16–20 JUNE 2014 ATLANTA, GA

AVIATION’S GLOBAL PROMISE – CHALLENGES AND OPPORTUNITIES

FINAL PROGRAM www.aiaa-aviation.org #aiaaAviation Premier Sponsor 14-315 © 2014 Lockheed Martin Corporation Lockheed 2014 ©

BUILDING THE FOUNDATION FOR INNOVATION At Lockheed Martin, we know that innovation and creativity are critical to solving complex business problems. We are proud to support this year’s AVIATION 2014 Forum and salute its mission to bring industry together to address the challenges of today and tomorrow.

www.lockheedmartin.com Executive Steering Committee AIAA AVIATION 2014 Welcome

Welcome to Atlanta and to AVIATION 2014; we’re excited to share this year’s program with you as we explore aviation’s global promise! An essential driver of economic growth and stability, the aviation enterprise is in a phase of evolving business models, increased efficiency demands, emerging manufacturing methods, and constantly evolving technology integration. These trends offer unprecedented Juan Alonso opportunities and challenges for new capabilities that could transform the way we Stanford University utilize this critical asset. This year’s forum will build on the foundation of AVIATION 2013 to stimulate thought-provoking conversations among industry leaders and the engineering and technical professionals that develop and operate aviation systems. A full program of detailed technical discussions will underpin the high-level plenary and panel conversations to provide a wide-ranging overview of the state of the art in our industry. Jennifer Byrne In addition to cutting-edge technical research presentations, industry executives Lockheed Martin Aeronautics and thought-leaders will discuss challenges and opportunities associated with international aviation integration and operations, global supply chain and risk management, NextGen and SESAR implementation, and technology development and implementation. We’ve invited local Atlanta aviation companies to discuss how they operate internationally from a worldwide hub. Government and industry experts from around the world will address the future of CFD and how it will impact the way we design and certify future aviation systems. Entrepreneurs and policymakers will Victoria Cox discuss the implications of and growing demand for the increased use of unmanned Federal Aviation Administration (retired) platforms in an already crowded airspace. These are just a few of the discussions planned for the forum this year. Everyone involved in the planning has worked to develop a robust, timely, and interesting program; we hope you take advantage of the many learning and networking opportunities throughout the week.

AVIATION 2O14 is proud to feature the following conferences: David R. Maroney 20th AIAA/CEAS Aeroacoustics Conference 7th AIAA Flow Control Conference The MITRE Corporation 30th AIAA Aerodynamic Measurement Technology and 44th AIAA Fluid Dynamics Conference Ground Testing Conference 19th AIAA International Space Planes and Hypersonic AIAA/3AF Aircraft Noise and Emissions Reduction Systems and Technologies Conference Symposium 11th AIAA/ASME Joint Thermophysics and Heat 32nd AIAA Applied Aerodynamics Conference Transfer Conference AIAA Atmospheric Flight Mechanics Conference 21st AIAA Lighter-Than-Air Systems Technology 6th AIAA Atmospheric and Space Environments Conference Conference 15th AIAA/ISSMO Multidisciplinary Analysis and John O’Leary 14th AIAA Aviation Technology, Integration, and Optimization Conference Airbus Americas Operations Conference AIAA Modeling and Simulation Technologies Conference AIAA Balloon Systems Conference 45th AIAA Plasmadynamics and Lasers Conference AIAA Flight Testing Conference 7th AIAA Theoretical Fluid Mechanics Conference

www.aiaa-aviation.org 3 #aiaaAviation Get Your Conference Info on the Go!

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FEATURES HOW TO DOWNLOAD Browse Program Any version can be run without an active Internet connection! You can also sync an itinerary you created online with the app by entering your unique itinerary name. View the program at your fingertips MyItinerary Mobile App MyItinerary Web App My Itinerary For optimal use, we recommend • For optimal use, we recommend: iPhone 3GS, iPod Touch (3rd generation), 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=8 Take notes during sessions • Download the MyItinerary app by Select the meeting “AIA A Aviation 2014” scanning the QR code or accessing City Map http://download.abstractcentral.com/ See the surrounding area and aiaa-mav14/index.htm the Hyatt Regency Atlanta • 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 #aiaaAviation

14-101 IntroContents

Welcome 3

Forum Overview 6 INTRODUCTION

Sponsors and Supporters 8

Keynote Speakers and Plenary Sessions 9

Special Sessions & Events 10 www.twitter.com/aiaa

Highlighted Sessions 12 www.facebook.com/AIAAfan HIGHLIGHTS Networking Events 13 www.youtube.com/wwwaiaaorg Educational Events 14 www.linkedin.com/companies/aiaa Recognition Events 15 www.flickr.com/aiaaevents Exposition Hall 19 http://bit.ly/1qCO7Qf

EXPOSITION Exhibitors 21 Join the conversation! General Information 24 #aiaaAviation

Author and Session Chair Information 25 On-Site Wi-Fi Information Network Name: AIAA 2014 ITAR Information 26 Password: aiaa2014 GENERAL

Organizing Committee 27

Committee Meetings 28

Sessions at a Glance 31

Author and Session Chair Index 41 AIAA is the world’s largest technical society dedicated to the global aerospace profession. With more than Technical Zones 148 PROGRAM 35,000 individual members worldwide, and one hundred corporate members, AIAA brings together industry, academia, and government to advance engineering Venue Map 149 and science in aviation, space, and defense. www.aiaa.org www.aiaa-aviation.org 5 #aiaaAviation IntroForum Overview

SATURDAY/ MONDAY TUESDAY SUNDAY 14 – 15 June 16 June 17 June 0700 hrs Networking Breakfast (0700 – 0800 hrs)

0730 hrs Speakers’ Briefing Speakers’ Briefing

0800 hrs Opening Keynote Plenary Panel 0830 hrs

0900 hrs Networking Break Networking Break in Exposition Hall

0930 hrs Panel: Aviation’s Panel: Aviation’s Challenges & 1000 hrs Challenges & Opportunities - Opportunities - Perspectives from Exposition 1030 hrs Georgia’s Global Brazil & China Hall Technical Technical Perspectives Open Sessions Sessions 1100 hrs

1130 hrs Continuing 1200 hrs Education Course and 1230 hrs Workshop Awards Luncheon: Celebrating 1300 hrs Networking Lunch on Own Networking Lunch on Own Achievements in Aerospace Sciences 1330 hrs

1400 hrs Panel: FAA Has Panel: Transformative 1430 hrs Selected UAS Exposition Aerospace System Test Sites – Hall Analysis, Design, 1500 hrs What Happens Open and Certification: Next? Technical A Vision for CFD Technical 1530 hrs Networking Break Networking Break Sessions in 2030 Sessions 1600 hrs Rising Leaders in Aerospace Forum 1630 hrs Leadership Exchange and Speed Networking 1700 hrs Hall Closed

1730 hrs Rising Leaders Fluid Dynamics William Littlewood in Aerospace Award Lecture Memorial Lecture 1800 hrs Forum Panel

1830 hrs Rising Leaders in Aerospace 1900 hrs Forum Reception William Littlewood Memorial Reception in Exposition Hall

1930 hrs

2000 hrs

2030 hrs

2100 hrs

2130 hrs

2200 hrs

www.aiaa-aviation.org 6 #aiaaAviation IntroForum Overview

WEDNESDAY THURSDAY FRIDAY 18 June 19 June 20 June 0700 hrs Networking Breakfast (0700 – 0800 hrs) Networking Breakfast (0700 – 0800 hrs)

0730 hrs Speakers’ Briefing Speakers’ Briefing Speakers’ Briefing

0800 hrs Plenary Panel Keynote Plenary Panel 0830 hrs

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

0930 hrs Keynote: Panel: Toward an Panel: NASA Aviation Noise Integrated Aeronautics Vision 1000 hrs Exposition Exposition & Emissions Global ATM – for the Hall Hall Reduction: NextGen/Sesar 21st Century: 1030 hrs Open Open Technical Challenges & Technical Technical Why a New Sessions Opportunities Sessions Sessions Strategy? 1100 hrs

1130 hrs Panel: Research Networks–Progress 1200 hrs & Future Plans

1230 hrs Awards Luncheon: Celebrating 1300 hrs Luncheon in Exposition Hall Achievements Networking Lunch on Own Networking Lunch on Own in Aircraft and 1330 hrs Atmospheric Systems Exposition 1400 hrs Hall Panel: Getting Panel: Creating Open Ready for the 1430 hrs a Successful Next Billion Commercial Dollar Aerospace 1500 hrs UAS Business Industry – The Environment– Low Altitude Technical Technical Technical 1530 hrs Networking Break Challenges & Networking Break Frontier Networking Break Sessions Sessions Sessions Opportunities 1600 hrs AMT Award Lecture 1630 hrs

1700 hrs

1730 hrs Thermophysics Aeroacoustics Aerodynamics Award Lecture Award Lecture Award Lecture 1800 hrs

1830 hrs

1900 hrs

1930 hrs Aeroacoustics Award Banquet

2000 hrs

2030 hrs

2100 hrs

2130 hrs

2200 hrs

www.aiaa-aviation.org 7 #aiaaAviation IntroSponsors and Supporters

Premier Sponsor

Other Sponsors

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www.aiaa-aviation.org 8 #aiaaAviation IntroKeynote Speakers and Plenary Sessions

Get the big picture on Aviation from the thought-leaders in the field during these high-level discussions and presentations.

Monday, 16 June Wednesday, 18 June 0800–0900 hrs Centennial I/II 0800–0900 hrs Centennial I/II

Opening Keynote Global Supply Chain Challenges and Opportunities Moderator: Trevor Stansbury, President, Supply Dynamics e Global Economic Impact of the Panelists: F-35 Lightning II Program Duane Hawkins, Senior Vice President, Supply Chain, Orlando Carvalho, Executive Vice Spirit AeroSystems President, Lockheed Martin Aeronautics Kurt Miller, Program Management – Subcontract Director, Lockheed Martin Aeronautics Tuesday, 17 June Thursday, 19 June 0800–0900 hrs Centennial I/II 0800–0900 hrs Centennial I/II Integration and Interoperability: Fly Smarter, Fly Cleaner, Fly Safer Thursday Morning Keynote Moderator: Ben Iannotta, Editor-in-Chief, Aerospace America NextGen Implementation Panelists: Challenges and Opportunities in an International Context Peter Cerda, Regional Vice President, The Americas, International Air Transport Association Michael Whitaker, Deputy Administrator, FAA Steve Kong, Business and Technical Development Manager, Inmarsat Aviation Allan McArtor, Chairman and CEO, Airbus Group, Inc. Tony Ng, Lockheed Martin Fellow, Lockheed Martin Corporation Friday, 20 June 0800–0900 hrs Centennial I/II 1230–1400 hrs Regency VII Aeronautics Technology Development Fly Your Ideas with Airbus Moderator: Glenn Roberts, Chief Engineer, The MITRE Corporation Join Airbus at AVIATION 2014 to find out more about Airbus’ global student challenge, network and enjoy lunch with Airbus Panelists: representatives. Airbus Fly Your Ideas challenges students Steve Bradford, Chief Scientist - Architecture & NextGEN worldwide to develop innovative ideas for a sustainable aviation Development, Office of the Chief Scientist, ANG-3 industry, with the chance to win €30,000 and shape the future Spiro Lekoudis, Director of Weapons Systems, Office of the of aviation. During this interactive event, Charles Champion, Assistant Secretary of Defense for Research and Engineering, Airbus Executive Vice President Engineering and patron of the United States Department of Defense competition will be joined by previous Fly Your Ideas Finalists to Al Romig, Vice President & Program Manager, Skunk Works share their insights and answer your questions. The event is free Engineering and Advanced Systems, Lockheed Martin of charge but you must register in advance by going to Aeronautics Company. www.airbus-fyi.com Jaiwon Shin, Associate Administrator for Aeronautics Research Mission Directorate, NASA Headquarters Speaker: Charles Champion, Airbus Executive Vice President Engineering

www.aiaa-aviation.org 9 #aiaaAviation Special Sessions & Events

These Forum 360 conversations with experts will cover a spectrum of timely topics including programs, systems, policy, operations, applications, platforms and more!

Monday, 16 June Tuesday, 17 June 0930–1130 hrs Regency VI 0930–1100 hrs Regency VI Aviation’s Challenges & Opportunities - Georgia’s Aviation’s Challenges & Opportunities - Global Perspectives Perspectives from Brazil & China Moderator: Steve Justice, Director, Georgia Center of Innovation Moderator: Joao Luis Azevedo, Senior Research Engineer, for Aerospace Instituto de Aeronautica e Espaco Panelists: Panelists: Jack Crisler, Vice President, New Business, Air Mobility, Luis Carlos Affonso, Chief Operating Officer, Embraer Special Forces, and Maritime Programs, Lockheed Martin Commercial Aviation Aeronautics Company Zhenghong Gao, Professor, Northwestern Polytechnical Steve Dickson, Senior Vice President–Flight Operations, Delta University Air Lines Carlos Americo Pacheco, Rector, Instituto Tecnologico de Al Hegner, Director – Base Maintenance, Delta Air Lines Aeronautica Guoqing Wang, President, Chinese Aeronautical Radio Electronics Research Institute 1400–1630 hrs Regency VI

Transformative Aerospace System Analysis, 1400–1600 hrs Regency VI Design and Certification: A Vision for CFD in 2030 Moderator: Robert D. Gregg III, Boeing Commercial Airplanes FAA Has Selected UAS Test Sites - Chief Aerodynamicist, The Boeing Company What Happens Next? Panelists: Moderator: Rich Christiansen, Vice President, Sierra Lobo, Inc. Wilson Felder, Distinguished Service Professor, School of Panelists: Systems and Enterprises, Stevens Institute of Technology Ro Bailey, Director, Pan-Pacific UAS Test Range Complex Parviz Moin, Franklin P. and Caroline M. Johnson Professor, Luis Cifuentes, Vice President, Division of Research, Department of Mechanical Engineering, Stanford University Commercialization and Outreach, Texas A&M University – Stephen Morford, Chief Engineer, Systems Analysis and Corpus Christi Aerodynamics, Pratt & Whitney Rose Mooney, Executive Director, Mid-Atlantic David Schuster, NASA Technical Fellow for Aerosciences, NASA Aviation Partnership Engineering and Safety Center, NASA Langley Research Al Palmer, Director, Center for UAS Research, Education and Center Training for John D. Odegard School of Aerospace Sciences, Jeffrey P. Slotnick, Boeing Technical Fellow, Computational University of North Dakota Sciences & Aerodynamics, Boeing Research & Technology Elizabeth Soltys, Program Manager, FAA UAS Test Sites Cord-Christian Rossow, Director, Institute of Aerodynamics Thomas Wilczek, Thomas Aerospace & Defense Industry and Flow Technology, German Aerospace Center (DLR) Liaison, Governor’s Office of Economic Development, Nevada UAS Test Site Ray Young, Technical Director, NUAIR

1730–1830 hrs Regency VI William Littlewood Memorial Lecture Axel Krein, Senior Vice President, Research and Technology, Airbus

Sponsored by:

www.aiaa-aviation.org 10 #aiaaAviation IntroSpecial Sessions & Events

Wednesday, 18 June Thursday, 19 June 0930–1130 hrs Regency VI 0930–1100 hrs Regency VI Aviation Noise and Emissions Reduction: Toward an Integrated Global ATM — NextGen/Sesar Challenges and Opportunities Moderator: Victoria Cox, Former Assistant Administrator for Carl Burleson, Acting Assistant Administrator for Policy, NextGen, FAA (retired) International Affairs and Environment, FAA Panelists: Dragoş Preda, Head of Flight Operations Data Management Edward Bolton, Assistant Administrator for NextGen, FAA ANG-1 Office, TAROM Marc Hamy, Vice President, SESAR Deployment, Airbus ProSky

1130–1230 hrs Regency VI 1400–1600 hrs Regency VI Research Networks — Progress & Future Plans Getting Ready for the Next Billion Dollar Moderator: Dominique Collin, Head of Acoustics, Safran Aerospace Industry — The Low Altitude Frontier Group, X-Noise Network Coordinator Moderators: Parimal Kopardekar, Manager, NextGen Concepts Panelists: and Technology Development Project, NASA Ames Research Ralph Cavalieri, Director, FAA Center of Excellence - Center and B. Danette Allen, Chief Technologist for Autonomy, Alternative Jet Fuels & Environment (ASCENT), Washington NASA Langley Research Center State University Panelists: Sylvain Cofsky, GARDN Executive Director Jesse Kallman, Global Business Development & Regulatory Janina Scheelhaase, ECATS Representative, DLR German Affairs, Airware Aerospace Center Andres Lacher, UAS Integration Research Lead, The MITRE Corporation 1400–1630 hrs Regency VI David Maroney, Principal Systems Engineer – Civil UAS Integration, The MITRE Corporation Creating a Successful Commercial UAS Business Rose Mooney, Executive Director, Mid-Atlantic Aviation Environment — Challenges & Opportunities Partnership Moderator: John Langford, CEO, Aurora Flight Sciences Mark Moore, Aerospace Engineer, NASA Langley Research Center Panelists: Nicholas Alley, President and CEO, Area-I, Inc. Friday, 20 June Morgan Cloud, Charles Howard Candler Professor of Law, 0930–1130 hrs Regency VI Emory University Steve Justice, Director, Georgia Center of Innovation NASA Aeronautics Vision for the 21st Century: for Aerospace Why a New Strategy? John Lambert, Senior Vice President, Nexutech Moderator: Robert Pearce, Director – Strategy, Architecture Rose Mooney, Executive Director, Mid-Atlantic Aviation & Analysis, NASA Aerospace Research Mission Directorate; Partnership NASA Headquarters Elizabeth Soltys, Program Manager, FAA UAS Test Sites Panelists: John Cavolowsky, Program Director – Airspace Operations and Safety, NASA Aeronautics Research Mission Directorate; NASA Headquarters Jay Dryer, Program Director – Advanced Air Vehicles Program, NASA Aeronautics Research Mission Directorate; NASA Headquarters Douglas Rohn, Program Director – Transformative Aeronautics Concepts, NASA Aeronautics Research Mission Directorate; NASA Headquarters Ed Waggoner, Program Director – Integrated Aviation Systems, NASA Aeronautics Research Mission Directorate; NASA Headquarters www.aiaa-aviation.org 11 #aiaaAviation IntroHighlighted Sessions

Sponsored by:

AIAA’s Rising Leaders in Aerospace Forum is a special initiative taking place during AVIATION 2014 that provides a forum for young aerospace leaders, age 35 and under, to learn from and engage with others. The multidimensional program features a leadership exchange/speed mentoring, panel session, Q&A with top industry leaders, and multiple opportunities for networking. This exciting and energetic forum will provide access to top aerospace leaders and their perspectives, with subject matter relevant to your career stage.

Program Agenda

Forum Chair: Ryan Rudy, Boeing Engineering Operations and Leadership Exchange and Speed Networking Technology Tuesday, 17 June International North Panel – Getting Involved 1600–1730 hrs Monday, 16 June International North Senior members of corporations and AIAA will be taking 1730–1830 hrs time to meet with people and share their experiences. This is a great way to get some insight from top-level officials and make This panel will have speakers that have been involved some great new contacts. And, maybe, they will end up being with AIAA in various ways. Their involvement with AIAA a mentor for more than just this event. Don’t miss a terrific comes from many different perspectives. See the different opportunity. ways you can get involved with AIAA: Board of Directors, Technical Committees, Standing Committees, local officer, or Senior Mentors: participant. Kathleen Atkins, Lockheed Martin Aeronautics/Director USMC/USCG C-130 Program Moderator: Ben Marchionna, Lockheed Martin Aerospace Cees Bil, Professor/Royal Melbourne Institute of Technology Panelists: Wilson Felder, Stevens Inst. Of Tech, FAA, TRW, US Military Kathleen Atkins, Lockheed Martin Aeronautics – AIAA Basil Hassan, Sandia National Laboratories/Manager, Aerospace Technical Activities Committee Systems Analysis Department Cees Bil, RMIT – Region/Section Officer, Technical Committee Sandy Magnus, AIAA/Executive Director member Mark Maughmer, Professor/Penn State University – 2014 Piper Networking Reception General Aviation Award Winner John O’Leary, Vice President, Engineering/Airbus Americas Monday, 16 June International North 1830–1930 hrs Alex Smits, Professor/Princeton University The reception is a perfect opportunity for young leaders to Dani Soban, Aerospace Lecturer/Queen’s University Belfast mingle with others who will be participating in the forum as Tony Springer, NASA/Lead Communications and Education attendee, presenter, or veteran professional. Come meet other participants in a casual environment. You’re bound to see them again throughout the week.

www.aiaa-aviation.org 12 #aiaaAviation IntroNetworking Events

Understanding the importance of networking with colleagues new and old, a series of activities have been planned that will help you connect with current colleagues and new acquaintances. Twitter Kiosks William Littlewood Memorial Reception There are several Twitter Kiosks in various locations. Tuesday, 17 June Exposition Hall Real-time tweets with the hashtag #aiaaAviation will be 1830–2000 hrs displayed on the monitor. To learn how to use Twitter visit A welcome reception will be held on Tuesday, 17 June, www.wikihow.com/Use-Twitter. 1830–2000 hrs, in the Exposition Hall. Take this opportunity Twitter Contest! The user with the most tweets will be to engage new contacts and refresh old ones. A ticket for the awarded an iPad Mini. For contest details and rules, please visit reception is required and included in the registration fee where www.aiaa-aviation.org/twittercontest. indicated. Additional tickets for guests may be purchased upon Sponsored by: registration or on site, as space is available. Sponsored by:

Networking Breakfasts Luncheon in the Exposition Hall A great way to start the day and interact with colleagues old Wednesday, 18 June Exposition Hall and new, networking breakfasts will be offered on Tuesday– 1230–1400 hrs Thursday, 0700–0800 hrs, on the Ballroom Level. This event is open to all forum attendees (no tickets are required). Networking Coffee Breaks CALL FOR NOMINATIONS Networking coffee breaks allow even more time for making AIAA/AAAE/ACC JAY HOLLINGSWORTH SPEAS new contacts, continuing discussions from sessions, visiting the exposition hall, or checking emails and voicemails to keep AIRPORT AWARD in touch with the office. Networking coffee breaks will be The award is presented to the nominee(s) judged to have located in the locations at the following times: contributed most significantly in recent years to the Monday, 16 June Meeting Room Foyers enhancement of relationships between airports and/or 0900–0930 hrs and 1530–1600 hrs heliports and their surrounding environments via exemplary innovation that might be replicated elsewhere. Recipient Tuesday, 17 June Exposition Hall receives a certificate and $7,500 USD honorarium. 0900–0930 hrs and 1530–1600 hrs Nominations must be submitted to AIAA on or before Wednesday, 18 June Exposition Hall 1 October 2014. For more information, contact AIAA Honors 0900–0930 hrs and 1530–1600 hrs and Awards at 703.264.7623 or at [email protected]. Thursday, 19 June 0900–0930 hrs Exposition Hall 1530–1600 hrs Meeting Room Foyers Friday, 20 June Meeting Room Foyers 0900–0930 hrs and 1530–1600 hrs

www.aiaa-aviation.org 13 #aiaaAviation IntroEducational Events

These activities are designed to provide participants with valuable knowledge, experience, and interaction. Electric Cargo Airplane Workshop NEQAIR Tutorial Sunday, 15 June Chicago A Thursday, 19 June Executive Conference Room 219 0800–1600 hrs 1400–1500 hrs This workshop will introduce 6–12 grade educators to the Open to all conference attendees concept and utility of a tethered flight engineering challenge. NEQAIR has been NASA’s main radiation code for the last The instructors, using curriculum that has been mapped to 30 years. It is a line-by-line radiation code that computes national standards, will help participants build an airplane spontaneous emission, absorption and stimulated emission with maximum dimensions of 3’ in length, width, and height due to transitions between various energy states of chemical that can carry the maximum amount of cargo as it flies around species along a line-of-sight. There have recently been a power pole that supplies electricity and mechanical support many substantial upgrades to the code (both in terms of the via a tether. efficiency in running the code, and the physics). This tutorial At the conclusion of this workshop, educators will have the will detail the latest updates, as well as show how to run and necessary tools to help students understand how engineers obtain the code. combine science, math, research and experimentation to build a successful cargo plane. Cost – free to 6–12 grade educators. You must register in advance! Instructors: Paul Wiedorn is a Technology and Engineering educator at Wilde Lake High School in Columbia, Maryland. A 1978 graduate of the Naval Academy, he has been able to apply his degrees in Naval Architecture and his engineering experience to help his students excel in the Maryland Engineering Challenges. Thomas Milnes is a Principal Mathematician and Navigation Modeling Section Head at the Johns Hopkins University/Applied Physics Laboratory (JHU/APL) and an expert at Strategic and Underwater Navigation Systems and Instrumentation. He is organizer and head judge for the Maryland Engineering Challenges Elementary School Paper Airplane and Middle and High School Electric Cargo Plane Challenges.

www.aiaa-aviation.org 14 #aiaaAviation Recognition Events

Join with us throughout AVIATION 2014 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. For over 75 years AIAA has been a champion to make sure that aerospace professionals are recognized for their contributions.

Monday, 16 June Aerodynamic Measurement 1730–1830 hrs Regency Ballroom VII Technology Award Fluid Dynamics Award Lecture Alexander J. Smits Eugene Higgins Professor of Mechanical Mixing in Turbulent Combustion: and Aerospace Engineering Physics and Computational Department of Mechanical and Aerospace Engineering Challenges Princeton University Paul E. Dimotakis, John K. Northrop Princeton, New Jersey Professor of Aeronautics and Professor of “For advancement of quantitative Applied Physics, California Institute of techniques in extreme conditions including Technology high Reynolds numbers and compressible flows, and in particular for research aiding Tuesday, 17 June understanding of hot-wire anemometry.” 1230–1400 hrs Centennial I/II Aerodynamics Award Awards Luncheon: Celebrating Achievements Michael S. Selig in Aerospace Sciences Associate Professor Aerospace Engineering Department A ticket for the luncheon is required and included in the University of Illinois at Urbana- registration fee where indicated. Additional tickets for guests Champaign may be purchased upon registration or on site, as space is Urbana, Illinois available. “In recognition of outstanding contributions The following awards will be presented: to applied aerodynamics research, design, and education, including leadership in the Aeroacoustics Award development and public dissemination of Edward J. Rice airfoil and propeller data.” Aerospace Engineer (Retired) NASA Glenn Research Center Fluid Dynamics Award Cleveland, Ohio Paul E. Dimotakis “For seminal contributions to the theories John K. Northrop Professor of Aeronautics of aircraft engine duct noise radiation and and Professor of Applied Physics grazing flow liner optimization.” California Institute of Technology Pasadena, California “For fundamental to turbulent mixing and combustion through careful and thorough experiments using novel techniques.”

www.aiaa-aviation.org 15 #aiaaAviation Recognition Events

Tuesday, 17 June (continued) Sustained Service Award 1730–1830 hrs Regency Ballroom VII Eric J. Jumper Professor Ground Testing Award University of Notre Dame Jeffrey Haas Notre Dame, Indiana Chief, Testing Division (retired) “For sustained service to AIAA as a member, Facilities and Testing Directorate Technical Committee member, Meeting NASA Glenn Research Center Chair, prolific author, and Student Section Cleveland, Ohio Faculty Advisor.” “For exceptional management of NASA Glenn Research Center’s test facility assets; Thermophysics Award for significant contributions to advance Van P. Carey aerodynamic and propulsion ground testing; and for leadership and service to AIAA.” Professor, A. Richard Newton Chair Mechanical Engineering Department University of California at Berkeley James A. Van Allen Space Berkeley, California Environments Award “For seminal and sustained contributions Stamatios M. Krimigis to the field of liquid-vapor phase change Emeritus Head, Space Department thermophysics, particularly near-interface Johns Hopkins University/Applied nano-scale and micro-scale phenomena, and Physics Laboratory transport in liquid-vapor systems.” Laurel, Maryland Aerodynamic Measurement Testing Best Paper “For pioneering studies of the radiation environment around all solar system planets “Dual-Pump CARS Of Air In A Heated Pressure Vessel Up To 55 and of interplanetary charged particles from Bar and 1300 K,” AIAA 2014-1098, Luca Cantu, Emanuela Gallo, Mercury to the local interstellar medium.” and Andrew Cutler, George Washington University and Paul Danehy, NASA Langley. Losey Atmospheric Sciences Award Applied Aerodynamics Best Paper John Hallett “Over Wing Nacelle Installations for Improved Energy Research Professor Emeritus Efficiency,” AIAA 2013-2920, John Hooker and Andrew Wick, Division of Atmospheric Sciences Lockheed Martin Aeronautics Company; Cale Zeune, Air Force Desert Research Institute Research Laboratory, Wright-Patterson AFB; and Anthony Reno, Nevada Agelastos, Sandia National Laboratories. “For outstanding scholarship that has led to a better understanding of the fundamental Atmospheric Flight Mechanics Best Paper processes of cloud microphysics and for “Flight Testing of a Subscale Aeroservoelastic Aircraft,” AIAA exceptional leadership as a mentor and a 2014-0032, Jeffrey Ouellette, Mayuresh Patil and Craig Woolsey, teacher of atmospheric physics.” Virginia Polytechnic Institute and State University.

Plasmadynamics and Lasers Award David Weaver Best Student Paper John T. Lineberry “Adjoint-Based Aerothermodynamic Shape Design of President and General Manager (retired) Hypersonic Vehicles in Non-Equilibrium Flows,” AIAA 2014- LyTec LLC 0513, Sean R. Copeland, Francisco Palacios, and Juan J. Alonso, Manchester, Tennessee Stanford University. “In recognition of a distinguished career in plasmadynamics and Fluid Dynamics Best Paper magnetohydrodynamics, for major “Direct Numerical Simulation Of The Aeroelastic Response Of contributions to terrestrial and aerospace A Panel Under High Speed Turbulent Boundary Layers,” AIAA applications, and fostering of scientific 2013-3200, Christopher Ostoich, Daniel Bodony, and Philippe and technological advancements through Geubelle, University of Illinois at Urbana-Champaign. international collaborations and AIAA.”

www.aiaa-aviation.org 16 #aiaaAviation IntroRecognition Events

Tuesday, 17 June (continued) Wednesday, 18 June Ground Testing Best Paper 1600–1700 hrs Regency Ballroom VII “Deployment of Particle Image Velocimetry into the Lockheed Aerodynamic Measurement Martin High Speed Wind Tunnel,” AIAA 2014-1238, Steven Beresh, Justin Wagner, Brian Pruett, and Russell Spillers, Sandia Technology Award Lecture National Laboratories; Michael McWithey and Jeffrey Gary, Lockheed Martin Missiles and Fire Control; Kurt Chankaya, Nanoscale Instrumentation for Lockheed Martin Space Systems. Measuring Turbulence Alexander J. Smits, Eugene Higgins Modeling and Simulation Best Papers Professor of Mechanical and Aerospace Engineering, Department of Mechanical “Propeller Slipstream Model for Small Unmanned Aerial and Aerospace Engineering, Princeton Vehicles,” AIAA 2013-4907, Waqas Khan, Ryan Caverly, and University Meyer Nahon, McGill University. 1730–1830 hrs Regency Ballroom VII “Modeling Wake Vortex Roll-Up and Vortex-Induced Forces and Moments for Tight Formation Flight,” AIAA 2013-5076, André Kaden and Robert Luckner, Technical University of Berlin. Thermophysics Award Lecture ermophysics of Vaporization Plasmadynamics and Lasers Best Paper and Condensation Processes – A “Experimental And Numerical Study Of Fast Gas Heating And Nanoscale Perspective O Atom Production In A Capillary Nanosecond Discharge,” Van P. Carey, Professor, A. Richard AIAA 2014-1030, Andrei Klochko, Arthur Salmon, Joseph Newton Chair, Mechanical Engineering Lemainque, Jean-Paul Booth, and Svetlana Starikovskaya, Ecole Department, University of California at Polytechnique; Nikolay Popov, Moscow State University; and Berkeley Mark Kushner and Zhongmin Ziong, University of Michigan. 1730–1830 hrs Regency Ballroom VI Plasmadynamics and Lasers Best Student Paper “Simulation of Reacting Flows in Magnetic Fields with Aeroacoustics Lecture Preconditioning,” AIAA 2013-2754, Amrita Lonkar, Francisco Palacios, and Juan J. Alonso, Stanford University. Turbofan Noise Research — Reconciling eory and Measurement Winners of the Aeroacoustics and Atmospheric Flight Brian J. Tester, ISVR, Southampton Mechanics Student Paper Competitions will also be announced. University 1730–1830 hrs Regency VI William Littlewood Memorial Lecture Axel Krein, Senior Vice President, Research and Technology, Airbus

Sponsored by:

www.aiaa-aviation.org 17 #aiaaAviation IntroRecognition Events

Thursday, 19 June Multidisciplinary Design Optimization Award 1230–1400 hrs Centennial I/II Robert A. Canfield Professor and Assistant Department Award Luncheon: Celebrating Achievements in Head Aerospace and Ocean Engineering Aircraft and Atmospheric Systems Virginia Polytechnic Institute and State University A ticket for the luncheon is required and included in the Blacksburg, Virginia registration fee where indicated. Additional tickets for guests may be purchased upon registration or on site, as space is “For pioneering research on design available. optimization methods leading to structural optimization software, application of MDO Sponsored by: to advanced aircraft concepts such as The following awards will be presented: sensorcraft and for leadership in the MDO community.” Aircraft Design Award Boeing 787 Dreamliner Team Piper General Aviation Award Seattle, Washington Mark D. Maughmer Award to be accepted by Professor of Aerospace Engineering Michael Sinnett, Vice President, Product Pennsylvania State University Development, The Boeing Company University Park, Pennsylvania “For the conception, design, and “For contributions to winglet designs on development of the Boeing 787 Dreamliner racing sailplanes, an advance that promoted leading to substantial airliner performance the broader acceptance and diffusion of improvements and significant advances in winglet technology in the general aviation aircraft design and technology.” community.” Hap Arnold Award For Excellence in Hypersonic Systems and Technologies Best Paper Aeronautical Program Management “Design of an Airframe Integrated 3-D Scramjet and Steven H. Walker Experimental Results at a Mach 10 Flight Condition,” AIAA 2012-5910, Luke J. Doherty, Michael K. Smart, and David J. Deputy Director Mee, The University of Queensland. Defense Advanced Research Projects Agency (DARPA) Multidisciplinary Design Optimization Best Paper Arlington, Virginia “Multi-Point, Multi-Mission, High-Fidelity Aerostructural “For outstanding and distinguished Optimization Of A Long-Range Aircraft Configuration,” AIAA leadership and management of the 2012-5706, Rhea Liem, University of Toronto, and Gaetan Air Force science and technology and Kenway and Joaquim Martins, University of Michigan-Ann acquisition at the Pentagon.” Arbor. Hypersonic Systems and Technologies Award Winner of the Multidisciplinary Design Optimization Student Paper Competition will be announced. John I. Erdos President and CEO (retired) 1730–1830 hrs Regency Ballroom VII GASL, Inc. Ronkonkoma, New York Aerodynamics Lecture “For over 40 years of visionary technical and organizational leadership of Low-Speed Airfoil Design and foundational technology, ground test, Application and flight test activities that became Michael S. Selig, Associate Professor, the cornerstones of the international Aerospace Engineering Department, knowledge base of hypersonic systems and University of Illinois at Urbana-Champaign technologies.”

www.aiaa-aviation.org 18 #aiaaAviation IntroExposition Hall

AIAA Hanley Atlanta Innovations Section 116 215 AIAA Pavilion OPAL-RT Exa Technologies Corp AIAA 114 213 Sales Office

Corporate Member & Embry- Desktop Exhibitor ADI Altair CEI GCIA Riddle Aeronautics Lounge 110 209 210 309 310 409 BETA CAE SG Photron Software Pointwise G.R.A.S Cradle Systems 108 207 208 307 308 407 Datakustik GmbH 406

Maplesoft MathWorks Tecplot NASA Lockheed 104 203 Martin 404 dSpace Dunmore ATK 102 201 202 302 402

ENTRANCE

Exhibitors by Booth Number

215 AIAA Atlanta Section 409 Georgia Center of Innovation for Aerospace 210 Altair 116 Hanley Innovations 209 Applied Dynamics International (ADI) 302 Lockheed Martin 402 ATK 104 Maplesoft 308 BETA CAE Systems USA, Inc. 203 MathWorks 309 Computational Engineering International (CEI) 202 National Aeronautics and Space Administration (NASA) 406 DataKustik GmbH 114 OPAL-RT Technologies 310 Desktop Aeronautics 207 Photron 102 dSpace 307 Pointwise, Inc. 201 Dunmore Corporation 108 SG - Space & Ground Engineering Solutions 110 Embry-Riddle Aeronautical University (ERAU) 208 Software Cradle 213 Exa Corporation 404 Tecplot 407 G.R.A.S Sound & Vibration

www.aiaa-aviation.org 19 #aiaaAviation IntroExposition Hall

The exposition hall, located in Centennial Ballroom III/IV is the hub of activity during this event— from seeing exhibitor displays to enjoying networking breaks and other functions, and browsing AIAA publications in the AIAA Pavilion. Make sure you stop by the exposition hall to keep up with the latest happenings! Most networking coffee breaks, luncheons, and receptions are all held in the exposition hall to give attendees and exhibitors the most opportunities to meet and do business. Exposition Hall Hours 30% Off All Books at AIAA AVIATION 2014 Tuesday, 17 June 0900–1230 hrs AIAA Publications is offering a special show discount on all titles 1400–1600 hrs featured at AVIATION 2014. Attendees can take advantage of a 1830–2000 hrs 30% discount off the list price of all books for sale at the AIAA Bookstore located in the AIAA Pavilion. This show special will Wednesday, 18 June 0900–1200 hrs only be available during the forum! Take advantage of these 1230–1600 hrs super savings and visit the AIAA Bookstore!

Thursday, 19 June 0900–1200 hrs Author Information Session Meet Dr. Joseph Schetz , Editor-in-Chief of the AIAA Education AIAA Pavilion Series, to receive information and ask questions about the process of writing and publishing a book with AIAA. Stop by the AIAA Pavilion, located in the Exposition Hall, Tuesday, 17 June, 1900–1930 hrs, in the AIAA Exposition Hall. to browse publications and merchandise, learn about your membership benefits, and meet AIAA staff.

www.aiaa-aviation.org 20 #aiaaAviation Exhibitors AIAA Atlanta Section 215 Computational Engineering International 607 www.aiaa-atlanta.org 2166 N. Salem Street Apex, NC 27523 www.ceisoftware.com [email protected] CEI makes the leading CFD post-processor, EnSight. Altair 210 EnSight creates dazzling animations, compelling images, and 1820 E Big Beaver Road persuasive plots that help you make decisions faster & with Troy, MI 48083 more confidence. www.altair.com [email protected] Datakustik GmbH 406 Altair is a leader in developing simulation-driven designs for Gewerbering 5 leading aerospace customers. Our world-class optimization Greifenberg, Bavaria methods provide designs that are lower weight, higher quality, Germany 86926 Software for Immission Protection and have better performance vs. traditional designs. www.datakustik.com [email protected] Applied Dynamics International 209 DataKustik GmbH is one of the leading manufacturers of 3800 Stone School Road software for immission protection. The company is known for Ann Arbor, MI 48108-2499 its powerful software products CadnaA, CadnaR and Bastian www.adi.com which are rich in features and technical innovations. [email protected] Applied Dynamics helps companies make better use of Desktop Aeronautics Inc. 310 simulation assets through all stages of product development, verification testing, demonstration, training, and maintenance. 1900 Embarcadero Road Suite 101 Our user base includes more than 50% of the Fortune 500 Palo Alto, CA 94303 aerospace and defense companies and extends into marine, www.desktopaero.com power systems, oil & gas, and the automotive industry. [email protected] Desktop Aeronautics provides conceptual aircraft design ATK 402 and shape optimization services to aircraft manufactures UT-03 DSBD and Government agencies, specializing in design for natural PO Box 98 laminar flow (NLF). We also develop and distribute licensed Magna, UT 84044–0098 software that addresses the needs of aircraft designers. We are www.atk.com NASA’s licensed commercial distributor of Cart3D. [email protected] ATK is on the forefront of R&D and manufacture of solid rocket propulsion, aircraft structures, missile components, dSPACE 102 small sats, solar arrays, satellite components, and flares and 50131 Pontiac Trail decoys. ATK provides affordable solutions to meet emerging Wixom, MI 48393-2020 needs. www.dspaceinc.com [email protected] BETA CAE Systems USA, Inc. 412 dSPACE is the world’s leading provider of hardware and software tools for developing and testing sophisticated 29800 Middlebelt Road electronic control systems. dSPACE systems play a vital Suite #100 Farmington Hills, MI 48334 role in product innovation industries. Learn more at: www.ansa-usa.com www.dspaceinc.com. [email protected] BETA CAE Systems is an engineering services company that distributes & supports the industry leading ANSA & META software. ANSA is CAE pre-processing tool for FE & CFD Analysis, for full-model build, from CAD to solver input file, in one integrated environment. META is a post-processor for analyzing results from ANSYS, NASTRAN, ABAQUS, LS- DYNA, PAMCRASH, RADIOSS, MADYMO, FLUENT, STAR CCM, CFD++ & other solvers.

www.aiaa-aviation.org 21 #aiaaAviation Exhibitors DUNMORE Corporation 201 Georgia Center of Innovation 409 145 Wharton Road for Aerospace Bristol, PA 19007 75 Fifth St NW www.dunmore.com R Suite 1200 [email protected] Atlanta, GA 30308 DUNMORE is a manufacturer of engineered films and tapes aerospace.gergiainnovation.org for aerospace, supplying multilayer insulation materials to [email protected] the aerospace industry for over twenty-five years. With a The Georgia Center of Innovation for Aerospace acts as highly technical product base of over 400 certified products, a catalyst, creating opportunities for Georgia aerospace DUNMORE is the trusted source for engineered aerospace companies through access to new technologies, university films and tapes. research, potential business collaborators and current industry information. Embry-Riddle Aeronautical University 110 600 S. Clyde Morris Blvd. Hanley Innovations 116 Daytona Beach, FL 32114 505 Spring Lake Road www.embryriddle.edu Ocala, FL 34472 [email protected] www.hanleyinnovations.com Embry-Riddle Aeronautical University, the world’s largest [email protected] university specializing in aviation and aerospace, offers more 2D and 3D aerodynamic software for Windows. Auto- than 40 baccalaureate, master’s and Ph.D. degree programs. gridding. Fully Integrated Workflow.. Subsonic, Transonic Embry-Riddle educates students at residential campuses and Supersonic Analysis. Present a watertight CAD .stl file of in Daytona Beach, Fl, and Prescott, AZ and through the your project for a personal demonstration of Stallion 3D at our Worldwide Campus with more than 150 locations. booth.

EXA Corporation 213 Lockheed-Martin Corporation 302 55 Network Drive 505 Spring Lake Road Burlington, MA 01803 Ocala, FL 344 781-564-0251 (phone) www.lockheedmartin.com 751-564-0299 (fax) [email protected] www.exa.com [email protected] Lockheed Martin is a global security and aerospace company that is principally engaged in the research, design, Exa Corporation offers a full suite of CFD/CAE simulation development, manufacture, integration and sustainment of design optimization software applications with aerodynamic, advanced technology systems, products and services. thermal and aeroacoustic simulation capabilities in addition to engineering consulting services. Exa’s products and services enable engineers to integrate simulation early in the design Maplesoft 104 process, therefore creating competitive designs, shortening 615 Kumpf Drive product design cycles and speeding time-to-market. Waterloo ON N2V 1K8 www.maplesoft.com G.R.A.S. Sound & Vibration 407 [email protected] Offering experts in a variety of engineering fields, extensive 2234 E Enterprise Parkway Twinsburg, OH 44087 experience in model-based design, and the system-level www.gras.uk modeling and analysis tools MapleSim and Maple, Maplesoft [email protected] can help reduce development risk and bring your products to market faster. G.R.A.S. has concentrated its efforts and expertise on the development and production of front-end acoustic products. This includes in principle all products necessary for the precise and reliable measurement, and recording of acoustic signals, from the transducer to the input of the A/D converter. The main line of instrumentation includes a broad range of standard measurement microphones and preamplifiers, all designed and manufactured in accordance with international standards.

www.aiaa-aviation.org 22 #aiaaAviation IntroExhibitors MathWorks 203 Pointwise, Inc. 307 3 Apple Hill Drive 213 S. Jennings Avenue Natick, MA 01760 Fort Worth, TX 76104 www.mathworks.com/academia www.pointwise.com 508.647.7000 [email protected] The MATLAB and Simulink product families are Pointwise is solving the top problem facing engineering fundamental applied math and computational tools at the analysts today: grid generation and preprocessing for world’s educational institutions. Adopted by more than 5000 computational fluid dynamics. Since 1994, Pointwise has universities and colleges, MathWorks products accelerate the supplied meshing tools to engineers and scientists worldwide. pace of learning, teaching, and research in engineering and science. MathWorks products also help prepare students for careers in industry worldwide, where the tools are widely SG-Space & Ground Engineering Solutions 108 used for data analysis, mathematical modeling, and algorithm 6A Aigiidon Street development in collaborative research and new product Athens, Attica Greece 11853 development. www.sg-incorp.com [email protected] NASA 701 SG Company provides integrated engineering solutions 300 E St. SW for air/space-based earth monitoring systems and develops Washington, D.C. 20024 special techniques for UAS (Unmanned Aerial Systems) earth www.nasa.gov observation applications in various disciplines. Innovate – Explore – Discover – Inspire: NASA highlights its advanced technology development and capabilities in Software Cradle 208 aeronautics, science, and human and space operations, that 70 Birch Alley, Suite 240 also have real world benefits here on Earth, today. Discover Beavercreek, OH 45440 NASA’s current and future missions to Mars and beyond, www.cradle-cfd.com and learn about the Agency’s contributions to the innovation [email protected] economy. Software Cradle is a leading provider of Computational Fluid Dynamics (CFD) software including SC/Tetra (general OPAL-RT TECHNOLOGIES 207 purpose unstructured mesh), scSTREAM (general purpose Cartesian mesh), and HEAT Designer (Cartesian mesh for 1751 Richardson, Suite 2525 Montreal Quebec H3K 1G6 electronics). Since inception in 1984, Cradle has established www.opal-rt.com itself as a major innovator for advancing the role of simulation [email protected] in engineering design. OPAL-RT: From Imagination… to Real-Time. OPAL-RT TECHNOLOGIES is a world leading developer of open, Tecplot, Inc 404 Real-Time Digital Simulators and Hardware-in-the-Loop 3535 Factoria Blvd SE, Suite 550 testing equipment for electrical, electro-mechanical and power Bellevue, WA 98006 electronics systems. Our simulators are used by engineers and 425-653-1200 X236 (phone) researchers at leading manufacturers, utilities, universities and 425-653-9200 (fax) research centers around the world. www.tecplot.com [email protected] Photron 207 Tecplot visualization tools—for simulations, analyses, and experiments—provide insight and understanding into 9520 Padgett Street, Suite 110 the mechanisms inside your data. Information critical in San Diego, CA 92126 pinpointing problems, optimizing designs, and explaining www.photron.com [email protected] physical observations. Photron’s wide range of light sensitive high-speed cameras including systems ideally suited to PIV and DIC, mega pixel to 21,000 frames per second (fps) and 4M pixels producing HD to 2,000 fps. Photron has a slow motion camera for every application.

www.aiaa-aviation.org 23 #aiaaAviation IntroGeneral Information

AIAA Registration and i. By paper number: Click the Membership “Paper Number” link, select the Information Center Hours conference year, and enter the AIAA is your vital lifelong link to the The AIAA Registration and Information paper number. collective creativity and brainpower Center will be located on the Ballroom of the aerospace profession and a ii. Use the Search textbox to champion for its achievements – Level at the Hyatt Regency. Hours are as find papers by author, title, or follows: and nonmembers who pay the full keyword. The Advanced Search conference registration fee will receive Sunday, 15 June 1500–1900 hrs link provides additional search their first year’s AIAA membership at no information and options. Monday, 16 June 0700–1730 hrs additional cost! Students who are not yet – Friday, 20 June 2. All manuscript files submitted by members may apply their registration four days prior to the conference fee toward their first year’s student AIAA ITAR Registration Hours are currently in the proceedings. member dues. (Free membership is Files submitted after that date, both not included in discounted group-rate Monday, 16 June 0930–1730 hrs original and revised manuscripts, registration.) Tuesday, 17 June 0700–1730 hrs will not be available until the final Wednesday, 18 June 0700–1730 hrs proceedings update, which may take Young Professional Guide for up to 15 business days after the last Gaining Management Support day of the conference. Wi-Fi Internet Access On Site Young professionals have the unique 3. Direct any questions concerning AIAA is providing limited Wi-Fi service opportunity to meet and learn from access to proceedings and/or ARC to for attendees to use while on site. To keep some of the most important people in the [email protected]. this service available and optimized for business by attending conferences and all attendees, please do not download files participating in AIAA activities. A detailed larger than 2MB, create multiple sessions Manuscript Revisions online guide, published by the AIAA across multiple devices, or download 1. Manuscript revision is open for all Young Professional Committee, is available multiple files in one session. If you receive presenting authors from 0900 hrs to help you gain support and financial an error message that an AIAA server is Eastern Time, 16 June through 2000 backing from your company. The guide blocking your current IP address, please hrs Eastern Time, 1 July 2014 explains the benefits of participation, offers inform the AIAA registration desk. recommendations and provides an example 2. Revisions submitted for manuscripts letter for seeking management support On-Site Wi-Fi Information already online will not refresh until and funding, and shows you how to get the after the proceedings have been most out of your participation. The online Network Name: AIAA 2014 updated, which may take up to 15 guide can be found on the AIAA website at business days after the last day of the Password: aiaa2014 www.aiaa.org/YPGuide. conference. Conference Proceedings Certificate of Attendance Nondiscriminatory Practices Proceedings for the forum will be AIAA accepts registrations irrespective Certificates of Attendance are available online. The cost is included of race, creed, gender, color, sexual available for attendees who request in the registration fee where indicated. orientation, physical handicap, and documentation at the forum itself. Online proceedings will be available on national or ethnic origin. Please request your copy at the AIAA 16 June 2014. Attendees who register in Registration and Information Center. advance for the online proceedings will Restrictions AIAA offers this service to better be provided with instructions on how to serve the needs of the professional Photos, video, or audio recording access them. Those registering on site will community. Claims of hours or of sessions or exhibits, as well as the be provided with instructions at that time. applicability toward professional unauthorized sale of AIAA-copyrighted Proceedings: education requirements are the material, is prohibited. 1. To view proceedings visit responsibility of the participant. www.aiaa.org >ARC>Meeting Papers. Employment Opportunities a. Log in with the link at the top right of the page. AIAA members can post and browse resumes, browse job listings, and access b. Select the appropriate conference other online employment resources from the list. by visiting the AIAA Career Center at c. Search for individual papers with http://careercenter.aiaa.org. the Quick Search toolbar in the upper-right corner of the page:

www.aiaa-aviation.org 24 #aiaaAviation IntroGeneral Information

Author and Session Chair Information

Speakers’ Briefings in Session Rooms Audiovisual Authors who are presenting papers will meet with session chairs Each session room will be preset with the following: one and co-chairs in their session rooms for a short 30-minute LCD projector, one screen, one microphone and sound briefing on the day of their sessions to exchange bios and review system (if necessitated by room size), and one laser pointer. final details prior to the session. Please attend on the day of Laptop computers will also be provided. You may also use your session(s). Laptops preloaded with the Speaker Briefing your own computer. Any additional audiovisual equipment preparation slides will be provided in each session room. requested onsite will be at cost to the presenter. Please note Speaker’s Briefing schedule is as follows: that AIAA does not provide security in the session rooms and Monday–Friday, 0730–0800 hrs recommends that items of value not be left unattended. Speakers’ Practice Room “No Paper, No Podium” and “No Podium, No Paper” Policy Speakers who wish to practice their presentations may do so in the Williams room located in the Atlanta Conference If a written paper is not submitted by the final manuscript Center (LL3). A sign-up sheet will be posted on the door. In deadline, authors will not be permitted to present the paper at consideration of others, please limit practice time to 30-minute the forum. Also, if the paper is not presented at the forum, it increments. will be withdrawn from the proceedings. It is the responsibility of those authors whose papers or presentations are accepted to Session Chair Reports ensure that a representative attends the conference to present the paper. These policies are intended to improve the quality of All session chairs are asked to complete a session chair report to the program for attendees. evaluate their session for future planning. AIAA has partnered with Canvas Solutions to provide an electronic Session Chair Journal Publication Report form. You can download the FREE mobile app in your App Store, AppWorld, or Marketplace by searching for AIAA has prior publication rights to any paper presented “Canvas Solutions, Inc.” The mobile app is free, so please be at its conferences. Authors who are seeking the opportunity sure to download it. Detailed instructions will be provided in for peer-reviewed publication are encouraged to submit the session rooms. If you do not have a tablet or a smartphone, their papers for consideration by one of the Institute’s simply use the report form as a guide and enter your session archival journals: AIAA Journal; Journal of Aircraft; Journal chair report information at the session chair reporting computer of Guidance, Control, and Dynamics; Journal of Propulsion station located on site near the AIAA registration area. Report and Power; Journal of Spacecraft and Rockets; Journal of data will be collected and used for future planning purposes, Thermophysics and Heat Transfer; or Journal of Aerospace including session topics and room allocations. Please submit Information Systems. Journal scopes and author guidelines and your session chair report electronically by 20 June 2014. instructions can be found in Aerospace Research Central at http://arc.aiaa.org/page/authorresources. You may submit your paper to a journal for review before the conference presentation date: http://mc.manuscriptcentral.com/aiaa.

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

www.aiaa-aviation.org 25 #aiaaAviation IntroITAR Information

International Traffic in Arms Regulations (ITAR) Access to ITAR Sessions: Presenting a Paper, AIAA speakers and attendees are reminded that some Chairing a Session, or Attending an ITAR- topics discussed in the conference could be controlled Restricted Presentation by the International Traffic in Arms Regulations (ITAR). Admittance to the restricted technical papers is controlled by U.S. nationals (U.S. citizens and permanent residents) are the U.S. International Traffic in Arms Regulations (ITAR). responsible for ensuring that technical data they present All attendees, presenters, and session chairs will need to register in open sessions to non-U.S. nationals in attendance or in for the conference and then visit the ITAR Registration Desk to conference proceedings are not export restricted by the ITAR. complete additional registration procedures. Anyone wising to U.S. nationals are likewise responsible for ensuring that they do enter the restricted session room MUST abide by the procedures not discuss ITAR export-restricted information with non-U.S. and submittal of verification documents mandated by the DoD. nationals in attendance. No Exceptions! ITAR-Restricted Sessions: New for This Year Availability of Manuscripts from ITAR-Restricted On Tuesday and Wednesday, a limited number of papers will be Sessions presented in “U.S.-Only” technical sessions. In addition to your forum registration, a separate registration process is required A DVD containing the manuscripts from the ITAR sessions to attend these restricted sessions. Please see the detailed will be available for purchase on site at the forum, by those who information on the ITAR Registration Grid to determine your are registered to attend the ITAR sessions, for $25. There will be individual requirements. no sale or distribution of these papers after the event.

ITAR Electronics Policy No phones, computers (other than the presenter), ipads, cameras, and other electronic devices with cameras or recording capabilities will be permitted in the ITAR session room. There will be a check-in desk in front of the room where you can check these devices during the time you are in the sessions.

Important session information for all attendees wishing to present or attend ITAR papers

AIAA Restricted Papers – ITAR Regulations Session Admittance Policy (Revised 10/19/2012)

Several papers scheduled to be presented at this conference will be restricted papers governed by ITAR (U.S. International Traffic in Arms Regulations). If you plan to attend any presentations restricted by ITAR, you must bring proof of citizenship PLUS the other verification documents as shown below. Please note that only U.S. Citizens and U.S. Resident Aliens can be considered for attendance at these restricted presentations. Admittance to restricted sessions and access to restricted technical papers is implemented and controlled by ITAR . All restricted session attendees (including speakers and session chairs for these sessions) MUST abide by the procedures and submittal of verification documents as noted below – NO EXCEPTIONS: ATTENDEE CLASSIFICATION IDENTIFICATION & PROOF OF EMPLOYMENT REQUIREMENTS U.S. Government Employees 1. Proof of U.S. Citizenship (for example, passport, birth certificate, voters registration card, naturalization papers), AND 2. Personal photographic identification: U.S. Government/Military Photo ID badge, such as CAC card U.S. Citizens 1. Proof of U.S. Citizenship (for example, passport, birth certificate, voters registration card, naturalization papers), AND 2. Personal photographic identification (passport, driver’s license, etc.), AND 3. Certification credentials based on DD Form 2345 (see below for details) Resident Aliens (U.S.) 1. Resident Alien Card, AND 2. Personal photographic identification (passport, driver’s license, etc.), AND 3. Certification credentials based on DD Form 2345 (see below for details)

DD Form 2345 individual certification credentials (required for U.S. & Resident Aliens) MUST be from one of the following: 1. Copy of an approved and active DD2345 for the individual, OR 2. Copy of an approved and active DD2345 for the individual’s employer PLUS evidence of current employment status with that employer (corporate ID, business card, etc.), OR 3. A listing of the individual’s employer in the most recent DoD quarterly Qualified U.S. Contractor Access List PLUS evidence of current employment status with that employer (corporate ID, business card, etc.). DD Form 2345 may be downloaded and completed online in order to apply for approval to be listed on the Qualified U.S. Contractor List, www.dlis.dla.mil/jcp. Allow at least 4-6 week (or longer) prior to the AIAA technical conference dates for you to receive the approval and be listed on the Qualified U.S. Contractor List.

How to get your ITAR Clearance: Bring all of the above listed identification, proof of employment and certification credentials to the AIAA ITAR Registration Desk in the AIAA Registration area. Your documents will be verified and you will be provided with a stamp indicating your ITAR clearance. Photo ID will be checked against your ITAR badge before admittance is granted to any ITAR presentation.

Please be advised that all policies and procedures MUST be followed or admittance to restricted sessions will not be permitted. www.aiaa-aviation.org 26 #aiaaAviation 10/19/2012 IntroOrganizing Committee

Executive Steering Committee Technical Chairs Ground Testing Juan Alonso, Department of Aeronautics Danielle (Dani) Soban, School of Tom Wayman, Gulfstream Aerospace and Astronautics, Stanford University Mechanical and Aerospace Engineering, Corporation Jennifer Byrne, Vice President, Queen’s University Belfast International Space Planes and Hypersonic Technical Operations, Lockheed Martin Andy Broeren, NASA Glenn Research Systems and Technologies Aeronautics Center Adam Siebenhaar, Aerojet Victoria Cox, Former Assistant ITAR Chair Lighter than Air Systems Technology Administrator for NextGen, Federal Elena Garcia, Georgia Institute of Brandon Buerge, Wichita State Aviation Administration (retired) Technology University David R. Maroney, Principal Systems Multidisciplinary Analysis and Optimization Engineer, The MITRE Corporation Technical Discipline Chairs Eliot Winer, Iowa State University John O’Leary, Vice President, Applied Aerodynamics Engineering, Airbus Americas Modeling and Simulation Technologies Brian McGrath, Johns Hopkins Randal Allen, Lonestar Aerospace Organizing Committee Aerodynamic Measurement Technology Plasmadynamics and Lasers Steven J. Beresh, Sandia National General Chair Laboratories Michael White, Ohio Aerospace Institute David R. Maroney, The MITRE Aeroacoustics Theoretical Fluid Mechanics Corporation Stewart Glegg, Florida Atlantic Rodney Bowersox, Texas A&M Integration Program Chair University University Rich Wahls, NASA Langley Research Aircraft Noise and Emissions Reduction Design Engineering Center Symposium Sidney Rowe, NASA International Chair J-P Clarke, Georgia Institute of Digital Avionics Joao Azevedo, R&D Engineer Technology John Moore, Rockwell Collins Membership Chair Atmospheric Flight Mechanics 11th AIAA/ASME Joint Thermophysics G. Alan Lowrey, Lockheed Martin Space Ashok Gopalarathnam, North Carolina and Heat Transfer Conference (AIAA Systems State University representative) Public Policy Chair Atmospheric and Space Environments William A. Wood, NASA Langley John Rose, The Boeing Company Jen-Ching (Paul) Tsao, Ohio Aerospace Research Center Young Professional Chair Institute 11th AIAA/ASME Joint Thermophysics Aviation, Technology, Integration and and Heat Transfer Conference (ASME Ryan Rudy, The Boeing Company Operations representative) Recognition Chair Joe Butterfield, Queen’s University Yaroslav Chudnovsky, Gas Technology Neal Pfeiffer, Mooney Aircraft Belfast Institute Education Chair Balloon Systems Product Support Dave Mitchell, Mitchell Aerospace Michael Fortenberry, Southwest Lori Fischer, Woodward AES Research Research Institute Local Area Representative Flight Testing Amy Kohler Hudnall, Georgia Center of Thane Lundberg, Edwards Air Force Innovation for Aerospace Base Flow Control Noel Clemens, The Ohio State University Fluid Dynamics Dan Bodony, University of Illinois at Urbana-Champaign AVIATION Forum

www.aiaa-aviation.org 27 #aiaaAviation IntroCommittee Meetings

Time Title Location Sunday, 15 June 2014 1400-1500 hrs APATC New Member Orientation Baker 1400-1600 hrs ASME HTD Executive Committee (closed) Vinings 1430-1500 hrs APATC Liaisons Subcommittee Edgewood 1500-1600 hrs APATC Education Subcommittee Edgewood 1500-1600 hrs APATC Honors and Awards Subcommittee Roswell 1500-1600 hrs APATC Membership and Nominations Subcommittee Lenox 1500-1600 hrs APATC Planning Subcommittee Kenneshaw 1500-1600 hrs APATC Publicity and Publications Subcommittee Marietta 1500-1600 hrs GTTC Steering Subcommittee Piedmont 1600-1700 hrs GTTC New Members and Mentors Meeting Hanover C/D/E 1600-1700 hrs FDTC Higher Order Methods DG Spring 1600-1700 hrs APATC Technical Activities Meeting Techwood 1600-1800 hrs FDTC Transition DG Inman 1600-1800 hrs ASME HTD Executive Committee (open) Vinings 1630-1830 hrs FDTC Low Re DG Dunwoody 1700-1800 hrs GTTC Introduction/Overview Hanover C/D/E 1700-1800 hrs APATC Steering Committee Baker 1730-1830 hrs FDTC New Member Orientation Harris 1800-1900 hrs GTTC Aero and Propulsion Subcommittee Hanover C/D/E 1800-2100 hrs Applied Aerodynamics TC Hanover F/G 1800-2100 hrs Atmospheric Flight Mechanics TC Spring 1830-2000 hrs FDTC Steering Committee Edgewood 1900-2000 hrs GTTC Conference Subcommittee Hanover C/D/E 1900-2100 hrs TAC Aircraft and Atmospheric Systems Group Piedmont 2000-2100 hrs GTTC Awards Subcommittee Hanover C/D/E 2100-2200 hrs GTTC Education and Student Activities Subcommittee Hanover C/D/E Monday, 16 June 2014 0800-1000 hrs K-10: Heat Transfer Equipment Chicago A 0800-1200 hrs Future of GTTC Working Group Executive Conf Suite 219 0800-1600 hrs GTTC Internal Balance WG Executive Conf Suite 226 1000-1200 hrs K-11: Heat Transfer in Combustion Chicago B 1130-1400 hrs General Aviation TC Chicago A 1230-1400 hrs Aviation MDO SPC Regency VII 1400-1600 hrs AATC Array Methods Wksp Planning Discussion Embassy C 1500-1600 hrs FDTC Low Order Modeling Tools for AFC DG Executive Conf Suite 219 1500-1630 hrs 2015 ASME/JSME/KSME Planning Meeting Chicago B 1600-1700 hrs FDTC Barriers/Challenges to Tech Transition DG Chicago C 1700-1900 hrs Computational Fluid Dynamics Committee on Standards Executive Conf Suite 219 1730-1830 hrs APATC Missile and Projectile Aeroprediction DG Hanover F 1730-1830 hrs GTTC Committee on Standards Executive Conf Suite 226 1730-1830 hrs APATC Low Boom DG Courtland 1800-1900 hrs HyTASP PC Steering Committee International South www.aiaa-aviation.org 28 #aiaaAviation IntroCommittee Meetings

Time Title Location Monday, 16 June 2014 (continued) 1800-2100 hrs 2015 ASME Congress and Expo Planning Meeting Chicago B 1800-2100 hrs Product Support TC Chicago A 1830-1930 hrs FDTC Turbulence Modeling Benchmarks WG Executive Conf Suite 222 1900-2000 hrs GTTC Publications Subcommittee Hanover B 1900-2000 hrs APATC Aerodynamic Design Optimization DG Chicago C 1900-2030 hrs APATC Validation of Numerical Models DG Hanover C 1900-2100 hrs APATC Rotorcraft Simulations & Performance Predictions DG Hanover A 1900-2100 hrs FDTC Fundamentals Flow Phenomena Subcommittee Embassy A 1900-2100 hrs FDTC Flow Control and Fluid Applications Subcommittee Embassy F 1900-2100 hrs TAC Aerospace Sciences Group Meeting Embassy C 1900-2200 hrs HyTASP PC International South 1900-2200 hrs Air Transportation Systems TC Embassy B 1900-2200 hrs CADWG Embassy D 1900-2200 hrs Digital Avionics TC Chicago D 1930-2130 hrs FDTC CFD Methods Subcommittee Embassy E Tuesday, 17 June 2014 0800-1500 hrs GTTC WT Model Attitude and Deformation Measurement WG Executive Conf Suite 222 0900-1700 hrs GTTC Dual Flow Reference Nozzle WG Chicago D 1000-1100 hrs AVIATION 2015 Executive Steering Committee International South 1100-1200 hrs AVIATION 2015 Forum Organizing Committtee International South 1500-1600 hrs TPTC Awards Subcommittee Chicago A 1500-1600 hrs TPTC Best Paper Subcommittee Chicago B 1600-1700 hrs TPTC Publications Subcommittee Executive Conf Suite 222 1600-1700 hrs TPTC Conferences Subcommittee Executive Conf Suite 223 1700-1800 hrs TPTC Nominations Subcommittee Executive Conf Suite 219 1700-1800 hrs TPTC Education Subcommittee Chicago A 1800-1900 hrs FDTC Free Shear Layer Mixing Layer Control DG Chicago B 1800-1900 hrs TPTC Publicity Subcommittee Executive Conf Suite 223 1830-1930 hrs K-19: Environmental Heat Transfer Executive Conf Suite 222 1830-2230 hrs Multidisciplinary Design Optimization TC Chicago C/D 1900-2000 hrs APATC Low Reynolds Number Aerodynamics DG Chicago A 1900-2200 hrs Fluid Dynamics TC Hanover C/D 1900-2200 hrs Thermophysics TC Hanover F/G 1900-2200 hrs Plasmadynamics and Lasers TC Hanover E 2000-2200 hrs Aerodynamic Measurement Technology TC Hanover A

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Time Title Location Wednesday, 18 June 2014 0800-0900 hrs K-22: Visualization of Heat Transfer Chicago B 0800-1000 hrs K-21: Heat Transfer Education Chicago A 0900-1200 hrs GTTC Dual Flow Reference Nozzle WG - Day 2 Chicago D 1000-1100 hrs AVIATION 2015 Technical Program Committee Meeting International South 1600-1800 hrs GTTC DOE Focus Group Chicago A 1700-1800 hrs FDTC Student Outreach Subcommittee Chicago B 1730-1900 hrs FDTC LES WG Chicago C 1730-1900 hrs FDTC Nonequilibrium Flows DG Executive Conf Suite 219 1730-1900 hrs FDTC Solver Technology for Turbulent Flows Chicago D 1800-2100 hrs Flight Testing TC Executive Conf Suite 222 1800-2100 hrs Modeling and Simulation TC Embassy A/B 1800-2200 hrs Atmospheric and Space Environments TC Executive Conf Suite 226 1900-2200 hrs Aeroacoustics TC Hanover C/D 1900-2200 hrs Aircraft Design TC Hanover E 1930-2200 hrs V/STOL Aircraft Systems TC Chicago A Thursday, 19 June 2014 0900-1200 hrs GTTC Wind Tunnel Flow Quality WG Chicago B 0930-1230 hrs DETC Subcommittee Chicago A 1000-1200 hrs K-9: Nano Scale Heat Transfer Chicago C 1400-1600 hrs K-6: Heat Transfer in Energy Systems Chicago C 1800-2100 hrs Ground Testing TC International South 1900-2200 hrs Transformational Flight PC Embassy C/D 1900-2200 hrs Design Engineering TC Chicago A

www.aiaa-aviation.org 30 #aiaaAviation IntroSessions at a Glance

Abbreviation Title Date Start Time End Time Location Aeroacoustics 20-AA-1 Airframe Noise I 16-Jun 0930 hrs 1230 hrs Hanover F 89-AA-2 CAA Numerical Techniques I 17-Jun 0930 hrs 1230 hrs Hanover A 90-AA-3 Leading Edge Noise 17-Jun 0930 hrs 1230 hrs Hanover B 93-AA-4 Jet Noise Near Field I 17-Jun 0930 hrs 1230 hrs Hanover E 94-AA-5 Hybrid Wing Body Aeroacoustics Test I 17-Jun 0930 hrs 1230 hrs Hanover F 123-AA-6 CAA Sound Generation I 17-Jun 1400 hrs 1730 hrs Hanover A 124-AA-7 Fluid Acoustic Phenomena I 17-Jun 1400 hrs 1730 hrs Hanover B 127-AA-8 Jet Noise Reduction I 17-Jun 1400 hrs 1730 hrs Hanover E 128-AA-9 NASA Gulfstream Airframe Noise Reduction 17-Jun 1400 hrs 1730 hrs Hanover F 164-AA-10 Jet Noise Prediction I 18-Jun 0930 hrs 1230 hrs Hanover A 165-AA-11 Propeller Noise I 18-Jun 0930 hrs 1230 hrs Hanover B 168-AA-12 Jet Noise Reduction II 18-Jun 0930 hrs 1230 hrs Hanover E 169-AA-13 Hybrid Wing Body Aeroacoustics Test II 18-Jun 0930 hrs 1230 hrs Hanover F 202-AA-14 CAA Numerical Techniques II 18-Jun 1400 hrs 1730 hrs Hanover A 203-AA-15 Propeller Noise II 18-Jun 1400 hrs 1730 hrs Hanover B 206-AA-16 Jet Noise Prediction II 18-Jun 1400 hrs 1730 hrs Hanover E 207-AA-17 Airframe Noise II 18-Jun 1400 hrs 1730 hrs Hanover F 248-AA-18 Jet Noise Measurements I 19-Jun 0930 hrs 1230 hrs Hanover A 249-AA-19 CAA Sound Generation II 19-Jun 0930 hrs 1230 hrs Hanover B 252-AA-20 Jet Noise Prediction III 19-Jun 0930 hrs 1230 hrs Hanover E 253-AA-21 Boundary Layer Noise 19-Jun 0930 hrs 1230 hrs Hanover F 254-AA-22 Acoustic Beamforming I 19-Jun 0930 hrs 1230 hrs Hanover G 261-AA-23 Fan Noise I 19-Jun 0930 hrs 1230 hrs Piedmont 264-AA-24 Duct Liners I 19-Jun 0930 hrs 1230 hrs Spring 267-AA-25 Propeller Noise III 19-Jun 0930 hrs 1230 hrs Vinings 282-AA-26 Jet Noise Measurements II 19-Jun 1400 hrs 1730 hrs Hanover A 283-AA-27 Trailing Edge Noise I 19-Jun 1400 hrs 1730 hrs Hanover B 285-AA-28 CAA Sound Generation III 19-Jun 1400 hrs 1730 hrs Hanover D 286-AA-29 Jet Noise Prediction IV 19-Jun 1400 hrs 1730 hrs Hanover E 287-AA-30 Airframe Noise III 19-Jun 1400 hrs 1730 hrs Hanover F 288-AA-31 Acoustic Beamforming II 19-Jun 1400 hrs 1730 hrs Hanover G 295-AA-32 Fan Noise II 19-Jun 1400 hrs 1730 hrs Piedmont 298-AA-33 Duct Propagation I 19-Jun 1400 hrs 1730 hrs Spring 319-AA-34 Fluid Acoustic Phenomena II 20-Jun 0930 hrs 1230 hrs Hanover A 320-AA-35 General Acoustics II 20-Jun 0930 hrs 1230 hrs Hanover B 321-AA-36 Low Noise Systems Integration 20-Jun 0930 hrs 1230 hrs Hanover C 322-AA-37 CAA Propagation and Scattering I 20-Jun 0930 hrs 1230 hrs Hanover D 323-AA-38 Jet Noise Measurements III 20-Jun 0930 hrs 1230 hrs Hanover E 324-AA-39 Broadband Fan Noise Panel Discussion 20-Jun 0930 hrs 1230 hrs Hanover F 334-AA-40 General Acoustics I 20-Jun 0930 hrs 1230 hrs Spring 333-AA-41 Duct Propagation II 20-Jun 0930 hrs 1100 hrs Spring 349-AA-42 Acoustic Measurements 20-Jun 1400 hrs 1730 hrs Hanover A 350-AA-43 Fluid Acoustic Phenomena III 20-Jun 1400 hrs 1730 hrs Hanover B www.aiaa-aviation.org 31 #aiaaAviation IntroSessions at a Glance

Abbreviation Title Date Start Time End Time Location Aeroacoustics (continued) 351-AA-44 Trailing Edge Noise II 20-Jun 1400 hrs 1730 hrs Hanover C 352-AA-45 CAA Propagation and Scattering II 20-Jun 1400 hrs 1730 hrs Hanover D 353-AA-46 Jet Noise Near Field II 20-Jun 1400 hrs 1730 hrs Hanover E 354-AA-47 Turbomachinery and Propeller Noise 20-Jun 1400 hrs 1730 hrs Hanover F 360-AA-48 Fan Noise III 20-Jun 1400 hrs 1730 hrs Piedmont 361-AA-49 Duct Liners II 20-Jun 1400 hrs 1730 hrs Spring Aircraft Design 10-ACD-1 Aircraft Design Methods and Tools I 16-Jun 0930 hrs 1230 hrs Embassy F 43-ACD-2 Aircraft Design Methods and Tools II 16-Jun 1400 hrs 1600 hrs Embassy F 44-ACD-3 Methods for Analysis and Design Under Uncertainty 16-Jun 1400 hrs 1730 hrs Embassy F 84-ACD-4 Structural Analysis, Design, and Optimization of 17-Jun 0930 hrs 1230 hrs Embassy F Aircraft 117-ACD-5 Aircraft Performance and Design Studies 17-Jun 1400 hrs 1600 hrs Embassy F 118-ACD-6 Hybrid Wing Body Design Case Studies 17-Jun 1400 hrs 1730 hrs Embassy F 160-ACD-7 Stability and Control Considerations in Aircraft Design 18-Jun 0930 hrs 1230 hrs Embassy F 197-ACD-8 Unmanned Aircraft Design Studies and Methods 18-Jun 1400 hrs 1600 hrs Embassy F 198-ACD-9 Design of Morphing Wing Concepts 18-Jun 1400 hrs 1730 hrs Embassy F 243-ACD-10 Aerodynamic Aircraft Design 19-Jun 0930 hrs 1230 hrs Embassy F 276-ACD-11 Aircraft Integration of Innovative Propulsion Concepts 19-Jun 1400 hrs 1600 hrs Embassy F 277-ACD-12 Aircraft Subsystems Design and Integration 19-Jun 1400 hrs 1730 hrs Embassy F 343-ACD-13 VSTOL 20-Jun 1400 hrs 1600 hrs Embassy D Atmospheric Flight Mechanics 15-AFM-1 Aeroservoelastic (ASE) Control, Modeling, Simulation, 16-Jun 0930 hrs 1230 hrs Hanover A and Optimization I 16-AFM-2 Aircraft Flight Dynamics, Handling Qualities, and 16-Jun 0930 hrs 1230 hrs Hanover B Performance I 49-AFM-3 Aeroservoelastic (ASE) Control, Modeling, Simulation, 16-Jun 1400 hrs 1530 hrs Hanover A and Optimization II 50-AFM-4 Aerodynamic Prediction Methods 16-Jun 1400 hrs 1730 hrs Hanover A 51-AFM-5 Aircraft Flight Dynamics, Handling Qualities, and 16-Jun 1400 hrs 1730 hrs Hanover B Performance II 104-AFM-7 Planetary Entry and Aeroassist Technology 17-Jun 0930 hrs 1230 hrs Spring 107-AFM-8 Best Atmospheric Flight Mechanics Student Paper 17-Jun 0930 hrs 1230 hrs Vinings Competition 141-AFM-11 Launch Vehicle, Missile, and Projectile Flight Dynamics 17-Jun 1400 hrs 1730 hrs Spring 144-AFM-12 Flight Test and System Identification 17-Jun 1400 hrs 1730 hrs Vinings 182-AFM-13 Small/Mini/Micro Aerial Vehicles I 18-Jun 0930 hrs 1230 hrs Spring 220-AFM-14 Small/Mini/Micro Aerial Vehicles II 18-Jun 1400 hrs 1730 hrs Spring Aerodynamic Measurement Technology and Ground Testing 27-AMT-1/GT-1 Ground Test Facility Operation and Improvement 16-Jun 0930 hrs 1230 hrs Piedmont 30-AMT-2/PDL-2 Diagnostics I 16-Jun 0930 hrs 1230 hrs Roswell 61-AMT-3/GT-2 Spectroscopic Velocimetry 16-Jun 1400 hrs 1730 hrs Piedmont 100-AMT-4/GT-3 In Honor of Dick Miles's (semi-) Retirement (Invited) 17-Jun 0930 hrs 1230 hrs Piedmont www.aiaa-aviation.org 32 #aiaaAviation IntroSessions at a Glance

