Tessler, NASA Langley Research Center, University, Blacksburg, VA; J. Guimard, National Institute of Technology, Gumi, Hampton, VA Airbus, Paris, France Korea (the Republic of); M. Cho, Seoul National University, Seoul, South Korea Friday, 9 January 2015 439-TES-4 Topics in Terrestrial Energy Tampa 1 Chaired by: E. KHALIL, Cairo University 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2015-2075 AIAA-2015-2076 AIAA-2015-2077 AIAA-2015-2078 AIAA-2015-2079 Oral Presentation Mixture Preparation Effects on Experimental Investigation of the Natural Ventilation System Versus Tensile Strength and Elongation of Numerical Investigation Of Stratum Review of Organic and Inorganic Distributed Combustion Effects of Central Fuel Injectors on Air Conditioning for Temperature Thermoset Polymer Composites for Ventilation Performance In Office Nanomaterials for Sustainable A. Khalil Hasan, A. Gupta, University of Premixed Swirling Flames Distribution in King Tutankhamuns’s Self-Healing Room Energy Maryland, College Park, College Park, MD N. Syred, F. Hatem, A. Valera-Medina, Gallery, Egyptian Museum R. Amano, A. Matt, Q. Zhang, S. Strong, A. ElHaroun, E. Bialy, Cairo University, Cairo, S. Arepalli, National Institute of Aerospace, R. Marsh, P. Bowen, Cardiff University, A. Zaki, E. Khalil, E. Bialy, W. AbdelMaksoud, S. Mishra, University of Wisconsin, Egypt; A. Fahim, Housing and Building Hampton, VA 173 Cardiff, United Kingdom Cairo University, Cairo, Egypt Milwaukee, Glendale, WI National Research Center, Cairo, Egypt; E. Khalil, Cairo University, Cairo, Egypt Friday, 9 January 2015 440-TP-10 Aerothermodynamics II/Other Thermophysics Topics Sun Ballroom 2 Chaired by: A. MARTIN, University of Kentucky 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2015-2080 AIAA-2015-2081 AIAA-2015-2082 AIAA-2015-2083 AIAA-2015-2084 An Expedient for Alleviating Blackout Analysis of Small Reentry Adjoint-Based Gradient The Effect of Applied Magnetic Field Numerical Study on Surface Oxidation Aerodynamic Heating and Drag on Vehicles Calculations for Projected-Force on Arc Spin Rate in High Pressure of Carbonaceous Nano- and Micro- Capsule Forward Heat Shield S. Ramjatan, S. Roy, University of Florida, Objective Functions in Viscous, Arc Heaters Particles in a Heavily Sooting Ethylene N. Morimoto, J. Yamashita, S. Aso, Y. Gainesville, Gainesville, FL; T. Magin, T. Nonequilibrium Hypersonic J. Sheeley, Aerospace Testing Alliance, Turbulent Jet Flame Tani, Kyushu University, Fukuoka, Japan Scholz, V. Van der Haegen, J. Thoemel, Environments Arnold AFB, TN M. Darbandi, M. Ghafourizadeh, Sharif von Kármán Institute for Fluid Dynamics, S. Copeland, F. Palacios, J. Alonso, University of Technology, Tehran, Iran; G. Rhode-Saint-Genèse, Belgium Stanford University, Stanford, CA Schneider, University of Waterloo, Waterloo, Canada Friday, 9 January 2015 441-TP-11 University Space Systems Programs and Microgravity Flight Activities Sun Ballroom B Chaired by: E. SILK, NASA-Goddard Space Flight Center 0930 hrs 1000 hrs 1030 hrs 1100 hrs Oral Presentation AIAA-2015-2085 AIAA-2015-2086 AIAA-2015-2087 The NASA Sounding Rockets Fifteen Years of the “Microgravity Dynamic Thermal Management for U.S. Naval Academy Small Satellite Program Research Team” (MRT) Project Aerospace Technology: A Review and Program: Leveraging Small P. Eberspeaker, C. Hesh, NASA Wallops Course at West Virginia University Outlook Satellites for Engineering Education Flight Facility, Wallops Island, VA J. Kuhlman, West Virginia University, T. Fisher, Purdue University, West Lafayette, and Research Morgantown, WV IN; K. Yerkes, L. Byrd, Air Force Research J. Kang, B. Bruninga, T. Lim, U.S. Naval Laboratory, Wright-Patterson AFB, OH; J. Academy, Annapolis, MD Murthy, University of Texas, Austin, Austin, TX; A. Alleyne, University of Illinois, Urbana- Champaign, Urbana, IL; M. Wolff, Wright State University, Dayton, OH; et al.

Author/Session Chair Index Abbas, A., 283-MDO-7 Adar, M., 42-SD-1 Akepati, A., 136-MAT-6 Allison, P., 41-PC-4 Angelidis, D., 303-WE-12 Abdalla, M., 95-STR-4 Addali, A., 150-TP-4 Akhil, G., 73-GNC-9 Allmaras, S., 169-FD-21, 321-FD-43 Angilella, A., 154-AS-2 Abdelghaffar, H., 224-GNC-21 Adhikari, S., 239-NDA-5 Akhtar, I., 268-FD-37, 285-MVC-5 Almeida, F., 124-GNC-13, 325-GNC-31 Angland, D., 59-APA-7 AbdelMaksoud, W., 439-TES-4 Adolf, F., 350-SOF-1 Aki, V., 74-GNC-10 Alonso, J., 7-APA-1, 189-NDA-4, 268-FD-37, 357-ACD-5, Anik, E., 102-WE-4 Abdelrahman, M., 168-FD-20, 312-APA-32 Adusumilli, S., 142-PC-9 Akiba, R., 151-UMS-2 385-OPS-1, 413-APA-43, 414-CMS-1, 440-TP-10 Ankersen, J., 199-STR-11 Abdi, F., 399-STR-18 Afonso, F., 148-STR-7 Al Azzawi, D., 272-GNC-25 Alphonso, M., 54-AA-2 Annaswamy, A., 373-GNC-35 Abdol-Hamid, K., 163-APA-18, 312-APA-32 Aftosmis, M., 84-MDO-3, 293-SD-10, 366-APA-38 Al Masoud, N., 317-EDU-1 Alstrom, B., 159-AFM-8 Annoni, J., 51-WE-2

