The Largest Event for Aerospace Research, Development, and Technology

13–17 JANUARY 2014 NATIONAL HARBOR, MARYLAND

THE LARGEST EVENT FOR AEROSPACE RESEARCH, DEVELOPMENT, AND TECHNOLOGY

FINAL PROGRAM www.aiaa.org/scitech2014 #aiaaSciTech

ENGINEERING A WORLD OF ACTION At Lockheed Martin, we believe that our nation’s continuing prosperity hinges on a robust pipeline of engineering talent in emerging, multidisciplinary technology ﬁelds. Today, the engineering profession faces three distinct challenges: capacity of our technical talent to ﬁll future jobs, our engineering workforce’s capability to address increasingly complex challenges, and America’s competitiveness on the world stage. Lockheed Martin is proud to sponsor the AIAA SciTech Forum as they nurture and inspire new generations of engineers ready to address the challenges of the 21st century.

www.lockheedmartin.com Executive Steering Committee AIAA SciTech 2014

Welcome Robert Braun Dear Colleagues: Georgia Institute of Technology We are very excited to welcome you to the 2014 AIAA Science and Technology Forum and Exposition (SciTech 2014), the inaugural SciTech event in the new AIAA event model!

From the small, but brilliantly simple innovations that affect everyday life to the major discoveries and missions that fuel our collective drive to accomplish amazing things, AIAA SciTech 2014 will give you extensive access to a wide range of state-of- John Evans the-art thinking in aerospace research, development, and technology. Lockheed Martin As a steering committee, we’ve worked to develop plenary sessions that provide insights into some of the most pressing issues that face our industry and our profession today – R&D policy, affordability, and education. We think the stimulating conversations we have planned with some of the foremost thinkers and decision makers in these areas will provide context for the other panel sessions and technical presentations planned throughout the week.

James Shields New this year are panel sessions designed to build on each day’s opening plenaries Draper Laboratory to allow for a deeper dive into some of the issues we uncover in the morning discussions. We encourage you to take advantage of this opportunity to interact with industry leaders in these intimate settings and to share your knowledge and insights.

The SciTech 2014 technical paper program is second to none in terms of the breadth and depth of cutting-edge aerospace research it represents. Nowhere else can you hear about so many of the cool things this amazing industry is working on in one place! The technical program committee that brought this all together deserves a Tom Shih huge thank you for their work to curate this content for us. Purdue University It’s such an exciting time to be a part of the aerospace profession. This week provides a unique opportunity for all of us to take a break from the office or the classroom and to celebrate the collective accomplishments of our community. Combining the conference programming with the numerous networking opportunities, Exposition Hall activities, and committee meetings makes for an experience you won’t find anywhere else. If you love aerospace, this is where it’s at. Have a great week!

David Throckmorton Northrop Grumman

www.aiaa.org/scitech2014 3 #aiaaSciTech Get Your Conference Info on the Go!

Download the FREE AIAA 2014 Conference Mobile App

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

FEATURES HOW TO DOWNLOAD Browse Program Any version can be run without an active Internet connection! You can also sync an itinerary you created online with the app by entering your unique itinerary name. View the program at your ﬁngertips MyItinerary Mobile App MyItinerary Web App My Itinerary For optimal use, we recommend • For optimal use, we recommend: iPhone 3GS, iPod Touch (3rd generation), Create your own conference s iPhone 3GS, iPod Touch (3rd 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 Conference Info searching for “ScholarOne” in the App 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 http://itunes.apple.com/us/app/scholarone- default browser my-itinerary/id497884329?mt=8t Take notes during sessions • Download the MyItinerary app by Select the meeting “AIA A SciTech 2014” scanning the QR code or accessing City Map http://download.abstractcentral.com/ See the surrounding area and aiaa-mst14/index.htm the Gaylord National Harbor • Once downloaded, you can bookmark the site to access it later or add a link Connect to Twitter to your home screen. Tweet about what you’re doing and who you’re meeting with #aiaaSciTech

14-101 Contents

Welcome 3

Forum Overview 6

INTRODUCTION Sponsors and Supporters 8

Keynote Speakers and Plenary Sessions 9

www.twitter.com/aiaa Highlighted Sessions 11

www.facebook.com/AIAAfan Networking Events 15

HIGHLIGHTS www.youtube.com/wwwaiaaorg Educational Events 16 www.linkedin.com/companies/aiaa Recognition Events 17 www.flickr.com/aiaaevents Exposition Hall 21 www.livestream.com/aiaa

Exhibitors 23 Join the conversation!

EXPOSITION #aiaaScitech Presentation Stage 29 On-Site Wi Fi Information Network Name: AIAA2014 General Information 31 Username: SciTech Password: 2014 Author and Session Chair Information 32 GENERAL Organizing Committee 33

Committee Meetings and Events 34

Sessions at a Glance 40 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 Author and Session Chair Index 51 corporate members, AIAA brings together industry, PROGRAM academia, and government to advance engineering and science in aviation, space, and defense. Venue Map 181 www.aiaa.org www.aiaa.org/scitech2014 5 #aiaaSciTech Forum Overview

SATURDAY/ MONDAY TUESDAY SUNDAY 11–12 January 13 January 14 January 0700 hrs Networking Breakfast in Exposition Hall (0700–0800 hrs) 0730 hrs Speakers’ Briefing Speakers’ Briefing 0800 hrs

0830 hrs Opening Keynote and Plenary Panel Keynote and Plenary Panel 0900 hrs

0930 hrs Networking Break Networking Break in Exposition Hall 1000 hrs National Space Technology

1030 hrs Exposition Hall Open Analysis and Strategy Workshop 1100 hrs Technical Perspectives Technical Sessions from CASE Sessions and Public 1130 hrs 2013 Listening B2B Session 1200 hrs Continuing Education 1230 hrs Courses and Workshops Durand Lectureship for Aerospace Sciences Awards Networking Lunch 1300 hrs Public Service and Public Luncheon on Own 1330 hrs Policy Luncheon Hall Closed

1400 hrs Speakers’ Briefing/Networking Break Speakers’ Briefing 1430 hrs MDO Special NDA Special Turning 1500 hrs Session Aeronautics Session Open Technology R&D Policy 1530 hrs Into a Business Exposition Hall Panel Networking Break Technical Technical Panel 1600 hrs Sessions Sessions

1630 hrs Rising Leaders 1700 hrs Keynote Hall Closed

1730 hrs Dryden Lectureship in Research 1800 hrs Reception in the Exposition Hall

1830 hrs AIAA Foundation 1900 hrs Associate Fellows Student Reception Reception (1845 hrs) Rising Leaders and Awards 1930 hrs Reception Ceremony

2000 hrs AIAA 2030 hrs Associate Fellows 2100 hrs Dinner 2130 hrs (Tickets Required)

2200 hrs

www.aiaa.org/scitech2014 6 #aiaaSciTech Forum Overview

WEDNESDAY THURSDAY FRIDAY 15 January 16 January 17 January 0700 hrs Networking Breakfast in Exposition Hall (0700–0800 hrs) Networking Breakfast in Exposition Hall (0700–0800 hrs) Networking Break 0730 hrs Speakers’ Briefing Speakers’ Briefing Speakers’ Briefing 0800 hrs

0830 hrs Keynote and Plenary Panel Keynote and Plenary Panel 0900 hrs

0930 hrs Networking Break in Exposition Hall Networking Break in Exposition Hall Technical 1000 hrs Sessions Exposition Hall Open 1030 hrs Additive Small Manufacturing Satellites 1100 hrs Technical Technical Sessions Panel Sessions Panel 1130 hrs

1200 hrs Aerospace Exposition Hall Open 1230 hrs Design and Structures Luncheon in Exposition Hall 1300 hrs Awards Networking Lunch Rising Leaders Luncheon and on Own Luncheon 1330 hrs Speakers’ Briefing Keynote

1400 hrs Speakers’ Briefing ASC Special 1430 hrs Session Emerging Future Networking Rising Technologies 1500 hrs Leaders Speed Aerospace Break Panel Networking Workforce 1530 hrs Technical Sessions Technical Development and Education 1600 hrs Networking Break Sessions 1630 hrs Corporate 1700 hrs Member Reception Member

1730 hrs von Kármán Lectureship in Astronautics 1800 hrs SDM Special Women 1830 hrs Session at SciTech Happy Hour 1900 hrs and Keynote 1930 hrs Speaker

2000 hrs

2030 hrs

2100 hrs

2130 hrs

2200 hrs

www.aiaa.org/scitech2014 7 #aiaaSciTech Sponsors and Supporters

Premier Sponsor and Durand Lectureship and Public Policy Luncheon Sponsor

Supporting Sponsors

www.aiaa.org/scitech2014 8 #aiaaSciTech Keynote Speakers and Plenary Sessions

Industry, academic, and government leaders share their perspectives on the new challenges, future opportunities, and emerging trends in Aerospace Science and Technology.

Monday, 13 January 1730–1830 hrs Potomac Ballroom C 0800–0930 hrs Potomac Ballroom A&B Dryden Lectureship in Research Monday Morning Opening Keynote Taking the Hype Out of and Plenary Panel Hypersonics: Research Contributions to Operational High- e Societal Importance of Federal Speed-Systems R&D Investments Mark J. Lewis, Director, The Science and Congressman Chaka Fattah, 2nd District Technology Policy Institute, Institute for Pennsylvania, U.S. House of Representatives Defense Analyses R&D Policy Implications and Investments Tuesday, 14 January Moderator: Robert Braun, David and Andrew Lewis Professor of Space Technology, Georgia Institute of Technology 0800–0930 hrs Potomac Ballroom A&B Panelists: Michael Gazarik, Associate Administrator, Space Technology Tuesday Morning Keynote and Mission Directorate, NASA Headquarters Plenary Panel Michael Griffin, Chairman and CEO, Schafer Corporation, AIAA President Innovating for an Era of Arati Prabhakar, Director, DARPA Aordability: e Future of the Space Industry 1230–1400 hrs Potomac Ballroom A&B Rick F. Ambrose, Executive Vice President, Lockheed Martin Space Systems Company Durand Lectureship for Public AIAA’s Role in Defining the Future of Aerospace Service and Public Policy Luncheon Moderator: Jim Albaugh, President, The Boeing Company American Space Strategy: Choose to (Retired), AIAA President-Elect Steer, Not Dri Panelists: Scott Pace, Director, Space Policy Institute, David Hills, Director, Research and Technology, Elliott School of International Affairs, Airbus Americas George Washington University Ray Johnson, Senior Vice President, Chief Technology Officer, Lockheed Martin Corporation Sponsored by Michael Ryschkewitsch, Head of the Space Sector of Johns Hopkins University, Applied Physics Laboratory John Tracy, Chief Technology Officer and Senior Vice President of Engineering, Operations, and Technology, The Boeing Company

www.aiaa.org/scitech2014 9 #aiaaSciTech Keynote Speakers and Plenary Sessions

Wednesday, 15 January Thursday, 16 January

0800–0930 hrs Potomac Ballroom A&B 0800–0930 hrs Potomac Ballroom A&B

Wednesday Morning Keynote and Thursday Morning Keynote and Plenary Panel Plenary Panel Tech Superiority in an Age Talent, the Coin of the Realm of Austerity C.D. Mote Jr., President, National Frank Kendall, Under Secretary of Defense Academy of Engineering for Acquisition, Technology and Logistics, Department of Defense Future of Aerospace Education and Designing for Affordability Professional Development Moderator: The Honorable Jacques S. Gansler, Professor Moderator: Alton Romig, Vice President, Engineering and and Roger C. Lipitz Chair, Glenn L. Martin Institute Fellow Advanced Systems, Chief Skunk, Lockheed Martin Aeronautics of Engineering Center for Public Policy & Private Enterprise, Panelists: School of Public Policy, University of Maryland Leland Nicolai, Emeritus Member, Lockheed Martin Panelists: Aeronautics Carl Avila, Director, Advanced Weapons and Missile Systems, David Radcliffe, Kamyar Haghighi Head of Engineering Boeing Defense, Space & Security Education and Epistemology Professor of Engineering John Bergeron, Senior Director, Raytheon Six Sigma, Education, Purdue University Engineering Technology and Mission Assurance, Ed Hoffman, Chief Knowledge Officer and APPEL Director, Raytheon Company NASA John Fisher, Chief Engineer, Engineering, Manufacturing, and Kate Stambaugh, Space Systems Engineer, JHU/Applied Physics Logistics, Northrop Grumman Electronic Systems Laboratory

1730–1830 hrs Potomac Ballroom C

von Kármán Lectureship in Astronautics Space Transportation: Past, Present, and . . . ?? Antonio L. Elias, Executive Vice President and Chief Technical Officer, Orbital Sciences Corporation

www.aiaa.org/scitech2014 10 #aiaaSciTech Highlighted Sessions

Monday, 13 January 1430–1630 hrs Potomac Ballroom C Aeronautics R&D Policy and the Strategic Direction 1000–1230 hrs Potomac Ballroom C of NASA’s Aeronautics Research Panel Analysis and Perspectives from the Complex Moderator: Robert Pearce, Director – Strategy, Architecture & Aerospace Systems Exchange (CASE) 2013 Analysis, NASA Aeronautics Research Mission Directorate Panelists: 1000–1025 hrs Marion Blakey, President and Chief Executive Officer, Characteristics of the Design and Development of Aerospace Industries Association Complex Aerospace Systems Alan Epstein, Vice-President, Technology and Environment, Authors: Anna-Maria Rivas McGowan, Senior Aerospace Pratt & Whitney Technologist, NASA Langley Research Center Les Lyles, Consultant, The Lyles Group Peter Parker, Senior Aerospace Technologist, NASA Langley Jaiwon Shin, Associate Administrator for Aeronautics Research Research Center Mission Directorate, NASA Headquarters

1025–1050 hrs 1430–1530 hrs Maryland Ballroom C Leadership in Pursuit of Systems inking for MDO Special Session Individuals and Organizations Authors: Kurt Detweiler, Deputy Center Chief Engineer, NASA MDAO - Boeing’s Perspective on is Key Langley Research Center Development Capability Need David Dress, Deputy, Space Technology Projects Office, NASA William Carrier, Vice President, Engineering, Boeing Langley Research Center 1050–1115 hrs Tuesday, 14 January e Future May Not Be Where We Are Looking Today 0930–1230 hrs National Harbor 7 Authors: Kennie Jones, Senior Aerospace Technologist, NASA National Space Technology Strategy Workshop Langley Research Center & Public Listening Session William Kimmel, Chief Technologist for Systems Analysis and Concepts Directorate, NASA Langley Research Center Chair: Dr. Mark Lewis, Director, Science and Technology Policy Institute 1115–1230 hrs The session will serve to kick off an extended effort to collect Insights from the CASE 2013 Conference Organizers inputs for the development of a National Space Technology Strategy. A panel consisting of representatives from the Moderator: Anna-Maria Rivas McGowan, Senior Aerospace President’s Office of Science and Technology Policy (OSTP) Technologist, NASA Langley Research Center and Office of Management and Budget (OMB) along with Panelists: several industrial chief technologists will pose and then work to frame the questions that will need to be answered in Allen Arrington, Engineering Manager, Sierra Lobo the development of a comprehensive and cohesive national Sophia Bright, Boeing Global Services and Support, strategy on space technology investment. The panel will The Boeing Company expect feedback and discussion from the audience as the David Dress, Deputy, Space Technology Projects Office, NASA boundaries and constraints of the framework are developed. Langley Research Center Questions such as “what are the gaps in the current U.S. Laura McGill, Deputy Vice President of Engineering, investment policy for space technology” and “what overlaps or Raytheon Company inefficiencies exist in the current U.S. portfolio” will be posed. In addition an examination of the strengths and weaknesses of the National Space Policy and National Space Transportation Policy related to technology policy and U.S. strategy for competitiveness will be discussed. This panel kicks off an effort by AIAA, working with the Science and Technology Policy Institute (STPI) to collect inputs in support of this initiative.

www.aiaa.org/scitech2014 11 #aiaaSciTech Highlighted Sessions

Tuesday, 14 January (continued) Wednesday, 15 January

1000–1230 hrs Chesapeake Conference 6 1000–1200 hrs Potomac Ballroom C Author Panel Additive Manufacturing – A Transformative Technology Panel Writing a New History “Space Shuttle Legacy: How We Did It and What We Learned” Moderator: Ed Morris, Director; Vice President, America Makes - National Additive Manufacturing Innovation Institute; Experts who contributed to the book Space Shuttle Legacy National Center for Defense Manufacturing and Machining examine key aspects of the Space Shuttle program including its (NCDMM) long history, its successes and failures, and what lessons it offers to those engaged in current or future spaceflight programs. Panelists: Moderator: Roger D. Launius, Associate Director for Collections William Flite, Project Engineering Senior Manager, Lockheed and Curatorial Affairs, Smithsonian Institution’s National Air Martin Aeronautics and Space Museum Dan Johns, Chief Technologist, Additive Manufacturing, GKN Aerospace Speakers: Eric MacDonald, Associate Director, W. M. Keck Center of 3D Vigor Yang, Chair, School of Aerospace Engineering, Georgia Innovation, The University of Texas at El Paso Institute of Technology Paul Susalla, Section Supervisor - Rapid Manufacturing, Global Matthew H. Hersch, Lecturer in Science, Technology and Powertrain Manufacturing Engineering, Ford Society, University of Pennsylvania Motor Company Linda Billings, Fellow, George Washington University School of Media and Public Affairs 1400–1600 hrs Potomac Ballroom C John M. Logsdon, Professor Emeritus of Political Science and International Affairs, George Washington University Emerging Technologies of Importance to Aerospace Panel 1430–1630 hrs Potomac Ballroom C Moderator: Daniel Jensen, Head of Engineering for Services, Turning Technology into a Business Panel Rolls-Royce Corporation Panelists: Moderator: Stephen Fleming, Vice President and Executive Director, Enterprise Innovation Institute at Georgia Tech W. Keith Belvin, Chief Technologist, NASA Langley Research Center Panelists: Rupak Biswas, Deputy Director, Exploration Technology Jason Dunn, Co-Founder and CTO, Made in Space, Inc. Directorate, NASA Ames Research Center Debra Facktor Lepore, Vice President and General Manager, Dan Bodony, Professor, University of Illinois at Urbana- Strategic Operations, Ball Aerospace Technologies Champaign Corporation Mark Moore, Design Engineer, NASA Langley Research Center David Thompson, CEO, Orbital Sciences Corporation John Tylko, President, Aurora Flight Sciences 1400–1500 hrs Maryland Ballroom C 1430–1530 hrs Maryland Ballroom C ASC Special Session NDA Special Session DLR’s Adaptive Structures Activities within the European Network Assuring Aero-Structural Reliability in an Uncertain World Hans-Peter Monner, Head of Department Adaptronics, DLR German Aerospace Center Ravi Chona, USAF Senior Scientist and Director, Structural Sciences Center, AFRL

www.aiaa.org/scitech2014 12 #aiaaSciTech IntroHighlighted Sessions

Wednesday, 15 January (continued) 1430–1630 hrs Potomac Ballroom C Future Aerospace Workforce Development and 1800–1900 hrs Chesapeake Conference C Education AIAA Advocacy and Grassroots Session Moderator: Vigor Yang, Chair, School of Aerospace Engineering, Georgia Institute of Technology This session will introduce participants to AIAA’s Grassroots Advocacy programs and efforts. It will review the AIAA Panelists: Congressional Visits Day program, and will explain why Jennifer Byrne, Vice President, Corporate Engineering and grassroots advocacy is vitally important to AIAA’s mission Technology, Lockheed Martin Corporation and to the benefit of the aerospace industry. The program will Carole Hedden, Senior Editor, Aviation Week also include an introduction to successful advocacy, review the role of Congress in the aerospace industry, and introduce Jaime Peraire, H.N. Slater Professor and Department Head, attendees to the basics of argumentation and persuasion. If Department of Aeronautics and Astronautics, Massachusetts you are interested in using your voice to make a difference in Institute of Technology Washington, D.C., this session is for you! Darryll Pines, Dean of Engineering, University of Maryland Larry Schneider, Vice President, Chief Project Engineer - 777 Thursday, 16 January Program, Boeing Commercial Airplanes 1800–2000 hrs National Harbor 3 1000–1200 hrs Potomac Ballroom C Women at SciTech Happy Hour and Small Satellite Technology and its Role in Education Keynote Speaker and Professional Development Panel The Women at SciTech Happy Hour and Keynote is hosted by the Moderator: Simon “Pete” Worden, Director, NASA Ames AIAA Guidance, Navigation, and Control Technical Committee. Research Center The speaker will be Sandra H. Magnus, Executive Director, AIAA. Panelists: Women participating in SciTech are invited to attend at no charge. Women are underrepresented in the engineering sciences and James Cutler, Assistant Professor, University of Michigan industry, and this event provides an opportunity to meet informally, Adarsh Deepak, Chairman, Taksha University and CEO, network, discuss experiences, and identify women who are leaders Science & Technology Corp. (STC) in their fields for possible special recognition by AIAA. Garrett Skrobot, Mission Manager, Launch Services Program, NASA Kennedy Space Center 1800–1900 hrs Maryland Ballroom C Bruce Yost, Program Manager for the Edison Small Spacecraft Flight Demonstration Program, NASA Ames Research Center SDM Special Session Directly following the panel discussion, poster sessions will be presented. See website for more details. Damping: e Turbulence of Structural Mechanics George Lesieutre, Professor and Department Head, Department of Aerospace Engineering, Pennsylvania State University 1200–1400 hrs Potomac Ballroom A&B Aerospace Design and Structures 1830–1930 hrs Chesapeake Conference D Awards Luncheon and Keynote Oh, My Aching Back: Protective Aircraft Seat Making a MUTT - Lessons from the Design Using Adaptive Structures Technology X-56A Program Norman Wereley, Minta Martin Professor and Department Chair, Peter Flick, Program Manager, X-56A Department of Aerospace Engineering, University of Maryland Program, AFRL/RQ A key goal in long duration flights is to protect the human body, especially the lumbar spine, against potentially injurious vibratory Jeff Beranek, Chief Engineer, X-56A and shock loads. To achieve this, vertically stroking seats can MAD MUTT Program, Lockheed Martin be used that adjust stroking load for wide range of occupant Advanced Development Programs weights and vibration or shock severity. This talk, hosted by the National Capital Section, discusses inter-disciplinary design of helicopter seats incorporating concepts from biomechanics, adaptive structures materials, and ground testing, to achieve a comprehensive occupant protection capability.

www.aiaa.org/scitech2014 13 #aiaaSciTech IntroHighlighted Sessions

RISING AIAA’s Rising Leaders in Aerospace Forum provides a forum for young LEADERS aerospace leaders, age 35 and under, to learn from and engage with others. The inAEROSPACE FORUM multidimensional program features a speed mentoring leadership exchange, panel or keynote sessions, Q&A with top industry leaders, and multiple opportunities for Forum Chair: Tim Hinermann, networking. This exciting and energetic forum will provide access to top aerospace Aerojet Rocketdyne leaders and their perspectives, with subject matter relevant to your career stage.

Program Agenda Rising Leaders Reception Rising Leaders Panel Session and Luncheon Monday, 13 January Potomac Ballroom 1-2 Thursday, 16 January Potomac Ballroom 1 1900–2000 hrs 1230–1400 hrs The reception will kick off the Rising Leaders in Aerospace Forum and is a perfect opportunity for young leaders to Expectations and Reality of Your Career mingle with others who will be participating in the forum as Moderator: Kate Stambaugh, JHU Applied Physics Laboratory attendee, presenter, or veteran professional. Come meet other Panelists: participants in a casual environment. You’re bound to see them again at the Speaker, Networking, or Young Professional Panel Ben Marchionna, Lockheed Martin Aeronautics Company events. Ryan Rudy, Boeing Engineering Operations & Technology Gregory P. Scott, Naval Research Laboratory Rising Leaders Keynote Cheryl Blomberg, University of Colorado Tuesday, 14 January Potomac Ballroom 1 1630–1730 hrs Hosted by Speaker to be announced; for latest information see www.aiaa.org/RLAF_SciTech Leadership Exchange and Speed Networking Wednesday, 15 January Potomac Ballroom D 1430–1600 hrs Senior Mentors: Jim Albaugh, AIAA President Elect Mike Griffin, AIAA President Kelly Laflin, Senior Specialist Engineer – CFD/AeroSciences, Cessna Aircraft George Lesieutre, Professor and Department Head, Penn State University Mark Lewis, Director, Science and Technology Policy Institute Sandy Magnus, Executive Director, AIAA Laura McGill, Engineering Deputy, Raytheon Company Laura Richard, Mission Manager, United Launch Alliance Merrie Sanchez, Senior Director – Space Exploration Systems, Sierra Nevada Corporation

www.aiaa.org/scitech2014 14 #aiaaSciTech Networking Events

Networking Breakfasts Welcome Reception A great way to start the day and interact with colleagues old Tuesday, 14 January Exposition Hall and new, networking breakfasts will be offered on Tuesday– 1730–1900 hrs Thursday, 0700–0800 hrs, in the Exposition Hall. This event is Take this opportunity to engage new contacts, refresh old open to all forum attendees (no tickets are required). ones, listen to the sounds of The Robert King Experience and have your photo taken at the Photo Fun Station (Booth 108). Networking Coffee Breaks A ticket for the reception is required, and is included in the Networking coffee breaks allow even more time for making registration fee where indicated. Additional tickets may be new contacts, continuing discussions from sessions, visiting purchased upon registration or on site, as space is available. the exposition hall, or checking emails and voicemails to keep in touch with the office. Networking coffee breaks will be AIAA/ARCS Alum Happy Hour located in the locations at the following times: Tuesday, 14 January Gaylord Belvedere Lobby Bar Monday, 13 January Foyer 1630–1730 hrs 0930–1000 hrs and 1400–1430 hrs If you are an alumni or current scholar supported by Sponsored by: Airbus Achievement Rewards for College Scientists (ARCS), or if you Tuesday, 14 January Exposition Hall represent one of 55 U.S. ARCS-funded universities, or if you 0930–1000 hrs and 1530–1600 hrs want to learn more about this organization, you are invited to an informal ARCS Networking Happy Hour. Many ARCS Wednesday, 15 January Exposition Hall alumni and faculty from ARCS universities are also active 0930–1000 hrs and 1500–1530 hrs members of AIAA, so we especially hope to see you there. Just Thursday, 16 January Exposition Hall follow signage to meet your ARCS colleagues. 0930–1000 hrs Thursday, 16 January Foyer Luncheon in the Exposition Hall 1530–1600 hrs Wednesday, 15 January Exposition Hall Friday, 17 January Foyer 1230–1330 hrs 0700–0730 hrs Lunch ticket included in registration packages where indicated. Please come to the registration desk if you are interested in AIAA Business to Business (B2B) Matchmaking Event purchasing a ticket (while supplies last). Monday, 13 January Potomac Ballroom 1–2 1000–1400 hrs Corporate Member & Exhibitor Reception This B2B Matchmaking event will help both our prime and Wednesday, 15 January Exposition Hall our small business members of the supply chain to learn about 1600–1730 hrs the latest technology opportunities, to form new alliances and By invitation only for AIAA Corporate Members and partnerships, and to maximize business resources. Companies Exhibiting Companies. Join us for a private reception and will outline what they’re looking for in partnerships, followed networking in the Exposition Hall directly following the close by one-on-one matchmaking and detailed discussion about of the exhibits. programs and opportunities. This event is complimentary for AIAA Corporate Members and there is a nominal fee of $200 AIAA Bookstore: Author Signings for all other attendees. Lunch will be served. Leland Nicolai, co-author of Fundamentals of Aircraft and Susan Nichols, Program Director, DARPA Small Business Airship Design, Vols. 1 & 2 Programs Office, SBIR/STTR Program Manager PM Networking Coffee Break, Tuesday, 14 January, Joseph Grant Ph.D., Space Technology Mission Directorate, 1530–1600 hrs NASA Headquarters, SBIR/STTR Program AM Networking Coffee Break, Wednesday, 15 January, Nafiz Karabudak, Global Technology Manager and SBIR/ 0930–1000 hrs STTR Technology Lead, Corporate Engineering and Technology, Michael V. Ciminera, author of The Aircraft Designers: A Lockheed Martin Corporation Grumman Historical Perspective, Opening Reception, Tuesday, 14 January, 1730–1900 hrs Kent Hollinger, author of Safety Management Systems for Aviation Practitioners: Real-World Lessons AM Networking Coffee Break, Tuesday, 14 January 0930– 1030 hrs Daniel P. Raymer, author of Aircraft Design: A Conceptual Approach, Fifth Edition Networking Luncheon, Wednesday, 15 January, 1230–1330 hrs www.aiaa.org/scitech2014 15 #aiaaSciTech Educational 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. Verification and Validation Best Practices for Introduction to the AIAA Educator Academy Integrated Computational Materials Engineering Wednesday, 15 January Chesapeake Conference A Tuesday, 14 January Chesapeake Conference K 1900–2100 hrs 1400–1600 hrs Do you ever wish your local schools taught AIAA-approved This tutorial will introduce the evolving V&V Guidelines aerospace curricula in grades 3-12? Well, now they can, if you and Recommended Best Practices for ICME. Concepts or your Section engages them in using one of the AIAA’s brand and methodology to support this process and improve new Educator Academy curriculum modules. Come find out communication between the validation team (model how! This presentation introduces the Educator Academy; developers and experimentalists) and the customer will be describes the three exciting inquiry-based modules, Space emphasized. The tutorial will lead the attendee through the Weather Balloon, Mars Rover Celebration, and Electric Cargo process using a realistic case study where a model is developed Plane; and gives details on how to adopt the Academy as one of to predict the fatigue crack growth life of forged and machined your STEM K-12 Outreach Programs. parts, which includes induced residual stresses. Get Your Green Card Workshop Wednesday, 15 January Chesapeake Conference 8 1000–1230 hrs Attorney Mark Harrington will present an overview of “Green Card” options available for foreign-born scientists and R&D engineers. This presentation will cover employer-sponsored Green Card cases as well as cases that can be self-filed directly by immigrants without the need for official sponsorship from an employer. A Q&A session will follow the presentation. Protecting Intellectual Property — Patents and Trademark Law Workshop Wednesday, 15 January Chesapeake Conference L 1430–1730 hrs Investing in innovation is one of the keys to maintaining a competitive edge and for expanding business opportunities. Protecting this investment through intellectual property rights such as patents, copyrights, and trademarks is essential in today’s global economy, particularly when contracting with government entities. The United States recently implemented extensive changes to the patent system with far-reaching effects for companies who wish to obtain and enforce their intellectual property rights. This workshop will explore various methods of protecting intellectual property, IP issues when contracting with government agencies, and how the new patent laws will impact your vital business assets.

www.aiaa.org/scitech2014 16 #aiaaSciTech Recognition Events

Join with us throughout the SciTech Forum as AIAA recognizes the very best in our industry: those individuals and teams who have taken aerospace technology to the next level…who have advanced the quality and depth of the aerospace profession…who have leveraged their aerospace knowledge for the benefit of society. Their achievements have inspired us to dream and to explore new frontiers. International Student Conference AIAA Foundation Student Reception and Sessions will recognize the accomplishments of the regional Awards Ceremony student conference winners from the 2013 Regional Student Monday, 13 January Potomac Ballroom D Conferences and they will present their award-winning work. 1830–2000 hrs These presenters are in the forefront of the student community that will soon be entering the workforce. This reception acknowledges and highlights university students who have performed significantly. Many of the Monday, 13 January attendees will be students who have won awards for work that Master Division they have done. This event will provide an opportunity for all 0930–1300 hrs National Harbor 6 students and those who have an interest in student activities to meet, recognize peers for excellence, and to mingle. Undergraduate Division 0930–1300 hrs National Harbor 2 Awards to be presented include: Team Division 1000–1200 hrs National Harbor 4 AIAA Foundation Orville and Wilbur Wright Graduate Awards Community Division 1430–1730 hrs Potomac Ballroom 3 AIAA Associate Fellows Reception and Dinner Monday, 13 January Cherry Blossom Ballroom Reception begins at 1845 hrs Dinner at 1930 hrs Luis P Zea Daniel Cuppoletti The 2014 Associate Fellows will be inducted during the University of Colorado- University of Cincinnati Associate Fellows Dinner. Each year, the Institute recognizes Boulder, Boulder, Cincinnati, Ohio exemplary professionals for their accomplishments in Colorado engineering or scientific work, outstanding merit, and contributions to the art, science, or technology of aeronautics or astronautics. AIAA Foundation Abe AIAA Foundation Abe M. M. Zarem Award For Zarem Educator Award Please support your colleagues, and join us for the induction Distinguished Achievement Astronautics: of the 2014 Associate Fellows. Tickets to this celebrated event Astronautics: are available on a first-come, first-served basis and can be purchased via the AIAA SciTech registration form or on site based on availability. Business attire is requested.

Eliseo Iglesias Harry R Millwater, Jr. University of Texas Professor/Educator at San Antonio, San University of Texas at San Antonio, Texas Antonio, San Antonio, Texas

Winners in the Master, Undergraduate, Team, and Community Divisions of the International Student Conference will also be announced.

www.aiaa.org/scitech2014 17 #aiaaSciTech Recognition Events

Aerospace Sciences Awards Luncheon ASEE/AIAA J. Leland Atwood Award Tuesday, 14 January Potomac Ballroom A&B Mark D. Maughmer 1230–1400 hrs Professor/Educator The Pennsylvania State University Join colleagues and friends for the AIAA Awards Luncheon in University Park, Pennsylvania celebrating discovery and achievements in aerospace sciences and aerospace literature. Ticket included in the registration “For weaving a unique tapestry of real- package where indicated. world engineering and engineering education.” Aerospace Sciences

AIAA Aerospace Guidance, Navigation, and Control Award Aerospace Literature Bernard Etkin University Professor Emeritus AIAA Gardner-Lasser Aerospace History Literature Award University of Toronto William Clancey Ontario, Canada Senior Research Scientist, Florida Institute “For outstanding achievement in and for Human and Machine Cognition dedication to research and education in the Pensacola, Florida field of guidance, navigation and control for “Working on Mars: Voyages of Scientific over a half century.” Discovery with The Mars Exploration Rovers” AIAA Intelligent Systems Award Heinz Erzberger AIAA History Manuscript Award Senior Scientist, Aviation Systems Division NASA Ames Research Center Lawrence Benson Moffett Field, California Air Force Historian (retired) Albuquerque, New Mexico “For pioneering research in developing intelligent systems that increase the “Quieting the Boom: The Shaped Sonic efficiency and safety of aircraft and air Boom Demonstrator and the Quest for traffic control operations.” Quiet Supersonic Flight” AIAA Lawrence Sperry Award AIAA Pendray Aerospace Literature Award Kimberley Clayfield Executive Manager, Space Sciences Wassim Haddad and Technology Professor of Aerospace Engineering Commonwealth Scientific and Industrial Georgia Institute of Technology Research Organisation (CSIRO) Daniel Guggenheim School of Aerospace Canberra ACT Australia Engineering “For significant and sustained contributions Atlanta, Georgia to the development of the Australian “For paramount and fundamental aerospace sector through national public contributions to the literature of dynamical policy, scientific leadership, and education systems and control for large-scale activities.” aerospace systems.” (Award will be presented by the AIAA Sydney Section) AIAA Mechanics and Control of Flight Award Maruthi R. Akella Associate Professor, Aerospace Engineering and Engineering Mechanics University of Texas at Austin Austin, Texas “For far-reaching theoretical and practical advances in aircraft/spacecraft guidance, navigation and control, particularly nonlinear attitude estimation and control.”

www.aiaa.org/scitech2014 18 #aiaaSciTech Recognition Events

Recognizing Technical and Scientific Excellence AIAA Sustained Service Awards (Best Papers and Student Paper Competitions) Wednesday, 15 January Presentation Stage Tuesday, 14 January Presentation Stage 0930–0945 hrs Exposition Hall 1745–1815 hrs Exposition Hall AIAA members will be recognized for their dedicated service. No Ticket Required Ramana Grandhi Best papers in the fields of aerospace sciences or aerospace Distinguished Professor design and structures will be recognized for technical and Wright State University scientific excellence. A certificate of merit will be presented to Dayton, Ohio authors. “For sustained and dedicated service ASME/Boeing Best Paper to AIAA through conference leadership, AIAA 2013-1702, “Dynamic Aeroservoelastic Response with significant publications in structural Nonlinear Structural Elements,” Mordechay Karpel, Technion- design, and leadership of the Israel Institute of Technology; Alexander Shousterman, Israeli Multidisciplinary Design Optimization Computational Fluid Dynamics Center; and Carlos Maderuelo and Non-Deterministic Approaches and Hector Climent, Airbus Military. Technical Committee.” Atmospheric Flight Mechanics Best Paper James Horkovich Engineering Fellow, AIAA Paper 2013-4844, “Virtual Deformation Control of RMS Systems Engineering the X-56A Model with Simulated Fiber Optic Sensors,” Peter Raytheon Advanced Systems Suh and Dimitri Mavris, George Institute of Technology; and Design Center Alexander Chin, NASA Dryden Tucson, Arizona Collier Research HyperSizer/AIAA Structures Best Paper “For professional commitment and leadership, for education and mentoring of AIAA 2013-1769, “Structural Assessment of Advanced scientist engineers, and for distinguished Composite Tow-Steered Shells,” K. Chauncey Wu, Bret contributions to science and innovation of Stanford, Glenn Hrinda, Zhuosong Wang, and Robert A. directed energy systems.” Martin, NASA Langley Research Center; and H. Alicia Kim, University of Bath. Paresh Parikh Computational Fluid Dynamics Best Student Paper Associate Director for Project Implementation, Research Directorate, AIAA 2013-2940, “Multidimensional Active Flux Schemes,” NASA Langley Research Center, Timothy Eymann, CREATE-AV/Kestrel and Phillip Roe, Hampton, Virginia University of Michigan. “For 25 years of continuous service to Gossamer Systems Best Paper AIAA and the Hampton Roads Section, including organization of the “Future In AIAA 2013-1671 “Deployable Helical Antennas for CubeSats,” Aerospace” scholarship program and service Gina Olson, Sergio Pellegrino, and Joseph Costantine, as a Section Officer, Committee Chair, and California Institute of Technology; and Jeremy Banik, Air Council Member.” Force Research Laboratory, Kirtland AFB. Balu Sekar Guidance, Navigation and Control Best Paper Senior Aerospace Engineer AIAA 2013-5202, “Experimental Validation of Pulse Phase ARFL/RZTC Tracking for X-ray Pulsar Based Spacecraft Navigation,” Kevin Wright-Patterson AFB, Ohio D. Anderson and Darryll Pines, University of Maryland. “For 30 years of participation in AIAA Shahyar Pirzadeh Memorial Award for Outstanding Paper in technical and section activities.” Meshing Visualization and Computational Environments AIAA 2013-1162, “Visualization and Analysis of Vortex Features in Helicopter Rotor Wakes,” David Kao, Jasim Ahmad, Terry Holst, and Brian Allan, NASA Langley Research Center.

www.aiaa.org/scitech2014 19 #aiaaSciTech IntroRecognition Events

Aerospace Design and Structures Awards Luncheon and Keynote Thursday, 16 January Potomac Ballroom A&B 1200–1400 hrs Join colleagues and friends for the AIAA Awards Luncheon to celebrate innovation and achievement in aerospace design and structures. Ticket included in the registration package where indicated. AIAA Aerospace Design Award Michael Benjamin Senior Engineer GE Aviation Cincinnati, Ohio “For leadership in the design of advanced fuel nozzles and combustors for the next generation of GE aircraft engines including the LEAP and GEnx.” AIAA Structures, Structural Dynamics, and Materials Award Daniel Inman “Kelly” Johnson Professor and Chair Department of Aerospace Engineering University of Michigan Ann Arbor, Michigan “For outstanding contributions and innovative integration of smart materials into both air and space vehicles ranging from flexible satellites to morphing aircraft structures.” AIAA Survivability Award John M. Vice President Skyward, Ltd. Hendersonville, North Carolina “For leadership and technical contributions instrumental in enhancing aircraft survivability through test and evaluation, combat data collection, and aircraft battle damage assessment and repair.” New Lectureship in Aerospace Engineering Seeks Nominees! Nominations are now being solicited for the inaugural Yvonne C. Brill Lectureship in Aerospace Engineering established in memory of Yvonne Brill, pioneering rocket scientist, AIAA Honorary Fellow, and NAE member, and are due to AIAA by 31 January 2014. The ideal nominee should have a distinguished career involving significant contributions in aerospace research and/or engineering and will be selected based on technical expertise, originality, and influence on other important aerospace issues such as ensuring a diverse and robust engineering community. NAE or AIAA members are eligible to place a nomination. Contact [email protected] to request the nomination form. www.aiaa.org/scitech2014 20 #aiaaSciTech IntroExposition Hall

PRESENTATION STAGE

Dunmore DSpace AUR ATA Ansys, Inc Photron FlexSys Dantec DAR and Dynamics AEDC Show J2 Ofﬁce 216 315 316 415 416 515 516 615 616 715 AIAA National Desktop Embry-Riddle IAC AIAA Forum CASIS Capital NRCNA ALEC Cray Aisle 300 Aisle 400 Aisle 600 Aisle 700 Aisle Academies 500 Aisle Aeronautics Information AIAA Section University Toronto Pavillion 214 313 314 413 414 513 514 613 614 713 Concord Cambridge BETA Metacomp Convergent Lift Univ. Press CAE Technologies Science Inc. Exhibitor 212 311 412 CD 612 711 Adapco Lounge Aerosoft Vigyan Tetra NRO

309 310 Tecplot 509 510 609 Software Photofun Pointwise Triumph Wolverine LA Vision CEI Quantel IDT Station Cradle 108 208 307 407 408 507 508 607 608 707

ONR Airborne National Systems Corporate Member Intelligent ONR Institute Boeing LMCO 104 Springer of Light 604 NASA Small Business Higher Orbits Aerospace Spotlight and ISSET Tri Models 102 201 202 301 302 402 502 602 701 702 ENTRANCE Exhibitors by Booth Number

309 Aerosoft, Inc. 102 Higher Orbits and ISSET 313 AIAA Capital Section 614 IAC 2014 Toronto (CASI) 713 AIAA Forum Information 707 Integrated Design Tools (IDT) 604 Airborne Systems 402 Intelligent Light 414 American Legislative Exchange Council (ALEC) 508 LaVision, Inc. 416 Ansys, Inc. 502 Lockheed Martin Corporation 616 Arnold Engineering Development Complex (AEDC) 612 Metacomp Technologies 415 ATA Engineering, Inc. 701 NASA 316 AUR, Inc. 313 National Capital Section (AIAA) 412 BETA CAE Systems USA, Inc. 301 National Institute of Aerospace (NIA) 302 Boeing Technology Services 609 National Reconnaissance Office (NRO) 311 Cambridge University Press 413 National Research Council of the National Academies 214 CASIS 104/201 Office of Naval Research (ONR) 509 CD-adapco 108 Photo Fun Station 607 Computational Engineering International 515 Photron 212 ConcordLift 307 Pointwise, Inc. 702 Corporate Member Small Business Spotlight 608 Quantel USA 711 Convergent Science, Inc. 208 Software Cradle 513 Cray, Inc. 202 Springer 615 Dantec Dynamics, Inc 407 Tecplot, Inc. 715 DARcorporation/J2 Aircraft Dynamics 510 Tetra Research Corporation 514 Desktop Aeronautics, Inc. 602 Tri Models, Inc. 315 dSPACE 408 Triumph Aerospace Systems - Newport News 216 Dunmore Corporation 310 ViGYAN, Inc. 613 Embry-Riddle Aeronautical University 507 Wolverine Ventures, Inc. 516 FlexSys www.aiaa.org/scitech2014 21 #aiaaSciTech IntroExposition Hall

The exposition hall is the hub of activity during this event. Networking coffee breaks and breakfasts, luncheons, receptions, recognition activities, and exhibitor presentations are all held in the exposition hall to give attendees and exhibitors an opportunity to celebrate technical excellence and connect with partners, industry-thought leaders, and collaborators who can help move your business forward. Exposition Hall Hours AIAA Pavilion Tuesday, 14 January 0700–1230 hrs Stop by the AIAA Pavilion, located in the Exposition Hall, 1400–1600 hrs to browse publications and merchandise, learn about your Wednesday, 15 January 0700–1600 hrs membership benefits, and meet AIAA staff. Thursday, 16 January 0700–1200 hrs 30% Off All Books at the AIAA SciTech 2014 Forum AIAA Publications is offering a special discount on all titles featured at the AIAA SciTech 2014 Forum. Attendees can Networking Activities in the Exposition Hall take advantage of a 30% discount off the list price of all books for sale at the AIAA Bookstore located in the AIAA Pavilion. Networking Breakfasts This special offer will only be available during the forum! Take Tuesday–Thursday, 14–16 January 0700–0800 hrs advantage of these super savings and visit the AIAA Bookstore! Networking Breaks AIAA Forum Information Tuesday, 14 January 0930–1000 hrs Come join us in the Exposition Hall at the Forum Information 1530–1600 hrs booth, #713, to learn about AIAA’s Forums. Drop off your Wednesday, 15 January 0930–1000 hrs business card for a chance to win a prize. Visit the booth before 1500–1530 hrs lunch on Wednesday to be eligible, the drawing will be held at 1245 hrs! Thursday, 16 January 0930–1000 hrs Photo Fun Station Reception Stop by and have your photo taken in front of one of four Tuesday, 14 January 1730–1900 hrs unique options, located next to the AIAA Pavilion! Open Luncheon Tuesday, 14 January, 1730–1900 hrs, and Wednesday, 15 January, 1400–1600 hrs. Wednesday, 15 January 1230–1330 hrs

www.aiaa.org/scitech2014 22 #aiaaSciTech Exhibitors Aerosoft, Inc. 309 Arnold Engineering Development Complex (AEDC) 616 2000 Kraft Drive, Suite 1400 100 Kindel Drive, Suite B-213 Blacksburg, VA 24060 Arnold AFB, TN 37389-2213 www.aerosoft.com www.arnold.af.mil [email protected] [email protected] AeroSoft specializes in high-fidelity numerical algorithms Arnold Engineering Development Complex for aerodynamics simulation and design. Services include (AEDC) is the most advanced and largest complex of flight licensing, training and support of GASP, our premier simulation test facilities in the world. The Complex operates structured and unstructured flow solver, as well as detailed aerodynamic and propulsion wind tunnels, rocket and turbine analysis of customer applications and customized solutions. engine test cells, space environmental chambers, arc heaters, Come by and see what’s new with GASP version 5.1. ballistic ranges and other specialized units.

Airborne Systems 604 ATA Engineering, Inc. 415 5800 Magnolia Avenue 1995 El Camino Real, Suite 200 Pennsauken, NJ 08109 San Diego, CA 92130 www.airborne-sys.com www.ata-e.com [email protected] [email protected] Airborne Systems is a world leader in the design, development, ATA Engineering, Inc (ATA) is an engineering consulting firm fabrication, test and integration of Entry Descent and that provides innovative solutions through test- and analysis- Landing Systems (EDLS), including parachutes systems, Air driven design by focusing on the needs of manufacturers in Bag Landing Attenuation systems, Inflatable Aerodynamic addressing their cost, quality, and time-to-market challenges Decelerators. We provide EDLS systems for various aircraft for their mechanical and aerospace systems. and spacecraft and are leading the development of new technologies including Inflatable Aerodynamic Decelerators. AUR, Inc 316 American Legislative Exchange Council (ALEC) 414 605 Preston Avenue 2900 Crystal Drive Blacksburg, VA 24060 Suite 600 www.aurinc.com Arlington, VA 22202 [email protected] www.alec.org AUR, Inc. (founded in 1973) develops and sells unique [email protected] miniature 3-velocity-component non-intrusive laser systems The American Legislative Exchange Council (ALEC) is built upon advanced technologies and software (AUR Studio™) America’s largest nonpartisan, membership organization of to solve complex flow problems in complex practical systems. state legistlators (2,000+) with a commitment to free markets AUR optimizes these capabilities for each application using its and limited government. Capitalizing on our members’ experience-based knowledge of complex flow problems. (See specialized knowledge, we have task forces and subcommittees our ad in the October 2012 Aerospace America for details.) focusing on national security, international relations, education and tort reform, among other issues. BETA CAE Systems USA, Inc. 412 29800 Middlebelt Road ANSYS, Inc. 416 Suite #100 275 Technology 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 brings clarity and insight to customers’ most distributes & supports the industry leading ANSA & META complex design challenges through fast, accurate and reliable software. ANSA is CAE pre-processing tool for FE & CFD engineering simulation. Our technology enables organizations Analysis, for full-model build, from CAD to solver input file, to predict with confidence that their products will thrive in one integrated environment. META is a post-processor for in the real world. Customers trust our software to help analyzing results from ANSYS, NASTRAN, ABAQUS, LS- ensure product integrity and drive business success through DYNA, PAMCRASH, RADIOSS, MADYMO, FLUENT, STAR innovation. CCM, CFD++ & other solvers.

www.aiaa.org/scitech2014 23 #aiaaSciTech Exhibitors Boeing Technology Services 302 Computational Engineering International 607 7755 E. Marginal Way S 2166 N. Salem Street Mail Code 1W-02 Apex, NC 27523 Seattle, WA 98108 www.ceisoftware.com http://www.boeing.com/commercial/techsvcs/boeingtech/ [email protected] Boeing Technology Services can help you find the Boeing CEI makes EnSight, the leading CFD and CSM post-processor testing facilities, test technicians and engineers to fit your and visualization software. EnSight is known for its strong needs at a wide variety of laboratories/test and measurements support for large models, transient models, and moving and facilities in the Puget Sound area, Southern California, adapting meshes. If you make a CFD or CSM solver, EnSight St. Louis, MO., Philadelphia, PA., and other Boeing is available to bundle with your software. Stop by the booth locations across the country. We can arrange on-site work, and see the new EnSight 10.1 with faster performance, native accommodating your need to have Boeing experts perform polyhedrals, and case linking. testing at your own location. ConcordLift 212 Cambridge University Press 311 PO Box 28205 32 Avenue of the Americas Baltimore, MD 21234 New York, NY 10013 www.concordlift.com www.cambridge.org/us/ [email protected] [email protected] This is a “thought experiment” for a low cost per ton mile Cambridge’s publishing in books and journals combines competitor for truck, train, ship cargo with fast direct airborne state-of-the-art content with the highest standards of service. ConcordLift develops theoretical studies on practical scholarship, writing and production. Visit our stand to problems and develops workable cost effective solutions. 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.cambridge.org/us/ Convergent Science, Inc. 711 6405 Century Avenue Suite 102 CASIS 214 Middleton, WI 53562 6905 N Wickham Rd convergecfd.com Suite 500 [email protected] Melbourne, FL 32940 www.iss-casis.org Convergent Science, Inc. is a world leader in Computational [email protected] Fluid Dynamics (CFD) software. Our flagship product, CONVERGE™, is a CFD software package that is The Center for the Advancement of Science in Space (CASIS) revolutionizing how fluid dynamics modeling is being used is the sole manager of the International Space Station (ISS) U.S. by engineers, researchers and designers. With CONVERGE™, National Laboratory. CASIS is responsible for managing and traditional CFD bottlenecks (namely grid generation) have promoting innovative research on the ISS capable of improving been removed from the modeling process, allowing users to life on Earth. spend more time analyzing their simulations and no time generating grids. CD-adapco 509 60 Broadhollow Road Melville, NY 11747 Cray, Inc 513 www.cd-adapco.com 901 Fifth Avenue, Suite 1000 [email protected] Seattle, WA 98164 www.cray.com CD-adapco is the world’s largest independent CFD-focused [email protected] provider of engineering simulation software, support and services. We have over 30 years experience in delivering Cray builds innovative supercomputing systems that industrial strength engineering simulation. The scope of enable scientists and engineers to meet existing and future our activities extends well beyond software development to computational challenges. Building on expertise in developing, encompass a wide range of CAE engineering services in both marketing and servicing the world’s most advanced CFD and FEA. supercomputers, Cray offers a comprehensive portfolio of high performance computing systems delivering unrivaled sustained performance on a wide range of applications.

www.aiaa.org/scitech2014 24 #aiaaSciTech IntroExhibitors DARcorporation/J2 Aircraft Dynamics 715 dSPACE 315 DARcorporation 50131 Pontiac Trail 1440 Wakarusa Drive Wixom, MI 48393-2020 Suite 500 www.dspaceinc.com Lawrence, KS 66049 [email protected] www.darcorp.com [email protected] dSPACE is the world’s leading provider of hardware and software tools for developing and testing sophisticated electronic control j2 Aircraft Dynamics Ltd systems. For over 20 years, dSPACE’s high-quality, off-the-shelf Daresbury Innovation Centre software and hardware tools have empowered engineers to Keckwick Lane design and innovate, while dramatically reducing development Daresbury, Warrington, Cheshire times and cost. Learn more by visiting: www.dspaceinc.com. WA4 4FS United Kingdom www.j2aircraft.com DUNMORE Corporation 216 [email protected] 145 Wharton Road DARcorporation: aeronautical engineering consulting Bristol, PA 19007 services in airplane design, wind turbine design, prototype www.dunmore.com R manufacturing, wind tunnel testing. DAR develops and sells [email protected] airplane design and analysis software. J2 Aircraft Dynamics DUNMORE is a manufacturer of engineered films and tapes develops and sells the j2 Universal Tool Kit software. J2 for aerospace, supplying multilayer insulation materials to software is used for aircraft design, flight test, simulation and the aerospace industry for over twenty-five years. With a accident investigation. highly technical product base of over 400 certified products, DUNMORE is the trusted source for engineered aerospace Dantec Dynamics, Inc. 615 films and tapes. 750 Blue Point Road Holtville, NY 11742 www.dantecdynamics.com Embry-Riddle Aeronautical University 613 [email protected] 600 S. Clyde Morris Blvd. Daytona Beach, FL 32114 Dantec Dynamics is a leading developer and supplier of www.embryriddle.edu advanced measurement systems for fluid mechanics, solid [email protected] mechanics, microfluidics, spray analysis and combustion technology. Our products include: PIV, CTA, LDA, PDA, PLIF, Embry-Riddle Aeronautical University, the world’s largest DIC, and more. Measurement data include velocity, turbulence, university specializing in aviation and aerospace, offers more particle size, concentration, temperature, combustion species, than 40 baccalaureate, master’s and Ph.D. degree programs. strain/stress and vibration. Embry-Riddle educates students at residential campuses in Daytona Beach, Fl, and Prescott, AZ and through the Desktop Aeronautics Inc. 514 Worldwide Campus with more than 150 locations. 1900 Embarcadero Road Suite 101 FlexSys 516 Palo Alto, CA 94303 2205 Commonwealth www.desktopaero.com Suite D [email protected] Ann Arbpr, MI 48105 Desktop Aeronautics provides conceptual aircraft design www.flxsys.com and shape optimization services to aircraft manufactures FlexSys is a world-leader in variable geometry wings that and Government agencies, specializing in design for natural offer significant reduction in fuel-burn (emissions), noise and laminar flow (NLF). We also develop and distribute licensed stresses. Leveraging our pioneering compliant systems design software that addresses the needs of aircraft designers. We are method, we demonstrated (TRL 6) lightweight, reliable and NASA’s licensed commercial distributor of Cart3D. cost-effective seamless shape-adaptive control surfaces. A Gulfstream business-jet retrofitted with FlexFoil is scheduled for flight tests in July 2014.

www.aiaa.org/scitech2014 25 #aiaaSciTech IntroExhibitors

Higher Orbits and ISSET 102 LaVision, Inc. 508 32 Upshur Road 211 W. Michigan Avenue, Suite 100 Annapolis, MD 21402 Ypsilanti, MI 48197 www.higherorbits.org www.lavisioninc.com www.isset.org [email protected] LaVision provides integrated imaging systems to scientific, industrial and education markets. LaVision has extensive Higher Orbits & ISSET (International Space School experience in optical techniques such as 2-D, stereo and Educational Trust) are “sister” non-profits that use space, tomographic particle image velocimetry, gaseous and liquid through a variety of experiences, to get individuals excited about STEM, Leadership and Teamwork. laser induced fluorescence, shadography for multi-phase flows, digital image correlation for deformation/strain, high-speed and ultra-high-speed imaging, and intensified camera systems. IAC 2014 Toronto 614 350 Terry Fox Drive, Suite 104 Lockheed-Martin Corporation 502 Kanata, Ontario K2K 2W5 Canada 6801 Rockledge Drive www.iac2014.org Bethesda, MD 20817 [email protected] or [email protected] www.lockheedmartin.com [email protected] The 2014 International Astronautical Congress – IAC 2014 – will attract over 3,000 space experts from around the world to Headquartered in Bethesda, Md., Lockheed Martin is a Toronto from 29 September – 5 October. Toronto is the ideal global security and aerospace company that employs about host city-accessible, affordable, efficient, safe, exciting – a 120,000 people worldwide and is principally engaged in the wonderful place to visit! research, design, development, manufacture, integration and sustainment of advanced technology systems, products and services. Its exhibit will feature programs from Lockheed Integrated Design Tools, Inc. (IDT) 707 Martin Aeronautics, Skunk Works®, including Stalker UAV and Advanced Air Mobility concepts. Space Systems Company 1W Mountain St. #3 Pasadena, CA 91106 will highlight the ongoing Human Space Flight activity and the www.idtvision.com next generation of robotic exploration missions. [email protected] Integrated Design Tools, Inc. (IDT) began in 1997 with the Metacomp Technologies 612 purpose of providing digital imaging solutions for scientific 28632 Roadside Drive, Suite 255 and industrial communities. Our standard is excellence Agoura Hills, CA 91301 supported by our team of leading scientists in the fields of www.metacomptech.com applied physics, imaging sensors, digital camera design and [email protected] software. While high-speed digital imaging is our specialty, IDT also offers highly integrated systems that include data Metacomp Technologies is at the forefront of cutting edge acquisition and signal synchronization modules. The product technology with its products Computation Fluid Dynamics lines embrace industry standards such as high-speed USB and CFD++, Mesh Generation MIMI and Computations Structural Gigabit Ethernet to supply plug-and-play instruments that are Mechanics CSM++, in widespread global use. Metacomp reliable, cost-effective, and easy to use. Technologies is a developer of comprehensive computational multiphysics tools for a better view of the world. Intelligent Light 402 301 Route 17 N. 7th Floor NASA 701 Rutherford, NJ 07070 www.ilight.com 300 E St. SW [email protected] Washington, D.C. 20024 www.nasa.gov Intelligent Light is bringing a revolution to CFD with the all- new Field View 13 and the capabilities of our Applied Research Innovate – Explore – Discover – Inspire: NASA highlights Group. Serving thousands of HPC users in the aerospace its advanced technology development and capabilities in community, Intelligent Light has developed deep expertise aeronautics, science, and human and space operations, that in CFD, computer science, and visualization is focused on also have real world benefits here on Earth, today. Discover delivering products and services that help customers achieve NASA’s current and future missions to Mars and beyond, extraordinary results. and learn about the Agency’s contributions to the innovation economy.

www.aiaa.org/scitech2014 26 #aiaaSciTech IntroExhibitors

National Institute of Aerospace 301 Photron 515 100 Exploration Way 9520 Padgett Street, Suite 110 Hampton, VA 23666 San Diego, CA 92126 [email protected] www.photron.com [email protected] National Institute of Aerospace is a non-profit research and graduate education institute conducting research sponsored by Photron’s wide range of light sensitive high-speed cameras NASA, other government agencies and the aerospace industry includes short inter-frame (222ns) times ideally suited for in the fields of space exploration, systems engineering, Particle Image Velocimetry (PIV), miniature cameras for materials science, flight systems, aerodynamics, air traffic microscopy, a full resolution at one million fps camera, to management, aviation safety, planetary and space science and 4M pixels production HD to 2,000 fps. Photron has the slow global climate change. motion camera for your fluidics application.

National Reconnaissance Office (NRO) 609 Pointwise, Inc. 307 14675 Lee Road 213 S. Jennings Avenue Chantilly, VA 21051 Fort Worth, TX 76104 dii.westfield.net www.pointwise.com [email protected] [email protected] The National Reconnaissance Office’s Director’s Pointwise, Inc. is solving the top problems facing engineering Innovation Initiative invests in advanced technologies, analysts today: mesh generation for computational fluid fosters innovation, and provides seed funding to push the dynamics. Manufacturing firms and research organizations use boundaries of technology to dramatically improve our satellite Pointwise’s mesh generation software to seamlessly bridge the reconnaissance capabilities. It presents an opportunity for gap between CAD and computational fluid dynamics analysis. developers not traditionally associated with the NRO to Find more information at pointwise.com. participate in building the National Reconnaissance Office of the 21st century. Quantel, USA 608 601 Haggerty Lane National Research Council of 413 Bozeman, MT 59715 the National Academies www.quantel-laser.com [email protected] 500 Fifth Street, NW Washington, DC 20001 Quantel is a recognized expert in the manufacturing of www.nationalacademies.org/rap solid-state laser systems for scientific, military and industrial [email protected] applications. We provide technologically advanced laser The National Research Council of the National Academies systems to help you to achieve your specific goals: pulsed offers awards for independent graduate, postdoctoral and solid-state lasers, tunable dye lasers, high power laser diodes. senior research in all fields in science and engineering to Quantel also provides manufacturers and optical users be conducted at participating U.S. federal laboratories and worldwide with industry leading laser damage testing. affiliated institutions. Awards include generous stipend, relocation, professional travel and health insurance. Online applications are on the website. Software Cradle 208 70 Birch Alley, Suite 240 Beavercreek, OH 45440 Office of Naval Research 104/201 www.cradle-cfd.com [email protected] 875 North Randolph Street Arlington, VA 22203 Software Cradle is a leading provider of Computational www.onr.navy.mil Fluid Dynamics (CFD) software including SC/Tetra (general [email protected] purpose unstructured mesh), scSTREAM (general purpose As an executive branch agency within the Department of Cartesian mesh), and HEAT Designer (Cartesian mesh for Defense, the Office of Naval Research (ONR) supports the electronics). Since inception in 1984, Cradle has established President’s budget. ONR provides technical advice to the Chief itself as a major innovator for advancing the role of simulation of Naval Operations and the Secretary of the Navy. The Naval in engineering design. Air Warfare and Weapons Division supports the Navy’s power projection needs, fostering the technology development of naval aircraft, structures, propulsion, autonomy, energetics, directed energy and electric weapons.

www.aiaa.org/scitech2014 27 #aiaaSciTech IntroExhibitors

Springer 202/204 Triumph Aerospace Systems-Newport News 608 233 Spring Street 703 Middle Ground Boulevard New York, NY 10013 Newport News, VA 23606 www.springer.com www.triumphgroup.com [email protected] [email protected] We are proud to be the publisher of choice for numerous Triumph Aerospace Systems-Newport News is an industry books, valued by researchers globally, and high-quality leader in the engineering and manufacture of complex journals. Come and browse our key titles! Get 20% off print aerospace hardware, and prototype systems for force books and eBooks – and learn about MyCopy (a printed eBook measurement devices, ground test and flight applications. for $24.99). Meet our Senior Editor Silvia Schilgerius to discuss We have been employed in the development of nearly every your publishing proposal. Ensure maximum readership for domestic fixed-wing aircraft, missile, and helicopter system. your work, too! Springer, your partner in publishing. Find all Our capabilities include Engineering; Design & Analysis; offers online @ springer.com/aiaa. Manufacturing; Instrumentation & Assembly; Composites; Turbomachinery; Testing Services; and Rotorcraft Services. Tecplot, Inc 407 3535 Factoria Blvd SE, Suite 550 ViGYAN, Inc. 310 Bellevue, WA 98006 30 Research Drive 425-653-1200 X236 (phone) Hampton, VA 23666 425-653-9200 (fax) www.vigyan.com www.tecplot.com [email protected] [email protected] For almost 35 years, ViGYAN has provided aerospace engineering Tecplot is the visualization tool of choice for thousands of research and development services to NASA, other government engineers and scientists worldwide. Its use while performing agencies and corporations. Our business areas include aeronautics simulations, analysis, or experiments, provides insight and space R&D; scientific; engineering, and business software and understanding of the mechanisms inside the data— development; educational support services; and computer information critical in pinpointing and solving problems technology services. We have specialized expertise in wind tunnel to optimize designs or processes, or to explain physical testing and systems, including the operation of the ViGYAN Wind observations. Tunnel in Hampton, Virginia. ViGYAN was selected as the 2010, NASA Langley Research Center Small Business Subcontractor of the Year. ViGYAN is a minority–owned, small disadvantaged Tetra Research Corporation 510 business (SDB) and is ISO 9001 certified. 420 Park Avenue W Princeton, IL 61356 www.tetraresearch.com Wolverine Ventures, Inc. 507 [email protected] 16593 121 Terrace N Tetra Research specialized in Loci/CHEM CFD software Jupiter, FL 33478 development and advanced flow applications. Loci/CHEM www.wolverine-ventures.com is a unique CFD analysis tool that is formally second order [email protected] accurate on polyhedral meshes, scales thousands of processors Wolverine Ventures, Inc. is an engineering software firm with and contains advanced physical and body dynamics modules. more than 40+ years of combined experience in customized We provide software support, customized development, and NPSS coding and complex systems modeling. As the exclusive application training services to allow you to make the most distributor of NPSS Software and the leading provider for efficient and productive use of Lodi/CHEM. NPSS related services, WVI is an unparalleled resource NPSS Sales, Service and Training. Tri Models Inc. 602 5191 Oceanus Drive Huntington Beach, CA 92649 www.trimodels.com [email protected] Tri Models is the premier supplier of wind tunnel models and ground test hardware for the global aerospace community. We play a vital role in the development of new systems for the airframers. Whether you have a new program or refining an existing vehicle, Tri Models can help.

www.aiaa.org/scitech2014 28 #aiaaSciTech IntroPresentation Stage

The Presentation Stage provides a range of learning, recognition, and networking opportunities. It offers exhibitors a chance to explain in detail how their products and services can help you achieve your goals, as well as providing the chance to hear other interesting demonstrations and discussions. Please join us in the exposition hall for the following special presentations!

Tuesday, 14 January Wednesday, 15 January Thursday, 16 January 0700–1230 & 1400–1600 Show Open 0700–1600 Show Open 0700–1200 Show Open 0700–0800 Networking Coffee Break 0700–0800 Networking Coffee Break 0700–0900 Networking Coffee Break 0930–1000 Networking Coffee Break 0930–1000 Networking Coffee Break 0930–1000 Networking Coffee Break 1530–1600 Networking Coffee Break 1230–1330 Networking Luncheon 1500–1530 Networking Coffee Break

Tuesday, 14 January 1545-1530 Triumph Aerospace Systems (Booth 408) Wind Tunnel Unsteady Aerodynamic 0930-0945 Dantec Dynamics, Inc. (Booth 615) Load Measurement New Developments and Improvements of Daniel Stuewe Measurement Technology for Aerodynamics and Measurement of static loads is conventionally performed using Material Testing a combination of strain gage measurements. For the case of Cliff Weissman an unsteady loading environment with energy content in the same frequency band as structural modes, measurements can The understanding and characterization of fluid and particle be significantly corrupted. M4 Engineering has developed a dynamics and material testing is crucial for many applications product to accurately measure such unsteady loads. in the aerospace industry. An overview of a few of the latest developments in advanced measurement techniques from Dantec Dynamics are presented with emphasis on aeronautic 1715-1730 Michael V. Ciminera (Author) R&D applications. e Aircra Designers: A Grumman Historical Perspective 0945-1000 dSPACE (Booth 315) Tools for Embedded Soware Development 1745-1815 and Validation Recognizing Technical Excellence: Certicates of Noal Garber, Account Manager Merit for Best Papers and Student Competitions The presentation will describe dSPACE tool-chain for model- based design, development and testing of embedded software. dSPACE tools for Rapid Controls Prototyping including Wednesday, 15 January solutions for simulation of Aerospace communication busses, and automatic code generation tool for efficient systems will be 0930-0945 presented. The presentation will include examples of successful applications currently in flight developed using dSPACE Presentation of Sustained Service Awards systems.

1530-1545 Concord Lift (Booth 212) 0945-1000 ViGYAN (Booth 310) Concord Li, a thought experiment. Is it possible to ViGYAN’s Wind Tunnel, Economies of Scale have very heavy li at very low cost per ton mile? Richard White, Vice President Stephen Funck Brief review of the value of various types of micro testing, which may eliminate the need for further testing, or provide a Concord Lift is a unique configuration that opens the way to firm foundation for macro testing. previously unreachable capabilities.

www.aiaa.org/scitech2014 29 #aiaaSciTech IntroPresentation Stage

Wednesday, 15 January (continued)

1245-1300 Daniel P. Raymer (Author) Aircra Design: A Conceptual Approach, Fih Edition Demonstration of software which is included in the publication.

1500-1515 Higher Orbits & ISSET (Booth 102) Mission Discovery Michelle Hamm Learn about a unique program that uses space to get students interested in Science, Technology, Engineering & Math, as well as Leadership and Teamwork. The culmination of program results in a student experiment flying to space.

1515-1530 BETA CAE Systems, USA, Inc (Booth 412) Advanced CAE pre- and post-processing solutions for Aerospace applications using ANSA and META Pravin Peddiraju, Team Lead, CFD Applications BETA CAE System’s flagship products, ANSA and MetaPost, are one of the leading Pre- and Post-processing software solutions in the CAE market, widely used in industries such as automotive, motor sports, defense, bio-medical, aerospace etc… This presentation will discuss in detail some of the features in the NSA-METAPost software suite for the Aerospace Industry. Thursday, 16 January

0930-0945 Boeing Technology Services (Booth 302) Boeing Transonic Wind Tunnel Model Roll Mechanism (MRM) Dale Belter Boeing Technology Services will present an overview of the new Model Roll Mechanism (MRM) that is now in use in the Boeing Transonic Wind Tunnel. The new MRM mounting system enables more functionality and productivity with the 180 degree roll capability plus less time required for testing parameter changes.

www.aiaa.org/scitech2014 30 #aiaaSciTech IntroGeneral Information

AIAA Registration and i. By paper number: Click the Certificate of Attendance “Paper Number” link, select the Information Center Hours conference year, and enter the Certificates of Attendance are The AIAA Registration and Information paper number. available for attendees who request documentation at the forum itself. Center will be located in the Foyer. ii. Use the Search textbox to Hours are as follows: Please request your copy at the AIAA find papers by author, title, or Registration and Information Center Sunday, 12 January 1500–1900 hrs keyword. The Advanced Search beginning on Wednesday. AIAA link provides additional search Monday, 13 January 0700–1800 hrs offers this service to better serve the information and options. needs of the professional community. Tuesday, 14 January 2. All manuscript files submitted by Claims of hours or applicability toward –Thursday, 16 January 0700–1730 hrs four days prior to the conference professional education requirements are Friday, 17 January 0700–1200 hrs are currently in the proceedings. the responsibility of the participant. Files submitted after that date, both Wi-Fi Internet Access On Site original and revised manuscripts, Employment Opportunities will not be available until the final AIAA is providing limited Wi-Fi service AIAA members can post and browse proceedings update, which may take for attendees to use while on site. To keep resumes, browse job listings, and access up to 15 business days after the last this service available and optimized for other online employment resources day of the conference. all attendees, please do not download files by visiting the AIAA Career Center larger than 2MB, create multiple sessions 3. AIAA provides limited Wi-Fi service at http://careercenter.aiaa.org. across multiple devices, or download for attendees to use while on site. Additionally, a message board will be multiple files in one session. If you receive To keep this service available and available for postings in the exhibit hall. an error message that an AIAA server optimized for all attendees, please is blocking your current IP address, do not download files larger than Membership please inform the AIAA Registration and 2MB, create multiple sessions across Information Center. multiple devices, or download AIAA is your vital lifelong link to the multiple files in one session. If collective creativity and brainpower On-Site Wi Fi Information you receive an error message that of the aerospace profession and a champion for its achievements – Network Name: AIAA2014 an AIAA server is blocking your current IP address, please inform the and nonmembers who pay the full Username: SciTech AIAA registration desk. conference registration fee will receive Password: 2014 their first year’s AIAA membership at no 4. Direct any questions concerning additional cost! Students who are not yet Conference Proceedings access to proceedings and/or ARC to members may apply their registration [email protected]. fee toward their first year’s student Proceedings for the forum will be member dues. (Free membership is available online. The cost is included Manuscript Revisions: not included in discounted group-rate in the registration fee where indicated. 1. To request access to submit a registration.) Online proceedings will be available on revision, email AIAA at revisions@ 13 January 2014. Attendees who register aiaa.org no later than seven Young Professional Guide for in advance for the online proceedings will business days after the last day of Gaining Management Support be provided with instructions on how to the conference. Include the name of access them. Those registering on site will Young professionals have the unique this conference as well as your paper be provided with instructions at that time. opportunity to meet and learn from number in the body of the email. some of the most important people in the Proceedings: 2. Revisions submitted for manuscripts business by attending conferences and 1. To view proceedings visit already online will not refresh until participating in AIAA activities. A detailed www.aiaa.org >ARC>Meeting Papers. after the proceedings have been online guide, published by the AIAA a. Log in with the link at the top updated, which may take up to 15 Young Professional Committee, is available right of the page. business days after the last day of the to help you gain support and financial conference. backing from your company. The guide b. Select the appropriate conference explains the benefits of participation, offers from the list. AIAA Livestream Channel recommendations and provides an example letter for seeking management support c. Search for individual papers with Visit www.livestream.com/aiaa to view and funding, and shows you how to get the the Quick Search toolbar in the selected keynotes and plenary sessions most out of your participation. The online upper-right corner of the page: from the week’s events. Share the link guide can be found on the AIAA website at so colleagues who cannot attend the www.aiaa.org/YPGuide. conference can watch live or view afterward. www.aiaa.org/scitech2014 31 #aiaaSciTech IntroGeneral Information

Nondiscriminatory Practices AIAA accepts registrations irrespective of race, creed, gender, color, sexual orientation, physical handicap, and Author and Session Chair Information national or ethnic origin. Speakers’ Briefings collected and used for future planning Restrictions in Session Rooms purposes, including session topics and Photos, video, or audio recording room allocations. Please submit your of sessions or exhibits, as well as the Authors who are presenting papers will session chair report electronically by 17 unauthorized sale of AIAA-copyrighted meet with session chairs and co-chairs in January 2014. material, is prohibited. their session rooms for a short 30-minute briefing on the day of their sessions to Audiovisual International Traffic in Arms exchange bios and review final details Each session room will be preset with Regulations (ITAR) prior to the session. Please attend on the the following: one laptop computer, day of your session(s). Laptops preloaded one LCD projector, one screen, one AIAA speakers and attendees are with the Speakers’ Briefing preparation microphone and sound system (if reminded that some topics discussed slides will be provided in each session necessitated by room size), and one laser at the forum could be controlled by room. Speakers’ Briefing schedule is as pointer. You may also use your own the International Traffic in Arms follows: computer. Any additional audiovisual Regulations (ITAR). U.S. nationals (U.S. Monday – Friday Morning Sessions equipment requested on site will be at citizens and permanent residents) are 0730–0800 hrs cost to the presenter. Please note that responsible for ensuring that technical AIAA does not provide security in the data they present in open sessions to Monday, Tuesday and Thursday non-U.S. nationals in attendance or in Afternoon Sessions session rooms and recommends that items of value not be left unattended. conference proceedings are not export 1400–1430 hrs restricted by the ITAR. U.S. nationals Wednesday Afternoon Sessions “No Paper, No Podium” and are likewise responsible for ensuring 1330–1400 hrs that they do not discuss ITAR export- “No Podium, No Paper” Policy restricted information with non-U.S. Speakers’ Practice Room If a written paper is not submitted by nationals in attendance. the final manuscript deadline, authors Speakers who wish to practice their will not be permitted to present the presentations may do so in the National paper at the forum. Also, if a paper Harbor Conference 1 and National is not presented at the forum, it will Harbor Conference 9 rooms. A sign- be withdrawn from the proceedings. up sheet will be posted on each door. It is the responsibility of those whose AIAA is the largest aerospace In consideration of others, please limit papers or presentations are accepted to professional society in the world, practice time to 30-minute increments. ensure that a representative attends the serving more than 35,000 individual conference to present the paper. These and corporate members from 80 Session Chair Reports policies are intended to improve the countries, who help make the world All session chairs are asked to complete quality of the program for attendees. safer, more connected, more accessible, a session chair report to evaluate their and more prosperous. AIAA brings session for future planning. AIAA has Journal Publication together industry, academia, and partnered with Canvas Solutions to government to advance engineering and Authors of appropriate papers are provide an electronic Session Chair science in aviation, space, and defense, encouraged to submit them for possible Report form. You can download the and provides its members with the publication in one of the Institute’s FREE mobile app in your App Store, lifelong community, connections, and archival journals: AIAA Journal; Journal AppWorld, or Marketplace by searching development opportunities that lead of Aircraft; Journal of Guidance, Control, for “Canvas Solutions, Inc.” The mobile to a thriving profession and enduring and Dynamics; Journal of Propulsion app is free, so please be sure to download contributions to society. and Power; Journal of Spacecraft and it. Detailed instructions will be provided Rockets; Journal of Thermophysics and American Institute of Aeronautics and in the session rooms. If you do not have Heat Transfer; or Journal of Aerospace Astronautics a tablet or a smartphone, simply use Information Systems (formerly Journal 1801 Alexander Bell Drive, Suite 500 the report form as a guide and enter of Aerospace Computing, Information, Reston, VA 20191-4344 your session chair report information and Communication). You may now 703.264.7500 or 800.639.AIAA (2422) at the session chair reporting computer submit your paper online at http:// Fax: 703.264.7657 station located on site near the AIAA mc.manuscriptcentral.com/aiaa. [email protected] registration area. Report data will be www.aiaa.org www.aiaa.org/scitech2014 32 #aiaaSciTech IntroOrganizing Committee

Executive Steering Committee Forum Organizing Committee Mary Snitch, Senior Manager, Strategic External Relations, Corporate Robert Braun, David and Andrew Supriya Banerjee, President & CEO, Engineering & Technology (CE&T), Lewis Professor of Space Technology, Finehas International, Inc. Lockheed Martin Corporation Georgia Institute of Technology Kim Flossie, Director of Business Gulshan Singh, Mechanical Engineer, Executive Steering Committee Chair: Development, Wolverine Ventures, Inc. General Electric - Global Research John Evans, Vice President, International, Lockheed Martin Steven Gorrell, Associate Professor, Corporation Brigham Young University Forum Technical Program Chairs Carlos Cesnik, Professor, University Ferd Grosveld, Manager Structural James Shields, Chief Executive Officer, of Michigan Charles Stark Draper Laboratory, Inc. Engineering, Northrop Grumman Robbie Robertson, Mission Lead, Joseph Gruber, Wyle Tom Shih, Head and Professor of Space Situational Awareness Air Aeronautics and Astronautics, Purdue Tim Hinerman, Aerojet Rocketdyne Force Research Lab, Space Vehicles University Directorate Forum General Chair: Tom Irvine, Deputy Associate David Throckmorton, Program Administrator, ARMD, NASA Manager, Northrop Grumman Essam E Khalil, Professor, Cairo University

AIAA SciTech 2014 Features: • 22nd AIAA/ASME/AHS Adaptive • 10th AIAA Multidisciplinary Structures Conference Design Optimization Specialist • 52nd AIAA Aerospace Sciences Conference Meeting • 16th AIAA Non-Deterministic • AIAA Atmospheric Flight Approaches Conference Mechanics Conference • 55th AIAA/ASME/ASCE/AHS/ • AIAA Spacecraft Structures ASC Structures, Structural Conference Dynamics, and Materials Conference • AIAA Guidance, Navigation, and Control Conference • 7th Symposium on Space Resource Utilization • AIAA Modeling and Simulation Technologies Conference • 32nd ASME Wind Energy Symposium Supported by: • AIAA Aerospace Design & • AIAA Aerospace Sciences Structures Technical Group Technical Group (Director: (Director: Kathleen Atkins, Dr. James Keenan, US Army Lockheed Martin Aeronautics AMRDEC) Company)

www.aiaa.org/scitech2014 33 #aiaaSciTech IntroCommittee Meetings and Events

Time Title Location Saturday, 11 January 2014 0800-1700 hrs AIAA CE Course: Decision Analysis Chesapeake Conference Room A 0800-1700 hrs 1st AIAA Sonic Boom Prediction Workshop Chesapeake Conference Room D 0800-1700 hrs Low Reynolds Number Workshop Chesapeake Conference Room E Sunday, 12 January 2014 0800-1700 hrs AIAA CE Course: Decision Analysis Chesapeake Conference Room A 0800-1700 hrs Introduction to Integrated Computational Materials Chesapeake Conference Room B 0900-1200 hrs TAC Director/Deputy Director Training National Harbor 5 0900-1430 hrs TAC TC/PC Chair Training National Harbor 4 1400-1800 hrs ASI-WG Chesapeake Conference Room 1 1430-1700 hrs TAC Workshop: Exploring Virtual Opportunities Information National Harbor 3 Session 1430-1500 hrs APATC Liaisons Subcommittee Chesapeake Conference Room C 1500-1600 hrs APATC Education Subcommittee Chesapeake Conference Room 2 1500-1600 hrs APATC Honors & Awards Subcommittee Chesapeake Conference Room 8 1500-1600 hrs APATC Membership & Nominations Subcommittee Chesapeake Conference Room 9 1500-1600 hrs APATC Planning Subcommittee Chesapeake Conference Room 12 1500-1600 hrs APATC Publicity & Publications Subcommittee Chesapeake Conference Room C 1600-1700 hrs APATC Technical Activities Subcommittee Chesapeake Conference Room C 1600-1700 hrs GEPC Steering Committee National Harbor 5 1600-1800 hrs FDTC CFD Undergraduate Education DG Chesapeake Conference Room 9 1600-1800 hrs FDTC High-Order Methods WG Chesapeake Conference Room D 1600-1800 hrs FDTC Transition DG Chesapeake Conference Room E 1600-1800 hrs Student Briefing National Harbor 4 1630-1930 hrs SRTC Book Subcommittee Chesapeake Conference Room 2 1700-1800 hrs APATC Steering Committee Chesapeake Conference Room C 1700-1800 hrs GEPC Conference Subcommittee National Harbor 5 1700-2200 hrs SDM Student Paper Competition National Harbor 6 1730-1800 hrs GTTC Membership Subcommittee National Harbor 10 1730-2030 hrs Structures TC National Harbor 11 1800-1900 hrs GTTC Steering Subcommittee National Harbor 10 1800-2100 hrs Applied Aerodynamics TC National Harbor 2 1800-2100 hrs Atmospheric Flight Mechanics TC Chesapeake Conference Room F 1800-2200 hrs GNC Student Paper Competition National Harbor 7 1830-2000 hrs TAC Aerospace Design & Structures Group Meeting Chesapeake Conference Room C 1830-2000 hrs TAC Aircraft & Atmospheric Systems Group Meeting Chesapeake Conference Room 8 1830-2000 hrs TAC Engineering & Technology Management Group Meeting Chesapeake Conference Room 9 1830-2000 hrs TAC Propulsion & Energy Group Meeting National Harbor 5 1830-2000 hrs TAC Space & Missiles Group Meeting Chesapeake Conference Room 12 1900-2000 hrs GTTC Introduction/Overview National Harbor 10 1900-2100 hrs Academic Affairs Committee Meeting Chesapeake Conference Room D 2000-2100 hrs GTTC Aerodynamics/Propulsion Subcommittee National Harbor 10

www.aiaa.org/scitech2014 34 #aiaaSciTech IntroCommittee Meetings and Events

Time Title Location Monday, 13 January 2014 0800-1600 hrs GTTC Dual Flow Reference Nozzle 1 Potomac Ballroom 6 0900-1000 hrs ABPTCs Steering Committee Chesapeake Conference Room K 0900-1500 hrs NIA Technical Advisory Committee Chesapeake Conference Room J 1000-1400 hrs B2B Matchmaking Potomac Ballroom 1&2 1000-1100 hrs ABPTCs Honors and Awards Subcommittee Chesapeake Conference Room 12 1100-1200 hrs ABPTCs Education Subcommittee Chesapeake Conference Room 12 1100-1400 hrs General Aviation TC Chesapeake Conference Room 11 1200-1230 hrs ABPTCs Communications Subcommittee Chesapeake Conference Room 12 1200-1400 hrs Space Operations & Support TC Chesapeake Conference Room K 1230-1530 hrs Communications Systems TC Chesapeake Conference Room L 1230-1400 hrs Durand Lectureship in Public Service / Public Policy Luncheon Potomac Ballroom A&B 1300-1400 hrs Student Conference Luncheon Potomac Ballroom 3 1300-1400 hrs ABPTCs Conference Subcommittee Chesapeake Conference Room 12 1300-1400 hrs HSABPTC Membership Subcommittee Chesapeake Conference Room 10 1300-1400 hrs GTETC Membership Subcommittee Potomac Ballroom 5 1300-1400 hrs ABPSITC Membership Subcommittee Potomac Ballroom 4 1330-1530 hrs P&E Group Meeting I Chesapeake Conference Room 1 1500-1700 hrs Education Series Editorial Advisory Board Potomac Ballroom 5 1500-1700 hrs Aerospace America Steering Committee Chesapeake Conference Room K 1600-1700 hrs ABP Working Groups Chesapeake Conference Room 10 1600-1700 hrs CGNS Committee on Standards Chesapeake Conference Room L 1630-1800 hrs CASE 2014 Planning Meeting Potomac Ballroom 4 1630-1730 hrs AMTTC New Member Orientation Chesapeake Conference Room 12 1700-1800 hrs FDTC Free Shear Mixing Layer Control DG Chesapeake Conference Room 11 1700-1830 hrs FDTC Low Re Aerodynamics DG Chesapeake Conference Room 1 1700-1900 hrs Computational Fluid Dynamics Committee on Standards Chesapeake Conference Room L 1700-1900 hrs FDTC Turbulence Modeling Benchmarks WG Chesapeake Conference Room J 1700-1900 hrs Solid Rockets TC Chesapeake Conference Room 2 1730-1830 hrs Dryden Lectureship in Research Potomac Ballroom C 1730-1830 hrs APATC Missile & Projectile Aeroprediction DG National Harbor 11 1730-1900 hrs APATC Validation of Numerical Models DG Maryland Ballroom 4 1800-2100 hrs Legal Aspects of Aeronautics and Astronautics TC Chesapeake Conference Room 10 1830-1930 hrs GTTC New Members Briefing Maryland Ballroom 3 1830-2000 hrs AMTTC Awards Subcommittee Chesapeake Conference Room 11 1830-2000 hrs Student Reception Potomac Ballroom D 1830-2030 hrs High Speed Air Breathing Propulsion TC Potomac Ballroom 6 1830-2030 hrs Gas Turbine Engines TC Maryland Ballroom 1 1830-2030 hrs Air Breathing Propulsion Systems Integration TC Maryland Ballroom 2 1830-2030 hrs University of Illinois, Department of Aerospace Engineering Chesapeake Conference Room D Reception 1845-1930 hrs Associate Fellows Reception Cherry Blossom Prefunction 1900-2000 hrs Verification and Validation Committee on Standards Chesapeake Conference Room L

www.aiaa.org/scitech2014 35 #aiaaSciTech IntroCommittee Meetings and Events

Time Title Location Monday, 13 January 2014 (continued) 1900-2100 hrs FDTC CFD Methods Subcommittee Chesapeake Conference Room 1 1900-2100 hrs FDTC Flow Control and Fluid Applications Subcommittee Chesapeake Conference Room J 1900-2200 hrs Terrestrial Energy Systems TC Chesapeake Conference Room K 1900-2200 hrs History TC Potomac Ballroom 4 1900-2200 hrs TAC Aerospace Sciences Group Meeting Maryland Ballroom 6 1900-2200 hrs Survivability TC Potomac Ballroom 5 1900-2200 hrs Intelligent Systems TC Potomac Ballroom 3 1900-2200 hrs Society and Aerospace Technology TC Chesapeake Conference Room 12 1900-2200 hrs Propellants & Combustion TC Maryland Ballroom A 1930-2030 hrs GTTC Awards Subcommittee Maryland Ballroom 3 1930-2130 hrs 2014 Associate Fellows Dinner Cherry Blossom Ballroom 1930-2130 hrs CADWG Chesapeake Conference Room 5&6 2100-2200 hrs FDTC Steering Committee Chesapeake Conference Room L 2030-2130 hrs GTTC Publications Subcommittee Maryland Ballroom 3 Tuesday, 14 January 2014 0800-1200 hrs AIAA Ethics Committee Chesapeake Conference Room 12 0800-1000 hrs Books Subcommittee Chesapeake Conference Room 10 0800-1200 hrs GTTC Future of Ground Testing WG Chesapeake Conference Room 11 0900-1200 hrs TAC Executive Board Meeting Potomac Ballroom 5 0930-1130 hrs Education Activities Committee Chesapeake Conference Room K 1000-1100 hrs SciTech Executive Steering Committee Chesapeake Conference Room 2 1000-1200 hrs Progress Series Editorial Advisory Board Chesapeake Conference Room 10 1000-1200 hrs AIAA Journal Editorial Advisory Board Potomac Ballroom 6 1100-1200 hrs SciTech Forum Organizing Committee Meeting Chesapeake Conference Room 1 1300-1400 hrs HyTASP Steering Committee Potomac Ballroom 5 1300-1400 hrs Compensation Committee Chesapeake Conference Room 2 1300-1700 hrs GTTC Dual Flow Reference Nozzle 2 Potomac Ballroom 4 1400-1500 hrs Pressure Gain Combustion Working Group Chesapeake Conference Room 1 1400-1600 hrs HyTASP PC Potomac Ballroom 5 1400-1600 hrs Verification and Validation Best Practices for Integrated Chesapeake Conference Room K Computational Materials Engineering Tutorial 1400-1600 hrs Emerging Technologies Committee Chesapeake Conference Room 12 1400-1800 hrs TAC New Initiatives Subcommittee Potomac Ballroom 6 1400-1800 hrs Student Activities Committee Potomac Ballroom 2&3 1500-1600 hrs ABPTCs PAW Committee Chesapeake Conference Room L 1500-1600 hrs TPTC Awards Subcommittee Chesapeake Conference Room 10 1500-1600 hrs TPTC Best Paper Subcommittee Chesapeake Conference Room 11 1530-1700 hrs Crichlow Prize Selection Committee Chesapeake Conference Room J 1530-1730 hrs Journal of Aircraft Editorial Advisory Board Chesapeake Conference Room 1

www.aiaa.org/scitech2014 36 #aiaaSciTech IntroCommittee Meetings and Events

Time Title Location Tuesday, 14 January 2014 (Continued) 1600-1700 hrs Book Authors Reception Chesapeake Conference Room 2 1600-1700 hrs TPTC Publications Subcommittee Chesapeake Conference Room 10 1600-1700 hrs TPTC Conferences Subcommittee Chesapeake Conference Room 11 1600-1730 hrs AIAA Cybersecurity Working Group National Harbor 2 1630-1730 hrs AIAA/ARCS Alum Happy Hour Belvedere Lobby Bar 1700-1800 hrs TPTC Nominations Subcommittee Chesapeake Conference Room 10 1700-1800 hrs TPTC Education Subcommittee Chesapeake Conference Room 11 1730-1930 hrs APATC Aerodynamic Design Optimization DG Maryland Ballroom 3 1730-2030 hrs ASME Wind Energy TC Chesapeake Conference Room J 1800-1900 hrs ABPTCs Working Groups Chesapeake Conference Room L 1800-1900 hrs TPTC Publicity Subcommittee Chesapeake Conference Room 10 1800-2000 hrs Information and Command and Control Systems TC Chesapeake Conference Room 12 1830-2030 hrs ASME Structures and Materials TC Chesapeake Conference Room A 1830-2030 hrs ABPTCs Meeting Woodrow Wilson B 1830-2130 hrs Space Resources TC Chesapeake Conference Room 11 1900-2200 hrs Aerodynamic Measurement Technology TC Potomac Ballroom 2&3 1900-2200 hrs Design Engineering TC Chesapeake Conference Room 1 1900-2200 hrs Aerospace Department Chair Association (ADCA) Maryland Ballroom A 1900-2200 hrs Materials TC Maryland Ballroom B 1900-2200 hrs Thermophysics TC Maryland Ballroom 1&2 1900-2200 hrs Fluid Dynamics TC Maryland Ballroom C 1900-2200 hrs Multidisciplinary Design Optimization TC Potomac Ballroom 6 1900-2200 hrs Adaptive Structures TC Potomac Ballroom 5 1900-2200 hrs Plasmadynamics and Lasers TC Maryland Ballroom 5 1900-2200 hrs Meshing, Visualization and Computational Environments TC Maryland Ballroom 6 1900-2200 hrs TAC Program Committee Group Meeting Chesapeake Conference Room K 1900-2200 hrs Aeroacoustics TC Chesapeake Conference Room 2 2000-2130 hrs FDTC Shock Wave/Boundary Layer Interaction DG Potomac Ballroom 4 2000-2200 hrs TAC Information Systems Group Meeting Chesapeake Conference Room 10 Wednesday, 15 January 2014 0800-1000 hrs Journals Subcommittee Chesapeake Conference Room J 0800-1100 hrs Winter Public Policy Committee Meeting Maryland Ballroom 2 0800-1200 hrs STEM K-12 Committee Meeting Chesapeake Conference Room 1 0800-1200 hrs DETC Subcommittee Chesapeake Conference Room K 0800-1200 hrs GTTC Model Attitude and Deformation WG Chesapeake Conference Room 12 0800-1400 hrs Mass Properties Committee on Standards for S-120 Chesapeake Conference Room 11 0830-0945 hrs Audit Committee Meeting Chesapeake Conference Room 10 0830-1700 hrs Systems Engineering TC Potomac Ballroom 1 0900-1100 hrs RAC V Meeting Chesapeake Conference Room 2 0900-1600 hrs Membership Committee Meeting Potomac Ballroom 3 1000-1200 hrs Finance Committee Meeting Potomac Ballroom 4

www.aiaa.org/scitech2014 37 #aiaaSciTech IntroCommittee Meetings and Events

Time Title Location Wednesday, 15 January 2014 (continued) 1000–1230 hrs Journals Editors-in-Chief Chesapeake Conference Room J 1030–1130 hrs SciTech 2015 Technical Program Committee Meeting Potomac Ballroom 5 1130–1230 hrs Aviation 2014 LM Planning Team Chesapeake Conference Room 2 1300–1400 hrs National Capital Section Council Chesapeake Conference Room K 1200-1500 hrs Energy Optimized Aircraft and Equipment Systems PC Chesapeake Conference Room 10 1300–1400 hrs National Capital Section Council Chesapeake Conference Room K 1300–1500 hrs P&E Group Meeting II Potomac Ballroom 2 1300–1500 hrs GTTC Wind Tunnel Flow Quality WG Chesapeake Conference Room 12 1300–1500 hrs RAC II Meeting Chesapeake Conference Room 2 1300–1500 hrs Journal of Guidance, Control, and Dynamics Editorial Advisory Chesapeake Conference Room 1 Board 1300–1600 hrs Corporate Membership Committee Potomac Ballroom 5&6 1300–1600 hrs Aircraft Design TC Potomac Ballroom 4 1300–1500 hrs Publications Planning and Review Subcommittee Chesapeake Conference Room J 1500–1700 hrs Journal of Aerospace Information Systems Editorial Advisory Board Chesapeake Conference Room 11 1500–1700 hrs Publications Ethical Standards Subcommittee Chesapeake Conference Room J 1500–1700 hrs RAC IV Meeting Chesapeake Conference Room 2 1500–1700 hrs RAC I Meeting Chesapeake Conference Room K 1530–1730 hrs International Activities Committee Baltimore 3–5 1530–2200 hrs Computer Systems TC Chesapeake Conference Room 12 1600–1730 hrs Corporate Member/Exhibitor Reception Prince George's Exhibit Hall D&E 1630–1830 hrs GTTC DOE Focus Group Potomac Ballroom 4 1730–1830 hrs ABCM/AIAA MOU Signing Baltimore 3–5 1730–1830 hrs von Kármán Lectureship in Astronautics Potomac Ballroom C 1730–1830 hrs FDTC Solver Technology for Turbulent Flows DG Potomac Ballroom 1 1730–1930 hrs Green Engineering PC Potomac Ballroom 5&6 1800–1900 hrs FDTC New Frontiers Subcommittee Chesapeake Conference Room J 1800–2000 hrs APATC Rotorcraft Simulations & Performance Predictions DG Chesapeake Conference Room 11 1830–1930 hrs GTTC Conferences Subcommittee Chesapeake Conference Room 10 1830–1930 hrs FDTC Large Eddy Simulation DG Chesapeake Conference Room K 1830–2030 hrs AMTTC Update Presentations Chesapeake Conference Room E 1830–2030 hrs Intelligent Light Customer Reception (Private Function) Azalea 3 1830–2130 hrs Small Satellite TC Maryland Ballroom 5 1800–2100 hrs Transformational Flight PC Potomac Ballroom 2 1800–2100 hrs V/STOL Aircraft Systems TC Chesapeake Conference Room 2 1800–2100 hrs Software TC Potomac Ballroom 3 1830–2030 hrs University of Michigan, Aerospace Centennial Celebration Dessert Maryland Ballroom C Reception 1830–2200 hrs Guidance, Navigation and Control TC Maryland Ballroom D 1900–2000 hrs APATC Low Reynolds Number Aerodynamic Modeling & Test DG Potomac Ballroom 1 1900–2100 hrs FDTC Fundamentals of Flow Phenom Subcommittee Chesapeake Conference Room L 1900–2100 hrs Introduction to the AIAA Educator Academy Chesapeake Conference Room A 1900–2200 hrs Spacecraft Structures TC Maryland Ballroom 4 www.aiaa.org/scitech2014 38 #aiaaSciTech IntroCommittee Meetings and Events