Abbreviation Title Date Start Time End Time Location Aerodynamic Measurement Technology and Ground Testing (continued) 136-AMT-5/GT-4 Imaging Methods 17-Jun 1400 hrs 1730 hrs Marietta 137-AMT-6/GT-5 Spectroscopic Temperature Measurement 17-Jun 1400 hrs 1730 hrs Piedmont 140-AMT-7/PDL-10 Diagnostics II 17-Jun 1400 hrs 1730 hrs Roswell 176-AMT-8/GT-6 Ground Test Facility Characterization 18-Jun 0930 hrs 1230 hrs Marietta 177-AMT-9/GT-7 Developments in Particle Image Velocimetry 18-Jun 0930 hrs 1230 hrs Piedmont 215-AMT-10/GT-8 Aerodynamic Force and Power Measurement 18-Jun 1400 hrs 1730 hrs Marietta 216-AMT-11/GT-9 Surface Sensors and Probes 18-Jun 1400 hrs 1730 hrs Piedmont 260-AMT-12/GT-11 Surface Field Measurements 19-Jun 0930 hrs 1230 hrs Marietta Aircraft Noise and Emissions Reduction Symposium 200-ANERS-1 ANERS-Design and Operations 18-Jun 1400 hrs 1630 hrs Embassy H 228-ANERS-2 What is the Right Balance Between Design and 18-Jun 1630 hrs 1730 hrs Embassy H Operations? 245-ANERS-3 ANERS-Technology 19-Jun 0930 hrs 1230 hrs Embassy H 279-ANERS-4 ANERS-ATM Operations 19-Jun 1400 hrs 1630 hrs Embassy H 302-ANERS-5 How Far Can We Get With Technology and Operations? 19-Jun 1630 hrs 1730 hrs Embassy H 316-ANERS-6 ANERS-Modeling 20-Jun 930 hrs 1230 hrs Embassy H 347-ANERS-7 ANERS-Policy and Economics 20-Jun 1400 hrs 1630 hrs Embassy H 366-ANERS-8 Can We Resolve the Most Pressing Modeling, Policy, 20-Jun 1630 hrs 1730 hrs Embassy H and Economic Challenges? Applied Aerodynamics 4-APA-1 Special Session: NATO Task Group AVT-201 I - 16-Jun 0930 hrs 1230 hrs Baker Experimental Investigations 5-APA-2 Special Session: Sonic Boom Activities I - 1st Sonic 16-Jun 0930 hrs 1230 hrs Courtland Boom Prediction Workshop Results 6-APA-3 Aerodynamic Analysis and Design: Design 16-Jun 0930 hrs 1230 hrs Dunwoody Methodologies 7-APA-4 Low Speed, Low Reynolds Number, Transonic, 16-Jun 0930 hrs 1230 hrs Edgewood Supersonic and Hypersonic Aerodynamics I 13-APA-5/FC-1 Flow Control (Active and Passive): Computational and 16-Jun 0930 hrs 1230 hrs Fairlie Experimental Results I 26-APA-6 Airfoil/Wing/Configuration Aerodynamics I 16-Jun 0930 hrs 1230 hrs Marietta 37-APA-7 Special Session: NATO Task Group AVT-201 II - CFD 16-Jun 1400 hrs 1730 hrs Baker Prediction and Flow Analyses 38-APA-8 Special Session: Sonic Boom Activities II 16-Jun 1400 hrs 1730 hrs Courtland 39-APA-9/FC-4 Flow Control (Active and Passive): Computational and 16-Jun 1400 hrs 1730 hrs Dunwoody Experimental Results II 40-APA-10 Low Speed, Low Reynolds Number, Transonic, 16-Jun 1400 hrs 1630 hrs Edgewood Supersonic and Hypersonic Aerodynamics II 47-APA-11 Aerodynamic Testing: Flight, Wind Tunnel and 16-Jun 1400 hrs 1730 hrs Fairlie Numerical Correlations I 71-APA-13 Low Reynolds Number Aerodynamics Discussion Panel 16-Jun 1630 hrs 1730 hrs Edgewood 77-APA-14 Special Session: NATO Task Group AVT-201 III - CFD 17-Jun 0930 hrs 1230 hrs Baker Prediction and Real Scale Analyses 78-APA-15 Special Session: Sonic Boom Activities III 17-Jun 0930 hrs 1230 hrs Courtland

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Abbreviation Title Date Start Time End Time Location Applied Aerodynamics (continued) 79-APA-16 Aerodynamics of Unmanned Aerial Vehicles I 17-Jun 0930 hrs 1230 hrs Dunwoody 80-APA-17 Wind Turbine Aerodynamics I 17-Jun 0930 hrs 1230 hrs Edgewood 87-APA-18 Aerodynamic Testing: Flight, Wind Tunnel and 17-Jun 0930 hrs 1230 hrs Fairlie Numerical Correlations II 109-APA-19 Special Session: NATO Task Group AVT-201 IV - 17-Jun 1400 hrs 1730 hrs Baker Stability and Control Analyses 110-APA-20 Special Session: Sonic Boom Activities IV - Low Sonic 17-Jun 1400 hrs 1730 hrs Courtland Boom Flight Demonstration 111-APA-21 Special Session: 2nd High-Lift Prediction Workshop I 17-Jun 1400 hrs 1730 hrs Dunwoody 112-APA-22 Flow Control (Active and Passive): Computational and 17-Jun 1400 hrs 1730 hrs Edgewood Experimental Results III 121-APA-23 Special Session: Aerodynamic-Structural Modeling, 17-Jun 1400 hrs 1730 hrs Fairlie Optimization, and Test Techniques for Flexible Wing Technology I 153-APA-25 Flow Control (Active and Passive): Computational and 18-Jun 0930 hrs 1230 hrs Baker Experimental Results IV 154-APA-26 Aerodynamic Testing: Flight, Wind Tunnel and 18-Jun 0930 hrs 1230 hrs Courtland Numerical Correlations III 155-APA-27 Special Session: 2nd High-Lift Prediction Workshop II 18-Jun 0930 hrs 1230 hrs Dunwoody 156-APA-28 Aerodynamic Analysis and Design: CFD Methods I 18-Jun 0930 hrs 1230 hrs Edgewood 162-APA-29 Special Session: Aerodynamic-Structural Modeling, 18-Jun 0930 hrs 1230 hrs Fairlie Optimization, and Test Techniques for Flexible Wing Technology II 189-APA-30 Flow Control (Active and Passive): Computational and 18-Jun 1400 hrs 1730 hrs Baker Experimental Results V 190-APA-31 Aerodynamic Analysis and Design: CFD Methods II 18-Jun 1400 hrs 1730 hrs Courtland 191-APA-32 Special Session: 2nd High-Lift Prediction Workshop III 18-Jun 1400 hrs 1730 hrs Dunwoody 192-APA-33 Vortical/Vortex Flow I 18-Jun 1400 hrs 1730 hrs Edgewood 201-APA-34 Low Speed, Low Reynolds Number, Transonic, 18-Jun 1400 hrs 1730 hrs Fairlie Supersonic and Hypersonic Aerodynamics III 236-APA-35 Aerodynamics of Unmanned Aerial Vehicles II 19-Jun 0930 hrs 1230 hrs Baker 237-APA-36 Other Topics in Applied Aerodynamics - Inlet, 19-Jun 0930 hrs 1230 hrs Courtland Compressor, Diffuser and Nozzle Aerodynamics 238-APA-37 Aerodynamic Testing: Flight, Wind Tunnel and 19-Jun 0930 hrs 1230 hrs Dunwoody Numerical Correlations IV 239-APA-38 Wind Turbine Aerodynamics II 19-Jun 0930 hrs 1230 hrs Edgewood 246-APA-39 Vortical/Vortex Flow II 19-Jun 0930 hrs 1230 hrs Fairlie 269-APA-40 Flow Control (Active and Passive): Computational and 19-Jun 1400 hrs 1730 hrs Baker Experimental Results VI 270-APA-41 Aerodynamic Analysis and Design: Higher Order 19-Jun 1400 hrs 1730 hrs Courtland Methods in CFD 271-APA-42 Aerodynamic Analysis and Design: Analysis Methods I 19-Jun 1400 hrs 1730 hrs Dunwoody 272-APA-43 Airfoil/Wing/Configuration Aerodynamics II 19-Jun 1400 hrs 1730 hrs Edgewood 280-APA-44 Missile, Projectile, Guided-Munitions, Carriage and 19-Jun 1400 hrs 1730 hrs Fairlie Store Separation Aerodynamics 294-APA-45 High Angle of Attack, High Lift and VSTOL/STOL 19-Jun 1400 hrs 1730 hrs Marietta Aerodynamics www.aiaa-aviation.org 34 #aiaaAviation IntroSessions at a Glance

Abbreviation Title Date Start Time End Time Location Applied Aerodynamics (continued) 308-APA-46 Other Topic in Applied Aerodynamics - UAVs and 20-Jun 0930 hrs 1230 hrs Baker Other Similar Vehicles 309-APA-47 Propeller Aerodynamics 20-Jun 0930 hrs 1230 hrs Courtland 310-APA-48 Aerodynamic Testing: Flight, Wind Tunnel and 20-Jun 0930 hrs 1230 hrs Dunwoody Numerical Correlations V 311-APA-49 Wind Turbine Aerodynamics III 20-Jun 0930 hrs 1230 hrs Edgewood 317-APA-50 Aerodynamic Analysis and Design: Analysis Methods II 20-Jun 0930 hrs 1230 hrs Fairlie 318-APA-51 Aerodynamic Analysis and Design: Optimization 20-Jun 0930 hrs 1230 hrs Greenbriar Methods I 330-APA-52 Aerodynamic Analysis and Design: Optimization 20-Jun 0930 hrs 1230 hrs Marietta Methods II 339-APA-53 Airfoil/Wing/Configuration Aerodynamics III 20-Jun 1400 hrs 1730 hrs Baker 340-APA-54 Vortical/Vortex Flow III 20-Jun 1400 hrs 1730 hrs Courtland 342-APA-56 Rotorcraft Aerodynamics 20-Jun 1400 hrs 1730 hrs Edgewood 348-APA-57 Low Speed, Low Reynolds Number, Transonic, 20-Jun 1400 hrs 1730 hrs Greenbriar Supersonic and Hypersonic Aerodynamics IV Atmospheric and Space Environments 17-ASE-1 Ice Protection Systems and Hydrophobic Coating 16-Jun 0930 hrs 1230 hrs Hanover C Application 18-ASE-2 Icing Weather and Forecasting 16-Jun 0930 hrs 1230 hrs Hanover D 52-ASE-3 Icing CFD 16-Jun 1400 hrs 1730 hrs Hanover C 53-ASE-4/FT-1 NASA Aviation Safety Technologies 16-Jun 1400 hrs 1730 hrs Hanover D 91-ASE-5 Icing Physics 17-Jun 0930 hrs 1230 hrs Hanover C 92-ASE-6/AFM-6/ Managing Wake Vortex Encounter I 17-Jun 0930 hrs 1230 hrs Hanover D FT-2 125-ASE-7 Ice Roughness Effects on Heat Transfer and Transition 17-Jun 1400 hrs 1730 hrs Hanover C 126-ASE-8/AFM-9/ Managing Wake Vortex Encounter II: Including Wake 17-Jun 1400 hrs 1730 hrs Hanover D FT-3 Vortex Modelling 166-ASE-9 3-D Model Design and Ice Measurement Methods for 18-Jun 0930 hrs 1230 hrs Hanover C Experimental Icing Simulation 167-ASE-10/FT-5 Volcanic Ash and Aviation 18-Jun 0930 hrs 1230 hrs Hanover D 204-ASE-11 Engine Icing I - Cloud Measurement and 18-Jun 1400 hrs 1530 hrs Hanover C Characterization 205-ASE-12 Numerical Weather Modeling 18-Jun 1400 hrs 1730 hrs Hanover D 225-ASE-13 AIRA - Aircraft Icing Research Alliance Panel 18-Jun 1530 hrs 1730 hrs Hanover C 250-ASE-14/GT-10 NASA Propulsion Systems Laboratory Ice Crystal 19-Jun 0930 hrs 1230 hrs Hanover C Engine Icing Test 251-ASE-15 Airspace Systems Hazards and Constraints 19-Jun 0930 hrs 1230 hrs Hanover D 284-ASE-16 Engine Icing II - Ice Crystal Accretion and Particle 19-Jun 1400 hrs 1730 hrs Hanover C Impact Dynamics

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Abbreviation Title Date Start Time End Time Location Aviation Technology, Integration, and Operations 8-ATIO-1 Terminal & Surface Operations I - Terminal Airspace 16-Jun 0930 hrs 1230 hrs Embassy D 9-ATIO-2 ATM-I Analysis Techniques in ATM 16-Jun 0930 hrs 1230 hrs Embassy E 41-ATIO-3 Terminal & Surface Operations II - Surface/Airport 16-Jun 1400 hrs 1730 hrs Embassy D Operations 42-ATIO-4 ATM-II Modeling & Simulation for ATM 16-Jun 1400 hrs 1730 hrs Embassy E 81-ATIO-5 Transformational Flight: Technical Gaps, Prizes, and 17-Jun 0930 hrs 1130 hrs Embassy C Private-Public Partnerships 82-ATIO-6 UAS Integration & Operations I 17-Jun 0930 hrs 1230 hrs Embassy D 83-ATIO-7 ATM-III Air/Ground Trajectory Enhancements 17-Jun 0930 hrs 1230 hrs Embassy E 60-ATIO-8 Special Session: Chinese Digital Avionics 16-Jun 1400 hrs 1730 hrs Marietta 113-ATIO-9 Transformational Flight - Advanced Concepts 17-Jun 1400 hrs 1600 hrs Embassy C 114-ATIO-10 Transformational Flight - Demand Modeling 17-Jun 1400 hrs 1730 hrs Embassy C 115-ATIO-11 UAS Integration & Operations II 17-Jun 1400 hrs 1730 hrs Embassy D 116-ATIO-12 ATM-IV Systems Evaluations in ATM 17-Jun 1400 hrs 1730 hrs Embassy E 157-ATIO-13 Transformational Flight - Electric Propulsion 18-Jun 0930 hrs 1230 hrs Embassy C Development and Testing 159-ATIO-14 ATM-V Benefit Analysis of ATM 18-Jun 0930 hrs 1230 hrs Embassy E 193-ATIO-15 Transformational Flight - Autonomy 18-Jun 1400 hrs 1730 hrs Embassy C 196-ATIO-16 ATM-VI Weather's Role in ATM 18-Jun 1400 hrs 1730 hrs Embassy E 240-ATIO-17 Transformational Flight - Distributed Electric 19-Jun 0930 hrs 1230 hrs Embassy C Propulsion 241-ATIO-18 General Aviation 19-Jun 0930 hrs 1230 hrs Embassy D 242-ATIO-19 ATM-VII Research Analysis in ATM 19-Jun 0930 hrs 1230 hrs Embassy E 273-ATIO-20 Transformational Flight - Distributed Electric 19-Jun 1400 hrs 1600 hrs Embassy C Propulsion Control 275-ATIO-22 Enroute Operations 19-Jun 1400 hrs 1730 hrs Embassy E 313-ATIO-23 Airline Operations I 20-Jun 0930 hrs 1230 hrs Embassy E 314-ATIO-24 Terminal & Surface Operations III - Approach 20-Jun 0930 hrs 1230 hrs Embassy F Operations 344-ATIO-25 Airline Operations II 20-Jun 1400 hrs 1730 hrs Embassy E 345-ATIO-26 Aircraft Economics 20-Jun 1400 hrs 1730 hrs Embassy F 367-ATIO-27 New Directions for NASA's Airspace R&D 19-Jun 1600 hrs 1730 hrs Embassy C Balloon Systems 194-BA-1 Balloon Systems 18-Jun 1400 hrs 1600 hrs Embassy D Design Engineering 274-DE-1 Design Engineering and Education 19-Jun 1400 hrs 1730 hrs Embassy D Flow Control 25-FC-2 Flow Control: Actuation and Sensing 16-Jun 0930 hrs 1230 hrs Lenox 31-FC-3/PDL-3 Plasma-Based Flow Control I 16-Jun 0930 hrs 1230 hrs Spring 59-FC-5 Special Session: Mixing Layer Flow Control 16-Jun 1400 hrs 1730 hrs Lenox 99-FC-7 Flow Control: Separated Flows 17-Jun 0930 hrs 1230 hrs Lenox 135-FC-8/APA-24 Aerodynamic Flow Control 17-Jun 1400 hrs 1730 hrs Lenox 175-FC-9 Flow Control: Boundary Layers 18-Jun 0930 hrs 1230 hrs Lenox

www.aiaa-aviation.org 36 #aiaaAviation IntroSessions at a Glance

Abbreviation Title Date Start Time End Time Location Flow Control (continued) 180-FC-10/PDL-11 Plasma-Based Flow Control II 18-Jun 0930 hrs 1130 hrs Roswell 214-FC-11 Flow Control: Active and Passive 18-Jun 1400 hrs 1730 hrs Lenox 259-FC-12 Closed-Loop Flow Control 19-Jun 0930 hrs 1230 hrs Lenox Fluid Dynamics 14-FD-1 High-Reynolds-Number Fluid Structure Interaction I 16-Jun 0930 hrs 1230 hrs Greenbriar (Invited) 22-FD-2 Turbulence Modeling I 16-Jun 0930 hrs 1230 hrs Harris 23-FD-3 Simulation Algorithms I 16-Jun 0930 hrs 1230 hrs Inman 24-FD-4 Ramjet and Scramjet Propulsion Systems I 16-Jun 0930 hrs 1230 hrs Kenneshaw 48-FD-5 High-Reynolds-Number Fluid Structure Interaction II 16-Jun 1400 hrs 1730 hrs Greenbriar (Invited) 55-FD-6 Turbulence Modeling II 16-Jun 1400 hrs 1730 hrs Harris 56-FD-7 Stability and Transition I 16-Jun 1400 hrs 1730 hrs Inman 57-FD-8 Ramjet and Scramjet Propulsion Systems II 16-Jun 1400 hrs 1730 hrs Kenneshaw 88-FD-9 Fluid Structure Interaction I 17-Jun 0930 hrs 1230 hrs Greenbriar 96-FD-10 Hypersonic Boundary Layer Transition I 17-Jun 0930 hrs 1230 hrs Inman 122-FD-11 Fluid Structure Interaction II 17-Jun 1400 hrs 1730 hrs Greenbriar 132-FD-12 Stability and Transition II 17-Jun 1400 hrs 1730 hrs Inman 133-FD-13 Vortex and Wake Dominated Flows 17-Jun 1400 hrs 1730 hrs Kenneshaw 163-FD-14 New Frontiers of Fluid Dynamics: Multiphase Flows 18-Jun 0930 hrs 1230 hrs Greenbriar (Invited) 171-FD-15 Other Topics in Fluid Dynamics 18-Jun 0930 hrs 1230 hrs Harris 172-FD-16 Supersonic Boundary Layers: Transition 18-Jun 0930 hrs 1230 hrs Inman 173-FD-17 Hypersonic Boundary Layer Transition II 18-Jun 0930 hrs 1230 hrs Kenneshaw 231-FD-18 Transition Open Forum 18-Jun 1800 hrs 2030 hrs Greenbriar 210-FD-19 Fluid Structure Interaction III 18-Jun 1400 hrs 1730 hrs Harris 211-FD-20 Stability and Transition III 18-Jun 1400 hrs 1730 hrs Inman 212-FD-21 CFD Methods 18-Jun 1400 hrs 1730 hrs Kenneshaw 247-FD-22 Low-Speed Boundary Layers: Stability, Transition, and 19-Jun 0930 hrs 1230 hrs Greenbriar Turbulent Structure 255-FD-23 Multiphase Flows I: Non-Newtonian Liquids, 19-Jun 0930 hrs 1230 hrs Harris Atomization, and Surface Tension Effects 256-FD-24 Simulation Algorithms II 19-Jun 0930 hrs 1230 hrs Inman 257-FD-25 Airfoils and Wings 19-Jun 0930 hrs 1230 hrs Kenneshaw 281-FD-26 Detonation and Supersonic Combustion 19-Jun 1400 hrs 1730 hrs Greenbriar 289-FD-27 Multiphase Flows II: Air/Water Systems and Icing 19-Jun 1400 hrs 1730 hrs Harris 290-FD-28 Supersonic Boundary Layers: Fundamental Studies 19-Jun 1400 hrs 1730 hrs Inman 291-FD-29 Simulation Algorithms III 19-Jun 1400 hrs 1730 hrs Kenneshaw 293-FD-30 Cavity and Shear Flows 19-Jun 1400 hrs 1730 hrs Lenox 325-FD-31 Aerothermodynamics and Reacting Flows 20-Jun 0930 hrs 1230 hrs Harris 326-FD-32 Large Eddy Simulations 20-Jun 0930 hrs 1230 hrs Inman 327-FD-33 Comparison between CFD and Measurements in 20-Jun 0930 hrs 1230 hrs Kenneshaw Hypervelocity Airflows Part I: Real-gas Effects on Laminar Shockwave Boundary Layer Interaction www.aiaa-aviation.org 37 #aiaaAviation IntroSessions at a Glance

Abbreviation Title Date Start Time End Time Location Fluid Dynamics 329-FD-34 Galerkin Methods 20-Jun 0930 hrs 1230 hrs Lenox 355-FD-35 Low-Speed Separated Flows 20-Jun 1400 hrs 1730 hrs Harris 356-FD-36 Turbulence Simulations 20-Jun 1400 hrs 1730 hrs Inman 357-FD-37 Shock-Boundary Layer Interactions 20-Jun 1400 hrs 1730 hrs Kenneshaw 358-FD-38 Acoustic and Unsteady Flows 20-Jun 1400 hrs 1730 hrs Lenox 359-FD-39 Comparison between CFD and Measurements in 20-Jun 1400 hrs 1730 hrs Marietta Hypervelocity Flows Part II: Shockwave Turbulent Boundary Layer Interaction in High Reynolds Number Duplicating Mach 5 – 8 Flows Flight Testing 158-FT-4 Flight Test Operations 18-Jun 0930 hrs 1230 hrs Embassy D International Space Planes and Hypersonic Systems and Technologies 58-HYTASP-1 Propulsion Cycle Performance-Scramjet Tests I 16-Jun 1400 hrs 1730 hrs Learning Center 98-HYTASP-2 Vehicle, Mission, and Trajectory Optimization 17-Jun 0930 hrs 1230 hrs Learning Center 101-HYTASP-3 Vehicle Systems 17-Jun 0930 hrs 1230 hrs Regency Ballroom V 134-HYTASP-4 Integration and Evaluation 17-Jun 1400 hrs 1730 hrs Learning Center 138-HYTASP-5 Vehicle, Mission, and Trajectory 17-Jun 1400 hrs 1730 hrs Regency Ballroom V 213-HYTASP-6 Propulsion Cycle Performance 18-Jun 1400 hrs 1730 hrs Learning Center 217-HYTASP-7 Review of Fundamental Research I (Invited) 18-Jun 1400 hrs 1600 hrs Regency Ballroom V 258-HYTASP-8 Propulsion Cycle Performance-Scramjet Tests II 19-Jun 0930 hrs 1230 hrs Learning Center 262-HYTASP-9 Propulsion Component Performance-Combustor 19-Jun 0930 hrs 1230 hrs Regency Ballroom V 292-HYTASP-10 Propulsion Component Performance 19-Jun 1400 hrs 1730 hrs Learning Center 296-HYTASP-11 Review of Fundamental Research II (Invited) 19-Jun 1400 hrs 1630 hrs Regency Ballroom V 328-HYTASP-12 Propulsion Component Performance-Injector 20-Jun 0930 hrs 1230 hrs Learning Center 331-HYTASP-13 Propulsion Component Performance-Inlets 20-Jun 0930 hrs 1230 hrs Regency Ballroom V 28-HYTASP-15 SPHS Introduction 16-Jun 0930 hrs 1000 hrs Regency Ballroom V 35-HYTASP-16 Global Reports I 16-Jun 1000 hrs 1230 hrs Regency Ballroom V 62-HYTASP-17 Global Reports II 16-Jun 1400 hrs 1600 hrs Regency Ballroom V 70-HYTASP-18 Fluid Analysis Panel 16-Jun 1600 hrs 1700 hrs Regency Ballroom V 178-HYTASP-19 Culpepper Lecture 18-Jun 0930 hrs 1030 hrs Regency Ballroom V 186-HYTASP-20 HYTASP Programs 18-Jun 1030 hrs 1230 hrs Regency Ballroom V 226-HYTASP-21 Hypersonic Aircraft Technology Advances and 18-Jun 1600 hrs 1730 hrs Regency Ballroom V Challenges Panel 303-HYTASP-22 Future of Hypersonics Panel 19-Jun 1630 hrs 1730 hrs Regency Ballroom V 129-HYTASP-23 Aerodynamic and Propulsion Test Unit (APTU) I 17-Jun 1400 hrs 1600 hrs Hanover G 208-HYTASP-24 Aerodynamic and Propulsion Test Unit (APTU) II 18-Jun 1400 hrs 1600 hrs Hanover G ITAR Sessions 130-ITAR-2 ITAR-Noise Modeling and Technologies for Quiet UAS 17-Jun 1400 hrs 1730 hrs Hanover G 170-ITAR-3 ITAR-Experimental Aero, Fluid and Thermal Sciences 18-Jun 0930 hrs 1200 hrs Hanover G 209-ITAR-5 ITAR-Hypersonic Vehicle Design 18-Jun 1400 hrs 1730 hrs Hanover G Lighter-than-Air Systems 195-LTA-1 Lighter-than-Air Systems 18-Jun 1400 hrs 1730 hrs Embassy D

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Abbreviation Title Date Start Time End Time Location Multidisciplinary Analysis and Optimization 11-MAO-1 Multidisciplinary Analysis and Optimization: Shape 16-Jun 0930 hrs 1230 hrs Embassy G and Topology I 12-MAO-2 Multidisciplinary Analysis and Optimization: MDO 16-Jun 0930 hrs 1230 hrs Embassy H Frameworks 45-MAO-3 Multidisciplinary Analysis and Optimization: Shape 16-Jun 1400 hrs 1730 hrs Embassy G and Topology II 46-MAO-4 Multidisciplinary Analysis and Optimization: 16-Jun 1400 hrs 1730 hrs Embassy H Applications I 85-MAO-5 Multidisciplinary Analysis and Optimization: Shape 17-Jun 0930 hrs 1230 hrs Embassy G and Topology III 86-MAO-6 Multidisciplinary Analysis and Optimization: 17-Jun 0930 hrs 1230 hrs Embassy H Metamodeling I 119-MAO-7 Multidisciplinary Analysis and Optimization: Emerging 17-Jun 1400 hrs 1730 hrs Embassy G Methods I 120-MAO-8 Multidisciplinary Analysis and Optimization: 17-Jun 1400 hrs 1730 hrs Embassy H Metamodeling II 161-MAO-9 Multidisciplinary Analysis and Optimization: Shape 18-Jun 0930 hrs 1230 hrs Embassy G and Topology Method Development 199-MAO-10 Multidisciplinary Analysis and Optimization: Emerging 18-Jun 1400 hrs 1730 hrs Embassy G Methods II 244-MAO-11 Multidisciplinary Analysis and Optimization: 19-Jun 0930 hrs 1230 hrs Embassy G Uncertainty I 278-MAO-12 Multidisciplinary Analysis and Optimization: 19-Jun 1400 hrs 1730 hrs Embassy G Uncertainty II 312-MAO-13 Multidisciplinary Analysis and Optimization: Emerging 20-Jun 0930 hrs 1230 hrs Embassy D Methods III 315-MAO-14 Multidisciplinary Analysis and Optimization: Vehicle 20-Jun 0930 hrs 1230 hrs Embassy G Design 346-MAO-15 Multidisciplinary Analysis and Optimization: 20-Jun 1400 hrs 1730 hrs Embassy G Applications II Modeling and Simulation Technologies 21-MST-1 M&S: Applications 16-Jun 0930 hrs 1230 hrs Hanover G 54-MST-2 M&S: Flight Simulator Technologies 16-Jun 1400 hrs 1730 hrs Hanover G 95-MST-3 M&S: Tools and Technologies 17-Jun 0930 hrs 1230 hrs Hanover G 174-MST-4 M&S: Vehicle Dynamics, Systems, and Environments 18-Jun 0930 hrs 1230 hrs Learning Center AND Uninhabited Aircraft Systems Plasmadynamics and Lasers 19-PDL-1 Laser Physics 16-Jun 0930 hrs 1230 hrs Hanover E 65-PDL-4 Plasma and Laser Enhanced Combustion/Propulsion 16-Jun 1400 hrs 1730 hrs Spring 64-PDL-5 Advanced Concepts and Advanced Computational 16-Jun 1400 hrs 1730 hrs Roswell Modeling of Plasmas and Lasers 181-PDL-6/FC-6 DBD Actuators 18-Jun 0930 hrs 1230 hrs Roswell 97-PDL-7 Aero-Optics I 17-Jun 0930 hrs 1230 hrs Kenneshaw 103-PDL-8 Re-Entry and Spacecraft Concepts 17-Jun 0930 hrs 1230 hrs Roswell 131-PDL-9 Radiation/Aero-Optics II 17-Jun 1400 hrs 1730 hrs Harris

www.aiaa-aviation.org 39 #aiaaAviation Intro

Abbreviation Title Date Start Time End Time Location Plasmadynamics and Lasers 219-PDL-12 Special Session: NATO-RTO-AVT-190, Standardization 18-Jun 1400 hrs 1730 hrs Roswell of DBD Actuators 147-PDL-13 Special Panel Session on Future Directions in Plasma 17-Jun 1730 hrs 1830 hrs Embassy A Aerodynamics Thermophysics and Heat Transfer 32-TP-1 Ablation I 16-Jun 0930 hrs 1230 hrs Techwood 33-TP-2 Heat Transfer Enhancement and Energy Harvesting I 16-Jun 0930 hrs 1230 hrs University 34-TP-3 Multi-Scale Heat Transfer I 16-Jun 0930 hrs 1230 hrs Vinings 66-TP-4 Ablation II 16-Jun 1400 hrs 1730 hrs Techwood 67-TP-5 Combustion, Fire and Propulsion Heat Transfer 16-Jun 1400 hrs 1730 hrs University 68-TP-6 Theoretical, Analytical and Computational Heat 16-Jun 1400 hrs 1730 hrs Vinings Transfer I 105-TP-7 Theoretical, Analytical and Computational Heat 17-Jun 0930 hrs 1230 hrs Techwood Transfer II 106-TP-8 Heat Transfer in Cooling, Heating and Power 17-Jun 0930 hrs 1230 hrs University Generation I 142-TP-9 Nonequilibrium Flows I 17-Jun 1400 hrs 1730 hrs Techwood 143-TP-10 Heat Transfer Enhancement and Energy Harvesting II 17-Jun 1400 hrs 1730 hrs University 183-TP-11 Aerothermodynamics I 18-Jun 0930 hrs 1230 hrs Techwood 184-TP-12 Theoretical, Analytical and Computational Heat 18-Jun 0930 hrs 1230 hrs University Transfer III 185-TP-13 Multi-Scale Heat Transfer II 18-Jun 0930 hrs 1230 hrs Vinings 221-TP-14 Aerothermodynamics II 18-Jun 1400 hrs 1730 hrs Techwood 222-TP-15 Multiphase, Jets and Thermosyphons I 18-Jun 1400 hrs 1730 hrs University 223-TP-16 Theoretical, Analytical and Computational Heat 18-Jun 1400 hrs 1730 hrs Vinings Transfer IV 265-TP-17 Nonequilibrium Flows II 19-Jun 0930 hrs 1230 hrs Techwood 266-TP-18 Heat Transfer in Cooling, Heating and Power 19-Jun 0930 hrs 1230 hrs University Generation II 299-TP-19 Thermal Management and Heat Pipes 19-Jun 1400 hrs 1730 hrs Techwood 300-TP-20 Multi-Scale Heat Transfer III 19-Jun 1400 hrs 1730 hrs University 335-TP-21 Other Heat Transfer Topics 20-Jun 0930 hrs 1230 hrs Techwood 336-TP-22 Other Topics in Thermophysics 20-Jun 0930 hrs 1230 hrs University 337-TP-23 Multi-Scale Heat Transfer IV 20-Jun 0930 hrs 1230 hrs Vinings 362-TP-24 Heat Transfer in Cooling, Heating and Power 20-Jun 1400 hrs 1730 hrs Techwood Generation III 363-TP-25 Multiphase, Jets and Thermosyphons II 20-Jun 1400 hrs 1730 hrs University 364-TP-26 Multi-Scale Heat Transfer V 20-Jun 1400 hrs 1730 hrs Vinings

www.aiaa-aviation.org 40 #aiaaAviation Monday Monday, 16 June 2014 1-SB-1 Monday Morning Speakers’ Briefing Session Rooms 0730 - 0800 hrs Monday, 16 June 2014 2-PLNRY-1 Monday Morning Opening Plenary Centennial I/II 0800 - 0900 hrs

The Global Economic Impact of the F-35 Lightning II Program Orlando Carvalho Executive Vice President, Lockheed Martin Aeronautics Monday, 16 June 2014 3-NW-1 Monday Morning Networking Coffee Break Meeting Room Foyers 0900 - 0930 hrs Monday, 16 June 2014 4-APA-1 Special Session: NATO Task Group AVT-201 I - Experimental Investigations Baker Chaired by: N. FRINK, NASA-Langley Research Center 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2014-2000 AIAA-2014-2001 AIAA-2014-2002 AIAA-2014-2003 AIAA-2014-2004 AIAA-2014-2005 The NATO STO Task Group AVT- Conceptual Design and UCAV model design and static Low-speed Dynamic Wind Tunnel High speed static experimental Experimental and numerical 201 on ‘Extended Assessment of Aerodynamic Analyses of a Generic experimental investigations Test Analysis of a Generic 53° investigations to estimate control analysis of the transonic vortical 41 Stability and Control Prediction UCAV Configuration to estimate control device Swept UCAV Configuration device effectiveness and S&C flow over a generic lambda wing Methods for NATO Air Vehicles’ C. Liersch, K. Huber, German Aerospace effectiveness and S&C capabilities D. Vicroy, NASA Langley Research capabilities configuration R. Cummings, U.S. Air Force Academy, Center (DLR), Braunschweig, Germany K. Huber, German Aerospace Center (DLR), Center, Hampton, VA; K. Huber, German M. Rein, German Aerospace Center (DLR), D. Zimper, German Aerospace Center Colorado Springs, CO; A. Schuette, Braunschweig, Germany; D. Vicroy, NASA Aerospace Center (DLR), Braunschweig, Göttingen, Germany; J. Irving, G. Rigby, (DLR), Cologne, Germany; M. Rein, German Aerospace Center (DLR), Langley Research Center, Hampton, VA; A. Germany; T. Loeser, German-Dutch Wind BAE Systems, Warton, United Kingdom; German Aerospace Center (DLR), Braunschweig, Germany Schuette, A. Huebner, German Aerospace Tunnels, Braunschweig, Germany; D. T. Birch, Defence Science and Technology Göttingen, Germany Center (DLR), Braunschweig, Germany Rohlf, German Aerospace Center (DLR), Laboratory, Portsmouth, United Kingdom Braunschweig, Germany Monday, 16 June 2014 5-APA-2 Special Session: Sonic Boom Activities I - 1st Sonic Boom Prediction Workshop Results Courtland Chaired by: K. WAITHE, Gulfstream Aerospace Corporation and M. PARK, NASA-Langley Research Center 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2014-2006 AIAA-2014-2007 AIAA-2014-2008 AIAA-2014-2009 Summary and Statistical Analysis Measurements Supporting 1st Sonic LAVA Simulations for the First AIAA Computational and Experimental of the First AIAA Sonic Boom Boom Prediction Workshop Cases Sonic Boom Prediction Workshop Assessment of Models for the Prediction Workshop J. Morgenstern, Lockheed Martin J. Housman, NASA Ames Research Center, First AIAA Sonic Boom Prediction M. Park, NASA Langley Research Center, Corporation, Palmdale, CA Mountain View, CA; E. Sozer, STC, Workshop Using Adaptive High Hampton, VA; J. Morgenstern, Lockheed Mountain View, CA; C. Kiris, NASA Ames Fidelity CFD methods Martin Corporation, Palmdale, CA Research Center, Mountain View, CA F. Dagrau, Dassault Aviation, Paris, France; A. Loseille, INRIA, Villeneuve d’Ascq, France; I. Salah El Din, ONERA, Toulouse, France Monday, 16 June 2014 6-APA-3 Aerodynamic Analysis and Design: Design Methodologies Dunwoody Chaired by: D. FINLEY, Lockheed Martin Aeronautics and T. DOUVILLE, TLG Aerospace, LLC. 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2014-2010 AIAA-2014-2011 AIAA-2014-2012 AIAA-2014-2013 A Generic Airfoil Design Method A Rapid Approach to the Collaborative Aircraft Design Re-designing door handles to Based on a Naturally Bounded Aerodynamic Design of a Flexible Methodology using ADAS Linked reduce aerodynamic drag in road PARSEC Approach High-Lift Wing to CEASIOM vehicles S. Ghosh, H. Ran, D. Mavris, Georgia G. Trapani, A. Savill, T. Kipouros, Cranfield M. Zhang, A. Rizzi, Royal Institute of G. Ramchandran, A. Nepak, Y. Institute of Technology, Atlanta, GA University, Cranfield, United Kingdom; C. Technology (KTH), Stockholm, Sweden; F. Mukkamala, Vellore Institute of Agostinelli, University of Bristol, Bristol, Nicolosi, A. De Marco, University of Naples Technology (VIT), Vellore, India United Kingdom; A. Rampurawala, Airbus, “Federico II”, Naples, Italy Filton, United Kingdom Monday, 16 June 2014 7-APA-4 Low Speed, Low Reynolds Number, Transonic, Supersonic and Hypersonic Aerodynamics I Edgewood Chaired by: K. ABDOL-HAMID, NASA Langley Research Center 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2014-2014 AIAA-2014-2015 AIAA-2014-2016 AIAA-2014-2017 AIAA-2014-2018 Static Stall Hysteresis of Low- Unsteady Effects on Airfoils in the Comparison Study of Non Upstream Effect of Trailing Edge Effects of Reynolds Number and Aspect-Ratio Wings Ground Proximity due to Unsteady Sinusoidal Pitch over Sinusoidal Tonal Emissions on a Laminar Turbulent Intensity on a Low M. Mizoguchi, Y. Kajikawa, H. Itoh, Flow Separations at Low Reynolds Pitch at Higher Angle of Attack Separation Bubble Reynolds Number Airfoil National Defense Academy, Yokosuka, Numbers R. Zaman, J. Lai, J. Young, M. Ashraf, S. Pröbsting, Delft University of S. Wang, Hong Kong Polytechnic Japan D. Mateescu, A. Panahi, C. Wang, McGill University of New South Wales at the Technology, Delft, The Netherlands; S. University, Hong Kong, Hong Kong; University, Montréal, Canada Australian Defence Force Academy, Yarusevych, University of Waterloo, Y. Zhou, M. Alam, Harbin Institute of

42 Canberra, Australia Waterloo, Canada Technology, Shenzhen, China Monday, 16 June 2014 8-ATIO-1 Terminal & Surface Operations I - Terminal Airspace Embassy D Chaired by: L. REN, GE Global Research Center 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2014-2019 AIAA-2014-2020 AIAA-2014-2021 AIAA-2014-2022 AIAA-2014-2023 AIAA-2014-2024 Characterization of Nationwide Design Characteristics of a Terminal A Tactical Separation Assurance Conflict Free Trajectory An Evaluation of Retrofit Flight GPU-based Parallelization for TRACON Departure Operations Departure Scheduler System for Terminal Airspace Optimisation with Target Tracking Deck Displays for Interval Schedule Optimization with M. Kistler, A. Capps, Mosaic ATM, Inc., A. Capps, Mosaic ATM, Inc., Fort Worth, H. Tang, NASA Ames Research Center, and Conformance Monitoring Management Uncertainty Leesburg, VA; S. Engelland, NASA Ames TX; M. Kistler, Mosaic ATM, Inc., Leesburg, Moffett Field, CA S. Vilardaga, Aerospace Research and K. Swieringa, S. Wilson, NASA Langley C. Bosson, M. Xue, University Affiliated Research Center, Fort Worth, TX VA; S. Engelland, NASA Ames Research Technology Centre (CTAE-ASCAMM), Research Center, Hampton, VA; R. Shay, Research Center, Moffett Field, CA; S. Center, Fort Worth, TX Barcelona, Spain; P. Duan, Ohio University, Double Black Aviation Technology, LLC, Zelinski, NASA Ames Research Center, Athens, OH; X. Prats, Technical University Littleton, CO Moffett Field, CA of Catalonia, Barcelona, Spain; M. Uijt De Haag, Ohio University, Athens, OH Monday, 16 June 2014 9-ATIO-2 ATM-I Analysis Techniques in ATM Embassy E Chaired by: Y. JUNG, NASA Ames Research Center 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2014-2025 AIAA-2014-2026 AIAA-2014-2027 AIAA-2014-2028 AIAA-2014-2029 Analysis of Airport Ground Delay Ground Delay Program Analytics Designing Strategic Planning Robust And Practical Traffic Flow A Multi-resolution Spatiotemporal Program Decisions Using Data with Behavioral Cloning and Strategies using Multi-Objective Management Optimization Algorithm Scenario Clustering Algorithm for Mining Techniques Inverse Reinforcement Learning Genetic Algorithms For Near-Term Implementation Flow Contingency Management D. Kulkarni, Y. Wang, B. Sridhar, NASA M. Bloem, NASA Ames Research Center, C. Taylor, T. Masek, C. Wanke, MITRE A. Saraf, G. Hunter, K. Ramamoorthy, K. J. Xie, Y. Zhou, Y. Wan, University of North Ames Research Center, Moffett Field, CA Moffett Field, CA; N. Bambos, Stanford Corporation, McLean, VA Cheng, K. Griffin, G. Nagle, Saab Sensis Texas, Denton, TX; S. Tien, C. Taylor, C. University, Stanford, CA Corporation, Campbell, CA Wanke, MITRE Corporation, McLean, VA Monday, 16 June 2014 10-ACD-1 Aircraft Design Methods and Tools I Embassy F Chaired by: W. ANEMAAT, DARcorporation 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2014-2030 AIAA-2014-2031 AIAA-2014-2032 AIAA-2014-2033 AIAA-2014-2034 AIAA-2014-2035 Aircraft Conceptual Design: Tools A Stochastic Process Metamodel Multi-Disciplinary Survey of Aircraft Component A Constrained Global Optimization The Multi-Disciplinary Optimization Evaluation for Levering Similar Trends across Engine Parameters and its Impact Multidisciplinary Design Framework for Aircraft Design Based on Self- D. Locatelli, B. Riggins, J. Schetz, R. Kapania, Concepts on Performance and Energy Optimization Considering Cost D. Poole, C. Allen, T. Rendall, University of Adaptive Approximation Model Virginia Polytechnic Institute and State J. Valenzuela-del Río, D. Mavris, Georgia Maneuverability Performance Bristol, Bristol, United Kingdom M. Liu, Y. Hu, Northwestern Polytechnical University, Blacksburg, VA; B. Robic, C. Institute of Technology, Atlanta, GA C. Gedeon, T. Takahashi, Arizona State X. Zhao, R. Curran, Delft University of University, Xi’an, China Leenaert, Snecma, Villaroche, France; et al. University, Tempe, AZ Technology, Delft, The Netherlands Monday, 16 June 2014 11-MAO-1 Multidisciplinary Analysis and Optimization: Shape and Topology I Embassy G Chaired by: V. KALIVARAPU, Iowa State University 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2014-2036 AIAA-2014-2037 AIAA-2014-2038 AIAA-2014-2039 Topology Optimization for Additive Topology Optimization of A Methodology for the Prediction of Automatic Design Evaluation of Manufacturing: Considering Thermoelastic Structures using Air Transportation Network Growth Nacelle Geometry Using 3D-CFD Maximum Overhang Constraint Stress-based Design Criteria Dynamics M. Albert, D. Bestle, Brandenburg A. Gaynor, Johns Hopkins University, J. Deaton, R. Grandhi, Wright State M. Hassan, D. Mavris, Georgia Institute of University of Technology, Cottbus, Baltimore, MD; N. Meisel, C. Williams, University, Dayton, OH Technology, Atlanta, GA Germany Virginia Polytechnic Institute and State University, Blacksburg, VA; J. Guest, Johns Hopkins University, Baltimore, MD 43 Monday, 16 June 2014 12-MAO-2 Multidisciplinary Analysis and Optimization: MDO Frameworks Embassy H Chaired by: B. ROTH, Walla Walla Univ 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2014-2040 AIAA-2014-2041 AIAA-2014-2042 AIAA-2014-2043 Optimization of Excess System Geometry and Structural Automatic Evaluation of Nonintrusive Continuum Sensitivity Capability for Increased Modeling for High-Fidelity Aircraft Multidisciplinary Derivatives Analysis for Aerodynamic Shape Reconfigurability Conceptual Design Optimization Using a Graph-Based Problem Optimization J. Watson, J. Allen, C. Mattson, Brigham J. Hwang, G. Kenway, J. Martins, Formulation in OpenMDAO M. Kulkarni, R. Canfield, M. Patil, Virginia Young University, Provo, UT; E. Cansler, S. University of Michigan, Ann Arbor, Ann J. Gray, T. Hearn, K. Moore, NASA Glenn Polytechnic Institute and State University, Ferguson, North Carolina State University, Arbor, MI Research Center, Cleveland, OH; J. Hwang, Blacksburg, VA Raleigh, NC J. Martins, University of Michigan, Ann Arbor, Ann Arbor, MI Monday, 16 June 2014 13-APA-5/FC-1 Flow Control (Active and Passive): Computational and Experimental Results I Fairlie Chaired by: S. SILTON, US Army Research Laboratory and H. BABINSKY, University of Cambridge 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2014-2044 AIAA-2014-2045 AIAA-2014-2046 AIAA-2014-2047 AIAA-2014-2048 AIAA-2014-2049 Numerical Exploration of Flow Aerodynamic Control of a Pitching Numerical analysis and UAV Numerical and Experimental Study on A continuous adjoint-based A Numerical Study of Flapping Control for Delay of Dynamic Stall Airfoil by Active Bleed application of the ACHEON vectorial the Ability of Dynamic Roughness to approach for the optimization of Plates Hinged with a Trailing-Edge on a Pitching Airfoil J. Kearney, A. Glezer, Georgia Institute of thrust nozzle Alter the Development of a Leading wing flapping Flap M. Visbal, Air Force Research Laboratory, Technology, Atlanta, GA A. Suñol, D. Vucinic, Vrije Universiteit Edge Vortex M. Wei, M. Xu, New Mexico State Y. Ren, C. Li, H. Dong, University of Wright-Patterson AFB, OH Brussel, Brussels, Belgium C. Griffin, W. Huebsch, West Virginia University, Las Cruces, NM Virginia, Charlottesville, Charlottesville, VA University, Morgantown, WV Monday, 16 June 2014 14-FD-1 High-Reynolds-Number Fluid Structure Interaction I (Invited) Greenbriar Chaired by: D. BODONY, University of Illinois at Urbana-Champaign and R. PONNAPPAN, US Air Force 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs Oral Presentation Oral Presentation Oral Presentation Oral Presentation Oral Presentation Open Discussion AFOSR Turbulence and Transition HIFiRE-1 Shock Boundary Layer Advancements & Experimental Fatigue Loading in Hypersonic Complex Fluid-Structure Program Overview Interaction Pressure Fluctuations Measurement Challenges of Shock Flight due to Large-Scale Interactions Arising from Shock R. Ponnappan, Air Force Office of Scientific R. Kimmel, Air Force Research Laboratory, Boundary Layer Interaction (SBLI) Unsteadiness Impingement on a Flexible Panel Research, Arlington, VA Wright-Patterson Air Force Base, OH Influence on the Dynamic Response J. Poggie, R. Gosse, Air Force Research M. Visbal, Air Force Research Laboratory, of a Flexible Panel Laboratory, Wright-Patterson Air Force Wright-Patterson Air Force Base, OH T. Beberniss, S. Spottswood, T. Eason, Base, OH Air Force Research Laboratory, Wright- Patterson Air Force Base, OH Monday, 16 June 2014 15-AFM-1 Aeroservoelastic (ASE) Control, Modeling, Simulation, and Optimization I Hanover A Chaired by: M. BRENNER, NASA-Dryden Flight Research Center and P. CHENG, Boeing Defense, Space & Security 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2014-2050 AIAA-2014-2051 AIAA-2014-2052 AIAA-2014-2053 AIAA-2014-2054 AIAA-2014-2055 Optimization of Control Surface Adaptive Aeroelastic Suppression Aeroelastic Optimization Study Robust Modal Filtering and Control Fabrication and Characterization of Aeroservoelastic Modeling and Parameters with Augmented Flutter of a Wind Turbine Blade Using Based on the X-56A Model of the X-56A Model with Simulated 3-D printed Heat Flux Sensors for Analysis of a Missile Control Boundary Constraints Trailing-edge Flap W. Li, C. Pak, NASA Dryden Flight Fiber Optic Sensor Failures Advanced Wind Tunnel Models and Surface with a Nonlinear K. Singh, L. McDonough, Miami University, N. Li, Yangzhou University, Yangzhou, Research Center, Edwards, CA P. Suh, A. Chin, NASA Dryden Flight Research Improved CFD Validation Electromechanical Actuator Oxford, OH China; M. Balas, University of Wyoming, Center, Edwards, CA; D. Mavris, Georgia J. Coggin, J. Schetz, Virginia Polytechnic A. Kayran, Middle East Technical Laramie, Laramie, WY Institute of Technology, Atlanta, GA Institute and State University, Blacksburg, VA; University, Ankara, Turkey; M. Nalci,

44 M. Newton, Newton Cyberfacturing, Orlando, ROKETSAN Missiles Industries, Inc., FL; R. Kapania, Virginia Polytechnic Institute Ankara, Turkey and State University, Blacksburg, VA; D. Howard, NextGen Aeronautics, Torrance, CA; H. Chung, Virginia Polytechnic Institute and State University, Blacksburg, VA Monday, 16 June 2014 16-AFM-2 Aircraft Flight Dynamics, Handling Qualities, and Performance I Hanover B Chaired by: N. FEZANS, DLR and M. BOLENDER, AFRL/RBCA 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2014-2056 AIAA-2014-2057 AIAA-2014-2058 AIAA-2014-2059 Flight Dynamics Simulation with F-35A High Angle of Attack Testing Alternative Trim Analysis A Takeoff Rotation Model Including Integrated Electrical System Model S. Baer, Lockheed Martin Corporation, Formulations for Vehicles with Pilot Technique Parameters for for Pilot-in-the-Loop Testing Edwards AFB, CA Redundant Multi-Axis Control Flight Test Data Reduction and T. Benoit, LMS International, Leuven, Belgium; Surfaces Expansion J. Verbeke, Kulab, Oostend, Belgium; R. De D. Garmendia, D. Mavris, Georgia Institute L. Van Bavel, Luc Van Bavel Design, Roo, Vives, Oostend, Belgium; Y. Lemmens, of Technology, Atlanta, GA Quebec City, Canada LMS International, Leuven, Belgium Monday, 16 June 2014 17-ASE-1 Ice Protection Systems and Hydrophobic Coating Application Hanover C Chaired by: R. KREEGER, NASA Glenn Research Center and J. PALACIOS, The Pennsylvania State University 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2014-2060 AIAA-2014-2061 AIAA-2014-2062 AIAA-2014-2063 AIAA-2014-2064 AIAA-2014-2065 Feasibility Study of a Hybrid Ice A robust coupling algorithm applied Heat and mass transfer analogies Ice Adhesion Strength on Behavior of a Small Water Droplet Experimental Investigation Protection System to thermal ice protection system for evaporation models at high Hydrophobic and Superhydrophobic on Superhydrophobic Coating of a Single Droplet on a T. Strobl, S. Storm, EADS, Munich, unsteady modeling evaporation rate Coatings and Heating Surface in Cold Superhydrophobic Coating in Icing Germany; D. Thompson, Mississippi State R. Chauvin, P. Villedieu, P. Trontin, ONERA, P. Trontin, P. Villedieu, ONERA, Toulouse, Y. Yeong, E. Loth, University of Virginia, Environment Wind Tunnel for the Development University, Mississippi State, MS; M. Toulouse, France; L. Bennani, Airbus, France Charlottesville, Charlottesville, VA; J. H. Endo, S. Kimura, Kanagawa Institute of of Ice-Protection System Hornung, Technical University of Munich, Toulouse, France Sokhey, Rolls-Royce North America, Technology, Kanagawa, Japan; M. Katuaki, M. Hasegawa, T. Hyugaji, Y. Yamagishi, S. Munich, Germany Indianapolis, IN; A. Lambourne, Rolls- H. Sakaue, Japan Aerospace Exploration Kimura, Kanagawa Institute of Technology, Royce Group plc, Derby, United Kingdom Agency (JAXA), Tokyo, Japan Atsugi, Japan; M. Katuaki, H. Sakaue, Japan Aerospace Exploration Agency (JAXA), Chofu, Japan Monday, 16 June 2014 18-ASE-2 Icing Weather and Forecasting Hanover D Chaired by: M. POLITOVICH, National Center for Atmospheric Research and J. MURRAY, NASA-Langley Research Center 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2014-2066 AIAA-2014-2067 AIAA-2014-2068 AIAA-2014-2069 AIAA-2014-2070 A Numerical Weather Model’s Weather Support for Terminal Area Application of a Nowcasting Tool for Improving Diagnoses of In-Flight Diagnosing and Forecasting In- Ability to Predict Aircraft and Icing Weather Information Analysis of Meteorological Conditions Icing Conditions in Regions of Flight Icing Conditions in Alaska Ground Icing Environments S. Landolt, M. Politovich, A. Schwartz, K. Associated with Engine Icing Sparsely Distributed Surface C. Wolff, D. Adriaansen, M. Politovich, G. Thompson, M. Politovich, National Center Goodrich, National Center for Atmospheric J. Black, J. Haggerty, G. McCabe, C. Observations National Center for Atmospheric Research,

45 for Atmospheric Research, Boulder, CO Research, Boulder, CO Wolff, G. Cunning, National Center for D. Adriaansen, G. Thompson, C. Wolff, M. Boulder, CO Atmospheric Research, Boulder, CO; A. Politovich, National Center for Atmospheric Grandin, Airbus, Toulouse, France Research, Boulder, CO Monday, 16 June 2014 19-PDL-1 Laser Physics Hanover E Chaired by: K. KREMEYER, PM & AM Research and A. YALIN, Colorado State University 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2014-2071 AIAA-2014-2072 AIAA-2014-2073 AIAA-2014-2074 AIAA-2014-2075 Laser Generated Plasma Using Shock Train Formation in COIL Effect of Ionization Waves on Development of a Photonic Crystal Computational Model and a Dual Pulse Approach with Lasers Propagation of a Laser-Supported Fiber Delivery System for Laser Calculation Method of Flammable Application to Laser Ignition I. Zilberter, J. Edwards, North Carolina Detonation Wave Ignition in Engines Oxyhydrogen Mixture Ignition with C. Dumitrache, A. Yalin, Colorado State State University, Raleigh, NC K. Shimamura, J. Ofosu, K. Komurasaki, C. Dumitrache, Colorado State University, Laser-Induced Plasma University, Fort Collins, CO; M. Shneider, University of Tokyo, Chiba, Japan; H. Fort Collins, CO; J. Rath, Seaforth, LLC, S. Ryzhkov, Moscow State Technical Princeton University, Princeton, NJ Koizumi, University of Tokyo, Tokyo, Japan Fort Collins, CO; A. Yalin, Colorado State University, Moscow, Russia; V. Kuzenov, University, Fort Collins, CO; S. Gupta, Russian Academy of Sciences, Moscow, Argonne National Laboratory, Argonne, IL Russia Monday, 16 June 2014 20-AA-1 Airframe Noise I Hanover F Chaired by: E. GARCIA, Georgia Institute of Technology 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2014-2076 AIAA-2014-2077 AIAA-2014-2078 AIAA-2014-2079 AIAA-2014-2080 Aerodynamic and Acoustic Design Numerical Investigation of a Incorporating and Minimizing Airframe noise source diagnostics Experimental Study on Slat Noise of Silent Leading Edge Device Realistic Nose Landing Gear Aircraft Noise Annoyance During of a large-scale semi-span model from 30P30N Three-Element M. Pott-Pollenske, J. Wild, German J. Dahan, C. O’Reilly, G. Efraimsson, Royal Conceptual Aircraft Design in DNW-NWB and experimental High-Lift Airfoil at JAXA Hard-Wall Aerospace Center (DLR), Braunschweig, Institute of Technology (KTH), Stockholm, A. Sahai, E. Stumpf, RWTH Aachen investigation of wing element Lowspeed Wind Tunnel Germany; L. Bertsch, German Aerospace Sweden University, Aachen, Germany modification for noise suppression M. Murayama, K. Nakakita, K. Yamamoto, Center (DLR), Göttingen, Germany V. Kopiev, M. Zaytsev, I. Belyaev, H. Ura, Y. Ito, Japan Aerospace Exploration TsAGI, Moscow, Russia; A. Gorbushin, I. Agency (JAXA), Mitaka, Japan; M. Chernyshev, TsAGI, Zhukovsky, Russia; M. Choudhari, NASA Langley Research Center, Pott-Pollenske, German Aerospace Center Hampton, VA (DLR), Braunschweig, Germany Monday, 16 June 2014 21-MST-1 M&S: Applications Hanover G Chaired by: J. KRUEP, Aerojet Rocketdyne 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2014-2081 AIAA-2014-2082 AIAA-2014-2083 AIAA-2014-2084 The Expanded Reach of Simulation Comparative Solution Methods for Response Surface Based An Approach for Modeling, Design, Based Aircraft System Verification the Integrated Problem of Sensors, Performance Analysis of an Air- and Energy Evaluation of Small and its Software Capability Weapons, and Targets Defense Missile System Against Convertible Aerial Vehicles Requirements K. Ezra, D. DeLaurentis, L. Mockus, Purdue Maneuvering Targets K. Phung, P. Morin, Pierre and Marie Curie

46 S. James, C. Savaglio, Applied Dynamics University, West Lafayette, IN K. Günaydin, T. Çimen, ROKETSAN Missiles University, Paris, France Corporation, Ann Arbor, MI Industries, Inc., Ankara, Turkey; O. Tekinalp, Middle East Technical University, Ankara, Turkey Monday, 16 June 2014 22-FD-2 Turbulence Modeling I Harris Chaired by: B. SMITH, Lockheed Martin Aeronautics 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2014-2085 AIAA-2014-2086 AIAA-2014-2087 AIAA-2014-2088 AIAA-2014-2089 Bayesian calibration of a k-ε Turbulence Model Extension for On the Accuracy of RANS Assessment of Higher-order RANS An Examination of Parameters turbulence model for predictive Low Speed Thermal Shear Layers Simulations of 2D Boundary Layers Closures in a Decelerated Planar Affecting Large Eddy Simulations of jet-in-crossflow simulations R. Bush, Pratt & Whitney, East Hartford, with OpenFOAM Wall-bounded Turbulent Flow a Square Cylinder J. Ray, S. Lefantzi, Sandia National CT S. Gomez, B. Graves, S. Poroseva, E. Jeyapaul, National Institute of M. Mankbadi, N. Georgiadis, NASA Glenn Laboratories, Livermore, CA; S. University of New Mexico, Albuquerque, Aerospace, Hampton, VA; G. Coleman, C. Research Center, Cleveland, OH Arunajatesan, L. DeChant, Sandia National Albuquerque, NM Rumsey, NASA Langley Research Center, Laboratories, Albuquerque, NM Hampton, VA Monday, 16 June 2014 23-FD-3 Simulation Algorithms I Inman Chaired by: E. WHITE, Texas A&M University and K. SREENIVAS, SimCenter: National Center for Computational Engineering 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2014-2090 AIAA-2014-2091 AIAA-2014-2092 AIAA-2014-2093 AIAA-2014-2094 High-Order Residual-Distribution First, Second, and Third Order Active Flux for Diffusion A High-Order Immersed Interface Decreasing the computing time of Hyperbolic Advection-Diffusion Finite-Volume Schemes for Navier- H. Nishikawa, National Institute of Method for Compressible Flows the CFD code Edge by LU-SGS and Schemes: 3rd-, 4th-, and 6th-Order Stokes Equations Aerospace, Hampton, VA; P. Roe, C. Brehm, M. Barad, NASA Ames Research line-implicit methods A. Mazaheri, NASA Langley Research Center, H. Nishikawa, National Institute of University of Michigan, Ann Arbor, Ann Center, Moffett Field, CA; C. Hader, E. Otero, Royal Institute of Technology Hampton, VA; H. Nishikawa, National Institute Aerospace, Hampton, VA Arbor, MI; T. Eymann, CREATE Kestrel University of Arizona, Tucson, Tucson, AZ (KTH), Stockholm, Sweden; P. Eliasson, of Aerospace, Hampton, VA Team, Eglin AFB, FL Swedish Defense Research Agency (FOI), Stockholm, Sweden Monday, 16 June 2014 24-FD-4 Ramjet and Scramjet Propulsion Systems I Kenneshaw Chaired by: J. EDWARDS 0930 hrs 1000 hrs 1030 hrs AIAA-2014-2095 AIAA-2014-2096 AIAA-2014-2097 Large-eddy / Reynolds-Averaged Supersonic Combustion Processes in Development and Application of Navier-Stokes Simulation of Cavity- an Inlet Fuelled 3D Non-Uniform- Numerical Technology for simulation Stabilized Ethylene Combustion Compression Scramjet Engine of different combustion types in high- A. Potturi, J. Edwards, North Carolina State M. Bricalli, L. Brown, R. Boyce, University speed viscous gas turbulent flows University, Raleigh, NC of Queensland, Brisbane, Australia A. Shiryaeva, K. Anisimov, TsAGI, Zhukovsky, Russia

47 Monday, 16 June 2014 25-FC-2 Flow Control: Actuation and Sensing Lenox Chaired by: R. WOSZIDLO, Technical University Berlin 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2014-2098 AIAA-2014-2099 AIAA-2014-2100 AIAA-2014-2101 AIAA-2014-2102 Wall-shear stress measurements Balanced Truncation of System Models Actuator and Sensor Placement for Optimized sensor placement using Estimation of Plume Concentration in an adverse pressure gradient Using Reduced Resolution Sensing for Flow Control stochastic estimation for a flow over a from a Moving Source with an turbulent boundary layer Plane Poiseuille Flow State Estimation M. Natarajan, J. Freund, D. Bodony, 2D airfoil with Coanda blowing Unmanned Aerial Vehicle K. Geurts, B. Nottebrock, W. Schroeder, A. Friedman, Y. Oshman, J. Cohen, Technion-- University of Illinois, Urbana-Champaign, P. Kumar, Y. El Sayed, R. Semaan, N. Gatsonis, M. Demetriou, T. Egorova, RWTH Aachen University, Aachen, Israel Institute of Technology, Haifa, Israel Urbana, IL Technical University of Braunschweig, Worcester Polytechnic Institute, Worcester, Germany Braunschweig, Germany MA Monday, 16 June 2014 26-APA-6 Airfoil/Wing/Configuration Aerodynamics I Marietta Chaired by: A. MCCOMAS, TLG Aerospace 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2014-2103 AIAA-2014-2104 AIAA-2014-2105 AIAA-2014-2106 AIAA-2014-2107 Computational Modelling of Fixed Impact of Forebody Strakes on Unsteady interactions of a Parametric Trade Study for Advanced Laminar Flow and Rotary Wing Aerodynamics Wing Rock behavior on a Generic wandering streamwise-oriented Supersonic Bi-Directional Flying Aerodynamic Configuration Operating in Close Proximity to Chine Body-Wing Configuration vortex with a wing Wing Optimization Design for Green Wavy Free Surfaces H. Qureshi, Y. Wang, W. Shi, Q. Li, Z. Qiu D. Garmann, M. Visbal, Air Force Research J. Gan, A. Lefebvre, D. Espinal, G. Zha, Aviation R. Prasad, V. Dwivedi, M. Damodaran, Shi, Beihang University, Beijing, China Laboratory, Wright-Patterson AFB, OH University of Miami, Miami, FL Z. Gao, Northwestern Polytechnical Indian Institute of Technology University, Xi’an, China Gandhinagar, Ahmedabad, India Monday, 16 June 2014 27-AMT-1/GT-1 Ground Test Facility Operation and Improvement Piedmont Chaired by: J. EVERHART, NASA-Langley Research Center and J. VAN AKEN, Jacobs Technology 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2014-2108 AIAA-2014-2109 AIAA-2014-2110 AIAA-2014-2111 Mach Number Control improvement Neural-Network Control of Wind Exploiting the Characteristics Reducing Cost and Increasing in ONERA S1MA large Transonic Tunnel Test Conditions of Kevlar-Wall Wind Tunnels Speed: Managing your Test Capital Wind Tunnel M. Rennie, P. Sutcliffe, A. Vorobiev, for Conventional Aerodynamic at the Intersection of Critical Value P. Crozier, C. Chargy, ONERA, Modane, University of Notre Dame, Notre Dame, IN; Measurements Streams and Knowledge France; R. Pichon, ONERA, Châtillon, A. Cain, Innovative Technology Applications K. Brown, W. Devenport, A. Borgoltz, P. McNamara, Sente Group, Suwanee, GA France Company, Chesterfield, MO Virginia Polytechnic Institute and State University, Blacksburg, VA Monday, 16 June 2014 28-HYTASP-15 SPHS Introduction Regency Ballroom V 0930 - 1000 hrs Chaired by: A. SIEBENHAAR, Aerojet Rocketdyne Adam Siebenhaar Aerojet Rocketdyne Monday, 16 June 2014 29-PANEL-1 Panel: Aviation’s Challenges & Opportunities - Georgia’s Global Perspectives Regency Ballroom VI 0930 - 1130 hrs Moderator: Steve Justice, Director, Georgia Center of Innovation for Aerospace 48 Panelists: Steve Dickson Al Hegner Jack Crisler Senior Vice President, Flight Operations Director, Base Maintenance Vice President, New Business, Air Mobility, Special Forces and Maritime Programs Delta Air Lines Delta Air Lines Lockheed Martin Aeronautics Company

Monday, 16 June 2014 30-AMT-2/PDL-2 Diagnostics I Roswell Chaired by: C. LIMBACH, Princeton University and J. POGGIE, USAF AFRL/RBAC 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2014-2112 AIAA-2014-2113 AIAA-2014-2114 AIAA-2014-2115 Emission Spectroscopy Time-Resolved Electron Temperature Radar REMPI measurements of N2 Measurement of Continuum Characterization of Thermal and Number Density Measurements rotational temperature Breakdown during Disc Spin-down Protection System Materials in in a Nanosecond Pulse Filament S. McGuire, R. Miles, Princeton University, in Low Pressure Air Arc-Heated Flows Discharge Using Thomson Scattering Princeton, NJ T. Acharya, J. Falgoust, M. Martin, D. Codron, B. Cruden, T. Ho, NASA Ames A. Roettgen, I. Shkurenkov, I. Adamovich, W. Louisiana State University, Baton Rouge, Research Center, Moffett Field, CA Lempert, Ohio State University, Columbus, OH LA; R. Rasmussen, Guidance Dynamics Corporation, Simi Valley, CA Monday, 16 June 2014 31-FC-3/PDL-3 Plasma-Based Flow Control I Spring Chaired by: V. NARAYANASWAMY, North Carolina State Univ and P. MORGAN, Ohio Aerospace Institute 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2014-2116 AIAA-2014-2117 AIAA-2014-2118 AIAA-2014-2119 Numerical Simulations Investigating Application of linear sliding Nanosecond pulsed discharge Effect of dielectric material on Flow Over Flat Plate Suction discharges for flow control: study plasma actuation: characteristics thermal effect produced by ns-DBD Perforations Driven by Dielectric of the energy coupling mechanisms and flow control performance plasma actuator Barrier Discharge Plasma Actuation P. Castera, P. Elias, ONERA, Palaiseau, Y. Wu, Xi’an Jiaotong University, Xi’an, G. Correale, M. Kotsonis, Delft University P. Morgan, Ohio Aerospace Institute, France; C. Laux, École Centrale Paris, China of Technology, Delft, The Netherlands Wright-Patterson AFB, OH; M. Visbal, Air Châtenay-Malabry, France Force Research Laboratory, Wright-Patterson AFB, OH Monday, 16 June 2014 32-TP-1 Ablation I Techwood Chaired by: D. KUNTZ, Sandia National Laboratories 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2014-2120 AIAA-2014-2121 AIAA-2014-2122 AIAA-2014-2123 AIAA-2014-2124 AIAA-2014-2125 Toward Ablative Material Response Numerical Investigation of Gas/Surface Interaction Study of Coupled CFD-Ablation Response Simulation of Ablating Hypersonic Development and Testing of an Coupling in DPLR Pyrolysis Gas Blowing Pattern Low-Density Ablators in Sub- and Model Simulations Using the libMesh Vehicles with Finite-Rate Surface Ablation Model Based on Plasma S. Muppidi, M. Barnhardt, ERC, Inc., and Thermal Response using Supersonic Plasmas Framework Chemistry Wind Tunnel Experiments Moffett Field, CA; N. Mansour, NASA Ames Orthotropic Charring Ablative B. Helber, A. Turchi, O. Chazot, T. Magin, G. Palmer, M. Barnhardt, ERC, Inc., Moffett E. Farbar, H. Alkandry, J. Wiebenga, I. A. Turchi, B. Helber, A. Munafò, T. Magin, Research Center, Moffett Field, CA Material von Kármán Institute for Fluid Dynamics, Field, CA; A. Amar, B. Kirk, NASA Johnson Boyd, University of Michigan, Ann Arbor, von Kármán Institute for Fluid Dynamics, H. Weng, A. Martin, University of Rhode-Saint-Genèse, Belgium; A. Hubin, Space Center, Houston, TX; Y. Chen, NASA Ann Arbor, MI Rhode-Saint-Genèse, Belgium

49 Kentucky, Lexington, Lexington, KY Vrije Universiteit Brussel, Brussels, Belgium Ames Research Center, Moffett Field, CA Monday, 16 June 2014 33-TP-2 Heat Transfer Enhancement and Energy Harvesting I University Chaired by: Y. CHUDNOVSKY, Gas Technology Institute and E. MAROTTA, FMC Technologies Inc 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2014-2126 AIAA-2014-2127 AIAA-2014-2128 AIAA-2014-2130 A Phase Change Study of Heat Transfer Enhancement in The effect of step length and Influence of a gap on Heat Transfer Electroplated Copper Wick Latent Heat Storage Units inclined angle of backward facing and Friction Factor in a Square Duct Structures T. Rozenfeld, Y. Kozak, G. Ziskind, Ben- step on heat transfer characteristics Roughened with Discrete Ribs S. Cai, A. Bhunia, Teledyne Scientific & Gurion University of the Negev, Beer- R. Moosavi, Florida International A. Chaube, Jabalpur Engineering Imaging, Thousand Oaks, CA Sheva, Israel University, Miami, FL; S. Gandjalikhan College, Jabalpur, India; S. Gupta, State Nasab, Shahid Bahonar University, Technological University of Madhya Kerman, Iran; R. Kiflemariam, C. Lin, Prades, Bhopal, India Florida International University, Miami, FL Monday, 16 June 2014 34-TP-3 Multi-Scale Heat Transfer I Vinings Chaired by: A. NARAYANASWAMY, Columbia University and A. HASHEMI, Lockheed Martin Space Systems 0930 hrs 1000 hrs 1030 hrs 1100 hrs Oral Presentation Oral Presentation AIAA-2014-2131 Oral Presentation Thermal conductivity of Superatom Electromagnetic Energy Density and Gridless Direct Simulation Monte When Can the Effective Medium Molecular Solids Power Dissipation Derived from the Carlo Approach for Analysis of Theory Be Used to Calculate Near- J. Malen, W. Ong, J. Epstein, A. Equivalent Circuit Approach Fractal-Like Spore Aggregates field Radiative Transfer between McGaughey, Carnegie Mellon University, J. Zhao, Harbin Institute of Technology, R. Jambunathan, D. Levin, Pennsylvania Multilayered Metamaterials? Pittsburgh, PA; X. Roy, E. O’Brien, Harbin, China; Z. Zhang, Georgia Institute State University, University Park, PA X. Liu, T. Bright, Z. Zhang, Georgia Columbia University, New York, NY of Technology, Atlanta, GA Institute of Technology, Atlanta, GA Monday, 16 June 2014 35-HYTASP-16 Global Reports I Regency Ballroom V 1000 - 1230 hrs Chaired by: A. SIEBENHAAR, Aerojet Rocketdyne

Participants: Michael Smart Christian Mundt Mario Cosmo Masataka Maita Richard Brown Steve Walker Australia Germany Italy Japan UK US

Monday, 16 June 2014 36-LNCH-1 Monday Networking Lunch Lunch on Own 1230 - 1400 hrs Monday, 16 June 2014 37-APA-7 Special Session: NATO Task Group AVT-201 II - CFD Prediction and Flow Analyses Baker Chaired by: A. SCHUETTE, DLR - German Aerospace Center 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs AIAA-2014-2132 AIAA-2014-2133 AIAA-2014-2134 AIAA-2014-2135 AIAA-2014-2136 Static and dynamic numerical Stability and Control CFD Numerical Simulation of Control CFD Predictions of Control Prediction and Validation of simulations of a generic UCAV Investigations of a Generic 53-deg Surface Deflections over a Generic Effectiveness for a Generic Highly Aerodynamic Characteristics for a configuration with and without Swept UCAV Configuration UCAV configuration at Off-design Swept UCAV Configuration Generic UCAV Configuration with control devices N. Frink, NASA Langley Research Center, Flow Conditions J. Coppin, T. Birch, Defence Science and Trailing-Edge Flaps A. Schuette, K. Huber, German Aerospace Hampton, VA D. Kennett, G. Hoholis, K. Badcock, Technology Laboratory, Fareham, United M. Young, Defence Science and Technology Center (DLR), Braunschweig, Germany; O. University of Liverpool, Liverpool, United Kingdom Organisation, Fishermans Bend, Australia; M.

50 Boelens, National Aerospace Laboratory Kingdom Ghoreyshi, A. Jirasek, R. Cummings, U.S. Air (NLR), Amsterdam, The Netherlands Force Academy, Colorado Springs, CO Monday, 16 June 2014 38-APA-8 Special Session: Sonic Boom Activities II Courtland Chaired by: L. BANGERT, NASA Langley Research Center 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2014-2137 AIAA-2014-2138 AIAA-2014-2139 Oral Presentation AIAA-2014-2140 AIAA-2014-2141 Boeing N+2 Supersonic Overview of Sonic Boom Reduction Uncertainty Quantification Sensitivity Study of Sonic Boom to Experimental and Computational Conceptual Design of Low-Boom Experimental Validation Phase II Efforts on the Lockheed Martin and Certification Prediction of Off Design Conditions Sonic Boom Assessment of Boeing Supersonic Aircraft with Flight Trim Program N+2 Supersonic Validations Low-Boom Supersonic Aircraft L. Ozoroski, NASA Langley Research N+2 Low Boom Models Requirement T. Magee, S. Fugal, L. Fink, The Boeing Program Configurations Center, Hampton, VA D. Durston, NASA Ames Research Center, I. Ordaz, K. Geiselhart, J. Fenbert, NASA Company, Huntington Beach, CA; S. Shaw, M. Buonanno, S. Chai, F. Marconi, T. West, Missouri University of Science Moffett Field, CA; A. Elmiligui, NASA Langley Langley Research Center, Hampton, VA The Boeing Company, Seattle, WA J. Morgenstern, Lockheed Martin and Technology, Rolla, MO; B. Reuter, Research Center, Hampton, VA; S. Cliff, NASA Corporation, Palmdale, CA University of Texas, Austin, Austin, TX; E. Ames Research Center, Moffett Field, CA; C. Walker, W. Kleb, M. Park, NASA Langley Winski, M. Carter, E. Walker, NASA Langley Research Center, Hampton, VA Research Center, Hampton, VA Monday, 16 June 2014 39-APA-9/FC-4 Flow Control (Active and Passive): Computational and Experimental Results II Dunwoody Chaired by: D. SMITH, Air Force Office of Scientific Research AFOSR and B. CYBYK, JHU/Applied Physics Laboratory 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2014-2142 AIAA-2014-2143 AIAA-2014-2144 AIAA-2014-2145 AIAA-2014-2146 AIAA-2014-2147 Numerical Simulation of a High-Lift Numerical Investigation of Leading Edge Separation Control Flow Control with Synthetic Jet Aerodynamic Response of a Wind Active Flow Control on a Two Configuration with Embedded Fluidic Tangential Blowing at the Rudder on an Airfoil in Fully-Reversed Actuators under Adverse Pressure Turbine Airfoil to Gurney Flap Element High-Lift Airfoil with Actuators of a Vertical Tailplane Airfoil Condition Gradient Laminar Boundary Layer Deployment Drooped Spoiler V. Vatsa, NASA Langley Research Center, A. Kroehnert, German Aerospace Center C. Clifford, A. Singhal, M. Samimy, Ohio M. Gül, O. Uzol, İ. Akmandor, Middle East P. Nikoueeyan, J. Strike, A. Magstadt, M. M. Casper, P. Scholz, Technical University Hampton, VA; D. Casalino, Exa Corporation, (DLR), Braunschweig, Germany State University, Columbus, OH Technical University, Ankara, Turkey Hind, J. Naughton, University of Wyoming, of Braunschweig, Braunschweig, Germany Stuttgart, Germany; J. Lin, NASA Langley Laramie, Laramie, WY Research Center, Hampton, VA; J. Appelbaum, Exa Corporation, Stuttgart, Germany Monday, 16 June 2014 40-APA-10 Low Speed, Low Reynolds Number, Transonic, Supersonic and Hypersonic Aerodynamics II Edgewood Chaired by: J. AZEVEDO 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs AIAA-2014-2148 AIAA-2014-2149 AIAA-2014-2150 AIAA-2014-2151 AIAA-2014-2152 A high-order immersed-boundary Comparison of CFD and quasi- Forward propulsion of a rigid Reynolds Number Effects on Propeller-Induced Flow Effects on method for simulations of flapping steady analysis of hovering plunging airfoil the Performance of Small-Scale Wings of Varying Planform at Low wings aerodynamics for a Ruby-throated N. Arora, A. Jain, A. Singh, A. Gupta, S. Propellers Reynolds Numbers C. Zhu, Vanderbilt University, Nashville, hummingbird Sanghi, Indian Institute of Technology R. Deters, G. Ananda Krishnan, M. Selig, G. Ananda Krishnan, R. Deters, M. Selig, TN; G. Li, University of Louisville, J. Song, H. Luo, Vanderbilt University, Delhi, New Delhi, India; H. Aono, Japan University of Illinois, Urbana-Champaign, University of Illinois, Urbana-Champaign, Louisville, KY; H. Luo, Vanderbilt Nashville, TN Aerospace Exploration Agency (JAXA), Urbana, IL Urbana, IL Sagamihara, Japan; et al.