174 Abdoli, A., 310-APA-30 Agarwal, R., 44-SD-3, 59-APA-7, 113-APA-12, Al Shoaibi, A., 401-TES-3 Alter, S., 115-APA-14 Anthony, R., 341-PC-17 Abdollahi, A., 333-IS-11 160-APA-15, 268-FD-37, 312-APA-32, 353-TP-8, Al-Dujaly, H., 319-FD-41 Altman, A., 210-ACD-3, 330-GT-6, 372-FD-49 Antoniadis, A., 68-FD-13, 169-FD-21 Abdul Rahim, N., 408-AMT-9 363-APA-35, 410-APA-40 Alauzet, F., 188-MVC-4, 432-MVC-6 Alvi, F., 54-AA-2, 66-FD-11, 171-FD-23, 318-FD-40 Antunes, A., 219-AS-4 Abdul-Latif, A., 257-APA-25 Agate, M., 61-AS-1 Alazard, D., 328-GNC-34, 377-GNC-39 Aly, A., 237-MST-9, 338-MST-13 Antunes, E., 98-TP-2 Abdulrahim, A., 102-WE-4 Agboola, B., 234-MAT-8 Alba, C., 300-TP-7 Alyanak, E., 33-MDO-1, 137-MDO-4 Anusonti-Inthra, P., 260-APA-28, 415-FD-50 Abe, T., 368-FD-45/PDL-9 Aggarwal, P., 149-STR-8 Albertani, R., 434-SD-20 Amano, H., 151-UMS-2 Aoki, T., 244-SCS-6, 297-STR-14 Abe, Y., 221-FD-29 Aggarwal, S., 113-APA-12 Albrecht, T., 221-FD-29 Amano, R., 299-TES-1, 342-PC-18, 401-TES-3, Aono, H., 67-FD-12/PDL-1 Abedi, H., 102-WE-4 Agha-Mohammadi, A., 132-ICC-1 Ales, F., 22-GNC-5, 72-GNC-8 439-TES-4 Aoyama, T., 261-APA-29 Abouobaia, E., 262-AS-5 Agnes, G., 147-SD-7, 315-AS-6, 391-SCS-9 Alexander, A., 309-AMT-5 Ambrose, S., 2-ISC-1 Applebaum, M., 163-APA-18 Abraham, J., 338-MST-13 Agostinelli, C., 7-APA-1 Alexandrov, N., 88-PC-5 Ameri, A., 66-FD-11, 75-GTE-2 Arad, E., 168-FD-20 Abramson, M., 35-MST-1 Agrawal, P., 175-GNC-16 Alexeenko, A., 99-TP-3 Ames, R., 299-TES-1 Araiba, K., 151-UMS-2 Abras, J., 217-APA-23, 365-APA-37 Agresta, A., 39-PC-2, 182-HSABP-6, 351-SRE-2 Alhajeri, H., 150-TP-4 Amoignon, O., 161-APA-16 Arakawa, Y., 152-WE-5 Abul-Huda, Y., 378-GT-8 Agudelo, D., 202-UMS-3 Alhawwary, M., 312-APA-32 Amzajerdian, F., 71-GNC-7 Araujo-Estrada, S., 159-AFM-8 Accardo, D., 100-UMS-1, 166-DA-1 Ahmad, J., 68-FD-13, 266-FD-35, 285-MVC-5 Ali, A., 312-APA-32 Anand, M., 39-PC-2 Arce, C., 203-WE-7 Acharya, V., 91-PC-8 Ahmad, N., 245-SD-9 Ali, K., 398-STR-17 Anand, V., 130-HSABP-3, 181-HSABP-5, 230-HSABP-7, Arena, A., 122-GNC-11 Achuthan, A., 395-SD-19 Ahmadi, G., 394-SD-18 Ali, M., 318-FD-40 279-HSABP-9/GTE-8 Arepalli, S., 136-MAT-6, 439-TES-4 Acikmese, B., 176-GNC-17 Ahmed, A., 285-MVC-5 Ali, Z., 128-GTE-3 Anders, S., 293-SD-10 Argrow, B., 20-GNC-3, 151-UMS-2, 296-SEN-2 Ackerman, K., 232-IS-7 Ahmed, K., 192-PC-12, 408-AMT-9 Alikhan, M., 55-AFM-3 Anderson, E., 153-WE-6 Ariff, O., 306-ABPSI-1 Acosta, D., 232-IS-7, 325-GNC-31 Ahmed, M., 162-APA-17 Alioli, M., 434-SD-20 Anderson, G., 84-MDO-3, 293-SD-10, 366-APA-38 Ariyibi, S., 426-GNC-43 Action, J., 47-STR-2, 399-STR-18 Ahmed, N., 22-GNC-5, 74-GNC-10 Alireza, S., 97-STR-6 Anderson, R., 100-UMS-1 Armanini, S., 55-AFM-3 Adair, J., 219-AS-4 Ahn, J., 349-SE-1, 426-GNC-43 Allaire, D., 34-MDO-2 Anderson, W., 321-FD-43, 331-GTE-7, 388-PC-20 Arndt, C., 91-PC-8 Adam, J., 176-GNC-17 Ahuja, K., 54-AA-2, 156-AA-5 Allen, A., 377-GNC-39 Andersson, B., 414-CMS-1 Arnett, T., 430-IS-13 Adamczak, D., 109-AFM-6 Aidi, B., 282-MAT-11 Allen, C., 7-APA-1, 51-WE-2, 89-PC-6, 160-APA-15, Andino, M., 164-APA-19/FD-19 Arnold, S., 47-STR-2, 82-MAT-3, 135-MAT-5, Adamczuk, R., 361-AMT-6/GT-7 Aigner, M., 24-GTE-1 413-APA-43 Andino, R., 29-ISC-4 249-STR-13, 282-MAT-11, 399-STR-18 Adamovich, I., 38-PC-1, 119-FD-16, 193-PDL-3, Aikens, K., 106-AA-4 Allen, M., 43-SD-2, 147-SD-7 Andrade, L., 19-GNC-2 Arora, N., 318-FD-40 243-PDL-13, 344-PDL-8, 389-PDL-11, Airoldi, S., 158-AFM-7 Allen, T., 246-SD-13/GEPC-5 Andreeva-Mori, A., 78-IS-4, 157-AA-6 Arras, M., 395-SD-19, 436-SD-22 416-FD-51/PDL-12 Aizengendler, M., 26-HSABP-1 Allevato, G., 80-ISC-3 Andriani, R., 39-PC-2, 182-HSABP-6, 351-SRE-2 Arrieta, A., 61-AS-1, 165-AS-3 Adams, B., 103-APA-9/NDA-1 Ajami, W., 299-TES-1 Alleyne, A., 441-TP-11 Andrus, I., 230-HSABP-7 Arsenault, T., 204-WE-8, 395-SD-19 Adams, D., 204-WE-8 Akcin, Y., 195-SCS-4 Allison, D., 137-MDO-4, 358-ACD-6 Anemaat, W., 307-ACD-4 Arthurs, F., 308-AFM-11 Author/Session Chair Index Artois, K., 330-GT-6 Baker, M., 269-FD-38 Battipede, M., 35-MST-1, 394-SD-18, 431-MST-16 Bernhammer, L., 152-WE-5, 302-WE-11, 394-SD-18 Blades, E., 42-SD-1 Arunajatesan, S., 3-AA-1 Baker, W., 273-GNC-26 Baudendistel, C., 198-STR-10 Berry, B., 196-SD-8 Blaisdell, G., 16-FD-57, 105-AA-3, 106-AA-4, Arya, H., 36-MST-2 Bakker, T., 124-GNC-13 Baum, J., 15-FD-5 Berry, M., 156-AA-5 174-FD-26, 208-AA-7 Arya, M., 145-SCS-3 Bakolas, E., 122-GNC-11 Baumert, A., 257-APA-25 Berry, S., 49-TP-1 Blake, W., 4-AFM-1, 186-MST-7 Asada, H., 13-FD-3 Balabanov, V., 236-MDO-6 Baumgardner, M., 389-PDL-11 Bertagne, C., 154-AS-2, 315-AS-6 Blanc, T., 285-MVC-5 Asada, K., 67-FD-12/PDL-1 Balachandran, S., 27-IS-1 Baurle, R., 131-HSABP-4 Besson, C., 157-AA-6 Blanchette, S., 350-SOF-1, 397-SOF-2 Asai, K., 6-AMT-1 Balakrishna, S., 127-GT-2, 329-GT-5 Bayen, A., 332-IS-10 Best, S., 428-GT-10 Blandino, J., 52-SCS-1, 244-SCS-6 Asay, M., 127-GT-2 Balakrishnan, S., 375-GNC-37, 424-GNC-41 Bays, L., 159-AFM-8 Bettadapura, A., 202-UMS-3, 301-UMS-5 Blankson, I., 356-ABPSI-2 Ashenafi, Y., 46-STR-1 Balas, G., 186-MST-7, 359-AFM-12 Bazzocchi, M., 247-SRE-1 Bewley, T., 167-DE-2 Blanton, E., 204-WE-8 Ashkanazy, J., 22-GNC-5 Balas, M., 18-GNC-1, 61-AS-1, 132-ICC-1, Beberniss, T., 436-SD-22 Beyhaghi, S., 401-TES-3 Blasco, P., 102-WE-4 Ashpis, D., 368-FD-45/PDL-9 253-WE-10, 423-GNC-40 Becar, J., 317-EDU-1 Bezos O’Connor, G., 69-GEPC-2 Blaylock, M., 101-WE-3 Ashraf, M., 372-FD-49 Baldauff, R., 98-TP-2, 150-TP-4 Beck, J., 22-GNC-5, 184-MAT-7, 286-NDA-6 Bhachu, K., 140-NDA-3 Blevins, A., 382-MST-14 Aso, S., 440-TP-10 Ball, D., 82-MAT-3 Beck, W., 6-AMT-1 Bhagat, N., 137-MDO-4 Blevins, J., 115-APA-14, 163-APA-18 Assaad, Z., 33-MDO-1 Ballard, M., 83-MAT-4 Bednarcyk, B., 47-STR-2, 82-MAT-3, 249-STR-13, Bhagwandin, V., 59-APA-7, 412-APA-42 Bliely, M., 368-FD-45/PDL-9 Assif, J., 300-TP-7 Ballinger, D., 35-MST-1 398-STR-17, 399-STR-18 Bhamidipati, K., 58-APA-6 Bloebaum, C., 33-MDO-1, 283-MDO-7 Ates, U., 178-GNC-19 Balunna, S., 234-MAT-8 Bedsole, R., 184-MAT-7 Bhamidipati, V., 82-MAT-3 Blom, A., 95-STR-4 Atescan, Y., 149-STR-8 Bandyopadhyay, S., 123-GNC-12, 345-SATS-2 Behl, S., 398-STR-17 Bhandari, S., 18-GNC-1, 151-UMS-2, 202-UMS-3, Blonigan, P., 322-FD-44, 415-FD-50 Atkins, E., 27-IS-1, 359-AFM-12, 380-IS-12 Bangert, L., 218-APA-24, 261-APA-29 Bejarano, F., 125-GNC-14 301-UMS-5 Blood, D., 234-MAT-8 Atmeh, G., 333-IS-11 Banik, J., 92-SCS-2 Beldica, C., 46-STR-1 Bhat, R., 262-AS-5 Blunck, D., 89-PC-6, 229-GTE-5 Aubert, M., 232-IS-7 Bansal, G., 414-CMS-1 Bell, G., 67-FD-12/PDL-1 Bhatia, M., 42-SD-1 Bobadilla, L., 324-GNC-30 Aubry, R., 314-APA-34 Bansmer, S., 257-APA-25 Bell, J., 23-GT-1 Bhattacharya, S., 185-MDO-5 Bobbitt, L., 127-GT-2 Audet, C., 366-APA-38 Barahona, B., 252-WE-9 Bellan, J., 40-PC-3, 289-PC-16 Bhaumik, S., 322-FD-44 Bodart, J., 415-FD-50 Auslander, D., 337-MST-12 Barakos, G., 108-AFM-5, 311-APA-31, 365-APA-37 Bellmann, T., 238-MST-10 Bhuiyan, A., 362-AMT-7 Bodnar, L., 317-EDU-1 Ausserer, J., 306-ABPSI-1 Barata, J., 25-HIS-1, 98-TP-2, 150-TP-4, 267-FD-36, Bello, R., 279-HSABP-9/GTE-8 Bi, N., 411-APA-41 Boehm, H., 86-MVC-2 175 Austin, J., 119-FD-16, 318-FD-40, 387-PC-19 356-ABPSI-2, 359-AFM-12, 411-APA-41 Belnap, B., 48-STR-3 Bialy, E., 439-TES-4 Boelens, O., 14-FD-4, 64-FD-9 Auweter-Kurtz, M., 201-TP-5 Barberan, C., 29-ISC-4 Belovich, V., 91-PC-8, 143-PC-10, 213-AMT-3, Biava, M., 311-APA-31 Bogdanoff, D., 277-GT-4 Avery, A., 405-ACD-8 Barbour, E., 387-PC-19 269-FD-38 Biber, K., 7-APA-1 Bogdanor, M., 399-STR-18 Avila, A., 32-MAT-2, 136-MAT-6 Bardet, P., 256-AMT-4 Belter, D., 23-GT-1 Bichal, A., 361-AMT-6/GT-7 Boge, T., 423-GNC-40 Axelrod, A., 27-IS-1 Bardhan, R., 73-GNC-9 Belvin, W., 292-SCS-7 Bichon, B., 0-ICME V&V Bogey, C., 106-AA-4 Azarova, O., 120-FD-17 Barkley, B., 367-AS-7 Ben Khelil, S., 60-APA-8 Bidgood, P., 379-GT-9 Bohun, M., 235-MAT-9 Azevedo, J., 58-APA-6, 161-APA-16, 258-APA-26, Barlow, J., 70-GNC-6 Bender, M., 382-MST-14 Bienert, N., 138-MST-5 Boidot, E., 332-IS-10 266-FD-35, 313-APA-33 Barnes, B., 71-GNC-7 Bendiksen, O., 93-SD-4 Bier, N., 257-APA-25 Bojko, B., 40-PC-3 Aziz, I., 285-MVC-5 Barnes, J., 271-GEPC-4/SAT-1 Benek, J., 13-FD-3 Bigarella, E., 258-APA-26 Bolan, J., 110-AMT-2 Azizi, B., 301-UMS-5 Barnhardt, M., 402-TP-9 Bengtson, R., 290-PDL-5 Bil, C., 33-MDO-1, 358-ACD-6, 405-ACD-8 Bolender, M., 26-HSABP-1, 109-AFM-6, 373-GNC-35 Babbie, C., 130-HSABP-3 Barone, D., 180-GTE-4 Bennett, D., 163-APA-18 Bilgen, O., 367-AS-7 Bollino, K., 124-GNC-13, 227-GNC-24 Babinsky, H., 15-FD-5, 419-FD-54 Barone, M., 3-AA-1, 152-WE-5 Bennett, M., 200-SUR-1 Bill, R., 196-SD-8 Bombardieri, R., 248-STR-12 Bacchetta, A., 328-GNC-34 Barral, N., 432-MVC-6 Benninghoff, H., 423-GNC-40 Billstein Andersson, A., 303-WE-12 Bond, I., 184-MAT-7, 334-MAT-12 Bach, A., 265-FD-34 Barrett-Gonzalez, R., 315-AS-6 Benton, J., 63-FD-8 Bimal Raj, K., 22-GNC-5 Bons, J., 66-FD-11, 75-GTE-2, 221-FD-29, 265-FD-34 Bacher, M., 257-APA-25 Barry, W., 25-HIS-1 Benton, S., 221-FD-29, 265-FD-34 Bin, J., 32-MAT-2 Boomsma, A., 101-WE-3 Badakhshan, A., 342-PC-18 Bartels, R., 246-SD-13/GEPC-5 Beran, P., 42-SD-1, 189-NDA-4 Bindolino, G., 44-SD-3 Boone, N., 183-IS-6 Badcock, K., 56-AFM-4 Barthelmie, R., 153-WE-6 Beresh, S., 256-AMT-4, 269-FD-38, 277-GT-4 Bird, J., 61-AS-1 Boopathy, K., 189-NDA-4 Badrya, C., 11-FD-1 Bartram, G., 384-NDA-8 Berg, J., 12-FD-2 Birkmire, B., 85-MST-4 Borer, N., 357-ACD-5 Bae, H., 189-NDA-4, 286-NDA-6, 384-NDA-8 Baruzzi, G., 263-FD-32 Berg, R., 265-FD-34 Bis, R., 380-IS-12 Borg, M., 49-TP-1, 62-FD-7 Baeder, J., 11-FD-1, 203-WE-7, 420-FD-55 Basgall, B., 404-ACD-7 Bergamini, A., 165-AS-3 Bisagni, C., 44-SD-3, 298-STR-15 Borg, S., 361-AMT-6/GT-7 Baeten, A., 197-STR-9 Bashirzadeh, Y., 408-AMT-9 Berger, K., 49-TP-1, 277-GT-4, 378-GT-8 Bisek, N., 419-FD-54 Borggaard, J., 263-FD-32 Bai, X., 275-GNC-28, 326-GNC-32 Basset, M., 36-MST-2 Berger, T., 5-AFM-2, 338-MST-13 Bishop, M., 56-AFM-4 Borghesi, G., 40-PC-3, 91-PC-8 Bailey, M., 396-SE-2 Bassi, F., 65-FD-10 Berger, Z., 156-AA-5 Bissonnette, W., 215-APA-21 Borovoy, V., 222-FD-30 Bain, M., 272-GNC-25 Bates, D., 19-GNC-2 Bergeron, K., 86-MVC-2, 114-APA-13 Bitche, R., 101-WE-3 Borut, A., 97-STR-6, 438-STR-21 Bajpai, G., 237-MST-9, 423-GNC-40 Bathel, B., 76-HSABP-2, 361-AMT-6/GT-7 Bergh, B., 29-ISC-4 Bittner, S., 295-SD-12 Bos, J., 408-AMT-9 Bak, C., 101-WE-3 Batra, A., 301-UMS-5 Bernal, L., 9-APA-3 Bityurin, V., 67-FD-12/PDL-1 Boschetti, P., 5-AFM-2, 108-AFM-5 Bakaul, S., 158-AFM-7, 216-APA-22 Batra, R., 438-STR-21 Bernard, S., 191-PC-11 Black, J., 22-GNC-5, 52-SCS-1, 433-SATS-4 Bose, D., 49-TP-1, 402-TP-9 Baker, J., 51-WE-2, 346-SCS-8 Battaglia, B., 161-APA-16 Bernardo, J., 157-AA-6 Blackwood, J., 115-APA-14 Boshinski, A., 200-SUR-1 Author/Session Chair Index Bosnyakov, S., 127-GT-2 Brown, C., 54-AA-2, 156-AA-5, 301-UMS-5 Cai, J., 84-MDO-3 Castelluccio, M., 246-SD-13/GEPC-5 Chavers, G., 176-GNC-17 Bossert, D., 51-WE-2 Brown, D., 371-FD-48 Cain, A., 106-AA-4, 216-APA-22 Castet, J., 233-IS-8 Chawner, J., 86-MVC-2 Bosworth, R., 79-ISC-2 Brown, J., 198-STR-10, 239-NDA-5, 286-NDA-6 Cairns, D., 204-WE-8 Castner, R., 218-APA-24 Chazot, O., 119-FD-16 Botez, R., 186-MST-7, 219-AS-4, 262-AS-5 Brown, M., 273-GNC-26 Calcagni, P., 166-DA-1 Castro, J., 182-HSABP-6 Che Man, M., 312-APA-32 Bottasso, C., 101-WE-3, 253-WE-10, 302-WE-11 Brown, R., 295-SD-12 Calderon, D., 393-SD-17 Castro, M., 383-MST-15 Chehroudi, B., 40-PC-3 Bouchenot, T., 334-MAT-12 Bruce, P., 259-APA-27, 419-FD-54 Caley, T., 271-GEPC-4/SAT-1 Caswell, A., 91-PC-8, 213-AMT-3, 279-HSABP-9/GTE-8, Chelliah, H., 76-HSABP-2, 89-PC-6, 241-PC-13 Boumehdi, M., 142-PC-9 Bruce, W., 218-APA-24 Calhoon, W., 143-PC-10 341-PC-17 Chen, C., 151-UMS-2 Bounajem, E., 146-SD-6 Bruni, C., 249-STR-13 Calise, A., 374-GNC-36 Cattafesta, L., 221-FD-29, 364-APA-36 Chen, D., 89-PC-6, 433-SATS-4 Bounthisane, R., 367-AS-7 Bruninga, B., 441-TP-11 Calomino, A., 402-TP-9 Cavagna, L., 219-AS-4 Chen, F., 256-AMT-4, 364-APA-36 Bourassa, C., 174-FD-26 Bruno, C., 182-HSABP-6 Calvert, M., 311-APA-31 Cavalieri, D., 144-PDL-2 Chen, H., 72-GNC-8, 107-ACD-1, 160-APA-15, Bouremel, Y., 411-APA-41 Bruns, J., 120-FD-17 Camarinha Fujiwara, G., 311-APA-31 Cavallaro, R., 46-STR-1, 148-STR-7, 248-STR-12 169-FD-21, 187-MST-8, 234-MAT-8, 348-SD-15, Bourgault-Cote, S., 111-APA-10 Bryant, L., 385-OPS-1 Cameron, C., 294-SD-11 Cavrois, B., 72-GNC-8 357-ACD-5 Bouriga, M., 429-GT-11 Bryden, K., 86-MVC-2, 299-TES-1 Campbell, D., 52-SCS-1, 195-SCS-4 Cebeci, H., 149-STR-8 Chen, J., 58-APA-6 Bowen, C., 367-AS-7 Brynildsen, S., 429-GT-11 Campbell, L., 391-SCS-9 Cecrdle, J., 395-SD-19 Chen, L., 406-AFM-15, 429-GT-11 Bowen, P., 352-TES-2, 439-TES-4 Bucci, R., 82-MAT-3 Campbell, R., 187-MST-8, 261-APA-29 Celestina, M., 69-GEPC-2 Chen, N., 428-GT-10 Bowen-Davies, G., 196-SD-8 Buckley, H., 60-APA-8, 371-FD-48 Canacci, V., 330-GT-6 Celestino, C., 48-STR-3 Chen, P., 7-APA-1, 113-APA-12, 246-SD-13/GEPC-5, Bowersox, R., 62-FD-7, 222-FD-30 Buerge, B., 330-GT-6 Canal Vila, M., 203-WE-7 Cerimele, C., 376-GNC-38 295-SD-12 Bowman, C., 78-IS-4 Bui, N., 171-FD-23 Candler, G., 62-FD-7, 300-TP-7, 402-TP-9 Ceruti, A., 57-APA-5 Chen, R., 150-TP-4, 250-TP-6 Boxx, I., 143-PC-10 Bülthoff, H., 139-MST-6 Candon, M., 231-HSABP-8 Cesare, S., 328-GNC-34 Chen, S., 39-PC-2, 366-APA-38 Boyd, D., 157-AA-6 Bulyshev, A., 71-GNC-7 Candon, S., 218-APA-24 Cesnik, C., 43-SD-2, 94-SD-5 Chen, T., 408-AMT-9 Boyd, I., 291-PDL-6 Buonanno, M., 146-SD-6 Canfield, R., 34-MDO-2, 96-STR-5 Cestino, E., 249-STR-13 Chen, W., 353-TP-8 Bradford, S., 195-SCS-4, 292-SCS-7 Buonocore, M., 328-GNC-34 Canfield, T., 65-FD-10 Cetiner, O., 270-FD-39 Chen, X., 93-SD-4 Bradley, M., 17-GEPC-1 Buoso, S., 61-AS-1 Cantu, L., 76-HSABP-2 Cetraro, G., 270-FD-39 Chen, Y., 132-ICC-1, 214-APA-20, 331-GTE-7 Bragg, M., 257-APA-25 Burchett, B., 4-AFM-1, 211-AFM-9 Canuto, E., 328-GNC-34 Ceyhan, O., 102-WE-4 Chen, Z., 244-SCS-6, 426-GNC-43 176 Braginsky, M., 399-STR-18 Burdette, D., 60-APA-8, 236-MDO-6 Cao, Y., 175-GNC-16 Ceze, M., 321-FD-43 Cheng, V., 35-MST-1 Bramesfeld, G., 215-APA-21 Burfitt, W., 378-GT-8 Capra, B., 182-HSABP-6 Chakraborty, I., 358-ACD-6 Cheng, Y., 18-GNC-1, 176-GNC-17, 393-SD-17 Brampton, C., 34-MDO-2, 95-STR-4, 367-AS-7 Burk, T., 19-GNC-2 Capristan, F., 189-NDA-4 Chakravarthy, A., 28-IS-2, 275-GNC-28, 326-GNC-32 Chern, S., 120-FD-17, 420-FD-55 Brand, Y., 27-IS-1 Burkhalter, J., 211-AFM-9 Carbon, D., 402-TP-9 Chan, D., 127-GT-2 Chernikov, D., 46-STR-1 Brandis, A., 402-TP-9 Burley, C., 323-GEPC-3 Carbonari, R., 232-IS-7 Chan, M., 301-UMS-5 Cheung, K., 147-SD-7, 150-TP-4, 194-SATS-1 Brauckmann, G., 115-APA-14 Burnett, B., 100-UMS-1 Cardenas, E., 5-AFM-2 Chan, S., 433-SATS-4 Cheung, R., 219-AS-4 Braun, R., 48-STR-3, 108-AFM-5, 109-AFM-6, 167-DE-2 Burnett, J., 301-UMS-5 Cardoso, K., 191-PC-11 Chan, W., 163-APA-18 Chevalier, J., 408-AMT-9 Braxmaier, C., 22-GNC-5, 72-GNC-8 Burnette, D., 243-PDL-13 Cardullo, F., 139-MST-6, 238-MST-10 Chandar, D., 68-FD-13 Chiba, K., 151-UMS-2 Brazell, M., 13-FD-3, 321-FD-43, 370-FD-47 Burns, W., 144-PDL-2 Carlson, H., 163-APA-18, 314-APA-34 Chandler, J., 17-GEPC-1 Chichester, R., 96-STR-5 Breen, N., 156-AA-5 Burnside, N., 57-APA-5 Carnes, T., 124-GNC-13 Chandler, P., 177-GNC-18 Childs, R., 362-AMT-7, 410-APA-40 Breitsamter, C., 14-FD-4 Burt, J., 99-TP-3, 353-TP-8 Carpenter, M., 323-GEPC-3 Chandramohan, R., 374-GNC-36 Childs, T., 250-TP-6 Brenner, M., 435-SD-21 Burt, R., 404-ACD-7 Carpenter, S., 200-SUR-1 Chang, C., 24-GTE-1 Chin, A., 435-SD-21, 436-SD-22 Brentner, K., 106-AA-4, 165-AS-3 Busa, J., 71-GNC-7 Carpenter, T., 434-SD-20 Chang, K., 336-MDO-8 Chin, J., 336-MDO-8 Bretl, K., 261-APA-29 Busa, K., 76-HSABP-2 Carr, R., 406-AFM-15 Chang, M., 9-APA-3 Chinske, C., 406-AFM-15 Breuer, K., 368-FD-45/PDL-9 Busari, T., 191-PC-11 Carr, Z., 402-TP-9 Chang, S., 136-MAT-6 Chiu, L., 196-SD-8 Bridges, J., 54-AA-2 Bush, R., 220-FD-28 Carrier, G., 60-APA-8 Chapelier, J., 13-FD-3 Chivaee, H., 102-WE-4, 303-WE-12, 311-APA-31 Briggs, H., 167-DE-2 Butler, R., 199-STR-11, 339-NDA-7 Carson, J., 71-GNC-7, 176-GNC-17 Chaput, A., 210-ACD-3 Chng, T., 193-PDL-3 Bright, A., 416-FD-51/PDL-12 Butnarasu, M., 8-APA-2 Carter, C., 40-PC-3, 182-HSABP-6 Charalampous, G., 40-PC-3 Cho, M., 31-MAT-1, 97-STR-6, 136-MAT-6, 165-AS-3, Briley, W., 153-WE-6 Buttner, A., 397-SOF-2 Carter, M., 218-APA-24 Charest, M., 65-FD-10 249-STR-13, 438-STR-21 Briones, A., 269-FD-38 Buzica, A., 14-FD-4 Cartmell, D., 85-MST-4 Chary, G., 347-SD-14 Cho, N., 273-GNC-26 Britcher, C., 429-GT-11 Byrd, L., 441-TP-11 Carton de Wiart, C., 13-FD-3 Chatelain, P., 102-WE-4 Cho, S., 175-GNC-16 Bromfield, M., 159-AFM-8 Byrne, A., 252-WE-9 Casbeer, D., 73-GNC-9, 183-IS-6 Chatterjee, T., 153-WE-6 Choe, R., 123-GNC-12 Brooks, D., 100-UMS-1 Bystry-Wells, D., 75-GTE-2 Casiez, P., 72-GNC-8 Chattopadhyay, A., 48-STR-3, 83-MAT-4, 149-STR-8, Choi, H., 77-IS-3, 426-GNC-43 Brooks, G., 314-APA-34 Cacan, M., 18-GNC-1 Casper, K., 62-FD-7, 269-FD-38, 277-GT-4 262-AS-5 Choi, J., 31-MAT-1, 65-FD-10, 260-APA-28 Brooks, J., 407-AMT-8 Caccamo, M., 202-UMS-3 Cassaro, M., 35-MST-1, 394-SD-18 Chaudhry, R., 62-FD-7 Choi, M., 92-SCS-2 Brophy, C., 341-PC-17 Cadou, C., 128-GTE-3, 242-PC-14 Castano, L., 158-AFM-7, 224-GNC-21 Chaudhuri, A., 185-MDO-5, 336-MDO-8 Choi, S., 161-APA-16, 283-MDO-7, 381-MDO-9 Brouwer, K., 146-SD-6 Cai, C., 174-FD-26, 353-TP-8 Casteleim, D., 152-WE-5 Chaurasia, A., 367-AS-7 Choi, Y., 416-FD-51/PDL-12 Brown, B., 78-IS-4, 430-IS-13 Cai, G., 82-MAT-3 Castellucci, M., 408-AMT-9 Chauveau, C., 191-PC-11 Chopra, I., 61-AS-1, 196-SD-8, 294-SD-11, 394-SD-18 Author/Session Chair Index Chou, A., 369-FD-46 Colket, M., 89-PC-6, 91-PC-8, 289-PC-16 Crawford, B., 258-APA-26 Dalenbring, M., 44-SD-3, 93-SD-4 de la Llave Plata, M., 13-FD-3 Choudhari, M., 62-FD-7, 173-FD-25 Collier, F., 69-GEPC-2 Crawley, M., 156-AA-5 Dalgarno, R., 399-STR-18 De Lellis, E., 100-UMS-1 Choudhuri, A., 401-TES-3 Collins, J., 234-MAT-8 Creary, G., 316-DE-3 Dalla Vedova, M., 431-MST-16 De Lucca, N., 144-PDL-2 Chow, R., 101-WE-3, 153-WE-6, 203-WE-7, 258-APA-26 Collopy, P., 396-SE-2 Creech, M., 191-PC-11 Dalle, D., 163-APA-18 de Niz, D., 414-CMS-1 Chowdhary, G., 27-IS-1, 125-GNC-14, 333-IS-11 Colonia, S., 108-AFM-5 Crespo, A., 12-FD-2 Damaren, C., 92-SCS-2, 226-GNC-23 De Palma, P., 231-HSABP-8 Chowdhury, S., 381-MDO-9 Colonius, T., 9-APA-3 Crespo, L., 140-NDA-3 Damiani, R., 50-WE-1, 252-WE-9 de Paula, A., 255-AA-8 Choze, S., 34-MDO-2 Colvin, T., 385-OPS-1 Crider, D., 5-AFM-2, 35-MST-1, 431-MST-16 Damodaran, M., 162-APA-17 De Pauw, B., 395-SD-19 Christian, J., 276-GNC-29 Combs, C., 407-AMT-8 Crispin, C., 77-IS-3 Damveld, H., 431-MST-16 De Ridder, K., 238-MST-10 Chu, Q., 72-GNC-8, 238-MST-10, 272-GNC-25, Comer, A., 269-FD-38 Criss, T., 176-GNC-17 Danehy, P., 76-HSABP-2, 256-AMT-4, 361-AMT-6/GT-7, De Smedt, S., 404-ACD-7 373-GNC-35, 374-GNC-36, 423-GNC-40, 431-MST-16 Commo, S., 379-GT-9 Croce, A., 101-WE-3 362-AMT-7 de Tejada Alvarez, A., 400-STR-19 Chung, J., 98-TP-2 Congedo, P., 189-NDA-4, 366-APA-38 Cross, C., 184-MAT-7 Daniel, D., 14-FD-4, 64-FD-9 de Visser, C., 55-AFM-3, 72-GNC-8, 85-MST-4, Chung, S., 27-IS-1, 90-PC-7, 123-GNC-12, 224-GNC-21, Conner, J., 122-GNC-11 Cross, M., 247-SRE-1 Daniel, W., 125-GNC-14 122-GNC-11, 158-AFM-7, 373-GNC-35, 423-GNC-40 233-IS-8, 324-GNC-30, 345-SATS-2, 375-GNC-37 Connolly, J., 423-GNC-40 Crossley, W., 107-ACD-1, 185-MDO-5, 286-NDA-6 Dannenhoffer, J., 86-MVC-2, 285-MVC-5 Deaton, J., 297-STR-14 Churchfield, M., 50-WE-1, 153-WE-6 Conway, M., 113-APA-12, 363-APA-35 Crouch, R., 399-STR-18 Dantsker, O., 6-AMT-1, 202-UMS-3 Debiasi, M., 411-APA-41 Chwalowski, P., 93-SD-4 Conyers, H., 237-MST-9 Crouch, T., 129-HIS-2 Dantsuka, Y., 300-TP-7 Debon, D., 47-STR-2 Chynoweth, B., 369-FD-46 Cook, B., 430-IS-13 Crouse, G., 405-ACD-8 Dao, T., 392-SD-16 DeBonis, J., 68-FD-13, 323-GEPC-3, 258-APA-26, Cichella, V., 123-GNC-12 Cook, R., 368-FD-45/PDL-9 Crowe, D., 356-ABPSI-2 Darakananda, D., 372-FD-49 410-APA-40 Cieslak, J., 125-GNC-14 Cook, S., 100-UMS-1, 251-UMS-4, 397-SOF-2 Crowell, A., 146-SD-6, 314-APA-34 Darbandi, M., 353-TP-8, 440-TP-10 Dec, J., 402-TP-9 Cifuentes, J., 298-STR-15 Cooley, P., 147-SD-7 Cruden, B., 402-TP-9 Darmofal, D., 169-FD-21, 317-EDU-1, 321-FD-43 DeChant, L., 121-FD-18, 421-FD-56 Cipolla, V., 148-STR-7 Cooper, J., 93-SD-4, 189-NDA-4, 219-AS-4, 248-STR-12, Cruise, D., 242-PC-14 Darr, S., 98-TP-2 Deck, S., 14-FD-4, 420-FD-55 Claggett, S., 246-SD-13/GEPC-5 295-SD-12, 393-SD-17 Cui, P., 276-GNC-29 das Gupta, A., 319-FD-41, 344-PDL-8 Decker, B., 271-GEPC-4/SAT-1 Clark, D., 286-NDA-6 Cope, E., 47-STR-2 Cui, X., 334-MAT-12, 437-STR-20 Dasari, A., 242-PC-14, 342-PC-18 Deierling, P., 32-MAT-2 Clark, I., 49-TP-1 Copeland, S., 414-CMS-1, 440-TP-10 Cui, Y., 416-FD-51/PDL-12 Daskilewicz, M., 