Time Title Location 1900-2200 hrs Structural Dynamics TC Maryland Ballroom B Wednesday, 15 January 2014 (continued) 1900-2200 hrs Non-Deterministic Approaches TC Potomac Ballroom D 1900-2200 hrs PDLTC Plasma Aerodynamics DG Maryland Ballroom 3 1900-2200 hrs Structures TC Maryland Ballroom A 1930-2030 hrs Ground Testing Committee on Standards Chesapeake Conference Room 10 1930-2200 hrs Alumni and Friends of UC Reception Woodrow Wilson B 1930-2200 hrs Unmanned Systems PC Chesapeake Conference Room J 2030-2130 hrs GTTC Education and Student Activities Subcommittee Chesapeake Conference Room 10 Thursday, 16 January 2014 0700-0930 hrs Standards Executive Council Chesapeake Conference Room 12 0730-1430 hrs Region & Section Activities Committee (RSAC) Potomac Ballroom 4 0800-1200 hrs Publications Committee Potomac Ballroom 2&3 0800-1600 hrs GTTC Internal Balances WG Potomac Ballroom 5&6 0800-1600 hrs Technical Activities Committee Potomac Ballroom D 0830-1200 hrs Honors and Awards Committee Chesapeake Conference Room 10 0930-1300 hrs Modeling and Simulation Technical Committee Chesapeake Conference Room 1 1000-1200 hrs Foundation Board of Trustees Chesapeake Conference Room 11 1300-1500 hrs Institute Development Committee Chesapeake Conference Room 11 1730-2000 hrs Ground Testing TC Potomac Ballroom D 1800-2000 hrs Women at SciTech Happy Hour and Keynote Speaker National Harbor 3 1830-1930 hrs AIAA National Capital Section Guest Speaker Chesapeake Conference Room D Friday, 17 January 2014 0800-1200 hrs Board of Directors Meeting Woodrow Wilson B&C

www.aiaa.org/scitech2014 39 #aiaaSciTech IntroSessions at a Glance

Abbreviation Title Date Start Time End Time Location Aeroacoustics AA-1 Airframe Noise and Sound Propagation 13-Jan 1000 hrs 1230 hrs Azalea 3 AA-2 Jet Noise I 13-Jan 1430 hrs 1730 hrs Woodrow Wilson C AA-3 Community Noise and Sonic Boom 14-Jan 1000 hrs 1230 hrs Woodrow Wilson B AA-4 Jet Noise II 14-Jan 1430 hrs 1730 hrs Azalea 2 AA-5 Fan and Duct Acoustics 15-Jan 1000 hrs 1230 hrs National Harbor Conference Room 3 AA-6 Jet Noise III 15-Jan 1400 hrs 1730 hrs Azalea 2 AA-7 Jet Noise IV 16-Jan 1430 hrs 1730 hrs Chesapeake Conference Room I AA-8 Computational Aeroacoustics 17-Jan 0800 hrs 1200 hrs Maryland Ballroom D Air Breathing Propulsion Systems Integration ABPSI-1 Group for Aeronautical Research and Technology in 14-Jan 1000 hrs 1230 hrs Chesapeake Conference Room 7 EURope (GARTEUR) I ABPSI-2 Air Breathing Propulsion System Integration and 14-Jan 1430 hrs 1730 hrs Maryland Ballroom D Optimization ABPSI-3 Group for Aeronautical Research and Technology in 15-Jan 1000 hrs 1230 hrs Chesapeake Conference Room 9 EURope (GARTEUR) II ABPSI-5 Educating Today's and Tomorrow's Propulsion 16-Jan 1430 hrs 1730 hrs National Harbor Conference Room 4 Engineers Aircraft Design ACD-1 Aircraft Design Methodologies 13-Jan 1000 hrs 1230 hrs Azalea 1 ACD-2 Aircraft Design Studies 13-Jan 1000 hrs 1230 hrs Azalea 2 ACD-3 Aircraft Design Issues 13-Jan 1430 hrs 1730 hrs Azalea 1 ACD-4 Aircraft Design Optimization 13-Jan 1430 hrs 1730 hrs Azalea 2 ACD-5 Aircraft Design Education 14-Jan 1000 hrs 1230 hrs Azalea 1 ACD-6 Electric Systems for Aircraft Design 14-Jan 1000 hrs 1230 hrs Azalea 2 ACD-7 Aircraft Design with Electric Propulsion 14-Jan 1430 hrs 1730 hrs Azalea 1 ACD-8 Unmanned Aircraft Design 15-Jan 1000 hrs 1230 hrs Azalea 1 Atmospheric Flight Mechanics AFM-1 Flight Dynamics and Handling Qualities I 13-Jan 1000 hrs 1230 hrs National Harbor Conference Room 12 AFM-2 LOC Prevention and Recovery (Invited) 13-Jan 1000 hrs 1230 hrs National Harbor Conference Room 13 AFM-3 Flight Dynamics and Handling Qualities II 13-Jan 1430 hrs 1730 hrs National Harbor Conference Room 13 AFM-4 Flight Dynamics and Handling Qualities III 14-Jan 1000 hrs 1230 hrs National Harbor Conference Room 12 AFM-5 Planetary Reentry I 14-Jan 1000 hrs 1230 hrs National Harbor Conference Room 13 AFM-6 Flight Dynamics and Handling Qualities IV 14-Jan 1430 hrs 1730 hrs National Harbor Conference Room 13 AFM-7 Aerodynamic Predictive Methods 15-Jan 1000 hrs 1230 hrs National Harbor Conference Room 13 AFM-8 Launch Vehicles 15-Jan 1400 hrs 1730 hrs National Harbor Conference Room 12 AFM-9 Micro UAVs 15-Jan 1400 hrs 1730 hrs National Harbor Conference Room 13 AFM-10 Planetary Reentry II 16-Jan 1000 hrs 1230 hrs National Harbor Conference Room 13 AFM-11 Planetary Reentry III 16-Jan 1430 hrs 1730 hrs National Harbor Conference Room 8

www.aiaa.org/scitech2014 40 #aiaaSciTech IntroSessions at a Glance

Abbreviation Title Date Start Time End Time Location Aerodynamic Measurement Technology AMT-1 Absorption and Emission Spectroscopy 14-Jan 1000 hrs 1230 hrs Maryland Ballroom 1 AMT-2 Volumetric Measurement Techniques 14-Jan 1000 hrs 1230 hrs Maryland Ballroom 2 AMT-3 Review of Skin Friction and Shear Stress Measurement 14-Jan 1430 hrs 1730 hrs Maryland Ballroom 1 Techniques (Invited) AMT-4 Supersonic Flow Diagnostics 14-Jan 1430 hrs 1730 hrs Maryland Ballroom 2 AMT-5/ Combustion Diagnostics I 15-Jan 1000 hrs 1230 hrs Maryland Ballroom 1 PC-11 AMT-6 Recent Advances and Applications of Stochastic 15-Jan 1400 hrs 1730 hrs Maryland Ballroom 2 Estimation Techniques (Invited) AMT-7 Advances in Coherent Anti-Stokes Raman Scattering 16-Jan 1000 hrs 1230 hrs Maryland Ballroom 1 and Other Spectroscopic Techniques AMT-8 Velocimetry 16-Jan 1000 hrs 1230 hrs Maryland Ballroom 2 AMT-9 Surface Measurements 16-Jan 1430 hrs 1730 hrs Maryland Ballroom 1 AMT-10/ Velocity and Other Measurements In Wind Tunnels 16-Jan 1430 hrs 1730 hrs Maryland Ballroom 2 GT-8 AMT-12/ Pressure and Temperature Measurements in Wind 17-Jan 0800 hrs 1200 hrs Maryland Ballroom 2 GT-10 Tunnels Applied Aerodynamics APA-1 Low Speed Low Reynolds Number Aerodynamics I 13-Jan 1000 hrs 1230 hrs National Harbor Conference Room 3 APA-2 Simulation of Rotor in Hover (Invited) I 13-Jan 1000 hrs 1230 hrs Maryland Ballroom D APA-3 Unsteady Aerodynamics I 13-Jan 1000 hrs 1230 hrs Maryland Ballroom 3 APA-4 Vortical/Vortex Flow 13-Jan 1000 hrs 1230 hrs Maryland Ballroom B APA-5 Weapons Aerodynamics and Store Separation I 13-Jan 1000 hrs 1230 hrs Maryland Ballroom A APA-6 Active and Passive Flow Control I 13-Jan 1430 hrs 1730 hrs Maryland Ballroom A APA-7 Best Practices for CFD Validation - Validation of 13-Jan 1430 hrs 1730 hrs Maryland Ballroom 4 Numerical Models Discussion Group (Invited) APA-8 Simulation of Rotor in Hover (Invited) II 13-Jan 1430 hrs 1730 hrs Maryland Ballroom 3 APA-9 Weapons Aerodynamics and Store Separation II 13-Jan 1430 hrs 1730 hrs National Harbor Conference Room 11 APA-10 Active and Passive Flow Control II 14-Jan 1000 hrs 1230 hrs Chesapeake Conference Room I APA-11 High Angle of Attack and High Lift Aerodynamics 14-Jan 1000 hrs 1230 hrs Maryland Ballroom 5 APA-12 Propeller/Rotorcraft Aerodynamics I 14-Jan 1000 hrs 1230 hrs Maryland Ballroom 4 APA-13 Special Session: Aerodynamic Design Optimization: 14-Jan 1000 hrs 1230 hrs Maryland Ballroom D Current Trends and Future Direction I APA-14 Special Session: CREATE-AV High Performance 14-Jan 1000 hrs 1230 hrs Woodrow Wilson A Computing Multiphysics Applications of Full-Up Air Vehicles I APA-15 Special Session: 2nd Cranked Arrow Wing Aerodynamic 14-Jan 1000 hrs 1230 hrs Maryland Ballroom B Project International (CAWAPI) I APA-16 Aerodynamic Design: Analysis, Methodologies and 14-Jan 1430 hrs 1730 hrs Maryland Ballroom 4 Optimization APA-17 Applied CFD 14-Jan 1430 hrs 1730 hrs National Harbor Conference Room 5 APA-18 Propeller/Rotorcraft Aerodynamics II 14-Jan 1430 hrs 1730 hrs Maryland Ballroom A APA-19 Special Session: Aerodynamic Design Optimization: 14-Jan 1430 hrs 1730 hrs Maryland Ballroom 3 Current Trends and Future Direction II APA-20 Icing Effects on Vehicle Aerodynamics 15-Jan 1000 hrs 1230 hrs Maryland Ballroom 3

www.aiaa.org/scitech2014 41 #aiaaSciTech IntroSessions at a Glance

Abbreviation Title Date Start Time End Time Location Applied Aerodynamics (continued) APA-21 Low Speed Low Reynolds Number Aerodynamics II 15-Jan 1000 hrs 1230 hrs Chesapeake Conference Room I APA-22 Special Session: 2nd High Lift Prediction Workshop 15-Jan 1000 hrs 1230 hrs Maryland Ballroom A (HiLiftPW-2) I APA-23 Special Session: CREATE-AV High Performance 15-Jan 1000 hrs 1230 hrs Maryland Ballroom 4 Computing Multiphysics Applications of Full-Up Air Vehicles II APA-24 Special Session: 2nd Cranked Arrow Wing Aerodynamic 15-Jan 1000 hrs 1230 hrs Maryland Ballroom D Project International (CAWAPI) II APA-25 Aerodynamic and Multi-Disciplinary Design and 15-Jan 1400 hrs 1730 hrs Maryland Ballroom 4 Optimization APA-26 Environmentally Friendly Aircraft Design - Laminar 15-Jan 1400 hrs 1730 hrs Maryland Ballroom A Flow Enabling Technology APA-27 Special Session: 2nd High Lift Prediction Workshop 15-Jan 1400 hrs 1730 hrs Maryland Ballroom 3 (HiLiftPW-2) II APA-28 Special Session: CREATE-AV High Performance 15-Jan 1400 hrs 1730 hrs Maryland Ballroom 5 Computing Multiphysics Applications of Full-Up Air Vehicles III APA-29 Airfoil/Wing/Configuration Aerodynamics 16-Jan 1000 hrs 1230 hrs Maryland Ballroom 5 APA-30 Innovative Aerodynamic Concept and Bio-inspired 16-Jan 1000 hrs 1230 hrs Maryland Ballroom 4 Designs APA-31 Wind Tunnel and Flight Test Aerodynamics 16-Jan 1000 hrs 1230 hrs Maryland Ballroom D APA-32 Active and Passive Flow Control V 16-Jan 1430 hrs 1730 hrs Maryland Ballroom A APA-33 Aerodynamic-Structural Dynamics Interaction 16-Jan 1430 hrs 1730 hrs Maryland Ballroom D APA-34 Characterization of the Physical Environments related 16-Jan 1430 hrs 1730 hrs Maryland Ballroom 4 to Space Launch System (SLS) (Invited) Adaptive Structures AS-1 Optimization and Structural Health Monitoring 15-Jan 1000 hrs 1230 hrs Chesapeake Conference Room D AS-2 Adaptive Actuation 15-Jan 1400 hrs 1730 hrs Chesapeake Conference Room D AS-3 Biomimitic Adaptive Flying Structures 16-Jan 1000 hrs 1230 hrs Chesapeake Conference Room D AS-4 Morphing 16-Jan 1430 hrs 1730 hrs Chesapeake Conference Room D AS-5 Modeling Simulation 17-Jan 0800 hrs 1100 hrs Chesapeake Conference Room D Atmospheric and Space Environments ASE-1 Topics in the Tropospheric Environment 15-Jan 1400 hrs 1730 hrs Chesapeake Conference Room 9 ASE-2 Topics in Space Environments 17-Jan 0800 hrs 1200 hrs Chesapeake Conference Room 9 Design Engineering DE-1 Design Engineering - Design Education 13-Jan 1000 hrs 1230 hrs Chesapeake Conference Room 6 DE-2 Design Engineering - Design Process 13-Jan 1430 hrs 1730 hrs Chesapeake Conference Room 6 DE-3 Design Engineering 14-Jan 1430 hrs 1730 hrs Chesapeake Conference Room D Education EDU-1 Advancing Aerospace Education I 13-Jan 1000 hrs 1230 hrs National Harbor Conference Room 5 EDU-2 Advancing Aerospace Education II: Best practices in 13-Jan 1430 hrs 1730 hrs National Harbor Conference Room 5 Teaching CFD in Undergraduate Aerospace Education

www.aiaa.org/scitech2014 42 #aiaaSciTech IntroSessions at a Glance

Abbreviation Title Date Start Time End Time Location Fluid Dynamics FD-1 Applications of CFD I 13-Jan 1000 hrs 1230 hrs Maryland Ballroom 5 FD-2 Bioinspired Aerodynamics: Experimental 13-Jan 1000 hrs 1230 hrs Woodrow Wilson A FD-3 Hypersonic Boundary Layer Transition I 13-Jan 1000 hrs 1230 hrs Chesapeake Conference Room 8 FD-4 Mesh Adaptation 13-Jan 1000 hrs 1230 hrs Chesapeake Conference Room I FD-5 Solver Technology for Turbulent Flows I 13-Jan 1000 hrs 1230 hrs Chesapeake Conference Room 7 FD-7 Bioinspired Aerodynamics: Numerical 13-Jan 1430 hrs 1730 hrs Maryland Ballroom 5 FD-8 CFD for Turbulent Flows 13-Jan 1430 hrs 1730 hrs Maryland Ballroom D FD-9 Jet Flows 13-Jan 1430 hrs 1730 hrs Maryland Ballroom 6 FD-10 Roughness-Influenced Boundary Layer Transition I 13-Jan 1430 hrs 1730 hrs National Harbor Conference Room 4 FD-11 Solver Technology for Turbulent Flows II 13-Jan 1430 hrs 1730 hrs National Harbor Conference Room 3 FD-12 Turbulence I: Jets and Wakes 13-Jan 1430 hrs 1730 hrs Chesapeake Conference Room 8 FD-13 Wing Aerodynamics 13-Jan 1430 hrs 1730 hrs Maryland Ballroom 2 FD-15 Higher-Order Methods I 14-Jan 1000 hrs 1230 hrs Chesapeake Conference Room 8 FD-16 Hypersonic Boundary Layer Transition II 14-Jan 1000 hrs 1230 hrs Maryland Ballroom 6 FD-17 Roughness-Influenced Boundary Layer Transition II 14-Jan 1000 hrs 1230 hrs Chesapeake Conference Room H FD-18 Shock Boundary Layer Interactions I 14-Jan 1000 hrs 1230 hrs National Harbor Conference Room 4 FD-19 Thermal Environment 14-Jan 1000 hrs 1230 hrs Chesapeake Conference Room G FD-20 Combustion Engines 14-Jan 1430 hrs 1730 hrs Maryland Ballroom 5 FD-21 RANS Turbulence Modeling: Strengths, Weaknesses and 14-Jan 1430 hrs 1730 hrs Chesapeake Conference Room 8 New Approaches FD-22 Turbulence II: Large Eddy Simulations 14-Jan 1430 hrs 1730 hrs National Harbor Conference Room 3 FD-23 Active and Passive Flow Control III 15-Jan 1000 hrs 1230 hrs National Harbor Conference Room 6 FD-24 Higher-Order Methods II 15-Jan 1000 hrs 1230 hrs Maryland Ballroom 5 FD-25 Hypersonic Boundary Layer Receptivity 15-Jan 1000 hrs 1230 hrs Maryland Ballroom 6 FD-26/ Overset Grid Methods 15-Jan 1000 hrs 1230 hrs National Harbor Conference Room 5 MVC-5 FD-27/TP-5 Rarefied Gas Dynamics in Micro- and Nano-Systems 15-Jan 1000 hrs 1230 hrs National Harbor Conference Room 4 FD-28 Flow Control of Bodies and Riblets 15-Jan 1400 hrs 1730 hrs Woodrow Wilson D FD-29 Higher-Order Methods III 15-Jan 1400 hrs 1730 hrs Chesapeake Conference Room 8 FD-30 Shock Interactions and Control 15-Jan 1400 hrs 1730 hrs Maryland Ballroom 6 FD-31 Shock-Dominated Flows 15-Jan 1400 hrs 1730 hrs National Harbor Conference Room 2 FD-32 Transition Open Forum 15-Jan 1400 hrs 1730 hrs National Harbor Conference Room 4 FD-33 Transonic and Supersonic Flows 15-Jan 1400 hrs 1730 hrs Azalea 1 FD-34 Vortex Flows 15-Jan 1400 hrs 1730 hrs National Harbor Conference Room 3 FD-35 Active and Passive Flow Control IV 16-Jan 1000 hrs 1230 hrs Azalea 2 FD-36 Applications of GPUs for CFD 16-Jan 1000 hrs 1230 hrs Azalea 3 FD-37 Boundary Layer Transition 16-Jan 1000 hrs 1230 hrs National Harbor Conference Room 3 FD-38 Shock Boundary Layer Interactions II 16-Jan 1000 hrs 1300 hrs Woodrow Wilson D FD-39 Synthetic Jets 16-Jan 1000 hrs 1230 hrs Maryland Ballroom 6 FD-40 Active and Passive Flow Control VI 16-Jan 1430 hrs 1730 hrs Chesapeake Conference Room 8 FD-41 Applications of CFD II 16-Jan 1430 hrs 1730 hrs Maryland Ballroom 6 FD-42 Boundary Layer Stabilization and Natural Laminar Flow 16-Jan 1430 hrs 1730 hrs Woodrow Wilson D FD-43 Higher-Order Methods IV 16-Jan 1430 hrs 1730 hrs Azalea 1

www.aiaa.org/scitech2014 43 #aiaaSciTech IntroSessions at a Glance

Abbreviation Title Date Start Time End Time Location Fluid Dynamics (continued) FD-44 Wing-Vortex Interactions 16-Jan 1430 hrs 1730 hrs Chesapeake Conference Room 9 FD-45 CFD Methods for Unsteady Flows 17-Jan 0800 hrs 1200 hrs Chesapeake Conference Room G FD-46 Error Estimation and Control 17-Jan 0800 hrs 1200 hrs Azalea 3 FD-47 Other CFD Methods 17-Jan 0800 hrs 1200 hrs Maryland Ballroom 1 FD-48 Reacting Flows (Invited) 17-Jan 0800 hrs 1200 hrs Azalea 1 FD-49 Shear and Slip Flows 17-Jan 0800 hrs 1200 hrs Azalea 2 FD-50 Turbulence III: Models and Simulations 17-Jan 0800 hrs 1200 hrs Chesapeake Conference Room I FD-51 Unsteady Aerodynamics II 17-Jan 0800 hrs 1200 hrs National Harbor Conference Room 10 Green Engineering GEPC-1 Progress in NASA's Environmentally Responsible 13-Jan 1430 hrs 1730 hrs Woodrow Wilson A Aviation Project GEPC-2 Progress Towards N+3 Technologies in NASA's Fixed 14-Jan 1430 hrs 1730 hrs Woodrow Wilson A Wing Project GEPC-3 NASA Aeronautical Sciences Project Overview and 15-Jan 1400 hrs 1730 hrs Woodrow Wilson A Progress GEPC-4 Energy Efficiency for the Future USAF Transport Fleet 16-Jan 1430 hrs 1730 hrs Woodrow Wilson A GEPC-5 Legacy Fleet Fuel Efficiency – Reducing the USAF’s 17-Jan 0800 hrs 1200 hrs Woodrow Wilson A Multi-Billion Dollar Annual Fuel Bill Guidance, Navigation, and Control GNC-1 Adaptive Control 13-Jan 1000 hrs 1230 hrs National Harbor Conference Room 8 GNC-2 Spacecraft Rendezvous and Proximity Operations 13-Jan 1000 hrs 1230 hrs National Harbor Conference Room 7 GNC-3 Mini/Micro Air Vehicles I 13-Jan 1430 hrs 1730 hrs National Harbor Conference Room 7 GNC-4 Onboard Systems Technologies for LOC Prevention & 13-Jan 1430 hrs 1730 hrs National Harbor Conference Room 12 Recovery – Improved Situational Awareness, Guidance, and Control, Session (Invited) I GNC-5 Space Exploration and Transportation 13-Jan 1430 hrs 1730 hrs National Harbor Conference Room 6 GNC-6 Onboard Systems Technologies for LOC Prevention & 14-Jan 1000 hrs 1230 hrs National Harbor Conference Room 8 Recovery – Improved Situational Awareness, Guidance, and Control, Session (Invited) II GNC-7 Spacecraft Navigation 14-Jan 1000 hrs 1230 hrs National Harbor Conference Room 5 GNC-8 Control of Uncertain Systems 14-Jan 1000 hrs 1300 hrs National Harbor Conference Room 3 GNC-9 Aircraft Guidance, Navigation and Control I 14-Jan 1430 hrs 1730 hrs National Harbor Conference Room 7 GNC-10 Novel Navigation, Estimation, and Tracking Methods 14-Jan 1430 hrs 1730 hrs National Harbor Conference Room 8 GNC-11 Validation of Onboard Systems Technologies for LOC 14-Jan 1430 hrs 1730 hrs National Harbor Conference Room 12 Prevention and Recovery, Session (Invited) I GNC-12 Intelligent Control in Aerospace Applications 15-Jan 1000 hrs 1230 hrs National Harbor Conference Room 7 GNC-13 Validation of Onboard Systems Technologies for LOC 15-Jan 1000 hrs 1230 hrs National Harbor Conference Room 8 Prevention and Recovery, Session (Invited) II GNC-14 Aircraft Guidance, Navigation and Control II 15-Jan 1400 hrs 1730 hrs National Harbor Conference Room 7 GNC-15 Multi-Vehicle Coordination and Control 15-Jan 1400 hrs 1730 hrs National Harbor Conference Room 8 GNC-16 Unmanned Autonomous Systems 15-Jan 1400 hrs 1730 hrs National Harbor Conference Room 5 GNC-17 Fault Detection, Isolation and Reconstruction 16-Jan 1000 hrs 1230 hrs National Harbor Conference Room 8 GNC-19 Aerospace Robotics 16-Jan 1430 hrs 1730 hrs National Harbor Conference Room 6 GNC-20 Aircraft Control and Guidance 16-Jan 1430 hrs 1730 hrs National Harbor Conference Room 12

www.aiaa.org/scitech2014 44 #aiaaSciTech IntroSessions at a Glance

Abbreviation Title Date Start Time End Time Location Guidance, Navigation, and Control (continued) GNC-21 Aircraft Guidance, Navigation and Control III 16-Jan 1430 hrs 1730 hrs National Harbor Conference Room 7 GNC-22 Spacecraft Attitude Control 16-Jan 1430 hrs 1730 hrs National Harbor Conference Room 13 GNC-23 Guidance, Navigation, and Control Concepts in Air 17-Jan 0800 hrs 1200 hrs National Harbor Conference Room 15 Traffic Management GNC-24 Mini/Micro Air Vehicles II 17-Jan 0800 hrs 1200 hrs National Harbor Conference Room 7 GNC-25 Missile Guidance, Navigation, and Control 17-Jan 0800 hrs 1200 hrs National Harbor Conference Room 8 Ground Testing GT-1 Experimental Uncertainty in Ground Test Facilities 13-Jan 1000 hrs 1230 hrs National Harbor Conference Room 10 GT-2 NASA's ATP National Force Measurement Project 13-Jan 1430 hrs 1730 hrs Maryland Ballroom B Update (Invited) GT-3 Rapid Prototyping Applications in Ground Testing 13-Jan 1430 hrs 1730 hrs National Harbor Conference Room 10 GT-4 Wind Tunnel Data Corrections 14-Jan 1430 hrs 1730 hrs Maryland Ballroom B GT-5 The Direction and Integration of Experimental Ground 15-Jan 1000 hrs 1230 hrs Maryland Ballroom B Test Capabilities and Computational Methods, Part II (Invited) GT-6 Test Facility and Systems Development I 15-Jan 1400 hrs 1730 hrs Maryland Ballroom D GT-7 Hypersonic Test Techniques with an Emphasis on Heat 16-Jan 1000 hrs 1230 hrs Maryland Ballroom 3 Shield Ablation GT-9 Test Facility and Systems Development II 16-Jan 1430 hrs 1730 hrs Maryland Ballroom 3 GT-11 High Reynolds Number Aerodynamics and Testing 17-Jan 0800 hrs 1200 hrs Maryland Ballroom 3 (Invited) Gas Turbine Engines GTE-1 Turbomachinery I 13-Jan 1000 hrs 1230 hrs Woodrow Wilson D GTE-2 Film Cooling 13-Jan 1430 hrs 1730 hrs Woodrow Wilson D GTE-3 Gas Turbine Combustor I 14-Jan 1000 hrs 1230 hrs Woodrow Wilson D GTE-4 Gas Turbine Combustor II 14-Jan 1430 hrs 1730 hrs Woodrow Wilson D GTE-5 Turbomachinery II 15-Jan 1000 hrs 1230 hrs Woodrow Wilson D GTE-6 Engine Systems I 16-Jan 1000 hrs 1230 hrs Azalea 1 GTE-7 Engine Systems II 16-Jan 1430 hrs 1730 hrs Azalea 2 History HIS-1 Aerospace Archives: All is NOT Lost - Keepers of the 13-Jan 1000 hrs 1230 hrs National Harbor Conference Room 15 Right Stuff HIS-2 History Session: Pioneering Contributions to 13-Jan 1430 hrs 1730 hrs National Harbor Conference Room 15 Aeronautics High Speed Air Breathing Propulsion HSABP-1 Pressure Gain Combustion I 13-Jan 1430 hrs 1730 hrs Chesapeake Conference Room 7 HSABP-2 CFD Analysis of Scramjets I 14-Jan 1430 hrs 1730 hrs Chesapeake Conference Room 7 HSABP-3 Experimental Investigations of Scramjets 15-Jan 1400 hrs 1730 hrs Chesapeake Conference Room 7 HSABP-4 CFD Analysis of Scramjets II 16-Jan 1000 hrs 1230 hrs Chesapeake Conference Room 7 HSABP-5 Pressure Gain Combustion II 16-Jan 1430 hrs 1730 hrs Chesapeake Conference Room 7

www.aiaa.org/scitech2014 45 #aiaaSciTech IntroSessions at a Glance

Abbreviation Title Date Start Time End Time Location Intelligent Systems IS-1 Adaptive and Predictive Systems 15-Jan 1000 hrs 1230 hrs National Harbor Conference Room 15 IS-2 Unmanned Aircraft Sensing and Control 15-Jan 1400 hrs 1730 hrs National Harbor Conference Room 15 IS-3 Applications of Unmanned Aerial Systems 16-Jan 1000 hrs 1230 hrs National Harbor Conference Room 15 IS-4 Intelligent Learning and Decision Making 16-Jan 1430 hrs 1730 hrs National Harbor Conference Room 15 International Student Conference ISC-1 International Student Conference-Master's Division 13-Jan 0930 hrs 1300 hrs National Harbor Conference Room 6 ISC-2 International Student Conference-Undergraduate 13-Jan 0930 hrs 1300 hrs National Harbor Conference Room 2 Division ISC-3 International Student Conference-Team Division 13-Jan 1000 hrs 1230 hrs National Harbor Conference Room 4 ISC-4 International Student Conference-Community 13-Jan 1430 hrs 1730 hrs Potomac Ballroom 3 Outreach Division Materials MAT-1 Nanostructured Materials I 13-Jan 1000 hrs 1230 hrs Chesapeake Conference Room A MAT-2 Integrated Computational Materials Engineering I 14-Jan 1000 hrs 1230 hrs Chesapeake Conference Room D MAT-3 Nanostructured Materials II 14-Jan 1000 hrs 1230 hrs Chesapeake Conference Room A MAT-4 Advanced Composites & Fabrics 14-Jan 1430 hrs 1730 hrs Chesapeake Conference Room A MAT-5 Integrated Computational Materials Engineering II 15-Jan 1000 hrs 1230 hrs Chesapeake Conference Room A MAT-6 Integrated Computational Materials Engineering III 15-Jan 1400 hrs 1730 hrs Chesapeake Conference Room A MAT-7 Multiscale Modeling of Materials I 16-Jan 1000 hrs 1230 hrs Chesapeake Conference Room A MAT-8 Material Testing & Characterization 16-Jan 1430 hrs 1730 hrs Chesapeake Conference Room B MAT-9 Multiscale Modeling of Materials II 16-Jan 1430 hrs 1730 hrs Chesapeake Conference Room A Multidisciplinary Design Optimization MDO-1 Optimization Methods and Algorithms I 13-Jan 1000 hrs 1230 hrs Chesapeake Conference Room 4 MDO-2 Aerodynamic and Aircraft Optimization 13-Jan 1430 hrs 1730 hrs Chesapeake Conference Room 4 MDO-3 Aeroelastic and Aero-Structures Optimization 14-Jan 1000 hrs 1230 hrs Chesapeake Conference Room 4 MDO-4 Structural and Topology Optimization 14-Jan 1430 hrs 1730 hrs Chesapeake Conference Room 4 MDO-5 Optimization Methods and Algorithms II 15-Jan 1000 hrs 1230 hrs Chesapeake Conference Room 4 MDO-6 Optimization Framework and Applications 15-Jan 1400 hrs 1730 hrs Chesapeake Conference Room 4 MDO-7 Aerodynamic Optimization 16-Jan 1000 hrs 1230 hrs Chesapeake Conference Room 4 MDO-8 Optimization Applications 16-Jan 1430 hrs 1730 hrs Chesapeake Conference Room 4 MDO-9 Optimization Methods and Algorithms III 17-Jan 0800 hrs 1100 hrs Chesapeake Conference Room 6 Modeling and Simulation Technologies MST-1 Applications of Modeling and Simulation 14-Jan 1000 hrs 1230 hrs National Harbor Conference Room 6 MST-2 Modeling and Simulation Tools and Technologies 14-Jan 1430 hrs 1730 hrs National Harbor Conference Room 6 MST-3 Air Traffic Management/Human Factors 15-Jan 1000 hrs 1230 hrs National Harbor Conference Room 12 MST-4 Simulation Requirements for LOC Prevention & 15-Jan 1400 hrs 1730 hrs National Harbor Conference Room 6 Recovery Training (Invited) MST-6 Modeling and Simulation of Uninhabited Aircraft 16-Jan 1430 hrs 1730 hrs National Harbor Conference Room 14 Systems (UAS) MST-7 Modeling and Simulation of Space Systems 17-Jan 0800 hrs 1200 hrs National Harbor Conference Room 14

www.aiaa.org/scitech2014 46 #aiaaSciTech IntroSessions at a Glance

Abbreviation Title Date Start Time End Time Location Meshing, Visualization, and Computational Environments MVC-1 Meshing Technology and Application 13-Jan 1000 hrs 1230 hrs Chesapeake Conference Room 9 MVC-2 Integrated Computational Environments 13-Jan 1430 hrs 1730 hrs Chesapeake Conference Room 9 MVC-3 Geometry Preparation and Grid Quality Assessment 14-Jan 1000 hrs 1230 hrs Chesapeake Conference Room 9 MVC-4 Current Status and Future Trends of Integrated 14-Jan 1430 hrs 1730 hrs Chesapeake Conference Room 9 Computational Environments Non-Deterministic Approaches NDA-1 Model Validation and Uncertainty Quantification 13-Jan 1000 hrs 1230 hrs Chesapeake Conference Room 5 NDA-2 Uncertainty Quantification Methods 13-Jan 1430 hrs 1730 hrs Chesapeake Conference Room 5 NDA-3 Probabilistic Methods for Diagnostics & Prognostics 14-Jan 1000 hrs 1230 hrs Chesapeake Conference Room 5 NDA-4 Reliability 14-Jan 1430 hrs 1730 hrs Chesapeake Conference Room 5 NDA-5 Validation & Uncertainty Quantification Applications 15-Jan 1000 hrs 1230 hrs Chesapeake Conference Room 5 NDA-6 Nondeterministic Methods for Design 15-Jan 1400 hrs 1730 hrs Chesapeake Conference Room 5 NDA-7 Nondeterministic Methods 16-Jan 1000 hrs 1230 hrs Chesapeake Conference Room 5 NDA-8 NASA Multidisciplinary UQ Challenge I 16-Jan 1430 hrs 1730 hrs Chesapeake Conference Room 5 NDA-9 NASA Multidisciplinary UQ Challenge II 17-Jan 0800 hrs 1100 hrs Chesapeake Conference Room 5 Space Operations OPS-1 Space Operations & Support 13-Jan 1430 hrs 1730 hrs National Harbor Conference Room 8 Propellants and Combustion PC-1 Fuels and Combustion Kinetics 13-Jan 1000 hrs 1230 hrs Chesapeake Conference Room G PC-2 Gas Turbine Combustion 13-Jan 1000 hrs 1230 hrs Chesapeake Conference Room H PC-3 Rockets and Airbreathing Propulsion I 13-Jan 1000 hrs 1230 hrs Maryland Ballroom 6 PC-4 Jet Fuel Surrogate Models and Kinetics (Invited) 13-Jan 1430 hrs 1730 hrs Chesapeake Conference Room I PC-5 Rockets and Airbreathing Propulsion II 13-Jan 1430 hrs 1730 hrs Chesapeake Conference Room G PC-6 Turbulent Flames I 13-Jan 1430 hrs 1730 hrs Chesapeake Conference Room H PC-7 Frontiers of Combustion Research (Invited) 14-Jan 1000 hrs 1230 hrs National Harbor Conference Room 2 PC-8 Heterogeneous Combustion and Propellants 14-Jan 1430 hrs 1730 hrs Chesapeake Conference Room G PC-9 Laminar Flames 14-Jan 1430 hrs 1730 hrs Chesapeake Conference Room I PC-10 Turbulent Flames II 14-Jan 1430 hrs 1730 hrs Chesapeake Conference Room H PC-12 Advanced Combustion Concepts and New Technologies 15-Jan 1000 hrs 1230 hrs National Harbor Conference Room 2 PC-13 Kinetic Model Reduction 15-Jan 1000 hrs 1230 hrs Chesapeake Conference Room H PC-14 Turbulent Combustion Modeling I 15-Jan 1000 hrs 1230 hrs Chesapeake Conference Room G PC-15 Detonation and PDEs I 15-Jan 1400 hrs 1730 hrs Chesapeake Conference Room H PC-16 Spray and Droplet Combustion I 15-Jan 1400 hrs 1730 hrs Chesapeake Conference Room G PC-17 Turbulent Combustion Modeling II 15-Jan 1400 hrs 1730 hrs Chesapeake Conference Room I PC-18 Plasma-Assisted Combustion II 16-Jan 1000 hrs 1230 hrs Chesapeake Conference Room G PC-19 Spray and Droplet Combustion II 16-Jan 1000 hrs 1230 hrs Chesapeake Conference Room H PC-20 Turbulent Combustion Modeling III 16-Jan 1000 hrs 1230 hrs National Harbor Conference Room 2 PC-21/ Combustion Diagnostics II 16-Jan 1430 hrs 1730 hrs Chesapeake Conference Room G AMT-11 PC-22 Plasma-Assisted Combustion III (Invited) 16-Jan 1430 hrs 1730 hrs Chesapeake Conference Room H PC-23 Detonation and PDEs II 17-Jan 0800 hrs 1200 hrs Chesapeake Conference Room H

www.aiaa.org/scitech2014 47 #aiaaSciTech IntroSessions at a Glance

Abbreviation Title Date Start Time End Time Location Plasmadynamics and Lasers PDL-1 Electric Propulsion/Laser Applications of Plasmas 13-Jan 1000 hrs 1230 hrs Maryland Ballroom 4 PDL-2 Plasma-Actuators and Flow Control I 13-Jan 1000 hrs 1230 hrs Maryland Ballroom 1 PDL-3 AeroOptics 13-Jan 1430 hrs 1730 hrs Azalea 3 PDL-4 Plasma-Actuators and Flow Control II 13-Jan 1430 hrs 1730 hrs Maryland Ballroom 1 PDL-5 Plasma-Actuators and Flow Control III 14-Jan 1000 hrs 1230 hrs Azalea 3 PDL-6 Plasma-Assisted Combustion I 14-Jan 1430 hrs 1730 hrs Azalea 3 PDL-7 Plasma Discharge Structure 14-Jan 1430 hrs 1730 hrs Maryland Ballroom 6 PDL-8 Magnetohydrodynamics/Microwave Plasmas 15-Jan 1000 hrs 1230 hrs Azalea 3 PDL-9 Non-Equilibrium Effects in Discharges 15-Jan 1400 hrs 1730 hrs Azalea 3 PDL-10 Plasma Discharge Modeling 16-Jan 1000 hrs 1230 hrs Chesapeake Conference Room 9 PDL-11 Plasma Diagnostics 16-Jan 1430 hrs 1730 hrs Maryland Ballroom 5 Society and Aerospace Technology SAT-1 Space and Society: Social Impacts of Air and Space 14-Jan 1000 hrs 1230 hrs National Harbor Conference Room 15 Technologies SAT-2 Space and Society: Social Dimensions of Space 14-Jan 1430 hrs 1730 hrs National Harbor Conference Room 15 Exploration and Exploitation Spacecraft Structures SCS-1 Materials for Gossamer Systems 14-Jan 1430 hrs 1730 hrs Chesapeake Conference Room 6 SCS-2 Solar Sails and Tensioned Membranes 15-Jan 1000 hrs 1230 hrs Chesapeake Conference Room 6 SCS-3 Packaging & Deployment of Gossamer Systems 15-Jan 1400 hrs 1730 hrs Chesapeake Conference Room 6 SCS-4 Testing of Large, Ultra-Lightweight Spacecraft 16-Jan 1000 hrs 1230 hrs Chesapeake Conference Room 6 SCS-5 Mechanics, Dynamics, & Control of Gossamer Systems 16-Jan 1430 hrs 1730 hrs Chesapeake Conference Room 6 SCS-6 Design, Analysis, & Test of Gossamer Systems 17-Jan 0800 hrs 1100 hrs Chesapeake Conference Room A Structural Dynamics SD-1 Computational Aeroelasticity ROM I 13-Jan 1000 hrs 1230 hrs Chesapeake Conference Room C SD-2 Energy Harvesting, Damping and Vibration 13-Jan 1000 hrs 1230 hrs Chesapeake Conference Room B Suppression SD-3 Aircraft Dynamics and Vibration 13-Jan 1430 hrs 1730 hrs Chesapeake Conference Room B SD-4 Computational Aeroelasticity I 13-Jan 1430 hrs 1730 hrs Chesapeake Conference Room C SD-5 Beam, Plate, Cable Dynamics 14-Jan 1000 hrs 1230 hrs Chesapeake Conference Room B SD-6 Computational Aeroelasticity ROM II 14-Jan 1000 hrs 1230 hrs Chesapeake Conference Room C SD-7 Computational Aeroelasticity II 14-Jan 1430 hrs 1730 hrs Chesapeake Conference Room C SD-8 Nonlinear Dynamics and Aeroelasticity 14-Jan 1430 hrs 1730 hrs Chesapeake Conference Room B SD-9 Adaptive Aeroelastic Wing Shaping Control I 15-Jan 1000 hrs 1230 hrs Chesapeake Conference Room C SD-10 Very Flexible Aircraft 15-Jan 1000 hrs 1230 hrs Chesapeake Conference Room B SD-11 Adaptive Aeroelastic Wing Shaping Control II 15-Jan 1400 hrs 1730 hrs Chesapeake Conference Room C SD-12 Aircraft Design and Nonlinear Dynamics 16-Jan 1000 hrs 1230 hrs Chesapeake Conference Room B SD-13 Limit Cycle Oscillations (LCO) & Aircraft Flutter 16-Jan 1000 hrs 1230 hrs Chesapeake Conference Room C SD-14 Rotorcraft 16-Jan 1430 hrs 1730 hrs Chesapeake Conference Room C SD-15 Nonlinear Dynamics and Flapping Flight 17-Jan 0800 hrs 1100 hrs Chesapeake Conference Room C SD-16 Space & Launch Vehicle Dynamics 17-Jan 0800 hrs 1100 hrs Chesapeake Conference Room B

www.aiaa.org/scitech2014 48 #aiaaSciTech IntroSessions at a Glance

Abbreviation Title Date Start Time End Time Location Systems Engineering SE-1 Systems Engineering 14-Jan 1430 hrs 1730 hrs National Harbor Conference Room 14 Software Systems SOF-1 Cybersecurity in Space Systems Panel 14-Jan 1430 hrs 1730 hrs National Harbor Conference Room 2 SOF-3 Software Systems 15-Jan 1400 hrs 1730 hrs National Harbor Conference Room 14 Space Resources SRE-1 In-Situ Resources: Identification and Manipulation 13-Jan 1430 hrs 1730 hrs National Harbor Conference Room 14 SRE-2 Resource Enabled Mission Concepts 14-Jan 1000 hrs 1230 hrs National Harbor Conference Room 14 SRE-3 Environmental Factors in Extraterrestrial Systems 14-Jan 1430 hrs 1730 hrs National Harbor Conference Room 4 Structures STR-1 Composite Micromechanics 13-Jan 1000 hrs 1230 hrs Chesapeake Conference Room D STR-2 Beams & Plates 13-Jan 1000 hrs 1230 hrs Chesapeake Conference Room F STR-3 Buckling and Structural Instability 13-Jan 1000 hrs 1230 hrs Chesapeake Conference Room E STR-4 Aeroelastic Analysis 13-Jan 1430 hrs 1730 hrs Chesapeake Conference Room E STR-5 Special Session on Open Source Software 13-Jan 1430 hrs 1730 hrs Chesapeake Conference Room D STR-6 Space Structures 13-Jan 1430 hrs 1730 hrs Chesapeake Conference Room F STR-7 Sandwich Structures 14-Jan 1000 hrs 1230 hrs Chesapeake Conference Room F STR-8 Application of Viscoelasticity and Viscoelastic Materials 14-Jan 1000 hrs 1230 hrs Chesapeake Conference Room E STR-9 Impact Mechanics and Structural Survivability 14-Jan 1430 hrs 1730 hrs Chesapeake Conference Room F STR-10 Structures Under Thermal Environment 14-Jan 1430 hrs 1730 hrs Chesapeake Conference Room E STR-11 Shell Bucking-Charles Rankin Special Session I 15-Jan 1000 hrs 1230 hrs Chesapeake Conference Room E STR-12 Advances in Design and Analysis of Structures 15-Jan 1000 hrs 1230 hrs Chesapeake Conference Room F STR-13 Shell Bucking-Charles Rankin Special Session II 15-Jan 1400 hrs 1730 hrs Chesapeake Conference Room E STR-14 Advances in Fatigue Analysis 15-Jan 1400 hrs 1730 hrs Chesapeake Conference Room B STR-15 Advanced Structures 15-Jan 1400 hrs 1730 hrs Chesapeake Conference Room F STR-16 Composite Mechanics Under Dynamic Load 16-Jan 1000 hrs 1230 hrs Chesapeake Conference Room E STR-17 Load Analysis and Design Process 16-Jan 1000 hrs 1230 hrs Chesapeake Conference Room F STR-18 Special Session - Composite Laminate Optimization 16-Jan 1430 hrs 1730 hrs Chesapeake Conference Room E STR-19 Advances in Fracture Mechanics 16-Jan 1430 hrs 1730 hrs Chesapeake Conference Room F STR-20 Damage Mechanics/Damage Tolerance 17-Jan 0800 hrs 1100 hrs Chesapeake Conference Room F STR-21 Structural Joints 17-Jan 0800 hrs 1100 hrs Chesapeake Conference Room E Survivability SUR-1 Air and Space Survivability 13-Jan 1430 hrs 1730 hrs Chesapeake Conference Room A Terrestrial Energy TES-1 Cutting Edge Energy Systems and Fuels 15-Jan 1000 hrs 1230 hrs Azalea 2 TES-2 Advances in Renewable Energy and Efficiency 15-Jan 1400 hrs 1730 hrs Maryland Ballroom B TES-3 Applications of Nanomaterials for Energy Storage 16-Jan 1000 hrs 1230 hrs Maryland Ballroom A TES-4 Advances in Combustion I 16-Jan 1430 hrs 1730 hrs Maryland Ballroom B TES-5 Advances in Combustion II 17-Jan 0800 hrs 1200 hrs Maryland Ballroom B

www.aiaa.org/scitech2014 49 #aiaaSciTech IntroSessions at a Glance

Abbreviation Title Date Start Time End Time Location Thermophysics TP-1 Aerothermodynamics I 14-Jan 1000 hrs 1230 hrs National Harbor Conference Room 11 TP-2 Thermal Protection Systems I 14-Jan 1000 hrs 1230 hrs National Harbor Conference Room 10 TP-3 Direct Simulation Monte Carlo Methods I 14-Jan 1430 hrs 1730 hrs National Harbor Conference Room 11 TP-4 Thermal Protection Systems II 14-Jan 1430 hrs 1730 hrs National Harbor Conference Room 10 TP-6 Heat Transfer 15-Jan 1000 hrs 1230 hrs National Harbor Conference Room 11 TP-7 Non-Equilibrium Flows I 15-Jan 1000 hrs 1230 hrs National Harbor Conference Room 10 TP-8 Cryogenics 15-Jan 1400 hrs 1730 hrs National Harbor Conference Room 11 TP-9 Non-Equilibrium Flows II 15-Jan 1400 hrs 1730 hrs National Harbor Conference Room 10 TP-10 Ablation I 16-Jan 1000 hrs 1230 hrs National Harbor Conference Room 11 TP-11 Direct Simulation Monte Carlo Methods II 16-Jan 1000 hrs 1230 hrs National Harbor Conference Room 10 TP-12 Ablation II 16-Jan 1430 hrs 1730 hrs National Harbor Conference Room 11 TP-13 Aerothermodynamics II 16-Jan 1430 hrs 1730 hrs National Harbor Conference Room 10 Wind Energy WE-1 Wind Turbine Airfoil Design and Analysis 13-Jan 1000 hrs 1230 hrs Woodrow Wilson C WE-2 Wind Turbine Blade Materials and Manufacturing 13-Jan 1000 hrs 1230 hrs Woodrow Wilson B WE-3 Blade and Turbine Design I 13-Jan 1430 hrs 1730 hrs National Harbor Conference Room 2 WE-4 Offshore Wind Energy Systems 13-Jan 1430 hrs 1730 hrs Woodrow Wilson B WE-5 Wind Turbine Aeroelasticity and Structural Dynamics I 14-Jan 1000 hrs 1230 hrs Woodrow Wilson C WE-6 Wind Farm and Turbine-Wake Interaction I 14-Jan 1430 hrs 1730 hrs Woodrow Wilson B WE-7 Wind Turbine Aeroelasticity and Structural Dynamics 14-Jan 1430 hrs 1730 hrs Woodrow Wilson C II WE-8 Atmospheric Physics and Inflow 15-Jan 1000 hrs 1230 hrs Woodrow Wilson C WE-9 Wind Turbine Loads, Dynamics, and Control I 15-Jan 1000 hrs 1230 hrs Woodrow Wilson B WE-10 Blade and Turbine Design II 15-Jan 1400 hrs 1730 hrs Woodrow Wilson B WE-11 Wind Farm and Turbine-Wake Interaction II 15-Jan 1400 hrs 1730 hrs Woodrow Wilson C WE-12 Wind Turbine Aeroelastics 16-Jan 1000 hrs 1230 hrs Woodrow Wilson B WE-13 Wind Turbine Loads, Dynamics, and Control II 16-Jan 1000 hrs 1230 hrs Woodrow Wilson C WE-14 Wind Turbine Monitoring and Performance 16-Jan 1430 hrs 1730 hrs Woodrow Wilson C

www.aiaa.org/scitech2014 50 #aiaaSciTech Monday Monday, 13 January 2014 1-SB-1 Monday Morning Speakers’ Brieﬁng Session Rooms 0730 - 0800 hrs Monday, 13 January 2014 2-PLNRY-1 Monday Morning Opening Keynote and Plenary Panel Potomac Ballroom A&B 0800 - 0930 hrs Keynote The Societal Importance of Federal R&D Investments The Honorable Chaka Fattah Congressman, 2nd District, Pennsylvania U.S. House of Representatives

Plenary Panel: R&D Policy Implications and Investments Moderator: Robert Braun, David and Andrew Lewis Professor of Space Technology, Georgia Institute of Technology Panelists: Dr. Michael Grifﬁn Dr. Michael Gazarik Dr. Arati Prabhakar Chairman and CEO Associate Administrator, Space Technology Mission Directorate Director Schafer Corporation NASA Headquarters DARPA AIAA President

Monday, 13 January 2014 51 3-ISC-1 International Student Conference - Master’s Division National Harbor Conf Rm 6 Chaired by: J. CORBETS 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs 1230 hrs AIAA-2014-0005 AIAA-2014-0006 AIAA-2014-0007 AIAA-2014-0008 AIAA-2014-0009 AIAA-2014-0010 Oral Presentation Wireless Magneto-Elastic Improved Mean Flow Solution The Development of a Two-Dimensional Weight Wing-flapping and abdomen Guaranteed Globally Optimal YPSE Exhibition - Forward Torque Sensor System for Solid Rocket Motors Hardware-in-the-Loop Attitude Function Development Using actuation optimization for continuous Reinforcement Flight Capability of a 500- G. Raghunath, A. Flatau, University A. Fist, J. Majdalani, University Determination and Control ZFEM hovering in the butterfly Idea Learning gram Cycloidal-Rotor Micro of Maryland, College Park, College of Tennessee Space Institute, Simulator for IlliniSat-2 A. Baines, H. Millwater, University of leuconoe H. Bijl, E. Van Kampen, Q. Chu, Air Vehicle Park, MD Tullahoma, TN P. Haddox, University of Illinois, Texas, San Antonio, San Antonio, TX T. Wilson, R. Albertani, Oregon State J. Mulder, Delft University of E. Shrestha, University of Maryland, Urbana-Champaign, Urbana, IL University, Corvallis, OR Technology, Delft, The Netherlands College Park, College Park, MD Monday, 13 January 2014 4-ISC-2 International Student Conference - Undergraduate Division National Harbor Conf Rm 2 Chaired by: C. TAVARES, The Boeing Company 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs 1230 hrs AIAA-2014-0011 AIAA-2014-0012 AIAA-2014-0013 AIAA-2014-0014 AIAA-2014-0015 AIAA-2014-0016 AIAA-2014-0017 Graphene-Silicon Composite A Preliminary Study of Three- Exploration of Emissions High Fidelity Simulation of a Thermophoretic Force A Hybrid Tricopter/Flying- Experimental Characterization Lithium-Ion Batteries for Micro Dimensional Turbulent Flow Modeling for a General Nonlinear Aircraft Measurements using a nano- Wing VTOL UAV of a Fuel Cell Hybrid Electrical Air Vehicles over Vortex Generators with a Aviation Airport A. Azocar, J. Valasek, Texas A&M Newton Thrust Stand S. Carlson, Brigham Young UAV Propulsion System S. Wingate, University of Maryland, Plenoptic Camera D. Katsaduros, M. Prall, M. Johnson, University, College Station, TX A. Ventura, University of Colorado, University, Provo, UT A. Gong, University of Sydney, College Park, College Park, MD L. McManus, Auburn University, Purdue University, West Lafayette, IN Colorado Springs, Colorado Springs, CO Sydney, Australia Auburn, AL Monday, 13 January 2014 5-NW-1 Monday Morning Networking Coffee Break Foyer 0930 - 1000 hrs Monday, 13 January 2014 6-AA-1 Airframe Noise and Sound Propagation Azalea 3 Chaired by: C. BURLEY, NASA-Langley Research Center 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2014-0018 AIAA-2014-0019 AIAA-2014-0020 AIAA-2014-0021 AIAA-2014-0022 Identification and Localization Morphing Flap Concept to Reduce Experimental aeroacoustics of Comparison of Aerodynamic A Time-Domain Simulation of Airfoil Noise Sources at Low the Flap Side Edge Noise for a two-strut, two-wheel landing Noise Propagation Techniques for Comparison with the ANSI Angles of Attack Aircraft Wing Slotted Flaps gear in a propeller wake M. Rumpfkeil, University of Dayton, Impedance Measurement M. Jiang, X. Li, W. Tong, Beihang Y. Tani, Y. Yamashita, K. Miyazaki, R. Chekiri, P. Lavoie, University Dayton, OH; D. Robertson, University G. Ke, Z. Zheng, University of University, Beijing, China S. Aso, Kyushu University, Fukuoka, of Toronto, Toronto, Canada; W. of Dayton Research Institute, Kansas, Lawrence, Lawrence, KS Japan; H. Ura, T. Ito, Japan Richarz, Aercoustics Engineering, Dayton, OH Aerospace Exploration Agency Ltd., Toronto, Canada (JAXA), Chofu, Japan Monday, 13 January 2014 7-ACD-1 Aircraft Design Methodologies Azalea 1 Chaired by: H. JIMENEZ, Georgia Institute of Technology 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2014-0023 AIAA-2014-0024 AIAA-2014-0025 AIAA-2014-0026 Conceptual Wing Design Allocating Section Thickness Aeroelastic Modeling of the A Semi-Analytical Weight Methodology for Aircraft with and Camber for Transonic X-56A Using a Rapid Model Estimation Method for Oval Hybrid Laminar Flow Control Wing Design Generator for Conceptual Design Fuselages in Conventional and K. Risse, E. Stumpf, RWTH Aachen C. Kady, T. Takahashi, Arizona State D. Bryson, E. Alyanak, Air Force Novel Aircraft University, Aachen, Germany; G. University, Tempe, AZ Research Laboratory, Wright- K. Schmidt, R. Vos, Delft University Schrauf, Airbus, Bremen, Germany Patterson AFB, OH of Technology, Delft, The Netherlands 52 Monday, 13 January 2014 8-ACD-2 Aircraft Design Studies Azalea 2 Chaired by: W. ANEMAAT, DARcorporation 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2014-0027 AIAA-2014-0028 AIAA-2014-0029 AIAA-2014-0030 AIAA-2014-0031 Preliminary Design of a Heavy Conceptual Design Study on LH2 Lighter-Than-Air Stationary Conceptual Design of a N+1 Take-off and landing using Short- and Medium-Haul Fueled Supersonic Transport Platform Concept Transonic Executive Jet ground based power - landing Turboprop-Powered Passenger considering Performance and C. Bil, J. Karnadi, RMIT University, N. Mora, N. Heitzman, S. Scoville, T. simulations using multibody Aircraft Environmental Impacts Melbourne, Australia Takahashi, Arizona State University, dynamics M. Iwanizki, N. Randt, S. Sartorius, T. Yuhara, K. Rinoie, University of Tempe, AZ P. Wu, M. Voskuijl, M. Van Tooren, Technical University of Munich, Tokyo, Tokyo, Japan; Y. Makino, Japan Delft University of Technology, Delft, Munich, Germany Aerospace Exploration Agency (JAXA), The Netherlands Tokyo, Japan Monday, 13 January 2014 9-AFM-1 Flight Dynamics and Handling Qualities I National Harbor Conf Rm 12 Chaired by: T. LAVIN, Sandia National Laboratories and M. BOLENDER, AFRL/RBCA 1000 hrs 1030 hrs 1100 hrs AIAA-2014-0032 AIAA-2014-0033 AIAA-2014-0034 Flight Testing of a Subscale Flight Testing Small UAVs Autonomous vertical landing Aeroservoelastic Aircraft for Aerodynamic Parameter on a marine vessel J. Ouellette, M. Patil, C. Woolsey, Estimation P. Nuthi, K. Subbarao, University of Virginia Polytechnic Institute and A. Chase, R. McDonald, California Texas, Arlington, Arlington, TX State University, Blacksburg, VA Polytechnic State University, San Luis Obispo, CA Monday, 13 January 2014 10-AFM-2 LOC Prevention and Recovery (Invited) National Harbor Conf Rm 13 Chaired by: K. SHWEYK, Boeing Engineering Operations & Technology 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2014-0035 Oral Presentation (Invited) AIAA-2014-0036 AIAA-2014-0037 Advanced Modeling and Integrated High-Fidelity Piloted Simulation Evaluation of Flight Test of Adaptive RHO Uncertainty Quantification for Modeling and Simulation a Model-Predictive Automatic Controller for Flying Qualities Flight Dynamics (VSST1-7) Development for LOC Research Recovery System to Prevent Specification/Protection and Interim Results and Challenges G. Shah, K. Cunningham, J. Foster, Vehicle Loss of Control on SAFE-Cue Integration D. Hyde, F. Brown, K. Shweyk, The NASA Langley Research Center, Approach N. Richards, R. Adams, Barron Boeing Company, Huntington Beach, Hampton, VA J. Litt, NASA Glenn Research Center, Associates, Inc., Charlottesville, VA; CA; G. Shah, NASA Langley Research Cleveland, OH; Y. Liu, N&R Engineering, D. Klyde, Systems Technology, Inc., Center, Hampton, VA Inc., Parma Heights, OH; T. Sowers, Hawthorne, CA; B. Cogan, NASA Vantage Partners, LLC, Cleveland, OH; Dryden Flight Research Center, A. Owen, Self, Middleburg Heights, OH; Edwards, CA T. Guo, NASA Glenn Research Center, Cleveland, OH Monday, 13 January 2014 11-APA-1 Low Speed Low Reynolds Number Aerodynamics I National Harbor Conf Rm 3 Chaired by: A. JONES, University of Maryland and M. CHANG, Lockheed Martin Aeronautics 1000 hrs 1030 hrs 1100 hrs AIAA-2014-0038 AIAA-2014-0039 AIAA-2014-0040 Wake Characteristics of a 2D Comparison of Computational Analysis of the Flow past Spanwise Tensioned Membrane Approaches for Rapid Airfoils with Gurney Flaps at

53 with Aerodynamic Loading Aerodynamic Assessment of Low Reynolds Numbers Z. Zhang, A. Wrist, J. Hubner, Small UAVs D. Mateescu, A. Panahi, V. Roy, University of Alabama, Tuscaloosa, T. Shafer, Naval Air Systems Command, McGill University, Montréal, Canada Tuscaloosa, AL; L. Ukeiley, University Patuxent River, MD; S. Viken, N. of Florida, Gainesville, Gainesville, FL Favaregh, NASA Langley Research Center, Hampton, VA; C. Zeune, Air Force Research Laboratory, Wright- Patterson AFB, OH; N. Williams, Defence Technology Agency, Auckland, New Zealand; J. Dansie, Australian National University, Melbourne, Australia Monday, 13 January 2014 12-APA-2 Simulation of Rotor in Hover (Invited) I Maryland Ballroom D Chaired by: N. HARIHARAN, CREATE-AV and T. EGOLF, Sikorsky Aircraft Corporation 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2014-0041 AIAA-2014-0042 AIAA-2014-0043 AIAA-2014-0044 AIAA-2014-0045 Simulation of Rotor in Hover: Assessment of Rotor Evaluating Tail Rotor Tip S-76 Rotor Hover Prediction OVERTURNS Simulation of Current State, Challenges and Aerodynamic Performances in Shapes using Computational Using U2NCLE Solver S-76 Rotor in Hover Standardized Evaluation Hover Using an Unstructured Fluid Dynamics C. Sheng, Q. Zhao, J. Wang, J. Baeder, S. Medida, T. Kalra, N. Hariharan, HPCMP CREATE-AV, Mixed Mesh Method G. Barakos, University of Liverpool, University of Toledo, Toledo, OH University of Maryland, College Park, Lorton, VA; T. Egolf, Sikorsky Aircraft M. Jung, J. Hwang, O. Kwon, Korea Liverpool, United Kingdom College Park, MD Corporation, Stratford, CT; L. Sankar, Advanced Institute of Science and Georgia Institute of Technology, Technology, Daejeon, South Korea Atlanta, GA Monday, 13 January 2014 13-APA-3 Unsteady Aerodynamics I Maryland Ballroom 3 Chaired by: J. DEBONIS, NASA Glenn Research Center and M. OL, Air Force Reseach Laboratory 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2014-0046 AIAA-2014-0047 AIAA-2014-0048 AIAA-2014-0049 On the use of Zonal Immersed Sampling Strategies for Validation of CFD Models For Unsteady Aerodynamic Boundary Conditions on a high Reduced-Order Modeling Simulating a Maneuvering Characteristics of Cambered Reynolds number afterbody flow of Nonlinear and Unsteady X-31 with Flight Test Data Four-digit NACA Airfoils at Low with a serrated skirt using ZDES Aerodynamics M. Ghoreyshi, A. Jirasek, R. Reynolds Number L. Mochel, P. Weiss, S. Deck, ONERA, M. Ghoreyshi, R. Cummings, A. Cummings, U.S. Air Force Academy, T. Ikeda, Japan Aerospace Exploration Meudon, France Lofthouse, U.S. Air Force Academy, Colorado Springs, CO Agency (JAXA), Chofu, Japan; D. Colorado Springs, CO Fujimoto, A. Inasawa, M. Asai, Tokyo Metropolitan University, Hino, Japan Monday, 13 January 2014 14-APA-4 Vortical/Vortex Flow Maryland Ballroom B Chaired by: A. MCCOMAS, TLG Aerospace 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2014-0050 AIAA-2014-0051 AIAA-2014-0052 AIAA-2014-0053 AIAA-2014-0054 Experimental results for Experimental Investigation of Simulations of Vortex Asymmetry An Analysis of the Unsteady Virtual Force Measurement of vortex dominated flow at a Vortex Asymmetry on a Conical on a Conical Forebody at High Wake Behind a Circular POD Modes for A Flat Plate in Lambda-wing with a round Forebody at High Angles of Angles of Incidence Cylinder using Lagrangian Low Reynolds Number Flows leading edge in steady flow Incidence J. Taligoski, A. Uzun, R. Kumar, Florida Coherent Structures Z. Liang, H. Dong, University S. Wiggen, German Aerospace J. Taligoski, E. Fernandez, R. Kumar, State University, Tallahassee, FL M. Rockwood, J. Morrida, M. Green, of Virginia, Charlottesville, Center (DLR), Göttingen, Germany Florida State University, Tallahassee, FL Syracuse University, Syracuse, NY Charlottesville, VA 54 Monday, 13 January 2014 15-APA-5 Weapons Aerodynamics and Store Separation I Maryland Ballroom A Chaired by: C. ROSEMA, US Army AMRDEC and B. MCGRATH, JHU/Applied Physics Laboratory 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2014-0055 AIAA-2014-0056 AIAA-2014-0057 AIAA-2014-0058 AIAA-2014-0059 Nonlinear Aerodynamic Fluidic control of a 155 mm Unsteady Aerodynamic Turbulence Model Effects Numerical Experiments on Predictions of Aircraft and spin-stabilized projectile using Simulations of a Finned on Cold-Gas Lateral Jet Finned Bodies Missiles Employing Trailing- Coanda effect Projectile at a Supersonic Interaction in a Supersonic S. Silton, Army Research Laboratory, Edge Flaps M. Zeidler, Nexter Munitions, Speed with Jet Interaction Crossflow Aberdeen Proving Ground, MD D. Lesieutre, Nielsen Engineering & Bourges, France; E. Garnier, ONERA, J. Sahu, Army Research Laboratory, J. DeSpirito, Army Research Research, Inc., Santa Clara, CA Meudon, France; R. Cayzac, Nexter Aberdeen Proving Ground, MD Laboratory, Aberdeen Proving Munitions, Bourges, France; A. Ground, MD Merlen, ONERA, Palaiseau, France Monday, 13 January 2014 16-DE-1 Design Engineering - Design Education Chesapeake Conf Rm 6 Chaired by: H. BRIGGS, ATA Engineering, Inc. and F. KAHLEN, University of Cape Town Libraries-Electr Jnls Only 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2014-0060 AIAA-2014-0061 AIAA-2014-0062 AIAA-2014-0063 Design Project for Aerospace Satellite Technology & Teaching Aircraft Systems An Aircraft Design Competition Specialization and Student Applications: Course Engineering as a Fundamental for High School STEM Research on the Combustion of Development and Principle of Design - University Improvement Bio-Derived Rocket Fuels Implementation of Texas Approach S. Smith, J. Hoagg, S. Bailey, V. Naoumov, N. Al Masoud, P. C. Cain, J. Jantzen, G. Schaffner, A. Chaput, H. Mark, University of University of Kentucky, Lexington, Sansevero, L. Guadagnoli, A. Moni, University of Cincinnati, Cincinnati, OH Texas, Austin, Austin, TX Lexington, KY D. Loukides, Central Connecticut State University, New Britain, CT Monday, 13 January 2014 17-EDU-1 Advancing Aerospace Education I National Harbor Conf Rm 5 Chaired by: R. LEBEAU, Saint Louis University 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2014-0064 AIAA-2014-0065 AIAA-2014-0066 Oral Presentation Oral Presentation A Viable and Comprehensive Implementation of Active Implementation of a Tiger Collegiate UAS Education Graduate UAS Education Process for Assessment and Cooperative Learning and Team into the NCSU Capstone T. Beneigh, Embry-Riddle D. Fisher, R. Gaeta, J. Jacob, J. Continuous Improvement Problem-based Learning in an Senior Aircraft Design Program Aeronautical University, Daytona Kidd, Oklahoma State University, towards Successful Accreditation Undergraduate Astrodynamics C. Hall, North Carolina State Beach, FL Stillwater, OK S. Karunamoorthy, Saint Louis Course University, Raleigh, NC University, St. Louis, MO S. Jayaram, Saint Louis University, St. Louis, MO Monday, 13 January 2014 18-FD-1 Applications of CFD I Maryland Ballroom 5 Chaired by: H. YANG, CFD Research Corporation and C. KIRIS 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2014-0067 AIAA-2014-0068 AIAA-2014-0069 AIAA-2014-0070 Modeling Slip at Triple Contact Discontinuous Galerkin A Comparative Study of The LAVA Computational Fluid Point in a Two Phase Flow Discretization of Chemically Gradient Reconstruction Dynamics Solver J. Thalakkottor, K. Mohseni, Reacting Flows Methods for Unstructured C. Kiris, M. Barad, J. Housman, University of Florida, Gainesville, A. Papoutsakis, Foundation for Research Meshes with Application to NASA Ames Research Center, Moffett Gainesville, FL and Technology Hellas (FORTH), Turbomachinery Flows Field, CA; E. Sozer, C. Brehm, S. Heraklion, Greece; I. Nompelis, K. Becker, G. Ashcroft, German Moini-Yekta, Science and Technology University of Minnesota, Minneapolis, Aerospace Center (DLR), Cologne, Corporation, Moffett Field, CA

55 Minneapolis, MN; J. Ekaterinaris, Germany Embry-Riddle Aeronautical University, Daytona Beach, FL Monday, 13 January 2014 19-FD-2 Bioinspired Aerodynamics: Experimental Woodrow Wilson A Chaired by: K. TAIRA, Florida State University and M. RINGUETTE, University at Buffalo 1000 hrs 1030 hrs 1100 hrs AIAA-2014-0071 AIAA-2014-0072 AIAA-2014-0073 Vorticity Generation and The roles of fish’s superficial Parameter Studies on Translating Transport on a Plunging Wing and canal lateral lines in the Rigid and Flexible Wings J. Buchholz, A. Eslam Panah, J. Akkala, sensing of an approaching wall P. Mancini, A. Jones, University of K. Wabick, C. Wojcik, University of Z. Ren, K. Mohseni, University of Maryland, College Park, College Park, Iowa, Iowa City, Iowa City, IA Florida, Gainesville, Gainesville, FL MD; M. Ol, K. Granlund, Air Force Research Laboratory, Wright-Patterson AFB, OH Monday, 13 January 2014 20-FD-3 Hypersonic Boundary Layer Transition I Chesapeake Conf Rm 8 Chaired by: X. ZHONG, University of California Los Angeles and S. SCHNEIDER, Purdue University 1000 hrs 1030 hrs 1100 hrs AIAA-2014-0074 AIAA-2014-0075 AIAA-2014-0076 Transition and Instability Traveling global instabilities HIFiRE-5 Flight Test Heating Measurements in a Mach 6 on the HIFiRE-5 elliptic cone Analysis Quiet Wind Tunnel model flow T. Juliano, D. Adamczak, R. Kimmel, R. Henderson, B. Chynoweth, A. P. Paredes, V. Theofilis, Technical Air Force Research Laboratory, Abney, C. Ward, S. Schneider, R. University of Madrid, Madrid, Spain Wright-Patterson AFB, OH Greenwood, Purdue University, West Lafayette, IN; et al. Monday, 13 January 2014 21-FD-4 Mesh Adaptation Chesapeake Conf Rm I Chaired by: K. FIDKOWSKI, University of Michigan and J. SITARAMAN, University of WY 1000 hrs 1030 hrs 1100 hrs AIAA-2014-0077 AIAA-2014-0078 AIAA-2014-0079 Adaptive Mesh Refinement Error Estimation and Adaptation Solution Algorithm For with High-Order Scheme for in Hybridized Discontinous Unstructured Grids Using an Unstructured Pressure- Galerkin Methods Quadrilateral Subdivision and Based Solver J. Dahm, K. Fidkowski, University of Hamiltonian Paths H. Yang, Z. Chen, A. Przekwas, Michigan, Ann Arbor, Ann Arbor, MI J. Sitaraman, B. Roget, University of CFD Research Corporation (CFDRC), Wyoming, Laramie, Laramie, WY Huntsville, AL; J. Dudley, Air Force Research Laboratory, Eglin AFB, FL Monday, 13 January 2014 22-FD-5 Solver Technology for Turbulent Flows I Chesapeake Conf Rm 7 Chaired by: B. DISKIN, National Institute of Aerospace and N. KROLL, DLR - German Aerospace Center 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2014-0080 Oral Presentation (Invited) AIAA-2014-0081 AIAA-2014-0082 AIAA-2014-0083 The DLR Flow Solver TAU - Convergence Enhancements for Unstructured Mesh Solution Evaluation of multigrid Turbulent Flow Validation in Status and Recent Algorithmic an Unstructured Grid Flow Solver Techniques using the NSU3D solutions for turbulent flows the Helios Strand Solver Developments A. Cary, A. Dorgan, M. Mani, The Solver B. Diskin, H. Nishikawa, National O. Tong, A. Katz, Utah State N. Kroll, S. Langer, A. Schwöppe, Boeing Company, St. Louis, MO D. Mavriplis, K. Mani, University of Institute of Aerospace, Hampton, VA University, Logan, UT; A. Wissink, German Aerospace Center (DLR), Wyoming, Laramie, Laramie, WY Army Aviation and Missile Research Braunschweig, Germany Development and Engineering Center, Moffett Field, CA 56 Monday, 13 January 2014 23-GNC-1 Adaptive Control National Harbor Conf Rm 8 Chaired by: M. BALAS, University of Wyoming and D. ALAZARD, Institut Supérieur de l’Aéronautique et de l’Espace 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2014-0084 AIAA-2014-0085 AIAA-2014-0086 AIAA-2014-0087 Exploring Adaptive Simple Adaptive Control in the Adaptive Control of a Flapping Real-Time Model Identification Incremental Backstepping Delta Domain Using a Linear Wing Robot Inspired by Bat using Simplex B-splines using Immersion and Matrix Inequality Flight Towards Modular Adaptive Invariance for an F-16 aircraft A. Cano Martinez, K. Sobel, City S. Dadashi, J. Gregory, Y. Lei, A. Control of a Civil Aircraft A. Ait Haddou Ali, Q. Chu, E. Van College of New York, New York, NY Kurdila, J. Bayandor, R. Mueller, L. Sun, Delft University of Kampen, C. de Visser, Delft University of Virginia Polytechnic Institute and Technology, Delft, The Netherlands Technology, Delft, The Netherlands State University, Blacksburg, VA Monday, 13 January 2014 24-GNC-2 Spacecraft Rendezvous and Proximity Operations National Harbor Conf Rm 7 Chaired by: S. STARIN, NASA-Goddard Space Flight Center and J. LIU, Boeing Defense, Space & Security 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2014-0088 AIAA-2014-0089 AIAA-2014-0090 AIAA-2014-0091 AIAA-2014-0092 Guidance for Autonomous Pose Estimation Using a Flash Spacecraft Rendezvous in Control Algorithms for Satellite Development of a Robotic Precision Landing on Lidar Elliptical Orbit using Nonlinear Rendezvous Maneuver in Simulation Platform for Atmosphereless Bodies T. Lim, A. Toombs, Naval Air Systems Model Predictive Control Elliptical Orbit Spacecraft Proximity I. Gerth, E. Mooij, Delft University of Command, Annapolis, MD P. Felisiak, K. Sibilski, W. Wroblewski, K. Sibilski, W. Wroblewski, P. Felisiak, Operations and Contact Technology, Delft, The Netherlands Wroclaw University of Technology, Wroclaw University of Technology, Dynamics Experiments Wroclaw, Poland; J. Sasiadek, Carleton Wroclaw, Poland; J. Sasiadek, Carleton A. Probe, J. Junkins, Texas A&M University, Ottawa, Canada University, Ottawa, Canada University, College Station, TX Monday, 13 January 2014 25-GT-1 Experimental Uncertainty in Ground Test Facilities National Harbor Conf Rm 10 Chaired by: J. KEGELMAN, NASA and R. DANFORTH, AERO Systems Engineering, Inc. 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2014-0093 AIAA-2014-0094 AIAA-2014-0095 AIAA-2014-0096 AIAA-2014-0097 Impact of Load Schedule Comparison of Pressures Driven An Alternative Strain Gage Repeatability Modeling for Within- and Between-Tunnel Design on the Quality of by Repetitive Nanosecond Pulses Balance Calibration Response Wind-Tunnel Measurements: Variations in Pressure Data for a Strain Gage Balance to AC Result Model Formulation Results for Three Langley Three Transonic Wind Tunnels Calibration Q. Chen, X. Meng, Y. Wang, R. DeLoach, NASA Langley Research Facilities R. DeLoach, NASA Langley Research R. DeLoach, NASA Langley Research Northwestern Polytechnical University, Center, Hampton, VA M. Hemsch, Self, Williamsburg, VA; H. Center, Hampton, VA Center, Hampton, VA Xi’an, China; F. Liu, S. Luo, University of Houlden, ViGYAN, Inc., Hampton, VA California, Irvine, Irvine, CA Monday, 13 January 2014 26-GTE-1 Turbomachinery I Woodrow Wilson D Chaired by: G. WELCH, NASA Glenn Research Center 1000 hrs 1030 hrs 1100 hrs AIAA-2014-0098 AIAA-2014-0099 AIAA-2014-0100 Dynamic Response Characteristics The Experimental Foundation Next Generation Traveling of Dual Flow-Path Integrally Used to Validate a Reduced Order Wave Excitation System for Bladed Rotors Model for Mistuned Rotors Integrally Bladed Rotors J. Beck, Air Force Research Laboratory, G. Cox, A. Palazotto, Air Force Institute J. Beck, J. Justice, O. Scott- Wright-Patterson AFB, OH; J. Slater, of Technology, Wright-Patterson AFB, Emuakpor, T. George, Air Force Wright State University, Dayton, OH; OH; J. Beck, J. Brown, Air Force Research Laboratory, Wright- J. Brown, C. Cross, Air Force Research Research Laboratory, Wright-Patterson Patterson AFB, OH Laboratory, Wright-Patterson AFB, OH AFB, OH 57 Monday, 13 January 2014 27-HIS-1 Aerospace Archives: All is NOT Lost - Keepers of the Right Stuff National Harbor Conf Rm 15 1000 - 1230 hrs Chaired by: T. CROUCH, National Air & Space Museum and C. MARTIN, NASA-Dryden Flight Research Center The AIAA History Technical Committee works to highlight the record of aerospace advances and recognize their impacts on modern society. To help dispel the myth that all the legacy materials of people and institutions have been lost, this session will provide a basic overview of what exists, where it is, and how it may be accessed. During this panel discussion,experts will talk about “best practices” and the individual and institutional responsibilities for preserving records.

Panelists: Ms. Dawne Dewey Dr. Deborah Douglas Ms. Marilyn Graskowiak Ms. Jane Odom Head of Archives and Special Collections Curator of Science & Technology Archivist Chief Archivist Wright State University MIT National Air & Space Museum NASA

Monday, 13 January 2014 28-ISC-3 International Student Conference - Team Division National Harbor Conf Rm 4 Chaired by: L. HANSEN, HRP Systems, Inc. 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2014-0101 AIAA-2014-0102 AIAA-2014-0103 AIAA-2014-0104 Autonomous Unmanned Aerial ATeP-UAV Sensor Testing LEOPARD: Low Earth Orbit When Do Endplates Work? Vehicle Platform Project for the Acquisition and A. Vaidyanathan, D. Kingman, S. Ericson, M. Kelly, N. Marshall, R. B. Finney, A. Fowler, I. Lin, J. Recovery of Debris T. Kurth, University of Southern Navarro, C. Newton, J. Parkhurst, Daniel Thomas, University of Alabama, C. Welch, K. Williamson, J. Wu, California, Los Angeles, CA Webster College, Nashua, NH; et al. Huntsville, Huntsville, AL University of Colorado, Boulder, Boulder, CO Monday, 13 January 2014 29-MAT-1 Nanostructured Materials I Chesapeake Conf Rm A Chaired by: G. ODEGARD; B. WARDLE, Massachusettes Institute of Technology and S. ROY, The University of Alabama 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2014-0105 AIAA-2014-0106 AIAA-2014-0107 AIAA-2014-0108 AIAA-2014-0109 Actuation of Bistable Multi-scale Modeling of Failure Fracture Toughness of Aligned New architecture and Monitoring Strain Rate Effects Laminates by Conductive in Nano-Particle Reinforced Carbon Nanotube Polymer processes for hierarchical on Nanocomposites using Polymer Nanocomposites for Polymers Using the Atomistic Nanocomposites for the composites of aligned carbon Piezospectroscopy use in Thermal-Mechanical J-Integral Reinforcement of Hierarchical nanotubes and continuous E. Durnberg, A. Jones, J. Rosas, Aerosurface De-icing Systems S. Roy, A. Akepati, University of Composite Materials carbon ﬁbers University of Central Florida, C. Brampton, C. Bowen, University Alabama, Tuscaloosa, Tuscaloosa, AL S. Wicks, B. Wardle, Massachusetts R. Guzman de Villoria, B. Wardle, N. Orlando, FL; G. Sunny, Air Force of Bath, Bath, United Kingdom; S. Institute of Technology, Cambridge, MA Yamamoto, Massachusetts Institute Research Laboratory, Eglin AFB, FL; Buschhorn, J. Lee, Massachusetts of Technology, Cambridge, MA S. Raghavan, University of Central Institute of Technology, Cambridge, Florida, Orlando, FL MA; S. Pickering, University of Bath, Bath, United Kingdom; B. Wardle, Massachusetts Institute of Technology, Cambridge, MA; et al. Monday, 13 January 2014 30-MDO-1 Optimization Methods and Algorithms I Chesapeake Conf Rm 4 Chaired by: G. MODGIL, Rolls-Royce Corporation and A. KO, Phoenix Integration, Inc. 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2014-0110 AIAA-2014-0111 AIAA-2014-0112 AIAA-2014-0113 AIAA-2014-0114 Revisiting Individual Discipline Reduced Order Techniques for Dimensionality Reduction In Continuum Sensitivity Analysis Metric-Based Mathematical

58 Feasible using matrix-free Sensitivity Analysis and Design Aerodynamic Design Using for Structural Shape Design Derivation of Aerofoil Design Inexact-Newton-Krylov Optimization of Aerospace Principal Component Analysis Variables Using Finite Volume Variables A. Dener, J. Hicken, Rensselaer Systems With Gradient Information Approach D. Poole, C. Allen, T. Rendall, Polytechnic Institute, Troy, NY J. Parrish, M. Rais-Rohani, J. S. Berguin, D. Mavris, Georgia K. Gobal, R. Grandhi, Wright State University of Bristol, Bristol, United Janus, Mississippi State University, Institute of Technology, Atlanta, GA University, Dayton, OH Kingdom Starkville, MS Monday, 13 January 2014 31-MVC-1 Meshing Technology and Application Chesapeake Conf Rm 9 Chaired by: B. SEKAR, USAF AFRL/RZTC and J. MASTERS, Aerospace Testing Alliance (ATA) 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2014-0115 AIAA-2014-0116 AIAA-2014-0117 AIAA-2014-0118 AIAA-2014-0119 Specialized CFD Grid Multi-Block Hierarchical Anisotropic Boundary Layer Automated Tetrahedral Mesh Practical and Reliable Mesh Generation Methods for Near- Unstructured Grid Generation Adaptivity of Multi-Element Generation for CFD Analysis of Generation for Complex, Real- Field Sonic Boom Prediction With Adaptation Wings Aircraft in Conceptual Design World Geometries M. Park, R. Campbell, A. Elmiligui, S. Karman, University of Tennessee, K. Chitale, University of Colorado, I. Ordaz, W. Li, R. Campbell, NASA A. Demargne, R. Evans, P. Tiller, NASA Langley Research Center, Chattanooga, Chattanooga, TN Boulder, Boulder, CO; M. Rasquin, Langley Research Center, Hampton, VA Cambridge Flow Solutions, Ltd., Hampton, VA; S. Cliff, NASA Ames Argonne National Laboratory, Cambridge, United Kingdom; W. Research Center, Moffett Field, CA; Argonne, IL; O. Sahni, M. Shephard, Dawes, Cambridge University, S. Nayani, Analytical Services and Rensselaer Polytechnic Institute, Cambridge, United Kingdom Materials, Inc., Hampton, VA Troy, NY; K. Jansen, University of Colorado, Boulder, Boulder, CO Monday, 13 January 2014 32-NDA-1 Model Validation and Uncertainty Quantiﬁcation Chesapeake Conf Rm 5 Chaired by: B. THACKER, Southwest Research Institue and J. PEPIN, Los Alamos National Laboratory 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2014-0120 AIAA-2014-0121 AIAA-2014-0122 AIAA-2014-0123 AIAA-2014-0124 Evaluation of Model Validation A Simple Probabilistic Options for the inclusion of Bayesian Calibration of Uncertainty Quantiﬁcation and Techniques in the Presence of Validation Metric for the model discrepancy in Bayesian Coupled Aerothermal Models Output Prediction in Multi-level Uncertainty Comparison of Uncertain calibration Using Time-Dependent Data Problems I. Voyles, C. Roy, Virginia Polytechnic Model and Test Results Y. Ling, J. Mullins, S. Mahadevan, E. DeCarlo, S. Mahadevan, C. Li, S. Mahadevan, Vanderbilt Institute and State University, B. Thacker, Southwest Research Vanderbilt University, Nashville, TN Vanderbilt University, Nashville, TN; University, Nashville, TN Blacksburg, VA Institute, San Antonio, TX; T. Paez, B. Smarslok, Air Force Research Thomas Paez Consulting, Sedona, AZ Laboratory, Wright-Patterson AFB, OH Monday, 13 January 2014 33-PANEL-1 Analysis and Perspectives from the Complex Aerospace System Exchange (CASE) 2013 Potomac Ballroom C 1000 - 1230 hrs 1000 - 1025 hrs Characteristics of the Design and Development of Complex Aerospace Systems

Anna-Maria Rivas McGowan Peter Parker Senior Aerospace Technologist, NASA Langley Research Center Senior Aerospace Technologist, NASA Langley Research Center

1025 - 1050 hrs Leadership in Pursuit of Systems Thinking for Individuals and Organizations

Kurt Detweiler David Dress 59 Deputy Center Chief Engineer, NASA Langley Research Center Deputy, Space Technology Projects Ofﬁce, NASA Langley Research Center

1050 - 1115 hrs The Future May Not Be Where We Are Looking Today

Kennie Jones William Kimmel Senior Aerospace Technologist, NASA Langley Research Center Chief Technologist for Systems Analysis and Concepts Directorate, NASA Langley Research Center

1115 - 1230 hrs Insights from the CASE 2013 Conference Organizers Moderator: Anna-Maria Rivas McGowan, Senior Aerospace Technologist, NASA Langley Research Center Panelists: Allen Arrington Sophia Bright David Dress Laura McGill Engineering Manager, Sierra Lobo Executive Assistant Deputy, Space Technology Projects Ofﬁce Deputy Vice President of Engineering Boeing Global Support & Services Engineering NASA Langley Research Center Raytheon Boeing Monday, 13 January 2014 34-PC-1 Fuels and Combustion Kinetics Chesapeake Conf Rm G Chaired by: H. CURRAN, National University of Ireland and X. YANG, Princeton University 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2014-0126 AIAA-2014-0127 AIAA-2014-0128 AIAA-2014-0129 Kinetic Surrogate Model for Autoignition Behavior of The Inﬂuence of Non-Uniform Experimental and Kinetic GTL Kerosene Synthetic Alternative Jet Initial Conditions on Temperature Studies of Acetylene Flames at N. Slavinskaya, E. Saibov, U. Fuels and Blends in a Rapid Field Development in Rapid Elevated Pressures Riedel, J. Herzler, C. Naumann, Compression Machine Compression Machine X. Shen, X. Yang, J. Santner, German Aerospace Center (DLR), D. Valco, University of Illinois, Urbana- Experiments Princeton University, Princeton, Stuttgart, Germany; L. Thomas, Air Champaign, Urbana, IL; G. Gentz, J. Neuman, C. Allen, Marquette NJ; J. Sun, University of Science Force Research Laboratory, Wright- Michigan State University, East Lansing, University, Milwaukee, WI and Technology of China, Hefei, Patterson AFB, OH; et al. MI; M. Colket, United Technologies China; Y. Ju, Princeton University, Corporation, East Hartford, CT; E. Princeton, NJ Toulson, Michigan State University, East Lansing, MI; T. Lee, University of Illinois, Urbana-Champaign, Urbana, IL Monday, 13 January 2014 35-PC-2 Gas Turbine Combustion Chesapeake Conf Rm H Chaired by: T. LIEUWEN, Georgia Institute of Technology 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2014-0130 AIAA-2014-0131 AIAA-2014-0132 AIAA-2014-0133 Development and Validation Large-Eddy Simulation of a Numerical simulations of soot A Parametric Study of of an Optically Accessible High High-Pressure, Single-Element and NOx distributions in a full Combustion Dynamics in

60 Power Gas Turbine Combustion Lean Direct-Injected Gas- scale aero-engine combustor a Single-Element Lean Experiment Turbine Combustor at two different ﬂight altitudes Direct Injection Gas A. Pratt, C. Slabaugh, R. Lucht, S. S. Kim, S. Menon, J. Darin, Georgia C. Eberle, T. Blacha, German Turbine Combustor: Part II: Meyer, Purdue University, West Institute of Technology, Atlanta, GA Aerospace Center (DLR), Stuttgart, Experimental Investigation Lafayette, IN Germany; P. Gerlinger, University of R. Gejji, C. Yoon, Purdue University, Stuttgart, Stuttgart, Germany; M. West Lafayette, IN; V. Sankaran, Air Aigner, German Aerospace Center Force Research Laboratory, Edwards (DLR), Stuttgart, Germany AFB, CA; W. Anderson, Purdue University, West Lafayette, IN Monday, 13 January 2014 36-PC-3 Rockets and Airbreathing Propulsion I Maryland Ballroom 6 Chaired by: J. OEFELEIN, Sandia National Laboratories and T. OMBRELLO, Air Force Research Laboratory 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2014-0134 AIAA-2014-0135 AIAA-2014-0136 AIAA-2014-0137 AIAA-2014-0138 Propellant Feed System Instability Analysis of Liquid Numerical Study of Cryogenic Development of a Facility for Large Eddy Simulation of Inﬂuence on Rocket Engine Films of Liquefying Hybrid Coaxial Jet under Supercritical Combustion Stability Experiments Supercritical Mixing and Combustion Instability Rocket Fuels under Supercritical Condition at Supercritical Pressure Combustion for Rocket P. Popov, A. Sideris, W. Sirignano, Operating Condition D. Muto, N. Tsuboi, Kyushu Institute J. Wegener, University of California, Los Applications University of California, Irvine, M. Adachi, University of Tokyo, of Technology, Kitakyushu, Japan; Angeles, Los Angeles, CA; I. Leyva, Air J. Hickey, M. Ihme, Stanford Irvine, CA Tokyo, Japan; T. Shimada, Japan H. Terashima, University of Tokyo, Force Research Laboratory, Edwards University, Stanford, CA Aerospace Exploration Agency Bunkyo, Japan AFB, CA; D. Forliti, Sierra Lobo, Inc., (JAXA), Kanagawa, Japan Edwards AFB, CA; D. Talley, Air Force Research Laboratory, Edwards AFB, CA Monday, 13 January 2014 37-PDL-1 Electric Propulsion/Laser Applications of Plasmas Maryland Ballroom 4 Chaired by: R. SEDWICK, University of Maryland 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2014-0139 AIAA-2014-0140 AIAA-2014-0141 AIAA-2014-0142 AIAA-2014-0143 Comparison of Ion Thruster Detection of Plume-Mode Performance of a Helicon Development of a Chemical Simultaneous Temperature, Plumes Generated in the SPPL-1 Transition for NEXT Neutralizer Thruster using Helium, Argon, Carbon Monoxide Laser Density and Velocity Facility with DSMC Simulations Cathode and Water Vapor K. Frederickson, Y. Ivanou, S. Measurements in Laser- using AMR M. Crofton, W. Cox, J. Young, K. A. Faust, R. Sedwick, University of Leonov, J. Rich, W. Lempert, I. Generated Plasmas by B. Korkut, Pennsylvania State University, Diamant, E. Beiting, The Aerospace Maryland, College Park, College Adamovich, Ohio State University, Rayleigh and Filtered Rayleigh University Park, PA; J. Young, University Corporation, El Segundo, CA; M. Park, MD Columbus, OH Scattering of Maryland, College Park, College Patterson, NASA Glenn Research C. Limbach, R. Miles, Princeton Park, MD; D. Levin, Pennsylvania Center, Cleveland, OH; et al. University, Princeton, NJ State University, University Park, PA; R. Sedwick, University of Maryland, College Park, College Park, MD Monday, 13 January 2014 38-PDL-2 Plasma-Actuators and Flow Control I Maryland Ballroom 1 Chaired by: D. ASHPIS, NASA Glenn Research Center 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2014-0144 AIAA-2014-0145 AIAA-2014-0146 AIAA-2014-0147 Dielectric Barrier Discharge Electrical and optical Improving Plasma Actuator Parametric Study of Particle Control and Thrust characteristics of pulsed dielectric Thrust at Low Pressure Size for Plasma Actuator PIV Enhancement by Diode Surface barrier discharges as a function Through Geometric Variation Measurements

61 A. Starikovskiy, M. Post, N. Tkach, of altitude conditions P. Friz, J. Rovey, Missouri University A. Masati, R. Sedwick, University R. Miles, Princeton University, N. Benard, D. Pai, A. Aba’a Ndong, E. of Science and Technology, Rolla, of Maryland, College Park, College Princeton, NJ Bayoda, N. Zouzou, E. Moreau, National MO Park, MD Center for Scientific Research (CNRS), Poitiers, France Monday, 13 January 2014 39-SD-1 Computational Aeroelasticity ROM I Chesapeake Conf Rm C Chaired by: J. COOPER, University of Bristol and N. FALKIEWICZ, Boeing Research & Technology 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2014-0148 AIAA-2014-0149 AIAA-2014-0150 AIAA-2014-0151 Response of a Panel to Shock Aerothermoelastic Simulation Modeling Crack Propagation Reduced Order Modeling for the Impingement: Modeling and of Air-Breathing Hypersonic within a Reduced- Order Model Nonlinear Geometric Response of Comparison with Experiments Vehicles Framework Some Joined Wings B. Miller, A. Crowell, R. Deshmukh, R. Klock, C. Cesnik, University of P. O’Hara, United Technologies G. Phlipot, X. Wang, M. Mignolet, A. Gogulapati, J. McNamara, Ohio Michigan, Ann Arbor, Ann Arbor, MI Corporation, Dayton, OH; J. Arizona State University, Tempe, AZ; State University, Columbus, OH; Hollkamp, Air Force Research L. Demasi, R. Cavallaro, San Diego V. Vyas, Arizona State University, Laboratory, Wright-Patterson AFB, OH State University, San Diego, CA Tempe, AZ; et al. Monday, 13 January 2014 40-SD-2 Energy Harvesting, Damping and Vibration Suppression Chesapeake Conf Rm B Chaired by: W. WELSH, Sikorsky Aircraft Corporation and Y. YIU, Lockheed Martin Space Systems 1000 hrs 1030 hrs 1100 hrs AIAA-2014-0152 AIAA-2014-0153 AIAA-2014-0154 Investigation on the Nonlinear Dynamics Modelling the Dynamic Response Effectiveness of a Nonlinear Characterization of of Bistable Composite Plates for Energy Sink on an Aeroelastic Piezoelectric Energy Harvesters Piezoelectric Energy Harvesting System from Hybrid Vibrations D. Betts, University of Bath, Bath, Y. Bichiou, H. Taha, M. Hajj, Virginia Z. Yan, A. Abdelkefi, M. Hajj, Virginia United Kingdom; R. Guyer, University Polytechnic Institute and State Polytechnic Institute and State of Nevada, Reno, Reno, NV; P. Le Bas, University, Blacksburg, VA University, Blacksburg, VA Los Alamos National Laboratory, Los Alamos, NM; C. Bowen, University of Bath, Bath, United Kingdom; D. Inman, University of Bristol, Bristol, United Kingdom; H. Kim, University of Bath, Bath, United Kingdom Monday, 13 January 2014 41-STR-1 Composite Micromechanics Chesapeake Conf Rm D Chaired by: M. HYER, Virginia Tech and T. AOKI, University of Tokyo 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2014-0155 AIAA-2014-0156 AIAA-2014-0157 AIAA-2014-0158 AIAA-2014-0159 Micromechanics Model to Link Analysis of Space Structures Progressive Failure Analysis on Fast Life Prediction Model for Optical Stress-sensing Alumina Microstructural Variability to Subject to Hypervelocity Textile Composites Composites Based on Multiple Nanocomposite Coatings for Fiber Reinforced Composite Impact D. Zhang, A. Waas, University of Temporal Scale Homogenization Aerospace Structures 62 Behavior A. Thurber, J. Bayandor, Virginia Michigan, Ann Arbor, Ann Arbor, MI; R. Crouch, C. Oskay, Vanderbilt G. Freihofer, A. Van Newkirk, A. L. Borkowski, K. Liu, A. Polytechnic Institute and State C. Yen, Army Research Laboratory, University, Nashville, TN; S. Clay, Air Gupta, S. Seal, S. Raghavan, Chattopadhyay, Arizona State University, Blacksburg, VA Aberdeen Proving Ground, MD Force Research Laboratory, Wright- University of Central Florida, University, Tempe, AZ Patterson AFB, OH Orlando, FL Monday, 13 January 2014 42-STR-2 Beams & Plates Chesapeake Conf Rm F Chaired by: L. DEMASI and W. YU, Purdue University 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2014-0160 AIAA-2014-0161 AIAA-2014-0162 AIAA-2014-0163 Informal Numerical Methods The effect of the order of A thin shell finite element for Cross-sectional modelling of for Generalized Beam-Column asymptotic stress field in a textile composite structures thin-walled composite beams Problems strain energy transformation W. Xu, A. Waas, University of E. Ferede, M. Abdalla, Delft S. Russell, Triumph Group, Inc., for beams and plates Michigan, Ann Arbor, Ann Arbor, MI University of Technology, Delft, The Dallas, TX J. Kim, Kumoh National Institute of Netherlands Technology, Gumi, South Korea Monday, 13 January 2014 43-STR-3 Buckling and Structural Instability Chesapeake Conf Rm E Chaired by: C. BISAGNI, Politecnico Di Milano and R. TAYLOR, Optimal Structures, LLC. 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2014-0164 AIAA-2014-0165 AIAA-2014-0166 AIAA-2014-0167 Buckling and Post-Buckling Buckling Analysis of Probabilistic Buckling Analysis Local Buckling of Blade Behavior of Unitized, Stiffened Curvilinearly Stiffened of Composite and Sandwich Stiffened Variable Angle Tow Tri-Axially Braided Composite Composite Panels with Cracks Cylindrical Shells Panels Textile Plates M. Jrad, A. Khan, R. Kapania, M. Alfano, C. Bisagni, Technical B. Coburn, Z. Wu, P. Weaver, C. Kosztowny, A. Waas, University of Virginia Polytechnic Institute and University of Milan, Milan, Italy University of Bristol, Bristol, United Michigan, Ann Arbor, Ann Arbor, MI State University, Blacksburg, VA Kingdom Monday, 13 January 2014 44-WE-1 Wind Turbine Airfoil Design and Analysis Woodrow Wilson C Chaired by: D. MANIACI, Sandia National Laboratories and C. VAN DAM 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2014-0168 AIAA-2014-0169 AIAA-2014-0170 AIAA-2014-0171 modeling and effects of base The Flow Field of a Dynamically Influence of 2D Steps and Experimental And Numerical drag on thick airfoils design Pitching Finite Span S809 Blade Distributed Roughness on Investigation Of An Optimized F. Grasso, Energy Research Center and its Control Transition on a NACA 63(3)- Airfoil For Vertical Axis Wind of the Netherlands, Petten, The K. Taylor, C. Leong, M. Amitay, 418 Turbines Netherlands Rensselaer Polytechnic Institute, Troy, NY R. Ehrmann, E. White, Texas A&M D. Ragni, C. Simao Ferreira, Delft University, College Station, TX University of Technology, Delft, The Netherlands; M. Barone, Sandia National Laboratories, Albuquerque, NM Monday, 13 January 2014 45-WE-2 Wind Turbine Blade Materials and Manufacturing Woodrow Wilson B Chaired by: D. MILLER, Mechanical and Industrial Engineering 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2014-0172 AIAA-2014-0173 AIAA-2014-0174 AIAA-2014-0175 Creep/Fatigue Response of A New Fatigue Analysis Effects of Tensile Stresses Optimal Design of Sandwich Resin Infused Biaxial Glass Procedure for Composite Wind on the Moisture Diffusion Core for Wind Turbine Blade Fabric Laminates in Reversed Turbine Blades Characteristics of Epoxy Glass Buckling Resistance Loading W. Hu, O. Zhupanska, J. Buchholz, Composites F. Stoll, Milliken & Company, D. Samborsky, J. Mandell, D. K. Choi, University of Iowa, Iowa M. Stoffels, D. Miller, D. Samborsky, Spartanburg, SC Miller, Montana State University, City, Iowa City, IA J. Mandell, Montana State