51 University, Nashville, TN Monday, 16 June 2014 41-ATIO-3 Terminal & Surface Operations II - Surface/Airport Operations Embassy D Chaired by: A. SARAF, Saab Sensis Corporation 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs AIAA-2014-2153 AIAA-2014-2154 AIAA-2014-2155 AIAA-2014-2156 AIAA-2014-2157 AIAA-2014-2158 AIAA-2014-2159 Runway Location and Orientation Improved Safety and Capability via Branch & Bound Global-Search Relating Airport Surface Collision Impact of Gate Availability on Development of a Bayesian Belief A System Dynamics Approach to Suitability Analysis Direct Computation of Takeoff and Algorithm for Aircraft Ground Potential to Taxiway Geometry and Departure Metering Benefits Network Runway Incursion Model Airport Modeling J. Laat, P. Roling, Delft University of Landing Performance Data Movement Optimization Traffic Flow H. Idris, N. Shen, Engility Corporation, L. Green, NASA Langley Research Center, P. Biesslich, M. Schroeder, Hamburg University Technology, Delft, The Netherlands L. Bays, Self, Kennesaw, GA; K. Halpin, P. Godbole, A. Ranade, R. Pant, Indian A. Ford, T. Waldron, Saab Sensis Billerica, MA Hampton, VA of Technology, Hamburg, Germany; V. Elite Electronic Engineering, Inc., Downers Institute of Technology Bombay, Mumbai, Corporation, East Syracuse, NY Gollnick, German Aerospace Center (DLR), Grove, IL India Hamburg, Germany; K. Lütjens, Hamburg University of Technology, Hamburg, Germany Monday, 16 June 2014 42-ATIO-4 ATM-II Modeling & Simulation for ATM Embassy E Chaired by: S. HASAN, LMI 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs AIAA-2014-2160 AIAA-2014-2161 AIAA-2014-2162 AIAA-2014-2163 AIAA-2014-2164 AIAA-2014-2165 AIAA-2014-2166 An Operations-Structured Model Air Route Clustering for a Queuing METROSIM: A Metroplex-Wide Decision-Theoretic Prediction and Assessing Relation between Human-In-The-Loop Simulation to Traffic Aware Planner (TAP) Flight for Strategic Prediction of Airport Network Model of the National Route Planning and Airport Policy Design of GDP Slot Auctions Performance of Schedule-Based Validate Capability-Aware Traffic Evaluation Arrival Rate and Departure Rate Airspace System Scheduling Tool J. Bono, Economists, Inc., San Francisco, Arrival Operation and Schedule Flow Management Concept J. Maris, M. Haynes, Advanced Aerospace Futures J. DeArmon, C. Taylor, T. Masek, C. F. Wieland, A. Tyagi, V. Kumar, W. Krueger, CA; D. Wolpert, Santa Fe Institute, Santa Nonconformance E. Bromberg, M. Elliott, S. AhmadBeygi, Solutions, LLC., Raleigh, NC; D. Wing, R. Dhal, S. Roy, Washington State Wanke, MITRE Corporation, McLean, VA Intelligent Automation, Inc., Rockville, MD Fe, NM; D. Xie, J. Grana, American J. Jung, J. Thipphavong, NASA Ames Research T. Lewis, J. Burke, Metron Aviation, NASA Langley Research Center, Hampton, University, Pullman, WA; S. Tien, C. Taylor, University, Washington, DC Center, Moffett Field, CA; L. Martin, San Jose Inc., Dulles, VA; V. Sud, Federal Aviation VA C. Wanke, MITRE Corporation, McLean, VA State University, San Jose, CA Administration, Washington, DC Monday, 16 June 2014 43-ACD-2 Aircraft Design Methods and Tools II Embassy F Chaired by: M. DRAKE, Boeing Commercial Airplanes 1400 hrs 1430 hrs 1500 hrs AIAA-2014-2167 AIAA-2014-2168 AIAA-2014-2169 Integrating a human designer’s An exercise in design process Application of an Aircraft Design- preferences in multidisciplinary simulation using agent models To-Noise Simulation Process design optimization based on Bayesian global L. Bertsch, German Aerospace Center P. Reverdy, A. Reddy, L. Martinelli, N. Leonard, optimization (DLR), Göttingen, Germany; W. Heinze, Princeton University, Princeton, NJ A. Garbo, X. Fei, B. German, Georgia Technical University of Braunschweig, Institute of Technology, Atlanta, GA Braunschweig, Germany; M. Lummer, German Aerospace Center (DLR), Braunschweig, Germany Monday, 16 June 2014 44-ACD-3 Methods for Analysis and Design Under Uncertainty Embassy F Chaired by: R. MCDONALD, California Polytechnic State University-San Luis Obispo 1400 hrs 1600 hrs 1630 hrs 1700 hrs No Presentations AIAA-2014-2170 AIAA-2014-2171 AIAA-2014-2172 Facilitating Technology Quantifying Random Variable A Visualization Method for Development Progression Dependence Structure Through Multidisciplinary System under through Quantitative Uncertainty Copulas Theory for Probabilistic Uncertainty Assessments Assessment S. Ghosh, D. Rancourt, M. Daskilewicz, K. Gatian, D. Mavris, Georgia Institute of T. Zaidi, H. Jimenez, D. Mavris, Georgia C. Lee, D. Mavris, Georgia Institute of Technology, Atlanta, GA Institute of Technology, Atlanta, GA Technology, Atlanta, GA 52 Monday, 16 June 2014 45-MAO-3 Multidisciplinary Analysis and Optimization: Shape and Topology II Embassy G Chaired by: R. KOLONAY, US Air Force Research Lab 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs AIAA-2014-2173 AIAA-2014-2174 AIAA-2014-2175 AIAA-2014-2176 AIAA-2014-2177 A Numerical Optimization Study on Dimensional Design Space Preliminary Structural Design Design and Validation of a A non-probabilistic reliability-based Winglets Exploration of Expensive Functions Using Topology Optimization with a Supersonic Natural Laminar Flow topology optimization method S. Khosravi, D. Zingg, University of with Access to Gradient Comparison of Results from Gradient Test Article based on equivalent loads Toronto, Toronto, Canada S. Berguin, D. Mavris, Georgia Institute of and Genetic Algorithm Methods P. Sturdza, D. Rajnarayan, Aerion M. Li, W. Tang, Southeast University, Technology, Atlanta, GA A. Burt, M. Tinker, NASA Marshall Space Corporation, Reno, NV Nanjing, China Flight Center, Huntsville, AL Monday, 16 June 2014 46-MAO-4 Multidisciplinary Analysis and Optimization: Applications I Embassy H Chaired by: C. BLOEBAUM, University at Buffalo 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs AIAA-2014-2178 AIAA-2014-2179 AIAA-2014-2180 AIAA-2014-2181 AIAA-2014-2182 Conceptual Design of a Multi-Ability L-Dominance: An Approximate- Multidisciplinary Analysis with Visualization of System Non Deterministic Approach for Reconfigurable Unmanned Aerial Domination Mechanism for SORCER using Domain-Specific Decomposition in a Value-Based Advanced Aircraft Configuration Vehicle (UAV) through a Synergy Adaptive Resolution of Pareto Objects Framework Design under Uncertainty of 3D CAD and Modular Platform Frontiers S. Burton, American Optimization, LLC, E. Tibor, Iowa State University, Ames, P. Prakasha, T. Nam, C. Perullo, D. Planning B. Hancock, T. Nysetvold, C. Mattson, Liberty Township, OH; R. Kolonay, M. IA; S. Miller, G. Stump, Pennsylvania Mavris, Georgia Institute of Technology, S. Chowdhury, Mississippi State University, Brigham Young University, Provo, UT Sobolewski, Air Force Research Laboratory, State University, University Park, PA; Atlanta, GA Mississippi State, MS; V. Maldonado, Wright-Patterson AFB, OH C. Bloebaum, B. Mesmer, Iowa State University of Texas, San Antonio, San University, Ames, IA; T. Simpson, Antonio, TX; R. Patel, A&A Company, Pennsylvania State University, University South Plainfield, NJ Park, PA; et al. Monday, 16 June 2014 47-APA-11 Aerodynamic Testing: Flight, Wind Tunnel and Numerical Correlations I Fairlie Chaired by: J. PINIER, NASA-Langley Research Center and S. MORRIS, Engineering Systems, Inc. 1400 hrs 1430 hrs 1500 hrs 1530 hrs AIAA-2014-2183 AIAA-2014-2184 AIAA-2014-2185 AIAA-2014-2186 Compressible Boundary Empirical Correlation for Characteristic Analysis and Performance Investigation of a Layer Turbulence Transition Hypersonic Aerodynamic Heating Experimental Study of Tracer Supersonic Air Intake in Presence Measurements with In-depth in Open Cavity Geometries Under Particles for PIV in Supersonic Flows of Boundary Layer Bleed Thermocouples Rarefied Flow Conditions F. Chen, H. Liu, Shanghai Jiao Tong M. Soltani, J. Sepahi Younsi, A. Daliri, X. Zhao, X. Guo, China Academy of P. Stevens, Raytheon Company, Tucson, AZ University, Shanghai, China; Z. Yang, Sharif University of Technology, Tehran, Aerospace Aerodynamics, Beijing, China Wright State University, Dayton, OH Iran Monday, 16 June 2014 48-FD-5 High-Reynolds-Number Fluid Structure Interaction II (Invited) Greenbriar Chaired by: K. CASPER, Sandia National Laboratories and R. BOWERSOX, Texas A&M University 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs Oral Presentation Oral Presentation Oral Presentation Oral Presentation Oral Presentation Oral Presentation Open Discussion Experimental Design for Studying Interaction of a Mach 2.25 Turbulence modification using Fluid-Structure Interactions in Turbulence Response to Local Modeling of Compliant Panels Fluid-Structure Interactions during turbulent boundary layer with dynamic wall boundary conditions Compressible Cavity Flows Pressure Gradients at Mach 5 Subjected to Shock Impingement in Hypersonic Boundary-Layer elastic panels using direct S. Duvvuri, M. Luhar, B. McKeon, J. Wagner, K. Casper, S. Beresh, P. Hunter, R. Bowersox, Texas A&M University, High Speed Flow Transition numerical simulation California Institute of Technology, R. Spillers, J. Henfling, Sandia National College Station, TX A. Gogulapati, R. Deshmukh, A. Crowell, K. Casper, M. Mesh, S. Beresh, Sandia C. Ostoich, P. Geubelle, D. Bodony, Pasaden, CA Laboratories, Albuquerque, NM; et al. J. McNamara, Ohio State University, National Laboratories, Albuquerque, NM University of Illinois, Urbana-Champaign, Columbus, OH; V. Vyas, X. Wang, Arizona Urbana, IL State University, Tempe, AZ; et al.

53 Monday, 16 June 2014 49-AFM-3 Aeroservoelastic (ASE) Control, Modeling, Simulation, and Optimization II Hanover A Chaired by: M. BRENNER, NASA-Dryden Flight Research Center and P. CHENG, Boeing Defense, Space & Security 1400 hrs 1430 hrs 1500 hrs AIAA-2014-2187 AIAA-2014-2188 AIAA-2014-2189 Control strategies for an Model Predictive Control of a Fly-by-Feel Sensing and Control: experimental morphing wing Nonlinear Aeroelastic System Using Aeroservoelasticity model Reduced-Order Volterra Models A. Mangalam, Tao of Systems Integration, L. Grigorie, R. Botez, University of Québec, R. Prazenica, Embry-Riddle Aeronautical Inc., Hampton, VA; M. Brenner, NASA Dryden Montréal, Canada University, Daytona Beach, FL Flight Research Center, Edwards, CA Monday, 16 June 2014 50-AFM-4 Aerodynamic Prediction Methods Hanover A Chaired by: T. LAVIN, Sandia National Laboratories and M. COTTING, US Air Force Test Pilot School 1400 hrs 1530 hrs 1600 hrs No Presentations AIAA-2014-2191 AIAA-2014-2192 Control Performance, Aerodynamic Simulation of a Variety of Wings Modeling and Validation of Coupled using a Reynolds Stress Model Simulation Techniques for Guided K. Thompson, H. Hassan, North Carolina Projectile Roll Dynamics State University, Raleigh, NC J. Sahu, F. Fresconi, K. Heavey, Army Research Laboratory, Aberdeen Proving Ground, MD Monday, 16 June 2014 51-AFM-5 Aircraft Flight Dynamics, Handling Qualities, and Performance II Hanover B Chaired by: M. COTTING, US Air Force Test Pilot School and K. CUNNINGHAM, NASA-Langley Research Center 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2014-2193 AIAA-2014-2194 AIAA-2014-2195 AIAA-2014-2196 AIAA-2014-2197 AIAA-2014-2198 Measuring Aircraft Nonlinearity Toward a Flying Qualities Standard A voluntary/involuntary pilot Image-Based Target Tracking of Hybrid Wing Body Model Implementation of a Trajectory Across Aerodynamic Attitude for Unmanned Aircraft model for helicopter flight Observable Features in Precision Identification Using Forced- Prediction Function for Trajectory Flight Envelope-Revisited With K. Greene, D. Kunz, Air Force Institute of dynamics and aeroservoelasticity Projectiles Oscillation Water Tunnel Data Based Operations Symmetrized Aerodynamics Technology, Wright-Patterson AFB, OH; M. P. Masarati, G. Quaranta, Technical L. Fairfax, Army Research Laboratory, P. Murphy, D. Vicroy, NASA Langley J. Benavides, Stinger Ghaffarian Technologies, A. Abdallah, B. Newman, Old Dominion Cotting, U.S. Air Force Test Pilot School, University of Milan, Milan, Italy; A. Aberdeen Proving Ground, MD Research Center, Hampton, VA; B. Inc., Moffett Field, CA; J. Kaneshige, NASA University, Norfolk, VA; A. Omran, Fiat Edwards AFB, CA Bernardini, G. Guglieri, Technical University Kramer, M. Kerho, Rolling Hills Research Ames Research Center, Moffett Field, CA; S. Industrial, Chicago, IL of Turin, Turin, Italy Corporation, El Segundo, CA Sharma, Stinger Ghaffarian Technologies, Inc., Moffett Field, CA; R. Panda, SAIC, Moffett Field, CA; M. Steglinski, Stinger Ghaffarian Technologies, Inc., Moffett Field, CA Monday, 16 June 2014 52-ASE-3 Icing CFD Hanover C Chaired by: W. WRIGHT, ASRC Aerospace Corporation and R. AUBERT, Bell Helicopter Textron Inc. 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs AIAA-2014-2199 AIAA-2014-2200 AIAA-2014-2201 AIAA-2014-2202 AIAA-2014-2203 Glaciated and mixed phase ice Icing Analysis of a Swept NACA Robust Surface Evolution and Mesh Computational Aerodynamic Large Eddy Simulation of Airfoil Ice accretion modeling using ONERA 0012 Wing Using LEWICE3D Deformation for Three Dimensional Analysis of Three-dimensional Ice Accretion Aerodynamics 2D icing suite Version 3.48 Aircraft Icing Applications on a Shapes on a NACA 23012 Airfoil C. Brown, R. Kunz, M. Kinzel, J. Lindau, J. P. Villedieu, P. Trontin, R. Chauvin, ONERA, C. Bidwell, NASA Glenn Research Center, Swept GLC-305 Airfoil G. Jun, University of Michigan, Ann Arbor, Ann Palacios, K. Brentner, Pennsylvania State University, University Park, PA 54 Toulouse, France Cleveland, OH X. Tong, D. Thompson, Q. Arnoldus, Arbor, MI; D. Oliden, Arizona State University, E. Collins, E. Luke, Mississippi State Tempe, AZ; M. Potapczuk, NASA Glenn University, Starkville, MS Research Center, Cleveland, OH; J. Tsao, Ohio Aerospace Institute, Cleveland, OH Monday, 16 June 2014 53-ASE-4/FT-1 NASA Aviation Safety Technologies Hanover D Chaired by: R. NEECE, NASA Langley Research Center and D. MARTINEZ, NASA-Langley Research Center 1400 hrs 1430 hrs 1500 hrs 1530 hrs Oral Presentation Oral Presentation Oral Presentation AIAA-2014-3365 Convective Induced Turbulence Information Management for Laser Imaging Through Obscurants Investigation of Aircraft Detection via Total Lightning Airplane State Awareness: (LITO) (Invited) Weather Radars with Enhanced Sensing (Invited) Challenges and Solutions (Invited) E. Billmers, R. Billmers, RL Associates, Measurement Capabilities (Invited) J. Krozel, Innovation Laboratory, Inc., S. Young, T. Daniels, NASA Langley Inc., Yardley, PA A. Pazmany, ProSensing, Inc., Amherst, Portland, OR; W. Deierling, R. Sharman, J. Research Center, Hampton, VA MA Williams, National Center for Atmospheric Research, Boulder, CO Monday, 16 June 2014 54-MST-2 M&S: Flight Simulator Technologies Hanover G Chaired by: F. STEINLE 1400 hrs 1430 hrs 1500 hrs AIAA-2014-2204 AIAA-2014-2205 AIAA-2014-2206 The Six Pillars of Simulation Objective Motion Cueing Test - Transfer of Training on the Vertical Architecture Experiences of a New User Motion Simulator B. Evans, Lockheed Martin Corporation, C. Seehof, U. Durak, H. Duda, German P. Zaal, San Jose State University Research Marietta, GA Aerospace Center (DLR), Braunschweig, Foundation, San Jose, CA; J. Schroeder, Germany Federal Aviation Administration, Moffett Field, CA; W. Chung, AMERICAN SYSTEMS Corporation, Lexington Park, MD Monday, 16 June 2014 55-FD-6 Turbulence Modeling II Harris Chaired by: S. SPEER, Northrop Grumman Corporation 1400 hrs 1430 hrs 1500 hrs 1530 hrs AIAA-2014-2207 AIAA-2014-2208 AIAA-2014-2209 AIAA-2014-2210 Velocity/Pressure-Gradient A New Low Reynolds Number One- Wall-Modeled Large-Eddy Simulation of the FAITH Hill Correlations in a FORANS Approach Equation Turbulence Model Based Simulations of a Supersonic Experiment using a Reynolds Stress to Turbulence Modeling on a k-k-ω Closure Turbulent Flow in a Square Duct Model S. Poroseva, University of New Mexico, T. Wray, R. Agarwal, Washington Z. Vane, I. Bermejo-Moreno, S. Lele, J. Rodio, C. Patton, North Carolina State Albuquerque, Albuquerque, NM; S. Murman, University in St. Louis, St. Louis, MO Stanford University, Stanford, CA University, Raleigh, NC; X. Xiao, Corvid NASA Ames Research Center, Moffett Field, CA Technologies, Inc., Mooresville, NC; H. Hassan, North Carolina State University, Raleigh, NC

55 Monday, 16 June 2014 56-FD-7 Stability and Transition I Inman Chaired by: K. CASSEL, Illinois Institute of Technology and R. KIMMEL, USAF AFRL/RQHF 1400 hrs 1430 hrs 1500 hrs AIAA-2014-2211 AIAA-2014-2212 AIAA-2014-2213 Validations of a Local Correlation- Numerical Study of Boundary Localized Streak Instabilities in Based Transition Model Using an Layer Receptivity to Free-stream Pressure Gradient Boundary Layers Unstructured Grid CFD Solver Disturbances and Surface Excrescences P. Hack, T. Zaki, Imperial College London, J. Wang, C. Sheng, University of Toledo, A. Sescu, Mississippi State University, London, United Kingdom Toledo, OH Mississippi State, MS; M. Visbal, D. Rizzetta, Air Force Research Laboratory, Wright- Patterson AFB, OH Monday, 16 June 2014 57-FD-8 Ramjet and Scramjet Propulsion Systems II Kenneshaw Chaired by: L. MADDALENA, The University of Texas at Arlington 1400 hrs 1430 hrs AIAA-2014-2214 AIAA-2014-2215 Consideration for Optimization of Fuel Base Flow Characterization of Distribution in a Scramjet Engine Clustered Linear Aerospike Nozzles S. Sato, Japan Aerospace Exploration in the Presence of External Flow Agency (JAXA), Kakuda, Japan; F. H. Takahashi, T. Tomita, S. Tomioka, N. Masaaki, Space Service, Kakuda, Japan; T. Sakuranaka, Japan Aerospace Exploration Watanabe, T. Munakata, Hitachi Solutions Agency (JAXA), Kakuda, Japan East Japan, Ltd., Sendai, Japan Monday, 16 June 2014 58-HYTASP-1 Propulsion Cycle Performance-Scramjet Tests I Learning Center Chaired by: F. FALEMPIN, MBDA and M. BULMAN, Aerojet Rocketdyne Corporation 1400 hrs 1600 hrs 1630 hrs 1700 hrs No Presentations AIAA-2014-2216 AIAA-2014-2217 AIAA-2014-2218 Sizing of Solar Thermal Thruster for Scramjet Tests in the ONERA F4 Scramjet Powered Vehicle Tests in Satellite Orbital Control Using High Hotshot Wind Tunnel the ONERA F4 Hotshot Wind Tunnel. Thrust One Tangent Burn P. Viguier, J. Garraud, J. Soutade, ONERA, Comparison to Numerical Simulations M. Soliman, National Authority for Remote Mauzac, France; S. Defoort, A. Ristori, Y. M. Ferrier, S. Defoort, P. Viguier, J. Garraud, J. Sensing and Space Sciences, Cairo, Egypt Moule, ONERA, Palaiseau, France Soutade, ONERA, Palaiseau, France Monday, 16 June 2014 59-FC-5 Special Session: Mixing Layer Flow Control Lenox Chaired by: U. KAUL, NASA-Ames and J. LITTLE, The University of Arizona 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs AIAA-2014-2219 AIAA-2014-2220 AIAA-2014-2221 AIAA-2014-2222 AIAA-2014-2223 Closed-loop control of experimental Effects of Ns-DBD Plasma Actuators On Controlling The Flow In a Mixing First Principles Based PID Control Optimization of Perturbation shear flows using machine learning on Turbulent Shear Layers Layer or Wake Created Downstream of Mixing Layer: Role of Inflow Parameters for Simulated Free T. Duriez, V. Parezanovic, J. Laurentie, C. R. Lehmann, D. Akins, J. Little, University of a ‘Lambda’ Notch Simulating Perturbation Spectrum Shear Layer Flow Fourment, J. Delville, J. Bonnet, National of Arizona, Tucson, Tucson, AZ the Flow Downstream of a Chevron U. Kaul, NASA Ames Research Center, R. Martin, U. Kaul, NASA Ames Research Center for Scientific Research (CNRS), Nozzle or a Lambda Wing Moffett field, CA Center, Moffett field, CA Poitiers, France; et al. E. Suehiro, L. Taubert, N. Zalewski, I. Wygnanski, University of Arizona, Tucson, Tucson, AZ

56 Monday, 16 June 2014 60-ATIO-8 Special Session: Chinese Digital Avionics Marietta Chaired by: M. BALCHANOS 1400 hrs 1430 hrs 1500 hrs AIAA-2014-2224 AIAA-2014-2225 AIAA-2014-2226 Research on Integrated Avionics An Approach Based on Models to Model-based Safety Ananlysis for System Safety Methodology the Design for Integrated Modular Integrated Avionics System G. Wang, Chinese Aeronautical Radio Avionics Q. Gu, Chinese Aeronautical Radio Electronics Research Institute, Shanghai, J. Wu, Chinese Aeronautical Radio Electronics Electronics Research Institute, Shanghai, China Research Institute, Shanghai, China China Monday, 16 June 2014 61-AMT-3/GT-2 Spectroscopic Velocimetry Piedmont Chaired by: A. FAGAN, NASA Glenn Research Center and J. MICHAEL, Iowa State University 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs Oral Presentation AIAA-2014-2227 AIAA-2014-2228 AIAA-2014-2229 AIAA-2014-2230 AIAA-2014-2231 AIAA-2014-2232 Vibrationally excited NO tagging Femtosecond Laser Electronic Three Component Velocity and 2-D Velocity and Vorticity Planar Doppler Velocimetry for Diagnosis of High Speed Flows Planar Imaging of Shock Waves for simultaneous velocimetry and Excitation Tagging (FLEET) Acceleration Measurement Using Measurements with FLEET Transonic Flowfields in the AEDC using Filtered Rayleigh Scattering at Low Pressure using Filtered thermometry in gaseous high- Fundamental Pulse Energy and FLEET N. Calvert, A. Dogariu, R. Miles, Princeton 16T Wind Tunnel J. George, T. Jenkins, Metrolaser, Inc., Rayleigh Scattering speed flows (Invited) Spectral Response P. Danehy, B. Bathel, NASA Langley University, Princeton, NJ J. Wehrmeyer, K. Scott, F. Heltsley, R. Laguna Hills, CA; R. Miles, Princeton T. Jenkins, J. George, Metrolaser, Inc., R. Sanchez-Gonzalez, R. Bowersox, S. N. DeLuca, R. Miles, Princeton University, Research Center, Hampton, VA; N. Calvert, Porter, Aerospace Testing Alliance, Arnold University, Princeton, NJ Laguna Hills, CA; F. Poehlmann, Fluence, North, Texas A&M University, College Princeton, NJ; W. Kulatilaka, N. Jiang, A. Dogariu, R. Miles, Princeton University, AFB, TN LLC, Newark, CA Station, TX Spectral Energies, LLC, Dayton, OH; J. Princeton, NJ Gord, Air Force Research Laboratory, Wright-Patterson AFB, OH Monday, 16 June 2014 62-HYTASP-17 Global Reports II Regency Ballroom V 1400 - 1600 hrs Chaired by: A. SIEBENHAAR, Aerojet Rocketdyne Participants: Michael Smart Christian Mundt Mario Cosmo Masataka Maita Richard Brown Steve Walker Australia Germany Italy Japan UK US

Monday, 16 June 2014 63-PANEL-2 Panel: Transformative Aerospace System Analysis, Design and Certification: A Vision for CFD in 2030 Regency Ballroom VI 1400 - 1630 hrs Moderator: Robert D. Gregg III, Boeing Commercial Airplanes Chief Aerodynamicist, The Boeing Company Panelists: Wilson Felder Parviz Moin Stephen Morford Cord-Christian Rossow David Schuster Jeffrey P. Slotnick Distinguished Service Professor Franklin P. and Caroline M. Johnson Professor Chief Engineer, Systems Analysis and Aerodynamics Director, Institute of Aerodynamics and NASA Technical Fellow for Aerosciences Boeing Technical Fellow, Computational School of Systems and Enterprises Department of Mechanical Engineering Pratt & Whitney Flow Technology NASA Engineering and Safety Center Sciences & Aerodynamics Stevens Institute of Technology Stanford University German Aerospace Center (DLR) NASA Langley Research Center Boeing Research & Technology

Monday, 16 June 2014 64-PDL-5 Advanced Concepts and Advanced Computational Modeling of Plasmas and Lasers Roswell Chaired by: S. WU, The University of Alabama in Huntsville and M. PANESI, University of Illinois at Urbana Champaign 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 57 AIAA-2014-2233 AIAA-2014-2234 AIAA-2014-2235 AIAA-2014-2236 AIAA-2014-2238 Modeling of an Electric Propulsion Laser Space Communication Concept Modeling of Non-equilibrium Normal Glow Discharge with A Three - Dimensional Numerical System: Towards a Hybrid System for deep-space interplanetary missions Plasmas in an Inductively Coupled Axial Magnetic Field in Molecular Study of Supernova Remnant Type- A. Christou, M. Jugroot, Royal Military using CubeSats Plasma Facility Hydrogen IA Evolution in an Inhomogeneous College of Canada, Kingston, Canada A. Rajguru, University of Southern California, W. Zang, A. Lani, University of Illinois, S. Surzhikov, Russian Academy of Interstellar Medium Los Angeles, CA; N. Jerred, S. Howe, Center Urbana-Champaign, Urbana, IL; M. Panesi, Sciences, Moscow, Russia; J. Shang, S. Surzhikov, M. Ermishkin, Russian for Space Nuclear Research, Idaho Falls, ID; von Kármán Institute for Fluid Dynamics, Wright State University, Dayton, OH Academy of Sciences, Moscow, Russia A. Faler, University of Southern California, Los Rhode-Saint-Genèse, Belgium Angeles, CA Monday, 16 June 2014 65-PDL-4 Plasma and Laser Enhanced Combustion/Propulsion Spring Chaired by: K. KREMEYER, PM & AM Research and M. KIM, niversity of Adelaide 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs AIAA-2014-2239 AIAA-2014-2240 AIAA-2014-2241 AIAA-2014-2242 AIAA-2014-2243 AIAA-2014-2244 AIAA-2014-2245 Nanosecond Plasma Enhanced Effects of a microwave induced Influence of excited oxygen Spark Ignition Studies for Code Development to Determine Two dimensional OH radical Hydrogen and Ethane Plasma Ignition of Transverse Hydrogen argon plasma jet on premixed generated by a RF plasma discharge Supersonic Combustors the Temperature from the OH* measurements in argon plasma- Assisted Ignition by NS discharge Jet Injected into Supersonic Oxygen and nonpremixed methane/air on atmospheric partially- premixed S. Brieschenk, Z. Denman, A. Chemiluminescence Recordings in a assisted combustion flame of behind Reflected Shock Wave Crossflow mixtures CH4/O2 and H2/O2 flames Veeraravagan, V. Wheatley, M. Smart, Supersonic Combusting Flow premixed and nonpremixed A. Starikovskiy, Princeton University, S. Nagaraja, L. Zhang, V. Yang, Georgia C. Fuh, W. Wu, C. Wang, Mississippi State K. Zähringer, K. Pliavaka, D. Thévenin, University of Queensland, St. Lucia, T. Sopek, S. Brieschenk, P. Lorrain, methane/air mixtures using cavity Princeton, NJ Institute of Technology, Atlanta, GA University, Starkville, MS University of Magdeburg, Magdeburg, Australia T. Mcintyre, R. Boyce, University of ringdown spectroscopy Germany; N. Kuntner, U. Riedel, University Queensland, Brisbane, Australia W. Wu, C. Fuh, C. Wang, Mississippi State of Stuttgart, Stuttgart, Germany University, Starkville, MS Monday, 16 June 2014 66-TP-4 Ablation II Techwood Chaired by: A. MAZAHERI, NASA-Langley Research Center and D. KUNTZ, Sandia National Laboratories 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2014-2246 AIAA-2014-2247 AIAA-2014-2248 AIAA-2014-2249 AIAA-2014-2250 AIAA-2014-2251 Pyrolysis Gas Composition for a Microscale Simulations of Porous Photogrammetric Surface Analysis Numerical study of spallation Ablation Radiation Coupling Experimental Characterization of Phenolic Impregnated Carbon TPS Materials: Application to of Ablation Processes in High phenomenon in an arc-jet Investigation in Earth Re-entry Using Ablation Species in an Air Plasma Ablator Heatshield: From Virgin Permeability Enthalpy Air Plasma Flow environment Plasma Wind Tunnel Experiments Ablating Boundary Layer Resin toBoundary Layer E. Stern, I. Nompelis, T. Schwartzentruber, S. Loehle, T. Staebler, Institute of R. Davuluri, A. Martin, University of S. Loehle, T. Hermann, Institute of Space M. MacDonald, C. Laux, École Centrale de J. Rabinovitch, V. Marx, G. Blanquart, G. Candler, University of Minnesota, Space Systems, Stuttgart, Germany; T. Kentucky, Lexington, Lexington, KY Systems, Stuttgart, Germany; F. Zander, Paris, Châtenay-Malabry, France California Institute of Technology, Minneapolis, Minneapolis, MN Reimer, German Aerospace Center (DLR), Centre for Hypersonics, Brisbane, Australia; Pasadena, CA Stuttgart, Germany H. Fulge, T. Marynowski, Institute of Space Systems, Stuttgart, Germany Monday, 16 June 2014 67-TP-5 Combustion, Fire and Propulsion Heat Transfer University Chaired by: T. SHIH, Purdue University and O. EZEKOYE, The University of Texas at Austin 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs AIAA-2014-2252 AIAA-2014-2253 AIAA-2014-2254 AIAA-2014-2255 AIAA-2014-2256 AIAA-2014-2257 AIAA-2014-2258 Temperature Profile Inversion From Turbulent Combustion CFD Solver in Analysis of Wavelength Modulation Flow Investigation and Acoustic Sensitivity Analysis and Verification Secondary reactions of turbulent A Numerical Study of Wind Effect CO2 Spectral Intensities Through a Rule-Based Framework Using a Spectroscopy for Water Vapour Measurements of a Turbulent Jet of a 1-D Surface Solid Combustion reacting flows over a film-cooled on Wood Chipboard with a Gasoline Levenberg-Marquardt Optimization Variable Pressure Flamelet Model Measurements in Supersonic Flame Model for a Fire CFD Boundary surface using OpenFOAM Fire in a Compartment and Tikhonov Regularization S. Thakur, Streamline Numerics, Inc., Combustion H. Nawroth, C. Paschereit, Technical Condition E. Ghasemi, S. Soleimani, C. Lin, Florida N. Cai, W. Chow, Hong Kong Polytechnic T. Ren, M. Modest, University of California, Gainesville, FL H. Fulge, S. Loehle, S. Fasoulas, University of Berlin, Berlin, Germany A. Brown, D. Glaze, F. Pierce, Sandia International University, Miami, FL University, Hong Kong, Hong Kong Merced, Merced, CA University of Stuttgart, Stuttgart, Germany National Laboratories, Albuquerque, NM 58 Monday, 16 June 2014 68-TP-6 Theoretical, Analytical and Computational Heat Transfer I Vinings Chaired by: G. WALKER, Vanderbilt University and O. KORNBERG, Mode Technology Group 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs AIAA-2014-2259 AIAA-2014-2260 AIAA-2014-2261 AIAA-2014-2262 AIAA-2014-2263 Bubble Growth in Flow Boiling on The unified nondiffusive-diffusive Investigation of the Melting Analytical/Numerical Study of Heat Two- and Three-Dimensional Heat an Uneven Wall model for phonon transport Behaviour of Ice Particles in an Transfer across a Single Infinite Transfer over a Wavy Wall H. Shmueli, G. Ziskind, R. Letan, Ben- applied to the transient gratings Acoustic Levitator Longitudinal Row of Circular Cylinders H. Shmueli, G. Ziskind, R. Letan, Ben- Gurion University of the Negev, Beer- experiment T. Hauk, EADS, Munich, Germany; I. O. Khan, Tuskegee University, Tuskegee, Gurion University of the Negev, Beer- Sheva, Israel A. Ramu, Y. Ma, University of California, Roisman, C. Tropea, Technical University of AL; W. Khan, National University of Sheva, Israel Merced, Merced, CA Darmstadt, Darmstadt, Germany Sciences and Technology, Karachi, Pakistan Monday, 16 June 2014 69-NW-2 Monday Afternoon Networking Coffee Break Meeting Room Foyers 1530 - 1600 hrs Monday, 16 June 2014 70-HYTASP-18 Fluid Analysis Panel Regency Ballroom V 1600 - 1700 hrs This panel is a discussion of the different perspectives (government, academia, industry) on CFD. Panelists: Graham Candler Aaron Auslender Bob Moehlenkamp Laurent Serre Vince Wheatley US US US ONERA Australia Monday, 16 June 2014 71-APA-13 Low Reynolds Number Aerodynamics Discussion Panel Edgewood 1630 - 1730 hrs Moderator: Ming Chang, Lockheed Martin Corporation

The topic of Low Reynolds Number Aerodynamics and Experimental Methods has been flourishing since the 90’s with sporadic advances in computational, analytical and experimental methods that has collectively percolated into unique micro vehicle demonstrations. Many of these have been from academia with industry developing niche applications that have become novelty items. This panel seeks to open a discussion forum with researchers, users and developers in this community to exchange scientific and engineering ideas, technical progress and path forward for micro vehicle research and application. Panelists: Michael Ol Anya Jones Dennis Finley Michael Selig Air Force Research Laboratory University of Maryland Lockheed Martin Aeronautics University of Illinois, Urbana-Champaign

Monday, 16 June 2014 72-LEC-1 Fluid Dynamics Award Lecture: Mixing in Turbulent Combustion: Physics and Computational Challenges Regency Ballroom VII 1730 - 1830 hrs Paul E. Dimotakis John K. Northrop Professor of Aeronautics and Professor of Applied Physics California Institute of Technology Pasadena, California Tuesday Tuesday, 17 June 2014

59 73-NW-3 Tuesday Morning Networking Breakfast Ballroom Level 0700 - 0800 hrs Tuesday, 17 June 2014 74-SB-2 Tuesday Morning Speakers’ Briefing Session Rooms 0730 - 0800 hrs Tuesday, 17 June 2014 75-PLNRY-2 Tuesday Morning Plenary Panel Centennial I/II 0800 - 0900 hrs Moderator: Ben Iannotta, Editor-in-Chief, Aerospace America Integration and Interoperability: Fly Smarter, Fly Cleaner, Fly Safer Panelists: Peter Cerda Allan McArtor Tony Ng Steve Kong Senior Vice President, The Americas Chairman and CEO Lockheed Martin Fellow Business and Technical Development Manager International Air Transport Association AIRBUS Group, Inc. Lockheed Martin Inmarsat Aviation

Tuesday, 17 June 2014 76-NW-4 Tuesday Morning Networking Coffee Break Exhibit Hall 0900 - 0930 hrs Tuesday, 17 June 2014 77-APA-14 Special Session: NATO Task Group AVT-201 III - CFD Prediction and Real Scale Analyses Baker Chaired by: D. VICROY, NASA-Langley Research Center and J. IRVING, BAE Systems 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2014-2264 AIAA-2014-2265 AIAA-2014-2266 AIAA-2014-2267 Static and Dynamic Simulations of Validation of Unsteady Aerodynamic Analysis of the transonic Model Scale and “Real” Flight a Generic UCAV Geometry Using Models of a Generic UCAV Using flow around a generic UCAV of Generic UCAV and Advanced the Kestrel Flow Solver Overset Grids configuration Combat Aircraft - An Industrial A. Lofthouse, M. Ghoreyshi, A. Jirasek, M. Ghoreyshi, A. Jirasek, R. Cummings, U.S. D. Zimper, German Aerospace Center Perspective R. Cummings, U.S. Air Force Academy, Air Force Academy, Colorado Springs, CO; (DLR), Cologne, Germany; D. Hummel, S. Hitzel, EADS, Manching, Germany; D. Colorado Springs, CO A. Da Ronch, University of Southampton, Technical University of Braunschweig, Zimper, German Air Force, Bonn, Germany Southampton, United Kingdom; M. Young, Braunschweig, Germany Defence Science and Technology Organisation, Fishermans Bend, Australia Tuesday, 17 June 2014 78-APA-15 Special Session: Sonic Boom Activities III Courtland Chaired by: L. OZOROSKI, NASA Langley Research Center 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs Oral Presentation AIAA-2014-2268 AIAA-2014-2269 Oral Presentation AIAA-2014-2270 AIAA-2014-2271 Comparison of sonic boom A Flight Research Overview of Full-Field Sonic Boom Simulation in A Method for Reducing Sonic Boom USM3D predictions of Supersonic Application of adjoint methodology propagation and loudness level WSPR, a Pilot Project for Sonic Real Atmosphere Strength by Tailoring the Shape of Nozzle Flow in various aspects of sonic boom calculations Boom Community Response R. Yamashita, K. Suzuki, University of the Propulsive Streamtube M. Carter, NASA Langley Research Center, design A. Loubeau, NASA Langley Research Center, L. Cliatt, E. Haering, T. Jones, E. Tokyo, Kashiwa, Japan T. Conners, Gulfstream Aerospace Hampton, VA; S. Nayani, Analytical S. Rallabhandi, National Institute of Hampton, VA; S. Rallabhandi, National Waggoner, A. Flattery, NASA Dryden Flight Corporation, Savannah, GA Services and Materials, Inc., Hampton, VA; Aerospace, Hampton, VA A. Elmiligui, R. Campbell, NASA Langley

60 Institute of Aerospace, Hampton, VA Research Center, Edwards, CA; S. Wiley, TYBRIN Corporation, Edwards, CA Research Center, Hampton, VA Tuesday, 17 June 2014 79-APA-16 Aerodynamics of Unmanned Aerial Vehicles I Dunwoody Chaired by: M. OL, Air Force Reseach Laboratory and Z. YANG, Wright State University 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2014-2272 AIAA-2014-2273 AIAA-2014-2277 AIAA-2014-2275 AIAA-2014-2276 AIAA-2014-2274 Development of an unmanned Experimental Optimization of a Is Flapping Flight Aerodynamically Computational Modeling of the A Pressure Disk Model for Modeling Numerical optimization of the aerial vehicle UAV for air quality Free-to-Rotate Wing for Small UAS Efficient? Aerodynamics and Flight Mechanics Installed Propeller Performance and S4 Éhecatl UAS airfoil using a measurement in urban areas M. Logan, R. Deloach, NASA Langley M. Nabawy, W. Crowther, University of of Maneuvers of UAV Induced by Effects on Unmanned Aircraft Systems morphing wing approach P. Haas, C. Balistreri, P. Pontelandolfo, G. Research Center, Hampton, VA Manchester, Manchester, United Kingdom Variable-Incidence Wings W. Coirier, M. Brown, Kratos/Digital Fusion, S. Oliviu, A. Simon, A. Koreanschi, R. Triscone, Hepia, Geneva, Switzerland; H. V. Dwivedi, M. Damodaran, Indian Inc., Huntsville, AL; Z. Hall, M. McDaniel, Army Botez, École de Technologie Supérieure, Pekoz, Pierre and Marie Curie University, Institute of Technology Gandhinagar, Aviation and Missile Research Development Montréal, Canada Paris, France; A. Pignatiello, University of Ahmedabad, India and Engineering Center, Huntsville, AL Bologna, Bologna, Italy Tuesday, 17 June 2014 80-APA-17 Wind Turbine Aerodynamics I Edgewood Chaired by: E. FELTROP, The Cessna Aircraft Company 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2014-2278 AIAA-2014-2279 AIAA-2014-2280 AIAA-2014-2281 AIAA-2014-2282 High-Fidelity Computational Wake Flow Simulations for a Mid- Investigation of Rotor Models for RANS Simulations of Sandia 100-m A Comparative Study of the Wake Simulation of the Interaction Sized Rim Driven Wind Turbine Wind Turbine Simulations Wind Turbine Blade: Effect of Leading- Characteristics behind a Single- between Tandem Wind Turbines A. Porteous, B. Kaiser, S. Poroseva, A. Mittal, K. Sreenivas, L. Taylor, L. Edge Tubercles and Slotted Tips Rotor Wind Turbine and Dual-Rotor K. Sreenivas, A. Mittal, L. Hereth, L. University of New Mexico, Albuquerque, Hereth, C. Hilbert, D. Hyams, University of T. Reinhart, S. Medida, T. Kalra, J. Baeder, Wind Turbines Taylor, C. Hilbert, University of Tennessee, Albuquerque, NM; C. Bond, University of Tennessee, Chattanooga, Chattanooga, TN University of Maryland, College Park, A. Ozbay, W. Tian, H. Hu, Iowa State Chattanooga, Chattanooga, TN Texas, Austin, Austin, TX; R. Hovsapian, College Park, MD University, Ames, IA Idaho National Laboratory, Idaho Falls, ID Tuesday, 17 June 2014 81-ATIO-5 Transformational Flight: Technical Gaps, Prizes, and Private-Public Partnerships Embassy C 0930 - 1130 hrs Chaired by: B. GERMAN, Georgia Institute of Technology Moderator: Brian German, Georgia Institute of Technology Panelists: Eric Allison Mark Moore Bruce Holmes Zee Aero NASA Langley NextGen Aeronautics

Tuesday, 17 June 2014 82-ATIO-6 UAS Integration & Operations I Embassy D Chaired by: V. SCHULTZ, NASA Langley Research Center and A. DESHMUKH, Gulfstream Aerospace Corp. 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2014-2283 AIAA-2014-2284 AIAA-2014-2285 AIAA-2014-2286 AIAA-2014-2287 AIAA-2014-2288 An Evaluation Framework for A Method for Risk Estimation Unmanned Aerial System (UAS) Building the Safety Case for UAS Autonomous Control of Uninhabited Exploration of the Trade Space Unmanned Aircraft Systems Analysis for Unmanned Aerial Safety Analysis Model Operations in Support of Natural Combat Air Vehicles in Heavily- Between Unmanned Aircraft Integration in the National Airspace System Operation over Populated V. Kumar, Intelligent Automation, Inc., Disaster Response Trafficked Military Airspace Systems Descent Maneuver System Areas Rockville, MD; S. Toussaint, Coherent B. Williams, Queensland University of K. Smith, R. Stengel, Princeton University, Performance and Sense-and Avoid J. Domercant, O. Pinon-Fischer, N. Knisely, J. Lazatin, California Polytechnic State Technical Services, Inc., Lexington Park, Technology, Brisbane, Australia; R. Clothier, Princeton, NJ System Performance Requirements D. Mavris, Georgia Institute of Technology, University, San Luis Obispo, CA MD; J. Luxhoj, Luxhoj Consulting and RMIT University, Melbourne, Australia; D. Jack, K. Hoffler, Adaptive Aerospace Atlanta, GA Research, LLC, Somerset, NJ; F. Wieland, N. Fulton, Commonwealth Scientific and Group, Inc., Hampton, VA Intelligent Automation, Inc., Rockville, MD Industrial Research Organisation (CSIRO), Canberra, Australia; S. Johnson, Queensland University of Technology, Brisbane, Australia;

61 X. Lin, Commonwealth Scientific and Industrial Research Organisation (CSIRO), Canberra, Australia; K. Cox, The Boeing Company, Brisbane, Australia Tuesday, 17 June 2014 83-ATIO-7 ATM-III Air/Ground Trajectory Enhancements Embassy E Chaired by: J. MARIS, Marinvent Corporation 0930 hrs 1000 hrs 1030 hrs AIAA-2014-2289 AIAA-2014-2290 AIAA-2014-2291 Three-Dimensional Trajectory Air to Ground Trajectory Construction of an aircraft’s Design for Reducing Climate Impact Synchronisation through Extended VNAV flight envelope for in-FMS of Trans-Atlantic Flights Predicted Profile: A Pilot Study flight trajectory computation and H. Ng, University of California, Santa J. Bronsvoort, G. McDonald, Airservices optimization: Application on the Cruz, Moffett Field, CA; B. Sridhar, N. Australia, Melbourne, Australia; J. Airbus A310 Chen, NASA Ames Research Center, Hochwarth, General Electric Company, B. Dancila, R. Botez, École de Technologie Moffett Field, CA; J. Li, Stinger Ghaffarian Grand Rapids, MI; E. Gallo, The Boeing Supérieure, Montréal, Canada Technologies, Inc., Moffett Field, CA Company, Madrid, Spain Tuesday, 17 June 2014 84-ACD-4 Structural Analysis, Design, and Optimization of Aircraft Embassy F Chaired by: W. CROSSLEY, Purdue University 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2014-2292 AIAA-2014-2293 AIAA-2014-2294 AIAA-2014-2295 AIAA-2014-2296 Preliminary Aero-thermal Fatigue Behaviour of Unitized Structural Design Optimisation Structural Optimization of The Conceptual Structural Design of Structural Simulation Structures Compared to Built-up and Aerothermoelastic Analysis of Composite Wings in an automated an Unmanned Space Vehicle with C. Pasiliao, M. Sytsma, Air Force Research Structures LAPCAT A2 Mach 5 Cruise Vehicle Multi-Disciplinary Environment Re-entry and Landing Capabilities Laboratory, Eglin AFB, FL; L. Neergaard, M. Patel, C. Bil, G. Clark, RMIT University, S. Sharifzadeh, P. Hendrick, Université T. Bach, L. Heinrich, S. Dähne, C. N. Paletta, M. Belardo, D. Lucariello, M. Z. Witeof, Leidos, Eglin AFB, FL; J. Trolier, Melbourne, Australia Libre de Bruxelles, Brussels, Belgium; Huehne, German Aerospace Center (DLR), De Stefano Fumo, U. Mercurio, Italian Leidos, King of Prussia, PA S. D’Mello, D. Verstraete, University of Braunschweig, Germany Aerospace Research Center (CIRA), Sydney, Sydney, Australia; F. Thirifay, Capua, Italy Cenaero, Gosselies, Belgium Tuesday, 17 June 2014 85-MAO-5 Multidisciplinary Analysis and Optimization: Shape and Topology III Embassy G Chaired by: V. TOROPOV, Queen Mary, University of London 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2014-2297 AIAA-2014-2298 AIAA-2014-2299 AIAA-2014-2300 New Projection Methods for Two-Phase Discrete Adjoint Method for Aerodynamic Sensitivity Analysis An Unsteady Continuous Adjoint Minimum and Maximum Length Scale Aeroelastic Design Optimization based on Modified Navier-Stokes Approach for Aerodynamic Design Control in Topology Optimization J. Thomas, E. Dowell, Duke University, Equations on Dynamic Meshes J. Carstensen, J. Guest, Johns Hopkins Durham, NC K. Gobal, R. Grandhi, Wright State T. Economon, F. Palacios, J. Alonso, University, Baltimore, MD University, Dayton, OH Stanford University, Stanford, CA

62 Tuesday, 17 June 2014 86-MAO-6 Multidisciplinary Analysis and Optimization: Metamodeling I Embassy H Chaired by: E. WINER, Iowa State University 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2014-2301 AIAA-2014-2302 AIAA-2014-2303 AIAA-2014-2304 AIAA-2014-2305 Surrogate Models and Mixtures of Optimization when Cost of Reducing Error of Polynomial Aero-Structure-Stealth Coupled RBF Metamodel Assisted Global Experts in Aerodynamic Performance Optimization is Comparable to the Approximation Outside of Optimization for High Aspect Ratio Optimization Method Using Particle Prediction for Mission Analysis Objective Function Designated Design Space for Wing Using Adaptive Metamodeling Swarm Evolution and Fuzzy R. Liem, University of Toronto, Toronto, A. Chaudhuri, R. Haftka, University of Practical Problems Method Clustering for Sequential Sampling Canada; J. Martins, University of Michigan, Florida, Gainesville, Gainesville, FL V. Balabanov, O. Weckner, J. Wu, The D. Wu, T. Long, Y. Li, M. Jiang, B. Huang, G. Xiaosong, T. Long, D. Wu, Z. Wang, L. Liu, Ann Arbor, Ann Arbor, MI Boeing Company, Seattle, WA Beijing Institute of Technology, Beijing, China Beijing Institute of Technology, Beijing, China Tuesday, 17 June 2014 87-APA-18 Aerodynamic Testing: Flight, Wind Tunnel and Numerical Correlations II Fairlie Chaired by: G. GATLIN and T. DOUVILLE, TLG Aerospace, LLC. 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2014-2306 AIAA-2014-2307 AIAA-2014-2308 AIAA-2014-2309 Experimental Investigation of Experimental Study of Circulation Experimental investigation of Experimental Study on Quasi- Periodic Wind Gust Generated in a Control Wings at Low Reynolds propeller induced ground vortex Limit-Cycle Wing Rock of a Chined Low Speed Wind Tunnel Numbers under headwind condition Forebody Configuration at High P. Deshpande, National Aerospace K. Kanistras, M. Rutherford, N. Vitzilaios, Y. Yang, A. Sciacchitano, L. Veldhuis, G. Angle of Attack Laboratories, Bangalore, India; S. Singh, K. Valavanis, University of Denver, Eitelberg, Delft University of Technology, W. Shi, D. Xueying, Y. Wang, Q. Li, Birla Institute of Technology, Ranchi, India; P. Denver, CO Delft, The Netherlands Beihang University, Beijing, China Narayanan, Naltech Private, Ltd., Bangalore, India; D. Babu, B. Sundaramoorthy, National Aerospace Laboratories, Bangalore, India Tuesday, 17 June 2014 88-FD-9 Fluid Structure Interaction I Greenbriar Chaired by: S. SILTON, US Army Research Laboratory 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2014-2310 AIAA-2014-2311 AIAA-2014-2312 AIAA-2014-2313 AIAA-2014-2314 Prediction of Transonic LCO using Effects of Flexible Wings in Hover An ALE Based Hybrid Meshfree Numerical Simulations of Streamwise- Velocity Measurements behind a an Harmonic Balance Method Flight at Fruit Fly Scale Local RBF-Cartesian FD scheme for Oriented Vortex/Flexible Wing Flexible Fence W. Yao, S. Marques, Queen’s University M. Sridhar, C. Kang, University of Incompressible flow around moving Interactions J. Seidel, T. McLaughlin, U.S. Air Force Belfast, Belfast, United Kingdom Alabama, Huntsville, Huntsville, AL boundaries C. Barnes, M. Visbal, Air Force Research Academy, Colorado Springs, CO A. Javed, K. Djidjeli, J. Xing, Z. Sun, Laboratory, Wright-Patterson AFB, OH; G. University of Southampton, Southampton, Huang, Wright State University, Dayton, OH United Kingdom Tuesday, 17 June 2014 89-AA-2 CAA Numerical Techniques I Hanover A Chaired by: D. CASALINO, EXA GmbH 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2014-2315 AIAA-2014-2316 AIAA-2014-2317 AIAA-2014-2318 AIAA-2014-2319 Performance improvements and Enhancing the Resolution A Fast GPU Based Bidiagonal Solver Adjoint Linearised Euler solver for Comparison of LES and Stochastic new solution strategies of Actran/ Characteristics of Aeroacoustic for Computational Aeroacoustics Goldstein acoustic analogy equations Source Generation Methods for TM for nacelle simulations Time-Reversal Using a Point-Time- S. Miao, X. Zhang, O. Parchment, for 3D non-uniform flow sound Aero- and Hydro-Acoustic Design B. Van Antwerpen, Y. Detandt, D. Reversal-Sponge-Layer X. Chen, University of Southampton, scattering problems: verification and Guidance Copiello, E. Rosseel, E. Gaudry, Free Field A. Mimani, C. Doolan, P. Medwell, Southampton, United Kingdom capability study M. Allan, O. Darbyshire, BAE Systems, Technologies, Mont-Saint-Guibert, Belgium University of Adelaide, Adelaide, Australia V. Semiletov, S. Karabasov, Queen Mary, Bristol, United Kingdom University of London, London, United Kingdom 63 Tuesday, 17 June 2014 90-AA-3 Leading Edge Noise Hanover B Chaired by: N. PEAKE, University of Cambridge 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2014-2320 AIAA-2014-2321 AIAA-2014-2322 AIAA-2014-2323 AIAA-2014-2324 AIAA-2014-2325 Noise Reduction Studies from the Reduced Dimension Modeling of An analytic approach to high- A Boundary Element Method Direct numerical simulation of 3D calculations of aerofoil- Leading Edge of Serrated Flat Leading Edge Turbulent Interaction frequency gust-aerofoil interaction iterative procedure to compute the acoustic reduction using serrated turbulence interaction noise and Plates Noise noise in steady shear flows compressible response of an airfoil trailing-edge on an isolated airfoil the effect of wavy leading edges S. Narayanan, P. Joseph, S. Haeri, J. Kim, J. Gill, X. Zhang, P. Joseph, University L. Ayton, N. Peake, University of subjected to incoming turbulence M. Sanjose, C. Meon, S. Moreau, A. S. Haeri, J. Kim, S. Narayanan, P. Joseph, University of Southampton, Southampton, of Southampton, Southampton, United Cambridge, Cambridge, United Kingdom L. de Santana, C. Schram, von Kármán Idier, P. Laffay, University of Sherbrooke, University of Southampton, Southampton, United Kingdom Kingdom; T. Node-Langlois, Airbus, Institute for Fluid Dynamics, Rhode-Saint- Sherbrooke, Canada United Kingdom Toulouse, France Genèse, Belgium; W. Desmet, Catholic University of Leuven, Leuven, Belgium Tuesday, 17 June 2014 91-ASE-5 Icing Physics Hanover C Chaired by: R. MOSER, AeroTex UK and K. AL-KHALIL, Cox & Company, Inc. 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2014-2326 AIAA-2014-2327 AIAA-2014-2328 AIAA-2014-2329 AIAA-2014-2330 AIAA-2014-2331 An Experimental Study of Wind- On the Numerical Solution of Effects of Surface Characteristics Time-Resolved Temperature Ice Roughness in Short Duration A Thermal Analysis of a Hot-Wire Driven Water Film Flows over Three-Dimensional Condensed and Droplet Diameter on the Distribution of Icing Process of SLD Icing Events Probe for Icing Applications Roughness Array Layer Films Freezing of Supercooled Water Supercooled Water in Microscopic S. McClain, D. Reed, Baylor University, P. Struk, NASA Glenn Research Center, K. Zhang, Y. Liu, A. Rothmayer, H. Hu, A. Rothmayer, H. Hu, Iowa State Droplets Impacting a Cooled Scale Waco, TX; M. Vargas, R. Kreeger, NASA Cleveland, OH; D. Rigby, Vantage Partners Iowa State University, Ames, IA University, Ames, IA Substrate M. Tanaka, Kanagawa Institute of Technology, Glenn Research Center, Cleveland, OH; J. LLC, Cleveland, OH; K. Venkataraman, J. Blake, D. Thompson, Mississippi State Kanagawa, Japan; M. Katuaki, Japan Tsao, Ohio Aerospace Institute, Cleveland, University of Texas, Austin, Austin, TX University, Mississippi State, MS; D. Raps, Aerospace Exploration Agency (JAXA), Tokyo, OH Eurocopter Deutschland, Donauworth, Japan; S. Kimura, Kanagawa Institute of Germany; T. Strobl, EADS, Munich, Technology, Kanagawa, Japan; H. Sakaue, Germany; E. Bonaccurso, Airbus Group Japan Aerospace Exploration Agency (JAXA), Innovations, Munich, Germany Tokyo, Japan Tuesday, 17 June 2014 92-ASE-6/AFM-6/FT-2 Managing Wake Vortex Encounter I Hanover D Chaired by: A. BROWN, National Research Council Canada and F. PROCTOR, NASA Langley Research Center 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2014-2332 AIAA-2014-2333 AIAA-2014-2334 AIAA-2014-2335 AIAA-2014-2336 AIAA-2014-2337 ATM Decision Support Tool for In-Flight Wake Encounter Prediction Investigation of Encounters Topological Approach to Multisensory In-Flight Testing of Airborne The Alleviation of Wake Vortex Wake Vortex Hazard Management with the Wake Encounter Avoidance with Deformed Wake Vortices Realization of Wake Turbulence LIDAR for Wake Vortex Detection, Encounter Loads, A Study of Flight Combining Sensors and Modeling and Advisory System using a Monte-Carlo Simulation Y. Takeshima, T. Misaka, S. Obayashi, Tohoku Characterization and Tracking Research Data

64 L. Mutuel, Thales Group, Seattle, WA; F. T. Bauer, D. Vechtel, F. Abdelmoula, T. Methodology University, Sendai, Japan; H. Kato, Japan M. Steen, M. Stanisak, T. Feuerle, A. Brown, National Research Council Barbaresco, P. Juge, M. Klein, D. Canal, Y. Immisch, German Aerospace Center (DLR), D. Bieniek, R. Luckner, Technical University Aerospace Exploration Agency (JAXA), Chofu, P. Hecker, Technical University of Canada, Ottawa, Canada Ricci, Thales Group, Limours, France; et al. Braunschweig, Germany of Berlin, Berlin, Germany Japan; S. Takahashi, University of Tokyo, Braunschweig, Braunschweig, Germany Kashiwa, Japan; I. Fujishiro, Keio University, Yokohama, Japan Tuesday, 17 June 2014 93-AA-4 Jet Noise Near Field I Hanover E Chaired by: S. REDONNET, ONERA 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2014-2338 AIAA-2014-2339 AIAA-2014-2340 AIAA-2014-2341 AIAA-2014-2342 On the Scaling of Jet Noise with On Coherence of Jet Noise Time-dependent prediction of the The Prediction of Noise due to Jet Decomposition of the Near-field Helmholtz Number Close to the K. Ahuja, Georgia Institute of Technology, unsteady pressure near-field from Turbulence Convecting past Flight Pressure in a Forced Subsonic Jet Jet Axis Atlanta, GA; D. Nance, Jacobs, Huntsville, an under-expanded jet Vehicle Trailing Edges M. Crawley, M. Samimy, Ohio State U. Michel, CFD Software GmbH, Berlin, AL; J. Carrigan, Georgia Institute of A. Rona, D. Di Stefano, A. Mancini, E. S. Miller, NASA Langley Research Center, University, Columbus, OH Germany; K. Ahuja, Georgia Institute of Technology, Atlanta, GA Hall, University of Leicester, Leicester, Hampton, VA Technology, Atlanta, GA United Kingdom Tuesday, 17 June 2014 94-AA-5 Hybrid Wing Body Aeroacoustics Test I Hanover F Chaired by: C. WHITFIELD, NASA-Langley Research Center 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs Oral Presentation AIAA-2014-2343 AIAA-2014-2344 AIAA-2014-2345 AIAA-2014-2346 Overview of the Hybrid Wing Body Development of a Microphone Calibrations of the NASA Langley Acoustic Data Processing and Shielding Characteristics using an Aeroacoustics Test in NASA Langley Phased Array Capability for the 14- by 22-Foot Subsonic Tunnel in Transient Signal Analysis for the Ultrasonic Configurable Artificial 14 by 22 Foot Wind Tunnel Langley 14- by 22-foot Subsonic Acoustic Configuration Hybrid Wing Body 14- by 22-Foot Noise Source to Generate Modes - T. Brooks, F. Hutcheson, M. Doty, W. Tunnel T. Spalt, T. Brooks, C. Bahr, NASA Langley Subsonic Wind Tunnel Test Experimental Measurements and Humphreys, S. Heath, C. Burley, NASA W. Humphreys, T. Brooks, C. Bahr, T. Research Center, Hampton, VA; L. Becker, C. Bahr, T. Brooks, W. Humphreys, T. Analytical Predictions Langley Research Center, Hampton, VA; Spalt, S. Bartram, W. Culliton, NASA D. Stead, Northrop Grumman Corporation, Spalt, NASA Langley Research Center, D. Sutliff, NASA Glenn Research Center, et al. Langley Research Center, Hampton, VA; Hampton, VA; G. Plassman, NASA Langley Hampton, VA; D. Stead, Northrop Cleveland, OH; B. Walker, Channel Islands et al. Research Center, Hampton, VA Grumman Corporation, Hampton, VA Acoustics, Camarillo, CA Tuesday, 17 June 2014 95-MST-3 M&S: Tools and Technologies Hanover G Chaired by: F. CARDULLO, State University of NY 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2014-2347 AIAA-2014-2348 AIAA-2014-2349 AIAA-2014-2350 AIAA-2014-2351 Analysis, Modeling and Simulation Methodology for Runway-Level DNL User Interface Validation using Stochastic Spatial Wind Field Right Ways to Use Flight Simulators of NextGen Trajectory-Based Contour Calibration in ANGIM to Mode Confusion Detection Simulation using a Potential Field M. Cevik, Turkish Air Force Air War Operations Capture Impacts of Deviation from J. Suraj Nandiganahalli, S. Lee, I. Hwang, M. Rhudy, Lafayette College, Easton, PA College, Istanbul, Turkey H. Powell, E. Elsayed, Rutgers University, Standard Day Sea-Level Atmosphere Purdue University, West Lafayette, IN; New Brunswick, NJ; C. Falk, D. M. LeVine, R. Moss, M. Kirby, D. Mavris, B. Yang, Optimal Synthesis, Inc., Los Livingston, Y. Ebrahimi, Federal Aviation Georgia Institute of Technology, Atlanta, GA Altos, CA

65 Administration, Atlantic City, NJ Tuesday, 17 June 2014 96-FD-10 Hypersonic Boundary Layer Transition I Inman Chaired by: M. BORG, Air Force Research Laboratory and H. JOHNSON, University of Minnesota 0930 hrs 1000 hrs 1030 hrs AIAA-2014-2352 AIAA-2014-2353 AIAA-2014-2354 Interaction of Acoustic and Entropy Numerical and experimental Numerical Investigation of Waves with Shocks investigation of laminar-turbulent Unsteady Heat Transfer on a T. Schilden, W. Schroeder, RWTH Aachen boundary layer transition on a blunt Double Wedge Geometry in University, Aachen, Germany; S. Ali, generic re-entry capsule Hypervelocity Flows R. Radespiel, Technical University of A. Theiss, German Aerospace Center (DLR), J. Komives, I. Nompelis, G. Candler, Braunschweig, Braunschweig, Germany Göttingen, Germany; S. Ali, Technical University of Minnesota, Minneapolis, University of Brunswick, Brunswick, Germany; Minneapolis, MN S. Hein, German Aerospace Center (DLR), Göttingen, Germany; D. Heitmann, R. Radespiel, Technical University of Brunswick, Brunswick, Germany Tuesday, 17 June 2014 97-PDL-7 Aero-Optics I Kenneshaw Chaired by: M. STANEK, Wright-Patterson Air Force Base 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2014-2355 AIAA-2014-2356 AIAA-2014-2357 AIAA-2014-2358 Aero-Optical Evaluation of Notional Aero-Optic Characterization of A Low-Dimensional Model of Investigation of turbulent shock Turrets in Subsonic, Transonic and Supersonic Boundary Layers in the Shock-Wake Interaction Over boundary interaction unsteadiness Supersonic Regimes Trisonic Gasdynamic Facility Turrets at Transonic Speeds and its effects on aero-optics in a W. Coirier, Kratos/Digital Fusion, Inc., D. Wittich, M. Paul, Air Force Research A. Vorobiev, S. Gordeyev, E. Jumper, Mach 2 corner flow Huntsville, AL; M. Whiteley, D. Goorskey, Laboratory, Kirtland AFB, NM; A. Ahmed, University of Notre Dame, Notre Dame, M. White, Ohio Aerospace Institute, R. Drye, MZA Associates Corporation, H. Ahmed, Auburn University, Auburn, AL; IN; S. Gogineni, Spectral Energies, LLC, Dayton, OH; M. Visbal, Air Force Research Dayton, OH; J. Barber, J. Stutts, Kratos/ A. Smith, S. Gordeyev, University of Notre Dayton, OH; M. Paul, D. Wittich, Air Force Laboratory, Wright-Patterson AFB, OH Digital Fusion, Inc., Huntsville, AL; et al. Dame, Notre Dame, IN Research Laboratory, Kirtland AFB, NM Tuesday, 17 June 2014 98-HYTASP-2 Vehicle, Mission, and Trajectory Optimization Learning Center Chaired by: R. BROWN, University of Strathclyde 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2014-2359 AIAA-2014-2360 AIAA-2014-2361 AIAA-2014-2362 AIAA-2014-2363 Multidisciplinary Design Multi-Phase Trajectory Optimisation Design and Optimization of RBCC Influence of Boundary Layer Robust Multidisciplinary Design and Optimization of Hypersonic for Access-to-Space with RBCC- Powered Suborbital Reusable Transition on the Trajectory Optimisation of a Reusable Launch Transport Configurations using Powered TSTO via Surrogated- Launch Vehicle Optimisation of a Reusable Launch Vehicle Waveriders Assisted Hybrid Evolutionary C. Gong, B. Chen, L. Gu, Northwestern Vehicle R. Wuilbercq, F. Pescetelli, A. Mogavero, M. Lobbia, Self, Los Angeles, CA; K. Algorithms Incorporating Pseudo- Polytechnical University, Xi’an, China R. Wuilbercq, F. Pescetelli, E. Minisci, R. E. Minisci, R. Brown, University of Suzuki, University of Tokyo, Kashiwa, Spectral Methods Brown, University of Strathclyde, Glasgow, Strathclyde, Glasgow, United Kingdom

66 Japan H. Ogawa, RMIT University, Melbourne, United Kingdom Australia; M. Kodera, S. Tomioka, S. Ueda, Japan Aerospace Exploration Agency (JAXA), Kakuda, Japan Tuesday, 17 June 2014 99-FC-7 Flow Control: Separated Flows Lenox Chaired by: G. DALE, Wright-Patterson Air Force Base and G. WOO, Georgia Institute of Technology 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2014-2364 AIAA-2014-2365 AIAA-2014-2366 AIAA-2014-2367 AIAA-2014-2368 AIAA-2014-2369 Active Flow Separation Control on A Theoretical Model for Microjet A Nonlinear Adaptive Method for Flow Separation Control Over a Shock-Induced Separation Control Control of Shock Wave-Boundary a NACA 0015 Wing using Fluidic Separation Control Microjet-Based Flow Separation Ramp Using Sweeping Jet Actuators by Using Nanosecond Pulsed SDBD Layer Interaction by Repetitive Actuators L. Van Dommelen, Florida A&M University- Control M. Koklu, L. Owens, NASA Langley Plasma actuators Laser Energy Depositions L. Pack Melton, NASA Langley Research Florida State University, Tallahassee, FL; R. B. Reese, F. Alvi, E. Collins, Florida Research Center, Hampton, VA Z. Chen, S. Zhang, B. Zhang, Northwestern A. Sasoh, A. Iwakawa, T. Osuka, R. Center, Hampton, VA Yapalparvi, ANSYS, Inc., Lebanon, NH Center for Advanced Aero-Propulsion, Polytechnical University, Xi’an, China; J. Ma, Majima, T. Tanba, T. Sakai, Nagoya Tallahassee, FL Aviation Industry Corporation of China (AVIC), University, Nagoya, Japan Hanzhong, China Tuesday, 17 June 2014 100-AMT-4/GT-3 In Honor of Dick Miles’s (semi-) Retirement (Invited) Piedmont Chaired by: P. DANEHY, NASA Langley Research Center 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs Oral Presentation Oral Presentation Oral Presentation Oral Presentation Oral Presentation Oral Presentation From Heating Air with 400 MW Gas Phase Coherent Rayleigh- Laser Diagnostics with Atomic Brief History and Introduction of The “final” years at Princeton Diagnostics by Dissociation Laser to Building Plasma Ramparts, Brillouin Scattering Diagnostics Vapor Filters Radar REMPI: Coherent Microwave (from a recent grad) R. Miles, A. Dogariu, Princeton University, And Other Fun Activities at P. Barker, University College London, A. Yalin, Colorado State University, Fort Scattering from Resonance J. Michael, Iowa State University, Ames, IA Princeton, NJ Princeton London, United Kingdom Collins, CO Enhanced Multiphoton Ionization S. Macheret, Lockheed Martin Corporation, Z. Zhang, University of Tennessee, Palmdale, CA Knoxville, Knoxville, TN; M. Shneider, Princeton University, Princeton, NJ Tuesday, 17 June 2014 101-HYTASP-3 Vehicle Systems Regency Ballroom V Chaired by: C. GOYNE, University of Virginia and R. FAULKNER, Aerojet Rocketdyne 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2014-2370 AIAA-2014-2371 AIAA-2014-2372 AIAA-2014-2373 Oral Presentation Cryogenic Propellant Tank and Coupled Simulation of CFD and System Studies on Active Thermal Novel Hybrid Ablative/Ceramic Technology Status of Ceramic Feedline Design Studies in the Flight Mechanics with a Two- Protection of a Hypersonic Development for Re-Entry Matrix Composites for Airbreathing Framework of the CHATT Project Species-Gas-Model for the Hot Suborbital Passenger Transport in Planetary Atmospheric Thermal and High Performance Orbital T. Schwanekamp, German Aerospace Staging of a Multistage Rocket Vehicle Protection: Interfacial Propulsion Applications Center (DLR), Bremen, Germany Y. Li, B. Reimann, T. Eggers, German T. Schwanekamp, German Aerospace Adhesive Selection and Test S. Beyer, S. Schmidt-Wimmer, F. Wigger, Aerospace Center (DLR), Braunschweig, Center (DLR), Bremen, Germany Verification Plan Astrium, Munich, Germany; C. Wilhemi, Germany J. Barcena, S. Florez, B. Perez, Tecnalia F. Uhlmann, EADS, Munich, Germany; P.