357-ACD-5 Deierling, W., 326-GNC-32 Clark, J., 171-FD-23 Coppotelli, G., 395-SD-19, 436-SD-22 Culler, A., 219-AS-4, 347-SD-14 Daskiran, O., 159-AFM-8 Del Frate, J., 212-AFM-10 177 Clark, M., 18-GNC-1 Corbets, J., 79-ISC-2 Cullinan, J., 334-MAT-12 Dasque, N., 209-ACD-2 Delabie, T., 276-GNC-29 Clay, S., 197-STR-9, 399-STR-18, 437-STR-20 Corbett, S., 58-APA-6 Cumer, C., 377-GNC-39 Date, H., 257-APA-25 Delaney, R., 79-ISC-2 Cleaver, D., 372-FD-49 Corke, T., 62-FD-7, 216-APA-22, 223-FD-31 Cummings, M., 232-IS-7 Datta, A., 196-SD-8, 294-SD-11 Delapierre, M., 292-SCS-7 Cleaver, T., 269-FD-38 Corle, E., 165-AS-3 Cummings, R., 14-FD-4, 64-FD-9, 86-MVC-2, Datta, S., 83-MAT-4 DeLaurentis, D., 45-SEN-1, 132-ICC-1, 187-MST-8 Clem, M., 361-AMT-6/GT-7 Cornelison, C., 277-GT-4 114-APA-13 Davidson, D., 242-PC-14 Delgado, A., 247-SRE-1 Clemens, N., 119-FD-16, 407-AMT-8 Cornish, A., 42-SD-1 Cunningham, K., 359-AFM-12 Davidson, L., 102-WE-4 Delot, A., 356-ABPSI-2 Clement, B., 233-IS-8 Corporan, E., 213-AMT-3 Curran, Q., 185-MDO-5 Davidson, T., 419-FD-54 Delp, C., 233-IS-8 Clement, T., 281-MAT-10 Corraro, F., 100-UMS-1 Currier, P., 151-UMS-2 Davies, M., 350-SOF-1, 397-SOF-2 Delpero, T., 165-AS-3 Cliff, S., 218-APA-24 Corrigan, A., 106-AA-4, 174-FD-26 Curro, J., 378-GT-8 Davila, C., 298-STR-15, 334-MAT-12 Demasi, L., 46-STR-1, 148-STR-7, 248-STR-12 Clifford, C., 265-FD-34 Corson, D., 216-APA-22 Curtis, J., 272-GNC-25, 424-GNC-41 Davila, J., 125-GNC-14 DeMoss, J., 127-GT-2, 329-GT-5 Clifford, J., 251-UMS-4 Cortesi, A., 61-AS-1 Cutler, A., 76-HSABP-2, 362-AMT-7 Davis, B., 52-SCS-1, 195-SCS-4 Dendinger, T., 358-ACD-6 Cloutier, D., 436-SD-22 Costa, R., 56-AFM-4 Cutrone, L., 231-HSABP-8 Davis, G., 391-SCS-9 Dener, A., 413-APA-43 Cluts, J., 54-AA-2 Costantine, J., 195-SCS-4 Cutshall, J., 167-DE-2 Davis, K., 80-ISC-3 Denissen, K., 310-APA-30, 409-APA-39 Cobb, R., 18-GNC-1, 45-SEN-1, 100-UMS-1, Costello, M., 18-GNC-1 Cybyk, B., 216-APA-22 Davis, M., 408-AMT-9 Dennis, B., 432-MVC-6 273-GNC-26 Cotting, M., 56-AFM-4 Czabaj, M., 74-GNC-10 Davis, P., 69-GEPC-2 Dennis, C., 242-PC-14 Coburn, B., 298-STR-15 Cottle, A., 24-GTE-1 Czech, M., 255-AA-8 Davis, R., 63-FD-8, 171-FD-23, 285-MVC-5, 414-CMS-1 Dennis, R., 299-TES-1 Cocks, P., 387-PC-19 Cotton, J., 47-STR-2 D’Amato, E., 124-GNC-13 Davis, T., 7-APA-1, 34-MDO-2, 54-AA-2, 66-FD-11 Deptula, P., 191-PC-11, 317-EDU-1 Coclite, A., 231-HSABP-8 Couaillier, V., 13-FD-3, 264-FD-33 D’Mello, R., 199-STR-11 Dawes, W., 172-FD-24, 220-FD-28 Derlaga, J., 263-FD-32 Coder, J., 121-FD-18 Couturier, P., 438-STR-21 Da Ronch, A., 56-AFM-4 Dawson, D., 318-FD-40 Dervieux, A., 432-MVC-6 Cogan, B., 325-GNC-31 Cowlagi, R., 225-GNC-22, 373-GNC-35 Dadian, O., 301-UMS-5 Dawson, S., 223-FD-31 Desgroux, P., 142-PC-9 Coggin, J., 246-SD-13/GEPC-5 Cox, C., 172-FD-24 Dahm, J., 415-FD-50 Dayton, J., 202-UMS-3, 301-UMS-5 Deshmukh, R., 146-SD-6, 435-SD-21 Coggon, S., 393-SD-17 Cox, J., 275-GNC-28 Dahm, W., 268-FD-37 de Andrade, D., 258-APA-26 Deshpande, T., 78-IS-4 Cognata, T., 315-AS-6 Cox, R., 5-AFM-2 Dai, L., 149-STR-8 de Araújo, T., 191-PC-11 DesJardin, P., 40-PC-3 Cohen, K., 77-IS-3, 78-IS-4, 183-IS-6, 430-IS-13 Coy, E., 242-PC-14 Dai, R., 427-GNC-44 De Breuker, R., 42-SD-1, 59-APA-7, 61-AS-1, 165-AS-3, Desmidt, H., 196-SD-8 Coil, M., 342-PC-18 Crabill, J., 370-FD-47 Dai, Y., 75-GTE-2, 337-MST-12 302-WE-11, 394-SD-18 DeSpirito, J., 409-APA-39 Cole, B., 233-IS-8 Cramer, C., 127-GT-2 Daigle, M., 380-IS-12 de Croon, G., 55-AFM-3 Destarac, D., 60-APA-8, 371-FD-48 Cole, R., 100-UMS-1 Cramer, N., 147-SD-7 Daily, J., 89-PC-6 De Gaspari, A., 219-AS-4 Devalla, V., 359-AFM-12 Coleman, D., 223-FD-31 Crandell, A., 191-PC-11 Daimon, Y., 90-PC-7 De La Garza, A., 146-SD-6 Devolites, J., 176-GNC-17 Author/Session Chair Index DeVoria, A., 266-FD-35 Dorsey, J., 52-SCS-1 Echols, J., 373-GNC-35 Erfani, R., 34-MDO-2 Fichter, W., 375-GNC-37 DeWald, A., 82-MAT-3 Dougherty, R., 106-AA-4 Eckert, Z., 344-PDL-8 Erfani, T., 34-MDO-2 Fidkowski, K., 118-FD-15, 170-FD-22, 321-FD-43, Dey, S., 86-MVC-2 Dowell, E., 295-SD-12 Eckhart, C., 5-AFM-2 Erickson, G., 163-APA-18 415-FD-50 Dhamankar, N., 105-AA-3 Dowling, A., 91-PC-8 Eckstein, E., 198-STR-10, 297-STR-14 Ermanni, P., 61-AS-1, 165-AS-3 Fields, T., 308-AFM-11 Dhanasar, M., 169-FD-21, 209-ACD-2, 356-ABPSI-2 Doyle, D., 315-AS-6 Economon, T., 413-APA-43, 414-CMS-1 Ernest, N., 183-IS-6 Fiepke, B., 235-MAT-9 Dhawan, S., 306-ABPSI-1 Doyle, S., 269-FD-38 Edefur, H., 64-FD-9 Erturk, S., 5-AFM-2, 159-AFM-8 Fievisohn, R., 181-HSABP-5 Di Donato, P., 380-IS-12 Drachinsky, A., 43-SD-2 Edoh, A., 63-FD-8 Ertveldt, J., 395-SD-19 Figueroa, J., 380-IS-12 Di Francesco, G., 124-GNC-13 Drake, M., 404-ACD-7 Edstrand, A., 364-APA-36 Ervin, B., 250-TP-6 Finley, D., 9-APA-3, 363-APA-35 Di Vito, V., 100-UMS-1 Drakes, J., 243-PDL-13 Edwards, C., 425-GNC-42 Esker, L., 350-SOF-1 Fiola, C., 410-APA-40 Dianics, J., 364-APA-36 Draper-Donley, M., 56-AFM-4 Edwards, J., 12-FD-2, 68-FD-13, 76-HSABP-2, 1 Etienne, S., 63-FD-8, 161-APA-16 Fiore, G., 311-APA-31 Dias, J., 308-AFM-11 Drela, M., 17-GEPC-1, 356-ABPSI-2 13-APA-12, 170-FD-22 Eun, W., 394-SD-18 Fischer, C., 286-NDA-6 Dias dos Santos, A., 75-GTE-2 Dress, D., 349-SE-1, 396-SE-2 Edwards, M., 256-AMT-4 Everhart, J., 429-GT-11 Fish, J., 399-STR-18 DiCarlo, A., 435-SD-21 Dressel, L., 27-IS-1 Edwards, S., 406-AFM-15 Eversman, W., 3-AA-1 Fisher, A., 216-APA-22 Diebold, J., 257-APA-25 Drikakis, D., 68-FD-13, 169-FD-21, 269-FD-38 Egolf, T., 114-APA-13, 260-APA-28, 365-APA-37 Ewere, F., 262-AS-5 Fisher, T., 441-TP-11 Diep, M., 350-SOF-1 Driscoll, J., 41-PC-4, 112-APA-11, 318-FD-40, 331-GTE-7 Egorov, I., 49-TP-1 Eymann, T., 10-APA-4, 217-APA-23 Flade, S., 271-GEPC-4/SAT-1 DiGirolamo, E., 357-ACD-5 Driscoll, R., 130-HSABP-3, 181-HSABP-5, Ehrhardt, D., 147-SD-7, 436-SD-22 Ezekoye, O., 235-MAT-9 Fladung, W., 436-SD-22 Ding, S., 299-TES-1 230-HSABP-7, 279-HSABP-9/GTE-8 Ehrmann, R., 101-WE-3 Ezhov, I., 49-TP-1 Flamm, J., 69-GEPC-2 Dinsmore, C., 315-AS-6 Droney, C., 17-GEPC-1 Eiler, J., 349-SE-1 Fabbi, G., 79-ISC-2 Flansburg, B., 96-STR-5 Dinzl, D., 62-FD-7 Drozdov, S., 222-FD-30 Eisenhauer, N., 191-PC-11 Fabiano, E., 381-MDO-9 Flatau, A., 367-AS-7 Dionisio, S., 328-GNC-34 Druyor, C., 188-MVC-4 Eitelberg, G., 23-GT-1 Fagley, C., 58-APA-6, 314-APA-34 Fleischmann, J., 79-ISC-2 Diosady, L., 65-FD-10 Du, Y., 263-FD-32 Ekaterinaris, J., 12-FD-2, 118-FD-15, 170-FD-22, Fahim, A., 401-TES-3, 439-TES-4 Fleming, P., 253-WE-10 Dipace, A., 148-STR-7 Duan, L., 173-FD-25 263-FD-32 Fahringer, T., 256-AMT-4 Fletcher, T., 199-STR-11 Dippold, V., 156-AA-5 Duan, P., 166-DA-1 Ekici, K., 302-WE-11 Falk, U., 44-SD-3 Flock, A., 26-HSABP-1 Diskin, B., 371-FD-48 Dubot, T., 251-UMS-4 Eklund, D., 103-APA-9/NDA-1 Falkiewicz, N., 146-SD-6, 246-SD-13/GEPC-5, Florance, J., 115-APA-14 178 Disotell, K., 313-APA-33 Duda, B., 418-FD-53 Eldred, M., 103-APA-9/NDA-1 347-SD-14 Flores, R., 396-SE-2 Dobre, S., 36-MST-2 Dufrene, A., 277-GT-4, 402-TP-9, 428-GT-10 Eldredge, J., 372-FD-49 Falugi, M., 398-STR-17 Foerster, F., 262-AS-5 Dodwell, T., 199-STR-11, 339-NDA-7 Dulikravich, G., 310-APA-30 Elhadidi, B., 168-FD-20 Fan, H., 65-FD-10 Follen, C., 24-GTE-1 Doepke, E., 262-AS-5 Dulin, D., 2-ISC-1, 84-MDO-3 Elham, A., 84-MDO-3 Fan, I., 380-IS-12 Fong, A., 35-MST-1 Dogan, A., 4-AFM-1, 5-AFM-2, 159-AFM-8, 186-MST-7 Dumitrache, C., 389-PDL-11 ElHaroun, A., 439-TES-4 Fang, E., 97-STR-6, 334-MAT-12, 437-STR-20 Fong, K., 173-FD-25 Dogariu, A., 193-PDL-3 Dumm, H., 79-ISC-2 Eliasson, P., 161-APA-16 Fang, H., 244-SCS-6, 346-SCS-8 Footdale, J., 244-SCS-6 Doggett, W., 52-SCS-1, 346-SCS-8 Dumont, A., 60-APA-8, 371-FD-48 Ellerbroek, J., 100-UMS-1, 122-GNC-11 Fang, J., 222-FD-30 Fork, R., 243-PDL-13 Dolan, B., 192-PC-12, 229-GTE-5 Duncan, G., 258-APA-26 Elliott, J., 366-APA-38 Fares, E., 418-FD-53 Forliti, D., 342-PC-18 Dolan, D., 385-OPS-1 Dunn, S., 428-GT-10 Ellison, G., 89-PC-6 Farnsworth, J., 58-APA-6, 257-APA-25, 364-APA-36 Forslund, A., 339-NDA-7 Doman, D., 225-GNC-22, 273-GNC-26, 327-GNC-33, Dunning, P., 34-MDO-2, 236-MDO-6 Elmiligui, A., 187-MST-8, 218-APA-24, 312-APA-32 Farokhi, S., 50-WE-1, 231-HSABP-8, 408-AMT-9 Forster, E., 189-NDA-4 373-GNC-35 Duong, N., 335-MAT-13 Elshabka, A., 237-MST-9, 338-MST-13 Farsadi, T., 204-WE-8 Forster, M., 364-APA-36 Domber, J., 48-STR-3, 391-SCS-9, 428-GT-10 Dupont, P., 309-AMT-5 Elston, J., 20-GNC-3, 296-SEN-2 Fasanella, N., 31-MAT-1, 95-STR-4 Forsythe, J., 114-APA-13, 217-APA-23, 314-APA-34 Domel, N., 121-FD-18 Duque, E., 285-MVC-5 Emam, S., 245-SD-9 Fasano, G., 100-UMS-1, 296-SEN-2 Fortner, E., 80-ISC-3 Domenico, D., 166-DA-1 Duraisamy, K., 268-FD-37, 370-FD-47 Emami, M., 247-SRE-1 Fasel, H., 364-APA-36, 417-FD-52 Fossati, M., 8-APA-2, 263-FD-32 Domingo, P., 342-PC-18 Duran, A., 95-STR-4 Emerson, B., 91-PC-8 Fear, A., 70-GNC-6 Foster, J., 288-PC-15 Dominguez, J., 247-SRE-1 Durnberg, E., 235-MAT-9 Ender, T., 349-SE-1 Feie, B., 430-IS-13 Fotia, M., 130-HSABP-3, 181-HSABP-5, 230-HSABP-7, Domyancic, L., 239-NDA-5 Dussling, J., 23-GT-1 Engelsen, F., 84-MDO-3 Feigh, K., 350-SOF-1, 397-SOF-2 279-HSABP-9/GTE-8 Donbar, J., 408-AMT-9 Dustin, J., 47-STR-2, 282-MAT-11 Engelstad, S., 47-STR-2, 399-STR-18 Feltrop, E., 312-APA-32, 412-APA-42 Foust, R., 345-SATS-2, 433-SATS-4 Dong, C., 434-SD-20 Dutta, A., 427-GNC-44 Engler, J., 166-DA-1 Fenercioglu, I., 372-FD-49 Francis, W., 52-SCS-1, 195-SCS-4 Dong, H., 310-APA-30 Dutta, D., 408-AMT-9 Enloe, L., 368-FD-45/PDL-9 Feng, R., 235-MAT-9 Francois, G., 93-SD-4 Dong, R., 232-IS-7 Duvall, R., 204-WE-8 Enright, J., 276-GNC-29 Ferguson, F., 169-FD-21, 209-ACD-2, 356-ABPSI-2 Frangenberg, M., 375-GNC-37 Dong, W., 111-APA-10 Dyess, C., 247-SRE-1 Enriquez, M., 202-UMS-3 Ferhat, I., 315-AS-6 Frank, C., 209-ACD-2 Dong, Y., 121-FD-18 Dykman, J., 246-SD-13/GEPC-5, 392-SD-16 Epp, C., 71-GNC-7 Fernandez, H., 69-GEPC-2 Franz, K., 405-ACD-8 Dongmo, J., 325-GNC-31 Dzamba, T., 276-GNC-29 Eppard, W., 163-APA-18 Feron, E., 332-IS-10 Fravolini, M., 28-IS-2, 125-GNC-14 Donnard, A., 72-GNC-8 Eberhard, A., 33-MDO-1 Eppink, J., 62-FD-7 Fertig, R., 184-MAT-7, 282-MAT-11 Frecker, M., 219-AS-4 Doom, J., 143-PC-10 Eberspeaker, P., 441-TP-11 Eppstein, M., 328-GNC-34 Fesq, L., 380-IS-12 Frederickson, K., 389-PDL-11 Dorduncu, M., 97-STR-6, 438-STR-21 Ebnit, A., 342-PC-18 Epstein, B., 413-APA-43 Feszty, D., 436-SD-22 Frediani, A., 148-STR-7, 248-STR-12 Dorrington, G., 231-HSABP-8 Echavarria, C., 5-AFM-2, 80-ISC-3, 108-AFM-5 Erer, K., 21-GNC-4, 178-GNC-19 Fetet, T., 379-GT-9 Freebury, G., 52-SCS-1, 195-SCS-4 Author/Session Chair Index Freihofer, G., 235-MAT-9 Gambone, E., 71-GNC-7 Ghiglino, P., 425-GNC-42 Gomez, A., 138-MST-5 Gray, M., 416-FD-51/PDL-12 French, M., 349-SE-1 Gamma, F., 39-PC-2, 182-HSABP-6, 351-SRE-2 Ghoman, S., 246-SD-13/GEPC-5 Gomez, S., 80-ISC-3 Green, L., 163-APA-18 Frendi, K., 262-AS-5 Gan, J., 93-SD-4, 261-APA-29 Ghoreyshi, M., 64-FD-9, 86-MVC-2, 114-APA-13 Gomroki, M., 328-GNC-34 Green, M., 11-FD-1, 270-FD-39, 322-FD-44 Frere, A., 102-WE-4 Gan, M., 202-UMS-3, 301-UMS-5 Ghose, D., 73-GNC-9, 74-GNC-10, 126-GNC-15, Gong, A., 179-GNC-20 Greenberg, J., 90-PC-7 Fresconi, F., 406-AFM-15, 409-APA-39 Gan, W., 412-APA-42 175-GNC-16 Gong, J., 29-ISC-4 Greendyke, R., 300-TP-7 Frey, T., 45-SEN-1 Gandhi, F., 154-AS-2, 165-AS-3, 196-SD-8, 262-AS-5 Ghosh, R., 349-SE-1 Gonyea, K., 48-STR-3 Greene, C., 387-PC-19 Fricke, T., 56-AFM-4 Gangadharan, S., 116-DE-1, 348-SD-15, 415-FD-50 Ghosh, S., 384-NDA-8 Gonzalez, D., 66-FD-11, 216-APA-22 Gregory, I., 139-MST-6 Friedmann, P., 42-SD-1 Gao, H., 43-SD-2, 429-GT-11 Giannattasio, P., 152-WE-5 Gonzalez, E., 288-PC-15, 331-GTE-7 Gregory, J., 6-AMT-1, 313-APA-33 Frink, N., 64-FD-9, 371-FD-48 Gao, J., 65-FD-10, 106-AA-4 Gibbs, S., 92-SCS-2 Gonzalez, P., 5-AFM-2 Greiser, S., 177-GNC-18 Fritz, L., 382-MST-14 Gao, S., 197-STR-9, 263-FD-32 Gibson, G., 2-ISC-1 Goodliff, S., 127-GT-2, 329-GT-5 Greitzer, E., 17-GEPC-1 Frost, S., 20-GNC-3, 132-ICC-1, 253-WE-10 Gao, X., 65-FD-10, 142-PC-9 Gidzak, V., 402-TP-9 Goorskey, D., 144-PDL-2 Gremillion, G., 224-GNC-21 Frulla, G., 249-STR-13 Garafolo, N., 394-SD-18 Giesy, D., 140-NDA-3 Gopalan, H., 68-FD-13 Greschik, G., 145-SCS-3 Fry, D., 187-MST-8 Garbeff, T., 361-AMT-6/GT-7, 362-AMT-7, 407-AMT-8 Gili, P., 35-MST-1 Gopalarathnam, A., 113-APA-12 Grewal, A., 395-SD-19 Fu, S., 169-FD-21 Garcia, E., 73-GNC-9, 183-IS-6, 358-ACD-6 Gilkey, L., 80-ISC-3 Goppert, J., 301-UMS-5 Griffin, K., 42-SD-1, 347-SD-14 Fuchs, A., 378-GT-8 Garcia, G., 274-GNC-27, 325-GNC-31, 423-GNC-40 Gillard, P., 191-PC-11 Gorbushin, A., 25-HIS-1, 127-GT-2 Griffith, D., 101-WE-3, 152-WE-5 Fuentealba, J., 186-MST-7 Garcia, J., 68-FD-13, 410-APA-40 Gillebaart, E., 59-APA-7 Gord, J., 110-AMT-2, 309-AMT-5 Grimes, J., 36-MST-2 Fuentes, J., 2-ISC-1 Gardner, N., 198-STR-10 Gilligan, E., 376-GNC-38 Gordeyev, S., 144-PDL-2, 223-FD-31 Grinstead, K., 306-ABPSI-1 Fuest, F., 110-AMT-2 Gariepy, M., 366-APA-38 Gimelshein, S., 318-FD-40 Gordnier, R., 223-FD-31 Grisham, J., 432-MVC-6 Fugal, S., 366-APA-38 Garland, M., 61-AS-1 Gingras, D., 237-MST-9, 337-MST-12 Gordon, A., 180-GTE-4, 297-STR-14, 334-MAT-12 Grogan, K., 89-PC-6 Fuggmann, S., 364-APA-36 Garmann, D., 223-FD-31 Girard, J., 249-STR-13 Gore, J., 242-PC-14 Groh, R., 95-STR-4 Fujii, K., 67-FD-12/PDL-1, 78-IS-4, 221-FD-29 Garmendia, D., 159-AFM-8, 358-ACD-6 Girolamo, D., 334-MAT-12 Gorospe, G., 380-IS-12 Gross, A., 269-FD-38, 322-FD-44 Fujikawa, T., 137-MDO-4 Garon, A., 63-FD-8 Gisler, R., 429-GT-11 Gorrell, S., 285-MVC-5, 317-EDU-1 Gross, J., 89-PC-6 Fujimatsu, N., 266-FD-35 Garrard, G., 378-GT-8 Glamm, R., 47-STR-2 Gorton, S., 196-SD-8 Grossir, G., 119-FD-16 Fujino, T., 343-PDL-7 Garrett, S., 418-FD-53 Glass, C., 115-APA-14 Gotika, P., 383-MST-15 Grover, M., 353-TP-8 179 Fujita, K., 201-TP-5 Gary, A., 210-ACD-3 Glauser, M., 156-AA-5 Goto, T., 250-TP-6 Gruenwald, B., 28-IS-2, 125-GNC-14 Fukao, T., 151-UMS-2 Gasch, M., 300-TP-7 Glaz, B., 42-SD-1, 146-SD-6, 220-FD-28 Goulart, P., 44-SD-3 Grunewald, E., 332-IS-10 Fukuda, Y., 273-GNC-26 Gassmann, V., 36-MST-2 Glaze, D., 289-PC-16 Gour, S., 74-GNC-10 Grunwald, W., 85-MST-4 Fukushima, S., 273-GNC-26 Gates, A., 116-DE-1 Glazkov, S., 127-GT-2 Govindaraju, P., 107-ACD-1 Guala, M., 51-WE-2 Fulayter, R., 278-GTE-6 Gath, P., 22-GNC-5, 72-GNC-8 Gleize, V., 371-FD-48 Goyal, V., 97-STR-6, 400-STR-19 Guan, Q., 89-PC-6 Fulcher, J., 346-SCS-8 Gatlin, G., 57-APA-5, 112-APA-11 Glezer, A., 171-FD-23 Goyne, C., 76-HSABP-2 Guangxing, W., 158-AFM-7, 216-APA-22 Funaki, I., 130-HSABP-3, 181-HSABP-5, 343-PDL-7 Gayretli, A., 195-SCS-4 Go, T., 55-AFM-3 Gözcü, O., 204-WE-8 Guardone, A., 189-NDA-4, 366-APA-38 Funk, C., 246-SD-13/GEPC-5 Gebre-Egziabher, D., 20-GNC-3 Gobal, K., 161-APA-16 Grady, N., 41-PC-4, 192-PC-12, 266-FD-35 Guelhan, A., 26-HSABP-1, 109-AFM-6, 369-FD-46 Fursht, G., 274-GNC-27 Gedeon, C., 357-ACD-5 Godar, T., 79-ISC-2 Graff, E., 164-APA-19/FD-19 Guerrant, D., 92-SCS-2 Furuya, H., 92-SCS-2, 145-SCS-3 Geerts, J., 309-AMT-5 Godard, J., 228-GT-3 Graham, C., 410-APA-40 Gugala, M., 63-FD-8, 415-FD-50 Fusco, J., 427-GNC-44 Geigle, K., 41-PC-4 Godines, C., 399-STR-18 Graham, J., 152-WE-5 Guha, T., 364-APA-36 Fusi, F., 61-AS-1, 189-NDA-4, 366-APA-38 Geikie, M., 192-PC-12 Goebel, K., 339-NDA-7, 380-IS-12 Gramanzini, J., 60-APA-8 Gui, H., 377-GNC-39 Gabet Hoffmeister, K., 110-AMT-2 Geister, D., 251-UMS-4 Goetzke, E., 33-MDO-1 Grandhi, R., 161-APA-16, 286-NDA-6, 297-STR-14 Guillen, E., 75-GTE-2 Gade, S., 324-GNC-30 Gejji, R., 331-GTE-7 Goff, G., 22-GNC-5 Granlund, K., 11-FD-1, 223-FD-31, 269-FD-38, Guilmineau, E., 14-FD-4 Gaffey, T., 294-SD-11 Geldermans, P., 4-AFM-1 Gogulapati, A., 146-SD-6, 327-GNC-33, 347-SD-14, 372-FD-49 Guimard, J., 438-STR-21 Gagnon, H., 60-APA-8, 148-STR-7 Gentile, V., 322-FD-44 435-SD-21 Grannan, N., 128-GTE-3 Guimond, S., 174-FD-26 Gai, S., 201-TP-5 George, B., 221-FD-29 Gokoglu, S., 351-SRE-2 Grant, M., 4-AFM-1, 55-AFM-3 Guldu, S., 95-STR-4 Gaitonde, D., 66-FD-11, 105-AA-3, 156-AA-5, George, J., 8-APA-2, 216-APA-22 Gokulakrishnan, P., 143-PC-10 Grant, P., 431-MST-16 Gulmammadov, F., 337-MST-12 216-APA-22, 221-FD-29, 322-FD-44 George, T., 184-MAT-7, 334-MAT-12, 335-MAT-13 Goldberg, B., 193-PDL-3 Grantham, T., 335-MAT-13 Gumapas, E., 367-AS-7 Galbraith, M., 13-FD-3, 169-FD-21, 321-FD-43 Georgiadis, N., 68-FD-13 Goldman, B., 295-SD-12 Grappasonni, C., 204-WE-8, 395-SD-19 Gumbert, C., 163-APA-18 Gallagher, J., 301-UMS-5 Geraedts, B., 91-PC-8 Goldstein, D., 353-TP-8 Grassi, M., 296-SEN-2 Gunasekaran, S., 330-GT-6, 372-FD-49 Gallman, J., 105-AA-3 German, B., 357-ACD-5 Gollner, M., 289-PC-16 Grasso, F., 51-WE-2, 102-WE-4, 203-WE-7 Gundy-Burlet, K., 397-SOF-2 Gallo, E., 76-HSABP-2 Geubelle, P., 149-STR-8 Gollnick, V., 349-SE-1 Gratton, G., 159-AFM-8 Guo, H., 214-APA-20, 312-APA-32 Gallopoulos, E., 12-FD-2 Ghaffari, F., 163-APA-18 Golubev, V., 3-AA-1, 168-FD-20 Grauer, J., 308-AFM-11 Guo, N., 291-PDL-6 Gamba, M., 112-APA-11, 242-PC-14, 256-AMT-4, Ghaffari, M., 199-STR-11 Goman, M., 159-AFM-8 Graves, R., 103-APA-9/NDA-1, 112-APA-11, 363-APA-35 Guo, P., 142-PC-9 318-FD-40, 342-PC-18, 378-GT-8 Ghafourizadeh, M., 440-TP-10 Gomariz-Sancha, A., 214-APA-20 Grawunder, M., 14-FD-4 Guo, T., 306-ABPSI-1 Gamble, G., 151-UMS-2 Ghanavati, M., 28-IS-2 Gombolay, M., 232-IS-7 Gray, J., 218-APA-24, 279-HSABP-9/GTE-8, 323-GEPC-3, Guo, X., 185-MDO-5, 409-APA-39 Gamble, K., 396-SE-2 Ghate, A., 153-WE-6 Gomes, W., 423-GNC-40 336-MDO-8 Guo, Y., 198-STR-10, 255-AA-8 Author/Session Chair Index Gupta, A., 186-MST-7, 401-TES-3, 407-AMT-8, Hancock, B., 80-ISC-3 Hay, A., 63-FD-8, 161-APA-16 Hillebrandt, M., 92-SCS-2 Hoos, K., 399-STR-18 439-TES-4 Hand, J., 200-SUR-1 Hayman, G., 50-WE-1, 252-WE-9 Hillewaert, K., 13-FD-3, 102-WE-4 Hopping, E., 80-ISC-3 Gurfil, P., 179-GNC-20, 374-GNC-36 Handschuh, K., 358-ACD-6 Haywood, J., 62-FD-7 Himeno, T., 128-GTE-3 Horn, K., 306-ABPSI-1 Gurfinkel, A., 397-SOF-2 Hangal, S., 36-MST-2 He, C., 187-MST-8 Himmler, A., 36-MST-2 Horne, J., 31-MAT-1 Gursoy, G., 158-AFM-7, 424-GNC-41 Hanhan, I., 235-MAT-9 He, F., 426-GNC-43 Hinckley, D., 328-GNC-34 Hornig, A., 86-MVC-2 Gursul, I., 265-FD-34, 372-FD-49 Hanlon, N., 77-IS-3 He, G., 372-FD-49 Hind, M., 203-WE-7 Hornung, H., 110-AMT-2, 378-GT-8 Gururaja, S., 199-STR-11 Hannan, M., 176-GNC-17 He, J., 106-AA-4 Hine, D., 217-APA-23 Hornung, M., 8-APA-2 Gustafson, P., 198-STR-10 Hannemann, K., 6-AMT-1 He, Y., 160-APA-15 Hines, G., 71-GNC-7 Horta, L., 92-SCS-2 Gutierrez, J., 75-GTE-2 Hansen, J., 397-SOF-2 He, Z., 24-GTE-1, 364-APA-36 Hinkle, J., 52-SCS-1, 346-SCS-8 Hosack, W., 345-SATS-2 Gutierrez, L., 335-MAT-13 Hansen, L., 80-ISC-3, 399-STR-18 Heald, J., 298-STR-15 Hinman, W., 7-APA-1 Hosder, S., 60-APA-8, 189-NDA-4, 381-MDO-9 Gutman, S., 21-GNC-4 Hansen, M., 332-IS-10 Heard, M., 80-ISC-3 Hipp, K., 265-FD-34 Hoskin, A., 48-STR-3 Gutmark, E., 54-AA-2, 106-AA-4, 128-GTE-3, Hanson, C., 376-GNC-38 Heath, C., 218-APA-24 Hirai, K., 300-TP-7 Hosseinverdi, S., 417-FD-52 130-HSABP-3, 181-HSABP-5, 192-PC-12, 229-GTE-5, Hanson, R., 242-PC-14 Hebert, C., 147-SD-7, 245-SD-9 Hirasawa, R., 276-GNC-29 Hosseinzadeh-Nik, Z., 63-FD-8 230-HSABP-7, 279-HSABP-9/GTE-8, 319-FD-41 Hao, A., 31-MAT-1 Heeb, N., 106-AA-4 Hirato, Y., 113-APA-12 Housley, P., 51-WE-2 Guzik, S., 65-FD-10 Hao, T., 194-SATS-1 Heeg, J., 93-SD-4 Hirsch, C., 65-FD-10, 264-FD-33 Housman, J., 163-APA-18 Haas, M., 387-PC-19 Hao, Y., 153-WE-6 Heid, M., 202-UMS-3 Hirsh, R., 71-GNC-7 Hovakimyan, N., 28-IS-2, 123-GNC-12, 232-IS-7, Habashi, W., 8-APA-2, 263-FD-32 Harada, A., 225-GNC-22, 273-GNC-26 Heidmann, J., 323-GEPC-3 Hirt, S., 259-APA-27, 356-ABPSI-2 324-GNC-30 Habbit, R., 108-AFM-5 Haraguchi, R., 429-GT-11 Heim, D., 364-APA-36 Hitachi, Y., 377-GNC-39 Hövelmann, A., 14-FD-4, 64-FD-9 Hackel, J., 249-STR-13 Hardalupas, Y., 40-PC-3, 90-PC-7 Heineck, J., 361-AMT-6/GT-7, 362-AMT-7, 407-AMT-8 Hitt, D., 241-PC-13, 328-GNC-34, 345-SATS-2 How, J., 125-GNC-14, 132-ICC-1, 251-UMS-4 Hackenberg, D., 100-UMS-1 Hardash, J., 271-GEPC-4/SAT-1 Heintz, K., 223-FD-31 Hitzel, S., 14-FD-4, 64-FD-9 Howar, F., 397-SOF-2 Hadaegh, F., 123-GNC-12, 345-SATS-2 Hariharan, N., 10-APA-4, 114-APA-13, 217-APA-23, Heister, S., 388-PC-20 Ho, J., 62-FD-7 Howard, K., 51-WE-2 Haddad, W., 177-GNC-18 260-APA-28, 314-APA-34, 365-APA-37 Heitland, C., 83-MAT-4 Hoang, T., 98-TP-2, 150-TP-4 Howard, M., 150-TP-4 Hadden, C., 149-STR-8 Hariton, E., 72-GNC-8 Helm, C., 222-FD-30 Hockley, C., 151-UMS-2 Howison, J., 302-WE-11 Hafer, W., 425-GNC-42 Harris, C., 54-AA-2 Helsen, R., 373-GNC-35 Hodge, L., 154-AS-2 Hrinda, G., 244-SCS-6 180 Haftka, R., 140-NDA-3, 185-MDO-5, 336-MDO-8, Harris, M., 12-FD-2, 253-WE-10 Hemati, M., 223-FD-31 Hodges, D., 434-SD-20 Hsu, P., 309-AMT-5 339-NDA-7 Harris, R., 3-AA-1 Hempley, L., 139-MST-6 Hodigere Siddaramaiah, V., 393-SD-17 Hu, C., 426-GNC-43 