63 Bozeman, MT University, Bozeman, MT Monday, 13 January 2014 46-LECT-1 Durand Lectureship and Luncheon: American Space Strategy: Choose to Steer, Not Drift Potomac Ballroom A&B 1230 - 1400 hrs Scott Pace Director, Space Policy Institute, Elliott School of International Affairs George Washington University Monday, 13 January 2014 47-NW-2 Monday Afternoon Networking Coffee Break Foyer 1400 - 1430 hrs Monday, 13 January 2014 48-SB-2 Monday Afternoon Speakers’ Briefing Session Rooms 1400 - 1430 hrs Monday, 13 January 2014 49-AA-2 Jet Noise I Woodrow Wilson C Chaired by: N. MURRAY, The University of Mississippi 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2014-0176 AIAA-2014-0177 AIAA-2014-0178 AIAA-2014-0179 AIAA-2014-0180 Analysis of a Shock-Associated Hybrid RANS-NLES of Real Computational Study of the Acoustic Source Localization Equilibrium Wall Model for Noise Prediction Model Using Geometry Hot Jets: Flow and Impact of Chevrons on Noise of Rectangular Jets using Large Eddy Simulations of Jets Measured Jet Far-Field Noise Noise Prediction Characteristics of Imperfectly Large Eddy Simulation with for Aeroacoustics Data M. Mahak, J. Tyacke, P. Tucker, Expanded Jet Flows Numerical Phased Arrays K. Aikens, N. Dhamankar, C. M. Dahl, NASA Glenn Research University of Cambridge, Cambridge, J. Liu, A. Corrigan, K. Kailasanath, Naval J. Erwin, P. Panickar, P. Vogel, N. Martha, Y. Situ, G. Blaisdell, Purdue Center, Cleveland, OH; J. Sharpe, United Kingdom Research Laboratory, Washington, Sinha, Combustion Research and University, West Lafayette, IN; A. Saginaw Valley State University, DC; N. Heeb, D. Munday, E. Gutmark, Flow Technology, Inc., Pipersville, PA Lyrintzis, Embry-Riddle Aeronautical University Center, MI University of Cincinnati, Cincinnati, OH University, Daytona Beach, FL; et al. Monday, 13 January 2014 50-ACD-3 Aircraft Design Issues Azalea 1 Chaired by: R. BARRETT-GONZALEZ, The University of Kansas 1430 hrs 1500 hrs 1530 hrs 1600 hrs AIAA-2014-0181 AIAA-2014-0182 AIAA-2014-0183 AIAA-2014-0184 Fuel-Burn Impact of Re- Liquefied Natural Gas Influences on Safety of Flight Extensions to aircraft pre- Designing Future Aircraft Aircraft: A Life Cycle Costing of WIG craft design for supersonic aircraft with Changes in Mission Perspective N. Kornev, A. Gross, University of M. Schuermann, P. Horst, Technical Specifications T. Conroy, K. Lim Ee Wei, C. Bil, Rostock, Rostock, Germany University of Braunschweig, A. Variyar, T. Lukaczyk, M. Colonno, G. Dorrington, RMIT University, Braunschweig, Germany; M. Gaffuri, J. Alonso, Stanford University, Melbourne, Australia German Aerospace Center (DLR), Braunschweig, Germany 64 Stanford, CA Monday, 13 January 2014 51-ACD-4 Aircraft Design Optimization Azalea 2 Chaired by: W. CROSSLEY, Purdue University 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2014-0185 AIAA-2014-0186 AIAA-2014-0187 AIAA-2014-0188 AIAA-2014-0189 Wing Configuration Impact Multidisciplinary Design Conceptual Design Computational Geometry Applications of multi-block CST on Design Optimums for a Optimization of Subsonic Strut- Optimization of an Augmented for Multi-fidelity and Multi- method for quasi-waverider Subsonic Passenger Transport Braced Wing Aircraft Stability Aircraft Incorporating disciplinary Analysis and design D. Wells, NASA Langley Research R. Gupta, W. Mallik, R. Kapania, J. Dynamic Response and Optimization C. Liu, Y. Duan, J. Cai, G. Yang, Center, Hampton, VA Schetz, Virginia Polytechnic Institute Actuator Constraints N. Bhagat, Universal Technology Northwestern Polytechnical and State University, Blacksburg, VA J. Welstead, G. Crouse, Auburn Corporation, Fairborn, OH; E. University, Xi’an, China University, Auburn, AL Alyanak, Air Force Research Laboratory, Wright-Patterson AFB, OH Monday, 13 January 2014 52-AFM-3 Flight Dynamics and Handling Qualities II National Harbor Conf Rm 13 Chaired by: K. CUNNINGHAM, NASA-Langley Research Center and P. WILLIAMS-HAYES, NASA Dryden Flight Research Center 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2014-0190 AIAA-2014-0191 AIAA-2014-0192 AIAA-2014-0193 AIAA-2014-0194 Trajectory Analysis of Basket Dynamic Analysis of the Meridian Trimming Mass-Actuated Lower Stratospheric Deployment Development of a Flight Data Engagement during Aerial Unmanned Aerial Vehicle Airplane in Turns with Zero Testing of a Ram-Air Parafoil System and Experimental Refueling N. Smith, L. Toledo, D. Kennedy, Side Slip Angle System Determination of Aerodynamic J. Masud, O. Khan, Air University, A. Sizemore, University of Kansas, A. Dogan, S. Erturk, University of T. Fields, University of Missouri, Kansas Loads on a Wing Spar Islamabad, Pakistan Lawrence, Lawrence, KS Texas, Arlington, Arlington, TX City, Kansas City, MO; O. Yakimenko, S. Abraham-Doman, C. Merrett, Naval Postgraduate School, Monterey, Carleton University, Ottawa, Canada CA; J. LaCombe, E. Wang, University of Nevada, Reno, Reno, NV Monday, 13 January 2014 53-APA-6 Active and Passive Flow Control I Maryland Ballroom A Chaired by: C. TILMANN, Air Force Reseach Laboratory and T. MCLAUGHLIN, US Air Force Academy 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs AIAA-2014-0195 AIAA-2014-0196 AIAA-2014-0197 AIAA-2014-0198 AIAA-2014-0199 AIAA-2014-0200 Pitching Airfoil Performance Investigation of an Improved Roll-modes generated in Enhancement of High-Lift Numerical Study of the Active Establishment of Mapping Enhancement Using Co-Flow Design for a Dielectric Barrier turbulent boundary layers with System Flap Performance Control of Underexpanded Jets Relationship between Plasma Jet Flow Control at High Mach Discharge Plasma Actuator for passive surface modifications using Active Flow Control K. Goparaju, D. Gaitonde, M. Actuator Parameters and Body Number} Flight Control of an Inflatable B. Nugroho, University of M. Desalvo, Georgia Institute of Zhuang, Ohio State University, Force based on Neural Networks A. Lefebvre, G. Zha, University of Wing Melbourne, Melbourne, Australia; Technology, Atlanta, GA; E. Whalen, Columbus, OH B. Wu, C. Gao, Y. Wang, Y. Wang, Miami, Coral Gables, FL J. Laten, R. LeBeau, Saint Louis E. Gnanamanickam, Embry-Riddle The Boeing Company, St. Louis, B. Zheng, Northwestern Polytechnical University, St. Louis, MO Aeronautical University, Daytona MO; A. Glezer, Georgia Institute of University, Xi’an, China; F. Liu, University Beach, FL; K. Kevin, J. Monty, N. Technology, Atlanta, GA of California, Irvine, Irvine, CA; et al. Hutchins, University of Melbourne, Melbourne, Australia Monday, 13 January 2014 54-APA-7 Best Practices for CFD Validation - Validation of Numerical Models Discussion Group (Invited) Maryland Ballroom 4 Chaired by: P. MORGAN, Ohio Aerospace Institute 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs AIAA-2014-0201 AIAA-2014-0202 AIAA-2014-0203 AIAA-2014-0204 AIAA-2014-0205 Oral Presentation (Invited) Turbulence Modeling Observations on CFD Verification Unsteady aerodynamic Lessons learned and best Assessment Criteria for Hypersonic Laminar-Turbulent Verification and Validation and Validation from the AIAA validation experiences from practices for fluid dynamic Computational Fluid Dynamics Transition: Suggestions for (Invited) Drag Prediction Workshops the Aeroelastic Prediction validation experiments Validation Benchmark Development and Validation of C. Rumsey, NASA Langley Research J. Morrison, W. Kleb, NASA Langley Workshop J. Benek, Air Force Research Experiments Numerical Models Center, Hampton, VA Research Center, Hampton, VA; J. Laboratory, Wright-Patterson AFB, OH

65 J. Heeg, NASA Langley Research W. Oberkampf, W. L. Oberkampf S. Schneider, Purdue University, West Vassberg, The Boeing Company, Center, Hampton, VA Consulting, Austin, TX; B. Smith, Lafayette, IN Huntington Beach, CA Utah State University, Logan, UT Monday, 13 January 2014 55-APA-8 Simulation of Rotor in Hover (Invited) II Maryland Ballroom 3 Chaired by: N. HARIHARAN, CREATE-AV and T. EGOLF, Sikorsky Aircraft Corporation 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2014-0206 AIAA-2014-0207 AIAA-2014-0208 AIAA-2014-0209 AIAA-2014-0210 Numerical Simulations Hover Predictions on the OVERFLOW Simulation of Helios Simulation of Rotors in Analysis of a Rotor in Hover of Rotors in Shipboard Sikorsky S-76 Rotor using Rotors in Hover: The Boeing Hover: The Boeing Company using Hybrid Methodology Environment Helios Company H. Tadghighi, The Boeing Company, R. Marpu, L. Sankar, Georgia Institute C. Crozon, R. Steijl, G. Barakos, M. Potsdam, R. Jain, U.S. Army, R. Narducci, The Boeing Company, Mesa, AZ of Technology, Atlanta, GA; T. Egolf, University of Liverpool, Liverpool, Moffett Field, CA; N. Hariharan, Philadelphia, PA Sikorsky Aircraft Corporation, Stratford, United Kingdom CREATE AV Team, Patuxent River, MD CT; N. Hariharan, HPCMP CREATE-AV, Lorton, VA Monday, 13 January 2014 56-APA-9 Weapons Aerodynamics and Store Separation II National Harbor Conf Rm 11 Chaired by: K. BREKKE, Sandia National Labs and J. DESPIRITO, US Army Research Laboratory 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2014-0211 AIAA-2014-0212 AIAA-2014-0213 AIAA-2014-0214 AIAA-2014-0215 Comparison of CFD-Based Solution-Adaptive Method for Studies of Vortex Interference Aerodynamics of Transonic Investigation of Aerodynamics Simulation of External Fuel Prediction of Aerodynamic Associated with Missile and Supersonic Projectiles in and Flight Mechanics Tank Separation to Flight Test Interaction in Multiple-Body Conﬁgurations Ground Effect Characteristics of Ground D. Finley, T. Messina, K. Chankaya, E. High-Speed Air-Delivered D. Lesieutre, O. Quijano, Nielsen G. Doig, S. Wang, University of New Effect Missile Blosch, Lockheed Martin Corporation, Systems Engineering & Research, Inc., Santa South Wales, Sydney, Australia; J. F. Li, China Academy of Aerospace Fort Worth, TX; J. Dreese, Pointwise, R. Harris, C. Talley, P. Liever, CFD Clara, CA Young, H. Kleine, University of New Aerodynamics, Beijing, China Inc., Fort Worth, TX Research Corporation (CFDRC), South Wales at the Australian Defence Huntsville, AL; E. Luke, Mississippi Force Academy, Canberra, Australia State University, Mississippi State, MS; J. Dudley, Air Force Research Laboratory, Eglin AFB, FL Monday, 13 January 2014 57-DE-2 Design Engineering - Design Process Chesapeake Conf Rm 6 Chaired by: S. ROWE, NASA Marshall Space Flight Center and D. STAGGERS, Raytheon Missile Systems 1430 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs No Presentations AIAA-2014-0216 AIAA-2014-0217 AIAA-2014-0218 AIAA-2014-0219 Tracking Design Evolution in Applying Model-Based Surrogate Modeling Based Thinking inside the Box (Bringing Aircraft Structural Modeling Development (MBD) to Uncertainty Quantiﬁcation In Back Touch and Feel to Structures H. Briggs, ATA Engineering, Inc., San embedded systems Subject Matter Expert Systems Design Instruction)

66 Diego, CA K. Tsujimoto, M. Shimoura, Y. F. Akram, National University of L. Gonzalez-Linero, Embry-Riddle Morita, H. Oyori, IHI Corporation, Sciences and Technology, Islamabad, Aeronautical University, Daytona Tomioka, Japan Pakistan; D. Mavris, Georgia Institute Beach, FL of Technology, Atlanta, GA Monday, 13 January 2014 58-EDU-2 Advancing Aerospace Education II: Best practices in Teaching CFD in Undergraduate Aerospace Education National Harbor Conf Rm 5 1430 - 1730 hrs Chaired by: K. RAVINDRA, Parks College of Engineering, Aviation & Technology Moderator: Dr. K. Ravindra, Associate Dean, Saint Louis University Panelists: Dr. Andrew Cary Dr. Brian Smith Dr. Russ Cummings Dr. Raymond LeBeau Senior Technical Fellow Lockheed Martin Fellow Professor of Aerospace Engineering Department of Aerospace and Mechanical Engineering The Boeing Company Lockheed Martin Corporation United States Air Force Academy Saint Louis University

Monday, 13 January 2014 59-FD-7 Bioinspired Aerodynamics: Numerical Maryland Ballroom 5 Chaired by: H. LUO, Vanderbilt University and M. GREEN, Syracuse University 1430 hrs 1500 hrs 1530 hrs 1600 hrs AIAA-2014-0220 AIAA-2014-0221 AIAA-2014-0222 AIAA-2014-0223 Climbing Flight of a Fruit Bat Nonlinear Aeroelastic Analysis of Global model reduction for Aerodynamic Force Modeling Deconstructed Highly Flexible Flapping Wings flows with moving boundary for Unsteady Wing Maneuvers K. Viswanath, K. Nagendra, D. Tafti, Using an ALE Formulation of H. Gao, M. Wei, New Mexico State R. Jantzen, K. Taira, Florida State Virginia Polytechnic Institute and Embedded Boundary Method University, Las Cruces, NM University, Tallahassee, FL; K. State University, Blacksburg, VA V. Lakshminarayan, C. Farhat, Stanford Granlund, M. Ol, Air Force Research University, Stanford, CA Laboratory, Wright-Patterson AFB, OH Monday, 13 January 2014 60-FD-8 CFD for Turbulent Flows Maryland Ballroom D Chaired by: C. GROTH, University of Toronto and Y. XIA, North Carolina State University 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs AIAA-2014-0224 AIAA-2014-0225 AIAA-2014-0226 AIAA-2014-0227 AIAA-2014-0228 AIAA-2014-0229 Implicit Large Eddy Simulation Hybrid RANS-LES Modeling Development of a coupled Evolving Solutions: Distributed High Reynolds Number Steady Numerical Prediction of Three- of Turbulent Flows by a Using a Low-Reynolds-Number compressible pressure-based computing and cutback trailing State Flow Simulation using Dimensional Non-Equilibrium Reconstructed Discontinuous k-ω Based Model solver edges Immersed Boundary Method Flows Using the Regularized Galerkin Method S. Arvidson, Saab, Linköping, P. Kambrath, A. Cary, The Boeing R. Watson, P. Tucker, University Y. Takahashi, T. Imamura, University Gaussian Moment Closure Y. Xia, H. Luo, North Carolina State Sweden; L. Davidson, Chalmers Company, St. Louis, MO of Cambridge, Cambridge, United of Tokyo, Tokyo, Japan C. Lam, C. Groth, University of University, Raleigh, NC University of Technology, Göteborg, Kingdom Toronto, Toronto, Canada Sweden; S. Peng, Swedish Defense Research Agency (FOI), Stockholm, Sweden Monday, 13 January 2014 61-FD-9 Jet Flows Maryland Ballroom 6 Chaired by: L. FUCHS, Lund University and R. BAURLE, NASA Langley Research Center 1430 hrs 1500 hrs 1530 hrs AIAA-2014-0230 AIAA-2014-0231 AIAA-2014-0232 Structural and Stability Vibrational Non-equilibrium Wedge Shock and Nozzle Characteristics of Jets in Effects in Supersonic Jet Mixing Exhaust Plume Interaction in a Crossflow H. Reising, U. Kc, S. Voelkel, N. Supersonic Jet Flow L. Gevorkyan, D. Getsinger, O. Smith, A. Clemens, V. Raman, P. Varghese, R. Castner, K. Zaman, A. Fagan, C. Karagozian, University of California, Los University of Texas, Austin, Austin, Heath, NASA Glenn Research Center, Angeles, Los Angeles, CA TX; et al. Cleveland, OH 67 Monday, 13 January 2014 62-FD-10 Roughness-Influenced Boundary Layer Transition I National Harbor Conf Rm 4 Chaired by: E. WHITE, Texas A&M University and M. KEGERISE, NASA-Langley Research Center 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs AIAA-2014-0233 AIAA-2014-0234 AIAA-2014-0235 AIAA-2014-0236 AIAA-2014-0237 AIAA-2014-0238 The Effect of Particle Lag on A Computational Approach Evolution of disturbances Comparing Experiment and Direct Numerical Simulation of Distributed Roughness Effects Supersonic Turbulent Boundary to Simulating the Effects of due to distributed surface Computation of Hypersonic Hypersonic Transition Induced on Blunt-Body Transition and Layer Statistics Realistic Surface Roughness on roughness in laminar Laminar Boundary Layers with by Ramp Roughness Elements Turbulent Heating K. Lowe, G. Byun, R. Simpson, Boundary Layer Transition boundary layers Isolated Roughness Z. Duan, Z. Xiao, S. Fu, Tsinghua B. Hollis, NASA Langley Research Virginia Polytechnic Institute and C. Langel, R. Chow, C. Van Dam, A. Sharma, S. Drews, University B. Bathel, NASA Langley Research University, Beijing, China Center, Hampton, VA State University, Blacksburg, VA University of California, Davis, Davis, of Texas, Austin, Austin, TX; M. Center, Hampton, VA; P. Iyer, University CA; M. Rumsey, D. Maniaci, Sandia Kuester, Texas A&M University, of Minnesota, Minneapolis, Minneapolis, National Laboratories, Albuquerque, College Station, TX; D. Goldstein, MN; P. Danehy, J. Inman, S. Jones, NM; R. Ehrmann, Texas A&M University of Texas, Austin, Austin, NASA Langley Research Center, University, College Station, TX; et al. TX; E. White, Texas A&M University, Hampton, VA; K. Mahesh, University of College Station, TX Minnesota, Minneapolis, Minneapolis, MN; et al. Monday, 13 January 2014 63-FD-11 Solver Technology for Turbulent Flows II National Harbor Conf Rm 3 Chaired by: W. ANDERSON, SimCenter at University of Tennessee at Chattanooga and E. SHIMA, Japan Aerospace Exploration Agency 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs Oral Presentation (Invited) AIAA-2014-0239 AIAA-2014-0240 AIAA-2014-0241 AIAA-2014-0242 AIAA-2014-0243 Numerical and Modeling Issues Verification and validation of Turbulent Flow Solver Validation Assessment of an Unstructured Steady three-dimensional Stanford University Unstructured in Steady Reynolds-averaged the Onera elsA flow solver on of FaSTAR and UPACS CFD Solver for RANS turbulent flow computations (SU2): Analysis and Design Navier-Stokes Equations RANS benchmarks A. Hashimoto, M. Murayama, K. Simulation on Body-Fitted with a parallel Newton-Krylov- Technology for Turbulent Flows J. Bussoletti, D. Kamenetskiy, The L. Cambier, V. Gleize, M. Julien, Yamamoto, T. Aoyama, Japan Cartesian Grids Schur algorithm F. Palacios, Stanford University, Boeing Company, Seattle, WA; ONERA, Châtillon, France Aerospace Exploration Agency T. Haga, K. Kuzuu, R. Takaki, E. M. Osusky, D. Zingg, University of Stanford, CA; K. Duraisamy, University F. Johnson, Self, Seattle, WA; L. (JAXA), Chofu, Japan; K. Tanaka, Shima, Japan Aerospace Exploration Toronto, Toronto, Canada of Michigan, Ann Arbor, Ann Arbor, MI; Wigton, V. Venkatakrishnan, The Ryoyu Systems Company, Ltd., Agency (JAXA), Sagamihara, Japan A. Aranake, S. Copeland, T. Economon, Boeing Company, Seattle, WA Nagoya, Japan A. Lonkar, Stanford University, Stanford, CA; et al. Monday, 13 January 2014 64-FD-12 Turbulence I: Jets and Wakes Chesapeake Conf Rm 8 Chaired by: M. PLESNIAK, George Washington University and P. SHEA, Syracuse University 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs AIAA-2014-0244 AIAA-2014-0245 AIAA-2014-0246 AIAA-2014-0247 AIAA-2014-0248 AIAA-2014-0249 Dynamics of Conserved Scalar Low-Dimensional Modeling of Numerical Simulations of a Wing Performance Insight Flow Phenomena in the Very Unsteady Numerical Simulations Mixing and Transport in Gas- a Mach 0.6 Axisymmetric Jet Particle-Laden Rectangular from the Self-Preserved Near Wake of a Flat Plate with of HTV-R Reentry Capsule by Phase Turbulent Jets P. Shea, Z. Berger, M. Berry, M. Supersonic Jet Impinging on a Turbulent Wake a Circular Trailing Edge Using Detached-Eddy Simulation M. Papageorge, F. Fuest, J. Sutton, Glauser, Syracuse University, Solid Wall S. Gunasekaran, A. Altman, M. Rai, NASA Ames Research Center, K. Takii, M. Kanazaki, Tokyo Ohio State University, Columbus, OH Syracuse, NY; S. Gogineni, Spectral K. Akhtar, S. Ragab, Virginia University of Dayton, Dayton, OH Moffett Field, CA Metropolitan University, Tokyo, Japan; K. Energies, LLC, Dayton, OH Ishiko, A. Hashimoto, T. Aoyama, Japan

68 Polytechnic Institute and State University, Blacksburg, VA Aerospace Exploration Agency (JAXA), Tokyo, Japan Monday, 13 January 2014 65-FD-13 Wing Aerodynamics Maryland Ballroom 2 Chaired by: C. KIRIS and D. KESSLER, Naval Research Laboratory 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs AIAA-2014-0250 AIAA-2014-0251 AIAA-2014-0252 AIAA-2014-0253 AIAA-2014-0254 AIAA-2014-0255 Transitional Flow over a Inclusion of Aeroelastic Twist Characterization of the flow Linear Stability Analysis of Modeling low-Reynolds- Curvature Effects of a SD7003 Wing Using Flux into the CFD Analysis of the field over a NACA 0015 airfoil Laminar Separation Bubble number flow over rough Cycloidally Rotating Airfoil Reconstruction Scheme Twin-Engine NASA Common using Stochastic estimation over NACA0012 airfoil at Low airfoils C. Fagley, C. Porter, T. McLaughlin, V. Skarolek, K. Miyaji, Yokohama Research Model based surface pressure and Reynolds Numbers D. Kessler, A. Corrigan, S. Qidwai, J. U.S. Air Force Academy, Colorado National University, Yokohama, K. Benedict, L. Hedges, A. Robinson, hot film measurements E. Jeyapandian, Infotech Enterprises, Thomas, Naval Research Laboratory, Springs, CO Japan Stark-AMI, Redmond, WA; P. E. Caraballo, T. Sullivan, R. You, Ltd., Bangalore, India; R. Mukherjee, Washington, DC Peddiraju, A. Papadopoulos, BETA Miami University, Oxford, OH; J. Indian Institute of Technology CAE Systems, Farmington Hills, MI; Little, University of Arizona, Tucson, Madras, Chennai, India V. Skaperdas, BETA CAE Systems, Tucson, AZ Thessaloniki, Greece; et al. Monday, 13 January 2014 66-GEPC-1 Progress in NASA’s Environmentally Responsible Aviation Project Woodrow Wilson A Chaired by: F. COLLIER, NASA-Langley Research Center 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs Oral Presentation (Invited) AIAA-2014-0256 AIAA-2014-0257 AIAA-2014-0258 Oral Presentation (Invited) AIAA-2014-0259 Status of the Environmentally Hybrid Wing Body Shielding Noise and Fuel Burn System Noise Assessment and An Overview of Flap and PRSEUS Structural Concept Responsible Aviation Project Studies using an Ultrasonic Reduction Potential of an the Potential for Low Noise Landing Gear Noise Reduction Development F. Collier, NASA Langley Research Configurable Fan Artificial Innovative Subsonic Transport Hybrid Wing Body Aircraft with M. Khorrami, NASA Langley Research A. Velicki, The Boeing Company, Center, Hampton, VA Noise Source Generating Configuration Open Rotor Propulsion Center, Hampton, VA Huntington Beach, CA; D. Jegley, Typical Turbofan Modes Y. Guo, The Boeing Company, R. Thomas, C. Burley, L. Lopes, NASA Langley Research Center, D. Sutliff, C. Brown, NASA Glenn Huntington Beach, CA; C. Nickol, C. C. Bahr, F. Gern, NASA Langley Hampton, VA Research Center, Cleveland, OH; B. Burley, R. Thomas, NASA Langley Research Center, Hampton, VA; D. Walker, Channel Islands Acoustics, Research Center, Hampton, VA Van Zante, NASA Glenn Research Camarillo, CA Center, Cleveland, OH Monday, 13 January 2014 67-GNC-3 Mini/Micro Air Vehicles I National Harbor Conf Rm 7 Chaired by: J. LANGELAAN, Pennsylvania State University and E. FREW, University of Colorado Boulder 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2014-0260 AIAA-2014-0261 AIAA-2014-0262 AIAA-2014-0263 AIAA-2014-0264 Improving Autonomous Soaring Optimal Persistent Surveillance Efficient Trajectory Closing the Loop in Dynamic Indoor Simulation Platform via Energy State Estimation and using Coordinated Soaring Development for UAS Dynamic Soaring for Forest Fire Detection and Extremum Seeking Control D. Makovkin, J. Langelaan, Soaring Applications J. Bird, J. Langelaan, Pennsylvania Surveillance S. Daugherty, J. Langelaan, Pennsylvania State University, W. Shaw-Cortez, E. Frew, University State University, University Park, PA; H. Zhu, H. Liu, University of Toronto, Pennsylvania State University, University University Park, PA of Colorado, Boulder, Boulder, CO C. Montella, J. Spletzer, J. Grenestedt, Toronto, Canada

69 Park, PA Lehigh University, Bethlehem, PA Monday, 13 January 2014 68-GNC-4 Onboard Systems Technologies for LOC Prevention & Recovery - Improved Situational Awareness, Guidance, and Control, Session (Invited) I National Harbor Conf Rm 12 Chaired by: D. CRIDER, National Transportation Safety Board and E. XARGAY 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs AIAA-2014-0265 AIAA-2014-0266 AIAA-2014-0267 AIAA-2014-0268 AIAA-2014-0269 AIAA-2014-0270 Initial Evaluations of Loss- An Adaptive Unknown Input Estimation of Airspeed Using An Adaptive Nonlinear Aircraft Flight Envelope Protection for Detection of the Impact of Ice of-Control (LOC) Prediction Observer for Fault Detection Continuous Polynomial Maneuvering Envelope NASA’s Transport Class Model Crystal Accretion in an Aircraft Algorithms using the NASA and Isolation of Aircraft Adaptive Estimator Estimation Approach for Online N. Tekles, F. Holzapfel, Technical Engine Compression System Ames Vertical Motion Actuator Faults H. Felemban, J. Che, C. Cao, Applications University of Munich, Garching, During Dynamic Operation Simulator H. Lee, S. Snyder, N. Hovakimyan, University of Connecticut, Storrs, S. Schuet, NASA Ames Research Center, Germany; E. Xargay, R. Choe, N. R. May, Vantage Partners, LLC, K. Krishnakumar, NASA Ames University of Illinois, Urbana- Storrs, CT; N. Hovakimyan, University Moffett Field, CA; T. Lombaerts, German Hovakimyan, University of Illinois, Cleveland, OH; T. Guo, D. Simon, Research Center, Moffett Field, CA Champaign, Urbana, IL of Illinois, Urbana-Champaign, Aerospace Center (DLR), Wessling, Urbana-Champaign, Urbana, IL; I. NASA Glenn Research Center, Urbana, IL; I. Gregory, NASA Langley Germany; D. Acosta, K. Wheeler, J. Gregory, NASA Langley Research Cleveland, OH Research Center, Hampton, VA Kaneshige, NASA Ames Research Center, Center, Hampton, VA Moffett Field, CA Monday, 13 January 2014 69-GNC-5 Space Exploration and Transportation National Harbor Conf Rm 6 Chaired by: J. REED, United Launch Alliance 1430 hrs 1500 hrs 1530 hrs 1600 hrs AIAA-2014-0271 AIAA-2014-0272 AIAA-2014-0273 AIAA-2014-0274 LPV techniques for the control of Stereo Vision Algorithm for Development of an Eddy- Stationkeeping Strategy and an airborne micro-launcher Hazard Detection during Current Actuator Test Bed Possible Lunar Halo Orbits for J. Bordeneuve-Guibé, D. Alazard, Planetary Landings B. Reinhardt, M. Peck, B. Hencey, Long-Term Space Station University of Toulouse, Toulouse, S. Woicke, E. Mooij, Delft University Cornell University, Ithaca, NY Y. Ulybyshev, RSC Energia, Korolev, France; J. Desmariaux, French Space of Technology, Delft, The Netherlands Russia Agency (CNES), Evry, France Monday, 13 January 2014 70-GT-2 NASA’s ATP National Force Measurement Project Update (Invited) Maryland Ballroom B Chaired by: R. RHEW, NASA-Langley Research Center and K. LYNN, NASA Langley Research Center 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs Oral Presentation (Invited) AIAA-2014-0275 Oral Presentation (Invited) AIAA-2014-0276 AIAA-2014-0277 AIAA-2014-0278 Partnership for the High-Reynolds Number AFRL/AEDC on un-start Loads Experimental Design Strain Gage Load Calibration Rotating Balances used for Revitalization of National Wind Active Blowing Semi-Span at High Incidence Angles Considerations for Calibration of the Wing Interface Fittings Fluid Pump Testing Tunnel Force Measurement Force Measurement System R. Guyton, Air Force Research of Semi Span Force for the Adaptive Compliant S. Skelley, NASA Marshall Space Capability (Revisited) Development (Revisited) Laboratory, Wright-Patterson AFB, OH Measurement Systems Trailing Edge Flap Flight Test Flight Center, Huntsville, AL K. Lynn, NASA Langley Research K. Lynn, NASA Langley Research S. Commo, NASA Langley Research E. Miller, A. Holguin, J. Cruz, W. Center, Hampton, VA Center, Hampton, VA Center, Hampton, VA Lokos, NASA Dryden Flight Research Center, Edwards, CA Monday, 13 January 2014 71-GT-3 Rapid Prototyping Applications in Ground Testing National Harbor Conf Rm 10 Chaired by: T. WAYMAN, Gulfstream Aerospace Corporation 1430 hrs 1500 hrs 1530 hrs 1600 hrs Oral Presentation (Invited) Oral Presentation (Invited) Oral Presentation (Invited) Panel Discussion Rapid Prototyping Methods Rapid Prototype Use in Wind Rapid Prototyping Methods for for Wind Tunnel Testing at Tunnel Models - The Boeing Wind Tunnel Testing at NASA Lockheed Martin Company Langley W. Baker, Lockheed Martin D. Belter, The Boeing Company, C. Laws, NASA Langley Research Corporation, Fort Worth, TX Seattle, WA Center, Hampton, VA Monday, 13 January 2014

70 72-GTE-2 Film Cooling Woodrow Wilson D Chaired by: D. BLUNCK, Air Force Reseach Laboratory and G. PANIAGUA, von Karman Institute 1430 hrs 1500 hrs AIAA-2014-0279 AIAA-2014-0280 Predicting Film Cooling An Experimental Study of Performance of Trailing-Edge Momentum-Preserving Shaped Cutback Turbine Blades by Holes for Film Cooling Using Detached-eddy Simulation PSP and PIV M. Effendy, Kingston University, London, W. Zhou, B. Johnson, H. Hu, Iowa United Kingdom; Y. Yao, University of State University, Ames, IA the West of England, Bristol, United Kingdom; J. Yao, University of Lincoln, Lincoln, United Kingdom; D. Marchant, Kingston University, London, United Kingdom Monday, 13 January 2014 73-HIS-2 History Session: Pioneering Contributions to Aeronautics National Harbor Conf Rm 15 Chaired by: C. MARTIN, NASA-Dryden Flight Research Center 1430 hrs 1500 hrs 1530 hrs 1600 hrs Oral Presentation (Invited) AIAA-2014-0281 AIAA-2014-0282 AIAA-2014-0283 Aeronautics - NASA’s First ‘A’ & The Public Domain, The Father Bartholomeu Lourenço The Navy’s Aerodynamics STOL Research 1960s - 1970s National Interest and The Fate de Gusmão: a Charlatan or Laboratory - 100 years of R. Ferguson, Historian of Technology of the NASA Technical Reports the First Practical Pioneer of Experimental Aerodynamics & Ramsey Fellow Server Aeronautics in History from A-1 to DDG-1000 T. Takahashi, Arizona State J. Melo De Sousa, Technical D. Haas, E. Silberg, K. Kimmel, University, Tempe, AZ University of Lisbon, Lisbon, Portugal Naval Surface Warfare Center, West Bethesda, MD Monday, 13 January 2014 74-HSABP-1 Pressure Gain Combustion I Chesapeake Conf Rm 7 Chaired by: T. O’BRIEN, Aerojet Rocketdyne and V. TANGIRALA, General Electric 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2014-0284 AIAA-2014-0285 AIAA-2014-0286 AIAA-2014-0287 AIAA-2014-0288 Numerical Analysis of a Comparative Numerical Study Cavity Ignition in Supersonic Rotating Detonation Engine Rapid Mixing of a Wall Rotating Detonation Engine in of RDE Injection Designs Flow by Pulse Detonation Interaction with an Annular Injectant in a Mach 2 Cross the Relative Reference Frame W. Stoddard, E. Gutmark, University T. Ombrello, C. Carter, Air Force Ejector Flow Using a Pulse Detonator D. Paxson, NASA Glenn Research of Cincinnati, Cincinnati, OH Research Laboratory, Wright- A. Naples, J. Hoke, Innovative W. Haw, P. King, Air Force Institute Center, Cleveland, OH Patterson AFB, OH; C. Tam, Taitech, Scientific Solutions, Inc., Dayton, of Technology, Wright-Patterson Inc., Dayton, OH; K. Hsu, Innovative OH; F. Schauer, Air Force Research AFB, OH; T. Ombrello, C. Carter, Air Scientific Solutions, Inc., Dayton, OH Laboratory, Wright-Patterson AFB, OH Force Research Laboratory, Wright- Patterson AFB, OH Monday, 13 January 2014 75-ISC-4 International Student Conference - Community Outreach Division Potomac Ballroom 3 Chaired by: C. BLOMBERG 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs Oral Presentation (Invited) Oral Presentation (Invited) Oral Presentation (Invited) Oral Presentation (Invited) Oral Presentation (Invited) Oral Presentation (Invited) Atmospheric Teaching MSU Space Cowboy’s Community University of Illinois at Chicago Texas A&M Sigma Gamma Tau Miners in Space Microgravity ASU/NASA Space Grant Experiment at Virginia Tech Outreach 2012-2013 Student Branch Community Community Outreach Research Outreach Outreach Program Outreach A. Sanford, D. Brown, Mississippi State Outreach 2012-2013 S. De Hoog, M. Pierce, A. Probe, E. Nickel, Missouri University of Science R. Gomez, D. Ixtabalan, Arizona K. Mosier, J. Jenkins, Virginia University, Mississippi State, MS O. Wingfield, University of Illinois, Texas A&M University, College and Technology, St. Louis, MO State University, Tempe, AZ Polytechnic Institute and State Chicago, Chicago, IL Station, TX University, Blacksburg, VA

71 Monday, 13 January 2014 76-LECT-2 MDO Special Session: MDAO - A Chief Engineer’s Perspective on this Key Development Capability Maryland Ballroom C 1430 - 1530 hrs William Carrier Vice President of Engineering Boeing Monday, 13 January 2014 77-MDO-2 Aerodynamic and Aircraft Optimization Chesapeake Conf Rm 4 Chaired by: S. RALLABHANDI, National Institute of Aerospace and J. HICKEN, Rensselaer Polytechnic Institute 1430 hrs 1530 hrs 1600 hrs 1630 hrs No Presentations AIAA-2014-0289 AIAA-2014-0290 AIAA-2014-0291 Multi-objective Airfoil Design Multi-point Adjoint-Based Aerodynamic Optimization of Using Variable-Fidelity CFD Design of Tilt-Rotors in a High-Wing Configuration for Simulations and Response Noninertial Reference Frame Near Future Aircraft Surface Surrogates W. Jones, E. Nielsen, E. Lee-Rausch, A. Hashimoto, S. Obayashi, Tohoku S. Koziel, L. Leifsson, Reykjavik NASA Langley Research Center, University, Sendai, Japan; S. Jeong, University, Reykjavik, Iceland Hampton, VA; C. Acree, NASA Ames Kyunghee University, Yongin, South Research Center, Moffett Field, CA Korea Monday, 13 January 2014 78-MVC-2 Integrated Computational Environments Chesapeake Conf Rm 9 Chaired by: N. TAYLOR, MBDA UK Limited and C. BRUNER, Sandia National Laboratories 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs AIAA-2014-0292 AIAA-2014-0293 AIAA-2014-0294 AIAA-2014-0295 AIAA-2014-0296 AIAA-2014-0297 Compression of Finite-Element FD-CADRE 2.0: A Flexible, Conservative Fitting for Multi- Developing an Integrated Evolutionary Optimization A Purposed Model Coupling Node Maps with Sub-Zone MPI-based Framework for Disciplinary Analysis Computational Environment of Multiscale Systems within Framework for the Rapid Load-On-Demand Moving Body and Multi- J. Dannenhoffer, Syracuse for the Detailed Design of a an Integrated Computational Assembly of Complex S. Imlay, C. Mackey, Tecplot, Inc., Disciplinary Simulations University, Syracuse, NY; R. Mixing Impeller Design Environment System Simulations within Bellevue, WA G. Power, C. Robinson, Aerospace Haimes, Massachusetts Institute of B. Sloan, K. Bryden, S. Suram, Ames Z. Reinhart, K. Bryden, Ames an Integrated Computational Testing Alliance, Arnold AFB, TN Technology, Cambridge, MA Laboratory, Ames, IA Laboratory, Ames, IA Environment G. McNunn, K. Bryden, Ames Laboratory, Ames, IA Monday, 13 January 2014 79-NDA-2 Uncertainty Quantification Methods Chesapeake Conf Rm 5 Chaired by: S. MAHADEVAN, Vanderbilt University and S. VENKATARAMAN, San Diego State University 1430 hrs 1530 hrs 1600 hrs 1630 hrs No Presentations AIAA-2014-0298 AIAA-2014-0299 AIAA-2014-0300 A Mixed Uncertainty Uncertainty Propagation Quantification of Margins and Quantification Approach with with Monotonicity Preserving Mixed Uncertainties Using Evidence Theory and Stochastic Robustness Evidence Theory and Stochastic Expansions J. Witteveen, Center for Mathematics Expansions H. Shah, S. Hosder, Missouri and Computer Science (CWI), H. Shah, S. Hosder, Missouri University of Science and Amsterdam, The Netherlands; G. University of Science and

72 Technology, Rolla, MO; T. Winter, M4 Iaccarino, Stanford University, Palo Technology, Rolla, MO; T. Winter, M4 Engineering, Inc., Long Beach, CA Alto, CA Engineering, Inc., Long Beach, CA Monday, 13 January 2014 80-OPS-1 Space Operations & Support National Harbor Conf Rm 8 Chaired by: L. BRYANT, Jet Propulsion Laboratory 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2014-0301 AIAA-2014-0302 AIAA-2014-0303 AIAA-2014-0304 AIAA-2014-0305 Debris Removal to Reduce Risk Soft Factors and Space Interplanetary Nuclear Range Safety Assessment Earth-to-Moon Low-Energy D. Finkleman, International Mission Failures: Quantifying Thermal Propulsion Shuttle Tool (RSAT): An analysis Transfers by Using Spatial Association for the Advancement the Effects of Management G. Falcone, S. Olcmen, University of environment for safety Transit Orbits of Space Safety, Noordwijk, The Decisions Alabama, Tuscaloosa, Tuscaloosa, AL assessment of launch and Y. Ren, J. Shan, York University, Netherlands L. Bryant, L. Meshkat, B. Waggoner, reentry vehicles Toronto, Canada R. Thomas, Jet Propulsion F. Capristan, J. Alonso, Stanford Laboratory, California Institute of University, Stanford, CA Technology, Pasadena, CA Monday, 13 January 2014 81-PANEL-2 Aeronautics R&D Policy and the Strategic Direction of NASA’s Aeronautics Research Panel Potomac Ballroom C 1430 - 1630 hrs Moderator: Robert Pearce, Director – Strategy, Architecture & Analysis, NASA Aeronautics Research Mission Directorate Panelists: Marion Blakey Alan Epstein Les Lyles Jaiwon Shin President and Chief Executive Officer Vice-President, Technology and Environment Consultant Associate Administrator for Aeronautics Research Mission Directorate Aerospace Industries Association Pratt & Whitney The Lyles Group NASA Headquarters Monday, 13 January 2014 82-PC-4 Jet Fuel Surrogate Models and Kinetics (Invited) Chesapeake Conf Rm I Chaired by: C. LI, Air Force Office of Scientific Research and Y. JU, Princeton University 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs Oral Presentation (Invited) Oral Presentation (Invited) Oral Presentation (Invited) AIAA-2014-0306 Oral Presentation (Invited) Oral Presentation (Invited) Challenges and Uncertainties Jet Fuel Combustion Kinetics Developing a detailed chemical Recent advances in chemical Development of Detailed and Uncertainty in A Priori Kinetics in Use of Surrogate Fuels - From Detailed Modeling to kinetic mechanism for large kinetics of jet fuels Reduced Kinetic Models for Predictions for Emulating Combustor Lumping jet-fuels: A focus on propene C. Westbrook, Lawrence Livermore Real Jet Fuels: Challenges and S. Klippenstein, Argonne National Performance H. Wang, Stanford University, chemistry National Laboratory, Livermore, CA Opportunities Laboratory, Argonne, IL M. Colket, United Technologies Stanford, CA H. Curran, National University of S. Won, Princeton University, Princeton, Corporation, New Haven, CT Ireland, Galway, Ireland NJ; S. Dooley, University of Limerick, Limerick, Ireland; T. Farouk, University of South Carolina, Columbia, Columbia, SC; F. Dryer, Y. Ju, Princeton University, Princeton, NJ Monday, 13 January 2014 83-PC-5 Rockets and Airbreathing Propulsion II Chesapeake Conf Rm G Chaired by: Z. JIANG and J. OEFELEIN, Sandia National Laboratories 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs AIAA-2014-0307 AIAA-2014-0308 AIAA-2014-0309 AIAA-2014-0310 AIAA-2014-0311 AIAA-2014-0312

Numerical study on mixing Large Eddy Simulation of CH4/O2 Research on the Combustion Numerical Simulations Large-Eddy Simulation of a On the Stochastic Modeling characteristics of coaxial Combustion of a Swirl-Coaxial of Bio-Derived Fuels in Hybrid of Combustive Flows in a Supersonic Burner of Subcritical Primary cryogenic N2/H2 injection Injector Propellant Rocket Engine Swirling-Oxidizer-Flow-Type G. Ribert, L. Bouheraoua, P. Atomization in Liquid Rocket under supercritical pressure S. Matsuyama, Japan Aerospace V. Naoumov, N. Knochenhauer, P. Hybrid Rocket Domingo, National Center for Engines Scientiﬁc Research (CNRS), St- 73 H. Terashima, M. Koshi, University of Exploration Agency (JAXA), Chofu, Sansevero, G. Adam, C. Freeto, T. M. Motoe, University of Tokyo, M. Kumar, Y. Sun, S. Thakur, Tokyo, Tokyo, Japan Japan Kimiecik, Central Connecticut State Bunkyo, Japan; T. Shimada, Japan Étienne-du-Rouvray, France University of Florida, Gainesville, University, New Britain, CT; et al. Aerospace Exploration Agency Gainesville, FL (JAXA), Sagamihara, Japan Monday, 13 January 2014 84-PC-6 Turbulent Flames I Chesapeake Conf Rm H Chaired by: M. IHME and L. SMITH, United Technologies Research Center 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs AIAA-2014-0313 AIAA-2014-0314 AIAA-2014-0315 AIAA-2014-0316 AIAA-2014-0317 AIAA-2014-0318 Detailed Characterization of Experimental Investigation OH PLIF Laser Diagnostics Investigation of Turbulent Multi-Point and Multi-Time Experimental Investigation Low Temperature Chemistry of Premixed Turbulent of Turbulent, Compressible, Lifted Planar Jet Flames Using Statistics of Temperature on Flow Characteristics of the and Turbulence Interaction Combustion in High Reynolds Premixed, Freely Propagating Highspeed Laser Imaging within Turbulent Non-Premixed Flash Swirl Spray in Reactor-Assisted Turbulent Number Regimes using PLIF Flame Kernels Diagnostics Jet Flames Using High-Speed H. Kim, W. Yoon, Yonsei University, Premixed Flames J. Temme, A. Skiba, T. Wabel, J. N. Grady, R. Pitz, Vanderbilt University, I. Boxx, German Aerospace Center Planar Rayleigh Scattering Seoul, South Korea B. Windom, S. Won, B. Jiang, Y. Ju, Driscoll, University of Michigan, Ann Nashville, TN; S. Menon, B. Ochs, T. (DLR), Stuttgart, Germany; C. Carter, T. McManus, M. Papageorge, Princeton University, Princeton, NJ Arbor, Ann Arbor, MI Slais, J. Berlette, Georgia Institute of Air Force Research Laboratory, F. Fuest, J. Sutton, Ohio State Technology, Atlanta, GA; et al. Wright-Patterson AFB, OH; W. Meier, University, Columbus, OH German Aerospace Center (DLR), Stuttgart, Germany Monday, 13 January 2014 85-PDL-3 AeroOptics Azalea 3 Chaired by: M. VISBAL, USAF AFRL/RBAC 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2014-0319 AIAA-2014-0320 AIAA-2014-0321 AIAA-2014-0322 AIAA-2014-0323 Estimation of Aero-Optical Numerical Simulation of aero- Aero-Optical Mitigation of Effect of Surface Unsteady LES Analysis of Hemisphere- Wavefronts Using Optical and optical aberrations in shock/ Turbulent Boundary Layers Pressure Field on Global Beam on-Cylinder Turret Aero-Optics Non-Optical Measurements boundary layer interactions Using Large-Eddy Break-Up Jitter for a Hemisphere-on- E. Mathews, K. Wang, M. Wang, E. R. Burns, S. Gordeyev, E. Jumper, (SBLIs) Devices Cylinder Turret Jumper, University of Notre Dame, University of Notre Dame, Notre M. White, Ohio Aerospace Institute, A. Smith, S. Gordeyev, University of N. De Lucca, S. Gordeyev, E. Jumper, Notre Dame, IN Dame, IN; S. Gogineni, Spectral Dayton, OH; M. Visbal, Air Force Notre Dame, Notre Dame, IN University of Notre Dame, Notre Energies, LLC, Dayton, OH; M. Research Laboratory, Wright- Dame, IN Paul, D. Wittich, Air Force Research Patterson AFB, OH Laboratory, Kirtland AFB, NM Monday, 13 January 2014 86-PDL-4 Plasma-Actuators and Flow Control II Maryland Ballroom 1 Chaired by: S. ROY, University of Florida 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs AIAA-2014-0324 AIAA-2014-0325 AIAA-2014-0326 AIAA-2014-0327 AIAA-2014-0328 AIAA-2014-0329 Modeling surface plasma NS-DBD plasma actuation on a Evaluating Force Field induced Comparison of Velocities Driven Thrust produced by corona Dielectric Barrier Discharge actuator for ﬂow control backward facing step by a Plasma Actuator using by Repetitive Nanosecond Pulses discharge - Application Development and Thrust J. Shang, G. Huang, Wright State G. Correale, T. Michelis, M. Kotsonis, the Reynolds-Averaged Navier vs AC Result to electrohydrodynamic Generation at Low and High University, Dayton, OH Delft University of Technology, Delft, Stokes Equation J. Li, J. Wang, X. Meng, Northwestern propulsion Pressure Conditions The Netherlands S. Grundmann, K. Barckmann, Polytechnical University, Xi’an, China; E. Moreau, N. Benard, University of S. Gordon, M. Post, A. Starikovskiy, F. Liu, S. Luo, University of California,

74 I. Maden, Technical University of Poitiers, Futuroscope, France; J. Lan R. Miles, Princeton University, Darmstadt, Darmstadt, Germany; Irvine, Irvine, CA Sun Luk, J. Chabriat, University of La Princeton, NJ J. Kriegseis, Karlsruhe Institute of Réunion, Saint Denis, France Technology, Karlsruhe, Germany Monday, 13 January 2014 87-SD-3 Aircraft Dynamics and Vibration Chesapeake Conf Rm B Chaired by: W. SCHNEIDER, Lockheed Martin Aeronautics and E. MCDONALD, Dynamic Concepts, Inc. 1430 hrs 1530 hrs 1600 hrs 1630 hrs No Presentations AIAA-2014-0330 AIAA-2014-0331 AIAA-2014-0333 In-Flight Wing Deformation Deformation Tracking of a Validation of an UAV F.E. Measurement System for Small Flexible Fence Model Using Operational Data Unmanned Aerial Vehicles J. Seidel, G. Womack, U.S. Air Force G. Coppotelli, M. Arras, C. Grappasonni, Z. Pang, C. Cesnik, E. Atkins, University Academy, Colorado Springs, CO University of Rome “La Sapienza”, of Michigan, Ann Arbor, Ann Arbor, MI Rome, Italy; P. Marzocca, D. Valyou, J. Miller, Clarkson University, Potsdam, NY Monday, 13 January 2014 88-SD-4 Computational Aeroelasticity I Chesapeake Conf Rm C Chaired by: B. GLAZ, U. S. Army Research Laboratory (APG) and D. PITT, Boeing Engineering Operations & Technology 1430 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs No Presentations AIAA-2014-0334 AIAA-2014-0335 AIAA-2014-0336 AIAA-2014-0337 Aeroelastic Response of Bird- Nonlinear Aeroelastic Analysis Higher-Order Transonic Flutter Efficient Time-Marching of Damaged Fan Blades Using a of a Truss Based Wing Aircraft Solutions Fluid-Thermal-Structural Coupled CFD/CSD Framework J. Coggin, R. Kapania, J. Schetz, H. M. Bhatia, P. Beran, Air Force Interactions E. Muir, P. Friedmann, University of Vijayakumari, Virginia Polytechnic Research Laboratory, Wright- B. Miller, J. McNamara, Ohio State Michigan, Ann Arbor, Ann Arbor, MI Institute and State University, Patterson AFB, OH University, Columbus, OH Blacksburg, VA; W. Zhao, University of Surrey, Guilford, United Kingdom Monday, 13 January 2014 89-SRE-1 In-Situ Resources: Identification and Manipulation National Harbor Conf Rm 14 Chaired by: D. LINNE, NASA Glenn Research Center and S. SCHMIDT, Northern Centre for Advanced Technology Inc 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2014-0338 AIAA-2014-0339 AIAA-2014-0340 AIAA-2014-0341 AIAA-2014-0342 Prospecting for Native Metals Wells for In-situ Extraction Production of Aerospace Fuels Electrostatic Particle-Size Flexible Mechanical Conveying in Lunar Polar Craters of Frozen Volatiles from from Non-Petroleum Raw Classification of Lunar Regolith of Regolith Under Micro- D. Boucher, NORCAT, Sudbury, Subsurface Lunar (or Materials: Technical Challenges for In-Situ Resource Utilization Gravity Canada; W. Platts, Groundhog Planetary) Regolith and Technology Opportunities H. Kawamoto, Waseda University, O. Walton, H. Vollmer, B. Vollmer, L. Geoscience, Pinedale, WY O. Walton, Grainflow Dynamics, Inc., A. Hepp, M. Kulis, NASA Glenn Tokyo, Japan Figueroa, Grainflow Dynamics, Inc., Livermore, CA Research Center, Cleveland, OH; Livermore, CA; A. Abdel-Hadi, Auburn M. Timko, Worcester Polytechnic University, Auburn, AL Institute, Worcester, MA; P. Psarras, D. Ball, Cleveland State University, Cleveland, OH; H. Wong, Aerodyne Research, Inc., Billerica, MA; et al. Monday, 13 January 2014 90-STR-4 Aeroelastic Analysis Chesapeake Conf Rm E Chaired by: K. GRIFFIN, Southwest Research Institute and Z. SOTOUDEH, Rensselaer Polytechnic Institute 1430 hrs 1530 hrs 1600 hrs 1630 hrs No Presentations AIAA-2014-0343 AIAA-2014-0344 AIAA-2014-0345 Optimisation of Tow-Steered Aeroelastic Tailoring of a Plate A Nonlinear Controller for Flutter Composite Wing Laminates for Wing with Functionally Graded Suppression: from Simulation to Aeroelastic Tailoring Materials Wind Tunnel Testing

75 O. Stodieck, J. Cooper, P. Weaver, P. Dunning, National Institute of A. Da Ronch, University of University of Bristol, Bristol, United Aerospace, Hampton, VA; B. Stanford, Southampton, Southampton, United Kingdom; P. Kealy, Airbus, Bristol, NASA Langley Research Center, Kingdom; N. Tantaroudas, K. Badcock, United Kingdom Hampton, VA; H. Kim, University J. Mottershead, University of Liverpool, of Bath, Bath, United Kingdom; C. Liverpool, United Kingdom Jutte, Craig Technologies, Inc., Cape Canaveral, FL Monday, 13 January 2014 91-STR-5 Special Session on Open Source Software Chesapeake Conf Rm D Chaired by: P. GUSTAFSON, Western Michigan University and A. NAJAFI, ANSYS, Inc. 1430 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs No Presentations AIAA-2014-0346 AIAA-2014-0347 AIAA-2014-0348 AIAA-2014-0349 Implementation of the CUDA Where Open Source FEA Fits in Open Source Software R: an opensource system for Cusp and CHOLMOD Solvers the CAE Ecosystem and What for Monte Carlo/DSMC statistics and data exploration in CalculiX to Know Before Adopting Applications J. Kapenga, J. McKean, Western P. Gustafson, J. Kapenga, Western J. Baylor, Convergent Mechanical E. de Doncker, J. Kapenga, Western Michigan University, Kalamazoo, MI Michigan University, Kalamazoo, MI Solutions, Seattle, WA Michigan University, Kalamazoo, MI Monday, 13 January 2014 92-STR-6 Space Structures Chesapeake Conf Rm F Chaired by: J. DOMBER, Ball Aerospace & Technologies Corporation and J. ZIPAY, NASA-Johnson Space Center 1430 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs No Presentations AIAA-2014-0350 AIAA-2014-0351 AIAA-2014-0352 AIAA-2014-0353 Preliminary Development of a Analysis of Reusable Long Term Displacement Data Photogrammetry Analysis Multifunctional Hot Structure Integrated Thermal Protection of Woven Fabric Webbings of a Hypersonic Inflatable Heat Shield Panel Elements with Various under Constant Load for Aerodynamic Decelerator S. Walker, K. Daryabeigi, J. Insulating Core Options Inflatable Structures Structural Test Article Samareh, S. Armand, NASA Langley F. Jiang, Z. Ye, W. Yu, Utah State S. Kenner, NASA Langley Research L. Li, R. Braun, Georgia Institute of Research Center, Hampton, VA University, Logan, UT; R. Kerans, Air Center, Hampton, VA Technology, Atlanta, GA; A. Cassell, Force Research Laboratory, Wright- NASA Ames Research Center, Moffett Patterson AFB, OH Field, CA Monday, 13 January 2014 93-SUR-1 Air and Space Survivability Chesapeake Conf Rm A Chaired by: S. POROSEVA, The University of New Mexico and J. RIMOLI, Georgia Institute of Technology 1430 hrs 1530 hrs 1600 hrs 1630 hrs No Presentations AIAA-2014-0354 AIAA-2014-0355 AIAA-2014-0356 An Approach for Evaluating Analysis of Aircraft Application of the “Selfish” Potential Aircraft Casualties Survivability Against Algorithm for the Survivability from Combat Threats Fragmenting Warhead Threat Analysis of Systems with J. Williamsen, J. Rhoads, M. Couch, H. Konokman, Scientific and Multiple Loads Institute for Defense Analyses, Technological Research Council of S. Poroseva, J. Lowe, B. Kaiser, Alexandria, VA Turkey (TÜBITAK), Ankara, Turkey; University of New Mexico,

76 A. Kayran, Middle East Technical Albuquerque, Albuquerque, NM University, Ankara, Turkey; M. Kaya, University of Turkish Aeronautical Association, Ankara, Turkey Monday, 13 January 2014 94-WE-3 Blade and Turbine Design I National Harbor Conf Rm 2 Chaired by: F. GRASSO and D. GRIFFITH 1430 hrs 1500 hrs 1530 hrs 1600 hrs AIAA-2014-0357 AIAA-2014-0358 AIAA-2014-0359 AIAA-2014-0360 Definition of the National Rotor On Calibration of Simpler Comprehensive Aerodynamic Structural Efficiency Analysis Testbed: An Aeroelastically Alternatives to Statistical Load Analysis of a 10 MW Wind of the Sandia 100 m Wind Relevant Research-Scale Wind Extrapolation for Wind Turbine Turbine Rotor Using 3D CFD Turbine Blade Turbine Rotor Design F. Zahle, C. Bak, N. Sørensen, S. N. Buckney, A. Pirrera, P. Weaver, B. Resor, D. Maniaci, Sandia National H. Nguyen, L. Manuel, University of Guntur, N. Troldborg, Technical University of Bristol, Bristol, United Laboratories, Albuquerque, NM Texas, Austin, Austin, TX; M. Barone, University of Denmark, Roskilde, Kingdom; D. Griffith, Sandia National Sandia National Laboratories, Denmark Laboratories, Albuquerque, NM Albuquerque, NM Monday, 13 January 2014 95-WE-4 Offshore Wind Energy Systems Woodrow Wilson B Chaired by: J. JONKMAN, National Renewable Energy Laboratory and J. BAKER, Frontier Wind 1430 hrs 1500 hrs 1530 hrs 1600 hrs AIAA-2014-0361 AIAA-2014-0362 AIAA-2014-0363 AIAA-2014-0364 Effects of Second-Order Development of a Maintenance Wind/Wave Misalignment in Active Horizontal Vane Hydrodynamic Forces on Option Model to Optimize the Loads Analysis of a Floating Control for Stabilizing Floating Offshore Wind Offshore Wind Farm Offshore Wind Turbine Platform Pitch Motion of Turbines Sustainment L. Barj, Pennsylvania State University, Floating Offshore Turbines T. Duarte, A. Sarmento, Technical P. Sandborn, G. Haddad, A. Kashani- University Park, PA; J. Jonkman, A. Y. Li, University of Texas, Dallas, University of Lisbon, Lisbon, Pour, University of Maryland, College Robertson, National Renewable Energy Richardson, TX; Z. Yang, Exa Portugal; J. Jonkman, National Park, College Park, MD Laboratory, Golden, CO; G. Stewart, M. Corporation, Livonia, MI; J. Seem, Renewable Energy Laboratory, Lackner, University of Massachusetts, Johnson Controls, Milwaukee, WI Golden, CO Amherst, Amherst, MA; L. Haid, University of Stuttgart, Stuttgart, Germany; et al. Monday, 13 January 2014 96-LECT-3 Dryden Lectureship: Taking the Hype Out of Hypersonics: Research Contributions to Operational High-Speed-Systems Potomac Ballroom C 1730 - 1830 hrs Mark J. Lewis Director The Science and Technology Policy Institute, Institute for Defense Analyses Tuesday 77 Tuesday, 14 January 2014 97-NW-3 Tuesday Morning Networking Breakfast Exhibit Hall 0700 - 0800 hrs Tuesday, 14 January 2014 98-SB-3 Tuesday Morning Speakers’ Briefing Session Rooms 0730 - 0800 hrs Tuesday, 14 January 2014 99-PLNRY-2 Tuesday Morning Keynote and Plenary Panel Potomac Ballroom A&B 0800 - 0930 hrs Keynote Innovating for an Era of Affordability: The Future of the Space Industry Rick Ambrose Executive Vice President Lockheed Martin Space Systems Company

Plenary Panel: AIAA’s Role in Defining the Future of Aerospace Moderator: Jim Albaugh, President, The Boeing Company (Retired); AIAA President-Elect Panelists: David Hills Ray Johnson Michael Ryschkewitsch John Tracy Director of Research & Technology Senior Vice President, Chief Technology Officer Head of the Space Sector of Chief Technology Officer and Airbus Americas Lockheed Martin Corporation Johns Hopkins University, Applied Physics Laboratory Senior Vice President of Engineering, Operations & Technology The Boeing Company Tuesday, 14 January 2014 100-LECT-4 National Space Technology Strategy Workshop & Public Listening Session National Harbor Conf Rm 7 0930 - 1230 hrs Chair: Dr. Mark Lewis; Director, Science and Technology Policy Institute Tuesday, 14 January 2014 101-NW-4 Tuesday Morning Networking Coffee Break Exhibit Hall 0930 - 1000 hrs Tuesday, 14 January 2014 102-AA-3 Community Noise and Sonic Boom Woodrow Wilson B Chaired by: A. PILON, Lockheed Martin Aeronautics 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2014-0365 AIAA-2014-0366 AIAA-2014-0367 AIAA-2014-0368 AIAA-2014-0369 On Noise Assessment for Turbofan and Propeller Aircraft Open Rotor Tone Shielding Sonic Boom Estimation using Effect of Low-Boom Waveform Blended Wing Body Aircraft Taxi Operating State Noise Methods for System Noise the Multipole Method for Free- on Focus Boom Using Lossy Y. Guo, The Boeing Company, Power Distance and Spectral Assessments Using Multiple Flight Experiments Nonlinear Tricomi Equation Huntington Beach, CA; C. Burley, Class Database Development Databases Y. Saito, T. Ukai, K. Miyakoshi, Analysis R. Thomas, NASA Langley Research Process for AEDT C. Bahr, R. Thomas, L. Lopes, C. K. Ohtani, S. Obayashi, Tohoku M. Kanamori, A. Hashimoto, T. Aoyama, Center, Hampton, VA J. Page, Wyle, Arlington, VA Burley, NASA Langley Research University, Sendai, Japan Japan Aerospace Exploration Agency Center, Hampton, VA; D. Van Zante, (JAXA), Chofu, Japan; M. Yamamoto, NASA Glenn Research Center, Research Center of Computational Cleveland, OH Mechanics, Inc., Shinagawa, Japan Tuesday, 14 January 2014

78 103-ABPSI-1 Group for Aeronautical Research and Technology in EURope (GARTEUR) I Chesapeake Conf Rm 7 Chaired by: T. BERENS, EADS Deutschland GmbH/Cassidian and A. DELOT, ONERA 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2014-0370 AIAA-2014-0371 AIAA-2014-0372 AIAA-2014-0373 An Overview of the Group Numerical Simulations for High Numerical Simulations of Wind Experimental Investigations for Aeronautical Research Offset Intake Diffuser Flows Tunnel Effects on Intake Flow on the Inﬂuence of Ingesting and Technology in EURope T. Berens, Cassidian, Manching, of a UAV Conﬁguration Boundary Layers into a (GARTEUR) Germany; A. Delot, ONERA, Meudon, D. Funes-Sebastian, L. Ruiz-Calavera, Diverterless S-Duct Intake H. Consigny, O. Vasseur, ONERA, France; M. Chevalier, Swedish Airbus, Getafe, Spain M. Rein, S. Koch, M. Ruetten, Palaiseau, France; A. Delot, ONERA, Defense Research Agency (FOI), German Aerospace Center (DLR), Meudon, France Stockholm, Sweden; J. van Muijden, Göttingen, Germany National Aerospace Laboratory (NLR), Amsterdam, The Netherlands Tuesday, 14 January 2014 104-ACD-5 Aircraft Design Education Azalea 1 Chaired by: R. MCDONALD, California Polytechnic State University-San Luis Obispo 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2014-0374 AIAA-2014-0375 AIAA-2014-0376 Oral Presentation Oral Presentation Incorporating Stakeholder Constrained Design and Attitude Determination AIAA Undergraduate Individual AIAA Undergraduate Team Considerations in the Aircraft Iteration of a New Aircraft Experiment for Aerospace Aircraft Design Competition Aircraft Design Competition Design Process: A Focus on Design Course at TU Munich Design Education Winner - Raphael Klein, TU Delft Winner - California Polytechnic Aircraft Design Education S. Sartorius, Technical University of M. Anderson, University of California, University of Technology State University, San Luis Obispo A. Coso, A. Pritchett, Georgia Munich, Garching, Germany San Diego, La Jolla, CA Speaker: Trevor Goehring Institute of Technology, Atlanta, GA Tuesday, 14 January 2014 105-ACD-6 Electric Systems for Aircraft Design Azalea 2 Chaired by: C. BIL, RMIT University 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2014-0377 AIAA-2014-0378 AIAA-2014-0379 AIAA-2014-0380 AIAA-2014-0381 All Electric System Architecture Conceptual Design of a High-voltage DC power grid Design of a Safe and Reliable A System and Mission Level for Aircraft and Propulsion Battery-Powered High Lift system for the More Electric Li-ion Battery System for Analysis of Electrically N. Morioka, IHI Corporation, Tokyo, System for Single-Aisle Aircraft Architecture Applications in Airborne System Actuated Flight Control Japan; H. Oyori, IHI Corporation, T. Lammering, A. Sauterleute, H. Oyori, IHI Corporation, Tomioka, J. Becker, C. Schaeper, J. Muennix, D. Surfaces using Pacelab SysArc Gunma, Japan B. Hauber, T. Schneider, Liebherr Japan; N. Morioka, IHI Corporation, Sauer, RWTH Aachen University, Aachen, I. Chakraborty, D. Mavris, Georgia Aerospace, Lindenberg, Germany; J. Mizuho, Japan; Y. Ota, K. Onishi, Germany; T. Lammering, A. Sauterleute, Institute of Technology, Atlanta, GA; Becker, C. Schaeper, RWTH Aachen Y. Shimomura, Sinfonia Technology Liebherr Aerospace, Lindenberg, M. Emeneth, A. Schneegans, PACE University, Aachen, Germany; et al. Company, Ltd., Ise, Japan Germany; et al. America, Inc., Seattle, WA Tuesday, 14 January 2014 106-AFM-4 Flight Dynamics and Handling Qualities III National Harbor Conf Rm 12 Chaired by: S. KOMADINA, Northrop Grumman Aerospace Systems and A. GOPALARATHNAM, North Carolina State University 1000 hrs 1030 hrs 1100 hrs AIAA-2014-0382 AIAA-2014-0383 AIAA-2014-0384 Fully-coupled 6 DoF Model Numerical analysis for an Dynamic Ground Effect on for Unmanned Version of aerial deployment motion of a the Longitudinal Stability of the SA160 General Aviation folded-wing airplane Airplanes during the Landing Aircraft K. Fujita, Tohoku University, Sendai, P. Gonzalez, P. Boschetti, E. M. Cardinal, P. Masson, Sherbrooke Japan; T. Motoda, Japan Aerospace Cardenas, M. Celi, Simón Bolívar University, Sherbrooke, Canada Exploration Agency (JAXA), Mitaka, University, Naiguata, Venezuela,

79 Japan; H. Nagai, Tohoku University, Bolivarian Republic of Sendai, Japan Tuesday, 14 January 2014 107-AFM-5 Planetary Reentry I National Harbor Conf Rm 13 Chaired by: M. GRANT, Purdue University 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2014-0385 AIAA-2014-0386 AIAA-2014-0387 AIAA-2014-0388 Statistical Entry, Descent, Supersonic Propulsive Divert Potential for Integrating Statistical Entry, Descent, and and Landing Performance Maneuvers for Future Robotic Entry Guidance into the Multi- Landing Flight Reconstruction Reconstruction of the Mars and Human Mars Missions Disciplinary Entry Vehicle with Flush Air Data System Science Laboratory A. Mandalia, R. Braun, Georgia Optimization Environment Observations using Inertial S. Dutta, R. Braun, Georgia Institute Institute of Technology, Atlanta, GA S. D’Souza, D. Kinney, J. Garcia, Navigation and Monte Carlo of Technology, Atlanta, GA NASA Ames Research Center, Moffett Techniques Field, CA; N. Sarigul-Klijn, University R. Lugo, R. Tolson, North Carolina of California, Davis, Davis, CA State University, Raleigh, NC; R. Blanchard, National Institute of Aerospace, Hampton, VA Tuesday, 14 January 2014 108-AMT-1 Absorption and Emission Spectroscopy Maryland Ballroom 1 Chaired by: S. ZAIDI, Agilent Technologies and Z. ZHANG, University of Tennessee 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2014-0389 AIAA-2014-0390 AIAA-2014-0391 AIAA-2014-0392 AIAA-2014-0393 Hypersonic scramjet testing Mid-infrared Absorption Sensor Exhaust Gas Analysis of a Investigation of LTE Condition Characterization of a High- via TDLAS measurements of for Measurements of CO and Rotating Detonation Engine using inside a Microwave Induced Power Microwave Induced temperature and column density CO2 in Propulsion Flows Tunable Diode Laser Absorption Nitrogen Plasma Torch Plasma inside an MP Torch in a reflected shock tunnel R. Spearrin, J. Jeffries, R. Hanson, Spectroscopy S. Zaidi, M. Denning, R. Urdahl, using Emission Spectroscopy I. Schultz, C. Goldenstein, C. Strand, Stanford University, Stanford, CA C. McGahan, B. Tom, Air Force Institute Agilent Technologies, Santa Clara, CA S. Zaidi, M. Vahidpour, J. Duimstra, J. Jeffries, R. Hanson, Stanford of Technology, Wright-Patterson AFB, G. Owen, R. Urdahl, Agilent University, Stanford, CA; C. Goyne, OH; A. Caswell, Spectral Energies, Technologies, Santa Clara, CA University of Virginia, Charlottesville, LLC, Dayton, OH; J. Gord, F. Schauer, Charlottesville, VA Air Force Research Laboratory, Wright- Patterson AFB, OH; J. Hoke, Innovative Scientific Solutions, Inc., Dayton, OH Tuesday, 14 January 2014 109-AMT-2 Volumetric Measurement Techniques Maryland Ballroom 2 Chaired by: B. THUROW, Auburn University and L. MA, Virginia Tech 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2014-0394 AIAA-2014-0395 AIAA-2014-0396 AIAA-2014-0397 AIAA-2014-0398 Practical aspects of Experimental methods to Calibration of a Microlens Calibration of Fiber Bundles 3D Particle Position three-dimensional flame quantify particle positional Array for a Plenoptic Camera for Flow and Combustion Reconstruction Accuracy in imaging using tomographic and displacement uncertainty C. Thomason, B. Thurow, T. Measurements Plenoptic PIV Fahringer, Auburn University, 80 chemiluminescence along the depth direction in M. Kang, X. Li, L. Ma, Virginia T. Fahringer, B. Thurow, Auburn W. Cai, X. Li, Y. Cao, J. Wang, L. digital in-line holography Auburn, AL Polytechnic Institute and State University, Auburn, AL Ma, Virginia Polytechnic Institute and D. Guildenbecher, P. Reu, M. Nemer, University, Blacksburg, VA State University, Blacksburg, VA Sandia National Laboratories, Albuquerque, NM; J. Gao, J. Chen, Purdue University, West Lafayette, IN Tuesday, 14 January 2014 110-APA-10 Active and Passive Flow Control II Chesapeake Conf Rm I Chaired by: J. FARNSWORTH, US Air Force Academy and G. GATLIN 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2014-0399 AIAA-2014-0400 AIAA-2014-0401 AIAA-2014-0402 AIAA-2014-0403 Suppression of Vortex Shedding Experimental Investigation Influence of Geometry Study of shock and induced Experimental Study on Bluff from a Circular Cylinder by using of High-Frequency-Actuation Variations on the Boundary flow dynamics by pulsed Body Drag Reduction with a Traveling Wave Wall Synthetic Jet Flow Control Layer Control with a Passively nanosecond DBD plasma Fluidic Oscillators W. Chen, Y. Liu, Iowa State University, M. Bottomley, A. Packwood, Moving Wall actuators R. Woszidlo, T. Stumper, C. Nayeri, Ames, IA; F. Xu, Harbin Institute of University of Surrey, Guildford, H. Koch, D. Kozulovic, Technical Z. Zhao, J. Li, J. Zheng, Y. Cui, C. Paschereit, Technical University of Technology, Shenzhen, China; H. Li, United Kingdom University of Braunschweig, B. Khoo, National University of Berlin, Berlin, Germany Harbin Institute of Technology, Harbin, Braunschweig, Germany Singapore, Singapore, Singapore China; H. Hu, Iowa State University, Ames, IA Tuesday, 14 January 2014 111-APA-11 High Angle of Attack and High Lift Aerodynamics Maryland Ballroom 5 Chaired by: D. LACY, Boeing Commercial Airplanes and G. ZHA 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2014-0404 AIAA-2014-0405 AIAA-2014-0406 AIAA-2014-0407 NASA Trapezoidal Wing Delaying the Onset of Stall by A Detailed Aerodynamic Aerodynamic effects of propeller Simulation using Stress-w Blade Shape Optimization Analysis of the Cyclorotor slipstream on a wing with and One-and Two-Equation V. Ahuja, C. Kannepalli, A. Zambon, Using Dynamic Mesh in CFD circulation control by internally Turbulence Model H. Naiman, Combustion Research J. Tang, Y. Hu, B. Song, blown flaps J. Rodio, North Carolina State and Flow Technology, Inc., Northwestern Polytechnical N. Beck, R. Radespiel, Technical University, Raleigh, NC; X. Pipersville, PA University, Xi’an, China University of Braunschweig, Xiao, Corvid Technologies, Inc., Braunschweig, Germany; C. Lenfers, Mooresville, NC; H. Hassan, North German Aerospace Center (DLR), Carolina State University, Raleigh, Braunschweig, Germany; J. Friedrichs, NC; C. Rumsey, NASA Langley Technical University of Braunschweig, Research Center, Hampton, VA Braunschweig, Germany; A. Rezaeian, German Aerospace Center (DLR), Göttingen, Germany Tuesday, 14 January 2014 112-APA-12 Propeller/Rotorcraft Aerodynamics I Maryland Ballroom 4 Chaired by: M. CALVERT, U.S. Army AMRDEC 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2014-0408 AIAA-2014-0409 AIAA-2014-0410 AIAA-2014-0411 CFD Analysis of Open Rotor Effective Blade Twist and High- and Low-Fidelity A Time Domain Analysis of Engines Using an Actuator Shape in Servo-Flap Rotor Investigations of Flexible Compressible Dynamic Stall 81 Disk Model Performance Design Propeller Blades by Implementation of Chirp B. Farrar, R. Agarwal, Washington F. Wei, A. Gates, Central Connecticut J. Sodja, R. De Breuker, Delft Signal Pitch Excursions University in St. Louis, St. Louis, MO State University, New Britain, CT University of Technology, Delft, D. Coleman, K. Heintz, F. Thomas, The Netherlands; D. Nozak, R. T. Corke, University of Notre Dame, Drazumeric, University of Ljubljana, Notre Dame, IN Ljubljana, Slovenia; P. Marzocca, Clarkson University, Potsdam, NY Tuesday, 14 January 2014 113-APA-13 Special Session: Aerodynamic Design Optimization: Current Trends and Future Direction I Maryland Ballroom D Chaired by: S. NADARAJAH and S. LEDOUX, Boeing Engineering Operations & Technology 1000 hrs 1030 hrs 1100 hrs 1130 hrs Oral Presentation (Invited) AIAA-2014-0412 AIAA-2014-0413 AIAA-2014-0414 Case Studies in Aerodynamic Adjoint-Based Aerodynamic Application of Control Point- Hybrid feedback design for Design Optimization Optimization Framework Based Aerodynamic Shape subsonic and transonic airfoils J. Vassberg, S. Ledoux, The Boeing F. Bisson, S. Nadarajah, McGill Optimization to Two-Dimensional and wings Company, Huntington Beach, CA; J. University, Montréal, Canada Drag Minimization M. Zhang, C. Wang, A. Rizzi, Royal Coder, Pennsylvania State University, D. Poole, C. Allen, T. Rendall, University Institute of Technology (KTH), University Park, PA of Bristol, Bristol, United Kingdom Stockholm, Sweden; R. Nangia, Bristol University, Bristol, United Kingdom Tuesday, 14 January 2014 114-APA-14 Special Session: CREATE-AV High Performance Computing Multiphysics Applications of Full-Up Air Vehicles I Woodrow Wilson A Chaired by: N. HARIHARAN, CREATE-AV 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs Oral Presentation (Invited) AIAA-2014-0415 AIAA-2014-0416 AIAA-2014-0417 AIAA-2014-0418 Kestrel Current Capabilities Multiple Bodies, Motion, and Validation of 3D RANS-SA Advances in Numerical Advanced Navy Applications and Future Direction for Fixed Mash-Ups: Handling Complex Calculations on Strand/ Methods for CREATE-AV Using CREATE-AV Kestrel Wing Aircraft Simulations Use-Cases with Kestrel Cartesian Meshes Analysis Tools T. Shafer, B. Green, B. Hallissy, D. S. Morton, D. McDaniel, CREATE D. McDaniel, University of Alabama, A. Wissink, Army Aviation and N. Burgess, Science and Technology Hine, Naval Air Systems Command, Kestrel Team, Eglin AFB, FL Birmingham, Birmingham, AL; T. Missile Research Development and Corporation, Moffett Field, CA Patuxent River, MD Tuckey, 96 RNCS, Eglin AFB, FL Engineering Center, Moffett Field, CA; A. Katz, Utah State University, Logan, UT; J. Sitaraman, University of Wyoming, Laramie, Laramie, WY Tuesday, 14 January 2014 115-APA-15 Special Session: 2nd Cranked Arrow Wing Aerodynamic Project International (CAWAPI) I Maryland Ballroom B Chaired by: K. ABDOL-HAMID, NASA Langley Research Center and J. PINIER, NASA-Langley Research Center 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2014-0419 AIAA-2014-0420 AIAA-2014-0421 AIAA-2014-0422 Toward Improved CFD Factors Influencing Accurate Aeroelastic Analysis of the Improved Predictions for high Predictions of Slender Airframe Shock Vortex Interaction CAWAPI F-16XL Configuration at Angle of Attack Flow around Aerodynamics Using the F-16XL Prediction on F-16XL Aircraft Transonic Speeds the F-16XL Aircraft Aircraft (CAWAPI-2) M. Tomac, A. Jirasek, A. Rizzi, A. Jirasek, Royal Institute of Technology A. Jirasek, M. Tomac, A. Rizzi, J. Luckring, NASA Langley Research Royal Institute of Technology (KTH), (KTH), Stockholm, Sweden; L. Cavagna, Royal Institute of Technology (KTH), Stockholm, Sweden L. Riccobene, S. Ricci, Technical Stockholm, Sweden

82 Center, Hampton, VA; A. Rizzi, Royal Institute of Technology (KTH), University of Milan, Milan, Italy; A. Rizzi, Stockholm, Sweden Royal Institute of Technology (KTH), Stockholm, Sweden Tuesday, 14 January 2014 116-FD-15 Higher-Order Methods I Chesapeake Conf Rm 8 Chaired by: K. FIDKOWSKI, University of Michigan and J. POGGIE, USAF AFRL/RBAC 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2014-0423 AIAA-2014-0424 AIAA-2014-0425 AIAA-2014-0426 Implicit Large-Eddy-Simulation Large Eddy Simulations using Detached Eddy Simulation of Numerical Simulation of High- of Compressible Flow High order Flux Reconstruction Flow over NACA0012 Airfoil Speed Flows Over Complex J. Poggie, N. Bisek, Air Force method on Hybrid at High Angle of Attack with Geometries with a High-Order Research Laboratory, Wright- Unstructured meshes Spectral Difference Method Multi-Zone Cut-Cell Method Patterson AFB, OH Y. LU, W. Dawes, University of J. Gao, X. Li, Beihang University, P. Greene, J. Eldredge, X. Zhong, Cambridge, Cambridge, United Kingdom Beijing, China J. Kim, University of California, Los Angeles, Los Angeles, CA Tuesday, 14 January 2014 117-FD-16 Hypersonic Boundary Layer Transition II Maryland Ballroom 6 Chaired by: T. JULIANO, US Air Force Research Laboratory and K. CASPER, Sandia National Laboratories 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2014-0427 AIAA-2014-0428 AIAA-2014-0429 AIAA-2014-0430 Transition Statistics Measured Laminar to turbulent transition HIFiRE-1 Surface Pressure Linearized Navier-Stokes on a 7-Degree Hypersonic on the HIFiRE-1 cone at Mach Fluctuations from High Reynolds, Simulation of the Spatial Stability Cone for Turbulent Spot 7 and high angle of attack High Angle Ground Test of a Hypersonic Boundary Modeling S. Willems, A. Guelhan, German T. Juliano, R. Kimmel, Air Force Research Layer in a Sharp Cone with High K. Casper, S. Beresh, J. Henfling, Aerospace Center (DLR), Cologne, Laboratory, Wright-Patterson AFB, Temperature Effects: The Caltech R. Spillers, Sandia National Germany; T. Juliano, National OH; S. Willems, A. Guelhan, German T5 Test Shot T2718 Laboratories, Albuquerque, NM Research Council, Beavercreek, OH; Aerospace Center (DLR), Cologne, L. Salemi, H. Fasel, A. Gross, University S. Schneider, Purdue University, West Germany; S. Schneider, Purdue of Arizona, Tucson, Tucson, AZ Lafayette, IN University, West Lafayette, IN Tuesday, 14 January 2014 118-FD-17 Roughness-Influenced Boundary Layer Transition II Chesapeake Conf Rm H Chaired by: H. JOHNSON, University of Minnesota and M. MALIK, NASA-Langley Research Center 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2014-0431 AIAA-2014-0432 AIAA-2014-0433 AIAA-2014-0434 Boundary Layer Tripping for a Roughness-Induced Transient High Fidelity Computational Aeroheating measurement of Simplified Landing Gear Model Growth on a Hypersonic Blunt Study of the HIFiRE-1 Apollo shaped capsule with G. Feltham, P. McCarthy, A. Ekmekci, Cone Boundary Layer Trip boundary layer trip in the free- University of Toronto, Toronto, N. Sharp, E. White, Texas A&M J. Gronvall, Ohio Aerospace Institute, piston shock tunnel HIEST Canada University, College Station, TX Dayton, OH; N. Bisek, J. Poggie, Air H. Tanno, T. Komuro, K. Sato, K. Itoh, Force Research Laboratory, Wright-

83 Japan Aerospace Exploration Agency Patterson AFB, OH (JAXA), Kakuda, Japan; R. Lillard, NASA Johnson Space Center, Houston, TX; J. Olejniczak, NASA Ames Research Center, Moffett Field, CA; et al. Tuesday, 14 January 2014 119-FD-18 Shock Boundary Layer Interactions I National Harbor Conf Rm 4 Chaired by: J. EDWARDS and R. BAURLE, NASA Langley Research Center 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2014-0435 AIAA-2014-0436 AIAA-2014-0437 AIAA-2014-0438 AIAA-2014-0439 Flow Interactions of Small Conditional Analysis of the LES for Separated Supersonic Investigation of Shock Wave - Study of transonic shock Cylindrical Protuberances and the Unsteadiness in Shock Wave Turbulent Boundary Layer and Boundary Layer Interactions in wave/boundary layer Supersonic Turbulent Boundary and Turbulent Boundary Layer Shock Interaction a 3.57 Aspect Ratio Tunnel interactions subject to Layer on a Flat Plate Interactions S. Chern, G. Lobser, M. Schoonmaker, S. Warning, M. Turlin, P. Ligrani, M. unsteady forcing E. Stephen, S. Morell, R. Decker, D. J. Li, S. Priebe, P. Martin, University United Launch Alliance, Denver, CO; McQuilling, Saint Louis University, J. Threadgill, P. Bruce, Imperial College Hope, T. McLaughlin, U.S. Air Force of Maryland, College Park, College C. Liu, University of Texas, Arlington, St. Louis, MO London, London, United Kingdom Academy, Colorado Springs, CO Park, MD Arlington, TX Tuesday, 14 January 2014 120-FD-19 Thermal Environment Chesapeake Conf Rm G Chaired by: Y. LIAN, University of Louisville and C. BOURASSA, GE Aviation 1000 hrs 1030 hrs 1100 hrs AIAA-2014-0440 AIAA-2014-0441 AIAA-2014-0442 Computational Fluid Dynamics Computational Analysis and Cavitation Modeling for Uncertainty Analysis for Payload Characterization of Cockpit Cryogenic Flows Using a Rule- Fairing Spacecraft Environmental Environmental Control System Based Framework Control Systems of a Fighter Aircraft S. Thakur, J. Wright, Streamline C. Groves, NASA Kennedy Space J. Masud, M. Ayyaz, Air University, Numerics, Inc., Gainesville, FL Center, Cape Canaveral, FL; M. Ilie, Islamabad, Pakistan University of Central Florida, Orlando, FL; P. Schallhorn, NASA Kennedy Space Center, Cape Canaveral, FL Tuesday, 14 January 2014 121-GNC-6 Onboard Systems Technologies for LOC Prevention & Recovery - Improved Situational Awareness, Guidance, and Control, Session (Invited) II National Harbor Conf Rm 8 Chaired by: D. CRIDER, National Transportation Safety Board and K. FEIGH, Georgia Institute of Technology 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2014-0443 AIAA-2014-0444 AIAA-2014-0445 AIAA-2014-0446 AIAA-2014-0447 Perceptual Modeling as a Tool to Simulator Evaluation of an A Materiel Solution to Aircraft Relaxation of Stability Flight Test Evaluation of the Prevent Aircraft Upset Associated In-Cockpit Cueing System for Upset Requirements for Extended SAFE-Cue System for Loss of with Spatial Disorientation Upset Recovery A. Kelley, Self, Arlington, VA; R. Kalman Filter Stability within Control Mitigation M. Newman, Environmental Tectonics N. Gandhi, N. Richards, A. Newman, Crew Systems, Seattle, GPS/INS Attitude Estimation D. Klyde, A. Lampton, D. Alvarez, Corporation, Southampton, PA; B. Bateman, Barron Associates, Inc., WA; B. Lawson, A. Rupert, Army M. Rhudy, Y. Gu, M. Napolitano, Systems Technology, Inc., Aeromedical Research Laboratory, 84 Lawson, Army Aeromedical Research Charlottesville, VA West Virginia University, Hawthorne, CA; N. Richards, Barron Laboratory, Fort Rucker, AL; B. McGrath, Fort Rucker, AL Morgantown, WV Associates, Inc., Charlottesville, QinetiQ, Canberra, Australia; A. Rupert, VA; B. Cogan, NASA Dryden Flight Army Aeromedical Research Laboratory, Research Center, Edwards, CA Fort Rucker, AL Tuesday, 14 January 2014 122-GNC-7 Spacecraft Navigation National Harbor Conf Rm 5 Chaired by: J. LIU, Boeing Defense, Space & Security 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2014-0448 AIAA-2014-0449 AIAA-2014-0450 AIAA-2014-0451 Finite-Time Control of Satellites Dual-purpose Resonate Computing an optimized Orbit Design and Control of in Elliptic Orbits Despite Actuators for Electromagnetic trajectory between Earth and Technology Validation Mission Uncertainties Using Solar Formation Flight and Wireless an EML2 halo orbit for Refractive Space Telescope Radiation Pressure Power Transfer P. Kokou, B. Le Bihan, J. Receveur, in Formation Flying L. Srinivasan, University of Nevada, A. Porter, D. Alinger, R. Sedwick, S. Lizy-Destrez, University of S. Park, Yonsei University, Seoul, Las Vegas, Las Vegas, NV; K. Lee, University of Maryland, College Toulouse, Toulouse, France South Korea Kwandong University, Gangwon, Park, College Park, MD; J. Merk, South Korea; S. Singh, University of R. Opperman, Aurora Flight Nevada, Las Vegas, Las Vegas, NV Sciences, Cambridge, MA; A. Buck, Massachusetts Institute of Technology, Cambridge, MA; et al. Tuesday, 14 January 2014 123-GNC-8 Control of Uncertain Systems National Harbor Conf Rm 3 Chaired by: D. ALAZARD, Institut Supérieur de l’Aéronautique et de l’Espace and N. NGUYEN, NASA-Ames Research Center 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2014-0452 AIAA-2014-0453 AIAA-2014-0454 AIAA-2014-0455 Eco-Inspired Robust Control L1 Adaptive Control Multi-Objective Optimal Robust Nonlinear H∞ Output- Design Algorithms For Linear Augmentation Configuration Control Modification Adaptive Feedback for Spacecraft Systems with Real Parameter for a Hypersonic Glider in the Control Method for Systems Attitude Control Uncertainty Presence of Uncertainties with Input and Unmatched A. Capua, A. Shapiro, Ben-Gurion R. Yedavalli, N. Devarakonda, R. S. Banerjee, M. Creagh, R. Boyce, Uncertainties University of the Negev, Beer Sheva, Chandavarkar, P. Sar, Ohio State University of Queensland, Brisbane, N. Nguyen, NASA Ames Research Israel; D. Choukroun, Delft University University, Columbus, OH Australia Center, Moffett Field, CA of Technology, Delft, The Netherlands Tuesday, 14 January 2014 124-GTE-3 Gas Turbine Combustor I Woodrow Wilson D Chaired by: C. GROTH, University of Toronto 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2014-0456 AIAA-2014-0457 AIAA-2014-0458 AIAA-2014-0459 Characterizing Thermal Characterization of Inverse The Use of an Ultra-Compact Hydroxyl Radical Distribution Exit Conditions for an Ultra Diffusion Flames in High Combustor as an Inter-Turbine under Colorless Distributed Compact Combustor Temperature Cross-flow Burner for Improved Engine Combustion Conditions C. Damele, M. Polanka, J. Wilson, D. Richardson, Air Force Research Performance A. Khalil Hasan, A. Gupta, University J. Rutledge, Air Force Institute Laboratory, Wright-Patterson AFB, OH; J. Miranda, M. Polanka, Air Force of Maryland, College Park, College of Technology, Wright-Patterson N. Jiang, A. Caswell, S. Roy, Spectral Institute of Technology, Wright- Park, MD AFB, OH Energies, LLC, Dayton, OH; D. Blunck, Patterson AFB, OH

85 A. Lynch, Air Force Research Laboratory, Wright-Patterson AFB, OH; et al. Tuesday, 14 January 2014 125-MAT-2 Integrated Computational Materials Engineering I Chesapeake Conf Rm D Chaired by: J. MATLIK, Rolls-Royce Corporation; S. ARNOLD and M. SANGID, Purdue University 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2014-0460 AIAA-2014-0461 AIAA-2014-0462 AIAA-2014-0463 Robust Informatics Achieving ICME with Multiscale Validation of Microstructure- Application of a Risk Infrastructure Required for Modeling: The Effects of Based Materials Modeling Quantification Approach to ICME Constituent Properties and M. Sangid, S. Yeratapally, A. Aerospace Manufacturing S. Arnold, F. Holland, B. Bednarcyk, Processing on the Performance Rovinelli, Purdue University, West Using Bayesian Networks NASA Glenn Research Center, of Laminated Polymer Matrix Lafayette, IN G. Hahn, M. Thomas, L. Pado, S. Cleveland, OH Composite Structures Liguore, S. Tyahla, The Boeing E. Pineda, B. Bednarcyk, S. Arnold, Company, St. Louis, MO NASA Glenn Research Center, Cleveland, OH Tuesday, 14 January 2014 126-MAT-3 Nanostructured Materials II Chesapeake Conf Rm A Chaired by: B. WARDLE, Massachusettes Institute of Technology; G. ODEGARD and S. ROY, The University of Alabama 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2014-0464 AIAA-2014-0465 AIAA-2014-0466 AIAA-2014-0467 AIAA-2014-0468 Influence of crosslink ratio on Self-sensing of Strain in Variation in Interlaminar Predicting Thermo-Mechanical Hybrid Carbon/Epoxy the thermomechanical properties Carbon Nanotube Modified Tension and Shear Strengths Response of Crosslinked Epoxy Composites with Interlocking of polymer nanocomposites and Carbon Fibre Reinforced due to Carbon Nanotube using ReaxFF Properties: The Graphene interphase: a molecular dynamics Composites Reinforcement in VARTM G. Odegard, B. Jensen, Michigan Nanostructure Morphology simulation W. Liu, P. Hubert, McGill University, Manufactured, Polymer- Technological University, Houghton, Investigation B. Kim, J. Choi, S. Yu, Seoul National Montréal, Canada Matrix, Laminated Composites MI; J. Wu, J. He, Z. Zhang, A. Avila, C. Goncalves, G. Carley, University, Seoul, South Korea; S. Yang, B. Martins, J. Kosmatka, University of Norwegian University of Science and Federal University of Minas Gerais, Dong-A University, Busan, South Korea; California, San Diego, San Diego, CA Technology, Trondheim, Norway Belo Horizonte, Brazil M. Cho, Seoul National University, Seoul, South Korea Tuesday, 14 January 2014 127-MDO-3 Aeroelastic and Aero-Structures Optimization Chesapeake Conf Rm 4 Chaired by: H. KIM, University of Bath and F. ENGELSEN, The Boeing Company 1000 hrs 1030 hrs 1100 hrs AIAA-2014-0469 AIAA-2014-0470 AIAA-2014-0471 Aeroelastic Shape Optimization Integration of Geometric Global/Local Multidisciplinary of a Flapping Wing Sensitivity and Spatial Gradient Design Optimization of E. Stewart, M. Patil, R. Canfield, Reconstruction for Aeroelastic Subsonic Wing Virginia Polytechnic Institute and State Shape Optimization Q. Liu, S. Mulani, R. Kapania,

86 University, Blacksburg, VA; R. Snyder, M. Kulkarni, R. Canfield, M. Patil, Virginia Polytechnic Institute and Air Force Research Laboratory, Wright- Virginia Polytechnic Institute and State University, Blacksburg, VA Patterson AFB, OH State University, Blacksburg, VA Tuesday, 14 January 2014 128-MST-1 Applications of Modeling and Simulation National Harbor Conf Rm 6 Chaired by: J. SCHMOLL, Lockheed Martin Corporation 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2014-0472 AIAA-2014-0473 AIAA-2014-0474 AIAA-2014-0475 AIAA-2014-0476 Frequency-Domain Method for Physics-based Multi-fidelity The Sea-based Automated A Framework for Integration Model Complexity Reduction Automated Simulation Updates Surrogate Modeling with Entropy- Launch and Recovery System of ns-3 with RAMS simulator of a Segmented Mirror based on Flight Data based Availability Methods Virtual Testbed T. Bakker, S. Patibandla, R. Klenke, Telescope E. Morelli, Sunflyte Enterprises, L. Leifsson, S. Koziel, Reykjavik C. Wilkinson, D. Findlay, Naval Air Virginia Commonwealth University, L. Dras, A. Jennings, R. Cobb, Air Williamsburg, VA; J. Cooper, Barron University, Reykjavik, Iceland; S. Systems Command, Patuxent River, Richmond, VA Force Institute of Technology, Wright- Associates, Inc., Charlottesville, VA Hosder, Missouri University of Science MD; K. Boothe, S. Dogra, Coherent Patterson AFB, OH and Technology, Rolla, MO; D. Riggins, Technical Services, Inc., Lexington Reykjavik University, Reykjavik, Iceland Park, MD Tuesday, 14 January 2014 129-MVC-3 Geometry Preparation and Grid Quality Assessment Chesapeake Conf Rm 9 Chaired by: S. ALTER, NASA-Langley Research Center and T. MICHAL, Boeing Engineering Operations & Technology 1000 hrs 1030 hrs 1100 hrs AIAA-2014-0477 AIAA-2014-0478 AIAA-2014-0479 An Approach Towards Truncation and Discretization Anisotropic Norm-Oriented Mesh Integrating CFD into the Error for Diffusion Schemes on Adaptation for Compressible Missile Concept Design Process Unstructured Meshes Flows N. Taylor, MBDA, Bristol, United G. Yan, V. Puneria, A. Jalali, C. A. Dervieux, French National Institute Kingdom Ollivier Gooch, University of British for Research in Computer Science Columbia, Vancouver, Canada and Control (INRIA), Sophia-Antipolis, France; F. Alauzet, A. Loseille, French National Institute for Research in Computer Science and Control (INRIA), Paris Rocquencourt, France Tuesday, 14 January 2014 130-NDA-3 Probabilistic Methods for Diagnostics & Prognostics Chesapeake Conf Rm 5 Chaired by: Y. LIU, Clarkson University and P. WANG, Wichita Univ 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2014-0480 AIAA-2014-0481 AIAA-2014-0482 AIAA-2014-0483 AIAA-2014-0484 An Uncertainty Quantification Statistical Aspects in Neural Probabilistic Design of Smart Probabilistic Prognosis Using A novel Bayesian Imaging Framework for Prognostics Network for the Purpose of Sensing Functions for Failure Dynamic Bayesian Networks Method for probabilistic and Condition-Based Prognostics Diagnostics and Prognostics G. Bartram, S. Mahadevan, delamination detection of Monitoring D. An, N. Kim, University of Florida, Z. Wang, A. Almaktoom, P. Wang, Vanderbilt University, Nashville, TN composite materials Gainesville, Gainesville, FL; J. Choi, Wichita State University, Wichita, KS

87 S. Sankararaman, Stinger Ghaffarian T. Peng, Arizona State University, Technologies, Inc., Moffett Field, CA Korea Aerospace University, Goyang, Tempe, AZ; A. Saxena, K. Goebel, South Korea NASA Ames Research Center, Moffett Field, CA; Y. Xiang, Y. Liu, Arizona State University, Tempe, AZ Tuesday, 14 January 2014 131-PANEL-3 Space Shuttle Legacy: How We Did and What We Learned Chesapeake Conf Rm 6 1000 - 1230 hrs Moderator: Roger D. Launius, Smithsonian Institution Speakers: Vigor Yang Matthew H. Hersch Linda Billings John M. Logsdon Georgia Institute of Technology University of Pennsylvania George Washington University George Washington University

Tuesday, 14 January 2014 132-PC-7 Frontiers of Combustion Research (Invited) National Harbor Conf Rm 2 Chaired by: J. TISHKOFF 1000 hrs 1030 hrs 1100 hrs Oral Presentation (Invited) Oral Presentation (Invited) Oral Presentation (Invited) DOE Gas Phase Chemical Physics AFOSR Energy Conversion and NSF Combustion, Fire, and program on research inspired by Combustion Sciences Program Plasma Systems Program ground transportation fuels Overview Overview W. Sisk, U.S. Department of Energy, C. Li, Air Force Office of Scientific R. Chen, National Science Washington, DC Research, Washington, DC Foundation, Washington, DC Tuesday, 14 January 2014 133-PDL-5 Plasma-Actuators and Flow Control III Azalea 3 Chaired by: J. ROVEY, Missouri University of Science & Technology and L. RAJA, The University of Texas at Austin 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2014-0485 AIAA-2014-0486 AIAA-2014-0487 Oral Presentation (Invited) Compressibility Effects on Dielectric Barrier Discharge Microwave Energy Deposition Modification of a Mach 2 Dielectric Barrier Discharge (DBD) Plasma Actuators Thrust in Supersonic Flows on Laser- rarefied air flow over a flat Actuation and Boundary Layer - Measurement Methodology Initiated Dipole Structures plate with a DC discharge Receptivity Incorporating New Anti-Thrust I. Mashek, V. Lashkov, R. Khoronzhuk, R. Joussot, V. Lago, National Center M. Denison, L. Massa, E. Cisneros, Hypothesis D. Potapenko, Saint Petersburg State for Scientific Research (CNRS), University of Texas, Arlington, D. Ashpis, NASA Glenn Research University, Saint Petersburg, Russia; V. Orléans, France; J. Parisse, National Arlington, TX Center, Cleveland, OH; M. Laun, Brovkin, Russian Academy of Sciences, Center for Scientific Research Sierra Lobo, Inc., Cleveland, OH Moscow, Russia (CNRS), Marseille, France Tuesday, 14 January 2014 134-SAT-1 Space and Society: Social Impacts of Air and Space Technologies National Harbor Conf Rm 15 Chaired by: C. HEARSEY, The University of Mississippi and B. STEINFELDT, Georgia Institute of Technology 1000 hrs 1030 hrs 1100 hrs AIAA-2014-0488 AIAA-2014-0489 Oral Presentation (Invited) Relationship between Fleet Global Geoglyph’s Development of the AIAA Characteristics and Welfare of Steganography : Uncovering Tucson Engineering/Art Project Stakeholders of Commercial Hidden Earth Art using M. Rouch, Raytheon Company, Air Transportation: Airlines, Space-Based X-Band Synthetic Tucson, AZ Manufacturers, and the Public Aperture Radar G. Waycaster, R. Haftka, N. Kim, V. J. Lobo, Hisdesat, Madrid, Spain;

88 Bilotkach, C. Gogu, C. Bes, University of Y. Garcia, Complutense University, Florida, Gainesville, Gainesville, FL Madrid, Spain Tuesday, 14 January 2014 135-SD-5 Beam, Plate, Cable Dynamics Chesapeake Conf Rm B Chaired by: S. LIGUORE, Boeing Engineering Operations & Technology and D. JOHNSON, NASA Glenn Research Center 1000 hrs 1030 hrs 1100 hrs AIAA-2014-0490 AIAA-2014-0491 AIAA-2014-0492 Experimental Investigation Inclusion of Shear Effects, Finite Element Structural of a Perturbation Model for Tension, and Damping in a DTF Updating using FRFs the Nonlinear Response of a Beam Model for Cable Modeling M. Arras, G. Coppotelli, University of Fatigue Cracked Beam K. Spak, Virginia Polytechnic Institute Rome “La Sapienza”, Rome, Italy P. Cooley, J. Slater, Wright State and State University, Blacksburg, VA; University, Dayton, OH; O. Shiryayev, G. Agnes, Jet Propulsion Laboratory, Petroleum Institute, Abu Dhabi, California Institute of Technology, United Arab Emirates Pasadena, CA; D. Inman, University of Michigan, Ann Arbor, Ann Arbor, MI Tuesday, 14 January 2014 136-SD-6 Computational Aeroelasticity ROM II Chesapeake Conf Rm C Chaired by: P. TAYLOR, Gulfstream Aerospace Corporation and J. MCNAMARA, The Ohio State University 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2014-0493 AIAA-2014-0494 AIAA-2014-0495 AIAA-2014-0496 Thermal Reduced Order Model An Efﬁcient Computational Forced Response Statistics of a Evaluation of Linear, Inviscid, Adaptation to Aero-Thermo- Method for Structurally Bladed Rotor with Geometric Viscous, and Reduced-Order Structural Interactions Nonlinear Joined Wings Based Mistuning Modeling Aeroelastic Solutions A. Matney, Arizona State University, on Modal Derivatives V. Vishwakarma, A. Sinha, of the AGARD 445.6 Wing Tempe, AZ; S. Spottswood, Air Force P. Tiso, Delft University of Pennsylvania State University, Using Root Locus Analysis Research Laboratory, Wright-Patterson Technology, Delft, The Netherlands; University Park, PA W. Silva, P. Chwalowski, B. Perry, AFB, OH; M. Mignolet, Arizona State L. Demasi, R. Cavallaro, San Diego NASA Langley Research Center, University, Tempe, AZ; A. Culler, Air Force State University, San Diego, CA Hampton, VA Research Laboratory, Wright-Patterson AFB, OH; J. McNamara, Ohio State University, Columbus, OH Tuesday, 14 January 2014 137-SRE-2 Resource Enabled Mission Concepts National Harbor Conf Rm 14 Chaired by: J. KLEINHENZ, NASA Glenn Research Center and P. VISSCHER 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2014-0497 AIAA-2014-0498 AIAA-2014-0499 AIAA-2014-0500 Waste Management Options Solar System Exploration Mars surface transport systems Robotic Asteroid Prospector for Long-Duration Space Augmented by Lunar and Outer utilizing in situ hydrogen (RAP) NIAC Phase 1 Results Missions: When to Reject, Planet Resource Utilization: R. Ash, Old Dominion University, W. James, V Inﬁnity Research, LLC, Norfolk, VA; S. Hancock, Science Altadena, CA; K. Zacny, Honeybee