67 Research & Innovation, San Sebastian, Peres, Astrium, Saint Médard en Jalles, Spain; J. Bouilly, G. Pinaud, Astrium, Saint France Médard en Jalles, France; W. Fischer, Astrium, Bremen, Germany; et al. Tuesday, 17 June 2014 102-PANEL-3 Panel: Aviation’s Challenges & Opportunities - Perspectives from Brazil & China Regency Ballroom VI 0930 - 1100 hrs Moderator: Joao Azevedo, Senior Research Engineer, Instituto de Aeronautica e Espaco Panelists: Luis Carlos Affonso Carlos Americo Pacheco Guoqing Wang Zhenghong Gao Chief Operating Officer, Embraer Commercial Aviation Rector, Instituto Tecnologico de Aeronautica President, Chinese Aeronautical Radio Electronics Research Institute Professor, Northwestern Polytechnical University

Tuesday, 17 June 2014 103-PDL-8 Re-Entry and Spacecraft Concepts Roswell Chaired by: M. PANESI, University of Illinois at Urbana Champaign and R. GOSSE, AFRL - Air Force Research Laboratory 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2014-2374 AIAA-2014-2375 AIAA-2014-2376 AIAA-2014-2377 AIAA-2014-2378 AIAA-2014-2379 Characterization of Stagnation- Numerical Investigation of the Non-equilibrium flowfield of RAM-C Effect of the Flight Condition on the Investigation of Dissociation USV3 Aerodynamics Assessment: Point Heat Flux for Earth Entry Dynamic Triggering of Electrodynamic II probe Thermochemical Non-equilibrium and Ionization Phenomena in a Step Forward in the Ongoing A. Brandis, ERC, Inc., Mountain View, Aerobraking at High Altitudes using D. Andrienko, J. Shang, Wright State Phenomenon for Super-Orbital Nonequilibrium Shock Layers Design Phase CA; C. Johnston, NASA Langley Research an Ablator with Alkali Metal University, Dayton, OH; S. Surzhikov, Reentry Vehicles A. Munafò, K. Heritier, M. Panesi, D. Cinquegrana, F. Petrosino, G. Pezzella, Center, Hampton, VA H. Katsurayama, Yamaguchi University, Ube, Russian Academy of Sciences, Moscow, H. Otsu, Ryukoku University, Otsu, Japan; T. University of Illinois, Urbana-Champaign, F. Capizzano, G. Andreutti, P. Catalano, Japan; T. Abe, Japan Aerospace Exploration Russia; G. Huang, Wright State University, Abe, K. Yamada, Japan Aerospace Exploration Urbana, IL Italian Aerospace Research Center (CIRA), Agency (JAXA), Sagamihara, Japan Dayton, OH Agency (JAXA), Sagamihara, Japan Capua, Italy; et al. Tuesday, 17 June 2014 104-AFM-7 Planetary Entry and Aeroassist Technology Spring Chaired by: T. LAVIN, Sandia National Laboratories and G. JOHNSTON, Infotech Enterprises 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2014-2381 AIAA-2014-2382 AIAA-2014-2383 AIAA-2014-2384 Extension and Enhancement of the Development of an Aerogel Sample Hypersonic Entry Vehicle State Time-varying entry heating profile Allen-Eggers Analytic Solution for Collector for Martian Dust Sample Estimation Using High-degree replication with a rotating arc jet Ballistic Entry Trajectories Return Cubature Kalman Filter test article Z. Putnam, R. Braun, Georgia Institute of T. Ozawa, T. Suzuki, Japan Aerospace T. Sun, M. Xin, University of Missouri, J. Grinstead, E. Venkatapathy, NASA Ames Technology, Atlanta, GA Exploration Agency (JAXA), Chofu, Japan; Columbia, Columbia, MO Research Center, Moffett Field, CA; E. Y. Hatakeyama, Nihon University, Tokyo, Noyes, J. Mach, D. Empey, Jacobs, Moffett Japan; M. Tabata, Japan Aerospace Field, CA; T. White, ERC, Inc., Moffett Exploration Agency (JAXA), Sagamihara, Field, CA; et al. Japan; K. Fujita, Japan Aerospace Exploration Agency (JAXA), Chofu, Japan Tuesday, 17 June 2014 105-TP-7 Theoretical, Analytical and Computational Heat Transfer II Techwood Chaired by: D. PYTEL, Lockheed Martin Space Systems 0930 hrs 1030 hrs 1100 hrs 1130 hrs Oral Presentation AIAA-2014-2385 AIAA-2014-2386 AIAA-2014-2387 75 Years of Progress: A History of Extending a Numerical Procedure A Nonlinear, Rescaling Based Transient radiative heat transfer the ASME Heat Transfer Division to Simulate the Micro/Nanoscale Inverse Heat Conduction Calibration in a suspension of ceria particles (Invited) Soot Formation in Ethylene-Air Method and Optimal Regularization undergoing non-stoichiometric W. Marner, University of California, Los Turbulent Flame Using Acetylene- Parameter Strategy reduction

68 Angeles, Los Angeles, CA Route Nucleation Y. Chen, J. Frankel, M. Keyhani, University L. Gampp, Swiss Federal Institute of M. Darbandi, M. Ghafourizadeh, Sharif of Tennessee, Knoxville, Knoxville, TN Technology Zurich, Zurich, Switzerland; University of Technology, Tehran, Iran; R. Bader, Australian National University, G. Schneider, University of Waterloo, Canberra, Australia; A. Steinfeld, Swiss Waterloo, Canada Federal Institute of Technology Zurich, Zurich, Switzerland; W. Lipinski, Australian National University, Canberra, Australia Tuesday, 17 June 2014 106-TP-8 Heat Transfer in Cooling, Heating and Power Generation I University Chaired by: J. ROUX, The University of Mississippi and A. MINNICH 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs Oral Presentation AIAA-2014-2388 Oral Presentation Oral Presentation AIAA-2014-2389 Screening of Oxides for Solar Interdisciplinary Analysis of a Turbine Sensitivity Analysis of a High Radiation Heat Sink for Heat A Realistic Radiative Heat Transfer Driven Thermochemical Water Blade With Internal Cooling Including Temperature Liquid Metal Based Dissipation in Liquid Metal Loops Model for Building Energy Splitting Local Distribution and Rotation Effects Solar Receiver A. Henry, G. Wilk, Georgia Institute of Simulation Programs A. Henry, C. Jarrett, Georgia Institute of B. Nouri, Brandenburg University of A. Henry, A. DeAngelis, Georgia Institute of Technology, Atlanta, GA W. Tam, W. Yuen, W. Chow, Hong Kong Technology, Atlanta, GA Technology, Cottbus, Germany; K. Lehmann, Technology, Atlanta, GA Polytechnic University, Hong Kong, Hong Rolls-Royce Group plc, Dahlewitz, Germany; Kong A. Kühhorn, Brandenburg University of Technology, Cottbus, Germany Tuesday, 17 June 2014 107-AFM-8 Best Atmospheric Flight Mechanics Student Paper Competition Vinings Chaired by: M. GRANT, Purdue University and C. SUCHOMEL, USAF 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2014-2390 AIAA-2014-2670 AIAA-2014-2543 AIAA-2014-2381 Parachute Dynamic Stability and Simultaneous Tracking of Multiple Solution of Lambert’s Theorem with Extension and Enhancement of the the Effects of Apparent Inertia Ground Targets from a Single Additional Terminal Constraints Allen-Eggers Analytic Solution for Jason Ginn, Georgia Institute of Multirotor UAV Karthikeyan Kalirajan, Indian Institute Ballistic Entry Trajectories Technology, Atlanta, GA Nathaniel R Miller, Texas A&M of Technology Bombay, Mumbai, Indi Zachary Putnam, Georgia Institute of University, College Station, TX Technology, Atlanta, GA

Tuesday, 17 June 2014 108-LNCH-2 Awards Luncheon: Celebrating Achievements in Aerospace Sciences Centennial I/II 1230 - 1400 hrs Tuesday, 17 June 2014 109-APA-19 Special Session: NATO Task Group AVT-201 IV - Stability and Control Analyses Baker Chaired by: R. CUMMINGS, US Air Force Academy 1400 hrs 1430 hrs 1500 hrs 1530 hrs AIAA-2014-2391 AIAA-2014-2392 AIAA-2014-2393 AIAA-2014-2394 Static and Dynamic Derivatives Stability and Control Assessment of Development of an aerodynamic The NATO STO AVT-201 Task Group on generic UCAV without and with a Generic UCAV Design Using the simulation model of a generic on Extended assessment of Stability leading edge control Edge Flow Solver configuration for S&C analyses an Control Prediction Methods

69 J. Le Roy, S. Morgand, D. Farcy, ONERA, M. Tomac, Royal Institute of Technology J. Irving, BAE Systems, Warton, United for NATO Air Vehicles: Summary, Lille, France (KTH), Stockholm, Sweden; M. Tormalm, Kingdom; D. Vicroy, NASA Langley Conclusions and Lessons Learned Swedish Defense Research Agency (FOI), Research Center, Hampton, VA; D. Farcy, A. Jirasek, R. Cummings, U.S. Air Force Stockholm, Sweden ONERA, Lille, France Academy, Colorado Springs, CO; A. Schuette, K. Huber, German Aerospace Center (DLR), Braunschweig, Germany Tuesday, 17 June 2014 110-APA-20 Special Session: Sonic Boom Activities IV - Low Sonic Boom Flight Demonstration Courtland Chaired by: D. RICHWINE, NASA-Langley Research Center 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs Oral Presentation Oral Presentation Oral Presentation Oral Presentation Oral Presentation Oral Presentation Overview of NASA High Speed ICAO Supersonics Task Group Boeing Low-Boom Flight Lockheed Martin Low-Boom Flight Advanced Adjoint Optimization The Need for Speed Project Research and Progress (SSTG) Status and Progress Demonstrator (LBFD) Concept Demonstrator (LBFD) Concept Capabilities in SU2 for the Design R. Cowart, Gulfstream Aerospace P. Coen, D. Richwine, NASA Langley S. Liu, Federal Aviation Administration, Formulation Study Formulation Study of a Low-Boom Flight Demonstrator Corporation, Savannah, GA Research Center, Hampton, VA Washington, DC; V. Sparrow, Pennsylvania T. Antani, H. Welge, S. Agrawal, C. M. Buonanno, J. Morgenstern, Lockheed J. Alonso, F. Palacios, T. Lukaczyk, State University, University Park, PA Nelson, T. Magee, S. Holllowell, The Martin Corporation, Palmdale, CA Stanford University, Stanford, CA Boeing Company, Seattle, WA; et al. Tuesday, 17 June 2014 111-APA-21 Special Session: 2nd High-Lift Prediction Workshop I Dunwoody Chaired by: C. RUMSEY, NASA-Langley Research Center and A. SCLAFANI, Boeing Engineering Operations & Technology 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs AIAA-2014-2395 AIAA-2014-2396 AIAA-2014-2397 AIAA-2014-2398 AIAA-2014-2399 Grid-Adapted FUN3D Computations Summary of JAXA Studies for the Investigation of Grid Generation Detached Eddy Simulation of the CIAM, Sukhoi NCT and Irkut for the Second High Lift Prediction 2nd AIAA CFD High Lift Prediction Strategy for prediction of High DLR-F11 wing/body Configuration Contribution to HiLiftPW-2 Workshop (Invited) Workshop Using Structured and Lift Flows as a Contribution to the 2nd AIAA V. Makarov, Y. Fedorchenko, V. Shorstov, E. Lee-Rausch, C. Rumsey, M. Park, NASA Unstructured Mesh CFD A. Moitra, P. Gujar, P. Gupta, D. Rajvanshi, CFD High Lift Prediction Workshop Central Institute of Aviation Motors, Langley Research Center, Hampton, VA M. Murayama, K. Yamamoto, Y. Ito, Japan Tata Consultancy Services, Bangalore, J. Escobar, C. Suarez, C. Silva, University Moscow, Russia; A. Babulin, K. Bolshunov, Aerospace Exploration Agency (JAXA), India of San Buenaventura, Bogota, Colombia; United Aircraft Corporation, Moscow, Tokyo, Japan; T. Hirai, K. Tanaka, Ryoyu O. Lopez, J. Velandia, C. Lara, University Russia Systems Company, Ltd., Tokyo, Japan of the Andes, Bogota, Colombia Tuesday, 17 June 2014 112-APA-22 Flow Control (Active and Passive): Computational and Experimental Results III Edgewood Chaired by: D. LACY, Boeing Commercial Airplanes and C. PASILIAO, US Air Force 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs AIAA-2014-2400 AIAA-2014-2401 AIAA-2014-2402 AIAA-2014-2403 AIAA-2014-2404 AIAA-2014-2405 AIAA-2014-2406 Evaluation criteria and Towards the Industrial Application Thrust Removal Methodology for Active Flow Control for an Finding Computationally Inexpensive Optimization by CFD analyses of Linear parameter-varying active performance comparison of of Active Flow Control in Civil the FAST-MAC Circulation Control Outer Wing Model of a Take-off Methods to Model the Flow Past Heavy riblet distribution over a transonic flow control for a 3D bluff body actuators for bluff-body flow Aircraft - An Active Highlift Flap Model Tested in the National Transport Aircraft Configuration - A Vehicles and the Design of Active Flow civil aircraft configuration exposed to cross-wind gusts control M. Meyer, W. Machunze, EADS, Munich, Transonic Facility Numerical Study Control Systems for Drag Reduction B. Mele, R. Tognaccini, University of J. Pfeiffer, R. King, Technical University of A. Seifert, Tel Aviv University, Tel Aviv, Germany; M. Bauer, Technical University of D. Chan, W. Milholen, G. Jones, NASA V. Ciobaca, J. Wild, German Aerospace D. Manosalvas, T. Economon, F. Palacios, A. Naples “Federico II”, Naples, Italy; P. Berlin, Berlin, Germany Israel Berlin, Berlin, Germany Langley Research Center, Hampton, VA; S. Center (DLR), Braunschweig, Germany Jameson, Stanford University, Stanford, CA Catalano, Italian Aerospace Research

70 Goodliff, Jacobs, Hampton, VA Center (CIRA), Naples, Italy Tuesday, 17 June 2014 113-ATIO-9 Transformational Flight - Advanced Concepts Embassy C Chaired by: R. MANGE, Lockheed Martin Corporation 1400 hrs 1430 hrs 1500 hrs 1530 hrs Oral Presentation Oral Presentation AIAA-2014-2407 AIAA-2014-2408 Leading Edge Distributed Electric Greased Lightning: A Cruise Conceptual Design of the Joby S2 Design of the ATG Javelin Personal Propulsion Wing Concept for CTOL, Efficient VTOL Aircraft Electric VTOL PAV Fighter Jet STOL, and VTOL Missions W. Fredericks, NASA Langley Research A. Stoll, E. Stilson, J. Bevirt, P. Pei, Joby B. Knapp, Tzunum Aircraft, Redmond, WA M. Moore, W. Fredericks, NASA Langley Center, Hampton, VA Aviation, Santa Cruz, CA Research Center, Hampton, VA Tuesday, 17 June 2014 114-ATIO-10 Transformational Flight - Demand Modeling Embassy C Chaired by: M. MOORE, NASA Langley Research Center 1400 hrs 1600 hrs 1630 hrs 1700 hrs No Presentations AIAA-2014-2409 AIAA-2014-2410 AIAA-2014-2411 Future Evaluation Worlds for NASA JPDO & NASA ARMD Multimodal Zip Vehicle Commuter Aircraft Aeronautics R&D Portfolio Analysis Analyses Demand Estimate: a Multinomial Y. Gawdiak, NASA Headquarters, Y. Gawdiak, NASA Headquarters, Logit Mode Choice Model Washington, DC; J. Creedon, Old Dominion Washington, DC; S. Trajkov, Saab Sensis D. Pu, A. Trani, N. Hinze, Virginia University, Norfolk, VA; B. Holmes, NextGen Corporation, Washington, DC; M. Narkus- Polytechnic Institute and State University, AeroSciences, LLC, Williamsburg, VA; S. Kramer, LMI, McLean, VA; D. Ballard, Blacksburg, VA Trajkov, Saab Sensis Corporation, Washington, GRA, Inc., Jenkintown, PA; J. Creedon, DC; M. Narkus-Kramer, LMI, McLean, VA; Old Dominion University, Norfolk, VA; R. S. Bertish, Federal Aviation Administration, Hemm, LMI, McLean, VA; et al. Washington, DC; et al. Tuesday, 17 June 2014 115-ATIO-11 UAS Integration & Operations II Embassy D Chaired by: V. SCHULTZ, NASA Langley Research Center and A. DESHMUKH, Gulfstream Aerospace Corp. 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2014-2412 AIAA-2014-2413 AIAA-2014-2414 AIAA-2014-2415 AIAA-2014-2416 AIAA-2014-2417 A Family of Well-Clear Boundary Investigating Detect-and-Avoid UAS Contingency Management: The UAVs for Law Enforcement: A Case Generation of Normalized Difference The Ability of RC Pilots to Maintain Models for the Integration of UAS Surveillance Performance for Effect of Different Procedures on Study for Connectivity and Fuel Vegetation Index Map for Precision Visual Line-of-Sight of their Vehicle in the NAS Unmanned Aircraft Systems ATC in Civil Airspace Operations Management Agriculture Using Small-Type A. Trujillo, R. Ghatas, NASA Langley C. Munoz, A. Narkawicz, J. Chamberlain, C. Park, S. Lee, University of California, L. Fern, R. Rorie, San Jose State D. Aksaray, K. Griendling, D. Mavris, Georgia Unmanned Aerial Vehicle Research Center, Hampton, VA; D. Burdette, M. Consiglio, J. Upchurch, NASA Langley Santa Cruz, Moffett Field, CA; E. Mueller, University, Moffett Field, CA; R. Shively, Institute of Technology, Atlanta, GA K. Chiba, T. Kamei, T. Ito, S. Sugai, S. Northrop Grumman Corporation, Hampton, Research Center, Hampton, VA NASA Ames Research Center, Mountain NASA Ames Research Center, Moffett Ohta, S. Satori, Hokkaido Institute of VA; R. McAdaragh, Stinger Ghaffarian View, CA Field, CA Technology, Sapporo, Japan Technologies, Inc., Hampton, VA Tuesday, 17 June 2014 116-ATIO-12 ATM-IV Systems Evaluations in ATM Embassy E Chaired by: M. BLOEM, NASA-Ames 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs AIAA-2014-2418 AIAA-2014-2419 AIAA-2014-2420 AIAA-2014-2421 AIAA-2014-2422 Measuring the early impacts of the System-Level Performance Evaluation A Frequency Analysis Approach for Integrating Advanced Technology Modeling the effect of uncertainty FAA Surveillance and Broadcast of ATD-1 Ground-Based Technologies Categorizing Air Traffic Behavior into Air Traffic Controller Training and NextGen concepts and Services Program T. Callantine, M. Kupfer, L. Martin, J. M. Drew, University of California, Santa S. Schultheis, MITRE Corporation, technologies on the national D. Howell, MCR, LLC, Beavercreek, OH; J. Mercer, San Jose State University, Moffett Cruz, Santa Cruz, CA; K. Sheth, NASA McLean, VA airspace system King, MCR, LLC, Washington, DC Field, CA; T. Prevot, NASA Ames Research Ames Research Center, Moffett Field, CA J. Archer, S. Landry, Purdue University, Center, Moffett Field, CA West Lafayette, IN

71 Tuesday, 17 June 2014 117-ACD-5 Aircraft Performance and Design Studies Embassy F Chaired by: H. JIMENEZ, Georgia Institute of Technology and T. TAKAHASHI, Arizona State University 1400 hrs 1430 hrs 1500 hrs 1530 hrs AIAA-2014-2423 AIAA-2014-2424 AIAA-2014-2425 AIAA-2014-2426 Multidisciplinary Design Optimization Analysis of the Effect of Cruise Reforming Field Performance Planform Selection for an Efficient of a Truss Braced Wing Concept Speed on Fuel Efficiency and Cost Federal Aviation Regulations for Supersonic Air Vehicle T. Nam, I. Chakraborty, J. Gross, D. Mavris, for a Truss-Braced Wing Concept Operational Safety and Consistency T. Takahashi, C. Kady, Arizona State Georgia Institute of Technology, Atlanta, GA; I. Chakraborty, J. Gross, T. Nam, C. T. Takahashi, A. Creighton, Arizona State University, Tempe, AZ J. Schetz, R. Kapania, Virginia Polytechnic Perullo, D. Mavris, Georgia Institute of University, Tempe, AZ Institute and State University, Blacksburg, VA Technology, Atlanta, GA Tuesday, 17 June 2014 118-ACD-6 Hybrid Wing Body Design Case Studies Embassy F Chaired by: H. JIMENEZ, Georgia Institute of Technology and T. TAKAHASHI, Arizona State University 1400 hrs 1600 hrs 1630 hrs No Presentations AIAA-2014-2427 AIAA-2014-2428 Hybrid-Wing-Body Vehicle Assessment of Electrically Actuated Composite Fuselage Analysis and Redundant Control Surface Layouts Case Study for a Hybrid Wing Body Concept V. Mukhopadhyay, NASA Langley Research D. Garmendia, I. Chakraborty, D. Trawick, Center, Hampton, VA D. Mavris, Georgia Institute of Technology, Atlanta, GA Tuesday, 17 June 2014 119-MAO-7 Multidisciplinary Analysis and Optimization: Emerging Methods I Embassy G Chaired by: J. MARTINS, University of Michigan 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs AIAA-2014-2429 AIAA-2014-2430 AIAA-2014-2431 AIAA-2014-2432 AIAA-2014-2433 AIAA-2014-2434 AIAA-2014-2435 Multidisciplinary Design Incorporation of Coupling Strength Improving Contextual Self- Profit and Operational-Based Value Parameterized Continuous Optimization Algorithm for Systems Fatigue Design Load Development Optimization of an Aircraft Wing Models in Decomposition Strategies Organizing Map Solution Times Functions Representations of the Pareto Governed by Chaotic Dynamics for Conceptual Structural via a Matrix-Free Approach for Value-based MDO Using GPU Parallel Training E. Goetzke, C. Bloebaum, B. Mesmer, Frontier as Decision Aids for Multi- A. Ashley, J. Hicken, Rensselaer Optimization A. Lambe, University of Toronto, Toronto, H. Kannan, C. Bloebaum, B. Mesmer, T. Richardson, J. Holub, E. Winer, Iowa Iowa State University, Ames, IA Attribute Design Polytechnic Institute, Troy, NY H. Li, H. Bae, Wright State University, Canada; G. Kennedy, Georgia Institute of Iowa State University, Ames, IA State University, Ames, IA M. Daskilewicz, B. German, Georgia Dayton, OH Technology, Atlanta, GA; J. Martins, University Institute of Technology, Atlanta, GA of Michigan, Ann Arbor, Ann Arbor, MI Tuesday, 17 June 2014 120-MAO-8 Multidisciplinary Analysis and Optimization: Metamodeling II Embassy H Chaired by: V. BALABANOV, Boeing Commercial Airplanes 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs AIAA-2014-2436 AIAA-2014-2437 AIAA-2014-2438 AIAA-2014-2439 AIAA-2014-2440 Managing Variable Fidelity Models Mid-Range Approximations in Optimistic Bias in Surrogate Global Search for Diverse Truss structure satellite bus geometry- in Population-based Optimization Sub-Spaces for MDO Problems with Prediction near Surrogate Optima Competitive Designs structure optimization involving mixed using Adaptive Model Switching Disparate Discipline Attributes A. Chaudhuri, R. Haftka, University of Y. Zhou, Dalian University of Technology, variables and expensive models A. Mehmani, Syracuse University, J. Ollar, Altair Engineering, Inc., Florida, Gainesville, Gainesville, FL Dalian, China; A. Chaudhuri, R. Haftka, using metamodel-based optimization Syracuse, NY; S. Chowdhury, A. Messac, Leamington Spa, United Kingdom; V. University of Florida, Gainesville, strategy Mississippi State University, Mississippi Toropov, University of Leeds, Leeds, United Gainesville, FL; G. Cheng, Dalian University L. Peng, L. Liu, T. Long, X. Guo, R. Shi, Beijing State, MS Kingdom; R. Jones, Altair Engineering, of Technology, Dalian, China Institute of Technology, Beijing, China

72 Inc., Leamington Spa, United Kingdom Tuesday, 17 June 2014 121-APA-23 Special Session: Aerodynamic-Structural Modeling, Optimization, and Test Techniques for Flexible Wing Technology I Fairlie Chaired by: N. NGUYEN, NASA-Ames Research Center and M. ROGERS, NASA Ames Research Center 1400 hrs 1430 hrs 1500 hrs 1530 hrs AIAA-2014-2441 AIAA-2014-2442 AIAA-2014-2443 AIAA-2014-2444 Experimental Investigation of a Design, Construction, and Tests of Aeroelastic Modeling and Drag Drag Optimization Study of Flexible Wing with a Variable Camber an Aeroelastic Wind Tunnel Model Optimization of Flexible Wing Variable Camber Continuous Continuous Trailing Edge Flap Design of a Variable Camber Continuous Aircraft with Variable Camber Trailing Edge Flap (VCCTEF) Using N. Nguyen, NASA Ames Research Center, Trailing Edge Flap (VCCTEF) Concept Continuous Trailing Edge Flap OVERFLOW Moffett Field, CA; E. Livne, N. Precup, Wing S. Lebofsky, E. Ting, Stinger Ghaffarian U. Kaul, N. Nguyen, NASA Ames Research University of Washington, Seattle, Seattle, E. Livne, N. Precup, M. Mor, University of Technologies, Inc., Mountain View, CA; Center, Moffett Field, CA WA; J. Urnes, The Boeing Company, St. Louis, Washington, Seattle, Seattle, WA N. Nguyen, NASA Ames Research Center, MO; C. Nelson, The Boeing Company, Seattle, Moffett Field, CA; K. Trinh, Stinger WA; E. Ting, Stinger Ghaffarian Technologies, Ghaffarian Technologies, Inc., Mountain Inc., Moffett Field, CA; et al. View, CA Tuesday, 17 June 2014 122-FD-11 Fluid Structure Interaction II Greenbriar Chaired by: H. LUO, Vanderbilt University 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2014-2445 AIAA-2014-2446 AIAA-2014-2447 AIAA-2014-2448 AIAA-2014-2449 AIAA-2014-2450 Effect of Wall Deformation on Computed and Experimental F/A-18 Twin-Tail Buffet Modeling Development and Validation of a Fluid-Structure Interaction in the Aerodynamic and Aeroelastic Aerodynamic Performance for Flutter/LCO Onset for the Boeing Using Non-Linear Eddy Viscosity Partitioned Fluid-Structure Solver Context of a Scramjet Intake Analysis of a Cycloidal Rotor Mixed Compression Intake Truss-Braced Wing Wind Tunnel Models for Transonic Panel Flutter with S. Frauholz, N. Hosters, B. Reinartz, M. L. Gagnon, G. Quaranta, M. Morandini, C. Yao, Z. Liu, J. Wei, S. Qu, G. Zhang, Model A. Elmekawy, O. Kandil, O. Baysal, Old Focus on Boundary Layer Effects Behr, RWTH Aachen University, Aachen, P. Masarati, Technical University of Milan, Harbin Institute of Technology, Harbin, R. Bartels, R. Scott, NASA Langley Dominion University, Norfolk, VA M. Alder, German Aerospace Center (DLR), Germany Milan, Italy; C. Xisto, J. Páscoa, University China Research Center, Hampton, VA Braunschweig, Germany of Beira Interior, Covilha, Portugal Tuesday, 17 June 2014 123-AA-6 CAA Sound Generation I Hanover A Chaired by: E. BRAMBLEY, University of Cambridge 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2014-2451 AIAA-2014-2452 AIAA-2014-2453 AIAA-2014-2454 AIAA-2014-2455 AIAA-2014-2456 The Fast Random Particle Method Internal noise suppression for Numerical Predictions of Exploration of temperature effects Direct aeroacoustics simulation Integrating CFD source predictions for Combustion Noise Prediction DNS of a turbulent jet-pipe Turbulence-Cascade Interaction on the far-field acoustic radiation of automotive engine cooling with time-domain CAA for intake F. Grimm, German Aerospace Center configuration Noise Using CAA with a Stochastic from a supersonic jet fan system: effect of upstream fan noise prediction (DLR), Stuttgart, Germany; R. Ewert, J. R. Sandberg, B. Tester, S. Olivetti, Model H. Hafsteinsson, L. Eriksson, N. Andersson, geometry on broadband noise Z. Rarata, G. Gabard, R. Sugimoto, Dierke, German Aerospace Center (DLR), University of Southampton, Southampton, V. Clair, C. Polacsek, T. Le Garrec, ONERA, Chalmers University of Technology, Göteborg, M. Piellard, B. Coutty, Delphi Thermal J. Coupland, R. Astley, University of Braunschweig, Germany; B. Noll, M. United Kingdom Châtillon, France; M. Jacob, École Centrale Sweden; P. Mora Sanchez, E. Gutmark, Systems, Bascharage, Luxembourg; V. Le Goff, Southampton, Southampton, United Aigner, German Aerospace Center (DLR), de Lyon, Ecully, France University of Cincinnati, Cincinnati, OH; E. V. Vidal, Euroxa, Paris La Défense, France; F. Kingdom; H. Namgoong, Rolls-Royce Stuttgart, Germany Prisell, FMV, Stockholm, Sweden Perot, Exa Corporation, Brisbane, CA Group plc, Derby, United Kingdom; et al. Tuesday, 17 June 2014 124-AA-7 Fluid Acoustic Phenomena I Hanover B Chaired by: Y. GUO, Boeing Defense, Space & Security and M. ROGER, Ecole Centrale de Lyon 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2014-2457 AIAA-2014-2458 AIAA-2014-2459 AIAA-2014-2460 AIAA-2014-2461 AIAA-2014-2462 Aero-Structural Acoustics of Uneven Aero-Structural Acoustics of Uneven Acoustic scattering by finite The Noise From Separated Flow Aeroacoustics of 2D and 3D Surface Effect of Step Rounding on Noise Surfaces Part 1: A General Model Surfaces Part 2: A Specific Forcing poroelastic plates S. Glegg, B. Bryan, Florida Atlantic Discontinuities from Forward-Facing Steps Approach to Radiated Sound by a Rough Wall Boundary Layer A. Cavalieri, Technological Institute of University, Boca Raton, FL; W. Devenport, M. Awasthi, W. Devenport, T. Meyers, W. J. Hao, M. Wang, University of Notre W. Blake, University of Notre Dame, Notre J. Anderson, Naval Surface Warfare Center, Aeronautics (ITA), São José dos Campos, M. Awasthi, Virginia Polytechnic Institute Alexander, Virginia Polytechnic Institute and Dame, Notre Dame, IN Dame, IN; J. Anderson, Naval Surface West Bethesda, MD; W. Blake, University Brazil; W. Wolf, University of Campinas, and State University, Blacksburg, VA State University, Blacksburg, VA; S. Glegg, Warfare Center, West Bethesda, MD of Notre Dame, Notre Dame, IN Campinas, Brazil; J. Jaworski, Lehigh Florida Atlantic University, Boca Raton, FL

73 University, Bethlehem, PA Tuesday, 17 June 2014 125-ASE-7 Ice Roughness Effects on Heat Transfer and Transition Hanover C Chaired by: M. VARGAS, NASA Glenn Research Center and P. VILLEDIEU 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2014-2463 AIAA-2014-2464 AIAA-2014-2465 Oral Presentation Oral Presentation Open Discussion Convection from Ice Roughness Transient Heat Transfer Infrared and Hot-Wire Boundary layer and heat transfer How Roughness Research can with Varying Flux Boundary Measurements of Surface Investigations of Ice Roughness characterization on surface with Improve LEWICE (Invited) Conditions Roughness due to Ice Accretion Induced Transition academic roughness (Invited) W. Wright, Vantage Partners, LLC, C. Walker, S. McClain, Baylor University, Y. Han, J. Palacios, Pennsylvania State S. McClain, C. Walker, L. Tecson, Baylor P. Reulet, D. Donjat, F. Micheli, B. Aupoix, Cleveland, OH; C. Bidwell, NASA Glenn Waco, TX University, University Park, PA University, Waco, TX ONERA, Toulouse, France Research Center, Cleveland, OH Tuesday, 17 June 2014 126-ASE-8/AFM-9/FT-3 Managing Wake Vortex Encounter II: Including Wake Vortex Modelling Hanover D Chaired by: A. BROWN, National Research Council Canada and F. PROCTOR, NASA Langley Research Center 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs AIAA-2014-2466 AIAA-2014-2467 AIAA-2014-2468 AIAA-2014-2469 AIAA-2014-2470 Evaluation of Fast-Time Wake First Results from the NASA Wake Observations of Small-scale Numerical Study of a Long-Lived, Impact of Wind and Obstacles on Vortex Models using Wake Vortex Measurements at the Atmospheric Variability and the Isolated Wake Vortex in Ground Wake Vortex Evolution in Ground Encounter Flight Test Data Memphis International Airport Importance of Accurate Weather Effect Proximity N. Ahmad, R. VanValkenburg, R. D. Delisi, M. Pruis, NorthWest Research Information in Deterministic and F. Proctor, NASA Langley Research Center, F. Holzäpfel, A. Stephan, N. Tchipev, T. Bowles, NASA Langley Research Center, Associates, Redmond, WA; D. Jacob, Probabilistic Fast-time Wake Vortex Hampton, VA Heel, S. Körner, German Aerospace Center Hampton, VA; F. Limon Duparcmeur, Craig Coherent Research Group, LLC, Ormond Modeling (DLR), Oberpfaffenhofen, Germany; T. Technologies, Inc., Hampton, VA Beach, FL; D. Lai, NorthWest Research M. Pruis, D. Delisi, NorthWest Research Misaka, Tohoku University, Sendai, Japan Associates, Redmond, WA Associates, Redmond, WA Tuesday, 17 June 2014 127-AA-8 Jet Noise Reduction I Hanover E Chaired by: P. JORDAN, PPRIME 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2014-2471 AIAA-2014-2472 AIAA-2014-2473 AIAA-2014-2474 AIAA-2014-2475 AIAA-2014-2476 A Formulation and Implementation Checkpointing Methods for Optimization of Blowing in a Supersonic Jet Noise Reduction Jet-wing interaction: computational Thermoacoustics of a turbulent of Adjoint-Based Supersonic Jet Adjoint-Based Supersonic Jet Noise Convergent-Divergent Nozzle for by Nozzle Fluidic Inserts with modelling based on MILES CABARET premixed flame Noise Reduction Reduction Noise Reduction Simulated Forward Flight and acoustic analogy G. Geiser, RWTH Aachen University, Aachen, A. Corrigan, Z. Spears, J. Liu, R. Z. Spears, A. Corrigan, K. Kailasanath, N. Sikarwar, P. Morris, Pennsylvania State R. Powers, C. Kuo, D. McLaughlin, P. V. Semiletov, S. Karabasov, Queen Mary, Germany; H. Nawroth, Technical University Ramamurti, K. Kailasanath, Naval Naval Research Laboratory, Washington, University, University Park, PA Morris, Pennsylvania State University, University of London, London, United of Berlin, Berlin, Germany; A. Hosseinzadeh, Research Laboratory, Washington, DC DC University Park, PA Kingdom; G. Faranosov, V. Kopiev, V. Technical University of Darmstadt, Darmstadt, Goloviznin, Central Aerohydrodynamic Germany; F. Zhang, H. Bockhorn, P. Institute, Moscow, Russia Habisreuther, Karlsruhe Institute of Technology, Karlsruhe, Germany; et al. Tuesday, 17 June 2014 128-AA-9 NASA Gulfstream Airframe Noise Reduction Hanover F Chaired by: M. KHORRAMI, NASA-Langley Research Center and D. LOCKARD, NASA-Langley Research Center 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs Oral Presentation AIAA-2014-2477 AIAA-2014-2478 AIAA-2014-2479 AIAA-2014-2480 AIAA-2014-2481 NASA-Gulfstream Joint Effort on Aerodynamic Measurements of a Aeroacoustic Evaluation of Flap Flow-Field Investigation of Gear- Towards Full Aircraft Airframe Towards Full Aircraft Airframe Airframe Noise Reduction: An Gulfstream Aircraft Model With and and Landing Gear Noise Reduction Flap Interaction on a Gulfstream Noise Prediction: Detached Eddy Noise Prediction: Lattice Boltzmann Overview Without Noise Reduction Concepts Concepts Aircraft Model Simulations Simulations M. Khorrami, NASA Langley Research D. Neuhart, J. Hannon, M. Khorrami, NASA M. Khorrami, W. Humphreys, D. Lockard, C. Yao, L. Jenkins, S. Bartram, J. Harris, M. Khorrami, NASA Langley Research M. Khorrami, NASA Langley Research Center, Center, Hampton, VA; T. Van de Ven, Langley Research Center, Hampton, VA NASA Langley Research Center, Hampton, M. Khorrami, NASA Langley Research Center, Hampton, VA; R. Mineck, Self, Hampton, VA; E. Fares, D. Casalino, Exa Gulfstream Aerospace Corporation, VA; P. Ravetta, AVEC, Inc., Blacksburg, VA Center, Hampton, VA; W. Mace, Sierra Yorktown, VA Corporation, Stuttgart, Germany 74 Savannah, GA Lobo, Inc., Hampton, VA Tuesday, 17 June 2014 129-HYTASP-23 Aerodynamic and Propulsion Test Unit (APTU) I Hanover G Chaired by: G. GARRARD, Aerospace Testing Alliance (ATA) 1400 hrs 1430 hrs 1500 hrs 1530 hrs AIAA-2014-2482 AIAA-2014-2483 AIAA-2014-2484 AIAA-2014-2485 Summary of Test Preparations Activation and Calibration Plans for In Place Calibration of the Design, Analyses, and Planned for the Medium Scale Critical the Aerodynamic and Propulsion Aerodynamic and Propulsion Test Calibration Tests for the Medium Scale Components Test Program at the Test Unit Heated Fuel System Unit Air, Isobutane, and Liquid Critical Components Direct Connect Aerodynamic and Propulsion Test (Invited) Oxygen System Venturi Tubes Facility Nozzles at the Aerodynamic Unit (Invited) K. Holst, Aerospace Testing Alliance, Arnold (Invited) and Propulsion Test Unit (Invited) S. Rigney, Aerospace Testing Alliance, AFB, TN G. Garrard, Aerospace Testing Alliance, K. Holst, Aerospace Testing Alliance, Arnold Arnold AFB, TN Arnold AFB, TN AFB, TN Tuesday, 17 June 2014 130-ITAR-2 ITAR-Noise Modeling and Technologies for Quiet UAS Hanover G Chaired by: E. GARCIA, Georgia Institute of Technology 1400 hrs 1600 hrs 1630 hrs No Presentations AIAA-2014-2486 AIAA-2014-2487 Aircraft Noise Prediction Using A Framework for Multidisciplinary Virtual Lab Conceptual Design of Quiet Small D. Robertson, C. Marks, University of Unmanned Aerial Systems Dayton Research Institute, Dayton, OH; D. Bryson, R. Miller, T. White, G. Reich, Air D. Bryson, G. Reich, Air Force Research Force Research Laboratory, Wright-Patterson Laboratory, Wright-Patterson AFB, OH AFB, OH; D. Robertson, C. Marks, University of Dayton Research Institute, Dayton, OH; et al. Tuesday, 17 June 2014 131-PDL-9 Radiation/Aero-Optics II Harris Chaired by: M. RENNIE and M. PANESI, University of Illinois at Urbana Champaign 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs AIAA-2014-2488 AIAA-2014-2489 AIAA-2014-2490 AIAA-2014-2491 AIAA-2014-2492 AIAA-2014-2493 AIAA-2014-2494 On View-Factor Approach for Radiation Transport Analysis of eRC Model for Prediction of Subsonic Boundary-Layer Simulating jet exhaust plumes for Shack-Hartmann Wavefront The Removal of Tunnel Vibration Radiation Transfer Equation Emission Spectroscopic Measurements Molecular Bands Radiation for Wavefront Spectra for a Range of optical propagation calculations Measurements of Supersonic Turbulent Induced Corruption in Aero-Optical D. Andrienko, Wright State University, in the Plenum Region of the NASA IHF Stardust Entry Conditions Reynolds Numbers O. Parmhed, H. Edefur, C. Fureby, M. Boundary Layers in the TGF Measurements Dayton, OH; S. Surzhikov, Russian Arc Jet Facility S. Surzhikov, Russian Academy of A. Smith, S. Gordeyev, University of Notre Henriksson, S. Peng, S. Wallin, Swedish A. Smith, S. Gordeyev, University of Notre N. De Lucca, S. Gordeyev, A. Smith, E. Academy of Sciences, Moscow, Russia; J. M. Winter, University of Kentucky, Lexington, Sciences, Moscow, Russia; J. Shang, Dame, Notre Dame, IN; T. Saxton-Fox, B. Defense Research Agency (FOI), Dame, Notre Dame, IN; H. Ahmed, A. Ahmed, Jumper, University of Notre Dame, Notre Shang, G. Huang, Wright State University, Lexington, KY; D. Prabhu, ERC, Inc., Moffett Wright State University, Dayton, OH McKeon, California Institute of Technology, Stockholm, Sweden; et al. Auburn University, Auburn, AL; D. Wittich, Air Dame, IN; M. Whiteley, MZA Associates Dayton, OH Field, CA; W. Williams, University of Kentucky, Pasadena, CA Force Research Laboratory, Kirtland AFB, NM Corporation, Dayton, OH; T. Neale, Arnold Lexington, Lexington, KY Engineering Development Center, Arnold AFB, TN Tuesday, 17 June 2014 132-FD-12 Stability and Transition II Inman Chaired by: K. CASPER, Sandia National Laboratories and E. WHITE, Texas A&M University 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs AIAA-2014-2495 AIAA-2014-2496 AIAA-2014-2497 AIAA-2014-2498 AIAA-2014-2499 AIAA-2014-2500 AIAA-2014-2501 Direct Numerical Simulation of Experimental Investigation of Gas Transient Growth in Hypersonic Stability analysis of high-speed Numerical Simulation of Numerical Investigation of transition An Experimental Study of Geometrical Parameter Effects Injection into the Boundary Layer on a Boundary Layers boundary-layer flow with gas injection Roughness-Induced Instability delay for various controlled Roughness-Induced Instabilities in a on the Hypersonic Ramp-Induced Slender Body in Supersonic Flow N. Bitter, J. Shepherd, California Institute A. Fedorov, V. Soudakov, Moscow Institute Growth and Transition at Mach 6 breakdown scenarios in a Mach 6 Supersonic Boundary Layer Transition B. Schmidt, N. Bitter, H. Hornung, of Technology, Pasadena, CA of Physics and Technology, Zhukovsky, J. Van den Eynde, N. Sandham, University Boundary Layer using porous walls M. Kegerise, R. King, M. Choudhari, F. Li, Z. Duan, Z. Xiao, Tsinghua University, J. Shepherd, California Institute of Russia; I. Leyva, Air Force Research of Southampton, Southampton, United C. Hader, C. Brehm, H. Fasel, University of A. Norris, NASA Langley Research Center, Laboratory, Edwards AFB, CA 75 Beijing, China Technology, Pasadena, CA Kingdom Arizona, Tucson, Tucson, AZ Hampton, VA Tuesday, 17 June 2014 133-FD-13 Vortex and Wake Dominated Flows Kenneshaw Chaired by: S. YARUSEVYCH, University of Waterloo 1400 hrs 1430 hrs 1500 hrs 1530 hrs AIAA-2014-2502 AIAA-2014-2503 AIAA-2014-2504 AIAA-2014-2505 Investigations of a Self Sustained Investigation of the Wake of A Computational Fluid Dynamic Study Numerical study on low Reynolds Vortex Flow System Inside a a Periodically Pitching Airfoil of Intense Cephalopod-like Motions number flow past two side by side Confined Machinery Duct Embedded in a Shear Layer A. Kazakidi, D. Tsakiris, Foundation for triangular cylinders J. Wang, W. Wang, B. Bernardo, The K. Zhang, Xi’an Jiaotong University, Xi’an, Research and Technology—Hellas (FORTH), S. Katiresan, A. Roy, Indian Institute of Aerospace Corporation, El Segundo, CA China; A. Naguib, M. Koochesfahani, Michigan Heraklion, Greece; F. Sotiropoulos, University Technology Kharagpur, Kharagpur, India State University, East Lansing, MI of Minnesota, Minneapolis, Minneapolis, MN; J. Ekaterinaris, University of Patras, Patra, Greece Tuesday, 17 June 2014 134-HYTASP-4 Integration and Evaluation Learning Center Chaired by: A. VEERARAVAGAN and G. JOHNSTON, Infotech Enterprises 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs AIAA-2014-2506 AIAA-2014-2507 Oral Presentation AIAA-2014-2508 AIAA-2014-2509 AIAA-2014-2510 AIAA-2014-2511 Characterization of a heterodyne Heat Transfer Measurements On New Range Safety Display for Acoustic Interferometry and the Application of CE/SE Method to Investigation of Strut-based RBCC Experimental research on thermal LITA setup for simultaneous flow Waverider at Hypersonic Mach Launch Operation using Real-Time Calibration Integral Equation Study Hypersonic Non-equilibrium Engine Configuration to Improve vibration characteristics of wing velocity and speed of sound Numbers Impact Point Dispersion Method for Inverse Heat Flows over Spheres Performance in Ramjet Mode structure for high-speed flight vehicles measurements N. Kanderpalli, S. Selvaraj, J. Gopalan, Y. Nam, T. Seong, J. Ahn, Korea Advanced Conduction H. Shen, C. Wen, H. Saldívar Massimi, W. Ya Jun, L. Jiang, Q. Fei, H. Guo Qiang, in high-temperature environment F. Förster, B. Weigand, University of K. Reddy, Indian Institute of Science, Institute of Science and Technology, J. Frankel, D. Bottländer, University of Hong Kong Polytechnic University, Hong W. Xiang Geng, L. Xiang, Northwestern D. Wu, Y. Wang, S. Zhao, B. Pan, S. Wu, Stuttgart, Stuttgart, Germany Bangalore, India Daejeon, South Korea Tennessee, Knoxville, Knoxville, TN Kong, Hong Kong Polytechnical University, Xi’an, China Beihang University, Beijing, China Tuesday, 17 June 2014 135-FC-8/APA-24 Aerodynamic Flow Control Lenox Chaired by: E. WHALEN, Boeing Engineering Operations & Technology and S. ANDERS, NASA LARC 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs AIAA-2014-2512 AIAA-2014-2513 AIAA-2014-2514 AIAA-2014-2515 AIAA-2014-2516 AIAA-2014-2517 AIAA-2014-2518 Numerical and Experimental Wind On the Effect of Sweep on Control of laminar separation on Optimal Design of Active Flow Reduced Order Modeling of Flow A Generalized Reduced-Order Experimental research on the Tunnel and Flight Testing of Active Separation Control airfoils using dynamic roughness Control for a Complex High-Lift over a NACA 0015 Airfoil For Model of Flow around an Airfoil effects of stator trailing edge Flow Control for Modified NACA P. Tewes, L. Taubert, I. Wygnanski, A. Rothmayer, Iowa State University, Configuration Control Application with Circulation Control blowing with variable stator on 643 − 618 Airfoil University of Arizona, Tucson, Tucson, AZ Ames, IA; W. Huebsch, West Virginia A. Nemili, E. Özkaya, N. Gauger, RWTH E. Caraballo, T. Sullivan, Miami University, R. Semaan, Y. El Sayed, S. Sattler, K. the reduction of stator/rotor J. Dianics, D. Ohno, S. Fuggmann, J. Lay, University, Morgantown, WV Aachen University, Aachen, Germany; Oxford, OH; J. Little, University of Arizona, Sultana, M. Burnazzi, P. Scholz, Technical interaction noise D. Heim, H. Fasel, University of Arizona, F. Kramer, T. Hoell, F. Thiele, Technical Tucson, Tucson, AZ University of Braunschweig, Braunschweig, W. Wang, T. Wang, Beihang University, Tucson, Tucson, AZ University of Berlin, Berlin, Germany Germany; et al. Beijing, China Tuesday, 17 June 2014 136-AMT-5/GT-4 Imaging Methods Marietta Chaired by: P. LAVOIE, University of Toronto and J. WEHRMEYER, Aerospace Testing Alliance (ATA) 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2014-2519 AIAA-2014-2520 AIAA-2014-2521 AIAA-2014-2522 AIAA-2014-2523 AIAA-2014-2524 Application of Stereoscopic Imaging Preliminary Investigation of Three- Visualization of flow separation Application of a Novel Projection Free flight measurement technique Development of a diode-pumped in Aerospace Ground Testing Dimensional Flame Measurements around an atmospheric re-entry Focusing Schlieren System in NASA in shock tunnel 100-ms quasi-continuous burst- B. Winkleman, K. Scott, G. Beitel, T. with a Plenoptic Camera capsule at low-subsonic Mach number Test Facilities B. Martinez, M. Bastide, P. Wey, French- mode laser for high-speed VanPelt, Aerospace Testing Alliance, Arnold J. Bolan, K. Johnson, B. Thurow, Auburn using Background-Oriented Schlieren A. Fagan, NASA Glenn Research Center, German Research Institute of Saint-Louis combustion diagnostics AFB, TN; B. Weaver, M. Conner, U.S. Air University, Auburn, AL (BOS) Cleveland, OH; D. L’Esperance, Metrolaser, (ISL), Saint-Louis, France J. Miller, J. Gord, Air Force Research Force, Arnold AFB, TN T. Mizukaki, Tokai University, Tokyo, Japan; Inc., Laguna Hills, CA; K. Zaman, NASA Laboratory, Wright-Patterson AFB, OH; T. S. Borg, P. Danehy, NASA Langley Research Glenn Research Center, Cleveland, OH Meyer, Iowa State University, Ames, IA;

76 Center, Hampton, VA; S. Murman, NASA Ames M. Slipchenko, J. Mance, S. Roy, Spectral Research Center, Moffett Field, CA Energies, LLC, Dayton, OH Tuesday, 17 June 2014 137-AMT-6/GT-5 Spectroscopic Temperature Measurement Piedmont Chaired by: B. BATHEL, NASA Langley Research Center and C. GOYNE, University of Virginia 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs AIAA-2014-2525 AIAA-2014-2526 AIAA-2014-2527 AIAA-2014-2528 AIAA-2014-2529 WIDECARS Measurements of High-Speed Imaging Optical Laser-Induced Gratings Rotational Temperature Molecular Rayleigh scattering to Major Species Concentration and Pyrometry for Study of Boron Measurements in Compressible, Measurement in an Arc-Heated measure fluctuations in density and Temperature Measurements in an Nitride Nanotube Generation High-Speed Free Jets Wind Tunnel by Laser Induced temperature in low speed heated Air-Ethylene Flame J. Inman, P. Danehy, S. Jones, J. Lee, J. Kuehner, A. Conlon, D. Rodriguez Fluorescence of Nitric Oxide wind tunnel flows E. Gallo, L. Cantu, A. Cutler, George NASA Langley Research Center, Hampton, Segura, X. Yang, Washington and Lee A-X(0,0) J. Panda, NASA Ames Research Center, Washington University, Washington, DC; H. VA University, Lexington, VA M. Kirschner, T. Sander, C. Mundt, Moffett Field, CA; S. Schery, Aerospace Chelliah, M. Rahimi, University of Virginia, University of the German Federal Armed Computing, Inc., Mountain View, CA Charlottesville, Charlottesville, VA Forces, Neubiberg, Germany Tuesday, 17 June 2014 138-HYTASP-5 Vehicle, Mission, and Trajectory Regency Ballroom V Chaired by: I. JAHN, The University of Queensland and B. MCGRATH, JHU/Applied Physics Laboratory 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs AIAA-2014-2530 AIAA-2014-2531 AIAA-2014-2532 AIAA-2014-2533 AIAA-2014-2534 Preliminary Design of a New Hybrid Investigation of Structure, Design and full 3D nose-to-tail L1 Augmentation Configuration for Effect of Initial Flight Path Angle and Technology Innovative Suborbital Thermal Protection System, and computation of a turbofan+ a Lateral/Directional Manoeuvre of Error and Control Constraint on the Vehicle for Space Tourism Passenger Stage Integration for scramjet Mach 8 civil aircraft a Hypersonic Glider in the Presence Optimized Ascent Trajectory of a C. Frank, J. Durand, Georgia Institute of the Hypersonic Transport System S. Defoort, M. Ferrier, L. Serre, ONERA, of Uncertainties Typical Launch Vehicle Technology, Atlanta, GA; H. Evain, C. Tyl, SpaceLiner Palaiseau, France S. Banerjee, M. Creagh, R. Boyce, A. Joshi, B. Sudhir Kumar, Indian Institute F. Mechentel, A. Brunet, University of A. Kopp, N. Garbers, German Aerospace University of Queensland, Brisbane, of Technology Mumbai, Mumbai, India Toulouse, Toulouse, France; et al. Center (DLR), Bremen, Germany Australia Tuesday, 17 June 2014 139-PANEL-4 Panel: FAA Has Selected the UAS Test Sites - What Happens Next? Regency Ballroom VI 1400 - 1600 hrs Moderator: Rich Christiansen, Vice President, Sierra Lobo, Inc. Panelists: Ro Bailey Ray Young Rose Mooney Lusi Cifuentes Elizabeth Soltys Al Palmer Thomas Wilczek Director Technical Director, NUAIR Executive Director, Mid-Atlantic Vice President, Division of Research Program Manager, FAA UAS Test Director, Center for UAS Research, Education Aerospace & Defense Industry Pan-Pacific UAS Test Range Complex Aviation Partnership Commercialization and Outreach Sites and Training for John D. Odegard School of Liaison, Governor’s Office of Economic Texas A&M University Aerospace Sciences Development, Nevada UAS Test Site University of North Dakota

77 Tuesday, 17 June 2014 140-AMT-7/PDL-10 Diagnostics II Roswell Chaired by: R. MILES, Princeton University and J. POGGIE, USAF AFRL/RBAC 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs AIAA-2014-2535 AIAA-2014-2536 AIAA-2014-2537 AIAA-2014-2538 AIAA-2014-2539 The combined use of the Schlieren Experimental Setup for Vacuum Aerothermodynamic Investigation Rayleigh and Thomson Scattering Characterization of an Electron effect and the absorption Ultraviolet Spectroscopy for Earth of Inductively Heated CO2 Plasma Diagnostics of Laser Air Sparks: A Gun Based on a Pseudospark for spectroscopy for the velocimetry of Re-entry Testing Flows for Mars Entry Testing Testbed for Tailoring Laser Plasmas Application in Hypersonic Shock supersonic and hypersonic flows T. Hermann, University of Stuttgart, T. Marynowski, S. Loehle, S. Fasoulas, A. C. Limbach, R. Miles, Princeton University, Tunnels D. Machado, Technological Institute of Stuttgart, Germany; F. Zander, University Meindl, F. Zander, University of Stuttgart, Princeton, NJ A. Guimarães, Technological Institute of Aeronautics (ITA), São José dos Campos, of Queensland, Saint Lucia, Australia; H. Stuttgart, Germany Aeronautics (ITA), São José dos Campos, Brazil; A. Oliveira, D. Carinhana, Institute Fulge, S. Loehle, S. Fasoulas, University of Brazil; D. Carinhana, A. Oliveira, Institute for Advanced Studies, São José dos Stuttgart, Stuttgart, Germany for Advanced Studies, São José dos Campos, Brazil Campos, Brazil Tuesday, 17 June 2014 141-AFM-11 Launch Vehicle, Missile, and Projectile Flight Dynamics Spring Chaired by: M. XIN, University of Missouri and F. FRESCONI, US Army Research Lab 1400 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs No Presentations AIAA-2014-2540 AIAA-2014-2541 AIAA-2014-2542 AIAA-2014-2543 Advanced Optical Sensor Nonlinear Stability Analysis Pressure/Temperature Solution of Lambert’s Theorem with Technology: Launch Vehicle and Methods for Guided Artillery Measurement of a Free-Flight Additional Terminal Constraints Spacecraft Applications Projectiles Object by PSP/TSP K. Kaliranjan, A. Joshi, Indian Institute of J. Orr, L. Trevino, C. Dalton, Draper M. Gross, J. Rogers, M. Costello, Georgia M. Ishii, National Research Institute Technology Bombay, Mumbai, India Laboratory, Huntsville, AL Institute of Technology, Atlanta, GA; F. of Police Science, Kashiwa, Japan; Y. Fresconi, Army Research Laboratory, Yamada, T. Miyazaki, University of Aberdeen Proving Ground, MD Electro-Communications, Chofu, Japan; H. Sakaue, Japan Aerospace Exploration Agency (JAXA), Chofu, Japan Tuesday, 17 June 2014 142-TP-9 Nonequilibrium Flows I Techwood Chaired by: B. CRUDEN, NASA-Ames Research Center and P. OOSTHUIZEN, Queen’s University 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2014-2544 AIAA-2014-2545 AIAA-2014-2546 AIAA-2014-2547 AIAA-2014-2548 AIAA-2014-2549 A Direct Simulation Monte Carlo Spectroscopic Investigation on Object-Oriented/Data-Oriented Non-Boltzmann Analysis of Experimental Study on Heat Flux Numerical Rebuilding of Shock Collision Limiter Scheme for Anomalous Heating in Free Piston Design of a Direct Simulation Hypersonic Air Re-Entry Flows Augmentation in High-enthalpy Tube Experiments in CO2 Flow Efficient Simulation of Viscous Shock Tunnel HIEST Monte Carlo Algorithm B. Lopez, M. Lino Da Silva, Technical Shock Tunnels under Conditions Relevant for Mars Continuum Flows S. Nomura, H. Takayanagi, K. Fujita, D. Liechty, NASA Langley Research Center, University of Lisbon, Lisbon, Portugal H. Tanno, T. Komuro, Japan Aerospace Entry Probes J. Burt, E. Josyula, Air Force Research Japan Aerospace Exploration Agency Hampton, VA Exploration Agency (JAXA), Kakuda, P. Noeding, Astrium, Bremen, Germany; Laboratory, Wright-Patterson AFB, OH (JAXA), Chofu, Japan; H. Tanno, T. Japan; N. Ohnishi, T. Ishihara, Y. Ogino, K. J. Martinez Schramm, German Aerospace Komuro, K. Itoh, Japan Aerospace Sawada, Tohoku University, Sendai, Japan Center (DLR), Göttingen, Germany Exploration Agency (JAXA), Kakuda, Japan Tuesday, 17 June 2014 143-TP-10 Heat Transfer Enhancement and Energy Harvesting II University Chaired by: T. OTANICAR 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs AIAA-2014-2550 AIAA-2014-2551 AIAA-2014-2552 AIAA-2014-2553 AIAA-2014-2129 Enhanced Convective Heat Transfer Effect of Heat Extraction from a A Validation of the Thermo-Fluid Natural Convection in an Enclosure Finite Element Method Based in Enclosures with Internal Heat Photovoltaic Module by Natural Characteristics for Laminated Screens with Micro Encapsulated Phase Model to Solve Three Dimensional Sinks and Forced Air Circulation with and Woven Copper Wire Mesh Enhancing Change Material: Experimental and Heat Conduction Equations for H. Wan, S. Patnaik, Air Force Research without Pre-Cooling of Air the Regenerative Compact Heat Numerical Study Photovoltaic Modules Laboratory, Wright-Patterson AFB, OH T. Hitchcock, M. Akbar, Tennessee State Exchanger Heat Transfer Areas Y. Khakpour, J. Seyed-Yagoobi, Worcester M. Akbar, T. Hitchcock, Tennessee State University, Nashville, TN F. Senda, South African Nuclear Energy Polytechnic Institute, Worcester, MA University, Nashville, TN

78 Corporation, Brits District, South Africa; R. Dobson, University of Stellenbosch, Stellenbosch, South Africa Tuesday, 17 June 2014 144-AFM-12 Flight Test and System Identification Vinings Chaired by: J. GRAUER, NASA Langley Research Center and N. FEZANS, DLR 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2014-2554 AIAA-2014-2555 AIAA-2014-2556 AIAA-2014-2557 AIAA-2014-2558 AIAA-2014-2559 Real-Time Onboard Global Aspects of Autonomous Recovery Real-Time Parameter Estimation Aerodynamic Parameter Estimation Aerodynamic Modeling and Flight Path Reconstruction Nonlinear Aerodynamic Modeling System for High Altitude Payloads using Output Error of a Missile Without Wind Angle Parameter Estimation of a Techniques Applied to Spin Tests from Flight Data by Using a Parafoil J. Grauer, NASA Langley Research Center, Measurements Quadrotor Helicopter J. Dias, Brazilian Air Force, São José dos J. Brandon, E. Morelli, NASA Langley S. Lee, J. Conner, A. Arena, Oklahoma Hampton, VA A. Aksu, ROKETSAN Missiles Industries, D. Kaya, A. Kutay, Middle East Technical Campos, Brazil Research Center, Hampton, VA State University, Stillwater, OK Inc., Ankara, Turkey University, Ankara, Turkey Tuesday, 17 June 2014 145-NW-5 Tuesday Afternoon Networking Coffee Break Exhibit Hall 1530 - 1600 hrs Tuesday, 17 June 2014 146-LEC-2 William Littlewood Memorial Lecture Centennial I/II 1730 - 1830 hrs

Future Aviation Challenges Axel Krein Senior Vice President, Airbus, UK France Sponsored by Airbus Tuesday, 17 June 2014 147-PDL-13 Special Panel Session on Future Directions in Plasma Aerodynamics Embassy A 1730 - 1830 hrs Moderator: Jonathan Poggie, Lead, High-Speed Flow Research Group, AFRL/RQHF Panelists: Lon Enloe Sergey Leonov Sergey Macheret Tom McLaughlin Richard B. Miles Jonathan Poggie Mo Samimy Julian Tishkoff United States Air Force Academy Ohio State University Lockheed Martin Corporation United States Air Force Academy Princeton University Air Force Research Laboratory (AFRL) Ohio State University Air Force Office of Scientific Research (AFOSR)

Tuesday, 17 June 2014 148-NW-6 Reception in the Exhibit Hall Exhibit Hall 1830 - 2000 hrs Wednesday Wednesday, 18 June 2014 149-NW-7 Wednesday Morning Networking Breakfast Ballroom Level 0700 - 0800 hrs Wednesday, 18 June 2014 150-SB-3 Wednesday Morning Speakers’ Briefing Session Rooms 0730 - 0800 hrs Wednesday, 18 June 2014 151-PLNRY-3 Wednesday Morning Plenary Panel Centennial I/II 79 0800 - 0900 hrs Moderator: Trevor Stansbury, President, Supply Dynamics Global Supply Chain Challenges and Opportunities Panelists: Duane Hawkins Fred Ross Senior Vice President, Supply Chain Vice President F-35 Supply Chain Management Spirit AeroSystems Lockheed Martin Aeronautics

Wednesday, 18 June 2014 152-NW-8 Wednesday Morning Networking Coffee Break Exhibit Hall 0900 - 0930 hrs Wednesday, 18 June 2014 153-APA-25 Flow Control (Active and Passive): Computational and Experimental Results IV Baker Chaired by: C. BIDWELL, NASA Glenn Research Center 0930 hrs 1000 hrs 1030 hrs AIAA-2014-2560 AIAA-2014-2561 AIAA-2014-2562 Experimental Investigation of Experimental Investigation of Active Control of Unsteady Aerodynamic a Vortex-Generator-Controlled Aerodynamic Load Reduction on a Loads Using Adaptive Blowing Intermediate Turbine Duct under Rotorcraft Fuselage with Rotor Effects H. Mueller-Vahl, Technion--Israel Institute the Influence of Rotating Wakes N. Schaeffler, B. Allan, NASA Langley Research of Technology, Haifa, Israel; C. Nayeri, C. M. Steiner, E. Göttlich, A. Marn, F. Center, Hampton, VA; O. Wong, P. Tanner, Paschereit, Technical University of Berlin, Heitmeier, Graz University of Technology, Joint Research Program Office, Hampton, VA Berlin, Germany; D. Greenblatt, Technion-- Graz, Austria Israel Institute of Technology, Haifa, Israel Wednesday, 18 June 2014 154-APA-26 Aerodynamic Testing: Flight, Wind Tunnel and Numerical Correlations III Courtland Chaired by: D. O’BRIEN, US Army RDECOM and B. CYBYK, JHU/Applied Physics Laboratory 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2014-2563 AIAA-2014-2564 AIAA-2014-2565 AIAA-2014-2566 AIAA-2014-2567 Low-speed Aerodynamic Force and flowfield measurements High-Frequency Sensor Data Evaluating Propulsor Mechanical A Flight-to-Ground Extrapolation Investigations of a Hybrid Wing of a bio-inspired flapping MAV Acquisition System (SDAC) for Flow Power in Powered Aircraft Methodology for Subsonic Plasma Body Configuration ‘Delfly Micro’ Flight Control and Aerodynamic Wind Tunnel Experiments Windtunnels and Its Validation by D. Vicroy, G. Gatlin, L. Jenkins, P. Murphy, S. Deng, M. Percin, B. van Oudheusden, Data Collection N. Siu, N. Titchener, A. Uranga, E. Greitzer, Real Flight Experiment QARMAN NASA Langley Research Center, Hampton, B. Remes, Delft University of Technology, O. Dantsker, R. Mancuso, M. Selig, M. Massachusetts Institute of Technology, I. Sakraker, O. Chazot, von Kármán VA Delft, The Netherlands; A. Tenaglia, Caccamo, University of Illinois, Urbana- Cambridge, MA Institute for Fluid Dynamics, Rhode-Saint- University of Pisa, Pisa, Italy Champaign, Urbana, IL Genèse, Belgium Wednesday, 18 June 2014 155-APA-27 Special Session: 2nd High-Lift Prediction Workshop II Dunwoody Chaired by: R. RUDNIK, DLR - German Aerospace Center and K. HUBER 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2014-2568 AIAA-2014-2569 AIAA-2014-2570 AIAA-2014-2571 Aerodynamic analysis of the 2nd High Lift flow computations using Parallel Adaptive Detached Eddy CFD Investigations of the High Lift Prediction Workshop by a the code HiFUN Simulations of the EUROLIFT HiLiftPW-2 Configuration with the Lattice-Boltzmann Method solver B. Narayanarao, N. Gopalakrishna, DLR-F11 high lift configuration MFlow Solver D. Holman, R. Brionnaud, M. Modena, Indian Institute of Science, Bangalore, M. Rasquin, Argonne National Laboratory, J. Chen, Y. Deng, N. Zhou, Y. Zhang, China Next Limit Technologies, Madrid, Spain India; Y. Patil, K. Ravindra, N. Shende, Argonne, IL; K. Chitale, Rensselaer Polytechnic Aerodynamics Research and Development S&I Engineering Solutions Pvt., Ltd., Institute, Troy, NY; M. Ali, K. Jansen, University Center, Mianyang, China Bangalore, India of Colorado, Boulder, Boulder, CO 80 Wednesday, 18 June 2014 156-APA-28 Aerodynamic Analysis and Design: CFD Methods I Edgewood Chaired by: P. MORGAN, Ohio Aerospace Institute and N. HARIHARAN, CREATE-AV 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2014-2572 AIAA-2014-2573 AIAA-2014-2574 AIAA-2014-2575 AIAA-2014-2576 Defect Correction and Error Exergy-based Aircraft Airfoil Stall Simulations with Thermal lattice Boltzmann Adjoint-Based Error Estimation and Transport Discretization Error Aeropropulsive Performance Algebraic Delayed DES and simulation with immersed solid Mesh Adaptation for Problems with Estimation for Applications in CFD Assessment: CFD Application to Physically Based Synthetic boundary model Output Constraints T. Phillips, C. Roy, Virginia Polytechnic Institute Boundary Layer Ingestion Turbulence for RANS-LES Transition G. Thandavamoorthy, P. Sagaut, Pierre and B. Rothacker, M. Ceze, K. Fidkowski, and State University, Blacksburg, VA A. Arntz, O. Atinault, D. Destarac, ONERA, D. François, R. Radespiel, Technical Marie Curie University, Paris, France; D. University of Michigan, Ann Arbor, Ann Meudon, France; A. Merlen, ONERA, University of Braunschweig, Braunschweig, Ricot, Renault, Guyancourt, France Arbor, MI Palaiseau, France Germany; A. Probst, German Aerospace Center (DLR), Göttingen, Germany Wednesday, 18 June 2014 157-ATIO-13 Transformational Flight - Electric Propulsion Development and Testing Embassy C Chaired by: B. GERMAN, Georgia Institute of Technology and M. MOORE, NASA Langley Research Center 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs Oral Presentation Oral Presentation Oral Presentation Oral Presentation Oral Presentation Enabling Electric Propulsion for Flight Design of the Hybrid Electric Lightweight Small-Scale Turbine A Small Heavy Fuel Engine for use Design and Testing of a Dual S. Clarke, Y. Lin, K. Kloesel, S. Ginn, NASA Integrated System Testbed Generators as a Flight Capable Lightweight Halbach Array Motor-Generator Dryden Flight Research Center, Edwards, CA T. Foster, A. Gibson, B. Schiltgen, Empirical R. Keogh, G. Thomas, Metis Design Electric APU Range Extender M. Ricci, LaunchPoint Technologies, Inc., Systems Aerospace, Inc., Pismo Beach, CA Corporation, San Francisco, CA G. Stevenson, GSE, Inc., South Lake Goleta, CA Tahoe, CA Wednesday, 18 June 2014 158-FT-4 Flight Test Operations Embassy D Chaired by: J. BRANDON, NASA-Langley Research Center and K. GARMAN, Federal Aviation Administration 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2014-2577 AIAA-2014-2578 AIAA-2014-2579 AIAA-2014-2580 AIAA-2014-2581 Flight Test Evaluation and System Evaluation of functional coatings Recent and Ongoing Hypersonic, Flight Tests of ASELPOD-New Fast and light acoustic flight test Identification of the Area-I for laminar flow applications on Space Transit, and Space Launch Generation Targeting Pod measurements in aircraft Prototype-Technology-Evaluation future business jets through ground Flight Tests B. Gokce, I. Koc, Y. Eldogan, O. Ozturk, E. Helffer, O. Deille, J. Briand, O. Research Aircraft (PTERA) and flight testing T. Jorris, U.S. Air Force, Edwards AFB, CA ASELSAN, Inc., Ankara, Turkey Delverdier, Airbus, Toulouse, France D. Kuehme, N. Alley, C. Phillips, Area-I, B. Berton, J. Courty, Dassault Group, Kennesaw, GA; B. Cogan, NASA Dryden Paris, France; M. Kok, E. Tobin, T. Young, Flight Research Center, Edwards, CA University of Limerick, Limerick, Ireland Wednesday, 18 June 2014 159-ATIO-14 ATM-V Benefit Analysis of ATM Embassy E Chaired by: J. POST, Federal Aviation Administration 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2014-2582 AIAA-2014-2583 AIAA-2014-2584 AIAA-2014-2585 AIAA-2014-2586 AIAA-2014-2587 Cloud Computing for Air Traffic Benefits Analysis of Wind-Optimal Benefits Analysis of Multi-Center Computer Simulation Model to Throughput Benefit Assessment Annualizing Throughput Benefits Management - Cost/Benefit Operations For Trans-Atlantic Flights Dynamic Weather Routes Measure Benefits of North Atlantic for Tactical Runway Configuration at Newark Airport using a New Analysis B. Sridhar, NASA Ames Research Center, K. Sheth, D. McNally, NASA Ames Data link Mandates and Reduced Management (TRCM) Approach to Converging Runway L. Ren, B. Beckmann, T. Citriniti, M. Moffett Field, CA; H. Ng, University of Research Center, Moffett Field, CA; A. Separation Minima N. Phojanamongkolkij, R. Oseguera-Lohr, Operations Castillo-Effen, General Electric Company, California, Santa Cruz, Santa Cruz, CA; F. Morando, A. Clymer, J. Lock, J. Petersen, A. Gunnam, GRA, Inc., Washington, DC; G. Lohr, NASA Langley Research Center, P. Lee, H. Idris, San Jose State University, Niskayuna, NY; D. Kulkarni, NASA Ames Linke, German Aerospace Center (DLR), University of California, Santa Cruz, A. Trani, T. Li, Virginia Polytechnic Institute Hampton, VA; J. Fenbert, Analytical San Jose, CA; N. Smith, NASA Ames Research Center, Moffett Field, CA Hamburg, Germany; N. Chen, NASA Ames Moffett Field, CA; et al. and State University, Blacksburg, VA; T. Mechanics Associates, Inc., Hampton, VA Research Center, Moffett Field, CA