Haga, T., 161-APA-16, 172-FD-24 Harstad, K., 289-PC-16 Hemsch, M., 103-APA-9/NDA-1 Hoekstra, J., 100-UMS-1, 122-GNC-11 Hu, D., 390-SATS-3 Hagen, B., 219-AS-4 Hart, K., 108-AFM-5, 167-DE-2 Henfling, J., 269-FD-38, 277-GT-4 Hoenisch, S., 26-HSABP-1 Hu, F., 106-AA-4 Hagerott, S., 5-AFM-2, 186-MST-7, 338-MST-13 Hartfield, R., 211-AFM-9 Hening, S., 28-IS-2 Hoff, B., 343-PDL-7 Hu, H., 8-APA-2, 75-GTE-2, 98-TP-2, 252-WE-9, Hahn, A., 210-ACD-3 Hartl, D., 154-AS-2, 315-AS-6 Henne, U., 6-AMT-1, 329-GT-5 Hofferth, J., 62-FD-7 256-AMT-4, 354-WE-13 Haimes, R., 285-MVC-5 Hartmann, J., 430-IS-13 Henry, D., 125-GNC-14 Hoffman, J., 247-SRE-1 Hu, M., 312-APA-32 Hajek, M., 383-MST-15 Hartmann, R., 170-FD-22 Henry, E., 198-STR-10, 239-NDA-5 Hoffmann, K., 414-CMS-1 Hu, Q., 70-GNC-6, 227-GNC-24, 292-SCS-7 Hajj, M., 313-APA-33 Hartmann, U., 361-AMT-6/GT-7 Hensch, A., 228-GT-3 Hofmann, D., 292-SCS-7 Hu, Y., 291-PDL-6, 321-FD-43, 398-STR-17 Hakojima, H., 357-ACD-5 Hartwig, J., 98-TP-2 Herald, W., 36-MST-2 Hoke, J., 130-HSABP-3, 181-HSABP-5, 230-HSABP-7, Hu, Z., 59-APA-7, 84-MDO-3, 107-ACD-1 Hale, L., 324-GNC-30, 384-NDA-8 Haruki, M., 227-GNC-24 Hereth, L., 50-WE-1, 51-WE-2 279-HSABP-9/GTE-8, 331-GTE-7, 341-PC-17 Hua, C., 406-AFM-15 Hale, R., 96-STR-5 Harvazinski, M., 342-PC-18 Herges, T., 51-WE-2, 153-WE-6 Holden, J., 271-GEPC-4/SAT-1 Huang, A., 17-GEPC-1 Halila, G., 258-APA-26 Harvin, S., 378-GT-8 Herman, F., 350-SOF-1 Holden, M., 277-GT-4, 402-TP-9 Huang, C., 331-GTE-7 Hall, C., 411-APA-41 Hasanzadeh Lashkajani, K., 188-MVC-4 Herrera, C., 436-SD-22 Holguin, A., 429-GT-11 Huang, G., 68-FD-13, 420-FD-55 Hall, D., 17-GEPC-1, 215-APA-21 Hasel, K., 17-GEPC-1 Herrington, J., 154-AS-2 Holley, A., 387-PC-19 Huang, P., 244-SCS-6 Hall, L., 163-APA-18 Hash, D., 201-TP-5 Hesh, C., 441-TP-11 Hollingsworth, K., 277-GT-4 Huang, W., 325-GNC-31 Hall, N., 249-STR-13 Hashemi, A., 250-TP-6 Heyde, E., 120-FD-17, 420-FD-55 Hollkamp, J., 245-SD-9 Huang, Y., 322-FD-44 Haller, T., 119-FD-16 Hashemi, M., 151-UMS-2, 202-UMS-3 Hickel, S., 174-FD-26 Holst, T., 285-MVC-5 Hubner, J., 270-FD-39 Hallissy, B., 10-APA-4, 217-APA-23 Hassan, A., 390-SATS-3 Hicken, J., 185-MDO-5, 283-MDO-7, 413-APA-43 Holup, A., 330-GT-6 Hückelheim, J., 63-FD-8 Halpin, K., 159-AFM-8 Hassan, E., 131-HSABP-4 Hield, P., 128-GTE-3 Holycross, C., 184-MAT-7, 334-MAT-12, 335-MAT-13 Hudson, J., 427-GNC-44 Halter, F., 191-PC-11 Hassan, H., 121-FD-18, 131-HSABP-4 Hiepler, D., 285-MVC-5 Holzapfel, F., 56-AFM-4, 125-GNC-14, 224-GNC-21, Hudson, L., 429-GT-11 Hamilton, T., 139-MST-6 Hassan, S., 356-ABPSI-2 Higgins, S., 78-IS-4 324-GNC-30, 373-GNC-35, 425-GNC-42 Hudson, T., 29-ISC-4 Hamlington, P., 268-FD-37 Hassanaly, M., 91-PC-8 Higuchi, K., 145-SCS-3 Holzwarth, R., 399-STR-18 Hueckelheim, J., 415-FD-50 Hamman, M., 299-TES-1 Hassouneh, M., 179-GNC-20 Higuera Caubilla, D., 417-FD-52 Homola, J., 138-MST-5 Huehne, C., 92-SCS-2, 168-FD-20, 391-SCS-9 Han, C., 85-MST-4, 237-MST-9 Hatem, F., 439-TES-4 Hilario, M., 343-PDL-7 Honami, S., 168-FD-20 Huelskamp, B., 91-PC-8, 143-PC-10, 213-AMT-3 Han, D., 291-PDL-6 Hatori, R., 375-GNC-37 Hilbert, C., 278-GTE-6 Hong, G., 237-MST-9, 337-MST-12 Huertas, A., 71-GNC-7 Han, J., 9-APA-3, 67-FD-12/PDL-1, 237-MST-9, Hauris, F., 367-AS-7 Hill, A., 176-GNC-17 Hong, S., 32-MAT-2 Hug, S., 418-FD-53 438-STR-21 Haw, W., 331-GTE-7 Hill, M., 82-MAT-3 Hooker, J., 312-APA-32 Hughes, C., 69-GEPC-2, 408-AMT-9 Author/Session Chair Index Hughes, M., 109-AFM-6, 402-TP-9 Iovnovich, M., 42-SD-1 Jeffers, W., 151-UMS-2 Johnston, G., 407-AMT-8 Kameya, Y., 168-FD-20 Hughes, R., 391-SCS-9 Ippolito, C., 28-IS-2 Jegley, D., 69-GEPC-2, 398-STR-17 Johnston, J., 83-MAT-4 Kamita, T., 244-SCS-6 Hugon, F., 225-GNC-22, 272-GNC-25, 373-GNC-35, Irsch, M., 171-FD-23 Jemcov, A., 120-FD-17, 144-PDL-2, 263-FD-32, Jolly, B., 108-AFM-5 Kamiya, T., 377-GNC-39 424-GNC-41 Isaksson, O., 339-NDA-7 331-GTE-7 Jones, A., 113-APA-12, 150-TP-4, 223-FD-31, Kampoon, J., 159-AFM-8 Hull, P., 149-STR-8 Ishida, A., 57-APA-5 Jenaro-Rabadan, G., 58-APA-6 250-TP-6, 270-FD-39, 311-APA-31, 372-FD-49, Kan, P., 156-AA-5 Hull, R., 126-GNC-15, 408-AMT-9 Ishida, T., 70-GNC-6 Jenie, Y., 100-UMS-1, 122-GNC-11 418-FD-53 Kanamori, M., 261-APA-29 Hulse, M., 52-SCS-1, 195-SCS-4 Ishihara, J., 138-MST-5 Jenkins, J., 217-APA-23, 233-IS-8 Jones, G., 329-GT-5, 411-APA-41 Kanazaki, M., 112-APA-11 Humbert, J., 4-AFM-1, 22-GNC-5, 158-AFM-7, Ishihara, K., 130-HSABP-3 Jennings, A., 52-SCS-1 Jones, M., 285-MVC-5 Kanda, H., 259-APA-27 224-GNC-21 Ishihara, T., 49-TP-1, 201-TP-5 Jennions, I., 380-IS-12 Jones, R., 336-MDO-8, 372-FD-49 Kaneshige, J., 232-IS-7, 325-GNC-31 Humphrey, L., 91-PC-8 Ishii, H., 157-AA-6 Jensen, E., 282-MAT-11 Jones, S., 35-MST-1 Kang, C., 58-APA-6 Hunsaker, D., 59-APA-7 Ishii, T., 208-AA-7 Jeon, H., 376-GNC-38 Jones, T., 52-SCS-1, 275-GNC-28, 346-SCS-8 Kang, J., 394-SD-18, 441-TP-11 Hunt, J., 57-APA-5 Ishimura, K., 48-STR-3, 292-SCS-7 Jeon, M., 252-WE-9 Jones, W., 86-MVC-2, 188-MVC-4, 432-MVC-6 Kang, S., 374-GNC-36 Hunt, S., 138-MST-5 Isola, D., 263-FD-32 Jeong, J., 382-MST-14 Jonkman, B., 302-WE-11 Kang, W., 427-GNC-44 Huo, H., 388-PC-20 Ito, E., 202-UMS-3 Jesus, A., 266-FD-35 Jonkman, J., 50-WE-1, 252-WE-9, 302-WE-11 Kanner, S., 50-WE-1 Huo, W., 402-TP-9 Ito, Y., 10-APA-4, 98-TP-2, 250-TP-6, 259-APA-27 Jewell, J., 119-FD-16, 378-GT-8 Joo, J., 219-AS-4, 258-APA-26 Kanno, T., 286-NDA-6 Hurley, O., 101-WE-3 Iuliana, C., 82-MAT-3 Jha, R., 367-AS-7 Jorris, T., 406-AFM-15 Kanoria, A., 162-APA-17 Husen, N., 6-AMT-1 Iuliano, E., 366-APA-38 Ji, A., 151-UMS-2 Joseph, A., 97-STR-6 Kanzawa, T., 227-GNC-24 Hutchins, A., 232-IS-7 Ivanco, T., 115-APA-14 Ji, L., 117-FD-14 Joshi, A., 22-GNC-5, 347-SD-14 Kaul, U., 266-FD-35, 320-FD-42 Huxdorf, O., 165-AS-3 Iwasaki, Y., 343-PDL-7 Ji, W., 97-STR-6, 197-STR-9 Joshi, D., 279-HSABP-9/GTE-8 Kao, D., 285-MVC-5 Huynh, H., 118-FD-15, 220-FD-28, 264-FD-33 Ixtabalan, D., 301-UMS-5 Jia, Y., 227-GNC-24, 291-PDL-6, 292-SCS-7 Joshi, R., 398-STR-17 Kao, J., 33-MDO-1, 185-MDO-5 Hwang, I., 226-GNC-23, 232-IS-7, 276-GNC-29, Iyer, S., 289-PC-16 Jiang, F., 147-SD-7 Jost, A., 215-APA-21 Kapadia, S., 321-FD-43 301-UMS-5 Izumi, T., 59-APA-7 Jiang, N., 91-PC-8, 110-AMT-2, 256-AMT-4 Josyula, E., 99-TP-3, 119-FD-16 Kapaku, R., 242-PC-14 Hwang, J., 33-MDO-1, 185-MDO-5, 260-APA-28 Jackson, B., 338-MST-13, 383-MST-15 Jimenez, B., 214-APA-20 Joulia, A., 251-UMS-4 Kapania, R., 33-MDO-1, 244-SCS-6, 245-SD-9, Hyer, M., 149-STR-8, 249-STR-13 Jackson, C., 415-FD-50 Jimenez, H., 107-ACD-1 Jovanov, K., 42-SD-1 246-SD-13/GEPC-5, 298-STR-15, 400-STR-19, 181 Hynds, T., 94-SD-5 Jackson, D., 98-TP-2 Jimenez Garcia, A., 365-APA-37 Jovic, S., 350-SOF-1 434-SD-20, 438-STR-21 Iannelli, A., 248-STR-12 Jackson, T., 191-PC-11 Jimenez Soler, P., 202-UMS-3 Jrad, M., 33-MDO-1 Kapat, J., 213-AMT-3 Iarve, E., 399-STR-18 Jacob, J., 214-APA-20, 301-UMS-5, 405-ACD-8 Jin, J., 149-STR-8 Ju, Y., 38-PC-1, 89-PC-6, 91-PC-8, 142-PC-9, 143-PC-10, Kara, K., 214-APA-20 Ibrahim, S., 401-TES-3 Jacobellis, G., 196-SD-8 Jin, Z., 390-SATS-3 289-PC-16, 343-PDL-7 Karagozian, A., 63-FD-8 Ichter, B., 354-WE-13 Jacobs, R., 384-NDA-8 Jing, C., 237-MST-9 Juang, J., 92-SCS-2 Karakaya, S., 195-SCS-4 Idan, M., 73-GNC-9, 274-GNC-27 Jacobson, K., 365-APA-37 Jinks, E., 259-APA-27 Juhasz, O., 186-MST-7 Karimi, N., 91-PC-8 Ifju, P., 336-MDO-8 Jacques, D., 273-GNC-26 Jinlu, Y., 241-PC-13 Juliano, T., 369-FD-46 Karl, C., 195-SCS-4 Ihi, R., 161-APA-16 Jafarnejadsani, H., 28-IS-2 Jirasek, A., 86-MVC-2, 93-SD-4, 114-APA-13, Jumper, E., 144-PDL-2, 330-GT-6 Karlgaard, C., 109-AFM-6 Ihme, M., 89-PC-6, 118-FD-15, 208-AA-7, 289-PC-16 Jaffe, R., 99-TP-3 161-APA-16 Jun, B., 178-GNC-19 Karman, S., 188-MVC-4, 432-MVC-6 Ilario da Silva, C., 357-ACD-5 Jagtap, S., 91-PC-8 Jo, Y., 283-MDO-7 Junell, J., 423-GNC-40 Karns, A., 309-AMT-5 Im, D., 161-APA-16 Jaiman, R., 68-FD-13 Jodeh, N., 18-GNC-1, 45-SEN-1 Jurkovich, M., 258-APA-26 Karpel, M., 394-SD-18 Im, H., 90-PC-7, 93-SD-4, 289-PC-16 Jain, A., 147-SD-7 Joerger, M., 100-UMS-1 Justice, R., 271-GEPC-4/SAT-1 Karwas, A., 85-MST-4 Imada, T., 376-GNC-38 Jain, N., 420-FD-55 Johann, U., 22-GNC-5, 72-GNC-8 Jutte, C., 236-MDO-6 Kasahara, J., 130-HSABP-3, 181-HSABP-5 Imaizumi, T., 261-APA-29 Jain, R., 217-APA-23, 260-APA-28 Johansen, C., 7-APA-1, 131-HSABP-4, 213-AMT-3 Kading, B., 390-SATS-3 Kashitani, M., 257-APA-25 Imamura, T., 162-APA-17 James, G., 346-SCS-8 Johnsen, E., 118-FD-15 Kaemming, T., 130-HSABP-3 Kasik, D., 332-IS-10 Imiela, M., 302-WE-11 James, K., 69-GEPC-2 Johnson, A., 176-GNC-17 Kageyama, K., 138-MST-5 Kassab, A., 174-FD-26 Imran, M., 320-FD-42 James, M., 82-MAT-3 Johnson, B., 75-GTE-2 Kahlen, F., 116-DE-1 Kast, S., 415-FD-50 Imtiaz, H., 268-FD-37 Jameson, A., 60-APA-8, 220-FD-28 Johnson, D., 43-SD-2, 436-SD-22 Kahsai, T., 397-SOF-2 Kaste, J., 274-GNC-27 Inagaki, A., 292-SCS-7 Jamoom, M., 100-UMS-1 Johnson, E., 22-GNC-5, 438-STR-21 Kailasanath, K., 54-AA-2, 106-AA-4, Kastengren, A., 40-PC-3 Inclan, E., 358-ACD-6 Jang, D., 77-IS-3 Johnson, H., 369-FD-46, 402-TP-9 279-HSABP-9/GTE-8, 341-PC-17 Kastner, J., 54-AA-2 Indig, N., 21-GNC-4 Janoyan, K., 204-WE-8 Johnson, J., 146-SD-6 Kale, S., 234-MAT-8 Kaszynski, A., 286-NDA-6 Ingenito, A., 39-PC-2, 182-HSABP-6, 351-SRE-2 Janson, A., 183-IS-6 Johnson, K., 110-AMT-2 Kalivarapu, V., 185-MDO-5 Katkin, R., 166-DA-1 Ingham, M., 233-IS-8 Janus, J., 185-MDO-5 Johnson, M., 80-ISC-3 Kallo, J., 271-GEPC-4/SAT-1 Kato, T., 343-PDL-7 Ingram, C., 107-ACD-1, 358-ACD-6 Jasmin, A., 297-STR-14 Johnson, N., 302-WE-11 Kaluvan, A., 57-APA-5 Katoshevski, D., 90-PC-7 Inman, D., 147-SD-7 Jatiningrum, D., 72-GNC-8, 85-MST-4 Johnson, R., 76-HSABP-2, 241-PC-13, 269-FD-38 Kalyanam, K., 177-GNC-18 Katsaduros, D., 80-ISC-3 Inoyama, D., 44-SD-3 Javed, U., 437-STR-20 Johnson, T., 324-GNC-30, 379-GT-9 Kamal, A., 237-MST-9, 338-MST-13 Katta, V., 289-PC-16 Inskeep, J., 218-APA-24 Jaworske, D., 235-MAT-9, 335-MAT-13, 351-SRE-2 Johnson, V., 396-SE-2 Kambampati, S., 294-SD-11 Katz, A., 10-APA-4, 117-FD-14, 172-FD-24 Ioppolo, T., 408-AMT-9 Jean-Baptiste, V., 186-MST-7 Johnston, C., 65-FD-10, 99-TP-3 Kamenetskiy, D., 321-FD-43, 366-APA-38 Kauffman, J., 94-SD-5, 262-AS-5 Author/Session Chair Index Kavsaoglu, M., 405-ACD-8 Khorrami, M., 69-GEPC-2 Klingshirn, C., 143-PC-10 Kosmatka, J., 94-SD-5 Kurbatskii, K., 319-FD-41 Kawachi, E., 191-PC-11 Khosravi, S., 236-MDO-6 Klochko, A., 193-PDL-3 Kosztowny, C., 197-STR-9, 298-STR-15 Kurdila, A., 382-MST-14 Kawano, T., 48-STR-3 Khraibut, A., 201-TP-5 Klomparens, R., 318-FD-40 Kotapati, R., 418-FD-53 Kurtz, J., 26-HSABP-1 Kaynak, U., 214-APA-20 Kielb, R., 295-SD-12 Klotz, J., 272-GNC-25 Kotikalpudi, A., 186-MST-7 Kusakawa, Y., 377-GNC-39 Kayran, A., 95-STR-4, 204-WE-8 Kier, T., 44-SD-3, 186-MST-7, 431-MST-16 Klyde, D., 56-AFM-4, 325-GNC-31 Kourdis, P., 89-PC-6, 289-PC-16 Kushner, L., 361-AMT-6/GT-7, 362-AMT-7, 407-AMT-8 Kazanskiy, P., 67-FD-12/PDL-1 Kikuchi, R., 303-WE-12 Knapke, R., 13-FD-3 Kourta, A., 171-FD-23 Kustova, E., 99-TP-3 Kazemi, L., 276-GNC-29 Kilgore, W., 127-GT-2, 329-GT-5 Knight, B., 435-SD-21 Kovvali, R., 434-SD-20 Kusunose, K., 259-APA-27 Ke, J., 68-FD-13 Kilic, M., 20-GNC-3 Knight, D., 120-FD-17 Kowalchuk, S., 36-MST-2, 178-GNC-19 Kutty, P., 109-AFM-6 Kearney, S., 256-AMT-4, 362-AMT-7 Kim, C., 191-PC-11 Knipe, K., 180-GTE-4, 235-MAT-9 Kowaltschek, S., 276-GNC-29, 377-GNC-39 Kuwahara, T., 191-PC-11 Kecskemety, K., 153-WE-6 Kim, D., 301-UMS-5, 348-SD-15, 398-STR-17, Knisely, A., 119-FD-16 Koziel, S., 60-APA-8, 160-APA-15, 189-NDA-4, Kwasa, B., 283-MDO-7 Kedare, S., 337-MST-12 415-FD-50 Knoblach, A., 177-GNC-18, 186-MST-7, 425-GNC-42 381-MDO-9 Kwatny, H., 237-MST-9, 423-GNC-40 Keidar, M., 194-SATS-1 Kim, G., 194-SATS-1 Knopp, T., 169-FD-21 Kraemer, E., 13-FD-3 Kwok, K., 46-STR-1 Keimer, R., 165-AS-3 Kim, H., 34-MDO-2, 94-SD-5, 95-STR-4, 178-GNC-19, Knoth, F., 14-FD-4 Kraft, E., 10-APA-4 Kwon, O., 260-APA-28 Keller, P., 52-SCS-1, 195-SCS-4 236-MDO-6, 367-AS-7, 393-SD-17 Knuts, S., 339-NDA-7 Kreger, S., 408-AMT-9 Kynaston, S., 339-NDA-7 Kelley, C., 101-WE-3 Kim, I., 195-SCS-4 Ko, A., 34-MDO-2, 185-MDO-5 Krenk, S., 438-STR-21 Kypraiou, A., 91-PC-8 Kelly, R., 144-PDL-2 Kim, J., 66-FD-11, 194-SATS-1, 208-AA-7, 374-GNC-36, Kobayashi, K., 78-IS-4 Kriesel, J., 309-AMT-5 Kyriazis, N., 170-FD-22 Kemal, J., 414-CMS-1 438-STR-21 Kobayashi, S., 376-GNC-38 Krishna, Y., 26-HSABP-1 L’Afflitto, A., 177-GNC-18 Kemenov, K., 143-PC-10 Kim, N., 140-NDA-3, 339-NDA-7 Kobayashi, T., 151-UMS-2 Krishnakumar, K., 70-GNC-6 LaBarge, S., 294-SD-11 Kemp, R., 152-WE-5 Kim, S., 194-SATS-1, 273-GNC-26, 382-MST-14 Kober, M., 86-MVC-2 Krishnamurthy, T., 239-NDA-5 Labusch, A., 238-MST-10 Kennedy, C., 151-UMS-2 Kim, T., 102-WE-4, 199-STR-11, 253-WE-10, 339-NDA-7 Koch, H., 428-GT-10 Krishnan, K., 267-FD-36 Lacarbonara, W., 57-APA-5 Kennedy, G., 283-MDO-7, 381-MDO-9 Kim, W., 136-MAT-6 Kochenderfer, M., 27-IS-1, 35-MST-1, 275-GNC-28 Krishnappa, S., 348-SD-15 Lacdao, C., 180-GTE-4 Kennedy, L., 176-GNC-17 Kim, Y., 35-MST-1, 175-GNC-16, 178-GNC-19, Kochersberger, K., 77-IS-3, 375-GNC-37 Krist, S., 163-APA-18 Lachaud, J., 300-TP-7 Kenner, W., 235-MAT-9 273-GNC-26, 426-GNC-43 Kochmann, D., 292-SCS-7 Krizo, M., 144-PDL-2 Lackner, M., 153-WE-6 Kenny, S., 140-NDA-3 Kimmel, K., 57-APA-5 Koga, S., 6-AMT-1, 127-GT-2, 259-APA-27 Krofta, J., 171-FD-23 Lacy, D., 164-APA-19/FD-19 182 Kenway, G., 60-APA-8, 160-APA-15, 236-MDO-6, Kimmel, R., 62-FD-7, 369-FD-46 Kohzai, M., 127-GT-2 Krokhmal, P., 46-STR-1 Lafferty, J., 277-GT-4, 369-FD-46, 378-GT-8 366-APA-38, 413-APA-43 Kindysheva, S., 88-PC-5 Koike, S., 6-AMT-1, 259-APA-27 Kroll, N., 65-FD-10, 220-FD-28, 264-FD-33 Lafleur, J., 21-GNC-4 Kern, Z., 18-GNC-1 King, B., 52-SCS-1 Kokkinakis, I., 169-FD-21 Krott, M., 294-SD-11 LaFontaine, J., 347-SD-14 Kerstein, A., 288-PC-15 King, G., 242-PC-14, 308-AFM-11 Kolmanovsky, I., 424-GNC-41 Krozel, J., 326-GNC-32 Lagoudas, D., 154-AS-2, 234-MAT-8 Keshmiri, S., 274-GNC-27, 325-GNC-31, 408-AMT-9, King, P., 130-HSABP-3, 202-UMS-3, 230-HSABP-7, Kolonay, R., 189-NDA-4, 295-SD-12 Krüger, T., 274-GNC-27 Lai, J., 372-FD-49 423-GNC-40 279-HSABP-9/GTE-8, 331-GTE-7 Kolosa, D., 427-GNC-44 Krüger, W., 43-SD-2 Lai, W., 319-FD-41 Keskin, A., 86-MVC-2 King, R., 62-FD-7, 268-FD-37 Kolter, Z., 435-SD-21 Ku, J., 150-TP-4 Lalit, H., 242-PC-14 Kessler, M., 13-FD-3 Kingston, D., 175-GNC-16 Komadina, S., 209-ACD-2 Kube-McDowell, M., 208-AA-7 Lam, D., 233-IS-8 Kessler, R., 169-FD-21, 420-FD-55 Kino, T., 201-TP-5 Komuro, T., 57-APA-5 Kuehhorn, A., 86-MVC-2 Lam, R., 34-MDO-2 Kessler, S., 315-AS-6 Kirik, J., 76-HSABP-2 Kondoh, Y., 376-GNC-38 Kuether, R., 147-SD-7 Lamacchia, E., 198-STR-10 Ketsdever, A., 291-PDL-6 Kirk, D., 26-HSABP-1 Kong, M., 343-PDL-7 Kuhlman, J., 267-FD-36, 428-GT-10, 441-TP-11 Lamberson, S., 10-APA-4 Keviczky, T., 226-GNC-23 Kirk, L., 49-TP-1 Konrath, R., 228-GT-3, 329-GT-5 Kühn, W., 329-GT-5 Lambert, L., 248-STR-12 Kew, R., 429-GT-11 Kirlik, A., 232-IS-7 Kontis, K., 364-APA-36 Kukreti, S., 183-IS-6, 430-IS-13 Lambert, T., 171-FD-23 Key, N., 278-GTE-6 Kiser, J., 368-FD-45/PDL-9 Kontogiannis, K., 209-ACD-2 Kulakhmetov, M., 99-TP-3 Lammering, T., 404-ACD-7 Keye, S., 127-GT-2 Kitagawa, K., 300-TP-7 Koo, B., 83-MAT-4, 149-STR-8 Kulis, M., 351-SRE-2 Lampinen, M., 268-FD-37 Kezirian, M., 85-MST-4 Kitamura, K., 363-APA-35 Koo, D., 60-APA-8 Kulkarni, C., 380-IS-12 Lampton, A., 56-AFM-4, 225-GNC-22, 325-GNC-31 Khali, E., 113-APA-12 Kivelevitch, E., 77-IS-3, 78-IS-4, 430-IS-13 Koo, H., 41-PC-4 Kulkarni, M., 34-MDO-2, 96-STR-5 Landegger, A., 271-GEPC-4/SAT-1 Khalil, E., 299-TES-1, 401-TES-3, 439-TES-4 Kleb, W., 115-APA-14 Koo, J., 31-MAT-1, 235-MAT-9, 281-MAT-10, Kumar, M., 40-PC-3, 63-FD-8, 74-GNC-10, 78-IS-4, Landman, D., 5-AFM-2 Khalil Hasan, A., 439-TES-4 Klein, C., 6-AMT-1, 329-GT-5 335-MAT-13 202-UMS-3, 226-GNC-23 Lang, A., 11-FD-1 Khalili, A., 367-AS-7 Klein, R., 209-ACD-2 Koo, S., 194-SATS-1 Kumar, P., 382-MST-14 Langel, C., 101-WE-3, 258-APA-26 Khan, A., 438-STR-21 Kleinhenz, J., 247-SRE-1, 351-SRE-2 Koolstra, H., 431-MST-16 Kumar, R., 54-AA-2, 113-APA-12, 269-FD-38, Langley, B., 335-MAT-13 Khan, M., 20-GNC-3, 180-GTE-4 Klenke, R., 124-GNC-13 Koomullil, R., 10-APA-4 364-APA-36, 428-GT-10 Langley, C., 404-ACD-7 Khan, O., 57-APA-5, 112-APA-11, 162-APA-17, Klepper, J., 217-APA-23 Koon, R., 47-STR-2 Kumar, S., 126-GNC-15, 319-FD-41, 400-STR-19, Lani, A., 201-TP-5 180-GTE-4, 356-ABPSI-2 Klepprt, J., 10-APA-4 Kopardekar, P., 332-IS-10 437-STR-20 Lappas, V., 145-SCS-3, 346-SCS-8, 425-GNC-42 Khan, S., 262-AS-5 Klimchenko, V., 311-APA-31 Koric, S., 234-MAT-8 Kumbasar, S., 124-GNC-13 Larchevêque, L., 309-AMT-5 Khanafseh, S., 100-UMS-1 Kliment, L., 393-SD-17, 436-SD-22 Korkut, B., 15-FD-5 Kuntz, D., 300-TP-7 Larsen, G., 303-WE-12 Khieu, L., 118-FD-15 Klimov, A., 67-FD-12/PDL-1 Kosarev, I., 88-PC-5 Kuo, C., 54-AA-2 Larsen, T., 303-WE-12 Khoo, B., 416-FD-51/PDL-12 Kline, S., 151-UMS-2 Koshi, M., 90-PC-7 Kuprowicz, N., 143-PC-10 Larwood, S., 302-WE-11 Author/Session Chair Index LaSarge, J., 433-SATS-4 Lempert, W., 38-PC-1, 88-PC-5, 119-FD-16, 193-PDL-3, Lin, J., 57-APA-5, 164-APA-19/FD-19 Lomba, R., 191-PC-11 Lynde, M., 261-APA-29 Lascara, B., 166-DA-1 243-PDL-13, 389-PDL-11 Lin, K., 40-PC-3, 437-STR-20 Lombaerts, T., 232-IS-7, 325-GNC-31 Lynn, K., 379-GT-9 Laten, J., 368-FD-45/PDL-9 Leng, J., 154-AS-2 Lin, S., 232-IS-7, 334-MAT-12 Long, D., 154-AS-2 Lyons, A., 29-ISC-4 Latz, J., 160-APA-15, 215-APA-21 Lenz, H., 166-DA-1 Lind, A., 418-FD-53 Long, T., 185-MDO-5 Lyrintzis, A., 105-AA-3, 106-AA-4, 208-AA-7 Lau, F., 148-STR-7 Leon, A., 404-ACD-7 Lind, R., 5-AFM-2 Long, W., 426-GNC-43 Lyu, Z., 236-MDO-6, 366-APA-38 Laurence, R., 296-SEN-2 Leone, F., 334-MAT-12, 437-STR-20 Linevsky, M., 289-PC-16 Lööf, J., 339-NDA-7 Ma, B., 213-AMT-3 Laurence, S., 378-GT-8 Leonhardt, B., 308-AFM-11 Ling, Y., 90-PC-7 Looye, G., 238-MST-10, 431-MST-16 Ma, H., 98-TP-2 Laurendeau, E., 111-APA-10, 188-MVC-4 Leonov, S., 119-FD-16, 416-FD-51/PDL-12 Lingenfelter, A., 200-SUR-1 Lopes, L., 323-GEPC-3 Ma, O., 359-AFM-12 Laux, C., 88-PC-5 Lesieutre, D., 409-APA-39 Link, A., 191-PC-11 Lopez, I., 196-SD-8 Mabe, J., 154-AS-2 Lavagnoli, S., 59-APA-7 Lesieutre, G., 46-STR-1, 219-AS-4 Linne, D., 247-SRE-1, 351-SRE-2 Lopp, G., 262-AS-5 Mabson, G., 398-STR-17 Lavandera, P., 297-STR-14 Lester, E., 397-SOF-2 Liou, W., 417-FD-52 Loquen, T., 377-GNC-39 Macdonald, R., 99-TP-3 LaViers, A., 324-GNC-30 Levandowski, C., 339-NDA-7 Lipinski, D., 12-FD-2 Lorain, P., 182-HSABP-6 MacFarlane, M., 4-AFM-1 Lavretsky, E., 373-GNC-35 Levert, M., 349-SE-1 Lisco, B., 235-MAT-9 Lord, W., 17-GEPC-1 Machida, S., 348-SD-15 Lawrence, D., 92-SCS-2, 296-SEN-2 Levesque, A., 188-MVC-4 Litchford, R., 343-PDL-7 Loseille, A., 188-MVC-4, 432-MVC-6 Mackunis, W., 168-FD-20, 424-GNC-41 Lawrence, T., 356-ABPSI-2 LeVett, M., 347-SD-14 Litke, P., 306-ABPSI-1 Loth, E., 180-GTE-4, 218-APA-24, 267-FD-36, MacLean, M., 277-GT-4, 402-TP-9 Lawson, B., 139-MST-6 Levin, D., 15-FD-5, 99-TP-3, 119-FD-16, 318-FD-40 Litt, J., 306-ABPSI-1 354-WE-13 Madavan, N., 17-GEPC-1 Lay, J., 364-APA-36 Lewalle, J., 156-AA-5 Little, J., 318-FD-40, 416-FD-51/PDL-12 Lou, J., 170-FD-22 Madden, M., 383-MST-15 Leal, P., 154-AS-2 Lewis, B., 171-FD-23 Litzinger, T., 289-PC-16 Louis, A., 202-UMS-3 Madenci, E., 97-STR-6, 398-STR-17, 438-STR-21 LeBeau, R., 171-FD-23, 317-EDU-1, 368-FD-45/PDL-9 Lewis, D., 31-MAT-1, 369-FD-46, 407-AMT-8 Liu, B., 373-GNC-35 Louisos, W., 345-SATS-2 Madsen, H., 152-WE-5, 303-WE-12 Lebofsky, S., 293-SD-10 Lewis, M., 66-FD-11, 216-APA-22 Liu, C., 84-MDO-3, 120-FD-17, 121-FD-18, 259-APA-27, Loureiro, N., 56-AFM-4 Maeda, K., 387-PC-19 Leccadito, M., 124-GNC-13 Leyva, I., 119-FD-16, 342-PC-18, 378-GT-8 310-APA-30, 319-FD-41, 418-FD-53, 420-FD-55 Lourier, J., 24-GTE-1 Maffioli, A., 411-APA-41 Lechniak, J., 58-APA-6, 406-AFM-15 Li, C., 88-PC-5, 140-NDA-3, 288-PC-15, 414-CMS-1 Liu, D., 2-ISC-1, 184-MAT-7, 200-SUR-1, 297-STR-14 Lovejoy, A., 398-STR-17 Maggiore, P., 431-MST-16 LeDigabel, S., 366-APA-38 Li, D., 94-SD-5, 169-FD-21, 245-SD-9, 394-SD-18, Liu, F., 208-AA-7, 227-GNC-24 Lowe, C., 251-UMS-4 Magin, T., 440-TP-10 Ledlow, T., 211-AFM-9 409-APA-39 Liu, H., 74-GNC-10, 255-AA-8 Lowe, K., 256-AMT-4, 407-AMT-8 Magree, D., 22-GNC-5 183 LeDoux, S., 60-APA-8, 366-APA-38 Li, H., 126-GNC-15, 256-AMT-4 Liu, J., 106-AA-4, 202-UMS-3, 299-TES-1 Löwe, J., 169-FD-21 Magstadt, A., 156-AA-5, 203-WE-7 Lee, A., 19-GNC-2, 35-MST-1 Li, J., 46-STR-1, 416-FD-51/PDL-12 Liu, K., 172-FD-24, 245-SD-9 Lowenberg, M., 159-AFM-8 Mahadevan, S., 82-MAT-3, 140-NDA-3, 384-NDA-8 Lee, C., 60-APA-8, 69-GEPC-2, 233-IS-8 Li, L., 48-STR-3 Liu, L., 185-MDO-5, 195-SCS-4 Lowry, H., 389-PDL-11 Mahapatra, S., 383-MST-15 Lee, D., 9-APA-3, 161-APA-16, 175-GNC-16, 191-PC-11, Li, M., 344-PDL-8 Liu, M., 227-GNC-24, 292-SCS-7 Lu, F., 