89 Reuse, or Recycle Historical Perspectives and Future D. Linne, B. Palaszewski, S. Possibilities Systems and Applications, Inc., Robotics, Pasadena, CA; J. Craft, Gokoglu, B. Balasubramaniam, B. Palaszewski, NASA Glenn Hampton, VA; J. Tynis, Old Dominion Honeybee Robotics, New York, NY; P. U. Hegde, C. Gallo, NASA Glenn Research Center, Cleveland, OH University, Norfolk, VA Chu, Honeybee Robotics, Pasadena, Research Center, Cleveland, OH CA; M. Cohen, Astrotecture™, Moffett Field, CA Tuesday, 14 January 2014 138-STR-7 Sandwich Structures Chesapeake Conf Rm F Chaired by: S. SMELTZER, NASA Langely Research Center and C. FOERSTER 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2014-0501 AIAA-2014-0502 AIAA-2014-0503 AIAA-2014-0504 A Three-Dimensional Multi- Design and Optimization of Degradation in Cellular Core Effects of Ply Stacking Sequence Stable Unit Cell for Energy Opencell™ Metal Sandwich Mechanical Properties due to in 3D Fiber Reinforced Foam Dissipation Cylindrical Panel Transverse Compression Core Sandwich Structures with M. Pontecorvo, S. Barbarino, F. A. Valente, PLY Technologies GmbH, H. Soliman, R. Kapania, Virginia Defects Gandhi, Rensselaer Polytechnic Hannover, Germany; A. Najaﬁ, Polytechnic Institute and State Z. Kier, A. Waas, University of Michigan, Institute, Troy, NY; S. Bland, ANSYS, Inc., Houston, TX University, Blacksburg, VA Ann Arbor, Ann Arbor, MI; C. Foerster, R. Snyder, J. Kudva, NextGen J. Rome, V. Goyal, The Aerospace Aeronautics, Torrance, CA; et al. Corporation, El Segundo, CA Tuesday, 14 January 2014 139-STR-8 Application of Viscoelasticity and Viscoelastic Materials Chesapeake Conf Rm E Chaired by: H. HILTON, University of Illinois at Urbana-Champaign and S. RAGHAVAN, University of Central Florida 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2014-0505 AIAA-2014-0506 AIAA-2014-0507 AIAA-2014-0508 AIAA-2014-0509 Variable Flight Velocity Uncertainty in Characterizations Testing of Viscoelastic Materials Finite Element for Viscoelastic Elastomeric Structural Attachment contributions to Elastic/ of Isotropic Linear Viscoelastic and their Implications on the Life Composite Plate Bending Concepts for Aircraft Flap Noise Viscoelastic Lifting Surface Shear and Bulk Moduli from 1 - Expectancy of GFRP Aircraft Using Efﬁcient Higher-Order Reduction - Challenges and Control Effectiveness D Tensile Experiments C. Goudie, C. Merrett, Carleton Displacement Field Approaches to Hyperelastic H. Hilton, N. Nguyen, University M. Michaeli, A. Shtark, H. Grosbein, University, Ottawa, Canada N. Nguyen Sy, J. Lee, M. Cho, Structural Modeling and Analysis of Illinois, Urbana-Champaign, Israel Military Industries, Ramat Seoul National University, Seoul, T. Sreekantamurthy, Analytical Urbana, IL Hasharon, Israel; E. Altus, Technion-- South Korea Mechanics Associates, Inc., Hampton, Israel Institute of Technology, Haifa, VA; T. Turner, J. Moore, J. Su, NASA Israel; H. Hilton, University of Illinois, Langley Research Center, Hampton, VA Urbana-Champaign, Urbana, IL Tuesday, 14 January 2014 140-TP-1 Aerothermodynamics I National Harbor Conf Rm 11 Chaired by: W. WOOD, Langley Research Center and A. HASHEMI, Lockheed Martin Space Systems 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2014-0510 AIAA-2014-0511 AIAA-2014-0512 AIAA-2014-0513 Experimental Studies of Orion MPCV Continuum RCS The Effects of Surface Roughness Adjoint-Based Spherical Capsule Wake Flows Heating Augmentation Model on Turbulent Heat Transfer Aerothermodynamic Shape with Reaction Control Jet Development Measured in Hypersonic Free Design of Hypersonic Vehicles Interaction A. Hyatt, ERC, Inc., Moffett Field, Flight in Non-Equilibrium Flows

90 T. Wadhams, CUBRC, Buffalo, NY CA; M. White, NASA Johnson Space M. Wilder, NASA Ames Research Center, S. Copeland, F. Palacios, J. Alonso, Center, Houston, TX Moffett Field, CA; D. Prabhu, ERC, Inc., Stanford University, Stanford, CA Moffett Field, CA; D. Reda, NASA Ames Research Center, Moffett Field, CA Tuesday, 14 January 2014 141-TP-2 Thermal Protection Systems I National Harbor Conf Rm 10 Chaired by: M. MARTIN, Louisiana State University and B. DROLEN, Boeing Defense, Space & Security 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2014-0514 AIAA-2014-0515 AIAA-2014-0516 AIAA-2014-0517 Development of A Simultaneous Singlet O2 Formation by Emission Intensity Influence of Nano-Scale Measurement Sensor for Ablative O-atom Recombination on Measurements around Mars Clusters on Gas Dynamics Thermal Protection Systems Fused Quartz Surfaces Entry Capsule with a Free- Parameters of Plasma Jet T. Sakai, K. Watanabe, H. Nakazawa, J. White, J. Marschall, R. Copeland, Piston-Driven Expansion Tube Created by Capillary Type M. Kuribayashi, H. Fukui, Nagoya SRI International, Menlo Park, CA H. Takayanagi, S. Nomura, K. Fujita, Discharge University, Nagoya, Japan; K. Kitagawa, Japan Aerospace Exploration Agency A. Klimov, A. Efimov, A. Pashchina, Aichi Institute of Technology, Toyota, (JAXA), Chofu, Japan Russian Academy of Sciences, Japan; et al. Moscow, Russia Tuesday, 14 January 2014 142-WE-5 Wind Turbine Aeroelasticity and Structural Dynamics I Woodrow Wilson C Chaired by: T. KIM 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2014-0518 AIAA-2014-0519 AIAA-2014-0520 AIAA-2014-0521 Modal Dynamics and Stability of Aeroelastic Vibration FAST Modular Wind Turbine Model-based Aeroservoelastic Large Multi-megawatt Deepwater Suppression of a Rotating CAE Tool: Nonmatching Spatial Design and Load Alleviation of Offshore Vertical-axis Wind Wind Turbine Blade using and Temporal Meshes Large Wind Turbines Turbines: Initial Support Structure Adaptive Control M. Sprague, J. Jonkman, National B. Ng, H. Hesse, R. Palacios, J. Graham, and Rotor Design Impact Studies N. Li, M. Balas, University of Renewable Energy Laboratory, E. Kerrigan, Imperial College London, B. Owens, D. Griffith, Sandia National Wyoming, Laramie, Laramie, WY Golden, CO London, United Kingdom Laboratories, Albuquerque, NM; J. Hurtado, Texas A&M University, College Station, TX Tuesday, 14 January 2014 143-LNCH-1 Aerospace Sciences Awards Lunch Potomac Ballroom A&B 1230 - 1400 hrs Tuesday, 14 January 2014 144-SB-4 Tuesday Afternoon Speakers’ Briefing Session Rooms 1400 - 1430 hrs Tuesday, 14 January 2014 145-AA-4 Jet Noise II Azalea 2

91 Chaired by: D. PAPAMOSCHOU, University of California Irvine 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs AIAA-2014-0522 AIAA-2014-0523 AIAA-2014-0524 AIAA-2014-0525 AIAA-2014-0526 AIAA-2014-0527 Observed Effect of Bypass Analysis of Supersonic Jet A study of the effects of Design and Analysis of a A Low-order Jet Noise Near-field Pressure and Far- Flow on Jet Noise Thrust with Fluidic Injection temperature on velocity and Supersonic Jet Noise Reduction Prediction Model for Chevrons field Acoustic Response of N. Murray, B. Jansen, University of D. Cuppoletti, E. Gutmark, University density fluctuations in high- Concept and Microjets Forced High-Speed Jets Mississippi, University, University, MS of Cincinnati, Cincinnati, OH; H. subsonic jets A. Pilon, Lockheed Martin N. Depuru Mohan, A. Dowling, M. Crawley, Ohio State University, Hafsteinsson, L. Eriksson, Chalmers C. Bogey, École Centrale de Lyon, Corporation, Palmdale, CA; D. University of Cambridge, Cambridge, Columbus, OH; A. Sinha, California University of Technology, Göteborg, Ecully, France McLaughlin, P. Morris, R. Powers, United Kingdom Institute of Technology, Pasadena, Sweden; E. Prisell, FMV, Stockholm, Pennsylvania State University, CA; M. Samimy, Ohio State Sweden University Park, PA University, Columbus, OH Tuesday, 14 January 2014 146-ABPSI-2 Air Breathing Propulsion System Integration and Optimization Maryland Ballroom D Chaired by: K. BLODGETT, GE Aviation and M. MCMILLAN, Syngenics Corporation 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs AIAA-2014-0528 AIAA-2014-0529 AIAA-2014-0530 AIAA-2014-0531 AIAA-2014-0532 AIAA-2014-0533 Design and Implementation Thermal Loss Determination Antares DLR-H2 - Fuel cell Design Optimization of a Thermal Management of Stereoscopic PIV of Waverotor Technology for Small Internal Combustion testing under aeronautical Scramjet Vehicle for Ascent Battery Module Consisting of Measurements of Swirl for Small-Bore Two-Stroke Engines conditions, modelling and test Using Surrogate Optimization Multiple Li-ion Cells for Hybrid Distortion on a Full-Scale Internal Combustion Engines J. Rittenhouse, A. Rowton, M. Polanka, J. Kallo, J. Schirmer, German D. Dalle, J. Driscoll, University of Power Systems Turbofan Engine Inlet M. Mataczynski, M. Polanka, Air Force Institute of Technology, Aerospace Center (DLR), Stuttgart, Michigan, Ann Arbor, Ann Arbor, MI F. He, X. Li, L. Ma, Virginia M. Nelson, K. Lowe, W. O’Brien, Air Force Institute of Technology, Wright-Patterson AFB, OH; J. Ausserer, Germany Polytechnic Institute and State Virginia Polytechnic Institute and Wright-Patterson AFB, OH; J. Hoke, P. Litke, Air Force Research Laboratory, University, Blacksburg, VA State University, Blacksburg, VA; Innovative Scientific Solutions, Inc., Wright-Patterson AFB, OH; K. Grinstead, K. Hoopes, Southwest Research Dayton, OH; D. Paxson, NASA Glenn Innovative Scientific Solutions, Inc., Institute, San Antonio, TX Research Center, Cleveland, OH Dayton, OH Tuesday, 14 January 2014 147-ACD-7 Aircraft Design with Electric Propulsion Azalea 1 Chaired by: D. EAMES, Rolls-Royce Corporation 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs AIAA-2014-0534 AIAA-2014-0535 AIAA-2014-0536 AIAA-2014-0537 AIAA-2014-0538 AIAA-2014-0539 Conceptual Design of Electric Misconceptions of Electric Electric Propulsion Modeling Fixed Pitch Propeller Design Impact of Advanced Energy Development of a Solar- Aircraft with Distributed Aircraft and their Emerging for Conceptual Aircraft Design for Electrically Powered Technologies on Aircraft Design Powered Unmanned Aerial Propellers: Multidisciplinary Aviation Markets R. McDonald, California Polytechnic Aircraft R. McDonald, California Polytechnic Vehicle Analysis Needs and Aerodynamic M. Moore, NASA Langley Research State University, San Luis Obispo, CA J. DeStories, T. Takahashi, Arizona State University, San Luis Obispo, CA Z. Lei, Tokyo University of Science, Modeling Development Center, Hampton, VA State University, Tempe, AZ Chino, Japan M. Patterson, B. German, Georgia Institute of Technology, Atlanta, GA Tuesday, 14 January 2014 148-AFM-6 Flight Dynamics and Handling Qualities IV National Harbor Conf Rm 13 Chaired by: A. DOGAN, University of Texas at Arlington and D. MURRI, NASA Langley Research Center 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs AIAA-2014-0540 AIAA-2014-0541 AIAA-2014-0542 AIAA-2014-0543 AIAA-2014-0544 AIAA-2014-0545 The Effects of a Leading Edge Modified Study of Trail Aircraft A Generic Nonlinear A Modified Analysis of Alternate Computation of Safe and Effect of Symmetric and Rotating Cylinder on the Trim Effect on Sweet Spot in Aerodynamic Model for Lateral Trimming Methods for Reachable Sets for Model-Free Asymmetric Span Morphing on Performance of a NACA 0015 Formation Flight Aircraft Flying Wing Aircraft at Sweet Dynamical Systems: Aircraft Flight Dynamics Airfoil at High Angles of Attack W. Okolo, A. Dogan, University of J. Grauer, E. Morelli, NASA Langley Spot in Formation Flight Longitudinal Dynamics C. Beaverstock, R. Ajaj, M. Friswell, D. Welsh, M. Lester, M. Lopes, R. Texas, Arlington, Arlington, TX; W. Research Center, Hampton, VA W. Okolo, A. Dogan, University of Texas, P. Nuthi, K. Subbarao, University of Swansea University, Swansea, Gates, J. Hoover, University of Notre Blake, Air Force Research Laboratory, Arlington, Arlington, TX; W. Blake, Air Texas, Arlington, Arlington, TX United Kingdom; R. De Breuker, Dame, Notre Dame, IN Wright-Patterson AFB, OH Force Research Laboratory, Wright- N. Werter, Delft University of

92 Patterson AFB, OH Technology, Delft, The Netherlands Tuesday, 14 January 2014 149-AMT-3 Review of Skin Friction and Shear Stress Measurement Techniques (Invited) Maryland Ballroom 1 Chaired by: T. LIU, Western Michigan University and V. OTUGEN, Southern Methodist University 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs Oral Presentation (Invited) Oral Presentation (Invited) Oral Presentation (Invited) Oral Presentation (Invited) Oral Presentation (Invited) Oral Presentation (Invited) An Improved Dynamic Shear Measurement of wall shear Wall shear-Stress Measurement Multi-Image Oil Film Polymer Films for Skin Extraction of Skin Friction Stress Sensor Calibration stress in a planar backward- with Micro-Pillars Interferometry Friction and Surface Shear Fields from Surface Flow Technique facing step flow using a micro- E. Gnanamanickam, Embry-Riddle J. Naughton, M. Hind, University of Measurements Visualizations C. Barnard, University of Florida, optical sensor Aeronautical University, Daytona, Wyoming, Laramie, Laramie, WY J. Crafton, J. Webb, N. T. Liu, Western Michigan University, Gainesville, Gainesville, FL; J. Meloy, U. Ayaz, T. Ioppolo, V. Otugen, FL; N. Hutchins, J. Monty, University Rogoshchenkov, R. Forlines, L. Goss, Kalamazoo, MI The Boeing Company, Seattle, WA; A. Southern Methodist University, of Melbourne, Parkville, Austria; J. S. Palluconi, Innovative Scientific Parikh, D. Blood, M. Sheplak, University Dallas, TX Sullivan, Purdue University, West Solutions, Inc., Dayton, OH; et al. of Florida, Gainesville, Gainesville, FL Lafayette, IN Tuesday, 14 January 2014 150-AMT-4 Supersonic Flow Diagnostics Maryland Ballroom 2 Chaired by: D. RICHARDSON, AFRL/RQTC and T. JENKINS, MetroLaser Inc 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs AIAA-2014-0546 AIAA-2014-0547 AIAA-2014-0548 AIAA-2014-0549 AIAA-2014-0550 AIAA-2014-0551 Planar Imaging of Shock Diagnosis of High Speed Design and Applications of Application of Rainbow Schlieren Turbulence Measurements for Flowfield Characterization of Waves at Low Pressure using Flows using Filtered Rayleigh a Sharp Focusing Schlieren Techniques to Shock-Containing Numerical Validation Acquired Linear Aerospike Nozzles Filtered Rayleigh Scattering Scattering System Jets from Cylindrical Nozzles by Ultra High-speed Rainbow H. Takahashi, S. Tomioka, T. Tomita, T. Jenkins, J. George, MetroLaser, J. George, T. Jenkins, Metrolaser, B. Brooker, C. DeSio, A. Few, S. R. Nakajima, T. Oka, University of Schlieren Deflectometry N. Sakuranaka, Japan Aerospace Inc., Laguna Hills, CA; F. Poehlmann, Inc., Laguna Hills, CA; R. Miles, Olcmen, University of Alabama, Kitakyushu, Kitakyushu, Japan; K. P. Kolhe, A. Agrawal, University of Exploration Agency (JAXA), Kakuda, Fluence, LLC, Newark, CA Princeton University, Princeton, NJ Tuscaloosa, Tuscaloosa, AL Konishi, Nagoya University, Nagoya, Alabama, Tuscaloosa, Tuscaloosa, AL Japan Japan; D. Ono, Y. Miyazato, University of Kitakyushu, Kitakyushu, Japan Tuesday, 14 January 2014 151-APA-16 Aerodynamic Design: Analysis, Methodologies and Optimization Maryland Ballroom 4 Chaired by: K. MASSEY, Georgia Tech Research Institute and J. LATZ, Northrop Grumman Aerospace Systems 1430 hrs 1500 hrs 1530 hrs 1600 hrs AIAA-2014-0552 AIAA-2014-0553 AIAA-2014-0554 AIAA-2014-0555 Multi-Objective Genetic Design Aerodynamic Shape Adjoint-based Shape Robust Design Consideration Optimisation for Early Design Optimization of Propulsion Optimization of High-lift Airfoil in the Multi-Disciplinary G. Ferraro, T. Kipouros, A. Savill, Airframe Integration While using the NSU2D Unstructured Optimization of a Flying Wing Cranfield University, Cranfield, United Matching Lift Distribution Mesh Solver UAV Design Kingdom; A. Rampurawala, Airbus, A. Gary, R. McDonald, California T. Nambu, Waseda University, Tokyo, L. Minghang, Y. Hu, Northwestern Bristol, United Kingdom Polytechnic State University, San Luis Japan; D. Mavriplis, K. Mani, University Polytechnical University, Xi’an, China Obispo, CA of Wyoming, Laramie, Laramie, WY Tuesday, 14 January 2014 152-APA-17 Applied CFD National Harbor Conf Rm 5 Chaired by: A. SCLAFANI, Boeing Engineering Operations & Technology and D. FINLEY, Lockheed Martin Aeronautics 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs AIAA-2014-0556 AIAA-2014-0557 AIAA-2014-0558 AIAA-2014-0559 AIAA-2014-0560 AIAA-2014-0561 Examination of Three- A Two-Dimensional/Infinite Cart3D Simulations for Numerical Prediction of Mean Computational and Experimental Simulation of Secondary and Dimensional Flow over a Swept Wing Navier-Stokes the First AIAA Sonic Boom Flow and Acoustic Field of a Assessment of Models for the Separated Flow in a Diffusing Chambered Inflatable Wing Solver Prediction Workshop Supersonic Impinging Jet First AIAA Sonic Boom Prediction S-Duct F. Zhang, K. Ghobadi, R. LeBeau, M. S. Ghasemi, A. Mosahebi, E. M. Aftosmis, NASA Ames Research K. Kurbatskii, ANSYS, Inc., Lebanon, Workshop C. Fiola, R. Agarwal, Washington McQuilling, Saint Louis University, Laurendeau, École Polytechnique de Center, Moffett Field, CA; M. Nemec, NH; S. Kumar, ANSYS, Inc., Pune, S. Cliff, D. Durston, W. Chan, NASA University in St. Louis, St. Louis, MO St. Louis, MO Montréal, Montréal, Canada Science and Technology Corporation, India; H. El-Asrag, ANSYS, Inc., Ames Research Center, Moffett Field, Moffett Field, CA Lebanon, NH CA; A. Elmiligui, NASA Langley Research

93 Center, Hampton, VA; S. Moini-Yekta, E. Sozer, Science and Technology Corporation, Moffett Field, CA; et al. Tuesday, 14 January 2014 153-APA-18 Propeller/Rotorcraft Aerodynamics II Maryland Ballroom A Chaired by: Y. LIAN, University of Louisville 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2014-0562 AIAA-2014-0563 AIAA-2014-0564 AIAA-2014-0565 AIAA-2014-0566 Experimental Investigation of Constrained and Unconstrained Propeller-Wing Interaction Aerodynamic installation Pylon trailing edge blowing the Propeller Design for future Propeller Blade Optimization Prediction for Early Design effects of CROR engines at effects on the performance QESTOL Aircraft in the BNF J. Dorfling, K. Rokhsaz, Wichita G. Ferraro, T. Kipouros, A. Savill, take-off configurations and noise production of a Project State University, Wichita, KS Cranfield University, Cranfield, C. Márquez Gutiérrez, German pusher propeller C. Lenfers, German Aerospace Center United Kingdom; A. Rampurawala, Aerospace Center (DLR), T. Sinnige, L. Veldhuis, Delft (DLR), Braunschweig, Germany; R. Airbus, Bristol, United Kingdom; C. Braunschweig, Germany; S. Steiner, University of Technology, Delft, The Janssen, Delft University of Technology, Agostinelli, Bristol University, Bristol, Rolls-Royce Group plc, Blankenfelde- Netherlands Delft, The Netherlands; N. Beck, J. United Kingdom Mahlow, Germany Friedrichs, Technical University of Braunschweig, Braunschweig, Germany; A. Rezaeian, German Aerospace Center (DLR), Braunschweig, Germany Tuesday, 14 January 2014 154-APA-19 Special Session: Aerodynamic Design Optimization: Current Trends and Future Direction II Maryland Ballroom 3 Chaired by: S. NADARAJAH and S. LEDOUX, Boeing Engineering Operations & Technology 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs AIAA-2014-0567 AIAA-2014-0568 AIAA-2014-0569 AIAA-2014-0570 AIAA-2014-0571 AIAA-2014-0572 RANS-based Aerodynamic Gradient-Based Aerodynamic Aerodynamic Shape Study of parameterizations in Application of Jetstream to a Aerodynamic Design Shape Optimization Optimization with the elsA Optimization by Automatic the project CEDESA Suite of Aerodynamic Shape Optimization: Physics-based Investigations of the Common Software Hybrid Genetic Tool O. Amoignon, Swedish Defense Optimization Problems Surrogate Approaches for Research Model Wing G. Carrier, D. Destarac, A. Dumont, OPTIMENGA_AERO Research Agency (FOI), Stockholm, K. Telidetzki, L. Osusky, D. Zingg, Airfoil and Wing Design Z. Lyu, G. Kenway, J. Martins, M. Meheut, I. Salah El Din, J. Peter, B. Epstein, Academic College of Tel Sweden; J. Hradil, J. Navratil, Brno University of Toronto, Toronto, Canada L. Leifsson, S. Koziel, Reykjavik University of Michigan, Ann Arbor, ONERA, Châtillon, France; et al. Aviv-Jaffa, Tel Aviv, Israel; S. Peigin, University of Technology, Brno, Czech University, Reykjavik, Iceland; Ann Arbor, MI OPTIMENGA, Ltd., Modiin, Israel Republic S. Hosder, Missouri University of Science and Technology, Rolla, MO Tuesday, 14 January 2014 155-DE-3 Design Engineering Chesapeake Conf Rm D Chaired by: G. HONEA, Raytheon Missile Systems and L. SAAM, ATA Engineering, Inc. (HQ) 1430 hrs 1530 hrs 1600 hrs 1630 hrs No Presentations AIAA-2014-0573 AIAA-2014-0574 AIAA-2014-0575 Optimization of mechanism Trawl-Door Design Optimization Hyperion - three years of design of flapping wing MAV by Local Surrogate Models novel aircraft design V. Kalpathy Venkiteswaran, H. Su, L. Leifsson, S. Koziel, Reykjavik J. Koster, University of Colorado, Ohio State University, Columbus, OH University, Reykjavik, Iceland; E. Boulder, Boulder, CO Hermannsson, R. Fakhraie, Royal Institute of Technology (KTH), Stockholm, Sweden 94 Tuesday, 14 January 2014 156-FD-20 Combustion Engines Maryland Ballroom 5 Chaired by: M. HARVAZINSKI, Air Force Research Laboratory and S. SILTON, US Army Research Laboratory 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs AIAA-2014-0576 AIAA-2014-0577 AIAA-2014-0578 AIAA-2014-0579 AIAA-2014-0580 AIAA-2014-0581 RANS-based Multi-Scale Parametric Trends in Assessing Energy Losses Further Assessment of Aerosol Modeling of Soot Acoustic timescale analysis of Simulations of a Scramjet the Combustion Stability Associated with the Pulsating Turbulent Inflow Boundary Nanoparticles in a Turbulent a model hot spot Combustor Characteristics of a Single- Flow in the Exhaust Port of an Conditions for Rocket Motor Diffusion Flame Using An M. Kurtz, J. Regele, Iowa State E. Hassan, D. Eklund, Air Force Element Gas-Gas Rocket Internal Combustion Engine Internal Flows Extended Detailed Kinetic University, Ames, IA Research Laboratory, Wright- Engine Y. Wang, B. Semlitsch, M. D. Gonzalez, Naval Surface Warfare Scheme Patterson AFB, OH; H. Aono, Japan M. Harvazinski, V. Sankaran, D. Mihaescu, L. Fuchs, Royal Institute Center, Indian Head, MD; M. Lewis, M. Darbandi, M. Ghafourizadeh, Aerospace Exploration Agency Talley, Air Force Research Laboratory, of Technology (KTH), Stockholm, Science and Technology Policy Sharif University of Technology, (JAXA), Sagamihara, Japan Edwards AFB, CA Sweden Institute, Washington, DC Tehran, Iran; G. Schneider, University of Waterloo, Waterloo, Canada Tuesday, 14 January 2014 157-FD-21 RANS Turbulence Modeling: Strengths, Weaknesses and New Approaches Chesapeake Conf Rm 8 Chaired by: B. SMITH, Lockheed Martin Aeronautics and R. BOWERSOX, Texas A&M University 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs AIAA-2014-0582 AIAA-2014-0583 AIAA-2014-0584 AIAA-2014-0585 AIAA-2014-0586 AIAA-2014-0587 Investigation of the Validity An Assessment of Attached Development of an extended Initial Validation of a Non- On “Steady” RANS Modeling Variable Surface Roughness of the Spalart-Allmaras and Mildly Separated Flows non-linear turbulence model and equilibrium Wilcox k - omega for improved Prediction of Modeling for Skin Friction Turbulence Model for Confined in Adverse Pressure Gradient its application for analysis of Turbulence Model in Subsonic Wall-bounded Separation Estimation Impinging Slot Jets Regions three-dimensional wall jets and Transonic Flow Regimes S. Jakirlic, R. Maduta, Technical S. Medida, J. Baeder, University A. Tahsini, S. Tadayon Mousavi, A. de Jesus, L. Schiavo, Technological K. Ishiko, Japan Aerospace Exploration T. Kudla, M. Rumpfkeil, University of University of Darmstadt, Darmstadt, of Maryland, College Park, College Aerospace Research Institute, Institute of Aeronautics (ITA), São Agency (JAXA), Tokyo, Japan; K. Dayton, Dayton, OH Germany Park, MD; N. Nigam, P. Chen, Tehran, Iran José dos Campos, Brazil; J. Azevedo, Tonsho, Ryoyu Systems Company, Intelligent Automation, Inc., Aeronautics and Space Institute (IAE), Ltd., Nagoya, Japan; A. Hashimoto, Rockville, MD São José dos Campos, Brazil; J. T. Aoyama, Y. Matsuo, A. Yoshizawa, Laval, Lille University of Science and Japan Aerospace Exploration Agency Technology, Villeneuve d’Ascq, France (JAXA), Tokyo, Japan Tuesday, 14 January 2014 158-FD-22 Turbulence II: Large Eddy Simulations National Harbor Conf Rm 3 Chaired by: S. HEINZ, University of Wyoming and J. SEIDEL, USAF Academy 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs AIAA-2014-0588 AIAA-2014-0589 AIAA-2014-0590 AIAA-2014-0591 AIAA-2014-0592 AIAA-2014-0593 High-Order Implicit Large- Unified RANS-LES Analysis Effect of Boundary Layer Analysis of the Onset Turbulence Structure Generating inflow turbulence Eddy Simulations of Supersonic of Turbulent Jets Covering Thickness on Jet Mixing in a of Dynamic Stall Using Characteristics of LES Methods for eddy simulation of Corner Flo Several Swirl Number Regimes Supersonic Turbulent Crossflow High-Fidelity Large-Eddy Implied by Stochastic Turbulence turbomachinery flows

95 N. Bisek, Air Force Research S. Heinz, C. Zemtsop, H. Gopalan, T. Rossmann, Lafayette College, Simulations Models S. Arolla, P. Durbin, Iowa State Laboratory, Wright-Patterson AFB, OH M. Stoellinger, University of Easton, PA; A. Pizzaia, Rutgers M. Visbal, Air Force Research P. Saha, S. Heinz, E. Kazemi, University University, Ames, IA Wyoming, Laramie, Laramie, WY University, Piscataway, NJ Laboratory, Wright-Patterson AFB, OH of Wyoming, Laramie, Laramie, WY Tuesday, 14 January 2014 159-GEPC-2 Progress Towards N+3 Technologies in NASA’s Fixed Wing Project Woodrow Wilson A Chaired by: R. WAHLS, NASA-Langley Research Center and N. MADAVAN, NASA Ames Research Center 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs Oral Presentation (Invited) AIAA-2014-0594 AIAA-2014-0595 AIAA-2014-0596 AIAA-2014-0597 AIAA-2014-0598 NASA Fixed Wing Project: Green A Noise and Emissions Changing the Paradigm - High Aspect Ratio Wing Current and Future Research in Aeroelastic Tailoring of the Technologies for Future Aircraft Assessment of the N3-X Feasibility of Protective Skins Design: Optimal Aerostructural Active Control of Lightweight, NASA Common Research Generations Transport for Composite Airliners Tradeoffs for the Next Flexible Structures Using the Model via Novel Material and R. Del Rosario, J. Koudelka, NASA Glenn J. Berton, W. Haller, NASA Glenn V. Johnson, R. Boone, S. Jones, V. Generation of Materials X-56 Aircraft Structural Configurations Research Center, Cleveland, OH; R. Research Center, Cleveland, OH Pendse, G. Hayward, Cessna Aircraft J. Martins, G. Kennedy, G. Kenway, J. Ryan, J. Bosworth, NASA Dryden C. Jutte, Craig Technologies, Inc., Wahls, NASA Langley Research Center, Company, Wichita, KS University of Michigan, Ann Arbor, Flight Research Center, Edwards, CA Cape Canaveral, FL; B. Stanford, C. Hampton, VA; N. Madavan, NASA Ames Ann Arbor, MI Wieseman, J. Moore, NASA Langley Research Center, Moffett Field, CA Research Center, Hampton, VA Tuesday, 14 January 2014 160-GNC-9 Aircraft Guidance, Navigation and Control I National Harbor Conf Rm 7 Chaired by: A. WILDSCHEK, European Aeronautic Defence and Space Company and T. ZSEDROVITS 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs AIAA-2014-0599 AIAA-2014-0600 AIAA-2014-0601 AIAA-2014-0602 AIAA-2014-0603 AIAA-2014-0604 Flight Dynamics and Control A Summary of Revisions A Robust and Self-Scheduled Flight Tests of a General Multi-Input Higher-order Towards Real-Time Visual and Related Challenges for Design Applied to a Turbulence Longitudinal Flight Control Aviation Envelope Protection Sliding Mode Control of IMU Data Fusion of a Commercial Blended Wing Response Analysis Method for System: a Multi-Model and and Stability Augmentation Aeroelastic Systems With T. Zsedrovits, Pázmány Péter Catholic Body Aircraft Flexible Aircraft Configurations Structured H-infinity Approach System Uncertainties and Gust Load University, Budapest, Hungary; A. Wildschek, EADS, Munich, C. Funk, B. Perry, W. Silva, NASA H. Lhachemi, D. Saussie, G. Zhu, J. Wilson, Upper Valley Aero, LLC, K. Lee, Kwandong University, P. Bauer, Hungarian Academy of Germany Langley Research Center, Hampton, École Polytechnique de Montréal, Hanover, NH; M. Peters, Saab Sensis Gangwon, South Korea; S. Singh, Sciences, Budapest, Hungary; A. VA; B. Newman, Old Dominion Montréal, Canada Corporation, East Syracuse, NY; G. University of Nevada, Las Vegas, Las Zarandy, Pázmány Péter Catholic University, Norfolk, VA Pettit, Dysim, Mattaponi, VA Vegas, NV University, Budapest, Hungary; B. Vanek, J. Bokor, Hungarian Academy of Sciences, Budapest, Hungary; T. Roska, Pázmány Péter Catholic University, Budapest, Hungary Tuesday, 14 January 2014 161-GNC-10 Novel Navigation, Estimation, and Tracking Methods National Harbor Conf Rm 8 Chaired by: L. POLLINI, University of Pisa and Y. CHENG, Mississippi State University 1430 hrs 1500 hrs 1530 hrs AIAA-2014-0605 AIAA-2014-0606 AIAA-2014-0607 UAS Source Localization Fixed-Point Smoothing Approach Solving Optimal Positioning with High Latency Sensors in for Dual-Mode Guidance Filtering Problems via Homotopy Turbulent Environments with Delayed Measurement Continuation 96 M. Palframan, C. Woolsey, Virginia S. Kim, Korea Advanced Institute of Y. Tian, Harbin Institute of Polytechnic Institute and State Science and Technology, Daejeon, South Technology, Harbin, China; Y. University, Blacksburg, VA Korea; B. Park, LIG Nex1, Seongnam, Cheng, Mississippi State University, South Korea; H. Choi, M. Tahk, Korea Mississippi State, MS Advanced Institute of Science and Technology, Daejeon, South Korea Tuesday, 14 January 2014 162-GNC-11 Validation of Onboard Systems Technologies for LOC Prevention and Recovery, Session (Invited) I National Harbor Conf Rm 12 Chaired by: K. FEIGH, Georgia Institute of Technology and D. CRIDER, National Transportation Safety Board 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs AIAA-2014-0608 AIAA-2014-0609 AIAA-2014-0610 AIAA-2014-0611 AIAA-2014-0612 AIAA-2014-0613 A Formal Approach to the Pilot Mental Models and Loss Certification Analysis for Sensitivity of the Generic Preliminary Analysis of Aircraft Pilot-in-the-Loop Flight Identication and Validation of of Control a Model-Based UAV Fault Transport Model upset Loss of Control Accidents: Worst Simulator for NASA’s Transport Empirical Dynamic Models S. Mamessier, K. Feigh, A. Pritchett, Detection System dynamics to time delay Case Precursor Combinations and Class Model L. Crespo, E. Morelli, S. Kenny, D. Dickson, Georgia Institute of B. Hu, P. Seiler, University S. Gill, M. Lowenberg, University Temporal Sequencing K. Ackerman, S. Pelech, R. D. Giesy, NASA Langley Research Technology, Atlanta, GA of Minnesota, Minneapolis, of Bristol, Bristol, United Kingdom; C. Belcastro, J. Foster, NASA Langley Carbonari, N. Hovakimyan, A. Center, Hampton, VA Minneapolis, MN L. Crespo, National Institute of Research Center, Hampton, VA; R. Kirlik, University of Illinois, Urbana- Aerospace, Hampton, VA; S. Neild, Newman, Crew Systems, Seattle, Champaign, Urbana, IL; I. Gregory, University of Bristol, Bristol, United WA; L. Groff, D. Crider, National NASA Langley Research Center, Kingdom; B. Krauskopf, University of Transportation Safety Board, Hampton, VA Auckland, Auckland, New Zealand; Washington, DC; D. Klyde, Systems G. Puyou, Airbus, Toulouse, France Technology, Inc., Hawthorne, CA Tuesday, 14 January 2014 163-GT-4 Wind Tunnel Data Corrections Maryland Ballroom B Chaired by: S. SIMERLY, NASA Glenn Research Center and R. GUYTON, USAF Wright Lab 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs AIAA-2014-0614 AIAA-2014-0615 AIAA-2014-0616 AIAA-2014-0617 AIAA-2014-0618 AIAA-2014-0619 A Practical Method to Verification and Expansion of Verification of the Hensel Spectral Characteristics of Towards Interference Corrections Measurement and Analysis Determine True Pitching the Hensel Blockage Correction Blockage Correction in Free-stream Turbulence in the for Three-Dimensional Models of Background Noise in NF-6 Moment for Internal Balance in the National Full-Scale the National Full-Scale National Transonic Facility in Kevlar-Walled Anechoic Test Pressurized Transonic Wind Wind Tunnel Testing with Aerodynamics Complex 80- by Aerodynamics Complex K. Owen, A. Owen, Complere, Inc., Sections Tunnel Longitudinal Variation in Flow 120-foot Wind Tunnel 40- by 80-foot Wind Tunnel Pacific Grove, CA K. Brown, W. Devenport, A. Borgoltz, Y. Ji, C. Gao, Z. Zhang, N. Wang, Angularity P. Goulding, NASA Ames Research Using Hypersonic Inflatable Virginia Polytechnic Institute and State B. Wu, Northwestern Polytechnical K. Kelly, Wichita State University, Center, Moffett Field, CA Aerodynamic Decelerators University, Blacksburg, VA; H. Ura, K. University, Xi’an, China Wichita, KS P. Goulding, NASA Ames Research Yamamoto, Japan Aerospace Exploration Center, Moffett Field, CA Agency (JAXA), Tokyo, Japan Tuesday, 14 January 2014 164-GTE-4 Gas Turbine Combustor II Woodrow Wilson D Chaired by: F. DRYER, Princeton University and L. MADDALENA, The University of Texas at Arlington 1430 hrs 1500 hrs 1530 hrs 1600 hrs AIAA-2014-0620 AIAA-2014-0621 AIAA-2014-0622 AIAA-2014-0623 Computational Study of LES Investigation of Flow Field Plasma Control of Combustion Recurrence Analysis of Combustion Dynamics in a Sensitivity in a Gas Turbine Instability in a Lean Direct Combustion Generated Noise Single-Element Lean Direct Model Combustor Injection Gas Turbine L. Kabiraj, H. Nawroth, A. Saurabh, Injection Gas Turbine Combustor Y. See, University of Michigan, Ann Combustor C. Paschereit, Technical University of C. Yoon, R. Gejji, W. Anderson, Arbor, Ann Arbor, MI; M. Ihme, J. D’Entremont, R. Gejji, V. Berlin, Berlin, Germany

97 Purdue University, West Lafayette, Stanford University, Stanford, CA Lakshmanan, P. Venkatesh, S. Bane, IN; V. Sankaran, Air Force Research W. Anderson, Purdue University, West Laboratory, Edwards AFB, CA Lafayette, IN Tuesday, 14 January 2014 165-HSABP-2 CFD Analysis of Scramjets I Chesapeake Conf Rm 7 Chaired by: B. SEKAR, USAF AFRL/RZTC and H. HASSAN, North Carolina State University 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs AIAA-2014-0624 AIAA-2014-0625 AIAA-2014-0626 AIAA-2014-0627 AIAA-2014-0628 AIAA-2014-0629 Turbulence Model Effects Comparison of Mode-Transition High Fidelity Analysis of a Turbulence / Chemistry Effect of ramp interaction on Multi-Objective Design and on RANS Simulations of the Phenomena in Axisymmetric Three Dimensional Supersonic Interactions in a Ramp- global mixing modes induced Trajectory Optimization of HIFiRE Flight 2 Ground Test and Rectangular Scramjet Pulse Detonation Combustor Stabilized Supersonic by hypermixers Space Transport Systems Configurations Flowpaths F. Malo-Molina, Air Force Research Hydrogen-Air Diffusion Flame L. Massa, University of Texas, with RBCC Propulsion via N. Georgiadis, M. Mankbadi, M. R. Yentsch, D. Gaitonde, Ohio State Laboratory, Wright-Patterson AFB, OH J. Fulton, Sandia National Arlington, Arlington, TX Evolutionary Algorithms and Vyas, NASA Glenn Research Center, University, Columbus, OH Laboratories, Albuquerque, NM; Pseudospectral Methods Cleveland, OH J. Edwards, North Carolina State M. Kodera, Japan Aerospace University, Raleigh, NC; A. Cutler, Exploration Agency (JAXA), Kakuda, George Washington University, Japan; H. Ogawa, RMIT University, Washington, DC; J. McDaniel, Melbourne, Australia; S. Tomioka, S. C. Goyne, University of Virginia, Ueda, Japan Aerospace Exploration Charlottesville, Charlottesville, VA Agency (JAXA), Kakuda, Japan Tuesday, 14 January 2014 166-LECT-5 NDA Special Session: Assuring Aero-Structural Reliability in an Uncertain World Maryland Ballroom C 1430 - 1530 hrs Ravi Chona USAF Senior Scientist and Director, Structural Sciences Center Air Force Research Laboratory Tuesday, 14 January 2014 167-MAT-4 Advanced Composites & Fabrics Chesapeake Conf Rm A Chaired by: K. SHIVAKUMAR, North Carolina Agricultural and Technical State University and A. KELKAR, Joint School of Nanoscience & Nanoengineering 1430 hrs 1530 hrs 1600 hrs 1630 hrs No Presentations AIAA-2014-0630 AIAA-2014-0631 AIAA-2014-0632 Microvascular composite skin Modeling of Plain Woven Novel Composite Space Shielding panels for hypersonic aircraft Fabrics for Inflatable Concepts for Hypervelocity A. Najafi, A. Coppola, S. Soghrati, Aerodynamic Decelerators Orbital Debris Impact Mitigation N. Sottos, S. White, P. Geubelle, J. Hill, R. Braun, Georgia Institute of S. Offenberger, J. Warren, T. Lacy, University of Illinois, Urbana- Technology, Atlanta, GA Mississippi State University, Mississippi Champaign, Urbana, IL State, MS; A. Al-Ostaz, University of Mississippi, Oxford, Oxford, MS; H. Toghiani, S. Kundu, Mississippi State University, Mississippi State, MS; et al. Tuesday, 14 January 2014 168-MDO-4 Structural and Topology Optimization Chesapeake Conf Rm 4 Chaired by: G. KENNEDY, University of Toronto and H. KIM, University of Bath 98 1430 hrs 1530 hrs 1600 hrs 1630 hrs No Presentations AIAA-2014-0633 AIAA-2014-0634 AIAA-2014-0635 Optimal Topology of Aircraft Aerostructural Level Set Rules, Precursors and Rib and Spar Structures under Topology Optimization for a Parameterisation Methodologies Aeroelastic Loads Common Research Model Wing for Topology Optimised Structural B. Stanford, NASA Langley Research P. Dunning, National Institute of Designs Realised Through Center, Hampton, VA; P. Dunning, Aerospace, Hampton, VA; B. Stanford, Additive Manufacturing National Institute of Aerospace, NASA Langley Research Center, M. Muir, EADS, Bristol, United Kingdom; Hampton, VA Hampton, VA; H. Kim, University of O. Querin, V. Toropov, University of Bath, Bath, United Kingdom Leeds, Leeds, United Kingdom Tuesday, 14 January 2014 169-MST-2 Modeling and Simulation Tools and Technologies National Harbor Conf Rm 6 Chaired by: R. RUFF 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs AIAA-2014-0636 AIAA-2014-0637 AIAA-2014-0638 AIAA-2014-0639 AIAA-2014-0640 AIAA-2014-0641 Openness Requirements for Accelerating Genetic Algorithm Numerical Study on Drag DIMMACSS-Stage: a Testability, Test Automation Validation of Different Control Next Generation Hardware-in- Profile Fitting Using a Six-DOF Reduction for Swept-back, Distributed Intelligence Model and Test Driven Development System Techniques using the-Loop Testing Systems Enhanced with GPU Coding Swept-front , Delta Grid Fin for a Multi-Agent Control for the Trick Simulation Toolkit Modeling and Simulation A. Himmler, dSPACE GmbH, R. Hartfield, J. Burkhalter, D. Benton, with Blunt and Sharp Leading System using Simulink and the J. Penn, L-3 Communications, M. Mohamed, Deference Systems Paderborn, Germany Auburn University, Auburn, AL Edges Stage robotic simulator Houston, TX Studies Center, Cairo, Egypt; A. Aly, W. Dan, Y. Yong, Beijing Institute of S. Walker, J. Shan, L. Liu, York Military Technical College, Cairo, Technology, Beijing, China University, Toronto, Canada Egypt; A. El Ramlawy, Deference Systems Studies Center, Cairo, Egypt Tuesday, 14 January 2014 170-MVC-4 Current Status and Future Trends of Integrated Computational Environments Chesapeake Conf Rm 9 1430 - 1730 hrs Chaired by: G. POWER, Aerospace Testing Alliance Computational environments are becoming increasingly critical for effective application of advanced computational tools through the management of the process and comprehension of the resulting data. Experts from government, industry and academia will discuss the current status and future trends of computational environments for improved engineering decision making. Panelists: Kenneth Moreland Kenneth “Mark” Bryden Andrew W. Cary David McDaniel Steve M. Legensky Computation, Computers, Information and Mathematics Program Director, Simulation, Modeling, and Decision Technical Fellow - CFD DoD CREATE/Kestrel Development Team General Manager and Founder Center Science The Boeing Company University of Alabama at Birmingham Intelligent Light Sandia National Laboratories Ames Laboratory

Tuesday, 14 January 2014 171-NDA-4 Reliability Chesapeake Conf Rm 5 Chaired by: G. BARTRAM, Vanderbilt University and L. DOMYANCIC, Southwest Research Institue 1430 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs No Presentations AIAA-2014-0642 AIAA-2014-0643 AIAA-2014-0644 AIAA-2014-0645 Probability of Failure Analysis Ignoring Dependence between Integration of System Reliability Estimation Using and Design Using An Efficient Failure Modes is Reasonable Reliability Analysis and Guided Tail Modeling with Sequential Sampling Approach for Low Probabilities of Failure FMECA to Efficiently Identify Adaptive Sampling Z. Wang, P. Wang, Wichita State C. Park, N. Kim, University of Florida, Structural Hot Spots E. Acar, TOBB University of University, Wichita, KS Gainesville, Gainesville, FL C. Quintana, H. Millwater, University Economics and Technology, Ankara, of Texas, San Antonio, San Antonio, Turkey; P. Ramu, Indian Institute of Technology Madras, Chennai, India 99 TX; R. Penmetsa, Air Force Research Laboratory, Wright-Patterson AFB, OH Tuesday, 14 January 2014 172-PANEL-4 Turning Technology Into a Business Panel Potomac Ballroom C 1430 - 1630 hrs Moderator: Stephen Fleming, Vice President & Executive Director, Enterprise Innovation Institute, Georgia Tech Panelists: Jason Dunn Debra Facktor Lepore David Thompson John Tylko Co-founder and CTO Vice President and General Manager, Strategic Operations CEO President Made In Space, Inc. Ball Aerospace & Technologies Corporation Orbital Sciences Corporation Aurora Flight Sciences Tuesday, 14 January 2014 173-PC-8 Heterogeneous Combustion and Propellants Chesapeake Conf Rm G Chaired by: X. YANG, Princeton University and A. HIGGINS, McGill University 1430 hrs 1500 hrs 1530 hrs 1600 hrs AIAA-2014-0646 AIAA-2014-0647 AIAA-2014-0648 AIAA-2014-0649 Ignition and Reaction Analysis Microsphere Composites of Burning Rate of nano- Evaluation of a laser beam of High Loading Nano-Al/ Nano-Al and Nanothermite: An Aluminum-Water Propellant at scanning method for correction Fluoropolymer Energetic Approach to Better Utilization High Pressures of multiple scattering and Composite Films of Nanomaterials W. Georges, Y. Yavor, A. Higgins, S. attenuation effects in dense J. DeLisio, University of Maryland, H. Wang, G. Jian, J. DeLisio, M. Goroshin, McGill University, Montréal, spray measurements College Park, College Park, MD; C. Zachariah, University of Maryland, Canada; R. Stowe, S. Ringuette, G. Charalampous, Y. Hardalupas, Huang, Nanjing University of Science College Park, College Park, MD Defense Research and Development Imperial College London, London, and Technology, Nanjing, China; G. Jian, Canada, Québec City, Canada United Kingdom M. Zachariah, University of Maryland, College Park, College Park, MD; G. Young, Naval Surface Warfare Center, Indian Head, MD Tuesday, 14 January 2014 174-PC-9 Laminar Flames Chesapeake Conf Rm I Chaired by: S. WON, Princeton University 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs AIAA-2014-0650 AIAA-2014-0651 AIAA-2014-0652 AIAA-2014-0653 AIAA-2014-0654 AIAA-2014-0655 Effects of Flow Strain Rates on Effect of Axial Diffusion on the Soot Formation in Laminar Minor Species Measurements in Role of Azimuthal Flow Further Aspects of the Counterflow Diffusion Flames Response of Over-ventilated Diffusion Flames of Diluted Premixed Cellular Tubular Flames Fluctuations on Flow Dynamics Behavior of Edge Flames with

100 at Subcritical and Supercritical Diffusion Flames to Axial Flow Ethylene in Air at Pressures up C. Hall, Vanderbilt University, Nashville, and Global Flame Response of a Fuel Spray in a Mixing Layer Pressures: Oxygen/Methane Perturbations to 20 ATM TN; W. Kulatilaka, N. Jiang, Spectral Axisymmetric Swirling Flames J. Greenberg, Technion--Israel Mixture N. Magina, T. Lieuwen, Georgia A. Karatas, O. Gulder, University of Energies, LLC, Dayton, OH; J. Gord, V. Acharya, T. Lieuwen, Georgia Institute of Technology, Haifa, Israel X. Wang, V. Yang, Georgia Institute Institute of Technology, Atlanta, GA Toronto, Toronto, Canada Air Force Research Laboratory, Wright- Institute of Technology, Atlanta, GA of Technology, Atlanta, GA Patterson AFB, OH; R. Pitz, Vanderbilt University, Nashville, TN Tuesday, 14 January 2014 175-PC-10 Turbulent Flames II Chesapeake Conf Rm H Chaired by: B. WINDOM, Princeton University and I. BOXX, DLR - German Aerospace Center 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2014-0656 AIAA-2014-0657 AIAA-2014-0658 AIAA-2014-0659 AIAA-2014-0660 OH-PLIF Studies in a LDI Swirl- Flow Dynamics of a Simplex Effect of Excitation Amplitude Stability Analysis of Reacting Investigation of Dimethyl Ether Stabilized Combustor Swirl Injector at Supercritical on Disturbance Field of a Wakes: The Physical Role of Combustion Instabilities in a R. Villalva Gomez, B. Dolan, D. Conditions Transversely Forced Swirl Flow Flame-Shear Layer Offset Partially - Premixed Gas Turbine Munday, E. Gutmark, University of H. Huo, X. Wang, V. Yang, Georgia and Flame B. Emerson, D. Noble, T. Lieuwen, Model Combustor Using High- Cincinnati, Cincinnati, OH Institute of Technology, Atlanta, GA J. O’Connor, Pennsylvania State Georgia Institute of Technology, Speed Laser Diagnostics University, University Park, PA Atlanta, GA P. Allison, Y. Chen, J. Driscoll, University of Michigan, Ann Arbor, Ann Arbor, MI Tuesday, 14 January 2014 176-PDL-6 Plasma-Assisted Combustion I Azalea 3 Chaired by: S. LEONOV, JIHT RAS 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2014-0661 AIAA-2014-0662 AIAA-2014-0663 AIAA-2014-0664 AIAA-2014-0665 Studying The Atmospheric Multi-Pulse Operation at Ignition of nanosecond Investigation of the Effects Ignition of CH4:O2:Ar and Plasma Jet For The Plasma- Plasma-Assistance in High- discharge in liquids: cavitation of Non-Equilibrium Plasma n-C4H10:O2:Ar(N2) mixtures Assisted Combustion Speed Combustor bubble, bushy and ﬁlamentary Discharges on Temperature with initial temperatures between S. Kolosenok, A. Savarovskii, S. Leonov, Ohio State University, discharge and OH Concentrations in 650-950 K by a surface pulsed A. Kuranov, Hypersonic Systems Columbus, OH; A. Napartovich, S. Starikovskaya, A. Rousseau, I. Low-Pressure Premixed Flames discharge Research Institute, Saint Petersburg, I. Kochetov, Russian Academy Marinov, Pierre and Marie Curie T. Li, I. Adamovich, J. Sutton, Ohio S. Stepanyan, École Polytechnique, Russia; V. Soukhomlinov, Saint of Sciences, Troitsk, Russia; D. University, Palaiseau, France State University, Columbus, OH Paris, France; M. Bouhmedi, G. Petersburg State University, Saint Yarantsev, Russian Academy of Vanhove, P. Desgroux, Lille University of Petersburg, Russia; V. Bychkov, Sciences, Moscow, Russia Science and Technology, Lille, France; Moscow State University, Moscow, N. Popov, Moscow State University, Russia Moscow, Russia; S. Starikovskaya, École Polytechnique, Paris, France Tuesday, 14 January 2014 177-PDL-7 Plasma Discharge Structure Maryland Ballroom 6 Chaired by: S. MACHERET, Lockheed Martin Aeronautics 1430 hrs 1500 hrs 1530 hrs AIAA-2014-0666 AIAA-2014-0667 AIAA-2014-0668 Filamentation of the nanosecond Studies of Nanosecond Pulse Turbulent Cascade Process in surface dielectric barrier Surface Ionization Wave Arc Driven Plasma Channels

101 discharge at elevated pressures Discharges over Solid and A. Tropina, Kharkov National S. Stepanyan, École Polytechnique, Liquid Dielectric Surfaces Automobile and Highway University, Paris, France; N. Popov, Moscow V. Petrishchev, S. Leonov, W. Kharkov, Ukraine; M. Shneider, State University, Moscow, Russia; S. Lempert, I. Adamovich, Ohio State R. Miles, Princeton University, Starikovskaya, École Polytechnique, University, Columbus, OH Princeton, NJ Paris, France Tuesday, 14 January 2014 178-SAT-2 Space and Society: Social Dimensions of Space Exploration and Exploitation National Harbor Conf Rm 15 Chaired by: C. HEARSEY, The University of Mississippi and B. STEINFELDT, Georgia Institute of Technology 1430 hrs 1500 hrs 1530 hrs 1600 hrs AIAA-2014-0669 AIAA-2014-0670 Oral Presentation (Invited) Oral Presentation (Invited) Astrosociology: Fostering Musical Counter Narratives: The Foreign Space Flight Legal and Policy Issues of Collaborative Synergy between Space, Skepticism, and Participant Problem: Can Emergent Private Sector Members of the Social Sciences Religion in American Music a Space Flight Operator Space Activities: Impacting and Those of the Traditional P. Blount, University of Mississippi, Balance Satisfaction of FAA the Evolution of International Space Community University, University, MS; J. Fussell, Informed Consent Information Space Law J. Pass, Astrosociology Research Self, Oxford, MS Requirements with ITAR? M. Mineiro, Science and Technology Institute, Huntington Beach, CA C. Hearsey, Astrosociology Research Policy Institute, Washington, DC Institute, Silver Spring, MD Tuesday, 14 January 2014 179-SCS-1 Materials for Gossamer Systems Chesapeake Conf Rm 6 Chaired by: M. SANTER, Imperial College London and M. SILVER, MIT Lincoln Laboratory 1430 hrs 1530 hrs 1600 hrs 1630 hrs No Presentations AIAA-2014-0671 AIAA-2014-0672 AIAA-2014-0673 Adaptive Multistable Flexible A Quasi-Static Nonlinear Model MOIRE: Membrane Material Composite Surfaces of Shape Memory Polymer Property Characterizations, Y. Cui, M. Santer, Imperial College Composite Beams for Space Testing and Lessons Learned London, London, United Kingdom Applications T. Copp, J. Domber, P. Atcheson, W. D. Bergman, B. Yang, University of Tandy, J. Kommers, Ball Aerospace Southern California, Los Angeles, CA; & Technologies Corporation, Boulder, H. Fang, Shanghai YS Information CO; B. Farmer, NeXolve Corporation, Technology Company, Ltd., Huntsville, AL Shanghai, China Tuesday, 14 January 2014 180-SD-7 Computational Aeroelasticity II Chesapeake Conf Rm C Chaired by: D. RAVEH and R. GORDNIER, Air Force Reseach Laboratory 1430 hrs 1530 hrs 1600 hrs 1630 hrs No Presentations AIAA-2014-0674 AIAA-2014-0675 AIAA-2014-0676 Computational Transonic The NASA High Speed ASE Analytical Correlation of a Flutter Solutions for Cranked Project: Computational Analyses Flexible Empennage Wind Wing Planforms of a Low-Boom Supersonic Tunnel Flutter Test at High E. Mellquist, The Aerospace Conﬁguration Transonic Mach Number Corporation, El Segundo, CA; O. W. Silva, NASA Langley Research Center, F. von Knoblauch, R. Moreno,

102 Bendiksen, University of California, Hampton, VA; A. De La Garza, P. Zink, P. Taylor, Gulfstream Aerospace Los Angeles, Los Angeles, CA E. Bounajem, C. Johnson, Lockheed Corporation, Savannah, GA; J. Martin Corporation, Fort Worth, TX; Newsom, Newsom Aerospace M. Buonanno, Lockheed Martin Consulting, LLC, Poquoson, VA Corporation, Palmdale, CA; et al. Tuesday, 14 January 2014 181-SD-8 Nonlinear Dynamics and Aeroelasticity Chesapeake Conf Rm B Chaired by: R. YURKOVICH and M. ALLEN, University of Wisconsin 1430 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs No Presentations AIAA-2014-0677 AIAA-2014-0678 AIAA-2014-0679 AIAA-2014-0680 Aeroelasticity and Dynamic Design and Development of Uncertainties in control surface Aeroservoelastic Optimization Analysis of Cracked Composite New Whirl Flutter Aeroelastic free-play and structural of Varying Wing Sweep Angle Wings Using Spectral Finite Demonstrator properties and their effect on Platform Element Method J. Cecrdle, J. Malecek, Aeronautical flutter and LCO S. Buchnik, M. Karpel, Technion-- R. Elkins, G. Wang, University of Research and Test Institute (VZLU), D. Pitt, P. Bansal, The Boeing Israel Institute of Technology, Haifa, Alabama, Huntsville, Huntsville, AL Prague, Czech Republic Company, St. Louis, MO Israel Tuesday, 14 January 2014 182-SE-1 Systems Engineering National Harbor Conf Rm 14 Chaired by: J. EILER, Stellar Solutions, Inc. and D. DRESS, NASA Langley Research Center 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2014-0681 AIAA-2014-0682 AIAA-2014-0683 AIAA-2014-0684 AIAA-2014-0685 An Integrated and Parametric Quantification of Margins and Requirements and Concepts of Proposed Variants for a Raytheon Weapon Server Environment for Generation, Uncertainties for Aerospace Operations for a Personalized Collaborative Aerospace (RWS) Selection and Evaluation of New Systems using Stochastic Air Transport System in 2050 Lifecycle Systems Engineering S. Baba, Raytheon Company, Architectures at a Conceptual Expansions N. Randt, S. Sartorius, Technical Master’s Program Tucson, AZ Level: Application to the T. West, S. Hosder, Missouri University of Munich, Munich, J. Silva, Georgia Institute of Environmental Control System University of Science and Germany Technology, Atlanta, GA C. Frank, W. Levy, E. Garcia, D. Technology, Rolla, MO; T. Winter, M4 Mavris, J. Durand, Georgia Institute of Engineering, Inc., Long Beach, CA Technology, Atlanta, GA Tuesday, 14 January 2014 183-SOF-1 Cybersecurity in Space Systems Panel National Harbor Conf Rm 2 1430 - 1730 hrs Chaired by: D. LAVALLEE, JHU/Applied Physics Laboratory 1430-1600 hrs Moderator: Richard M. (Dickie) George, Senior Advisor for Cybersecurity, JHU/APL The panel will include any aspect of spacecraft, link, ground station, and operations centers. national security, civilian, and commercial systems will be discussed. Panelists: Sam Adhikari Col. Scott Lathrop Dr. Norm Moulton Dr. Mark Maybury Phil Bounds (Ret) VP, Operations and Research, Sysoft Corporation, Deputy Director, Advanced Capabilities Directorate Director, J9, Advanced Concepts and Technologies Chief Technology Officer, MITRE Corporation Senior Strategic Security Advisor for Human 103 and Chair of the AIAA Cybersecurity Working U.S. Cyber Command U.S. Cyber Command Former Chief Scientist and Author of Air Force Exploration and Operations Mission Directorate, Group Cyber Vision 2025 NASA HQ

1600-1730 hrs AIAA Cybersecurity Working Group, Open Meeting

Tuesday, 14 January 2014 184-SRE-3 Environmental Factors in Extraterrestrial Systems National Harbor Conf Rm 4 Chaired by: D. BOUCHER, Deltion Innovations Ltd. and D. CLARK, Lockheed Martin Space Systems 1430 hrs 1500 hrs 1530 hrs 1600 hrs AIAA-2014-0686 AIAA-2014-0687 AIAA-2014-0688 AIAA-2014-0689 Lunar Rover Analogue Mission Lunabotics Student Paper Award: Planetary Drill Evolution Lunar Polar Environmental Deployments The University of Alabama MOLE S. Schmidt, M. Viel, T. Atwell, Testing: Regolith Simulant P. Visscher, D. Woolley, Ontario Drive System Deltion Innovations Ltd., Sudbury, Conditioning and Gear, New Hamburg, Canada J. Headley, C. Leslie, D. Sandel, B. Canada J. Kleinhenz, NASA Glenn Research Grace, A. Faulkner, K. Ricks, University Center, Cleveland, OH of Alabama, Tuscaloosa, Tuscaloosa, AL Tuesday, 14 January 2014 185-STR-9 Impact Mechanics and Structural Survivability Chesapeake Conf Rm F Chaired by: M. ROYBAL, Raytheon Missile Systems and R. KOCH, Naval Undersea Warfare Center 1430 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs No Presentations AIAA-2014-0690 AIAA-2014-0691 AIAA-2014-0692 AIAA-2014-0693 The Vertical Drop Water Impact Baseline Analysis of LSDyna to Investigation of Composite Slosh Damping with Floating of Civil Aircraft Fuselage Model the Effectiveness of an Patch Performance Under Low- Electroactive Microbafﬂes Structure based on SPH and Explosive Containment Box for Velocity Impact Loading V. Santhanam, R. Baum, D. Kim, S. ALE methods Aircraft Protection G. Goodmiller, S. TerMaath, Gangadharan, Embry-Riddle Aeronautical Y. Ren, J. Xiang, Beihang University, A. Costain, J. Bayandor, Virginia University of Tennessee, Knoxville, University, Daytona Beach, FL Beijing, China Polytechnic Institute and State Knoxville, TN University, Blacksburg, VA Tuesday, 14 January 2014 186-STR-10 Structures Under Thermal Environment Chesapeake Conf Rm E Chaired by: B. WILLIS, Boeing Defense, Space & Security and O. ZHUPANSKA, The University of Iowa 1430 hrs 1530 hrs 1600 hrs 1630 hrs No Presentations AIAA-2014-0694 AIAA-2014-0695 AIAA-2014-0696 Peridynamics for Fully Coupled C0-type efﬁcient higher-order FEM Correlation of Sandwich Thermomechanical Analysis of plate theory for the thermo- Composite Antenna Structure Fiber Reinforced Laminates mechanical analysis of laminated Subject to Thermal Distortion S. Oterkus, E. Madenci, University of composite plates H. Soliman, Virginia Polytechnic Arizona, Tucson, Tucson, AZ J. Han, Seoul National University, Seoul, Institute and State University, South Korea; J. Kim, Kumoh National Blacksburg, VA; T. Stoumbos, Orbital Institute of Technology, Gyeongbuk, Sciences Corporation, Dulles, VA

104 South Korea; M. Cho, Seoul National University, Seoul, South Korea Tuesday, 14 January 2014 187-TP-3 Direct Simulation Monte Carlo Methods I National Harbor Conf Rm 11 Chaired by: K. STEPHANI, University of Michigan and J. KUHLMAN, West Virginia University 1430 hrs 1500 hrs 1530 hrs 1600 hrs AIAA-2014-0697 Oral Presentation (Invited) AIAA-2014-0698 AIAA-2014-0699 Efficient Direct Simulation Monte An Accurate Direct Numerical DSMC Calculations of Electron Effects of surface Carlo Modeling of Very Low Simulation of the Shock Wave Density Flow Fields near chemistry on high-altitude Knudsen Number Gas Flows Structure Reentering Space Vehicles with aerothermodynamics of space J. Burt, E. Josyula, Air Force E. Malkov, M. Ivanov, Russian SMILE++ Software System vehicles Research Laboratory, Wright- Academy of Sciences, Novosibirsk, Y. Bondar, A. Shevyrin, A. Kashkovsky, A. Shumakova, A. Shevyrin, Y. Patterson AFB, OH Russia M. Ivanov, Russian Academy of Bondar, A. Kashkovsky, M. Ivanov, Sciences, Novosibirsk, Russia Russian Academy of Sciences, Novosibirsk, Russia Tuesday, 14 January 2014 188-TP-4 Thermal Protection Systems II National Harbor Conf Rm 10 Chaired by: J. OCHTERBECK, Clemson University and E. SILK, NASA-Goddard Space Flight Center 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs AIAA-2014-0700 AIAA-2014-0701 AIAA-2014-0702 AIAA-2014-0703 AIAA-2014-0704 AIAA-2014-0705 Flexible Thermal Protection Measurements of Film Cooling Design, Integration, and Initial Unsteady Simulation of One Feasibility Improvement of Reduction of Aerodynamic System Physics-Based Performance in Supersonic Testing of an Integrated System Dimensional Heat Transfer Non-Ablative Lightweight TPS Heating with Opposing Jet Modeling for Temperature Environments for Thermal Conductivity in Porous Media with a for Mars Aero-flyby Sample through Extended Nozzle in Profile Predictions D. Maqbool, M. Collett, K. Dellimore, Measurement of Insulation Temperature Jump Condition Collection Mission High Enthalpy Flow G. Rossman, R. Braun, Georgia University of Maryland, College Materials at High Pressure P. Gangwar, M. Martin, Louisiana T. Suzuki, T. Aoki, T. Ogasawara, K. N. Morimoto, J. Yoon, S. Aso, Y. Institute of Technology, Atlanta, Park, College Park, MD; J. Ruf, R. Nutsugah, Southern University and State University, Baton Rouge, LA Fujita, Japan Aerospace Exploration Tani, Kyushu University, Fukuoka, GA; J. Dec, NASA Langley Research NASA Marshall Space Flight Center, A&M, Baton Rouge, LA; M. Triay, A. Agency (JAXA), Tokyo, Japan; Japan Center, Hampton, VA Huntsville, AL; C. Cadou, University Cooley, D. Sparacino, T. LaCour, J. J. Koyanagi, Tokyo University of of Maryland, College Park, College Castillo, Louisiana State University, Science, Tokyo, Japan Park, MD Baton Rouge, LA; et al. Tuesday, 14 January 2014 189-WE-6 Wind Farm and Turbine-Wake Interaction I Woodrow Wilson B Chaired by: S. SCHMITZ, Pennsylvania State University 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs AIAA-2014-0706 AIAA-2014-0707 AIAA-2014-0708 AIAA-2014-0709 AIAA-2014-0710 AIAA-2014-0711 Experimental quantification Evaluation of the effect of Analyzing Effects of Turbulence Optimal control of wind farm The Effect of Various Actuator- Modelling Extreme Wind of the entrainment of kinetic Realistic and Synthetic Inflow on Power Generation Using power extraction in large eddy Line Modeling Approaches on Events in a Wind Farm using energy and production of on the Power and Loading Wind Plant Monitoring Data simulations Turbine-Turbine Interactions Large Eddy Simulation turbulence in the wake of Pattern of Wind Turbine J. Zhang, B. Hodge, National J. Goit, J. Meyers, Catholic University and Wake-Turbulence Statistics R. Storey, S. Norris, J. Cater, 105 a wind turbine with Particle H. Gopalan, D. Chandar, C. Gundling, Renewable Energy Laboratory, of Leuven, Leuven, Belgium in Atmospheric Boundary- University of Auckland, Auckland, Image Velocimetry J. Sitaraman, University of Wyoming, Golden, CO; S. Chowdhury, Layer Flow New Zealand L. Lignarolo, D. Ragni, C. Simao Laramie, Laramie, WY; W. Henshaw, Syracuse University, Syracuse, NY; P. Jha, Pennsylvania State University, Ferreira, G. van Bussel, Delft J. Mirocha, Lawrence Livermore Y. Wan, National Renewable Energy University Park, PA; M. Churchfield, University of Technology, Delft, The National Laboratory, Livermore, Laboratory, Golden, CO P. Moriarty, National Renewable Netherlands CA; et al. Energy Laboratory, Golden, CO; S. Schmitz, Pennsylvania State University, University Park, PA Tuesday, 14 January 2014 190-WE-7 Wind Turbine Aeroelasticity and Structural Dynamics II Woodrow Wilson C Chaired by: M. LACKNER, University of Massachusetts and B. OWENS 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs AIAA-2014-0712 AIAA-2014-0713 AIAA-2014-0714 AIAA-2014-0715 AIAA-2014-0716 AIAA-2014-0717 Cyber-physical Energy Floquet Stability Analysis of Aerodynamic Sensitivity Analysis Wind Turbine Structural Model Aeroelastic Study of a Vertical Wind Turbine Fluid-Structure Harvesting through Flow- Wind Turbines Using Input- of Rotor Imbalance and Shear Using Non-Linear Modal Axis Wind Turbine with Interaction using an Actuator Induced Oscillations of a Output Models Web Disbond Detection Strategies Formulations Troposkien Shape Line Solver and a Finite Rectangular Plate C. Bottasso, Technical University for Offshore Structural Health L. Bernhammer, R. De Breuker, Delft A. Fereidooni, F. Nitzsche, E. Matida, Element Solver in a Tightly- K. Onoue, A. Song, B. Strom, K. Breuer, of Munich, Munich, Germany; S. Prognostics Management of Wind University of Technology, Delft, The Carleton University, Ottawa, Canada Coupled Implementation Brown University, Providence, RI Cacciola, Technical University of Turbine Blades Netherlands; M. Karpel, Technion-- J. Motta-Mena, P. Jha, R. Campbell, Milan, Milan, Italy N. Myrent, N. Bilal, D. Adams, Purdue Israel Institute of Technology, Haifa, S. Schmitz, J. Brasseur, Pennsylvania University, West Lafayette, IN; D. Israel State University, University Park, PA Griffith, Sandia National Laboratories, Albuquerque, NM Tuesday, 14 January 2014 191-NW-5 Tuesday Afternoon Networking Coffee Break Exhibit Hall 1530 - 1600 hrs Tuesday, 14 January 2014 192-NW-6 Reception in the Exhibit Hall Exhibit Hall 1730 - 1900 hrs Wednesday Wednesday, 15 January 2014 193-NW-7 Wednesday Morning Networking Breakfast Exhibit Hall 0700 - 0800 hrs Wednesday, 15 January 2014 194-SB-5 Wednesday Morning Speakers’ Briefing Session Rooms 0730 - 0800 hrs Wednesday, 15 January 2014 195-PLNRY-3 Wednesday Morning Keynote and Plenary Panel Potomac Ballroom A&B 0800 - 0930 hrs Keynote Tech Superiority in an Age of Austerity Frank Kendall Under Secretary of Defense for Acquisition, Technology and Logistics Department of Defense

Plenary Panel: Design for Affordability 106 Moderator: The Honorable Jacques S. Gansler, Professor and Roger C. Lipitz Chair, Glenn L. Martin Institute Fellow of Engineering Center for Public Policy & Private Enterprise, School of Public Policy, University of Maryland Panelists: Carl Avila John Bergeron John Fisher Director Advanced Weapons and Missile Systems Senior Director, Raytheon Six Sigma, Engineering, Technology & Mission Assurance Chief Engineer, Engineering, Manufacturing & Logistics Boeing Raytheon Company Northrop Grumman Electronic Systems

Wednesday, 15 January 2014 196-NW-8 Wednesday Morning Networking Coffee Break Exhibit Hall 0930 - 1000 hrs Wednesday, 15 January 2014 197-AA-5 Fan and Duct Acoustics National Harbor Conf Rm 3 Chaired by: W. EVERSMAN, Missouri University of Science and Technology 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2014-0718 AIAA-2014-0719 AIAA-2014-0720 AIAA-2014-0721 Experimental Simulation of A Mode Propagation Database The Numerical Analysis of Recent Improvements to the Ducted Fan Acoustics at Very Suitable for Code Validation Forward Fan Noise Shielding Acoustic Testing Laboratory Small Scale Utilizing the NASA Glenn Effect on the Over-the-Wing at the NASA Glenn Research A. Truong, D. Papamoschou, Advanced Noise Control Fan Nacelle Configuration Center University of California, Irvine, and Artificial Sources Y. Fukushima, T. Misaka, S. Obayashi, D. Sutliff, NASA Glenn Research Irvine, CA D. Sutliff, NASA Glenn Research Tohoku University, Sendai, Japan; Center, Cleveland, OH Center, Cleveland, OH D. Sasaki, Kanazawa Institute of Technology, Nonoichi, Japan; K. Nakahashi, Japan Aerospace Exploration Agency (JAXA), Chofu, Japan Wednesday, 15 January 2014 198-ABPSI-3 Group for Aeronautical Research and Technology in EURope (GARTEUR) II Chesapeake Conf Rm 9 Chaired by: A. DELOT, ONERA and T. BERENS, EADS Deutschland GmbH/Cassidian 1000 hrs 1030 hrs 1100 hrs 1130 hrs Oral Presentation (Invited) AIAA-2014-0722 AIAA-2014-0723 AIAA-2014-0724 An Overview of the Group Numerical and Experimental DES Computations for a Subsonic Flow Control using Vortex for Aeronautical Research Investigations on Highly UAV Configuration with a Highly Generators or Micro-Jets and Technology in EURope Integrated Subsonic Air Intakes Integrated S-Shaped Intake Duct Applied in an UCAV Intake (GARTEUR) T. Berens, Cassidian, Manching, A. Delot, ONERA, Meudon, France; T. M. Tormalm, Swedish Defense H. Consigny, O. Vasseur, ONERA, Germany; A. Delot, ONERA, Meudon, Berens, Cassidian, Manching, Germany; Research Agency (FOI), Stockholm, Palaiseau, France; A. Delot, ONERA, France; M. Tormalm, Swedish Defense M. Tormalm, Swedish Defense Research Sweden Meudon, France Research Agency (FOI), Stockholm, Agency (FOI), Stockholm, Sweden; M. Sweden; L. Ruiz-Calavera, D. Funes- Säterskog, Saab, Linköping, Sweden; N. Sebastian, Airbus, Getafe, Spain; M. Ceresola, Alenia Aermacchi, Turin, Italy Rein, German Aerospace Center (DLR), Göttingen, Germany; et al. Wednesday, 15 January 2014 199-ACD-8 Unmanned Aircraft Design Azalea 1 Chaired by: G. CROUSE, Sierra Nevada Corporation 1000 hrs 1030 hrs 1100 hrs AIAA-2014-0725 AIAA-2014-0726 AIAA-2014-0727 A Parametric Study of Modeling and Evaluation of a Performance and Testing of a Maximum Flight Efficiency for Spherical VTOL Aerial Vehicle Quad Rotor Biplane Micro Air Micro Aerial Vehicles with Ground Mobility Vehicle for Multi Role Missions

107 C. Kroninger, A. Harrington, M. W. Loh, J. Jacob, Oklahoma State V. Hrishikeshavan, C. Bogdanowicz, Munson, Army Research Laboratory, University, Stillwater, OK I. Chopra, University of Maryland, Aberdeen Proving Ground, MD College Park, College Park, MD Wednesday, 15 January 2014 200-AFM-7 Aerodynamic Predictive Methods National Harbor Conf Rm 13 Chaired by: J. GRAUER, NASA - Dynamic Systems & Control Branch 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2014-0728 AIAA-2014-0729 AIAA-2014-0730 AIAA-2014-0731 AIAA-2014-0732 Analytically-derived Unsteady and Post-Stall Rapid Aerodynamic Parameter Roll Damping Derivatives from Assessing the Impact of Aerodynamic Force and Aerodynamic Modeling for Flight Identification on a Large Generalized Lifting-Surface Aerodynamic Modelling on Moment Coefficients of Dynamics Simulation Transport Aircraft Theory and Wind Tunnel Manoeuvring Aircraft Resident Space Objects in R. Paul, North Carolina State University, C. Raab, German Aerospace Center Forced-Oscillation Tests A. Da Ronch, University of Free-Molecular Flow Raleigh, NC; J. Murua, University of (DLR), Braunschweig, Germany A. Pototzky, NASA Langley Research Southampton, Southampton, United K. Hart, S. Dutta, K. Simonis, B. Surrey, Guildford, United Kingdom; A. Center, Hampton, VA Kingdom; A. McCracken, K. Badcock, Steinfeldt, R. Braun, Georgia Institute Gopalarathnam, North Carolina State University of Liverpool, Liverpool, of Technology, Atlanta, GA University, Raleigh, NC United Kingdom Wednesday, 15 January 2014 201-AMT-5/PC-11 Combustion Diagnostics I Maryland Ballroom 1 Chaired by: P. DANEHY, NASA Langley Research Center and J. SUTTON, Ohio State University 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2014-0733 AIAA-2014-0734 AIAA-2014-0735 AIAA-2014-0736 Oral Presentation (Invited) High-Repetition-Rate OH-PLIF High Repetition Rate OH- Three-Dimensional High-speed radiographic spray Long-record-length burst-mode and PIV Measurements in Bluff PLIF of a Jet Flame in a Measurements of Turbulent imaging with a broadband planar imaging for combustion Body Stabilized Flames Vitiated Swirling Crossflow Jet Flames at kHz Rate tube source diagnostics A. Caswell, N. Jiang, S. Roy, and a Qualitative Analysis Based on Tomographic B. Halls, T. Morgan, T. Heindel, T. J. Michael, P. Venkateswaran, Iowa Spectral Energies, LLC, Dayton, Using Proper Orthogonal Chemiluminescence Meyer, Iowa State University, Ames, State University, Ames, IA; J. Miller, OH; B. Huelskamp, Innovative Decomposition X. Li, L. Ma, Virginia Polytechnic IA; A. Kastengren, Argonne National Air Force Research Laboratory, Scientific Solutions, Inc., Dayton, P. Panda, M. Roa, R. Lucht, Purdue Institute and State University, Laboratory, Argonne, IL Wright-Patterson AFB, OH; M. OH; J. Monfort, University of Dayton University, West Lafayette, IN Blacksburg, VA Slipchenko, Spectral Energies, Research Institute, Dayton, OH; A. LLC, Dayton, OH; J. Gord, Air Lynch, Air Force Research Laboratory, Force Research Laboratory, Wright- Wright-Patterson AFB, OH; et al. Patterson AFB, OH; S. Roy, Spectral Energies, LLC, Dayton, OH; et al. Wednesday, 15 January 2014 202-APA-20 Icing Effects on Vehicle Aerodynamics Maryland Ballroom 3 Chaired by: S. MORRIS, Engineering Systems, Inc. and H. HU, Iowa State University 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2014-0737 AIAA-2014-0738 AIAA-2014-0739 AIAA-2014-0740 AIAA-2014-0741 Prediction of ice accretion on Splashing Model for Impact of Thermal Analysis and Testing Numerical Simulation of An Experimental Investigation the nacelle of a turboprop Supercooled Large Droplets on of a Cone with Leading Edge Supercooled Large Droplets on Wind-Driven Rivulet/Film

108 aircraft a Thin Liquid Film Hot Air Anti-icing System Using the Moment of Fluid Flows over a NACA0012 Airfoil C. Gallego Cañizares, L. Ruiz- E. Norde, J. Hospers, E. van der W. Dong, J. Zhu, M. Zheng, Method by Using Digital Image Projection Calavera, Airbus, Getafe, Spain Weide, H. Hoeijmakers, University of Shanghai Jiao Tong University, Y. Lian, University of Louisville, Technique Twente, Enschede, The Netherlands Shanghai, China Louisville, KY K. Zhang, B. Johnson, A. Rothmayer, H. Hu, Iowa State University, Ames, IA Wednesday, 15 January 2014 203-APA-21 Low Speed Low Reynolds Number Aerodynamics II Chesapeake Conf Rm I Chaired by: J. MASTERS, Aerospace Testing Alliance (ATA) 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2014-0742 AIAA-2014-0743 AIAA-2014-0744 AIAA-2014-0745 AIAA-2014-0746 Experimental Analysis of Low Reynolds Number Propeller Slipstream Flow Field around Asymmetric A Flat Plate with Unsteady Power Requirements for Experimental Studies on Flat Interference with Wing Flapping Flat Plate Optimized Motion: Effect of Angle of Fixed-, Flapping-, and Rotary- Plates Aerodynamic Characteristics of using Micro Genetic Algorithm Attack on Vortex Shedding Wing Micro Air Vehicles R. Stevens, H. Babinsky, University Mars Airplane at Low Reynolds P. Palar, University of Tokyo, Tokyo, X. Xia, K. Mohseni, University of B. Pipenberg, M. Maughmer, of Cambridge, Cambridge, United Number Japan; L. Zuhal, Bandung Institute of Florida, Gainesville, Gainesville, FL Pennsylvania State University, Kingdom F. Makino, H. Nagai, Tohoku Technology, Bandung, Indonesia University Park, PA University, Sendai, Japan Wednesday, 15 January 2014 204-APA-22 Special Session: 2nd High Lift Prediction Workshop (HiLiftPW-2) I Maryland Ballroom A Chaired by: D. MAVRIPLIS, University of Wyoming and C. WOEBER, Pointwise, Inc. 1000 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2014-0747 AIAA-2014-0748 AIAA-2014-0749 AIAA-2014-0750 Overview and Summary of the Second AIAA High Lift Prediction NSU3D Results for the Second Finite Element Flow Simulations Results from the 2nd AIAA CFD Workshop High-Lift Prediction Workshop of the EUROLIFT DLR-F11 High High Lift Prediction Workshop C. Rumsey, NASA Langley Research Center, Hampton, VA; J. Slotnick, The D. Mavriplis, University of Wyoming, Lift Conﬁguration using Edge Boeing Company, Huntington Beach, CA Laramie, Laramie, WY; M. Long, K. Chitale, Rensselaer Polytechnic P. Eliasson, Swedish Defense Scientiﬁc Simulations, League City, Institute, Troy, NY; M. Rasquin, Research Agency (FOI), Stockholm, TX; T. Lake, University of Wyoming, Argonne National Laboratory, Lemont, Sweden Laramie, Laramie, WY IL; J. Martin, Massachusetts Institute of Technology, Cambridge, MA; K. Jansen, University of Colorado, Boulder, Boulder, CO Wednesday, 15 January 2014 205-APA-23 Special Session: CREATE-AV High Performance Computing Multiphysics Applications of Full-Up Air Vehicles II Maryland Ballroom 4 Chaired by: N. HARIHARAN, CREATE-AV; D. MCDANIEL, University of Alabama at Birmingham; B. HALLISSY, NAVAIR and T. SHAFER, NAVAIR 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2014-0751 AIAA-2014-0752 AIAA-2014-0753 AIAA-2014-0754 AIAA-2014-0755 Prediction of Unsteady Flow CFD Solver Comparison of Low Inlet/Engine Integration A-10 LAU-131 Jettison CFD CREATETM-AV DaVinci Strategic in UCAV Weapon’s Bay Using Mach Number Flow over the Examples Using Coupled Analysis Airlift Pilot Project CREATE-AV’s Kestrel ROBIN Fuselage Transient and Steady Engine C. Lillian, SURVICE Engineering, G. Roth, U.S. Air Force, Dayton, OH; B. Hallissy, CREATE AV Team, J. Abras, CREATE AV Team, Patuxent Performance Models with Kestrel Belcamp, MD J. Zhu, Flairsoft Federal, Dayton,

109 Patuxent River, MD; N. Hariharan, River, MD; N. Hariharan, HPCMP S. Morton, CREATE Kestrel Team, Eglin OH; R. Buchy, Nova Technology CREATE AV Team, Lorton, VA CREATE-AV, Lorton, VA AFB, FL Solutions, LLC, Dayton, OH Wednesday, 15 January 2014 206-APA-24 Special Session: 2nd Cranked Arrow Wing Aerodynamic Project International (CAWAPI) II Maryland Ballroom D Chaired by: A. ELMILIGUI, NASA Langley Research Center and G. GATLIN 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2014-0756 AIAA-2014-0757 AIAA-2014-0758 AIAA-2014-0759 USM3D Numerical Simulations Flow Analysis of the F-16XL Vortex Flows of the F-16XL What was Learned in For the F-16XL Aircraft Aircraft (CAWAPI-2) At Transonic Configuration - CAWAPI-II Predicting Slender Airframe Configuration Flow Conditions Free-Flight Simulations Aerodynamics with the F16-XL A. Elmiligui, K. Abdol-Hamid, NASA O. Boelens, National Aerospace S. Hitzel, Cassidian, Manching, Aircraft Langley Research Center, Hampton, VA; Laboratory (NLR), Amsterdam, The Germany A. Rizzi, Royal Institute of P. Cavallo, Combustion Research and Netherlands; J. Luckring, NASA Langley Technology (KTH), Stockholm, Flow Technology, Inc., Pipersville, PA Research Center, Hampton, VA Sweden Wednesday, 15 January 2014 207-AS-1 Optimization and Structural Health Monitoring Chesapeake Conf Rm D Chaired by: D. AMBUR, NASA Langley Research Center and V. GIURGIUTIU, University of South Carolina 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2014-0760 AIAA-2014-0761 AIAA-2014-0762 AIAA-2014-0763 AIAA-2014-0764 Integrated experimental and Multidisciplinary Performance Design and Optimisation of Topology Optimization & A visco-electric device for numerical investigation for Based Optimization of Composite Corrugated Skin for Experimental Validation of vibration energy harvesting on damage diagnosis in composite Morphing Aircraft a Span Morphing Wing 0-υ Honeycomb for Adaptive rotorcraft materials A. Suleman, University of Victoria, Y. Xia, R. Ajaj, M. Friswell, Swansea Morphing Wing R. Mahmood, E. Smith, G. Lesieutre, T. Peng, Arizona State University, Victoria, Canada; F. Lau, J. Vale, University, Swansea, United Kingdom A. Dale, J. Cooper, University of Pennsylvania State University, Tempe, AZ; A. Saxena, K. Goebel, F. Afonso, Technical University of Bristol, Bristol, United Kingdom; A. University Park, PA NASA Ames Research Center, Moffett Lisbon, Lisbon, Portugal Mosquera, ACEL, Ltd., Daresbury, Field, CA; Y. Xiang, Y. Liu, Arizona United Kingdom State University, Tempe, AZ Wednesday, 15 January 2014 208-FD-23 Active and Passive Flow Control III National Harbor Conf Rm 6 Chaired by: D. MILLER, Lockheed Martin Corporation and M. MCQUILLING, Saint Louis University 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2014-0765 AIAA-2014-0766 AIAA-2014-0767 AIAA-2014-0768 AIAA-2014-0769 Numerical investigation Effects of Burst Frequency and Experimental Study of Nano- Detached Eddy Simulations Vorticity and Turbulence of Active Flow Control on Momentum Coefficient of DBD second Pulse Plasma Actuator of a Synthetic Jet for a Properties of Microjet Arrays a pitching NACA 0015 Actuator on Control of Deep-stall for Low Reynolds Number High-angle-of-attack Airfoil for Active Flow Control airfoil using Detached-Eddy Flow around NACA0015 at Flow Control -Influence of the Jet Angle- E. Fernandez, F. Alvi, Florida State Simulation Rec=2.6x10^{5} S. Sekimoto, T. Sulaiman, University Y. Ishibashi, K. Miyaji, Yokohama University, Tallahassee, FL 110 L. Wang, L. Li, S. Fu, Tsinghua H. Aono, Japan Aerospace Exploration of Tokyo, Sagamihara, Japan; M. National University, Yokohama, University, Beijing, China Agency (JAXA), Sagamihara, Japan; Anyoji, T. Nonomura, K. Fujii, Japan Japan K. Okada, Ryoyu Systems Company, Aerospace Exploration Agency Ltd., Nagoya, Japan; T. Nonomura, (JAXA), Sagamihara, Japan S. Kawai, M. Sato, A. Yakeno, Japan Aerospace Exploration Agency (JAXA), Sagamihara, Japan; et al. Wednesday, 15 January 2014 209-FD-24 Higher-Order Methods II Maryland Ballroom 5 Chaired by: H. HUYNH, NASA Glenn Research Center and T. FISHER, Sandia National Laboratories 1000 hrs 1030 hrs 1100 hrs AIAA-2014-0770 AIAA-2014-0771 AIAA-2014-0772 High-Order Implicit-Explicit High-order temporal accuracy Higher-order Multi- Multi-block Time-stepping for 3D finite-element ALE flow dimensional Limiting Strategy Method for Hyperbolic PDEs simulations for Correction Procedure via T. Nielsen, NASA Marshall Space A. Hay, S. Etienne, D. Pelletier, Reconstruction Flight Center, Huntsville, AL; T. A. Garon, École Polytechnique de J. Park, T. Chang, C. Kim, Seoul Fisher, Sandia National Laboratories, Montréal, Montréal, Canada National University, Seoul, South Albuquerque, NM; S. Frankel, Purdue Korea University, West Lafayette, IN Wednesday, 15 January 2014 210-FD-25 Hypersonic Boundary Layer Receptivity Maryland Ballroom 6 Chaired by: V. THEOFILIS, Universidad Politécnica de Madrid and J. SCHMISSEUR, USAF AFOSR/NA 1000 hrs 1030 hrs 1100 hrs AIAA-2014-0773 AIAA-2014-0774 AIAA-2014-0775 Characterization of a Laser- Parametric Study of Boundary- Numerical simulation of Generated Perturbation in Layer Receptivity to Freestream hypersonic non-equilibrium High-Speed Flow for Receptivity Hot-Spot Perturbation over a boundary-layer receptivity Studies Blunt Compression Cone and stability A. Chou, S. Schneider, Purdue University, Y. Huang, X. Zhong, University of X. Wang, X. Zhong, University West Lafayette, IN; M. Kegerise, NASA California, Los Angeles, Los Angeles, CA of California, Los Angeles, Los Langley Research Center, Hampton, VA Angeles, CA Wednesday, 15 January 2014 211-FD-26/MVC-5 Overset Grid Methods National Harbor Conf Rm 5 Chaired by: M. GALBRAITH; D. THOMPSON, Mississippi State University and P. BUNING, NASA Langley Research Center 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2014-0776 AIAA-2014-0777 AIAA-2014-0778 AIAA-2014-0779 A 3-D Discontinuous Galerkin Analysis of a Chimera Development of Arbitrary Automatic Structured and Chimera Overset Method Scheme with a Finite Element Unstructured Chimera Grid Unstructured Grid Cell M. Galbraith, P. Orkwis, University of Discretization S. Zhang, ESI Group, Huntsville, AL; Remediation for Overset Cincinnati, Cincinnati, OH; J. Benek, D. French, M. Galbraith, University of X. Zhao, Alabama A&M University, Meshes Air Force Research Laboratory, Cincinnati, Cincinnati, OH; J. Benek, Huntsville, AL; H. Guan, AVIC The J. Steinbrenner, Pointwise, Inc., Fort Wright-Patterson AFB, OH Air Force Research Laboratory, First Aircraft Institute, Xi’an, China Worth, TX Wright-Patterson AFB, OH 111 Wednesday, 15 January 2014 212-FD-27/TP-5 Rarefied Gas Dynamics in Micro- and Nano-Systems National Harbor Conf Rm 4 Chaired by: M. MARTIN, Louisiana State University; D. HITT, University of Vermont and M. KHAN, Tuskegee University 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs Oral Presentation (Invited) Oral Presentation (Invited) Oral Presentation (Invited) Oral Presentation (Invited) Oral Presentation (Invited) Research in Rarefied Gas Development of New Development of Kundsen Challenges in Rarefied Flows Gas Flow and Heat Transfer Dynamics at the Micro-Scale at Computational Methods for Pumps for Micro-Scale at the Micro-Scale in Arrays of Nano-Scale Purdue University Micro-Scale Rarefied Flow Applications M. Gallis, Sandia National Structures A. Alexeenko, Purdue University, D. Kessler, Naval Research M. Martin, Louisiana State Laboratories, Albuquerque, NM M. Martin, Louisiana State West Lafayette, IN Laboratory, Washington, DC University, Baton Rouge, LA University, Baton Rouge, LA Wednesday, 15 January 2014 213-GNC-12 Intelligent Control in Aerospace Applications National Harbor Conf Rm 7 Chaired by: A. LAMPTON, Systems Technology, Inc. 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2014-0780 AIAA-2014-0781 AIAA-2014-0782 AIAA-2014-0783 Derivation and Comparison Output Feedback M-MRAC Frequency Limited Adaptive Frequency Limited Adaptive between Numerical Based and Backstepping With Aerospace Control Using a Quadratic Control Using a Quadratic Novel Analytical Compromise Applications Stability Framework: Stability Stability Framework: Solutions to the Multi-Objective V. Stepanyan, University of and Convergence Guaranteed Stability Limits Control Allocation Problem California, Santa Cruz, Moffett Field, J. Muse, Air Force Research J. Muse, Air Force Research F. Salama, A. Savvaris, Cranfield CA; K. Krishnakumar, NASA Ames Laboratory, Wright-Patterson AFB, OH Laboratory, Wright-Patterson AFB, OH University, Cranfield, United Kingdom Research Center, Moffett Field, CA Wednesday, 15 January 2014 214-GNC-13 Validation of Onboard Systems Technologies for LOC Prevention and Recovery, Session (Invited) II National Harbor Conf Rm 8 Chaired by: K. FEIGH, Georgia Institute of Technology and E. XARGAY 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2014-0784 AIAA-2014-0785 AIAA-2014-0786 AIAA-2014-0787 AIAA-2014-0788 Loss-of-Control Prediction An Evaluation of Flight Safety Recoverable sets of initial Software Implementation and Frequency-Limited Adaptive and Prevention for NASA’s Assessment and Management conditions and their use for Verification of Sliding-Mode Control of a Generic Transport Transport Class Model to avoid Loss of Control during aircraft flight planning after a Control and Fault Detection Model in the Presence of J. Chongvisal, R. Malawy, D. Talleur, Takeoff loss of control event Methods System Uncertainty and Losses A. Kirlik, N. Hovakimyan, University S. Balachandran, E. Atkins, K. McDonough, I. Kolmanovsky, E. A. Esna Ashari, E. Feron, Georgia in Control Effectiveness of Illinois, Urbana-Champaign, University of Michigan, Ann Arbor, Atkins, University of Michigan, Ann Institute of Technology, Atlanta, GA G. De La Torre, T. Yucelen, E. Urbana, IL; C. Belcastro, NASA Ann Arbor, MI Arbor, Ann Arbor, MI Johnson, W. Haddad, T. Rajpurohit, Langley Research Center, Hampton, Georgia Institute of Technology, VA Atlanta, GA Wednesday, 15 January 2014 215-GT-5 The Direction and Integration of Experimental Ground Test Capabilities and Computational Methods, Part II (Invited) Maryland Ballroom B Chaired by: S. DUNN, Jacobs Technology, T. TREPAL, Institute for Defense Analysis 1000 hrs 1030 hrs Oral Presentation (Invited) Panelists: Findings from the Part I/CASE Mr. Alex Krynytzky, The Boeing Company, Seattle WA Dr. Rubén del Rosario, NASA Glenn Research Center, Cleveland, OH Session on the Direction and Mr. Shigeya Watanabe, Japan Aerospace Exploration Agency Dr. Edward Marquart, Raytheon Missile Systems, Tucson, AZ Integration of GT and CFD Mr. Tom Wayman, Gulfstream Aerospace Corporation, Savannah, GA Dr. Greg Power, Aerospace Testing Alliance, Arnold Engineering S. Dunn, Jacobs, Hampton, VA and Development Center, TN 112 Wednesday, 15 January 2014 216-GTE-5 Turbomachinery II Woodrow Wilson D Chaired by: G. WELCH, NASA Glenn Research Center and S. SUBRAMANIAN, QuEST Global, Inc. 1000 hrs 1030 hrs 1100 hrs AIAA-2014-0789 AIAA-2014-0790 AIAA-2014-0791 Investigation of Non- Full-Annulus Simulation of Non- Thermocouple Recovery synchronous Vibration Synchronous Blade Vibration of Factor for Temperature Mechanism for a High Speed an Axial Compressor Measurements in Axial Compressor Using D. Espinal, G. Zha, University of Miami, Turbomachinery Test Facilities Delayed DES Coral Gables, FL; H. Im, Honeywell M. Fernelius, S. Gorrell, Brigham H. Im, G. Zha, University of Miami, International, Inc., Rancho Palos Young University, Provo, UT Coral Gables, FL Verdes, CA Wednesday, 15 January 2014 217-IS-1 Adaptive and Predictive Systems National Harbor Conf Rm 15 Chaired by: R. SAVELY, NASA Johnson Space Center 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2014-0792 AIAA-2014-0793 AIAA-2014-0794 AIAA-2014-0795 A Concept for Adaptation of Satisfiability Checking of LTL Inference of Aerodynamic An Adaptive Expert System Perceptual Capabilities for UAV Specifications for Verifiable Loads Under Uncertainty Using for the Autonomous Detection Platforms using Case-Based UAV Mission Planning Strain Measurements and of Aviation Mishap Leading Reasoning B. Kim, L. Humphrey, Air Force Bayesian Networks Indicators C. Hellert, P. Stütz, University of Research Laboratory, Wright- D. Rancourt, S. Ghosh, N. Weston, D. Haas, Naval Surface Warfare the German Federal Armed Forces, Patterson AFB, OH D. Mavris, Georgia Institute of Center, West Bethesda, MD; J. Neubiberg, Germany Technology, Atlanta, GA Walker, Quadelta, Inc., Arlington, VA; M. Morales, Computer Sciences Corporation, Bethesda, MD Wednesday, 15 January 2014 218-MAT-5 Integrated Computational Materials Engineering II Chesapeake Conf Rm A Chaired by: M. SANGID, Purdue University; J. MATLIK, Rolls-Royce Corporation and S. ARNOLD 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2014-0796 AIAA-2014-0797 AIAA-2014-0798 AIAA-2014-0799 AIAA-2014-0800 Multi-Scale Crystal Plasticity Examples of QuesTek Multi-scale Intrinsic Flaws in Effect of soft segment fraction Modeling the Coupled FEM Approach to Modeling Innovations’ Application Composite Materials on rate dependent damping of Transport-Deformation Nickel-Based Superalloys ICME to Materials Design, J. Goodsell, R. Pipes, Purdue polyurethane and polyurethane- Response of Titanium S. Ghosh, Johns Hopkins University, Development, and Rapid University, West Lafayette, IN clay nanocomposites Alloys Subjected to Thermo- Baltimore, MD Qualification T. Sain, E. Arruda, B. Yeom, A. Waas, Mechanical Environment J. Sebastian, G. Olson, QuesTek University of Michigan, Ann Arbor, Ann C. Oskay, H. Yan, Vanderbilt Innovations, LLC, Evanston, IL Arbor, MI University, Nashville, TN Wednesday, 15 January 2014 219-MDO-5 Optimization Methods and Algorithms II Chesapeake Conf Rm 4 Chaired by: J. CHRISSIS, USAF and V. TOROPOV, University of Leeds 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2014-0801 AIAA-2014-0802 AIAA-2014-0803 AIAA-2014-0804 AIAA-2014-0805 Using Estimation Techniques in A Multifidelity Approach to A Multi-Objective Post-Optimality Extensibility of a Linear Rapid Robust Design Optimization Multidisciplinary Design Aircraft Conceptual Design Data Handling Approach to Robust Design Methodology Using a Trended Kriging B. Steinfeldt, R. Braun, Georgia Under Uncertainty Robust Optimization B. Steinfeldt, R. Braun, Georgia Surrogate Model Institute of Technology, Atlanta, GA L. Ng, K. Willcox, Massachusetts K. Ryan, M. Lewis, K. Yu, University Institute of Technology, Atlanta, GA S. Choi, H. Kwon, Korea Advanced Institute of Technology, Cambridge, MA of Maryland, College Park, College Institute of Science and Technology, Park, MD Daejeon, South Korea