81 Research Center, Moffett Field, CA Graham, N. Campos, Federal Aviation Administration, Washington, DC Wednesday, 18 June 2014 160-ACD-7 Stability and Control Considerations in Aircraft Design Embassy F Chaired by: W. ANEMAAT, DARcorporation and N. HALL, Lockheed Martin Corporation 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2014-2588 AIAA-2014-2589 AIAA-2014-2590 AIAA-2014-2591 AIAA-2014-2592 Gust rejection using force adaptive Handling Quality of Aircraft An Adaptive Aeroelastic Control Wake Identification Based Wake Stability and Control Effects on the feedback for roll Equipped with Sidesticks Approach using Non Linear Impact Alleviation Control Design Optimization of a Box-Wing L. Castano, J. Humbert, University of L. Zaichik, Y. Yashin, P. Desyatnik, K. Reduced Order Models J. Ehlers, D. Fischenberg, D. Niedermeier, Aircraft Maryland, College Park, College Park, Grinev, V. Perebatov, TsAGI, Zhukovsky, N. Tantaroudas, University of Liverpool, German Aerospace Center (DLR), S. Andrews, R. Perez, Royal Military MD; T. McKenna, Aurora Flight Sciences, Russia Liverpool, United Kingdom; A. Da Ronch, Braunschweig, Germany College of Canada, Kingston, Canada McLean, VA University of Southampton, Southampton, United Kingdom; G. Gai, K. Badcock, University of Liverpool, Liverpool, United Kingdom Wednesday, 18 June 2014 161-MAO-9 Multidisciplinary Analysis and Optimization: Shape and Topology Method Development Embassy G Chaired by: J. HICKEN, Rensselaer Polytechnic Institute 0930 hrs 1000 hrs 1030 hrs AIAA-2014-2593 AIAA-2014-2594 AIAA-2014-2595 Topology Optimisation: Increasing Strategies for Solving High-Fidelity Robust Optimizations of Structural the Speed and Reliability of Design Aerodynamic Shape Optimization and Aerodynamic Designs L. Kelly, A. Keane, A. Sobester, D. Toal, Problems K. Boopathy, M. Rumpfkeil, University of University of Southampton, Southampton, Z. Lyu, J. Martins, University of Michigan, Dayton, Dayton, OH United Kingdom Ann Arbor, Ann Arbor, MI Wednesday, 18 June 2014 162-APA-29 Special Session: Aerodynamic-Structural Modeling, Optimization, and Test Techniques for Flexible Wing Technology II Fairlie Chaired by: N. NGUYEN, NASA-Ames Research Center and S. ANDERS, NASA LARC 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2014-2596 AIAA-2014-2597 AIAA-2014-2598 AIAA-2014-2599 Trim and Structural Optimization Flight Performance Analysis of the Aerodynamic and Static Deflection A Model of Fluid-Structure- of Subsonic Transport Wings using Truss-Braced Wing Aircraft Analysis of a Flexible Wing Aircraft Interaction for Impulsively Started Nonconventional Aeroelastic K. Reynolds, E. Ting, N. Nguyen, NASA With Distributed Propulsion Spanwise-Flexible Wings Tailoring Ames Research Center, Moffett Field, CA A. Tsoi, University of Colorado, Boulder, M. Jain, Technical University of Darmstadt, B. Stanford, NASA Langley Research Boulder, CO; K. Reynolds, N. Nguyen, NASA Darmstadt, Germany; J. Wong, D. Rival, Center, Hampton, VA Ames Research Center, Moffett Field, CA University of Calgary, Calgary, Canada Wednesday, 18 June 2014 163-FD-14 New Frontiers of Fluid Dynamics: Multiphase Flows (Invited) Greenbriar Chaired by: D. BODONY, University of Illinois at Urbana-Champaign 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs Oral Presentation Oral Presentation Oral Presentation Oral Presentation Oral Presentation Oral Presentation AFOSR Turbulence and Transition Numerical simulations of gas-liquid Towards Large Eddy Simulation of Spray Combustion and Large Eddy Nanofluid Fuels - Liquid Fuels with Recent developments in Program Overview interfaces in compressible flows: Turbulent Liquid Atomization Simulation Stable Suspensions of Nanoparticles compressible multiphase flows C. Li, Air Force Office of Scientific shock waves, droplets and bubbles O. Desjardins, Cornell University, Ithaca, V. Raman, University of Texas, Austin, L. Qiao, S. Tanvir, Purdue University, West B. Balachandar, University of Illinois, Research, Arlington, VA E. Johnsen, M. Henry de Frahan, S. Alahyari NY Austin, TX Lafayette, IN Urbana-Champaign, Urbana, IL Beig, University of Michigan, Ann Arbor, MI Wednesday, 18 June 2014 164-AA-10 Jet Noise Prediction I Hanover A 82 Chaired by: C. TAM, Florida State Univeristy 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2014-2600 AIAA-2014-2601 AIAA-2014-2602 AIAA-2014-2603 AIAA-2014-2604 AIAA-2014-2605 Influence of nozzle-exit boundary- Unstructured Large Eddy Accurate and Efficient Jet Flow and RANS/CAA based Prediction of Jet Numerical Study of Noise The Effect of Base-Flow Changes layer profile on high-subsonic jets Simulations for Nozzle Interior Noise Simulations Using the CDE Mixing Noise in Cruise Flight Sources Characteristics in An on Kelvin-Helmholtz Instability and C. Bogey, O. Marsden, École Centrale de Flow Modeling and Jet Noise (Compact Disturbance Equations) C. Appel, A. Klabes, K. Rossignol, M. Underexpanded Jet Flow Noise Radiation in Jets Lyon, Ecully, France Predictions Y. Du, P. Morris, Pennsylvania State Herr, German Aerospace Center (DLR), J. Liu, A. Corrigan, K. Kailasanath, Naval E. Kay, A. Agarwal, University of Cambridge, G. Brès, S. Bose, F. Ham, Cascade University, University Park, PA Braunschweig, Germany Research Laboratory, Washington, DC; N. Cambridge, United Kingdom; A. Cavalieri, Technologies, Inc., Palo Alto, CA; S. Lele, Heeb, E. Gutmark, University of Cincinnati, Technological Institute of Aeronautics (ITA), Stanford University, Stanford, CA Cincinnati, OH São José dos Campos, Brazil Wednesday, 18 June 2014 165-AA-11 Propeller Noise I Hanover B Chaired by: M. KINGAN, ISVR 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2014-2606 AIAA-2014-2607 AIAA-2014-2608 AIAA-2014-2609 AIAA-2014-2610 AIAA-2014-2611 Contra-Rotating Open Rotor Tone Modeling Rotor Unsteady Forces and Boundary Layer Ingestion Noise Predicting the Tonal Noise of an Prediction of Contra-Rotating Open Influence of the noise prediction Noise Prediction Sound due to Ingestion of Spatially and Turbulence Scale Analysis at Open Rotor in a Wind Tunnel with Rotor broadband noise in isolated model on the aeroacoustic E. Envia, NASA Glenn Research Center, Inhomogeneous Turbulence High and Low Advance Ratios Acoustically Lined Walls and installed configurations optimization of a contra-rotating Cleveland, OH J. Anderson, M. Catlett, D. Stewart, Naval D. Wisda, W. Alexander, W. Devenport, P. Sureshkumar, M. Kingan, University T. Node-Langlois, F. Wlassow, V. Languille, fan Surface Warfare Center, West Bethesda, MD Virginia Polytechnic Institute and State of Southampton, Southampton, United Y. Colin, B. Caruelle, Airbus, Toulouse, G. Grasso, J. Christophe, C. Schram, T. University, Blacksburg, VA; S. Glegg, Kingdom; A. Parry, Rolls-Royce Group plc, France; J. Gill, University of Southampton, Verstraete, von Kármán Institute for Fluid Florida Atlantic University, Boca Raton, FL Derby, United Kingdom Southampton, United Kingdom; et al. Dynamics, Rhode-Saint-Genèse, Belgium Wednesday, 18 June 2014 166-ASE-9 3-D Model Design and Ice Measurement Methods for Experimental Icing Simulation Hanover C Chaired by: J. TSAO, Ohio Aerospace Institute and B. WOODARD, University of Illinois 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2014-2612 AIAA-2014-2613 AIAA-2014-2614 AIAA-2014-2615 AIAA-2014-2616 AIAA-2014-2617 Ice Shapes on a Tail Rotor Implementation and Validation of Validation of 3-D Ice Accretion Validation of 3-D Ice Accretion 3D Swept Hybrid Wing Design Large-Scale Swept-Wing Icing R. Kreeger, NASA Glenn Research Center, 3-D Ice Accretion Measurement Measurement Methodology for Measurement Methodology Using Method for Icing Wind Tunnel Tests Simulations in the NASA Glenn Cleveland, OH; J. Tsao, Ohio Aerospace Methodology Experimental Aerodynamic Simulation Pressure-Sensitive Paint G. Fujiwara, B. Wiberg, B. Woodard, Icing Research Tunnel Using Institute, Cleveland, OH S. Lee, Vantage Partners, LLC, Cleveland, A. Broeren, G. Addy, NASA Glenn Research M. Monastero, M. Bragg, University of M. Bragg, University of Illinois, Urbana- LEWICE3D OH; A. Broeren, R. Kreeger, M. Potapczuk, Center, Cleveland, OH; S. Lee, Vantage Illinois, Urbana-Champaign, Urbana, IL Champaign, Urbana, IL B. Wiberg, G. Fujiwara, B. Woodard, NASA Glenn Research Center, Cleveland, Partners, LLC, Cleveland, OH; M. Monastero, M. Bragg, University of Illinois, Urbana- OH; L. Utt, University of Akron, Akron, OH University of Illinois, Urbana-Champaign, Champaign, Urbana, IL Urbana, IL Wednesday, 18 June 2014 167-ASE-10/FT-5 Volcanic Ash and Aviation Hanover D Chaired by: J. MURRAY, NASA-Langley Research Center and N. KROTKOV, NASA Goddard Space Flight Center 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs Oral Presentation Oral Presentation Oral Presentation Oral Presentation AIAA-2014-2618 Oral Presentation The Airborne Volcanic Object In Situ Observations and Sampling NASA Vehicle Integrated Propulsion Development of multi-satellite Real Time Volcanic Cloud Products Dispersion and microphysical Imaging Detector (AVOID): System of Volcanic Emissions with Research (VIPR) Project - Low algorithms for global detection and and Predictions for Aviation Alerts properties of the Kasatochi volcanic description and flight-test results Unmanned Aircraft (Invited) Concentration Volcanic Ash characterization of volcanic clouds N. Krotkov, S. Habib, A. da Silva, NASA plume : a new perspective for (Invited) D. Pieri, Jet Propulsion Laboratory, Ingestion Testing (Invited) (Invited) Goddard Space Flight Center, Greenbelt, aviation safety (Invited) F. Prata, Nicarnica Aviation, Lillestrom, California Institute of Technology, J. Lekki, NASA Glenn Research Center, J. Sieglaff, University of Wisconsin, MD; E. Hughes, K. Yang, University of J. Murray, J. Vernier, NASA Langley Norway; F. Dezitter, Airbus, Toulouse, Pasadena, CA Cleveland, OH Madison, Madison, WI; M. Pavolonis, Maryland, College Park, College Park, MD; Research Center, Hampton, VA K. Brentzel, NASA Goddard Space Flight 83 France National Oceanic and Atmospheric Administration, Madison, WI Center, Greenbelt, MD; et al. Wednesday, 18 June 2014 168-AA-12 Jet Noise Reduction II Hanover E Chaired by: K. AHUJA, Georgia Institute of Technology 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2014-2619 AIAA-2014-2620 AIAA-2014-2621 AIAA-2014-2622 AIAA-2014-2623 Reduction of Radiation Efficiency in On the use of Plasma Synthetic Jets Experimental and Numerical Study Computational Study of the Effect Aero-acoustic Characteristics of High-Speed Jets for the control of jet flow and noise of Jet Noise Reduction of HBPR of Slotted Air Injection on Jet Noise Compressible Jets from Chevron D. Papamoschou, J. Xiong, F. Liu, M. Huet, ONERA, Châtillon, France Engine by Microjet Injection R. Ramamurti, A. Corrigan, J. Liu, K. Nozzle University of California, Irvine, Irvine, CA S. Enomoto, K. Yamamoto, Japan Kailasanath, Naval Research Laboratory, S. Nikam, S. Sharma, Indian Institute of Aerospace Exploration Agency (JAXA), Washington, DC; B. Henderson, NASA Technology Bombay, Mumbai, India Tokyo, Japan; M. Koenig, D. Collin, Glenn Research Center, Cleveland, OH Snecma, Moissy-Cramayel, France Wednesday, 18 June 2014 169-AA-13 Hybrid Wing Body Aeroacoustics Test II Hanover F Chaired by: M. DOTY, NASA - LARC Aeroacoustics Branch 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2014-2624 AIAA-2014-2625 AIAA-2014-2626 AIAA-2014-2627 AIAA-2014-2628 Shielding of Turbomachinery Jet Noise Shielding Provided by a Noise Scaling and Community Noise Grid Sensitivity Study for Slat Noise Numerical Assessment of Acoustic Broadband Noise from a Hybrid Hybrid Wing Body Aircraft Metrics for the Hybrid Wing Body Simulations Installation Effects Characterizing wing Body Aircraft Configuration M. Doty, T. Brooks, C. Burley, C. Bahr, Aircraft D. Lockard, M. Choudhari, P. Buning, NASA NASA/LaRC Quiet Flow Facility F. Hutcheson, T. Brooks, C. Burley, C. Bahr, NASA Langley Research Center, Hampton, C. Burley, T. Brooks, F. Hutcheson, M. Langley Research Center, Hampton, VA using Computational AeroAcoustics NASA Langley Research Center, Hampton, VA; VA; D. Pope, Analytical Services and Doty, L. Lopes, NASA Langley Research S. Redonnet, ONERA, Châtillon, France D. Stead, Northrop Grumman Corporation, Materials, Inc., Hampton, VA Center, Hampton, VA; D. Pope, Analytical Hampton, VA; D. Pope, Analytical Services and Services and Materials, Inc., Hampton, VA Materials, Inc., Hampton, VA Wednesday, 18 June 2014 170-ITAR-3 ITAR-Experimental Aero, Fluid and Thermal Sciences Hanover G Chaired by: E. GARCIA, Georgia Institute of Technology 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2014-2629 AIAA-2014-2630 AIAA-2014-2631 AIAA-2014-2632 AIAA-2014-2633 The Effect of Surface Roughness on Lean Blowout Study on the HIFiRE Investigations of a Backward- The Thermal Environment from Calibration, Validation, and CFD Predictions of HIFiRE Flight 2 Flight 2 Combustor Facing Step Flameholder For Large-scale Composite Aviation Uncertainty Analysis of a Laser- Experiment J. Liu, Taitech, Inc., Wright-Patterson Scramjet Combustor Applications Fires Based Humidity Sensor J. Liu, C. Tam, K. Lin, Taitech, Inc., Wright- AFB, OH; M. Gruber, Air Force Research C. Tam, K. Hsu, M. Gruber, Air Force A. Brown, Sandia National Laboratories, D. Plemmons, N. Galyen, A. Jackson, Patterson AFB, OH; M. Gruber, Air Force Laboratory, Wright-Patterson AFB, OH Research Laboratory, Wright-Patterson Albuquerque, NM Aerospace Testing Alliance, Arnold AFB, Research Laboratory, Wright-Patterson AFB, OH TN; R. Hutchings, MIRATEK Corporation, AFB, OH Arnold AFB, TN Wednesday, 18 June 2014 171-FD-15 Other Topics in Fluid Dynamics Harris Chaired by: N. GATSONIS, Worcester Polytechnic Institute and S. AVERKIN 0930 hrs 1000 hrs 1030 hrs AIAA-2014-2634 AIAA-2014-2635 AIAA-2014-2636 Automatic derivation of stability Simulation of Cold Nitrogen Flows Non-Equilibrium Radiative Gas equations in arbitrary coordinates in Nanonozzles with Atmospheric Dynamics of Small Meteor and for different flow regimes Inlet Pressures S. Surzhikov, Russian Academy of F. Pinna, von Kármán Institute for Fluid N. Gatsonis, S. AVerkin, Worcester Sciences, Moscow, Russia Dynamics, Rhode-Saint-Genèse, Belgium; Polytechnic Institute, Worcester, MA K. Groot, Delft University of Technology, Delft, The Netherlands 84 Wednesday, 18 June 2014 172-FD-16 Supersonic Boundary Layers: Transition Inman Chaired by: L. DUAN, Missouri University of Science and Technology 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2014-2637 AIAA-2014-2638 AIAA-2014-2639 AIAA-2014-2640 The nonlinear instability of the Flow Disturbance and Surface Effects of Forward and Backward DNS of Wave Packets in a supersonic crossflow vortex Roughness Effects on Cross-Flow Facing Steps on the Crossflow Supersonic Boundary layer: A G. Xu, G. Liu, X. Jiang, China Boundary-Layer Transition in Receptivity and Stability in Validation for a Popular Transition Aerodynamics Research and Development Supersonic Flows Supersonic Boundary Layers Prediction Method Based on Linear Center, Mianyang, China L. Owens, G. Beeler, P. Balakumar, NASA P. Balakumar, R. King, J. Eppink, NASA Stability Theory Langley Research Center, Hampton, VA; Langley Research Center, Hampton, VA C. Su, Tianjin University, Tianjin, China P. McGuire, University of California, San Diego, San Diego, CA Wednesday, 18 June 2014 173-FD-17 Hypersonic Boundary Layer Transition II Kenneshaw Chaired by: K. CASPER, Sandia National Laboratories 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2014-2641 AIAA-2014-2642 AIAA-2014-2643 AIAA-2014-2644 AIAA-2014-2645 Effect of a Normal Shock Wave The role of Görtler vortices in Measuring Transition and High-Frequency Measurements of High-temperature gas effects at a on Freestream Total Pressure the hypersonic boundary layer Instabilities in a Mach 6 Hypersonic Acoustic and Entropy Disturbances capsule under re-entry and wind- Fluctuations in a Low-Density Mach transition Quiet Wind Tunnel in a Hypersonic Wind Tunnel tunnel conditions 6 Flow J. Ren, Tsinghua University, Beijing, China; B. Chynoweth, C. Ward, S. Schneider, S. Ali, J. Wu, R. Radespiel, Technical C. Stemmer, J. Fehn, Technical University C. Mai, R. Bowersox, Texas A&M J. Liu, Tianjin University, Tianjin, China; S. Purdue University, West Lafayette, IN University of Braunschweig, Braunschweig, of Munich, Munich, Germany University, College Station, TX Fu, Tsinghua University, Beijing, China Germany; T. Schilden, W. Schroeder, RWTH Aachen University, Aachen, Germany Wednesday, 18 June 2014 174-MST-4 M&S: Vehicle Dynamics, Systems, and Environments AND Uninhabited Aircraft Systems Learning Center Chaired by: E. BURNETT, Lockheed Martin Aeronautics 0930 hrs 1000 hrs 1030 hrs AIAA-2014-2646 AIAA-2014-2647 AIAA-2014-2648 Multi-Body Large Displacement Wind Field Velocity and Acceleration Computational Improvements to Equations of Motion for Flexible Estimation Using a Small UAV Multibody Projectile Dynamics Bodies Represented as Finite M. Rhudy, Lafayette College, Easton, Simulation Element Models PA; Y. Gu, West Virginia University, M. Gross, J. Rogers, M. Costello, Georgia R. McMonagle, Northrop Grumman Morgantown, WV; H. Chao, University of Institute of Technology, Atlanta, GA Corporation, Redondo Beach, CA Kansas, Lawrence, Lawrence, KS Wednesday, 18 June 2014 175-FC-9 Flow Control: Boundary Layers Lenox Chaired by: W. HUEBSCH, West Virginia University and J. SAHU, US Army Research Laboratory 0930 hrs 1000 hrs 1030 hrs AIAA-2014-2649 AIAA-2014-2650 AIAA-2014-2651 Direct Numerical Simulation of Energy and fluid transportation in Effects of Moving Surface Riblets Geometric Effects on Turbulent turbulent boundary-layer under on a Transitional Flow affected by Flows over Riblets the micro-ramp control Adverse Pressure Gradient J. Ng, R. Jaiman, T. Lim, National B. Wang, L. Weidong, S. Mingbo, Y. Zhao, G. Campitelli, West Virginia University, University of Singapore, Singapore, National University of Defense Technology, Morgantown, WV; V. Krastev, University Singapore Changsha, China of Naples “Parthenope”, Naples, Italy; W. Huebsch, West Virginia University, Morgantown, WV 85 Wednesday, 18 June 2014 176-AMT-8/GT-6 Ground Test Facility Characterization Marietta Chaired by: J. KEGELMAN, NASA and B. MILLS 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2014-2652 AIAA-2014-2653 AIAA-2014-2654 AIAA-2014-2655 AIAA-2014-2656 AIAA-2014-2657 Characterization of the NASA Design and Calibration of the A Study of Potential Test Status of the Holloman High Speed Numerical Studies of Acoustic and Multiple Flow Regimes in a Single Langley Arc Heated Scramjet Test AEDC H3 Mach 3.0 High Heat Flux Capabilities of the NASA Langley Maglev Test Track (HHSMTT) Thermal Coupling in Sonic Fatigue Hypersonic Shock Tube Experiment Facility using NO PLIF Nozzle 0.3-Meter Transonic Cryogenic H. Gurol, D. Ketchen, L. Holland, General Tests for Hypersonic Vehicle M. Kotov, L. Ruleva, S. Solodovnikov, I. F. Kidd, V. Narayanaswamy, North Carolina G. Hammock, Aerospace Testing Alliance, Wind Tunnel Atomics, San Diego, CA; M. Hooser, D. W. Yu, S. Zhong, X. Huang, Peking Kryukov, S. Surzhikov, Russian Academy State University, Raleigh, NC; P. Danehy, J. Arnold AFB, TN B. Phillips, C. Britcher, Old Dominion Minto, 46th Test Group, Holloman AFB, University, Beijing, China of Sciences, Moscow, Russia Inman, B. Bathel, K. Cabell, NASA Langley University, Norfolk, VA NM; N. Bosmajian, The Boeing Company, Research Center, Hampton, VA; et al. Seal Beach, CA; et al. Wednesday, 18 June 2014 177-AMT-9/GT-7 Developments in Particle Image Velocimetry Piedmont Chaired by: V. NARAYANASWAMY, North Carolina State Univ and J. WAGNER, Sandia National Laboratories 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2014-2658 AIAA-2014-2659 AIAA-2014-2660 AIAA-2014-2661 AIAA-2014-2662 Hierarchy of Hybrid Unsteady-Flow Time Resolved High Dynamic Self-Calibration Performance in PIV in the Trisonic GasDynamics Modeling the Effect of Refraction Simulations Integrating Time- Range PIV using Local Uncertainty Stereoscopic PIV Acquired in a Facility at a Flat Interface on Plenoptic Resolved PIV/PTV with Unsteady Estimation Methods Transonic Wind Tunnel M. Liber, M. Reeder, D. Wolfe, Air Force Particle Reconstruction CFD T. Persoons, Trinity College Dublin, Dublin, S. Beresh, J. Wagner, B. Pruett, J. Institute of Technology, Wright-Patterson C. Thomason, T. Fahringer, K. Johnson, B. F. Yamamoto, T. Suzuki, University of Ireland Henfling, R. Spillers, Sandia National AFB, OH; R. Schmit, B. Hagen, Air Force Thurow, Auburn University, Auburn, AL Fukui, Fukui, Japan Laboratories, Albuquerque, NM; B. Smith, Research Laboratory, Wright-Patterson Utah State University, Logan, UT AFB, OH Wednesday, 18 June 2014 178-HYTASP-19 Culpepper Lecture Regency Ballroom V 0930 - 1030 hrs Chaired by: A. SIEBENHAAR, Aerojet Rocketdyne

Hooray for Ray In memory of the Australian Hypersonics Pioneer Ray Stalker Richard Morgan Australia Wednesday, 18 June 2014 179-LEC-5 Aviation Noise and Emissions Reduction: Challenges and Opportunities Regency Ballroom VI 0930 - 1130 hrs Carl Burleson Dragos Preda Assistant Administrator for Policy, International Affairs and Environment, Federal Aviation Administration Head of Flight Operations Data Management Office, TAROM

Wednesday, 18 June 2014 180-FC-10/PDL-11 Plasma-Based Flow Control II Roswell Chaired by: D. RIZZETTA, USAF and N. HARADA, Nagaoka University of Technology 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2014-2663 AIAA-2014-2664 AIAA-2014-2665 AIAA-2014-2666 Effective Mechanisms for Turbulent- Delay of Finite-Span Excrescence- Control of Separated Flow on a Exploratory Investigation of separation Control by DBD Plasma Induced Transition Using Plasma- NACA 0015 Airfoil using Three- Asymmetric Control of a Supersonic Actuator around NACA0015 at Based Control Dimensional Plasma Actuator Round Jet via Plasma Actuation 86 Reynolds Number 1,600,000 D. Rizzetta, M. Visbal, Air Force Research C. Wong, L. Wang, Z. Wu, C. Li, M. Alam, D. Gonzalez, Naval Surface Warfare M. Sato, Japan Aerospace Exploration Laboratory, Wright-Patterson AFB, OH Y. Zhou, Harbin Institute of Technology, Center, Indian Head, MD; D. Gaitonde, Agency (JAXA), Sagamihara, Japan; K. Shenzhen, China Ohio State University, Columbus, OH; Asada, University of Tokyo, Sagamihara, M. Lewis, Institute for Defense Analyses, Japan; T. Nonomura, H. Aono, A. Yakeno, Washington, DC K. Fujii, Japan Aerospace Exploration Agency (JAXA), Sagamihara, Japan Wednesday, 18 June 2014 181-PDL-6/FC-6 DBD Actuators Roswell Chaired by: N. BISEK, Air Force Reseach Laboratory and C. SUCHOMEL, USAF 0930 hrs 1130 hrs 1200 hrs No Presentations AIAA-2014-2667 AIAA-2014-2668 Properties of Flows Induced by Development of a Multilevel DBD Plasma Actuators with Fine Plasma Generator for Dielectric Structural Exposed Electrodes Barrier Discharge Actuators H. Hagiwara, S. Ogata, Tokyo Metropolitan C. Borghi, A. Cristofolini, F. Dragonas, G. University, Hachioji, Japan; T. Segawa, Grandi, G. Neretti, University of Bologna, National Institute of Advanced Industrial Bologna, Italy Science and Technology, Tsukuba, Japan Wednesday, 18 June 2014 182-AFM-13 Small/Mini/Micro Aerial Vehicles I Spring Chaired by: R. LIND, University of Florida and A. DA RONCH, University of Southampton 0930 hrs 1000 hrs 1030 hrs AIAA-2014-2669 AIAA-2014-2670 AIAA-2014-2671 Implementation and Validation of an Simultaneous Tracking of Multiple Adaptive Robust Attitude Controller Actuator Disk Model for Aerodynamic Ground Targets from a Single Design for a Quadrotor Platform Analysis of Propelled UAVs Multirotor UAV E. Yilmaz, A. Kutay, Middle East Technical G. Guzel, Ö. Atesoglu, ASELSAN, Inc., N. Miller, Texas A&M University, College University, Ankara, Turkey Ankara, Turkey Station, TX; J. Rogers, Georgia Institute of Technology, Atlanta, GA Wednesday, 18 June 2014 183-TP-11 Aerothermodynamics I Techwood Chaired by: A. HYATT, European Research Council (ERC) and C. KOBUS, Oakland University 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2014-2672 AIAA-2014-2673 AIAA-2014-2674 AIAA-2014-2675 AIAA-2014-2676 Comprehensive Uncertainty Analysis Assessment of Convective and Conceptual Analysis of Electron Features of Afterbody Radiative Transpiration Cooling at Hypersonic of Mars Entry Flows over Hypersonic Radiative Heating for Jupiter Trojan Transpiration Cooling for the Heating for Earth Entry Flight - AKTiV on SHEFEX II Inflatable Atmospheric Decelerators Sample Return Capsule Leading Edges of Hypersonic C. Johnston, NASA Langley Research H. Boehrk, German Aerospace Center A. Brune, T. West, S. Hosder, Missouri K. Fujita, H. Takayanagi, S. Matsuyama, Vehicles Center, Hampton, VA; A. Brandis, ERC, (DLR), Stuttgart, Germany University of Science and Technology, Rolla, K. Yamada, T. Abe, Japan Aerospace H. Alkandry, K. Hanquist, I. Boyd, Inc., Mountain View, CA MO; K. Edquist, NASA Langley Research Exploration Agency (JAXA), Tokyo, Japan University of Michigan, Ann Arbor, Ann Center, Hampton, VA Arbor, MI

87 Wednesday, 18 June 2014 184-TP-12 Theoretical, Analytical and Computational Heat Transfer III University Chaired by: E. KINZEL, Missouri University of Science & Technology 0930 hrs 1000 hrs 1130 hrs 1200 hrs AIAA-2014-2677 Oral Presentation AIAA-2014-2678 AIAA-2014-2679 A Finite Volume Based Method for Photogallery: Heat and Mass Heat and mass transfers within Uncertainty Quantification for Narrow-Band Simulations of Thermal Transfer Visualization (Invited) decomposing carbon fibers/epoxy Multiscale Thermal Transport Radiation from Participating Media C. Choi, Michigan Technological University, resin composite materials Simulations A. Sventitskiy, C. Mundt, University of the Houghton, MI; K. Kihm, University of V. Biasi, G. Leplat, ONERA, Toulouse, L. Phinney, J. Lechman, W. Erikson, Sandia German Federal Armed Forces, Neubiberg, Tennessee, Knoxville, Knoxville, TN France; F. Feyel, P. Beauchene, ONERA, National Laboratories, Albuquerque, NM Germany Châtillon, France Wednesday, 18 June 2014 185-TP-13 Multi-Scale Heat Transfer II Vinings Chaired by: J. MALEN, Carnegie Mellon University and M. MARTIN, Louisiana State University 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs Oral Presentation AIAA-2014-2680 AIAA-2014-2681 Oral Presentation Oral Presentation Spectral Phonon Transport Measurements of Thermal Molecular Dynamics Studies of Tunable Thermal Conductivity of Modal Decomposition of Thermal Properties from Direct Green- Conductance of Suspended Polymeric Thermal Accommodation on Carbon Nanoparticle Beds via Surface Transport Across Interfaces Kubo Thermal Conductivity Nanowires Using Novel Bi-Material Surfaces Phonon Polaritons K. Gordiz, A. Henry, Georgia Institute of Decomposition Cantilever Sensing Technique N. Mehta, D. Levin, A. van Duin, B. Cola, Georgia Institute of Technology, Technology, Atlanta, GA A. Henry, W. Lv, Georgia Institute of C. Canetta, A. Narayanaswamy, Columbia Pennsylvania State University, University Atlanta, GA Technology, Atlanta, GA University, New York, NY Park, PA Wednesday, 18 June 2014 186-HYTASP-20 HYTASP Programs Regency Ballroom V 1030 - 1230 hrs Chaired by: A. SIEBENHAAR, Aerojet Rocketdyne Participants: Roger Longstaff Tom Jackson Charles Brink Gennaro Russo Francois Falempin Skylon HiFire X-51 HYPLANE MBDA

Wednesday, 18 June 2014 187-PANEL-5 Research Networks - Progress and Future Plans Regency Ballroom VI 1130 - 1230 hrs Moderator: Dominique Collin, Head of Acoustics, Safran Group, X-Noise Network Coordinator Panelists: Janina Scheelhaase Sylvain Cofsky Ralph Cavalieri ECATS Representative Executive Director Director, FAA Center of Excellence - Alternative Jet Fuels & Environment DLR German Aerospace Center GARDN Washington State University

Wednesday, 18 June 2014 188-LNCH-3 Luncheon in the Exhibit Hall Exhibit Hall 1230 - 1400 hrs Wednesday, 18 June 2014

88 189-APA-30 Flow Control (Active and Passive): Computational and Experimental Results V Baker Chaired by: K. KARA, Khalifa University of Science, Technology & Research and G. ZHA 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2014-2682 AIAA-2014-2683 AIAA-2014-2684 AIAA-2014-2685 AIAA-2014-2686 AIAA-2014-2687 Co-Flow Jet Airfoil Trade Study Co-Flow Jet Airfoil Trade Study Part Wind Tunnel Experiments on a Wall-normal vorticity injection in Hybrid RANS-LES Computation LES on Turbulent Separated Flow Part I: Energy Consumption and II: Moment and Drag NACA0015 Airfoil Equipped with separation control of NACA 0012 of Flow over NACA0015 Airfoil around NACA0015 at Reynolds Aerodynamic Efficiency A. Lefebvre, G. Zha, University of Miami, Vectorizable Dielectric Barrier airfoil Manipulated with Jet Actuators Number 1,600,000 toward Active A. Lefebvre, G. Zha, University of Miami, Miami, FL Discharge Plasma Actuators P. Munday, K. Taira, Florida State S. Peng, A. Jirasek, Swedish Defense Flow Control Miami, FL C. Borghi, A. Cristofolini, A. Rossetti, G. University, Tallahassee, FL Research Agency (FOI), Stockholm, K. Asada, University of Tokyo, Sagamihara, Neretti, S. Paolo, A. Talamelli, University Sweden Japan; M. Sato, T. Nonomura, S. Kawai, H. of Bologna, Bologna, Italy Aono, A. Yakeno, Japan Aerospace Exploration Agency (JAXA), Sagamihara, Japan; et al. Wednesday, 18 June 2014 190-APA-31 Aerodynamic Analysis and Design: CFD Methods II Courtland Chaired by: L. WANG, University of Tennessee at Chattanooga and R. VERMELAND, Lockheed Martin Aeronautics 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2014-2688 AIAA-2014-2689 AIAA-2014-2690 AIAA-2014-2691 AIAA-2014-2692 AIAA-2014-2694 Shock detection and capturing Arbitrary Lagrangian-Eulerian Comparative study of linear and Assessment of automatic Hybrid Prediction of Supersonic Aerodynamics An Improved Object-Oriented methods for high order Form of Flowfield Dependent non-linear RANS models for corner RANS/LES Models for Industrial for a Mars Entry Capsule Using Large Cartesian Grid Framework Discontinuous-Galerkin Finite Variation Method for Moving flows CFD Eddy Simulation Implementing Three Dimensional \ Element Methods Boundary Problems M. Bordji, F. Gand, V. Brunet, S. Deck, G. Pont, P. Cinnella, J. Robinet, P. Brenner, S. Matsuyama, H. Takayanagi, K. Fujita, linebreak Normal Ray Refinement A. Sheshadri, A. Jameson, Stanford M. Fadhli, A. Omar, W. Asrar, International ONERA, Meudon, France Astrium, Paris, France K. Mitsuo, M. Watanabe, Japan Aerospace M. Bopp, D. Dement, S. Ruffin, W. Lee, University, Stanford, CA Islamic University Malaysia, Kuala Lumpur, Exploration Agency (JAXA), Chofu, Japan; H. Georgia Institute of Technology, Atlanta, Malaysia Nishijima, IHI Aerospace Engineering Co., LTD., GA Tokyo, Japan Wednesday, 18 June 2014 191-APA-32 Special Session: 2nd High-Lift Prediction Workshop III Dunwoody Chaired by: J. SLOTNICK, Boeing Engineering Operations & Technology 1400 hrs 1430 hrs 1500 hrs 1530 hrs AIAA-2014-2695 AIAA-2014-2696 AIAA-2014-2697 Open Discussion Using XDB Workflows to Analyze OVERFLOW Analysis of the DLR-F11 High Lift OVERFLOW Analysis of the 30 Minute group discussion to wrap the 2nd AIAA CFD High Lift Configuration from HiLiftPW-2 DLR F11 Wind Tunnel Model the High-Lift Prediction Workshop Prediction Workshop Simulations Including Transition Modeling T. Pulliam, NASA Ames Research Center, E. Duque, Intelligent Light, Rutherford, NJ J. Coder, Pennsylvania State University, Moffett Field, CA; A. Sclafani, The Boeing University Park, PA Company, Huntington Beach, CA Wednesday, 18 June 2014 192-APA-33 Vortical/Vortex Flow I Edgewood Chaired by: K. DENISSEN, Sandia National Labs and V. BHAGWANDIN, US Army Research Laboratory 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2014-2698 AIAA-2014-2699 AIAA-2014-2700 AIAA-2014-2701 AIAA-2014-2702 AIAA-2014-2703 Exploring Vortex Stability on Two- The Effect of Edge Discontinuities On the Stable Leading Edge Vortex A Time-Lag Approach for Prediction Numerical Investigation of the Numerical Investigation of Three- Dimensional Rotating Plates with and Curvature on Vortex Growth in Rotating Systems of Trailing Edge Separation in Aerodynamics of a Delta Wing in Dimensional Vortical Flow for an Varying Sweepback and Stabilization for Low Aspect E. Limacher, D. Rival, University of Unsteady Flow Ground Effect Ellipsoid Model J. Wong, D. Rival, University of Calgary, Ratio Accelerating Plates Calgary, Calgary, Canada S. Narsipur, A. Gopalarathnam, J. Q. Qu, Z. Lu, P. Liu, Beihang University, A. Haas, University of Arizona, Tucson, Calgary, Canada J. Fernando, D. Rival, University of Edwards, North Carolina State University, Beijing, China; R. Agarwal, Washington Tucson, AZ; A. Gross, New Mexico State Calgary, Calgary, Canada Raleigh, NC University in St. Louis, St. Louis, MO University, Las Cruces, NM; H. Fasel, University of Arizona, Tucson, Tucson, AZ Wednesday, 18 June 2014

89 193-ATIO-15 Transformational Flight - Autonomy Embassy C Chaired by: B. ALLEN, NASA Langley Research Center 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs Oral Presentation AIAA-2014-2704 Oral Presentation Oral Presentation AIAA-2014-2705 Oral Presentation Oral Presentation Applied Autonomy for Safety, Wetware, Hardware, or Software Control Automation for Advanced Machine Intelligence for Deciding Reducing Size, Weight, and Power Adaptive Mission Management for Development and Flight Efficiency and Mobility in Civil Incapacitation: Observational Single Pilot Operations to Go Around (SWaP) of Perception Systems in Safe, Efficient, Mobility Demonstration of a Variable Aviation Methods to Determine When K. Goodrich, P. Schutte, NASA Langley M. Motter, NASA Langley Research Center, Small Autonomous Aerial Systems I. Gregory, NASA Langley Research Center, Autonomy Ground Collision B. Allen, NASA Langley Research Center, Autonomy Should Assume Control Research Center, Hampton, VA; R. Hampton, VA K. Jones, NASA Langley Research Center, Hampton, VA Avoidance System Hampton, VA A. Trujillo, I. Gregory, NASA Langley Williams, Analytical Mechanics Associates, Hampton, VA; J. Gross, West Virginia M. Skoog, NASA Dryden Flight Research Research Center, Hampton, VA Inc., Hampton, VA University, Morgantown, WV Center, Edwards, CA Wednesday, 18 June 2014 194-BA-1 Balloon Systems Embassy D Chaired by: Z. MIAN 1400 hrs 1430 hrs 1500 hrs AIAA-2014-2706 AIAA-2014-2707 AIAA-2014-2708 The French balloon program 2012 Qualification of the new French Structural feasibility analysis - 2015 balloon system and the new of a large non-conventional V. Dubourg, A. Vargas, P. Cocquerez, Canadian launch site stratospheric non-rigid airship French Space Agency (CNES), Toulouse, A. Vargas, French Space Agency (CNES), A. Suñol, D. Vucinic, Vrije Universiteit France Toulouse, France; D. Levesque, Canadian Brussel, Brussels, Belgium Space Agency, Montréal, Canada; V. Dubourg, French Space Agency (CNES), Toulouse, France; S. Lafrance, R. Grenier, Canadian Space Agency, Montréal, Canada Wednesday, 18 June 2014 195-LTA-1 Lighter-than-Air Systems Embassy D Chaired by: Z. MIAN, Georgia Institute of Technology 1400 hrs 1600 hrs 1630 hrs 1700 hrs No Presentations AIAA-2014-2709 AIAA-2014-2710 AIAA-2014-2711 An Airship Platform for the Conceptual Design of a Winged Evaluation of a Water Channel-Based AirBorne Laser (ABL) Hybrid Airship Platform for Characterizing Aerostat R. Salvage, Self, Victorville, CA A. Haque, W. Asrar, A. Omar, E. Sulaeman, Flight Dynamics: A Case Study on a J. Ali, International Islamic University Lighter-Than-Air Wind Energy System Malaysia, Kuala Lumpur, Malaysia C. Vermillion, B. Glass, Altaeros Energies,

90 Boston, MA; S. Greenwood, University of Michigan, Ann Arbor, Ann Arbor, MI Wednesday, 18 June 2014 196-ATIO-16 ATM-VI Weather’s Role in ATM Embassy E Chaired by: A. DESHMUKH, Gulfstream Aerospace Corp. 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2014-2712 AIAA-2014-2713 AIAA-2014-2714 AIAA-2014-2715 AIAA-2014-2716 AIAA-2014-2717 Clustering Days with Similar Airport Predicting Ground Delay Representative Weather-Impact Convective Weather Impact Operational Evaluation of a Decision Risk in the Use of Weather Conditions Program At An Airport Based On Scenarios for Strategic Traffic Flow Forecasting in the Terminal Area Weather-Avoidance Rerouting Convective Weather Forecasts for S. Grabbe, B. Sridhar, NASA Ames Meteorological Conditions Planning S. Campbell, R. DeLaura, Lincoln System Trajectory-Based Operations Research Center, Moffett Field, CA; A. A. Mukherjee, University of California, S. Tien, C. Taylor, C. Wanke, MITRE Laboratory, Massachusetts Institute of P. Borchers, NASA Ames Research Center, M. Matthews, R. DeLaura, Lincoln Mukherjee, University of California, Santa Santa Cruz, Santa Cruz, CA; S. Grabbe, Corporation, McLean, VA Technology, Lexington, MA Moffett Field, CA; K. Roach, University Laboratory, Massachusetts Institute of Cruz, Moffett Field, CA B. Sridhar, NASA Ames Research Center, Affiliated Research Center (UARC), Fort Technology, Lexington, MA Moffett Field, CA Worth, TX; L. Morgan-Ruszkowski, Flatirons Solutions, Inc., Fort Worth, TX Wednesday, 18 June 2014 197-ACD-8 Unmanned Aircraft Design Studies and Methods Embassy F Chaired by: D. WELLS, NASA Langley Research Center and C. BIL, RMIT University 1400 hrs 1430 hrs 1500 hrs 1530 hrs AIAA-2014-2718 AIAA-2014-2719 AIAA-2014-2720 AIAA-2014-2721 Unlimited Endurance Low Altitude A Multi-Disciplinary Integrated Design A Virtual Experimentation Platform Design and Testing of an Air- Wind Powered Unmanned Aerial Environment for Requirements Enabling the Design, Testing, and Deployed Unmanned Underwater Vehicle Development and Performance Verification of an Unmanned Aerial Vehicle M. Sadraey, Daniel Webster College, Evaluation of Autonomous Systems Vehicle through Cyber-Physical, T. Young, Naval Research Laboratory, Nashua, NH R. Roe, S. Ford, G. Cinar, Z. Mian, D. Mavris, Component-Based Design Washington, DC Georgia Institute of Technology, Atlanta, GA B. Laughlin, S. Briceno, D. Mavris, Georgia Institute of Technology, Atlanta, GA Wednesday, 18 June 2014 198-ACD-9 Design of Morphing Wing Concepts Embassy F Chaired by: D. WELLS, NASA Langley Research Center and H. JIMENEZ, Georgia Institute of Technology 1400 hrs 1600 hrs 1630 hrs 1700 hrs No Presentations AIAA-2014-2722 AIAA-2014-2723 AIAA-2014-2724 Optimization Framework for Studies on Morphing Aircraft Aerodynamic Performance of Design of Morphing Wings Design including Engine parameters Corrugated Skins for Spanwise J. Yang, J. Cooper, University of Bristol, using Genetic Algorithm Wing Morphing Bristol, United Kingdom; R. Nangia, A. Chamarthi, R. Pant, Indian Institute of J. Fincham, Swansea University, Swansea, Nangia Associates, Bristol, United Technology Bombay, Mumbai, India United Kingdom; R. Ajaj, University of Kingdom; J. Simpson, Fraunhofer, Valley, Southampton, Southampton, United Germany Kingdom; M. Friswell, Swansea University,

91 Swansea, United Kingdom Wednesday, 18 June 2014 199-MAO-10 Multidisciplinary Analysis and Optimization: Emerging Methods II Embassy G Chaired by: H. KIM, University of Illinois 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2014-2725 AIAA-2014-2726 AIAA-2014-2727 AIAA-2014-2728 AIAA-2014-2729 AIAA-2014-2730 Development of Installed Propulsion Towards Gradient-Based Design A Visually-Informed Decision- Incorporating Value-Driven Design Many Objective Visual Analytics: In A Hybrid Differential Evolution Performance Model for High- Optimization of Flexible Transport Making Platform for Model-based into the Visualization of Design Search of Search-as-a-Service Self-Organizing-Map Algorithm for Performance Aircraft Conceptual Aircraft with Flutter Constraints Design of Wind Farms Spaces Using Contextual Self- M. Woodruff, T. Simpson, Pennsylvania Optimization of Expensive Black- Design G. Kennedy, Georgia Institute of S. Chowdhury, Mississippi State University, Organizing Maps: A Case Study of State University, University Park, PA; P. box Functions D. Allison, Optimal Flight Sciences, LLC, Technology, Atlanta, GA; G. Kenway, J. Mississippi State, MS; A. Mehmani, W. Satellite Design Reed, Cornell University, Ithaca, NY S. Subramanian, D. DeLaurentis, Purdue Dayton, OH; E. Alyanak, Air Force Research Martins, University of Michigan, Ann Arbor, Tong, Syracuse University, Syracuse, NY; T. Richardson, H. Kannan, C. Bloebaum, E. University, West Lafayette, IN Laboratory, Wright-Patterson AFB, OH Ann Arbor, MI A. Messac, Mississippi State University, Winer, Iowa State University, Ames, IA Mississippi State, MS Wednesday, 18 June 2014 200-ANERS-1 ANERS-Design and Operations Embassy H Chaired by: R. DEL ROSARIO, NASA Glenn Research Center 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs AIAA-2014-2731 AIAA-2014-2732 AIAA-2014-2733 AIAA-2014-2734 AIAA-2014-2735 Development of Generic Vehicles Design Optimization and Staging Flybrid: Envisaging the Future Application of Mixture Design of Robust Coupled Optimization of for Fleet-Level Analysis of Noise Assignment for Long-Range Aircraft Hybrid-Powered Regional Aviation Experiments for Dynamic Fleet- Aircraft Design and Fleet Allocation and Emissions Tradeoffs Operations G. Bona, M. Bucari, A. Castagnoli, L. Level Evaluation of Multi-Objective for Multiple Markets M. LeVine, A. Wilson, M. Kirby, D. R. Perez, P. Jansen, Royal Military College Trainelli, Technical University of Milan, Environmental Technology Trade-offs P. Jansen, R. Perez, Royal Military College Mavris, Georgia Institute of Technology, of Canada, Kingston, Canada Milan, Italy J. Bernardo, E. Lacouture, M. Kirby, D. Mavris, of Canada, Kingston, Canada Atlanta, GA Georgia Institute of Technology, Atlanta, GA Wednesday, 18 June 2014 201-APA-34 Low Speed, Low Reynolds Number, Transonic, Supersonic and Hypersonic Aerodynamics III Fairlie Chaired by: C. TILMANN, Air Force Reseach Laboratory 1400 hrs 1430 hrs 1500 hrs AIAA-2014-2736 AIAA-2014-2737 AIAA-2014-2738 Predictions of a Supersonic Jet-in- Kriging-model-based uncertainty Experimental Study of Unswept Crossflow: Comparisons Among CFD quantification in computational and Swept Oblique Shock-Turbulent Solvers and with Experiment fluid dynamics Boundary Layer Interactions J. DeSpirito, Army Research Laboratory, S. Kawai, Japan Aerospace Exploration J. Hainsworth, R. Dawson, J. Little, Aberdeen Proving Ground, MD; K. Kennedy, C. Agency (JAXA), Sagamihara, Japan; K. University of Arizona, Tucson, Tucson, AZ Mikkelsen, Army Aviation and Missile Research Shimoyama, Tohoku University, Sendai, Development and Engineering Center, Japan Redstone Arsenal, AL; R. Chaplin, Defence Science and Technology Laboratory, Fareham, United Kingdom Wednesday, 18 June 2014 202-AA-14 CAA Numerical Techniques II Hanover A Chaired by: C. BAILLY, Ecole Centrale de Lyon 1400 hrs 1430 hrs 1500 hrs 1530 hrs AIAA-2014-2739 AIAA-2014-2740 AIAA-2014-2742 AIAA-2014-2743 A Non-Conforming Finite Element A Discontinuous Galerkin Broadband Model for Impedance Development and testing of a time- Method for Computational Spectral Element Method for the Boundary Condition in a Navier- domain equivalent source method Aeroacoustics in Rotating Systems direct numerical simulation of Stokes Solver for acoustic scattering A. Hüppe, Vienna University of Technology, aeroacoustics T. Jadhav, A. Khondge, ANSYS, Inc., Pune, S. Swift, G. Blaisdell, Purdue University,

92 Vienna, Austria; J. Grabinger, Friedrich- D. Flad, A. Beck, G. Gassner, C. Munz, India; V. Ivanov, B. Makarov, C. Hill, West Lafayette, IN; A. Lyrintzis, Embry- Alexander University, Erlangen, Germany; M. University of Stuttgart, Stuttgart, Germany ANSYS, Inc., Lebanon, NH Riddle Aeronautical University, Daytona Kaltenbacher, Vienna University of Technology, Beach, FL Vienna, Austria; A. Reppenhagen, G. Dutzler, VIRTUAL VEHICLE Research and Test Center (ViF), Graz, Austria; W. Kühnel, MAHLE Group, Stuttgart, Germany Wednesday, 18 June 2014 203-AA-15 Propeller Noise II Hanover B Chaired by: E. ENVIA, NASA Glenn Research Center 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs AIAA-2014-2744 AIAA-2014-2745 AIAA-2014-2746 AIAA-2014-2747 AIAA-2014-2748 AIAA-2014-2749 AIAA-2014-2750 Tone and Broadband Noise Analysis of Advanced Open Rotor Sound Radiated from a Rotor and Z08: low-speed aero-acoustic Investigation of Counter Rotating Open-Rotor low speed Auralization of Flyover Noise from Separation from Acoustic Data of Noise Measurements Its Relation to Rotating Frame experimental characterization of Open Rotor Orthogonal Blade/ aero-acoustics: wind tunnel Open Rotor Engines Using Model a Scale-Model Counter-Rotating M. Kingan, C. Ekoule, University of Measurements of Ingested Turbulence open rotor installation on aircraft Vortex Interaction Noise characterization of an advanced Scale Test Data Open Rotor Southampton, Southampton, United W. Alexander, W. Devenport, D. Wisda, C. Paquet, E. Julliard, J. Ricouard, P. F. Falissard, ONERA, Châtillon, France; G. blade design in isolated and S. Rizzi, NASA Langley Research Center, D. Stephens, NASA Glenn Research Kingdom; A. Parry, K. Britchford, Rolls- Virginia Polytechnic Institute and State Spiegel, Airbus, Toulouse, France Delattre, ONERA, Meudon, France installed configurations Hampton, VA; D. Stephens, J. Berton, D. Center, Cleveland, OH; D. Sree, Tuskegee Royce Group plc, Derby, United Kingdom University, Blacksburg, VA; M. Morton, Naval R. Fernando, Snecma, Moissy-Cramayel, Van Zante, NASA Glenn Research Center, University, Tuskegee, AL Air Warfare Center, Patuxent River, MD; France; M. Leroux, Airbus, Toulouse, Cleveland, OH; J. Wojno, T. Goerig, GE S. Glegg, Florida Atlantic University, Boca France Aviation, Cincinnati, OH Raton, FL Wednesday, 18 June 2014 204-ASE-11 Engine Icing I - Cloud Measurement and Characterization Hanover C Chaired by: P. STRUK, NASA Glenn Research Center and M. OLIVER, NASA Glenn Research Center 1400 hrs 1430 hrs 1500 hrs AIAA-2014-2751 AIAA-2014-2752 AIAA-2014-2753 Development of a Sensor for Simulation of fluid flow and AIRBUS Flight Tests in High Total Total Temperature and Humidity collection efficiency for an SEA Water Content Regions Measurements under Mixed-Phase multi-element probe A. Grandin, J. Merle, M. Weber, Airbus, and Glaciated Icing Conditions D. Rigby, Vantage Partners, LLC, Toulouse, France; J. Strapp, Environment D. Fuleki, A. Mahallati, T. Currie, J. Cleveland, OH; P. Struk, C. Bidwell, NASA Canada, Toronto, Canada; A. Protat, MaCleod, D. Knezevici, National Research Glenn Research Center, Cleveland, OH Centre for Australian Weather and Climate Council Canada, Ottawa, Canada Research, Melbourne, Australia; P. King, Coriolis Weather, Toronto, Canada Wednesday, 18 June 2014 205-ASE-12 Numerical Weather Modeling Hanover D Chaired by: N. AHMAD, NASA Langley Research Center and G. THOMPSON, NCAR-RAL 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs Oral Presentation Oral Presentation Oral Presentation Oral Presentation Oral Presentation Oral Presentation Global to Local Scale Atmospheric A Motion-Based Piloted Flight Recent advances in direct numerical Numerical Simulations of Cirrus GPU-accelerated Cartesian mesh Medium Range Multi-model Simulation using an Adaptive Simulation for a Realistic Weather model prediction of supercooled Bands and their Relation to wind simulations over arbitrarily Regional Ensemble Forecasting Unstructured Grid (Invited) Environment (Invited) water drops and application to Turbulence (Invited) complex terrain (Invited) over the Western U.S. (Invited) D. Bacon, Leidos Corporation, Sterling, T. Daniels, S. Young, E. Evans, P. aircraft icing (Invited) R. Sharman, S. Trier, National Center for I. Senocak, Boise State University, D. Koracin, J. Lewis, A. Young, Desert VA, VA Schaffner, NASA Langley Research Center, G. Thompson, National Center for Atmospheric Research, Boulder, CO; J. Boise, ID Research Institute, Reno, NV; R. Vellore, Hampton, VA Atmospheric Research, Boulder, CO Kim, NASA Ames Research Center, Moffett Indian Institute of Tropical Meteorology, Field, CA Pune, India 93 Wednesday, 18 June 2014 206-AA-16 Jet Noise Prediction II Hanover E Chaired by: W. SCHROEDER, RWTH AACHEN 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2014-2754 AIAA-2014-2755 AIAA-2014-2756 AIAA-2014-2757 AIAA-2014-2758 AIAA-2014-2759 Noise of high-performance aircrafts An Extended Lattice Boltzmann Dual-stream jet noise simulations with A Complex Ray-Tracing Tool for A coherence-matched linear model Flow Dynamics and Aeroacoustics at afterburner Methodology for High Subsonic Jet realistic nozzle geometries using a High-Frequency Mean-Field Flow for subsonic jet noise of Heated Coaxial Jets at Subsonic C. Tam, S. Parrish, Florida State University, Noise Prediction fully unstructured LES solver Interaction Effects in Jets Y. Baqui, A. Agarwal, University of Mach Numbers Tallahassee, FL P. Lew, P. Gopalakrishnan, D. Casalino, R. A. Fosso Pouangue, M. Sanjose, S. J. Stone, R. Self, C. Howls, University Cambridge, Cambridge, United Kingdom; M. Gloor, S. Buehler, L. Kleiser, Swiss Shock, Y. Li, R. Zhang, Exa Corporation, Moreau, University of Sherbrooke, of Southampton, Southampton, United A. Cavalieri, Technological Institute of Federal Institute of Technology, Zurich, Burlington, MA; et al. Sherbrooke, Canada Kingdom Aeronautics (ITA), São José dos Campos, Switzerland Brazil Wednesday, 18 June 2014 207-AA-17 Airframe Noise II Hanover F Chaired by: C. BURLEY, NASA-Langley Research Center 1400 hrs 1430 hrs 1500 hrs 1530 hrs AIAA-2014-2760 AIAA-2014-2762 AIAA-2014-2763 AIAA-2014-2764 Acoustic Shielding of a Tapered Acoustics and Surface Pressure On LAGOON Nose Landing Gear Generating Trailing-Edge Noise Wing Measurements from Tandem CFD/CAA Computation over Predictions Using Synthetic C. Marks, D. Robertson, University of Cylinder Configurations Unstructured Mesh using a ZDES Turbulence Dayton Research Institute, Dayton, OH; F. Hutcheson, T. Brooks, D. Lockard, approach A. Iob, wavePRO, Turin, Italy; R. Arina, D. Bryson, G. Reich, Air Force Research M. Choudhari, NASA Langley Research F. de la Puente, L. Sanders, F. Vuillot, Technical University of Turin, Turin, Italy; Laboratory, Wright-Patterson AFB, OH Center, Hampton, VA; D. Stead, Northrop ONERA, Châtillon, France P. Batten, S. Chakravarthy, Metacomp Grumman Corporation, Hampton, VA Technologies, Agoura Hills, CA Wednesday, 18 June 2014 208-HYTASP-24 Aerodynamic and Propulsion Test Unit (APTU) II Hanover G Chaired by: G. GARRARD, Aerospace Testing Alliance (ATA) 1400 hrs 1430 hrs AIAA-2014-2765 AIAA-2014-2766 Upgrades to the Aerodynamic and Upgrades to the Aerodynamic and Propulsion Test Unit Heated Fuel Propulsion Test Unit Facility Control System (Invited) System and Simulator in Support K. Butler, Aerospace Testing Alliance, of the Medium Scale Critical Arnold AFB, TN Components Direct Connect Test Program (Invited) B. Boylston, Aerospace Testing Alliance, Arnold AFB, TN Wednesday, 18 June 2014 209-ITAR-5 ITAR-Hypersonic Vehicle Design Hanover G Chaired by: E. GARCIA, Georgia Institute of Technology 1400 hrs 1600 hrs 1630 hrs 1700 hrs No Presentations AIAA-2014-2767 AIAA-2014-2768 AIAA-2014-2769 Flight Test Experiment Design and Responsive Rocket Vehicles for Comparison of Trajectory Methods Aerodynamic Parameter Estimation High Altitude Reconnaissance for Hypersonic Gliding Vehicles for the X-51A Waverider B. Hellman, Air Force Research Laboratory, B. Hellman, Air Force Research Laboratory, E. Morelli, NASA Langley Research Center, Wright-Patterson AFB, OH Wright-Patterson AFB, OH Hampton, VA; S. Rexius, J. Lechniak, Hypersonic Combined Test Force, Edwards

94 AFB, CA Wednesday, 18 June 2014 210-FD-19 Fluid Structure Interaction III Harris Chaired by: M. YU, University of Maryland, Baltimore County 1400 hrs 1430 hrs 1500 hrs 1530 hrs AIAA-2014-2770 AIAA-2014-2771 AIAA-2014-2772 AIAA-2014-2773 The Effects of Static Aeroelasticity Wind Tunnel Characterization of Coupled CFD/CSD Simulations of Large displacement body-fitted on the Performance of Supersonic/ Fluid-Structure Interactions for the UH-60A Main Rotor in Forward FSI simulations using a mesh- Hypersonic Nozzles Various Suspension Lines and Maneuvering Flight connectivity-change moving mesh U. Duzel, S. Eyi, Middle East Technical T. Siefers, T. McLaughlin, U.S. Air Force J. Ickes, J. Wang, C. Sheng, University of strategy University, Ankara, Turkey Academy, Colorado Springs, CO; K. Toledo, Toledo, OH N. Barral, F. Alauzet, French National Bergeron, Army Research, Development Institute for Research in Computer Science and Engineering Command, Natick, MA and Control (INRIA), Le Chesnay, France Wednesday, 18 June 2014 211-FD-20 Stability and Transition III Inman Chaired by: H. REED, Texas A&M University and S. SCHNEIDER, Purdue University 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2014-2774 AIAA-2014-2775 AIAA-2014-2776 AIAA-2014-2777 AIAA-2014-2778 AIAA-2014-2779 High-frequency instabilities along Numerical Investigation of Numerical Investigation of Nonlinear Detuning of Mack-Mode Experimental and Numerical Hypersonic Boundary Layer the windward face of a hypersonic Wavepackets in a Hypersonic High- Laminar-Turbulent Transition for a Instabilities Investigation of Instabilities in Transition on a 7 Degree Half- yawed circular cone Enthalpy Boundary Layer on a Flared Cone at Mach 6 J. Kuehl, H. Reed, T. Kocian, N. Oliviero, Conical Boundary Layers at Mach 6 Angle Cone at Mach 10 P. Paredes, V. Theofilis, Technical University 5deg Sharp Cone J. Sivasubramanian, H. Fasel, University of Texas A&M University, College Station, TX F. Munoz, R. Radespiel, A. Theiss, S. Hein, G. Grossir, F. Pinna, G. Bonucci, T. Regert, of Madrid, Madrid, Spain; H. Reed, Texas L. Salemi, H. Fasel, University of Arizona, Arizona, Tucson, Tucson, AZ Technical University of Braunschweig, P. Rambaud, O. Chazot, von Kármán A&M University, College Station, TX Tucson, Tucson, AZ; S. Wernz, E. Marquart, Braunschweig, Germany Institute for Fluid Dynamics, Rhode-Saint- Raytheon Missile Systems, Tucson, AZ Genèse, Belgium Wednesday, 18 June 2014 212-FD-21 CFD Methods Kenneshaw Chaired by: H. HUYNH, NASA Glenn Research Center 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2014-2780 AIAA-2014-2781 AIAA-2014-2782 AIAA-2014-2783 AIAA-2014-2784 AIAA-2014-2785 Using Multi-Dimensional Linear A Hybridized Discontinuous From 2nd Order Accurate to 4th A Hybridized Discontinuous DNS of Flows over Periodic Hills A hierarchical Cartesian method for Discretization Over Unsteady Galerkin Method for Unsteady Order Accurate Spatial and Temporal Galerkin Method for Turbulent using a Discontinuous Galerkin conjugated heat transfer Convection Adapted Control Flows with Shock-Capturing Schemes for Unstructured Grids Compressible Flow Spectral-Element Method G. Brito Gadeschi, M. Meinke, W. Volumes A. Jaust, J. Schuetz, M. Woopen, RWTH H. Yang, Z. Chen, A. Przekwas, CFD Research M. Woopen, T. Ludescher, G. May, RWTH L. Diosady, S. Murman, NASA Ames Schroeder, RWTH Aachen University, J. Moore, J. Moore, Self, Blacksburg, VA Aachen University, Aachen, Germany Corporation, Huntsville, AL; J. Dudley, Air Force Aachen University, Aachen, Germany Research Center, Moffett Field, CA Aachen, Germany Research Laboratory, Eglin AFB, FL Wednesday, 18 June 2014 213-HYTASP-6 Propulsion Cycle Performance Learning Center Chaired by: L. MCKINNEY, McKinney Associates 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs AIAA-2014-2786 AIAA-2014-2787 AIAA-2014-2788 AIAA-2014-2789 AIAA-2014-2790 Quasi-One-Dimensional Hybrid Propulsion Parametric and Design and Optimization of a Fundamental Architecture and Mach 4 Wind Tunnel Experiment Investigation of Combustion Modular Model: a novel engine Notional Scramjet by Means of Analysis of an Antimatter Ultra- of Hypersonic Pre-Cooled Turbojet Processes on Scramjet Performance analysis tool conceived for design Stream Thrust Analysis and Design Intense Laser Derived Combined Engine T. Vanyai, S. Brieschenk, M. Bricalli, R. optimization of Experiments Cycle Ramjet-Rocket Propulsion H. Taguchi, K. Harada, H. Kobayashi, M. Boyce, University of Queensland, Brisbane, A. Mogavero, I. Taylor, R. Brown, M. Akpolat, Atilim University, Ankara, System Hongoh, D. Masaki, S. Nishida, Japan Australia University of Strathclyde, Glasgow, United Turkey; K. Toker, ROKETSAN Missiles R. Lemoyne, Self, Running Springs, CA Aerospace Exploration Agency (JAXA), Kingdom Industries, Inc., Ankara, Turkey; M. Genc, Tokyo, Japan Erciyes University, Kayseri, Turkey 95 Wednesday, 18 June 2014 214-FC-11 Flow Control: Active and Passive Lenox Chaired by: L. PACK MELTON, NASA-Langley Research Center and A. AHMED 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2014-2791 AIAA-2014-2792 AIAA-2014-2793 AIAA-2014-2794 AIAA-2014-2795 AIAA-2014-2796 Axisymmetric Jet Subjected to Control of Wing Tip Vortex Bleed and Vortex Generator Unsteady Flow Injection in Fully-Resolved Lattice-Boltzmann PIV Wake Measurements of a Low Radial and Azimuthal Forcing Structure Using Fluidic Actuation Effectiveness for Separation Turbulent Cavity Flow Simulation of Vane-Type Vortex Aspect Ratio Circulation Control Wing A. Ahmed, A. Weiner, Auburn University, M. Dghim, M. Ferchichi, Royal Military College Prevention in a Transonic Diffuser M. Garcia Sainz, J. Delnero, J. Marañon, Generators with Spanwise Variation in Efflux Auburn, AL of Canada, Kingston, Canada; M. Benchiekh, J. Oorebeek, H. Babinsky, University of National University of La Plata, La Plata, B. Koenig, E. Fares, Exa Corporation, D. Miklosovic, M. Perry, U.S. Naval University of Monastir, Monastir, Tunisia Cambridge, Cambridge, United Kingdom Argentina Stuttgart, Germany Academy, Annapolis, MD Wednesday, 18 June 2014 215-AMT-10/GT-8 Aerodynamic Force and Power Measurement Marietta Chaired by: R. RHEW, NASA-Langley Research Center and T. WADHAMS, CUBRC 1400 hrs 1430 hrs 1500 hrs 1530 hrs Oral Presentation AIAA-2014-2797 AIAA-2014-2798 AIAA-2014-2799 Aerodynamic Force and Power A New Global Regression Analysis Development of a new rig with Development and Feasibility of a Measurement: A Brief History and Method for the Prediction of Wind enhanced specifications for wind Non-Invasive, Wireless Parachute Current Capabilities (Invited) Tunnel Model Weight Corrections tunnel tests of “isolated” CROR Load Distribution Measuring R. Rhew, K. Lynn, NASA Langley Research N. Ulbrich, Jacobs, Moffett Field, CA; M. propulsion systems System Center, Hampton, VA Amaya, NASA Ames Research Center, Moffett J. Séchaud, ONERA, Modane, France T. Fields, University of Missouri, Kansas Field, CA; T. Bridge, Jacobs, Moffett Field, CA City, Kansas City, MO Wednesday, 18 June 2014 216-AMT-11/GT-9 Surface Sensors and Probes Piedmont Chaired by: T. IOPPOLO, Southern University and J. MELOY, Boeing Test & Evaluation 1400 hrs 1430 hrs 1500 hrs Oral Presentation AIAA-2014-2800 AIAA-2014-2801 Correction Uncertainty of Remotely Skin Friction Sensor Validation for Rapid Flow Surveys via Rotating Measured Pressure Signals in Tap/ High-Speed, High-Enthalpy Flow Rake System and Use in Powered Tubing/Transducer Systems Applications Wind Tunnel Models M. Hind, J. Naughton, University of R. Meritt, J. Schetz, Virginia Polytechnic M. Lieu, M. Drela, A. Uranga, E. Greitzer, Wyoming, Laramie, Laramie, WY Institute and State University, Blacksburg, VA Massachusetts Institute of Technology, Cambridge, MA Wednesday, 18 June 2014 217-HYTASP-7 Review of Fundamental Research I (Invited) Regency Ballroom V Chaired by: M. ONOFRI, University of Rome “”La Sapienza”” and J. SCHMISSEUR, USAF AFOSR/NA 1400 hrs 1430 hrs 1500 hrs 1530 hrs AIAA-2014-2803 AIAA-2014-2804 AIAA-2014-2805 AIAA-2014-2806 Experimental Study of Strut Permeability Measurements of Uncertainty Analysis of Radiative Airborne Observation of Re-entries Injectors for Scramjet Combustors Complex Porous Structures for Heating for Multiple Planetary - Lessons Learned and Future (Invited) Reusable Thermal Protection Entry Cases (Invited) Perspectives (Invited) F. Vergine, L. Maddalena, University of Systems (Invited) T. West, A. Brune, S. Hosder, Missouri M. Winter, University of Kentucky, Texas, Arlington, Arlington, TX S. Gulli, L. Maddalena, University of Texas, University of Science and Technology, Lexington, Lexington, KY Arlington, Arlington, TX; C. McKelvey, Rolla, MO A. Brown, C-CAT, Inc., Kennedale, TX; Y. Nikishkov, A. Makeev, University of Texas,

96 Arlington, Arlington, TX Wednesday, 18 June 2014 218-PANEL-6 Panel: Creating a Successful Commercial UAS Business Environment - Challenges & Opportunities Regency Ballroom VI 1400 - 1630 hrs Moderator: John Langford, CEO, Aurora Flight Sciences Panelists: Nicholas Alley Morgan Cloud Steve Justice John Lambert Rose Mooney Elizabeth Soltys President and CEO Charles Howard Candler Professor of Law Director Senior Vice President Executive Director Program Manager Area-I, Inc. Emory University Georgia Center of Innovation for Aerospace Nexutech, LLC Mid-Atlantic Aviation Partnership FAA UAS Test Sites

Wednesday, 18 June 2014 219-PDL-12 Special Session: NATO-RTO-AVT-190, Standardization of DBD Actuators Roswell Chaired by: S. ROY, University of Florida and C. SUCHOMEL, USAF 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs Oral Presentation AIAA-2014-2807 AIAA-2014-2808 AIAA-2014-2809 AIAA-2014-2810 AIAA-2014-2811 AIAA-2014-2812 Measurements and Calculations Characterization of the time- Numerical Simulation of sinusoidal Electromagnetic and Ozone Evaluation of Dielectric-Barrier- Understanding SDBD Actuators: Flow Control at Subsonic Speeds of Thrust for Various Standard dependent behaviour of dielectric DBD actuators and comparison with Emissions from Dielectric Barrier Discharge Actuator Substrate An Experimental Study on Plasma using Serpentine Plasma Actuators and Non-standard DBD Plasma barrier discharge plasma actuators experiments Discharge Plasma Actuators Materials Characteristics K. Kontis, H. Zare-Behtash, University of Actuators (Invited) A. Naghib Lahouti, R. Pimentel, Defense F. Rogier, G. Dufour, K. Kourtzanidis, N. Houser, P. Lavoie, University of Toronto, S. Wilkinson, E. Siochi, NASA Langley P. Leyland, Swiss Federal Institute of Glasgow, Glasgow, United Kingdom; S. S. Roy, University of Florida, Gainesville, Research and Development Canada, ONERA, Toulouse, France Toronto, Canada; R. Pimentel, Y. de Villers, Research Center, Hampton, VA; G. Sauti, Technology, Lausanne, Switzerland; Roy, University of Florida, Gainesville, Gainesville, FL Québec, Canada; P. Lavoie, University of Defense Research and Development T. Xu, National Institute of Aerospace, R. Pimentel, Defense Research and Gainesville, FL Toronto, Toronto, Canada Canada, Québec, Canada; T. Ringuette, Hampton, VA; M. Meador, H. Guo, NASA Development Canada, Valcartier, Canada; Numerica Technologies, Inc., Québec, Glenn Research Center, Cleveland, OH R. Geuns, S. Goekce, P. Peschke, C. Canada Hollenstein, Swiss Federal Institute of Technology, Lausanne, Switzerland; et al. Wednesday, 18 June 2014 220-AFM-14 Small/Mini/Micro Aerial Vehicles II Spring Chaired by: M. ABDULRAHIM, AeroVironment Inc and K. HOFFLER, Adaptive Aerospace Group, Inc. 1400 hrs 1430 hrs 1500 hrs AIAA-2014-2813 AIAA-2014-2814 AIAA-2014-2815 Computational Studies of Pressure Flight Test Protocol for Electric Moment Generation of Stabilizing Sensor Placement for a Fish- Powered Small Unmanned Aerial Axes for Insect-Inspired Flapping Inspired UUV Systems Wing Flight R. Ramamurti, J. Geder, A. Thangawng, M. McCrink, J. Gregory, Ohio State I. Faruque, University of Maryland, College G. Edelmann, Naval Research Laboratory, University, Columbus, OH Park, College Park, MD; P. Samuel, Washington, DC Daedalus Flight Systems, Rockville, MD; J. Humbert, University of Maryland, College Park, College Park, MD Wednesday, 18 June 2014 221-TP-14 Aerothermodynamics II Techwood Chaired by: C. JOHNSTON, NASA-Langley Research Center and K. NAWAZ, Johnson Controls Inc. 1400 hrs 1430 hrs 1500 hrs AIAA-2014-2816 AIAA-2014-2817 AIAA-2014-2818 Analysis of Tile Calibration Tests in Rough wall heat flux augmentation Hypersonic Vehicle Leading the PTF: Compression-Pad Surface analysis in the framework of the Thermal Protection Technology Heating Distribution ExoMars project F. Li, X. Zhao, China Academy of T. Gokcen, A. Alunni, K. Skokova, ERC, Inc., D. Neeb, A. Guelhan, German Aerospace Aerospace Aerodynamics, Beijing, China Moffett Field, CA; D. Empey, Sierra Lobo, Center (DLR), Cologne, Germany; J. Inc., Moffett Field, CA; Y. Chen, NASA Ames Merrifield, Fluid Gravity Engineering, Ltd.,

97 Research Center, Moffett Field, CA Emsworth, United Kingdom Wednesday, 18 June 2014 222-TP-15 Multiphase, Jets and Thermosyphons I University Chaired by: P. YEE, The Aerospace Corporation and S. SUBIA, Sandia National Laboratories 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2014-2819 AIAA-2014-2820 AIAA-2014-2821 AIAA-2014-2822 AIAA-2014-2823 AIAA-2014-2824 BGK and MD Simulations of H2O Numerical investigation of ice particle Global Temperature Measurement Fluid-Structure Interactions in a The effect of noncondensables on Preconditioning Methods for Supersonic Condensed Jets accretion on heated surfaces with of Boiling Water using Dual- Tube Bundle Subject to Cross-Flow. convection in binary-fluid coolants Multiphase Flows Z. Li, A. Borner, A. Rahnamoun, D. Levin, application to aircraft engines Luminescent Imaging Part B : Two-Phase Flow Modeling Y. Li, M. Yoda, Georgia Institute of A. Gupta, K. Sreenivas, L. Taylor, A. van Duin, Pennsylvania State University, D. Kintea, I. Roisman, C. Tropea, Technical G. Hideki, T. Miyazaki, University of E. Tixier, C. Béguin, S. Etienne, D. Technology, Atlanta, GA University of Tennessee, Chattanooga, University Park, PA University of Darmstadt, Darmstadt, Germany Electro-Communications, Tokyo, Japan; Pelletier, A. Hay, G. Ricciardi, École Chattanooga, TN H. Sakaue, Japan Aerospace Exploration Polytechnique de Montréal, Montréal, Agency (JAXA), Tokyo, Japan Canada Wednesday, 18 June 2014 223-TP-16 Theoretical, Analytical and Computational Heat Transfer IV Vinings Chaired by: S. CAI, Teledyne Scientific & Imaging and J. LEE, The Aerospace Corporation 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2014-2825 AIAA-2014-2826 AIAA-2014-2827 AIAA-2014-2828 AIAA-2014-2829 AIAA-2014-2830 Two-Dimensional Analysis of Solids Simulation of a Two Moving Fronts A Numerical Study of Opposing Effect of Wavelength and Numerical Analysis of Ultrafast Heat Transfer in Cross Flow of Gas Subjected to Exponential Heating and Ablation in a Composite Thermal Mixed Convective Heat Transfer Amplitude on Heat Transfer over a Acoustic Wave Generated over a Smooth and Modified Tube Surface Convection Using Thermal Protection System Via an Interface from a Vertical Isothermal Plate Wavy Wall by Picosecond Laser Pulse in L. Ishay, Y. Aharon, G. Ziskind, Ben-Gurion Diffusion and Propagation Models Tracking Method with Laminar and Turbulent Flow H. Shmueli, G. Ziskind, R. Letan, Ben- Multilayers University of the Negev, Beer-Sheva, Israel S. Yi, E. Fong, T. Lam, The Aerospace H. Machado, Aeronautics and Space Institute P. Oosthuizen, Queen’s University, Gurion University of the Negev, Beer- D. Wang, Y. Ma, University of California, Corporation, El Segundo, CA (IAE), São José dos Campos, Brazil Kingston, Canada Sheva, Israel Merced, Merced, CA Wednesday, 18 June 2014 224-NW-9 Wednesday Afternoon Networking Coffee Break Exhibit Hall 1530 - 1600 hrs Wednesday, 18 June 2014 225-ASE-13 AIRA - Aircraft Icing Research Alliance Panel Hanover C 1530 - 1730 hrs Chaired by: J. MACLEOD, National Research Council Canada and M. WADEL, NASA Glenn Research Center

Panelists: HAIC/HIWC International Field Campaign: Overview and Preliminary Outcomes Overview of NASA’s Icing Research Efforts Overview of AIRA Activities and Research Focus Areas Tom Ratvasky Alice Grandin Fabien Dezitter Mary Wadel Jim MacLeod NASA Airbus Airbus Branch Chief, Aircraft Icing, NASA Chair AIRA, NRC

Wednesday, 18 June 2014 226-HYTASP-21 Hypersonic Aircraft Technology Advances and Challenges Panel Regency Ballroom V 1600 - 1730 hrs Moderator: Unmeel Mehta, NASA Ames Research Center Panelists: Rob Vermeland Roger Longstaff Johan Steelant Michael Smart Kevn Bowcutt US UK ESA Australia US

Wednesday, 18 June 2014

98 227-LEC-4 Aerodynamic Measurement Technology Award Lecture: “Nanoscale Instrumentation for Measuring Turbulence” Regency Ballroom VII 1600 - 1700 hrs Alexander J. Smits Eugene Higgins Professor of Mechanical and Aerospace Engineering, Department of Mechanical and Aerospace Engineering, Princeton University, Princeton, NJ Wednesday, 18 June 2014 228-ANERS-2 What is the Right Balance Between Design and Operations? Embassy H 1630 - 1730 hrs Moderator: Eric Nesbitt, The Boeing Company Panelists: Juan Alonso John-Paul Clarke Stanford University Georgia Institute of Technology

Wednesday, 18 June 2014 229-LEC-6 Aeroacoustics Lecture: “Turbofan Noise Research - Reconciling Theory and Measurement” Regency Ballroom VI 1730 - 1830 hrs Brian J. Tester ISVR, Southampton University, Highfield Southampton, United Kingdom Wednesday, 18 June 2014 230-LEC-7 Thermophysics Award Lecture: “Thermophysics of Vaporization and Condensation Processes - A Nanoscale Perspective” Regency Ballroom VII 1730 - 1830 hrs Van P. Carey, Professor A. Richard Newton Chair, Mechanical Engineering Department University of California at Berkeley, Berkeley, CA Wednesday, 18 June 2014 231-FD-18 Transition Open Forum Greenbriar 1800 - 2030 hrs Chaired by: H. REED, Texas A&M University Thursday Thursday, 19 June 2014 232-NW-10 Thursday Morning Networking Breakfast Ballroom Level 0700 - 0800 hrs Thursday, 19 June 2014 233-SB-4 Thursday Morning Speakers’ Briefing Session Rooms 0730 - 0800 hrs Thursday, 19 June 2014 234-PLNRY-4 Thursday Morning Plenary Centennial I/II 99 0800 - 0900 hrs