230-HSABP-7, 279-HSABP-9/GTE-8, 432-MVC-6 Mahony, D., 150-TP-4 273-GNC-26, 283-MDO-7, 325-GNC-31 Li, S., 241-PC-13 Liu, N., 24-GTE-1, 323-GEPC-3 Lu, H., 35-MST-1 Mai, C., 62-FD-7 Lee, H., 165-AS-3 Li, W., 255-AA-8 Liu, P., 59-APA-7, 113-APA-12, 214-APA-20, 312-APA-32, Lu, L., 222-FD-30 Maiaru, M., 199-STR-11 Lee, J., 58-APA-6, 165-AS-3, 226-GNC-23, 249-STR-13, Li, X., 106-AA-4, 275-GNC-28 437-STR-20 Lu, P., 72-GNC-8, 177-GNC-18, 272-GNC-25, Maina, M., 214-APA-20 314-APA-34, 367-AS-7 Li, Y., 268-FD-37 Liu, Q., 33-MDO-1 374-GNC-36, 376-GNC-38 Mainini, L., 283-MDO-7, 336-MDO-8 Lee, K., 252-WE-9, 377-GNC-39 Li, Z., 99-TP-3, 169-FD-21 Liu, T., 6-AMT-1, 337-MST-12, 372-FD-49 Lu, Y., 172-FD-24, 220-FD-28 Maiti, D., 298-STR-15 Lee, N., 145-SCS-3 Liang, C., 65-FD-10, 172-FD-24, 370-FD-47 Liu, X., 97-STR-6, 291-PDL-6, 334-MAT-12, 437-STR-20 Lua, J., 97-STR-6, 334-MAT-12 Majdalani, J., 79-ISC-2 Lee, S., 50-WE-1, 122-GNC-11, 153-WE-6, 178-GNC-19, Liang, R., 31-MAT-1 Liu, Y., 8-APA-2, 149-STR-8, 187-MST-8, 234-MAT-8, Lucht, R., 110-AMT-2, 143-PC-10, 242-PC-14, Majji, M., 29-ISC-4, 296-SEN-2 191-PC-11, 252-WE-9, 276-GNC-29, 315-AS-6, Liang, Z., 347-SD-14, 435-SD-21 239-NDA-5, 275-GNC-28, 306-ABPSI-1, 402-TP-9, 362-AMT-7 Majumdar, A., 98-TP-2 349-SE-1 Liao, G., 432-MVC-6 405-ACD-8 Luckring, J., 14-FD-4, 64-FD-9 Makarov, A., 26-HSABP-1 Lee, U., 70-GNC-6 Lidor, A., 241-PC-13 Livermore, R., 18-GNC-1, 100-UMS-1 Lugo, M., 184-MAT-7, 281-MAT-10, 282-MAT-11 Makuni, T., 15-FD-5 Lee, W., 200-SUR-1 Lie, F., 20-GNC-3 Livne, E., 293-SD-10, 435-SD-21 Luke, E., 40-PC-3, 105-AA-3 Maldonado, C., 291-PDL-6 Lee, Y., 348-SD-15 Lietz, C., 174-FD-26 Llysenkov, A., 127-GT-2 Luna, M., 71-GNC-7 Malecek, J., 395-SD-19 Lefebvre, A., 162-APA-17 Lieu, M., 17-GEPC-1 Lo, K., 364-APA-36 Lundgren, E., 400-STR-19 Maley, J., 74-GNC-10 Lefkowitz, J., 38-PC-1, 142-PC-9, 343-PDL-7 Lieuwen, T., 41-PC-4, 91-PC-8 Lobbia, M., 160-APA-15 Luo, H., 12-FD-2, 63-FD-8, 118-FD-15, 170-FD-22 Malik, M., 323-GEPC-3 Leger, T., 418-FD-53 Lightfoot, M., 342-PC-18 Löbl, D., 56-AFM-4 Luo, L., 12-FD-2, 51-WE-2, 170-FD-22 Malinek, P., 395-SD-19 Lei, G., 111-APA-10 Lightsey, E., 70-GNC-6, 396-SE-2 Lobser, G., 120-FD-17, 420-FD-55 Luo, W., 169-FD-21 Mallet, M., 264-FD-33 Leicht, T., 65-FD-10, 170-FD-22 Lignarolo, L., 51-WE-2 Lock, G., 299-TES-1 Luo, Z., 198-STR-10 Mallik, W., 246-SD-13/GEPC-5 Leifsson, L., 60-APA-8, 160-APA-15, 189-NDA-4, Liguore, S., 97-STR-6, 348-SD-15 Locke, J., 57-APA-5 Luterbacher, R., 184-MAT-7 Malloy, D., 14-FD-4, 64-FD-9 381-MDO-9 Lillard, R., 49-TP-1 Lofthouse, A., 64-FD-9, 86-MVC-2, 114-APA-13 Lutz, T., 29-ISC-4, 228-GT-3 Malo-Molina, F., 231-HSABP-8 Leitner, M., 186-MST-7 Lim, J., 191-PC-11, 394-SD-18 Logan, M., 100-UMS-1 Lv, Y., 118-FD-15 Malouin, B., 366-APA-38 Lele, S., 153-WE-6, 266-FD-35, 318-FD-40 Lim, T., 72-GNC-8, 441-TP-11 Loh, W., 214-APA-20 Lyford, A., 400-STR-19 Manar, F., 270-FD-39, 372-FD-49 Lemainque, J., 193-PDL-3 Limbach, C., 193-PDL-3, 256-AMT-4 Lohner, R., 15-FD-5 Lyle, K., 92-SCS-2 Mancini, P., 270-FD-39, 372-FD-49 Lemmens, Y., 393-SD-17 Liming, H., 241-PC-13 Lokos, W., 429-GT-11 Lynch, A., 75-GTE-2, 91-PC-8, 110-AMT-2, 213-AMT-3 Mancuso, R., 202-UMS-3 Lemonds, T., 404-ACD-7 Lin, E., 187-MST-8 Lolatte, A., 204-WE-8 Lynch, E., 114-APA-13, 314-APA-34, 341-PC-17 Mandel, O., 72-GNC-8 Author/Session Chair Index Mandell, J., 204-WE-8 Marzuoli, A., 332-IS-10 McClearn, M., 80-ISC-3 Meneghini, J., 255-AA-8 Mina, S., 116-DE-1 Manero, A., 180-GTE-4 Masaki, D., 128-GTE-3 McClung, R., 82-MAT-3 Meng, T., 390-SATS-3 Mine, R., 412-APA-42 Mangina, R., 368-FD-45/PDL-9 Masarati, P., 434-SD-20 McComas, A., 215-APA-21 Menier, V., 432-MVC-6 Minesugi, K., 48-STR-3 Mani, K., 236-MDO-6 Masi, A., 63-FD-8 McCourt, M., 272-GNC-25, 424-GNC-41 Menon, A., 393-SD-17 Minnetyan, L., 399-STR-18 Maniaci, D., 51-WE-2, 101-WE-3, 153-WE-6 Maslov, A., 419-FD-54 McCoy, T., 252-WE-9 Menon, P., 180-GTE-4, 232-IS-7 Minton, T., 300-TP-7 Mankbadi, R., 3-AA-1 Masson, B., 272-GNC-25 McDaniel, D., 10-APA-4, 114-APA-13 Menon, S., 41-PC-4, 172-FD-24, 192-PC-12, 266-FD-35, Mirmirani, M., 100-UMS-1 Mannarino, A., 125-GNC-14 Massotti, L., 427-GNC-44 McDaniel, J., 76-HSABP-2 288-PC-15, 320-FD-42 Mirochnitchenko, V., 33-MDO-1 Mannucci, T., 373-GNC-35 Masters, D., 160-APA-15 McDevitt, M., 241-PC-13 Mercer, J., 138-MST-5 Misaka, T., 157-AA-6, 303-WE-12 Manquinho, P., 356-ABPSI-2, 359-AFM-12 Masters, J., 188-MVC-4, 217-APA-23 McDevitt, T., 362-AMT-7 Meritt, R., 407-AMT-8, 408-AMT-9 Mishra, A., 236-MDO-6 Mansor, S., 257-APA-25, 312-APA-32 Mastorakos, E., 91-PC-8, 192-PC-12 McDonald, R., 210-ACD-3, 357-ACD-5 Merkle, C., 63-FD-8 Mishra, S., 439-TES-4 Mansour, N., 300-TP-7, 417-FD-52, 421-FD-56 Masud, J., 57-APA-5, 112-APA-11, 162-APA-17, McDonough, K., 424-GNC-41 Merrell, M., 33-MDO-1 Misiorowski, M., 165-AS-3 Mao, Y., 337-MST-12 320-FD-42, 356-ABPSI-2 McEver, J., 132-ICC-1 Merrett, C., 46-STR-1, 249-STR-13 Misra, G., 376-GNC-38 Mapes, T., 61-AS-1 Masuda, K., 377-GNC-39 McFarland, J., 82-MAT-3 Merrill, B., 370-FD-47 Mital, S., 82-MAT-3, 249-STR-13 Maqbool, D., 242-PC-14 Masutti, D., 119-FD-16 McFeat, J., 380-IS-12 Merz, C., 311-APA-31 Mitchell, J., 179-GNC-20 Maqueda Jimenez, I., 195-SCS-4 Mat, S., 257-APA-25 McGee, T., 176-GNC-17 Mesbahi, M., 70-GNC-6, 273-GNC-26 Mitchell, T., 301-UMS-5 Marchese, A., 389-PDL-11 Mat Lazim, T., 257-APA-25 McGowan, D., 134-LEC-3 Mesmer, B., 33-MDO-1, 283-MDO-7 Mitsuhashi, R., 151-UMS-2 Marconi Rocco, E., 423-GNC-40 Mataczynski, M., 278-GTE-6 McGowan, G., 211-AFM-9, 409-APA-39 Messac, A., 381-MDO-9 Mittal, A., 50-WE-1, 51-WE-2, 153-WE-6 Marcum, D., 188-MVC-4 Matheis, J., 174-FD-26 McGrath, B., 139-MST-6, 257-APA-25, 409-APA-39 Methel, J., 278-GTE-6 Miura, K., 294-SD-11 Mardanpour, P., 96-STR-5 Mathur, T., 196-SD-8 McGuire, S., 193-PDL-3 Meyer, P., 97-STR-6 Miyake, Y., 291-PDL-6 Marek, J., 197-STR-9 Matlik, J., 0-ICME V&V, 82-MAT-3, 135-MAT-5 McKenna, T., 158-AFM-7 Meyer, R., 184-MAT-7 Miyazato, Y., 412-APA-42 Margosian, K., 58-APA-6 Matlis, E., 62-FD-7 McKiernan, G., 369-FD-46 Meyer, S., 92-SCS-2 Miyazawa, Y., 225-GNC-22, 273-GNC-26 Marineau, E., 309-AMT-5, 369-FD-46, 407-AMT-8 Matney, A., 347-SD-14 McLaughlin, D., 54-AA-2, 204-WE-8, 309-AMT-5, Mezzapesa, S., 395-SD-19 Mizukaki, T., 361-AMT-6/GT-7 Mariotti, A., 140-NDA-3 Matson, E., 301-UMS-5 411-APA-41 Mian, H., 58-APA-6 Moccia, A., 100-UMS-1 Markfort, C., 303-WE-12 Matsuda, H., 225-GNC-22 McLaughlin, T., 26-HSABP-1, 58-APA-6, 67-FD-12/PDL-1, Michaels, D., 42-SD-1 Modgil, G., 140-NDA-3 184 Marks, C., 219-AS-4 Matsumoto, S., 376-GNC-38 314-APA-34, 418-FD-53 Micol, J., 429-GT-11 Moeck, J., 279-HSABP-9/GTE-8 Maron, L., 168-FD-20 Matsumura, T., 361-AMT-6/GT-7 McManus, T., 41-PC-4, 143-PC-10, 213-AMT-3 Mignolet, M., 113-APA-12, 146-SD-6, 147-SD-7, Moghadassian, B., 354-WE-13 Marpu, R., 365-APA-37 Matsuno, Y., 275-GNC-28 McMullan, W., 418-FD-53 347-SD-14, 435-SD-21 Moguel, I., 380-IS-12 Marques, F., 295-SD-12 Matsuo, A., 130-HSABP-3, 181-HSABP-5, 387-PC-19 McNally, J., 171-FD-23 Mignot, J., 425-GNC-42 Mohammed-Taifour, A., 269-FD-38 Marschall, J., 300-TP-7 Matsuoka, A., 377-GNC-39 McNamara, J., 44-SD-3, 146-SD-6, 153-WE-6, Miguel Alfaro, D., 203-WE-7 Mohan, A., 66-FD-11, 221-FD-29 Marsden, O., 106-AA-4 Matsuoka, K., 130-HSABP-3, 181-HSABP-5 327-GNC-33, 339-NDA-7, 347-SD-14, 435-SD-21 Mikkelsen, R., 102-WE-4, 303-WE-12 Mohite, P., 199-STR-11 Marsden, W., 47-STR-2 Matt, A., 439-TES-4 McQuilling, M., 171-FD-23, 419-FD-54 Mikulas, M., 292-SCS-7 Mohseni, K., 12-FD-2, 77-IS-3, 168-FD-20, 226-GNC-23, Marsh, R., 352-TES-2, 439-TES-4 Mattei, M., 124-GNC-13 Medley, J., 253-WE-10 Milbredt, O., 332-IS-10 266-FD-35, 267-FD-36, 327-GNC-33, Marshall, D., 251-UMS-4 Mattos, B., 210-ACD-3 Mehdi, S., 123-GNC-12 Miles, J., 157-AA-6 383-MST-15, 411-APA-41 Marshall, G., 281-MAT-10 Mattson, C., 80-ISC-3 Meheut, M., 60-APA-8 Miles, R., 38-PC-1, 193-PDL-3, 256-AMT-4, 290-PDL-5 Mokhtar, W., 429-GT-11 Martel, J., 108-AFM-5 Matunaga, S., 194-SATS-1 Mehta, M., 351-SRE-2 Milionis, A., 267-FD-36 Moler, M., 5-AFM-2 Martin, A., 49-TP-1, 300-TP-7, 440-TP-10 Matyash, S., 127-GT-2 Mehta, S., 272-GNC-25, 424-GNC-41 Miller, B., 146-SD-6, 347-SD-14 Molina, R., 335-MAT-13 Martin, C., 356-ABPSI-2 Matz, D., 109-AFM-6, 376-GNC-38 Mehta, U., 103-APA-9/NDA-1 Miller, C., 376-GNC-38 Molinari, G., 61-AS-1 Martin, E., 13-FD-3 Maughmer, M., 9-APA-3, 121-FD-18 Mehta, Y., 75-GTE-2 Miller, D., 33-MDO-1, 171-FD-23, 204-WE-8 Molinaro, N., 408-AMT-9 Martin, K., 71-GNC-7 Maul, W., 380-IS-12 Meiboom, M., 20-GNC-3 Miller, E., 429-GT-11 Mollenhauer, D., 399-STR-18 Martin, L., 232-IS-7 Mavriplis, D., 13-FD-3, 117-FD-14, 236-MDO-6, Meid, C., 180-GTE-4 Miller, J., 395-SD-19 Monastero, M., 257-APA-25 Martin, M., 222-FD-30 321-FD-43, 370-FD-47, 381-MDO-9 Meier, W., 143-PC-10 Miller, R., 288-PC-15 Moncayo, H., 100-UMS-1, 272-GNC-25, 301-UMS-5, Martin, R., 198-STR-10 Mavris, D., 107-ACD-1, 132-ICC-1, 157-AA-6, Meinke, M., 420-FD-55 Miller, S., 208-AA-7, 258-APA-26 380-IS-12 Martinez, I., 404-ACD-7 159-AFM-8, 199-STR-11, 209-ACD-2, 236-MDO-6, Meiring, J., 151-UMS-2 Miller, T., 154-AS-2, 342-PC-18 Mondal, K., 373-GNC-35 Martinez, M., 165-AS-3 237-MST-9, 358-ACD-6, 384-NDA-8, 406-AFM-15 Mejia-Ariza, J., 195-SCS-4 Millet, T., 139-MST-6 Monegato, G., 148-STR-7 Martinez Schramm, J., 6-AMT-1 May, G., 432-MVC-6 Mekkes, G., 378-GT-8 Mills, D., 408-AMT-9 Monfort, J., 213-AMT-3 Martins, B., 94-SD-5 Mayeur, J., 371-FD-48 Mele, B., 266-FD-35 Mills, M., 277-GT-4 Mongia, H., 242-PC-14 Martins, J., 33-MDO-1, 60-APA-8, 185-MDO-5, Mazellier, N., 171-FD-23 Mellquist, E., 93-SD-4 Millsaps, K., 180-GTE-4 Mongrard, O., 72-GNC-8 236-MDO-6, 336-MDO-8, 366-APA-38, 413-APA-43 Mazzacavallo, B., 284-MST-11 Melo De Sousa, J., 24-GTE-1, 112-APA-11 Milluzzo, J., 418-FD-53 Monk, D., 278-GTE-6 Martos, D., 112-APA-11 Mazzulla, A., 132-ICC-1 Melvin, R., 366-APA-38 Milos, F., 300-TP-7 Monner, H., 165-AS-3, 219-AS-4 Marx, S., 191-PC-11 McAlister, D., 351-SRE-2 Melvin, S., 411-APA-41 Miltner, M., 166-DA-1 Monnier, B., 221-FD-29 Marzocca, P., 57-APA-5, 149-STR-8, 204-WE-8, McCallum, H., 80-ISC-3 Menart, J., 79-ISC-2 Min, B., 260-APA-28 Montgomery, J., 176-GNC-17 249-STR-13, 394-SD-18, 395-SD-19 McCarthy, D., 196-SD-8 Mendez, B., 203-WE-7 Min, J., 97-STR-6 Moon, G., 178-GNC-19 Author/Session Chair Index Moore, E., 116-DE-1 Müller, J., 63-FD-8, 415-FD-50 Nakajima, Y., 276-GNC-29 Nguyen, J., 35-MST-1 O’Hara, P., 245-SD-9 Moore, F., 211-AFM-9, 409-APA-39 Mummidivarapu, S., 430-IS-13 Nakakita, K., 6-AMT-1, 259-APA-27 Nguyen, L., 3-AA-1, 168-FD-20 Oates, W., 32-MAT-2, 234-MAT-8 Moore, J., 176-GNC-17, 292-SCS-7 Munafò, A., 99-TP-3 Nakamura, R., 427-GNC-44 Nguyen, N., 28-IS-2, 125-GNC-14, 293-SD-10, Obayashi, S., 157-AA-6, 303-WE-12 Moore, L., 211-AFM-9 Munday, D., 130-HSABP-3, 181-HSABP-5, Nakamura, Y., 138-MST-5, 363-APA-35 333-IS-11, 392-SD-16 Obenchain, M., 94-SD-5 Moore, M., 33-MDO-1, 357-ACD-5 279-HSABP-9/GTE-8 Nakane, S., 91-PC-8 Nguyen, T., 342-PC-18 Oberleithner, K., 66-FD-11 Mor, M., 293-SD-10 Munday, P., 171-FD-23 Nakao, S., 257-APA-25 Nguyen Sy, N., 249-STR-13 Ochi, Y., 124-GNC-13, 337-MST-12 Mora, P., 54-AA-2 Mundis, N., 117-FD-14 Nakazawa, H., 300-TP-7 Ni, M., 174-FD-26 Ochs, B., 41-PC-4, 192-PC-12, 266-FD-35 Mora-Camino, F., 179-GNC-20 Munduate, X., 203-WE-7 Nanamori, Y., 227-GNC-24 Nichols, R., 10-APA-4, 217-APA-23, 306-ABPSI-1 Odaguil, F., 219-AS-4 Morajkar, R., 112-APA-11 Munguia, B., 171-FD-23 Nangia, R., 64-FD-9, 93-SD-4, 248-STR-12, 413-APA-43 Nichols, T., 20-GNC-3 Odegard, G., 31-MAT-1, 149-STR-8 Moralev, I., 67-FD-12/PDL-1 Munoz, C., 166-DA-1 Nannapaneni, S., 384-NDA-8 Nickol, C., 69-GEPC-2 ODowd, M., 72-GNC-8 Morandini, M., 434-SD-20 Munson, M., 171-FD-23 Naoumov, V., 191-PC-11, 317-EDU-1 Nie, Y., 238-MST-10, 431-MST-16 Oefelein, J., 41-PC-4, 288-PC-15 Moraru, G., 369-FD-46 Muppidi, S., 49-TP-1 Naples, A., 230-HSABP-7, 341-PC-17 Nielsen, E., 218-APA-24, 323-GEPC-3 Ogawa, H., 67-FD-12/PDL-1, 182-HSABP-6, Morency, F., 429-GT-11 Muralidharan, B., 172-FD-24 Naraghi, M., 32-MAT-2 Niemiec, R., 196-SD-8 231-HSABP-8 Moreno, C., 186-MST-7 Muraoka, K., 124-GNC-13 Narang-Siddarth, A., 274-GNC-27, 425-GNC-42 Niermeyer, P., 324-GNC-30 Ogburn, M., 360-AFM-13 Moreno, R., 295-SD-12 Murayama, M., 259-APA-27 Nardini, M., 248-STR-12 Nieuwenhuizen, F., 139-MST-6 Ogino, Y., 13-FD-3, 49-TP-1, 59-APA-7, 161-APA-16, Morgan, D., 123-GNC-12, 345-SATS-2 Murdy, M., 80-ISC-3 Narducci, R., 114-APA-13, 260-APA-28 Nigam, N., 7-APA-1 201-TP-5 Morgan, N., 65-FD-10 Murman, S., 65-FD-10, 68-FD-13, 108-AFM-5, 3 Narisetti, R., 295-SD-12 Nikaido, B., 68-FD-13 Oh, G., 426-GNC-43 Morgan, P., 103-APA-9/NDA-1, 168-FD-20 61-AMT-6/GT-7, 410-APA-40 Nark, D., 157-AA-6 Nikoloutsakos, N., 12-FD-2 Oh, J., 82-MAT-3 Morgan, R., 126-GNC-15 Murphey, T., 195-SCS-4, 244-SCS-6 Narkawicz, A., 166-DA-1 Nikoueeyan, P., 203-WE-7 Ohnishi, N., 49-TP-1, 201-TP-5 Mori, K., 363-APA-35 Murphy, J., 191-PC-11, 350-SOF-1, 397-SOF-2 Nash, A., 211-AFM-9 Ning, A., 50-WE-1 Ohno, D., 364-APA-36 Mori, O., 92-SCS-2 Murphy, K., 115-APA-14 Natali, M., 235-MAT-9 Ning, X., 298-STR-15 Ohtani, K., 6-AMT-1 Moriarty, P., 153-WE-6, 354-WE-13 Murphy, P., 5-AFM-2 Natori, M., 145-SCS-3 Nishida, H., 368-FD-45/PDL-9 Okada, K., 67-FD-12/PDL-1 Morimoto, N., 440-TP-10 Murray, J., 162-APA-17, 311-APA-31 Natsui, G., 213-AMT-3 Nishihara, M., 119-FD-16 Okada, T., 348-SD-15 Morita, R., 362-AMT-7 Murray, V., 300-TP-7 Naughton, B., 51-WE-2 Nishimuro, J., 348-SD-15 Okai, K., 128-GTE-3 185 Morrida, J., 144-PDL-2 Murray, W., 278-GTE-6 Naughton, J., 203-WE-7 Nitzsche, F., 436-SD-22 Okatan, M., 424-GNC-41 Morris, C., 14-FD-4, 115-APA-14, 421-FD-56 Murri, D., 159-AFM-8 Navalkar, S., 394-SD-18 Niu, R., 124-GNC-13 Okhovat, S., 229-GTE-5 Morris, P., 54-AA-2, 106-AA-4, 208-AA-7 Murthy, J., 441-TP-11 Navaratne, R., 165-AS-3 Noble, D., 383-MST-15 Okolo, W., 4-AFM-1, 159-AFM-8, 186-MST-7 Morris, S., 8-APA-2, 111-APA-10, 263-FD-32, 352-TES-2 Murthy, P., 47-STR-2, 199-STR-11 Nawroth, H., 66-FD-11, 192-PC-12 Noevere, A., 96-STR-5 Okuizumi, N., 92-SCS-2, 145-SCS-3 Morrison, J., 61-AS-1 Musa, N., 312-APA-32 Nayani, S., 218-APA-24, 261-APA-29, 429-GT-11 Nogar, S., 327-GNC-33 Okuma, M., 292-SCS-7 Mortazavi, M., 120-FD-17 Muse, J., 125-GNC-14, 373-GNC-35 Nayeri, C., 66-FD-11, 164-APA-19/FD-19, 259-APA-27, Nogawa, Y., 194-SATS-1 Okuno, A., 145-SCS-3 Mortazavi, S., 433-SATS-4 Musielak, D., 130-HSABP-3 265-FD-34 Noh, K., 191-PC-11 Ol, M., 7-APA-1, 223-FD-31, 330-GT-6, 372-FD-49, Morteza Khosravi, M., 252-WE-9 Muto, D., 388-PC-20 Neaves, M., 415-FD-50 Noll, B., 24-GTE-1 411-APA-41 Morton, S., 10-APA-4 Mutuel, L., 251-UMS-4 Neely, A., 201-TP-5 Nompelis, I., 62-FD-7, 99-TP-3, 300-TP-7, 402-TP-9 Olansen, J., 176-GNC-17 Mosharov, V., 222-FD-30 Myers, L., 411-APA-41 Neema, K., 45-SEN-1 Nonomura, T., 67-FD-12/PDL-1, 221-FD-29, Olcmen, S., 319-FD-41 Motevalli, P., 80-ISC-3 Myers, T., 56-AFM-4 Nees, J., 278-GTE-6 368-FD-45/PDL-9 Olejniczak, J., 49-TP-1 Motosuke, M., 168-FD-20 Myklebust, A., 358-ACD-6 Nehrenz, M., 179-GNC-20 Noriega, A., 100-UMS-1 Olivari, M., 139-MST-6 Motoyama, N., 376-GNC-38 Myrent, N., 204-WE-8 Neidigk, S., 204-WE-8 Norris, J., 369-FD-46 Oliver, J., 185-MDO-5 Motta, V., 394-SD-18 Naboulsi, S., 180-GTE-4, 235-MAT-9 Neilld, S., 159-AFM-8 Norwood, D., 96-STR-5, 400-STR-19, 437-STR-20 Oliveras, O., 346-SCS-8 Mounaim-Rousselle, C., 191-PC-11 Nadarajah, S., 60-APA-8, 263-FD-32, 413-APA-43 Nelson, A., 409-APA-39 Noumi, A., 227-GNC-24 Oliviero, F., 148-STR-7, 248-STR-12 Mozer, F., 337-MST-12 Nagai, H., 57-APA-5 Nelson, C., 106-AA-4, 216-APA-22 Novak, J., 18-GNC-1 Ollar, J., 336-MDO-8 Mravcak, V., 131-HSABP-4 Nagamachi, M., 191-PC-11 Nelson, J., 393-SD-17 Novikov, A., 49-TP-1 Ollivier Gooch, C., 263-FD-32 Mrema, H., 169-FD-21 Nagaraja, S., 88-PC-5, 343-PDL-7 Nemati, A., 202-UMS-3 Numata, D., 6-AMT-1 Olsen, M., 417-FD-52 Mueller, F., 12-FD-2, 170-FD-22 Nagasaki, T., 98-TP-2, 250-TP-6 Nemec, M., 293-SD-10, 366-APA-38 Nunes, M., 179-GNC-20 Olson, E., 358-ACD-6 Mueller, M., 41-PC-4, 242-PC-14 Nagasawa, M., 145-SCS-3 Neufeld, D., 429-GT-11 Nunes, R., 191-PC-11 Omagari, K., 48-STR-3 Mueller, R., 382-MST-14 Nagatani, K., 4-AFM-1 Neuman, J., 89-PC-6 Nuthi, P., 423-GNC-40 Omar, S., 2-ISC-1 Muir, E., 42-SD-1 Naghipour, P., 399-STR-18 Neves, F., 25-HIS-1, 359-AFM-12, 411-APA-41 Nysetvold, T., 80-ISC-3 Ombrello, T., 142-PC-9, 182-HSABP-6, 388-PC-20 Mujumdar, P., 347-SD-14 Naik, R., 235-MAT-9, 335-MAT-13 Newill, B., 317-EDU-1 O`Connor, J., 91-PC-8 Omidshafiei, S., 132-ICC-1 Mulani, S., 33-MDO-1 Naik, S., 362-AMT-7 Newman, B., 274-GNC-27, 424-GNC-41 O’Brien, D., 111-APA-10, 312-APA-32 Omori, T., 162-APA-17 Mulder, J., 431-MST-16 Najafi, A., 197-STR-9 Newman, J., 321-FD-43 O’Brien, J., 208-AA-7 Omran, A., 299-TES-1 Mulder, M., 72-GNC-8, 85-MST-4 Najafi, S., 405-ACD-8 Newman, M., 139-MST-6 O’Byrne, S., 26-HSABP-1, 193-PDL-3 Omrani, P., 140-NDA-3 Muli, M., 36-MST-2 Nakagami, S., 181-HSABP-5 Newsom, J., 211-AFM-9 O’Connell, M., 188-MVC-4 Ong, B., 281-MAT-10 Müller, H., 174-FD-26 Nakajima, T., 259-APA-27 Ngaya, T., 365-APA-37 O’Connor, K., 354-WE-13 Ono, D., 412-APA-42 Author/Session Chair Index Ono, Y., 168-FD-20 Palazotto, A., 46-STR-1, 148-STR-7, 248-STR-12, Passalaqua, A., 63-FD-8 Peter, F., 404-ACD-7, 425-GNC-42 Ploen, S., 176-GNC-17 Onufer, J., 163-APA-18 394-SD-18 Patel, D., 116-DE-1, 199-STR-11, 400-STR-19 Peter, J., 60-APA-8 Poggie, J., 418-FD-53, 421-FD-56 Ooyama, T., 261-APA-29 Palei, V., 168-FD-20 Patel, H., 151-UMS-2 Peters, J., 157-AA-6 Pogorelov, A., 420-FD-55 Oppenheimer, M., 327-GNC-33, 373-GNC-35 Paley, D., 359-AFM-12, 375-GNC-37 Patel, M., 216-APA-22 Peterson, D., 131-HSABP-4 Polanka, M., 24-GTE-1, 75-GTE-2, 128-GTE-3, Opromolla, R., 296-SEN-2 Palosz, A., 243-PDL-13 Patel, N., 404-ACD-7 Peterson, G., 2-ISC-1 278-GTE-6, 306-ABPSI-1 Orefice, M., 100-UMS-1 Pamadi, B., 163-APA-18 Patil, M., 34-MDO-2, 96-STR-5, 324-GNC-30, 384-NDA-8 Peterson, J., 426-GNC-43 Polivanov, P., 419-FD-54 Orkwis, P., 15-FD-5 Pan, K., 39-PC-2 Patnaik, S., 250-TP-6 Peterson, L., 391-SCS-9 Pollini, L., 18-GNC-1, 139-MST-6 Orr, J., 376-GNC-38 Panchal, K., 162-APA-17 Patterson, M., 226-GNC-23, 357-ACD-5 Petit, X., 342-PC-18 Polsky, S., 114-APA-13, 187-MST-8 Orra, T., 357-ACD-5 Panda, P., 110-AMT-2 Patton, B., 281-MAT-10 Petrishchev, V., 193-PDL-3, 416-FD-51/PDL-12 Ponnappan, R., 16-FD-57 Osborn, M., 241-PC-13 Pandey, A., 6-AMT-1 Paul, L., 348-SD-15 Petro, E., 366-APA-38 Pontecorvo, M., 165-AS-3, 262-AS-5 Oskay, C., 399-STR-18 Pandya, M., 371-FD-48 Paulson, C., 33-MDO-1 Petrosky, B., 256-AMT-4 Poole, D., 160-APA-15, 413-APA-43 Ossmann, D., 272-GNC-25, 424-GNC-41 Panek, J., 23-GT-1 Paulson, J., 163-APA-18 Petrovic, V., 253-WE-10 Poovathingal, S., 300-TP-7 Ostermann, F., 164-APA-19/FD-19 Panesi, M., 99-TP-3, 201-TP-5, 402-TP-9 Pavese, C., 253-WE-10 Petway, L., 71-GNC-7 Pope, D., 296-SEN-2 Ostieri, M., 266-FD-35 Pang, Q., 117-FD-14 Paxson, D., 181-HSABP-5, 230-HSABP-7, 278-GTE-6, Pfaender, H., 157-AA-6 Popov, N., 88-PC-5, 193-PDL-3, 290-PDL-5 Ostoja-Starzewski, M., 234-MAT-8 Paniagua, G., 26-HSABP-1, 59-APA-7, 171-FD-23, 279-HSABP-9/GTE-8 Pfifer, H., 177-GNC-18, 186-MST-7, 359-AFM-12, Poroseva, S., 5-AFM-2, 108-AFM-5, 200-SUR-1 Ostovari, S., 167-DE-2 411-APA-41 Peace, A., 214-APA-20 425-GNC-42 Porte-Agel, F., 303-WE-12 Osusky, M., 371-FD-48 Pankaja Kaluarachchi, R., 2-ISC-1 Pearl, J., 345-SATS-2 Pfitzner, M., 174-FD-26 Porteous, A., 108-AFM-5 Othman, N., 112-APA-11 Pankow, D., 337-MST-12 Pechlivanoglou, G., 265-FD-34 Pham, D., 197-STR-9 Post, M., 162-APA-17 Otsuka, H., 4-AFM-1 Pankow, M., 48-STR-3 Peck, J., 300-TP-7 Pham, K., 73-GNC-9 Post, N., 204-WE-8 Otto, N., 350-SOF-1 Panourgias, K., 118-FD-15 Pedersen, M., 303-WE-12 Phan, C., 400-STR-19 Postma, J., 330-GT-6 Ou, D., 429-GT-11 Pant, K., 435-SD-21 Pedrazzani, J., 408-AMT-9 Phan, N., 398-STR-17 Potekhina, I., 26-HSABP-1 Owen, A., 306-ABPSI-1 Papadakis, G., 411-APA-41 Peet, Y., 153-WE-6, 370-FD-47 Phelan, S., 236-MDO-6 Powell, D., 32-MAT-2, 136-MAT-6, 184-MAT-7 Owens, D., 56-AFM-4 Papadimitriou, C., 160-APA-15 Peeters, D., 95-STR-4 Philen, M., 262-AS-5 Powers, J., 120-FD-17 Owens, J., 414-CMS-1 Papadimitriou, D., 160-APA-15 Pegues, J., 282-MAT-11 Philipsen, I., 330-GT-6 Powers, R., 54-AA-2, 309-AMT-5 186 Owis, F., 312-APA-32 Papageorge, M., 256-AMT-4 Pei, J., 163-APA-18, 211-AFM-9 Phillips, K., 428-GT-10 Prabhakar, P., 199-STR-11 Owji, A., 334-MAT-12 Papamoschou, D., 157-AA-6, 208-AA-7 Peigin, S., 413-APA-43 Phillips, T., 263-FD-32 Prabhu, D., 369-FD-46 Oyama, A., 67-FD-12/PDL-1, 78-IS-4 Pappa, R., 92-SCS-2, 292-SCS-7 Peiro, J., 152-WE-5 Phillips, W., 59-APA-7 Prakash, N., 97-STR-6 Oyori, H., 116-DE-1 Paquette, J., 204-WE-8 Pelham, J., 380-IS-12 Philpott, S., 48-STR-3 Prakash, O., 359-AFM-12 Oza, N., 332-IS-10 Parambil, N., 199-STR-11 