113 Wednesday, 15 January 2014 220-MST-3 Air Traffic Management/Human Factors National Harbor Conf Rm 12 Chaired by: F. CARDULLO, State University of NY 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2014-0806 AIAA-2014-0807 AIAA-2014-0808 AIAA-2014-0809 AIAA-2014-0810 Exploration of the Theoretical Aircraft Trajectory Design Based Evaluation of Haptic Shared An Experimental Comparison Multimodal Pilot Behavior in Physical Capacity of the John on Reducing the Combined Control and a Highway-in-the- of Haptic and Automated Pilot Multi-Axis Tracking Tasks with F. Kennedy International Effects of Carbon-Di-Oxide, Sky Display for Personal Aerial Support Systems Time-Varying Motion Cueing Airport Runway System Oxides of Nitrogen and Contrails Vehicles M. Olivari, F. Nieuwenhuizen, H. Gains K. Neitzke, NASA Langley Research B. Sridhar, N. Chen, NASA Ames F. Nieuwenhuizen, H. Bülthoff, Bülthoff, Max Planck Institute for P. Zaal, San Jose State University Center, Hampton, VA; N. Guerreiro, Research Center, Moffett Field, CA; H. Max Planck Institute for Biological Biological Cybernetics, Tübingen, Research Foundation, San Jose, Analytical Mechanics Associates, Inc., Ng, University of California, Santa Cruz, Cybernetics, Tübingen, Germany Germany; L. Pollini, University of CA; D. Pool, Delft University of Hampton, VA Moffett Field, CA Pisa, Pisa, Italy Technology, Delft, The Netherlands Wednesday, 15 January 2014 221-NDA-5 Validation & Uncertainty Quantification Applications Chesapeake Conf Rm 5 Chaired by: B. BICHON, Southwest Research Institue and G. MODGIL, Rolls-Royce Corporation 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2014-0811 AIAA-2014-0812 AIAA-2014-0813 AIAA-2014-0814 Handling Bias and Uncertainty A Pre-Validation Study on Uncertainty Quantification Uncertainty analysis of in Model Verification and Supersonic Wind Tunnel of Hypersonic Reentry Flows corrugated skin with random Validation associated with Data Collected from Legacy using Sparse Sampling and elastic parameters and surface Heated Pipes Pressurized to Aerothermal Experiments Stochastic Expansions topology Failure M. Balch, Arctan, Inc., Alexandria, T. West, S. Hosder, Missouri A. Kundu, Swansea University, V. Romero, Sandia National VA; B. Smarslok, Air Force Research University of Science and Technology, Swansea, United Kingdom; F. Laboratories, Albuquerque, NM Laboratory, Wright-Patterson AFB, OH Rolla, MO DiazDelaO, University of Liverpool, Liverpool, United Kingdom; M. Friswell, S. Adhikari, Swansea University, Swansea, United Kingdom Wednesday, 15 January 2014 222-PANEL-5 Additive Manufacturing - A Transformative Technology Panel Potomac Ballroom C 1000 - 1200 hrs Moderator: Ed Morris, Director; Vice President, America Makes - National Additive Manufacturing Innovation Institute; National Center for Defense Manufacturing and Machining (NCDMM) Panelists: William Flite Dan Johns Eric MacDonald Paul Susalla Project Engineering Senior Manager Chief Technologist, Additive Manufacturing Associate Director, W. M. Keck Center of 3D Innovation Section Supervisor - Rapid Manufacturing, Global Powertrain Lockheed Martin Aeronautics GKN Aerospace The University of Texas at El Paso Manufacturing Engineering Ford Motor Company

Wednesday, 15 January 2014 223-PC-12 Advanced Combustion Concepts and New Technologies National Harbor Conf Rm 2 Chaired by: M. ANAND, Rolls-Royce Corporation and B. WINDOM, Princeton University 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2014-0815 AIAA-2014-0816 AIAA-2014-0817 AIAA-2014-0818 Transient Injection of Gas vs. Condensed Phase Characterization of Patterened A New Cool Flame: Supercritical Fuel Reactions in Nano-Thermites Galvanic Porous Silicon for Establishment and Studies of S. Leonov, I. Adamovich, W. R. Jacob, G. Jian, P. Guerieri, M. On-Chip Combustion Dynamics and Kinetics Lempert, Ohio State university, Zachariah, University of Maryland, N. Piekiel, W. Churaman, C. Morris, D. S. Won, B. Jiang, Y. Ju, Princeton Columbus, OH College Park, College Park, MD Lunking, Army Research Laboratory, University, Princeton, NJ Adelphi, MD Wednesday, 15 January 2014 224-PC-13 Kinetic Model Reduction Chesapeake Conf Rm H 114 Chaired by: J. BELLAN, Jet Propulsion Laboratory 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2014-0819 AIAA-2014-0820 AIAA-2014-0821 AIAA-2014-0822 Dimensionality Reduction Model Reduction Opportunities Correlated Dynamic Adaptive Comparison of ODE Solver for Using a Dominant Dynamic in Detailed Simulations of Chemistry and Multi-timescale Chemical Kinetics and Reactive Variable, Self Similarity and Combustion Dynamics Modeling of Ignition and CFD Applications Data Tabulation: Application to R. Munipalli, HyPerComp, Inc., Combustion of a n-Heptane/ C. Stone, Computational Science Hydrocarbon Oxidation Westlake Village, CA; X. Zhu, Brown Air Mixture and Engineering, LLC, Chicago, IL; P. Kourdis, J. Bellan, California University, Providence, RI; S. Menon, W. Sun, Princeton University, F. Bisetti, King Abdullah University Institute of Technology, Pasadena, Georgia Institute of Technology, Princeton, NJ; H. El-Asrag, ANSYS, of Science and Technology, Thuwal, CA; K. Harstad, Jet Propulsion Atlanta, GA; J. Hesthaven, Brown Inc., Lebanon, NH; Y. Ju, Princeton Saudi Arabia Laboratory, California Institute of University, Providence, RI University, Princeton, NJ Technology, Pasadena, CA Wednesday, 15 January 2014 225-PC-14 Turbulent Combustion Modeling I Chesapeake Conf Rm G Chaired by: S. MENON, Georgia Institute of Technology 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2014-0823 AIAA-2014-0824 AIAA-2014-0825 AIAA-2014-0826 AIAA-2014-0827 Models for the LES equations LES of Premixed Flame Flashback Large Eddy Simulation of Towards Predictive Reacting Large Eddy Simulation of to describe multi-species in a Turbulent Channel Turbulent Reacting Jet in Cross Flow LES Non-premixed Turbulent mixing occurring at C. Lietz, M. Hassanaly, V. Raman, Flow with Adaptive Mesh P. Cocks, V. Sankaran, M. Soteriou, Combustion Using Nanosecond supercritical pressure University of Texas, Austin, Austin, Refinement United Technologies Corporation, Pulsed Actuators G. Borghesi, J. Bellan, California TX; H. Kolla, J. Chen, Sandia National B. Muralidharan, S. Menon, Georgia East Hartford, CT C. Wang, Yuan Ze University, Chung, Institute of Technology, Pasadena, CA Laboratories, Livermore, CA; A. Gruber, Institute of Technology, Atlanta, GA Taiwan SINTEF Energy Research, Trondheim, Norway Wednesday, 15 January 2014 226-PDL-8 Magnetohydrodynamics/Microwave Plasmas Azalea 3 Chaired by: N. BISEK, Air Force Reseach Laboratory 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2014-0828 AIAA-2014-0829 AIAA-2014-0830 AIAA-2014-0831 Shock Wave Propagation A Three-Dimensional Ignition of electric gas Characteristics of localized through Region of Electrical Numerical Study of MHD discharge in the deeply microwave discharges on surface and Magnetic Fields Action interaction between Supernova subcritical field of quasi- of aerodynamic models A. Erofeev, T. Lapushkina, S. Remnants and Interstellar optical microwave beam with P. Lavrov, A. Ravaev, I. Esakov, Poniaev, Russian Academy of Wind an electromagnetic vibrator Russian Academy of Sciences, Sciences, Saint Petersburg, Russia S. Surzhikov, M. Ermishkin, Russian mounted over a metal screen Moscow, Russia Academy of Sciences, Moscow, Russia A. Ravaev, L. Grachev, I. Esakov, A. Vasilyev, Russian Academy of Sciences, Moscow, Russia Wednesday, 15 January 2014 227-SCS-2 Solar Sails and Tensioned Membranes Chesapeake Conf Rm 6 Chaired by: V. LAPPAS, University of Surrey and M. MCEACHEN, ATK Space Systems 1000 hrs 1030 hrs 1100 hrs AIAA-2014-0832 AIAA-2014-0833 AIAA-2014-0834 Nonflatness of Solar Sail Optical Control of Solar Sails Systematic Surface Deviation Membrane Predicted by using Distributed Reflectivity and Shape Control of a Large Nonlinear Finite Element A. Borggräfe, J. Heiligers, University Mesh Reflector Analyses of Strathclyde, Glasgow, United L. Xiao, W. Minger, Tongji University, Y. Satou, Tokyo Institute of Technology, Kingdom; M. Ceriotti, University of Shanghai, China; X. Ma, H. Fang, 115 Yokohama, Japan; N. Okuizumi, Glasgow, Glasgow, United Kingdom; Shanghai YS Information Technology Japan Aerospace Exploration Agency C. McInnes, University of Strathclyde, Company, Ltd., Shanghai, China (JAXA), Sagamihara, Japan; G. Ono, Glasgow, United Kingdom University of Tokyo, Tokyo, Japan; H. Furuya, H. Sakamoto, Tokyo Institute of Technology, Yokohama, Japan; Y. Shirasawa, Japan Aerospace Exploration Agency (JAXA), Sagamihara, Japan; et al. Wednesday, 15 January 2014 228-SD-9 Adaptive Aeroelastic Wing Shaping Control I Chesapeake Conf Rm C Chaired by: H. KIM, Boeing Defense, Space & Security and J. SLATER, Wright State University 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2014-0835 AIAA-2014-0836 AIAA-2014-0837 AIAA-2014-0838 AIAA-2014-0839 Control System Design for a Static Aeroelastic Analysis with Static Aeroelastic and Static Aeroelastic Scaling Flutter Analysis of Mission- Variable Camber Continuous an Inviscid Cartesian Method Longitudinal Trim Model of and Analysis of a Sub-Scale Adaptive Wing with Variable Trailing Edge Flap System on D. Rodriguez, Science and Flexible Wing Aircraft Using Flexible Wing Wind Tunnel Camber Continuous Trailing an Elastic Wing Technology Corporation, Moffett Finite-Element Vortex-Lattice Model Edge Flap C. Morris, J. Sheahan, J. Dykman, Field, CA; M. Aftosmis, NASA Ames Coupled Solution E. Ting, S. Lebofsky, Stinger N. Nguyen, NASA Ames Research D. Clingman, J. Urnes, The Boeing Research Center, Moffett Field, CA; E. Ting, Stinger Ghaffarian Ghaffarian Technologies, Inc., Center, Moffett Field, CA; E. Ting, Company, St. Louis, MO M. Nemec, Science and Technology Technologies, Inc., Moffett Field, CA; Moffett Field, CA; N. Nguyen, NASA Stinger Ghaffarian Technologies, Inc., Corporation, Moffett Field, CA; S. N. Nguyen, NASA Ames Research Ames Research Center, Moffett Field, Moffett Field, CA; D. Nguyen, University Smith, Zee Aero, Mountain View, CA Center, Moffett Field, CA; K. Trinh, CA; K. Trinh, Stinger Ghaffarian of California, Berkeley, Berkeley, CA; K. Stinger Ghaffarian Technologies, Inc., Technologies, Inc., Moffett Field, CA Trinh, Stinger Ghaffarian Technologies, Moffett Field, CA Inc., Moffett Field, CA Wednesday, 15 January 2014 229-SD-10 Very Flexible Aircraft Chesapeake Conf Rm B Chaired by: R. MALLA, University of Connecticut and R. SCOTT, NASA-Langley Research Center 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2014-0840 AIAA-2014-0841 AIAA-2014-0842 AIAA-2014-0843 Nonlinear Aeroelastic Behavior Computational Nonlinear Nonlinear Model Reduction for Predictive Control for of High Aspect Ratio Wing Aeroelasticity of Very Flexible Aeroelastic Control of Flexible Alleviation of Gust Loads on Excited by Time Dependent Aircraft with Deformable Aircraft Described by Large Very Flexible Aircraft Thrust Airfoils Finite-Element Models R. Simpson, R. Palacios, H. Hesse, P. Mardanpour, D. Hodges, R. W. Su, University of Alabama, Y. Wang, W. Andrew, R. Palacios, Imperial College London, London, Rezvani, Georgia Institute of Tuscaloosa, Tuscaloosa, AL Imperial College London, London, United Kingdom; P. Goulart, Swiss Technology, Atlanta, GA United Kingdom Federal Institute of Technology, Zürich, Switzerland Wednesday, 15 January 2014 231-STR-11 Shell Bucking-Charles Rankin Special Session I Chesapeake Conf Rm E Chaired by: M. HILBURGER, NASA-Langley Research Center and R. YOUNG, NASA-Langley Research Center 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2014-0844 AIAA-2014-0845 AIAA-2014-0846 AIAA-2014-0847 AIAA-2014-0848 Minimum Weight Design of an The Use of the STAGS Finite High-Fidelity Buckling Analysis Post-buckling Response of STAGS Developments for Axially Compressed Isotropic Element Code in Stitched of Composite Cylinders using Scarf Repaired Laminates Residual Strength Analysis Prismatic Panel Consisting of a Structures Development the STAGS Finite Element Code Using a Refined Zigzag Methods for Metallic Fuselage Series of Cylindrical Segments D. Jegley, A. Lovejoy, NASA Langley M. Hilburger, NASA Langley Research Element Structures and Verification by STAGS Research Center, Hampton, VA Center, Hampton, VA A. Borut, E. Madenci, University R. Young, C. Rose, NASA Langley D. Bushnell, Self, Palo Alto, CA; M. of Arizona, Tucson, Tucson, AZ; A. Research Center, Hampton, VA

116 Jacoby, Lockheed Martin Corporation, Tessler, NASA Langley Research Palo Alto, CA Center, Hampton, VA Wednesday, 15 January 2014 232-STR-12 Advances in Design and Analysis of Structures Chesapeake Conf Rm F Chaired by: D. PHILLIPS, NASA-Marshall Space Flight Center and M. WOLFF, Gulfstream Aerospace Corporation 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2014-0849 AIAA-2014-0850 AIAA-2014-0851 AIAA-2014-0852 A Computational Model for the Analysis of the Effect of a Forming Process Analysis of Single Edge Notch Tension Flow of Resin in Self-Healing Wrinkle on the Elastic Wave Vibration Damping Laminated Test on Cross-Ply Laminated Composites Propagation in Membrane Steel Using Finite Element Composites for Intralaminar J. Hall, T. Rendall, I. Qamar, R. Structures Analysis Fracture Properties Trask, University of Bristol, Bristol, Y. Akaike, T. Yokozeki, University C. Sun, W. Zhou, United Technologies S. Boyd, W. Ji, A. Joseph, A. Waas, United Kingdom of Tokyo, Tokyo, Japan; A. Kanda, Corporation, Syracuse, NY; P. Pankaj, University of Michigan, Ann Arbor, Japan Aerospace Exploration Agency Larsen & Toubro, Ltd., Mumbai, Ann Arbor, MI (JAXA), Tokyo, Japan India; A. Sardar, J. Covington, M. Lombardo, United Technologies Corporation, Syracuse, NY Wednesday, 15 January 2014 233-TES-1 Cutting Edge Energy Systems and Fuels Azalea 2 Chaired by: B. SLOAN, Iowa State University 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2014-0853 AIAA-2014-0854 AIAA-2014-0855 AIAA-2014-0856 AIAA-2014-0857 Butyl Nonanoate as a Future High Velocity Oxy Fuel Development of passive Reducing the Space and Power Design and Production Biofuel for Clean Gas Turbine Thermal Spray Gun Design wireless temperature sensors Consumption for Aerospace of Composite Structures: Engines D. Mohamed, L. Cabrera, N. Love, using metamaterials Water Treatment by Improving Thermoplastic Wind Turbine A. Khalil Hasan, A. Gupta, University A. Choudhuri, University of Texas, El H. Karim, A. Choudhuri, University of Aeration Process Using Blades of Maryland, College Park, College Paso, El Paso, TX Texas, El Paso, El Paso, TX Innovative mixing Power R. Amano, L. Forsythe, University of Park, MD Reclamation Device Wisconsin, Milwaukee, Milwaukee, R. Amano, University of Wisconsin, WI Milwaukee, Milwaukee, WI; A. Alkhalidi, Hashemite University, Amman, Jordan; H. Albabaa, University of Wisconsin, Milwaukee, Milwaukee, WI Wednesday, 15 January 2014 234-TP-6 Heat Transfer National Harbor Conf Rm 11 Chaired by: E. SHORT, Raytheon Company 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2014-0858 AIAA-2014-0859 AIAA-2014-0860 AIAA-2014-0861 AIAA-2014-0862 Fractal Loop Heat Pipe Neutron Imaging of an Evaluation of Multi-Louvered The Study of Air-Cooled Assessment of Combined Performance Comparisons Unbalanced Flat-Plate Fin Based Heat Exchangers Condenser (ACC) Under Wind Natural Convection- of a Soda Lime Glass and Oscillating Heat Pipe for use in Automobile Exhaust Velocity and Environmental Radiation in a Participating 117 Compressed Carbon Foam J. Monroe, S. Thompson, Z. Energy Harvesting Systems Temperature Conditions Square Cavity Including Wick Aspin, Mississippi State University, J. Athavale, J. Pandit, S. Ekkad, M. Darbandi, A. Behrouzifar, Compressibility Effects D. Myre, KDM Systems, Inc., Mississippi State, MS; D. Jacobson, S. Huxtable, Virginia Polytechnic H. Salemkar, Sharif University M. Darbandi, B. Abrar, Sharif Chantilly, VA; E. Silk, NASA Goddard D. Hussey, National Institute Institute and State University, of Technology, Tehran, Iran; G. University of Technology, Tehran, Space Flight Center, Greenbelt, MD of Standards and Technology, Blacksburg, VA Schneider, University of Waterloo, Iran; G. Schneider, University of Gaithersburg, MD Waterloo, Canada Waterloo, Waterloo, Canada Wednesday, 15 January 2014 235-TP-7 Non-Equilibrium Flows I National Harbor Conf Rm 10 Chaired by: R. GOSSE, AFRL - Air Force Research Laboratory and A. SURESH, GE 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2014-0863 AIAA-2014-0864 AIAA-2014-0865 AIAA-2014-0866 Passive control of hypersonic Influence of State-to-State Computational Modeling Consistent Implementation of non-equilibrium boundary Transport Coefficients on of the Flow Environment in State-to-State Collision Models layers using regular porous Surface Heat Transfer in Inductively Coupled Plasma Jet for Direct Simulation Monte coating Hypersonic Flows Facilities Carlo X. Wang, X. Zhong, University E. Josyula, Air Force Research P. Norman, T. Schwartzentruber, G. C. Zhang, T. Schwartzentruber, of California, Los Angeles, Los Laboratory, Wright-Patterson AFB, Candler, University of Minnesota, University of Minnesota, Angeles, CA OH; E. Kustova, Saint Petersburg Minneapolis, Minneapolis, MN Minneapolis, Minneapolis, MN State University, Saint Petersburg, Russia; P. Vedula, University of Oklahoma, Norman, Norman, OK; J. Burt, Universal Technology Corporation, Beachwood, OH Wednesday, 15 January 2014 236-WE-8 Atmospheric Physics and Inflow Woodrow Wilson C Chaired by: S. ANANTHAN, US DOE and S. SCHRECK, National Renewable Energy Laboratory, National Wind Technology Center 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2014-0867 AIAA-2014-0868 AIAA-2014-0869 AIAA-2014-0870 Blade Boundary Layer Transition in Atmospheric Towards a Blade-Resolved On the Use of Site Data to Response to Atmospheric Turbulence Structure from Hybrid URANS-LES of the NREL Define Extreme Turbulence Boundary Layer Turbulence Neutral to Convective Stability 5-MW Wind Turbine Rotor within Conditions for Wind Turbine on a NREL 5MW Wind Turbine States Large Eddy Simulation of the Design Blade with Hybrid URANS-LES B. Jayaraman, J. Brasseur, Atmospheric Boundary Layer J. Moon, W. Sahasakkul, M. Soni, L. G. Vijayakumar, A. Lavely, B. Pennsylvania State University, A. Lavely, G. Vijayakumar, B. Craven, Manuel, University of Texas, Austin, Jayaraman, B. Craven, J. Brasseur, University Park, PA B. Jayaraman, Pennsylvania State Austin, TX Pennsylvania State University, University, University Park, PA; E. University Park, PA Paterson, Virginia Polytechnic Institute and State University, Blacksburg, VA; T. Nandi, Pennsylvania State University, University Park, PA; et al. Wednesday, 15 January 2014 237-WE-9 Wind Turbine Loads, Dynamics, and Control I Woodrow Wilson B Chaired by: M. BALAS, University of Wyoming 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2014-0871 AIAA-2014-0872 AIAA-2014-0873 AIAA-2014-0874 AIAA-2014-0875 Synthetic Jet based Active An Active Fault-Tolerant Effects of gain-scheduling Sizing and Control of Trailing Wind Turbine and Wind Farm Flow Control of Dynamic Stall Control Approach to Wind methods in a classical wind Edge Flaps on a Smart Rotor for Control Testing in a Boundary

118 Phenomenon on Wind Turbines Turbine Torque Load Control turbine controller on wind Maximum Power Generation in Layer Wind Tunnel Under Yaw Misalignment against Actuator Faults turbine aero-servo-elastic Low Fatigue Wind Regimes C. Bottasso, Technical University S. Tran, Rensselaer Polytechnic Institute, H. Badihi, Y. Zhang, H. Hong, modes and loads J. Smit, L. Bernhammer, Delft University of Munich, Munich, Germany; F. Troy, NY; D. Corson, Altair Engineering, Concordia University, Montréal, C. Tibaldi, L. Henriksen, M. Hansen, of Technology, Delft, The Netherlands; L. Campagnolo, Technical University of Inc., Clifton Park, NY; O. Sahni, Canada C. Bak, Technical University of Bergami, M. Gaunaa, DTU Wind Energy, Milan, Milan, Italy Rensselaer Polytechnic Institute, Troy, NY Denmark, Lyngby, Denmark Roskilde, Denmark Wednesday, 15 January 2014 238-LNCH-2 Luncheon in the Exhibit Hall Exhibit Hall 1230 - 1330 hrs Wednesday, 15 January 2014 239-SB-6 Wednesday Afternoon Speakers’ Briefing Session Rooms 1330 - 1400 hrs Wednesday, 15 January 2014 240-AA-6 Jet Noise III Azalea 2 Chaired by: K. AHUJA, Georgia Institute of Technology and K. TEERLINCK, United Technologies Research Center 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs AIAA-2014-0876 AIAA-2014-0877 AIAA-2014-0878 AIAA-2014-0879 AIAA-2014-0880 AIAA-2014-0881 AIAA-2014-0882 Noise from Aft Deck Exhaust Resonant Interaction of a Developing an Empirical Model Experimental Study on Acoustic Experimental Investigation of Investigation of the Acoustic Generation Nozzles—Differences in Rectangular Jet with a Flat- for Jet-Surface Interaction Phenomena of Supersonic Jet Two Impinging Model Scale Instabilities of Supersonic Mechanism of a Supersonic Jet Experimental Embodiments plate Noise Impinging on Inclined Flat Plate Jets Impinging Jets Using Unsteady Impinging on Deflectors J. Bridges, NASA Glenn Research K. Zaman, A. Fagan, M. Clem, C. C. Brown, NASA Glenn Research M. Akamine, Y. Nakanishi, K. Okamoto, L. Myers, C. Kuo, D. McLaughlin, Pressure Sensitive Paint S. Tsutsumi, R. Takaki, Japan Center, Cleveland, OH Brown, NASA Glenn Research Center, Center, Cleveland, OH University of Tokyo, Chiba, Japan; S. Pennsylvania State University, T. Davis, A. Edstrand, L. Cattafesta, Aerospace Exploration Agency Cleveland, OH Teramoto, T. Okunuki, University of University Park, PA F. Alvi, Florida State University, (JAXA), Sagamihara, Japan; Y. Tokyo, Tokyo, Japan; S. Tsutsumi, Japan Tallahassee, FL; D. Yorita, K. Asai, Nakanishi, K. Okamoto, University of Aerospace Exploration Agency (JAXA), Tohoku University, Sendai, Japan Tokyo, Kashiwa, Japan; S. Teramoto, Kanagawa, Japan University of Tokyo, Bunkyo, Japan Wednesday, 15 January 2014 241-AFM-8 Launch Vehicles National Harbor Conf Rm 12 Chaired by: M. LOWENBERG, University of Bristol and B. BURCHETT, Rose-Hulman Institute of Technology 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2014-0883 AIAA-2014-0884 AIAA-2014-0885 AIAA-2014-0886 AIAA-2014-0887 AIAA-2014-0888 Predictive Optimal Pulse- Impact of Cross-axis Structural Low Cost, High Limit Circular Motion of GPS-Denied State Estimation Trajectory Simulation of jet Control for Symmetric Dynamics on Validation of Linear Maneuverability Projectile Spinning Projectiles Induced by for Spin-Stabilized Precision Flexible Missiles and the Effect Projectiles Models for Space Launch System Guidance and Flight Control Backlash of Actuators Projectiles of Flexibility on Hit Precision B. Burchett, Rose-Hulman Institute of J. Pei, S. Derry, NASA Langley Research F. Fresconi, Army Research W. Zhou, S. Yang, L. Zhao, Beijing L. Fairfax, J. Maley, F. Fresconi, S. Yao, Z. Wu, C. Yang, Beihang Technology, Terre Haute, IN Center, Hampton, VA; J. Newsom, Laboratory, Aberdeen Proving Institute of Technology, Beijing, China Army Research Laboratory, Aberdeen University, Beijing, China Analytical Mechanics Associates, Inc., Ground, MD Proving Ground, MD Hampton, VA; Z. Zhou, NASA Langley Research Center, Hampton, VA Wednesday, 15 January 2014 242-AFM-9 Micro UAVs National Harbor Conf Rm 13 Chaired by: R. LIND, University of Florida and E. MORELLI, NASA Langley Research Center 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs AIAA-2014-0889 AIAA-2014-0890 AIAA-2014-0891 AIAA-2014-0892 AIAA-2014-0893 AIAA-2014-0894 AIAA-2014-0895 An Experimental Study of In-Flight Oscillation of Flapping Effect of the Parametric Characterization of a Neural Model of an Entomopter Flow structures, transport and Nonlinear Dynamics of Stroke Kinematics and Wing Wing Vehicle Excitation on the Longitudinal Simplified Dynamics Model for Aerodynamics navigation in hurricanes Flapping Wing MAV Using Planform Design for Slow A. Jennings, Air Force Institute of Stability of Hovering MAVs/ Control and Design of Flexible K. Sibilski, Air Force Institute of D. Lipinski, K. Mohseni, University of Cycle-Averaged Force Forward Flapping Flight Technology, Wright-Patterson AFB, Insects Flapping Wing MAVs Technology, Warsaw, Poland; P. Florida, Gainesville, Gainesville, FL Coefficients W. Fassmann, S. Thomson, Brigham OH; M. Mayhew, Virginia Military H. Taha, A. Nayfeh, M. Hajj, Virginia S. Nogar, A. Gogulapati, J. Czekalowski, Institute of Aviation, A. Rege, K. Subbarao, B. Dennis, Young University, Provo, UT Institute, Lexington, VA; J. Black, Air Polytechnic Institute and State McNamara, A. Serrani, Ohio State Warsaw, Poland; W. Wroblewski, University of Texas, Arlington,

119 Force Institute of Technology, Wright- University, Blacksburg, VA University, Columbus, OH Wroclaw University of Technology, Arlington, TX Patterson AFB, OH Wroclaw, Poland; A. Zyluk, Air Force Institute of Technology, Warsaw, Poland Wednesday, 15 January 2014 243-AMT-6 Recent Advances and Applications of Stochastic Estimation Techniques (Invited) Maryland Ballroom 2 Chaired by: P. LAVOIE, University of Toronto and L. UKEILEY, University of Florida 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs Oral Presentation (Invited) Oral Presentation (Invited) AIAA-2014-0896 Oral Presentation (Invited) Oral Presentation (Invited) Oral Presentation (Invited) AIAA-2014-0897 Simultaneous use of PIV, wall Surface Quantity Based Flow Velocity Field Estimation Validation of Estimation Methods Stochastic Estimation of Multi-time-delay LSE-POD Stochastic estimation of shear stress and pressure Field Estimation Using Unsteady Wall Pressure via Time Resolved PIV in High Acoustic Source Terms in the complementary approach applied cavity shear layer and fully measurements for separation L. Ukeiley, A. Nickels, University of Measurements in a Leading Speed Compressible Jets Vortex Sound Analogy to unsteady high Reynolds developed turbulent channel control on a NACA 0015 profile Florida, Gainesville, Gainesville, FL; Edge Slat Flow P. Shea, M. Glauser, Z. Berger, M. Berry, N. Zawodny, D. Dussault, L. Ukeiley, number near wake flow flows: linear and non linear J. Bonnet, B. Noack, V. Parezanovic, R. Reger, L. Cattafesta, Florida State S. Wilkins, P. Richard, J. Hall, Syracuse University, Syracuse, NY; B. University of Florida, Gainesville, V. Durgesh, California State multi-time-delay analyses National Center for Scientific University, Tallahassee, FL University of New Brunswick, Kiel, Air Force Research Laboratory, Gainesville, FL; L. Cattafesta, Florida University, Northridge, CA; J. D. Lasagna, Southampton University, Research (CNRS), Poitiers, France Fredericton, Canada Wright-Patterson AFB, OH; S. Gogineni, State University, Gainesville, FL Naughton, University of Wyoming, Southampton, United Kingdom; L. Spectral Energies, LLC, Dayton, OH; Laramie, Laramie, WY Fronges, M. Orazi, G. Iuso, Technical et al. University of Turin, Turin, Italy Wednesday, 15 January 2014 244-APA-25 Aerodynamic and Multi-Disciplinary Design and Optimization Maryland Ballroom 4 Chaired by: J. MURRAY, Sandia National Laboratories and J. GUGLIELMO, Boeing Defense, Space & Security 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs AIAA-2014-0898 AIAA-2014-0899 AIAA-2014-0900 AIAA-2014-0901 AIAA-2014-0902 AIAA-2014-0903 AIAA-2014-0904 Efficient Global Optimization A numerical study of adaptive Variable-Fidelity Aerodynamic An Invariant Formulation for Wing Shape Optimization Multipoint Aerodynamic High Efficient Global Optimization of using a Multi-objective FFD in aerodynamic shape Design Using Gradient- the Minimum Induced Drag Using Local Response Surface Fidelity Shape Optimization of Vortex Generators on a Super Approach Infill Sampling optimization Enhanced Kriging Surrogate Conditions of Non-planar Wing Approximations, Space an Isolated Engine Nacelle Critical Infinite-Wing Using Criteria O. Amoignon, Swedish Defense Model with Regression Systems Mapping and Physics-Based H. Toubin, I. Salah El Din, M. Kriging-Based Surrogate Models S. Yi H. Kwon, S. Choi, Korea Research Agency (FOI), Stockholm, Y. Jo, S. Choi, Korea Advanced L. Demasi, A. Dipace, San Diego State Surrogates Meheut, ONERA, Meudon, France N. Namura, S. Obayashi, Tohoku Advanced Institute of Science and Sweden; J. Hradil, J. Navratil, Brno Institute of Science and Technology, University, San Diego, CA; G. Monegato, S. Koziel, L. Leifsson, Reykjavik University, Sendai, Japan; S. Jeong, Technology, Daejeon, South Korea University of Technology, Brno, Czech Daejeon, South Korea Technical University of Turin, Turin, Italy; University, Reykjavik, Iceland Kyunghee University, Yongin, South Republic R. Cavallaro, San Diego State University, Korea San Diego, CA Wednesday, 15 January 2014 245-APA-26 Environmentally Friendly Aircraft Design - Laminar Flow Enabling Technology Maryland Ballroom A Chaired by: S. FERGUSON, Boeing Defense, Space & Security and R. WAHLS, NASA-Langley Research Center 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2014-0905 AIAA-2014-0906 AIAA-2014-0907 AIAA-2014-0908 AIAA-2014-0909 AIAA-2014-0910 Aerodynamically Optimal Preliminary Experimental Computational Assessment of High-fidelity Aerodynamic Laminar Flow Control Flight Effects of Step Excrescences Regional Aircraft Concepts: Assessment of the Boundary the Boundary Layer Ingesting Shape Optimization of Experiment Design and on a Swept Wing in a Low- Conventional and Blended- Layer Ingestion Benefit for the Nacelle Design of the D8 Aircraft Unconventional Aircraft Execution Disturbance Wind Tunnel Wing-Body Designs D8 Aircraft S. Pandya, NASA Ames Research Center, through Axial Deformation A. Tucker, Air Force Research G. Duncan, B. Crawford, M. Tufts, T. Reist, D. Zingg, University of A. Uranga, M. Drela, E. Greitzer, Moffett Field, CA; A. Uranga, A. Espitia, H. Gagnon, D. Zingg, University of Laboratory, Wright-Patterson AFB, W. Saric, H. Reed, Texas A&M

120 Toronto, Toronto, Canada N. Titchener, M. Lieu, N. Siu, A. Huang, Massachusetts Institute of Toronto, Toronto, Canada OH; W. Saric, H. Reed, Texas A&M University, College Station, TX Massachusetts Institute of Technology, Cambridge, MA University, College Station, TX Technology, Cambridge, MA; et al. Wednesday, 15 January 2014 246-APA-27 Special Session: 2nd High Lift Prediction Workshop (HiLiftPW-2) II Maryland Ballroom 3 Chaired by: R. RUDNIK, DLR - German Aerospace Center and T. WAYMAN, Gulfstream Aerospace Corporation 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs AIAA-2014-0911 AIAA-2014-0912 AIAA-2014-0913 AIAA-2014-0914 AIAA-2014-0915 AIAA-2014-0916 AIAA-2014-0917 Lattice-Boltzmann Flow Contribution from Metacomp NSMB contribution to the 2nd Numerical Simulation of DLR-F11 DLR Contribution to the 2nd CRUNCH CFD Calculations for Time-resolved adaptive FEM Simulations for the HiLiftPW-2 Technologies, Inc. to the High Lift Prediction Workshop High Lift Conﬁguration from High Lift Prediction Workshop HiLiftPW-2 with Discretization simulation of the DLR-F11 B. Koenig, Exa GmbH, Stuttgart, Second High Lift Prediction T. Deloze, E. Laurendeau, École HiLiftPW-2 using STAR-CCM+ R. Rudnik, German Aerospace Center Error Predictions aircraft model at high Reynolds Germany Workshop Polytechnique de Montréal, J. Hanke, P. Shankara, D. Snyder, (DLR), Braunschweig, Germany P. Cavallo, CRAFT Tech, Dublin, PA number U. Goldberg, Y. Allaneau, Metacomp Montréal, Canada Computational Dynamics Ltd., Winter J. Hoffman, J. Jansson, R. Vilela de Technologies, Agoura Hills, CA Garden, FL Abreu, N. Jansson, Royal Institute of Technology (KTH), Stockholm, Sweden Wednesday, 15 January 2014 247-APA-28 Special Session: CREATE-AV High Performance Computing Multiphysics Applications of Full-Up Air Vehicles III Maryland Ballroom 5 Chaired by: N. HARIHARAN, CREATE-AV; D. MCDANIEL, University of Alabama at Birmingham; B. HALLISSY, NAVAIR and T. SHAFER, NAVAIR 1400 hrs 1430 hrs 1500 hrs 1530 hrs AIAA-2014-0918 AIAA-2014-0919 AIAA-2014-0920 AIAA-2014-0921 CREATE-AV Quality Assurance: 3-D DES and RANS Validation Fundamental Physics The CREATE-DaVinci Power Best Practices for Validating Using CREATE-AV Kestrel Validation Using CREATE-AV User Experience and Supporting Computation- T. Shafer, D. Hine, J. Laiosa, B. KestrelTM Part I B. Rooney, Air Force Life Cycle Based Engineering Software Hallissy, J. Forsythe, Naval Air D. Hine, J. Forsythe, B. Hallissy, T. Management Center, Wright- B. Hallissy, D. Hine, J. Laiosa, T. Systems Command, Patuxent Shafer, J. Laiosa, Naval Air Systems Patterson AFB, OH Shafer, J. Forsythe, J. Abras, CREATE River, MD Command, Patuxent River, MD AV Team, Patuxent River, MD; et al. Wednesday, 15 January 2014 248-AS-2 Adaptive Actuation Chesapeake Conf Rm D Chaired by: D. MCGOWAN, NASA Langley Research Center and F. GANDHI, Rensselaer Polytechnic Inst 1400 hrs 1500 hrs 1530 hrs 1600 hrs No Presentations AIAA-2014-0922 AIAA-2014-0923 AIAA-2014-0924 Active Flow Control via Piezo- Adaptive-Twist Airfoil Based on Synergistic Smart Morphing Actuated Airfoils for High-Lift Electrostatic Stiffness Variation Aileron: Aero-structural C. Behr, M. Sinapius, Technical W. Raither, L. De Simoni, L. Di Lillo, Performance Analysis University of Braunschweig, Swiss Federal Institute of Technology, A. Pankonien, K. Duraisamy, C. Braunschweig, Germany; P. Wierach, Zürich, Switzerland; A. Bergamini, Faria, D. Inman, University of German Aerospace Center (DLR), Swiss Federal Laboratories for Michigan, Ann Arbor, Ann Arbor, MI Braunschweig, Germany Materials Science and Technology, Dübendorf, Switzerland; P. Ermanni, Swiss Federal Institute of Technology, Zürich, Switzerland Wednesday, 15 January 2014 249-ASE-1 Topics in the Tropospheric Environment Chesapeake Conf Rm 9 Chaired by: N. AHMAD, NASA Langley Research Center and M. POLITOVICH, National Center for Atmospheric Research 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs AIAA-2014-0925 AIAA-2014-0926 AIAA-2014-0927 AIAA-2014-0928 AIAA-2014-0929 Wake Vortex Evolution During Numerical Simulation of Jet- Review of Idealized Aircraft Simulating the Freezing of Study of Icing Process using Approach and Landing With and Wake Vortex Interaction Wake Vortex Models Supercooled Water Droplets Dual-Luminescence Imaging Without Plate Lines T. Misaka, S. Obayashi, Tohoku N. Ahmad, F. Proctor, NASA Langley Impacting a Cooled Substrate for Aircraft-Icing Prevention F. Holzäpfel, A. Stephan, University, Sendai, Japan; A. Stephan, Research Center, Hampton, VA J. Blake, D. Thompson, Mississippi H. Sakaue, K. Morita, Japan F. Holzäpfel, T. Gerz, German Aerospace 121 German Aerospace Center (DLR), State University, Mississippi Aerospace Exploration Agency Oberpfaffenhofen, Germany; T. Misaka, Center (DLR), Oberpfaffenhofen, State, MS; D. Raps, Eurocopter (JAXA), Chofu, Japan; M. Tanaka, Tohoku University, Sendai, Japan; Germany; K. Nakahashi, Japan Deutschland, Donauworth, Germany; S. Kimura, Kanagawa Institute of S. Körner, German Aerospace Center Aerospace Exploration Agency (JAXA), T. Strobl, EADS, Munich, Germany Technology, Atsugi, Japan (DLR), Oberpfaffenhofen, Germany Chofu, Japan Wednesday, 15 January 2014 250-FD-28 Flow Control of Bodies and Riblets Woodrow Wilson D Chaired by: J. LITTLE, The University of Arizona and K. GRANLUND, Air Force Research Laboratory 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs AIAA-2014-0932 AIAA-2014-0930 AIAA-2014-0931 AIAA-2014-0933 AIAA-2014-0934 Aerodynamic Flow Control of Closed-Loop Flow Control on Asymmetric Vortex State Flow Control over a Conical Direct Numerical Simulations a Moving Axisymmetric Bluff a Ogive Forebody at a High Response to Open-Loop Forebody Using Pulsed of High-Speed Turbulent Body Angle of Attack using Model Actuation for Variations in Nanosecond Discharge Actuators Boundary Layers over Riblets T. Lambert, B. Vukasinovic, A. Glezer, Predictive Control Angle of Attack and Reynolds Y. Long, H. Li, X. Meng, Northwestern L. Duan, National Institute of Georgia Institute of Technology, C. Porter, C. Fagley, J. Seidel, T. Number Polytechnical University, Xi’an, China; Aerospace, Hampton, VA; M. Atlanta, GA McLaughlin, U.S. Air Force Academy, J. Farnsworth, C. Fagley, C. Porter, T. F. Liu, S. Luo, University of California, Choudhari, NASA Langley Research Colorado Springs, CO McLaughlin, U.S. Air Force Academy, Irvine, Irvine, CA Center, Hampton, VA Colorado Springs, CO Wednesday, 15 January 2014 251-FD-29 Higher-Order Methods III Chesapeake Conf Rm 8 Chaired by: H. HUYNH, NASA Glenn Research Center and N. BURGESS, University of Wyoming 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs AIAA-2014-0935 AIAA-2014-0936 AIAA-2014-0937 AIAA-2014-0938 AIAA-2014-0939 Canonical Test Cases for High- Higher Order Multigrid High-Order Flux Correction/ A Hybridized Discontinuous A Finite Volume Method Based Order Unstructured Implicit Algorithms for a Discontinuous Finite Difference Schemes for Galerkin Method for Three- on WENO Reconstruction for Large Eddy Simulation Galerkin RANS Solver Strand Grids Dimensional Compressible Compressible Flows on Hybrid B. Vermeire, S. Nadarajah, McGill M. Wallraff, T. Leicht, German A. Katz, D. Work, Utah State Flow Problems Grids University, Montréal, Canada; P. Aerospace Center (DLR), University, Logan, UT M. Woopen, A. Balan, G. May, H. Luo, North Carolina State Tucker, University of Cambridge, Braunschweig, Germany RWTH Aachen University, Aachen, University, Raleigh, NC Cambridge, United Kingdom Germany Wednesday, 15 January 2014 252-FD-30 Shock Interactions and Control Maryland Ballroom 6 Chaired by: M. MCQUILLING, Saint Louis University and R. SCHMIT, USAF AFRL 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs AIAA-2014-0940 AIAA-2014-0941 AIAA-2014-0942 AIAA-2014-0943 AIAA-2014-0944 A body-force based method Characterization of the Shear Active Transonic Shock Control Three-dimensional shock Numerical Simulation of to generate supersonic Layer in a Mach 3 Shock/ A. Gissen, B. Vukasinovic, A. Glezer, control bumps: effects of Energy Deposition in a equilibrium turbulent Turbulent Boundary Layer Georgia Institute of Technology, geometry Supersonic Flow Past a boundary layer proﬁles Interaction Atlanta, GA; S. Gogineni, Spectral P. Bruce, Imperial College London, Hemisphere M. Waindim, D. Gaitonde, R. C. Helm, S. Priebe, J. Li, University Energies, LLC, Dayton, OH; M. London, United Kingdom; S. M. Mortazavi, D. Knight, Rutgers Yentsch, Ohio State University, of Maryland, College Park, College Paul, D. Wittich, Air Force Research Colliss, H. Babinsky, University of University, New Brunswick, NJ; Columbus, OH Park, MD; D. Pierre, National Center Laboratory, Kirtland AFB, NM Cambridge, Cambridge, United O. Azarova, Russian Academy of

122 for Scientific Research (CNRS), Kingdom Sciences, Moscow, Russia; J. Shi, Marseille, France; P. Martin, H. Yan, Northwestern Polytechnical University of Maryland, College Park, University, Xi’an, China College Park, MD Wednesday, 15 January 2014 253-FD-31 Shock-Dominated Flows National Harbor Conf Rm 2 Chaired by: A. GROSS, New Mexico State University and V. NARAYANASWAMY, University of Texas @ Austin 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs AIAA-2014-0945 AIAA-2014-0946 AIAA-2014-0947 AIAA-2014-0948 AIAA-2014-0949 Adaptive Shock Control Bumps Influence of Different Inlet Entropy Viscosity Approach Blast Loading on the Head Under Study of Shock Trains and E. Jinks, P. Bruce, M. Santer, Flow on the Ring-like Vortex for Compressible Turbulent a Military Helmet: Effect of Face Pseudo-Shock Waves in Imperial College London, London, Structure in MVG Controlled Simulations using Discontinuous Shield and Mandible Protection Constant Area Ducts United Kingdom Supersonic Ramp Flow Spectral Element Method D. Mott, Naval Research Laboratory, T. Oka, D. Ono, Y. Miyazato, Y. Yan, C. Liu, University of Texas, H. Abbassi, F. Mashayek, University Washington, DC; T. Young, Berkeley University of Kitakyushu, Arlington, Arlington, TX of Illinois, Chicago, Chicago, IL; G. Research Associates, Beltsville, MD; D. Kitakyushu, Japan Jacobs, San Diego State University, San Schwer, Naval Research Laboratory, Diego, CA Washington, DC Wednesday, 15 January 2014 254-FD-32 Transition Open Forum National Harbor Conf Rm 4 1400 - 1730 hrs Chaired by: H. REED, Texas A&M University and G. HUANG, Wright State University Wednesday, 15 January 2014 255-FD-33 Transonic and Supersonic Flows Azalea 1 Chaired by: W. LIOU, Western Michigan University and S. GORDEYEV, University of Notre Dame 1400 hrs 1430 hrs 1500 hrs 1530 hrs AIAA-2014-0950 AIAA-2014-0951 AIAA-2014-0952 AIAA-2014-0954 Numerical Investigation of Computational Analysis Validation of a Lattice-Boltzmann SDNS of large domain Effects of Transonic Wind of Shock Wave Turbulent Approach for Transonic and supersonic boundary layers Tunnel Porous Walls on Two- Boundary Layer Interaction Supersonic Flow Simulations over weakly and strongly Dimensional Airfoil Tests T. Leger, J. Poggie, Air Force E. Fares, M. Wessels, R. Zhang, C. adiabatic walls J. Jin, C. Gao, Z. Zhao, Z. Zhang, Research Laboratory, Wright- Sun, N. Gopalaswamy, P. Roberts, Exa I. Beekman, Princeton University, Northwestern Polytechnical University, Patterson AFB, OH Corporation, Burlington, MA; et al. Princeton, NJ; S. Priebe, P. Martin, Xi’an, China; J. Xiong, F. Liu, University University of Maryland, College Park, of California, Irvine, Irvine, CA; et al. College Park, MD Wednesday, 15 January 2014 256-FD-34 Vortex Flows National Harbor Conf Rm 3 Chaired by: M. GREEN, Syracuse University 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2014-0955 AIAA-2014-0956 AIAA-2014-0957 AIAA-2014-0958 AIAA-2014-0959 AIAA-2014-0960 Wingtip Vortices from an Vortex Flow Control over a The Impact of an Experimental Investigation of Vortex Control by Pulsed Vortex Control by Non- Exergy-Based Perspective Delta Wing Using Leading- Inhomogeneous Temperature Turbulent Swirling Wakes Power Pumping Equilibrium Plasma M. Memon, K. Wabick, A. Altman, edge Rudder Field on the Precessing M. Hind, J. Naughton, University of A. Klimov, V. Bityurin, I. Moralev, A. Klimov, V. Bityurin, M. Sidorenko, University of Dayton, Dayton, OH; Z. Yang, X. Meng, W. Li, J. Cai, Vortex Core in Swirling Jets Wyoming, Laramie, Laramie, WY S. Bychkov, L. Pyatnitsky, N. I. Moralev, B. Tolkunov, A. Efimov, R. Buffo, RWTH Aachen University, Northwestern Polytechnical Undergoing Vortex Breakdown Tretyakova, Russian Academy of Russian Academy of Sciences, Aachen, Germany University, Xi’an, China L. Rukes, M. Sieber, C. Nayeri, C. Sciences, Moscow, Russia Moscow, Russia; et al. 123 Paschereit, Technical University of Berlin, Berlin, Germany Wednesday, 15 January 2014 257-GEPC-3 NASA Aeronautical Sciences Project Overview and Progress Woodrow Wilson A Chaired by: M. ROGERS, NASA Ames Research Center and D. WILLIAMS, NASA Langley Research Center 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs Oral Presentation (Invited) Oral Presentation (Invited) Oral Presentation (Invited) Oral Presentation (Invited) Oral Presentation (Invited) Oral Presentation (Invited) Oral Presentation (Invited) NASA Aeronautical Sciences NASA Aeronautical Sciences NASA Aeronautical Sciences NASA Aeronautical Sciences NASA Aeronautical Sciences NASA Aeronautical Sciences NASA Aeronautical Sciences Project Overview Project - Revolutionary Project - Structures and Project - MDAO and Systems Project - Combustion Overview Project - Innovative Project - Controls Overview J. Heidmann, NASA Glenn Research Computational Aerosciences Materials Overview Analysis Overview J. Moder, D. Bulzan, NASA Glenn Measurements Overview S. Garg, NASA Glenn Research Center, Cleveland, OH Overview D. Hopkins, NASA Glenn Research J. Robinson, J. Viken, NASA Langley Research Center, Cleveland, OH T. Jones, NASA Langley Research Center, Cleveland, OH M. Malik, NASA Langley Research Center, Cleveland, OH Research Center, Hampton, VA Center, Hampton, VA Center, Hampton, VA Wednesday, 15 January 2014 258-GNC-14 Aircraft Guidance, Navigation and Control II National Harbor Conf Rm 7 Chaired by: F. ALMEIDA, Instituto de Aeronáutica e Espaço and N. SMITH 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2014-0961 AIAA-2014-0962 AIAA-2014-0963 AIAA-2014-0964 AIAA-2014-0965 AIAA-2014-0966 Three-dimensional Guidance Physically Integrated Incremental Nonlinear Development of the SAFE- Selective Reinitialisation Optimal Collision Avoidance Filter for Autonomous Collision Reference Model and Its Aids Dynamic Inversion and Control Cue System Component Multiple Model Adaptive Trajectories via Direct Orthogonal Avoidance in Model Based Flight Control Allocation for a Tilt Rotor UAV Mechanizations for Loss of Estimation for Fault Detection Collocation for Unmanned/ D. Galisteu, F. Almeida, Aeronautics Development G. Di Francesco, M. Mattei, E. Control Mitigation and Diagnosis Remotely Piloted Aircraft Sense and Space Institute (IAE), São José F. Zhang, S. Braun, F. Holzapfel, D’Amato, Second University of A. Lampton, D. Klyde, D. Lee, P. Lu, E. Van Kampen, Delft and Avoid Operations dos Campos, Brazil Technical University of Munich, Naples, Aversa, Italy Systems Technology, Inc., University of Technology, Delft, The N. Smith, R. Cobb, S. Pierce, Air Force Munich, Germany Hawthorne, CA; B. Cogan, NASA Netherlands Institute of Technology, Wright-Patterson Dryden Flight Research Center, AFB, OH; V. Raska, Air Force Research Edwards, CA Laboratory, Wright-Patterson AFB, OH Wednesday, 15 January 2014 259-GNC-15 Multi-Vehicle Coordination and Control National Harbor Conf Rm 8 Chaired by: E. FREW, University of Colorado Boulder 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2014-0967 AIAA-2014-0968 AIAA-2014-0969 AIAA-2014-0970 AIAA-2014-0971 AIAA-2014-0972 A Sense and Avoid System Coordinated Transport of Guided Exploration for Decentralized Model Predictive Incomplete Information Trajectory Generation and for Unmanned Aircraft in a Slung Load by a Team of Coordinated Autonomous Control for Planning Three- Pursuit-Evasion Games with Collision Avoidance for Safe Formation Flight Autonomous Rotorcraft Soaring Flight Dimensional Conflict-Free Uncertain Relative Dynamics Operation of Cooperating UAVs J. Cooper, J. Schierman, Barron Z. Li, J. Horn, J. Langelaan, K. Cheng, J. Langelaan, Pennsylvania Trajectories K. Cavalieri, Texas A&M University, V. Cichella, R. Choe, B. Mehdi, E. Associates, Inc., Charlottesville, VA Pennsylvania State University, State University, University Park, PA N. Yokoyama, National Defense College Station, TX; N. Satak, Air Xargay, N. Hovakimyan, University 124 University Park, PA Academy, Yokosuka, Japan Force Research Laboratory, Eglin of Illinois, Urbana-Champaign, AFB, FL; J. Hurtado, Texas A&M Urbana, IL; A. Trujillo, NASA Langley University, College Station, TX Research Center, Hampton, VA; et al. Wednesday, 15 January 2014 260-GNC-16 Unmanned Autonomous Systems National Harbor Conf Rm 5 Chaired by: R. BEVILACQUA, Rensselaer Polytechnic Institute and S. ULRICH, Carleton University 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs AIAA-2014-0973 AIAA-2014-0974 AIAA-2014-0975 AIAA-2014-0976 AIAA-2014-0977 AIAA-2014-0978 AIAA-2014-0979 Hovering control for a Autonomous Parafoil Return- 3D Shape Mapping of Obstacle Scan registration using Region- Safety Critical Platform for Mini Integration of Real-Time Investigation of an stratospheric airship in to-Point Vehicle for High Using Stereo Vision Sensor on growing clustering NDT UAS Insertion into the Common Autonomous UAV with Autonomous Landing Sensor unknown wind Altitude Ballooning Quadrotor UAV S. Ahuja, S. Waslander, University of Airspace Commercial R/C Aircraft for Unmanned Aerial Systems Z. Zheng, M. Zhu, D. Shi, Z. Wu, S. Lee, A. Arena, Oklahoma State J. Park, Y. Kim, Seoul National Waterloo, Waterloo, Canada B. Vanek, P. Bauer, I. Gozse, M. Lukatsi, S. Lee, Oklahoma State University, J. McCafferty, D. Woodward, G. Ray, Beihang University, Beijing, China University, Stillwater, OK University, Seoul, South Korea I. Reti, J. Bokor, Hungarian Academy of Stillwater, OK A. Bachelani, B. Kim, University of Sciences, Budapest, Hungary Kansas, Lawrence, Lawrence, KS Wednesday, 15 January 2014 261-GT-6 Test Facility and Systems Development I Maryland Ballroom D Chaired by: J. MICOL, NASA-Langley Research Center and R. PARYZ 1400 hrs 1430 hrs 1500 hrs 1530 hrs AIAA-2014-0980 AIAA-2014-0981 AIAA-2014-0982 AIAA-2014-0983 Mechanical Characteristics of AFRL/AEDC Instant Loads at Towards EFD/CFD Integration: Development of Dynamic Electromagnetic Shakers and High Incidence Angles Development of DAHWIN - Force Measurement its Force Control T. Reynolds, Air Force Research Digital/Analog-Hybrid Wind Capabilities at AEDC Tunnel 9 C. Ma, Z. Wu, C. Yang, Beihang Laboratory, Wright-Patterson AFB, OH Tunnel A. Collopy, S. Lee, University of University, Beijing, China S. Watanabe, S. Kuchi-ishi, K. Maryland, College Park, College Murakami, A. Hashimoto, H. Kato, T. Park, MD; E. Marineau, Arnold Yamashita, Japan Aerospace Exploration Engineering Development Center, Agency (JAXA), Chofu, Japan; et al. Silver Spring, MD Wednesday, 15 January 2014 262-HSABP-3 Experimental Investigations of Scramjets Chesapeake Conf Rm 7 Chaired by: R. SPRINGER, Johns Hopkins University Applied Physics Laboratory 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs Oral Presentation (Invited) AIAA-2014-0984 AIAA-2014-0985 AIAA-2014-0986 AIAA-2014-0987 AIAA-2014-0988 X-51A Flight Demonstration Filtered Rayleigh Scattering Implementation of Maximum- Characterization of a Systematic Application of Plasma-assisted combustion Program Overview (Oral) Measurements in Helium-Air Likelihood Expectation- Dual-Mode Scramjet via Background Oriented Schlieren in supersonic airflow: C. Brink, Air Force Research Mixing Experiments of Selected Maximization Algorithm for Stereoscopic Particle Image for Shock-Boundary Layer optimization of electrical Laboratory, Wright-Patterson AFB, OH Streamwise Vortex Interactions in Tomographic Reconstruction of Velocimetry Interaction Study discharge geometry a Mach 2.5 Flow TDLAT Measurements B. Rice, C. Goyne, J. McDaniel, R. J. Geerts, K. Yu, University of S. Leonov, Ohio State university, M. Crisanti, F. Vergine, L. K. Busa, J. McDaniel, University of Rockwell, University of Virginia, Maryland, College Park, College Columbus, OH; A. Vincent- Maddalena, University of Texas, Virginia, Charlottesville, Charlottesville, Charlottesville, Charlottesville, VA Park, MD Randonnier, V. Sabelnikov, ONERA, Arlington, Arlington, TX VA; M. Brown, Air Force Research Palaiseau, France; A. Firsov, D. Laboratory, Wright-Patterson AFB, OH; Yarantsev, Russian Academy of G. Diskin, NASA Langley Research Sciences, Moscow, Russia Center, Hampton, VA Wednesday, 15 January 2014 263-IS-2 Unmanned Aircraft Sensing and Control National Harbor Conf Rm 15 Chaired by: K. COHEN and E. KIVELEVITCH, University of Cincinnati 1400 hrs 1430 hrs 1500 hrs 1530 hrs AIAA-2014-0989 AIAA-2014-0990 AIAA-2014-0991 AIAA-2014-0992 A Neural Network Approach to Autonomous Soaring Using Dynamic Multi-Task Allocation Intelligent Fuzzy Flight control an Attitude Heading Reference Reinforcement Learning for for Collaborative Unmanned of an Autonomous Quadrotor System Trajectory Generation Aircraft Systems UAV

125 M. Leccadito, T. Bakker, R. Klenke, T. Woodbury, C. Dunn, J. Valasek, T. Bakker, R. Klenke, Virginia V. Fnu, K. Cohen, University of Virginia Commonwealth University, Texas A&M University, College Commonwealth University, Cincinnati, Cincinnati, OH Richmond, VA Station, TX Richmond, VA Wednesday, 15 January 2014 264-LECT-6 ASC Special Session: DLR’s Adaptive Structures Activities within the European Network Maryland Ballroom C 1400 - 1500 hrs Hans-Peter Monner Head of Department Adaptronics DLR German Aerospace Center Wednesday, 15 January 2014 265-MAT-6 Integrated Computational Materials Engineering III Chesapeake Conf Rm A Chaired by: S. ARNOLD; J. MATLIK, Rolls-Royce Corporation and M. SANGID, Purdue University 1400 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs No Presentations AIAA-2014-0993 AIAA-2014-0994 AIAA-2014-0995 AIAA-2014-0996 AIAA-2014-0997 Multi-scale computational Modelling the High Multi-Scale Modeling of Free- Atomistic Simulations A novel Volume-Compensated modeling of two-phased metal Temperature Fatigue Edge Micro-Cracks with XFEM as Part of an Integrated Particle method (VCPM) using GMC method Behaviour of Titanium Alloys J. Dustin, The Boeing Company, Computational Environment for elasticity and plasticity M. Ghorbani Moghaddam, A. Achuthan, H. Basoalto, J. Brooks, University of Seattle, WA; R. Pipes, Purdue for Structural Design analysis Clarkson University, Potsdam, NY; B. Birmingham, Birmingham, United University, West Lafayette, IN E. Wimmer, C. Freeman, M. H. Chen, Y. Liu, Arizona State Bednarcyk, S. Arnold, E. Pineda, NASA Kingdom Christensen, W. Wolf, D. Rigby, W. University, Tempe, AZ Glenn Research Center, Cleveland, OH Hamm, Materials Design, Inc., Santa Fe, NM; et al. Wednesday, 15 January 2014 266-MDO-6 Optimization Framework and Applications Chesapeake Conf Rm 4 Chaired by: R. KHIRE, United Technologies Research Center and R. KAPANIA 1400 hrs 1500 hrs 1530 hrs 1600 hrs No Presentations AIAA-2014-0998 AIAA-2014-0999 AIAA-2014-1000 Exploring the Trade-offs between Multilevel Design Optimization Experimental Validation of Wind Farm Capacity Factor and With Application to Material- the EBF3PanelOpt Vibro- Noise Impact through Novel Product Systems acoustic Analysis of Panels Pareto Translation S. DorMohammadi, M. Rais-Rohani, with Straight and Curvilinear W. Tong, S. Chowdhury, A. Mehmani, Mississippi State University, stiffeners O. Peele, Syracuse University, Syracuse, Mississippi State, MS; M. Rouhi, P. Joshi, S. Mulani, R. Kapania, NY; A. Messac, Mississippi State Concordia University, Montréal, Virginia Polytechnic Institute and University, Mississippi State, MS Canada State University, Blacksburg, VA Wednesday, 15 January 2014 267-MST-4 Simulation Requirements for LOC Prevention & Recovery Training (Invited) National Harbor Conf Rm 6 Chaired by: D. CRIDER, National Transportation Safety Board 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2014-1001 AIAA-2014-1002 AIAA-2014-1003 AIAA-2014-1004 AIAA-2014-1005 AIAA-2014-1006 Progress in Loss of Control An Evaluation of Several Stall Flight Simulator Augmentation Pilot Vehicle System Modeling Research into reduction of Air Frame Icing Inﬂuences Mitigation Models for Commercial Transport for Stall and Upset Training Using Sub-Scale Flight Loss-of-Control accident rate in a on the Risk of Loss of Control D. Crider, National Transportation Training D. Gingras, J. Ralston, R. Oltman, C. Experiments meaningful and measurable way In-ﬂight Safety Board, Washington, DC J. Schroeder, Federal Aviation Wilkening, R. Watts, Bihrle Applied T. Kumar, Y. Gu, West Virginia through the use of innovative P. Ransbury, D. Carroll, Aviation Administration, Moffett Field, CA; Research, Inc., Hampton, VA; P. University, Morgantown, WV pilot training techniques Performance Solutions, Mesa, AZ J. Burki-Cohen, U.S. Department of Derochers, Test Pilot, Inc., Peaser, TX J. Priest, Calspan Corporation, 126 Transportation, Cambridge, MA; D. Buffalo, NY Shikany, The Boeing Company, Seattle, WA; D. Gingras, Bihrle Applied Research, Inc., Hampton, VA; P. Desrochers, Test Pilot, Inc., Weatherford, TX Wednesday, 15 January 2014 268-NDA-6 Nondeterministic Methods for Design Chesapeake Conf Rm 5 Chaired by: N. KIM, University of Florida and S. HOSDER, Missouri University of Science and Technology 1400 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs No Presentations AIAA-2014-1007 AIAA-2014-1008 AIAA-2014-1009 AIAA-2014-1010 AIAA-2014-1011 Aggressive Design Under Optimal Design and Performance of Different Deciding How Conservative Utilizing an Adjustment Factor Uncertainty Tolerancing of Compressor Alloys by Assessing Epistemic A Designer Should Be: to Scale Between Multiple P. Seshadri, P. Constantine, G. Blades Subject to and Aleatory Uncertainty in Simulating Future Tests and Fidelities Within a Design Iaccarino, Stanford University, Manufacturing Variability the Crack Growth Rates Redesign Process: A Stepping Stone to Stanford, CA E. Dow, Q. Wang, Massachusetts K. Bhachu, R. Haftka, N. Kim, N. Price, T. Matsumura, R. Haftka, Dialable Fidelity Design Institute of Technology, Cambridge, MA University of Florida, Gainesville, N. Kim, University of Florida, C. Fischer, R. Grandhi, Wright State Gainesville, FL; C. Hurst, Cessna Gainesville, Gainesville, FL University, Dayton, OH Aircraft Company, Wichita, KS Wednesday, 15 January 2014 269-PANEL-6 Emerging Technologies of Importance to Aerospace Panel Potomac Ballroom C 1400 - 1600 hrs Moderator: Dan Jensen, Engineering Manager, Rolls-Royce Corporation Panelists: Foundational Shifts in Computing-Enabled Design & Engineering NASA Embarks on the Quantum Computing Path Distributed Electric Propulsion: An Emerging Technology for Aircraft Emerging Technologies and Potential Impact for the NASA Mission Dan Bodony Rupak Biswas Mark Moore W. Keith Belvin Professor Deputy Director, Exploration Technology Directorate Design Engineer Chief Technologist University of Illinois at Urbana-Champaign NASA Ames Research Center NASA Langley Research Center NASA Langley Research Center

Wednesday, 15 January 2014 270-PANEL-7 International Session - Status of Pressure Gain Combustion for Propulsion, Research & Applications I Maryland Ballroom 1 1400 - 1630 hrs Chaired by: Venkat Tangirala, General Electric Global Research Center, NY and Chris Brophy, Naval Postgraduate School, Monterey, CA Sponsor: AIAA - Pressure Gain Combustion Working Group for Program Committee

Panelists: Dr. François Falempin Jiro Kasahara K. Kailasanath Jeong-Yeol Choi Chief Engineer for Advanced Powered Airframe, MDNA Professor, Nagoya University Director, Laboratories for Computational Physics & Fluid Dynamics Professor, Department of Aerospace Engineering France Nagoya, Japan Naval Research Laboratory Pusan National University Washington, DC Busan Republic of Korea

Wednesday, 15 January 2014 127 271-PC-15 Detonation and PDEs I Chesapeake Conf Rm H Chaired by: A. STARIKOVSKIY, Princeton University; T. NGUYEN, Aerojet Rocketdyne and T. NGUYEN, Aerojet Rocketdyne 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs AIAA-2014-1012 AIAA-2014-1013 AIAA-2014-1014 AIAA-2014-1015 AIAA-2014-1016 Experiments and development Propellant Plenum Dynamics Towards Efficient, Unsteady, Periodic Exhaust Flow through Study on Detonation-Engine of Long-test-duration in a Two-dimensional Rotating Three-Dimensional Rotating a Converging-Diverging Nozzle Momentum-and-Thrust loss Hypervelocity Detonation- Detonation Experiment Detonation Engine Simulations Downstream of a Rotating Measurement by Ballistic driven Shock Tunnel (LHDst) M. Fotia, J. Hoke, Innovative D. Schwer, A. Corrigan, K. Detonation Engine Pendulum and Laser Z. Jiang, Chinese Academy of Scientific Solutions, Inc., Dayton, Kailasanath, Naval Research B. Rankin, J. Hoke, Innovative Displacement Method Sciences, Beijing, China OH; F. Schauer, Air Force Research Laboratory, Washington, DC Scientific Solutions, Inc., Dayton, T. Ashida, University of Tsukuba, Laboratory, Wright-Patterson AFB, OH OH; F. Schauer, Air Force Research Tsukuba, Japan; J. Kasahara, Nagoya Laboratory, Wright-Patterson AFB, OH University, Nagoya, Japan Wednesday, 15 January 2014 272-PC-16 Spray and Droplet Combustion I Chesapeake Conf Rm G Chaired by: C. BRUNO, United Technologies Research Center and H. EL-ASRAG, Massachusettes Institute of Technology 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2014-1017 AIAA-2014-1018 AIAA-2014-1019 AIAA-2014-1020 AIAA-2014-1021 AIAA-2014-1022 Modeling of Fuel Vapor Jet Effect of Turbulence Modeling Experimental Study of Initial Direct Numerical Simulations Liquid Spray Characterization Flame stability analysis in Eruption Induced by Local on Spray Dynamics for an Diameter Effects on Convection- of Heptane Spray Autoignition in Flow Field with Centripetal an ultra compact combustor Droplet Heating Evaporating Acetone Spray Jet free Droplet Combustion in in Methane-air Mixtures Acceleration using a probability density J. Sim, King Abdullah University of H. El-Asrag, Ansys, Inc., Lebanon, the Standard Atmosphere for Relevant to Dual-fuel Engines D. Richardson, Air Force Research function approach for large- Science and Technology, Thuwal, NH; M. Braun, Ansys, Inc., n-Heptane, n-Octane, and E. Demosthenous, G. Borghesi, E. Laboratory, Wright-Patterson AFB, eddy simulation of spray Saudi Arabia; H. Im, University of Darmstadt, Germany; M. Sami, n-Decane: International Space Mastorakos, R. Cant, University OH; A. Brinker, M. Polanka, Air combustion Michigan, Ann Arbor, Ann Arbor, MI; Ansys, Inc., Austin, TX Station and Ground-based of Cambridge, Cambridge, United Force Institute of Technology, C. Heye, V. Raman, University of S. Chung, King Abdullah University Kingdom Wright-Patterson AFB, OH; A. Lynch, Texas, Austin, Austin, TX of Science and Technology, Thuwal, Experiments D. Blunck, Air Force Research Saudi Arabia Y. Liu, J. Rah, K. Trenou, Cornell Laboratory, Wright-Patterson AFB, OH University, Ithaca, NY; M. Hicks, NASA Glenn Research Center, Cleveland, OH; C. Avedisian, Cornell University, Ithaca, NY Wednesday, 15 January 2014 273-PC-17 Turbulent Combustion Modeling II Chesapeake Conf Rm I Chaired by: O. GULDER, UTIAS University of Toronto and M. MUELLER, Princeton University 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2014-1023 AIAA-2014-1024 AIAA-2014-1025 AIAA-2014-1026 AIAA-2014-1027 AIAA-2014-1028 Large-eddy simulations of a A High-Order Finite-Volume Direct numerical simulation of Numerical Simulation of a Modeling Supersonic Turbulent A flame-generated-manifold 128 highly turbulent counterflow Scheme for Large-Eddy bluff-body-stabilized premixed Scramjet using a Storage/ Reacting Flows with a Variable chemistry based transport premixed burner Simulation of Turbulent flames Retrieval Chemistry Scheme Turbulent Prandtl and Schmidt PDF model for gas-turbine K. Kemenov, W. Calhoon, CRAFT Premixed Flames P. Arias, B. Lee, H. Im, King Abdullah Y. Zhang, CD-adapco, Melville, NY Numbers Model combustor simulations Tech, Huntsville, AL L. Tobaldini Neto, C. Groth, University University of Science and Technology, J. Wang, F. Chen, H. Liu, Shanghai A. Gupta, J. Zhu, M. Anand, Rolls- of Toronto, Toronto, Canada Thuwal, Saudi Arabia Jiao Tong University, Shanghai, China Royce Group plc, Indianapolis, IN; R. Eggels, Rolls-Royce Group plc, Dahlewitz, Germany Wednesday, 15 January 2014 274-PDL-9 Non-Equilibrium Effects in Discharges Azalea 3 Chaired by: S. STARIKOVSKAYA, Ecole Polytechnique, Paris 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2014-1029 AIAA-2014-1030 AIAA-2014-1031 AIAA-2014-1032 AIAA-2014-1033 AIAA-2014-1034 Formation of vibrational Experimental and numerical Thermal Ionization Instability High Energy Plume Study of Catalytic Effects at An Examination of Nitric Oxide distribution function of study of fast gas heating and O Development in Air Plasma Impingement on Spacecraft Reentry Vehicle Kinetics in a Plasma Afterglow electronically-excited N2(A , v) atom production in a capillary Generated by Repetitive NS Systems V. Bityurin, A. Bocharov, Russian with Significant Vibrational molecules in nitrogen discharge nanosecond discharge Dielectric Barrier Discharge J. Young, R. Sedwick, University Academy of Sciences, Moscow, Loading plasma A. Klochko, A. Salmon, École A. Starikovskiy, M. Shneider, of Maryland, College Park, College Russia D. Burnette, I. Shkurenkov, I. N. Popov, Moscow State University, Polytechnique, Paris, France; N. Popov, Princeton University, Princeton, NJ; Park, MD; S. Dumpala, K. Rajan, Adamovich, W. Lempert, Ohio State Moscow, Russia Moscow State University, Moscow, D. Marinov, S. Starikovskaya, École Iowa State University, Ames, IA University, Columbus, OH Russia; J. Booth, École Polytechnique, Polytechnique, Palaiseau, France Paris, France; M. Kushner, Z. Xiong, University of Michigan, Ann Arbor, Ann Arbor, MI; et al. Wednesday, 15 January 2014 275-SCS-3 Packaging & Deployment of Gossamer Systems Chesapeake Conf Rm 6 Chaired by: S. PELLEGRINO, California Institute of Technology and G. GRESCHIK, TentGuild Engineering Co 1400 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs No Presentations AIAA-2014-1035 AIAA-2014-1036 AIAA-2014-1037 AIAA-2014-1038 AIAA-2014-1039 Strain Energy Deployment Elastic Spiral Folding for Flat Self-Supporting Membrane Deployment mechanics Stepwise Deployment of of Telescope Outer Barrel Membrane Apertures Structures with Curved Creases of highly compacted thin Membrane Space Structures with Assemblies W. Reynolds, T. Murphey, Air Force for Smooth Packaging and membrane structures Rolled-up Booms: Experiments M. Silver, Lincoln Laboratory, Research Laboratory, Kirtland Deployment M. Arya, S. Pellegrino, California and Simulations Massachusetts Institute of AFB, NM N. Lee, S. Pellegrino, California Institute of Technology, Pasadena, CA N. Okuizumi, Japan Aerospace Technology, Lexington, MA; P. Institute of Technology, Pasadena, CA Exploration Agency (JAXA), Sagamihara, Warren, Physical Sciences, Inc., Japan; N. Katsumata, Muroran Institute Andover, MA of Technology, Muroran, Japan; M. Natori, H. Yamakawa, Waseda University, Shinjuku, Japan Wednesday, 15 January 2014 276-SD-11 Adaptive Aeroelastic Wing Shaping Control II Chesapeake Conf Rm C Chaired by: K. GRIFFIN, Southwest Research Institute and F. NITZSCHE, Carleton University 1400 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs No Presentations AIAA-2014-1040 AIAA-2014-1041 AIAA-2014-1042 AIAA-2014-1043 AIAA-2014-1044 Flight Dynamic Modeling and Aeroelastic Wing Shaping Optimal and Decentralized Lyapunov Stability Analysis of A Preliminary Study for Stability Analysis of Flexible Wing Control Subject to Actuation Controller Designs for an an Aeroleastic Torsion Model Optimal Longitudinal-Mode Generic Transport Aircraft Constraints Elastically Shaped Aircraft A. Ishihara, Carnegie Mellon Flight Control through N. Nguyen, NASA Ames Research S. Swei, N. Nguyen, NASA Ames W. Nobleheart, A. Chakravarthy, University, Moffett Field, CA; N. Distributed Aeroelastic Shaping

129 Center, Moffett Field, CA; E. Ting, Research Center, Moffett Field, CA Wichita State University, Wichita, Nguyen, NASA Ames Research C. Ippolito, NASA Ames Research Stinger Ghaffarian Technologies, Inc., KS; N. Nguyen, NASA Ames Research Center, Moffett Field, CA Center, Moffett Field, CA; E. Ting, Moffett Field, CA; D. Nguyen, University Center, Moffett Field, CA Stinger Ghaffarian Technologies, of California, Berkeley, Berkeley, CA; K. Inc., Moffett Field, CA; N. Nguyen, Trinh, Stinger Ghaffarian Technologies, NASA Ames Research Center, Moffett Inc., Moffett Field, CA Field, CA; K. Trinh, Stinger Ghaffarian Technologies, Inc., Moffett Field, CA Wednesday, 15 January 2014 277-SOF-3 Software Systems National Harbor Conf Rm 14 Chaired by: D. LAVALLEE, JHU/Applied Physics Laboratory and J. PARKER, NASA-Goddard Space Flight Center 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs AIAA-2014-1045 AIAA-2014-1046 AIAA-2014-1047 AIAA-2014-1048 AIAA-2014-1049 AIAA-2014-1050 AIAA-2014-1051 libm3l and lsipdx - Utilities for Situational and Terrain QuickSAT-ARLX: An Open Biometrics Based Identification Verification of Video Frame A Modular Software Platform A Proposed Approach for Use of Inter-Process Data Transfer Awareness and Warning Source Space Hypervisor and Authentication in Latency Telemetry for UAV for Unmanned Aerial Vehicle Assurance Cases in Certification and Synchronization System Implementation on A. Santangelo, sci_Zone, Rio Aerospace Applications Systems Using A Secondary Autopilot Systems of Airborne Software A. Jirasek, A. Rizzi, Royal Institute Android Smartphone for Rancho, NM S. Adhikari, N. Wheeler, Sysoft Optical Method G. Ward, G. Bakirtzis, R. Klenke, A. Bateman, J. Cooper, Barron of Technology (KTH), Stockholm, Manned Aviation Applications Corporation, Readington, NJ S. Siewert, M. Ahmad, Trellis Logic, Virginia Commonwealth University, Associates, Inc., Charlottesville, VA; Sweden D. Bershadsky, L. Dressel, E. LLC, Anchorage, AK; K. Yao, AAI Richmond, VA K. Wasson, J. Knight, Dependable Johnson, Georgia Institute of Corporation, Hunt Valley, MD Computing, Inc., Charlottesville, Technology, Atlanta, GA VA; M. DeVore, Barron Associates, Inc., Charlottesville, VA; A. Hocking, Dependable Computing, Inc., Charlottesville, VA Wednesday, 15 January 2014 278-STR-13 Shell Bucking-Charles Rankin Special Session II Chesapeake Conf Rm E Chaired by: M. HILBURGER, NASA-Langley Research Center and D. JEGLEY, NASA Langley Research Center 1400 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs No Presentations AIAA-2014-1052 AIAA-2014-1053 AIAA-2014-1055 AIAA-2014-1056 Buckling Testing and Analysis of Buckling Design and Analysis Static and Dynamic Tests of Structural Performance of Honeycomb Sandwich Panel Arc of a Payload Fairing 1/6th Composite Cylindrical Shells Advanced Composite Tow- Segments of a Full-Scale Fairing Cylindrical Arc-Segment Panel under Axial Compression Steered Shells With Cutouts Barrel: Comparison of In- and D. Kosareo, Vantage Partners, LLC, C. Bisagni, Technical University of K. Wu, B. Stanford, NASA Langley Out-of-Autoclave Facesheet Brook Park, OH; S. Oliver, NASA Milan, Milan, Italy Research Center, Hampton, VA; Configurations Marshall Space Flight Center, J. Turpin, Kansas Space Grant E. Pineda, D. Myers, NASA Glenn Huntsville, AL; B. Bednarcyk, E. Consortium, Wichita, KS; R. Martin, Research Center, Cleveland, OH; D. Pineda, NASA Glenn Research Center, NASA Langley Research Center, Kosareo, Vantage Partners, LLC, Brook Cleveland, OH Hampton, VA Park, OH; B. Zalewski, ZIN Technologies, Inc., Middleburg Heights, OH; S. Kellas, G. Dixon, NASA Langley Research Center, Hampton, VA; et al. Wednesday, 15 January 2014 279-STR-14 Advances in Fatigue Analysis Chesapeake Conf Rm B Chaired by: S. ENGELSTAD, Lockheed Martin Aeronautics and M. ENRIGHT, Southwest Research Institue 1400 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs No Presentations AIAA-2014-1057 AIAA-2014-1058 AIAA-2014-1059 AIAA-2014-1060 Experimental Evaluation of A New Ductility Criterion for A Continuum Damage and Stress Concentration Factor in

130 StRATUS Fatigue-Creep Life Prediction of Discrete Crack module for Sheet Metal with Permanent M. Falugi, Air Force Research High Temperature Components Fatigue Damage Prediction of Plastic Deformation Laboratory, Wright-Patterson AFB, OH S. Zhu, H. Huang, Y. Liu, L. He, D. Laminated Composite Structures W. Chan, K. Lawrence, M. Meng, University of Electronic Science X. Fang, N. Simon, J. Lua, Global Ramasamy, University of Texas, and Technology, Chengdu, China Engineering and Materials, Inc., Arlington, Arlington, TX Princeton, NJ Wednesday, 15 January 2014 280-STR-15 Advanced Structures Chesapeake Conf Rm F Chaired by: L. HARDAWAY, Ball Aerospace & Technologies Corporation and M. SCHULTZ, NASA Langley Research Center 1400 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs No Presentations AIAA-2014-1061 AIAA-2014-1062 AIAA-2014-1063 AIAA-2014-1064 Mechanical Behavior of Advanced Grid-Stiffened Evaluation of Initial Curvature Nonlinear Finite Element Composite Lattice Cylinders Composite Shells for Heavy- Effect on the Snap-through Analysis of a Composite Non- T. Aoki, T. Yokozeki, University of Tokyo, Lift Helicopter Blade Spars Load of Bi-stable Composites Cylindrical Pressurized Aircraft Tokyo, Japan; K. Terashima, T. Kamita, S. Narayanan Nampy, United J. Lee, J. Ryu, M. Cho, S. Kim, Fuselage Structure Japan Aerospace Exploration Agency Technologies Corporation, Chula K. Cho, Seoul National University, A. Przekop, Analytical Mechanics (JAXA), Tsukuba, Japan Vista, CA; E. Smith, C. Bakis, Seoul, South Korea Associates, Inc., Hampton, VA; H. Pennsylvania State University, Wu, P. Shaw, The Boeing Company, University Park, PA Seal Beach, CA Wednesday, 15 January 2014 281-TES-2 Advances in Renewable Energy and Efficiency Maryland Ballroom B Chaired by: B. SLOAN, Iowa State University and E. KHALIL, Cairo University 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs AIAA-2014-1065 AIAA-2014-1066 AIAA-2014-1067 AIAA-2014-1068 AIAA-2014-1069 AIAA-2014-1070 AIAA-2014-1071 Energy Efficient Designs of Strategic Roadmap for Water Green Engineering in Clean Role of Toluene on Flow Field Velocity Performance of Wind Turbine Thermochemical Low Carbon Buildings Energy Nexus Rooms and Surgical operating Hydrocarbon Formation at Measurement Around a Blades with Several Designs Characterization of Materials E. Khalil, Cairo University, Cairo, E. Khalil, Cairo University, Cairo, Theatres Thermal Stage of Claus Process Horizontal-Axis Wind Turbine R. Amano, A. Alsultan, A. Gupta, using a Novel Laser-Heating Egypt Egypt E. Khalil, Cairo University, Cairo, S. Ibrahim, University of Maryland, R. Amano, S. Shen, University of University of Wisconsin, Milwaukee, Technique Egypt College Park, College Park, MD; Wisconsin, Milwaukee, Milwaukee, WI Milwaukee, WI C. Presser, A. Nazarian, J. Conny, A. Al Shoaibi, Petroleum Institute, National Institute of Standards and Abu Dhabi, United Arab Emirates; Technology, Gaithersburg, MD A. Gupta, University of Maryland, College Park, College Park, MD Wednesday, 15 January 2014 282-TP-8 Cryogenics National Harbor Conf Rm 11 Chaired by: E. SILK, NASA-Goddard Space Flight Center and P. YEE, The Aerospace Corporation 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs Oral Presentation (Invited) AIAA-2014-1072 AIAA-2014-1073 AIAA-2014-1074 AIAA-2014-1075 Space Cryogenics Between 1 Modeling and Design of a Non- A Wide Temperature Range, Flow Visualization of Liquid Demonstration of a 10 K and 10 Kelvin Moving part 4He Superfluid Reliable, Compact Cryogenic Hydrogen Line Chill Down Tests Turbo-Brayton Cryocooler for E. Silk, NASA Goddard Space Flight Circulator for Cooling of Large Thermal Switch E. Rame, J. Hartwig, J. McQuillen, Space Applications Center, Greenbelt, MD Superconducting Magnets in W. Chen, D. Fogg, Creare, Inc., NASA Glenn Research Center, J. Breedlove, K. Cragin, M. Zagarola, Space Science Applications Hanover, NH Cleveland, OH Creare, Inc., Hanover, NH

131 A. Jahromi, F. Miller, University of Wisconsin, Madison, Madison, WI Wednesday, 15 January 2014 283-TP-9 Non-Equilibrium Flows II National Harbor Conf Rm 10 Chaired by: D. PYTEL, Lockheed Martin Space Systems and J. BATSON, Lockheed Martin Space Systems 1400 hrs 1430 hrs 1500 hrs 1530 hrs AIAA-2014-1076 AIAA-2014-1077 AIAA-2014-1078 AIAA-2014-1079 Comparison of Vibrational Hybrid Monte Carlo - generalized Three Dimensional Simulation Analysis of rovibrational Relaxation Modeling for Strongly polynomial chaos sampling of of Shock Layer Ionization for relaxation in nitrogen via Non-Equilibrium Flows quasi-classical trajectories for RAM-C II Flight Tests direct atomic simulation T. Deschenes, M. Braunstein, rapid nonequilibrium reacting S. Surzhikov, Russian Academy of P. Valentini, P. Norman, C. Zhang, Spectral Sciences, Inc., Burlington, flow simulations Sciences, Moscow, Russia T. Schwartzentruber, University MA; I. Boyd, University of Michigan, M. Kulakhmetov, A. Alexeenko, of Minnesota, Minneapolis, Ann Arbor, Ann Arbor, MI Purdue University, West Lafayette, IN Minneapolis, MN Wednesday, 15 January 2014 284-WE-10 Blade and Turbine Design II Woodrow Wilson B Chaired by: D. CAIRNS, Montana State University and R. DAMIANI, NREL 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2014-1080 AIAA-2014-1081 AIAA-2014-1082 AIAA-2014-1083 AIAA-2014-1084 AIAA-2014-1085 PIV-Based Analysis of 2D and 3D Cross-sectional Analysis Structural Optimization of Multi- Effects of Defects Part A: Effects of Defects: Part B—A An Experimental Investigation Flow Phenomena of Vertical Axis of Composite Beams with Megawatt, Offshore Vertical Axis Treatment of Manufacturing Comparison of Progressive on the Aeromechanics and Wind Turbine Aerodynamics Distributed Loads Wind Turbine Rotors Defects as Uncertainty Variables Damage Modeling of Fiberglass/ Near Wake Characteristics G. Tescione, D. Ragni, C. He, C. Simao W. Yu, Utah State University, M. Schelbergen, L. Bernhammer, in a Wind Blade Probabilistic Epoxy Composite Structures with of Dual-Rotor Wind Turbines Ferreira, G. van Bussel, Delft University Logan, UT C. Simao Ferreira, E. Ferede, Delft Design Framework Manufacturing Induced Flaws (DRWTs) of Technology, Delft, The Netherlands University of Technology, Delft, The T. Riddle, D. Cairns, J. Nelson, Montana J. Nelson, D. Cairns, T. Riddle, Montana A. Ozbay, W. Tian, H. Hu, Iowa State Netherlands State University, Bozeman, MT State University, Bozeman, MT University, Ames, IA Wednesday, 15 January 2014 285-WE-11 Wind Farm and Turbine-Wake Interaction II Woodrow Wilson C Chaired by: J. WHITE, Sandia National Laboratories and B. JAYARAMAN 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs AIAA-2014-1086 AIAA-2014-1087 AIAA-2014-1088 AIAA-2014-1089 AIAA-2014-1090 Wind Farm simulations using Sensitivity Analysis of Wind Scaled Wind Farm Technology Implementing the Dynamic Wake Wind Turbine Performance a Full Rotor Model for Wind Plant Performance to Key Facility Overview Meandering Model in the NWTC Losses in Array Operation as a Turbines Turbine Design Parameters: A J. Berg, J. Bryant, B. LeBlanc, D. Design Codes Function of Turbine Spacing and J. Sitaraman, D. Mavriplis, University Systems Engineering Approach Maniaci, B. Naughton, J. Paquette, Y. Hao, M. Lackner, University of Upstream Wake Number of Wyoming, Laramie, Laramie, K. Dykes, A. Ning, R. King, P. Graf, G. Sandia National Laboratories, Massachusetts, Amherst, Amherst, B. Ennis, Purdue University, West WY; E. Duque, Intelligent Light, Scott, P. Veers, National Renewable Albuquerque, NM; et al. MA; R. Keck, University of Oslo, Oslo, Lafayette, IN; D. Adams, Vanderbilt Rutherford, NJ Energy Laboratory, Golden, CO Norway; S. Lee, M. Churchfield, P. University, Nashville, TN; S. Fleeter, Moriarty, National Renewable Energy Purdue University, West Lafayette, IN Laboratory, Golden, CO Wednesday, 15 January 2014 286-NW-9 Wednesday Afternoon Networking Coffee Break Exhibit Hall 1500 - 1530 hrs Wednesday, 15 January 2014 287-LECT-7 von Karman Lecture: Space Transportation: Past, Present, and . . . ?? Potomac Ballroom C 1730 - 1830 hrs Antonio L. Elias Executive Vice President and Chief Technical Officer

132 Orbital Sciences Corporation Thursday Thursday, 16 January 2014 288-NW-10 Thursday Morning Networking Breakfast Exhibit Hall 0700 - 0800 hrs Thursday, 16 January 2014 289-SB-7 Thursday Morning Speakers’ Brieﬁng Session Rooms 0730 - 0800 hrs Thursday, 16 January 2014 290-PLNRY-4 Thursday Morning Keynote and Plenary Panel Potomac Ballroom A&B 0800 - 0930 hrs Keynote Talent, the Coin of the Realm C.D. Mote, Jr. President National Academy of Engineering

Plenary Panel: Future of Aerospace Education and Professional Development Moderator: Alton Romig, Vice President, Engineering and Advanced Systems, Chief Skunk, Lockheed Martin Aeronautics Panelists: Ed Hoffman Leland Nicolai David Radcliffe Kate Stambaugh Chief Knowledge Ofﬁcer and APPEL Director Emeritus Member Kamyar Haghighi Head of Engineering Education and Epistemology Space Systems Engineer NASA Lockheed Martin Aeronautics Professor of Engineering Education JHU/Applied Physics Laboratory Purdue University

Thursday, 16 January 2014 291-NW-11 Thursday Morning Networking Coffee Break Exhibit Hall 0930 - 1000 hrs Thursday, 16 January 2014 292-AFM-10 Planetary Reentry II National Harbor Conf Rm 13 133 Chaired by: S. KOMADINA, Northrop Grumman Aerospace Systems 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2014-1091 AIAA-2014-1092 AIAA-2014-1093 AIAA-2014-1094 AIAA-2014-1095 Trajectory and Thermal Analysis Supersonic Inflatable An Analytical Approach Mars Science Laboratory Asymmetrically Stacked for Disk-shaped Dust Particles Aerodynamic Decelerators for to Modeling Supersonic Aerodatabase Trajectory Tori Hypersonic Inflatable through a Shock Layer use on Sounding Rocket Payloads Retropropulsion Flow Field Reconstruction and Uncertainty Aerodynamic Decelerator Y. Toki, Y. Ogino, N. Ohnishi, K. M. Miller, B. Steinfeldt, R. Braun, Components Assessment Design Study for Mars Entry Sawada, Tohoku University, Sendai, Georgia Institute of Technology, C. Cordell, R. Braun, Georgia Institute P. Kutty, C. Karlgaard, Analytical B. Harper, R. Braun, Georgia Institute Japan Atlanta, GA of Technology, Atlanta, GA Mechanics Associates, Inc., of Technology, Atlanta, GA Hampton, VA Thursday, 16 January 2014 293-AMT-7 Advances in Coherent Anti-Stokes Raman Scattering and Other Spectroscopic Techniques Maryland Ballroom 1 Chaired by: S. NAIK, Purdue University and S. KEARNEY, Sandia National Laboratories 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2014-1096 AIAA-2014-1097 AIAA-2014-1098 AIAA-2014-1099 Oral Presentation (Invited) Development of Combined Pure-Rotational fs/ps CARS Dual-pump CARS of Air in a Application of a Two-color Kilohertz-rate Imaging of Dual-Pump Vibrational and Pure- Measurements of Temperature Heated Pressure Vessel up to Polarization Spectroscopy Chemical Species using Rotational Coherent Anti-Stokes and Concentration using a 55 Bar and 1300 K Technique for Detection of Ultrashort-Pulse Lasers.” Raman Scattering (DPVCARS and Second-Harmonic Bandwidth L. Cantu, E. Gallo, A. Cutler, George Carbon Monoxide W. Kulatilaka, S. Roy, Spectral PRCARS) System Compressed Probe Washington University, Newport A. Bhuiyan, A. Satija, R. Lucht, Energies, LLC, Dayton, OH; J. Gord, A. Satija, R. Lucht, Purdue University, S. Kearney, D. Scoglietti, Sandia News, VA; P. Danehy, NASA Langley Purdue University, West Lafayette, IN Air Force Research Laboratory, West Lafayette, IN National Laboratories, Albuquerque, NM Research Center, Hampton, VA Wright-Patterson AFB, OH Thursday, 16 January 2014 294-AMT-8 Velocimetry Maryland Ballroom 2 Chaired by: S. BERESH, Sandia National Laboratories and K. LOWE, Virginia Tech 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2014-1100 AIAA-2014-1101 AIAA-2014-1102 AIAA-2014-1103 AIAA-2014-1104 Jupiter and Saturn’s Unique Effects of Spatial Realignment An examination of MHz rate Spectral analysis of over- Time-Domain Cross-Correlation Flow Structures Extracted from in Stereo PIV Self-Calibration PIV in a heated supersonic jet expanded cold jets via Scan DGV (CCS-DGV) for Images by Using Optical Flow S. Beresh, Sandia National B. Brock, R. Haynes, B. Thurow, 3-component point Doppler Mean-Velocity Boundary Layer Method Laboratories, Albuquerque, NM; Auburn University, Auburn, AL; G. velocimetry Measurements T. Liu, Western Michigan University, B. Smith, Utah State University, Lyons, N. Murray, University of T. Ecker, D. Brooks, K. Lowe, W. Ng, D. Cadel, T. Ecker, T. Lowe, Virginia Kalamazoo, MI Logan, UT Mississippi, Oxford, Oxford, MS Virginia Polytechnic Institute and Polytechnic Institute and State State University, Blacksburg, VA University, Blacksburg, VA Thursday, 16 January 2014 295-APA-29 Airfoil/Wing/Configuration Aerodynamics Maryland Ballroom 5 Chaired by: K. LAFLIN, Cessna Aircraft Company 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2014-1105 AIAA-2014-1106 AIAA-2014-1107 AIAA-2014-1108 AIAA-2014-1109 Sweep effects on non-linear Aerodynamics and Flow A Numerical Study of the A Numerical Study of the Numerical Study of Transient Lifting Line Theory near Stall Physics of a NACA 4412 Airfoil Aerodynamics of Cessna 172 Unsteady Motion of a Wing Behavior of a NACA 0008 Airfoil S. Gallay, S. Ghasemi, E. in Dynamic Ground Effect Aircrafts in Echelon formation using N-Body Approximation Equipped with a Gurney Flap Laurendeau, École Polytechnique de Q. Qu, X. Jia, W. Wang, Beihang M. Gunasekaran, R. Mukherjee, V. Kumar, R. Mukherjee, Indian Using a Control-Volume Based Montréal, Montréal, Canada University, Beijing, China; R. Indian Institute of Technology Institute of Technology Madras, Finite-Element Collocated Scheme Agarwal, Washington University Madras, Chennai, India Chennai, India M. Khoshlessan, S. Karimian, M. Mani, in St. Louis, St. Louis, MO; P. Liu, Amirkabir University of Technology, 134 Beihang University, Beijing, China Tehran, Iran Thursday, 16 January 2014 296-APA-30 Innovative Aerodynamic Concept and Bio-inspired Designs Maryland Ballroom 4 Chaired by: K. VANDEN, USAF and C. SHENG, University of Toledo 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2014-1110 AIAA-2014-1111 AIAA-2014-1112 AIAA-2014-1113 AIAA-2014-1114 Investigation of Moving Development of Atmospheric Lift enhancement in formation Experimental Study on the A Quasi-Steady Model for the Surface Approach to Viscous Satellite Concept based on flying in ground effect over a Unsteady Aerodynamics of a Lift on a Hovering Flexible Drag Reduction Sailing wavy surface Robotic Hawkmoth Manduca Wing P. Sünder, S. Sartorius, Technical W. Engblom, Embry-Riddle C. Chabalko, B. Balachandran, sexta model C. Kang, University of Michigan, University of Munich, Munich, Aeronautical University, Daytona University of Maryland, College Park, J. Han, J. Chang, Korea Aerospace Ann Arbor, Ann Arbor, MI; W. Shyy, Germany Beach, FL College Park, MD University, Goyang, South Korea; Hong Kong University of Science J. Kim, J. Han, Korea Advanced and Technology, Clear Water Bay, Institute of Science and Technology, Hong Kong Daejeon, South Korea Thursday, 16 January 2014 297-APA-31 Wind Tunnel and Flight Test Aerodynamics Maryland Ballroom D Chaired by: A. MAJAMAKI, The Aerospace Corporation and C. BIDWELL, NASA Glenn Research Center 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2014-1115 AIAA-2014-1116 AIAA-2014-1117 AIAA-2014-1118 AIAA-2014-1119 NASA Orion Flush Air Data Quantification of the Error A Flight Test Technique for Precise Numerical Investigation of Dynamic Stability Testing of Sensing System Feasibility Induced at Air Data Sensors Angle-of-Attack Measurements Installation Effects in Open a Reentry Lifting Capsule in a Determination and due to Basket Engagement with Application to Laminar Flow Jet Wind Tunnel Airfoil Transonic Wind Tunnel Development during Aerial Refueling Control Flight Research Experiments S. Koga, A. Hidaka, R. Tagai, T. E. Artz, N. Dona, T. Yechout, U.S. Air J. Masud, O. Khan, Air University, A. Tucker, Air Force Research Laboratory, A. Sheikh-AlShabab, P. Tucker, Kimura, T. Yoshinaga, S. Nagai, Force Academy, Colorado Springs, CO Islamabad, Pakistan Wright-Patterson AFB, OH; W. Saric, H. University of Cambridge, Cambridge, Japan Aerospace Exploration Agency Reed, Texas A&M University, College United Kingdom (JAXA), Chofu, Japan; et al. Station, TX Thursday, 16 January 2014 298-AS-3 Biomimitic Adaptive Flying Structures Chesapeake Conf Rm D Chaired by: R. BARRETT-GONZALEZ, The University of Kansas and B. ARRITT, AFRL - Air Force Research Laboratory 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2014-1120 AIAA-2014-1121 AIAA-2014-1122 AIAA-2014-1123 Bat-Inspired Flapping Flight The Design of a Corrugated Structural Characterization of Inertial Effects Due to Passive P. Chen, S. Joshi, NextGen Skin for the FishBAC Compliant the Fish Bone Active Camber Wing Morphing in Ornithopters Aeronautics, Torrance, CA; S. Structure Morphing Airfoil A. Wissa, J. Hubbard, University Swartz, K. Breuer, Brown University, I. Dayyani, B. Woods, M. Friswell, B. Woods, M. Friswell, Swansea of Maryland, College Park, College Providence, RI; G. Reich, Air Force Swansea University, Swansea, University, Swansea, United Kingdom Park, MD; Y. Tummala, M. Frecker, Research Laboratory, Wright- United Kingdom Pennsylvania State University,