NextGen Implementation Challenges and Opportunities in an International Context Michael Whitaker Deputy Administrator, FAA Thursday, 19 June 2014 235-NW-11 Thursday Morning Networking Coffee Break Exhibit Hall 0900 - 0930 hrs Thursday, 19 June 2014 236-APA-35 Aerodynamics of Unmanned Aerial Vehicles II Baker Chaired by: B. MCGRATH, JHU/Applied Physics Laboratory 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2014-2831 AIAA-2014-2832 AIAA-2014-2833 AIAA-2014-2834 AIAA-2014-2835 AIAA-2014-2836 Prediction of Aerodynamic Numerical Study of Ram Air Airfoils Kinematics and Inertial Effects in Instantaneous Forces in Locust Accelerating Bio-Inspired MAV On the Effect of Rapid Area Change Characteristics of a Ram-Air Parachute and Upper Surface Bleed-Air Control Locust Flapping Wings Flapping Wings Computations using GPUs in Perching-Like Maneuvers M. Ghoreyshi, J. Seidel, A. Jirasek, A. K. Bergeron, Army Research, Development S. Shkarayev, R. Kumar, University of S. Shkarayev, R. Kumar, University of A. Amritkar, D. Tafti, P. Sathre, K. Hou, S. D. Polet, T. Christensen, D. Rival, Lofthouse, R. Cummings, U.S. Air Force and Engineering Command, Natick, MA; Arizona, Tucson, Tucson, AZ Arizona, Tucson, Tucson, AZ Chivukula, W. Feng, Virginia Polytechnic University of Calgary, Calgary, Canada; Academy, Colorado Springs, CO; K. J. Seidel, M. Ghoreyshi, A. Jirasek, A. Institute and State University, Blacksburg, VA G. Weymouth, Southampton Marine Bergeron, Army Research, Development Lofthouse, R. Cummings, U.S. Air Force and Maritime Institute, Calgary, United and Engineering Command, Natick, MA Academy, Colorado Springs, CO Kingdom Thursday, 19 June 2014 237-APA-36 Other Topics in Applied Aerodynamics - Inlet, Compressor, Diffuser and Nozzle Aerodynamics Courtland Chaired by: S. MORRIS, Engineering Systems, Inc. and A. SCLAFANI, Boeing Engineering Operations & Technology 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2014-2837 AIAA-2014-2838 AIAA-2014-2839 AIAA-2014-2840 Effect of number of slots and Numerical Investigation of Engine Experimental Investigation of the Application study of the curved overlap on the performance of Exhaust Plume Characteristics of Flow in a Stalling Engine Inlet surface compression system Non-circular Ejector Air Diffuser Unmanned Combat Air Vehicles S. Übelacker, R. Hain, C. Kähler, University in three-dimensional sidewall P. Singh, Defence Research and M. Ruetten, S. Karl, German Aerospace of the German Federal Armed Forces, compression inlet Development Organization, Delhi, India; S. Center (DLR), Göttingen, Germany; E. Neubiberg, Germany L. Zhang, K. Zhang, L. Wang, Nanjing Singh, Indian Institute of Technology Delhi, Lindermeir, German Aerospace Center University of Aeronautics and Astronautics, New Delhi, India (DLR), Oberpfaffenhofen, Germany Nanjing, China Thursday, 19 June 2014 238-APA-37 Aerodynamic Testing: Flight, Wind Tunnel and Numerical Correlations IV Dunwoody Chaired by: S. SAXENA, General Electric Company and H. BABINSKY, University of Cambridge 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2014-2841 AIAA-2014-2842 AIAA-2014-2843 AIAA-2014-2844 Supersonic NLF Robustness Flight Aeroelastic Effects in Maximum Lift High lift INflight VAlidation (HINVA) Aerodynamic Characterization Testing: Transition Due to Discrete Prediction of a Transport Aircraft - Overview about the 1st Flight Test of HEXAFLY Scramjet Propelled Roughness Elements and Comparison to Flight Data Campaign Hypersonic Vehicle A. Garzon, J. Matisheck, Aerion S. Keye, D. Rohlmann, German Aerospace R. Rudnik, German Aerospace Center G. Pezzella, M. Marini, M. Cicala, A. Corporation, Reno, NV; D. Banks, M. Center (DLR), Braunschweig, Germany (DLR), Braunschweig, Germany; D. Vitale, Italian Aerospace Research Center Frederick, NASA Armstrong Flight Research Schwetzler, Airbus, Bremen, Germany (CIRA), Capua, Italy; T. Langener, J. Center, Edwards, CA Steelant, ESA, Noordwijk, The Netherlands 100 Thursday, 19 June 2014 239-APA-38 Wind Turbine Aerodynamics II Edgewood Chaired by: J. MURRAY, Sandia National Laboratories 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2014-2845 AIAA-2014-2846 AIAA-2014-2847 AIAA-2014-2848 AIAA-2014-2849 Shape Optimization of NREL S809 Combined Upwind/Downwind Development of Free Vortex Wake A Simulation of Operational Inclusion of a Simple Dynamic Airfoil for Wind Turbine Blades Plasma-Based Flow Control on a Method for Yaw Misalignment Damage for Wind Turbine Blades Inflow Model in the Blade Element Using a Multi-Objective Genetic Vertical-Axis Wind Turbine Effect on the Thrust Vector and G. Fiore, M. Selig, University of Illinois, Momentum Theory for Wind Algorithm R. Lautman, D. Greenblatt, Technion--Israel Generated Power Urbana-Champaign, Urbana, IL Turbine Application Y. He, R. Agarwal, Washington University Institute of Technology, Haifa, Israel H. Abedi, L. Davidson, Chalmers University X. Chen, R. Agarwal, Washington in St. Louis, St. Louis, MO of Technology, Göteborg, Sweden; S. University in St. Louis, St. Louis, MO Voutsinas, National Technical University of Athens, Athens, Greece Thursday, 19 June 2014 240-ATIO-17 Transformational Flight - Distributed Electric Propulsion Embassy C Chaired by: S. RIZZI, NASA-Langley Research Center 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2014-2850 AIAA-2014-2851 AIAA-2014-2852 Oral Presentation Oral Presentation Tradespace Exploration of Drag Reduction Through Distributed Wing Aerodynamic Analysis Aural Effects of Distributed A Modeling Approach to Predict Distributed Propulsors for Advanced Electric Propulsion Incorporating One-Way Interaction Propulsion Cabin Noise due to Distributed On-Demand Mobility Concepts A. Stoll, J. Bevirt, Joby Aviation, Santa Cruz, with Distributed Propellers D. Palumbo, D. Nark, C. Burley, S. Asynchronous Propellers N. Borer, M. Moore, A. Turnbull, NASA CA; M. Moore, W. Fredericks, N. Borer, NASA M. Patterson, B. German, Georgia Institute Rizzi, NASA Langley Research Center, A. Allen, R. Cabell, D. Nark, NASA Langley Langley Research Center, Hampton, VA Langley Research Center, Hampton, VA of Technology, Atlanta, GA Hampton, VA Research Center, Hampton, VA Thursday, 19 June 2014 241-ATIO-18 General Aviation Embassy D Chaired by: C. BIL, RMIT University 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2014-2853 AIAA-2014-2854 AIAA-2014-2855 AIAA-2014-2856 AIAA-2014-2857 AIAA-2014-2858 Ground Performance of a Light Subsonic Business-Class Jet Design: A Preliminary Study of High Lift Feasibility Focused Design of Electric Development of a Castering Pitfalls in Future Air Vehicle Design: Airplane on a Grassy Airfield A Systems Approach to Aircraft System Design and Actuation for a On-demand Aircraft Concepts Nosegear for a Tandem Wing Light Transformational Requirements J. Pytka, L. Kaznowski, Lublin University Synthesis and Optimization Personal Air Vehicle Concept E. Estrada Rodas, J. Lewe, D. Mavris, Georgia Aircraft B. Seeley, CAFE Foundation, Santa of Technology, Lublin, Poland K. Bowerman, P. Chandran, D. Ixtabalan, I. Chakraborty, B. Lozano, T. Nam, D. Mavris, Institute of Technology, Atlanta, GA I. Faruque, University of Maryland, College Rosa, CA D. Sheets, T. Takahashi, Arizona State Georgia Institute of Technology, Atlanta, GA Park, College Park, MD University, Tempe, AZ Thursday, 19 June 2014 242-ATIO-19 ATM-VII Research Analysis in ATM Embassy E Chaired by: A. MUKHERJEE, University of California Santa Cruz 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2014-2859 AIAA-2014-2860 AIAA-2014-2861 AIAA-2014-2862 AIAA-2014-2863 An Independent and Coordinated An Overview of Current Capabilities Autonomous System for Air Traffic Requirements for Communication Large-Scale Data Analysis for Criterion for Kinematic Aircraft and Research Activities in the Control in Terminal Airspace Systems in Future Passenger Air Characterization of the Effect of Maneuvers Airspace Operations Laboratory at A. Nikoleris, H. Erzberger, NASA Ames Transportation Wind Forecast Errors on ETAs A. Narkawicz, C. Munoz, G. Hagen, NASA NASA Ames Research Center Research Center, Moffett Field, CA J. Zambrano, O. Yeste, R. Landry, V. Vaddi, P. Sengupta, M. Tandale, Optimal Langley Research Center, Hampton, VA T. Prevot, N. Smith, E. Palmer, NASA University of Québec, Montréal, Canada Synthesis, Inc., Los Altos, CA; J. Robinson Ames Research Center, Moffett Field, CA; III, NASA Ames Research Center, Moffett T. Callantine, P. Lee, J. Mercer, San Jose Field, CA State University, Moffett Field, CA; et al. 101 Thursday, 19 June 2014 243-ACD-10 Aerodynamic Aircraft Design Embassy F Chaired by: P. RAJ, Virginia Polytechnic Institute and State University 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2014-2864 AIAA-2014-2865 AIAA-2014-2866 AIAA-2014-2867 AIAA-2014-2868 AIAA-2014-2869 Parametric Design Space Drag Model for Airplanes with A Study of Airplane Excrescence UCAV Shape Design with Variable- Planform Optimization of a Flying Shape and Kinematic Design Exploration and Uncertainty Propellers Drag Fidelity Aerodynamic Analysis Wing with a Solid Homogeneous Optimization of the Pterosaur Characterization of Advanced N. Pfeiffer, Pfeiffer Consulting, Wichita, N. Pfeiffer, Pfeiffer Consulting, Wichita, Using Kriging Surrogate Model with Structure replica Concepts Using Gaussian Processes KS; D. Lednicer, Aeromechanical Solutions, KS; D. Lednicer, Aeromechanical Solutions, Regression D. Pate, B. German, Georgia Institute of M. Zakaria, H. Taha, M. Hajj, Virginia H. Schwartz, Georgia Institute of Redmond, WA Redmond, WA Y. Jo, Korea Advanced Institute of Science Technology, Atlanta, GA Polytechnic Institute and State University, Technology, Atlanta, GA and Technology, Daejeon, South Korea; Blacksburg, VA S. Choi, Virginia Polytechnic Institute and State University, Blacksburg, VA; D. Lee, Korea Advanced Institute of Science and Technology, Daejeon, South Korea Thursday, 19 June 2014 244-MAO-11 Multidisciplinary Analysis and Optimization: Uncertainty I Embassy G Chaired by: R. CANFIELD, Virginia Tech 0930 hrs 1000 hrs 1030 hrs AIAA-2014-2870 AIAA-2014-2871 AIAA-2014-2872 Statistical Sensitivity Analysis Uncertainty Propagation for a Covariance Matching Collaborative Considering both Aleatory Subsonic Aircraft in a Coupled Fluid- Optimization for Uncertainty-based and Epistemic Uncertainties in Structure Interaction Environment Multidisciplinary Aircraft Design Multidisciplinary Design during Conceptual Design S. Ghosh, C. Lee, D. Mavris, Georgia Z. Jiang, W. Chen, Northwestern University, K. Raghunath, U.S. Air Force, Robins Institute of Technology, Atlanta, GA Evanston, IL; B. German, Georgia Institute of AFB, GA; D. Rancourt, D. Mavris, Georgia Technology, Atlanta, GA Institute of Technology, Atlanta, GA Thursday, 19 June 2014 245-ANERS-3 ANERS-Technology Embassy H Chaired by: F. COLLIER, NASA-Langley Research Center 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2014-2873 AIAA-2014-2874 AIAA-2014-2875 AIAA-2014-2876 AIAA-2014-2877 AIAA-2014-2878 Assessing the potential benefit of Updated Estimates of N+2 Aircraft Technology Portfolio Analysis Analysis of Vehicle Class DNL Contour Area Sensitivity Representing Multiple Airlines to future technologies to reduce the Technologies Towards meeting a for Environmentally Responsible Contributions to Total DNL to Fleet-Level Operational Study Fleet-Level Environmental environmental impact of airport 2020 Carbon Neutral Goal Aviation Response Characteristics Metrics operations H. Pfaender, H. Jimenez, J. Schutte, D. T. Thompson, Metron Aviation, Inc., J. Bernardo, O. Kiehl, M. Kirby, D. J. Bernardo, M. Kirby, D. Mavris, Georgia I. Tetzloff, W. Crossley, Purdue University, N. Dzikus, German Aerospace Center Mavris, Georgia Institute of Technology, Dulles, VA Mavris, Georgia Institute of Technology, Institute of Technology, Atlanta, GA West Lafayette, IN (DLR), Hamburg, Germany; R. Wollenheit, Atlanta, GA Atlanta, GA German Aerospace Center (DLR), Braunschweig, Germany; M. Schaefer, German Aerospace Center (DLR), Cologne, Germany; V. Gollnick, German Aerospace Center (DLR), Hamburg, Germany Thursday, 19 June 2014 246-APA-39 Vortical/Vortex Flow II Fairlie Chaired by: M. CALVERT, U.S. Army AMRDEC and M. SYTSMA, University of Florida 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2014-2879 AIAA-2014-2880 AIAA-2014-2881 AIAA-2014-2882 3D Flow Field Investigations on Visualization and PIV Aerodynamics of Pitching Wings: Non-linearity of apparent mass for Flapping Wing Aerodynamics Measurements of Leading-edge Theory and Experiments multi-element bodies H. Ehlers, R. Konrath, German Aerospace Vortex generated by Rigid Flapping H. Yu, L. Bernal, University of Michigan, K. Granlund, M. Ol, Air Force Research 102 Center (DLR), Göttingen, Germany; Wings of Different Planforms Ann Arbor, Ann Arbor, MI; K. Granlund, M. Laboratory, Wright-Patterson AFB, OH; L. R. Wokoeck, R. Radespiel, Technical P. Deshpande, R. Antony, National Ol, Air Force Research Laboratory, Wright- Bernal, University of Michigan, Ann Arbor, University of Braunschweig, Braunschweig, Aerospace Laboratories, Bangalore, India; Patterson AFB, OH Ann Arbor, MI Germany P. Narayanan, Naltech Private, Ltd., Bangalore, India; A. Rajashesan, National Institute of Technology, Trichy, India; D. Singh, Manipal Institute of Technology, Manipal, India; G. Ramesh, National Aerospace Laboratories, Bangalore, India Thursday, 19 June 2014 247-FD-22 Low-Speed Boundary Layers: Stability, Transition, and Turbulent Structure Greenbriar Chaired by: B. THUROW, Auburn University 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2014-2883 AIAA-2014-2884 AIAA-2014-2885 AIAA-2014-2886 AIAA-2014-2887 AIAA-2014-2888 Phase Relationships in Presence On non-parallel-flow effects on On the Growth of Görtler Vortices Stability of a boundary layer flow Comparison of Large Scale Features Distributed Roughness Shielding in of a Synthetic Large-Scale in a boundary-layer instability: a non- Excited by Distributed Roughness in the wake of a medium height in Zero and Adverse Pressure a Blasius Boundary Layer Turbulent Boundary Layer perturbative approach based on Elements roughness element Gradient Turbulent Boundary M. Kuester, Texas A&M University, College S. Duvvuri, B. McKeon, California Institute local expansion A. Sescu, R. Pendyala, D. Thompson, B. Plogmann, W. Wuerz, E. Kraemer, Layers Station, TX; A. Sharma, University of Texas, of Technology, Pasadena, CA Z. Huang, Tianjin University, Tianjin, China; Mississippi State University, Mississippi University of Stuttgart, Stuttgart, Germany M. Melnick, B. Thurow, Auburn University, Austin, Austin, TX; E. White, Texas A&M X. Wu, Imperial College London, London, State, MS Auburn, AL University, College Station, TX; D. Goldstein, United Kingdom University of Texas, Austin, Austin, TX Thursday, 19 June 2014 248-AA-18 Jet Noise Measurements I Hanover A Chaired by: P. MORRIS, Pennsylvania State University 0930 hrs 1000 hrs 1030 hrs AIAA-2014-2889 AIAA-2014-2890 AIAA-2014-2891 An experimental investigation Twin Jet Effects on Noise of Round Instability Modes in Screeching into noise radiation from thin and Rectangular Jets: Experiment Elliptical Jets rectangular jets and Model D. Mitchell, D. Honnery, J. Soria, Monash R. Henrywood, A. Agarwal, H. Babinsky, R. Bozak, NASA Glenn Research Center, University, Clayton, Australia University of Cambridge, Cambridge, Cleveland, OH United Kingdom Thursday, 19 June 2014 249-AA-19 CAA Sound Generation II Hanover B Chaired by: T. IMAMURA, The University of Tokyo 0930 hrs 1000 hrs 1030 hrs AIAA-2014-2892 AIAA-2014-2893 AIAA-2014-2894 Evaluation of a time-linearized Numerical Investigation of Active Lattice-Boltzmann Simulations of Navier-Stokes method for booster Flow Control using Steady Blowing the Aeroacoustics Properties of tone noise analyses for Landing Gear Noise Reduction Round Cavities N. Wukie, P. Orkwis, University of Cincinnati, M. Aubert, O. Stanlov, D. Angland, X. A. Hazir, D. Casalino, R. Denis, A. Ribeiro, Cincinnati, OH; J. Wojno, T. Goerig, General Zhang, University of Southampton, Exa Corporation, Stuttgart, Germany Electric Company, Cincinnati, OH Southampton, United Kingdom Thursday, 19 June 2014 103 250-ASE-14/GT-10 NASA Propulsion Systems Laboratory Ice Crystal Engine Icing Test Hanover C Chaired by: M. BRAVIN and J. PATRICK, Lockheed Martin Corporation 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1200 hrs AIAA-2014-2895 AIAA-2014-2896 AIAA-2014-2897 AIAA-2014-2898 AIAA-2014-2899 Turbofan Ice Crystal Rollback PSL Icing Facility Upgrade NASA Glenn Propulsion Systems Validation Ice Crystal Icing Engine Modeling of Commercial Turbofan Investigation and Preparations Overview Lab: 2012 Inaugural Ice Crystal Test in the Propulsion Systems Engine with Ice Crystal Ingestion; Leading to Inaugural Ice Crystal T. Griffin, NASA Glenn Research Center, Cloud Calibration Laboratory at NASA Glenn Follow-On Engine Test at NASA PSL-3 test Facility Cleveland, OH; P. Lizanich, Sierra Lobo, J. Van Zante, NASA Glenn Research Research Center J. Veres, P. Jorgenson, NASA Glenn R. Goodwin, D. Dischinger, Honeywell Inc., Cleveland, OH; D. Dicki, NASA Glenn Center, Cleveland, OH; B. Rosine, Jacobs, M. Oliver, NASA Glenn Research Center, Research Center, Cleveland, OH; R. International, Inc., Phoenix, AZ Research Center, Cleveland, OH Cleveland, OH Cleveland, OH Coennen, Kent State University, Kent, OH Thursday, 19 June 2014 251-ASE-15 Airspace Systems Hazards and Constraints Hanover D Chaired by: J. MURRAY, NASA-Langley Research Center and M. POLITOVICH, National Center for Atmospheric Research 0930 hrs 1000 hrs 1030 hrs AIAA-2014-2900 AIAA-2014-2901 AIAA-2014-2902 Airline and airport operations Observed Heuristics and Biases in Air An Optimized Neural Network under lightning threats - Safety Traffic Management Decision Making Approach for Rapid Unpressurized risks, impacts, uncertainties, and Using Convective Weather Uncertainty Compartment Venting Predictions how to deal with them all W. Gibbons, General Dynamics P. Rodi, Lockheed Martin Corporation, M. Steiner, W. Deierling, K. Ikeda, E. Corporation, Washington, DC; J. Jonsson, Houston, TX Nelson, National Center for Atmospheric Hi-Tec Systems, Washington, DC; S. Research, Boulder, CO; R. Bass, Federal Abelman, R. Bass, Federal Aviation Aviation Administration, Washington, DC Administration, Washington, DC Thursday, 19 June 2014 252-AA-20 Jet Noise Prediction III Hanover E Chaired by: R. EWERT, DLR - German Aerospace Center 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2014-2903 AIAA-2014-2904 AIAA-2014-2905 AIAA-2014-2906 AIAA-2014-2907 Continued development of the one- Experiments on Exhaust Noise Analysis of LES for source modeling Acoustic waveforms produced by a How Small can a Nozzle be for way Euler equations: application of Tightly Integrated Propulsion in jet noise laboratory scale supersonic jet Accurately Scaling Jet Noise to a to jets Systems A. Bassetti, German Aerospace Center (DLR), R. Fiévet, C. Tinney, University of Texas, Larger Nozzle? A. Towne, T. Colonius, California Institute J. Bridges, C. Brown, R. Bozak, NASA Berlin, Germany; J. Nichols, University of Austin, Austin, TX; W. Baars, University of A. Karon, K. Ahuja, Georgia Institute of of Technology, Pasadena, CA Glenn Research Center, Cleveland, OH Minnesota, Minneapolis, Minneapolis, MN Melbourne, Melbourne, Australia Technology, Atlanta, GA Thursday, 19 June 2014 253-AA-21 Boundary Layer Noise Hanover F Chaired by: W. DEVENPORT, Virginia Tech 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2014-2908 AIAA-2014-2909 AIAA-2014-2910 AIAA-2014-2911 AIAA-2014-2912 Noise from Boundary Layer Flow An experimental characterisation of Empirical Spectral Model of Surface The Noise Generating and Analysis of Numerical Simulation over Fabric Covered Perforate wall pressure wavevector-frequency Pressure Fluctuations beneath Suppressing Characteristics of Bio- Database for Acoustic Radiation Panels spectra in the presence of pressure Adverse Pressure Gradients Inspired Rough Surfaces from High-Speed Turbulent W. Alexander, W. Devenport, Virginia gradients M. Catlett, J. Forest, J. Anderson, D. I. Clark, W. Devenport, Virginia Polytechnic Boundary Layers Polytechnic Institute and State University, E. Salze, C. Bailly, O. Marsden, E. Stewart, Naval Surface Warfare Center, Institute and State University, Blacksburg, VA; L. Duan, Missouri University of Science Blacksburg, VA Jondeau, D. Juve, École Centrale de Lyon, West Bethesda, MD J. Jaworski, Lehigh University, Bethlehem, PA; and Technology, Rolla, MO; M. Choudhari, Ecully, France C. Daly, N. Peake, University of Cambridge, NASA Langley Research Center, Hampton, Cambridge, United Kingdom; S. Glegg, Florida VA Atlantic University, Boca Raton, FL 104 Thursday, 19 June 2014 254-AA-22 Acoustic Beamforming I Hanover G Chaired by: R. DOUGHERTY, OptiNav Inc 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2014-2913 AIAA-2014-2914 AIAA-2014-2915 AIAA-2014-2916 AIAA-2014-2917 AIAA-2014-2918 Predicting far-field broadband On Using Functional Beamforming A Two-Microphone Method For The Detection of Non-Stationary An Experimental Comparison of Compressive sensing based noise levels from in-duct phased To Resolve Noise Sources On A Estimation Of The Mode Amplitude Aeroacoustic Sources by Time- Beamforming, Time-reversal and beamforming and its application in array measurements Large Wind Turbine Distribution on Multimode Broadband Domain Imaging Methods Near-field Acoustic holography for aeroacoustic experiment B. Tester, University of Southampton, R. Ramachandran, G. Raman, Illinois Sound Field in Finie-Length Ducts With I. Rakotoarisoa, J. Fischer, D. Marx, V. Aeroacoustic Source Localization Q. Wei, W. Yu, X. Huang, Peking Southampton, United Kingdom; Y. Institute of Technology, Chicago, IL Uniform Mean Flow Valeau, C. Prax, L. Brizzi, National Center Z. Prime, A. Mimani, D. Moreau, C. University, Beijing, China Özyörük, Middle East Technical University, P. Joseph, University of Southampton, for Scientific Research (CNRS), Poitiers, Doolan, University of Adelaide, Adelaide, Ankara, Turkey Southampton, United Kingdom; F. Mouries, France; et al. Australia Snecma, Paris, France; L. Enghardt, German Aerospace Center (DLR), Berlin, Germany Thursday, 19 June 2014 255-FD-23 Multiphase Flows I: Non-Newtonian Liquids, Atomization, and Surface Tension Effects Harris Chaired by: C. TSAI, Lockheed Martin Space Systems and R. SINGH, General Electric Global Research 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2014-2919 AIAA-2014-2920 AIAA-2014-2921 AIAA-2014-2922 Breakup of non-Newtonian Liquid Predicted Liquid Atomization from Transients in Surface Tension Fluid-Particle Interaction in Vortex- Droplets a Spent Nuclear Fuel Reprocessing Driven Flows under Microgravity Induced Dual-Phase Flows Above a P. Khare, V. Yang, Georgia Institute of Pressurization Event A. Karnam, R. Basavanahalli, Indian Sediment Bed Technology, Atlanta, GA A. Brown, F. Gelbard, D. Louie, C. Feng, Institute of Science, Bangalore, India J. Rauleder, J. Leishman, University of N. Bixler, Sandia National Laboratories, Maryland, College Park, College Park, MD Albuquerque, NM Thursday, 19 June 2014 256-FD-24 Simulation Algorithms II Inman Chaired by: J. EDWARDS and J. SITARAMAN, University of WY 0930 hrs 1000 hrs 1030 hrs AIAA-2014-2923 AIAA-2014-2924 AIAA-2014-2925 A Guide to the Implementation Energy stable overset grid methods Multi-scale mesh adaptation for of Boundary Conditions in for hyperbolic problems viscous flows Compact High-Order Methods for N. Sharan, C. Pantano, D. Bodony, A. Loseille, V. Menier, French National Compressible Aerodynamics University of Illinois, Urbana-Champaign, Institute for Research in Computer Science G. Mengaldo, D. De Grazia, F. Witherden, Urbana, IL and Control (INRIA), Paris, France A. Farrington, P. Vincent, S. Sherwin, Imperial College London, London, United Kingdom; et al. Thursday, 19 June 2014 257-FD-25 Airfoils and Wings Kenneshaw Chaired by: J. SCHETZ, Virginia Polytechnic Institute and State University and K. GRANLUND, Air Force Research Laboratory 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2014-2926 AIAA-2014-2927 AIAA-2014-2928 AIAA-2014-2929 Unsteady aerodynamics of an Airfoils Supporting Non-unique Studies of Wings Supporting Non- Transitional Flow and Aeroacoustic airfoil in an oscillating free stream Transonic Solutions for Unsteady unique Solutions in Transonic Flows Prediction of NACA0018 at C. Strangfeld, Technical University of Viscous Flows K. Ou, Honda Aircraft Company, Re=1.6x10^5 Berlin, Berlin, Germany; H. Mueller-Vahl, K. Ou, Honda Aircraft Company, Greensboro, NC; A. Jameson, Stanford F. Mendonca, CD-adapco, London, United D. Greenblatt, Technion--Israel Institute Greensboro, NC; A. Jameson, Stanford University, Stanford, CA; J. Vassberg, The Kingdom; S. Kumar Bonthu, G. Kim, of Technology, Haifa, Israel; C. Nayeri, C. University, Stanford, CA; J. Vassberg, The Boeing Company, Long Beach, CA CD-adapco, Seoul, South Korea

105 Paschereit, Technical University of Berlin, Boeing Company, Long Beach, CA Berlin, Germany Thursday, 19 June 2014 258-HYTASP-8 Propulsion Cycle Performance-Scramjet Tests II Learning Center Chaired by: M. MAITA, Japan Aerospace Exploration Agency and M. KNISKERN, Sandia National Laboratories 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2014-2930 AIAA-2014-2931 AIAA-2014-2932 AIAA-2014-2933 AIAA-2014-2934 Experimental Testing of an Freejet Testing of the 75%-scale Combustion of hydrogen in hot Experimental and Numerical Experimental Investigation of Airframe Integrated 3-D Scramjet HIFiRE 7 REST Scramjet Engine air flows within LAPCAT-II Dual Investigations of a Scramjet Model the Starting Behavior of a three- at True Mach 10 Flight Conditions Y. Wilson Chan, S. Razzaqi, D. Wise, M. Mode Ramjet combustor at Onera- Tested in the H2K Blow Down Wind dimensional SCRamjet Intake with L. Doherty, M. Smart, D. Mee, University Smart, University of Queensland, Brisbane, LAERTE facility - Experimental and Tunnel at Mach 7 Flight Condition a Movable Cowl and Exchangeable of Queensland, Brisbane, Australia Australia Numerical Investigation J. Riehmer, German Aerospace Center (DLR), Cowl Geometry at Different Mach A. Vincent-Randonnier, Y. Moule, M. Cologne, Germany; E. Rabadan, University Numbers Ferrier, ONERA, Palaiseau, France of Stuttgart, Stuttgart, Germany; A. Guelhan, A. Flock, A. Guelhan, German Aerospace German Aerospace Center (DLR), Cologne, Center (DLR), Cologne, Germany Germany; B. Weigand, University of Stuttgart, Stuttgart, Germany Thursday, 19 June 2014 259-FC-12 Closed-Loop Flow Control Lenox Chaired by: D. WILLIAMS, Illinois Institute of Technology and S. GORDEYEV, University of Notre Dame 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2014-2935 AIAA-2014-2936 AIAA-2014-2937 AIAA-2014-2938 Closed-loop Control of Shock Location Robust Nonlinear Control of Two-Dimensional Optimisation Indirect adaptive control of in Mach 1.8 Direct Connect Wind Airfoil Gust-Induced Limit Cycle by Iterative Learning for Flow unknown diffusion equation Tunnel Oscillations Using Synthetic Jet Separation Control T. Airimitoaie, C. Collewet, National J. Ashley, M. Szmuk, N. Clemens, M. Akella, Actuators Z. Cai, D. Angland, X. Zhang, University Institute for Research in Computer Science University of Texas, Austin, Austin, TX; J. V. Golubev, L. Nguyen, M. Counts, B. of Southampton, Southampton, United and Control, Rennes, France Donbar, Air Force Research Laboratory, Wright- Guenthoer, W. MacKunis, N. Ramos, Kingdom; P. Chen, China Aerodynamics Patterson AFB, OH; S. Gogineni, Spectral Embry-Riddle Aeronautical University, Research and Development Center, Energies, LLC, Dayton, OH Daytona Beach, FL Mianyang, China Thursday, 19 June 2014 260-AMT-12/GT-11 Surface Field Measurements Marietta Chaired by: M. REEDER, Air Force Institute of Technology and K. LOWE, Virginia Tech 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2014-2939 AIAA-2014-2940 AIAA-2014-2941 AIAA-2014-2942 AIAA-2014-2943 Transition Detection for Low Speed Large-Span, Non-Contact Surface Characterization of Signal Output of Temperature Cancellation Method Fast Response PSP Measurement In Wind Tunnel Testing using Infrared Profilometry for Laminar-Flow Pressure-Sensitive Paint by Quantum of Motion-Capturing PSP System a Hypersonic Wind Tunnel Thermography Diagnostics Efficiency using Integration Sphere Y. Yamada, T. Okabe, T. Miyazazki, X. Xiang, M. Yuan, J. Yu, China Academy L. Joseph, A. Borgoltz, W. Devenport, B. Crawford, G. Duncan, D. West, W. H. Saeki, H. Ishikawa, Tokyo University of University of Electro-Communications, of Aerospace Aerodynamics, Beijing, Virginia Polytechnic Institute and State Saric, Texas A&M University, College Science, Katsushika, Japan; H. Sakaue, Chofu, Japan; H. Sakaue, Japan Aerospace China; L. Chen, Chinese Academy of University, Blacksburg, VA Station, TX Japan Aerospace Exploration Agency (JAXA), Exploration Agency (JAXA), Chofu, Japan Sciences, Beijing, China

106 Chofu, Japan Thursday, 19 June 2014 261-AA-23 Fan Noise I Piedmont Chaired by: L. LIEBER, Honeywell Aerospace 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2014-2944 AIAA-2014-2945 AIAA-2014-2946 AIAA-2014-2947 AIAA-2014-2948 AIAA-2014-2949 Analysis of Mean Loading Effects in Modelling the Nonlinear Sound RANS-informed fan noise Direct Noise Computation of Numerical Optimization of Fan Tonal noise generation mechanisms Fan Broadband Noise Simulations Propagation and Radiation of prediction: separation and Linear and Nonlinear Rotor-Stator Tonal Noise Control using Acoustic in low-speed mixed-flow fans S. Grace, Boston University, Boston, Supersonic Fan Tones extrapolation of rotor wake and Interaction Modes in Transonic Modulation of Slowly-Rotating T. Newman, A. Agarwal, A. Dowling, MA; L. Ayton, University of Cambridge, O. Adetifa, A. McAlpine, G. Gabard, potential field Cascades Obstructions University of Cambridge, Cambridge, Cambridge, United Kingdom University of Southampton, Southampton, R. Jaron, A. Moreau, S. Guerin, German B. Pimenta, R. Bobenrieth Miserda, S. Magne, M. Sanjose, S. Moreau, United Kingdom; R. Stimpson, Dyson, Ltd., United Kingdom Aerospace Center (DLR), Berlin, Germany University of Brasilia, Brasilia, Brazil A. Berry, University of Sherbrooke, Malmesbury, United Kingdom Sherbrooke, Canada Thursday, 19 June 2014 262-HYTASP-9 Propulsion Component Performance-Combustor Regency Ballroom V Chaired by: A. VIVIANI, Seconda Università di Napoli and R. STARKEY, University of Colorado Boulder 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2014-2950 AIAA-2014-2951 AIAA-2014-2952 AIAA-2014-2953 AIAA-2014-2954 Combustor and Material Integration Mixing and Mass Exchange for Design of a Model Scramjet Experimental Design of a Cavity Inverse Simulation for Hypersonic for high speed aircraft in the European Cavities in Supersonic Flows Combustor for Vortex-Enhanced Flameholder in a Mach 8 Shape- Vehicle Analysis research Program ATLLAS2 F. Barnes, Q. Tu, C. Segal, University of Mixing and Combustion Studies Transitioning Scramjet S. Forbes-Spyratos, I. Jahn, D. Preller, M. M. Bouchez, B. Le Naour, MBDA, Bourges, Florida, Gainesville, Gainesville, FL C. Ground, W. Zhu, L. Maddalena, Z. Denman, S. Brieschenk, A. Smart, University of Queensland, Brisbane, France; C. Davoine, J. Justin, ONERA, University of Texas, Arlington, Arlington, TX Veeraravagan, V. Wheatley, M. Smart, Australia Châtillon, France; J. von Wolfersdorf, M. University of Queensland, Brisbane, Abdelmoula, University of Stuttgart, Stuttgart, Australia Germany; et al. Thursday, 19 June 2014 263-PANEL-7 Towards an Integrated Global ATM - NextGen/Sesar Regency Ballroom VI 0930 - 1100 hrs Moderator: Victoria Cox, Former Assistant Administrator for NextGen, FAA (retired) Panelists: Edward Bolton Marc Hamy Assistant Administrator for NextGen FAA ANG-1 Vice President, SESAR Deployment, Airbus ProSky

Thursday, 19 June 2014 264-AA-24 Duct Liners I Spring Chaired by: G. EFRAIMSSON, KTH Royal Institute Of Technology 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2014-2955 AIAA-2014-2956 AIAA-2014-2957 AIAA-2014-2958 AIAA-2014-2959 AIAA-2014-2960 Comparison of impedance eduction Determination of Liner Impedance Experimental evaluation of the A new computational model for Combined Numerical and Simulations of acoustic wave results using different methods and under High Temperature and acoustic damping effect of single- circumferentially non-uniform liner Experimental Study of a Slit propagation in an impedance test rigs Grazing Flow Conditions layer perforated liners with joint X. Wang, Beihang University, Beijing, Resonator Under Grazing Flow tube using a frequency-domain L. Zhou, H. Boden, Royal Institute of R. Kabral, H. Boden, Royal Institute of bias-grazing flow China; L. Huang, University of Hong H. Denayer, Catholic University of Leuven, linearized Navier-Stokes Technology (KTH), Stockholm, Sweden; Technology (KTH), Stockholm, Sweden; T. C. Ji, D. Zhao, S. Li, X. Li, Nanyang Kong, Hong Kong, China; X. Sun, Beihang Leuven, Belgium; J. Tournadre, LMS methodology C. Lahiri, F. Bake, L. Enghardt, German Elnady, Ain Shams University, Cairo, Egypt Technological University, Singapore, University, Beijing, China International, Leuven, Belgium; W. De W. Na, S. Boij, G. Efraimsson, Royal Aerospace Center (DLR), Berlin, Germany; Singapore Roeck, W. Desmet, Catholic University of Institute of Technology (KTH), Stockholm, S. Busse-Gerstengarbe, Technical University Leuven, Leuven, Belgium; P. Martinez-Lera, Sweden of Berlin, Berlin, Germany; et al. LMS International, Leuven, Belgium Thursday, 19 June 2014

107 265-TP-17 Nonequilibrium Flows II Techwood Chaired by: D. LIECHTY, NASA-Langley Research Center and C. KOBUS, Oakland University 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2014-2961 AIAA-2014-2962 AIAA-2014-2963 AIAA-2014-2964 AIAA-2014-2965 AIAA-2014-2966 Nonequilibrium Modeling of Measurement and Characterization Thermochemical Nonequilibrium Quasiclassical Trajectory Analysis of Radiation intensity measurement Development of Mutation++: Oxygen in Reflected Shock Tube of Mid-wave Infrared Radiation in Modeling of Electronically Excited the N2-N2 Reaction Using New Ab in VUV wavelength region behind Multicomponent Thermodynamic Flows CO2 Shocks Molecular Oxygen Initio Potential Energy Surfaces strong shock wave for future and Transport Properties for K. Neitzel, J. Kim, I. Boyd, University of B. Cruden, A. Brandis, D. Prabhu, ERC, J. Kim, I. Boyd, University of Michigan, J. Bender, G. Candler, S. Doraiswamy, sample return missions Ionized Plasmas written in C++ Michigan, Ann Arbor, Ann Arbor, MI Inc., Moffett Field, CA Ann Arbor, Ann Arbor, MI University of Minnesota, Minneapolis, H. Takayanagi, K. Fujita, Japan Aerospace J. Scoggins, T. Magin, von Kármán Minneapolis, MN Exploration Agency (JAXA), Chofu, Japan; H. Institute for Fluid Dynamics, Rhode-Saint- Ishida, Waseda University, Shinjuku, Japan; K. Genèse, Belgium Yamada, T. Abe, Japan Aerospace Exploration Agency (JAXA), Chofu, Japan Thursday, 19 June 2014 266-TP-18 Heat Transfer in Cooling, Heating and Power Generation II University Chaired by: K. NAWAZ, Johnson Controls Inc. and H. MA, University of Missouri 0930 hrs 1000 hrs 1030 hrs AIAA-2014-2967 Oral Presentation AIAA-2014-2968 Convective heat transfer Measurement of Interface Thermal Heat transfer characteristics of characteristics of supercritical Resistance with Neutron Diffraction hydrocarbon fuel in a horizontal hydrocarbon fuel in small non- S. Lee, Columbia University, New York, NY small tube under different circular cross-section channels pressures Y. Guo, Z. Yang, L. Jiang, Z. Liu, Q. Bi, Z. Yang, L. Jiang, Y. Guo, Z. Liu, Q. Bi, Xi’an Jiaotong University, Xi’an, China Xi’an Jiaotong University, Xi’an, China Thursday, 19 June 2014 267-AA-25 Propeller Noise III Vinings Chaired by: D. LOCKARD, NASA-Langley Research Center 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2014-2969 AIAA-2014-2970 AIAA-2014-2971 AIAA-2014-2972 AIAA-2014-2973 Influence of Torque Ratio on Open Rotor Blade Leading Edge Installation Effects on Contra- Aerodynamic and Aeroacoustics Cyclostationary Spectral Analysis for Counter Rotating Open Rotor Optimization to Mitigate Noise Rotating Open Rotor Noise at Predictions of Wells Turbines Using the Measurement of and Prediction of Interaction Noise Increase Due to Flow Incidence High-Speed LBM Wind Turbine Swishing Noise G. Delattre, ONERA, Meudon, France; F. H. Namgoong, Rolls-Royce Group plc, Y. Colin, F. Wlassow, B. Caruelle, T. Node- M. Meskine, F. Perot, M. Kim, Exa C. Cheong, University of Pusan, Pusan, South Falissard, ONERA, Châtillon, France Derby, United Kingdom Langlois, M. Omais, P. Spiegel, Airbus, Corporation, Brisbane, CA; R. Starzmann, Korea; P. Joseph, University of Southampton, Toulouse, France; et al. T. Carolus, University of Siegen, Siegen, Southampton, United Kingdom Germany Thursday, 19 June 2014 268-LNCH-4 Awards Luncheon: Celebrating Achievements in Aircraft and Atmospheric Systems Centennial I/II 1230 - 1400 hrs Thursday, 19 June 2014 269-APA-40 Flow Control (Active and Passive): Computational and Experimental Results VI Baker Chaired by: V. BHAGWANDIN, US Army Research Laboratory and G. GATLIN 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2014-2974 AIAA-2014-2975 AIAA-2014-2976 AIAA-2014-2977 AIAA-2014-2978 AIAA-2014-2979 Improving robust stability by Towards the Noise Reduction of Effectiveness of Flow Separation Comparison of Experimental and Large Low-Frequency Oscillations Active Control of Flow over increasing the number of controlled Piezoelectrical-Driven Synthetic Jet Control on Contour Bumps under Computational Flow Structure Initiated by Sub-Optimal Flow Backward Facing Step by Synthetic degrees of freedom Actuators a Mach 1.3 Freestream: An Investigations of a Normal-Hole Control on a Post-Stall Airfoil Jets 108 T. Airimitoaie, C. Collewet, National M. Jabbal, S. Kykkotis, Brunel University, Experimental Study Bled Supersonic Boundary Layer C. Bernardini, S. Benton, K. Hipp, J. Bons, Z. Zhang, D. Li, Northwestern Polytechnical Institute for Research in Computer Science Uxbridge, United Kingdom K. Lo, University of Manchester, J. Oorebeek, H. Babinsky, University of Ohio State University, Columbus, OH University, Xi’an, China; X. Ming, Nanjing and Control, Rennes, France Manchester, United Kingdom; H. Zare- Cambridge, Cambridge, United Kingdom; University of Aeronautics and Astronautics, Behtash, K. Kontis, University of Glasgow, M. Ugolotti, P. Orkwis, S. Duncan, Nanjing, China Glasgow, United Kingdom University of Cincinnati, Cincinnati, OH Thursday, 19 June 2014 270-APA-41 Aerodynamic Analysis and Design: Higher Order Methods in CFD Courtland Chaired by: J. SLOTNICK, Boeing Engineering Operations & Technology and P. MORGAN, Ohio Aerospace Institute 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs AIAA-2014-2980 AIAA-2014-2981 AIAA-2014-2982 AIAA-2014-2983 AIAA-2014-2984 AIAA-2014-2985 AIAA-2014-2986 A Streamline/Upwind Petrov A High-Order Discontinuous Time-integration for incompressible High-Order Finite-Element Method A Comparative Study of High-order residual-based compact A high-order and conservative method Galerkin Overset Grid Scheme for Galerkin Method for External viscous flows: Stepsize and order and Dynamic Adaptation for Two- Discontinuous High Order Methods schemes for compressible flows on is developed for the numerical the Navier-Stokes Equations with Aerodynamics selection based on the BDF Dimensional Laminar and Turbulent for Compressible Flows overset grids treatment of interface conditions in Moving Domains I. Bosnyakov, S. Lyapunov, A. Troshin, V. A. Hay, S. Etienne, D. Pelletier, École Navier-Stokes C. Breviglieri, L. Paula, Aeronautics and P. Outtier, C. Content, P. Cinnella, Paris patched grids, based on the use of C. Liu, J. Newman, W. Anderson, Vlasenko, A. Wolkov, TsAGI, Zhukovsky, Polytechnique de Montréal, Montréal, B. Reza Ahrabi, W. Anderson, J. Newman, Space Institute (IAE), São José dos Institute of Technology, Paris, France a fictitious grid methodology. The University of Tennessee, Chattanooga, Russia; C. Hirsch, NUMECA International, Canada University of Tennessee, Chattanooga, Campos, Brazil; W. Wolf, F. Moreira, proposed approach is compared with a Chattanooga, TN Brussels, Belgium Chattanooga, TN University of Campinas, Campinas, Brazil; non-conservative interpolation of the J. Azevedo, Technological Institute of Aeronautics (ITA), São José dos Campos, state variables from the neighbouring Brazil domain for selected internal flow problems B. Maugars, ONERA, Châtillon, France; P. Cinnella, Paris Institute of Technology, Paris, France; B. Michel, ONERA, Châtillon, France Thursday, 19 June 2014 271-APA-42 Aerodynamic Analysis and Design: Analysis Methods I Dunwoody Chaired by: K. VANDEN, USAF and D. LACY, Boeing Commercial Airplanes 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2014-2987 AIAA-2014-2988 AIAA-2014-2989 AIAA-2014-2990 AIAA-2014-2991 AIAA-2014-2992 Development of a Transonic Highly non-planar Lifting Systems: Application of Non-Planar Lifting- Aerodynamic Analysis of Next Development and Application of Investigation on Non-linear Fin Aerodynamic Database for A relative assessment of existing Line Theory to Simple Aeroelastic Generation Supersonic Decelerators a New Unsteady Far-Field Drag Characteristic of Yawing Moment of Incorporation into Missile Datcom Potential-Methodologies to accurately Problems S. Muppidi, ERC, Inc., Moffett Field, CA; Decomposition Method Twin-tailed Configuration W. Coirier, J. Stutts, Kratos/Digital estimate the Induced Drag A. Kuenn, L. Kliment, K. Rokhsaz, Wichita C. Tang, NASA Ames Research Center, H. Toubin, D. Bailly, ONERA, Meudon, Y. Qin, Y. Wang, Q. Li, Beihang University, Fusion, Inc., Huntsville, AL; C. Rosema, J. Schirra, RMIT University, Melbourne, State University, Wichita, KS Moffett Field, CA; J. Van Norman, NASA France Beijing, China Army Aviation and Missile Research Australia; J. Watmuff, M. Bauschat, Aachen Langley Research Center, Hampton, VA; Development and Engineering Center, University of Applied Sciences, Aachen, D. Bose, NASA Ames Research Center, Huntsville, AL Germany Moffett Field, CA Thursday, 19 June 2014 272-APA-43 Airfoil/Wing/Configuration Aerodynamics II Edgewood Chaired by: L. WANG, University of Tennessee at Chattanooga and J. LATZ, Northrop Grumman Aerospace Systems 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2014-2993 AIAA-2014-2994 AIAA-2014-2995 AIAA-2014-2996 AIAA-2014-2997 AIAA-2014-2998 Experimental Dynamic Stall Study Investigation of Unsteady Flow on Impact of Mean Flow Shear on the Multifidelity Airfoil Shape Feature Based Grid Adaption for Non-Linear Aerodynamic Modeling In An Airfoil a High Aspect Ratio Wing Wake Vortical Structure behind Optimization Using Adaptive the Study of Dynamic Stall of Airfoils for Accurate Blade J. Marañon, J. Delnero, A. Canchero, S. Skomorokhov, B. Nikolay, G. Mansur, Oscillating Airfoils Meshing K. Hord, Y. Lian, University of Louisville, Element Propeller Performance National University of La Plata, La Plata, TsAGI, Zhukovsky, Russia M. Yu, Z. Wang, S. Farokhi, University of D. Dalle, K. Fidkowski, University of Louisville, KY Predictions Argentina Kansas, Lawrence, Lawrence, KS Michigan, Ann Arbor, Ann Arbor, MI J. Dorfling, K. Rokhsaz, Wichita State University, Wichita, KS 109 Thursday, 19 June 2014 273-ATIO-20 Transformational Flight - Distributed Electric Propulsion Control Embassy C Chaired by: B. GERMAN, Georgia Institute of Technology 1400 hrs 1430 hrs 1500 hrs 1530 hrs AIAA-2014-2999 AIAA-2014-3000 Oral Presentation Oral Presentation NASA Langley Distributed Enabling Advanced Wind-Tunnel Rapid Control Law Development Streamlined Methods for Flight Test Propulsion VTOL TiltWing Aircraft Research Methods Using the NASA Enabled By General Dynamics Evaluation of Unique Distributed Testing, Modeling, Simulation, Langley 12-Foot Low Speed Tunnel Formulation and Modular Simulation Propulsion Concepts Control, and Flight Test R. Busan, P. Rothhaar, M. Croom, P. Environment for VTOL TiltWing P. Rothhaar, NASA Langley Research Development Murphy, NASA Langley Research Center, UAV with Distributed Propulsion - Center, Hampton, VA P. Rothhaar, P. Murphy, B. Bacon, I. Hampton, VA; S. Grafton, Analytical Challenges and Opportunities Gregory, J. Grauer, R. Busan, NASA Mechanics Associates, Inc., Hampton, VA; I. Gregory, NASA Langley Research Center, Langley Research Center, Hampton, VA; A. O’Neal, ViGYAN, Inc., Hampton, VA Hampton, VA et al. Thursday, 19 June 2014 274-DE-1 Design Engineering and Education Embassy D Chaired by: V. BALABANOV, Boeing Commercial Airplanes and S. ROWE, NASA Marshall Space Flight Center 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs AIAA-2014-3001 AIAA-2014-3002 AIAA-2014-3003 AIAA-2014-3004 AIAA-2014-3005 ‘Projet Epervier’: Design, Build and Analysis of Aspect Ratio and Aerial Robotic Autonomous Patrol Optimization of Air Distribution in Projet Pégase: Increasing Interest Flight Test of a Full-Scale Aerobatic Winglet Height of a Box Wing and Surveillance System a Preliminary Design Stage of an in STEM Through Design and Flight Aircraft at the Universite de Design A. Khalid, Southern Polytechnic State Aero-Engine Combustor of a Human Powered Aircraft Sherbrooke P. Kumar, A. Khalid, Southern Polytechnic University, Marietta, GA A. Angersbach, D. Bestle, Brandenburg F. Bolduc-Teasdale, E. Demers Bouchard, D. Rancourt, M. Lavoie, F. Charron, University State University, Marietta, GA University of Technology, Cottbus, D. Rancourt, F. Charron, University of of Sherbrooke, Sherbrooke, Canada Germany Sherbrooke, Sherbrooke, Canada Thursday, 19 June 2014 275-ATIO-22 Enroute Operations Embassy E Chaired by: K. MARAIS, Purdue University 1400 hrs 1600 hrs 1630 hrs No Presentations AIAA-2014-3006 AIAA-2014-3007 Commercial Airline Altitude Total Fuel Reduction via Formation Optimization Strategies for Flights; A New Approach to Air- Reduced Cruise Fuel Consumption Corridor Path Optimization L. Jensen, R. Hansman, Massachusetts F. Asadi, S. Malaek, Sharif University of Institute of Technology, Cambridge, MA; Technology, Tehran, Iran J. Venuti, T. Reynolds, Lincoln Laboratory, Massachusetts Institute of Technology, Lexington, MA Thursday, 19 June 2014 276-ACD-11 Aircraft Integration of Innovative Propulsion Concepts Embassy F Chaired by: M. HOLLY, Boeing Defense, Space & Security 1400 hrs 1430 hrs AIAA-2014-3008 AIAA-2014-3009 Design of Hybrid-Electric Propulsion The Application of LENR to Systems for Light Aircraft Synergistic Mission Capabilities C. Friedrich, P. Robertson, University of D. Wells, NASA Langley Research Center, Cambridge, Cambridge, United Kingdom Hampton, VA; D. Mavris, Georgia Institute of Technology, Atlanta, GA

110 Thursday, 19 June 2014 277-ACD-12 Aircraft Subsystems Design and Integration Embassy F Chaired by: J. MERRET, Gulfstream Aerospace Corporation 1400 hrs 1600 hrs 1630 hrs 1700 hrs No Presntations AIAA-2014-3010 AIAA-2014-3011 AIAA-2014-3012 Design of an Improved Green System-Level Performance Impact Vehicle and Mission Level Taxiing System Focused around the of Active Flow Control Vertical Tails Subsystem Architecture Comparison Landing Gear on a Commercial Transport Model Using Pacelab SysArc C. Frank, J. Durand, W. Levy, F. Allair, D. Family I. Chakraborty, D. Trawick, D. Mavris, Mavris, Georgia Institute of Technology, R. Jacobs, D. Mavris, Georgia Institute of Georgia Institute of Technology, Atlanta, Atlanta, GA Technology, Atlanta, GA GA; M. Emeneth, A. Schneegans, PACE America, Inc., Seattle, WA Thursday, 19 June 2014 278-MAO-12 Multidisciplinary Analysis and Optimization: Uncertainty II Embassy G Chaired by: B. MESMER, Iowa State Univ 1400 hrs 1430 hrs 1500 hrs AIAA-2014-3013 AIAA-2014-3014 AIAA-2014-3015 Multi-Fidelity Uncertainty Decoupled UMDO formulation The Multi-disciplinary Robust Quantification: Application to a for interdisciplinary coupling Optimization for Tailless Aircraft Vertical Axis Wind Turbine Under satisfaction under uncertainty M. Liu, Y. Hu, Northwestern Polytechnical an Extreme Gust L. Brevault, M. Balesdent, N. Berend, University, Xi’an, China A. Padron, J. Alonso, F. Palacios, Stanford ONERA, Palaiseau, France; R. Le Riche, University, Stanford, CA; M. Barone, M. National Center for Scientific Research Eldred, Sandia National Laboratories, (CNRS), St. Etienne, France Albuquerque, NM Thursday, 19 June 2014 279-ANERS-4 ANERS-ATM Operations Embassy H Chaired by: P. HULLAH, Eurocontrol 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs AIAA-2014-3016 AIAA-2014-3017 AIAA-2014-3018 AIAA-2014-3019 AIAA-2014-3020 Identification of Flights for Cost- Achieving Climate-optimal Climb, Cruise and Descent 3D Vertical Navigation Trajectory Runway Shape Optimization for Efficient Climate Impact Reduction Trajectories: How Do We Allocate Trajectory Optimization Algorithm Optimization Algorithm for the Reducing Airport Environmental N. Chen, NASA Ames Research Center, Responsibilities? for the FMS CMA-9000 Lockheed L-1011 Impact and Increasing Aircraft Moffett Field, CA; P. Kirschen, University of T. Thompson, Metron Aviation, Inc., R. Félix Patrón, Y. Berrou, R. Botez, École A. Murrieta Mendoza, R. Botez, University Productivity Michigan, Moffett Field, Moffett Field, CA; Dulles, VA de Technologie Supérieure, Montréal, of Québec, Montréal, Canada; D. Labour, A. Elham, R. Curran, Delft University of B. Sridhar, NASA Ames Research Center, Canada CMC Electronics-Esterline, Montréal, Technology, Delft, The Netherlands Moffett Field, CA; H. Ng, University of Canada California, Santa Cruz, Moffett Field, CA Thursday, 19 June 2014 280-APA-44 Missile, Projectile, Guided-Munitions, Carriage and Store Separation Aerodynamics Fairlie Chaired by: C. ROSEMA, US Army AMRDEC and K. DENISSEN, Sandia National Labs 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs AIAA-2014-3021 AIAA-2014-3022 AIAA-2014-3023 AIAA-2014-3024 AIAA-2014-3025 AIAA-2014-3026 AIAA-2014-3027 Numerical Experiments on Finned Effect of Projectile Aft End Turbulence Model Effects on Cold- Unsteady Aerodynamic Simulations Complex Geometry Effects on Open Mitigation of Wind Tunnel Wall Joint Experimental/Computational Bodies on Stability, Range, and Gas Lateral Jet Interaction in a of a Finned Projectile at a Supersonic Cavity Dynamics Interactions in Subsonic Cavity Investigation Into the Effects of Finite S. Silton, Army Research Laboratory, Maneuverability Supersonic Crossflow Speed with Jet Interaction K. Casper, J. Wagner, S. Beresh, J. Flows Width on Transonic Cavity Flow Aberdeen Proving Ground, MD S. Silton, F. Fresconi, Army Research J. DeSpirito, Army Research Laboratory, J. Sahu, F. Fresconi, K. Heavey, Army Research Henfling, R. Spillers, B. Pruett, Sandia J. Wagner, K. Casper, S. Beresh, B. Pruett, S. Arunajatesan, M. Barone, J. Wagner, Laboratory, Aberdeen Proving Ground, MD Aberdeen Proving Ground, MD Laboratory, Aberdeen Proving Ground, MD National Laboratories, Albuquerque, NM R. Spillers, J. Henfling, Sandia National K. Casper, S. Beresh, Sandia National Laboratories, Albuquerque, NM Laboratories, Albuquerque, NM 111 Thursday, 19 June 2014 281-FD-26 Detonation and Supersonic Combustion Greenbriar Chaired by: P. HAMLINGTON 1400 hrs 1430 hrs 1500 hrs 1530 hrs AIAA-2014-3028 AIAA-2014-3029 AIAA-2014-3030 AIAA-2014-3031 Detonation initiation and Detonation initiation and Large-Eddy Simulation of Examination of Turbulent Flow propagation in the nonuniform propagation in supersonic Supersonic Reacting Mixing Layers Effects in Rotating Detonation supersonic combustible mixtures combustible mixtures with a cavity A. Kartha, P. Subbareddy, G. Candler, Engines X. Cai, J. Liang, Z. Lin, National University embedded in the channel University of Minnesota, Minneapolis, C. Towery, K. Smith, P. Shrestha, P. of Defense Technology, Changsha, China; X. Cai, J. Liang, Z. Lin, National University Minneapolis, MN; P. Dimotakis, California Hamlington, University of Colorado, F. Zhuang, Academy of Equipment, Beijing, of Defense Technology, Changsha, China; Institute of Technology, Pasadena, CA Boulder, Boulder, CO; M. Van Schoor, Midé China F. Zhuang, Academy of Equipment, Beijing, Technology, Medford, MA China Thursday, 19 June 2014 282-AA-26 Jet Noise Measurements II Hanover A Chaired by: J. BRIDGES, NASA Glenn Research Center 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2014-3032 AIAA-2014-3033 AIAA-2014-3034 AIAA-2014-3035 AIAA-2014-3036 AIAA-2014-3037 Large-Scale Jet Noise Testing, Large-Scale Jet Noise Testing, Large-Scale Jet Noise Testing, Large-Scale Jet Noise Testing, Large-Scale Jet Noise Testing, Unstructured LES of the baseline Reduction and Methods Validation Reduction and Methods Validation Reduction and Methods Validation Reduction and Methods Validation Reduction and Methods Validation EXEJET dual-stream jet “EXEJET”: 1. Project Overview and “EXEJET”: 2. Optimisation of ‘EXEJET’: 3. Hybrid RANS-CAA “EXEJET”: 4. Flows characterization “EXEJET”: 5. Analysis of jet-airfoil M. Sanjose, A. Fosso Pouangue, S. Focus on Installation chevron design aimed at jet noise methods for noise prediction of with PIV in the CEPRA19 anechoic interaction noise by microphone Moreau, G. Wang, T. Padois, University of J. Huber, G. Drochon, C. Bonnaud, A. reduction of future turbofans dual stream jets wind tunnel of ONERA array techniques Sherbrooke, Sherbrooke, Canada Pintado-Peno, Airbus, Toulouse, France; M. Koenig, G. Bodard, I. Kernemp, G. Brichet, G. Bodard, M. Koenig, Snecma, F. David, J. Jourdan, F. Cléro, ONERA, Châtillon, V. Fleury, R. Davy, ONERA, Châtillon, F. Cléro, ONERA, Châtillon, France; G. Snecma, Moissy-Cramayel, France Moissy-Cramayel, France France; J. Huber, Airbus, Toulouse, France; M. France Bodard, Snecma, Villaroche, France Koenig, Snecma, Moissy-Cramayel, France Thursday, 19 June 2014 283-AA-27 Trailing Edge Noise I Hanover B Chaired by: P. JOSEPH, University of Southampton 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2014-3038 AIAA-2014-3039 AIAA-2014-3040 AIAA-2014-3041 AIAA-2014-3042 AIAA-2014-3043 Noise Sources of Trailing-Edge Trailing Edge Noise of Partially Adjoint-based Trailing-Edge Noise Specification of Porous Materials for Volume Noise Sources in Turbulent Simulation of Tonal Noise Turbulence Controlled by Porous Porous Airfoils Minimization using Porous Material Low-Noise Trailing-Edge Applications Wake Interaction Problems: True Generated by Transition Flow Past Media T. Geyer, E. Sarradj, Brandenburg B. Zhou, N. Gauger, S. Koh, M. Meinke, M. Herr, K. Rossignol, J. Delfs, German Quadrupole Noise? Airfoil Using High-Order Schemes S. Koh, M. Meinke, W. Schroeder, B. University of Technology, Cottbus, W. Schroeder, RWTH Aachen University, Aerospace Center (DLR), Braunschweig, C. Yu, S. Lele, Stanford University, on Unstructured Grids Zhou, N. Gauger, RWTH Aachen University, Germany Aachen, Germany Germany; N. Lippitz, M. Mößner, Technical Stanford, CA H. Yang, CFD Research Corporation, Aachen, Germany University of Braunschweig, Braunschweig, Huntsville, AL Germany Thursday, 19 June 2014 284-ASE-16 Engine Icing II - Ice Crystal Accretion and Particle Impact Dynamics Hanover C Chaired by: C. TAN, GE Global Research and D. FULEKI, National Research Council Canada 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2014-3044 AIAA-2014-3045 AIAA-2014-3046 AIAA-2014-3047 AIAA-2014-3048 AIAA-2014-3049 Possible Mechanisms for Turbofan Ice Particle Impacts on a Moving Investigation of the Impact Experimental Measurement of Modeling and Analysis of Ice Shed in Experimental Studies of Mixed- Engine Ice Crystal Icing at High Wedge Behaviour of Ice Particles Frozen and Partially Melted Water Multistage Compressor of Jet Engines Phase Sticking Efficiency for Ice Altitude M. Vargas, P. Struk, R. Kreeger, NASA T. Hauk, EADS, Munich, Germany; I. Droplet Impact Dynamics R. Kundu, J. Prasad, Georgia Institute of Crystal Accretion in Jet Engines J. Tsao, Ohio Aerospace Institute, Glenn Research Center, Cleveland, OH; J. Roisman, C. Tropea, Technical University of J. Palacios, S. Yan, Pennsylvania State Technology, Atlanta, GA; R. Singh, S. Saxena, T. Currie, D. Fuleki, A. Mahallati, National Cleveland, OH; P. Struk, M. Oliver, NASA Palacios, Pennsylvania State University, Darmstadt, Darmstadt, Germany University, University Park, PA; C. Tan, General Electric Company, Niskayuna, NY; Research Council Canada, Ottawa, Canada Glenn Research Center, Cleveland, OH University Park, PA; K. Iyer, R. Gold, General Electric Company, Niskayuna, NY; A. Breeze-Stringfellow, T. Nakano, General Johns Hopkins University Applied Physics R. Kreeger, NASA Glenn Research Center, Electric Company, Cincinnati, OH

112 Laboratory, Laurel, MD Cleveland, OH Thursday, 19 June 2014 285-AA-28 CAA Sound Generation III Hanover D Chaired by: J. COUPLAND, University of Southampton 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2014-3050 AIAA-2014-3051 AIAA-2014-3052 AIAA-2014-3053 AIAA-2014-3054 AIAA-2014-3055 Wall-resolved Large Eddy Variations on the same BANC High-Order Discontinuous Galerkin Linear- and Non-Linear Prediction of harmonic sound Large-Scale High-Lift CAA-RPM Simulation of a highlift airfoil: Category 8 theme: Towards the and Hybrid RANS/LES Method for Perturbation Equations with power generated by a modern Simulations detailed flow analysis and noise Development of a High Fidelity Prediction of Launch Vehicle Lift- Relaxation Source Terms for Forced turbofan with heterogeneous OGV A. Kolb, EADS, Munich, Germany; A. generation study Acoustic Hybrid Method using Off Acoustic Environments Eddy Simulation of Aeroacoustic and internal bifurcations Buescher, Airbus, Bremen, Germany; R. M. Terracol, E. Manoha, ONERA, Châtillon, Computational AeroAcoustics R. Harris, CFD Research Corporation, Sound Generation V. Bonneau, Snecma, Villaroche, France; Ewert, German Aerospace Center (DLR), France S. Redonnet, ONERA, Châtillon, France; Huntsville, AL; E. Collins, A. Sescu, R. Ewert, J. Dierke, A. Neifeld, German C. Polacsek, ONERA, Châtillon, France; R. Braunschweig, Germany G. Cunha, National Institute for Space E. Luke, Mississippi State University, Aerospace Center (DLR), Braunschweig, Barrier, ONERA, Meudon, France Research (INPE), São Paulo, Brazil Mississippi State, MS Germany; M. Alavi Moghadam, RWTH Aachen University, Aachen, Germany Thursday, 19 June 2014 286-AA-29 Jet Noise Prediction IV Hanover E Chaired by: D. MCLAUGHLIN, Pennsylvania State University 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2014-3056 AIAA-2014-3057 AIAA-2014-3058 AIAA-2014-3059 AIAA-2014-3060 AIAA-2014-3061 Thoughts on Use of University-Scale Recent progress in LES computation ARMAX system identification Towards Prediction of Jet Noise Numerical and Experimental Study Just enough jitter for jet noise? Rocket Models to Study Launch for aeroacoustics of turbulent hot applied to a subsonic turbulent jet Installation Effect using Stochastic of JFI Effect on Swept Wing M. Zhang, P. Jordan, G. Lehnasch, National Acoustics jet. Comparison to experiments and S. Piantanida, M. Le Rallic, P. Jordan, Source Modeling V. Kopiev, I. Belyaev, G. Faranosov, V. Center for Scientific Research (CNRS), K. Ahuja, D. Alvord, J. Mattingly, J. near field analysis T. Duriez, National Center for Scientific A. Neifeld, R. Ewert, M. Steger, D. Kopiev, N. Ostrikov, M. Zaytsev, TsAGI, Poitiers, France; A. Cavalieri, Technological Mittelman, D. Dickey, D. Alvord, Georgia M. Lorteau, F. Cléro, F. Vuillot, ONERA, Research (CNRS), Poitiers, France Keller, German Aerospace Center (DLR), Moscow, Russia; et al. Institute of Aeronautics (ITA), São Institute of Technology, Atlanta, GA Châtillon, France Braunschweig, Germany; M. Steger, Rolls- Paulo, Brazil; A. Agarwal, University of Royce Deutschland, Blankenfelde-Mahlow, Cambridge, Cambridge, United Kingdom Germany Thursday, 19 June 2014 287-AA-30 Airframe Noise III Hanover F Chaired by: C. BAHR, NASA-Langley Research Center 1400 hrs 1430 hrs 1500 hrs 1530 hrs AIAA-2014-3062 AIAA-2014-3063 AIAA-2014-3064 AIAA-2014-3065 An Experimental Investigation of the Experimental study of a noise Listening to Turbulence: Measuring Composite Materials Providing 30P30N Multi-Element High-Lift Airfoil reduction concept for realistic Coherence Decay at Different Improved Acoustic Transmission K. Pascioni, L. Cattafesta, Florida State landing gear geometries Positions on an Aircraft in Cruise Loss for UAVs University, Tallahassee, FL; M. Choudhari, I. Belyaev, V. Kopiev, I. Pankratov, M. Flight J. Callicoat, R. Gaeta, J. Jacob, Oklahoma NASA Langley Research Center, Hampton, VA Zaytsev, TsAGI, Moscow, Russia S. Haxter, C. Spehr, German Aerospace State University, Stillwater, OK Center (DLR), Göttingen, Germany 113 Thursday, 19 June 2014 288-AA-31 Acoustic Beamforming II Hanover G Chaired by: P. SIJTSMA, National Aerospace Laboratory (NLR) 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2014-3066 AIAA-2014-3067 AIAA-2014-3068 AIAA-2014-3069 AIAA-2014-3070 AIAA-2014-3071 Functional Beamforming for Engine noise source breakdowns Validation of Beamforming Analysis Phased-array measurements of Microphone-array measurements of a Advanced Aeroacoustic Testing Aeroacoustic Source Distributions from an improved inverse method Methodology with Synthesized full-scale military jet noise Rolls-Royce BR700 series aeroengine Techniques Using Various Methods R. Dougherty, OptiNav, Inc., Bellevue, WA (AFINDS) of processing phased Acoustic Time History Data: Sub- B. Harker, K. Gee, T. Neilsen, Brigham in an indoor test-bed and comparison of Acoustic Holography array measurements Scale Fan Rig System Young University, Provo, UT; A. Wall, with free-field data K. Chelliah, G. Raman, Illinois Institute of B. Tester, University of Southampton, T. Marotta, L. Lieber, Honeywell Air Force Research Laboratory, Wright- S. Funke, H. Siller, W. Hage, German Technology, Chicago, IL Southampton, United Kingdom International, Inc., Phoenix, AZ; R. Patterson AFB, OH; M. James, Blue Aerospace Center (DLR), Berlin, Germany; Dougherty, OptiNav, Inc., Bellevue, WA Ridge Research and Consulting, LLC, O. Lemke, Rolls-Royce Group plc, Dahlewitz, Asheville, NC Germany Thursday, 19 June 2014 289-FD-27 Multiphase Flows II: Air/Water Systems and Icing Harris Chaired by: P. ANSELL 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs AIAA-2014-3072 AIAA-2014-3073 AIAA-2014-3074 AIAA-2014-3075 AIAA-2014-3076 A 3D Mesh Deformation Technique Icing Collection Efficiency Prediction Unsteady Modes in the Flowfield Virus Transport Aboard Commercial Multi-Phase Modeling of Rainbird for Irregular In-flight Ice Accretion Using an Eulerian-Eulerian Approach about an Airfoil with a Horn-Ice Shape Regional Aircraft Water Injection Shapes D. da Silva, Embraer, São José dos Campos, P. Ansell, University of Illinois, Urbana- S. Taherian, H. Rahai, J. Bonifacio, B. Vu, N. Moss, Z. Sampson, NASA A. Pendenza, W. Habashi, M. Fossati, Brazil; N. Bachchan, I. Kim, O. Peroomian, Champaign, Urbana, IL; M. Bragg, University California State University, Long Beach, Kennedy Space Center, Cape Canaveral, FL McGill University, Montréal, Canada Metacomp Technologies, Los Angeles, CA of Washington, Seattle, Seattle, WA CA; R. Horstman, Self, Snohomish, WA Thursday, 19 June 2014 290-FD-28 Supersonic Boundary Layers: Fundamental Studies Inman Chaired by: H. JOHNSON, University of Minnesota 1400 hrs 1430 hrs 1500 hrs AIAA-2014-3077 AIAA-2014-3078 AIAA-2014-3079 Spectral Analysis of Stationary DNS of a flat-plate supersonic Effects of Surface Curvature Crossflow Vortex Tracks in boundary layer using the on Flow Interactions of Small Sublimating Chemical Using Image discontinuous Galerkin spectral Cylindrical Protuberances and the Processing element method Supersonic Turbulent Boundary P. McGuire, University of California, San M. Atak, University of Stuttgart, Stuttgart, Layer Diego, La Jolla, CA Germany; J. Larsson, University of E. Stephen, K. Huynh, A. Kwakenat, E. Maryland, College Park, College Park, McCartney, R. Decker, T. McLaughlin, U.S. MD; G. Gassner, C. Munz, University of Air Force Academy, Colorado Springs, CO Stuttgart, Stuttgart, Germany Thursday, 19 June 2014 291-FD-29 Simulation Algorithms III Kenneshaw Chaired by: C. ROY, Virginia Tech and H. LUO, North Carolina State University 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2014-3080 AIAA-2014-3081 AIAA-2014-3082 AIAA-2014-3083 AIAA-2014-3084 AIAA-2014-3085 Parallelization of Unsteady On the Multi-GPU Computing of Accelerating Finite-Volume Based GPU Port of A Parallel A Preconditioned Non-Singular Implicit Runge-Kutta Physical-Time Adaptive Mesh Refinement for a Reconstructed Discontinuous Lattice Boltzmann Flow Solutions Incompressible Navier-Stokes Eigensystem for the Navier- Marching in Low Mach Preconditioned Unstructured Navier-Stokes Solvers Galerkin Method for Compressible on a Graphics Processing Unit Using Solver based on OpenACC and Stokes Equations with Finite-Rate Density-Based Methods A. Schwing, NASA Johnson Space Center, Flows on 3D Hybrid Grids CUDA MVAPICH2 Chemistry L. Alves, Federal University of Rio Grande do Houston, TX; I. Nompelis, G. Candler, Y. Xia, L. Luo, H. Luo, J. Lou, J. Edwards, G. Guzel, T. Akgun, ASELSAN, Inc., L. Luo, J. Edwards, H. Luo, F. Mueller, N. Currier, K. Sreenivas, University of Sul, Niterói, Brazil; C. Falcão, Fluminense 114 University of Minnesota, Minneapolis, F. Mueller, North Carolina State University, Ankara, Turkey North Carolina State University, Raleigh, Tennessee, Chattanooga, Chattanooga, TN Federal University, Porto Alegre, Brazil; F. Minneapolis, MN Raleigh, NC NC Medeiros, Military Institute of Engineering, Rio de Janeiro, Brazil Thursday, 19 June 2014 292-HYTASP-10 Propulsion Component Performance Learning Center Chaired by: R. BROWN, University of Strathclyde and T. O’BRIEN, Aerojet Rocketdyne 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2014-3086 AIAA-2014-3087 AIAA-2014-3088 AIAA-2014-3089 AIAA-2014-3090 AIAA-2014-3091 Low-Order Modelling of the Non- Semi-Zonal Hybrid RANS/LES Validation of a Novel OpenFOAM Testing of DLR C/C-SiC and C/C for Numerical Simulation of RBCC Multi-Disciplinary Design of a Local Acoustic Reacting Combustion Turbulence Modeling with RANS Solver using a Supersonic, Non- HIFiRE 8 Scramjet Combustor Single Expansion Ramp Nozzle in Rocket Engine Thrust Augmentation Chamber-Dome Interface in Rocket Sensor Based Interfacing Applied to reacting Channel Flow D. Glass, D. Capriotti, NASA Langley Ejector Mode Ejector for Endoatmospheric Flight Engines Supersonic Flows N. Droeske, University of Stuttgart, Stuttgart, Research Center, Hampton, VA; T. Reimer, Z. Zhengze, L. Peijin, Q. Fei, W. T. Takahashi, G. Gibson, Arizona State M. Schulze, T. Sattelmayer, Technical K. Makowka, M. Gurtner, D. Paukner, T. Germany; K. Makowka, Technical University M. Kütemeyer, German Aerospace Center Xiang Geng, L. Xiang, H. Guo Qiang, University, Tempe, AZ University of Munich, Garching, Germany Sattelmayer, O. Haidn, Technical University of Munich, Munich, Germany; P. Nizenkov, (DLR), Stuttgart, Germany; M. Smart, Northwestern Polytechnical University, of Munich, Munich, Germany J. Vellaramkalayil, University of Stuttgart, University of Queensland, Brisbane, Xi’an, China Stuttgart, Germany; T. Sattelmayer, Technical Australia University of Munich, Munich, Germany; J. von Wolfersdorf, University of Stuttgart, Stuttgart, Germany Thursday, 19 June 2014 293-FD-30 Cavity and Shear Flows Lenox Chaired by: R. SCHMIT, USAF AFRL and M. SAMIMY, The Ohio State University 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs AIAA-2014-3092 AIAA-2014-3093 Oral Presentation Oral Presentation AIAA-2014-3094 AIAA-2014-3095 AIAA-2014-3096 Numerical Simulations of Subsonic Predicting Acoustic Wave Shear Layer Growth Rate of a Compressibility Effects in the High-Speed Schlieren Imaging of Influence of Spanwise Domain on On the Growth of a Plane Mixing and Transonic Open-Cavity Flows Generation and Amplification Rectangular Cavity Shear Layer over a Finite-Width a High-Speed Jet Impinging on a the Large Eddy Simulation of an Layer from Laminar or Turbulent Y. Sun, A. Nair, K. Taira, L. Cattafesta, inside a Rectangular Cavity R. Schmit, J. Grove, Air Force Research Rectangular Cavity Flat Plate Idealised Mixing Layer Initial Conditions Florida State University, Tallahassee, FL; R. Schmit, J. Grove, Air Force Research Laboratory, Wright-Patterson AFB, OH; S. Beresh, J. Wagner, B. Pruett, J. J. Diebold, G. Elliott, University of Illinois, W. McMullan, University of Leicester, W. McMullan, University of Leicester, G. Brès, Cascade Technologies, Inc., Palo Laboratory, Wright-Patterson AFB, OH M. Frede, University of Dayton Research Henfling, R. Spillers, Sandia National Urbana-Champaign, Urbana, IL Leicester, United Kingdom Leicester, United Kingdom Alto, CA; L. Ukeiley, University of Florida, Institute, Dayton, OH Laboratories, Albuquerque, NM Gainesville, Gainesville, FL Thursday, 19 June 2014 294-APA-45 High Angle of Attack, High Lift and VSTOL/STOL Aerodynamics Marietta Chaired by: A. JONES, University of Maryland and M. CHANG, Lockheed Martin Aeronautics 1400 hrs 1430 hrs 1500 hrs 1530 hrs AIAA-2014-3097 AIAA-2014-3098 AIAA-2014-3099 AIAA-2014-3100 Numerical investigation on the Investigation of Turbulence Models Pressure Field of High Reynolds Off Ship Measurement of Ship development of the Phantom Yaw for the Supersonic Transport Number Turbulent Pulsed Jets Air Wakes Using Instrumented Effect on a maneuvering missile Configuration at Low-Speed and J. Calzada, I. Choutapalli, University of Unmanned Aerial Vehicles C. Schnepf, O. Wysocki, E. Schuelein, High Alpha Flight Condition Texas, Pan American, Edinburg, TX M. Snyder, U.S. Naval Academy, German Aerospace Center (DLR), K. Ohira, Ryoyu Systems Company, Ltd., Annapolis, MD; A. Kumar, P. Ben- Göttingen, Germany Nagoya, Japan; D. Kwak, Japan Aerospace Tzvi, George Washington University, Exploration Agency (JAXA), Tokyo, Japan Washington, DC 115 Thursday, 19 June 2014 295-AA-32 Fan Noise II Piedmont Chaired by: M. DAHL, NASA Glenn Research Center 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2014-3101 AIAA-2014-3102 AIAA-2014-3103 AIAA-2014-3104 AIAA-2014-3105 AIAA-2014-3106 Towards Lattice-Boltzmann Turbofan Inlet Distortion Noise Improved Broadband Liner On the generation and propagation Prediction of BPF tones emitted Preliminary Study on Acoustic Prediction of Turbofan Engine Noise Prediction with a Hybrid CFD-CAA Optimization Applied to the of multiple pure tones inside by the inlet of an aero-engine Detection of Faults Experienced by D. Casalino, A. Ribeiro, E. Fares, S. Approach Advanced Noise Control Fan turbofans at transonic regime model using in-duct angular mode a High-Bypass Turbofan Engine Noelting, Exa Corporation, Stuttgart, J. Winkler, C. Reimann, R. Reba, United D. Nark, M. Jones, NASA Langley Research J. Thisse, C. Polacsek, S. Léwy, ONERA, spectrum measurements D. Boyle, NASA Dryden Flight Research Germany; A. Mann, F. Perot, Exa Technologies Corporation, East Hartford, Center, Hampton, VA; D. Sutliff, NASA Châtillon, France; A. Lafitte, Snecma, G. Reboul, C. Polacsek, G. Billonnet, Center, Edwards, CA Corporation, Brisbane, CA; et al. CT; J. Gilson, Pratt & Whitney, East Glenn Research Center, Cleveland, OH Villaroche, France ONERA, Châtillon, France; J. Roux, Hartford, CT Snecma, Moissy-Cramayel, France Thursday, 19 June 2014 296-HYTASP-11 Review of Fundamental Research II (Invited) Regency Ballroom V Chaired by: M. MAITA, Japan Aerospace Exploration Agency and S. SCHNEIDER, Purdue University 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs AIAA-2014-3107 AIAA-2014-3108 AIAA-2014-3109 AIAA-2014-3110 AIAA-2014-3111 The reacting transverse jet in Mach 10 Boundary Layer Transition Free-flight aerodynamic tests Visualization of Hypersonic MDO for Hypersonic Scramjet supersonic crossflow: physics and Experiments on Sharp and Blunted of reentry vehicles in high- Boundary-Layer Transition on a Vehicle Development (Invited) properties (invited) Cones (Invited) temperature real-gas flow (Invited) Slender Cone (Invited) R. Starkey, University of Colorado, M. Gamba, University of Michigan, Ann E. Marineau, D. Lewis, G. Moraru, J. H. Tanno, K. Sato, T. Komuro, K. Itoh, S. Laurence, A. Wagner, H. Ozawa, K. Boulder, Boulder, CO Arbor, Ann Arbor, MI; V. Miller, Stanford Lafferty, Arnold Engineering Development Japan Aerospace Exploration Agency Hannemann, German Aerospace Center University, Stanford, CA; G. Mungal, Santa Center, Silver Springs, MD (JAXA), Kakuda, Japan (DLR), Göttingen, Germany Clara University, Santa Clara, CA Thursday, 19 June 2014 297-PANEL-8 Panel: Getting Ready for the Next Billion Dollar Aerospace Industry - The Low Altitude Frontier Regency Ballroom VI 1400 - 1600 hrs Moderators: B. Danette Allen, Chief Technologist for Autonomy, NASA Langley Research Center Parimal Kopardekar, Manager, NextGen Concepts and Technology Development Project, NASA Ames Research Center Panelists: Jesse Kallman Andrew Lacher David Maroney Rose Mooney Mark Moore Global Business Development & Regulatory Affairs UAS Integration Research Lead rinciple Systems Engineer - Civil UAS IntegrationThe Executive Director Aerospace Engineer, Airware The MITRE Corporation The MITRE Corporation Mid-Atlantic Aviation Partnership NASA Langley Research Center

Thursday, 19 June 2014 298-AA-33 Duct Propagation I Spring Chaired by: W. EVERSMAN, Missouri University of Science and Technology 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2014-3112 AIAA-2014-3113 AIAA-2014-3114 AIAA-2014-3115 AIAA-2014-3116 AIAA-2014-3117 Duct spinning mode’s particle The Effect of Steady Flow Distortion A three-dimensional cylindrical Generation and scattering of Numerical Analysis of the Tonal Acoustic eigenmode analysis for velocity imaging with in-duct on Mode Propagation in a Turbofan model for non-linear propagation acoustic modes in ducts with flow Sound Pressure Level Distribution ducted inhomogeneous mean flow circular microphone array Intake prediction in lined intake ducts with S. Sack, M. Åbom, Royal Institute of in the Vaned Diffuser of a C. Weckmüller, S. Guerin, L. Enghardt, J. Q. Wei, X. Huang, Peking University, R. Astley, R. Sugimoto, G. Gabard, University uniform flow Technology (KTH), Stockholm, Sweden; Centrifugal Compressor Hurst, German Aerospace Center (DLR), Beijing, China of Southampton, Southampton, United M. Kassem, Airbus, Toulouse, France; A. C. Schram, K. Kucukcoskun, von Kármán M. Banica, M. Fischer, H. Feld, ABB Group, Berlin, Germany Kingdom; E. Norde, E. Grift, University Bennani, École Polytechnique, Palaiseau, Institute for Fluid Dynamics, Rhode-Saint- Baden, Switzerland; R. Habing, German-Dutch of Twente, Twente, The Netherlands; M. France Genèse, Belgium Wind Tunnels, Emmeloord, The Netherlands; Bocquier, École Centrale de Lyon, Lyon, France C. Spinder, ABB Group, Baden, Switzerland