Pellegrino, S., 46-STR-1, 145-SCS-3, 195-SCS-4, Phlipot, G., 435-SD-21 Prall, M., 80-ISC-3 Ozawa, T., 201-TP-5 Paranjape, A., 56-AFM-4, 324-GNC-30 292-SCS-7, 298-STR-15, 391-SCS-9 Phong, V., 157-AA-6 Prazenica, R., 18-GNC-1, 100-UMS-1, 126-GNC-15, Ozawa, Y., 357-ACD-5 Paraschivoiu, I., 188-MVC-4 Pelletier, D., 63-FD-8, 161-APA-16 Piatak, D., 115-APA-14 301-UMS-5 Ozbay, A., 354-WE-13 Pardeshi, I., 299-TES-1 Pelletier, F., 19-GNC-2 Pidaparti, R., 167-DE-2 Preci, A., 109-AFM-6, 201-TP-5 Ozburn, R., 78-IS-4 Parisch, M., 328-GNC-34 Peltier, S., 182-HSABP-6 Pienaar, L., 275-GNC-28 Precup, N., 293-SD-10 Ozger, E., 308-AFM-11 Park, C., 376-GNC-38 Pendyala, R., 62-FD-7 Pierpaoli, P., 225-GNC-22 Prenter, R., 66-FD-11, 75-GTE-2 Ozgoren, M., 21-GNC-4 Park, J., 175-GNC-16 Peng, L., 185-MDO-5, 383-MST-15 Pierrottet, D., 71-GNC-7 Previtali, F., 165-AS-3 Öznalbant, Z., 405-ACD-8 Park, M., 218-APA-24 Peng, T., 239-NDA-5 Pieterse, F., 330-GT-6 Prevot, T., 138-MST-5 Pachter, M., 73-GNC-9, 177-GNC-18 Park, S., 275-GNC-28 Penhallegon, W., 166-DA-1 Pigeon, A., 188-MVC-4 Price, C., 428-GT-10 Pachuilo, M., 290-PDL-5 Park, Y., 192-PC-12, 199-STR-11, 376-GNC-38 Penmetsa, R., 286-NDA-6, 297-STR-14, 334-MAT-12 Pilon, A., 106-AA-4 Price, S., 179-GNC-20 Pacini, M., 139-MST-6 Parker, R., 402-TP-9 Pepley, D., 270-FD-39 Pineda, E., 47-STR-2, 82-MAT-3, 97-STR-6, 249-STR-13 Priolo, F., 108-AFM-5, 158-AFM-7 Pack, D., 225-GNC-22 Parks, G., 286-NDA-6 Pereira, D., 295-SD-12 Pinier, J., 115-APA-14, 163-APA-18, 261-APA-29 Pripstein, E., 47-STR-2 Pack, S., 192-PC-12, 229-GTE-5 Parlette, E., 312-APA-32 Pereira, G., 136-MAT-6 Pinon-Fischer, O., 209-ACD-2 Probst, A., 169-FD-21 Padmanabhan, M., 295-SD-12 Parrish, J., 34-MDO-2, 185-MDO-5 Perelstein, Y., 319-FD-41 Pintelon, R., 395-SD-19 Pröbsting, S., 203-WE-7 Page, J., 128-GTE-3, 272-GNC-25 Parsani, M., 323-GEPC-3 Perez, D., 70-GNC-6, 122-GNC-11, 175-GNC-16, Pinto, J., 348-SD-15 Prosser, D., 410-APA-40 Paixão, V., 56-AFM-4 Parsons, N., 99-TP-3 427-GNC-44 Pio, D., 258-APA-26 Pruett, B., 269-FD-38, 277-GT-4 Pak, C., 296-SEN-2 Paryz, R., 228-GT-3, 329-GT-5 Perez, J., 377-GNC-39 Pipenberg, B., 9-APA-3 Przekop, A., 297-STR-14 Pal, G., 400-STR-19, 437-STR-20 Parziale, N., 110-AMT-2, 271-GEPC-4/SAT-1, Perez, R., 339-NDA-7, 384-NDA-8, 435-SD-21 Pirrera, A., 198-STR-10, 297-STR-14 Puig, J., 123-GNC-12 Palacios, F., 7-APA-1, 371-FD-48, 413-APA-43, 309-AMT-5, 378-GT-8 Perez Rocha, A., 272-GNC-25, 301-UMS-5, 380-IS-12 Pitt, D., 113-APA-12 Purinton, D., 163-APA-18 414-CMS-1, 440-TP-10 Pascazio, G., 231-HSABP-8 Perhinschi, M., 272-GNC-25, 380-IS-12 Pitz, R., 41-PC-4, 142-PC-9, 192-PC-12, 266-FD-35 Putman, P., 183-IS-6 Palacios, J., 102-WE-4 Paschereit, C., 66-FD-11, 164-APA-19/FD-19, Perrotta, G., 79-ISC-2 Platts, W., 247-SRE-1 Putnam, D., 391-SCS-9 Palacios, R., 43-SD-2, 44-SD-3, 56-AFM-4, 61-AS-1 259-APA-27, 265-FD-34, 279-HSABP-9/GTE-8 Perseghetti, B., 301-UMS-5 Platzer, M., 372-FD-49 Puttannaiah, K., 373-GNC-35 Palar, P., 286-NDA-6 Pasiliao, C., 32-MAT-2, 58-APA-6, 93-SD-4, Persson, P., 13-FD-3, 50-WE-1, 170-FD-22 Plemmons, D., 110-AMT-2 Putzke, H., 80-ISC-3 Palaszewski, B., 351-SRE-2 161-APA-16, 168-FD-20, 295-SD-12, 347-SD-14 Pervan, B., 100-UMS-1 Plesniak, M., 172-FD-24 Pylorof, D., 122-GNC-11 Author/Session Chair Index Pytel, D., 250-TP-6 Rampurawala, A., 7-APA-1 Reuss, S., 169-FD-21 Rodrigues, C., 150-TP-4, 267-FD-36 Rufer, S., 277-GT-4 Qian, J., 435-SD-21 Rana, Z., 169-FD-21, 269-FD-38 Reuter, C., 91-PC-8, 289-PC-16 Rodriguez, A., 28-IS-2, 301-UMS-5, 373-GNC-35 Ruff, R., 186-MST-7 Qian, S., 408-AMT-9 Ranade, I., 75-GTE-2 Reyes, J., 335-MAT-13 Rodriguez, D., 293-SD-10 Rufino, G., 296-SEN-2 Qin, N., 58-APA-6, 310-APA-30 Ranatunga, V., 197-STR-9, 438-STR-21 Reynolds, C., 29-ISC-4 Rodriguez-Rivera, G., 204-WE-8 Ruggles-Wrenn, M., 297-STR-14 Qu, K., 15-FD-5 Randall, S., 181-HSABP-5 Reynolds, W., 145-SCS-3 Roettgen, A., 389-PDL-11 Rukes, L., 66-FD-11 Qu, Q., 59-APA-7, 113-APA-12, 160-APA-15, 312-APA-32 Ranjan, R., 288-PC-15, 320-FD-42 Rezayat, A., 395-SD-19 Rogers, D., 433-SATS-4 Rumpfkeil, M., 81-LEC-2, 189-NDA-4, 258-APA-26, Quackenbush, T., 260-APA-28, 294-SD-11 Rankin, B., 91-PC-8, 181-HSABP-5, 242-PC-14, Rhew, R., 23-GT-1, 379-GT-9 Rogers, J., 406-AFM-15 363-APA-35 Quaranta, G., 61-AS-1, 189-NDA-4, 366-APA-38, 331-GTE-7, 341-PC-17 Rhudy, M., 45-SEN-1 Rogers, M., 323-GEPC-3 Rumsey, C., 68-FD-13, 323-GEPC-3, 371-FD-48 394-SD-18 Rankin, J., 166-DA-1 Ribert, G., 342-PC-18 Rogers, S., 163-APA-18 Runyon, B., 335-MAT-13 Queiroz, R., 255-AA-8 Rans, C., 317-EDU-1 Ricci, S., 44-SD-3, 219-AS-4 Roh, I., 367-AS-7 Rupert, A., 139-MST-6 Quero-Martin, D., 58-APA-6 Rao, A., 34-MDO-2, 226-GNC-23 Rice, B., 76-HSABP-2 Rokhsaz, K., 393-SD-17, 436-SD-22 Ruscher, C., 156-AA-5 Quest, J., 127-GT-2, 228-GT-3, 257-APA-25, 329-GT-5 Rao, S., 196-SD-8 Rice, T., 204-WE-8, 270-FD-39 Rollin, V., 136-MAT-6 Russell, S., 97-STR-6 Quijada, G., 108-AFM-5 Rao, Y., 85-MST-4 Rich, B., 430-IS-13 Rollins, P., 144-PDL-2 Rutledge, J., 75-GTE-2 Quijano, O., 409-APA-39 Rashid, A., 251-UMS-4, 271-GEPC-4/SAT-1 Rich, J., 119-FD-16, 389-PDL-11 Romano, P., 294-SD-11 Rye, M., 70-GNC-6 Quindlen, J., 125-GNC-14 Raska, V., 100-UMS-1 Richard, L., 437-STR-20 Romeo, S., 431-MST-16 Rynders, R., 48-STR-3 Quix, H., 228-GT-3 Rasmussen, S., 175-GNC-16 Richards, B., 202-UMS-3 Romero, V., 103-APA-9/NDA-1, 339-NDA-7 Ryszka, K., 64-FD-9 Quon, E., 117-FD-14 Rassaian, M., 95-STR-4, 197-STR-9 Richards, H., 297-STR-14 Romli, F., 306-ABPSI-1 Ryu, J., 136-MAT-6, 165-AS-3 Raahemifar, K., 276-GNC-29 Ratliff, R., 178-GNC-19 Richards, Z., 174-FD-26 Rone, W., 373-GNC-35 Saam, L., 316-DE-3 Radchenko, V., 222-FD-30 Ratnoo, A., 21-GNC-4, 73-GNC-9, 126-GNC-15, Richardson, C., 139-MST-6 Roquemore, W., 289-PC-16 Saavedra, J., 59-APA-7 Rafael, C., 258-APA-26 175-GNC-16 Richardson, D., 110-AMT-2, 341-PC-17 Roscher, B., 152-WE-5 Saberi, H., 294-SD-11 Raffel, M., 311-APA-31 Rausch, R., 115-APA-14 Richie, D., 171-FD-23 Rose, C., 298-STR-15 Sabo, K., 356-ABPSI-2 Raffler, T., 224-GNC-21, 324-GNC-30 Raveh, D., 42-SD-1, 43-SD-2, 93-SD-4, 435-SD-21 Richter, K., 311-APA-31 Rose, G., 292-SCS-7 Sabouri, M., 353-TP-8 Raghavan, S., 235-MAT-9, 348-SD-15 Raz, A., 132-ICC-1 Ricklick, M., 128-GTE-3, 415-FD-50 Rosema, C., 7-APA-1, 412-APA-42 Sada, A., 335-MAT-13 Ragheb, A., 113-APA-12 Reasor, D., 14-FD-4, 58-APA-6, 64-FD-9 Riel, J., 126-GNC-15 Rosenberg, A., 354-WE-13 Sagban, M., 116-DE-1 187 Raghunath, G., 367-AS-7 Rechlin, A., 257-APA-25 Riemenschneider, J., 165-AS-3, 219-AS-4 Rosenberg, D., 241-PC-13 Saharan, A., 234-MAT-8 Ragni, D., 51-WE-2, 152-WE-5, 203-WE-7, 215-APA-21 Reda, D., 369-FD-46 Riga, J., 47-STR-2 Rosenbladt, D., 47-STR-2 Sahni, O., 216-APA-22 Rahimi, M., 76-HSABP-2, 241-PC-13 Reddy, S., 310-APA-30 Rigby, K., 251-UMS-4 Rosendall, P., 176-GNC-17 Said, M., 257-APA-25 Rahman, M., 268-FD-37 Redmond, B., 430-IS-13 Riggs, C., 26-HSABP-1 Rosenfeld, N., 57-APA-5 Saiki, H., 151-UMS-2 Rahmani, A., 225-GNC-22, 328-GNC-34 Reed, C., 176-GNC-17 Rigney, T., 69-GEPC-2 Ross, J., 57-APA-5 Sain, T., 234-MAT-8 Rahn, C., 294-SD-11 Reed, E., 114-APA-13 Riley, Z., 146-SD-6 Rossmann, T., 362-AMT-7 Sakai, M., 11-FD-1 Rai, A., 83-MAT-4 Reed, H., 112-APA-11, 258-APA-26, 422-FD-58, Rimoli, J., 200-SUR-1 Roughen, K., 269-FD-38 Sakai, S., 377-GNC-39 Rai, M., 417-FD-52 425-GNC-42 Rinoie, K., 11-FD-1 Rouhi Youssefi, M., 120-FD-17 Sakai, T., 300-TP-7 Raina, A., 50-WE-1, 252-WE-9 Regele, J., 63-FD-8 Risse, K., 404-ACD-7, 405-ACD-8 Rouquette, N., 233-IS-8 Sakamoto, H., 92-SCS-2, 145-SCS-3, 292-SCS-7 Rainbird, J., 152-WE-5 Regueiro, P., 28-IS-2 Ritter, M., 43-SD-2 Rouseau, C., 437-STR-20 Sakovsky, M., 195-SCS-4 Rais-Rohani, M., 185-MDO-5, 189-NDA-4 Reidling, S., 151-UMS-2 Rivers, M., 228-GT-3 Rouser, K., 80-ISC-3 Sakuragi, Y., 387-PC-19 Raj, P., 245-SD-9 Rein, K., 213-AMT-3 Rizzetta, D., 67-FD-12/PDL-1 Rousso, A., 142-PC-9 Salami, E., 306-ABPSI-1 Raja, L., 290-PDL-5, 344-PDL-8, 416-FD-51/PDL-12 Reinders, C., 281-MAT-10 Rizzi, A., 64-FD-9, 413-APA-43 Routhier, L., 408-AMT-9 Salemi, L., 173-FD-25 Rajagopal, K., 424-GNC-41 Reisenthel, P., 409-APA-39 Rizzi, S., 323-GEPC-3 Rowe, S., 116-DE-1 Salmon, A., 193-PDL-3 Rajendran, H., 199-STR-11 Reising, H., 119-FD-16 Rizzo, E., 148-STR-7, 248-STR-12 Rowley, C., 223-FD-31 Salvetti, M., 140-NDA-3 Rajmohan, N., 187-MST-8 Reist, T., 60-APA-8 Roa, M., 110-AMT-2 Rowton, A., 306-ABPSI-1 Samami, H., 34-MDO-2 Raju, G., 95-STR-4 Rekedal, K., 184-MAT-7 Roach, D., 204-WE-8 Roy, C., 263-FD-32, 286-NDA-6, 324-GNC-30, Samaratunga, D., 367-AS-7 Raju, I., 438-STR-21 Remaki, L., 170-FD-22 Roback, V., 71-GNC-7 384-NDA-8, 415-FD-50 Samborsky, D., 204-WE-8 Ramachandran, S., 250-TP-6 Rems, F., 423-GNC-40 Robbins, D., 47-STR-2, 399-STR-18 Roy, R., 420-FD-55 Samimy, M., 54-AA-2, 156-AA-5, 265-FD-34, Raman, V., 41-PC-4, 91-PC-8, 174-FD-26, 192-PC-12 Ren, J., 344-PDL-8 Robertson, A., 252-WE-9 Roy, S., 31-MAT-1, 83-MAT-4, 110-AMT-2, 136-MAT-6, 416-FD-51/PDL-12 Ramaprabhu, P., 51-WE-2 Ren, X., 83-MAT-4, 367-AS-7 Robertson, E., 71-GNC-7 185-MDO-5, 213-AMT-3, 256-AMT-4, 309-AMT-5, Sandberg, R., 68-FD-13, 270-FD-39 Ramasamy, S., 20-GNC-3 Ren, Y., 74-GNC-10, 198-STR-10, 310-APA-30 Robertson, G., 269-FD-38 319-FD-41, 344-PDL-8, 440-TP-10 Sanders, B., 346-SCS-8 Ramesh, K., 76-HSABP-2 Renac, F., 13-FD-3 Robeson, M., 196-SD-8 Roza, M., 238-MST-10 Sanders, G., 247-SRE-1, 351-SRE-2 Ramey, J., 115-APA-14 Renard, N., 420-FD-55 Robinson, J., 21-GNC-4 Rozek, M., 233-IS-8 Sanei, S., 282-MAT-11 Ramezani, A., 170-FD-22 Rendall, T., 160-APA-15, 413-APA-43 Rockwell, R., 76-HSABP-2 Rubinsky, S., 21-GNC-4 Sanford, A., 29-ISC-4 Ramjatan, S., 440-TP-10 Rennie, M., 144-PDL-2, 330-GT-6 Rockwood, M., 322-FD-44 Rudnik, R., 228-GT-3, 257-APA-25, 329-GT-5 Sangan, C., 299-TES-1 Ramos, N., 168-FD-20 Resor, B., 101-WE-3 Rodi, P., 363-APA-35 Rudolph, D., 251-UMS-4 Sangid, M., 135-MAT-5, 234-MAT-8 Ramos, P., 72-GNC-8 Réthoré, P., 215-APA-21 Rodio, J., 121-FD-18 Ruess, M., 198-STR-10 Sankar, L., 260-APA-28, 365-APA-37 Author/Session Chair Index Sankaran, V., 288-PC-15, 342-PC-18 Schatz, S., 125-GNC-14 Schwenke, D., 99-TP-3 Sexton, B., 246-SD-13/GEPC-5 Shin, D., 91-PC-8 Sankararaman, S., 339-NDA-7 Schatzman, D., 168-FD-20 Schwer, D., 174-FD-26, 341-PC-17 Shaeffer, R., 98-TP-2 Shin, H., 31-MAT-1, 136-MAT-6 Sansone, M., 3-AA-1 Schauer, F., 130-HSABP-3, 181-HSABP-5, Schwille, J., 98-TP-2 Shafer, T., 10-APA-4, 217-APA-23 Shin, J., 382-MST-14 Santangelo, A., 194-SATS-1, 345-SATS-2 230-HSABP-7, 279-HSABP-9/GTE-8, 331-GTE-7, Schwoch, G., 166-DA-1 Shafirovich, E., 247-SRE-1 Shin, S., 367-AS-7, 394-SD-18 Santarpia, E., 248-STR-12 341-PC-17 Schwoeppe, A., 371-FD-48 Shah, H., 151-UMS-2, 189-NDA-4 Shindo, M., 78-IS-4 Santer, M., 61-AS-1, 195-SCS-4, 259-APA-27, Scheichl, R., 199-STR-11 Sclafani, A., 313-APA-33 Shah, J., 232-IS-7 Shinohara, T., 128-GTE-3 411-APA-41 Schenk, M., 346-SCS-8 Sclafani, R., 376-GNC-38 Shahid, Z., 271-GEPC-4/SAT-1 Shirasawa, Y., 92-SCS-2 Santhanam, V., 415-FD-50 Schepers, G., 102-WE-4 Scott, K., 361-AMT-6/GT-7 Shaler, K., 153-WE-6 Shish, K., 232-IS-7, 325-GNC-31 Santner, J., 89-PC-6 Schetz, J., 246-SD-13/GEPC-5, 407-AMT-8, 408-AMT-9 Scott, M., 246-SD-13/GEPC-5 Shamsaei, N., 184-MAT-7, 281-MAT-10, 282-MAT-11 Shivakumar, K., 438-STR-21 Santoro, B., 289-PC-16 Scheuermann, E., 18-GNC-1 Scott, R., 93-SD-4, 246-SD-13/GEPC-5 Shan, J., 74-GNC-10, 85-MST-4, 195-SCS-4 Shkurenkov, I., 243-PDL-13, 389-PDL-11 Sanyal, A., 376-GNC-38 Schiavo, L., 266-FD-35 Scott, S., 335-MAT-13 Shan, X., 58-APA-6 Shneider, M., 290-PDL-5 Saracoglu, B., 411-APA-41 Schirmer, J., 271-GEPC-4/SAT-1 Scott-Emuakpor, O., 184-MAT-7, 286-NDA-6, Shankar, P., 124-GNC-13, 273-GNC-26, 325-GNC-31, Shojaei, A., 399-STR-18 Saranathan, H., 4-AFM-1 Schmaus, J., 294-SD-11 334-MAT-12, 335-MAT-13 376-GNC-38 Short, E., 150-TP-4 Sardeshmukh, S., 388-PC-20 Schmidt, B., 110-AMT-2 Scotti, A., 44-SD-3, 434-SD-20 Shankar, R., 82-MAT-3 Short, S., 25-HIS-1 Saribay, Z., 196-SD-8 Schmidt, H., 164-APA-19/FD-19 Seager, C., 363-APA-35 Shankar, U., 376-GNC-38 Shrestha, E., 359-AFM-12 Saric, W., 112-APA-11, 258-APA-26 Schmisseur, J., 119-FD-16 Secco, N., 210-ACD-3 Shannon, C., 57-APA-5 Shrestha, U., 89-PC-6 Sarim, M., 202-UMS-3 Schmitt, F., 27-IS-1 Secheli, G., 145-SCS-3 Sharma, A., 344-PDL-8, 354-WE-13 Shtessel, Y., 243-PDL-13, 425-GNC-42 Sarkar, P., 252-WE-9 Schmitt, R., 51-WE-2 Sedaghati, R., 262-AS-5 Sharma, S., 335-MAT-13 Shu, F., 11-FD-1 Sartor, F., 412-APA-42 Schmitz, S., 50-WE-1, 102-WE-4, 165-AS-3, 303-WE-12 Sedlack, M., 297-STR-14 Sharman, R., 326-GNC-32 Shumway, N., 378-GT-8 Sartor, P., 93-SD-4, 189-NDA-4, 393-SD-17 Schneider, G., 353-TP-8, 440-TP-10 See, Y., 118-FD-15, 266-FD-35, 289-PC-16, 320-FD-42, Shcherbanev, S., 142-PC-9 Shweyk, K., 5-AFM-2 Sartori, L., 101-WE-3 Schneider, S., 369-FD-46 420-FD-55 She, H., 211-AFM-9 Shyong, W., 176-GNC-17 Sasaki, J., 151-UMS-2 Schneider, T., 404-ACD-7 Seefeldt, P., 391-SCS-9 Shea, P., 156-AA-5 Sibille, L., 247-SRE-1 Sasaki, T., 191-PC-11, 227-GNC-24 Schneider, W., 43-SD-2, 93-SD-4 Seely, D., 281-MAT-10 Sheaf, C., 15-FD-5 Sibilski, K., 359-AFM-12 Sasanapuri, B., 319-FD-41 Schnell, T., 166-DA-1 Segal, C., 12-FD-2 Sheeley, J., 440-TP-10 Sidorenko, A., 419-FD-54 188 Sasiadek, J., 70-GNC-6, 122-GNC-11, 175-GNC-16 Schnetter, P., 274-GNC-27 Seidel, G., 31-MAT-1, 83-MAT-4, 96-STR-5, 97-STR-6, Shelton, R., 383-MST-15 Sieber, M., 66-FD-11 Sasidharan Nair, U., 105-AA-3 Schnipke, E., 151-UMS-2 334-MAT-12, 367-AS-7 Shen, H., 41-PC-4 Sierakowski, R., 149-STR-8 Sasoh, A., 261-APA-29 Schoenenberger, M., 109-AFM-6 Seidel, J., 58-APA-6, 86-MVC-2, 114-APA-13, Shen, M., 113-APA-12, 334-MAT-12 Sigal, E., 21-GNC-4 SathiaNarayanan, A., 26-HSABP-1 Scholbrock, A., 253-WE-10 314-APA-34, 418-FD-53 Shen, Q., 428-GT-10 Sigthorsson, D., 327-GNC-33 Sathyan, A., 183-IS-6, 430-IS-13 Scholz, P., 168-FD-20 Seifert, A., 168-FD-20 Shen, X., 89-PC-6 Siikonen, T., 268-FD-37 Sathyanarayanan, S., 250-TP-6 Scholz, T., 440-TP-10 Seifert, D., 96-STR-5 Sheng, C., 121-FD-18, 161-APA-16, 214-APA-20, Silk, E., 98-TP-2, 441-TP-11 Satija, A., 362-AMT-7 Schoonmaker, M., 120-FD-17, 420-FD-55 Seiler, P., 51-WE-2, 177-GNC-18, 253-WE-10 294-SD-11, 365-APA-37, 411-APA-41 Silton, S., 409-APA-39 Sato, M., 67-FD-12/PDL-1, 124-GNC-13, 138-MST-5, Schoukens, J., 395-SD-19 Seitzman, J., 142-PC-9 Shepherd, J., 110-AMT-2, 378-GT-8 Silva, A., 25-HIS-1, 98-TP-2, 150-TP-4, 267-FD-36, 259-APA-27 Schreck, S., 303-WE-12 Sekhar, S., 417-FD-52, 421-FD-56 Sheplak, M., 234-MAT-8, 408-AMT-9 356-ABPSI-2, 411-APA-41 Satori, S., 151-UMS-2 Schreiner, S., 247-SRE-1 Sekula, M., 115-APA-14 Sher, E., 241-PC-13 Silva, G., 189-NDA-4, 258-APA-26 Satou, Y., 92-SCS-2, 145-SCS-3 Schrempp, M., 36-MST-2 Selfridge, J., 18-GNC-1 Sherer, S., 363-APA-35 Silva, W., 146-SD-6 Sattelmayer, T., 342-PC-18 Schreyer, A., 309-AMT-5 Selig, M., 113-APA-12, 202-UMS-3, 311-APA-31, Sherry, M., 303-WE-12 Silva-Martinez, J., 200-SUR-1 Sauder, J., 292-SCS-7 Schrijer, F., 322-FD-44 346-SCS-8, 354-WE-13 Sheshadri, A., 370-FD-47 Silver, M., 195-SCS-4 Saunders, R., 154-AS-2 Schrock, C., 13-FD-3 Sell, B., 279-HSABP-9/GTE-8 Sheta, E., 3-AA-1 Sim, J., 90-PC-7 Saunders-Smits, G., 317-EDU-1 Schroeder, J., 35-MST-1, 138-MST-5 Sellers, W., 429-GT-11 Sheth, R., 315-AS-6 Simao Ferreira, C., 51-WE-2, 152-WE-5, 215-APA-21 Saupe, F., 425-GNC-42 Schroeder, W., 420-FD-55 Selvam, M., 414-CMS-1 Shewhart, A., 75-GTE-2 Simeone, S., 7-APA-1 Sawada, K., 13-FD-3, 59-APA-7, 161-APA-16 Schueltke, F., 404-ACD-7 Selvarathinam, A., 437-STR-20 Shi, J., 377-GNC-39 Simmons, S., 127-GT-2 Sawaki, Y., 161-APA-16 Schuet, S., 232-IS-7, 325-GNC-31 Semenov, A., 127-GT-2 Shi, K., 263-FD-32 Simms, G., 89-PC-6 Sawant, S., 15-FD-5 Schulte, A., 27-IS-1 Semper, S., 179-GNC-20 Shi, L., 370-FD-47 Simonetti, A., 166-DA-1 Sawyer, J., 290-PDL-5 Schulze, M., 342-PC-18 Sengezer, E., 31-MAT-1 Shi, P., 434-SD-20 Simonis, K., 108-AFM-5 Sayles, A., 434-SD-20 Schulze, P., 56-AFM-4, 325-GNC-31 Sengupta, P., 180-GTE-4 Shi, R., 185-MDO-5 Simpson, J., 165-AS-3 Scanlan, J., 33-MDO-1, 202-UMS-3 Schumacher, C., 183-IS-6 Senses, B., 34-MDO-2 Shi, Y., 85-MST-4, 237-MST-9 Simpson, R., 44-SD-3 Scarano, F., 203-WE-7, 322-FD-44 Schutte, J., 107-ACD-1, 157-AA-6 Seo, S., 192-PC-12 Shields, C., 29-ISC-4 Simsek, O., 308-AFM-11 Scarborough, D., 41-PC-4, 192-PC-12, 266-FD-35 Schuurman, M., 317-EDU-1 Serrani, A., 327-GNC-33 Shields, M., 327-GNC-33 Simsiriwong, J., 184-MAT-7, 249-STR-13 Scarth, C., 189-NDA-4 Schwaab, Q., 269-FD-38 Serrano Galiano, S., 270-FD-39 Shih, T., 250-TP-6, 299-TES-1 Singh, A., 268-FD-37, 289-PC-16, 306-ABPSI-1 Schairer, E., 361-AMT-6/GT-7, 407-AMT-8 Schwartzentruber, T., 49-TP-1, 99-TP-3, 300-TP-7, Sertse, H., 83-MAT-4, 97-STR-6 Shim, D., 175-GNC-16 Singh, K., 295-SD-12 Scharf, D., 176-GNC-17 353-TP-8 Sescu, A., 62-FD-7, 105-AA-3 Shimomura, T., 227-GNC-24 Singh, R., 214-APA-20 Scharnhorst, R., 306-ABPSI-1 Schweickart, R., 48-STR-3, 428-GT-10 Seume, J., 354-WE-13, 361-AMT-6/GT-7 Shimoyama, K., 157-AA-6 Singh, S., 377-GNC-39 Author/Session Chair Index Sinkovec, B., 401-TES-3 Song, W., 43-SD-2 Steele, A., 354-WE-13 Subbarao, K., 333-IS-11, 423-GNC-40 Taha, H., 313-APA-33, 327-GNC-33 Sirigu, G., 35-MST-1 Sorensen, K., 65-FD-10 Steele, B., 424-GNC-41 Subbareddy, P., 62-FD-7, 402-TP-9 Tahara, H., 194-SATS-1 Sirk, A., 247-SRE-1 Sorgenfrei, M., 179-GNC-20 Stefani, F., 290-PDL-5 Subramanian, G., 345-SATS-2, 433-SATS-4 Taira, K., 171-FD-23, 221-FD-29, 270-FD-39, 372-FD-49 Sirohi, J., 43-SD-2, 294-SD-11, 416-FD-51/PDL-12 Sotak, M., 132-ICC-1 Steffens, M., 406-AFM-15 Subramanian, N., 83-MAT-4 Tak, B., 36-MST-2 Sitaraman, J., 10-APA-4, 172-FD-24, 236-MDO-6, Sotiropoulos, F., 101-WE-3, 303-WE-12 Steijl, R., 108-AFM-5, 364-APA-36 Subramanian, S., 24-GTE-1, 75-GTE-2 Takahashi, H., 356-ABPSI-2 370-FD-47, 381-MDO-9 Sotoudeh, Z., 147-SD-7, 248-STR-12, 434-SD-20 Stein, C., 154-AS-2 Suciu, G., 17-GEPC-1 Takahashi, K., 191-PC-11 Siu, N., 17-GEPC-1 Soulopoulos, N., 40-PC-3 Stein, J., 315-AS-6 Sudalagunta, P., 245-SD-9 Takahashi, M., 70-GNC-6, 227-GNC-24, 276-GNC-29 Sivasubramanian, B., 348-SD-15 Sowers, T., 306-ABPSI-1 Steinberg, A., 91-PC-8, 143-PC-10 Suder, K., 69-GEPC-2 Takahashi, T., 33-MDO-1, 84-MDO-3, 137-MDO-4, Sivilli, R., 233-IS-8 Soykasap, O., 195-SCS-4 Steinfeldt, B., 108-AFM-5, 167-DE-2 Suga, Y., 384-NDA-8 307-ACD-4, 357-ACD-5, 404-ACD-7 Skiba, A., 41-PC-4 Sørensen, J., 311-APA-31 Stelldinger, E., 86-MVC-2 Suganuma, Y., 257-APA-25 Takai, M., 145-SCS-3 Skomin, P., 191-PC-11, 317-EDU-1 Sørensen, N., 215-APA-21 Stepanov, V., 26-HSABP-1 Sugioka, Y., 6-AMT-1 Takaki, R., 172-FD-24 Skuratov, A., 222-FD-30 Spagnolo, S., 59-APA-7 Stepanyan, S., 142-PC-9 Suh, P., 237-MST-9 Takano, H., 375-GNC-37 Slabaugh, C., 143-PC-10 Spak, K., 147-SD-7 Stepanyan, V., 70-GNC-6 Suk, J., 194-SATS-1, 273-GNC-26, 382-MST-14 Takarics, B., 359-AFM-12 Slaby, M., 15-FD-5 Spedding, G., 7-APA-1 Stephan, J., 375-GNC-37 Suleman, A., 148-STR-7 Takeichi, N., 138-MST-5 Slais, T., 41-PC-4, 266-FD-35 Spencer, G., 171-FD-23 Stephan, T., 271-GEPC-4/SAT-1 Sullivan, J., 6-AMT-1 Takeno, J., 157-AA-6 Slater, J., 147-SD-7, 239-NDA-5 Speth, R., 156-AA-5 Stephani, K., 291-PDL-6 Sullivan, R., 46-STR-1, 249-STR-13 Takita, Y., 257-APA-25 Sledge, I., 77-IS-3 Spetzler, M., 274-GNC-27 Stephen, E., 26-HSABP-1, 222-FD-30 Sultan, C., 70-GNC-6, 245-SD-9, 315-AS-6 Tal, E., 392-SD-16 Slinger, C., 253-WE-10 Speyer, J., 374-GNC-36 Stepp, N., 80-ISC-3 Sun, C., 235-MAT-9, 427-GNC-44 Taleb, Y., 433-SATS-4 Slipchenko, M., 256-AMT-4 Spietz, P., 391-SCS-9 Sterling, A., 281-MAT-10 Sun, L., 225-GNC-22 Taligoski, J., 113-APA-12 Sloan, S., 2-ISC-1 Spillers, R., 269-FD-38, 277-GT-4 Stern, E., 300-TP-7 Sun, T., 74-GNC-10 Talleur, D., 232-IS-7 Slotnick, J., 86-MVC-2 Spivey, N., 436-SD-22 Stevens, C., 130-HSABP-3, 230-HSABP-7, Sun, W., 38-PC-1, 142-PC-9, 289-PC-16, 343-PDL-7 Talley, D., 342-PC-18 Smarslok, B., 140-NDA-3, 339-NDA-7, 384-NDA-8, Spottswood, S., 347-SD-14 279-HSABP-9/GTE-8 Sun, Y., 63-FD-8 Talnikar, C., 415-FD-50 435-SD-21 Sprague, M., 302-WE-11 Stewart, S., 204-WE-8 Sunada, Y., 11-FD-1, 162-APA-17 Tamijani, A., 398-STR-17 Smeltzer, S., 199-STR-11 Springer, R., 231-HSABP-8 Stier, B., 399-STR-18 Sundararaghavan, V., 31-MAT-1, 95-STR-4 Taminger, K., 351-SRE-2 189 Smith, A., 79-ISC-2 Sproul, A., 437-STR-20 Stipcich, G., 170-FD-22 Suo, Q., 108-AFM-5 Tampi, S., 400-STR-19 Smith, B., 114-APA-13, 220-FD-28 Sreehari, V., 298-STR-15 Stockton, N., 183-IS-6 Suplisson, A., 273-GNC-26 Tan, R., 151-UMS-2 Smith, E., 196-SD-8, 294-SD-11 Sreeja, S., 21-GNC-4 Stoddard, W., 181-HSABP-5 Surka, D., 233-IS-8 Tanaka, H., 292-SCS-7 Smith, J., 247-SRE-1, 331-GTE-7, 421-FD-56 Sreenivas, K., 50-WE-1, 51-WE-2, 153-WE-6, 278-GTE-6 Stodieck, O., 93-SD-4 Surratt, M., 85-MST-4 Tanaka, K., 48-STR-3 Smith, L., 231-HSABP-8, 241-PC-13, 418-FD-53 