135 Patterson AFB, OH University Park, PA; M. Northrup, University of Maryland, College Park, College Park, MD Thursday, 16 January 2014 299-FD-35 Active and Passive Flow Control IV Azalea 2 Chaired by: D. WILLIAMS, Illinois Institute of Technology and S. ANDERS, NASA Langley Research Center 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2014-1124 AIAA-2014-1125 AIAA-2014-1126 AIAA-2014-1127 Interaction of a Finite Span Understanding Leading Edge Applications of String-type Pulsed dielectric barrier discharge Synthetic Jet near the Tip of a Stall Physics by Acoustic DBD Plasma Actuators for Flow for manipulation of turbulent Sweptback Wing Excitation Control in Turbomachineries flow downstream a backward- J. Vasile, M. Amitay, Rensselaer C. Bernardini, S. Benton, J. Bons, T. Segawa, T. Matsunuma, National facing-step Polytechnic Institute, Troy, NY Ohio State University, Columbus, OH Institute of Advanced Industrial N. Benard, P. Sujar-Garrido, K. Bayoda, Science and Technology, Tsukuba, J. Bonnet, E. Moreau, National Center Japan for Scientific Research (CNRS), Chasseneuil, France Thursday, 16 January 2014 300-FD-36 Applications of GPUs for CFD Azalea 3 Chaired by: H. LUO, North Carolina State University and R. AGARWAL, Washington University in St Louis 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2014-1128 AIAA-2014-1129 AIAA-2014-1130 AIAA-2014-1131 Numerical Simulations OpenACC-based GPU Performance Assessment of Directive-Based GPU of Newtonian and Non- Acceleration of a 3-D Multi-block LES Simulations Programming for Newtonian Fluids on GPU Unstructured Discontinuous using Directive-based GPU Computational Fluid Dynamics K. Jin, P. Vanka, University of Illinois, Galerkin Method Computation in a Cluster B. Pickering, C. Roy, Virginia Urbana-Champaign, Urbana, IL; R. Y. Xia, L. Luo, H. Luo, North Carolina Environment Polytechnic Institute and State Agarwal, Washington University in State University, Raleigh, NC L. Luo, J. Edwards, H. Luo, North University, Blacksburg, VA St. Louis, St. Louis, MO Carolina State University, Raleigh, NC Thursday, 16 January 2014 301-FD-37 Boundary Layer Transition National Harbor Conf Rm 3 Chaired by: R. RADESPIEL, Technische Universitat Braunschweig and M. MALIK, NASA-Langley Research Center 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2014-1132 AIAA-2014-1133 AIAA-2014-1134 AIAA-2014-1135 Nonlinear Development and Enhancement of a Correlation- DNS Study on Mechanism Predictions of Transition on a Secondary Instability of Traveling Based Transition Turbulence of Formation of Lambda Hovering Tilt-Rotor Blade Crossflow Vortices Model for Simulating Crossflow Rotational Core in Late M. Zhao, Z. Xiao, S. Fu, Tsinghua F. Li, M. Choudhari, NASA Langley Instability Boundary Layer Transition University, Beijing, China Research Center, Hampton, VA; L. J. Choi, O. Kwon, Korea Advanced Y. Yan, A. Kaur, C. Liu, University of Duan, National Institute of Aerospace, Institute of Science and Technology, Texas, Arlington, Arlington, TX Hampton, VA; C. Chang, NASA Langley Daejeon, South Korea

136 Research Center, Hampton, VA Thursday, 16 January 2014 302-FD-38 Shock Boundary Layer Interactions II Woodrow Wilson D Chaired by: D. GAITONDE, The Ohio State University and M. PARK, NASA-Langley Research Center 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2014-1136 AIAA-2014-1137 AIAA-2014-1138 AIAA-2014-1139 Shock Wave Laminar Numerical Prediction of Shock- Flow Separation Associated Inﬂuence of entropy layer on Boundary Layer Interaction Boundary Layer Interaction with 3-D Shock-Boundary the ﬂow over a wedge and a Over a Double Wedge in a between a Pair of Fins in Layer Interaction (SBLI) pair of wedges on the plate High Mach Number Flow Hypersonic Flow R. Morajkar, R. Klomparens, W. I. Egorov, V. Borovoy, N. M. Badr, D. Knight, Rutgers V. Bhagwandin, Army Research Eagle, J. Driscoll, M. Gamba, Palchekovskaya, A. Skuratov, I. University, New Brunswick, NJ Laboratory, Aberdeen Proving University of Michigan, Ann Arbor, Struminskaya, TsAGI, Zhukovsky, Russia Ground, MD Ann Arbor, MI Thursday, 16 January 2014 303-FD-39 Synthetic Jets Maryland Ballroom 6 Chaired by: E. WHALEN, Boeing Engineering Operations & Technology and C. MCGINLEY, NASA Langley Research Center 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2014-1140 AIAA-2014-1141 AIAA-2014-1142 AIAA-2014-1143 AIAA-2014-1144 Numerical Investigation Interaction of a Finite Span Phase-Averaging Methods for a The Time-Resolved Internal and Design, Modeling and Testing of Flow Structures and Synthetic Jet with a Laminar Naturally Oscillating Flow Field External Flow Field Properties of of Synthetic Jet Actuators for Interactions due to a Pitched Boundary Layer: Effect of Jet S. Gaertlein, R. Woszidlo, F. Ostermann, a Fluidic Oscillator MAV Flight Control Synthetic Jet in a Laminar Geometry and Orientation C. Nayeri, C. Paschereit, Technical F. Ostermann, R. Woszidlo, S. Gaertlein, S. Bhatt, V. Golubev, Y. Tang, Boundary Layer T. Van Buren, C. Leong, M. Amitay, University of Berlin, Berlin, Germany C. Nayeri, C. Paschereit, Technical Embry-Riddle Aeronautical University, J. Li, O. Sahni, Rensselaer Rensselaer Polytechnic Institute, Troy, NY University of Berlin, Berlin, Germany Daytona Beach, FL Polytechnic Institute, Troy, NY Thursday, 16 January 2014 304-GNC-17 Fault Detection, Isolation and Reconstruction National Harbor Conf Rm 8 Chaired by: F. MORA-CAMINO, ENAC and D. ALAZARD, Institut Supérieur de l’Aéronautique et de l’Espace 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2014-1145 AIAA-2014-1146 AIAA-2014-1147 AIAA-2014-1148 AIAA-2014-1149 Adaptive Hybrid Unscented MPC Based Handling Sensor Fault Detection and Fault Tolerant LPV Control of Reduced Order and Prioritized Kalman Filter for Aircraft Sensor Qualities Assessment for a Isolation for Redundant Air the GTM UAV with Dynamic Reference Governors for Limit Fault Detection, Isolation and Transportation Aircraft with Data Sensors Control Allocation Protection in Aircraft Gas Reconstruction Failed Actuators L. Van Eykeren, Q. Chu, Delft B. Vanek, T. Peni, Z. Szabo, J. Turbine Engines P. Lu, L. Van Eykeren, E. Van Kampen, L. Zhong, F. Mora-Camino, French University of Technology, Delft, The Bokor, Hungarian Academy of Y. Tian, I. Kolmanovsky, University of Q. Chu, Delft University of Technology, Civil Aviation University, Toulouse, Netherlands Sciences, Budapest, Hungary Michigan, Ann Arbor, Ann Arbor, MI Delft, The Netherlands; B. Yu, Concordia France University, Montréal, Canada Thursday, 16 January 2014 305-GT-7 Hypersonic Test techniques with an Emphasis on Heat Shield Ablation Maryland Ballroom 3 Chaired by: J. EVERHART, NASA-Langley Research Center and D. NOBLE, Georgia Institute of Technology 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2014-1150 AIAA-2014-1151 AIAA-2014-1152 AIAA-2014-1153 AIAA-2014-1154 Experiment Method of Remote Recession Sensing of Development of Naphthalene Detection of Nitrogen Flow Entry, Descent and Landing Lightweight Charring Ablators Ablative Heat Shield Materials PLIF for Visualizing Ablation Condensation in a Hypersonic Aerothermodynamics: H. Gao, China Academy of Aerospace M. Winter, University of Kentucky, Products from a Space Capsule Wind-Tunnel using a Static NASA Langley Experimental Aerodynamics, Beijing, China Lexington, Lexington, KY; M. Heat Shield Pressure Probe Capabilities and Contributions Stackpoole, NASA Ames Research C. Combs, N. Clemens, University of G. Grossir, P. Rambaud, von Kármán B. Hollis, K. Berger, S. Berry, G. Center, Moffett Field, CA; A. Nawaz, Texas, Austin, Austin, TX; P. Danehy, Institute for Fluid Dynamics, Rhode- Brauckmann, G. Buck, M. DiFulvio,

137 Sierra Lobo, Inc., Moffett Field, CA; NASA Langley Research Center, Saint-Genèse, Belgium NASA Langley Research Center, G. Gonzales, ERC, Inc., Moffett Field, Hampton, VA Hampton, VA; et al. CA; T. Ho, Santa Clara University, Moffett Field, CA Thursday, 16 January 2014 306-GTE-6 Engine Systems I Azalea 1 Chaired by: J. CONVERY, GE Aviation 1000 hrs 1030 hrs 1100 hrs AIAA-2014-1155 AIAA-2014-1156 AIAA-2014-1157 Evaluation of Coefficients of Evaluation of Ash Particle Synchrotron XRD Measurements Restitution Using High Speed Rebounds in a Simulated Gas of Thermal Barrier Coatings Particle Shadow Velocimetry Turbine Environment Subjected to Loads Representing with Application to Particle M. Lawrence, S. Whitaker, J. Bons, Operational Conditions of Separators for Gas Turbine Ohio State University, Columbus, OH Rotating Gas Turbine Blades Engines K. Knipe, A. Manero, S. Siddiqui, S. S. Whitaker, B. Peterson, J. Bons, Sofronsky, P. Fouquet, University of Ohio State University, Columbus, OH Central Florida, Orlando, FL; C. Meid, German Aerospace Center (DLR), Cologne, Germany; et al. Thursday, 16 January 2014 307-HSABP-4 CFD Analysis of Scramjets II Chesapeake Conf Rm 7 Chaired by: F. MALO-MOLINA, Air Force Reseach Laboratory and C. BRUNO, United Technologies Research Center 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2014-1158 AIAA-2014-1159 AIAA-2014-1160 AIAA-2014-1161 AIAA-2014-1162 Numerical Investigation of a Inlet Fuel Injection in a Mach 12 Evaluation of Mixing-Limited Large-Eddy Simulations The Response of the Supersonic Cavity Flameholder Shape-Transitioning Scramjet Quasi-Global Wind-US Model of a Dual-Mode Scramjet Supersonic Reacting D. Peterson, E. Hassan, Air Force J. Barth, V. Wheatley, M. Smart, for HIFire 2 Flowpath Combustor: Operating Point Mixing Layer to the Inflow Research Laboratory, Wright- University of Queensland, Brisbane, M. Borghi, W. Engblom, Embry- “A” of University of Virginia’s Fluctuations Patterson AFB, OH; S. Tuttle, Naval Australia Riddle Aeronautical University, Scramjet Experiments A. Tahsini, Aerospace Research Research Laboratory, Washington, Daytona Beach, FL; N. Georgiadis, W. Chan, University of Michigan, Institute, Tehran, Iran DC; M. Hagenmaier, C. Carter, Air NASA Glenn Research Center, Ann Arbor, Ann Arbor, MI; M. Ihme, Force Research Laboratory, Wright- Cleveland, OH Stanford University, Stanford, CA Patterson AFB, OH Thursday, 16 January 2014 308-IS-3 Applications of Unmanned Aerial Systems National Harbor Conf Rm 15 Chaired by: K. KOCHERSBERGER, Virginia Polytechnic Institute and State University 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2014-1163 AIAA-2014-1164 AIAA-2014-1165 AIAA-2014-1166 A control technique for Project FREDE as a Development of an Optionally 3-D Scene Understanding from automatic taxi in fixed wing Stratospheric Experiment Piloted Vehicle using a Image-based Reconstructions C. Zammit, D. Zammmit-Mangion, with Semi-Autonomus Control Humanoid Robot Using a Small Unmanned Aircraft University of Malta, Msida, Malta System H. Jeong, J. Kim, D. Shim, Korea G. Christie, L. Stiltner, K. Kroeger, K. J. Gorski, Wroclaw University of Advanced Institute of Science and Kochersberger, Virginia Polytechnic

138 Technology, Wroclaw, Poland Technology, Daejeon, South Korea Institute and State University, Blacksburg, VA Thursday, 16 January 2014 309-MAT-7 Multiscale Modeling of Materials I Chesapeake Conf Rm A Chaired by: S. WANTHAL, The Boeing Company; R. FERTIG, University of Wyoming and G. SEIDEL, Virginia Polytechnic Institute and State Universit 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2014-1167 AIAA-2014-1168 AIAA-2014-1169 AIAA-2014-1170 Validation of Computational Modeling and Effect of Fiber Volume Fraction On the Constitutive Relations Variational Asymptotic Experimental Characterization Variation Across Multiple for Damaged Elastoplastic Micromechanics Modeling of of Macroscale Piezoresistivity in Length Scales on Composite Materials Coupling Anisotropic Thermomechanical Behavior of Aligned Carbon Nanotube and Stress Variation: The Possibility Damage and Plasticity Materials Fuzzy Fiber Nanocomposites of Stochastic Multiscale L. Zhang, W. Yu, Utah State C. Teng, W. Yu, Utah State A. Chaurasia, X. Ren, Y. Li, E. Sengezer, Analysis University, Logan, UT University, Logan, UT J. Burton, G. Seidel, Virginia Polytechnic R. Fertig, E. Jensen, University of Institute and State University, Wyoming, Laramie, Laramie, WY Blacksburg, VA Thursday, 16 January 2014 310-MDO-7 Aerodynamic Optimization Chesapeake Conf Rm 4 Chaired by: T. TAKAHASHI, Santa Clara University and M. RUMPFKEIL, University of Dayton 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2014-1171 AIAA-2014-1172 AIAA-2014-1173 AIAA-2014-1174 Active Subspaces for Shape Four Suggestions for Better Automated Low-ﬁdelity A General Purpose Adjoint Optimization Parametric Geometries Model Selection for CFD- Formulation for Inviscid T. Lukaczyk, Stanford University, A. Sobester, University of based Aerodynamic Shape 2D/3D Fluid Dynamic Stanford, CA; P. Constantine, Southampton, Southampton, United Optimization Optimization Colorado School of Mines, Golden, Kingdom S. Koziel, L. Leifsson, Reykjavik G. Caramia, A. Dadone, Technical CO; F. Palacios, J. Alonso, Stanford University, Reykjavik, Iceland University of Bari, Bari, Italy University, Stanford, CA Thursday, 16 January 2014 311-NDA-7 Nondeterministic Methods Chesapeake Conf Rm 5 Chaired by: D. VILLANUEVA, Universal Technology Corp and J. MCFARLAND 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2014-1175 AIAA-2014-1176 AIAA-2014-1177 AIAA-2014-1178 A Dynamic Data Driven Approach Decomposed Multilevel Data Assimilation for Turbulent Computational Effort to Online Flight Envelope Optimization under Epistemic Flows vs. Accuracy Tradeoff in Updating for Self Aware Uncertainty H. Kato, Japan Aerospace Exploration Uncertainty Quantiﬁcation Aerospace Vehicles B. Nesbit, M. Rais-Rohani, S. Agency (JAXA), Chofu, Japan; S. J. Mullins, S. Mahadevan, Vanderbilt D. Allaire, M. Lecerf, K. Willcox, DorMohammadi, Mississippi State Obayashi, Tohoku University, Sendai, University, Nashville, TN Massachusetts Institute of Technology, University, Starkville, MS Japan Cambridge, MA; D. Kordonowy, Aurora

139 Flight Sciences, Cambridge, MA Thursday, 16 January 2014 312-PANEL-8 Small Satellite Technology and its Role in Education and Professional Development Panel Potomac Ballroom C 1000 - 1200 hrs Moderator: Simon “Pete” Worden, Center Director, NASA Ames Research Center Panelists: James Cutler Adarsh Deepak Garrett Skrobot Bruce Yost Assistant Professor CEO, Chairman Mission Manager, Launch Services Program Program Manager, Edison Small Spacecraft Flight Demonstration Program University of Michigan Science and Technology Corporation (STC), Taksha University NASA Kennedy Space Center NASA Ames Research Center

Thursday, 16 January 2014 313-PANEL-9 Green Engineering Demands on Workforce Development Woodrow Wilson A 1000 - 1230 hrs Moderator: Franz-Josef Kahlen, Associate Professor, Department of Mechanical Engineering, University of Cape Town Panelists: Shannon Flumerfelt Mike Bailey Clark Briggs Director and Professor Design Engineer Vice President, Aerospace & Defense Business Development Oakland University GE ATA Engineering, Inc. Thursday, 16 January 2014 314-PANEL-10 International Session - Status of Pressure Gain Combustion for Propulsion, Research & Applications II National Harbor Conf Rm 7 1000 - 1200 hrs Session Chairs: Dan Paxson, NASA Glenn Research Center, OH and Chris Brophy, Naval Postgraduate School, CA Sponsor: AIAA - Pressure Gain Combustion Working Group for Program Committee

Panelists: Sergey Frolov Jian-Ping Wang Ming-Hsun Wu Ratiba Zitoun Professor, Semenov Institute of Chemical Physics, Professor, Department of Mechanics and Aerospace Engineering Professor, Department of Mechanical Engineering Professor, University of Poitiers - CNRS - ENSMA Russian Academy of Sciences Peking University National Cheng Kung University France Moscow, Russian Federation Beijing, China Taiwan

Thursday, 16 January 2014 315-PC-18 Plasma-Assisted Combustion II Chesapeake Conf Rm G Chaired by: Y. IKEDA, Imagineering, Inc. 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2014-1179 AIAA-2014-1180 AIAA-2014-1181 AIAA-2014-1182 Time Dependent Ignition in Ethanol-Containing Hydrogen and Methane SI Engine with Repetitive NS Measurements of Species Mixtures after Nanosecond Plasma Assisted Ignition by Spark Plug Formation in Nanosecond- Discharge NS discharge behind Reﬂected S. Pancheshnyi, Paul Sabatier Pulsed Plasma Discharges in I. Kosarev, S. Kindusheva, N. Shock Wave University, Toulouse, France; A. C2H4/O2/Ar Mixtures Aleksandrov, Moscow Institute of A. Starikovskiy, Princeton University, Nikipelov, E. Anokhin, Moscow J. Lefkowitz, B. Windom, W. Physics and Technology, Moscow, Princeton, NJ Institute of Physics and Technology, MacDonald, S. Adams, Princeton Russia; A. Starikovskiy, Princeton Moscow, Russia; A. Starikovskiy, University, Princeton, NJ; T. Chen, University, Princeton, NJ Princeton University, Princeton, NJ

140 Princeton High School, Princeton, NJ; M. Uddi, Princeton University, Princeton, NJ; et al. Thursday, 16 January 2014 316-PC-19 Spray and Droplet Combustion II Chesapeake Conf Rm H Chaired by: K. MCMANUS, GE 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2014-1183 AIAA-2014-1184 AIAA-2014-1185 AIAA-2014-1186 AIAA-2014-1187 Exploration of Near-Field Plume A Parametric Investigation Numerical investigation of Large-eddy simulation study of Novel Concept for Gas Properties for Aerated-Liquid Jets of Gelled Propellant Spray primary air-blast atomization injector geometry on liquid jet Injection at Low Pressure in an Using X-Ray Radiography Characteristics Utilizing and modal analysis of flow in cross-flow and validation with Effervescent Atomizer K. Lin, Taitech, Inc., Beavercreek, OH; Impinging Jet Geometry instabilities experiments J. Masud, M. Ahmed, Air University, C. Carter, S. Smith, Air Force Research N. Rodrigues, P. Sojka, Purdue J. McCaslin, O. Desjardins, Cornell M. Owkes, Cornell University, Ithaca, Islamabad, Pakistan Laboratory, Wright-Patterson AFB, University, West Lafayette, IN University, Ithaca, NY NY; M. Pai, General Electric Company, OH; A. Kastengren, Argonne National Niskayuna, NY; O. Desjardins, Cornell Laboratory, Argonne, IL University, Ithaca, NY Thursday, 16 January 2014 317-PC-20 Turbulent Combustion Modeling III National Harbor Conf Rm 2 Chaired by: V. RAMAN, The University of Texas at Austin and J. O’CONNOR, Sandia National Laboratories 1000 hrs 1030 hrs 1100 hrs AIAA-2014-1188 AIAA-2014-1189 AIAA-2014-1190 Large Eddy Simulation Diffusion Flame LES Simulation Several Fundamental Issues of Supersonic Turbulent Using The Partially Stirred in Large Eddy Simulation Combustion with FMDF Reactor Reaction Rate Model of Supercritical Mixing and A. Irannejad, F. Jaberi, Michigan N. Salvador, National Institute for Space Combustion State University, East Lansing, MI; J. Research (INPE), São José dos Campos, H. Huo, X. Wang, V. Yang, Georgia Komperda, F. Mashayek, University Brazil; W. Dourado, M. Mendonca, Institute of Technology, Atlanta, GA of Illinois, Chicago, Chicago, IL Aeronautics and Space Institute (IAE), São José dos Campos, Brazil Thursday, 16 January 2014 318-PDL-10 Plasma Discharge Modeling Chesapeake Conf Rm 9 Chaired by: J. POGGIE, USAF AFRL/RBAC 1000 hrs 1030 hrs 1100 hrs AIAA-2014-1191 AIAA-2014-1192 AIAA-2014-1193 A Unified Hyperbolic Model for An Approximate Riemann Numerical Simulation of Two- Coupled Fluid Dynamics and Solver for Relativistic Two-fluid Dimensional Structure of Glow Electromagnetics in Aerospace Plasmadynamics Discharge considering kinetics Applications R. Thompson, A. Wilson, T. Moeller, D. Storozhev, S. Surzhikov, Russian R. Thompson, T. Moeller, A. Wilson, University of Tennessee Space Academy of Sciences, Moscow, University of Tennessee Space Institute, Tullahoma, TN; C. Merkle, Russia

141 Institute, Tullahoma, TN; C. Merkle, Purdue University, West Lafayette, IN Purdue University, West Lafayette, IN Thursday, 16 January 2014 319-SCS-4 Testing of Large, Ultra-Lightweight Spacecraft Chesapeake Conf Rm 6 1000 - 1230 hrs Moderator: Jeanette Domber, Principal Systems Engineer and MOIRE Program Manger, Ball Aerospace & Technologies, Corporation Panelists: Tom Murphey Richard Pappa Michael McEachen James Moore Chief Technology Ofﬁcer Senior Research Engineer BD/IRAD Lead - Deployables Division Vice President High Strain Dynamics NASA Langley Research Center ATK - Goleta ManTech (Nexolve)

Thursday, 16 January 2014 320-SD-12 Aircraft Design and Nonlinear Dynamics Chesapeake Conf Rm B Chaired by: V. WICKRAMASINGHE and D. HODGES, Georgia Institute of Technology 1000 hrs 1030 hrs 1100 hrs AIAA-2014-1194 AIAA-2014-1195 AIAA-2014-1196 Zero-Lift Drag Prediction A Flutter Analysis Procedure Aeroelastic Characteristic of an Including Aeroelastic Effects Applicable to Conceptual Airfoil Containing Laminated J. Camberos, R. Kolonay, F. Eastep, Design Composite Plate R. Taylor, Air Force Research R. Yurkovich, Self, St. Louis, MO R. Drazumeric, B. Gjerek, F. Kosel, Laboratory, Wright-Patterson AFB, OH University of Ljubljana, Ljubljana, Slovenia; P. Marzocca, Clarkson University, Potsdam, NY Thursday, 16 January 2014 321-SD-13 Limit Cycle Oscillations (LCO) & Aircraft Flutter Chesapeake Conf Rm C Chaired by: W. SMITH, Lockheed Martin Corporation and C. HEBERT, Sierra Nevada Corporation 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2014-1197 AIAA-2014-1198 AIAA-2014-1199 AIAA-2014-1200 Visualizing a Flutter Mechanism Adapted K-Method for A Physical Understanding Numerical Study of Effect as a Traveling Wave Through Frequency-Domain ASE Control of Joined Wing’s Limit of Control Surface on Wing Animation of Simulation Results Stability Margin Analysis Cycle Oscillations Driven Flutter in Transonic Flow for the Semi-Span Super-Sonic Z. Wang, P. Chen, ZONA Technology, by Structural Geometric K. Lai, X. Zhang, T. Kim, National Transport Wind-Tunnel Model Inc., Scottsdale, AZ Nonlinearities University of Singapore, Singapore, D. Christhilf, Analytical Mechanics R. Cavallaro, L. Demasi, San Diego Singapore Associates, Inc., Hampton, VA State University, San Diego, CA Thursday, 16 January 2014 322-STR-16 Composite Mechanics Under Dynamic Load Chesapeake Conf Rm E Chaired by: J. MIN, NASA Glenn Research Center and R. SULLIVAN, Mississippi State University 1000 hrs 1030 hrs 1100 hrs AIAA-2014-1201 AIAA-2014-1202 AIAA-2014-1203 Lack of statistical rigor Geometrically Nonlinear A Novel Structural Element in composite materials Stress Recovery in Composite Combining Load Carrying and experimentation and lessons Laminates Subjected to Energy Dissipation Capability learned from the science of Dynamic Loading S. Bland, R. Snyder, J. Kudva, medicine T. Hartman, Dassault Group, NextGen Aeronautics, Torrance, P. Gustafson, Western Michigan Providence, RI; M. Hyer, S. Case, CA; S. Barbarino, M. Pontecorvo, University, Kalamazoo, MI; J. Virginia Polytechnic Institute and F. Gandhi, Rensselaer Polytechnic 142 Jastifer, Saint Alphonsus Coughlin State University, Blacksburg, VA Institute, Troy, NY; et al. Foot & Ankle Clinic, Boise, IN; J. Kapenga, J. McKean, Western Michigan University, Kalamazoo, MI Thursday, 16 January 2014 323-STR-17 Load Analysis and Design Process Chesapeake Conf Rm F Chaired by: H. LEE, NASA-Johnson Space Center and S. CLAY, Air Force Reseach Laboratory 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2014-1204 AIAA-2014-1205 AIAA-2014-1206 AIAA-2014-1207 Flight Loads Monitoring of USFS Preliminary Wing Weight Flight Loads Spectra of Two The Use of Relational Design in Aerial Supervision Modules Estimation Under Probabilistic Business Jets Aircraft Product Development L. Kliment, K. Rokhsaz, A. Menon, Loads for a Transport Aircraft L. Kliment, K. Rokhsaz, A. Menon, M. Berceli, Gulfstream Aerospace Wichita State University, Wichita, KS; J. J. Corman, D. Rancourt, C. Lee, J. Nelson, B. Terning, E. Weinstein, Corporation, Savannah, GA Nelson, B. Terning, U.S. Forest Service D. Mavris, Georgia Institute of Wichita State University, Wichita, KS Washington Office West, Boise, ID; Technology, Atlanta, GA; T. Wilson, E. Weinstein, FAA William J. Hughes Airbus, Bristol, United Kingdom Technical Center, Atlantic City, NJ Thursday, 16 January 2014 324-TES-3 Applications of Nanomaterials for Energy Storage Maryland Ballroom A 1000 - 1230 hrs Chaired by: B. SLOAN, Iowa State University Batteries and supercapacitors are gaining considerable interest for energy storage applications in memory backup devices, electric vehicles, and emergency power supplies in rural as well as urban areas. The volumetric and gravimetric specific energy density of supercapacitors and batteries can be improved further by a choice of innovative nanomaterials and their modifications. The high surface area, selective prorosity, enhanced mechanical, thermal and electrical properties of nanomaterials provide considerable improvement in the efficiencies of the electrodes and electrolytes used in these storage devices. The present talk will provide an overview of the application of nanomaterials including carbon nanotubes, graphene as well as naturally occurring halloysite nanotubes for supercapacitors, batteries and hydrogen storage. The future prospects as well as limitations of the use of these nanomaterials for portable energy storage will be discussed.

Sivaram Arepalli National Institute of Aerospace, Hampton, VA Thursday, 16 January 2014 325-TP-10 Ablation I National Harbor Conf Rm 11 Chaired by: N. DOUGHERTY, ERC Incorporated and C. BOYACK, Raytheon Missile Systems 1000 hrs 1030 hrs 1100 hrs AIAA-2014-1208 AIAA-2014-1209 AIAA-2014-1210 Numerical and experimental Simulation of Flow-tube Effect of Microstructure on study of carbon fiber oxidation Oxidation on the Carbon Carbon-based Surface Ablators F. Panerai, A. Martin, University of Preform of PICA using DSMC Kentucky, Lexington, Lexington, KY; H. Weng, H. Zhang, A. Martin, S. Poovathingal, T. Schwartzentruber, N. Mansour, NASA Ames Research University of Kentucky, Lexington, University of Minnesota, Minneapolis, Center, Moffett Field, CA Lexington, KY Minneapolis, MN Thursday, 16 January 2014 143 326-TP-11 Direct Simulation Monte Carlo Methods II National Harbor Conf Rm 10 Chaired by: J. BATSON, Lockheed Martin Space Systems and D. PYTEL, Lockheed Martin Space Systems 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2014-1211 AIAA-2014-1212 AIAA-2014-1213 AIAA-2014-1214 Development of the Ellipsoidal Simulation of Radiation Development of DSMC Experimental and Statistical Bhatnagar-Gross- Generated by Chemical Chemistry Models for Nitrogen Computational Investigation Krook method for Hypersonic Reactions in Weakly Ionized Collisions Using Accurate of Rarefied Hypersonic Flows Shock Waves using DSMC Theoretical Calculations Aerodynamics V. Patil, D. Levin, Pennsylvania State T. Zhu, Z. Li, N. Parsons, D. Levin, N. Parsons, T. Zhu, D. Levin, A. van T. Ozawa, T. Suzuki, K. Fujita, University, University Park, PA Pennsylvania State University, Duin, Pennsylvania State University, Japan Aerospace Exploration Agency University Park, PA University Park, PA (JAXA), Chofu, Japan Thursday, 16 January 2014 327-WE-12 Wind Turbine Aeroelastics Woodrow Wilson B Chaired by: L. MANUEL, University of Texas at Austin 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2014-1215 AIAA-2014-1216 AIAA-2014-1217 AIAA-2014-1218 AIAA-2014-1219 On Modeling Coupled Computation of Two- Time-varying Flexible Airfoil Improved Power Coefficient of Flow-induced instability of Influences of Wind, Wave, dimensional Wind Turbine Airfoil Shape Effects on Flapping Horizontal Axis Wind Turbines wind turbine blades and Current Loads on an Characteristics Using Advanced Airfoil Power Extraction Using Optimized Lift Control P. Pourazarm, Y. Modarres-Sadeghi, M. Offshore Wind Turbine during Turbulence and Transition C. Hoke, J. Young, J. Lai, University J. Cooney, T. Williams, T. Corke, Lackner, University of Massachusetts, a Hurricane Modeling Methods and a GPU- of New South Wales at the University of Notre Dame, Notre Amherst, Amherst, MA E. Kim, L. Manuel, University of Accelerated Navier-Stokes Solver Australian Defence Force Academy, Dame, IN Texas, Austin, Austin, TX T. Reinhart, S. Medida, S. Thomas, J. Canberra, Australia Baeder, University of Maryland, College Park, College Park, MD Thursday, 16 January 2014 328-WE-13 Wind Turbine Loads, Dynamics, and Control II Woodrow Wilson C Chaired by: B. NAUGHTON, Sandia National Laboratories 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2014-1220 AIAA-2014-1221 AIAA-2014-1222 AIAA-2014-1223 AIAA-2014-1224 Gain Scheduled Active Power An Experimental Investigation Optimal control for load Investigation of the effect Nonlinear Legendre Spectral Control for Wind Turbines on Dynamic Wind Loads Acting alleviation in wind turbines of off-axis spar cap plies Finite Elements for Wind S. Wang, P. Seiler, University on a Wind Turbine Model in B. Van Parys, Swiss Federal Institute on damage equivalent Turbine Blade Dynamics of Minnesota, Minneapolis, Atomspheric Boundary Layer of Technology, Zürich, Switzerland; loads in wind turbines with Q. Wang, M. Sprague, J. Jonkman, Minneapolis, MN Winds B. Ng, Imperial College London, superelement blade definition National Renewable Energy W. Tian, A. Ozbay, H. Hu, Iowa State London, United Kingdom; P. Goulart, M. Gozcu, M. Olgun, A. Kayran, Laboratory, Golden, CO University, Ames, IA Swiss Federal Institute of Technology, Middle East Technical University, Zürich, Switzerland; R. Palacios, Ankara, Turkey Imperial College London, London, United Kingdom Thursday, 16 January 2014 329-LNCH-3 Aerospace Design and Structures Awards Lunch and Keynote Making a MUTT - Lessons from the X-56A Program Potomac Ballroom A&B 1200 - 1400 hrs Peter Flick Program Manager, X-56A Program, AFRL/RQ

Jeff Beranek Chief Engineer, X-56A Program, Lockheed Martin-Skunk Works

144 Thursday, 16 January 2014 330-SB-8 Thursday Afternoon Speakers’ Brieﬁng Session Rooms 1400 - 1430 hrs Thursday, 16 January 2014 331-AA-7 Jet Noise IV Chesapeake Conf Rm I Chaired by: D. SUTLIFF, NASA Glenn Research Center 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2014-1225 AIAA-2014-1226 AIAA-2014-1227 AIAA-2014-1228 AIAA-2014-1229 Investigation of acoustic Analysis of High Speed Jet Experimental Reynolds Stress Mach-number dependence Mach-number dependence waves emanated from a Flow Physics with Time- Spectra in Hot Supersonic of acoustic source properties of acoustic source properties supersonic jet using ultra-high Resolved PIV Round Jets in high speed jets -- Part I: in high speed jets -- Part II: speed whole-ﬁeld optical Z. Berger, M. Berry, P. Shea, M. D. Brooks, T. Ecker, K. Lowe, W. Ng, ensemble statistics of active event-based description measurements Glauser, Syracuse University, Virginia Polytechnic Institute and regions P. Kan, J. Lewalle, Z. Berger, P. Shea, W. Mitchell, A. Agrawal, University of Syracuse, NY; N. Jiang, S. Gogineni, State University, Blacksburg, VA J. Lewalle, P. Kan, Syracuse Syracuse University, Syracuse, NY; B. Alabama, Tuscaloosa, Tuscaloosa, AL Spectral Energies, LLC, Dayton, University, Syracuse, NY; S. Kiel, Air Force Research Laboratory, OH; et al. Gogineni, Spectral Energies, LLC, Wright-Patterson AFB, OH; S. Dayton, OH Gogineni, Spectral Energies, LLC, Dayton, OH; et al. Thursday, 16 January 2014 332-ABPSI-5 Educating Today’s and Tomorrow’s Propulsion Engineers National Harbor Conf Rm 4 1430 - 1730 hrs Chaired by: R. SCHARNHORST, Boeing Defense, Space & Security and E. LOTH, University of Virginia This will be a discussion about teaching current engineering students the fundamentals of propulsion. Panelists: Dr. Phil Ligrani Dr. Ramesh Agarwal Dr. William Anderson Dr. Eric Loth Oliver C. Parks Endowed Chair Director, Aerospace Research and Education Center Professor, School of Aeronautics and Astronautics Rolls Royce Professor, Mechanical and Aerospace Engineering Professor, Aerospace and Mechanical Engineering Washington University Director, Global Engineering Program University of Virginia St. Louis University Purdue University

Thursday, 16 January 2014 333-AFM-11 Planetary Reentry III National Harbor Conf Rm 8 Chaired by: C. COX, Air Force Reseach Laboratory and P. WILLIAMS-HAYES, NASA Dryden Flight Research Center 1430 hrs 1500 hrs 1530 hrs AIAA-2014-1230 AIAA-2014-1231 AIAA-2014-1232 A Plasma Aerocapture and RED-Data2 Commercial Reentry Optimization of a Martian Entry System for Manned Recorder: Size Reduction and Aero-Gravity Assist Missions and Planetary Deep Improved Electronics Design J. Knittel, M. Lewis, K. Yu, University Space Orbiters A. Sidor, R. Braun, Georgia Institute of of Maryland, College Park, College D. Kirtley, J. Slough, MSNW, LLC, Technology, Atlanta, GA; D. DePasquale, Park, MD Redmond, WA Terminal Velocity Aerospace, LLC, Washington, DC

145 Thursday, 16 January 2014 334-AMT-9 Surface Measurements Maryland Ballroom 1 Chaired by: T. IOPPOLO, Southern University and J. NAUGHTON, University of Wyoming 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2014-1233 AIAA-2014-1234 AIAA-2014-1235 AIAA-2014-1236 AIAA-2014-1237 Micro-scale Untethered Analysis of an Untethered Flow Testing of a MEMS Time-Resolved PSP Imaging Global Luminescent Oil-film Sensor for Temperature Micro-Photonic Wall Pressure Floating Element Shear Stress of Unsteady Shock-Wave Skin-Friction Meter Generalized Measurements Sensor Sensor Phenomena Using a High- to Three-Dimensional Geometry M. Manzo, T. Ioppolo, Southern M. Manzo, T. Ioppolo, Southern Z. Zhao, Tufts University, Medford, Speed Camera and Applied to FAITH Hill Methodist University, Dallas, TX Methodist University, Dallas, TX MA; J. Gallman, Spirit Aerosystems, D. Numata, K. Asai, Tohoku N. Husen, Purdue University, West Wichita, KS; K. Long, Aerospace University, Sendai, Japan Lafayette, IN; S. Woodiga, T. Computing, Inc., Mountain View, Liu, Western Michigan University, CA; R. White, Tufts University, Kalamazoo, MI; J. Sullivan, Purdue Medford, MA University, West Lafayette, IN Thursday, 16 January 2014 335-AMT-10/GT-8 Velocity and Other Measurements In Wind Tunnels Maryland Ballroom 2 Chaired by: K. KONTIS, University of Glasgow and J. WAGNER, Sandia National Laboratories 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs AIAA-2014-1238 AIAA-2014-1239 AIAA-2014-1240 AIAA-2014-1241 AIAA-2014-1242 AIAA-2014-1243 Deployment of Particle Image Development of Non-Intrusive Borescopic Laser Doppler Spatially-resolved TDLAS Evaluation of a Thermal-Tuft Implementation of a Laser Velocimetry into the Lockheed Velocity Measurement Velocimetry Probe measurements of temperature, Probe for Turbulent Separating Hygrometer in a Transonic K. O’Brien, S. Olcmen, University of Martin High Speed Wind Capabilities at AEDC Tunnel 9 H2O column density, and and Reattaching Flows Wind Tunnel Tunnel J. Brooks, A. Gupta, University of Alabama, Tuscaloosa, Tuscaloosa, AL velocity in a direct-connect Q. Schwaab, J. Weiss, École N. Galyen, M. Mills, D. Plemmons, S. Beresh, J. Wagner, B. Pruett, Maryland, College Park, College scramjet combustor Polytechnique de Montréal, Aerospace Testing Alliance, Arnold R. Spillers, Sandia National Park, MD; M. Smith, E. Marineau, I. Schultz, C. Goldenstein, J. Jeffries, Montréal, Canada AFB, TN Laboratories, Albuquerque, NM; M. Arnold Engineering Development R. Hanson, Stanford University, McWithey, J. Gary, Lockheed Martin Center, Silver Spring, MD Stanford, CA; R. Rockwell, C. Goyne, Corporation, Grand Prairie, TX; et al. University of Virginia, Charlottesville, Charlottesville, VA Thursday, 16 January 2014 336-APA-32 Active and Passive Flow Control V Maryland Ballroom A Chaired by: K. KARA, Khalifa University of Science, Technology & Research and B. CYBYK, JHU/Applied Physics Laboratory 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs AIAA-2014-1244 AIAA-2014-1245 AIAA-2014-1246 AIAA-2014-1247 AIAA-2014-1248 AIAA-2014-1249 Enhanced Aerodynamic Effect of Strouhal Number and A Novel Vortex Generator for Aerothermodynamics of LES Simulation of Forced High- Active Wave Cancelation using Performance of a Wind Reynolds Number on Flow Mitigation of Shock-Induced Lifting-Body Configuration in Speed Jet Plasma Actuators in Flight Turbine Airfoil Section using Control Authority of DBD Plasma Separation Hypersonic Flow with Aerodisk J. Kim, S. Kim, BOOLT Simulation C. Tropea, A. Kurz, S. Grundmann, Plasma Actuation Actuator on NACA0012 Airfoil P. Sharma, S. Ghosh, Indian Institute at Nose Technology, Seoul, South Korea; B. Simon, Technical University of 146 I. Brownstein, Brown University, T. Sulaiman, University of Tokyo, of Technology Madras, Chennai, S. Khurana, K. Suzuki, University of M. Samimy, Ohio State University, Darmstadt, Griesheim, Germany Providence, RI; C. Szlatenyi, Tokyo, Japan; H. Aono, Japan India Tokyo, Kashiwa, Japan Columbus, OH Navatek, Ltd., North Kingstown, Aerospace Exploration Agency (JAXA), RI; K. Breuer, Brown University, Sagamihara, Japan; S. Sekimoto, Providence, RI University of Tokyo, Tokyo, Japan; M. Anyoji, T. Nonomura, K. Fujii, Japan Aerospace Exploration Agency (JAXA), Sagamihara, Japan Thursday, 16 January 2014 337-APA-33 Aerodynamic-Structural Dynamics Interaction Maryland Ballroom D Chaired by: J. AZEVEDO 1430 hrs 1500 hrs 1530 hrs AIAA-2014-1250 AIAA-2014-1251 AIAA-2014-1252 Effects of aspect ratio on Coupled CFD/CSD Simulations Understanding Store Loads fluid-structure interactions in of Helicopter Rotors with a using DES and Strongly- membrane wings Free Wake Model Coupled Aeroelastic R. Bleischwitz, B. Ganapathisubramani, J. Ickes, J. Wang, Q. Zhao, C. Simulations R. De Kat, University of Southampton, Sheng, University of Toledo, Toledo, G. Barakos, University of Liverpool, Southampton, United Kingdom OH Liverpool, United Kingdom Thursday, 16 January 2014 338-APA-34 Characterization of the Physical Environments related to Space Launch System (SLS) (Invited) Maryland Ballroom 4 Chaired by: K. ABDOL-HAMID, NASA Langley Research Center and J. PINIER, NASA-Langley Research Center 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2014-1253 AIAA-2014-1254 AIAA-2014-1255 AIAA-2014-1256 AIAA-2014-1257 An Overview of the Space Launch System Ascent Space Launch System Base Aerodynamic Tests of the Overview of Space Launch Characterization of the Space Static Aerodynamics Database Heating Test: Sub-Scale Space Launch System for System Ascent Aerothermal Launch Vehicle Aerodynamic Development Rocket Engine/Motor Design, Database Development Environments Environments J. Pinier, D. Bennett, G. Erickson, N. Development and Performance V. Pritchett, M. Mayle, J. Blevins, C. Morris, NASA Marshall Space J. Blevins, NASA Marshall Space Flight Favaregh, H. Houlden, W. Tomek, Analysis NASA Marshall Space Flight Center, Flight Center, Houston, TX Center, Huntsville, AL; C. Kiris, NASA NASA Langley Research Center, M. Mehta, NASA Marshall Space Huntsville, AL; W. Crosby, D. Ames Research Center, Moffett Field, Hampton, VA; et al. Flight Center, Huntsville, AL; A. Purinton, Jacobs, Huntsville, AL CA; R. Rausch, D. Bennett, NASA Dufrene, CUBRC, Buffalo, NY; R. Langley Research Center, Hampton, VA Kirchner, Jacobs, Huntsville, AL Thursday, 16 January 2014 339-AS-4 Morphing Chesapeake Conf Rm D Chaired by: I. CHOPRA, University of Maryland and H. MONNER, DLR - German Aerospace Center 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2014-1258 AIAA-2014-1259 AIAA-2014-1260 AIAA-2014-1261 AIAA-2014-1262 Active use of elasticity concept Application of Active Camber Feasible Conceptual Design of Development and Wind Tunnel Design of a Morphing Wing Tip and adaptive structures Morphing Concept to a Morphing Structures Test of Variable Camber I. Chekkal, R. Cheung, C. Wales, G. Amiryants, TsAGI, Zhukovsky, Regional Aircraft R. De Breuker, N. Werter, Delft Morphing Wing J. Cooper, University of Bristol, Russia S. Ricci, A. De Gaspari, Technical University of Technology, Delft, T. Yokozeki, A. Sugiura, University Bristol, United Kingdom; N. Allen, University of Milan, Milan, Italy; A. The Netherlands; C. Beaverstock, of Tokyo, Tokyo, Japan; Y. Hirano, S. Lawson, Aircraft Research

147 Antunes, F. Odaguil, G. Rodrigues M. Friswell, Swansea University, Japan Aerospace Exploration Agency Association, Ltd., Bedford, United de Lima, Embraer, São José dos Swansea, United Kingdom (JAXA), Tokyo, Japan Kingdom; et al. Campos, Brazil Thursday, 16 January 2014 340-FD-40 Active and Passive Flow Control VI Chesapeake Conf Rm 8 Chaired by: S. BANE, Purdue University- Sch of Aero and Astro and D. SMITH, Air Force Office of Scientific Research AFOSR 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2014-1263 AIAA-2014-1264 AIAA-2014-1265 AIAA-2014-1266 AIAA-2014-1267 Lift and Drag Control of DBD Plasma Actuator Design A Study of Physics and Control Passive Control of Self-Induced Three-dimensional Instabilities NACA 23012 Airfoil Model by for Optimal Flow Control of a Flow over an Airfoil in Roll Oscillations Using Bleed in Vortex/Wall Interactions: Surface HF Plasma Actuator T. Williams, A. Jemcov, T. Corke, Fully-Reverse Condition T. Hu, Z. Wang, I. Gursul, University Linear Stability and Flow P. Kazansky, I. Moralev, A. Klimov, University of Notre Dame, Notre C. Clifford, A. Singhal, M. Samimy, of Bath, Bath, United Kingdom Control V. Bityurin, Russian Academy of Dame, IN Ohio State University, Columbus, OH S. Benton, J. Bons, Ohio State Sciences, Moscow, Russia University, Columbus, OH Thursday, 16 January 2014 341-FD-41 Applications of CFD II Maryland Ballroom 6 Chaired by: M. WEI, New Mexico State Universtiy and K. MOHSENI, University of Florida 1430 hrs 1500 hrs 1530 hrs AIAA-2014-1268 AIAA-2014-1269 AIAA-2014-1270 Coupled Fluid-Structure Extension of the -Re Model Hydrodynamic Forces γ θt Interaction Analysis of Solid for Prediction of Crossflow and Moments on Slender Rocket Motor with Flexible Transition Axisymmetric Bodies with Inhibitors C. Grabe, A. Krumbein, German Decks in Translation H. Yang, CFD Research Corporation Aerospace Center (DLR), Göttingen, C. Marshall, T. Jeans, G. Holloway, (CFDRC), Huntsville, AL; J. West, Germany University of New Brunswick, NASA Marshall Space Flight Center, Fredericton, Canada; G. Watt, Huntsville, AL Defense Research and Development Canada, Dartmouth, Canada Thursday, 16 January 2014 342-FD-42 Boundary Layer Stabilization and Natural Laminar Flow Woodrow Wilson D Chaired by: R. KIMMEL, USAF AFRL/VAAA 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2014-1271 AIAA-2014-1272 AIAA-2014-1273 AIAA-2014-1274 AIAA-2014-1275 Numerical and experimental Plasma-Based Flow Control Control of Transitional and Behavior of a NLF Airfoil in An assessment of Scale Effects studies of high-speed for Delay of Excrescence Turbulent Flows using Plasma Flight through Atmospheric on Boundary Layer Transition boundary-layer stability on a Generated Transition Driven Fluidic Devices Turbulence on Natural Laminar Flow sharp cone with localized wall D. Rizzetta, M. Visbal, Air Force P. Morgan, Ohio Aerospace Institute, A. Reeh, C. Tropea, Technical Nacelles heating or cooling Research Laboratory, Wright- Cleveland, OH; M. Visbal, Air University of Darmstadt, Darmstadt, B. Raghunathan, CD-adapco, 148 A. Fedorov, V. Soudakov, I. Egorov, Patterson AFB, OH Force Research Laboratory, Wright- Germany Melville, NY; S. Raghunathan, TsAGI, Zhukovsky, Russia; A. Patterson AFB, OH Queen’s University Belfast, Belfast, Sidorenko, Y. Gromyko, D. Bountin, United Kingdom; J. Wang, Kingston Russian Academy of Sciences, University, London, United Kingdom Novosibirsk, Russia; et al. Thursday, 16 January 2014 343-FD-43 Higher-Order Methods IV Azalea 1 Chaired by: X. GAO, Colorado State Univ and E. JOHNSEN, University of Michigan 1430 hrs 1500 hrs 1530 hrs AIAA-2014-1276 AIAA-2014-1277 AIAA-2014-1278 A Simple Method to Improve A fourth-order finite-volume A Comparison of Higher-Order the Accuracy of Advection method for compressible Shock Capturing Schemes in Discontinuous Galerkin Navier-Stokes equations with Within the LAVA CFD Solver Methods for Navier-Stokes adaptive mesh refinement C. Brehm, M. Barad, J. Housman, C. Simulations X. Gao, S. Guzik, Colorado State Kiris, NASA Ames Research Center, E. Johnsen, A. Nair, University of University, Fort Collins, CO; P. Moffett Field, CA Michigan, Ann Arbor, Ann Arbor, MI Colella, Lawrence Berkeley National Laboratory, Berkeley, CA Thursday, 16 January 2014 344-FD-44 Wing-Vortex Interactions Chesapeake Conf Rm 9 Chaired by: C. BARNES, AFRL/RBAC and D. GARMANN, Air Force Research Laboratory 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs AIAA-2014-1279 AIAA-2014-1280 AIAA-2014-1281 AIAA-2014-1282 AIAA-2014-1283 AIAA-2014-1284 Experimental Studies On Stereo PIV Measurements Investigation of aeroelastic Interaction of a streamwise- Experimental and Computational Experimental Study of Vortex The Effect Of Leading Edge of Low-Aspect-Ratio Low- effects in streamwise-oriented oriented vortex with a wing Investigation of the Flow through Dynamics during Blade-Vortex Tubercles On Laminar Reynolds-Number Wings with vortex/wing interactions D. Garmann, M. Visbal, Air Force an Oscillating-Wing Power Interactions Separation Bubble Sinusoidal Leading Edges C. Barnes, M. Visbal, R. Gordnier, Air Research Laboratory, Wright- Generator D. Peng, J. Gregory, Ohio State K. Natarajan, S. Sudhakar, S. for Improved Computational Force Research Laboratory, Wright- Patterson AFB, OH I. Fenercioglu, B. Zaloglu, Istanbul University, Columbus, OH Palpandian, National Aerospace Modeling Patterson AFB, OH Technical University, Istanbul, Turkey; J. Laboratories, Bangalore, India J. Melo De Sousa, Technical Young, M. Ashraf, J. Lai, University of University of Lisbon, Lisbon, Portugal New South Wales, Canberra, Australia; M. Platzer, AeroHydro Research & Technology Associates, Pebble Beach, CA Thursday, 16 January 2014 345-GEPC-4 Energy Efficiency for the Future USAF Transport Fleet Woodrow Wilson A Chaired by: G. DALE, Wright-Patterson Air Force Base 1430 hrs 1500 hrs 1600 hrs 1630 hrs 1700 hrs Oral Presentation (Invited) AIAA-2014-1285 AIAA-2014-1286 Oral Presentation (Invited) Oral Presentation (Invited) From Laboratory to Design of a Hybrid Wing Body for Fuel Efficient Air Mobility Revolutionary Configurations Hybrid Electric Distributed New Opportunities for Flightline: Case Studies of Operations at Transonic Flight Conditions for Energy Efficiency Propulsion Mission Analysis, Environmental Progression in Operationalizing Energy J. Hooker, Lockheed Martin Corporation, Marietta, GA S. Wakayama, The Boeing Company, Terminal Area Operations Aviation Efficient Technologies Huntington Beach, CA and Short Field Performance R. Kawai, D. Brown, The Boeing

149 D. Erbschloe, Air Force Air Mobility Methodology Development Company, Huntington Beach, CA Command, Scott AFB, IL B. Schiltgen, M. Green, Empirical Systems Aerospace, Inc., Pismo Beach, CA Thursday, 16 January 2014 346-GNC-19 Aerospace Robotics National Harbor Conf Rm 6 Chaired by: D. CHOUKROUN, TUD-Delft University of Technology and F. MORA-CAMINO, ENAC 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2014-1287 AIAA-2014-1288 AIAA-2014-1289 AIAA-2014-1290 AIAA-2014-1291 Lie groups approach to space Simple Adaptive Control Resource Aggregated Admissible Subspace TRajectory Optimal Airborne Trajectories robots kinematics modelling for Spacecraft Proximity Reconfigurable Control and Optimizer (ASTRO) for for Data Collected from J. Lisowski, Polish Academy of Sciences, Operations Risk-Allocative Path Planning for Autonomous Robot Operations Emplaced Ground Sensor Warsaw, Poland; T. Barcinski, West S. Ulrich, D. Hayhurst, A. Saenz On-orbit Servicing and Assembly on the Space Station Arrays Pomeranian University of Technology in Otero, D. Miller, Massachusetts of Satellites G. Chamitoff, A. Saenz Otero, J. Katz, N. Jodeh, T. Coon, T. Masternak, Szczecin, Szczecin, Poland; T. Rybus, K. Institute of Technology, Cambridge, C. Jewison, B. McCarthy, D. Sternberg, S. Ulrich, Massachusetts Institute of R. Cobb, J. Agte, Air Force Institute Seweryn, Polish Academy of Sciences, MA D. Strawser, C. Fang, Massachusetts Technology, Cambridge, MA of Technology, Wright-Patterson Warsaw, Poland Institute of Technology, Cambridge, MA AFB, OH Thursday, 16 January 2014 347-GNC-20 Aircraft Control and Guidance National Harbor Conf Rm 12 Chaired by: D. ALAZARD, Institut Supérieur de l’Aéronautique et de l’Espace and D. SAUSSIE, Ecole Polytechnique de Montreal 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2014-1292 AIAA-2014-1293 AIAA-2014-1294 AIAA-2014-1295 AIAA-2014-1296 Demonstration of the Optimal Autopilot for a Nonlinear Non- A Realistic Flight Path A Study on Input Design Lyapunov Characteristic Control Modification for 6-DOF Minimum Phase Tail-Controlled Parameterization for Method for Nonlinear Non- Exponent Maps for Multi-Body Control of a General Aviation Missile Calculation of Noise Minimal Minimum Phase Systems Space Systems Analysis Aircraft A. Siddarth, University of Washington, Trajectories using Bi-level T. Hironori, National Defense D. Pagnozzi, J. Biggs, University S. Reed, J. Steck, Wichita State Seattle, WA; F. Peter, F. Holzapfel, Optimal Control Academy, Yokosuka, Japan; Y. of Strathclyde, Glasgow, United University, Wichita, KS; N. Nguyen, Technical University of Munich, Munich, M. Richter, M. Bittner, R. Rieck, F. Miyazawa, Kyushu University, Kingdom NASA Ames Research Center, Moffett Germany; J. Valasek, Texas A&M Holzapfel, Technical University of Fukuoka, Japan Field, CA University, College Station, TX Munich, Garching, Germany Thursday, 16 January 2014 348-GNC-21 Aircraft Guidance, Navigation and Control III National Harbor Conf Rm 7 Chaired by: H. LIU, University of Toronto and O. TEKINALP, Middle East Technical University 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs AIAA-2014-1297 AIAA-2014-1298 AIAA-2014-1299 AIAA-2014-1300 AIAA-2014-1301 AIAA-2014-1302 Modified State Observer Based Nonlinear Helicopter and Ship Towards an Improved Metric An enhanced automatic taxi Simulation Analysis of a Design of a Full State SDRE Adaptation for a General Models for Predictive Control of Refinements to Monocular control algorithm for fixed Sensor Data Fusion for Close Tracking Controller for an Aviation Aircraft - Simulation of Ship Landing Operations Vision-aided Navigation wing aircraft Formation Flight Unmanned Aircraft and Flight Test T. Ngo, C. Sultan, Virginia Systems C. Zammit, D. Zammmit-Mangion, D. Löbl, F. Holzapfel, Technical O. Tekinalp, A. Prach, Middle East V. Subba Reddiar Pappu, J. Steck, Polytechnic Institute and State J. Langford, E. Johnson, Georgia University of Malta, Msida, Malta University of Munich, Munich, Technical University, Ankara, Turkey Wichita State University, Wichita, University, Blacksburg, VA Institute of Technology, Atlanta, GA Germany 150 KS; K. Rajagopal, S. Balakrishnan, Missouri University of Science and Technology, Rolla, MO Thursday, 16 January 2014 349-GNC-22 Spacecraft Attitude Control National Harbor Conf Rm 13 Chaired by: L. GIULICCHI, European Space Agency and S. STARIN, NASA-Goddard Space Flight Center 1430 hrs 1500 hrs 1530 hrs 1600 hrs AIAA-2014-1303 AIAA-2014-1304 AIAA-2014-1305 AIAA-2014-1306 Fault-tolerant Control of Jump Space-Based Large Spinning CMG Isolator Design with Satellite Payload Motion Linear Systems with Discrete Sensor Pointing and Control Consideration of Singularity Control for Remote Sensing Mode Observations and its Design and Its Application to Problem S. Chatterjee, H. Hablani, Indian Application to Spacecraft NASA’s SMAP Spacecraft Y. Cui, G. Zheng, Tsinghua University, Institute of Technology Bombay, Magnetic Attitude Control J. Liu, The Boeing Company, El Beijing, China Mumbai, India A. Sadon, Ben-Gurion University Segundo, CA of the Negev, Beer Sheva, Israel; D. Choukroun, Delft University of Technology, Delft, The Netherlands Thursday, 16 January 2014 350-GT-9 Test Facility and Systems Development II Maryland Ballroom 3 Chaired by: S. RYLE and J. WEISS, Ecole de Technologie Superieure 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs AIAA-2014-1307 AIAA-2014-1308 AIAA-2014-1309 AIAA-2014-1310 AIAA-2014-1311 AIAA-2014-1312 Design, Construction, and Development and High-Fidelity Model of An Investigation of a Spacecraft Development of a Dynamic Development of a Magnetic Validation of a New Wind Characterization of a Four Axis Transient Turbine Facility On-orbit Advanced Refueling Propulsion Test Apparatus Suspension and Balance Tunnel for the Study of Positioning System to Facilitate for Off-Design Aerothermal System M. Morris, L. Daniel, J. Jacob, A. System for Supersonic Wind Pressure-Driven Separating Low Reynolds Number Testing N. Silvernail, Embry-Riddle Aeronautical Arena, R. Gaeta, Oklahoma State Tunnels and Reattaching Flows Research S. Lavagnoli, V. Andreoli, V. Villace, University, Daytona Beach, FL; D. University, Stillwater, OK Y. Takagi, H. Sawada, S. Obayashi, A. Mohammed Taifour, Q. Schwaab, T. Linehan, M. Shields, K. Mohseni, G. Paniagua, von Kármán Institute Sathyanarayan, Duke University, Tohoku University, Sendai, Japan J. Pioton, J. Weiss, University of University of Florida, Gainesville, for Fluid Dynamics, Rhode-Saint- Durham, NC; S. Gangadharan, Embry- Québec, Montréal, Canada Gainesville, FL Genèse, Belgium Riddle Aeronautical University, Daytona Beach, FL Thursday, 16 January 2014 351-GTE-7 Engine Systems II Azalea 2 Chaired by: S. JAMES, Honeywell Inc. and C. CHUCK, Boeing Commercial Airplanes 1430 hrs 1500 hrs 1530 hrs AIAA-2014-1313 AIAA-2014-1314 AIAA-2014-1315 Engine-Integrated Solid Fluid Dynamics of an Inertial Low-Fuel Consumption Gas Oxide Fuel Cells for Efficient Particle Separator Turbine Engines for Extended- Electrical Power Generation D. Barone, E. Loth, University Range UAVs on Aircraft of Virginia, Charlottesville, R. Andriani, Technical University of D. Waters, C. Cadou, University of Charlottesville, VA; P. Snyder, Rolls- Milan, Milan, Italy; A. Ingenito, F.

151 Maryland, College Park, College Royce Group plc, Indianapolis, IN Gamma, A. Agresta, University of Park, MD Rome “La Sapienza”, Rome, Italy Thursday, 16 January 2014 352-HSABP-5 Pressure Gain Combustion II Chesapeake Conf Rm 7 Chaired by: D. PAXSON, NASA Glenn Research Center and G. PANIAGUA, von Karman Institute 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2014-1316 AIAA-2014-1317 AIAA-2014-1318 AIAA-2014-1319 AIAA-2014-1320 RDE Integration with T63 Study on a Rotary-Valved Experimental Study of Study on a Rotary-Valved Cell Width of Methane Air Turboshaft Engine Components Four-Cylinder Pulse Detonation High-Frequency Fluidic Valve Four-Cylinder Pulse Detonation Mixtures at Elevated Initial D. Welsh, P. King, Air Force Institute Rocket : Thrust Measurement Injectors for Detonation Engine Rocket: Six Degree-of- Pressure and Temperature of Technology, Wright-Patterson by Ground Test Applications Freedom Flight Measurement C. Stevens, J. Hoke, Innovative AFB, OH; F. Schauer, J. Hoke, Air T. Morozumi, R. Sakamoto, T. J. Peace, D. Joshi, F. Lu, University of K. Matsuoka, S. Takagi, J. Kasahara, Scientific Solutions, Inc., Dayton, Force Research Laboratory, Wright- Kashiwazaki, University of Tsukuba, Texas, Arlington, Arlington, TX Nagoya University, Nagoya, Japan; OH; F. Schauer, Air Force Research Patterson AFB, OH Tsukuba, Japan; J. Kasahara, K. T. Morozumi, T. Kashiwazaki, Y. Laboratory, Wright-Patterson AFB, OH Matsuoka, University of Nagoya, Fujiwara, University of Tsukuba, Nagoya, Japan; A. Matsuo, Keio Tsukuba, Japan; et al. University, Yokohama, Japan; et al. Thursday, 16 January 2014 353-IS-4 Intelligent Learning and Decision Making National Harbor Conf Rm 15 Chaired by: S. ADHIKARI, Sysoft 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs AIAA-2014-1321 AIAA-2014-1322 AIAA-2014-1323 AIAA-2014-1324 AIAA-2014-1325 AIAA-2014-1326 Knowledge elicitation and Prototyping and training of Memetic Engineering as a Collaborative Learning using A Framework for Behavior Cost-Strategy Recognition representation for module computer vision algorithms in a Basis for Learning in Robotic Fuzzy Logic (CLIFF): Part 1 Learning in Differential Games Method for Behavior Learning: based perceptual capabilities synthetic UAV mission test bed Communities S. Mitchell, K. Cohen, University of and Safe Strategies Two Players Learning onboard UAVs G. Hummel, D. Smirnov, University W. Truszkowski, NASA Goddard Cincinnati, Cincinnati, OH N. Satak, University of Florida, Simultaneously D. Smirnov, P. Stütz, University of of the German Federal Armed Forces, Space Flight Center, Greenbelt, MD; Shalimar, Shalimar, FL; J. Hurtado, N. Satak, University of Florida, the German Federal Armed Forces, Neubiberg, Germany; A. Kronenberg, C. Rouff, Near Infinity Corporation, Texas A&M University, College Shalimar, Shalimar, FL; J. Hurtado, Neubiberg, Germany Karlsruhe University of Applied Sciences, Annapolis Junction, MD; M. Station, TX Texas A&M University, College Karlsruhe, Germany; P. Stütz, University Akhavannik, Patent and Trademark Station, TX of the German Federal Armed Forces, Office, Alexandria, VA Neubiberg, Germany Thursday, 16 January 2014 354-MAT-8 Material Testing & Characterization Chesapeake Conf Rm B Chaired by: A. AVILA, Universidade Federal de Minas Gerais; D. POWELL, Southern Research Institute and R. NAIK, Pratt & Whitney 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2014-1327 AIAA-2014-1328 AIAA-2014-1329 AIAA-2014-1330 AIAA-2014-1331 Icephobic Coating Evaluation Time-Dependent Behavior Development of a Gigacycle Pileup Investigation on Work Design, Analysis, and On-Sun for Aerospace Application of High Strength Kevlar and Bending Fatigue Test Method Hardened Copper During Evaluation of Reflective Strips C. Laforte, C. Blackburn, J. Perron, Vectran Webbing G. Kurtz, O. Scott-Emuakpor, T. Sharp Tip Nanoindentation Under Controlled Buckling University of Québec, Saguenay, T. Jones, W. Doggett, NASA Langley George, J. Beck, Air Force Research J. Gale, A. Achuthan, Clarkson D. Jaworske, NASA Glenn Research

152 Canada; R. Aubert, Bell Helicopter Research Center, Hampton, VA Laboratory, Wright-Patterson AFB, OH University, Potsdam, NY Center, Cleveland, OH; E. Sechkar, Textron, Inc., Hurst, TX ZIN Technologies, Inc., Cleveland, OH; A. Colozza, Vantage Partners, LLC, Cleveland, OH Thursday, 16 January 2014 355-MAT-9 Multiscale Modeling of Materials II Chesapeake Conf Rm A Chaired by: G. SEIDEL, Virginia Polytechnic Institute and State Universit; R. FERTIG, University of Wyoming and S. WANTHAL, The Boeing Company 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2014-1332 AIAA-2014-1333 AIAA-2014-1334 AIAA-2014-1335 AIAA-2014-1336 Static and dynamic fracture Statistical Multiscale Modeling A Comprehensive Evaluation A Variational Asymptotic Coupled atomistic-continuum simulation using a novel of Bond Clusters in Smart of the Predictive Capabilities Method for Unit Cell simulations at finite temperature particle method with multi- Polymer using Coupled of Several Advanced Homogenization of using a three-layer-mesh body potentials Molecular Dynamics and Micromechanics Approaches Hyperelastic Heterogeneous bridging domain method (TBDM) H. Chen, Y. Liu, Arizona State Spring-Damper Model H. Sertse, L. Zhang, W. Yu, Z. Ye, Materials A. Sadeghirad, Global Engineering and University, Tempe, AZ J. Zhang, B. Koo, Y. Liu, A. Utah State University, Logan, UT L. Zhang, W. Yu, Utah State Materials, Inc., Princeton, NJ; F. Liu, Chattopadhyay, Arizona State University, Logan, UT University of Utah, Salt Lake City, Salt University, Tempe, AZ Lake City, UT Thursday, 16 January 2014 356-MDO-8 Optimization Applications Chesapeake Conf Rm 4 Chaired by: E. JOHNSON and R. KOLONAY, US Air Force Research Lab 1430 hrs 1500 hrs 1530 hrs 1600 hrs AIAA-2014-1337 AIAA-2014-1338 AIAA-2014-1339 AIAA-2014-1340 Optimum Design of a Fuel Effect of Aerodynamic Fuel Tank Baffle Optimisation Multiobjective Design Exploration Efficient Mid-Size Business Jet Modeling on Optimum Wing For Mechanical Damping of an Aero-Acoustic Rocket J. Lyddon, M. Nguyen, J. Kinematics for Hovering MAVs J. Hall, T. Rendall, C. Allen, Launch Site Design Problem with Quackenbush, T. Schadegg, T. Z. Yan, H. Taha, M. Hajj, Virginia University of Bristol, Bristol, United Evolutionary Computation and Takahashi, Arizona State University, Polytechnic Institute and State Kingdom Large Eddy Simulations Tempe, AZ University, Blacksburg, VA T. Tatsukawa, Japan Aerospace Exploration Agency (JAXA), Tokyo, Japan; Y. Nagata, Tokyo University of Science, Tokyo, Japan; T. Nonomura, A. Oyama, K. Fujii, Japan Aerospace Exploration Agency (JAXA), Tokyo, Japan; M. Yamamoto, Tokyo University of Science, Tokyo, Japan Thursday, 16 January 2014 357-MST-6 Modeling and Simulation of Uninhabited Aircraft Systems (UAS) National Harbor Conf Rm 14 Chaired by: D. KEATING, The Charles Stark Draper Laboratory, Inc. 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs AIAA-2014-1341 AIAA-2014-1342 AIAA-2014-1343 AIAA-2014-1344 AIAA-2014-1345 AIAA-2014-1346 Modeling and Simulation of Frequency-Domain System On the Viability of Energy Identification of Low Order Study of Target Centric Modeling and Simulation of

153 Autonomous Thermal Soaring Identification and Simulation Harvesting Piezoelectric Devices Equivalent Transfer Function Cyclic Pursuit for MAVs using Propeller Propulsion Model with Horizon Simulation of a Quadrotor Controller for Supplemental Power Model of Trex-700E Helicopter Hardware In Loop Simulator Using Wind Tunnel Framework W. Wei, N. Schwartz, K. Cohen, Generation in Uninhabited from Flight Test Data S. Daingade, A. Borkar, A. Sinha, H. A. kamal, A. Aly, A. Elshabka, Z. Li, E. Mehiel, California University of Cincinnati, Cincinnati, Aircraft Systems M. Mohajerani, Concordia Arya, Indian Institute of Technology Military Technical College, Cairo, Polytechnic State University, San Luis OH A. Feiguel, French Institute for Advanced University, Montréal, Canada; H. Bombay, Mumbai, India Egypt Obispo, CA Mechanics, Clermont-Ferrand, France; T. Bolandhemmat, MicroPilot, Inc., Ricks, K. McWilliams, T. Lacy, O. Myers, Stony Mountain, Canada; Y. Zhang, P. Donohoe, Mississippi State University, Concordia University, Montréal, Mississippi State, MS; et al. Canada; H. Loewen, MicroPilot, Inc., Stony Mountain, Canada Thursday, 16 January 2014 358-NDA-8 NASA Multidisciplinary UQ Challenge I Chesapeake Conf Rm 5 Chaired by: L. CRESPO, National Institute of Aerospace and S. KENNY, NASA Langley Research Center 1430 hrs 1500 hrs 1530 hrs 1600 hrs AIAA-2014-1347 AIAA-2014-1348 AIAA-2014-1349 AIAA-2014-1350 The NASA Langley A Probabilistic Approach to the A Hybrid Bayesian Solution Robust Decision Making Multidisciplinary Uncertainty NASA Langley Multidisciplinary to NASA Uncertainty Applied to the NASA Quantification Challenge Uncertainty Quantification Quantification Challenge Multidisciplinary Uncertainty L. Crespo, S. Kenny, D. Giesy, Challenge Problem A. Srivastava, A. Subramaniyan, Quantification Challenge NASA Langley Research Center, R. Ghanem, C. Thimissetti, I. Yadegar, General Electric Company, Problem Hampton, VA V. Kasharvazaddeh, University of Niskayuna, NY K. Van Buren, F. Hemez, Los Alamos Southern California, Los Angeles, CA; J. National Laboratory, Los Alamos, NM Red-Horse, Sandia National Laboratories, Albuquerque, NM; R. Moser, University of Texas, Austin, Austin, TX; et al. Thursday, 16 January 2014 359-PANEL-11 Future Aerospace Workforce Development and Education Panel Potomac Ballroom C 1430 - 1630 hrs Moderator: Vigor Yang, Chair, School of Aerospace Engineering, Georgia Institute of Technology Panelists: Jennifer Byrne Carole Hedden Jaime Peraire Darryll Pines Larry Schneider Vice President, Corporate Engineering & Technology Senior Editor H.N. Slater Professor and Department Head Dean of Engineering Vice President, Chief Project Engineer - 777 Program Lockheed Martin Corporation Aviation Week Department of Aeronautics and Astronautics University of Maryland Boeing Commercial Airplanes Massachusetts Institute of Technology

Thursday, 16 January 2014 360-PC-21/AMT-11 Combustion Diagnostics II Chesapeake Conf Rm G Chaired by: C. CADOU, University of Maryland and S. NAIK, Purdue University 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs AIAA-2014-1351 AIAA-2014-1352 AIAA-2014-1353 AIAA-2014-1354 AIAA-2014-1355 AIAA-2014-1356 Laser-induced breakdown O2 rotational temperature Advanced methods for High repetition rate two- Sooting Jet Diffusion Flame Development of a Mid-IR Laser spectroscopy measurements in measurements using 2+1 extracting flow and dimensional laser induced Thermometry at 5 kHz using Diagnostic for Combustion turbulent methane flames radar resonance-enhanced combustion physics from high incandescence studies in a Femtosecond Coherent Anti- Efficiency M. Kotzagianni, University of Patras, multiphoton ionization speed laser diagnostics C2H4/H2/N2 non-premixed Stokes Raman Scattering S. Wakefield, Air Force Institute of Patras, Greece; R. Yuan, E. Mastorakos, Y. Wu, Z. Zhang, University of A. Wickersham, X. Li, L. Ma, Virginia flame C. Fineman, R. Lucht, Purdue Technology, Wright-Patterson AFB, OH; University of Cambridge, Cambridge, Tennessee, Knoxville, Knoxville, TN Polytechnic Institute and State P. Venkateswaran, J. Michael, University, West Lafayette, IN B. Sell, F. Schauer, Air Force Research United Kingdom; S. Couris, University of University, Blacksburg, VA D. Diaz, T. Meyer, Iowa State Laboratory, Wright-Patterson AFB, OH; Patras, Patras, Greece University, Ames, IA M. Fotia, J. Hoke, Innovative Scientific Solutions, Inc., Dayton, OH 154 Thursday, 16 January 2014 361-PC-22 Plasma-Assisted Combustion III (Invited) Chesapeake Conf Rm H Chaired by: T. OMBRELLO, Air Force Research Laboratory and W. SUN, Georgia Institute of Technology 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs Oral Presentation (Invited) Oral Presentation (Invited) Oral Presentation (Invited) Oral Presentation (Invited) Oral Presentation (Invited) Oral Presentation (Invited) Experiments on Plasma- Laser fluorescence and Fundamental processes in Kinetics of ignition of heavy Plasma activated low Plasma-assisted stabilization of Assisted Combustion in scattering studies of plasma Plasma Assisted Combustion hydrocarbons by nonequilibrium temperature combustion lean flames using nanosecond Supersonic Airflow assisted combustion kinetics in A. Starikovskiy, Princeton University, plasmas of pulsed discharges at Y. Ju, W. Sun, J. Lefkowitz, Princeton discharges S. Leonov, Ohio State University, nsec pulsed plasmas Princeton, NJ low initial temperatures University, Princeton, NJ C. Laux, École Centrale de Paris, Columbus, OH W. Lempert, Ohio State University, S. Starikovskaya, École Polytechnique, Paris, France Columbus, OH Paris, France Thursday, 16 January 2014 362-PDL-11 Plasma Diagnostics Maryland Ballroom 5 Chaired by: I. ADAMOVICH, Ohio University 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2014-1357 AIAA-2014-1358 AIAA-2014-1359 AIAA-2014-1360 AIAA-2014-1361 Sodium Cluster Ion Thomson Scattering Studies in Femtosecond TALIF Imaging Absolute concentration Time-Resolved Measurements Recombination Rate He and He/H2 Nanosecond of Atomic Hydrogen in Pulsed, measurements of atomic of Temperature and Species Measurements by Radar Pulse Nonequilibrium Plasmas Non-Equilibrium Plasmas oxygen in a flame using radar Concentrations Distributions in REMPI A. Roettgen, I. Shkurenkov, I. J. Schmidt, W. Kulatilaka, S. Roy, REMPI Ar-Based Mixtures Excited by a J. Sawyer, Z. Zhang, University of Adamovich, W. Lempert, Ohio State Spectral Energies, LLC, Dayton, OH; T. Chng, R. Miles, Princeton Nanosecond Pulse Discharge Tennessee, Knoxville, Knoxville, TN University, Columbus, OH K. Frederickson, W. Lempert, Ohio University, Princeton, NJ Z. Yin, A. Pulcini, I. Adamovich, State University, Columbus, OH; J. W. Lempert, Ohio State University, Gord, Air Force Research Laboratory, Columbus, OH Wright-Patterson AFB, OH Thursday, 16 January 2014 363-SCS-5 Mechanics, Dynamics, & Control of Gossamer Systems Chesapeake Conf Rm 6 Chaired by: H. FANG 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs AIAA-2014-1362 AIAA-2014-1363 AIAA-2014-1364 AIAA-2014-1365 AIAA-2014-1366 AIAA-2014-1367 On the Existence and Effect of Boundary Conditions Multibody Dynamics for Impact Tearing Behavior of Initial Deformation Properties MOIRE Gossamer Space Characteristics of a Class of on Geometric Control for an Biologically Inspired Smart Thin Aluminum Foil of Solar Sail Membrane for Telescope - Membrane Analysis Inflatable Toroid Envelopes Inflatable Pathfinder System Space Structure K. Woo, Chungbuk University, Cheongju, Equivalent Stiffness W. Tandy, T. Copp, L. Campbell, G. Greschik, TentGuild Engineering J. Fulcher, S. Smith, University of T. Sinn, M. Vasile, University of South Korea; C. Jenkins, Montana State H. Furuya, A. Yamasaki, Y. Matsuo, R. Thompson, R. Schweickart, D. Company, Boulder, CO Kentucky, Lexington, Lexington, KY; Strathclyde, Glasgow, United University, Bozeman, MT Tokyo Institute of Technology, Waller, Ball Aerospace & Technologies J. Baker, University of Kentucky, Kingdom Yokohama, Japan Corporation, Boulder, CO Paducah, Paducah, KY Thursday, 16 January 2014 364-SD-14 Rotorcraft Chesapeake Conf Rm C Chaired by: A. DATTA, Science & Technology Corporation and P. FRIEDMANN, University of Michigan 1430 hrs 1500 hrs 1530 hrs 1600 hrs AIAA-2014-1368 AIAA-2014-1369 AIAA-2014-1370 AIAA-2014-1371 Passive Tailboom Vibration Interfacial Strain Energy Nonlinear Modeling and Aerodynamics-Structural Coupled Control Using Fluidic Flexible Dissipation of Hybrid Analysis of Wind Turbine Analysis of a Bearingless Rotor Matrix Composite (F2MC) Tubes Nanocomposite Beams Under Blades using a Flexible Multi-body model K. Miura, C. Rahn, E. Smith, Axial Strain Fields Y. Bichiou, A. Abdelkefi, M. Hajj, W. Eun, H. Ryu, S. Shin, Seoul National Pennsylvania State University, B. Glaz, J. Riddick, E. Habtour, H. Virginia Polytechnic Institute and University, Seoul, South Korea; Y. Kee, University Park, PA Kang, Army Research Laboratory, State University, Blacksburg, VA D. Kim, Korea Aerospace Research Aberdeen Proving Ground, MD Institute, Daejeon, South Korea 155 Thursday, 16 January 2014 365-STR-18 Special Session - Composite Laminate Optimization Chesapeake Conf Rm E Chaired by: M. RASSAIAN, Boeing Engineering Operations & Technology and A. BLOM, The Boeing Company 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs AIAA-2014-1372 AIAA-2014-1373 AIAA-2014-1374 AIAA-2014-1375 AIAA-2014-1376 AIAA-2014-1377 Combining Topology and Sensitivity Analysis of Out- On Further Developments of Comparison of Methodologies for Optimal Design of Hierarchical Analysis and Lamination Parameter of-Plane Composite Lamina Feasible Region of Lamination Optimal Design of a Composite Postbuckling Behaviour of Optimization of Nano-Enhanced Optimisation Properties Relative to Parameters for Symmetric Plate under Practical Design Laminated Composite Plates Composite Sandwich Plates D. Peeters, D. van Baalen, M. Configuration and Constitutive Composite Laminates Constraints using Lamination Parameters S. DorMohammadi, M. Rais-Rohani, Abdalla, Delft University of Properties G. Raju, Z. Wu, P. Weaver, University R. Taylor, Optimal Structures, Keller, Z. Wu, G. Raju, S. White, P. Weaver, Mississippi State University, Mississippi Technology, Delft, The Netherlands J. Weigand, S. TerMaath, University of of Bristol, Bristol, United Kingdom TX; M. Admani, Altair Engineering, Inc., University of Bristol, Bristol, United State, MS; M. Rouhi, Concordia Tennessee, Knoxville, Knoxville, TN Lewisville, TX; J. Strain, University of Kingdom University, Montréal, Canada Texas, Arlington, Arlington, TX Thursday, 16 January 2014 366-STR-19 Advances in Fracture Mechanics Chesapeake Conf Rm F Chaired by: I. RAJU, NASA-Langley Research Center and G. MABSON, Boeing Engineering Operations & Technology 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2014-1378 AIAA-2014-1379 AIAA-2014-1380 AIAA-2014-1381 AIAA-2014-1382 A Thermodynamically Interlaminar Fracture Crack Arrestment of Pi-Joined A Modified Interaction Integral Validation of Crack Growth Consistent Cohesive Zone Toughness Characterization Bonded Composites for 3D Extended Finite Analysis Technique for a Fiber Model for Mixed-Mode of Z-Pinned and Flocked J. Action, S. Engelstad, Lockheed Element based Crack Growth Metal Laminate Fracture Composite Laminates Martin Corporation, Marietta, GA Prediction D. Wieland, Southwest Research L. Zhang, W. Yu, Utah State V. Ranatunga, Miami University, N. Simon, M. Stuebner, X. Fang, Institute, San Antonio, TX; G. Abumeri, University, Logan, UT Middletown, OH; S. Clay, Air Force J. Lua, Global Engineering and AlphaSTAR Corporation, Long Beach, Research Laboratory, Wright- Materials, Inc., Princeton, NJ CA; A. McCloskey, Northrop Grumman Patterson AFB, OH Corporation, El Segundo, CA Thursday, 16 January 2014 367-TES-4 Advances in Combustion I Maryland Ballroom B Chaired by: B. SLOAN, Iowa State University 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2014-1383 AIAA-2014-1384 AIAA-2014-1385 AIAA-2014-1386 AIAA-2014-1387 Swirl and Lateral Jet Injection Effect of Multi-Tube Fuel Updates to Simulation of a Shear Flow and Central Acoustic Streaming Effects in for Mixing and Combustion Injector Design on Flame Single-Element Lean-Direct Recirculation Zone Interaction High Intensity Swirl Burners Efficiency Stability and NOx Pollutant Injection Combustor Using a in Reactive Swirling Flows N. Syred, J. Lewis, A. Valera Medina, D. Lilley, Lilley & Associates, Emissions from Syngas Flames Polyhedral Mesh Derived from N. Syred, A. Valera Medina, P. P. Bowen, Cardiff University, Cardiff, Stillwater, OK S. Sarker, S. Hossain, S. Maldonado, Hanging-Node Elements Bowen, R. Marsh, Cardiff University, United Kingdom N. Love, A. Choudhuri, University of C. Wey, N. Liu, NASA Glenn Research Cardiff, United Kingdom Texas, El Paso, El Paso, TX Center, Cleveland, OH Thursday, 16 January 2014 368-TP-12 Ablation II National Harbor Conf Rm 11 Chaired by: D. KUNTZ, Sandia National Laboratories and A. MARTIN, University of Kentucky 1430 hrs 1500 hrs 1530 hrs AIAA-2014-1388 Oral Presentation (Invited) AIAA-2014-1389 Measurement of pyrolysis Model and analysis of gas flow Measurement of Tube Wall products from phenolic polymer and heat transport in porous Ablation in Hypervelocity thermal decomposition IsoQ arc-jet samples Flows H. Wong, J. Peck, R. Edwards, Aerodyne I. Cozmuta, Science and Technology M. Hildebrand, J. Huneault, Research, Inc., Billerica, MA; G. Reinisch, Corporation, Moffett Field, CA; J. J. Loiseau, A. Higgins, McGill University of Texas, Austin, Austin, TX; J. Lachaud, University of California, University, Montréal, Canada Lachaud, University of California, Santa Santa Cruz, Moffett Field, CA

156 Cruz, Moffett Field, CA; N. Mansour, NASA Ames Research Center, Moffett Field, CA Thursday, 16 January 2014 369-TP-13 Aerothermodynamics II National Harbor Conf Rm 10 Chaired by: R. AMANO, University of Wisconsin and M. HOWARD, Sandia National Laboratories 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2014-1390 AIAA-2014-1391 AIAA-2014-1392 AIAA-2014-1393 AIAA-2014-1394 Numerical Analysis on Assessment of Residual Numerical Investigations Approximate Prediction for Integrated Fluid-Thermal- Aerothermodynamic Distribution Method Heat of Thermal Loss effects on Aerodynamic Heating and Structural Analysis for Characteristics of Blunt-nosed Flux Prediction Capabilities: Thermoacoustic Instabilities in Design for Leading-edge Predicting Aerothermal Cone in Free-piston Shock Application to Atmospheric Entry a model Combustor Bluntness on Hypersonic Environment of Hypersonic Tunnel HIEST Problems A. Filosa, B. Noll, R. Lückerat, Vehicles Vehicles T. Ishihara, Y. Ogino, N. Ohnishi, K. H. Deconinck, J. Garicano Mena, A. Lani, German Aerospace Center (DLR), G. Yang, Y. Duan, C. Liu, J. S. Zhang, F. Chen, H. Liu, Shanghai Sawada, Tohoku University, Sendai, von Kármán Institute for Fluid Dynamics, Stuttgart, Germany Cai, Northwestern Polytechnical Jiao Tong University, Shanghai, China Japan; H. Tanno, Japan Aerospace Rhode-Saint-Genèse, Belgium; R. Pepe, University, Xi’an, China Exploration Agency (JAXA), Kakuda, Università degli studi della Basilicata Japan Viale dell, Potenza, Italy Thursday, 16 January 2014 370-WE-14 Wind Turbine Monitoring and Performance Woodrow Wilson C Chaired by: P. SEILER, University of Minnesota 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs AIAA-2014-1395 AIAA-2014-1396 AIAA-2014-1397 AIAA-2014-1398 AIAA-2014-1399 AIAA-2014-1400 Wireless Structural Health Wind Turbine Rotor Blade Employing Wind Farm Exploration of Modal FENSAP-ICE Simulation of Characterizing the effects of Monitoring of Wind Turbine Monitoring using Digital Image Performance Data for Model Decomposition Techniques for Complex Wind Turbine Icing inﬂow on a 2.5 MW research Blades Using an Energy Correlation: Assessment on a Validation and Turbine Layout/ Wind Turbines Events, and Comparison to utility turbine Harvester as a Sensor Scaled Model Geometry Optimization A. Mittal, K. Sreenivas, L. Observed Performance Data K. Howard, M. Guala, University D. Lim, S. Mantell, P. Seiler, J. Winstroth, J. Seume, Leibniz B. DuPont, Oregon State University, Taylor, University of Tennessee, D. Switchenko, W. Habashi, of Minnesota, Minneapolis, University of Minnesota, University of Hannover, Hannover, Corvallis, OR; J. Cagan, Carnegie Chattanooga, Chattanooga, TN McGill University, Montréal, Minneapolis, MN Minneapolis, Minneapolis, MN Germany Mellon University, Pittsburgh, PA Canada; T. Reid, I. Ozcer, G. Baruzzi, Newmerical Technologies International, Montréal, Canada Thursday, 16 January 2014 371-NW-12 Thursday Afternoon Networking Coffee Break Foyer 1530 - 1600 hrs Thursday, 16 January 2014 372-LECT-8 SDM Special Session: Damping: The Turbulence of Structural Mechanics Maryland Ballroom C 1800 - 1900 hrs George Lesieutre Professor and Department Head, Department of Aerospace Engineering

157 Pennsylvania State University Friday Friday, 17 January 2014 373-NW-13 Friday Morning Networking Coffee Break Foyer 0700 - 0730 hrs Friday, 17 January 2014 374-SB-9 Friday Morning Speakers’ Briefing Session Rooms 0730 - 0800 hrs Friday, 17 January 2014 375-AA-8 Computational Aeroacoustics Maryland Ballroom D Chaired by: V. GOLUBEV, Embry-Riddle Aeronautical University (ERAU) 0800 hrs 0830 hrs 0900 hrs 0930 hrs 1000 hrs 1030 hrs AIAA-2014-1401 AIAA-2014-1402 AIAA-2014-1403 AIAA-2014-1404 AIAA-2014-1405 AIAA-2014-1406 Digital Filter-based Turbulent Numerical simulation of the Near-Field and Far-Field Acoustics propagation and Comparison of Computational Pressure Loading Within Inflow Generation for Jet effect of a low bypass cooling Spectral Analysis of Supersonic wave interference by scalar Aeroacoustics Prediction of Rectangular Cavities With and Aeroacoustics on Non-Uniform stream on supersonic jet noise Jet with and without Fluidic wave equation Acoustic Transmission Through Without a Captive Store Structured Grids Y. Du, P. Morris, Pennsylvania State Injection J. Shang, Wright State University, a Three Dimensional Stator M. Barone, S. Arunajatesan, Sandia N. Dhamankar, Purdue University, University, University Park, PA H. Hafsteinsson, L. Eriksson, N. Dayton, OH Geometry with Experiment National Laboratories, Albuquerque, NM West Lafayette, IN; C. Martha, Intel Andersson, Chalmers University of D. Hixon, University of Toledo, Corporation, Santa Clara, CA; Y. Technology, Göteborg, Sweden; D. Toledo, OH; E. Envia, M. Dahl, D. Situ, K. Aikens, G. Blaisdell, Purdue Cuppoletti, E. Gutmark, University of Sutliff, NASA Glenn Research Center, University, West Lafayette, IN; A. Cincinnati, Cincinnati, OH; E. Prisell, Cleveland, OH Lyrintzis, Embry-Riddle Aeronautical FMV, Stockholm, Sweden University, Daytona Beach, FL; et al. Friday, 17 January 2014 376-AMT-12/GT-10 Pressure and Temperature Measurements in Wind Tunnels Maryland Ballroom 2 Chaired by: M. WRENN, Aerospace Testing Alliance (ATA) and D. PLEMMONS, Aerospace Testing Alliance (ATA) 0800 hrs 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs No Presentations AIAA-2014-1407 AIAA-2014-1408 AIAA-2014-1409 AIAA-2014-1410 AIAA-2014-1411 AIAA-2014-1412 Global Pressure and Development of Temperature- Translational Temperature Design of Static Pressure Quantitative Boundary-Layer Automatic Data Processing Temperature Measurements of Sensitive Paint with Measurements in Shock Layer Probes for Improved Free- Transition Measurements Using of Pressure-Sensitive Paint Ballistic-Range Testing by PSP High Performance and by Point-measurement Laser Stream Characterization in IR Thermography Measurement in a Wind Tunnel and TSP Techniques Responsibility for Aerodynamic Absorption Spectroscopy Hypersonic Wind-Tunnels B. Crawford, G. Duncan, D. West, W. M. Kurita, K. Nakakita, K. Mitsuo, H. Sakaue, Y. Iijima, Japan Heating Measurement S. Nomura, Japan Aerospace Exploration G. Grossir, S. Paris, P. Rambaud, von Saric, Texas A&M University, College Japan Aerospace Exploration Agency Aerospace Exploration Agency T. Horagiri, H. Nagai, Tohoku Agency (JAXA), Chofu, Japan; G. Ito, Kármán Institute for Fluid Dynamics, Station, TX (JAXA), Chofu, Japan; H. Yamaya, T. (JAXA), Chofu, Japan; Y. Yamada, University, Sendai, Japan University of Tokyo, Kashiwa, Japan; Rhode-Saint-Genèse, Belgium; B. Van Nakajima, IHI Corporation, Tomioka, T. Miyazaki, University of Electro- K. Fujita, Japan Aerospace Exploration Hove, Royal Observatory of Belgium, Japan Communications, Chofu, Japan; M. Agency (JAXA), Chofu, Japan; K. Brussels, Belgium Ishii, National Research Institute of Komurasaki, University of Tokyo, Police Science, Kashiwa, Japan Kashiwa, Japan Friday, 17 January 2014 377-AS-5 Modeling Simulation Chesapeake Conf Rm D Chaired by: W. YU, Purdue University and R. BOTEZ, Ecole de Technologie Superieure 0800 hrs 0830 hrs 0900 hrs 0930 hrs 1000 hrs AIAA-2014-1413 AIAA-2014-1414 AIAA-2014-1415 AIAA-2014-1416 AIAA-2014-1417 Simultaneous Optimum Design A Process Chain for Structural Connectivity of Shape Memory Cross-sectional modelling of an Shape Memory Alloy Actuated of Structure and Actuator Optimization of a Smart Droop Alloy-based Self-Folding initially curved and pre-twisted Morphing Cellular Frame using Locations for Plate Model of Nose for an Active Blown High Structures smart beam Bi-stable von-Mises Trusses 158 High Precision Space Antenna Lift System E. Peraza Hernandez, D. Hartl, V. Valliappan, D. Harursampath, Indian with Variable Length Links Y. Satou, H. Furuya, Tokyo Institute A. Rudenko, H. Monner, M. Rose, E. Akleman, K. Frei, Texas A&M Institute of Science, Bangalore, India; S. S. Barbarino, F. Gandhi, Rensselaer of Technology, Yokohama, Japan; N. German Aerospace Center (DLR), University, College Station, TX Roy, Indian Institute of Technology Dehli, Polytechnic Institute, Troy, NY Kogiso, Osaka Prefecture University, Braunschweig, Germany Delhi, India; W. Yu, Purdue University, Sakai, Japan West Lafayette, IN Friday, 17 January 2014 378-ASE-2 Topics in Space Environments Chesapeake Conf Rm 9 Chaired by: N. GREEN, Jet Propulsion Laboratory and E. BERING, University of Houston 0800 hrs 0830 hrs 0900 hrs 0930 hrs 1000 hrs AIAA-2014-1418 AIAA-2014-1419 AIAA-2014-1420 AIAA-2014-1421 AIAA-2014-1422 Developing a Model to Ascribe Spacecraft deep charging The Best GEO Daytime Solar Array in Dense Plasma ISS Space Plasma Laboratory: Physical Meaning to Feature numerical evaluation basing Spacecraft Charging Index B. Vayner, Ohio Aerospace Institute, An ISS instrument package Vector Elements Derived FengYun-2 satellite high - Part II Cleveland, OH for investigating the from Infrasound Signals from energy electron data D. Ferguson, Air Force Research opening/closing of solar and Rocket Launches C. Yang, Chinese Academy of Laboratory, Kirtland AFB, NM; heliospheric magnetic fields J. Seaward, M. Archambault, F. Sciences, Beijing, China V. Davis, SAIC, San Diego, CA; E. Bering, G. Edeen, University of Ham, Florida Institute of Technology, A. Wheelock, Air Force Research Houston, Houston, TX; S. Antiochos, Melbourne, FL Laboratory, Kirtland AFB, NM C. DeVore, B. Thompson, NASA Goddard Space Flight Center, Greenbelt, MD; M. Carter, Ad Astra Rocket Company, Webster, TX; et al. Friday, 17 January 2014 379-FD-45 CFD Methods for Unsteady Flows Chesapeake Conf Rm G Chaired by: D. PELLETIER, École polytechnique de Montréal and A. KATZ 0800 hrs 0830 hrs 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2014-1423 AIAA-2014-1424 AIAA-2014-1425 AIAA-2014-1426 AIAA-2014-1427 AIAA-2014-1428 AIAA-2014-1429 AIAA-2014-1430 A numerical study of the An Unsteady Preconditioning Unsteady Simulation Least Squares Shadowing An Efficient Flexible GMRES The Discontinuous Galerkin A Modified AUSM+-up Scheme Experimental and Numerical influence of aspect ratio and gap Scheme Based on Convective- Paradigms for Trailing Edge for Sensitivity Analysis of Solver for the Fully-coupled method for partially ionized for Simulation of Flow Around Study of the Flow Field of a on 3D galloping of square prisms Upwind Split-Pressure (CUSP) Ejection Turbulent Fluid Flows Time-spectral Aeroelastic gas compressible flows Rotary Blades Translating Droplet S. Corbeil-Letourneau, S. Etienne, Artificial Dissipation R. Watson, P. Tucker, University P. Blonigan, S. Gomez, Q. System under the influence of J. Xu, W. Song, Z. Han, X. Yang, P. Zhang, A. DeVoria, K. Mohseni, A. Hay, D. Pelletier, A. Garon, École A. Katz, D. Folkner, Utah State of Cambridge, Cambridge, United Wang, Massachusetts Institute of N. Mundis, D. Mavriplis, University of electromagnetic fields Northwestern Polytechnical University of Florida, Gainesville, Polytechnique de Montréal, Montréal, University, Logan, UT; V. Sankaran, Kingdom Technology, Cambridge, MA Wyoming, Laramie, Laramie, WY K. Panourgias, J. Ekaterinaris, University, Xi’an, China Gainesville, FL Canada Air Force Research Laboratory, Embry-Riddle Aeronautical University, Edwards AFB, CA Daytona Beach, FL Friday, 17 January 2014 380-FD-46 Error Estimation and Control Azalea 3 Chaired by: C. ROY, Virginia Tech and R. STARKEY, University of Colorado Boulder 0800 hrs 0830 hrs 0900 hrs 0930 hrs 1000 hrs AIAA-2014-1431 AIAA-2014-1432 AIAA-2014-1433 AIAA-2014-1434 AIAA-2014-1435 A Discrete Error Transport Error Transport Equation Interpolation Method needed for Optimal Error Control Verification of the Unified Equation Source Model for Boundary Conditions for Numerical Uncertainty Analysis using Discrete Adjoint Error Coordinate System by the Mesh Adaptation the Euler and Navier-Stokes of Computational Fluid Dynamics Estimates in Unsteady Flow Method of Manufactured N. Currier, K. Franko, Sandia Equations C. Groves, NASA Kennedy Space Problems Solutions National Laboratories, Albuquerque, T. Phillips, C. Roy, Virginia Center, Cape Canaveral, FL; M. Ilie, B. Flynt, D. Mavriplis, University of C. Woods, R. Starkey, University of NM Polytechnic Institute and State University of Central Florida, Orlando, Wyoming, Laramie, Laramie, WY Colorado, Boulder, Boulder, CO 159 University, Blacksburg, VA FL; P. Schallhorn, NASA Kennedy Space Center, Cape Canaveral, FL Friday, 17 January 2014 381-FD-47 Other CFD Methods Maryland Ballroom 1 Chaired by: R. LOHNER and P. CIZMAS, Texas A&M University 0800 hrs 0830 hrs 0900 hrs 0930 hrs 1000 hrs 1030 hrs AIAA-2014-1436 AIAA-2014-1437 AIAA-2014-1438 AIAA-2014-1439 AIAA-2014-1440 AIAA-2014-1441 The Use of Dynamic Basis On Mesh-Particle Techniques A Simple Algorithm to Enforce Comparison of Lattice-Boltzmann Gradient Calculation Methods Modifying an unstructured Functions in Proper Orthogonal R. Lohner, F. Camelli, George Mason Mass Conservation for CFD and Finite Difference Solvers on Arbitrary Polyhedral Roe solver for large eddy Decomposition University, Fairfax, VA; J. Baum, F. Solvers With Embedded, R. Lohner, George Mason University, Unstructured Meshes for Cell- simulation B. Freno, R. Fontenot, N. Matula, Togashi, O. Soto, SAIC, McLean, VA Moving CSD Surfaces Fairfax, VA; A. Corrigan, Naval Research Centered CFD Solvers R. Watson, P. Tucker, Z. Wang, P. Cizmas, Texas A&M University, R. Lohner, George Mason University, Laboratory, Washington, DC; K. E. Sozer, C. Brehm, Science and University of Cambridge, Cambridge, College Station, TX Fairfax, VA; J. Baum, F. Togashi, O. Wichmann, W. Wall, Technical University Technology Corporation, Moffett United Kingdom; X. Yuan, Tsinghua Soto, SAIC, McLean, VA of Munich, Munich, Germany Field, CA; C. Kiris, NASA Ames University, Beijing, China Research Center, Moffett Field, CA Friday, 17 January 2014 382-FD-48 Reacting Flows (Invited) Azalea 1 Chaired by: M. PANESI, University of Illinois at Urbana Champaign and J. SCHMISSEUR, USAF AFOSR/NA 0800 hrs 0830 hrs 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs Oral Presentation Oral Presentation Oral Presentation Oral Presentation Oral Presentation AIAA-2014-1442 Oral Presentation Oral Presentation Computational Chemistry, In Depth Study of Dissociating Calculation of State-Specific Construction of physics Detailed Analyses of Oxygen Modeling dissociating flows Phys4EntryDB: a Database Macroscopic Models for Non- Detailed Numerical Simulation, Flows Using Ab Initio Models Rate Coefficients for Non- based non-equilibrium Thermochemistry Based on using close-coupled energy for State-to-State Kinetics of Equilibrium High Enthalpy and Information Theory for T. Schwartzentruber, University equilibrium Hypersonics thermochemical models State-Resolved Kinetics transfer models Planetary Atmospheres Flows Reacting Flows of Minnesota, Minneapolis, Applications M. Panesi, University of Illinois, I. Boyd, University of Michigan, Ann I. Adamovich, Ohio State University, A. Laricchiuta, I. Armenise, M. G. Colonna, National Research P. Varghese, University of Texas, Minneapolis, MN R. Jaffe, D. Schwenke, G. Chaban, Urbana-Champaign, Urbana, IL Arbor, Ann Arbor, MI Columbus, OH Cacciatore, National Research Council Council (CNR), Bari, Italy; A. Austin, Austin, TX NASA Ames Research Center, Moffett (CNR), Bari, Italy; R. Celiberto, Technical Bourdon, École Centrale de Paris, Field, CA University of Bari, Bari, Italy; F. Esposito, Paris, France; L. Pietanza, National National Research Council (CNR), Research Council (CNR), Bari, Italy; Bari, Italy; P. Gamallo, University of A. Guy, M. Perrin, École Centrale de Barcelona, Barcelona, Spain; et al. Paris, Paris, France Friday, 17 January 2014 383-FD-49 Shear and Slip Flows Azalea 2 Chaired by: S. GORDEYEV, University of Notre Dame 0800 hrs 0830 hrs 0900 hrs 0930 hrs AIAA-2014-1443 AIAA-2014-1444 AIAA-2014-1445 AIAA-2014-1446 The Effect of First- and Linear Stability Analysis of Viscous/inviscid Interacting Experimental Investigation of Second-Order Slip Condition Binary Compressible Mixing Shear Flow Theory with Aspect-Ratio Effects in Transonic on Oscillatory Flows: Several Layers Modified By a Jet or a Inferences and Their Rectangular Cavity Flows Exact Solutions Wake Deficit Applications to CFD J. Wagner, S. Beresh, K. Casper, B.