116 Thursday, 19 June 2014 299-TP-19 Thermal Management and Heat Pipes Techwood Chaired by: A. WILLIAMS, Air Force Reseach Laboratory and L. PHINNEY, Sandia National Laboratories 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2014-3118 AIAA-2014-3119 AIAA-2014-3120 AIAA-2014-3121 AIAA-2014-3122 AIAA-2014-3123 Electro-Wetting of a Heated Surface Controllable Nanoparticle Radiative Thermal-Electromagnetic Analysis Performance of Thermally Simulation of thermal storage in Numerical simulation, parametric in the Presence and Absence of Properties for High-Turndown Ratio of Infrared Antennas Radiating Fractal Extended wax-impregnated porous foams study and optimization of Gravity to Enhance Liquid Film Heat Rejection J. Wilson, E. Kinzel, Missouri University Surfaces of Varying Cross-Section with a pore-scale submodel thermoelectric generators for self- Boiling Heat Transfer T. Otanicar, R. Smith, University of Tulsa, of Science and Technology, Rolla, MO; D. Calamas, P. Hines, Georgia Southern G. Jackson, K. Smith, T. Fisher, P. cooling of devices V. Patel, Worcester Polytechnic Institute, Tulsa, OK J. Ginn, Plasmonics, Inc., Orlando, FL; University, Statesboro, GA McCarthy, Purdue University, West R. Kiflemariam, C. Lin, R. Moosavi, Florida Worcester, MA; F. Robinson, NASA Goddard B. Lail, Florida Institute of Technology, Lafayette, IN International University, Miami, FL Space Flight Center, Greenbelt, MD; J. Seyed- Melbourne, FL; G. Boreman, University of Yagoobi, Worcester Polytechnic Institute, North Carolina, Charlotte, Charlotte, NC Worcester, MA; J. Didion, NASA Goddard Space Flight Center, Greenbelt, MD Thursday, 19 June 2014 300-TP-20 Multi-Scale Heat Transfer III University Chaired by: P. HOPKINS 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs Oral Presentation Oral Presentation Oral Presentation AIAA-2014-3124 Oral Presentation Oral Presentation Wetting the Surface: Thermal Thermal Boundary Conductance An Experiment to Measure Near- Minimum Radiative Heat Transfer Influence of Non-thermal Electron Connections between Time Confinement with Liquids in Thin between Carbon Nanotube field Radiation between Planar Between Two Planar Metallic Dynamics on Electron Phonon Domain Thermoreflectance and Silicon and Silicon Oxide with Surface Surfaces at Nanoscale Distances Surfaces Coupling in Thin Gold Films Broadband Frequency Domain B. Donovan, P. Hopkins, University of Functionalization J. Watjen, B. Zhao, Z. Zhang, Georgia J. Mayo, A. Narayanaswamy, Columbia A. Giri, J. Gaskins, P. Hopkins, University of Thermoreflectance for Measuring Virginia, Charlottesville, Charlottesville, VA L. Chen, S. Kumar, Georgia Institute of Institute of Technology, Atlanta, GA University, New York, NY Virginia, Charlottesville, Charlottesville, VA Phonon Mean Free Paths Technology, Atlanta, GA X. Chen, C. Hua, A. Minnich, California Institute of Technology, Pasadena, CA Thursday, 19 June 2014 301-NW-12 Thursday Afternoon Networking Coffee Break Meeting Room Foyers 1530 - 1600 hrs Thursday, 19 June 2014 367-ATIO-27 New Directions for NASA’s Airspace R&D Embassy C 1600 - 1730 hrs Moderator: John Cavolowsky, Director, Airspace Systems Program, NASA Panelists: John Cavolowsky Akbar Sultan Leighton Quon Parimal Kopardekar Director, Airspace Systems Program Deputy Director, Airspace Systems Program Project Manager, System Analysis and Integration Evaluation Project Manager, Concepts and Technology Development Project NASA NASA NASA NASA

Thursday, 19 June 2014 302-ANERS-5 How Far Can We Get With Technology and Operations? Embassy H 1630 - 1730 hrs Chaired by: F. COLLIER, NASA-Langley Research Center Moderator: Fay Collier Panelists: Charles Etter Jeff Schutte Chris Markou Gulfstream Aerospace Corporation Georgia Institute of Technology International Air Transport Association (IATA)

Thursday, 19 June 2014 117 303-HYTASP-22 Future of Hypersonics Panel Regency Ballroom V 1630 - 1730 hrs Chaired by: L. MADDALENA, The University of Texas at Arlington Participants: Peter Erbland Chris Gettinger Francois Falempin Vince Wheatley US US France Australia

Thursday, 19 June 2014 304-LEC-8 Aerodynamics Award Lecture “Low-Speed Airfoil Design and Application” Regency Ballroom VII 1730 - 1830 hrs Michael S. Selig Associate Professor, Aerospace Engineering Department University of Illinois at Urbana-Champaign, Urbana, IL Friday Friday, 20 June 2014 305-SB-5 Friday Morning Speakers’ Briefing Session Rooms 0730 - 0800 hrs Friday, 20 June 2014 306-PLNRY-5 Friday Morning Plenary Panel Centennial I/II 0800 - 0900 hrs Moderator: Glenn Roberts, Chief Engineer, The MITRE Corporation Aeronautics Technology Development Panelists: Al Romig Steve Bradford Sprio Lekoudis Jaiwon Shin Vice President & Program Manager, Chief Scientist, Architecture & NextGEN Development Director of Weapons Systems Associate Administrator for Aeronautics Research Mission Directorate Skunk Works Engineering and Advanced Systems Office of the Chief Scientist, ANG-3 Office of the Assistant Secretary of Defense for Research and Engineering NASA Headquarters Lockheed Martin Aeronautics United States Department of Defense

Friday, 20 June 2014 307-NW-13 Friday Morning Networking Coffee Break Meeting Room Foyers 0900 - 0930 hrs Friday, 20 June 2014 308-APA-46 Other Topic in Applied Aerodynamics - UAVs and Other Similar Vehicles Baker Chaired by: M. OL, Air Force Reseach Laboratory 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2014-3125 AIAA-2014-3126 AIAA-2014-3127 AIAA-2014-3128 AIAA-2014-3129 AIAA-2014-3130 Scale and origin of the dynamics of The effect of wheel geometry on Boomerang Flight Tests The Effect of Passive Deformation Computation of 3D-Flow over Investigation of the Unsteady an air outlet the total aerodynamic drag of a B. Pomeroy, D. Uhlig, University of Illinois, on the Lift Produced by a Rotating a Parafoil Canopy for UAVs Aerodynamic Characteristics of T. Gericke, P. Scholz, Technical University road vehicle Urbana-Champaign, Urbana, IL Hinged Wing applications a Unmanned Aerial Vehicle with

118 of Braunschweig, Braunschweig, Germany M. Tsubokura, R. Kobayashi, S. Ota, N. Beals, A. Jones, University of Maryland, G. Andreutti, F. Capizzano, N. Favaloro, Variable-Sweep Morphing Hokkaido University, Sapporo, Japan; S. College Park, College Park, MD Italian Aerospace Research Center (CIRA), H. Han, J. Hu, Y. Yu, Beijing Institute of Okamine, T. Onuma, TOPY Industries, Capua, Italy Technology, Beijing, China Ltd., Toyokawa, Japan; N. Sasuga, DOME, Maibara, Japan; et al. Friday, 20 June 2014 309-APA-47 Propeller Aerodynamics Courtland Chaired by: A. MCCOMAS, TLG Aerospace 0930 hrs 1000 hrs 1030 hrs AIAA-2014-3131 AIAA-2014-3132 AIAA-2014-3133 Time-Accurate Simulations of a Optimal Circulation Distribution Validation of Aerodynamic and Spinning Propeller Using OVERFLOW2 on Propeller with the Influence of Aeroacoustic Simulations of Contra- W. Westmoreland, Dynetics, Inc., Viscosity Rotating Open Rotors at Low-Speed Huntsville, AL; M. McDaniel, Z. Hall, J. Klesa, University of West Bohemia, Flight Conditions Army Aviation and Missile Research Plzen, Czech Republic A. Stuermer, R. Akkermans, German Development and Engineering Center, Aerospace Center (DLR), Braunschweig, Redstone Arsenal, AL Germany Friday, 20 June 2014 310-APA-48 Aerodynamic Testing: Flight, Wind Tunnel and Numerical Correlations V Dunwoody Chaired by: K. KARA, Khalifa University of Science, Technology & Research 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2014-3134 AIAA-2014-3135 AIAA-2014-3136 AIAA-2014-3137 AIAA-2014-3138 Aerodynamic Shape Optimization NASA Common Research Model Experimental and Numerical Analysis Plume-Induced Effects on the Near- A Numerical Analysis of Unsteady of the Front Part of an Anti-Tank Test Envelope Extension with Active of the Flow Patterns Around a Wake Region of a Generic Space Aerodynamics of Formula Car Missile Based on Wind Tunnel Sting Damping at NTF Sounding Rocket in the Transonic Launcher Geometry During Dynamic Cornering Motion Testing and CFD Simulation M. Rivers, NASA Langley Research Center, Regime D. Saile, A. Guelhan, German Aerospace K. Nara, M. Tsubokura, J. Ikeda, Hokkaido G. Ocokoljic, Military Technical Institute, Hampton, VA; S. Balakrishna, ViGYAN, A. Avelar, J. Falc, Aeronautics and Space Center (DLR), Cologne, Germany University, Sapporo, Japan Belgrade, Serbia; B. Rasuo, A. Bengin, Inc., Hampton, VA Institute (IAE), São José dos Campos, Brazil; University of Belgrade, Belgrade, Serbia J. Jia Ling Hsu, University of Vale do Paraíba, São José dos Campos, Brazil; E. Basso, Aeronautics and Space Institute (IAE), São José dos Campos, Brazil; P. Martinez Romero, Technological Institute of Aeronautics (ITA), São José dos Campos, Brazil Friday, 20 June 2014 311-APA-49 Wind Turbine Aerodynamics III Edgewood Chaired by: M. CONWAY, The Aerospace Corporation 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2014-3139 AIAA-2014-3140 AIAA-2014-3141 AIAA-2014-3142 Flow Physics and Performance of Coriolis Effect on Dynamic Stall Experimental and Computational Dynamic separation on a pitching Vertical Axis Wind Turbine Arrays in a Vertical Axis Wind Turbine at Wake Characterization of a Vertical and surging airfoil as a model for

119 K. Duraisamy, University of Michigan, Ann Moderate Reynolds Number Axis Wind Turbine flow over vertical axis wind turbine Arbor, Ann Arbor, MI; V. Lakshminarayan, H. Hsieh-chen, T. Colonius, California D. Barsky, A. Posa, M. Rahromostaqim, M. blades Stanford University, Stanford, CA Institute of Technology, Pasadena, CA Leftwich, E. Balaras, George Washington R. Dunne, B. McKeon, California Institute University, Washington, DC of Technology, Pasadena, CA Friday, 20 June 2014 312-MAO-13 Multidisciplinary Analysis and Optimization: Emerging Methods III Embassy D Chaired by: P. ROHL, Advatech Pacific Inc 0930 hrs 1000 hrs AIAA-2014-3143 AIAA-2014-3144 MDO and Cross-Disciplinary On Using Genetic Algorithm Practice in R&D: A Portrait of Optimized Activation Functions to Principles and Current Practice Increase Neural Network Accuracy A. McGowan, NASA Langley Research Center, P. Rodi, Lockheed Martin Corporation, Hampton, VA; P. Papalambros, University of Houston, TX Michigan, Ann Arbor, Ann Arbor, MI Friday, 20 June 2014 313-ATIO-23 Airline Operations I Embassy E Chaired by: D. THIPPHAVONG, NASA Ames Research Center 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2014-3145 AIAA-2014-3146 AIAA-2014-3147 AIAA-2014-3148 AIAA-2014-3149 An Approach to Forecast Air Traffic A study into modeling coordination Agent Based Modeling of Air An Evaluation of a Flight Deck A New Spacing Algorithm to Movements at Capacity-Constrained in disruption management by Carrier Behavior for Evaluation of Interval Management Algorithm Support Near-Term Interval Airports Airline Operations Control Technology Equipage and Adoption including Delayed Target Management Operations S. Wenzel, K. Koelker, German Aerospace S. Bouarfa, H. Blom, R. Curran, K. B. Horio, A. DeCicco, V. Stouffer, S. Trajectories L. Weitz, MITRE Corporation, McLean, VA Center (DLR), Hamburg, Germany; P. Biesslich, Hindriks, Delft University of Technology, Hasan, R. Rosenbaum, LMI, McLean, VA; K. Swieringa, M. Underwood, B. Barmore, Hamburg University of Technology, Hamburg, Delft, The Netherlands J. Smith, NASA Langley Research Center, R. Leonard, NASA Langley Research Germany; K. Lütjens, German Aerospace Hampton, VA Center, Hampton, VA Center (DLR), Hamburg, Germany Friday, 20 June 2014 314-ATIO-24 Terminal & Surface Operations III - Approach Operations Embassy F Chaired by: P. BORCHERS, NASA Ames Research Center 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2014-3150 AIAA-2014-3151 AIAA-2014-3152 AIAA-2014-3153 AIAA-2014-3154 AIAA-2014-3155 Kinematic Modeling of Separation Enhancement of a time and Precision Arrival Scheduling for Analytical Assessment of Evaluation of Temporal Spacing Decentralized Automated Algorithm Compression for Paired Approaches energy management algorithm for Tactical Reconfiguration Simultaneous Parallel Approach Errors Associated with Interval for Self-merging and Self-spacing to Closely-Spaced Parallel Runways continuous descent operations S. Zelinski, NASA Ames Research Center, Feasibility from Total System Error Management Algorithms in the Next Generation Air Traffic M. Madden, NASA Langley Research X. Prats, C. Barrado, M. Perez-Batlle, Moffett Field, CA M. Madden, NASA Langley Research X. Bai, S. Vaddi, Optimal Synthesis, Inc., Control Center, Hampton, VA Technical University of Catalonia, Center, Hampton, VA Los Altos, CA; D. Mulfinger, NASA Ames M. Fruhnert, J. Guo, Purdue University, Barcelona, Spain; S. Vilardaga, ASCAMM, Research Center, Moffett Field, CA West Lafayette, IN

120 Barcelona, Spain; I. Bas, F. Birling, GTD, Barcelona, Spain; et al. Friday, 20 June 2014 315-MAO-14 Multidisciplinary Analysis and Optimization: Vehicle Design Embassy G Chaired by: T. TAKAHASHI, Arizona State University 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2014-3156 AIAA-2014-3157 AIAA-2014-3158 AIAA-2014-3159 AIAA-2014-3160 AIAA-2014-3161 A Multi-Disciplinary Survey of Creating a Test Validated Structural A Design Study Employing Aeroelastic Characterization of an Aero- Stochastic Multicriteria Acceptability Exploring Composite Panels Using Energy Maneuverability for Dynamic Finite Element Model of Tailoring and an Active Aeroelastic Structural Interaction for the Analysis for Nominal is Best MCDA Multi-Objective Optimization and Subsonic Endurance Based Aircraft the X 56A Aircraft Wing Design Approach on a Tailless Hybrid Wing Body Center Section in in the context of Generic Vehicles Varying Load Conditions C. Gedeon, T. Takahashi, Arizona State C. Pak, S. Truong, NASA Dryden Flight Lambda Wing Configuration Conceptual Phase Structural Sizing M. LeVine, L. Huynh, M. Kirby, D. K. Von Hagel, S. Joglekar, M. Pankow, S. University, Tempe, AZ Research Center, Edwards, CA E. Alyanak, E. Pendleton, Air Force Research J. Corman, D. Mavris, Georgia Institute of Mavris, Georgia Institute of Technology, Ferguson, North Carolina State University, Laboratory, Wright-Patterson AFB, OH Technology, Atlanta, GA Atlanta, GA Raleigh, NC Friday, 20 June 2014 316-ANERS-6 ANERS-Modeling Embassy H Chaired by: R. MIAKE-LYE, Aerodyne Research Inc 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2014-3162 AIAA-2014-3163 AIAA-2014-3164 AIAA-2014-3165 AIAA-2014-3166 AIAA-2014-3167 Verification of Noise Forecast En Route Jet Aircraft Noise Analysis Implementation of INM and ECAC Long-term Alternative Fuels Meeting Emissions Reduction Test Cell Emission Measurement Capabilities for Application to Full- M. Hassan, J. Tai, R. Denney, B. 3rd Edition in Noise Mapping Scenarios Targets: A Probabilistic Lifecycle of Commercial Aircraft Engine: scale Supersonic-capable Jet Engine Havrilesko, Georgia Institute of Software/Assessing all Noise H. Pfaender, A. Payan, D. Mavris, Georgia Assessment of the Production of CFM56-7B26 Development Technology, Atlanta, GA Sources in one Model Institute of Technology, Atlanta, GA Alternative Jet Fuels E. Turgut, M. Cavcar, O. Yay, E. Yilmaz, W. Lundberg, D. Drye, Air Force Life Cycle A. Notario, F. Probst, DataKustik GmbH, A. Payan, M. Kirby, C. Justin, D. Mavris, Anadolu University, Eskisehir, Turkey; M. Management Center, Wright-Patterson Greifenberg, Germany Georgia Institute of Technology, Atlanta, Ucarsu, Turkish Technic, Istanbul, Turkey; AFB, OH GA O. Usanmaz, Anadolu University, Eskisehir, Turkey; et al. Friday, 20 June 2014 317-APA-50 Aerodynamic Analysis and Design: Analysis Methods II Fairlie Chaired by: R. VERMELAND, Lockheed Martin Aeronautics and A. SCLAFANI, Boeing Engineering Operations & Technology 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2014-3168 AIAA-2014-3169 AIAA-2014-3170 AIAA-2014-3171 AIAA-2014-3172 Verification and Validation of HiFiLES: Enforcing Boundary Conditions for New Numerical Study of Boundary the Effects of Turbulence Model A Method to Allocate Camber, a High-Order LES unstructured solver Discrete Nonlinear Aerodynamic Layer Behavior on A Morphing Corrections on Drag Prediction of Thickness and Incidence on a Swept on multi-GPU platforms Reduced-Order Models Wing-with-Aileron System NASA Common Research Model Wing M. López, A. Sheshadri, J. Bull, T. K. Washabaugh, C. Farhat, Stanford A. Koreanschi, S. Oliviu, R. Botez, École de J. Chen, China Aerodynamics Research and T. Takahashi, D. Dulin, C. Kady, Arizona Economon, J. Romero, J. Watkins, University, Stanford, CA Technologie Supérieure, Montréal, Canada Development Center, Mianyang, China State University, Tempe, AZ Stanford University, Stanford, CA; et al. Friday, 20 June 2014 318-APA-51 Aerodynamic Analysis and Design: Optimization Methods I Greenbriar Chaired by: J. LATZ, Northrop Grumman Aerospace Systems 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2014-3173 AIAA-2014-3174 AIAA-2014-3175 AIAA-2014-3176 AIAA-2014-3177 Single-objective and Multi-objective Track by Track Robust Optimization Uncertainty Propagation for Robust Adjoint-Based Shape Optimization Comparison of Newton and Robust Optimization of Airfoils of a F1 Front Wing using Adjoint Aerodynamic Shape Optimization for the Aerodynamic Components Newton-GMRES Methods for Three using Adjoint Solutions Solutions and Radial Basis Functions D. Papadimitriou, C. Papadimitriou, of Drag in Viscous Flows Dimensional Supersonic Nozzle Design G. Petrone, ANSYS, Inc., Sheffield, G. Petrone, ANSYS, Inc., Sheffield, United University of Thessaly, Volos, Greece F. Bisson, S. Nadarajah, McGill University, B. Yildizlar, S. Eyi, Middle East Technical United Kingdom; C. Hill, ANSYS, Inc., Kingdom; C. Hill, ANSYS, Inc., Lebanon, Montréal, Canada University, Ankara, Turkey; M. Yumusak, Lebanon, NH NH; M. Biancolini, Tor Vergata University, ROKETSAN Missiles Industries, Inc., Ankara, Rome, Italy Turkey

121 Friday, 20 June 2014 319-AA-34 Fluid Acoustic Phenomena II Hanover A Chaired by: M. POTT-POLLENSKE, DLR - German Aerospace Center 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2014-3178 AIAA-2014-3179 AIAA-2014-3180 AIAA-2014-3181 AIAA-2014-3182 Spectral Broadening by Shear Resonance Frequency of Helmholtz Tonal Noise Excited by Plasma in Aeroacoustic tunnel effect in noise Large Eddy Simulation of Stall Layers of Open Jet Wind Tunnels Dampers in the Presence of High- Cylinder Wakes Using Closed-loop shielding problems Noise P. Sijtsma, National Aerospace Laboratory Temperature Grazing Flows Control J. Delfs, German Aerospace Center (DLR), W. Wolf, University of Campinas, (NLR), Emmeloord, The Netherlands; S. D. Wassmer, B. Cosic, C. Paschereit, W. Yu, X. Huang, Peking University, Braunschweig, Germany Campinas, Brazil; J. Kocheemoolayil, S. Oerlemans, Siemens, Brande, Denmark; T. Technical University of Berlin, Berlin, Beijing, China Lele, Stanford University, Stanford, CA Tibbe, Philips, Drachten, The Netherlands Germany Friday, 20 June 2014 320-AA-35 General Acoustics II Hanover B Chaired by: M. HERR, DLR - German Aerospace Center 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2014-3183 AIAA-2014-3184 AIAA-2014-3185 AIAA-2014-3186 AIAA-2014-3187 Feedback Control of Transient Noise Source Ranking of a Creative Means of Making Acoustic Synthesis of a Rotor BVI Noise Active noise control simulation Growth of Thermoacoustic Hairdryer Measurements Inexpensively with Active Controller Through of tonal turbofan noise in aero Oscillations B. Akhmetov, S. Gupta, K. Ahuja, Georgia Hair Dryer Noise Reduction as an an Efficient Aerodynamics/ engines D. Zhao, Nanyang Technological University, Institute of Technology, Atlanta, GA Example Aeroacoustics Solver Y. Pasco, T. Guédeney, A. Leung-Tack, A. Singapore, Singapore; M. Reyhanoglu, S. Gupta, B. Akhmetov, K. Ahuja, Georgia A. Anobile, G. Bernardini, Roma Tre University, Berry, S. Moreau, P. Masson, University of Embry-Riddle Aeronautical University, Institute of Technology, Atlanta, GA Rome, Italy; C. Testa, Italian Institute for Naval Sherbrooke, Sherbrooke, Canada Daytona Beach, FL Hydrodynamic Research and Ship Model Basin, Rome, Italy; M. Gennaretti, Roma Tre University, Rome, Italy Friday, 20 June 2014 321-AA-36 Low Noise Systems Integration Hanover C Chaired by: L. ENGHARDT, DLR - German Aerospace Center 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2014-3188 AIAA-2014-3189 AIAA-2014-3190 AIAA-2014-3191 AIAA-2014-3192 Simulation of the Installation Installation Effects of a Propeller A coupling of computational methods Installation Effects of a Propeller Effect of water-droplets on flow- Effects of the Aircraft Engine Rear Mounted on a Wing with Coanda Flap. for CROR installation effects Mounted on a High-Lift Wing with induced pulsations in pipe with Fan Noise with ACTRAN/DGM Part II: Numerical Investigation and L. Sanders, D. Mincu, W. Denis, ONERA, a Coanda Flap. Part I: Aeroacoustic two closed-side branches: an A. Mosson, Airbus, Toulouse, France; D. Experimental Validation Châtillon, France; P. Vitagliano, M. Minervino, Experiments experimental study Binet, J. Caprile, Free Field Technologies, J. Dierke, R. Akkermans, J. Delfs, R. Italian Aerospace Research Center (CIRA), R. Akkermans, M. Pott-Pollenske, H. Buchholz, F. Sanna, J. Golliard, TNO, Delft, The Toulouse, France Ewert, German Aerospace Center (DLR), Naples, Italy; J. Kennedy, Trinity College J. Delfs, D. Almoneit, German Aerospace Netherlands Braunschweig, Germany Dublin, Dublin, Ireland; et al. Center (DLR), Braunschweig, Germany Friday, 20 June 2014 322-AA-37 CAA Propagation and Scattering I Hanover D Chaired by: J. GALLMAN, Gulfstream 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2014-3193 AIAA-2014-3194 AIAA-2014-3195 AIAA-2014-3196 AIAA-2014-3197 Acoustic-entropy coupling behavior Further development of a time Predicting the Noise Transmission Wave Confinement: Long-Distance Effects of distance between plates and acoustic scattering properties domain boundary integral equation through a Structure Loaded with a Acoustics Propagation through on flows around a cascade of flat of a Laval nozzle method for aeroacoustic scattering Low Mach Number Turbulent Flow Realistic Environments plates with acoustic resonance W. Ullrich, J. Gikadi, C. Jörg, T. computations S. Caro, CD-adapco, Lyon, France; F. J. Steinhoff, A. Wilson, S. Chitta, H. Yokoyama, H. Yamamoto, K. Kitamiya, Sattelmayer, Technical University of F. Hu, Old Dominion University, Norfolk, VA Mendonca, CD-adapco, London, United WaveCPC, Inc., Tullahoma, TN; F. A. Iida, Toyohashi University of Technology, Munich, Garching, Germany Kingdom; V. Cotoni, CD-adapco, San Caradonna, Army Aviation and Missile Toyohashi, Japan Diego, CA; P. Shorter, T. Connelly, CD- Research Development and Engineering

122 adapco, Detroit, MI Center, Moffett Field, CA Friday, 20 June 2014 323-AA-38 Jet Noise Measurements III Hanover E Chaired by: A. AGARWAL, University of Cambridge 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2014-3198 AIAA-2014-3199 AIAA-2014-3200 AIAA-2014-3201 AIAA-2014-3202 Jet-Surface Interaction Test: Flow Comparison of two time-domain Far-Field Acoustic Measurements of Near-field Shocks Radiated by Noise from a Supersonic Round Jet Measurement Results measures of nonlinearity in near-field Dual Impinging Scale Model Jets High-Speed Free-Shear-Flow Discharging into a Duct C. Brown, M. Wernet, NASA Glenn propagation of high-power jet noise L. Myers, C. Kuo, D. McLaughlin, Turbulence K. Zaman, A. Fagan, NASA Glenn Research Research Center, Cleveland, OH K. Gee, T. Neilsen, D. Thomas, B. Reichman, Pennsylvania State University, University D. Buchta, A. Anderson, J. Freund, Center, Cleveland, OH M. Muhlestein, Brigham Young University, Park, PA University of Illinois, Urbana-Champaign, Provo, UT; J. Downing, Blue Ridge Research Urbana, IL and Consulting, LLC, Asheville, NC; et al. Friday, 20 June 2014 324-AA-39 Broadband Fan Noise Panel Discussion Hanover F 0930 - 1230 hrs Chaired by: E. ENVIA, NASA Glenn Research Center and J. COUPLAND, University of Southampton Moderators: Edmund Envia, John Coupland

The Broadband Fan Noise Panel Discussion will serve as a forum for assessing the current state of the art in predicting fan broadband noise using a portfolio of benchmark problems for which information on the mean flow, turbulence characteristics, and the sound field exists. Friday, 20 June 2014 325-FD-31 Aerothermodynamics and Reacting Flows Harris Chaired by: J. SCHMISSEUR, USAF AFOSR/NA 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2014-3203 AIAA-2014-3204 AIAA-2014-3205 AIAA-2014-3206 AIAA-2014-3207 AIAA-2014-3208 Scalar Conservation in Large Eddy Effect of Thermal Non-equilibrium Generalized Multi-Group Macroscopic Development of Reduced Chemistry High Fidelity Modeling of Energy Formulation of a New Set of Simulations of Reacting Flows on Compressible Isotropic Modeling for Thermo-Chemical Non- Models for High Enthalpy and Transfer and Chemical Reactions in Simplified Conventional Burnett P. Subbareddy, G. Candler, P. Ferrero, Turbulence Equilibrium Gas Mixtures Plasma Flows Shock Waves Equations for Computation of University of Minnesota, Minneapolis, A. Neville, I. Nompelis, P. Subbareddy, Y. Liu, NASA Ames Research Center, A. Bellemans, A. Munafó, T. Magin, von T. Zhu, Z. Li, N. Parsons, D. Levin, Rarefied Hypersonic Flows Minneapolis, MN G. Candler, University of Minnesota, Moffett Field, CA; M. Panesi, University Kármán Institute for Fluid Dynamics, Pennsylvania State University, University W. Zhao, W. Chen, Zhejiang University, Minneapolis, Minneapolis, MN of Illinois, Urbana-Champaign, Urbana, IL; Rhode-Saint-Genèse, Belgium; A. Parente, Park, PA Hangzhou, China; R. Agarwal, Washington M. Vinokur, NASA Ames Research Center, G. Degrez, Université Libre de Bruxelles, University in St. Louis, St. Louis, MO Moffett Field, CA; A. Sahai, University of Brussels, Belgium Illinois, Urbana-Champaign, Urbana, IL Friday, 20 June 2014 326-FD-32 Large Eddy Simulations Inman Chaired by: J. POGGIE, USAF AFRL/RBAC and G. MATHEOU, Jet Propulsion Laboratory 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2014-3209 AIAA-2014-3210 AIAA-2014-3211 AIAA-2014-3212 AIAA-2014-3213 AIAA-2014-3214 Scalar excursions in large-eddy Simulation of the Compressible Multiscale Large Eddy Simulation of A Sub-grid Scale Model with A High Resolution Low-pass Subgrid-Scale Modeling of simulations Taylor Green Vortex using High- Turbulence Using High-Order Finite Non-traditional Eddy-Viscosity Differential Filter for Large Eddy Baroclinic Vorticity G. Matheou, Jet Propulsion Laboratory, Order Flux Reconstruction Schemes Element Methods Coefficient Simulations on Unstructured Grids G. Sidharth, G. Candler, University of California Institute of Technology, J. Bull, A. Jameson, Stanford University, L. Wang, W. Anderson, L. Taylor, University J. Taghinia, M. Rahman, T. Siikonen, Aalto A. Najafiyazdi, M. Najafiyazdi, L. Minnesota, Minneapolis, Minneapolis, Pasadena, CA; P. Dimotakis, California Stanford, CA of Tennessee, Chattanooga, Chattanooga, University, Espoo, Finland Mongeau, McGill University, Montréal, MN; P. Dimotakis, California Institute of

123 Institute of Technology, Pasadena, CA TN Canada Technology, Pasadena, CA Friday, 20 June 2014 327-FD-33 Comparison between CFD and Measurements in Hypervelocity Airflows Part I: Real-gas Effects on Laminar Shockwave Boundary Layer Interaction Kenneshaw Chaired by: M. MACLEAN, CUBRC and T. WADHAMS, CUBRC 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs Oral Presentation Oral Presentation AIAA-2014-3366 Oral Presentation Oral Presentation Oral Presentation Measurements of Real-gas Effects Simulations of Separated Flow of US3D Predictions of Double-Cone Shock Wave Interactions: A CFD Computations of High-Enthalpy Comparison between CFD and on Laminar Shockwave Boundary Air at High Enthalpy with LAURA and Hollow Cylinder-Flare Flows at Study of CUBRC LENS-XX Laminar Laminar Air Flow Around Measurements for Real-gas Effects Layer Interaction (Invited) and FUN3D (Invited) High-Enthalpy (Invited) Experiments (Invited) Double Cone and Cylinder/Flare on Laminar Shockwave Boundary M. Holden, M. MacLean, A. Dufrene, P. Gnoffo, NASA Langley Research Center, I. Nompelis, G. Candler, University of D. Prabhu, ERC, Inc., Moffett Field, CA Geometries (Invited) Layer Interaction (Invited) CUBRC, Inc., Buffalo, NY Hampton, VA Minnesota, Minneapolis, MN H. Alkandry, A. Anna, I. Boyd, University M. MacLean, M. Holden, A. Dufrene, of Michigan, Ann Arbor, MI CUBRC, Inc., Buffalo, NY Friday, 20 June 2014 328-HYTASP-12 Propulsion Component Performance-Injector Learning Center Chaired by: F. FALEMPIN, MBDA 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2014-3215 AIAA-2014-3216 AIAA-2014-3217 AIAA-2014-3218 Unsteady RANS Investigation of a Effect of Incoming Boundary Experimental and Numerical Pre-Injection Radical Production Hydrogen-Fueled Staged Supersonic Layer on Supersonic Mixing Layer Investigation of the Flow using Catalytic Fuel Treatment for Combustor with Lobed Injectors Generated by Wall-Mounted Ramp Characteristics of a Strut Injector Scramjet Applications K. Makowka, Technical University of Injector for Scramjets D. Paukner, M. Gurtner, O. Haidn, Munich, Munich, Germany; N. Droeske, T. Arai, Y. Yamauchi, S. Sakaue, Osaka C. Ground, F. Vergine, L. Maddalena, Technical University of Munich, Garching, J. Vellaramkalayil, University of Stuttgart, Prefecture University, Sakai, Japan University of Texas, Arlington, Arlington, TX Germany Stuttgart, Germany; T. Sattelmayer, Technical University of Munich, Munich, Germany; J. von Wolfersdorf, University of Stuttgart, Stuttgart, Germany Friday, 20 June 2014 329-FD-34 Galerkin Methods Lenox Chaired by: K. FIDKOWSKI, University of Michigan 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2014-3219 AIAA-2014-3220 AIAA-2014-3221 AIAA-2014-3222 A Reconstructed Discontinuous An implicit, reconstructed Analysis of Improved Advection Exploration of POD-Galerkin Galerkin Method Based on a Gas discontinuous Galerkin method for the Schemes for Discontinuous Galerkin Method in Developing a Flame Kinetic Scheme for Compressible unsteady compressible Navier-Stokes Methods Model for Combustion Instability Flows on Arbitrary Grids equations on 3D hybrid grids L. Khieu, E. Johnsen, University of Problems L. Xu, Y. Xia, H. Luo, North Carolina State Y. Xia, H. Luo, C. Wang, North Carolina Michigan, Ann Arbor, Ann Arbor, MI C. Huang, W. Anderson, C. Merkle, Purdue University, Raleigh, NC State University, Raleigh, NC; R. University, West Lafayette, IN Nourgaliev, Lawrence Livermore National Laboratory, Livermore, CA Friday, 20 June 2014 330-APA-52 Aerodynamic Analysis and Design: Optimization Methods II Marietta Chaired by: G. ZHA 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2014-3223 AIAA-2014-3224 AIAA-2014-3254 AIAA-2014-3255 Comparison of Local and Global Simulation-Driven Aerodynamic Shape Aerodynamic Modeling Techniques Analysis and Design Optimization Constrained Aerodynamic Shape Optimization with Automated Low- for Efficient Supersonic Air Vehicle of Blunt Bodies In Hypersonic Flow Optimization Fidelity Model Setup Multidisciplinary Design Optimization T. Piskin, S. Eyi, Middle East Technical D. Poole, C. Allen, T. Rendall, University of S. Koziel, L. Leifsson, Y. Tesfahunegn, C. Meckstroth, University of Dayton Research University, Ankara, Turkey; M. Yumusak, Bristol, Bristol, United Kingdom Reykjavik University, Reykjavik, Iceland Institute, Dayton, OH; E. Alyanak, N. Lindsley, ROKETSAN Missiles Industries, Inc., M. Gabbard, Air Force Research Laboratory, Ankara, Turkey

124 Wright-Patterson AFB, OH; A. Hunton, Ohio Aerospace Institute, Dayton, OH Friday, 20 June 2014 331-HYTASP-13 Propulsion Component Performance-Inlets Regency Ballroom V Chaired by: M. BULMAN, Aerojet Rocketdyne Corporation 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2014-3227 AIAA-2014-3228 AIAA-2014-3229 AIAA-2014-3230 Startability analysis of Busemann Sensitivity of the Performance of a Integration methodology for Investigation into the Flow Physics intakes with overboard spillage 3-Dimensional Hypersonic Inlet to waverider-derived hypersonic inlet of Hypersonic Variable Geometry N. Moradian, E. Timofeev, McGill Shape Deformations and vehicle forebody Inlet Starting University, Montréal, Canada; R. Tahir, RBT H. Kline, F. Palacios, J. Alonso, Stanford Y. Li, P. An, C. Pan, R. Chen, Y. You, A. Grainger, S. Brieschenk, University Consultants, Etobicoke, Canada; S. Molder, University, Stanford, CA Xiamen University, Xiamen, China of Queensland, Brisbane, Australia; R. Smart Aeronautics, Toronto, Canada Boyce, University of New South Wales at the Australian Defence Force Academy, Canberra, Australia; R. Malpress, D. Buttsworth, University of Southern Queensland, Toowoomba, Australia Friday, 20 June 2014 332-PANEL-9 Panel: NASA Aeronautics Vision for the 21st Century: Why a New Strategy? Regency Ballroom VI 0930 - 1130 hrs Moderator: Robert Pearce, Director, Strategy, Architecture & Analysis, NASA Aeronautics Research Mission Directorate; NASA Headquarters Panelists: John Cavolowsky Jay Dryer Douglas Rohn Ed Waggoner Program Director - Airspace Operations and Safety Program Director - Advanced Air Vehicles Program Program Director - Transformative Aeronautics Concepts Program Director - Integrated Aviation Systems NASA Aeronautics Research Mission Directorate NASA Aeronautics Research Mission Directorate NASA Aeronautics Research Mission Directorate NASA Aeronautics Research Mission Directorate NASA Headquarters NASA Headquarters NASA Headquarters NASA Headquarters Friday, 20 June 2014 333-AA-41 Duct Propagation II Spring Chaired by: S. RIENSTRA, Technische Universiteit Eindhoven 0930 hrs 1000 hrs 1030 hrs AIAA-2014-3231 AIAA-2014-3232 AIAA-2014-3233 In-Duct and Farfield Experimental Generation and transmission of Theoretical Study and Numerical Measurements from the ANCF spiral acoustic waves in multi-stage Validation of Sound Radiation from for the Purpose of Improved subsonic radial compressors Coaxial Annular Duct Broadband Liner Optimization M. Roger, École Centrale de Lyon, Lyon, X. Liu, X. Huang, Peking University, D. Sutliff, NASA Glenn Research Center, France; S. Moreau, A. Marsan, University Beijing, China Cleveland, OH; M. Jones, NASA Langley of Sherbrooke, Sherbrooke, Canada Research Center, Hampton, VA; D. Nark, NASA Glenn Research Center, Cleveland, OH Friday, 20 June 2014 334-AA-40 General Acoustics I Spring Chaired by: H. BODEN 0930 hrs 1100 hrs 1130 hrs No Presentations AIAA-2014-3225 AIAA-2014-3226 Noise Produced by a Tandem Optimized cloaking design Diaphragm: Experimental and in moving fluid based on the Numerical Investigations scattering analysis method U. Karban, G. Ogus, K. Kucukcoskun, C. X. Huang, S. Zhong, Peking University, Schram, von Kármán Institute for Fluid Beijing, China Dynamics, Rhode-Saint-Genèse, Belgium;

125 C. Sovardi, W. Polifke, Technical University of Munich, Garching, Germany Friday, 20 June 2014 335-TP-21 Other Heat Transfer Topics Techwood Chaired by: C. LIN, Florida International University and D. HASH, NASA Ames Research Center 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2014-3234 AIAA-2014-3235 AIAA-2014-3236 AIAA-2014-3237 Thermal Analysis of a Satellite Optimization of Heat Exchanger Investigation of Kinetics of Iso- Steady State Simulation of Gaseous instrument of Vuilleumier Heat Pump using Octane Autoignition Combustor Using Local Extiction B. Chen, Chinese Academy of Sciences, Teaching-Learning Based Algorithm Q. Chen, Y. Hong, W. Zhao, L. Li, Academy Eddy Dissipation Concept Beijing, China S. Gadiraju, Y. Bedekar, J. Longitn, Stony of Equipment, Beijing, China S. Soleimani, E. Ghasemi, C. Lin, Florida Brook University, Stony Brook, NY; S. International University, Miami, FL Paul, H. Peter, Y. Huang, ThermoLift, Inc., Stony Brook, NY Friday, 20 June 2014 336-TP-22 Other Topics in Thermophysics University Chaired by: G. ZISKIND, Ben-Gurion University of the Negev and A. ALEXEENKO, Purdue University 0930 hrs 1000 hrs 1030 hrs AIAA-2014-3238 AIAA-2014-3239 AIAA-2014-3240 A Robustness Study for a D-Bay Thermal Environmental Stress Non-Destructive Testing of Grid Generation Criteria using Screen Optimization Materials Using Thermal Imaging Surrogate Models A. Whelan, Raytheon Company, Tucson, AZ R. McMasters, Virginia Military Institute, M. Pustelnik, L. Santos, Embraer, São Lexington, VA José dos Campos, Brazil; D. Ferrari, Technological Institute of Aeronautics (ITA), São José dos Campos, Brazil Friday, 20 June 2014 337-TP-23 Multi-Scale Heat Transfer IV Vinings Chaired by: A. HENRY, Georgia Institute of Technology and T. FISHER 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2014-3242 Oral Presentation Oral Presentation Oral Presentation Oral Presentation A numerical study of 2D AC Thermal Conductivity Spectroscopy: Ballistic phonon transport in Size Effects on the Thermal Electrically Tunable & Highly electrothermal pump by lattice Analysis of Spot Size Suppression cryogenic InP transistors Conductivity of Amorphous Silicon Reversible Thermal Transport in a Boltzmann method Using Monte Carlo Simulations J. Schleeh, Chalmers University of and Carbon Films Lithium Ion Battery Q. Ren, C. Chan, University of Arizona, D. Ding, A. Minnich, California Institute of Technology, Göteborg, Sweden; J. Mateos, J. Gaskins, University of Virginia, Y. Hu, G. Chen, Massachusetts Institute of Tucson, Tucson, AZ Technology, Pasadena, CA University of Salamanca, Salamanca, Charlottesville, Charlottesville, VA; M. Technology, Cambridge, MA Spain; N. Wadefalk, J. Grahn, Chalmers Elahi, Z. Leseman, University of New University of Technology, Göteborg, Mexico, Albuquerque, Albuquerque, Sweden; A. Minnich, California Institute of NM; P. Hopkins, University of Virginia, Technology, Pasadena, CA Charlottesville, Charlottesville, VA Friday, 20 June 2014 338-LNCH-5 Friday Networking Lunch Lunch on Own 1230 - 1400 hrs Friday, 20 June 2014 339-APA-53 Airfoil/Wing/Configuration Aerodynamics III Baker Chaired by: J. GUGLIELMO, Boeing Defense, Space & Security and A. JONES, University of Maryland 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2014-3243 AIAA-2014-3244 AIAA-2014-3245 AIAA-2014-3246 AIAA-2014-3247 AIAA-2014-3248 Effective Angle of Attack Control of Influence of Trailing Edge Brushes CFD evaluation of the effects of Measurements of a Symmetric 2D Numerical and Experimental Computational and Experimental 126 a Flat Plate Flapping-Foil Turbine on Upstream Moving Pressure stall control devices and transition Airfoil Morphed by Macro Fiber Investigation on the Effect of a Characterization of Dynamic Stall C. Usoh, J. Young, J. Lai, M. Ashraf, Waves in Transonic Flow tapes on stall behavior of airplanes Composite Actuators Fowler Flap Gap and Overlap Size on 9-12% Thick Airfoils University of New South Wales at the J. Nies, H. Olivier, RWTH Aachen A. Moitra, Tata Consultancy Services, Y. Bouremel, W. Chan, National University of on the Flow Field P. Davidson, J. Strike, M. Hind, J. Australian Defence Force Academy, University, Aachen, Germany Bangalore, India Singapore, Singapore, Singapore; G. Jones, M. Ferchichi, S. Graveline, D. Demel, Sitaraman, J. Naughton, University of Canberra, Australia Imperial College London, London, United Royal Military College of Canada, Wyoming, Laramie, Laramie, WY Kingdom; M. Debiasi, National University of Kingston, Canada Singapore, Singapore, Singapore Friday, 20 June 2014 340-APA-54 Vortical/Vortex Flow III Courtland Chaired by: J. PINIER, NASA-Langley Research Center and K. VANDEN, USAF 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs AIAA-2014-3249 AIAA-2014-3250 AIAA-2014-3251 AIAA-2014-3252 AIAA-2014-3253 Proper Orthogonal Decomposition Physically-based reduced order A NUFFT Technique for Flow Progress Towards Aeroelastic Computational Analysis of a Tip of a Turbulent Pulsed Jet model for unsteady aerodynamic Fluctuation Analysis Based on the Modeling of Wind Turbine Blades Vortex Structure Shed from a Bio- O. Huerta, University of Texas, Pan American, loads of a L-shaped Gurney flap Unsteady Flow Simulation with using Harmonic Balance and the inspired Blade Edinburg, TX; D. Hernandez, Center for V. Motta, G. Quaranta, Technical University Variable Physical Time Stepping Gamma-Re_Theta Transition Model S. Gomez, L. Gilkey, B. Kaiser, S. Research in Optics, Leon Guanajuato, Mexico; of Milan, Milan, Italy Scheme J. Howison, K. Ekici, University of Poroseva, University of New Mexico, I. Choutapalli, University of Texas, Pan G. Wang, Y. Liu, H. Mian, Z. Ye, Northwestern Tennessee, Knoxville, Knoxville, TN Albuquerque, Albuquerque, NM American, Edinburg, TX Polytechnical University, Xi’an, China Friday, 20 June 2014 342-APA-56 Rotorcraft Aerodynamics Edgewood Chaired by: M. CALVERT, U.S. Army AMRDEC 1400 hrs 1430 hrs 1500 hrs 1530 hrs AIAA-2014-3256 AIAA-2014-3257 AIAA-2014-3258 AIAA-2014-3259 Quantification of the Evolution of Classical and snapshot forms of the Time-Spectral Rotorcraft Efficient and Adaptive Algorithm a Vortical Sheet in the Wake of a POD technique applied to a helical Simulations on Overset Grids for Aerodynamic Investigations of Hovering Rotor vortex filament J. Leffell, Stanford University, Stanford, Micro Helicopters J. Milluzzo, U.S. Naval Academy, S. Mula, C. Cameron, C. Tinney, J. Sirohi, CA; S. Murman, T. Pulliam, NASA Ames M. Gloor, P. Jenny, Swiss Federal Institute Annapolis, MD; J. Leishman, University of University of Texas, Austin, Austin, TX Research Center, Moffett Field, CA of Technology, Zurich, Switzerland Maryland, College Park, College Park, MD Friday, 20 June 2014 343-ACD-13 VSTOL Embassy D Chaired by: R. MANGE, Lockheed Martin Corporation and J. SOKHEY, Rolls-Royce Corporation 1400 hrs 1430 hrs 1500 hrs AIAA-2014-3260 AIAA-2014-3261 AIAA-2014-3262 Computational design of a concept An investigation into the effect of Application of the finite element helicopter’s fuselage the airfoil on the aerodynamics of method to study the dynamics of a P. Yadav, R. Yadav, G. Gupta, Indian the MAV scale cycloidal propeller helicopter Institute of Technology Bombay, Mumbai, under hovering status T. Gorecki, Institute of Aviation, Warsaw, India Y. Hu, Northwestern Polytechnical Poland University, Xi’an, China Friday, 20 June 2014 127 344-ATIO-25 Airline Operations II Embassy E Chaired by: D. DELAURENTIS, Purdue University 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2014-3263 AIAA-2014-3264 AIAA-2014-3265 AIAA-2014-3266 AIAA-2014-3267 AIAA-2014-3268 Optimizing Commercial Flight Fuel Influence of SHM Techniques on Modeling Delay and Delivery Electric Taxi Systems: An operations A Multi-Tier Evolution Model of Air Function-Structure Interdependence Consumption Through Changes Scheduled Maintenance for Aircraft Accuracy for Mixed Absolute and and value estimation Transportation Networks of Passenger Air Transportation: in Federal Regulations and Pilot Composite Structures Relative Spacing Operations C. Wijnterp, P. Roling, Delft University K. Song, J. Lewe, D. Mavris, Georgia Application of a Systemic Approach Techniques X. Chen, C. Bil, H. Ren, RMIT University, I. Levitt, Federal Aviation Administration, of Technology, Delft, The Netherlands; Institute of Technology, Atlanta, GA S. Lehner, V. Gollnick, German Aerospace N. Heitzman, T. Takahashi, Arizona State Melbourne, Australia Atlantic City, NJ; L. Weitz, MITRE Corporation, W. Wilde, KLM Royal Dutch Airlines, Center (DLR), Hamburg, Germany University, Tempe, AZ McLean, VA; B. Barmore, NASA Langley Schiphol, The Netherlands; R. Curran, Research Center, Hampton, VA; M. Castle, Delft University of Technology, Delft, The Aurora Sciences, LLC, Washington, DC Netherlands Friday, 20 June 2014 345-ATIO-26 Aircraft Economics Embassy F Chaired by: F. WIELAND, Intelligent Automation, Inc. 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs AIAA-2014-3269 AIAA-2014-3270 AIAA-2014-3271 AIAA-2014-3272 AIAA-2014-3273 Strategic Evolution in Aviation Transportation System-of-Systems Identification of Key Factors Improving Feasibility of Point to Value assessment method applied Modeling & Requirements Analysis Simulator for Multimodal Demand in Integrating Aircraft and the Point Operations Through Civil to aircraft exterior cleaning Y. Gawdiak, NASA Headquarters, Washington, and Emissions Forecasts Associated Supply Chains during Aerial Refuelling J. Sluis, P. Roling, Delft University of DC; J. Creedon, Old Dominion University, J. Lewe, H. Pfaender, L. Hivin, L. Zhang, Early Design Phases R. McRoberts, J. Early, M. Price, Queen’s Technology, Delft, The Netherlands; Norfolk, VA; V. Stouffer, LMI, McLean, VA; R. D. Mavris, Georgia Institute of Technology, Z. Tang, O. Pinon-Fischer, D. Mavris, University Belfast, Belfast, United Kingdom J. Berg, KLM Royal Dutch Airlines, Hemm, NextGen AeroSciences, LLC, Hampton, Atlanta, GA Georgia Institute of Technology, Atlanta, Schiphol, The Netherlands; R. Curran, VA; M. Narkus-Kramer, LMI, McLean, VA; S. GA Delft University of Technology, Delft, The Trajkov, Saab Sensis Corporation, Washington, Netherlands DC; et al. Friday, 20 June 2014 346-MAO-15 Multidisciplinary Analysis and Optimization: Applications II Embassy G Chaired by: S. FERGUSON, North Carolina State University 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs AIAA-2014-3274 AIAA-2014-3275 AIAA-2014-3276 AIAA-2014-3277 AIAA-2014-3278 Aerostructural optimization of Aerodynamic Shape Optimization The Influence of Structural Optimization of a Lunar Pallet Reducing Spacecraft Jitter During the Common Research Model of an Adaptive Morphing Trailing Variability on Limit Cycle Oscillation Lander Reinforcement Structure Satellite Reorientation Maneuvers configuration Edge Wing Behaviour Using a Genetic Algorithm via Solar Array Dynamics G. Kenway, G. Kennedy, University of Z. Lyu, J. Martins, University of Michigan, R. Hayes, W. Yao, S. Marques, Queen’s A. Burt, P. Hul, NASA Marshall Space Flight D. Herber, J. McDonald, University of Illinois, Michigan, Ann Arbor, Ann Arbor, MI; J. Ann Arbor, Ann Arbor, MI University Belfast, Belfast, United Kingdom Center, Huntsville, AL Urbana-Champaign, Urbana, IL; O. Alvarez- Martins, Georgia Institute of Technology, Salazar, Jet Propulsion Laboratory, California Atlanta, GA Institute of Technology, Pasadena, CA; G. Krishnan, J. Allison, University of Illinois, Urbana-Champaign, Urbana, IL Friday, 20 June 2014 347-ANERS-7 ANERS-Policy and Economics Embassy H Chaired by: D. DIMITRIU, Manchester Metropolitan University 1400 hrs 1430 hrs 1500 hrs AIAA-2014-3279 AIAA-2014-3280 AIAA-2014-3281 Climate-related Regulatory Scenario Exploration for Best options for regulating air Fees: How Do They Compare to Sustainability of the Multimodal transport’s full climate impact from Operating Costs? Intercity Transportation System an economic and environmental T. Thompson, Metron Aviation, Inc., L. Hivin, J. Lewe, H. Pfaender, D. Mavris, point of view - Main results from Dulles, VA Georgia Institute of Technology, Atlanta, DLR research project AviClim 128 GA J. Scheelhaase, R. Sausen, K. Dahlmann, M. Jung, H. Keimel, H. Niesse, German Aerospace Center (DLR), Cologne, Germany; et al. Friday, 20 June 2014 348-APA-57 Low Speed, Low Reynolds Number, Transonic, Supersonic and Hypersonic Aerodynamics IV Greenbriar Chaired by: J. DESPIRITO, US Army Research Laboratory and S. SAXENA, General Electric Company 1400 hrs 1430 hrs 1500 hrs 1530 hrs AIAA-2014-3282 AIAA-2014-3283 AIAA-2014-3284 AIAA-2014-3285 Glow Discharge Visualization of Numerical Simulation of Flow Predictive wall model for Numerical analysis of static and Hypersonic Separated Flow past Field around an Inflatable Reentry temperature fluctuations in dynamic performances of grid fin Cylinder/Plate Juncture Vehicle during a Demonstration hypersonic turbulent boundary controlled missiles H. Itoh, T. Ishida, Y. Miyoshi, M. Flight layers A. Despeyroux, R. Desaulnier, R. Luciano, Mizoguchi, National Defense Academy, Y. Takahashi, D. Ha, Hokkaido University, C. Helm, P. Martin, University of Maryland, M. Piotrowski, J. Hickey, X. Wu, Royal Yokosuka, Japan Sapporo, Japan; K. Yamada, T. Abe, Japan College Park, College Park, MD Military College of Canada, Kingston, Aerospace Exploration Agency (JAXA), Canada; et al. Sagamihara, Japan Friday, 20 June 2014 349-AA-42 Acoustic Measurements Hanover A Chaired by: F. HUTCHESON, NASA-Langley Research Center 1400 hrs 1430 hrs 1500 hrs 1530 hrs AIAA-2014-3286 AIAA-2014-3287 AIAA-2014-3288 AIAA-2014-3289 Extraction of Turbofan Combustion Flow modelling and noise Design of a low-noise aeroacoustic Improving the performance of Noise Spectra Using a combined generation of interacting prisms wind tunnel facility at Brunel aeroacoustic measurements beneath Coherence-Beamforming Technique Z. Prime, D. Moreau, C. Doolan, University University a turbulent boundary layer in a P. Rodriguez-Garcia, K. Holland, B. Tester, of Adelaide, Adelaide, Australia; M. Mat A. Vathylakis, T. Chong, Brunel University, wake flow University of Southampton, Southampton, Ali, Malaysia-Japan International Institute Uxbridge, United Kingdom S. Haxter, C. Spehr, German Aerospace Center United Kingdom of Technology, Kuala Lumpur, Malaysia (DLR), Göttingen, Germany; M. Hartmann, Volkswagen AG, Wolfsburg, Germany; J. Ocker, Porsche AG, Weissach, Germany; H. Tokuno, Daimler AG, Sindelfingen, Germany; G. Wickern, Audi AG, Ingolstadt, Germany Friday, 20 June 2014 350-AA-43 Fluid Acoustic Phenomena III Hanover B Chaired by: D. JUVE, Ecole Centrale de Lyon 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2014-3290 AIAA-2014-3291 AIAA-2014-3292 AIAA-2014-3293 AIAA-2014-3294 AIAA-2014-3295 An Experimental Study of the Effect of Mach number on Experimental and numerical Simulation of Sound Generated Tandem Cylinder Flow and Noise Aerodynamic Noise Prediction for Flow-induced Noise Created by a boundary layer noise investigation on noise induced by a by Large-Scale Vortices in a Control a Rod-Airfoil Configuration using Wall-mounted Finite Length Airfoil X. Gloerfelt, Paris Institute of Technology, butterfly valve Shear Layer by Hybrid DVM/APE H. Liu, Xi’an Jiaotong University, Xi’an, China; Large Eddy Simulations D. Moreau, Z. Prime, C. Doolan, University Paris, France; F. Margnat, National Center A. Chauvin, M. Sanjose, G. Lobel, S. Approach M. Azarpeyvand, University of Bristol, Bristol, B. Agrawal, A. Sharma, Iowa State 129 of Adelaide, Adelaide, Australia for Scientific Research (CNRS), Poitiers, Moreau, M. Brouillette, University of X. Jing, L. Wu, X. Dai, M. Song, X. Sun, United Kingdom; C. Ilario da Silva, Embraer, University, Ames, IA France Sherbrooke, Sherbrooke, Canada Beihang University, Beijing, China São José dos Campos, Brazil; J. Wei, Xi’an Jiaotong University, Xi’an, China Friday, 20 June 2014 351-AA-44 Trailing Edge Noise II Hanover C Chaired by: V. GOLUBEV, Embry-Riddle Aeronautical University (ERAU) and S. GLEGG, Florida Atlantic University 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2014-3296 AIAA-2014-3297 AIAA-2014-3298 AIAA-2014-3299 AIAA-2014-3300 AIAA-2014-3301 Trailing edge noise prediction for Experimental and numerical study Generic Airfoil Trailing-Edge Noise Predictions of the effect of wing Reduction of Bluntness-induced Tomographic PIV for Beveled rotating serrated blades on noise reduction mechanisms of Prediction using Stochastic Sound camber and thickness on airfoil Vortex Shedding Noise Using Trailing Edge Aeroacoustics S. Sinayoko, University of Southampton, the airfoil with serrated trailing Sources from Synthetic Turbulence self-noise Plasma Actuators S. Pröbsting, A. Gupta, F. Scarano, Delft Southampton, United Kingdom; M. edge C. Rautmann, J. Dierke, R. Ewert, N. Hu, C. Marks, M. Rumpfkeil, University of J. Kim, L. Al-Sadawi, T. Chong, Brunel University of Technology, Delft, The Azarpeyvand, University of Bristol, Bristol, L. Ji, W. Qiao, F. Tong, K. Xu, W. Chen, J. Delfs, German Aerospace Center (DLR), Dayton Research Institute, Dayton, OH; University, Uxbridge, United Kingdom Netherlands; Y. Guan, S. Morris, University United Kingdom; B. Lyu, University of Northwestern Polytechnical University, Braunschweig, Germany G. Reich, Air Force Research Laboratory, of Notre Dame, Notre Dame, IN Cambridge, Cambridge, United Kingdom Xi’an, China Wright-Patterson AFB, OH Friday, 20 June 2014 352-AA-45 CAA Propagation and Scattering II Hanover D Chaired by: R. ASTLEY, ISVR/University of Southampton 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2014-3302 AIAA-2014-3303 AIAA-2014-3304 AIAA-2014-3305 AIAA-2014-3306 AIAA-2014-3307 A Complex Equivalent Source Effect of Upstream Turbulence Wall Modeled Large Eddy Rnoise: A RANS Based Airfoil Gradient Term Filtering for Stable Development of Higher-Order Method for Scattering Effect of on Flow-Acoustic Resonance Simulation of Airfoil Trailing Edge Trailing-edge Noise Prediction Sound Propagation with Linearized Accurate Spatial Interpolation Aircraft Noise Interactions in Transitional Airfoils Noise Model Euler Equations Scheme for Unstructured Cartesian Y. Hou, X. Zhang, D. Angland, University V. Golubev, L. Nguyen, R. Mankbadi, J. Kocheemoolayil, S. Lele, Stanford M. Kamruzzaman, D. Bekiropoulos, A. X. Zhang, X. Chen, J. Gill, Southampton Grids of Southampton, Southampton, United Embry-Riddle Aeronautical University, University, Stanford, CA Wolf, T. Lutz, E. Kraemer, University of University, Southampton, United Kingdom Y. Tamaki, T. Imamura, University of Kingdom Daytona Beach, FL; M. Roger, École Stuttgart, Stuttgart, Germany Tokyo, Tokyo, Japan Centrale de Lyon, Ecully, France; J. Dudley, Air Force Research Laboratory, Eglin AFB, FL; M. Visbal, Air Force Research Laboratory, Wright-Patterson AFB, OH Friday, 20 June 2014 353-AA-46 Jet Noise Near Field II Hanover E Chaired by: A. PILON, Lockheed Martin Aeronautics 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2014-3308 AIAA-2014-3309 AIAA-2014-3310 AIAA-2014-3312 AIAA-2014-3313 AIAA-2014-3314 Numerical Prediction of an Acoustic The Azimuthal Variations of Near Pressure-density gradient correlations Investigation of Supersonic Jet Flow Aeroacoustic study of Internal Acoustics of Jet Surface Interaction Field of a Supersonic Jet Impinging on Field Pressure Fluctuations in in the near-field of a transonic jet Using Modal Decomposition Mixing Nozzles with Forced Lobed - Scrubbing Noise a Plate at Different Inclination Angles Elliptical Jets E. Miguel, National Research Council R. Larusson, H. Hafsteinsson, N. Mixers using a High-Mach Subsonic A. Khavaran, NASA Glenn Research Center, V. Golubev, A. Lyrintzis, R. Mankbadi, Embry- S. Sharma, A. Chatterjee, Indian Institute (CNR), Rome, Italy; L. Gefen, Roma Tre Andersson, L. Eriksson, Chalmers Lattice Boltzmann Scheme Cleveland, OH

130 Riddle Aeronautical University, Daytona Beach, of Technology Bombay, Mumbai, India; M. University, Rome, Italy; C. Freitas, S. University of Technology, Göteborg, K. Habibi, L. Mongeau, McGill University, FL; K. Kurbatskii, ANSYS, Inc., Lebanon, NH; Kanniyam Natarajan, National Aerospace Grizzi, National Research Council (CNR), Sweden Montréal, Canada; D. Casalino, Exa B. Guenthoer, Embry-Riddle Aeronautical Laboratories, Bangalore, India Rome, Italy; R. Camussi, Roma Tre Corporation, Stuttgart, Germany; P. Lew, University, Daytona Beach, FL University, Rome, Italy; M. Felli, National Exa Corporation, Burlington, MA Research Council (CNR), Rome, Italy Friday, 20 June 2014 354-AA-47 Turbomachinery and Propeller Noise Hanover F Chaired by: W. ALEXANDER, Virginia Tech 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs AIAA-2014-3315 AIAA-2014-3316 AIAA-2014-3317 AIAA-2014-3318 AIAA-2014-3319 AIAA-2014-3320 AIAA-2014-3321 On the generation of indirect Analysis of Dual Rotating Rake A cross-comparison of different Radial mode analysis of broadband Acoustic Localization of Vane Faults Non-orthogonality and Transient Core noise - Identification of combustion noise Data from the NASA Glenn post-processing and acoustic noise in flow ducts using a in Turbomachinery Based on Source Growth Analysis of a Premixed broadband noise sources of a C. Tam, S. Parrish, Florida State University, Advanced Noise Control Fan Duct measurement devices for high combined axial and azimuthal Modeling Flame-Acoustic Interaction in a turbo-shaft engine Tallahassee, FL with Artificial Sources speed near field noise on the S1MA sensor array W. Jürgens, U. Tapken, O. Lemke, I. Choked Combustor B. Pardowitz, U. Tapken, K. Knobloch, F. M. Dahl, D. Sutliff, NASA Glenn Research BHCR open rotor test rig U. Tapken, D. Gutsche, L. Enghardt, Röhle, L. Enghardt, German Aerospace D. Zhao, C. Ji, S. Li, X. Li, Nanyang Bake, German Aerospace Center (DLR), Center, Cleveland, OH F. Mery, ONERA, Modane, France German Aerospace Center (DLR), Berlin, Center (DLR), Berlin, Germany Technological University, Singapore, Berlin, Germany; E. Bouty, Turbomeca, Germany Singapore Bordes, France; I. Davis, Trinity College Dublin, Dublin, Ireland; et al. Friday, 20 June 2014 355-FD-35 Low-Speed Separated Flows Harris Chaired by: D. WILLIAMS, Illinois Institute of Technology 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2014-3322 AIAA-2014-3323 AIAA-2014-3324 AIAA-2014-3325 AIAA-2014-3326 AIAA-2014-3327 Cylinder in the vicinity of a bluff Analysis of Unsteady Flow Past a Investigation of the NACA 4412 Experimental and Numerical Flow Wind Tunnel Investigation of the Wind Attached and Separated Flow body leading edge Circular Cylinder Using a Harmonic Trailing Edge Separation Using a Analysis around Circular Cylinders Flow Patterns in the Neighborhood of Simulations with Realizable Unified T. Michelis, M. Kotsonis, Delft University of Balance Method Lattice-Boltzmann Approach Using POD and DMD the Mobile Integration Tower (IMT) RANS-LES Methods Technology, Delft, The Netherlands E. Clark, K. Ekici, University of Tennessee, B. Koenig, E. Fares, Exa Corporation, M. Sakai, Y. Sunada, T. Imamura, K. in the Centro de Lançamento de M. Stoellinger, S. Heinz, University of Knoxville, Knoxville, TN; P. Beran, Air Force Stuttgart, Germany; A. Jammalamadaka, Rinoie, University of Tokyo, Tokyo, Japan Alcântara (CLA) Wyoming, Laramie, Laramie, WY; P. Research Laboratory, Wright-Patterson Y. Li, Exa Corporation, Burlington, MA F. Brasileiro, University of Vale do Paraíba, São Balakumar, NASA Langley Research AFB, OH José dos Campos, Brazil; A. Avelar, A. Faria, G. Center, Hampton, VA Fisch, Aeronautics and Space Institute (IAE), São José dos Campos, Brazil Friday, 20 June 2014 356-FD-36 Turbulence Simulations Inman Chaired by: G. BLAISDELL, Purdue University and O. KHAN, Tuskegee Univ 1400 hrs 1430 hrs 1500 hrs 1530 hrs AIAA-2014-3328 AIAA-2014-3329 AIAA-2014-3330 AIAA-2014-3331 Large-Scale Structures in Implicit Detached-Eddy Simulation of A Gas-Kinetic Scheme for Turbulent Improvements to Rahman-Agarwal- Large-Eddy Simulation of a Reattaching Shear Layer in Flow Siikonen One-Equation Turbulence Compressible Turbulent Flow Compressible Turbulent Flow M. Righi, Zurich University of Applied Model Based on k-epsilon Closure J. Poggie, Air Force Research Laboratory, T. Leger, J. Poggie, Air Force Research Sciences, Winterthur, Switzerland M. Rahman, Aalto University, Helsinki, Finland; Wright-Patterson AFB, OH Laboratory, Wright-Patterson AFB, OH R. Agarwal, Washington University in St. Louis, 131 St. Louis, MO; M. Lampinen, T. Siikonen, Aalto University, Helsinki, Finland Friday, 20 June 2014 357-FD-37 Shock-Boundary Layer Interactions Kenneshaw Chaired by: J. BENEK 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2014-3332 AIAA-2014-3333 AIAA-2014-3334 AIAA-2014-3335 AIAA-2014-3336 AIAA-2014-3337 Effects of Laminar-Turbulent High-resolution PIV measurements An investigation of interactions High-Order Implicit Large-Eddy The Effect of Wind Tunnel Size Numerical Prediction of Shock- Transition on the Shock-Wave/ of a transitional shock wave- between normal shocks and Simulations of a Supersonic Corner and Shock Strength on Incident Boundary Layer Interaction Boundary-Layer Interaction boundary layer interaction transitional boundary layers Flow over a Compression Ramp Shock Boundary Layer Interaction between a Pair of Fins in E. Schuelein, German Aerospace Center R. Giepman, F. Schrijer, B. van T. Davidson, H. Babinsky, University of N. Bisek, Air Force Research Laboratory, Experiments Hypersonic Flow (DLR), Göttingen, Germany Oudheusden, Delft University of Cambridge, Cambridge, United Kingdom Wright-Patterson AFB, OH J. Benek, C. Suchyta, Air Force Research V. Bhagwandin, Army Research Laboratory, Technology, Delft, The Netherlands Laboratory, Wright-Patterson AFB, OH; Aberdeen Proving Ground, MD H. Babinsky, University of Cambridge, Cambridge, United Kingdom Friday, 20 June 2014 358-FD-38 Acoustic and Unsteady Flows Lenox Chaired by: P. MORRIS, Pennsylvania State University and L. CATTAFESTA, FAMU-FSU College of Engineering 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs AIAA-2014-3338 AIAA-2014-3339 AIAA-2014-3340 AIAA-2014-3341 AIAA-2014-3342 Determination of Acoustic Acoustic streaming and its modeling A Method for Estimating Surface Study of unsteady shock motion in A combustion instability model Scattering Matrices Using Nonlinear in a traveling-wave thermoacoustic Pressure Forces and Far-Field shock/turbulence interaction accounting for dynamic flame-flow- Disturbance Equations heat engine Acoustics P. Sashittal, Y. Madras Sethuraman, Indian acoustic interactions S. Koeglmeier, Technical University of Munich, C. Scalo, S. Lele, L. Hesselink, Stanford A. Nickels, L. Ukeiley, University of Florida, Institute of Technology Bombay, Mumbai, R. Assier, X. Wu, Imperial College London, Munich, Germany; R. Kaess, Astrium, Munich, University, Stanford, CA Gainesville, Gainesville, FL; R. Reger, India; J. Larsson, University of Maryland, London, United Kingdom Germany; T. Sattelmayer, Technical University L. Cattafesta, Florida State University, College Park, College Park, MD; K. Sinha, of Munich, Munich, Germany Tallahassee, FL Indian Institute of Technology Bombay, Mumbai, India Friday, 20 June 2014 359-FD-39 Comparison between CFD and Measurements in Hypervelocity Flows Part II: Shockwave Turbulent Boundary Layer Interaction in High Reynolds Number Duplicating Marietta Mach 5 - 8 Flows Chaired by: M. MACLEAN, CUBRC and T. WADHAMS, CUBRC 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs Oral Presentation Oral Presentation Oral Presentation Oral Presentation Oral Presentation Oral Presentation Measurements of Shockwave US3D Simulations of High-Reynolds Comparison of Turbulence Models Shock Wave Interactions: A CFD Simulations of Separated Turbulent Comparison between CFD and Turbulent Boundary Layer Number Hypersonic Separated for Prediction of Shockwave Study of CUBRC LENS-II Turbulent Flow with LAURA and FUN3D Measurements for Shockwave Interaction for High Reynolds Flows (Invited) Turbulent Boundary Layer Experiments (Invited) (Invited) Turbulent Boundary Layer Interaction Number Duplicated Mach 5 - 8 G. Candler, I. Nompelis, University of Interaction in Hypervelocity Flow D. Prabhu, ERC, Inc., Moffett Field, CA P. Gnoffo, NASA Langley Research Center, for High Reynolds Number Duplicated Flows (Invited) Minnestoa, Minneapolis, MN (Invited) Hampton, VA Mach 5 - 8 Flows (Invited) 132 M. Holden, T. Wadhams, M. MacLean, R. Bowersox, Texas A&M University, T. Wadhams, M. Holden, M. MacLean, CUBRC, Inc., Buffalo, NY College Station, TX CUBRC, Inc., Buffalo, NY Friday, 20 June 2014 360-AA-48 Fan Noise III Piedmont Chaired by: D. NARK, NASA-Langley Research Center 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2014-3344 AIAA-2014-3345 AIAA-2014-3346 AIAA-2014-3347 AIAA-2014-3348 AIAA-2014-3349 On the Influence of Rotor Design The effect of airfoil clocking on An experimental study on router Experimental study and velocity Noise generation and propagation for Experimental and Numerical Study on an Acoustically 3d-Designed noise generation and propagation cooling fan noise reduction by scaling of the tip-leakage noise different turning mid turbine frame on Noise Reduction Mechanisms of Turbine Exit Guide Vane in a two shaft test turbine inflow screens generated by low-speed axial setups in a two shaft test turbine the Linear Cascade with Serrated T. Selic, A. Marn, Graz University of C. Faustmann, S. Bauinger, A. Marn, E. Y. Xu, X. Li, Beihang University, Beijing, flow-fans C. Faustmann, S. Zerobin, A. Marn, Graz Trailing Edge Technology, Graz, Austria Göttlich, Graz University of Technology, China E. Canepa, A. Cattanei, F. Mazzocut University of Technology, Graz, Austria; M. W. Qiao, L. Ji, F. Tong, W. Chen, K. Xu, Graz, Austria Zecchin, University of Genoa, Genoa, Italy Spitalny, German Aerospace Center (DLR), Northwestern Polytechnical University, Berlin, Germany; D. Broszat, MTU Aero Xi’an, China Engines AG, Munich, Germany; E. Göttlich, Graz University of Technology, Graz, Austria Friday, 20 June 2014 361-AA-49 Duct Liners II Spring Chaired by: W. WATSON, NASA-Langley Research Center 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs AIAA-2014-3350 AIAA-2014-3351 AIAA-2014-3352 AIAA-2014-3353 AIAA-2014-3354 Hard wall-soft wall-vorticity Single Mode Theory for Impedance Evaluation of a Variable-Impedance Nonlinear absorption characteristics Direct numerical simulation and scattering in shear flow Eduction in Large-Scale Ducts with Ceramic Matrix Composite Acoustic and micro flow physics of resonator analytical modeling of locally reacting, S. Rienstra, D. Singh, Technical University Grazing Flow Liner under high sound intensity single degree of freedom acoustic of Eindhoven, Eindhoven, The Netherlands W. Watson, M. Jones, NASA Langley Research M. Jones, W. Watson, D. Nark, B. J. Xu, X. Li, Y. Guo, Beihang University, liners with turbulent grazing flow Center, Hampton, VA; J. June, University of Howerton, NASA Langley Research Center, Beijing, China Q. Zhang, D. Bodony, University of Illinois, Florida, Gainesville, Gainesville, FL Hampton, VA Urbana-Champaign, Urbana, IL Friday, 20 June 2014 362-TP-24 Heat Transfer in Cooling, Heating and Power Generation III Techwood Chaired by: G. ZISKIND, Ben-Gurion University of the Negev and K. MCKITTRICK, Stinger Ghaffarian Technologies, Inc. 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs AIAA-2014-3355 AIAA-2014-3356 AIAA-2014-3357 AIAA-2014-3358 AIAA-2014-3359 Simulation of heat transfer of Development and Selection of Gas- Natural Convective Heat Transfer Numerical analysis of heat transfer Effect of Buoyancy on Heat Transfer mildly-cracked n-decane in a tube Liquid High Pressure Heat Exchangers from a Horizontal Isothermal deterioration of China RP-3 Characteristics of Supercritical Carbon with 3-dimensional equation of for External Combustion Heat driven Circular Element Imbedded in a Flat aviation kerosene in a circular tube Dioxide in the Heating Mode state look-up table Heat Pumps Adiabatic Surface with a Parallel at supercritical pressures S. Pidaparti, E. Umrigar, J. McFarland, D. Z. Liu, J. Liang, Y. Pan, National University Y. Bedekar, ThermoLift, Inc., Stony Adiabatic Covering Surface Z. Liu, J. Liang, Y. Pan, National University Ranjan, Texas A&M University, College of Defense Technology, Changsha, China Brook, NY P. Oosthuizen, Queen’s University, of Defense Technology, Changsha, China Station, TX; M. Anderson, University of Kingston, Canada Wisconsin, Madison, Madison, WI Friday, 20 June 2014 363-TP-25 Multiphase, Jets and Thermosyphons II University Chaired by: C. PARK, University of Nevada, Reno and C. LIN, Florida International University 1400 hrs 1430 hrs 1500 hrs 1530 hrs AIAA-2014-3360 AIAA-2014-3361 AIAA-2014-3362 AIAA-2014-3363 The effect of noncondensables A CFD model for the Multipurpose Modeling of Droplets Deformations Length of the Entrance, Fully on the buoyancy-thermocapillary Hydrogen Test Bed (MHTB) near the Leading Edge of an Airfoil developed and hydraulic convection in confined and volatile Ground-Based Self-Pressurization S. Sor, A. Garcia-Magariño, National characteristics of bubbly flows in fluids and Pressure Control Experiments Institute of Aerospace Technology, Madrid, helical coils T. Qin, R. Grigoriev, Georgia Institute of O. Kartuzova, M. Kassemi, J. Agui, J. Spain R. Moosavi, Florida International Technology, Atlanta, GA Moder, NASA Glenn Research Center, University, Miami, FL; H. Saffari, Iran Cleveland, OH University of Science and Technology, 133 Tehran, Iran; R. Kiflemariam, C. Lin, Florida International University, Miami, FL Friday, 20 June 2014 364-TP-26 Multi-Scale Heat Transfer V Vinings Chaired by: B. COLA, Georgia Institute of Technology and I. COTOROS, Lockheed Martin Space Systems 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs Oral Presentation Oral Presentation Oral Presentation Oral Presentation Oral Presentation AIAA-2014-3364 Size Effects in the Thermal Molecular Dynamics Simulations of Coherent and Incoherent Thermal Ensemble Averaging vs. Understanding Quasiballistic Selective Thermal Emission with Conductivity of GaAs/AlAs Thermal Transport in Polythiophene Transport in Nanomeshes Time Sampling for Molecular Thermal Transport in Broad- Thin Films of Polar Materials Superlattices: Period Thickness Chains N. Ravichandran, A. Minnich, California Dynamics Simulations of Thermal band Frequency-domain A. Narayanaswamy, J. Mayo, C. Canetta, Versus Sample Thickness A. Henry, W. Lv, Georgia Institute of Institute of Technology, Pasadena, CA Conductivity Thermoreflectance Columbia University, New York, NY R. Cheaito, J. Gaskins, University of Technology, Atlanta, GA K. Gordiz, A. Henry, Georgia Institute of C. Hua, A. Minnich, California Institute of Virginia, Charlottesville, Charlottesville, VA; Technology, Atlanta, GA Technology, Pasadena, CA G. Balakrishnan, T. Rotter, University of New Mexico, Albuquerque, Albuquerque, NM; P. Hopkins, University of Virginia, Charlottesville, Charlottesville, VA Friday, 20 June 2014 365-NW-14 Friday Afternoon Networking Coffee Break Meeting Room Foyers 1530 - 1600 hrs Friday, 20 June 2014 366-ANERS-8 Can We Resolve the Most Pressing Modeling, Policy, and Economic Challenges? Embassy H 1630 - 1730 hrs Moderator: Lourdes Maurice Panelists: John Cavolowsky Kevin Welsh Goergeta Dinu NASA FAA TAROM