Sridhar, M., 58-APA-6 Stoellinger, M., 13-FD-3, 420-FD-55 Surti, T., 398-STR-17 Tanaka, N., 357-ACD-5 Smith, M., 117-FD-14, 180-GTE-4, 309-AMT-5, Sridhar, S., 430-IS-13 Stoevesandt, B., 152-WE-5 Surzhikov, S., 201-TP-5, 363-APA-35, 389-PDL-11 Tancred, J., 363-APA-35 365-APA-37, 407-AMT-8, 410-APA-40 Sringeri, S., 197-STR-9 Stookesberry, D., 114-APA-13 Sutcliffe, P., 330-GT-6 Tang, C., 49-TP-1 Smith, N., 278-GTE-6 Srinivasan, G., 367-AS-7 Storms, B., 362-AMT-7 Sutton, J., 38-PC-1, 41-PC-4, 110-AMT-2, 143-PC-10, Tang, D., 202-UMS-3 Smith, P., 335-MAT-13 Srivastava, A., 332-IS-10 Stouffer, S., 89-PC-6, 213-AMT-3 213-AMT-3, 256-AMT-4 Tang, G., 406-AFM-15 Smith, S., 40-PC-3, 346-SCS-8 Srivastava, N., 51-WE-2 Stoumbos, T., 44-SD-3, 400-STR-19, 434-SD-20 Suzuki, S., 348-SD-15 Tang, H., 343-PDL-7, 344-PDL-8 Smith, T., 131-HSABP-4 St. George, A., 130-HSABP-3, 181-HSABP-5, Straub, J., 77-IS-3, 194-SATS-1, 345-SATS-2, Suzuki, T., 201-TP-5 Tang, J., 121-FD-18, 140-NDA-3, 241-PC-13 Smyers, B., 219-AS-4 230-HSABP-7, 279-HSABP-9/GTE-8 390-SATS-3, 433-SATS-4 Swank, A., 72-GNC-8 Tang, Y., 241-PC-13 Snyder, M., 126-GNC-15 Stachura, M., 20-GNC-3 Straub, M., 276-GNC-29 Swann, M., 33-MDO-1 Tang, Z., 214-APA-20 Snyder, P., 180-GTE-4 Stallngs, D., 33-MDO-1 Straubel, M., 391-SCS-9 Swasey, R., 29-ISC-4 Tangirala, V., 181-HSABP-5 Snyder, S., 123-GNC-12 Stalnov, O., 59-APA-7 Strawson, J., 167-DE-2 Sweet, B., 139-MST-6 Tani, H., 90-PC-7 Sobester, A., 33-MDO-1, 77-IS-3, 84-MDO-3, Stanek, M., 144-PDL-2 Streett, C., 115-APA-14 Swei, S., 28-IS-2, 147-SD-7, 392-SD-16, 427-GNC-44 Tani, N., 98-TP-2 202-UMS-3, 209-ACD-2 Stanford, B., 198-STR-10, 236-MDO-6 Strike, J., 203-WE-7, 428-GT-10 Swenson, E., 85-MST-4 Tani, Y., 440-TP-10 Sobieczky, H., 310-APA-30 Stanley, S., 181-HSABP-5 Strobl, T., 8-APA-2 Swenson, H., 275-GNC-28 Tanimoto, R., 49-TP-1 Sobiesiak, L., 226-GNC-23 Stansbury, R., 100-UMS-1, 202-UMS-3, 251-UMS-4 Strömbäck, P., 21-GNC-4 Swiler, L., 103-APA-9/NDA-1 Tanner, G., 335-MAT-13 Söderberg, R., 339-NDA-7 Staples, D., 186-MST-7 Strong, S., 439-TES-4 Sydney, A., 57-APA-5 Tanno, H., 49-TP-1, 57-APA-5 Sodja, J., 165-AS-3, 394-SD-18 Starikovskaia, S., 88-PC-5, 142-PC-9, 193-PDL-3 Strub, G., 36-MST-2 Sydney, N., 375-GNC-37 Tantaroudas, N., 56-AFM-4 Sofge, D., 375-GNC-37 Starikovskiy, A., 38-PC-1, 88-PC-5, 142-PC-9, Struminskaya, I., 222-FD-30 Sydnor, G., 23-GT-1 Tao, C., 195-SCS-4 Soler, G., 350-SOF-1 229-GTE-5, 341-PC-17 Stubblebine, A., 78-IS-4, 430-IS-13 Syred, N., 352-TES-2, 439-TES-4 Tardif, P., 263-FD-32 Soliman, H., 244-SCS-6 Starin, S., 72-GNC-8 Stumpf, E., 404-ACD-7, 405-ACD-8 Szilder, K., 111-APA-10 Tartaruga, I., 393-SD-17 Son, O., 270-FD-39 Starr, M., 267-FD-36 Stupik, J., 19-GNC-2 Tabanli, H., 26-HSABP-1 Tatsukawa, T., 67-FD-12/PDL-1, 78-IS-4 Sondergaard, R., 269-FD-38 Stassen, H., 166-DA-1 Su, W., 43-SD-2, 94-SD-5, 435-SD-21 Tagashira, T., 128-GTE-3 Taub, I., 21-GNC-4 Song, H., 117-FD-14, 435-SD-21 Stastny, T., 423-GNC-40 Su, Y., 235-MAT-9 Taghavi, R., 85-MST-4, 408-AMT-9 Taubert, L., 164-APA-19/FD-19 Song, S., 174-FD-26 Steck, J., 382-MST-14, 424-GNC-41 Subba Reddiar Pappu, V., 424-GNC-41 Taguchi, M., 363-APA-35 Taur, D., 73-GNC-9, 126-GNC-15 Author/Session Chair Index Tavares, C., 2-ISC-1 Thorne, J., 117-FD-14 Tran, T., 274-GNC-27, 424-GNC-41 Unnikrishnan, V., 136-MAT-6 Vasista, S., 219-AS-4 Tawfik, T., 168-FD-20 Thorsson, S., 197-STR-9 Trask, R., 184-MAT-7 Upadhyay, C., 199-STR-11 Vassberg, J., 60-APA-8, 220-FD-28, 413-APA-43 Taylor, B., 174-FD-26, 186-MST-7 Threadgill, J., 419-FD-54 Travaglini, L., 44-SD-3, 219-AS-4 Upadhyay, P., 66-FD-11 Vasu, S., 89-PC-6, 213-AMT-3, 229-GTE-5 Taylor, J., 267-FD-36 Thurier, P., 219-AS-4 Trawny, N., 71-GNC-7, 176-GNC-17 Upadhyaya, P., 437-STR-20 Vazquez, A., 31-MAT-1 Taylor, L., 50-WE-1, 51-WE-2, 153-WE-6 Thurow, B., 110-AMT-2, 256-AMT-4, 361-AMT-6/GT-7 Trepanier, J., 366-APA-38 Urakubo, T., 151-UMS-2 Vedula, P., 99-TP-3 Taylor, N., 86-MVC-2, 160-APA-15, 209-ACD-2, Tian, R., 11-FD-1 Trevino, L., 300-TP-7 Uranga, A., 17-GEPC-1 Vega, K., 337-MST-12 285-MVC-5 Tian, W., 354-WE-13 Trinh, G., 194-SATS-1 Üre, N., 132-ICC-1 Vegh, J., 357-ACD-5 Taylor, P., 295-SD-12, 393-SD-17 Tibaldi, C., 101-WE-3, 253-WE-10 Troldborg, N., 215-APA-21 Urnes, J., 392-SD-16 Velez, C., 213-AMT-3 Taylor, R., 438-STR-21 Tichenor, N., 416-FD-51/PDL-12 Trombetta, J., 200-SUR-1 Usui, H., 291-PDL-6 Velicki, A., 398-STR-17 Tchatchueng Kammegne, M., 262-AS-5 Tiemsin, P., 256-AMT-4 Tropina, A., 256-AMT-4 Utyuzhnikov, S., 34-MDO-2 Venetis, I., 12-FD-2 Tegtmeier, C., 415-FD-50 Tigges, M., 376-GNC-38 Trujillo, A., 139-MST-6 Uzol, O., 102-WE-4 Venkataraman, R., 177-GNC-18 Tekin, R., 21-GNC-4, 126-GNC-15, 178-GNC-19 Tilmann, C., 259-APA-27 Truong, H., 392-SD-16 Uzumcu, S., 232-IS-7 Venkatesh, V., 82-MAT-3 Tekinalp, O., 124-GNC-13, 276-GNC-29, 308-AFM-11, Timme, S., 412-APA-42 Tsai, C., 267-FD-36 Uzun, A., 113-APA-12 Vera, J., 98-TP-2 328-GNC-34, 426-GNC-43 Tinelli, C., 397-SOF-2 Tsao, H., 331-GTE-7 Vaddi, V., 275-GNC-28 Verberg, R., 163-APA-18, 314-APA-34 Telidetzki, K., 60-APA-8 Ting, E., 293-SD-10, 392-SD-16 Tsolas, N., 38-PC-1 Valasek, J., 224-GNC-21, 308-AFM-11 Verelst, D., 101-WE-3 Temme, J., 41-PC-4 Tippur, H., 184-MAT-7 Tsosie, J., 2-ISC-1 Valdez, J., 179-GNC-20 Vergnol, A., 72-GNC-8 Templon, N., 330-GT-6 Tirri, A., 100-UMS-1 Tsoutsanis, P., 68-FD-13, 169-FD-21 Vale, J., 148-STR-7 Verma, S., 26-HSABP-1 Teng, T., 431-MST-16 Tischler, M., 5-AFM-2, 186-MST-7, 338-MST-13 Tsuboi, N., 388-PC-20 Valentich, G., 54-AA-2 Vescovini, R., 44-SD-3 Teodorescu, M., 28-IS-2, 147-SD-7 Tishkoff, J., 38-PC-1 Tsuchiya, T., 137-MDO-4, 275-GNC-28, 286-NDA-6 Valentini, P., 99-TP-3, 353-TP-8 Vian, J., 132-ICC-1 Teope, K., 279-HSABP-9/GTE-8 Tiso, P., 148-STR-7 Tsunoda, A., 98-TP-2 Valenzuela-del Río, J., 384-NDA-8 Viana, F., 34-MDO-2 Terashima, H., 90-PC-7, 388-PC-20 Titchener, N., 17-GEPC-1 Tsushima, N., 94-SD-5 Valera-Medina, A., 352-TES-2, 439-TES-4 Viaud, F., 425-GNC-42 Terashima, K., 244-SCS-6 Tobias, E., 338-MST-13 Tsutsumi, S., 172-FD-24, 208-AA-7 Valle, G., 346-SCS-8 Vich, O., 395-SD-19 Terekhov, I., 349-SE-1 Tobin, S., 402-TP-9 Tu, S., 117-FD-14 Vallée, N., 342-PC-18 Vieira, D., 411-APA-41 TerMaath, S., 400-STR-19, 437-STR-20 Togai, K., 38-PC-1 Tucker, E., 378-GT-8 Valyou, D., 204-WE-8, 395-SD-19 Viertler, F., 383-MST-15 190 Terning, B., 393-SD-17 Togayev, A., 272-GNC-25 Tucker, M., 385-OPS-1 van Bussel, G., 51-WE-2 Vijayakumar, N., 432-MVC-6 Tescione, G., 152-WE-5 Tognaccini, R., 266-FD-35 Tucker, P., 63-FD-8, 75-GTE-2, 105-AA-3, 128-GTE-3 Van Dam, C., 101-WE-3, 153-WE-6, 258-APA-26 Vijgen, P. 112-APA-11, 411-APA-41 Tesfahunegn, Y., 60-APA-8, 160-APA-15, 189-NDA-4 Tokudome, S., 208-AA-7 Tuckey, T., 10-APA-4 Van der Haegen, V., 440-TP-10 Villalpando, C., 71-GNC-7 Tessler, A., 438-STR-21 Tola, C., 204-WE-8 Tuegel, E., 81-LEC-2, 189-NDA-4 Van Dyne, D., 52-SCS-1 Villalva Gomez, R., 192-PC-12, 229-GTE-5 Teunisse, N., 148-STR-7 Tomac, M., 64-FD-9 Tufts, M., 112-APA-11, 258-APA-26 Van Every, D., 428-GT-10 Villanueva, D., 140-NDA-3 Tewes, P., 164-APA-19/FD-19 Tomar, V., 234-MAT-8 Tuggle, R., 45-SEN-1 Van Eykeren, L., 272-GNC-25 Vinogradov, V., 26-HSABP-1 Thacker, B., 239-NDA-5 Tomek, W., 163-APA-18 Tumuklu, O., 318-FD-40 Van Hall, J., 336-MDO-8 Viquerat, A., 145-SCS-3, 346-SCS-8 Thakur, S., 12-FD-2, 40-PC-3 Tomioka, S., 137-MDO-4, 356-ABPSI-2 Turin, P., 337-MST-12 Van Haver, S., 358-ACD-6 Visbal, M., 62-FD-7, 67-FD-12/PDL-1, 221-FD-29, Thalakkottor, J., 267-FD-36 Tomita, T., 356-ABPSI-2 Turkoglu, K., 132-ICC-1, 151-UMS-2, 179-GNC-20, Van Kampen, E., 100-UMS-1, 122-GNC-11, 158-AFM-7, 223-FD-31, 265-FD-34 Thamm, R., 238-MST-10 Ton, C., 375-GNC-37 405-ACD-8 177-GNC-18, 238-MST-10, 272-GNC-25, 373-GNC-35, Visconti, U., 394-SD-18 Thapa Magar, K., 253-WE-10 Tong, O., 172-FD-24 Turner, M., 13-FD-3, 271-GEPC-4/SAT-1 374-GNC-36, 423-GNC-40, 431-MST-16 Viska, S., 151-UMS-2 Theis, J., 359-AFM-12, 425-GNC-42 Tong, W., 381-MDO-9 Turner, T., 154-AS-2, 165-AS-3 van Kuik, G., 302-WE-11 Visonneau, M., 14-FD-4 Theodore, C., 196-SD-8 Tong, Z., 160-APA-15 Turpin, J., 198-STR-10 van Oudheusden, B., 322-FD-44 Visser, T., 158-AFM-7 Theodoulis, S., 36-MST-2, 126-GNC-15, 327-GNC-33 Tonini, G., 151-UMS-2 Tuttle, S., 241-PC-13 van Paassen, M., 85-MST-4 Vitek, J., 204-WE-8 Theuerkauf, S., 341-PC-17 Torens, C., 350-SOF-1 Tweddle, B., 176-GNC-17 van Schie, S., 209-ACD-2 Vizcaino, J., 351-SRE-2 Theunissen, R., 51-WE-2 Tormalm, M., 64-FD-9 Tyacke, J., 75-GTE-2, 105-AA-3 van Tooren, M., 84-MDO-3 Voce, N., 174-FD-26 Thoemel, J., 440-TP-10 Toropov, V., 336-MDO-8 Tyagi, A., 7-APA-1 Van Zante, D., 69-GEPC-2 Vogel, M., 235-MAT-9 Thomas, F., 216-APA-22, 223-FD-31 Torres, J., 36-MST-2 Uchiyama, K., 375-GNC-37, 377-GNC-39 Van Zwieten, T., 376-GNC-38 Vogel, R., 235-MAT-9 Thomas, J., 302-WE-11, 371-FD-48 Totani, K., 201-TP-5 Uehara, D., 294-SD-11 Vanden, K., 59-APA-7, 410-APA-40 von Gosen, F., 164-APA-19/FD-19 Thomas, R., 69-GEPC-2, 255-AA-8 Totoki, H., 124-GNC-13 Ueno, M., 127-GT-2 Vanderwyst, A., 73-GNC-9, 310-APA-30 von Knoblauch, F., 295-SD-12 Thompson, D., 8-APA-2 Toxopeus, S., 14-FD-4 Ui, K., 208-AA-7 Vane, Z., 266-FD-35 Voros, R., 396-SE-2 Thompson, L., 213-AMT-3 Toyoda, A., 261-APA-29 Uijt De Haag, M., 166-DA-1 Vanhove, G., 142-PC-9 Vos, R., 358-ACD-6, 404-ACD-7 Thompson, M., 301-UMS-5 Tracey, B., 268-FD-37 Ukeiley, L., 3-AA-1, 58-APA-6, 221-FD-29, 259-APA-27 Vanlanduit, S., 395-SD-19 Voutsinas, S., 102-WE-4 Thompson, P., 56-AFM-4 Tran, A., 96-STR-5 Ulbrich, N., 429-GT-11 Varghese, P., 119-FD-16 Voyles, I., 286-NDA-6 Thompson, R., 36-MST-2, 391-SCS-9, 428-GT-10 Tran, D., 301-UMS-5 Ulrich, S., 179-GNC-20, 337-MST-12, 377-GNC-39 Varney, J., 80-ISC-3 Vu, B., 12-FD-2 Thompson, S., 281-MAT-10 Tran, H., 132-ICC-1 Ulybyshev, D., 204-WE-8 Vasconcellos, R., 295-SD-12 Vu, T., 238-MST-10, 328-GNC-34 Thompson, V., 271-GEPC-4/SAT-1 Tran, J., 43-SD-2 Umezawa, K., 297-STR-14 Vasilevskii, E., 49-TP-1 Vukasinovic, B., 171-FD-23 Thomson, M., 292-SCS-7 Tran, S., 216-APA-22 Umezawa, M., 291-PDL-6 Vasisht, S., 273-GNC-26 Vyas, V., 146-SD-6, 147-SD-7 Author/Session Chair Index W.Case, S., 282-MAT-11 Wang, W., 59-APA-7, 113-APA-12, 289-PC-16 Wendt, F., 252-WE-9 Wilroy, J., 11-FD-1 Wu, W., 82-MAT-3 Waas, A., 47-STR-2, 95-STR-4, 97-STR-6, 197-STR-9, Wang, X., 84-MDO-3, 85-MST-4, 113-APA-12, Weng, H., 49-TP-1 Wilson, J., 128-GTE-3, 168-FD-20 Wu, Y., 94-SD-5, 110-AMT-2 199-STR-11, 298-STR-15, 399-STR-18 146-SD-6, 147-SD-7, 173-FD-25, 244-SCS-6, Werner, H., 359-AFM-12, 425-GNC-42 Wilson, S., 7-APA-1, 131-HSABP-4 Wu, Z., 95-STR-4, 140-NDA-3, 291-PDL-6, 298-STR-15, Wabel, T., 41-PC-4 388-PC-20, 435-SD-21 Werner, S., 143-PC-10 Wilson, T., 393-SD-17 395-SD-19 Wachspress, D., 260-APA-28, 365-APA-37 Wang, Y., 43-SD-2, 56-AFM-4, 158-AFM-7, Wernert, P., 211-AFM-9 Wilson, W., 71-GNC-7 Wurst, M., 13-FD-3 Wada, K., 208-AA-7 216-APA-22, 244-SCS-6, 388-PC-20, 435-SD-21 Wernet, M., 54-AA-2 Winchester, J., 415-FD-50 Wygnanski, I., 164-APA-19/FD-19 Wada, T., 38-PC-1, 142-PC-9 Wang, Z., 50-WE-1, 70-GNC-6, 117-FD-14, 179-GNC-20, Wersinger, J., 2-ISC-1 Windom, B., 91-PC-8 Wynn, A., 43-SD-2 Waddel, M., 26-HSABP-1 224-GNC-21, 227-GNC-24, 265-FD-34, 268-FD-37, Werter, N., 61-AS-1 Winer, E., 185-MDO-5 Xargay, E., 123-GNC-12, 232-IS-7 Wadhams, T., 277-GT-4, 369-FD-46 292-SCS-7, 295-SD-12, 321-FD-43, 354-WE-13, Wertz, J., 198-STR-10 Winski, C., 218-APA-24 Xia, Q., 291-PDL-6 Wagner, A., 6-AMT-1 370-FD-47 West, D., 112-APA-11 Winter, M., 201-TP-5, 428-GT-10 Xia, X., 168-FD-20, 411-APA-41 Wagner, C., 321-FD-43 Wanthal, S., 97-STR-6, 281-MAT-10, 334-MAT-12 West, M., 29-ISC-4 Winternitz, L., 179-GNC-20 Xia, Y., 118-FD-15, 170-FD-22 Wagner, J., 256-AMT-4, 269-FD-38, 277-GT-4, Ward, M., 18-GNC-1 West, S., 48-STR-3 Winters, C., 193-PDL-3 Xiang, J., 94-SD-5, 169-FD-21, 198-STR-10, 245-SD-9, 309-AMT-5 Warde, S., 47-STR-2 West, T., 103-APA-9/NDA-1, 261-APA-29 Wintzer, M., 218-APA-24 394-SD-18 Wagnild, R., 369-FD-46 Wardle, B., 31-MAT-1, 149-STR-8, 367-AS-7 Wetzel, K., 50-WE-1, 96-STR-5, 252-WE-9 Wischek, J., 180-GTE-4 Xiao, S., 199-STR-11 Wahidi, R., 11-FD-1, 319-FD-41 Warren, J., 92-SCS-2, 292-SCS-7 Wey, C., 24-GTE-1, 323-GEPC-3 Wischt, R., 394-SD-18 Xiao, X., 121-FD-18 Wahls, R., 17-GEPC-1 Warren, P., 195-SCS-4 Whalen, E., 7-APA-1, 164-APA-19/FD-19 Wisnom, M., 334-MAT-12 Xie, J., 197-STR-9, 332-IS-10 Waindim, M., 322-FD-44 Washburn, A., 164-APA-19/FD-19 Wheaton, B., 62-FD-7 Wissink, A., 10-APA-4, 172-FD-24 Xie, K., 291-PDL-6, 428-GT-10 Waite, J., 295-SD-12 Watanabe, H., 377-GNC-39 Whitacre, W., 22-GNC-5, 74-GNC-10 Witeof, Z., 347-SD-14 Xie, P., 359-AFM-12 Waithe, K., 218-APA-24, 261-APA-29 Watanabe, K., 300-TP-7 Whitcomb, J., 83-MAT-4 Witteveen, J., 140-NDA-3, 339-NDA-7 Xin, M., 74-GNC-10 Wake, B., 260-APA-28 Watanabe, T., 67-FD-12/PDL-1, 78-IS-4, 128-GTE-3 White, C., 48-STR-3 Wlezien, R., 62-FD-7, 416-FD-51/PDL-12 Xiong, F., 107-ACD-1, 374-GNC-36 Waldman, J., 391-SCS-9 Waters, D., 128-GTE-3 White, E., 121-FD-18, 134-LEC-3, 203-WE-7 Woerner, P., 32-MAT-2 Xiong, J., 208-AA-7 Waldman, R., 8-APA-2 Watkins, S., 67-FD-12/PDL-1 White, L., 342-PC-18 Wohl, C., 256-AMT-4 Xiong, Y., 374-GNC-36 Waldmann, A., 228-GT-3 Watson, L., 245-SD-9 White, S., 95-STR-4 Wohlbier, J., 65-FD-10 Xiong, Z., 373-GNC-35 Wales, C., 219-AS-4 Watson, R., 128-GTE-3 White, T., 402-TP-9 Woike, M., 361-AMT-6/GT-7 Xu, H., 410-APA-40 191 Walker, A., 183-IS-6 Watton, J., 82-MAT-3 Whiteaker, K., 428-GT-10 Wolf, C., 311-APA-31 Xu, J., 373-GNC-35 Walker, D., 200-SUR-1 Wayman, T., 428-GT-10 Whitehouse, G., 260-APA-28, 365-APA-37 Wolf, W., 266-FD-35 Xu, K., 290-PDL-5 Walker, E., 103-APA-9/NDA-1, 127-GT-2, 261-APA-29, Weatheritt, J., 68-FD-13 Whiteley, M., 144-PDL-2 Wolff, M., 96-STR-5, 441-TP-11 Xu, L., 72-GNC-8, 357-ACD-5 329-GT-5, 361-AMT-6/GT-7 Weaver, A., 299-TES-1 Wick, A., 312-APA-32 Wolff, T., 354-WE-13 Xu, R., 276-GNC-29 Walker, M., 265-FD-34 Weaver, J., 382-MST-14 Wickramasinghe, N., 273-GNC-26 Won, S., 38-PC-1, 91-PC-8, 289-PC-16 Xu, S., 63-FD-8, 377-GNC-39, 415-FD-50 Walker, S., 85-MST-4 Weaver, P., 93-SD-4, 95-STR-4, 189-NDA-4, 198-STR-10, Wicks, M., 216-APA-22 Wong, H., 300-TP-7 Xu, X., 106-AA-4, 412-APA-42 Wall, J., 376-GNC-38 297-STR-14, 298-STR-15 Wicks, S., 31-MAT-1 Wong, S., 233-IS-8 Xu, Y., 226-GNC-23, 343-PDL-7 Wallace, B., 204-WE-8 Webb, N., 416-FD-51/PDL-12 Wiebe, R., 384-NDA-8 Woodard, B., 257-APA-25 Xuan, L., 118-FD-15 Waller, D., 48-STR-3, 391-SCS-9, 428-GT-10 Webster, J., 19-GNC-2 Wienke, F., 302-WE-11 Woodbury, T., 224-GNC-21, 308-AFM-11 Xue, B., 374-GNC-36 Walsh, P., 26-HSABP-1 Webster, R., 278-GTE-6 Wiese, C., 80-ISC-3 Woodgate, M., 311-APA-31 Yakeno, A., 67-FD-12/PDL-1 Walsh, S., 389-PDL-11 Weekes, B., 43-SD-2 Wiese, D., 373-GNC-35 Woolsey, C., 224-GNC-21 Yalin, A., 193-PDL-3, 389-PDL-11 Walter, R., 243-PDL-13 Wegener, J., 342-PC-18 Wieseman, C., 236-MDO-6 Woopen, M., 432-MVC-6 Yamada, J., 145-SCS-3 Waltz, J., 65-FD-10 Wehrmeyer, J., 309-AMT-5, 361-AMT-6/GT-7 Wieser, D., 259-APA-27 Work, D., 172-FD-24 Yamaguchi, I., 375-GNC-37 Wan, H., 250-TP-6 Wei, D., 241-PC-13 Wilcox, L., 427-GNC-44 Woszidlo, R., 164-APA-19/FD-19 Yamaguchi, Y., 257-APA-25 Wan, Y., 226-GNC-23, 332-IS-10 Wei, F., 116-DE-1 Wilder, M., 277-GT-4, 369-FD-46 Wrage, L., 397-SOF-2, 414-CMS-1 Yamakawa, H., 145-SCS-3 Wang, B., 343-PDL-7 Wei, J., 226-GNC-23 Wilhite, A., 96-STR-5 Wray, A., 402-TP-9 Yamamoto, K., 259-APA-27 Wang, C., 331-GTE-7 Wei, M., 43-SD-2 Wilkie, W., 92-SCS-2 Wray, T., 410-APA-40 Yamasaki, T., 375-GNC-37 Wang, G., 58-APA-6, 108-AFM-5, 262-AS-5 Wei, W., 78-IS-4, 430-IS-13 Wilkinson, M., 297-STR-14 Wright, A., 253-WE-10 Yamashita, J., 440-TP-10 Wang, H., 197-STR-9 Weier, T., 221-FD-29 Willcox, K., 34-MDO-2, 185-MDO-5, 283-MDO-7 Wright, C., 20-GNC-3 Yamazaki, M., 92-SCS-2 Wang, J., 121-FD-18, 167-DE-2, 224-GNC-21, Weihs, D., 241-PC-13 Willems, S., 369-FD-46 Wright, J., 12-FD-2, 127-GT-2 Yamazaki, W., 152-WE-5, 384-NDA-8 291-PDL-6, 365-APA-37 Weinstein, M., 226-GNC-23 Williams, B., 241-PC-13, Wright, M., 379-GT-9, 402-TP-9 Yan, G., 263-FD-32 Wang, K., 412-APA-42 Weintraub, I., 327-GNC-33 Williams, C., 382-MST-14 Wright, S., 277-GT-4 Yan, Y., 121-FD-18, 245-SD-9, 259-APA-27, 310-APA-30, Wang, L., 170-FD-22, 321-FD-43 Weiss, J., 269-FD-38, 429-GT-11 Williams, D., 221-FD-29, 323-GEPC-3 Wrist, A., 270-FD-39 319-FD-41, 418-FD-53 Wang, N., 241-PC-13 Weitl, R., 380-IS-12 Williams, G., 343-PDL-7 Wu, H., 281-MAT-10, 289-PC-16 Yan, Z., 313-APA-33 Wang, P., 110-AMT-2 Weitz, L., 166-DA-1 Williams, J., 326-GNC-32 Wu, J., 265-FD-34 Yang, B., 178-GNC-19, 180-GTE-4, 232-IS-7, 390-SATS-3 Wang, Q., 89-PC-6, 289-PC-16, 302-WE-11, Welch, G., 128-GTE-3 Williams, L., 241-PC-13 Wu, K., 198-STR-10 Yang, C., 140-NDA-3, 395-SD-19 322-FD-44, 415-FD-50 Welsh, W., 94-SD-5, 295-SD-12 Williams-Hayes, P., 212-AFM-10, 360-AFM-13 Wu, M., 35-MST-1, 275-GNC-28 Yang, J., 82-MAT-3, 93-SD-4 Wang, S., 31-MAT-1, 253-WE-10, 372-FD-49 Wen, C., 179-GNC-20 Willis, B., 297-STR-14, 395-SD-19, 436-SD-22 Wu, S., 435-SD-21 Yang, M., 31-MAT-1 Author/Session Chair Index Yang, S., 91-PC-8, 107-ACD-1, 113-APA-12, 203-WE-7, Yucelen, T., 28-IS-2, 125-GNC-14, 426-GNC-43 Zhao, X., 257-APA-25 343-PDL-7 Yurchenko, N., 221-FD-29 Zhao, Y., 107-ACD-1, 178-GNC-19 Yang, T., 165-AS-3 Z. Ben-Asher, J., 21-GNC-4 Zhao, Z., 226-GNC-23, 359-AFM-12, 416-FD-51/PDL-12 Yang, V., 88-PC-5, 343-PDL-7, 388-PC-20 Zaal, P., 139-MST-6 Zheltovodov, A., 222-FD-30 Yang, W., 343-PDL-7 Zacny, K., 247-SRE-1 Zhen, C., 394-SD-18 Yang, X., 38-PC-1, 89-PC-6, 101-WE-3 Zagnoli, D., 75-GTE-2 Zheng, J., 176-GNC-17, 198-STR-10, 416-FD-51/PDL-12 Yang, Y., 259-APA-27, 310-APA-30 Zahle, F., 101-WE-3, 215-APA-21 Zheng, M., 111-APA-10 Yang, Z., 223-FD-31, 364-APA-36 Zaidi, S., 309-AMT-5 Zheng-Chun, H., 237-MST-9 Yantek, S., 301-UMS-5 Zakar, D., 98-TP-2 Zhong, X., 173-FD-25 Yao, E., 235-MAT-9 Zakaria, M., 313-APA-33 Zhou, C., 268-FD-37, 321-FD-43 Yao, Y., 113-APA-12, 178-GNC-19, 222-FD-30, Zaki, A., 439-TES-4 Zhou, E., 399-STR-18 426-GNC-43 Zakrajsek, A., 235-MAT-9 Zhou, W., 75-GTE-2, 353-TP-8 Yasar, M., 237-MST-9, 423-GNC-40 Zaleksi, S., 90-PC-7 Zhou, Y., 332-IS-10 Yasue, K., 13-FD-3, 127-GT-2 Zaloglu, B., 372-FD-49 Zhou, Z., 227-GNC-24, 246-SD-13/GEPC-5, 292-SCS-7, Yavrucuk, I., 158-AFM-7, 424-GNC-41 Zaman, K., 156-AA-5 412-APA-42 Yechout, T., 57-APA-5 Zamanian, A., 408-AMT-9 Zhu, F., 7-APA-1, 310-APA-30 Yeh, C., 171-FD-23 Zander, M., 92-SCS-2 Zhu, G., 392-SD-16 Yen, Y., 299-TES-1, 342-PC-18, 401-TES-3 Zanforlin, R., 225-GNC-22 Zhu, H., 74-GNC-10 Yeo, D., 359-AFM-12, 375-GNC-37 Zanon, A., 152-WE-5 Zhu, J., 111-APA-10, 122-GNC-11 Yerkes, K., 441-TP-11 Zare-Behtash, H., 364-APA-36 Zhu, Q., 232-IS-7 Yetter, R., 38-PC-1 Zawodny, N., 157-AA-6 Zhu, T., 99-TP-3 Yi, S., 161-APA-16 Zdunek, A., 44-SD-3 Zhu, Y., 242-PC-14 Yin, C., 303-WE-12 Zeng, Z., 108-AFM-5 Zhupanska, O., 32-MAT-2, 46-STR-1, 149-STR-8 Yin, H., 395-SD-19 Zeppieri, S., 89-PC-6, 289-PC-16 Zientarski, L., 219-AS-4 192 Yin, P., 263-FD-32 Zetocha, P., 233-IS-8 Zilhão, L., 24-GTE-1 Yin, Z., 193-PDL-3 Zeune, C., 312-APA-32 Zillies, J., 251-UMS-4 Yocius, M., 166-DA-1 Zha, G., 93-SD-4, 162-APA-17, 261-APA-29, 263-FD-32, Zimmerman, C., 383-MST-15 Yokozeki, T., 244-SCS-6 364-APA-36 Zingg, D., 148-STR-7, 236-MDO-6, 371-FD-48, Yoo, Y., 194-SATS-1 Zhang, B., 370-FD-47 413-APA-43 Yoon, J., 67-FD-12/PDL-1 Zhang, C., 173-FD-25, 294-SD-11 Zink, G., 229-GTE-5 Yoon, S., 382-MST-14 Zhang, D., 97-STR-6, 199-STR-11 Zink, P., 146-SD-6 Yoon, W., 191-PC-11 Zhang, F., 373-GNC-35 Zipay, J., 198-STR-10 Yoshida, K., 4-AFM-1 Zhang, H., 374-GNC-36 Zolghadri, A., 125-GNC-14 Yoshino, S., 244-SCS-6 Zhang, J., 70-GNC-6, 215-APA-21, 227-GNC-24, Zorn, J., 63-FD-8 Young, D., 366-APA-38, 415-FD-50 292-SCS-7, 294-SD-11, 409-APA-39 Zou, R., 185-MDO-5 Young, J., 372-FD-49 Zhang, K., 8-APA-2, 149-STR-8 Zuercher, T., 151-UMS-2 Young, M., 159-AFM-8, 343-PDL-7 Zhang, L., 83-MAT-4, 149-STR-8, 359-AFM-12, Zuo, P., 59-APA-7 Young, R., 367-AS-7 388-PC-20 Zyluk, A., 359-AFM-12 Young, W., 281-MAT-10 Zhang, M., 413-APA-43 Yu, H., 9-APA-3 Zhang, P., 12-FD-2 Yu, K., 181-HSABP-5, 309-AMT-5 Zhang, Q., 439-TES-4 Yu, M., 117-FD-14 Zhang, R., 395-SD-19 Yu, P., 425-GNC-42 Zhang, T., 211-AFM-9, 334-MAT-12, 431-MST-16 Yu, W., 47-STR-2, 83-MAT-4, 97-STR-6, 147-SD-7, Zhang, W., 201-TP-5, 303-WE-12 149-STR-8, 219-AS-4, 297-STR-14 Zhang, X., 59-APA-7, 241-PC-13, 372-FD-49 Yu, Y., 373-GNC-35 Zhang, Y., 107-ACD-1, 142-PC-9, 160-APA-15, Yu, Z., 276-GNC-29, 197-STR-9 169-FD-21, 357-ACD-5, 406-AFM-15 Yuan, S., 362-AMT-7 Zhang, Z., 15-FD-5, 110-AMT-2, 232-IS-7 236-MDO-6, Yuan, W., 111-APA-10 268-FD-37, 269-FD-38, 270-FD-39, 290-PDL-5 Yuan, X., 122-GNC-11 Zhao, J., 187-MST-8 Yuceil, K., 26-HSABP-1 Zhao, Q., 365-APA-37, 411-APA-41 Yucel, A., 77-IS-3, 430-IS-13 Zhao, W., 246-SD-13/GEPC-5 IntroVenue Information