160 Z. Zhang, R. Agarwal, Washington M. Mendonca, Aeronautics and Z. Gao, Y. Shen, Chinese Academy Pruett, R. Spillers, J. Henfling, Sandia University in St. Louis, St. Louis, MO Space Institute (IAE), São José dos of Sciences, Beijing, China; G. Zha, National Laboratories, Albuquerque, NM Campos, Brazil University of Miami, Miami, FL Friday, 17 January 2014 384-FD-50 Turbulence III: Models and Simulations Chesapeake Conf Rm I Chaired by: M. PLESNIAK, George Washington University 0800 hrs 0830 hrs 0900 hrs 0930 hrs AIAA-2014-1447 AIAA-2014-1448 AIAA-2014-1449 AIAA-2014-1450 Multi-scale simulations of Hybrid Turbulence Model DNS Study of Turbulence Effects of a gain-based optimal turbulent wall-bounded and Simulations of Internal and Structure in a Boundary Layer forcing on turbulent channel flow wake flows External Flows C. Liu, Y. Yan, University of Texas, A. Sharma, University of Texas, Austin, R. Ranjan, S. Menon, Georgia A. Gross, H. Fasel, University of Arlington, Arlington, TX Austin, TX; R. Moarref, M. Luhar, Institute of Technology, Atlanta, GA Arizona, Tucson, Tucson, AZ California Institute of Technology, Pasadena, CA; D. Goldstein, University of Texas, Austin, Austin, TX; B. McKeon, California Institute of Technology, Pasadena, CA Friday, 17 January 2014 385-FD-51 Unsteady Aerodynamics II National Harbor Conf Rm 10 Chaired by: K. GRANLUND, Air Force Research Laboratory and J. BUCHHOLZ, University of Iowa 0800 hrs 0830 hrs 0900 hrs 0930 hrs 1000 hrs 1030 hrs AIAA-2014-1451 AIAA-2014-1452 AIAA-2014-1453 AIAA-2014-1454 AIAA-2014-1455 AIAA-2014-1456 Experimental Investigation of The Effect of Tip Clearance Computational Investigation Code Verification for Unsteady Fluid-Structure Interactions Scaling Vehicle Dynamics and Flows with Three-Dimensional on Low Reynolds Number of Flow Structure and 3-D Fluid-Structure Interaction in a Tube Bundle Subject to Fluid Dynamics in Gusting Separation Rotating Wings Aerodynamic Performance in problems Cross-Flow. Part A: Porous Flows M. Balthazar, A. Gross, H. Fasel, F. Manar, A. Jones, University of Low Aspect Ratio Revolving K. Yu, S. Etienne, A. Hay, D. Medium Approach D. Williams, L. Grimaud, Illinois University of Arizona, Tucson, Maryland, College Park, College Plates at Low Reynolds Pelletier, École Polytechnique de E. Tixier, C. Béguin, S. Etienne, D. Institute of Technology, Chicago, IL Tucson, AZ Park, MD number Montréal, Montréal, Canada Pelletier, A. Hay, École Polytechnique C. LI, H. Dong, University of Virginia, de Montréal, Montréal, Canada; G. Charlottesville, Charlottesville, VA Ricciardi, CEA CADARACHE, Saint- Paul-Lez-Durance, France Friday, 17 January 2014 386-GEPC-5 Legacy Fleet Fuel Efficiency - Reducing the USAF’s Multi-Billion Dollar Annual Fuel Bill Woodrow Wilson A Chaired by: G. DALE, Wright-Patterson Air Force Base 0800 hrs 0830 hrs 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs Oral Presentation (Invited) Oral Presentation (Invited) Oral Presentation (Invited) AIAA-2014-1457 AIAA-2014-1458 AIAA-2014-1459 AIAA-2014-1460 Oral Presentation (Invited) C-5 Fuel Efficiency Initiatives C-130 Fuel Efficiency Legacy Drag Reduction Studies Summary of Flight Testing Computational Aerodynamic Formation Flight for Operational Analysis for Assessment of Formation Flight M. Chang, S. Macheret, Lockheed Improvements through D. Carter, Air Force Research and Results for the Formation Analysis for the Formation Aerodynamic Benefit the Formation Flight for Benefits to the C-130 and C-5 Martin Corporation, Palmdale, Reduced Airframe Drag Laboratory, Wright-Patterson AFB, OH Flight for Aerodynamic Benefit Flight for Aerodynamic Benefit Simulation Development and Aerodynamic Benefit Program Mobility Fleets CA; J. Hooker, Lockheed Martin J. Hooker, Lockheed Martin Program Program Validation T. Flanzer, S. Bieniawski, The Boeing M. Niestroy, Lockheed Martin Corporation, Marietta, GA Corporation, Marietta, GA S. Bieniawski, The Boeing Company, J. Slotnick, The Boeing Company, D. Halaas, S. Bieniawski, B. Company, Seattle, WA Corporation, Fort Worth, TX

161 Seattle, WA; S. Rosenzweig, The Huntington Beach, CA Whitehead, The Boeing Company, Boeing Company, Long Beach, Seattle, WA; W. Blake, Air Force CA; W. Blake, Air Force Research Research Laboratory, Wright- Laboratory, Wright-Patterson AFB, OH Patterson AFB, OH Friday, 17 January 2014 387-GNC-23 Guidance, Navigation, and Control Concepts in Air Traffic Management National Harbor Conf Rm 15 Chaired by: L. WEITZ, The MITRE Corporation 0800 hrs 0830 hrs 0900 hrs 0930 hrs 1000 hrs 1030 hrs AIAA-2014-1461 AIAA-2014-1462 AIAA-2014-1463 AIAA-2014-1464 AIAA-2014-1465 AIAA-2014-1466 Application of Complexity Optimizing Metering for Application of MINLP Techniques Evaluating Tradeoff between Probabilistic Airport Capacity Co-evolutionary Approach to Map to Reduce Air Traffic Trajectory Timing Uncertainty to Conflict Resolution of Multiple Environmental Impact and Prediction Incorporating Improve Robustness of Routing Complexity in a Sector W. Kirkman, T. Gaydos, L. Weitz, Aircraft Operational Costs for Enroute Weather Forecast Uncertainty Algorithms against Disruptive Y. Hong, Y. Kim, Seoul National MITRE Corporation, McLean, VA M. Richter, M. Hochstrasser, Technical Air Traffic R. Kicinger, J. Chen, Metron Aviation, Events on the Airport Surface University, Seoul, South Korea; K. University of Munich, Garching, N. Chen, B. Sridhar, NASA Ames Inc., Dulles, VA; M. Steiner, J. Pinto, R. Kicinger, M. Ganji, J. Chen, R. Lee, Korea Aerospace University, Germany; L. Walter, French-German Research Center, Moffett Field, National Center for Atmospheric Reddy, Metron Aviation, Inc., Dulles, Goyang, South Korea Research Institute of Saint-Louis CA; H. Ng, University of California, Research, Boulder, CO VA; M. Ellejmi, EUROCONTROL, (ISL), Saint-Louis, France; M. Bittner, Santa Cruz, Moffett Field, CA; J. Li, Brétigny/Orge, France F. Holzapfel, Technical University of Stinger Ghaffarian Technologies, Inc., Munich, Garching, Germany Moffett Field, CA Friday, 17 January 2014 388-GNC-24 Mini/Micro Air Vehicles II National Harbor Conf Rm 7 Chaired by: S. WASLANDER, University of Waterloo and M. OPPENHEIMER, AFRL/RBCA 0800 hrs 0830 hrs 0900 hrs 0930 hrs 1000 hrs 1030 hrs AIAA-2014-1467 AIAA-2014-1468 AIAA-2014-1469 AIAA-2014-1470 AIAA-2014-1471 AIAA-2014-1472 Quarter Cycle Modulation of a Yaw Dynamics Identification Control of Wing Stroke Plane Longitudinal flight control Analytical Formulation Of Velocity Obstacle Method for Minimally Actuated Biomimetic of an Insect-Inspired Flapping Angle for Stabilizing of a of flapping wing micro air Heave-Yaw Modes For A Non-cooperative Autonomous Vehicle Wing Micro Air Vehicle Hovering Flapping-Wing Air vehicles Coaxial Rotor Micro Aerial Collision Avoidance System M. Oppenheimer, Air Force Research I. Faruque, University of Maryland, Vehicle S. Tahmasian, C. Woolsey, H. Taha, Vehicle for UAVs Laboratory, Wright-Patterson AFB, College Park, College Park, MD; P. J. Lee, J. Kim, J. Han, Korea Virginia Polytechnic Institute and P. Singh, C. Venkatesan, Indian Y. Jenie, E. Van Kampen, C. de OH; I. Weintraub, D. Sigthorsson, Samuel, Daedalus Flight Systems, Advanced Institute of Science and State University, Blacksburg, VA Institute of Technology Kanpur, Visser, Q. Chu, Delft University of General Dynamics Information Rockville, MD; J. Humbert, University Technology, Daejeon, South Korea Kanpur, India Technology, Delft, The Netherlands Technology, Dayton, OH; D. Doman, of Maryland, College Park, College Air Force Research Laboratory, Park, MD Wright-Patterson AFB, OH Friday, 17 January 2014 389-GNC-25 Missile Guidance, Navigation, and Control National Harbor Conf Rm 8 Chaired by: R. CAICEDO, The Boeing Company and S. WELLS, Raytheon Missile Systems 0800 hrs 0830 hrs 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2014-1473 AIAA-2014-1474 AIAA-2014-1475 AIAA-2014-1476 AIAA-2014-1477 AIAA-2014-1478 AIAA-2014-1479 AIAA-2014-1480 Partial Integrated Guidance Pitch/Yaw Channels Control An Alternative Attitude Control A Dynamic Pressure Estimation Guidance Augmentation for Capture Conditions in a Multiple Shooting Condensing Real-Time Optimal Gain and Control with Input Design for a 155mm Projectile Strategy for SCRAMSPACE 1 Algorithm for Cruise Missiles Improved Target Visibility Pursuit-Evasion Game between for Online Gain Scheduling in Scheduling for Nonlinear Constraints and Impact Angle with Rotating Canards, using Experiment G. Tusun, H. Caglar, Roketsan L. Cancemi, M. Innocenti, L. Pollini, Players with Second-Order Interceptor Guidance Dynamic Inversion X. Wang, J. Wang, Peking University, a H∞ Loop-Shaping Design S. Banerjee, M. Creagh, R. Boyce, Missiles Industries, Inc., Ankara, University of Pisa, Pisa, Italy Dynamics L. Walter, French-German Research L. Walter, G. Schlöffel, S.

162 Beijing, China Procedure University of Queensland, Brisbane, Turkey Y. Liu, York University, Toronto, Institute of Saint-Louis (ISL), Saint-Louis, Fleischmann, French-German F. Sève, S. Theodoulis, P. Wernert, Australia Canada; N. Qi, Harbin Institute of France; F. Holzapfel, Technical University Research Institute of Saint-Louis French-German Research Institute Technology, Harbin, China; J. Shan, of Munich, Garching, Germany; E. (ISL), Saint-Louis, France; F. of Saint-Louis (ISL), Saint-Louis, York University, Toronto, Canada; X. Kostina, University of Marburg, Marburg, Holzapfel, F. Peter, Technical France; M. Zasadzinski, M. Shi, Harbin Institute of Technology, Germany; G. Schlöffel, French-German University of Munich, Garching, Boutayeb, University of Lorraine, Harbin, China Research Institute of Saint-Louis (ISL), Germany Longwy, France Saint-Louis, France Friday, 17 January 2014 390-GT-11 High Reynolds Number Aerodynamics and Testing (Invited) Maryland Ballroom 3 Chaired by: R. WAHLS, NASA-Langley Research Center and J. QUEST, ETW GmbH 0800 hrs 0830 hrs 0900 hrs 0930 hrs AIAA-2014-1481 AIAA-2014-1482 AIAA-2014-1483 AIAA-2014-1484 Subsonic Transonic Applied Application of Nano-Tubes for Real-Flight Reynolds Number Assessing Model Dynamics Refinements By Using Key the Detection of Boundary Microphone-Array Measurements within the Critical Alpha Range Strategies - STARBUKS Layer Transition on a Scaled Model in ETW H. Quix, J. Quest, European Transonic R. Paryz, NASA Langley Research C. Klein, U. Henne, German T. Ahlefeldt, German Aerospace Center Windtunnel, Cologne, Germany Center, Hampton, VA Aerospace Center (DLR), Göttingen, (DLR), Göttingen, Germany; J. Quest, Germany European Transonic Windtunnel, Cologne, Germany Friday, 17 January 2014 391-MDO-9 Optimization Methods and Algorithms III Chesapeake Conf Rm 6 Chaired by: M. PATTERSON and R. GRANDHI, Wright State University 0800 hrs 0830 hrs 0900 hrs 0930 hrs 1000 hrs 1030 hrs AIAA-2014-1485 AIAA-2014-1486 AIAA-2014-1487 AIAA-2014-1488 AIAA-2014-1489 AIAA-2014-1490 A Response Surface Model Surrogate-assisted Self- A Novel Approach to A surrogate modeling Thrust-Power Pareto Fronts Application of Multifidelity Using the Sorted k-fold accelerated Particle Swarm Simultaneous Selection of approach to support real-time based on Experiments for Expected Improvement Approach Optimization Surrogate Models, Constitutive structural assessment and Small Flapping Wings Algorithms to Aeroelastic A. Vasu, R. Grandhi, Wright State K. Haji Hajikolaei, Simon Fraser Kernels, and Hyper-parameter decision-making A. Chaudhuri, R. Haftka, P. Ifju, Design Optimization University, Dayton, OH University, Surrey, Canada; A. Safari, Values L. Mainini, K. Willcox, Massachusetts K. Chang, University of Florida, P. Reisenthel, Nielsen Engineering University of Stavanger, Stavanger, A. Mehmani, S. Chowdhury, J. Zhang, Institute of Technology, Cambridge, Gainesville, Gainesville, FL & Research, Inc., Santa Clara, Norway; G. Wang, Simon Fraser Syracuse University, Syracuse, NY; A. MA CA; T. Allen, Ohio State University, University, Surrey, Canada; H. Lemu, Messac, Mississippi State University, Columbus, OH University of Stavanger, Stavanger, Mississippi State, MS Norway Friday, 17 January 2014 392-MST-7 Modeling and Simulation of Space Systems National Harbor Conf Rm 14 Chaired by: C. IH, Boeing Defense, Space & Security 0800 hrs 0830 hrs 0900 hrs 0930 hrs 1000 hrs 1030 hrs AIAA-2014-1491 AIAA-2014-1492 AIAA-2014-1493 AIAA-2014-1494 AIAA-2014-1495 AIAA-2014-1496 Dynamic Network Modeling for Finding the Force—Consistent Robotic Simulation Lean Development with Automatic Parameter Tuning Ground Contact Modeling for Spaceflight Logistics Particle Seeding for Satellite Experiments Demonstrating the Morpheus Flight and for the Morpheus Vehicle Using the Morpheus Test Vehicle K. Ho, O. De Weck, J. Hoffman, Aerodynamics Docking Proximity Operations Simulation Software Particle Swarm Optimization Simulation Massachusetts Institute of Technology, J. Parham, Lincoln Laboratory, and Contact Dynamics A. Brogley, L-3 Communications, B. Birge, L-3 Communications, L. Cordova, L-3 Communications,

163 Cambridge, MA; R. Shishko, Jet Massachusetts Institute of A. Probe, J. Junkins, Texas A&M Houston, TX Houston, TX Houston, TX Propulsion Laboratory, California Institute Technology, Lexington, MA; L. Barba, University, College Station, TX of Technology, Pasadena, CA Boston University, Boston, MA Friday, 17 January 2014 393-NDA-9 NASA Multidisciplinary UQ Challenge II Chesapeake Conf Rm 5 Chaired by: L. CRESPO, National Institute of Aerospace and S. KENNY, NASA Langley Research Center 0800 hrs 0830 hrs 0900 hrs 0930 hrs 1000 hrs 1030 hrs AIAA-2014-1497 AIAA-2014-1498 AIAA-2014-1499 AIAA-2014-1500 AIAA-2014-1501 AIAA-2014-1502 Uncertainty Quantification Efficient Quantification Bayesian Framework for A Probabilistic Treatment of An integrated and efficient A Bayesian Multilevel Methods for Model Calibration, and Risk Analysis for Multidisciplinary Uncertainty Multiple Uncertainty Types: numerical framework for Framework for Uncertainty Validation, and Risk Analysis Layered Uncertainty using Quantification and NASA UQ Challenge uncertainty quantification: Characterization and the NASA C. Safta, K. Chowdhary, K. Sargsyan, Optimization: NASA UQ Optimization J. McFarland, B. Bichon, D. Riha, application to the NASA Langley Langley Multidisciplinary UQ H. Najm, B. Debusschere, Sandia Challenge C. Liang, Vanderbilt University, Southwest Research Institute, San multidisciplinary Uncertainty Challenge National Laboratories, Livermore, A. Chaudhuri, G. Waycaster, N. Price, Nashville, TN Antonio, TX Quantification Challenge J. Nagel, B. Sudret, Swiss Federal CA; L. Swiler, Sandia National T. Matsumura, C. Park, R. Haftka, E. Patelli, University of Liverpool, Institute of Technology, Zürich, Laboratories, Albuquerque, NM; et al. University of Florida, Gainesville, Liverpool, United Kingdom; D. Alvarez, Switzerland Gainesville, FL National University of Colombia, Manizales, Colombia; M. Broggi, M. de Angelis, University of Liverpool, Liverpool, United Kingdom Friday, 17 January 2014 394-PC-23 Detonation and PDEs II Chesapeake Conf Rm H Chaired by: W. SUN, Georgia Institute of Technology and H. HUO, General Electric 0800 hrs 0830 hrs 0900 hrs 0930 hrs 1000 hrs AIAA-2014-1503 AIAA-2014-1504 AIAA-2014-1505 AIAA-2014-1506 AIAA-2014-1507 Average and Instantaneous Reflection Phenomena of Numerical Investigation of Numerical Simulation of Revisiting the Zeldovich Heat Release to the Walls of Oblique Detonation Wave Detonation Transmission Highly Unstable Detonation Spontaneous Propagation an RDE around Hypersonic Spherical Mechanism based on High- Using a High Resolution Concept S. Theuerkauf, F. Schauer, R. Projectiles on Plane Plate order Discontinuous Galerkin Scheme D. Kassoy, University of Colorado, Anthony, Air Force Research S. Sumiya, University of Tsukuba, Scheme D. Cho, T. Kim, J. Choi, Pusan Boulder, Boulder, CO Laboratory, Wright-Patterson AFB, Tsukuba, Japan; S. Maeda, Y. Lv, M. Ihme, Stanford University, National University, Busan, South OH; J. Hoke, Innovative Scientific University of Saitama, Saitama, Stanford, CA Korea Solutions, Inc., Beavercreek, OH Japan; J. Kasahara, University of Nagoya, Nagoya, Japan; A. Matsuo, Keio University, Yokohama, Japan Friday, 17 January 2014 395-SCS-6 Design, Analysis, & Test of Gossamer Systems Chesapeake Conf Rm A Chaired by: D. LICHODZIEJEWSKI, Airborne Systems NA and J. MOORE, ManTech Nexolve Corporation 0800 hrs 0830 hrs 0900 hrs 0930 hrs 1000 hrs 1030 hrs AIAA-2014-1508 AIAA-2014-1509 AIAA-2014-1510 AIAA-2014-1511 AIAA-2014-1512 AIAA-2014-1513 Analytical Investigation of a Development of the MOIRE: Ground Test Bed Testing and Application of New Conceptual Design of Precision of Large Deployable High Precision Reflector Deorbitsail flight model Results for a Large Membrane Numerically Determined Near-term Realizable Space Reflector H. Fang, Shanghai YS Information O. Stohlman, V. Lappas, University of Telescope Expandable and Foldable Solar Power Satellite A. Jennings, J. Black, J. Heller, Air Technology Company, Ltd., Shanghai, Surrey, Guildford, United Kingdom J. Domber, P. Atcheson, J. Kommers, Space Structures F. Zheng, M. Chen, Xidian University, Force Institute of Technology, Wright-

164 China; P. Huang, China Academy of Ball Aerospace & Technologies D. Kling, Folded Structures Company, Xi’an, China Patterson AFB, OH Space Technology (CAST), Xi’an, China; Corporation, Boulder, CO Ringoes, NJ; J. Hinkle, R. Cook, C. Y. Zhou, Tongji University, Shanghai, Willey, ILC Dover, Frederica, DE; W. China; L. Liu, Shanghai YS Information Doggett, NASA Langley Research Technology Company, Ltd., Shanghai, Center, Hampton, VA China; Y. Liang, W. Jiang, China Academy of Space Technology (CAST), Xi’an, China; et al. Friday, 17 January 2014 396-SD-15 Nonlinear Dynamics and Flapping Flight Chesapeake Conf Rm C Chaired by: S. RIZZI, NASA-Langley Research Center and A. SCOTTI, Pilatus Aircraft Ltd 0800 hrs 0830 hrs 0900 hrs 0930 hrs 1000 hrs 1030 hrs AIAA-2014-1514 AIAA-2014-1515 AIAA-2014-1516 AIAA-2014-1517 AIAA-2014-1518 AIAA-2014-1519 Relationships between Analysis of the Hammering Characterizing the Role A Structural Dynamic Analysis Substructuring with Nonlinear A Computational Analysis for Nonlinear Normal Modes and Mechanism of a Special of Plasticity in Structural of a Crane Fly Forewing Reduced Order Models and Flapping Wing by Coupling the Response to Random Inputs Percussive System for Response to High Speed Flows J. Rubio, P. Schilling, U. Chakravarty, Interface Reduction with Geometrically Exact Beam and J. Schoneman, M. Allen, R. Kuether, Planetary Exploration A. Gogulapati, J. LaFontaine, J. University of New Orleans, New Characteristic Constraint Modes Preconditioned Navier-Stokes University of Wisconsin, Madison, L. Vila, R. Malla, University of McNamara, Ohio State University, Orleans, LA R. Kuether, M. Allen, University of Solution Madison, WI Connecticut, Storrs, Storrs, CT Columbus, OH Wisconsin, Madison, Madison, WI H. Cho, J. Kwak, S. Shin, Seoul National University, Seoul, South Korea; N. Lee, S. Lee, Inha University, Incheon, South Korea Friday, 17 January 2014 397-SD-16 Space & Launch Vehicle Dynamics Chesapeake Conf Rm B Chaired by: T. KINNEY, NASA-Kenndey Space Center and B. WILLIS, Boeing Defense, Space & Security 0800 hrs 0830 hrs 0900 hrs 0930 hrs 1000 hrs AIAA-2014-1520 AIAA-2014-1521 AIAA-2014-1522 AIAA-2014-1523 AIAA-2014-1524 In-Flight Aeroelastic Stability A Structural Dynamics Analysis An Investigation of Bafﬂes and Prediction of Internal Cavity Study of piecewise linear of the Thermal Protection Methodology for Development Asperities on Slosh Behavior in Vibro-Acoustic Environment for isolator mounted on System on the NASA HIAD, of Earth Entry Vehicles Propellant Tanks of Spacecraft Space Vehicles nonproportional damped Part I: Linear Theory S. Perino, J. Bayandor, Virginia and Launch Vehicles D. Inoyama, R. Agarwal, T. structures under liftoff preload B. Goldman, E. Dowell, Duke Polytechnic Institute and State A. Peddu, T. Mehta, P. Stoumbos, Orbital Sciences X. Wang, T. Zheng, Tsinghua University, Durham, NC University, Blacksburg, VA Sathyanarayan, S. Gangadharan, Corporation, Dulles, VA University, Beijing, China Embry-Riddle Aeronautical University, Daytona Beach, FL Friday, 17 January 2014 398-STR-20 Damage Mechanics/Damage Tolerance Chesapeake Conf Rm F Chaired by: S. RUSSELL, Triumph Aerostructures and V. RANATUNGA, Miami Univeristy 0800 hrs 0830 hrs 0900 hrs 0930 hrs 1000 hrs AIAA-2014-1525 AIAA-2014-1526 AIAA-2014-1527 AIAA-2014-1528 AIAA-2014-1529 Damage Prediction Calculation of Equivalent Initial Inﬂuence of Fiber Packing Rotorcraft Real Time Damage Sequential Bayesian Approach in Composites due to Flaw Size Distributions for on the Deformation and Alleviation through Load to Probabilistic Damage Compression after Impact by Multiple Site Damage Damage Development in Fiber Limiting Control Tolerance Analysis Using Peridynamics G. Renaud, M. Liao, Y. Bombardier, Reinforced Laminates during C. Thaiss, C. McColl, Technical Data K. Halbert, L. Fitzwater, The Boeing A. Borut, E. Madenci, University National Research Council Canada, Curing Analysis, Inc., Falls Church, VA; J. Company, Chicago, IL of Arizona, Tucson, Tucson, AZ; N. Ottawa, Canada P. Prabhakar, A. Waas, University of Horn, E. Keller, A. Ray, Pennsylvania 165 Phan, Naval Surface Warfare Center, Michigan, Ann Arbor, Ann Arbor, MI State University, University Park, Patuxent, MD PA; R. Semidey, Naval Air Systems Command, Patuxent River, MD; et al. Friday, 17 January 2014 399-STR-21 Structural Joints Chesapeake Conf Rm E Chaired by: A. SELVARATHINAM, Lockheed Martin Corporation and S. TERMAATH, University of Tennessee 0800 hrs 0830 hrs 0900 hrs 0930 hrs 1000 hrs AIAA-2014-1530 AIAA-2014-1531 AIAA-2014-1532 AIAA-2014-1533 AIAA-2014-1534 Internally Reinforced Adhesively Bonded Joint Analytical Prediction of Experimental Characterization of Delamination Arrest by Adhesively Bonded Metal to Modeling using Finite Element Failure Strength of Co-cured Full Field Creep Deformation in Multiple Fasteners in Bonded Composite Joints Method for Failure Mode Composite Skin-Stiffener Joints Adhesively Bonded Joints Composite Structures S. Clay, Air Force Research Prediction M. Banker, B. Varughese, National S. Venkataraman, J. Casini, J. Barragan, K. Lin, L. Richard, W. Liu, University Laboratory, Wright-Patterson AFB, T. Stoumbos, S. Setoodeh, J. Aerospace Laboratories, Bangalore, San Diego State University, San of Washington, Seattle, Seattle, WA OH; V. Ranatunga, Miami University, Francis, D. Curtis, Orbital Sciences India Diego, CA Middletown, OH Corporation, Dulles, VA Friday, 17 January 2014 400-TES-5 Advances in Combustion II Maryland Ballroom B Chaired by: B. SLOAN, Iowa State University and D. LILLEY 0800 hrs 0830 hrs 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2014-1535 AIAA-2014-1536 AIAA-2014-1537 AIAA-2014-1538 AIAA-2014-1539 AIAA-2014-1540 AIAA-2014-1541 Testing of a New Drag Simple Empirical Fluid Dynamics Of Combustion: Thermal Analyses of Flow Computer Modeling of Fires: A Chemical Reactor Based Investigation of Combustion Relationship for Non-Spherical Thermodynamic Calculation of A Primer Regimes In Enclosures Under A Primer on Film Boiling For Thermal and Altitude-Ignition Particle Geometries Using the Volume and Temperature of D. Lilley, Lilley & Associates, Furniture Fires D. Lilley, Lilley & Associates, Decomposition of Organic Performance of a Small Two-Fluid Model Smoke from Fires Stillwater, OK E. Khalil, Cairo University, Cairo, Stillwater, OK Liquids: Application to Diethyl Hydrogen-Fueled Reversed- A. Chowdhury, M. Sarker, N. Love, D. Lilley, Lilley & Associates, Egypt Carbonate and Aqueous Glycerin Flow Turbine Combustor A. Choudhuri, University of Texas, El Stillwater, OK Mixtures K. Okai, T. Himeno, T. Watanabe, Paso, El Paso, TX W. Kuo, A. Lowery, Cornell University, University of Tokyo, Tokyo, Japan; Ithaca, NY; W. Tsang, National H. Kobayashi, H. Taguchi, Japan Institute of Standards and Technology, Aerospace Exploration Agency Gaithersburg, MD; C. Avedisian, Cornell (JAXA), Tokyo, Japan University, Ithaca, NY

Author/Session Chair Index Aba’a Ndong, A., 38-PDL-2 Aftosmis, M., 152-APA-17, 228-SD-9 Alauzet, F., 129-MVC-3 Ambur, D., 207-AS-1 Arnold, S., 125-MAT-2, 218-MAT-5, 265-MAT-6 Abbassi, H., 253-FD-31 Agarwal, R., 112-APA-12, 152-APA-17, 295-APA-29, Alazard, D., 23-GNC-1, 69-GNC-5, 123-GNC-8, Amiryants, G., 339-AS-4 Arolla, S., 158-FD-22 166 Abdalla, M., 42-STR-2, 365-STR-18 300-FD-36, 383-FD-49, 397-SD-16 304-GNC-17, 347-GNC-20 Amitay, M., 44-WE-1, 299-FD-35, 303-FD-39 Arras, M., 87-SD-3, 135-SD-5 Abdel-Hadi, A., 89-SRE-1 Agnes, G., 135-SD-5 Albabaa, H., 233-TES-1 Amoignon, O., 154-APA-19, 244-APA-25 Arritt, B., 298-AS-3 Abdelkeﬁ, A., 40-SD-2, 364-SD-14 Agostinelli, C., 153-APA-18 Albertani, R., 3-ISC-1 An, D., 130-NDA-3 Arruda, E., 218-MAT-5 Abdol-Hamid, K., 115-APA-15, 206-APA-24, 338-APA-34 Agrawal, A., 150-AMT-4, 331-AA-7 Aleksandrov, N., 315-PC-18 Anand, M., 223-PC-12, 273-PC-17 Artz, E., 297-APA-31 Abney, A., 20-FD-3 Agresta, A., 351-GTE-7 Alexeenko, A., 212-FD-27/TP-5, 283-TP-9 Ananthan, S., 236-WE-8 Arunajatesan, S., 375-AA-8 Abraham-Doman, S., 52-AFM-3 Agte, J., 346-GNC-19 Alfano, M., 43-STR-3 Anders, S., 299-FD-35 Arvidson, S., 60-FD-8 Abrar, B., 234-TP-6 Ahlefeldt, T., 390-GT-11 Alinger, D., 122-GNC-7 Anderson, M., 104-ACD-5 Arya, H., 357-MST-6 Abras, J., 205-APA-23, 247-APA-28 Ahmad, M., 277-SOF-3 Alkhalidi, A., 233-TES-1 Anderson, W., 35-PC-2, 63-FD-11, 164-GTE-4 Arya, M., 275-SCS-3 Abumeri, G., 366-STR-19 Ahmad, N., 249-ASE-1 Allaire, D., 311-NDA-7 Andersson, N., 375-AA-8 Asai, K., 240-AA-6, 334-AMT-9 Acar, E., 171-NDA-4 Ahmed, M., 316-PC-19 Allaneau, Y., 246-APA-27 Andreoli, V., 350-GT-9 Asai, M., 13-APA-3 Acharya, V., 174-PC-9 Ahuja, K., 240-AA-6 Allen, C., 30-MDO-1, 34-PC-1, 113-APA-13, 356-MDO-8 Andrew, W., 229-SD-10 Ash, R., 137-SRE-2 Achuthan, A., 265-MAT-6, 354-MAT-8 Ahuja, S., 260-GNC-16 Allen, M., 181-SD-8, 396-SD-15 Andriani, R., 351-GTE-7 Ashcroft, G., 18-FD-1 Ackerman, K., 162-GNC-11 Ahuja, V., 111-APA-11 Allen, N., 339-AS-4 Anemaat, W., 8-ACD-2 Ashida, T., 271-PC-15 Acosta, D., 68-GNC-4 Aigner, M., 35-PC-2 Allen, T., 391-MDO-9 Anokhin, E., 315-PC-18 Ashpis, D., 38-PDL-2, 133-PDL-5 Acree, C., 77-MDO-2 Aikens, K., 49-AA-2, 375-AA-8 Allison, P., 175-PC-10 Anthony, R., 394-PC-23 Ashraf, M., 344-FD-44 Action, J., 366-STR-19 Ait Haddou Ali, A., 23-GNC-1 Almaktoom, A., 130-NDA-3 Antiochos, S., 378-ASE-2 Aso, S., 6-AA-1, 188-TP-4 Adachi, M., 36-PC-3 Ajaj, R., 148-AFM-6, 207-AS-1 Almeida, F., 258-GNC-14 Antunes, A., 339-AS-4 Aspin, Z., 234-TP-6 Adam, G., 83-PC-5 Akaike, Y., 232-STR-12 Alonso, J., 50-ACD-3, 80-OPS-1, 140-TP-1, 310-MDO-7 Anyoji, M., 208-FD-23, 336-APA-32 Atcheson, P., 179-SCS-1, 395-SCS-6 Adamczak, D., 20-FD-3 Akamine, M., 240-AA-6 Alsultan, A., 281-TES-2 Aoki, T., 41-STR-1, 188-TP-4, 280-STR-15 Athavale, J., 234-TP-6 Adamovich, I., 37-PDL-1, 176-PDL-6, 177-PDL-7, Akepati, A., 29-MAT-1 Alter, S., 129-MVC-3 Aono, H., 156-FD-20, 208-FD-23, 336-APA-32 Atkins, E., 87-SD-3, 214-GNC-13 223-PC-12, 274-PDL-9, 362-PDL-11, 382-FD-48 Akhavannik, M., 353-IS-4 Altman, A., 64-FD-12, 256-FD-34 Aoyama, T., 63-FD-11, 64-FD-12, 102-AA-3, 157-FD-21 Atwell, T., 184-SRE-3 Adams, D., 190-WE-7, 285-WE-11 Akhtar, K., 64-FD-12 Altus, E., 139-STR-8 Aranake, A., 63-FD-11 Aubert, R., 354-MAT-8 Adams, R., 10-AFM-2 Akkala, J., 19-FD-2 Akleman, E., 377-AS-5 Alvarez, D., 121-GNC-6, 393-NDA-9 Archambault, M., 378-ASE-2 Ausserer, J., 146-ABPSI-2 Adams, S., 315-PC-18 Akram, F., 57-DE-2 Alvi, F., 208-FD-23, 240-AA-6 Arena, A., 260-GNC-16, 350-GT-9 Avedisian, C., 272-PC-16, 400-TES-5 Adhikari, S., 221-NDA-5, 277-SOF-3, 353-IS-4 Al Masoud, N., 16-DE-1 Aly, A., 169-MST-2, 357-MST-6 Arias, P., 273-PC-17 Avila, A., 126-MAT-3, 354-MAT-8 Admani, M., 365-STR-18 Al Shoaibi, A., 281-TES-2 Alyanak, E., 7-ACD-1, 51-ACD-4 Armand, S., 92-STR-6 Ayaz, U., 149-AMT-3 Afonso, F., 207-AS-1 Al-Ostaz, A., 167-MAT-4 Amano, R., 233-TES-1, 281-TES-2, 369-TP-13 Armenise, I., 382-FD-48 Ayyaz, M., 120-FD-19 Author/Session Chair Index Azarova, O., 252-FD-30 Bauer, P., 160-GNC-9, 260-GNC-16 Betts, D., 40-SD-2 Bondar, Y., 187-TP-3 Brock, B., 294-AMT-8 Azevedo, J., 157-FD-21, 337-APA-33 Baum, J., 381-FD-47 Bevilacqua, R., 260-GNC-16 Bonnet, J., 243-AMT-6, 299-FD-35 Broggi, M., 393-NDA-9 Azocar, A., 4-ISC-2 Baum, R., 185-STR-9 Bhachu, K., 268-NDA-6 Bons, J., 299-FD-35, 306-GTE-6, 340-FD-40 Brogley, A., 392-MST-7 Baba, S., 182-SE-1 Baurle, R., 61-FD-9, 119-FD-18 Bhagat, N., 51-ACD-4 Boone, R., 159-GEPC-2 Brooker, B., 150-AMT-4 Babinsky, H., 203-APA-21, 252-FD-30 Bayandor, J., 23-GNC-1, 41-STR-1, 185-STR-9, Bhagwandin, V., 302-FD-38 Booth, J., 274-PDL-9 Brooks, D., 294-AMT-8, 331-AA-7 Bachelani, A., 260-GNC-16 397-SD-16 Bhatia, M., 88-SD-4 Boothe, K., 128-MST-1 Brooks, J., 265-MAT-6, 335-AMT-10/GT-8 Badcock, K., 90-STR-4, 200-AFM-7 Baylor, J., 91-STR-5 Bhatt, S., 303-FD-39 Bordeneuve-Guibé, J., 69-GNC-5 Brovkin, V., 133-PDL-5 Badihi, H., 237-WE-9 Bayoda, E., 38-PDL-2 Bhuiyan, A., 293-AMT-7 Borggräfe, A., 227-SCS-2 Brown, C., 66-GEPC-1, 240-AA-6 Badr, M., 302-FD-38 Bayoda, K., 299-FD-35 Bichiou, Y., 40-SD-2, 364-SD-14 Borghesi, G., 225-PC-14, 272-PC-16 Brown, D., 75-ISC-4, 345-GEPC-4 Baeder, J., 12-APA-2, 157-FD-21, 327-WE-12 Beaverstock, C., 148-AFM-6, 339-AS-4 Bichon, B., 221-NDA-5, 393-NDA-9 Borghi, M., 307-HSABP-4 Brown, F., 10-AFM-2 Bahr, C., 66-GEPC-1, 102-AA-3 Beck, J., 26-GTE-1, 354-MAT-8 Bidwell, C., 297-APA-31 Borgoltz, A., 163-GT-4 Brown, J., 26-GTE-1 Bailey, S., 16-DE-1 Beck, N., 111-APA-11, 153-APA-18 Bieniawski, S., 386-GEPC-5 Borkar, A., 357-MST-6 Brown, K., 163-GT-4 Baines, A., 3-ISC-1 Becker, J., 105-ACD-6 Biggs, J., 347-GNC-20 Borkowski, L., 41-STR-1 Brown, M., 262-HSABP-3 Bak, C., 94-WE-3, 237-WE-9 Becker, K., 18-FD-1 Bijl, H., 3-ISC-1 Borovoy, V., 302-FD-38 Brownstein, I., 336-APA-32 Baker, J., 95-WE-4, 363-SCS-5 Bednarcyk, B., 125-MAT-2, 265-MAT-6, 278-STR-13 Bil, C., 8-ACD-2, 50-ACD-3, 105-ACD-6 Borut, A., 231-STR-11, 398-STR-20 Bruce, P., 119-FD-18, 252-FD-30, 253-FD-31 Baker, W., 71-GT-3 Beekman, I., 255-FD-33 Bilal, N., 190-WE-7 Boschetti, P., 106-AFM-4 Bruner, C., 78-MVC-2 Bakirtzis, G., 277-SOF-3 Béguin, C., 385-FD-51 Bilotkach, V., 134-SAT-1 Bosworth, J., 159-GEPC-2 Bruno, C., 272-PC-16, 307-HSABP-4 Bakis, C., 280-STR-15 Behr, C., 248-AS-2 Bird, J., 67-GNC-3 Botez, R., 377-AS-5 Bryant, J., 285-WE-11 Bakker, T., 128-MST-1, 263-IS-2 Behrouzifar, A., 234-TP-6 Birge, B., 392-MST-7 Bottasso, C., 190-WE-7, 237-WE-9 Bryant, L., 80-OPS-1 Balachandran, B., 296-APA-30 Beiting, E., 37-PDL-1 Bisagni, C., 43-STR-3, 278-STR-13 Bottomley, M., 110-APA-10 Bryden, K., 78-MVC-2 Balachandran, S., 214-GNC-13 Belcastro, C., 162-GNC-11, 214-GNC-13 Bisek, N., 116-FD-15, 118-FD-17, 158-FD-22, Boucher, D., 89-SRE-1, 184-SRE-3 Bryson, D., 7-ACD-1 Balakrishnan, S., 348-GNC-21 Bellan, J., 224-PC-13, 225-PC-14 226-PDL-8 Bouheraoua, L., 83-PC-5 Buchholz, J., 19-FD-2, 45-WE-2, 385-FD-51 Balan, A., 251-FD-29 Belter, D., 71-GT-3 Bisetti, F., 224-PC-13 Bouhmedi, M., 176-PDL-6 Buchnik, S., 181-SD-8 Balas, M., 23-GNC-1, 142-WE-5, 237-WE-9 Benard, N., 38-PDL-2, 86-PDL-4, 299-FD-35 Bisson, F., 113-APA-13 Bounajem, E., 180-SD-7 Buchy, R., 205-APA-23

167 Balasubramaniam, B., 137-SRE-2 Bendiksen, O., 180-SD-7 Bittner, M., 347-GNC-20, 387-GNC-23 Bountin, D., 342-FD-42 Buck, A., 122-GNC-7 Balch, M., 221-NDA-5 Benedict, K., 65-FD-13 Bityurin, V., 256-FD-34, 274-PDL-9, 340-FD-40 Bourassa, C., 120-FD-19 Buck, G., 305-GT-7 Ball, D., 89-SRE-1 Beneigh, T., 17-EDU-1 Blacha, T., 35-PC-2 Bourdon, A., 382-FD-48 Buckney, N., 94-WE-3 Balthazar, M., 385-FD-51 Benek, J., 54-APA-7, 211-FD-26/MVC-5 Black, J., 242-AFM-9, 395-SCS-6 Boutayeb, M., 389-GNC-25 Buffo, R., 256-FD-34 Bane, S., 164-GTE-4, 340-FD-40 Bennett, D., 338-APA-34 Blackburn, C., 354-MAT-8 Bowen, C., 29-MAT-1, 40-SD-2 Bülthoff, H., 220-MST-3 Banerjee, S., 123-GNC-8, 389-GNC-25 Benton, D., 169-MST-2 Blaisdell, G., 49-AA-2, 375-AA-8 Bowen, P., 367-TES-4 Bulzan, D., 257-GEPC-3 Banker, M., 399-STR-21 Benton, S., 299-FD-35, 340-FD-40 Blake, J., 249-ASE-1 Bowersox, R., 157-FD-21 Buning, P., 211-FD-26/MVC-5 Bansal, P., 181-SD-8 Beran, P., 88-SD-4 Blake, W., 148-AFM-6, 386-GEPC-5 Boxx, I., 84-PC-6, 175-PC-10 Buonanno, M., 180-SD-7 Barad, M., 18-FD-1, 343-FD-43 Berceli, M., 323-STR-17 Blanchard, R., 107-AFM-5 Boyack, C., 325-TP-10 Burchett, B., 241-AFM-8 Barakos, G., 12-APA-2, 55-APA-8, 337-APA-33 Berens, T., 103-ABPSI-1, 198-ABPSI-3 Bland, S., 138-STR-7, 322-STR-16 Boyce, R., 123-GNC-8, 389-GNC-25 Burgess, N., 114-APA-14, 251-FD-29 Barba, L., 392-MST-7 Beresh, S., 117-FD-16, 294-AMT-8, 335-AMT-10/GT-8, Bleischwitz, R., 337-APA-33 Boyd, I., 283-TP-9, 382-FD-48 Burkhalter, J., 169-MST-2 Barbarino, S., 138-STR-7, 322-STR-16, 377-AS-5 383-FD-49 Blevins, J., 338-APA-34 Boyd, S., 232-STR-12 Burki-Cohen, J., 267-MST-4 Barcinski, T., 346-GNC-19 Berg, J., 285-WE-11 Blodgett, K., 146-ABPSI-2 Brampton, C., 29-MAT-1 Burley, C., 6-AA-1, 66-GEPC-1, 102-AA-3 Barckmann, K., 86-PDL-4 Bergami, L., 237-WE-9 Blom, A., 365-STR-18 Brasseur, J., 190-WE-7, 236-WE-8 Burnette, D., 274-PDL-9 Barj, L., 95-WE-4 Bergamini, A., 248-AS-2 Blomberg, C., 75-ISC-4 Brauckmann, G., 305-GT-7 Burns, R., 85-PDL-3 Barnard, C., 149-AMT-3 Berger, K., 305-GT-7 Blonigan, P., 379-FD-45 Braun, M., 272-PC-16 Burt, J., 187-TP-3, 235-TP-7 Barnes, C., 344-FD-44 Berger, Z., 64-FD-12, 243-AMT-6, 331-AA-7 Blood, D., 149-AMT-3 Braun, R., 92-STR-6, 107-AFM-5, 167-MAT-4, 188-TP-4, Burton, J., 309-MAT-7 Barone, D., 351-GTE-7 Bergman, D., 179-SCS-1 Blosch, E., 56-APA-9 200-AFM-7, 219-MDO-5, 292-AFM-10, 333-AFM-11 Busa, K., 262-HSABP-3 Barone, M., 44-WE-1, 94-WE-3, 375-AA-8 Berguin, S., 30-MDO-1 Blount, P., 178-SAT-2 Braun, S., 258-GNC-14 Buschhorn, S., 29-MAT-1 Barragan, J., 399-STR-21 Bering, E., 378-ASE-2 Blunck, D., 72-GTE-2, 124-GTE-3, 272-PC-16 Braunstein, M., 283-TP-9 Bushnell, D., 231-STR-11 Barrett-Gonzalez, R., 50-ACD-3, 298-AS-3 Berlette, J., 84-PC-6 Bocharov, A., 274-PDL-9 Breedlove, J., 282-TP-8 Bussoletti, J., 63-FD-11 Barth, J., 307-HSABP-4 Bernardini, C., 299-FD-35 Boelens, O., 206-APA-24 Brehm, C., 18-FD-1, 343-FD-43, 381-FD-47 Bychkov, S., 256-FD-34 Bartram, G., 130-NDA-3, 171-NDA-4 Bernhammer, L., 190-WE-7, 237-WE-9, 284-WE-10 Bogdanowicz, C., 199-ACD-8 Brekke, K., 56-APA-9 Bychkov, V., 176-PDL-6 Baruzzi, G., 370-WE-14 Berry, M., 64-FD-12, 243-AMT-6, 331-AA-7 Bogey, C., 145-AA-4 Breuer, K., 190-WE-7, 298-AS-3, 336-APA-32 Byun, G., 62-FD-10 Basoalto, H., 265-MAT-6 Berry, S., 305-GT-7 Bokor, J., 160-GNC-9, 260-GNC-16, 304-GNC-17 Bridges, J., 240-AA-6 Cabrera, L., 233-TES-1 Bateman, A., 121-GNC-6, 277-SOF-3 Bershadsky, D., 277-SOF-3 Bolandhemmat, H., 357-MST-6 Briggs, H., 16-DE-1, 57-DE-2 Cacciatore, M., 382-FD-48 Bathel, B., 62-FD-10 Berton, J., 159-GEPC-2 Bolender, M., 9-AFM-1 Brink, C., 262-HSABP-3 Cacciola, S., 190-WE-7 Batson, J., 283-TP-9, 326-TP-11 Bes, C., 134-SAT-1 Bombardier, Y., 398-STR-20 Brinker, A., 272-PC-16 Cadel, D., 294-AMT-8 Author/Session Chair Index Cadou, C., 188-TP-4, 351-GTE-7, 360-PC-21/AMT-11 Cavallaro, R., 39-SD-1, 136-SD-6, 244-APA-25, Chevalier, M., 103-ABPSI-1 Cohen, K., 263-IS-2, 353-IS-4, 357-MST-6 Craven, B., 236-WE-8 Cagan, J., 370-WE-14 321-SD-13 Chitale, K., 31-MVC-1, 204-APA-22 Cohen, M., 137-SRE-2 Crawford, B., 245-APA-26, 376-AMT-12/GT-10 Caglar, H., 389-GNC-25 Cavallo, P., 206-APA-24, 246-APA-27 Chng, T., 362-PDL-11 Colella, P., 343-FD-43 Crawley, M., 145-AA-4 Cai, J., 51-ACD-4, 256-FD-34, 369-TP-13 Cayzac, R., 15-APA-5 Cho, D., 394-PC-23 Coleman, D., 112-APA-12 Creagh, M., 123-GNC-8, 389-GNC-25 Cai, W., 109-AMT-2 Cecrdle, J., 181-SD-8 Cho, H., 396-SD-15 Colket, M., 34-PC-1, 82-PC-4 Crespo, L., 162-GNC-11, 358-NDA-8, 393-NDA-9 Caicedo, R., 389-GNC-25 Celi, M., 106-AFM-4 Cho, K., 280-STR-15 Collett, M., 188-TP-4 Crider, D., 68-GNC-4, 121-GNC-6, 162-GNC-11, Cain, C., 16-DE-1 Celiberto, R., 382-FD-48 Cho, M., 126-MAT-3, 139-STR-8, 186-STR-10, Collier, F., 66-GEPC-1 267-MST-4 Cairns, D., 284-WE-10 Ceresola, N., 198-ABPSI-3 280-STR-15 Colliss, S., 252-FD-30 Crisanti, M., 262-HSABP-3 Calhoon, W., 273-PC-17 Ceriotti, M., 227-SCS-2 Choe, R., 68-GNC-4, 259-GNC-15 Collopy, A., 261-GT-6 Crofton, M., 37-PDL-1 Calvert, M., 112-APA-12 Cesnik, C., 39-SD-1, 87-SD-3 Choi, H., 161-GNC-10 Colonna, G., 382-FD-48 Crosby, W., 338-APA-34 Camberos, J., 320-SD-12 Chabalko, C., 296-APA-30 Choi, J., 126-MAT-3, 130-NDA-3, 301-FD-37, 394-PC-23 Colonno, M., 50-ACD-3 Cross, C., 26-GTE-1 Cambier, L., 63-FD-11 Chaban, G., 382-FD-48 Choi, K., 45-WE-2 Colozza, A., 354-MAT-8 Crossley, W., 51-ACD-4 Camelli, F., 381-FD-47 Chabriat, J., 86-PDL-4 Choi, S., 219-MDO-5, 244-APA-25 Combs, C., 305-GT-7 Crouch, R., 41-STR-1 Campagnolo, F., 237-WE-9 Chakraborty, I., 105-ACD-6 Chongvisal, J., 214-GNC-13 Commo, S., 70-GT-2 Crouch, T., 27-HIS-1 Campbell, L., 363-SCS-5 Chakravarthy, A., 276-SD-11 Chopra, I., 199-ACD-8, 339-AS-4 Conny, J., 281-TES-2 Crouse, G., 51-ACD-4, 199-ACD-8 Campbell, R., 31-MVC-1, 190-WE-7 Chakravarty, U., 396-SD-15 Chou, A., 210-FD-25 Conroy, T., 50-ACD-3 Crowell, A., 39-SD-1 Cancemi, L., 389-GNC-25 Chamitoff, G., 346-GNC-19 Choudhari, M., 250-FD-28, 301-FD-37 Consigny, H., 103-ABPSI-1, 198-ABPSI-3 Crozon, C., 55-APA-8 Candler, G., 235-TP-7 Chan, W., 152-APA-17, 279-STR-14, 307-HSABP-4 Choudhuri, A., 233-TES-1, 367-TES-4, 400-TES-5 Constantine, P., 268-NDA-6, 310-MDO-7 Cruz, J., 70-GT-2 Canﬁeld, R., 127-MDO-3 Chandar, D., 189-WE-6 Choukroun, D., 123-GNC-8, 346-GNC-19, 349-GNC-22 Convery, J., 306-GTE-6 Cui, Y., 110-APA-10, 179-SCS-1 Cano Martinez, A., 23-GNC-1 Chandavarkar, R., 123-GNC-8 Chow, R., 62-FD-10 Cook, R., 395-SCS-6 Cui, Y., 349-GNC-22 Cant, R., 272-PC-16 Chang, C., 301-FD-37 Chowdhary, K., 393-NDA-9 Cooley, A., 188-TP-4 Culler, A., 136-SD-6 Cantu, L., 293-AMT-7 Chang, J., 296-APA-30 Chowdhury, A., 400-TES-5 Cooley, P., 135-SD-5 Cummings, R., 13-APA-3 Cao, C., 68-GNC-4 Chang, K., 391-MDO-9 Chowdhury, S., 189-WE-6, 266-MDO-6, 391-MDO-9 Coon, T., 346-GNC-19 Cunningham, K., 10-AFM-2, 52-AFM-3 Cao, Y., 109-AMT-2 Chang, M., 11-APA-1, 386-GEPC-5 Chrissis, J., 219-MDO-5 Cooney, J., 327-WE-12 Cuppoletti, D., 145-AA-4, 375-AA-8

168 Capristan, F., 80-OPS-1 Chang, T., 209-FD-24 Christensen, M., 265-MAT-6 Cooper, J., 39-SD-1, 90-STR-4, 128-MST-1, 207-AS-1, Curran, H., 34-PC-1, 82-PC-4 Capua, A., 123-GNC-8 Chankaya, K., 56-APA-9 Christhilf, D., 321-SD-13 259-GNC-15, 277-SOF-3, 339-AS-4 Currier, N., 380-FD-46 Caraballo, E., 65-FD-13 Chaput, A., 16-DE-1 Christie, G., 308-IS-3 Copeland, R., 141-TP-2 Curtis, D., 399-STR-21 Caramia, G., 310-MDO-7 Charalampous, G., 173-PC-8 Chu, P., 137-SRE-2 Copeland, S., 63-FD-11, 140-TP-1 Cutler, A., 165-HSABP-2, 293-AMT-7 Carbonari, R., 162-GNC-11 Chase, A., 9-AFM-1 Chu, Q., 3-ISC-1, 23-GNC-1, 304-GNC-17, 388-GNC-24 Copp, T., 179-SCS-1, 363-SCS-5 Cybyk, B., 336-APA-32 Cardenas, E., 106-AFM-4 Chatterjee, S., 349-GNC-22 Chuck, C., 351-GTE-7 Coppola, A., 167-MAT-4 Czekalowski, P., 242-AFM-9 Cardinal, M., 106-AFM-4 Chattopadhyay, A., 41-STR-1, 355-MAT-9 Chung, S., 272-PC-16 Coppotelli, G., 87-SD-3, 135-SD-5 D’Amato, E., 258-GNC-14 Cardullo, F., 220-MST-3 Chaudhuri, A., 391-MDO-9, 393-NDA-9 Churaman, W., 223-PC-12 Corbeil-Letourneau, S., 379-FD-45 D’Entremont, J., 164-GTE-4 Carley, G., 126-MAT-3 Chaurasia, A., 309-MAT-7 Churchﬁeld, M., 189-WE-6, 285-WE-11 Corbets, J., 3-ISC-1 Da Ronch, A., 90-STR-4, 200-AFM-7 Carlson, S., 4-ISC-2 Che, J., 68-GNC-4 Chwalowski, P., 136-SD-6 Cordell, C., 292-AFM-10 Dadashi, S., 23-GNC-1 Carrier, G., 154-APA-19 Chekiri, R., 6-AA-1 Chynoweth, B., 20-FD-3 Cordova, L., 392-MST-7 Dadone, A., 310-MDO-7 Carroll, D., 267-MST-4 Chekkal, I., 339-AS-4 Cichella, V., 259-GNC-15 Corke, T., 112-APA-12, 327-WE-12, 340-FD-40 Dahl, M., 49-AA-2, 375-AA-8 Carter, C., 74-HSABP-1, 84-PC-6, 307-HSABP-4, Chen, F., 273-PC-17, 369-TP-13 Cisneros, E., 133-PDL-5 Corman, J., 323-STR-17 Dahm, J., 21-FD-4 316-PC-19 Chen, H., 265-MAT-6, 355-MAT-9 Cizmas, P., 381-FD-47 Correale, G., 86-PDL-4 Daingade, S., 357-MST-6 Carter, D., 386-GEPC-5 Chen, J., 109-AMT-2, 225-PC-14, 387-GNC-23 Clark, D., 184-SRE-3 Corrigan, A., 49-AA-2, 65-FD-13, 271-PC-15, 381-FD-47 Dale, A., 207-AS-1 Carter, M., 378-ASE-2 Chen, M., 395-SCS-6 Clay, S., 41-STR-1, 323-STR-17, 366-STR-19, Corson, D., 237-WE-9 Dale, G., 345-GEPC-4, 386-GEPC-5 Cary, A., 22-FD-5, 60-FD-8 Chen, N., 220-MST-3, 387-GNC-23 399-STR-21 Coso, A., 104-ACD-5 Dalle, D., 146-ABPSI-2 Case, S., 322-STR-16 Chen, P., 157-FD-21, 298-AS-3, 321-SD-13 Clem, M., 240-AA-6 Costain, A., 185-STR-9 Damele, C., 124-GTE-3 Casini, J., 399-STR-21 Chen, Q., 25-GT-1 Clemens, N., 61-FD-9, 305-GT-7 Couch, M., 93-SUR-1 Damiani, R., 284-WE-10 Casper, K., 117-FD-16, 383-FD-49 Chen, R., 132-PC-7 Cliff, S., 31-MVC-1, 152-APA-17 Couris, S., 360-PC-21/AMT-11 Dan, W., 169-MST-2 Cassell, A., 92-STR-6 Chen, T., 315-PC-18 Clifford, C., 340-FD-40 Covington, J., 232-STR-12 Danehy, P., 62-FD-10, 201-AMT-5/PC-11, 293-AMT-7, Castillo, J., 188-TP-4 Chen, W., 110-APA-10, 282-TP-8 Clingman, D., 228-SD-9 Cox, C., 333-AFM-11 305-GT-7 Castner, R., 61-FD-9 Chen, Y., 175-PC-10 Cobb, R., 128-MST-1, 258-GNC-14, 346-GNC-19 Cox, G., 26-GTE-1 Danforth, R., 25-GT-1 Caswell, A., 108-AMT-1, 124-GTE-3, 201-AMT-5/PC-11 Chen, Z., 21-FD-4 Coburn, B., 43-STR-3 Cox, W., 37-PDL-1 Daniel, L., 350-GT-9 Cater, J., 189-WE-6 Cheng, K., 259-GNC-15 Cocks, P., 225-PC-14 Cozmuta, I., 368-TP-12 Dannenhoffer, J., 78-MVC-2 Cattafesta, L., 240-AA-6, 243-AMT-6 Cheng, Y., 161-GNC-10 Coder, J., 113-APA-13 Craft, J., 137-SRE-2 Dansie, J., 11-APA-1 Cavagna, L., 115-APA-15 Chern, S., 119-FD-18 Cogan, B., 10-AFM-2, 121-GNC-6, 258-GNC-14 Crafton, J., 149-AMT-3 Darbandi, M., 156-FD-20, 234-TP-6 Cavalieri, K., 259-GNC-15 Cheung, R., 339-AS-4 Coggin, J., 88-SD-4 Cragin, K., 282-TP-8 Darin, J., 35-PC-2 Author/Session Chair Index Daryabeigi, K., 92-STR-6 DeSio, C., 150-AMT-4 Dress, D., 182-SE-1 Ekkad, S., 234-TP-6 Farhat, C., 59-FD-7 Datta, A., 364-SD-14 Desjardins, O., 316-PC-19 Dressel, L., 277-SOF-3 Eklund, D., 156-FD-20 Faria, C., 248-AS-2 Daugherty, S., 67-GNC-3 Desmariaux, J., 69-GNC-5 Drews, S., 62-FD-10 Ekmekci, A., 118-FD-17 Farmer, B., 179-SCS-1 Davidson, L., 60-FD-8 DeSpirito, J., 15-APA-5, 56-APA-9 Driscoll, J., 84-PC-6, 146-ABPSI-2, 175-PC-10, El Ramlawy, A., 169-MST-2 Farnsworth, J., 110-APA-10, 250-FD-28 Davis, T., 240-AA-6 Desrochers, P., 267-MST-4 302-FD-38 El-Asrag, H., 152-APA-17, 224-PC-13, 272-PC-16 Farouk, T., 82-PC-4 Davis, V., 378-ASE-2 Destarac, D., 154-APA-19 Drolen, B., 141-TP-2 Eldredge, J., 116-FD-15 Farrar, B., 112-APA-12 Dawes, W., 31-MVC-1, 116-FD-15 DeStories, J., 147-ACD-7 Dryer, F., 82-PC-4, 164-GTE-4 Eliasson, P., 204-APA-22 Faruque, I., 388-GNC-24 Dayyani, I., 298-AS-3 Devarakonda, N., 123-GNC-8 Du, Y., 375-AA-8 Elkins, R., 181-SD-8 Fasel, H., 117-FD-16, 384-FD-50, 385-FD-51 de Angelis, M., 393-NDA-9 Devenport, W., 163-GT-4 Duan, L., 250-FD-28, 301-FD-37 Ellejmi, M., 387-GNC-23 Fassmann, W., 242-AFM-9 De Breuker, R., 112-APA-12, 148-AFM-6, 190-WE-7, DeVore, C., 378-ASE-2 Duan, Y., 51-ACD-4, 369-TP-13 Elmiligui, A., 31-MVC-1, 152-APA-17, 206-APA-24 Faulkner, A., 184-SRE-3 339-AS-4 DeVore, M., 277-SOF-3 Duan, Z., 62-FD-10 Elshabka, A., 357-MST-6 Faust, A., 37-PDL-1 de Doncker, E., 91-STR-5 DeVoria, A., 379-FD-45 Duarte, T., 95-WE-4 Emeneth, M., 105-ACD-6 Favaregh, N., 11-APA-1, 338-APA-34 De Gaspari, A., 339-AS-4 Dhamankar, N., 49-AA-2, 375-AA-8 Dudley, J., 21-FD-4, 56-APA-9 Emerson, B., 175-PC-10 Fedorov, A., 342-FD-42 De Hoog, S., 75-ISC-4 Di Francesco, G., 258-GNC-14 Dufrene, A., 338-APA-34 Engblom, W., 296-APA-30, 307-HSABP-4 Feigh, K., 121-GNC-6, 162-GNC-11, 214-GNC-13 de Jesus, A., 157-FD-21 Di Lillo, L., 248-AS-2 Duimstra, J., 108-AMT-1 Engelsen, F., 127-MDO-3 Feiguel, A., 357-MST-6 De Kat, R., 337-APA-33 Diamant, K., 37-PDL-1 Dumont, A., 154-APA-19 Engelstad, S., 279-STR-14, 366-STR-19 Felemban, H., 68-GNC-4 De La Garza, A., 180-SD-7 Diaz, D., 360-PC-21/AMT-11 Dumpala, S., 274-PDL-9 Ennis, B., 285-WE-11 Felisiak, P., 24-GNC-2 De La Torre, G., 214-GNC-13 DiazDelaO, F., 221-NDA-5 Duncan, G., 245-APA-26, 376-AMT-12/GT-10 Enright, M., 279-STR-14 Feltham, G., 118-FD-17 De Lucca, N., 85-PDL-3 Dickson, D., 162-GNC-11 Dunn, C., 263-IS-2 Envia, E., 375-AA-8 Fenercioglu, I., 344-FD-44 De Simoni, L., 248-AS-2 DiFulvio, M., 305-GT-7 Dunn, S., 215-GT-5 Epstein, B., 154-APA-19 Ferede, E., 42-STR-2, 284-WE-10 de Visser, C., 23-GNC-1, 388-GNC-24 Dipace, A., 244-APA-25 Dunning, P., 90-STR-4, 168-MDO-4 Erbschloe, D., 345-GEPC-4 Fereidooni, A., 190-WE-7 De Weck, O., 392-MST-7 Diskin, B., 22-FD-5 DuPont, B., 370-WE-14 Erickson, G., 338-APA-34 Ferguson, D., 378-ASE-2 DeBonis, J., 13-APA-3 Diskin, G., 262-HSABP-3 Duque, E., 285-WE-11 Ericson, S., 28-ISC-3 Ferguson, S., 245-APA-26 Debusschere, B., 393-NDA-9 Dixon, G., 278-STR-13 Duraisamy, K., 63-FD-11, 248-AS-2 Eriksson, L., 145-AA-4, 375-AA-8 Fernandez, E., 14-APA-4, 208-FD-23

169 Dec, J., 188-TP-4 Dogan, A., 52-AFM-3, 148-AFM-6 Durand, J., 182-SE-1 Ermanni, P., 248-AS-2 Fernelius, M., 216-GTE-5 DeCarlo, E., 32-NDA-1 Doggett, W., 354-MAT-8, 395-SCS-6 Durbin, P., 158-FD-22 Ermishkin, M., 226-PDL-8 Feron, E., 214-GNC-13 Deck, S., 13-APA-3 Dogra, S., 128-MST-1 Durgesh, V., 243-AMT-6 Erofeev, A., 226-PDL-8 Ferraro, G., 151-APA-16, 153-APA-18 Decker, R., 119-FD-18 Doig, G., 56-APA-9 Durnberg, E., 29-MAT-1 Erturk, S., 52-AFM-3 Fertig, R., 309-MAT-7, 355-MAT-9 Deconinck, H., 369-TP-13 Dolan, B., 175-PC-10 Durston, D., 152-APA-17 Erwin, J., 49-AA-2 Few, A., 150-AMT-4 Del Rosario, R., 159-GEPC-2 Doman, D., 388-GNC-24 Dussault, D., 243-AMT-6 Esakov, I., 226-PDL-8 Fidkowski, K., 21-FD-4, 116-FD-15 DeLisio, J., 173-PC-8 Domber, J., 92-STR-6, 179-SCS-1, 395-SCS-6 Dustin, J., 265-MAT-6 Eslam Panah, A., 19-FD-2 Fields, T., 52-AFM-3 Dellimore, K., 188-TP-4 Domingo, P., 83-PC-5 Dutta, S., 107-AFM-5, 200-AFM-7 Esna Ashari, A., 214-GNC-13 Figueroa, L., 89-SRE-1 DeLoach, R., 25-GT-1 Domyancic, L., 171-NDA-4 Dykes, K., 285-WE-11 Espinal, D., 216-GTE-5 Filosa, A., 369-TP-13 Delot, A., 103-ABPSI-1, 198-ABPSI-3 Dona, N., 297-APA-31 Dykman, J., 228-SD-9 Espitia, A., 245-APA-26 Findlay, D., 128-MST-1 Deloze, T., 246-APA-27 Dong, H., 14-APA-4, 385-FD-51 Eagle, W., 302-FD-38 Esposito, F., 382-FD-48 Fineman, C., 360-PC-21/AMT-11 Demargne, A., 31-MVC-1 Dong, W., 202-APA-20 Eames, D., 147-ACD-7 Etienne, S., 209-FD-24, 379-FD-45, 385-FD-51 Finkleman, D., 80-OPS-1 Demasi, L., 39-SD-1, 42-STR-2, 136-SD-6, 244-APA-25, Donohoe, P., 357-MST-6 Eastep, F., 320-SD-12 Eun, W., 364-SD-14 Finley, D., 56-APA-9, 152-APA-17 321-SD-13 Dooley, S., 82-PC-4 Eberle, C., 35-PC-2 Evans, R., 31-MVC-1 Finney, B., 28-ISC-3 Demosthenous, E., 272-PC-16 Dorﬂing, J., 153-APA-18 Ecker, T., 294-AMT-8, 331-AA-7 Everhart, J., 305-GT-7 Fiola, C., 152-APA-17 Dener, A., 30-MDO-1 Dorgan, A., 22-FD-5 Economon, T., 63-FD-11 Eversman, W., 197-AA-5 Firsov, A., 262-HSABP-3 Denison, M., 133-PDL-5 DorMohammadi, S., 266-MDO-6, 311-NDA-7, Edeen, G., 378-ASE-2 Fagan, A., 61-FD-9, 240-AA-6 Fischer, C., 268-NDA-6 Denning, M., 108-AMT-1 365-STR-18 Edstrand, A., 240-AA-6 Fagley, C., 65-FD-13, 250-FD-28 Fisher, D., 17-EDU-1 Dennis, B., 242-AFM-9 Dorrington, G., 50-ACD-3 Edwards, J., 119-FD-18, 165-HSABP-2, 300-FD-36 Fahringer, T., 109-AMT-2 Fisher, T., 209-FD-24 DePasquale, D., 333-AFM-11 Dougherty, N., 325-TP-10 Edwards, R., 368-TP-12 Fairfax, L., 241-AFM-8 Fist, A., 3-ISC-1 Depuru Mohan, N., 145-AA-4 Dourado, W., 317-PC-20 Effendy, M., 72-GTE-2 Fakhraie, R., 155-DE-3 Fitzwater, L., 398-STR-20 Derochers, P., 267-MST-4 Dow, E., 268-NDA-6 Eﬁmov, A., 141-TP-2, 256-FD-34 Falcone, G., 80-OPS-1 Flanzer, T., 386-GEPC-5 Derry, S., 241-AFM-8 Dowell, E., 397-SD-16 Eggels, R., 273-PC-17 Falkiewicz, N., 39-SD-1 Flatau, A., 3-ISC-1 Dervieux, A., 129-MVC-3 Dowling, A., 145-AA-4 Egolf, T., 12-APA-2, 55-APA-8 Falugi, M., 279-STR-14 Fleeter, S., 285-WE-11 Desalvo, M., 53-APA-6 Dras, L., 128-MST-1 Egorov, I., 302-FD-38, 342-FD-42 Fang, C., 346-GNC-19 Fleischmann, S., 389-GNC-25 Deschenes, T., 283-TP-9 Drazumeric, R., 112-APA-12, 320-SD-12 Ehrmann, R., 44-WE-1, 62-FD-10 Fang, H., 179-SCS-1, 227-SCS-2, 363-SCS-5, 395-SCS-6 Flynt, B., 380-FD-46 Desgroux, P., 176-PDL-6 Dreese, J., 56-APA-9 Eiler, J., 182-SE-1 Fang, X., 279-STR-14, 366-STR-19 Fnu, V., 263-IS-2 Deshmukh, R., 39-SD-1 Drela, M., 245-APA-26 Ekaterinaris, J., 18-FD-1, 379-FD-45 Fares, E., 255-FD-33 Foerster, C., 138-STR-7 Author/Session Chair Index Fogg, D., 282-TP-8 Gaitonde, D., 53-APA-6, 165-HSABP-2, 252-FD-30, Gerth, I., 24-GNC-2 Gordeyev, S., 85-PDL-3, 255-FD-33, 383-FD-49 Gruber, A., 225-PC-14 Folkner, D., 379-FD-45 302-FD-38 Gerz, T., 249-ASE-1 Gordnier, R., 180-SD-7, 344-FD-44 Grundmann, S., 86-PDL-4, 336-APA-32 Fontenot, R., 381-FD-47 Galbraith, M., 211-FD-26/MVC-5 Getsinger, D., 61-FD-9 Gordon, S., 86-PDL-4 Gu, Y., 121-GNC-6, 267-MST-4 Forlines, R., 149-AMT-3 Gale, J., 354-MAT-8 Geubelle, P., 167-MAT-4 Goroshin, S., 173-PC-8 Guadagnoli, L., 16-DE-1 Forliti, D., 36-PC-3 Galisteu, D., 258-GNC-14 Gevorkyan, L., 61-FD-9 Gorrell, S., 216-GTE-5 Guala, M., 370-WE-14 Forsythe, J., 247-APA-28 Gallay, S., 295-APA-29 Ghafourizadeh, M., 156-FD-20 Gorski, J., 308-IS-3 Guan, H., 211-FD-26/MVC-5 Forsythe, L., 233-TES-1 Gallego Cañizares, C., 202-APA-20 Ghanem, R., 358-NDA-8 Goss, L., 149-AMT-3 Guelhan, A., 117-FD-16 Foster, J., 10-AFM-2, 162-GNC-11 Gallis, M., 212-FD-27/TP-5 Ghasemi, S., 152-APA-17, 295-APA-29 Gosse, R., 235-TP-7 Guerieri, P., 223-PC-12 Fotia, M., 271-PC-15, 360-PC-21/AMT-11 Gallman, J., 334-AMT-9 Ghobadi, K., 152-APA-17 Goudie, C., 139-STR-8 Guerreiro, N., 220-MST-3 Fouquet, P., 306-GTE-6 Gallo, C., 137-SRE-2 Ghorbani Moghaddam, M., 265-MAT-6 Goulart, P., 229-SD-10, 328-WE-13 Guglielmo, J., 244-APA-25 Fowler, A., 28-ISC-3 Gallo, E., 293-AMT-7 Ghoreyshi, M., 13-APA-3 Goulding, P., 163-GT-4 Guildenbecher, D., 109-AMT-2 Francis, J., 399-STR-21 Galyen, N., 335-AMT-10/GT-8 Ghosh, S., 217-IS-1, 218-MAT-5, 336-APA-32 Goyal, V., 138-STR-7 Gulder, O., 174-PC-9, 273-PC-17 Frank, C., 182-SE-1 Gamallo, P., 382-FD-48 Giesy, D., 162-GNC-11, 358-NDA-8 Goyne, C., 108-AMT-1, 165-HSABP-2, 262-HSABP-3, Gunasekaran, M., 295-APA-29 Frankel, S., 209-FD-24 Gamba, M., 302-FD-38 Gill, S., 162-GNC-11 335-AMT-10/GT-8 Gunasekaran, S., 64-FD-12 Franko, K., 380-FD-46 Gamma, F., 351-GTE-7 Gingras, D., 267-MST-4 Gozcu, M., 328-WE-13 Gundling, C., 189-WE-6 Frecker, M., 298-AS-3 Ganapathisubramani, B., 337-APA-33 Gissen, A., 252-FD-30 Gozse, I., 260-GNC-16 Guntur, S., 94-WE-3 Frederickson, K., 37-PDL-1, 362-PDL-11 Gandhi, F., 138-STR-7, 248-AS-2, 322-STR-16, Giurgiutiu, V., 207-AS-1 Grabe, C., 341-FD-41 Guo, T., 10-AFM-2, 68-GNC-4 Freeman, C., 265-MAT-6 377-AS-5 Gjerek, B., 320-SD-12 Grace, B., 184-SRE-3 Guo, Y., 66-GEPC-1, 102-AA-3 Freeto, C., 83-PC-5 Gandhi, N., 121-GNC-6 Glauser, M., 64-FD-12, 243-AMT-6, 331-AA-7 Grachev, L., 226-PDL-8 Gupta, A., 41-STR-1, 124-GTE-3, 233-TES-1, 273-PC-17, Frei, K., 377-AS-5 Gangadharan, S., 185-STR-9, 350-GT-9, 397-SD-16 Glaz, B., 88-SD-4, 364-SD-14 Grady, N., 84-PC-6 281-TES-2, 335-AMT-10/GT-8 Freihofer, G., 41-STR-1 Gangwar, P., 188-TP-4 Gleize, V., 63-FD-11 Graf, P., 285-WE-11 Gupta, R., 51-ACD-4 French, D., 211-FD-26/MVC-5 Ganji, M., 387-GNC-23 Glezer, A., 53-APA-6, 250-FD-28, 252-FD-30 Graham, J., 142-WE-5 Gursul, I., 340-FD-40 Freno, B., 381-FD-47 Gao, C., 53-APA-6, 163-GT-4, 255-FD-33 Gnanamanickam, E., 53-APA-6, 149-AMT-3 Grandhi, R., 30-MDO-1, 268-NDA-6, 391-MDO-9 Gustafson, P., 91-STR-5, 322-STR-16 Fresconi, F., 241-AFM-8 Gao, H., 59-FD-7, 305-GT-7 Gobal, K., 30-MDO-1 Granlund, K., 19-FD-2, 59-FD-7, 250-FD-28, 385-FD-51 Gutmark, E., 49-AA-2, 74-HSABP-1, 145-AA-4,

170 Frew, E., 67-GNC-3, 259-GNC-15 Gao, J., 109-AMT-2, 116-FD-15 Goebel, K., 130-NDA-3, 207-AS-1 Grant, M., 107-AFM-5 175-PC-10, 375-AA-8 Friedmann, P., 88-SD-4, 364-SD-14 Gao, X., 343-FD-43 Gogineni, S., 64-FD-12, 85-PDL-3, 243-AMT-6, Grappasonni, C., 87-SD-3 Guy, A., 382-FD-48 Friedrichs, J., 111-APA-11, 153-APA-18 Gao, Z., 383-FD-49 252-FD-30, 331-AA-7 Grasso, F., 44-WE-1, 94-WE-3 Guyer, R., 40-SD-2 Friswell, M., 148-AFM-6, 207-AS-1, 221-NDA-5, Garcia, E., 182-SE-1 Gogu, C., 134-SAT-1 Grauer, J., 148-AFM-6, 200-AFM-7 Guyton, R., 70-GT-2, 163-GT-4 298-AS-3, 339-AS-4 Garcia, J., 107-AFM-5 Gogulapati, A., 39-SD-1, 242-AFM-9, 396-SD-15 Green, B., 114-APA-14 Guzik, S., 343-FD-43 Friz, P., 38-PDL-2 Garcia, Y., 134-SAT-1 Goit, J., 189-WE-6 Green, M., 14-APA-4, 59-FD-7, 256-FD-34, 345-GEPC-4 Guzman de Villoria, R., 29-MAT-1 Fronges, L., 243-AMT-6 Garg, S., 257-GEPC-3 Gokoglu, S., 137-SRE-2 Green, N., 378-ASE-2 Haas, D., 73-HIS-2, 217-IS-1 Fu, S., 62-FD-10, 208-FD-23, 301-FD-37 Garicano Mena, J., 369-TP-13 Goldberg, U., 246-APA-27 Greenberg, J., 174-PC-9 Habashi, W., 370-WE-14 Fuchs, L., 61-FD-9, 156-FD-20 Garmann, D., 344-FD-44 Goldenstein, C., 108-AMT-1, 335-AMT-10/GT-8 Greene, P., 116-FD-15 Hablani, H., 349-GNC-22 Fuest, F., 64-FD-12, 84-PC-6 Garnier, E., 15-APA-5 Goldman, B., 397-SD-16 Greenwood, R., 20-FD-3 Habtour, E., 364-SD-14 Fujii, K., 208-FD-23, 336-APA-32, 356-MDO-8 Garon, A., 209-FD-24, 379-FD-45 Goldstein, D., 62-FD-10, 384-FD-50 Gregory, I., 68-GNC-4, 162-GNC-11 Haddad, G., 95-WE-4 Fujimoto, D., 13-APA-3 Gary, A., 151-APA-16 Golubev, V., 303-FD-39, 375-AA-8 Gregory, J., 23-GNC-1, 344-FD-44 Haddad, W., 214-GNC-13 Fujita, K., 106-AFM-4, 141-TP-2, 188-TP-4, 326-TP-11, Gary, J., 335-AMT-10/GT-8 Gomez, R., 75-ISC-4 Greitzer, E., 245-APA-26 Haddox, P., 3-ISC-1 376-AMT-12/GT-10 Gates, A., 112-APA-12 Gomez, S., 379-FD-45 Grenestedt, J., 67-GNC-3 Hafsteinsson, H., 145-AA-4, 375-AA-8 Fujiwara, Y., 352-HSABP-5 Gates, R., 148-AFM-6 Goncalves, C., 126-MAT-3 Greschik, G., 275-SCS-3, 363-SCS-5 Haftka, R., 134-SAT-1, 268-NDA-6, 391-MDO-9, Fukui, H., 141-TP-2 Gatlin, G., 110-APA-10, 206-APA-24 Gong, A., 4-ISC-2 Griffin, K., 90-STR-4, 276-SD-11 393-NDA-9 Fukushima, Y., 197-AA-5 Gaunaa, M., 237-WE-9 Gonzales, G., 305-GT-7 Griffith, D., 94-WE-3, 142-WE-5, 190-WE-7 Haga, T., 63-FD-11 Fulcher, J., 363-SCS-5 Gaydos, T., 387-GNC-23 Gonzalez, D., 156-FD-20 Grimaud, L., 385-FD-51 Hagenmaier, M., 307-HSABP-4 Fulton, J., 165-HSABP-2 Geerts, J., 262-HSABP-3 Gonzalez, P., 106-AFM-4 Grinstead, K., 146-ABPSI-2 Hahn, G., 125-MAT-2 Funes-Sebastian, D., 103-ABPSI-1, 198-ABPSI-3 Gejji, R., 35-PC-2, 164-GTE-4 Gonzalez-Linero, L., 57-DE-2 Groff, L., 162-GNC-11 Haid, L., 95-WE-4 Funk, C., 160-GNC-9 Gentz, G., 34-PC-1 Goodmiller, G., 185-STR-9 Gromyko, Y., 342-FD-42 Haimes, R., 78-MVC-2 Furuya, H., 227-SCS-2, 363-SCS-5, 377-AS-5 George, J., 150-AMT-4 Goodsell, J., 218-MAT-5 Gronvall, J., 118-FD-17 Haji Hajikolaei, K., 391-MDO-9 Fussell, J., 178-SAT-2 George, T., 26-GTE-1, 354-MAT-8 Gopalan, H., 158-FD-22, 189-WE-6 Grosbein, H., 139-STR-8 Hajj, M., 40-SD-2, 242-AFM-9, 356-MDO-8, 364-SD-14 Gaertlein, S., 303-FD-39 Georges, W., 173-PC-8 Gopalarathnam, A., 106-AFM-4, 200-AFM-7 Gross, A., 50-ACD-3, 117-FD-16, 253-FD-31, 384-FD-50, Halaas, D., 386-GEPC-5 Gaeta, R., 17-EDU-1, 350-GT-9 Georgiadis, N., 165-HSABP-2, 307-HSABP-4 Gopalaswamy, N., 255-FD-33 385-FD-51 Halbert, K., 398-STR-20 Gaffuri, M., 50-ACD-3 Gerlinger, P., 35-PC-2 Goparaju, K., 53-APA-6 Grossir, G., 305-GT-7, 376-AMT-12/GT-10 Hall, C., 17-EDU-1, 174-PC-9 Gagnon, H., 245-APA-26 German, B., 147-ACD-7 Gord, J., 108-AMT-1, 174-PC-9, 201-AMT-5/PC-11, Groth, C., 60-FD-8, 124-GTE-3, 273-PC-17 Hall, J., 232-STR-12, 243-AMT-6, 356-MDO-8 Gern, F., 66-GEPC-1 293-AMT-7, 362-PDL-11 Groves, C., 120-FD-19, 380-FD-46 Haller, W., 159-GEPC-2 Author/Session Chair Index Hallissy, B., 114-APA-14, 205-APA-23, 247-APA-28 Heiligers, J., 227-SCS-2 Hoke, J., 74-HSABP-1, 108-AMT-1, 146-ABPSI-2, Hummel, G., 353-IS-4 Jaberi, F., 317-PC-20 Halls, B., 201-AMT-5/PC-11 Heindel, T., 201-AMT-5/PC-11 271-PC-15, 352-HSABP-5, 360-PC-21/AMT-11, Humphrey, L., 217-IS-1 Jacob, J., 17-EDU-1, 199-ACD-8, 350-GT-9 Ham, F., 378-ASE-2 Heintz, K., 112-APA-12 394-PC-23 Huneault, J., 368-TP-12 Jacob, R., 223-PC-12 Hamm, W., 265-MAT-6 Heinz, S., 158-FD-22 Holguin, A., 70-GT-2 Huo, H., 175-PC-10, 317-PC-20, 394-PC-23 Jacobs, G., 253-FD-31 Han, J., 186-STR-10, 296-APA-30, 388-GNC-24 Heitzman, N., 8-ACD-2 Holland, F., 125-MAT-2 Hurst, C., 268-NDA-6 Jacobson, D., 234-TP-6 Han, Z., 379-FD-45 Heller, J., 395-SCS-6 Hollis, B., 62-FD-10, 305-GT-7 Hurtado, J., 142-WE-5, 259-GNC-15, 353-IS-4 Jacoby, M., 231-STR-11 Hancock, S., 137-SRE-2 Hellert, C., 217-IS-1 Hollkamp, J., 39-SD-1 Husen, N., 334-AMT-9 Jaffe, R., 382-FD-48 Hanke, J., 246-APA-27 Helm, C., 252-FD-30 Holloway, G., 341-FD-41 Hussey, D., 234-TP-6 Jahromi, A., 282-TP-8 Hansen, L., 28-ISC-3 Hemez, F., 358-NDA-8 Holzapfel, F., 68-GNC-4, 258-GNC-14, 347-GNC-20, Hutchins, N., 53-APA-6, 149-AMT-3 Jain, R., 55-APA-8 Hansen, M., 237-WE-9 Hemsch, M., 25-GT-1 348-GNC-21, 387-GNC-23, 389-GNC-25 Huxtable, S., 234-TP-6 Jakirlic, S., 157-FD-21 Hanson, R., 108-AMT-1, 335-AMT-10/GT-8 Hencey, B., 69-GNC-5 Holzäpfel, F., 249-ASE-1 Huynh, H., 209-FD-24, 251-FD-29 Jalali, A., 129-MVC-3 Hao, Y., 285-WE-11 Henderson, R., 20-FD-3 Honea, G., 155-DE-3 Hwang, J., 12-APA-2 James, S., 351-GTE-7 Hardalupas, Y., 173-PC-8 Henfling, J., 117-FD-16, 383-FD-49 Hong, H., 237-WE-9 Hyatt, A., 140-TP-1 James, W., 137-SRE-2 Hardaway, L., 280-STR-15 Henne, U., 390-GT-11 Hong, Y., 387-GNC-23 Hyde, D., 10-AFM-2 Jansen, B., 145-AA-4 Hariharan, N., 12-APA-2, 55-APA-8, 114-APA-14, Henriksen, L., 237-WE-9 Hooker, J., 345-GEPC-4, 386-GEPC-5 Hyer, M., 41-STR-1, 322-STR-16 Jansen, K., 31-MVC-1, 204-APA-22 205-APA-23, 247-APA-28 Henshaw, W., 189-WE-6 Hoopes, K., 146-ABPSI-2 Iaccarino, G., 79-NDA-2, 268-NDA-6 Janssen, R., 153-APA-18 Harper, B., 292-AFM-10 Hepp, A., 89-SRE-1 Hoover, J., 148-AFM-6 Ibrahim, S., 281-TES-2 Jansson, J., 246-APA-27 Harrington, A., 199-ACD-8 Hermannsson, E., 155-DE-3 Hope, D., 119-FD-18 Ickes, J., 337-APA-33 Jansson, N., 246-APA-27 Harris, R., 56-APA-9 Herzler, J., 34-PC-1 Hopkins, D., 257-GEPC-3 Ifju, P., 391-MDO-9 Jantzen, J., 16-DE-1 Harstad, K., 224-PC-13 Hesse, H., 142-WE-5, 229-SD-10 Horagiri, T., 376-AMT-12/GT-10 Ih, C., 392-MST-7 Jantzen, R., 59-FD-7 Hart, K., 200-AFM-7 Hesthaven, J., 224-PC-13 Horn, J., 259-GNC-15, 398-STR-20 Ihme, M., 36-PC-3, 84-PC-6, 164-GTE-4, 307-HSABP-4, Janus, J., 30-MDO-1 Hartfield, R., 169-MST-2 Heye, C., 272-PC-16 Horst, P., 50-ACD-3 394-PC-23 Jastifer, J., 322-STR-16 Hartl, D., 377-AS-5 Hicken, J., 30-MDO-1, 77-MDO-2 Hosder, S., 79-NDA-2, 128-MST-1, 154-APA-19, Iijima, Y., 376-AMT-12/GT-10 Jaworske, D., 354-MAT-8 Hartman, T., 322-STR-16 Hickey, J., 36-PC-3 182-SE-1, 221-NDA-5, 268-NDA-6 Ikeda, T., 13-APA-3 Jayaram, S., 17-EDU-1

171 Hartwig, J., 282-TP-8 Hicks, M., 272-PC-16 Hospers, J., 202-APA-20 Ikeda, Y., 315-PC-18 Jayaraman, B., 236-WE-8, 285-WE-11 Harursampath, D., 377-AS-5 Hidaka, A., 297-APA-31 Hossain, S., 367-TES-4 Ilie, M., 120-FD-19, 380-FD-46 Jeans, T., 341-FD-41 Harvazinski, M., 156-FD-20 Higgins, A., 173-PC-8, 368-TP-12 Houlden, H., 25-GT-1, 338-APA-34 Im, H., 216-GTE-5, 272-PC-16, 273-PC-17 Jeffries, J., 108-AMT-1, 335-AMT-10/GT-8 Hashemi, A., 140-TP-1 Hilburger, M., 231-STR-11, 278-STR-13 Housman, J., 18-FD-1, 343-FD-43 Imamura, T., 60-FD-8 Jegley, D., 66-GEPC-1, 231-STR-11, 278-STR-13 Hashimoto, A., 63-FD-11, 64-FD-12, 77-MDO-2, Hildebrand, M., 368-TP-12 Hovakimyan, N., 68-GNC-4, 162-GNC-11, 214-GNC-13, Imlay, S., 78-MVC-2 Jemcov, A., 340-FD-40 102-AA-3, 157-FD-21, 261-GT-6 Hill, J., 167-MAT-4 259-GNC-15 Inasawa, A., 13-APA-3 Jenie, Y., 388-GNC-24 Hassan, E., 156-FD-20, 307-HSABP-4 Hilton, H., 139-STR-8 Howard, K., 370-WE-14 Ingenito, A., 351-GTE-7 Jenkins, C., 363-SCS-5 Hassan, H., 111-APA-11, 165-HSABP-2 Himeno, T., 400-TES-5 Howard, M., 369-TP-13 Inman, D., 40-SD-2, 135-SD-5, 248-AS-2 Jenkins, J., 75-ISC-4 Hassanaly, M., 225-PC-14 Himmler, A., 169-MST-2 Hradil, J., 154-APA-19, 244-APA-25 Inman, J., 62-FD-10 Jenkins, T., 150-AMT-4 Hauber, B., 105-ACD-6 Hind, M., 149-AMT-3, 256-FD-34 Hrishikeshavan, V., 199-ACD-8 Innocenti, M., 389-GNC-25 Jennings, A., 128-MST-1, 242-AFM-9, 395-SCS-6 Haw, W., 74-HSABP-1 Hine, D., 114-APA-14, 247-APA-28 Hsu, K., 74-HSABP-1 Inoyama, D., 397-SD-16 Jensen, B., 126-MAT-3 Hay, A., 209-FD-24, 379-FD-45, 385-FD-51 Hinkle, J., 395-SCS-6 Hu, B., 162-GNC-11 Ioppolo, T., 149-AMT-3, 334-AMT-9 Jensen, E., 309-MAT-7 Hayhurst, D., 346-GNC-19 Hirano, Y., 339-AS-4 Hu, H., 72-GTE-2, 110-APA-10, 202-APA-20, 284-WE- Ippolito, C., 276-SD-11 Jeong, H., 308-IS-3 Haynes, R., 294-AMT-8 Hironori, T., 347-GNC-20 10, 328-WE-13 Irannejad, A., 317-PC-20 Jeong, S., 77-MDO-2, 244-APA-25 Hayward, G., 159-GEPC-2 Hitt, D., 212-FD-27/TP-5 Hu, T., 340-FD-40 Ishibashi, Y., 208-FD-23 Jewison, C., 346-GNC-19 He, C., 284-WE-10 Hitzel, S., 206-APA-24 Hu, W., 45-WE-2 Ishihara, A., 276-SD-11 Jeyapandian, E., 65-FD-13 He, F., 146-ABPSI-2 Hixon, D., 375-AA-8 Hu, Y., 111-APA-11, 151-APA-16 Ishihara, T., 369-TP-13 Jha, P., 189-WE-6, 190-WE-7 He, J., 126-MAT-3 Ho, K., 392-MST-7 Huang, A., 245-APA-26 Ishii, M., 376-AMT-12/GT-10 Ji, W., 232-STR-12 He, L., 279-STR-14 Ho, T., 305-GT-7 Huang, C., 173-PC-8 Ishiko, K., 64-FD-12, 157-FD-21 Ji, Y., 163-GT-4 Headley, J., 184-SRE-3 Hoagg, J., 16-DE-1 Huang, G., 86-PDL-4, 254-FD-32 Ito, G., 376-AMT-12/GT-10 Jia, X., 295-APA-29 Hearsey, C., 134-SAT-1, 178-SAT-2 Hochstrasser, M., 387-GNC-23 Huang, H., 279-STR-14 Ito, T., 6-AA-1 Jian, G., 173-PC-8, 223-PC-12 Heath, C., 61-FD-9 Hocking, A., 277-SOF-3 Huang, P., 395-SCS-6 Itoh, K., 118-FD-17 Jiang, B., 84-PC-6, 223-PC-12 Hebert, C., 321-SD-13 Hodge, B., 189-WE-6 Huang, Y., 210-FD-25 Iuso, G., 243-AMT-6 Jiang, F., 92-STR-6 Hedges, L., 65-FD-13 Hodges, D., 229-SD-10, 320-SD-12 Hubbard, J., 298-AS-3 Ivanou, Y., 37-PDL-1 Jiang, M., 6-AA-1 Heeb, N., 49-AA-2 Hoeijmakers, H., 202-APA-20 Hubert, P., 126-MAT-3 Ivanov, M., 187-TP-3 Jiang, N., 124-GTE-3, 174-PC-9, 201-AMT-5/PC-11, Heeg, J., 54-APA-7 Hoffman, J., 246-APA-27, 392-MST-7 Hubner, J., 11-APA-1 Iwanizki, M., 8-ACD-2 331-AA-7 Hegde, U., 137-SRE-2 Hoke, C., 327-WE-12 Huelskamp, B., 201-AMT-5/PC-11 Ixtabalan, D., 75-ISC-4 Jiang, W., 395-SCS-6 Heidmann, J., 257-GEPC-3 Humbert, J., 388-GNC-24 Iyer, P., 62-FD-10 Jiang, Z., 83-PC-5, 271-PC-15 Author/Session Chair Index Jimenez, H., 7-ACD-1 Kanazaki, M., 64-FD-12 Kelley, A., 121-GNC-6 Kirchner, R., 338-APA-34 Koo, B., 355-MAT-9 Jin, J., 255-FD-33 Kanda, A., 232-STR-12 Kelly, K., 163-GT-4 Kiris, C., 18-FD-1, 65-FD-13, 338-APA-34, 343-FD-43, Kordonowy, D., 311-NDA-7 Jin, K., 300-FD-36 Kaneshige, J., 68-GNC-4 Kelly, M., 28-ISC-3 381-FD-47 Korkut, B., 37-PDL-1 Jinks, E., 253-FD-31 Kang, C., 296-APA-30 Kemenov, K., 273-PC-17 Kirkman, W., 387-GNC-23 Körner, S., 249-ASE-1 Jirasek, A., 13-APA-3, 115-APA-15, 277-SOF-3 Kang, H., 364-SD-14 Kennedy, D., 52-AFM-3 Kirlik, A., 162-GNC-11, 214-GNC-13 Kornev, N., 50-ACD-3 Jo, Y., 244-APA-25 Kang, M., 109-AMT-2 Kennedy, G., 159-GEPC-2, 168-MDO-4 Kirtley, D., 333-AFM-11 Kosareo, D., 278-STR-13 Jodeh, N., 346-GNC-19 Kannepalli, C., 111-APA-11 Kenner, S., 92-STR-6 Kitagawa, K., 141-TP-2 Kosarev, I., 315-PC-18 Johnsen, E., 343-FD-43 Kapania, R., 43-STR-3, 51-ACD-4, 88-SD-4, 127-MDO-3, Kenny, S., 162-GNC-11, 358-NDA-8, 393-NDA-9 Kivelevitch, E., 263-IS-2 Kosel, F., 320-SD-12 Johnson, B., 72-GTE-2, 202-APA-20 138-STR-7, 266-MDO-6 Kenway, G., 154-APA-19, 159-GEPC-2 Kleb, W., 54-APA-7 Koshi, M., 83-PC-5 Johnson, C., 180-SD-7 Kapenga, J., 91-STR-5, 322-STR-16 Kerans, R., 92-STR-6 Klein, C., 390-GT-11 Kosmatka, J., 126-MAT-3 Johnson, D., 135-SD-5 Kara, K., 336-APA-32 Kerrigan, E., 142-WE-5 Kleine, H., 56-APA-9 Koster, J., 155-DE-3 Johnson, E., 214-GNC-13, 277-SOF-3, 348-GNC-21, Karagozian, A., 61-FD-9 Kessler, D., 65-FD-13, 212-FD-27/TP-5 Kleinhenz, J., 137-SRE-2, 184-SRE-3 Kostina, E., 389-GNC-25 356-MDO-8 Karatas, A., 174-PC-9 Kevin, K., 53-APA-6 Klenke, R., 128-MST-1, 263-IS-2, 277-SOF-3 Kosztowny, C., 43-STR-3 Johnson, F., 63-FD-11 Karim, H., 233-TES-1 Khalil, E., 281-TES-2, 400-TES-5 Kliment, L., 323-STR-17 Kotsonis, M., 86-PDL-4 Johnson, H., 118-FD-17 Karimian, S., 295-APA-29 Khalil Hasan, A., 124-GTE-3, 233-TES-1 Klimov, A., 141-TP-2, 256-FD-34, 340-FD-40 Kotzagianni, M., 360-PC-21/AMT-11 Johnson, M., 4-ISC-2 Karlgaard, C., 292-AFM-10 Khan, A., 43-STR-3 Kling, D., 395-SCS-6 Koudelka, J., 159-GEPC-2 Johnson, V., 159-GEPC-2 Karman, S., 31-MVC-1 Khan, M., 212-FD-27/TP-5 Klippenstein, S., 82-PC-4 Kourdis, P., 224-PC-13 Jones, A., 11-APA-1, 19-FD-2, 29-MAT-1, 385-FD-51 Karnadi, J., 8-ACD-2 Khan, O., 52-AFM-3, 297-APA-31 Klochko, A., 274-PDL-9 Koyanagi, J., 188-TP-4 Jones, K., 33-PANEL-1 Karpel, M., 181-SD-8, 190-WE-7 Khire, R., 266-MDO-6 Klock, R., 39-SD-1 Koziel, S., 77-MDO-2, 128-MST-1, 154-APA-19, Jones, S., 62-FD-10, 159-GEPC-2 Karunamoorthy, S., 17-EDU-1 Khoo, B., 110-APA-10 Klomparens, R., 302-FD-38 155-DE-3, 244-APA-25, 310-MDO-7 Jones, T., 257-GEPC-3, 354-MAT-8 Kasahara, J., 271-PC-15, 352-HSABP-5, 394-PC-23 Khoronzhuk, R., 133-PDL-5 Klyde, D., 10-AFM-2, 121-GNC-6, 162-GNC-11, Kozulovic, D., 110-APA-10 Jones, W., 77-MDO-2 Kashani-Pour, A., 95-WE-4 Khorrami, M., 66-GEPC-1 258-GNC-14 Krauskopf, B., 162-GNC-11 Jonkman, J., 95-WE-4, 142-WE-5, 328-WE-13 Kasharvazaddeh, V., 358-NDA-8 Khoshlessan, M., 295-APA-29 Knight, D., 252-FD-30, 302-FD-38 Kriegseis, J., 86-PDL-4 Joseph, A., 232-STR-12 Kashiwazaki, T., 352-HSABP-5 Khurana, S., 336-APA-32 Knight, J., 277-SOF-3 Krishnakumar, K., 68-GNC-4, 213-GNC-12