AIAA SciTech 2015 Technical Zones The technical program has been placed within the hotel in zones to keep related session topics and technical conference together. Please visit one of the zones to listen to a technical paper that is of interest to you!

ZONE ADS: Aerospace Design and Structures

ZONE AS: Aerospace Sciences

ZONE IS: Information Systems

Exposition Hall Lower Level of the Convention Center, 2 floors below AIAA Registration

Additional Hotel-Side Meeting Rooms: Hemingway & Sanchez Boardrooms Level 4 (hotel) via Emerald Bay Elevators

Orange Blossom Ballroom Atrium Level (hotel) on St. George Street

Emerald 1-8 Meeting Rooms Lower Level (hotel) via Emerald Bay Elevators

St. George Meeting Rooms Atrium Level (hotel) on St. George Street

Business Center Mezzanine Level of the Convention Center, 1 floor below AIAA Registration

www.aiaa-SciTech.org 54193 #aiaaSciTech IntroVenue Map

Forum 360

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FLAGLER VERO

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ZONE ADS: Aerospace Design and Structures

ZONE AS: Aerospace Sciences

ZONE IS: Information Systems

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Page 1 of 1 2O16 4–8 JANUARY 2016 SAN DIEGO, CA THANK YOU! Thank you for making AIAA SciTech 2015 an exceptional experience, where researchers from around the world can share the most original perspectives, collaborate on stimulating ideas, and inﬂ uence the future of aerospace. We hope that you accomplished your goals, learned something new, caught up with colleagues, and established new connections. We look forward to seeing you in 2016! Thanks to the individuals who spent hundreds of volunteer hours building a stellar program—the members of R the Executive Steering, Organizing, and Technical Program Committees.

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