172 Joshi, D., 352-HSABP-5 Kashkovsky, A., 187-TP-3 Kicinger, R., 387-GNC-23 Knipe, K., 306-GTE-6 Kroeger, K., 308-IS-3 Joshi, P., 266-MDO-6 Kassoy, D., 394-PC-23 Kidd, J., 17-EDU-1 Knittel, J., 333-AFM-11 Kroll, N., 22-FD-5 Joshi, S., 298-AS-3 Kastengren, A., 201-AMT-5/PC-11, 316-PC-19 Kiel, B., 243-AMT-6, 331-AA-7 Knochenhauer, N., 83-PC-5 Kronenberg, A., 353-IS-4 Josyula, E., 187-TP-3, 235-TP-7 Kato, H., 261-GT-6, 311-NDA-7 Kier, Z., 138-STR-7 Ko, A., 30-MDO-1 Kroninger, C., 199-ACD-8 Jrad, M., 43-STR-3 Katsaduros, D., 4-ISC-2 Kim, B., 126-MAT-3, 217-IS-1, 260-GNC-16 Kobayashi, H., 400-TES-5 Krumbein, A., 341-FD-41 Ju, Y., 34-PC-1, 82-PC-4, 84-PC-6, 223-PC-12, Katsumata, N., 275-SCS-3 Kim, C., 209-FD-24 Koch, H., 110-APA-10 Kuchi-ishi, S., 261-GT-6 224-PC-13, 361-PC-22 Katz, A., 22-FD-5, 114-APA-14, 251-FD-29, 379-FD-45 Kim, D., 185-STR-9, 364-SD-14 Koch, R., 185-STR-9 Kudla, T., 157-FD-21 Juliano, T., 20-FD-3, 117-FD-16 Katz, J., 346-GNC-19 Kim, E., 327-WE-12 Koch, S., 103-ABPSI-1 Kudva, J., 138-STR-7, 322-STR-16 Julien, M., 63-FD-11 Kaur, A., 301-FD-37 Kim, H., 40-SD-2, 84-PC-6, 90-STR-4, 127-MDO-3, Kochersberger, K., 308-IS-3 Kuester, M., 62-FD-10 Jumper, E., 85-PDL-3 Kawai, R., 345-GEPC-4 168-MDO-4, 228-SD-9 Kochetov, I., 176-PDL-6 Kuether, R., 396-SD-15 Jung, M., 12-APA-2 Kawai, S., 208-FD-23 Kim, J., 42-STR-2, 116-FD-15, 186-STR-10, Kodera, M., 165-HSABP-2 Kuhlman, J., 187-TP-3 Junkins, J., 24-GNC-2, 392-MST-7 Kawamoto, H., 89-SRE-1 296-APA-30, 308-IS-3, 336-APA-32, 388-GNC-24 Koenig, B., 246-APA-27 Kulakhmetov, M., 283-TP-9 Justice, J., 26-GTE-1 Kaya, M., 93-SUR-1 Kim, N., 130-NDA-3, 134-SAT-1, 171-NDA-4, 268-NDA-6 Koga, S., 297-APA-31 Kulatilaka, W., 174-PC-9, 293-AMT-7, 362-PDL-11 Jutte, C., 90-STR-4, 159-GEPC-2 Kayran, A., 93-SUR-1, 328-WE-13 Kim, S., 35-PC-2, 161-GNC-10, 280-STR-15, 336-APA-32 Kogiso, N., 377-AS-5 Kulis, M., 89-SRE-1 Kabiraj, L., 164-GTE-4 Kazansky, P., 340-FD-40 Kim, T., 142-WE-5, 321-SD-13, 394-PC-23 Kokou, P., 122-GNC-7 Kulkarni, M., 127-MDO-3 Kady, C., 7-ACD-1 Kazemi, E., 158-FD-22 Kim, Y., 260-GNC-16, 387-GNC-23 Kolhe, P., 150-AMT-4 Kumar, M., 83-PC-5 Kahlen, F., 16-DE-1 Kc, U., 61-FD-9 Kimiecik, T., 83-PC-5 Kolla, H., 225-PC-14 Kumar, R., 14-APA-4 Kailasanath, K., 49-AA-2, 271-PC-15 Ke, G., 6-AA-1 Kimmel, K., 73-HIS-2 Kolmanovsky, I., 214-GNC-13, 304-GNC-17 Kumar, S., 152-APA-17 Kaiser, B., 93-SUR-1 Kealy, P., 90-STR-4 Kimmel, R., 20-FD-3, 117-FD-16, 342-FD-42 Kolonay, R., 320-SD-12, 356-MDO-8 Kumar, T., 267-MST-4 Kallo, J., 146-ABPSI-2 Kearney, S., 293-AMT-7 Kimura, S., 249-ASE-1 Kolosenok, S., 176-PDL-6 Kumar, V., 295-APA-29 Kalpathy Venkiteswaran, V., 155-DE-3 Keating, D., 357-MST-6 Kimura, T., 297-APA-31 Komadina, S., 106-AFM-4, 292-AFM-10 Kundu, A., 221-NDA-5 Kalra, T., 12-APA-2 Keck, R., 285-WE-11 Kindusheva, S., 315-PC-18 Kommers, J., 179-SCS-1, 395-SCS-6 Kundu, S., 167-MAT-4 kamal, A., 357-MST-6 Kee, Y., 364-SD-14 King, P., 74-HSABP-1, 352-HSABP-5 Komperda, J., 317-PC-20 Kuntz, D., 368-TP-12 Kambrath, P., 60-FD-8 Kegelman, J., 25-GT-1 King, R., 285-WE-11 Komurasaki, K., 376-AMT-12/GT-10 Kuo, C., 240-AA-6 Kamenetskiy, D., 63-FD-11 Kegerise, M., 62-FD-10, 210-FD-25 Kingman, D., 28-ISC-3 Komuro, T., 118-FD-17 Kuo, W., 400-TES-5 Kamita, T., 280-STR-15 Kelkar, A., 167-MAT-4 Kinney, D., 107-AFM-5 Konishi, K., 150-AMT-4 Kuranov, A., 176-PDL-6 Kan, P., 331-AA-7 Kellas, S., 278-STR-13 Kinney, T., 397-SD-16 Konokman, H., 93-SUR-1 Kurbatskii, K., 152-APA-17 Kanamori, M., 102-AA-3 Keller, E., 398-STR-20 Kipouros, T., 151-APA-16, 153-APA-18 Kontis, K., 335-AMT-10/GT-8 Kurdila, A., 23-GNC-1 Author/Session Chair Index Kuribayashi, M., 141-TP-2 LaVallee, D., 183-SOF-1, 277-SOF-3 Lewis, M., 156-FD-20, 219-MDO-5, 333-AFM-11 Liu, F., 25-GT-1, 53-APA-6, 86-PDL-4, 250-FD-28, Lukaczyk, T., 50-ACD-3, 310-MDO-7 Kurita, M., 376-AMT-12/GT-10 Lavely, A., 236-WE-8 Leyva, I., 36-PC-3 255-FD-33, 355-MAT-9 Lukatsi, M., 260-GNC-16 Kurth, T., 28-ISC-3 Lavin, T., 9-AFM-1 Lhachemi, H., 160-GNC-9 Liu, H., 67-GNC-3, 273-PC-17, 348-GNC-21, 369-TP-13 Luke, E., 56-APA-9 Kurtz, G., 354-MAT-8 Lavoie, P., 6-AA-1, 243-AMT-6 Li, C., 32-NDA-1, 82-PC-4, 132-PC-7 Liu, J., 24-GNC-2, 49-AA-2, 122-GNC-7, 349-GNC-22 Lunking, D., 223-PC-12 Kurtz, M., 156-FD-20 Lavrov, P., 226-PDL-8 Li, F., 56-APA-9, 301-FD-37 Liu, K., 41-STR-1 Luo, H., 59-FD-7, 60-FD-8, 251-FD-29, 300-FD-36 Kurz, A., 336-APA-32 Lawrence, K., 279-STR-14 Li, H., 110-APA-10, 250-FD-28 Liu, L., 169-MST-2, 395-SCS-6 Luo, L., 300-FD-36 Kushner, M., 274-PDL-9 Lawrence, M., 306-GTE-6 Li, J., 86-PDL-4, 110-APA-10, 119-FD-18, 252-FD-30, Liu, N., 367-TES-4 Luo, S., 25-GT-1, 86-PDL-4, 250-FD-28 Kustova, E., 235-TP-7 Laws, C., 71-GT-3 303-FD-39, 387-GNC-23 Liu, P., 295-APA-29 Lv, Y., 394-PC-23 Kutty, P., 292-AFM-10 Lawson, B., 121-GNC-6 Li, L., 92-STR-6, 208-FD-23 Liu, Q., 127-MDO-3 Lyddon, J., 356-MDO-8 Kuzuu, K., 63-FD-11 Lawson, S., 339-AS-4 Li, N., 142-WE-5 Liu, T., 149-AMT-3, 294-AMT-8, 334-AMT-9 Lynch, A., 124-GTE-3, 201-AMT-5/PC-11, 272-PC-16 Kwak, J., 396-SD-15 Le Bas, P., 40-SD-2 Li, T., 176-PDL-6 Liu, W., 126-MAT-3, 399-STR-21 Lynn, K., 70-GT-2 Kwon, H., 219-MDO-5, 244-APA-25 Le Bihan, B., 122-GNC-7 Li, W., 31-MVC-1, 256-FD-34 Liu, Y., 10-AFM-2, 110-APA-10, 130-NDA-3, 207-AS-1, Lyons, G., 294-AMT-8 Kwon, O., 12-APA-2, 301-FD-37 LeBeau, R., 17-EDU-1, 53-APA-6, 152-APA-17 Li, X., 6-AA-1, 109-AMT-2, 116-FD-15, 146-ABPSI-2, 265-MAT-6, 272-PC-16, 279-STR-14, 355-MAT-9, Lyrintzis, A., 49-AA-2, 375-AA-8 Lachaud, J., 368-TP-12 LeBlanc, B., 285-WE-11 201-AMT-5/PC-11, 360-PC-21/AMT-11 389-GNC-25 Lyu, Z., 154-APA-19 Lackner, M., 95-WE-4, 190-WE-7, 285-WE-11, Lebofsky, S., 228-SD-9 Li, Y., 95-WE-4, 309-MAT-7 Lizy-Destrez, S., 122-GNC-7 Ma, C., 261-GT-6 327-WE-12 Leccadito, M., 263-IS-2 Li, Z., 259-GNC-15, 326-TP-11, 357-MST-6 Löbl, D., 348-GNC-21 Ma, L., 109-AMT-2, 146-ABPSI-2, 201-AMT-5/PC-11, LaCombe, J., 52-AFM-3 Lecerf, M., 311-NDA-7 LI, C., 385-FD-51 Lobo, J., 134-SAT-1 360-PC-21/AMT-11 LaCour, T., 188-TP-4 Ledoux, S., 113-APA-13 Lian, Y., 120-FD-19, 153-APA-18, 202-APA-20 Lobser, G., 119-FD-18 Ma, X., 227-SCS-2 Lacy, D., 111-APA-11 LeDoux, S., 113-APA-13, 154-APA-19 Liang, C., 393-NDA-9 Loewen, H., 357-MST-6 Mabson, G., 366-STR-19 Lacy, T., 167-MAT-4, 357-MST-6 Lee, B., 273-PC-17 Liang, Y., 395-SCS-6 Lofthouse, A., 13-APA-3 MacDonald, W., 315-PC-18 Laﬂin, K., 295-APA-29 Lee, C., 323-STR-17 Liang, Z., 14-APA-4 Loh, W., 199-ACD-8 Macheret, S., 177-PDL-7, 386-GEPC-5 LaFontaine, J., 396-SD-15 Lee, D., 258-GNC-14 Liao, M., 398-STR-20 Lohner, R., 381-FD-47 Mackey, C., 78-MVC-2 Laforte, C., 354-MAT-8 Lee, H., 68-GNC-4, 323-STR-17 Lichodziejewski, D., 395-SCS-6 Loiseau, J., 368-TP-12 Madavan, N., 159-GEPC-2 Lai, J., 327-WE-12, 344-FD-44 Lee, J., 29-MAT-1, 139-STR-8, 280-STR-15, 388-GNC-24 Lietz, C., 225-PC-14 Lokos, W., 70-GT-2 Maddalena, L., 164-GTE-4, 262-HSABP-3

173 Lai, K., 321-SD-13 Lee, K., 122-GNC-7, 160-GNC-9, 387-GNC-23 Lieu, M., 245-APA-26 Lombaerts, T., 68-GNC-4 Maden, I., 86-PDL-4 Laiosa, J., 247-APA-28 Lee, N., 275-SCS-3, 396-SD-15 Lieuwen, T., 35-PC-2, 174-PC-9, 175-PC-10 Lombardo, M., 232-STR-12 Madenci, E., 186-STR-10, 231-STR-11, 398-STR-20 Lake, T., 204-APA-22 Lee, S., 260-GNC-16, 261-GT-6, 285-WE-11, 396-SD-15 Liever, P., 56-APA-9 Long, K., 334-AMT-9 Maduta, R., 157-FD-21 Lakshmanan, V., 164-GTE-4 Lee, T., 34-PC-1 Lignarolo, L., 189-WE-6 Long, M., 204-APA-22 Maeda, S., 394-PC-23 Lakshminarayan, V., 59-FD-7 Lee-Rausch, E., 77-MDO-2 Ligrani, P., 119-FD-18 Long, Y., 250-FD-28 Magina, N., 174-PC-9 Lam, C., 60-FD-8 Lefebvre, A., 53-APA-6 Liguore, S., 125-MAT-2, 135-SD-5 Lonkar, A., 63-FD-11 Mahadevan, S., 32-NDA-1, 79-NDA-2, 130-NDA-3, Lambert, T., 250-FD-28 Lefkowitz, J., 315-PC-18, 361-PC-22 Lillard, R., 118-FD-17 Lopes, L., 66-GEPC-1, 102-AA-3 311-NDA-7 Lammering, T., 105-ACD-6 Leger, T., 255-FD-33 Lilley, D., 367-TES-4, 400-TES-5 Lopes, M., 148-AFM-6 Mahak, M., 49-AA-2 Lampton, A., 121-GNC-6, 213-GNC-12, 258-GNC-14 Lei, Y., 23-GNC-1 Lillian, C., 205-APA-23 Loseille, A., 129-MVC-3 Mahesh, K., 62-FD-10 Lan Sun Luk, J., 86-PDL-4 Lei, Z., 147-ACD-7 Lim, D., 370-WE-14 Loth, E., 332-ABPSI-5, 351-GTE-7 Mahmood, R., 207-AS-1 Langel, C., 62-FD-10 Leicht, T., 251-FD-29 Lim, T., 24-GNC-2 Loukides, D., 16-DE-1 Mainini, L., 391-MDO-9 Langelaan, J., 67-GNC-3, 259-GNC-15 Leifsson, L., 77-MDO-2, 128-MST-1, 154-APA-19, Lim Ee Wei, K., 50-ACD-3 Love, N., 233-TES-1, 367-TES-4, 400-TES-5 Majamaki, A., 297-APA-31 Langer, S., 22-FD-5 155-DE-3, 244-APA-25, 310-MDO-7 Limbach, C., 37-PDL-1 Lovejoy, A., 231-STR-11 Majdalani, J., 3-ISC-1 Langford, J., 348-GNC-21 Lempert, W., 37-PDL-1, 177-PDL-7, 223-PC-12, Lin, I., 28-ISC-3 Lowe, J., 93-SUR-1 Makino, F., 203-APA-21 Lani, A., 369-TP-13 274-PDL-9, 361-PC-22, 362-PDL-11 Lin, K., 316-PC-19, 399-STR-21 Lowe, K., 62-FD-10, 146-ABPSI-2, 294-AMT-8, 331-AA-7 Makino, Y., 8-ACD-2 Lappas, V., 227-SCS-2, 395-SCS-6 Lemu, H., 391-MDO-9 Lind, R., 242-AFM-9 Lowe, T., 294-AMT-8 Makovkin, D., 67-GNC-3 Lapushkina, T., 226-PDL-8 Lenfers, C., 111-APA-11, 153-APA-18 Linehan, T., 350-GT-9 Lowenberg, M., 162-GNC-11, 241-AFM-8 Malawy, R., 214-GNC-13 Laricchiuta, A., 382-FD-48 Leong, C., 44-WE-1, 303-FD-39 Ling, Y., 32-NDA-1 Lowery, A., 400-TES-5 Maldonado, S., 367-TES-4 Lasagna, D., 243-AMT-6 Leonov, S., 37-PDL-1, 176-PDL-6, 177-PDL-7, Linne, D., 89-SRE-1, 137-SRE-2 Lu, F., 352-HSABP-5 Malecek, J., 181-SD-8 Lashkov, V., 133-PDL-5 223-PC-12, 262-HSABP-3, 361-PC-22 Liou, W., 255-FD-33 Lu, P., 258-GNC-14, 304-GNC-17 Maley, J., 241-AFM-8 Laten, J., 53-APA-6 Lesieutre, D., 15-APA-5, 56-APA-9 Lipinski, D., 242-AFM-9 LU, Y., 116-FD-15 Malik, M., 118-FD-17, 257-GEPC-3, 301-FD-37 Latz, J., 151-APA-16 Lesieutre, G., 207-AS-1 Lisowski, J., 346-GNC-19 Lua, J., 279-STR-14, 366-STR-19 Malkov, E., 187-TP-3 Lau, F., 207-AS-1 Leslie, C., 184-SRE-3 Litke, P., 146-ABPSI-2 Lucht, R., 35-PC-2, 201-AMT-5/PC-11, 293-AMT-7, Malla, R., 229-SD-10, 396-SD-15 Laun, M., 133-PDL-5 Lester, M., 148-AFM-6 Litt, J., 10-AFM-2 360-PC-21/AMT-11 Mallik, W., 51-ACD-4 Laurendeau, E., 152-APA-17, 246-APA-27, 295-APA-29 Levin, D., 37-PDL-1, 326-TP-11 Little, J., 65-FD-13, 250-FD-28 Lückerat, R., 369-TP-13 Malo-Molina, F., 165-HSABP-2, 307-HSABP-4 Laux, C., 361-PC-22 Levy, W., 182-SE-1 Liu, C., 51-ACD-4, 119-FD-18, 253-FD-31, 301-FD-37, Luckring, J., 115-APA-15, 206-APA-24 Mamessier, S., 162-GNC-11 Lavagnoli, S., 350-GT-9 Lewalle, J., 331-AA-7 369-TP-13, 384-FD-50 Lugo, R., 107-AFM-5 Manar, F., 385-FD-51 Laval, J., 157-FD-21 Lewis, J., 367-TES-4 Luhar, M., 384-FD-50 Mancini, P., 19-FD-2 Author/Session Chair Index Mandalia, A., 107-AFM-5 Matsunuma, T., 299-FD-35 McWilliams, K., 357-MST-6 Miranda, J., 124-GTE-3 Morioka, N., 105-ACD-6 Mandell, J., 45-WE-2 Matsuo, A., 352-HSABP-5, 394-PC-23 McWithey, M., 335-AMT-10/GT-8 Mirocha, J., 189-WE-6 Morita, K., 249-ASE-1 Manero, A., 306-GTE-6 Matsuo, Y., 157-FD-21, 363-SCS-5 Medida, S., 12-APA-2, 157-FD-21, 327-WE-12 Misaka, T., 197-AA-5, 249-ASE-1 Morita, Y., 57-DE-2 Mani, K., 22-FD-5, 151-APA-16 Matsuoka, K., 352-HSABP-5 Mehdi, B., 259-GNC-15 Mitchell, S., 353-IS-4 Morozumi, T., 352-HSABP-5 Mani, M., 22-FD-5, 295-APA-29 Matsuyama, S., 83-PC-5 Meheut, M., 154-APA-19, 244-APA-25 Mitchell, W., 331-AA-7 Morrida, J., 14-APA-4 Maniaci, D., 44-WE-1, 62-FD-10, 94-WE-3, 285-WE-11 Mattei, M., 258-GNC-14 Mehiel, E., 357-MST-6 Mitsuo, K., 376-AMT-12/GT-10 Morris, C., 223-PC-12, 228-SD-9, 338-APA-34 Mankbadi, M., 165-HSABP-2 Matula, N., 381-FD-47 Mehmani, A., 266-MDO-6, 391-MDO-9 Mittal, A., 370-WE-14 Morris, M., 350-GT-9 Mansour, N., 325-TP-10, 368-TP-12 Maughmer, M., 203-APA-21 Mehta, M., 338-APA-34 Miura, K., 364-SD-14 Morris, P., 145-AA-4, 375-AA-8 Mantell, S., 370-WE-14 Mavriplis, D., 22-FD-5, 151-APA-16, 204-APA-22, Mehta, T., 397-SD-16 Miyaji, K., 65-FD-13, 208-FD-23 Morris, S., 202-APA-20 Manuel, L., 94-WE-3, 236-WE-8, 327-WE-12 285-WE-11, 379-FD-45, 380-FD-46 Meid, C., 306-GTE-6 Miyakoshi, K., 102-AA-3 Morrison, J., 54-APA-7 Manzo, M., 334-AMT-9 Mavris, D., 30-MDO-1, 57-DE-2, 105-ACD-6, 182-SE-1, Meier, W., 84-PC-6 Miyazaki, K., 6-AA-1 Mortazavi, M., 252-FD-30 Maqbool, D., 188-TP-4 217-IS-1, 323-STR-17 Mellquist, E., 180-SD-7 Miyazaki, T., 376-AMT-12/GT-10 Morton, S., 114-APA-14, 205-APA-23 Marchant, D., 72-GTE-2 May, G., 251-FD-29 Melo De Sousa, J., 73-HIS-2, 344-FD-44 Miyazato, Y., 150-AMT-4, 253-FD-31 Mosahebi, A., 152-APA-17 Mardanpour, P., 229-SD-10 May, R., 68-GNC-4 Meloy, J., 149-AMT-3 Miyazawa, Y., 347-GNC-20 Moser, R., 358-NDA-8 Marineau, E., 261-GT-6, 335-AMT-10/GT-8 Mayhew, M., 242-AFM-9 Memon, M., 256-FD-34 Moarref, R., 384-FD-50 Mosier, K., 75-ISC-4 Marinov, D., 274-PDL-9 Mayle, M., 338-APA-34 Mendonca, M., 317-PC-20, 383-FD-49 Mochel, L., 13-APA-3 Mosquera, A., 207-AS-1 Marinov, I., 176-PDL-6 McCafferty, J., 260-GNC-16 Meng, D., 279-STR-14 Modarres-Sadeghi, Y., 327-WE-12 Motoda, T., 106-AFM-4 Mark, H., 16-DE-1 McCarthy, B., 346-GNC-19 Meng, X., 25-GT-1, 86-PDL-4, 250-FD-28, 256-FD-34 Moder, J., 257-GEPC-3 Motoe, M., 83-PC-5 Marpu, R., 55-APA-8 McCarthy, P., 118-FD-17 Menon, A., 323-STR-17 Modgil, G., 30-MDO-1, 221-NDA-5 Mott, D., 253-FD-31 Márquez Gutiérrez, C., 153-APA-18 McCaslin, J., 316-PC-19 Menon, S., 35-PC-2, 84-PC-6, 224-PC-13, 225-PC-14, Moeller, T., 318-PDL-10 Motta-Mena, J., 190-WE-7 Marschall, J., 141-TP-2 McCloskey, A., 366-STR-19 384-FD-50 Mohajerani, M., 357-MST-6 Mottershead, J., 90-STR-4 Marsh, R., 367-TES-4 McColl, C., 398-STR-20 Merk, J., 122-GNC-7 Mohamed, D., 233-TES-1 Mueller, M., 273-PC-17 Marshall, C., 341-FD-41 McComas, A., 14-APA-4 Merkle, C., 318-PDL-10 Mohamed, M., 169-MST-2 Mueller, R., 23-GNC-1 Marshall, N., 28-ISC-3 McCracken, A., 200-AFM-7 Merlen, A., 15-APA-5 Mohammed Taifour, A., 350-GT-9 Muennix, J., 105-ACD-6

174 Martha, C., 49-AA-2, 375-AA-8 McDaniel, D., 114-APA-14, 205-APA-23, 247-APA-28 Merrett, C., 52-AFM-3, 139-STR-8 Mohseni, K., 18-FD-1, 19-FD-2, 203-APA-21, 242-AFM-9, Muir, E., 88-SD-4 Martin, A., 325-TP-10, 368-TP-12 McDaniel, J., 165-HSABP-2, 262-HSABP-3 Meshkat, L., 80-OPS-1 341-FD-41, 350-GT-9, 379-FD-45 Muir, M., 168-MDO-4 Martin, C., 27-HIS-1, 73-HIS-2 McDonald, E., 87-SD-3 Messac, A., 266-MDO-6, 391-MDO-9 Moini-Yekta, S., 18-FD-1, 152-APA-17 Mukherjee, R., 65-FD-13, 295-APA-29 Martin, J., 204-APA-22 McDonald, R., 9-AFM-1, 104-ACD-5, 147-ACD-7, Messina, T., 56-APA-9 Monegato, G., 244-APA-25 Mulani, S., 127-MDO-3, 266-MDO-6 Martin, M., 141-TP-2, 188-TP-4, 212-FD-27/TP-5 151-APA-16 Meyer, S., 35-PC-2 Monfort, J., 201-AMT-5/PC-11 Mulder, J., 3-ISC-1 Martin, P., 119-FD-18, 252-FD-30, 255-FD-33 McDonough, K., 214-GNC-13 Meyer, T., 201-AMT-5/PC-11, 360-PC-21/AMT-11 Moni, A., 16-DE-1 Mullins, J., 32-NDA-1, 311-NDA-7 Martin, R., 278-STR-13 McEachen, M., 227-SCS-2 Meyers, J., 189-WE-6 Monner, H., 339-AS-4, 377-AS-5 Munday, D., 49-AA-2, 175-PC-10 Martins, B., 126-MAT-3 McFarland, J., 311-NDA-7, 393-NDA-9 Michael, J., 201-AMT-5/PC-11, 360-PC-21/AMT-11 Monroe, J., 234-TP-6 Mundis, N., 379-FD-45 Martins, J., 154-APA-19, 159-GEPC-2 McGahan, C., 108-AMT-1 Michaeli, M., 139-STR-8 Montella, C., 67-GNC-3 Munipalli, R., 224-PC-13 Marzocca, P., 87-SD-3, 112-APA-12, 320-SD-12 McGinley, C., 303-FD-39 Michal, T., 129-MVC-3 Monty, J., 53-APA-6, 149-AMT-3 Munson, M., 199-ACD-8 Masati, A., 38-PDL-2 McGowan, D., 248-AS-2 Michelis, T., 86-PDL-4 Mooij, E., 24-GNC-2, 69-GNC-5 Murakami, K., 261-GT-6 Mashayek, F., 253-FD-31, 317-PC-20 McGrath, B., 15-APA-5, 121-GNC-6 Micol, J., 261-GT-6 Moon, J., 236-WE-8 Muralidharan, B., 225-PC-14 Mashek, I., 133-PDL-5 McInnes, C., 227-SCS-2 Mignolet, M., 39-SD-1, 136-SD-6 Moore, J., 139-STR-8, 159-GEPC-2, 395-SCS-6 Murayama, M., 63-FD-11 Massa, L., 133-PDL-5, 165-HSABP-2 McKean, J., 91-STR-5, 322-STR-16 Mihaescu, M., 156-FD-20 Moore, M., 147-ACD-7 Murphey, T., 275-SCS-3 Massey, K., 151-APA-16 McKeon, B., 384-FD-50 Miles, R., 37-PDL-1, 38-PDL-2, 86-PDL-4, 150-AMT-4, Mora, N., 8-ACD-2 Murray, J., 244-APA-25 Masson, P., 106-AFM-4 McLaughlin, D., 145-AA-4, 240-AA-6 177-PDL-7, 362-PDL-11 Mora-Camino, F., 304-GNC-17, 346-GNC-19 Murray, N., 49-AA-2, 145-AA-4, 294-AMT-8 Masternak, T., 346-GNC-19 McLaughlin, T., 53-APA-6, 65-FD-13, 119-FD-18, Miller, B., 39-SD-1, 88-SD-4 Morajkar, R., 302-FD-38 Murri, D., 148-AFM-6 Masters, J., 31-MVC-1, 203-APA-21 250-FD-28 Miller, D., 45-WE-2, 208-FD-23, 346-GNC-19 Morales, M., 217-IS-1 Murua, J., 200-AFM-7 Mastorakos, E., 272-PC-16, 360-PC-21/AMT-11 McManus, K., 316-PC-19 Miller, E., 70-GT-2 Moralev, I., 256-FD-34, 340-FD-40 Muse, J., 213-GNC-12 Masud, J., 52-AFM-3, 120-FD-19, 297-APA-31, McManus, L., 4-ISC-2 Miller, F., 282-TP-8 Moreau, E., 38-PDL-2, 86-PDL-4, 299-FD-35 Muto, D., 36-PC-3 316-PC-19 McManus, T., 84-PC-6 Miller, J., 87-SD-3, 201-AMT-5/PC-11 Morell, S., 119-FD-18 Myers, D., 278-STR-13 Mataczynski, M., 146-ABPSI-2 McMillan, M., 146-ABPSI-2 Miller, M., 292-AFM-10 Morelli, E., 128-MST-1, 148-AFM-6, 162-GNC-11, Myers, L., 240-AA-6 Mateescu, D., 11-APA-1 McNamara, J., 39-SD-1, 88-SD-4, 136-SD-6, Mills, M., 335-AMT-10/GT-8 242-AFM-9 Myers, O., 357-MST-6 Mathews, E., 85-PDL-3 242-AFM-9, 396-SD-15 Millwater, H., 3-ISC-1, 171-NDA-4 Moreno, R., 180-SD-7 Myre, D., 234-TP-6 Matida, E., 190-WE-7 McNunn, G., 78-MVC-2 Min, J., 322-STR-16 Morgan, P., 54-APA-7, 342-FD-42 Myrent, N., 190-WE-7 Matlik, J., 125-MAT-2, 218-MAT-5, 265-MAT-6 McQuillen, J., 282-TP-8 Mineiro, M., 178-SAT-2 Morgan, T., 201-AMT-5/PC-11 Nadarajah, S., 113-APA-13, 154-APA-19, 251-FD-29 Matney, A., 136-SD-6 McQuilling, M., 119-FD-18, 152-APA-17, 208-FD-23, Minger, W., 227-SCS-2 Moriarty, P., 189-WE-6, 285-WE-11 Nagai, H., 106-AFM-4, 203-APA-21, 376-AMT-12/GT-10 Matsumura, T., 268-NDA-6, 393-NDA-9 252-FD-30 Minghang, L., 151-APA-16 Morimoto, N., 188-TP-4 Nagai, S., 297-APA-31 Author/Session Chair Index Nagata, Y., 356-MDO-8 Newton, C., 28-ISC-3 Odaguil, F., 339-AS-4 Ozcer, I., 370-WE-14 Pashchina, A., 141-TP-2 Nagel, J., 393-NDA-9 Ng, B., 142-WE-5, 328-WE-13 Odegard, G., 29-MAT-1, 126-MAT-3 Packwood, A., 110-APA-10 Pass, J., 178-SAT-2 Nagendra, K., 59-FD-7 Ng, H., 220-MST-3, 387-GNC-23 Oefelein, J., 36-PC-3, 83-PC-5 Pado, L., 125-MAT-2 Patelli, E., 393-NDA-9 Naik, R., 354-MAT-8 Ng, L., 219-MDO-5 Offenberger, S., 167-MAT-4 Paez, T., 32-NDA-1 Paterson, E., 236-WE-8 Naik, S., 293-AMT-7, 360-PC-21/AMT-11 Ng, W., 294-AMT-8, 331-AA-7 Ogasawara, T., 188-TP-4 Page, J., 102-AA-3 Patibandla, S., 128-MST-1 Naiman, H., 111-APA-11 Ngo, T., 348-GNC-21 Ogawa, H., 165-HSABP-2 Pagnozzi, D., 347-GNC-20 Patil, M., 9-AFM-1, 127-MDO-3 Nair, A., 343-FD-43 Nguyen, D., 228-SD-9, 276-SD-11 Ogino, Y., 292-AFM-10, 369-TP-13 Pai, D., 38-PDL-2 Patil, V., 326-TP-11 Najaﬁ, A., 91-STR-5, 138-STR-7, 167-MAT-4 Nguyen, H., 94-WE-3 Ohnishi, N., 292-AFM-10, 369-TP-13 Pai, M., 316-PC-19 Patterson, M., 37-PDL-1, 147-ACD-7, 391-MDO-9 Najm, H., 393-NDA-9 Nguyen, M., 356-MDO-8 Ohtani, K., 102-AA-3 Palacios, F., 63-FD-11, 140-TP-1, 310-MDO-7 Paul, M., 85-PDL-3, 252-FD-30 Nakahashi, K., 197-AA-5, 249-ASE-1 Nguyen, N., 123-GNC-8, 139-STR-8, 228-SD-9, Oka, T., 150-AMT-4, 253-FD-31 Palacios, R., 142-WE-5, 229-SD-10, 328-WE-13 Paul, R., 200-AFM-7 Nakajima, R., 150-AMT-4 276-SD-11, 347-GNC-20 Okada, K., 208-FD-23 Palar, P., 203-APA-21 Paxson, D., 74-HSABP-1, 146-ABPSI-2, 352-HSABP-5 Nakajima, T., 376-AMT-12/GT-10 Nguyen, T., 271-PC-15 Okai, K., 400-TES-5 Palaszewski, B., 137-SRE-2 Peace, J., 352-HSABP-5 Nakakita, K., 376-AMT-12/GT-10 Nguyen Sy, N., 139-STR-8 Okamoto, K., 240-AA-6 Palazotto, A., 26-GTE-1 Peck, J., 368-TP-12 Nakanishi, Y., 240-AA-6 Nickel, E., 75-ISC-4 Okolo, W., 148-AFM-6 Palchekovskaya, N., 302-FD-38 Peck, M., 69-GNC-5 Nakazawa, H., 141-TP-2 Nickels, A., 243-AMT-6 Okuizumi, N., 227-SCS-2, 275-SCS-3 Palframan, M., 161-GNC-10 Peddiraju, P., 65-FD-13 Nambu, T., 151-APA-16 Nickol, C., 66-GEPC-1 Okunuki, T., 240-AA-6 Palluconi, S., 149-AMT-3 Peddu, A., 397-SD-16 Namura, N., 244-APA-25 Nielsen, E., 77-MDO-2 Ol, M., 13-APA-3, 19-FD-2, 59-FD-7 Palpandian, S., 344-FD-44 Peele, O., 266-MDO-6 Nandi, T., 236-WE-8 Nielsen, T., 209-FD-24 Olcmen, S., 80-OPS-1, 150-AMT-4, 335-AMT-10/GT-8 Panahi, A., 11-APA-1 Peeters, D., 365-STR-18 Nangia, R., 113-APA-13 Niestroy, M., 386-GEPC-5 Olejniczak, J., 118-FD-17 Pancheshnyi, S., 315-PC-18 Pei, J., 241-AFM-8 Naoumov, V., 16-DE-1, 83-PC-5 Nieuwenhuizen, F., 220-MST-3 Olgun, M., 328-WE-13 Panda, P., 201-AMT-5/PC-11 Peigin, S., 154-APA-19 Napartovich, A., 176-PDL-6 Nigam, N., 157-FD-21 Olivari, M., 220-MST-3 Pandit, J., 234-TP-6 Pelech, S., 162-GNC-11 Naples, A., 74-HSABP-1 Nikipelov, A., 315-PC-18 Oliver, S., 278-STR-13 Pandya, S., 245-APA-26 Pellegrino, S., 275-SCS-3 Napolitano, M., 121-GNC-6 Ning, A., 285-WE-11 Ollivier Gooch, C., 129-MVC-3 Panerai, F., 325-TP-10 Pelletier, D., 209-FD-24, 379-FD-45, 385-FD-51 Narayanan Nampy, S., 280-STR-15 Nishikawa, H., 22-FD-5 Olson, G., 218-MAT-5 Panesi, M., 382-FD-48 Pendse, V., 159-GEPC-2

175 Narayanaswamy, V., 253-FD-31 Nitzsche, F., 190-WE-7, 276-SD-11 Oltman, R., 267-MST-4 Pang, Z., 87-SD-3 Peng, D., 344-FD-44 Narducci, R., 55-APA-8 Noack, B., 243-AMT-6 Ombrello, T., 36-PC-3, 74-HSABP-1, 361-PC-22 Paniagua, G., 72-GTE-2, 350-GT-9, 352-HSABP-5 Peng, S., 60-FD-8 Natarajan, K., 344-FD-44 Noble, D., 175-PC-10, 305-GT-7 Onishi, K., 105-ACD-6 Panickar, P., 49-AA-2 Peng, T., 130-NDA-3, 207-AS-1 Natori, M., 275-SCS-3 Nobleheart, W., 276-SD-11 Ono, D., 150-AMT-4, 253-FD-31 Pankaj, P., 232-STR-12 Peni, T., 304-GNC-17 Naughton, B., 285-WE-11, 328-WE-13 Nogar, S., 242-AFM-9 Ono, G., 227-SCS-2 Pankonien, A., 248-AS-2 Penmetsa, R., 171-NDA-4 Naughton, J., 149-AMT-3, 243-AMT-6, 256-FD-34, Noll, B., 369-TP-13 Onoue, K., 190-WE-7 Panourgias, K., 379-FD-45 Penn, J., 169-MST-2 334-AMT-9 Nompelis, I., 18-FD-1 Oppenheimer, M., 388-GNC-24 Papadopoulos, A., 65-FD-13 Pepe, R., 369-TP-13 Naumann, C., 34-PC-1 Nomura, S., 141-TP-2, 376-AMT-12/GT-10 Opperman, R., 122-GNC-7 Papageorge, M., 64-FD-12, 84-PC-6 Pepin, J., 32-NDA-1 Navarro, R., 28-ISC-3 Nonomura, T., 208-FD-23, 336-APA-32, 356-MDO-8 Orazi, M., 243-AMT-6 Papamoschou, D., 145-AA-4, 197-AA-5 Peraza Hernandez, E., 377-AS-5 Navratil, J., 154-APA-19, 244-APA-25 Norde, E., 202-APA-20 Ordaz, I., 31-MVC-1 Papoutsakis, A., 18-FD-1 Perino, S., 397-SD-16 Nawaz, A., 305-GT-7 Norman, P., 235-TP-7, 283-TP-9 Orkwis, P., 211-FD-26/MVC-5 Paquette, J., 285-WE-11 Perrin, M., 382-FD-48 Nawroth, H., 164-GTE-4 Norris, S., 189-WE-6 Oskay, C., 41-STR-1, 218-MAT-5 Paredes, P., 20-FD-3 Perron, J., 354-MAT-8 Nayani, S., 31-MVC-1 Northrup, M., 298-AS-3 Ostermann, F., 303-FD-39 Parezanovic, V., 243-AMT-6 Perry, B., 136-SD-6, 160-GNC-9 Nayeri, C., 110-APA-10, 256-FD-34, 303-FD-39 Nozak, D., 112-APA-12 Osusky, L., 154-APA-19 Parham, J., 392-MST-7 Peter, F., 347-GNC-20, 389-GNC-25 Nayfeh, A., 242-AFM-9 Nugroho, B., 53-APA-6 Osusky, M., 63-FD-11 Parikh, A., 149-AMT-3 Peter, J., 154-APA-19 Nazarian, A., 281-TES-2 Numata, D., 334-AMT-9 Ota, Y., 105-ACD-6 Paris, S., 376-AMT-12/GT-10 Peters, M., 160-GNC-9 Neild, S., 162-GNC-11 Nuthi, P., 9-AFM-1, 148-AFM-6 Oterkus, S., 186-STR-10 Park, B., 161-GNC-10 Peterson, B., 306-GTE-6 Neitzke, K., 220-MST-3 Nutsugah, R., 188-TP-4 Otugen, V., 149-AMT-3 Park, C., 171-NDA-4, 393-NDA-9 Peterson, D., 307-HSABP-4 Nelson, J., 284-WE-10, 323-STR-17 O’Brien, K., 335-AMT-10/GT-8 Ouellette, J., 9-AFM-1 Park, J., 209-FD-24, 260-GNC-16 Petrishchev, V., 177-PDL-7 Nelson, M., 146-ABPSI-2 O’Brien, T., 74-HSABP-1 Owen, A., 10-AFM-2, 163-GT-4 Park, M., 31-MVC-1, 302-FD-38 Pettit, G., 160-GNC-9 Nemec, M., 152-APA-17, 228-SD-9 O’Brien, W., 146-ABPSI-2 Owen, G., 108-AMT-1 Park, S., 122-GNC-7 Phan, N., 398-STR-20 Nemer, M., 109-AMT-2 O’Connor, J., 175-PC-10, 317-PC-20 Owen, K., 163-GT-4 Parker, J., 277-SOF-3 Phillips, D., 232-STR-12 Nesbit, B., 311-NDA-7 O’Hara, P., 39-SD-1 Owens, B., 142-WE-5, 190-WE-7 Parkhurst, J., 28-ISC-3 Phillips, T., 380-FD-46 Neuman, J., 34-PC-1 Obayashi, S., 77-MDO-2, 102-AA-3, 197-AA-5, Owkes, M., 316-PC-19 Parrish, J., 30-MDO-1 Phlipot, G., 39-SD-1 Newman, B., 160-GNC-9 244-APA-25, 249-ASE-1, 311-NDA-7, 350-GT-9 Oyama, A., 356-MDO-8 Parsons, N., 326-TP-11 Pickering, B., 300-FD-36 Newman, M., 121-GNC-6 Oberkampf, W., 54-APA-7 Oyori, H., 57-DE-2, 105-ACD-6 Paryz, R., 261-GT-6, 390-GT-11 Pickering, S., 29-MAT-1 Newman, R., 121-GNC-6, 162-GNC-11 Ochs, B., 84-PC-6 Ozawa, T., 326-TP-11 Paschereit, C., 110-APA-10, 164-GTE-4, 256-FD-34, Piekiel, N., 223-PC-12 Newsom, J., 180-SD-7, 241-AFM-8 Ochterbeck, J., 188-TP-4 Ozbay, A., 284-WE-10, 328-WE-13 303-FD-39 Pierce, M., 75-ISC-4 Author/Session Chair Index Pierce, S., 258-GNC-14 Pritchett, A., 104-ACD-5, 162-GNC-11 Ranatunga, V., 366-STR-19, 398-STR-20, 399-STR-21 Rhudy, M., 121-GNC-6 Rooney, B., 247-APA-28 Pierre, D., 252-FD-30 Pritchett, V., 338-APA-34 Rancourt, D., 217-IS-1, 323-STR-17 Ribert, G., 83-PC-5 Rosas, J., 29-MAT-1 Pietanza, L., 382-FD-48 Probe, A., 24-GNC-2, 75-ISC-4, 392-MST-7 Randt, N., 8-ACD-2, 182-SE-1 Ricci, S., 115-APA-15, 339-AS-4 Rose, C., 231-STR-11 Pilon, A., 102-AA-3, 145-AA-4 Proctor, F., 249-ASE-1 Ranjan, R., 384-FD-50 Ricciardi, G., 385-FD-51 Rose, M., 377-AS-5 Pineda, E., 125-MAT-2, 265-MAT-6, 278-STR-13 Pruett, B., 335-AMT-10/GT-8, 383-FD-49 Rankin, B., 271-PC-15 Riccobene, L., 115-APA-15 Rosema, C., 15-APA-5 Pinier, J., 115-APA-15, 338-APA-34 Przekop, A., 280-STR-15 Ransbury, P., 267-MST-4 Rice, B., 262-HSABP-3 Rosenzweig, S., 386-GEPC-5 Pinto, J., 387-GNC-23 Przekwas, A., 21-FD-4 Raps, D., 249-ASE-1 Rich, J., 37-PDL-1 Roska, T., 160-GNC-9 Pioton, J., 350-GT-9 Psarras, P., 89-SRE-1 Raska, V., 258-GNC-14 Richard, L., 399-STR-21 Rossman, G., 188-TP-4 Pipenberg, B., 203-APA-21 Pulcini, A., 362-PDL-11 Rasquin, M., 31-MVC-1, 204-APA-22 Richard, P., 243-AMT-6 Rossmann, T., 158-FD-22 Pipes, R., 218-MAT-5, 265-MAT-6 Puneria, V., 129-MVC-3 Rassaian, M., 365-STR-18 Richards, N., 10-AFM-2, 121-GNC-6 Roth, G., 205-APA-23 Pirrera, A., 94-WE-3 Purinton, D., 338-APA-34 Rausch, R., 338-APA-34 Richardson, D., 124-GTE-3, 150-AMT-4, 272-PC-16 Rothmayer, A., 202-APA-20 Pitt, D., 88-SD-4, 181-SD-8 Puyou, G., 162-GNC-11 Ravaev, A., 226-PDL-8 Richarz, W., 6-AA-1 Rouch, M., 134-SAT-1 Pitz, R., 84-PC-6, 174-PC-9 Pyatnitsky, L., 256-FD-34 Raveh, D., 180-SD-7 Richter, M., 347-GNC-20, 387-GNC-23 Rouff, C., 353-IS-4 Pizzaia, A., 158-FD-22 Pytel, D., 283-TP-9, 326-TP-11 Ravindra, K., 58-EDU-2 Ricks, K., 184-SRE-3 Rouhi, M., 266-MDO-6, 365-STR-18 Platts, W., 89-SRE-1 Qamar, I., 232-STR-12 Ray, A., 398-STR-20 Ricks, T., 357-MST-6 Rousseau, A., 176-PDL-6 Platzer, M., 344-FD-44 Qi, N., 389-GNC-25 Ray, G., 260-GNC-16 Riddick, J., 364-SD-14 Rovey, J., 38-PDL-2, 133-PDL-5 Plemmons, D., 335-AMT-10/GT-8, 376-AMT-12/GT-10 Qidwai, S., 65-FD-13 Receveur, J., 122-GNC-7 Riddle, T., 284-WE-10 Rovinelli, A., 125-MAT-2 Plesniak, M., 64-FD-12, 384-FD-50 Qu, Q., 295-APA-29 Red-Horse, J., 358-NDA-8 Rieck, R., 347-GNC-20 Rowe, S., 57-DE-2 Poehlmann, F., 150-AMT-4 Quackenbush, J., 356-MDO-8 Reda, D., 140-TP-1 Riedel, U., 34-PC-1 Rowton, A., 146-ABPSI-2 Poggie, J., 116-FD-15, 118-FD-17, 255-FD-33, Querin, O., 168-MDO-4 Reddy, R., 387-GNC-23 Rigby, D., 265-MAT-6 Roy, C., 32-NDA-1, 300-FD-36, 380-FD-46 318-PDL-10 Quest, J., 390-GT-11 Reed, H., 245-APA-26, 254-FD-32, 297-APA-31 Riggins, D., 128-MST-1 Roy, S., 29-MAT-1, 86-PDL-4, 124-GTE-3, 126-MAT-3, Polanka, M., 124-GTE-3, 146-ABPSI-2, 272-PC-16 Quijano, O., 56-APA-9 Reed, J., 69-GNC-5 Riha, D., 393-NDA-9 201-AMT-5/PC-11, 293-AMT-7, 362-PDL-11, 377-AS-5 Politovich, M., 249-ASE-1 Quintana, C., 171-NDA-4 Reed, S., 347-GNC-20 Rimoli, J., 93-SUR-1 Roy, V., 11-APA-1 Pollini, L., 161-GNC-10, 220-MST-3, 389-GNC-25 Quix, H., 390-GT-11 Reeh, A., 342-FD-42 Ringuette, M., 19-FD-2 Roybal, M., 185-STR-9

176 Poniaev, S., 226-PDL-8 Raab, C., 200-AFM-7 Rege, A., 242-AFM-9 Ringuette, S., 173-PC-8 Rubio, J., 396-SD-15 Pontecorvo, M., 138-STR-7, 322-STR-16 Radespiel, R., 111-APA-11, 301-FD-37 Regele, J., 156-FD-20 Rinoie, K., 8-ACD-2 Rudenko, A., 377-AS-5 Pool, D., 220-MST-3 Ragab, S., 64-FD-12 Reger, R., 243-AMT-6 Risse, K., 7-ACD-1 Rudnik, R., 246-APA-27 Poole, D., 30-MDO-1, 113-APA-13 Raghavan, S., 29-MAT-1, 41-STR-1, 139-STR-8 Reich, G., 298-AS-3 Rittenhouse, J., 146-ABPSI-2 Ruetten, M., 103-ABPSI-1 Poovathingal, S., 325-TP-10 Raghunath, G., 3-ISC-1 Reid, T., 370-WE-14 Rizzetta, D., 342-FD-42 Ruf, J., 188-TP-4 Popov, N., 176-PDL-6, 177-PDL-7, 274-PDL-9 Raghunathan, B., 342-FD-42 Rein, M., 103-ABPSI-1, 198-ABPSI-3 Rizzi, A., 113-APA-13, 115-APA-15, 206-APA-24, Ruff, R., 169-MST-2 Popov, P., 36-PC-3 Raghunathan, S., 342-FD-42 Reinhardt, B., 69-GNC-5 277-SOF-3 Ruiz-Calavera, L., 103-ABPSI-1, 198-ABPSI-3, Poroseva, S., 93-SUR-1 Ragni, D., 44-WE-1, 189-WE-6, 284-WE-10 Reinhart, T., 327-WE-12 Rizzi, S., 396-SD-15 202-APA-20 Porter, A., 122-GNC-7 Rah, J., 272-PC-16 Reinhart, Z., 78-MVC-2 Roa, M., 201-AMT-5/PC-11 Rukes, L., 256-FD-34 Porter, C., 65-FD-13, 250-FD-28 Rahn, C., 364-SD-14 Reinisch, G., 368-TP-12 Roberts, P., 255-FD-33 Rumpfkeil, M., 6-AA-1, 157-FD-21, 310-MDO-7 Post, M., 38-PDL-2, 86-PDL-4 Rai, M., 64-FD-12 Reisenthel, P., 391-MDO-9 Robertson, A., 95-WE-4 Rumsey, C., 54-APA-7, 111-APA-11, 204-APA-22 Potapenko, D., 133-PDL-5 Rais-Rohani, M., 30-MDO-1, 266-MDO-6, 311-NDA-7, Reising, H., 61-FD-9 Robertson, D., 6-AA-1 Rumsey, M., 62-FD-10 Pototzky, A., 200-AFM-7 365-STR-18 Reist, T., 245-APA-26 Robinson, A., 65-FD-13 Rupert, A., 121-GNC-6 Potsdam, M., 55-APA-8 Raither, W., 248-AS-2 Ren, X., 309-MAT-7 Robinson, C., 78-MVC-2 Russell, S., 42-STR-2, 398-STR-20 Pourazarm, P., 327-WE-12 Raja, L., 133-PDL-5 Ren, Y., 80-OPS-1, 185-STR-9 Robinson, J., 257-GEPC-3 Rutledge, J., 124-GTE-3 Powell, D., 354-MAT-8 Rajagopal, K., 348-GNC-21 Ren, Z., 19-FD-2 Rockwell, R., 262-HSABP-3, 335-AMT-10/GT-8 Ryan, J., 159-GEPC-2 Power, G., 78-MVC-2, 170-MVC-4 Rajan, K., 274-PDL-9 Renaud, G., 398-STR-20 Rockwood, M., 14-APA-4 Ryan, K., 219-MDO-5 Powers, R., 145-AA-4 Rajpurohit, T., 214-GNC-13 Rendall, T., 30-MDO-1, 113-APA-13, 232-STR-12, Rodio, J., 111-APA-11 Rybus, T., 346-GNC-19 Prabhakar, P., 398-STR-20 Raju, G., 365-STR-18 356-MDO-8 Rodrigues, N., 316-PC-19 Ryle, S., 350-GT-9 Prabhu, D., 140-TP-1 Raju, I., 366-STR-19 Resor, B., 94-WE-3 Rodrigues de Lima, G., 339-AS-4 Ryu, H., 364-SD-14 Prach, A., 348-GNC-21 Rallabhandi, S., 77-MDO-2 Reti, I., 260-GNC-16 Rodriguez, D., 228-SD-9 Ryu, J., 280-STR-15 Prall, M., 4-ISC-2 Ralston, J., 267-MST-4 Reu, P., 109-AMT-2 Roettgen, A., 362-PDL-11 Saam, L., 155-DE-3 Pratt, A., 35-PC-2 Raman, V., 61-FD-9, 225-PC-14, 272-PC-16, 317-PC-20 Reynolds, T., 261-GT-6 Rogers, M., 257-GEPC-3 Sabelnikov, V., 262-HSABP-3 Presser, C., 281-TES-2 Ramasamy, M., 279-STR-14 Reynolds, W., 275-SCS-3 Roget, B., 21-FD-4 Sadeghirad, A., 355-MAT-9 Price, N., 268-NDA-6, 393-NDA-9 Rambaud, P., 305-GT-7, 376-AMT-12/GT-10 Rezaeian, A., 111-APA-11, 153-APA-18 Rogoshchenkov, N., 149-AMT-3 Sadon, A., 349-GNC-22 Priebe, S., 119-FD-18, 252-FD-30, 255-FD-33 Rame, E., 282-TP-8 Rezvani, R., 229-SD-10 Rokhsaz, K., 153-APA-18, 323-STR-17 Saenz Otero, A., 346-GNC-19 Priest, J., 267-MST-4 Rampurawala, A., 151-APA-16, 153-APA-18 Rhew, R., 70-GT-2 Rome, J., 138-STR-7 Safari, A., 391-MDO-9 Prisell, E., 145-AA-4, 375-AA-8 Ramu, P., 171-NDA-4 Rhoads, J., 93-SUR-1 Romero, V., 221-NDA-5 Safta, C., 393-NDA-9 Author/Session Chair Index Saha, P., 158-FD-22 Satija, A., 293-AMT-7 Schultz, M., 280-STR-15 Sharpe, J., 49-AA-2 Silvernail, N., 350-GT-9 Sahasakkul, W., 236-WE-8 Sato, K., 118-FD-17 Schwaab, Q., 335-AMT-10/GT-8, 350-GT-9 Shaw, P., 280-STR-15 Sim, J., 272-PC-16 Sahni, O., 31-MVC-1, 237-WE-9, 303-FD-39 Sato, M., 208-FD-23 Schwartz, N., 357-MST-6 Shaw-Cortez, W., 67-GNC-3 Simao Ferreira, C., 44-WE-1, 189-WE-6, 284-WE-10 Sahu, J., 15-APA-5 Satou, Y., 227-SCS-2, 377-AS-5 Schwartzentruber, T., 235-TP-7, 283-TP-9, 325-TP-10, Shea, P., 64-FD-12, 243-AMT-6, 331-AA-7 Simerly, S., 163-GT-4 Saibov, E., 34-PC-1 Sauer, D., 105-ACD-6 382-FD-48 Sheahan, J., 228-SD-9 Simon, B., 336-APA-32 Sain, T., 218-MAT-5 Saurabh, A., 164-GTE-4 Schweickart, R., 363-SCS-5 Sheikh-AlShabab, A., 297-APA-31 Simon, D., 68-GNC-4 Saito, Y., 102-AA-3 Saussie, D., 160-GNC-9, 347-GNC-20 Schwenke, D., 382-FD-48 Shen, S., 281-TES-2 Simon, N., 279-STR-14, 366-STR-19 Sakai, T., 141-TP-2 Sauterleute, A., 105-ACD-6 Schwer, D., 253-FD-31, 271-PC-15 Shen, X., 34-PC-1 Simonis, K., 200-AFM-7 Sakamoto, H., 227-SCS-2 Savarovskii, A., 176-PDL-6 Schwöppe, A., 22-FD-5 Shen, Y., 383-FD-49 Simpson, R., 62-FD-10, 229-SD-10 Sakamoto, R., 352-HSABP-5 Savely, R., 217-IS-1 Sclafani, A., 152-APA-17 Sheng, C., 12-APA-2, 296-APA-30, 337-APA-33 Sinapius, M., 248-AS-2 Sakaue, H., 249-ASE-1, 376-AMT-12/GT-10 Savill, A., 151-APA-16, 153-APA-18 Scoglietti, D., 293-AMT-7 Shephard, M., 31-MVC-1 Singh, P., 388-GNC-24 Sakuranaka, N., 150-AMT-4 Savvaris, A., 213-GNC-12 Scott, G., 285-WE-11 Sheplak, M., 149-AMT-3 Singh, S., 122-GNC-7, 160-GNC-9 Salah El Din, I., 154-APA-19, 244-APA-25 Sawada, H., 350-GT-9 Scott, R., 229-SD-10 Shevyrin, A., 187-TP-3 Singhal, A., 340-FD-40 Salama, F., 213-GNC-12 Sawada, K., 292-AFM-10, 369-TP-13 Scott-Emuakpor, O., 26-GTE-1, 354-MAT-8 Shi, D., 260-GNC-16 Sinha, A., 136-SD-6, 145-AA-4, 357-MST-6 Salemi, L., 117-FD-16 Sawyer, J., 362-PDL-11 Scotti, A., 396-SD-15 Shi, J., 252-FD-30 Sinha, N., 49-AA-2 Salemkar, H., 234-TP-6 Saxena, A., 130-NDA-3, 207-AS-1 Scoville, S., 8-ACD-2 Shi, X., 389-GNC-25 Sinn, T., 363-SCS-5 Salmon, A., 274-PDL-9 Schadegg, T., 356-MDO-8 Seal, S., 41-STR-1 Shields, M., 350-GT-9 Sinnige, T., 153-APA-18 Salvador, N., 317-PC-20 Schaeper, C., 105-ACD-6 Seaward, J., 378-ASE-2 Shikany, D., 267-MST-4 Sirignano, W., 36-PC-3 Samareh, J., 92-STR-6 Schaffner, G., 16-DE-1 Sebastian, J., 218-MAT-5 Shim, D., 308-IS-3 Sisk, W., 132-PC-7 Samborsky, D., 45-WE-2 Schallhorn, P., 120-FD-19, 380-FD-46 Sechkar, E., 354-MAT-8 Shima, E., 63-FD-11 Sitaraman, J., 21-FD-4, 114-APA-14, 189-WE-6, Sami, M., 272-PC-16 Scharnhorst, R., 332-ABPSI-5 Sedwick, R., 37-PDL-1, 38-PDL-2, 122-GNC-7, 274-PDL-9 Shimada, T., 36-PC-3, 83-PC-5 285-WE-11 Samimy, M., 145-AA-4, 336-APA-32, 340-FD-40 Schauer, F., 74-HSABP-1, 108-AMT-1, 271-PC-15, See, Y., 164-GTE-4 Shimomura, Y., 105-ACD-6 Situ, Y., 49-AA-2, 375-AA-8 Samuel, P., 388-GNC-24 352-HSABP-5, 360-PC-21/AMT-11, 394-PC-23 Seem, J., 95-WE-4 Shimoura, M., 57-DE-2 Siu, N., 245-APA-26 Sandborn, P., 95-WE-4 Schelbergen, M., 284-WE-10 Segawa, T., 299-FD-35 Shin, S., 364-SD-14, 396-SD-15 Sizemore, A., 52-AFM-3

177 Sandel, D., 184-SRE-3 Schetz, J., 51-ACD-4, 88-SD-4 Seidel, G., 309-MAT-7, 355-MAT-9 Shirasawa, Y., 227-SCS-2 Skaperdas, V., 65-FD-13 Sanford, A., 75-ISC-4 Schiavo, L., 157-FD-21 Seidel, J., 87-SD-3, 158-FD-22, 250-FD-28 Shiryayev, O., 135-SD-5 Skarolek, V., 65-FD-13 Sangid, M., 125-MAT-2, 218-MAT-5, 265-MAT-6 Schierman, J., 259-GNC-15 Seiler, P., 162-GNC-11, 328-WE-13, 370-WE-14 Shishko, R., 392-MST-7 Skelley, S., 70-GT-2 Sankar, L., 12-APA-2, 55-APA-8 Schilling, P., 396-SD-15 Sekar, B., 31-MVC-1, 165-HSABP-2 Shivakumar, K., 167-MAT-4 Skiba, A., 84-PC-6 Sankaran, V., 35-PC-2, 156-FD-20, 164-GTE-4, Schiltgen, B., 345-GEPC-4 Sekimoto, S., 208-FD-23, 336-APA-32 Shkurenkov, I., 274-PDL-9, 362-PDL-11 Skuratov, A., 302-FD-38 225-PC-14, 379-FD-45 Schirmer, J., 146-ABPSI-2 Sell, B., 360-PC-21/AMT-11 Shneider, M., 177-PDL-7, 274-PDL-9 Slabaugh, C., 35-PC-2 Sankararaman, S., 130-NDA-3 Schlöffel, G., 389-GNC-25 Selvarathinam, A., 399-STR-21 Short, E., 234-TP-6 Slais, T., 84-PC-6 Sansevero, P., 16-DE-1, 83-PC-5 Schmidt, J., 362-PDL-11 Semidey, R., 398-STR-20 Shrestha, E., 3-ISC-1 Slater, J., 26-GTE-1, 135-SD-5, 228-SD-9 Santangelo, A., 277-SOF-3 Schmidt, K., 7-ACD-1 Semlitsch, B., 156-FD-20 Shtark, A., 139-STR-8 Slavinskaya, N., 34-PC-1 Santer, M., 179-SCS-1, 253-FD-31 Schmidt, S., 89-SRE-1, 184-SRE-3 Sengezer, E., 309-MAT-7 Shumakova, A., 187-TP-3 Slipchenko, M., 201-AMT-5/PC-11 Santhanam, V., 185-STR-9 Schmisseur, J., 210-FD-25, 382-FD-48 Serrani, A., 242-AFM-9 Shweyk, K., 10-AFM-2 Sloan, B., 78-MVC-2, 233-TES-1, 281-TES-2, 324-TES-3, Santner, J., 34-PC-1 Schmit, R., 252-FD-30 Sertse, H., 355-MAT-9 Shyy, W., 296-APA-30 367-TES-4, 400-TES-5 Sar, P., 123-GNC-8 Schmitz, S., 189-WE-6, 190-WE-7 Seshadri, P., 268-NDA-6 Sibilski, K., 24-GNC-2, 242-AFM-9 Slotnick, J., 204-APA-22, 386-GEPC-5 Sardar, A., 232-STR-12 Schmoll, J., 128-MST-1 Setoodeh, S., 399-STR-21 Siddarth, A., 347-GNC-20 Slough, J., 333-AFM-11 Sargsyan, K., 393-NDA-9 Schneegans, A., 105-ACD-6 Seume, J., 370-WE-14 Siddiqui, S., 306-GTE-6 Smarslok, B., 32-NDA-1, 221-NDA-5 Saric, W., 245-APA-26, 297-APA-31, 376-AMT-12/GT-10 Schneider, G., 156-FD-20, 234-TP-6 Sève, F., 389-GNC-25 Sideris, A., 36-PC-3 Smart, M., 307-HSABP-4 Sarigul-Klijn, N., 107-AFM-5 Schneider, S., 20-FD-3, 54-APA-7, 117-FD-16, Seweryn, K., 346-GNC-19 Sidor, A., 333-AFM-11 Smeltzer, S., 138-STR-7 Sarker, M., 400-TES-5 210-FD-25 Shafer, T., 11-APA-1, 114-APA-14, 205-APA-23, Sidorenko, A., 342-FD-42 Smirnov, D., 353-IS-4 Sarker, S., 367-TES-4 Schneider, T., 105-ACD-6 247-APA-28 Sidorenko, M., 256-FD-34 Smit, J., 237-WE-9 Sarmento, A., 95-WE-4 Schneider, W., 87-SD-3 Shah, G., 10-AFM-2 Sieber, M., 256-FD-34 Smith, A., 85-PDL-3 Sartorius, S., 8-ACD-2, 104-ACD-5, 182-SE-1, Schoneman, J., 396-SD-15 Shah, H., 79-NDA-2 Siewert, S., 277-SOF-3 Smith, B., 54-APA-7, 157-FD-21, 294-AMT-8 296-APA-30 Schoonmaker, M., 119-FD-18 Shan, J., 80-OPS-1, 169-MST-2, 389-GNC-25 Sigthorsson, D., 388-GNC-24 Smith, D., 340-FD-40 Sasaki, D., 197-AA-5 Schrauf, G., 7-ACD-1 Shang, J., 86-PDL-4, 375-AA-8 Silberg, E., 73-HIS-2 Smith, E., 207-AS-1, 280-STR-15, 364-SD-14 Sasiadek, J., 24-GNC-2 Schreck, S., 236-WE-8 Shankara, P., 246-APA-27 Silk, E., 188-TP-4, 234-TP-6, 282-TP-8 Smith, L., 84-PC-6 Satak, N., 259-GNC-15, 353-IS-4 Schroeder, J., 267-MST-4 Shapiro, A., 123-GNC-8 Silton, S., 15-APA-5, 156-FD-20 Smith, M., 335-AMT-10/GT-8 Säterskog, M., 198-ABPSI-3 Schuermann, M., 50-ACD-3 Sharma, A., 62-FD-10, 384-FD-50 Silva, J., 182-SE-1 Smith, N., 52-AFM-3, 258-GNC-14 Sathyanarayan, D., 350-GT-9 Schuet, S., 68-GNC-4 Sharma, P., 336-APA-32 Silva, W., 136-SD-6, 160-GNC-9, 180-SD-7 Smith, O., 61-FD-9 Sathyanarayan, P., 397-SD-16 Schultz, I., 108-AMT-1, 335-AMT-10/GT-8 Sharp, N., 118-FD-17 Silver, M., 179-SCS-1, 275-SCS-3 Smith, S., 16-DE-1, 228-SD-9, 316-PC-19, 363-SCS-5 Author/Session Chair Index Smith, W., 321-SD-13 Steiner, S., 153-APA-18 Sumiya, S., 394-PC-23 Tangirala, V., 74-HSABP-1 Timko, M., 89-SRE-1 Snyder, D., 246-APA-27 Steinfeldt, B., 134-SAT-1, 178-SAT-2, 200-AFM-7, Sun, C., 232-STR-12, 255-FD-33 Tani, Y., 6-AA-1, 188-TP-4 Ting, E., 228-SD-9, 276-SD-11 Snyder, P., 351-GTE-7 219-MDO-5, 292-AFM-10 Sun, J., 34-PC-1 Tanno, H., 118-FD-17, 369-TP-13 Tishkoff, J., 132-PC-7 Snyder, R., 127-MDO-3, 138-STR-7, 322-STR-16 Stepanyan, S., 176-PDL-6, 177-PDL-7 Sun, L., 23-GNC-1 Tantaroudas, N., 90-STR-4 Tiso, P., 136-SD-6 Snyder, S., 68-GNC-4 Stepanyan, V., 213-GNC-12 Sun, W., 224-PC-13, 361-PC-22, 394-PC-23 Tatsukawa, T., 356-MDO-8 Titchener, N., 245-APA-26 Sobel, K., 23-GNC-1 Stephan, A., 249-ASE-1 Sun, Y., 83-PC-5 Tavares, C., 4-ISC-2 Tixier, E., 385-FD-51 Sobester, A., 310-MDO-7 Stephani, K., 187-TP-3 Sünder, P., 296-APA-30 Taylor, K., 44-WE-1 Tkach, N., 38-PDL-2 Sodja, J., 112-APA-12 Stephen, E., 119-FD-18 Sunny, G., 29-MAT-1 Taylor, L., 370-WE-14 Tobaldini Neto, L., 273-PC-17 Sofronsky, S., 306-GTE-6 Sternberg, D., 346-GNC-19 Suram, S., 78-MVC-2 Taylor, N., 78-MVC-2, 129-MVC-3 Togashi, F., 381-FD-47 Soghrati, S., 167-MAT-4 Stevens, C., 352-HSABP-5 Suresh, A., 235-TP-7 Taylor, P., 136-SD-6, 180-SD-7 Toghiani, H., 167-MAT-4 Sojka, P., 316-PC-19 Stevens, R., 203-APA-21 Surzhikov, S., 226-PDL-8, 283-TP-9, 318-PDL-10 Taylor, R., 43-STR-3, 320-SD-12, 365-STR-18 Toki, Y., 292-AFM-10 Soliman, H., 138-STR-7, 186-STR-10 Stewart, E., 127-MDO-3 Sutliff, D., 66-GEPC-1, 197-AA-5, 331-AA-7, 375-AA-8 Teerlinck, K., 240-AA-6 Toledo, L., 52-AFM-3 Song, A., 190-WE-7 Stewart, G., 95-WE-4 Sutton, J., 64-FD-12, 84-PC-6, 176-PDL-6, Tekinalp, O., 348-GNC-21 Tolkunov, B., 256-FD-34 Song, B., 111-APA-11 Stiltner, L., 308-IS-3 201-AMT-5/PC-11 Tekles, N., 68-GNC-4 Tolson, R., 107-AFM-5 Song, W., 379-FD-45 Stoddard, W., 74-HSABP-1 Suzuki, K., 336-APA-32 Telidetzki, K., 154-APA-19 Tom, B., 108-AMT-1 Soni, M., 236-WE-8 Stodieck, O., 90-STR-4 Suzuki, T., 188-TP-4, 326-TP-11 Temme, J., 84-PC-6 Tomac, M., 115-APA-15 Soteriou, M., 225-PC-14 Stoellinger, M., 158-FD-22 Swartz, S., 298-AS-3 Teng, C., 309-MAT-7 Tomek, W., 338-APA-34 Soto, O., 381-FD-47 Stoffels, M., 45-WE-2 Swei, S., 276-SD-11 Teramoto, S., 240-AA-6 Tomioka, S., 150-AMT-4, 165-HSABP-2 Sotoudeh, Z., 90-STR-4 Stohlman, O., 395-SCS-6 Swiler, L., 393-NDA-9 Terashima, H., 36-PC-3, 83-PC-5 Tomita, T., 150-AMT-4 Sottos, N., 167-MAT-4 Stoll, F., 45-WE-2 Switchenko, D., 370-WE-14 Terashima, K., 280-STR-15 Tong, O., 22-FD-5 Soudakov, V., 342-FD-42 Stone, C., 224-PC-13 Syred, N., 367-TES-4 TerMaath, S., 185-STR-9, 365-STR-18, 399-STR-21 Tong, W., 6-AA-1, 266-MDO-6 Soukhomlinov, V., 176-PDL-6 Storey, R., 189-WE-6 Szabo, Z., 304-GNC-17 Terning, B., 323-STR-17 Tonsho, K., 157-FD-21 Sowers, T., 10-AFM-2 Storozhev, D., 318-PDL-10 Szlatenyi, C., 336-APA-32 Tescione, G., 284-WE-10 Toombs, A., 24-GNC-2 Sozer, E., 18-FD-1, 152-APA-17, 381-FD-47 Stoumbos, T., 186-STR-10, 397-SD-16, 399-STR-21 Tadayon Mousavi, S., 157-FD-21 Tessler, A., 231-STR-11 Tormalm, M., 198-ABPSI-3

178 Sørensen, N., 94-WE-3 Stowe, R., 173-PC-8 Tadghighi, H., 55-APA-8 Thacker, B., 32-NDA-1 Toropov, V., 168-MDO-4, 219-MDO-5 Spak, K., 135-SD-5 Strain, J., 365-STR-18 Tafti, D., 59-FD-7 Thaiss, C., 398-STR-20 Toubin, H., 244-APA-25 Sparacino, D., 188-TP-4 Strand, C., 108-AMT-1 Tagai, R., 297-APA-31 Thakur, S., 83-PC-5, 120-FD-19 Toulson, E., 34-PC-1 Spearrin, R., 108-AMT-1 Strawser, D., 346-GNC-19 Taguchi, H., 400-TES-5 Thalakkottor, J., 18-FD-1 Tran, S., 237-WE-9 Spillers, R., 117-FD-16, 335-AMT-10/GT-8, 383-FD-49 Strobl, T., 249-ASE-1 Taha, H., 40-SD-2, 242-AFM-9, 356-MDO-8, 388-GNC-24 Theodoulis, S., 389-GNC-25 Trask, R., 232-STR-12 Spletzer, J., 67-GNC-3 Strom, B., 190-WE-7 Tahk, M., 161-GNC-10 Theofilis, V., 20-FD-3, 210-FD-25 Trenou, K., 272-PC-16 Spottswood, S., 136-SD-6 Struminskaya, I., 302-FD-38 Tahmasian, S., 388-GNC-24 Theuerkauf, S., 394-PC-23 Tretyakova, N., 256-FD-34 Sprague, M., 142-WE-5, 328-WE-13 Stuebner, M., 366-STR-19 Tahsini, A., 157-FD-21, 307-HSABP-4 Thimissetti, C., 358-NDA-8 Triay, M., 188-TP-4 Springer, R., 262-HSABP-3 Stumper, T., 110-APA-10 Taira, K., 19-FD-2, 59-FD-7 Thomas, F., 112-APA-12 Trinh, K., 228-SD-9, 276-SD-11 Sreekantamurthy, T., 139-STR-8 Stumpf, E., 7-ACD-1 Takagi, S., 352-HSABP-5 Thomas, J., 28-ISC-3, 65-FD-13 Troldborg, N., 94-WE-3 Sreenivas, K., 370-WE-14 Stütz, P., 217-IS-1, 353-IS-4 Takagi, Y., 350-GT-9 Thomas, L., 34-PC-1 Tropea, C., 336-APA-32, 342-FD-42 Sridhar, B., 220-MST-3, 387-GNC-23 Su, H., 155-DE-3 Takahashi, H., 150-AMT-4 Thomas, M., 125-MAT-2 Tropina, A., 177-PDL-7 Srinivasan, L., 122-GNC-7 Su, J., 139-STR-8 Takahashi, T., 7-ACD-1, 8-ACD-2, 73-HIS-2, 147-ACD-7, Thomas, R., 66-GEPC-1, 80-OPS-1, 102-AA-3 Trujillo, A., 259-GNC-15 Srivastava, A., 358-NDA-8 Su, W., 229-SD-10 310-MDO-7, 356-MDO-8 Thomas, S., 327-WE-12 Truong, A., 197-AA-5 Stackpoole, M., 305-GT-7 Subba Reddiar Pappu, V., 348-GNC-21 Takahashi, Y., 60-FD-8 Thomason, C., 109-AMT-2 Truszkowski, W., 353-IS-4 Staggers, D., 57-DE-2 Subbarao, K., 9-AFM-1, 148-AFM-6, 242-AFM-9 Takaki, R., 63-FD-11, 240-AA-6 Thompson, B., 378-ASE-2 Tsang, W., 400-TES-5 Stanford, B., 90-STR-4, 159-GEPC-2, 168-MDO-4, Subramanian, S., 216-GTE-5 Takayanagi, H., 141-TP-2 Thompson, D., 211-FD-26/MVC-5, 249-ASE-1 Tsuboi, N., 36-PC-3 278-STR-13 Subramaniyan, A., 358-NDA-8 Takii, K., 64-FD-12 Thompson, R., 318-PDL-10, 363-SCS-5 Tsujimoto, K., 57-DE-2 Starikovskaya, S., 176-PDL-6, 177-PDL-7, 274-PDL-9, Sudhakar, S., 344-FD-44 Taligoski, J., 14-APA-4 Thompson, S., 234-TP-6 Tsutsumi, S., 240-AA-6 361-PC-22 Sudret, B., 393-NDA-9 Talleur, D., 214-GNC-13 Thomson, S., 242-AFM-9 Tucker, A., 245-APA-26, 297-APA-31 Starikovskiy, A., 38-PDL-2, 86-PDL-4, 271-PC-15, Sugiura, A., 339-AS-4 Talley, C., 56-APA-9 Threadgill, J., 119-FD-18 Tucker, P., 49-AA-2, 60-FD-8, 251-FD-29, 297-APA-31, 274-PDL-9, 315-PC-18, 361-PC-22 Sujar-Garrido, P., 299-FD-35 Talley, D., 36-PC-3, 156-FD-20 Thurber, A., 41-STR-1 379-FD-45, 381-FD-47 Starin, S., 24-GNC-2, 349-GNC-22 Sulaiman, T., 208-FD-23, 336-APA-32 Tam, C., 74-HSABP-1 Thurow, B., 109-AMT-2, 294-AMT-8 Tuckey, T., 114-APA-14 Starkey, R., 380-FD-46 Suleman, A., 207-AS-1 Tanaka, K., 63-FD-11 Tian, W., 284-WE-10, 328-WE-13 Tufts, M., 245-APA-26 Steck, J., 347-GNC-20, 348-GNC-21 Sullivan, J., 149-AMT-3, 334-AMT-9 Tanaka, M., 249-ASE-1 Tian, Y., 161-GNC-10, 304-GNC-17 Tummala, Y., 298-AS-3 Steijl, R., 55-APA-8 Sullivan, R., 322-STR-16 Tandy, W., 179-SCS-1, 363-SCS-5 Tibaldi, C., 237-WE-9 Turlin, M., 119-FD-18 Steinbrenner, J., 211-FD-26/MVC-5 Sullivan, T., 65-FD-13 Tang, J., 111-APA-11 Tiller, P., 31-MVC-1 Turner, T., 139-STR-8 Steiner, M., 387-GNC-23 Sultan, C., 348-GNC-21 Tang, Y., 303-FD-39 Tilmann, C., 53-APA-6 Turpin, J., 278-STR-13 Author/Session Chair Index Tusun, G., 389-GNC-25 Vassberg, J., 54-APA-7, 113-APA-13 Wakayama, S., 345-GEPC-4 Wei, F., 112-APA-12 Willcox, K., 219-MDO-5, 311-NDA-7, 391-MDO-9 Tuttle, S., 307-HSABP-4 Vasseur, O., 103-ABPSI-1, 198-ABPSI-3 Wakefield, S., 360-PC-21/AMT-11 Wei, M., 59-FD-7, 341-FD-41 Willems, S., 117-FD-16 Tyacke, J., 49-AA-2 Vasu, A., 391-MDO-9 Wales, C., 339-AS-4 Wei, W., 357-MST-6 Willey, C., 395-SCS-6 Tyahla, S., 125-MAT-2 Vayner, B., 378-ASE-2 Walker, B., 66-GEPC-1 Weigand, J., 365-STR-18 Williams, D., 257-GEPC-3, 299-FD-35, 385-FD-51 Tynis, J., 137-SRE-2 Vedula, P., 235-TP-7 Walker, J., 217-IS-1 Weinstein, E., 323-STR-17 Williams, N., 11-APA-1 Uddi, M., 315-PC-18 Veers, P., 285-WE-11 Walker, S., 92-STR-6, 169-MST-2 Weintraub, I., 388-GNC-24 Williams, T., 327-WE-12, 340-FD-40 Ueda, S., 165-HSABP-2 Veldhuis, L., 153-APA-18 Wall, W., 381-FD-47 Weiss, J., 335-AMT-10/GT-8, 350-GT-9 Williams-Hayes, P., 52-AFM-3, 333-AFM-11 Ukai, T., 102-AA-3 Velicki, A., 66-GEPC-1 Waller, D., 363-SCS-5 Weiss, P., 13-APA-3 Williamsen, J., 93-SUR-1 Ukeiley, L., 11-APA-1, 243-AMT-6 Venkatakrishnan, V., 63-FD-11 Wallraff, M., 251-FD-29 Weitz, L., 387-GNC-23 Williamson, K., 28-ISC-3 Ulrich, S., 260-GNC-16, 346-GNC-19 Venkataraman, S., 79-NDA-2, 399-STR-21 Walter, L., 387-GNC-23, 389-GNC-25 Welch, C., 28-ISC-3 Willis, B., 186-STR-10, 397-SD-16 Ulybyshev, Y., 69-GNC-5 Venkatesan, C., 388-GNC-24 Walton, O., 89-SRE-1 Welch, G., 26-GTE-1, 216-GTE-5 Wilson, A., 318-PDL-10 Ura, H., 6-AA-1, 163-GT-4 Venkatesh, P., 164-GTE-4 Wan, Y., 189-WE-6 Wells, D., 51-ACD-4 Wilson, J., 124-GTE-3, 160-GNC-9 Uranga, A., 245-APA-26 Venkateswaran, P., 201-AMT-5/PC-11, Wang, C., 113-APA-13, 225-PC-14 Wells, S., 389-GNC-25 Wilson, T., 3-ISC-1, 323-STR-17 Urdahl, R., 108-AMT-1 360-PC-21/AMT-11 Wang, E., 52-AFM-3 Welsh, D., 148-AFM-6, 352-HSABP-5 Wimmer, E., 265-MAT-6 Urnes, J., 228-SD-9 Ventura, A., 4-ISC-2 Wang, G., 181-SD-8, 391-MDO-9 Welsh, W., 40-SD-2 Windom, B., 84-PC-6, 175-PC-10, 223-PC-12, Uzun, A., 14-APA-4 Vergine, F., 262-HSABP-3 Wang, H., 82-PC-4, 173-PC-8 Welstead, J., 51-ACD-4 315-PC-18 Vahidpour, M., 108-AMT-1 Vermeire, B., 251-FD-29 Wang, J., 12-APA-2, 86-PDL-4, 109-AMT-2, 273-PC-17, Weng, H., 325-TP-10 Wingate, S., 4-ISC-2 Vaidyanathan, A., 28-ISC-3 Viel, M., 184-SRE-3 337-APA-33, 342-FD-42, 389-GNC-25 Wernert, P., 389-GNC-25 Wingfield, O., 75-ISC-4 Valasek, J., 4-ISC-2, 263-IS-2, 347-GNC-20 Vijayakumar, G., 236-WE-8 Wang, K., 85-PDL-3 Werter, N., 148-AFM-6, 339-AS-4 Winstroth, J., 370-WE-14 Valco, D., 34-PC-1 Vijayakumari, H., 88-SD-4 Wang, L., 208-FD-23 Wessels, M., 255-FD-33 Winter, M., 305-GT-7 Vale, J., 207-AS-1 Viken, J., 257-GEPC-3 Wang, M., 85-PDL-3 West, D., 376-AMT-12/GT-10 Winter, T., 79-NDA-2, 182-SE-1 Valente, A., 138-STR-7 Viken, S., 11-APA-1 Wang, N., 163-GT-4 West, J., 341-FD-41 Wissa, A., 298-AS-3 Valentini, P., 283-TP-9 Vila, L., 396-SD-15 Wang, P., 130-NDA-3, 171-NDA-4 West, T., 182-SE-1, 221-NDA-5 Wissink, A., 22-FD-5, 114-APA-14 Valera Medina, A., 367-TES-4 Vilela de Abreu, R., 246-APA-27 Wang, Q., 268-NDA-6, 328-WE-13, 379-FD-45 Westbrook, C., 82-PC-4 Witteveen, J., 79-NDA-2

179 Valliappan, V., 377-AS-5 Villace, V., 350-GT-9 Wang, S., 56-APA-9, 328-WE-13 Weston, N., 217-IS-1 Wittich, D., 85-PDL-3, 252-FD-30 Valyou, D., 87-SD-3 Villalva Gomez, R., 175-PC-10 Wang, W., 295-APA-29 Wey, C., 367-TES-4 Woeber, C., 204-APA-22 van Baalen, D., 365-STR-18 Villanueva, D., 311-NDA-7 Wang, X., 39-SD-1, 174-PC-9, 175-PC-10, 210-FD-25, Whalen, E., 53-APA-6, 303-FD-39 Woicke, S., 69-GNC-5 Van Buren, K., 358-NDA-8 Vincent-Randonnier, A., 262-HSABP-3 235-TP-7, 317-PC-20, 389-GNC-25, 397-SD-16 Wheatley, V., 307-HSABP-4 Wojcik, C., 19-FD-2 Van Buren, T., 303-FD-39 Visbal, M., 85-PDL-3, 158-FD-22, 342-FD-42, 344-FD-44 Wang, Y., 25-GT-1, 53-APA-6, 156-FD-20, 229-SD-10 Wheeler, K., 68-GNC-4 Wolf, W., 265-MAT-6 van Bussel, G., 189-WE-6, 284-WE-10 Vishwakarma, V., 136-SD-6 Wang, Z., 130-NDA-3, 171-NDA-4, 321-SD-13, Wheeler, N., 277-SOF-3 Wolff, M., 232-STR-12 Van Dam, C., 44-WE-1, 62-FD-10 Visscher, P., 137-SRE-2, 184-SRE-3 340-FD-40, 381-FD-47 Wheelock, A., 378-ASE-2 Womack, G., 87-SD-3 van der Weide, E., 202-APA-20 Viswanath, K., 59-FD-7 Wanthal, S., 309-MAT-7, 355-MAT-9 Whitaker, S., 306-GTE-6 Won, S., 82-PC-4, 84-PC-6, 174-PC-9, 223-PC-12 van Duin, A., 326-TP-11 Voelkel, S., 61-FD-9 Ward, C., 20-FD-3 White, E., 44-WE-1, 62-FD-10, 118-FD-17 Wong, H., 89-SRE-1, 368-TP-12 Van Eykeren, L., 304-GNC-17 Vogel, P., 49-AA-2 Ward, G., 277-SOF-3 White, J., 141-TP-2, 285-WE-11 Woo, K., 363-SCS-5 Van Hove, B., 376-AMT-12/GT-10 Vollmer, B., 89-SRE-1 Wardle, B., 29-MAT-1, 126-MAT-3 White, M., 85-PDL-3, 140-TP-1 Wood, W., 140-TP-1 Van Kampen, E., 3-ISC-1, 23-GNC-1, 258-GNC-14, Vollmer, H., 89-SRE-1 Warning, S., 119-FD-18 White, R., 334-AMT-9 Woodbury, T., 263-IS-2 304-GNC-17, 388-GNC-24 von Knoblauch, F., 180-SD-7 Warren, J., 167-MAT-4 White, S., 167-MAT-4, 365-STR-18 Woodiga, S., 334-AMT-9 van Muijden, J., 103-ABPSI-1 Vos, R., 7-ACD-1 Warren, P., 275-SCS-3 Whitehead, B., 386-GEPC-5 Woods, B., 298-AS-3 Van Newkirk, A., 41-STR-1 Voskuijl, M., 8-ACD-2 Waslander, S., 260-GNC-16, 388-GNC-24 Wichmann, K., 381-FD-47 Woods, C., 380-FD-46 Van Parys, B., 328-WE-13 Voyles, I., 32-NDA-1 Wasson, K., 277-SOF-3 Wickersham, A., 360-PC-21/AMT-11 Woodward, D., 260-GNC-16 Van Tooren, M., 8-ACD-2 Vukasinovic, B., 250-FD-28, 252-FD-30 Watanabe, K., 141-TP-2 Wickramasinghe, V., 320-SD-12 Woolley, D., 184-SRE-3 Van Zante, D., 66-GEPC-1, 102-AA-3 Vyas, M., 165-HSABP-2 Watanabe, S., 261-GT-6 Wicks, S., 29-MAT-1 Woolsey, C., 9-AFM-1, 161-GNC-10, 388-GNC-24 Vanden, K., 296-APA-30 Vyas, V., 39-SD-1 Watanabe, T., 400-TES-5 Wieland, D., 366-STR-19 Woopen, M., 251-FD-29 Vanek, B., 160-GNC-9, 260-GNC-16, 304-GNC-17 Waas, A., 41-STR-1, 42-STR-2, 43-STR-3, 138-STR-7, Waters, D., 351-GTE-7 Wierach, P., 248-AS-2 Work, D., 251-FD-29 Vanhove, G., 176-PDL-6 218-MAT-5, 232-STR-12, 398-STR-20 Watson, R., 60-FD-8, 379-FD-45, 381-FD-47 Wieseman, C., 159-GEPC-2 Woszidlo, R., 110-APA-10, 303-FD-39 Vanka, P., 300-FD-36 Wabel, T., 84-PC-6 Watt, G., 341-FD-41 Wiggen, S., 14-APA-4 Wrenn, M., 376-AMT-12/GT-10 Varghese, P., 61-FD-9, 382-FD-48 Wabick, K., 19-FD-2, 256-FD-34 Watts, R., 267-MST-4 Wigton, L., 63-FD-11 Wright, J., 120-FD-19 Variyar, A., 50-ACD-3 Wadhams, T., 140-TP-1 Waycaster, G., 134-SAT-1, 393-NDA-9 Wilder, M., 140-TP-1 Wrist, A., 11-APA-1 Varughese, B., 399-STR-21 Waggoner, B., 80-OPS-1 Wayman, T., 71-GT-3, 246-APA-27 Wildschek, A., 160-GNC-9 Wroblewski, W., 24-GNC-2, 242-AFM-9 Vasile, J., 299-FD-35 Wagner, J., 335-AMT-10/GT-8, 383-FD-49 Weaver, P., 43-STR-3, 90-STR-4, 94-WE-3, 365-STR-18 Wilkening, C., 267-MST-4 Wu, B., 53-APA-6, 163-GT-4 Vasile, M., 363-SCS-5 Wahls, R., 159-GEPC-2, 245-APA-26, 390-GT-11 Webb, J., 149-AMT-3 Wilkins, S., 243-AMT-6 Wu, H., 280-STR-15 Vasilyev, A., 226-PDL-8 Waindim, M., 252-FD-30 Wegener, J., 36-PC-3 Wilkinson, C., 128-MST-1 Wu, J., 28-ISC-3, 126-MAT-3 Author/Session Chair Index Wu, K., 278-STR-13 Yen, C., 41-STR-1 Zhang, J., 355-MAT-9 Wu, Y., 360-PC-21/AMT-11 Yentsch, R., 165-HSABP-2, 252-FD-30 zhang, S., 369-TP-13 Wu, Z., 43-STR-3, 241-AFM-8, 260-GNC-16, 261-GT-6, Yeom, B., 218-MAT-5 Zhang, C., 235-TP-7, 283-TP-9 365-STR-18 Yeratapally, S., 125-MAT-2 Zhang, D., 41-STR-1 Wu, P., 8-ACD-2 Yi, S., 244-APA-25 Zhang, F., 152-APA-17, 258-GNC-14 Xargay, E., 68-GNC-4, 214-GNC-13, 259-GNC-15 Yin, Z., 362-PDL-11 Zhang, H., 325-TP-10 Xia, X., 203-APA-21 Yiu, Y., 40-SD-2 Zhang, J., 189-WE-6, 391-MDO-9 Xia, Y., 60-FD-8, 207-AS-1, 300-FD-36 Yokoyama, N., 259-GNC-15 Zhang, K., 202-APA-20 Xiang, J., 185-STR-9 Yokozeki, T., 232-STR-12, 280-STR-15, 339-AS-4 Zhang, L., 309-MAT-7, 355-MAT-9, 366-STR-19 Xiang, Y., 130-NDA-3, 207-AS-1 Yong, Y., 169-MST-2 Zhang, M., 113-APA-13 Xiao, L., 227-SCS-2 Yoon, C., 35-PC-2, 164-GTE-4 Zhang, P., 379-FD-45 Xiao, X., 111-APA-11 Yoon, J., 188-TP-4 Zhang, R., 255-FD-33 Xiao, Z., 62-FD-10, 301-FD-37 Yoon, W., 84-PC-6 Zhang, S., 211-FD-26/MVC-5 Xiong, J., 255-FD-33 Yorita, D., 240-AA-6 Zhang, X., 321-SD-13 Xiong, Z., 274-PDL-9 Yoshinaga, T., 297-APA-31 Zhang, Y., 237-WE-9, 273-PC-17, 357-MST-6 Xu, F., 110-APA-10 Yoshizawa, A., 157-FD-21 Zhang, Z., 11-APA-1, 108-AMT-1, 126-MAT-3, Xu, J., 379-FD-45 You, R., 65-FD-13 163-GT-4, 255-FD-33, 360-PC-21/AMT-11, Xu, W., 42-STR-2 Young, G., 173-PC-8 362-PDL-11, 383-FD-49 Yadegar, I., 358-NDA-8 Young, J., 37-PDL-1, 56-APA-9, 274-PDL-9, 327-WE-12, Zhao, L., 241-AFM-8 Yakeno, A., 208-FD-23 344-FD-44 Zhao, M., 301-FD-37 Yakimenko, O., 52-AFM-3 Young, R., 231-STR-11 Zhao, Q., 12-APA-2, 337-APA-33 Yamada, Y., 376-AMT-12/GT-10 Young, T., 253-FD-31 Zhao, W., 88-SD-4 Yamakawa, H., 275-SCS-3 Yu, B., 304-GNC-17 Zhao, X., 211-FD-26/MVC-5 Yamamoto, K., 63-FD-11, 163-GT-4 Yu, K., 219-MDO-5, 262-HSABP-3, 333-AFM-11, Zhao, Z., 110-APA-10, 255-FD-33, 334-AMT-9

180 Yamamoto, M., 102-AA-3, 356-MDO-8 385-FD-51 Zheng, B., 53-APA-6 Yamamoto, N., 29-MAT-1 Yu, S., 126-MAT-3 Zheng, F., 395-SCS-6 Yamasaki, A., 363-SCS-5 Yu, W., 42-STR-2, 92-STR-6, 284-WE-10, 309-MAT-7, Zheng, G., 349-GNC-22 Yamashita, T., 261-GT-6 355-MAT-9, 366-STR-19, 377-AS-5 Zheng, J., 110-APA-10 Yamashita, Y., 6-AA-1 Yuan, R., 360-PC-21/AMT-11 Zheng, M., 202-APA-20 Yamaya, H., 376-AMT-12/GT-10 Yuan, X., 381-FD-47 Zheng, T., 397-SD-16 Yan, G., 129-MVC-3 Yucelen, T., 214-GNC-13 Zheng, Z., 6-AA-1, 260-GNC-16 Yan, H., 218-MAT-5, 252-FD-30 Yuhara, T., 8-ACD-2 Zhong, L., 304-GNC-17 Yan, Y., 253-FD-31, 301-FD-37, 384-FD-50 Yurkovich, R., 181-SD-8, 320-SD-12 Zhong, X., 20-FD-3, 116-FD-15, 210-FD-25, 235-TP-7 Yan, Z., 40-SD-2, 356-MDO-8 Zaal, P., 220-MST-3 Zhou, W., 72-GTE-2, 232-STR-12, 241-AFM-8 Yang, B., 179-SCS-1 Zachariah, M., 173-PC-8, 223-PC-12 Zhou, Y., 395-SCS-6 Yang, C., 241-AFM-8, 261-GT-6, 378-ASE-2 Zacny, K., 137-SRE-2 Zhou, Z., 241-AFM-8 Yang, G., 51-ACD-4, 369-TP-13 Zagarola, M., 282-TP-8 Zhu, G., 160-GNC-9 Yang, H., 18-FD-1, 21-FD-4, 341-FD-41 Zahle, F., 94-WE-3 Zhu, H., 67-GNC-3 Yang, S., 126-MAT-3, 241-AFM-8 Zaidi, S., 108-AMT-1 Zhu, J., 202-APA-20, 205-APA-23, 273-PC-17 Yang, V., 174-PC-9, 175-PC-10, 317-PC-20 Zalewski, B., 278-STR-13 Zhu, M., 260-GNC-16 Yang, X., 34-PC-1, 173-PC-8, 379-FD-45 Zaloglu, B., 344-FD-44 Zhu, S., 279-STR-14 Yang, Z., 95-WE-4, 256-FD-34 Zaman, K., 61-FD-9, 240-AA-6 Zhu, T., 326-TP-11 Yao, J., 72-GTE-2 Zambon, A., 111-APA-11 Zhu, X., 224-PC-13 Yao, K., 277-SOF-3 Zammit, C., 308-IS-3, 348-GNC-21 Zhuang, M., 53-APA-6 Yao, S., 241-AFM-8 Zammmit-Mangion, D., 308-IS-3, 348-GNC-21 Zhupanska, O., 45-WE-2, 186-STR-10 Yao, Y., 72-GTE-2 Zarandy, A., 160-GNC-9 Zingg, D., 63-FD-11, 154-APA-19, 245-APA-26 Yarantsev, D., 176-PDL-6, 262-HSABP-3 Zasadzinski, M., 389-GNC-25 Zink, P., 180-SD-7 Yavor, Y., 173-PC-8 Zawodny, N., 243-AMT-6 Zipay, J., 92-STR-6 Ye, Z., 92-STR-6, 355-MAT-9 Zeidler, M., 15-APA-5 Zouzou, N., 38-PDL-2 Yechout, T., 297-APA-31 Zemtsop, C., 158-FD-22 Zsedrovits, T., 160-GNC-9 Yedavalli, R., 123-GNC-8 Zeune, C., 11-APA-1 Zuhal, L., 203-APA-21 Yee, P., 282-TP-8 Zha, G., 53-APA-6, 111-APA-11, 216-GTE-5, 383-FD-49 Zyluk, A., 242-AFM-9 LEGEND Car Rental Elevators Restrooms IntroVenuePhones Map Smoking Gaylord National Resort & Convention Center Information Desk

1 9

2 3 10 11

5 4 21 31 8 7 6 41 51 NATIONAL HARBOR CONFERENCE ROOMS ZONE E LEGEND Car Rental 1 2 3 Elevators ZONE D WOODROW WILSON MAGNOLIA BALLROOM Restrooms 5 HOTEL D 4 C 3 Phones BALLROOM LEVEL A 2 B 1 ANNAPOLIS Smoking AZALEA CHERRY BLOSSOM PRESIDENTIAL CAMELLIA BALLROOM 1 2 3 4 FORT WASHINGTON Information Desk BOARDROOM 1 2 3 BOARDROOM REGISTRATION 1 9 ZONE A 1 2 3 10 11 1 2 C A 312 CAB C A 2 3 KEYNOTES AND5 4 STAGE21 31 645 FDE 3 4 LUNCHEONS8 7 6 41 51 4 5 D B NATIONAL HARBOR 978 IGH 6 CONFERENCE ROOMS ZONE E D B 5 6 POTOMAC BALLROOM 11 2101 LJK CHESAPEAKE MARYLAND 1 2 3 ZONE B ZONE D WOODROW WILSON ZONEMAGNOLIA C CONFERENCEBALLROOM ROOMS BALLROOM 5 HOTEL D 4 C 3 BALLROOM LEVEL A 2 B 1 ANNAPOLIS AZALEA CHERRY BLOSSOM PRESIDENTIAL CAMELLIA BALLROOM 1 2 3 4 FORT WASHINGTON BOARDROOM 1 2 3 BOARDROOM REGISTRATION ZONE A 1 1 2 C A 312 CAB C A 2 3 KEYNOTES AND STAGE 645 FDE 3 4 LUNCHEONS 4 5 D B 978 IGH 6 EXPOSITION D B 5 6 POTOMAC BALLROOM 11 2101 LJK HALL MARYLAND CHESAPEAKE ZONE B ZONEPRINCE C CONFERENCE GEORGE’S ROOMS EXHIBITBALLROOMION HALL

E D C B A

EXPOSITION HALL PRINCE GEORGE’S EXHIBITION HALL

Legend E D C B A ZONE A ZONE D ZONE E Aerospace Design and Structures Aerospace Sciences Aerospace Sciences ZONE B Aircraft Atmosphere Systems Engineering and Technology Management Aerospace Sciences Propulsion and Energy Information Systems Propulsion and Energy ZONE C Space and Missiles Propulsion and Energy

www.aiaa.org/scitech2014 18151 #aiaaSciTech Universityer of Michigan | Aerospace Engineering 100 YYears of Aerospace Research and Education Septemberpt 18-20, 2014, Ann Arbor

Visit us at Aero100.engin.edu

Join Us!

MICHIGAN AEROSPACE CENTENNIAL CELEBRATION Alumni, Clarence “Kelly” Johnson (1932 BSE, 1933 DESSERT RECEPTION MSE, 1964 PhD - Hon), pictured in the WEDNESDAY, JANUARY 15, 2014 University of Michigan wind tunnel in 1933 6:30 8:30PM with early single tail Model 10 Electra; Johnson’s aerodynamic MARYLAND BALLROOM C testing here led to the twin tail design, later a Lockheed trademark.

SAVE THE DATE! September 18-20, 2014 - Ann Arbor Centennial Celebration Events

For more events and information, [email protected] | 734.647.4701

www.aiaa.org/scitech2014 52 #aiaaSciTech 5–9 JANUARY 2015 KISSIMMEE, FLORIDA

Challenges for aerospace science, SECURE YOUR SPONSORSHIP TODAY! research, and development will linger Text message Merrie Scott at 703.674.7324 into 2015. But it’s basic human nature to ﬁnd innovative solutions – particularly in the ﬁeld of aerospace – to overcome BOOK YOUR EXPOSITION SPACE NOW! challenges and create new opportunities. Text message Chris Grady at 703.727.3806 We’ll see you at AIAA SciTech 2015 when we discover the science and STAY INFORMED! technologies that will shape the future Sign up for email alerts at of aerospace! www.aiaa-SciTech.org AIAA SCITECH 2015 WILL FEATURE THE FOLLOWING CONFERENCES: 23rd AIAA/ASME/AHS Adaptive Structures Conference 53rd AIAA Aerospace Sciences Meeting AIAA Atmospheric Flight Mechanics Conference AIAA Guidance, Navigation, and Control Conference AIAA Modeling and Simulation Technologies Conference 11th AIAA Multidisciplinary Design Optimization Specialist Conference 17th AIAA Non-Deterministic Approaches Conference AIAA Spacecraft Structures Conference (formerly the AIAA Gossamer Systems Forum) 56th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference 8th Symposium on Space Resource Utilization 33rd ASME Wind Energy Symposium