Author/Session Chair Index Abdallah, A., 51-AFM-5 Akhmetov, B., 320-AA-35 Alvarez-Salazar, O., 346-MAO-15 Arntz, A., 156-APA-28 Bahr, C., 0-, 94-AA-5, 169-AA-13, 287-AA-30 Abdelmoula, F., 92-ASE-6/AFM-6/FT-2 Akins, D., 59-FC-5 Alves, L., 291-FD-29 Arora, N., 40-APA-10 Bai, X., 314-ATIO-24 Abdelmoula, M., 262-HYTASP-9 Akkermans, R., 309-APA-47, 321-AA-36 Alvi, F., 99-FC-7 Arunajatesan, S., 22-FD-2, 280-APA-44 Bailly, C., 202-AA-14, 253-AA-21 Abdol-Hamid, K., 7-APA-4 Akmandor, İ., 39-APA-9/FC-4 Alvord, D., 286-AA-29 Asada, K., 180-FC-10/PDL-11, 189-APA-30 Bailly, D., 271-APA-42 Abdulrahim, M., 220-AFM-14 Akpolat, M., 213-HYTASP-6 Alyanak, E., 199-MAO-10, 315-MAO-14, 330-APA-52 Asadi, F., 275-ATIO-22 Bake, F., 264-AA-24, 354-AA-47 Abe, T., 103-PDL-8, 183-TP-11, 265-TP-17, 348-APA-57 Aksaray, D., 115-ATIO-11 Amar, A., 32-TP-1 Ashley, A., 119-MAO-7 Balabanov, V., 86-MAO-6, 120-MAO-8, 274-DE-1 Abedi, H., 239-APA-38 Aksu, A., 144-AFM-12 Amaya, M., 215-AMT-10/GT-8 Ashley, J., 259-FC-12 Balachandar, B., 163-FD-14 Abelman, S., 251-ASE-15 Al-Khalil, K., 91-ASE-5 Amritkar, A., 236-APA-35 Ashraf, M., 7-APA-4, 339-APA-53 Balakrishna, S., 310-APA-48 Åbom, M., 298-AA-33 Al-Sadawi, L., 351-AA-44 An, P., 331-HYTASP-13 Asrar, W., 190-APA-31, 195-LTA-1 Balakrishnan, G., 364-TP-26 Acharya, T., 30-AMT-2/PDL-2 Alahyari Beig, S., 163-FD-14 Ananda Krishnan, G., 40-APA-10 Assier, R., 358-FD-38 Balakumar, P., 172-FD-16, 355-FD-35 134 Adamovich, I., 30-AMT-2/PDL-2 Alam, M., 7-APA-4, 180-FC-10/PDL-11 Anders, S., 135-FC-8/APA-24, 162-APA-29 Astley, R., 123-AA-6, 229-LEC-6, 298-AA-33, 352-AA-45 Balaras, E., 311-APA-49 Addy, G., 166-ASE-9 Alauzet, F., 210-FD-19 Anderson, A., 323-AA-38 Atak, M., 290-FD-28 Balas, M., 15-AFM-1 Adetifa, O., 261-AA-23 Alavi Moghadam, M., 285-AA-28 Anderson, J., 124-AA-7, 165-AA-11, 253-AA-21 Atesoglu, Ö., 182-AFM-13 Balchanos, M., 60-ATIO-8 Adriaansen, D., 18-ASE-2 Albert, M., 11-MAO-1 Anderson, M., 362-TP-24 Atinault, O., 156-APA-28 Balesdent, M., 278-MAO-12 Agarwal, A., 164-AA-10, 206-AA-16, 248-AA-18, Alder, M., 122-FD-11 Anderson, W., 270-APA-41, 326-FD-32, 329-FD-34 Aubert, M., 249-AA-19 Balistreri, C., 79-APA-16 261-AA-23, 286-AA-29, 323-AA-38 Alexander, W., 124-AA-7, 165-AA-11, 203-AA-15, Andersson, N., 123-AA-6, 353-AA-46 Aubert, R., 52-ASE-3 Ballard, D., 114-ATIO-10 Agarwal, R., 55-FD-6, 192-APA-33, 239-APA-38, 253-AA-21, 354-AA-47 Andreutti, G., 103-PDL-8, 308-APA-46 Aupoix, B., 125-ASE-7 Bambos, N., 9-ATIO-2 325-FD-31, 356-FD-36 Alexeenko, A., 336-TP-22 Andrews, S., 160-ACD-7 Avelar, A., 310-APA-48, 355-FD-35 Banerjee, S., 138-HYTASP-5 Agostinelli, C., 6-APA-3 Ali, J., 195-LTA-1 Andrienko, D., 103-PDL-8, 131-PDL-9 AVerkin, S., 171-FD-15 Bangert, L., 38-APA-8 Agrawal, B., 350-AA-43 Ali, M., 155-APA-27 Anemaat, W., 10-ACD-1, 160-ACD-7 Awasthi, M., 124-AA-7 Banica, M., 298-AA-33 Agrawal, S., 110-APA-20 Ali, S., 96-FD-10, 173-FD-17 Angersbach, A., 274-DE-1 Ayton, L., 90-AA-3, 261-AA-23 Banks, D., 238-APA-37 Agui, J., 363-TP-25 Alkandry, H., 32-TP-1, 183-TP-11, 327-FD-33 Angland, D., 249-AA-19, 259-FC-12, 352-AA-45 Azarpeyvand, M., 350-AA-43, 351-AA-44 Baqui, Y., 206-AA-16 Aharon, Y., 223-TP-16 Allair, F., 277-ACD-12 Anisimov, K., 24-FD-4 Azevedo, J., 40-APA-10, 270-APA-41 Barad, M., 23-FD-3 Ahmad, N., 126-ASE-8/AFM-9/FT-3, 205-ASE-12 Allan, B., 153-APA-25 Anna, A., 327-FD-33 Baars, W., 252-AA-20 Barbaresco, F., 92-ASE-6/AFM-6/FT-2 AhmadBeygi, S., 42-ATIO-4 Allan, M., 89-AA-2 Anobile, A., 320-AA-35 Babinsky, H., 13-APA-5/FC-1, 214-FC-11, Barber, J., 97-PDL-7 Ahmed, A., 97-PDL-7, 131-PDL-9, 214-FC-11 Allen, A., 240-ATIO-17 Ansell, P., 289-FD-27 238-APA-37, 248-AA-18, 269-APA-40, 357-FD-37 Barcena, J., 101-HYTASP-3 Ahmed, H., 97-PDL-7, 131-PDL-9 Allen, B., 193-ATIO-15 Antani, T., 110-APA-20 Babu, D., 87-APA-18 Barker, P., 100-AMT-4/GT-3 Ahn, J., 134-HYTASP-4 Allen, C., 10-ACD-1, 330-APA-52 Antony, R., 246-APA-39 Babulin, A., 111-APA-21 Barmore, B., 313-ATIO-23, 344-ATIO-25 Ahuja, K., 93-AA-4, 168-AA-12, 252-AA-20, Allen, J., 12-MAO-2 Aono, H., 40-APA-10, 180-FC-10/PDL-11, 189-APA-30 Bach, T., 84-ACD-4 Barnes, C., 88-FD-9 286-AA-29, 320-AA-35 Alley, N., 158-FT-4 Appel, C., 164-AA-10 Bachchan, N., 289-FD-27 Barnes, F., 262-HYTASP-9 Aigner, M., 123-AA-6 Allison, D., 199-MAO-10 Appelbaum, J., 39-APA-9/FC-4 Bacon, B., 273-ATIO-20 Barnhardt, M., 32-TP-1 Airimitoaie, T., 259-FC-12, 269-APA-40 Allison, J., 346-MAO-15 Arai, T., 328-HYTASP-12 Bacon, D., 205-ASE-12 Barone, M., 278-MAO-12, 280-APA-44 Ajaj, R., 198-ACD-9 Almoneit, D., 321-AA-36 Archer, J., 116-ATIO-12 Badcock, K., 37-APA-7, 160-ACD-7 Barrado, C., 314-ATIO-24 Akbar, M., 143-TP-10 Alonso, J., 85-MAO-5, 110-APA-20, 278-MAO-12, Arena, A., 144-AFM-12 Bader, R., 105-TP-7 Barral, N., 210-FD-19 Akella, M., 259-FC-12 331-HYTASP-13 Arina, R., 207-AA-17 Bae, H., 119-MAO-7 Barrier, R., 285-AA-28 Akgun, T., 291-FD-29 Alunni, A., 221-TP-14 Arnoldus, Q., 52-ASE-3 Baer, S., 16-AFM-2 Barsky, D., 311-APA-49 Author/Session Chair Index Bartels, R., 122-FD-11 Bernardini, C., 269-APA-40 Bolan, J., 136-AMT-5/GT-4 Brasileiro, F., 355-FD-35 Buning, P., 169-AA-13 Bartram, S., 94-AA-5, 128-AA-9 Bernardini, G., 320-AA-35 Bolduc-Teasdale, F., 274-DE-1 Braun, R., 104-AFM-7, 107-AFM-8 Buonanno, M., 38-APA-8, 110-APA-20 Bas, I., 314-ATIO-24 Bernardo, B., 133-FD-13 Bolender, M., 16-AFM-2 Bravin, M., 250-ASE-14/GT-10 Burdette, D., 115-ATIO-11 Basavanahalli, R., 255-FD-23 Bernardo, J., 200-ANERS-1, 245-ANERS-3 Bolshunov, K., 111-APA-21 Breeze-Stringfellow, A., 284-ASE-16 Burke, J., 42-ATIO-4 Bass, R., 251-ASE-15 Berrou, Y., 279-ANERS-4 Bona, G., 200-ANERS-1 Brehm, C., 23-FD-3, 132-FD-12 Burley, C., 94-AA-5, 169-AA-13, 207-AA-17, 240-ATIO-17 Bassetti, A., 252-AA-20 Berry, A., 261-AA-23, 320-AA-35 Bonaccurso, E., 91-ASE-5 Brenner, M., 15-AFM-1, 49-AFM-3 Burnazzi, M., 135-FC-8/APA-24 Basso, E., 310-APA-48 Bertish, S., 114-ATIO-10 Bond, C., 80-APA-17 Brenner, P., 190-APA-31 Burnett, E., 174-MST-4 Bastide, M., 136-AMT-5/GT-4 Berton, B., 158-FT-4 Bonifacio, J., 289-FD-27 Brentner, K., 52-ASE-3 Burt, A., 45-MAO-3, 346-MAO-15 Bathel, B., 61-AMT-3/GT-2, 37-AMT-6/GT-5, Berton, J., 203-AA-15 Bonnaud, C., 282-AA-26 Brentzel, K., 167-ASE-10/FT-5 Burt, J., 142-TP-9 176-AMT-8/GT-6 Bertsch, L., 20-AA-1, 43-ACD-2 Bonneau, V., 285-AA-28 Brès, G., 164-AA-10, 293-FD-30 Burton, S., 46-MAO-4 Batten, P., 207-AA-17 Bestle, D., 11-MAO-1, 274-DE-1 Bonnet, J., 59-FC-5 Brevault, L., 278-MAO-12 Busan, R., 273-ATIO-20 Bauer, M., 112-APA-22 Bevirt, J., 113-ATIO-9, 240-ATIO-17 Bono, J., 42-ATIO-4 Breviglieri, C., 270-APA-41 Bush, R., 22-FD-2 Bauer, T., 92-ASE-6/AFM-6/FT-2 Beyer, S., 101-HYTASP-3 Bons, J., 269-APA-40 Briand, J., 158-FT-4 Busse-Gerstengarbe, S., 264-AA-24 Bauinger, S., 360-AA-48 Bhagwandin, V., 192-APA-33, 269-APA-40, 357-FD-37 Bonucci, G., 211-FD-20 Bricalli, M., 24-FD-4, 213-HYTASP-6 Butler, K., 208-HYTASP-24 Bauschat, M., 271-APA-42 Bhunia, A., 33-TP-2 Boopathy, K., 161-MAO-9 Briceno, S., 197-ACD-8 Buttsworth, D., 331-HYTASP-13 Bays, L., 41-ATIO-3 Bi, Q., 266-TP-18 Bopp, M., 190-APA-31 Brichet, G., 282-AA-26 Cabell, K., 176-AMT-8/GT-6 Baysal, O., 122-FD-11 Biancolini, M., 318-APA-51 Borchers, P., 196-ATIO-16, 314-ATIO-24 Bridge, T., 215-AMT-10/GT-8 Cabell, R., 240-ATIO-17 Beals, N., 308-APA-46 Biasi, V., 184-TP-12 Bordji, M., 190-APA-31 Bridges, J., 252-AA-20, 282-AA-26 Caccamo, M., 154-APA-26 Beauchene, P., 184-TP-12 Bidwell, C., 52-ASE-3, 125-ASE-7, 153-APA-25, Boreman, G., 299-TP-19 Brieschenk, S., 65-PDL-4, 213-HYTASP-6, Cai, N., 67-TP-5 Beberniss, T., 14-FD-1 204-ASE-11 Borer, N., 240-ATIO-17 262-HYTASP-9, 331-HYTASP-13 Cai, S., 33-TP-2, 223-TP-16 Beck, A., 202-AA-14 Bieniek, D., 92-ASE-6/AFM-6/FT-2 Borg, M., 96-FD-10 Bright, T., 34-TP-3 Cai, X., 281-FD-26 Becker, L., 94-AA-5 Biesslich, P., 41-ATIO-3, 313-ATIO-23 Borg, S., 136-AMT-5/GT-4 Brionnaud, R., 155-APA-27 Cai, Z., 259-FC-12 Beckmann, B., 159-ATIO-14 Bil, C., 84-ACD-4, 197-ACD-8, 241-ATIO-18, 344-ATIO-25 Borghi, C., 181-PDL-6/FC-6, 189-APA-30 Britcher, C., 176-AMT-8/GT-6 Cain, A., 27-AMT-1/GT-1 Bedekar, Y., 335-TP-21, 362-TP-24 Billmers, E., 53-ASE-4/FT-1 Borgoltz, A., 27-AMT-1/GT-1, 260-AMT-12/GT-11 Britchford, K., 203-AA-15 Calamas, D., 299-TP-19 135 Beeler, G., 172-FD-16 Billmers, R., 53-ASE-4/FT-1 Borner, A., 222-TP-15 Brito Gadeschi, G., 212-FD-21 Callantine, T., 116-ATIO-12, 242-ATIO-19 Béguin, C., 222-TP-15 Billonnet, G., 295-AA-32 Bose, D., 271-APA-42 Brizzi, L., 254-AA-22 Callicoat, J., 287-AA-30 Behr, M., 122-FD-11 Binet, D., 321-AA-36 Bose, S., 164-AA-10 Broeren, A., 166-ASE-9 Calvert, M., 246-APA-39, 342-APA-56 Beitel, G., 136-AMT-5/GT-4 Birch, T., 4-APA-1, 37-APA-7 Bosmajian, N., 176-AMT-8/GT-6 Bromberg, E., 42-ATIO-4 Calvert, N., 61-AMT-3/GT-2 Bekiropoulos, D., 352-AA-45 Birling, F., 314-ATIO-24 Bosnyakov, I., 270-APA-41 Bronsvoort, J., 83-ATIO-7 Calzada, J., 294-APA-45 Belardo, M., 84-ACD-4 Bisek, N., 181-PDL-6/FC-6, 357-FD-37 Bosson, C., 8-ATIO-1 Brooks, T., 94-AA-5, 169-AA-13, 207-AA-17 Cameron, C., 342-APA-56 Bellemans, A., 325-FD-31 Bisson, F., 318-APA-51 Botez, R., 49-AFM-3, 79-APA-16, 83-ATIO-7, Broszat, D., 360-AA-48 Campbell, R., 78-APA-15 Belyaev, I., 20-AA-1, 286-AA-29, 287-AA-30 Bitter, N., 132-FD-12 279-ANERS-4, 317-APA-50 Brouillette, M., 350-AA-43 Campbell, S., 196-ATIO-16 Ben-Tzvi, P., 294-APA-45 Bixler, N., 255-FD-23 Bottländer, D., 134-HYTASP-4 Brown, A., 67-TP-5, 92-ASE-6/AFM-6/FT-2, 126-ASE-8/ Campitelli, G., 175-FC-9 Benavides, J., 51-AFM-5 Black, J., 18-ASE-2 Bouarfa, S., 313-ATIO-23 AFM-9/FT-3, 170-ITAR-3, 217-HYTASP-7, 255-FD-23 Campos, N., 159-ATIO-14 Benchiekh, M., 214-FC-11 Blaisdell, G., 202-AA-14, 356-FD-36 Bouchez, M., 262-HYTASP-9 Brown, C., 52-ASE-3, 252-AA-20, 323-AA-38 Camussi, R., 353-AA-46 Bender, J., 265-TP-17 Blake, J., 91-ASE-5 Bouilly, J., 101-HYTASP-3 Brown, K., 27-AMT-1/GT-1 Canal, D., 92-ASE-6/AFM-6/FT-2 Benek, J., 357-FD-37 Blake, W., 124-AA-7 Bouremel, Y., 339-APA-53 Brown, L., 24-FD-4 Canchero, A., 272-APA-43 Bengin, A., 310-APA-48 Blanquart, G., 66-TP-4 Bouty, E., 354-AA-47 Brown, M., 79-APA-16 Candler, G., 66-TP-4, 96-FD-10, 265-TP-17, Bennani, A., 298-AA-33 Bloebaum, C., 46-MAO-4, 119-MAO-7, 199-MAO-10 Bowerman, K., 241-ATIO-18 Brown, R., 98-HYTASP-2, 213-HYTASP-6, 281-FD-26, 291-FD-29, 325-FD-31, 326-FD-32, Bennani, L., 17-ASE-1 Bloem, M., 9-ATIO-2, 116-ATIO-12 Bowersox, R., 48-FD-5, 61-AMT-3/GT-2, 173-FD-17, 292-HYTASP-10 327-FD-33, 359-FD-39 Benoit, T., 16-AFM-2 Blom, H., 313-ATIO-23 359-FD-39 Brune, A., 183-TP-11, 217-HYTASP-7 Canepa, E., 360-AA-48 Benton, S., 269-APA-40 Bobenrieth Miserda, R., 261-AA-23 Bowles, R., 126-ASE-8/AFM-9/FT-3 Brunet, A., 138-HYTASP-5 Canetta, C., 185-TP-13, 364-TP-26 Beran, P., 355-FD-35 Bockhorn, H., 127-AA-8 Boyce, R., 24-FD-4, 65-PDL-4, 138-HYTASP-5, Brunet, V., 190-APA-31 Canfield, R., 12-MAO-2, 244-MAO-11 Berend, N., 278-MAO-12 Bocquier, M., 298-AA-33 213-HYTASP-6, 331-HYTASP-13 Bryan, B., 124-AA-7 Cansler, E., 12-MAO-2 Beresh, S., 48-FD-5, 177-AMT-9/GT-7, Bodard, G., 282-AA-26 Boyd, I., 32-TP-1, 183-TP-11, 265-TP-17, 27-FD-33 Bryson, D., 130-ITAR-2, 207-AA-17 Cantu, L., 137-AMT-6/GT-5 280-APA-44, 293-FD-30 Boden, H., 264-AA-24, 334-AA-40 Boyle, D., 295-AA-32 Bucari, M., 200-ANERS-1 Capizzano, F., 103-PDL-8, 308-APA-46 Berg, J., 345-ATIO-26 Bodony, D., 14-FD-1, 25-FC-2, 48-FD-5, 163-FD-14, Boylston, B., 208-HYTASP-24 Buchholz, H., 321-AA-36 Capps, A., 8-ATIO-1 Bergeron, K., 210-FD-19, 236-APA-35 256-FD-24, 361-AA-49 Bozak, R., 248-AA-18, 252-AA-20 Buchta, D., 323-AA-38 Caprile, J., 321-AA-36 Berguin, S., 45-MAO-3 Boehrk, H., 183-TP-11 Bragg, M., 166-ASE-9, 289-FD-27 Buehler, S., 206-AA-16 Capriotti, D., 292-HYTASP-10 Bermejo-Moreno, I., 55-FD-6 Boelens, O., 37-APA-7 Brambley, E., 123-AA-6 Buescher, A., 285-AA-28 Caraballo, E., 135-FC-8/APA-24 Bernal, L., 246-APA-39 Bogey, C., 164-AA-10 Brandis, A., 103-PDL-8, 183-TP-11, 265-TP-17 Bull, J., 317-APA-50, 326-FD-32 Caradonna, F., 322-AA-37 Bernardini, A., 51-AFM-5 Boij, S., 264-AA-24 Brandon, J., 144-AFM-12, 158-FT-4 Bulman, M., 58-HYTASP-1, 331-HYTASP-13 Cardullo, F., 95-MST-3 Author/Session Chair Index Carinhana, D., 140-AMT-7/PDL-10 Chen, G., 337-TP-23 Cliatt, L., 78-APA-15 Cristofolini, A., 181-PDL-6/FC-6, 189-APA-30 De Grazia, D., 256-FD-24 Caro, S., 322-AA-37 Chen, J., 155-APA-27, 317-APA-50 Cliff, S., 38-APA-8 Croom, M., 273-ATIO-20 de la Puente, F., 207-AA-17 Carolus, T., 267-AA-25 Chen, L., 260-AMT-12/GT-11, 300-TP-20 Clifford, C., 39-APA-9/FC-4 Crossley, W., 84-ACD-4, 245-ANERS-3 De Lucca, N., 131-PDL-9 Carrigan, J., 93-AA-4 Chen, N., 83-ATIO-7, 159-ATIO-14, 279-ANERS-4 Clothier, R., 82-ATIO-6 Crowell, A., 48-FD-5 De Marco, A., 6-APA-3 Carstensen, J., 85-MAO-5 Chen, P., 259-FC-12 Clymer, A., 159-ATIO-14 Crowther, W., 79-APA-16 De Roeck, W., 264-AA-24 Carter, M., 38-APA-8, 78-APA-15 Chen, Q., 335-TP-21 Cocquerez, P., 194-BA-1 Crozier, P., 27-AMT-1/GT-1 De Roo, R., 16-AFM-2 Caruelle, B., 165-AA-11, 267-AA-25 Chen, R., 331-HYTASP-13 Coder, J., 191-APA-32 Cruden, B., 30-AMT-2/PDL-2, 142-TP-9, 265-TP-17 de Santana, L., 90-AA-3 Casalino, D., 39-APA-9/FC-4, 89-AA-2, 128-AA-9, Chen, W., 244-MAO-11, 325-FD-31, 351-AA-44, Codron, D., 30-AMT-2/PDL-2 Culliton, W., 94-AA-5 De Stefano Fumo, M., 84-ACD-4 206-AA-16, 249-AA-19, 295-AA-32, 353-AA-46 360-AA-48 Coen, P., 110-APA-20 Cummings, R., 4-APA-1, 37-APA-7, 77-APA-14, de Villers, Y., 219-PDL-12 Casper, K., 48-FD-5, 132-FD-12, 173-FD-17, 280-APA-44 Chen, X., 89-AA-2, 239-APA-38, 300-TP-20, Coennen, R., 250-ASE-14/GT-10 109-APA-19, 236-APA-35 DeAngelis, A., 106-TP-8 Casper, M., 39-APA-9/FC-4 344-ATIO-25, 352-AA-45 Cogan, B., 158-FT-4 Cunha, G., 285-AA-28 DeArmon, J., 42-ATIO-4 Cassel, K., 56-FD-7 Chen, Y., 32-TP-1, 105-TP-7, 221-TP-14 Coggin, J., 15-AFM-1 Cunning, G., 18-ASE-2 Deaton, J., 11-MAO-1 Castagnoli, A., 200-ANERS-1 Chen, Z., 99-FC-7, 212-FD-21 Cohen, J., 25-FC-2 Cunningham, K., 51-AFM-5 Debiasi, M., 339-APA-53 Castano, L., 160-ACD-7 Cheng, G., 120-MAO-8 Coirier, W., 79-APA-16, 97-PDL-7, 271-APA-42 Curran, R., 10-ACD-1, 279-ANERS-4, 313-ATIO-23, DeChant, L., 22-FD-2 Castera, P., 31-FC-3/PDL-3 Cheng, K., 9-ATIO-2 Cola, B., 185-TP-13, 364-TP-26 344-ATIO-25, 345-ATIO-26 DeCicco, A., 313-ATIO-23 Castillo-Effen, M., 159-ATIO-14 Cheng, P., 15-AFM-1, 49-AFM-3 Coleman, G., 22-FD-2 Currie, T., 204-ASE-11, 284-ASE-16 Deck, S., 190-APA-31 Castle, M., 344-ATIO-25 Cheong, C., 267-AA-25 Colin, Y., 165-AA-11, 267-AA-25 Currier, N., 291-FD-29 Decker, R., 290-FD-28 Catalano, P., 103-PDL-8, 112-APA-22 Chernyshev, I., 20-AA-1 Collewet, C., 259-FC-12, 269-APA-40 Cutler, A., 137-AMT-6/GT-5 Defoort, S., 58-HYTASP-1, 138-HYTASP-5 Catlett, M., 165-AA-11, 253-AA-21 Chiba, K., 115-ATIO-11 Collier, F., 245-ANERS-3, 302-ANERS-5 Cybyk, B., 39-APA-9/FC-4, 154-APA-26 Degrez, G., 325-FD-31 Cattafesta, L., 287-AA-30, 293-FD-30, 358-FD-38 Chin, A., 15-AFM-1 Collin, D., 168-AA-12 D’Mello, S., 84-ACD-4 Deierling, W., 53-ASE-4/FT-1, 251-ASE-15 Cattanei, A., 360-AA-48 Chitale, K., 155-APA-27 Collins, E., 52-ASE-3, 99-FC-7, 285-AA-28 Da Ronch, A., 77-APA-14, 160-ACD-7, 182-AFM-13 Deille, O., 158-FT-4 Cavalieri, A., 124-AA-7, 164-AA-10, 206-AA-16, Chitta, S., 322-AA-37 Colonius, T., 252-AA-20, 311-APA-49 da Silva, A., 167-ASE-10/FT-5 Del Rosario, R., 200-ANERS-1 286-AA-29 Chivukula, S., 236-APA-35 Conlon, A., 137-AMT-6/GT-5 da Silva, D., 289-FD-27 Delattre, G., 203-AA-15, 267-AA-25 Cavcar, M., 316-ANERS-6 Choi, C., 184-TP-12 Connelly, T., 322-AA-37 Dagrau, F., 5-APA-2 DeLaura, R., 196-ATIO-16 136 Cevik, M., 95-MST-3 Choi, S., 243-ACD-10 Conner, J., 144-AFM-12 Dahan, J., 20-AA-1 DeLaurentis, D., 21-MST-1, 199-MAO-10, 344-ATIO-25 Ceze, M., 156-APA-28 Chong, T., 349-AA-42, 351-AA-44 Conner, M., 136-AMT-5/GT-4 Dahl, M., 295-AA-32, 354-AA-47 Delfs, J., 283-AA-27, 319-AA-34, 321-AA-36, 351-AA-44 Chai, S., 38-APA-8 Choudhari, M., 20-AA-1, 132-FD-12, 169-AA-13, Conners, T., 78-APA-15 Dahlmann, K., 347-ANERS-7 Delisi, D., 126-ASE-8/AFM-9/FT-3 Chakraborty, I., 117-ACD-5, 118-ACD-6, 207-AA-17, 253-AA-21, 287-AA-30 Consiglio, M., 115-ATIO-11 Dähne, S., 84-ACD-4 Delnero, J., 214-FC-11, 272-APA-43 241-ATIO-18, 277-ACD-12 Choutapalli, I., 294-APA-45, 340-APA-54 Content, C., 270-APA-41 Dai, X., 350-AA-43 Deloach, R., 79-APA-16 Chakravarthy, S., 207-AA-17 Chow, W., 67-TP-5, 106-TP-8 Conway, M., 311-APA-49 Dale, G., 99-FC-7 DeLuca, N., 61-AMT-3/GT-2 Chamarthi, A., 198-ACD-9 Chowdhury, S., 46-MAO-4, 120-MAO-8, 199-MAO-10 Cooper, J., 198-ACD-9 Daliri, A., 47-APA-11 Delverdier, O., 158-FT-4 Chamberlain, J., 115-ATIO-11 Christensen, T., 236-APA-35 Copiello, D., 89-AA-2 Dalle, D., 272-APA-43 Delville, J., 59-FC-5 Chan, C., 337-TP-23 Christophe, J., 165-AA-11 Coppin, J., 37-APA-7 Dalton, C., 141-AFM-11 Demel, D., 339-APA-53 Chan, D., 112-APA-22 Christou, A., 64-PDL-5 Corman, J., 315-MAO-14 Daly, C., 253-AA-21 Dement, D., 190-APA-31 Chan, W., 339-APA-53 Chudnovsky, Y., 33-TP-2 Correale, G., 31-FC-3/PDL-3 Damodaran, M., 26-APA-6, 79-APA-16 Demers Bouchard, E., 274-DE-1 Chandran, P., 241-ATIO-18 Chung, H., 15-AFM-1 Corrigan, A., 127-AA-8, 164-AA-10, 168-AA-12 Dancila, B., 83-ATIO-7 Demetriou, M., 25-FC-2 Chang, M., 294-APA-45 Chung, W., 54-MST-2 Cosic, B., 319-AA-34 Danehy, P., 61-AMT-3/GT-2, 100-AMT-4/GT-3, 1 Denayer, H., 264-AA-24 Chao, H., 174-MST-4 Chynoweth, B., 173-FD-17 Costello, M., 141-AFM-11, 174-MST-4 36-AMT-5/GT-4, 137-AMT-6/GT-5, 176-AMT-8/GT-6 Deng, S., 154-APA-26 Chaplin, R., 201-APA-34 Cicala, M., 238-APA-37 Cotoni, V., 322-AA-37 Daniels, T., 53-ASE-4/FT-1, 205-ASE-12 Deng, Y., 155-APA-27 Chargy, C., 27-AMT-1/GT-1 Çimen, T., 21-MST-1 Cotoros, I., 364-TP-26 Dantsker, O., 154-APA-26 Denis, R., 249-AA-19 Charron, F., 274-DE-1 Cinar, G., 197-ACD-8 Cotting, M., 50-AFM-4, 51-AFM-5 Darbandi, M., 105-TP-7 Denis, W., 321-AA-36 Chatterjee, A., 353-AA-46 Cinnella, P., 190-APA-31, 270-APA-41 Counts, M., 259-FC-12 Darbyshire, O., 89-AA-2 Denissen, K., 192-APA-33, 280-APA-44 Chaube, A., 33-TP-2 Cinquegrana, D., 103-PDL-8 Coupland, J., 123-AA-6, 285-AA-28, 324-AA-39 Daskilewicz, M., 44-ACD-3, 119-MAO-7 Denman, Z., 65-PDL-4, 262-HYTASP-9 Chaudhuri, A., 86-MAO-6, 120-MAO-8 Ciobaca, V., 112-APA-22 Courty, J., 158-FT-4 David, F., 282-AA-26 Denney, R., 316-ANERS-6 Chauvin, A., 350-AA-43 Citriniti, T., 159-ATIO-14 Coutty, B., 123-AA-6 Davidson, L., 239-APA-38 Desaulnier, R., 348-APA-57 Chauvin, R., 17-ASE-1, 52-ASE-3 Clair, V., 123-AA-6 Cowart, R., 110-APA-20 Davidson, P., 339-APA-53 Deshmukh, A., 82-ATIO-6, 115-ATIO-11, 196-ATIO-16 Chazot, O., 32-TP-1, 154-APA-26, 211-FD-20 Clark, E., 355-FD-35 Cox, K., 82-ATIO-6 Davidson, T., 357-FD-37 Deshmukh, R., 48-FD-5 Cheaito, R., 364-TP-26 Clark, G., 84-ACD-4 Crawford, B., 260-AMT-12/GT-11 Davis, I., 354-AA-47 Deshpande, P., 87-APA-18, 246-APA-39 Chelliah, H., 137-AMT-6/GT-5 Clark, I., 107-AFM-8, 253-AA-21 Crawley, M., 93-AA-4 Davoine, C., 262-HYTASP-9 Desjardins, O., 163-FD-14 Chelliah, K., 288-AA-31 Clarke, S., 157-ATIO-13 Creagh, M., 138-HYTASP-5 Davuluri, R., 66-TP-4 Desmet, W., 90-AA-3, 264-AA-24 Chen, B., 98-HYTASP-2, 335-TP-21 Clemens, N., 259-FC-12 Creedon, J., 114-ATIO-10, 345-ATIO-26 Davy, R., 282-AA-26 Despeyroux, A., 348-APA-57 Chen, F., 47-APA-11 Cléro, F., 282-AA-26, 286-AA-29 Creighton, A., 117-ACD-5 Dawson, R., 201-APA-34 DeSpirito, J., 201-APA-34, 280-APA-44, 348-APA-57 Author/Session Chair Index Destarac, D., 156-APA-28 Dubourg, V., 194-BA-1 Emeneth, M., 277-ACD-12 Faulkner, R., 101-HYTASP-3 Foster, T., 157-ATIO-13 Desyatnik, P., 160-ACD-7 Duda, H., 54-MST-2 Empey, D., 104-AFM-7, 221-TP-14 Faustmann, C., 360-AA-48 Fourment, C., 59-FC-5 Detandt, Y., 89-AA-2 Dudley, J., 212-FD-21, 352-AA-45 Endo, H., 17-ASE-1 Favaloro, N., 308-APA-46 François, D., 156-APA-28 Deters, R., 40-APA-10 Dufour, G., 219-PDL-12 Engelland, S., 8-ATIO-1 Fedorchenko, Y., 111-APA-21 Frank, C., 138-HYTASP-5, 277-ACD-12 Devenport, W., 27-AMT-1/GT-1, 124-AA-7, Dufrene, A., 327-FD-33 Enghardt, L., 254-AA-22, 264-AA-24, 298-AA-33, Fedorov, A., 132-FD-12 Frankel, J., 105-TP-7, 134-HYTASP-4 165-AA-11, 203-AA-15, 253-AA-21, 260-AMT-12/GT-11 Dulin, D., 317-APA-50 321-AA-36, 354-AA-47 Fehn, J., 173-FD-17 Frauholz, S., 122-FD-11 Dezitter, F., 167-ASE-10/FT-5 Dumitrache, C., 19-PDL-1 Enomoto, S., 168-AA-12 Fei, Q., 134-HYTASP-4, 292-HYTASP-10 Frede, M., 293-FD-30 Dghim, M., 214-FC-11 Duncan, G., 260-AMT-12/GT-11 Envia, E., 165-AA-11, 203-AA-15, 324-AA-39 Fei, X., 43-ACD-2 Frederick, M., 238-APA-37 Dhal, R., 42-ATIO-4 Duncan, S., 269-APA-40 Eppink, J., 172-FD-16 Feld, H., 298-AA-33 Fredericks, W., 113-ATIO-9, 240-ATIO-17 Di Stefano, D., 93-AA-4 Dunne, R., 311-APA-49 Epstein, J., 34-TP-3 Félix Patrón, R., 279-ANERS-4 Freitas, C., 353-AA-46 Dianics, J., 135-FC-8/APA-24 Duque, E., 191-APA-32 Erikson, W., 184-TP-12 Felli, M., 353-AA-46 Fresconi, F., 50-AFM-4, 141-AFM-11, 280-APA-44 Dias, J., 144-AFM-12 Duraisamy, K., 311-APA-49 Eriksson, L., 123-AA-6, 353-AA-46 Feltrop, E., 80-APA-17 Freund, J., 25-FC-2, 323-AA-38 Dickey, D., 286-AA-29 Durak, U., 54-MST-2 Ermishkin, M., 64-PDL-5 Fenbert, J., 38-APA-8, 159-ATIO-14 Friedman, A., 25-FC-2 Dicki, D., 250-ASE-14/GT-10 Durand, J., 138-HYTASP-5, 277-ACD-12 Erzberger, H., 242-ATIO-19 Feng, C., 255-FD-23 Friedrich, C., 276-ACD-11 Didion, J., 299-TP-19 Duriez, T., 59-FC-5, 286-AA-29 Escobar, J., 111-APA-21 Feng, W., 236-APA-35 Frink, N., 4-APA-1, 37-APA-7 Diebold, J., 293-FD-30 Durston, D., 38-APA-8 Espinal, D., 26-APA-6 Ferchichi, M., 214-FC-11, 339-APA-53 Friswell, M., 198-ACD-9 Dierke, J., 123-AA-6, 285-AA-28, 321-AA-36, 351-AA-44 Dutzler, G., 202-AA-14 Estrada Rodas, E., 241-ATIO-18 Ferguson, S., 12-MAO-2, 315-MAO-14, 346-MAO-15 Fruhnert, M., 314-ATIO-24 Dimitriu, D., 347-ANERS-7 Duvvuri, S., 48-FD-5, 247-FD-22 Etienne, S., 222-TP-15, 270-APA-41 Fern, L., 115-ATIO-11 Fu, S., 173-FD-17 Dimotakis, P., 281-FD-26, 326-FD-32 Duzel, U., 210-FD-19 Evain, H., 138-HYTASP-5 Fernando, J., 192-APA-33 Fugal, S., 38-APA-8 Ding, D., 337-TP-23 Dwivedi, V., 26-APA-6, 79-APA-16 Evans, B., 54-MST-2 Fernando, R., 203-AA-15 Fuggmann, S., 135-FC-8/APA-24 Diosady, L., 212-FD-21 Dzikus, N., 245-ANERS-3 Evans, E., 205-ASE-12 Ferrari, D., 336-TP-22 Fuh, C., 65-PDL-4 Dischinger, D., 250-ASE-14/GT-10 Early, J., 345-ATIO-26 Everhart, J., 27-AMT-1/GT-1 Ferrero, P., 325-FD-31 Fujii, K., 180-FC-10/PDL-11 Djidjeli, K., 88-FD-9 Eason, T., 14-FD-1 Eversman, W., 298-AA-33 Ferrier, M., 58-HYTASP-1, 138-HYTASP-5, 258-HYTASP-8 Fujishiro, I., 92-ASE-6/AFM-6/FT-2 Dobson, R., 143-TP-10 Ebrahimi, Y., 95-MST-3 Ewert, R., 123-AA-6, 252-AA-20, 285-AA-28, Feuerle, T., 92-ASE-6/AFM-6/FT-2 Fujita, K., 104-AFM-7, 142-TP-9, 183-TP-11, 137 Dogariu, A., 61-AMT-3/GT-2, 100-AMT-4/GT-3 Economon, T., 85-MAO-5, 112-APA-22, 317-APA-50 286-AA-29, 321-AA-36, 351-AA-44 Feyel, F., 184-TP-12 190-APA-31, 265-TP-17 Doherty, L., 258-HYTASP-8 Edefur, H., 131-PDL-9 Eyi, S., 210-FD-19, 318-APA-51, 330-APA-52 Fezans, N., 16-AFM-2, 144-AFM-12 Fujiwara, G., 166-ASE-9 Domercant, J., 82-ATIO-6 Edelmann, G., 220-AFM-14 Eymann, T., 23-FD-3 Fidkowski, K., 156-APA-28, 272-APA-43, 329-FD-34 Fuleki, D., 204-ASE-11, 284-ASE-16 Donbar, J., 259-FC-12 Edquist, K., 183-TP-11 Ezekoye, O., 67-TP-5 Fields, T., 215-AMT-10/GT-8 Fulge, H., 66-TP-4, 67-TP-5, 140-AMT-7/PDL-10 Dong, H., 13-APA-5/FC-1 Edwards, J., 19-PDL-1, 24-FD-4, 192-APA-33, Ezra, K., 21-MST-1 Fiévet, R., 252-AA-20 Fulton, N., 82-ATIO-6 Donjat, D., 125-ASE-7 256-FD-24, 291-FD-29 Fadhli, M., 190-APA-31 Fincham, J., 198-ACD-9 Funke, S., 288-AA-31 Donovan, B., 300-TP-20 Efraimsson, G., 20-AA-1, 264-AA-24 Fagan, A., 61-AMT-3/GT-2, 136-AMT-5/GT-4, 323-AA-38 Fink, L., 38-APA-8 Fureby, C., 131-PDL-9 Doolan, C., 89-AA-2, 254-AA-22, 349-AA-42, 350-AA-43 Eggers, T., 101-HYTASP-3 Fahringer, T., 177-AMT-9/GT-7 Finley, D., 6-APA-3 Gabard, G., 123-AA-6, 261-AA-23, 298-AA-33 Doraiswamy, S., 265-TP-17 Egorova, T., 25-FC-2 Fairfax, L., 51-AFM-5 Fiore, G., 239-APA-38 Gabbard, M., 330-APA-52 Dorfling, J., 272-APA-43 Ehlers, H., 246-APA-39 Falc, J., 310-APA-48 Fisch, G., 355-FD-35 Gadiraju, S., 335-TP-21 Doty, M., 94-AA-5, 169-AA-13 Ehlers, J., 160-ACD-7 Falcão, C., 291-FD-29 Fischenberg, D., 160-ACD-7 Gaeta, R., 287-AA-30 Dougherty, R., 254-AA-22, 288-AA-31 Eitelberg, G., 87-APA-18 Falempin, F., 58-HYTASP-1, 328-HYTASP-12 Fischer, J., 254-AA-22 Gagnon, L., 122-FD-11 Douville, T., 6-APA-3, 87-APA-18 Ekaterinaris, J., 133-FD-13 Faler, A., 64-PDL-5 Fischer, M., 298-AA-33 Gai, G., 160-ACD-7 Dowell, E., 85-MAO-5 Ekici, K., 340-APA-54, 355-FD-35 Falgoust, J., 30-AMT-2/PDL-2 Fischer, W., 101-HYTASP-3 Gaitonde, D., 180-FC-10/PDL-11 Dowling, A., 261-AA-23 Ekoule, C., 203-AA-15 Falissard, F., 203-AA-15, 267-AA-25 Fisher, T., 299-TP-19, 337-TP-23 Gallman, J., 229-LEC-6, 322-AA-37 Downing, J., 323-AA-38 El Sayed, Y., 25-FC-2, 135-FC-8/APA-24 Falk, C., 95-MST-3 Flad, D., 202-AA-14 Gallo, E., 83-ATIO-7, 137-AMT-6/GT-5 Dragonas, F., 181-PDL-6/FC-6 Elahi, M., 337-TP-23 Faranosov, G., 127-AA-8, 286-AA-29 Flattery, A., 78-APA-15 Galyen, N., 170-ITAR-3 Drake, M., 43-ACD-2 Eldogan, Y., 158-FT-4 Farbar, E., 32-TP-1 Fleury, V., 282-AA-26 Gamba, M., 296-HYTASP-11 Drela, M., 216-AMT-11/GT-9 Eldred, M., 278-MAO-12 Farcy, D., 109-APA-19 Flock, A., 258-HYTASP-8 Gampp, L., 105-TP-7 Drew, M., 116-ATIO-12 Elham, A., 279-ANERS-4 Fares, E., 128-AA-9, 214-FC-11, 295-AA-32, 355-FD-35 Florez, S., 101-HYTASP-3 Gan, J., 26-APA-6 Drochon, G., 282-AA-26 Elias, P., 31-FC-3/PDL-3 Farhat, C., 317-APA-50 Fong, E., 223-TP-16 Gand, F., 190-APA-31 Droeske, N., 292-HYTASP-10, 328-HYTASP-12 Eliasson, P., 23-FD-3 Faria, A., 355-FD-35 Forbes-Spyratos, S., 262-HYTASP-9 Gandjalikhan Nasab, S., 33-TP-2 Drye, D., 316-ANERS-6 Elliott, G., 293-FD-30 Farokhi, S., 272-APA-43 Ford, A., 41-ATIO-3 Gao, Z., 26-APA-6 Drye, R., 97-PDL-7 Elliott, M., 42-ATIO-4 Farrington, A., 256-FD-24 Ford, S., 197-ACD-8 Garbers, N., 138-HYTASP-5 Du, Y., 164-AA-10 Elmekawy, A., 122-FD-11 Faruque, I., 220-AFM-14, 241-ATIO-18 Forest, J., 253-AA-21 Garbo, A., 43-ACD-2 Duan, L., 172-FD-16, 253-AA-21 Elmiligui, A., 38-APA-8, 78-APA-15 Fasel, H., 132-FD-12, 135-FC-8/APA-24, 1 Förster, F., 134-HYTASP-4 Garcia, E., 20-AA-1, 130-ITAR-2, 170-ITAR-3, 209-ITAR-5 Duan, P., 8-ATIO-1 Elnady, T., 264-AA-24 92-APA-33, 211-FD-20 Fossati, M., 289-FD-27 Garcia Sainz, M., 214-FC-11 Duan, Z., 132-FD-12 Elsayed, E., 95-MST-3 Fasoulas, S., 67-TP-5, 140-AMT-7/PDL-10 Fosso Pouangue, A., 206-AA-16, 282-AA-26 Garcia-Magariño, A., 363-TP-25 Author/Session Chair Index Garman, K., 158-FT-4 Glaze, D., 67-TP-5 Grandin, A., 18-ASE-2, 204-ASE-11 Guo, H., 219-PDL-12 Haque, A., 195-LTA-1 Garmann, D., 26-APA-6 Glegg, S., 124-AA-7, 165-AA-11, 203-AA-15, Granlund, K., 246-APA-39, 257-FD-25 Guo, J., 314-ATIO-24 Harada, K., 213-HYTASP-6 Garmendia, D., 16-AFM-2, 118-ACD-6 253-AA-21, 351-AA-44 Grant, M., 107-AFM-8 Guo, X., 47-APA-11, 120-MAO-8 Harada, N., 180-FC-10/PDL-11 Garrard, G., 129-HYTASP-23, 208-HYTASP-24 Glezer, A., 13-APA-5/FC-1 Grasso, G., 165-AA-11 Guo, Y., 124-AA-7, 266-TP-18, 361-AA-49 Hariharan, N., 156-APA-28 Garraud, J., 58-HYTASP-1 Gloerfelt, X., 350-AA-43 Grauer, J., 144-AFM-12, 273-ATIO-20 Guo Qiang, H., 134-HYTASP-4, 292-HYTASP-10 Harker, B., 288-AA-31 Garzon, A., 238-APA-37 Gloor, M., 206-AA-16, 342-APA-56 Graveline, S., 339-APA-53 Gupta, A., 40-APA-10, 222-TP-15, 351-AA-44 Harris, J., 128-AA-9 Gaskins, J., 300-TP-20, 337-TP-23, 364-TP-26 Gnoffo, P., 327-FD-33, 359-FD-39 Graves, B., 22-FD-2 Gupta, G., 343-ACD-13 Harris, R., 285-AA-28 Gassner, G., 202-AA-14, 290-FD-28 Gobal, K., 85-MAO-5 Gray, J., 12-MAO-2 Gupta, P., 111-APA-21 Hartmann, M., 349-AA-42 Gatian, K., 44-ACD-3 Godbole, P., 41-ATIO-3 Green, L., 41-ATIO-3 Gupta, S., 19-PDL-1, 33-TP-2, 320-AA-35 Hasan, S., 42-ATIO-4, 313-ATIO-23 Gatlin, G., 87-APA-18, 154-APA-26, 269-APA-40 Goekce, S., 219-PDL-12 Greenblatt, D., 153-APA-25, 239-APA-38, 257-FD-25 Gurol, H., 176-AMT-8/GT-6 Hasegawa, M., 17-ASE-1 Gatsonis, N., 25-FC-2, 171-FD-15 Goerig, T., 203-AA-15, 249-AA-19 Greene, K., 51-AFM-5 Gurtner, M., 292-HYTASP-10, 328-HYTASP-12 Hash, D., 335-TP-21 Gaudry, E., 89-AA-2 Goetzke, E., 119-MAO-7 Greenwood, S., 195-LTA-1 Gutmark, E., 123-AA-6, 164-AA-10 Hashemi, A., 34-TP-3 Gauger, N., 135-FC-8/APA-24, 283-AA-27 Gogineni, S., 97-PDL-7, 259-FC-12 Gregory, I., 193-ATIO-15, 273-ATIO-20 Gutsche, D., 354-AA-47 Hassan, H., 50-AFM-4, 55-FD-6 Gawdiak, Y., 114-ATIO-10, 345-ATIO-26 Gogulapati, A., 48-FD-5 Gregory, J., 220-AFM-14 Guzel, G., 182-AFM-13, 291-FD-29 Hassan, M., 11-MAO-1, 316-ANERS-6 Gaynor, A., 11-MAO-1 Gokce, B., 158-FT-4 Greitzer, E., 154-APA-26, 216-AMT-11/GT-9 Ha, D., 348-APA-57 Hatakeyama, Y., 104-AFM-7 Gedeon, C., 10-ACD-1, 315-MAO-14 Gokcen, T., 221-TP-14 Grenier, R., 194-BA-1 Haas, A., 192-APA-33 Hauk, T., 68-TP-6, 284-ASE-16 Geder, J., 220-AFM-14 Gold, R., 284-ASE-16 Griendling, K., 115-ATIO-11 Haas, P., 79-APA-16 Havrilesko, B., 316-ANERS-6 Gee, K., 288-AA-31, 323-AA-38 Goldstein, D., 247-FD-22 Griffin, C., 13-APA-5/FC-1 Habashi, W., 289-FD-27 Haxter, S., 287-AA-30, 349-AA-42 Gefen, L., 353-AA-46 Golliard, J., 321-AA-36 Griffin, K., 9-ATIO-2 Habib, S., 167-ASE-10/FT-5 Hay, A., 222-TP-15, 270-APA-41 Geiselhart, K., 38-APA-8 Gollnick, V., 41-ATIO-3, 245-ANERS-3, 344-ATIO-25 Griffin, T., 250-ASE-14/GT-10 Habibi, K., 353-AA-46 Hayes, R., 346-MAO-15 Geiser, G., 127-AA-8 Goloviznin, V., 127-AA-8 Grift, E., 298-AA-33 Habing, R., 298-AA-33 Haynes, M., 42-ATIO-4 Gelbard, F., 255-FD-23 Golubev, V., 259-FC-12, 351-AA-44, 352-AA-45, Grigorie, L., 49-AFM-3 Habisreuther, P., 127-AA-8 Hazir, A., 249-AA-19 Genc, M., 213-HYTASP-6 353-AA-46 Grigoriev, R., 363-TP-25 Hack, P., 56-FD-7 He, Y., 239-APA-38 Gennaretti, M., 320-AA-35 Gomez, S., 22-FD-2, 340-APA-54 Grimm, F., 123-AA-6 Hader, C., 23-FD-3, 132-FD-12 Hearn, T., 12-MAO-2 138 George, J., 61-AMT-3/GT-2 Gong, C., 98-HYTASP-2 Grinev, K., 160-ACD-7 Haeri, S., 90-AA-3 Heath, S., 94-AA-5 Georgiadis, N., 22-FD-2 Gonzalez, D., 180-FC-10/PDL-11 Grinstead, J., 104-AFM-7 Haering, E., 78-APA-15 Heavey, K., 50-AFM-4, 280-APA-44 Gericke, T., 308-APA-46 Goodliff, S., 112-APA-22 Grizzi, S., 353-AA-46 Hafsteinsson, H., 123-AA-6, 353-AA-46 Hecker, P., 92-ASE-6/AFM-6/FT-2 German, B., 43-ACD-2, 81-ATIO-5, 119-MAO-7, Goodrich, K., 18-ASE-2, 193-ATIO-15 Groot, K., 171-FD-15 Haftka, R., 86-MAO-6, 120-MAO-8 Heeb, N., 164-AA-10 157-ATIO-13, 240-ATIO-17, 243-ACD-10, Goodwin, R., 250-ASE-14/GT-10 Gross, A., 192-APA-33 Hage, W., 288-AA-31 Heel, T., 126-ASE-8/AFM-9/FT-3 244-MAO-11, 273-ATIO-20 Goorskey, D., 97-PDL-7 Gross, J., 117-ACD-5, 193-ATIO-15 Hagen, B., 177-AMT-9/GT-7 Heim, D., 135-FC-8/APA-24 Geubelle, P., 48-FD-5 Gopalakrishna, N., 155-APA-27 Gross, M., 141-AFM-11, 174-MST-4 Hagen, G., 242-ATIO-19 Hein, S., 96-FD-10, 211-FD-20 Geuns, R., 219-PDL-12 Gopalakrishnan, P., 206-AA-16 Grossir, G., 211-FD-20 Haggerty, J., 18-ASE-2 Heinrich, L., 84-ACD-4 Geurts, K., 25-FC-2 Gopalan, J., 134-HYTASP-4 Ground, C., 262-HYTASP-9, 328-HYTASP-12 Hagiwara, H., 181-PDL-6/FC-6 Heinz, S., 355-FD-35 Geyer, T., 283-AA-27 Gopalarathnam, A., 192-APA-33 Grove, J., 293-FD-30 Haidn, O., 292-HYTASP-10, 328-HYTASP-12 Heinze, W., 43-ACD-2 Ghafourizadeh, M., 105-TP-7 Gorbushin, A., 20-AA-1 Gruber, M., 170-ITAR-3 Hain, R., 237-APA-36 Heitmann, D., 96-FD-10 Ghasemi, E., 67-TP-5, 335-TP-21 Gord, J., 61-AMT-3/GT-2, 136-AMT-5/GT-4 Gu, L., 98-HYTASP-2 Hainsworth, J., 201-APA-34 Heitmeier, F., 153-APA-25 Ghatas, R., 115-ATIO-11 Gordeyev, S., 97-PDL-7, 131-PDL-9, 259-FC-12 Gu, Q., 60-ATIO-8 Hajj, M., 243-ACD-10 Heitzman, N., 344-ATIO-25 Ghoreyshi, M., 37-APA-7, 77-APA-14, 236-APA-35 Gordiz, K., 185-TP-13, 364-TP-26 Gu, Y., 174-MST-4 Hall, E., 93-AA-4 Helber, B., 32-TP-1 Ghosh, S., 6-APA-3, 44-ACD-3, 244-MAO-11 Gorecki, T., 343-ACD-13 Guan, Y., 351-AA-44 Hall, N., 160-ACD-7 Helffer, E., 158-FT-4 Gibbons, W., 251-ASE-15 Gosse, R., 14-FD-1, 103-PDL-8 Guédeney, T., 320-AA-35 Hall, Z., 79-APA-16, 309-APA-47 Hellman, B., 209-ITAR-5 Gibson, A., 157-ATIO-13 Göttlich, E., 153-APA-25, 360-AA-48 Guelhan, A., 221-TP-14, 258-HYTASP-8, 310-APA-48 Halpin, K., 41-ATIO-3 Helm, C., 348-APA-57 Gibson, G., 292-HYTASP-10 Goyne, C., 101-HYTASP-3, 137-AMT-6/GT-5 Guenthoer, B., 259-FC-12, 353-AA-46 Ham, F., 164-AA-10 Heltsley, F., 61-AMT-3/GT-2 Giepman, R., 357-FD-37 Grabbe, S., 196-ATIO-16 Guerin, S., 261-AA-23, 298-AA-33 Hamlington, P., 281-FD-26 Hemm, R., 114-ATIO-10, 345-ATIO-26 Gikadi, J., 322-AA-37 Grabinger, J., 202-AA-14 Guest, J., 11-MAO-1, 85-MAO-5 Hammock, G., 176-AMT-8/GT-6 Henderson, B., 168-AA-12 Gilkey, L., 340-APA-54 Grace, S., 261-AA-23 Guglielmo, J., 339-APA-53 Han, H., 308-APA-46 Hendrick, P., 84-ACD-4 Gill, J., 90-AA-3, 165-AA-11, 352-AA-45 Grafton, S., 273-ATIO-20 Guglieri, G., 51-AFM-5 Han, Y., 125-ASE-7 Henfling, J., 48-FD-5, 177-AMT-9/GT-7, 280-APA-44, Gilson, J., 295-AA-32 Graham, T., 159-ATIO-14 Guimarães, A., 140-AMT-7/PDL-10 Hancock, B., 46-MAO-4 293-FD-30 Ginn, J., 107-AFM-8, 299-TP-19 Grahn, J., 337-TP-23 Gujar, P., 111-APA-21 Hannemann, K., 296-HYTASP-11 Henriksson, M., 131-PDL-9 Ginn, S., 157-ATIO-13 Grainger, A., 331-HYTASP-13 Gül, M., 39-APA-9/FC-4 Hannon, J., 128-AA-9 Henry, A., 106-TP-8, 185-TP-13, 337-TP-23, 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Holst, K., 129-HYTASP-23 Huet, M., 168-AA-12 Jackson, A., 170-ITAR-3 Jones, A., 294-APA-45, 308-APA-46, 339-APA-53 Karabasov, S., 89-AA-2, 127-AA-8 Holub, J., 119-MAO-7 Hughes, E., 167-ASE-10/FT-5 Jackson, G., 299-TP-19 Jones, G., 112-APA-22, 339-APA-53 Karban, U., 334-AA-40 Holzäpfel, F., 126-ASE-8/AFM-9/FT-3 Hul, P., 346-MAO-15 Jacob, D., 126-ASE-8/AFM-9/FT-3 Jones, K., 193-ATIO-15 Karl, S., 237-APA-36 Hong, Y., 335-TP-21 Hullah, P., 279-ANERS-4 Jacob, J., 287-AA-30 Jones, M., 295-AA-32, 333-AA-41, 361-AA-49 Karnam, A., 255-FD-23 Hongoh, M., 213-HYTASP-6 Humbert, J., 160-ACD-7, 220-AFM-14 Jacob, M., 123-AA-6 Jones, R., 120-MAO-8 Karon, A., 252-AA-20 Honnery, D., 248-AA-18 Hummel, D., 77-APA-14 Jacobs, R., 277-ACD-12 Jones, S., 137-AMT-6/GT-5 Kartha, A., 281-FD-26 Hooser, M., 176-AMT-8/GT-6 Humphreys, W., 94-AA-5, 128-AA-9 Jadhav, T., 202-AA-14 Jones, T., 78-APA-15 Kartuzova, O., 363-TP-25 Hopkins, P., 300-TP-20, 337-TP-23, 364-TP-26 Hunter, G., 9-ATIO-2 Jahn, I., 138-HYTASP-5, 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286-AA-29 Kegerise, M., 132-FD-12 Klabes, A., 164-AA-10 Kremeyer, K., 19-PDL-1, 65-PDL-4 Lakshminarayan, V., 311-APA-49 Lehner, S., 344-ATIO-25 Keimel, H., 347-ANERS-7 Kleb, W., 38-APA-8 Krishnan, G., 346-MAO-15 Lam, T., 223-TP-16 Leifsson, L., 330-APA-52 Keller, D., 286-AA-29 Klein, M., 92-ASE-6/AFM-6/FT-2 Kroehnert, A., 39-APA-9/FC-4 Lambe, A., 119-MAO-7 Leishman, J., 255-FD-23, 342-APA-56 Kelly, L., 161-MAO-9 Kleiser, L., 206-AA-16 Krotkov, N., 167-ASE-10/FT-5 Lambourne, A., 17-ASE-1 Lekki, J., 167-ASE-10/FT-5 Kennedy, G., 119-MAO-7, 199-MAO-10, 346-MAO-15 Klesa, J., 309-APA-47 Krozel, J., 53-ASE-4/FT-1 Lampinen, M., 356-FD-36 Lele, S., 55-FD-6, 164-AA-10, 283-AA-27, 319-AA-34, Kennedy, J., 321-AA-36 Kliment, L., 271-APA-42 Krueger, W., 42-ATIO-4 Landolt, S., 18-ASE-2 352-AA-45, 358-FD-38 Kennedy, K., 201-APA-34 Kline, H., 331-HYTASP-13 Kruep, J., 21-MST-1 Landry, R., 242-ATIO-19 Lemke, O., 288-AA-31, 354-AA-47 Kennett, D., 37-APA-7 Kloesel, K., 157-ATIO-13 Kryukov, I., 176-AMT-8/GT-6 Landry, S., 116-ATIO-12 Lemmens, Y., 16-AFM-2 Kenway, G., 12-MAO-2, 199-MAO-10, 346-MAO-15 Knapp, B., 113-ATIO-9 Kucukcoskun, K., 298-AA-33, 334-AA-40 Langener, T., 238-APA-37 Lemoyne, R., 213-HYTASP-6 Keogh, R., 157-ATIO-13 Knezevici, D., 204-ASE-11 Kuehl, J., 211-FD-20 Languille, V., 165-AA-11 Lempert, W., 30-AMT-2/PDL-2 Kerho, M., 51-AFM-5 Knisely, N., 82-ATIO-6 Kuehme, D., 158-FT-4 Lani, A., 64-PDL-5 Leonard, N., 43-ACD-2 Kernemp, I., 282-AA-26 Kniskern, M., 258-HYTASP-8 Kuehner, J., 137-AMT-6/GT-5 Lara, C., 111-APA-21 Leonard, R., 313-ATIO-23 Ketchen, D., 176-AMT-8/GT-6 Knobloch, K., 354-AA-47 Kuenn, A., 271-APA-42 Larsson, J., 290-FD-28, 358-FD-38 Leplat, G., 184-TP-12 Keye, S., 238-APA-37 Kobayashi, H., 213-HYTASP-6 Kuester, M., 247-FD-22 Larusson, R., 353-AA-46 Leroux, M., 203-AA-15 Keyhani, M., 105-TP-7 Kobayashi, R., 308-APA-46 Kühhorn, A., 106-TP-8 Latz, J., 272-APA-43, 318-APA-51 Leseman, Z., 337-TP-23 Khakpour, Y., 143-TP-10 Kobus, C., 183-TP-11, 265-TP-17 Kühnel, W., 202-AA-14 Laughlin, B., 197-ACD-8 Letan, R., 68-TP-6, 223-TP-16 Khalid, A., 274-DE-1 Koc, I., 158-FT-4 Kulatilaka, W., 61-AMT-3/GT-2 Laurence, S., 296-HYTASP-11 Leung-Tack, A., 320-AA-35 Khan, O., 68-TP-6, 356-FD-36 Kocheemoolayil, J., 319-AA-34, 352-AA-45 Kulkarni, D., 9-ATIO-2, 159-ATIO-14 Laurentie, J., 59-FC-5 Levesque, D., 194-BA-1 140 Khan, W., 68-TP-6 Kocian, T., 211-FD-20 Kulkarni, M., 12-MAO-2 Lautman, R., 239-APA-38 Levin, D., 34-TP-3, 185-TP-13, 222-TP-15, 325-FD-31 Khare, P., 255-FD-23 Kodera, M., 98-HYTASP-2 Kumar, A., 294-APA-45 Laux, C., 31-FC-3/PDL-3, 66-TP-4 LeVine, M., 95-MST-3, 200-ANERS-1, 315-MAO-14 Khavaran, A., 353-AA-46 Koeglmeier, S., 358-FD-38 Kumar, P., 25-FC-2, 274-DE-1 Lavin, T., 50-AFM-4, 104-AFM-7 Levitt, I., 344-ATIO-25 Khieu, L., 329-FD-34 Koelker, K., 313-ATIO-23 Kumar, R., 236-APA-35 Lavoie, M., 274-DE-1 Levy, W., 277-ACD-12 Khondge, A., 202-AA-14 Koenig, B., 214-FC-11, 355-FD-35 Kumar, S., 300-TP-20 Lavoie, P., 136-AMT-5/GT-4, 219-PDL-12 Lew, P., 206-AA-16, 353-AA-46 Khorrami, M., 128-AA-9 Koenig, M., 168-AA-12, 282-AA-26 Kumar, V., 42-ATIO-4, 82-ATIO-6 Lay, J., 135-FC-8/APA-24 Lewe, J., 241-ATIO-18, 344-ATIO-25, 345-ATIO-26, Khosravi, S., 45-MAO-3 Koh, S., 283-AA-27 Kumar Bonthu, S., 257-FD-25 Lazatin, J., 82-ATIO-6 347-ANERS-7 Kidd, F., 176-AMT-8/GT-6 Koizumi, H., 19-PDL-1 Kundu, R., 284-ASE-16 Le Garrec, T., 123-AA-6 Lewis, D., 296-HYTASP-11 Kiehl, O., 245-ANERS-3 Kok, M., 158-FT-4 Kuntner, N., 65-PDL-4 Le Goff, V., 123-AA-6 Lewis, J., 205-ASE-12 Kiflemariam, R., 33-TP-2, 299-TP-19, 363-TP-25 Koklu, M., 99-FC-7 Kuntz, D., 32-TP-1, 66-TP-4 Le Naour, B., 262-HYTASP-9 Lewis, M., 180-FC-10/PDL-11 Kihm, K., 184-TP-12 Kolb, A., 285-AA-28 Kunz, D., 51-AFM-5 Le Rallic, M., 286-AA-29 Lewis, T., 42-ATIO-4 Kim, G., 257-FD-25 Kolonay, R., 45-MAO-3, 46-MAO-4 Kunz, R., 52-ASE-3 Le Riche, R., 278-MAO-12 Léwy, S., 295-AA-32 Kim, H., 199-MAO-10 Komives, J., 96-FD-10 Kuo, C., 127-AA-8, 323-AA-38 Le Roy, J., 109-APA-19 Leyland, P., 219-PDL-12 Kim, I., 289-FD-27 Komurasaki, K., 19-PDL-1 Kupfer, M., 116-ATIO-12 Lebofsky, S., 121-APA-23 Leyva, I., 132-FD-12 Kim, J., 90-AA-3, 205-ASE-12, 265-TP-17, 351-AA-44 Komuro, T., 142-TP-9, 296-HYTASP-11 Kurbatskii, K., 353-AA-46 Lechman, J., 184-TP-12 Li, C., 13-APA-5/FC-1, 163-FD-14, 180-FC-10/PDL-11 Kim, M., 65-PDL-4, 267-AA-25 Konrath, R., 246-APA-39 Kutay, A., 144-AFM-12, 182-AFM-13 Lechniak, J., 209-ITAR-5 Li, D., 269-APA-40 Kimmel, R., 14-FD-1, 56-FD-7 Kontis, K., 219-PDL-12, 269-APA-40 Kütemeyer, M., 292-HYTASP-10 Lednicer, D., 243-ACD-10 Li, F., 132-FD-12, 221-TP-14 Kimura, S., 17-ASE-1, 91-ASE-5 Koochesfahani, M., 133-FD-13 Kuzenov, V., 19-PDL-1 Lee, C., 44-ACD-3, 244-MAO-11 Li, G., 40-APA-10 King, J., 116-ATIO-12 Kopiev, V., 20-AA-1, 127-AA-8, 286-AA-29, 287-AA-30 Kwak, D., 294-APA-45 Lee, D., 243-ACD-10 Li, H., 119-MAO-7 King, P., 204-ASE-11 Kopp, A., 138-HYTASP-5 Kwakenat, A., 290-FD-28 Lee, J., 137-AMT-6/GT-5, 223-TP-16 Li, J., 83-ATIO-7 King, R., 112-APA-22, 132-FD-12, 172-FD-16 Koracin, D., 205-ASE-12 Kykkotis, S., 269-APA-40 Lee, P., 159-ATIO-14, 242-ATIO-19 Li, L., 335-TP-21 Kingan, M., 165-AA-11, 203-AA-15 Koreanschi, A., 79-APA-16, 317-APA-50 L’Esperance, D., 136-AMT-5/GT-4 Lee, S., 95-MST-3, 115-ATIO-11, 144-AFM-12, Li, M., 45-MAO-3 Kintea, D., 222-TP-15 Kornberg, O., 68-TP-6 Laat, J., 41-ATIO-3 166-ASE-9, 266-TP-18 Li, N., 15-AFM-1 Kinzel, E., 184-TP-12, 299-TP-19 Körner, S., 126-ASE-8/AFM-9/FT-3 Labour, D., 279-ANERS-4 Lee, W., 190-APA-31 Li, Q., 26-APA-6, 87-APA-18, 271-APA-42 Kinzel, M., 52-ASE-3 Kotov, M., 176-AMT-8/GT-6 Lacouture, E., 200-ANERS-1 Lee-Rausch, E., 111-APA-21 Li, S., 264-AA-24, 354-AA-47 Kipouros, T., 6-APA-3 Kotsonis, M., 31-FC-3/PDL-3, 355-FD-35 Lacy, D., 112-APA-22, 271-APA-42 Leenaert, C., 10-ACD-1 Li, T., 159-ATIO-14 Kirby, M., 95-MST-3, 200-ANERS-1, 245-ANERS-3, Kourtzanidis, K., 219-PDL-12 Laffay, P., 90-AA-3 Lefantzi, S., 22-FD-2 Li, W., 15-AFM-1 315-MAO-14, 316-ANERS-6 Kozak, Y., 33-TP-2 Lafferty, J., 296-HYTASP-11 Lefebvre, A., 26-APA-6, 189-APA-30 Li, X., 264-AA-24, 354-AA-47, 360-AA-48, 361-AA-49 Author/Session Chair Index Li, Y., 86-MAO-6, 101-HYTASP-3, 206-AA-16, Lockard, D., 128-AA-9, 169-AA-13, 207-AA-17, Machunze, W., 112-APA-22 Martin, A., 32-TP-1, 66-TP-4 McDonald, G., 83-ATIO-7 222-TP-15, 331-HYTASP-13, 355-FD-35 267-AA-25 MacKunis, W., 259-FC-12 Martin, L., 42-ATIO-4, 116-ATIO-12 McDonald, J., 346-MAO-15 Li, Z., 222-TP-15, 325-FD-31 Loehle, S., 66-TP-4, 67-TP-5, 140-AMT-7/PDL-10 MacLean, M., 327-FD-33, 359-FD-39 Martin, M., 30-AMT-2/PDL-2, 185-TP-13 McDonald, R., 44-ACD-3 Lian, Y., 272-APA-43 Loeser, T., 4-APA-1 MaCleod, J., 204-ASE-11, 225-ASE-13 Martin, P., 348-APA-57 McDonough, L., 15-AFM-1 Liang, J., 281-FD-26, 362-TP-24 Lofthouse, A., 77-APA-14, 236-APA-35 Maddalena, L., 57-FD-8, 217-HYTASP-7, Martin, R., 59-FC-5 McFarland, J., 362-TP-24 Liber, M., 177-AMT-9/GT-7 Logan, M., 79-APA-16 262-HYTASP-9, 303-HYTASP-22, 328-HYTASP-12 Martinelli, L., 43-ACD-2 McGaughey, A., 34-TP-3 Lieber, L., 261-AA-23, 288-AA-31 Lohr, G., 159-ATIO-14 Madden, M., 314-ATIO-24 Martinez, B., 136-AMT-5/GT-4 McGowan, A., 312-MAO-13 Liechty, D., 142-TP-9, 265-TP-17 Long, T., 86-MAO-6, 120-MAO-8 Madras Sethuraman, Y., 358-FD-38 Martinez, D., 53-ASE-4/FT-1 McGrath, B., 138-HYTASP-5, 236-APA-35 Liem, R., 86-MAO-6 Longitn, J., 335-TP-21 Magee, T., 38-APA-8, 110-APA-20 Martinez Romero, P., 310-APA-48 McGuire, P., 172-FD-16, 290-FD-28 Liersch, C., 4-APA-1 Lopes, L., 169-AA-13 Magin, T., 32-TP-1, 265-TP-17, 325-FD-31 Martinez Schramm, J., 142-TP-9 McGuire, S., 30-AMT-2/PDL-2 Lieu, M., 216-AMT-11/GT-9 Lopez, B., 142-TP-9 Magne, S., 261-AA-23 Martinez-Lera, P., 264-AA-24 Mcintyre, T., 65-PDL-4 Lim, T., 175-FC-9 Lopez, O., 111-APA-21 Magstadt, A., 39-APA-9/FC-4 Martins, J., 12-MAO-2, 86-MAO-6, 119-MAO-7, McKelvey, C., 217-HYTASP-7 Limacher, E., 192-APA-33 López, M., 317-APA-50 Mahallati, A., 204-ASE-11, 284-ASE-16 161-MAO-9, 199-MAO-10, 346-MAO-15 McKenna, T., 160-ACD-7 Limbach, C., 30-AMT-2/PDL-2, 140-AMT-7/PDL-10 Lorrain, P., 65-PDL-4 Mai, C., 173-FD-17 Marx, D., 254-AA-22 McKeon, B., 48-FD-5, 131-PDL-9, 247-FD-22, Limon Duparcmeur, F., 126-ASE-8/AFM-9/FT-3 Lorteau, M., 286-AA-29 Maita, M., 258-HYTASP-8, 296-HYTASP-11 Marx, V., 66-TP-4 311-APA-49 Lin, C., 33-TP-2, 67-TP-5, 299-TP-19, 335-TP-21, Loseille, A., 5-APA-2, 256-FD-24 Majima, R., 99-FC-7 Marynowski, T., 66-TP-4, 140-AMT-7/PDL-10 McKinney, L., 213-HYTASP-6 363-TP-25 Loth, E., 17-ASE-1 Makarov, B., 202-AA-14 Masaaki, F., 57-FD-8 McKittrick, K., 362-TP-24 Lin, J., 39-APA-9/FC-4 Lou, J., 291-FD-29 Makarov, V., 111-APA-21 Masaki, D., 213-HYTASP-6 McLaughlin, D., 127-AA-8, 286-AA-29, 323-AA-38 Lin, K., 170-ITAR-3 Loubeau, A., 78-APA-15 Makeev, A., 217-HYTASP-7 Masarati, P., 51-AFM-5, 122-FD-11 McLaughlin, T., 88-FD-9, 210-FD-19, 290-FD-28 Lin, X., 82-ATIO-6 Louie, D., 255-FD-23 Makowka, K., 292-HYTASP-10, 328-HYTASP-12 Masek, T., 9-ATIO-2, 42-ATIO-4 McMasters, R., 336-TP-22 Lin, Y., 157-ATIO-13 Lowe, K., 260-AMT-12/GT-11 Malaek, S., 275-ATIO-22 Masson, P., 320-AA-35 McMonagle, R., 174-MST-4 Lin, Z., 281-FD-26 Lozano, B., 241-ATIO-18 Maldonado, V., 46-MAO-4 Mat Ali, M., 349-AA-42 McMullan, W., 293-FD-30 Lind, R., 182-AFM-13 Lu, Z., 192-APA-33 Malen, J., 34-TP-3, 185-TP-13 Mateescu, D., 7-APA-4 McNally, D., 159-ATIO-14 Lindau, J., 52-ASE-3 Lucariello, D., 84-ACD-4 Malpress, R., 331-HYTASP-13 Mateos, J., 337-TP-23 McNamara, J., 48-FD-5 141 Lindermeir, E., 237-APA-36 Luciano, R., 348-APA-57 Mance, J., 136-AMT-5/GT-4 Matheou, G., 326-FD-32 McNamara, P., 27-AMT-1/GT-1 Lindsley, N., 330-APA-52 Luckner, R., 92-ASE-6/AFM-6/FT-2 Mancini, A., 93-AA-4 Matisheck, J., 238-APA-37 McRoberts, R., 345-ATIO-26 Linke, F., 159-ATIO-14 Ludescher, T., 212-FD-21 Mancuso, R., 154-APA-26 Matsuyama, S., 183-TP-11, 190-APA-31 Meador, M., 219-PDL-12 Lino Da Silva, M., 142-TP-9 Luhar, M., 48-FD-5 Mangalam, A., 49-AFM-3 Matthews, M., 196-ATIO-16 Mechentel, F., 138-HYTASP-5 Lipinski, W., 105-TP-7 Lukaczyk, T., 110-APA-20 Mange, R., 113-ATIO-9, 343-ACD-13 Mattingly, J., 286-AA-29 Meckstroth, C., 330-APA-52 Lippitz, N., 283-AA-27 Luke, E., 52-ASE-3, 285-AA-28 Mankbadi, M., 22-FD-2 Mattson, C., 12-MAO-2, 46-MAO-4 Medeiros, F., 291-FD-29 Little, J., 59-FC-5, 135-FC-8/APA-24, 201-APA-34 Lummer, M., 43-ACD-2 Mankbadi, R., 352-AA-45, 353-AA-46 Maugars, B., 270-APA-41 Medida, S., 80-APA-17 Liu, C., 270-APA-41 Lundberg, W., 316-ANERS-6 Mann, A., 295-AA-32 Mavris, D., 6-APA-3, 10-ACD-1, 11-MAO-1, 15-AFM-1, Medwell, P., 89-AA-2 Liu, F., 168-AA-12 Luo, H., 40-APA-10, 122-FD-11, 291-FD-29, 329-FD-34 Manoha, E., 285-AA-28 16-AFM-2, 44-ACD-3, 45-MAO-3, 46-MAO-4, Mee, D., 258-HYTASP-8 Liu, G., 172-FD-16 Luo, L., 291-FD-29 Manosalvas, D., 112-APA-22 82-ATIO-6, 95-MST-3, 115-ATIO-11, 117-ACD-5, Mehmani, A., 120-MAO-8, 199-MAO-10 Liu, H., 47-APA-11, 350-AA-43 Lütjens, K., 41-ATIO-3, 313-ATIO-23 Mansour, N., 32-TP-1 118-ACD-6, 197-ACD-8, 200-ANERS-1, Mehta, N., 185-TP-13 Liu, J., 127-AA-8, 164-AA-10, 168-AA-12, 170-ITAR-3, Lutz, T., 352-AA-45 Mansur, G., 272-APA-43 241-ATIO-18, 244-MAO-11, 245-ANERS-3, Meindl, A., 140-AMT-7/PDL-10 173-FD-17 Luxhoj, J., 82-ATIO-6 Marais, K., 275-ATIO-22 76-ACD-11, 277-ACD-12, 315-MAO-14, Meinke, M., 212-FD-21, 283-AA-27 Liu, L., 86-MAO-6, 120-MAO-8 Lv, W., 185-TP-13, 364-TP-26 Marañon, J., 214-FC-11, 272-APA-43 316-ANERS-6, 344-ATIO-25, 345-ATIO-26, Meisel, N., 11-MAO-1 Liu, M., 10-ACD-1, 278-MAO-12 Lyapunov, S., 270-APA-41 Marconi, F., 38-APA-8 347-ANERS-7 Mele, B., 112-APA-22 Liu, P., 192-APA-33 Lynn, K., 215-AMT-10/GT-8 Margnat, F., 350-AA-43 May, G., 212-FD-21 Melnick, M., 247-FD-22 Liu, S., 110-APA-20 Lyrintzis, A., 202-AA-14, 353-AA-46 Marineau, E., 296-HYTASP-11 Mayo, J., 300-TP-20, 364-TP-26 Meloy, J., 216-AMT-11/GT-9 Liu, X., 34-TP-3, 333-AA-41 Lyu, B., 351-AA-44 Marini, M., 238-APA-37 Mazaheri, A., 23-FD-3, 66-TP-4 Mendonca, F., 257-FD-25, 322-AA-37 Liu, Y., 91-ASE-5, 325-FD-31, 340-APA-54 Lyu, Z., 161-MAO-9, 346-MAO-15 Maris, J., 42-ATIO-4, 83-ATIO-7 Mazzocut Zecchin, F., 360-AA-48 Mengaldo, G., 256-FD-24 Liu, Z., 122-FD-11, 266-TP-18, 362-TP-24 Ma, H., 266-TP-18 Marks, C., 130-ITAR-2, 207-AA-17, 351-AA-44 McAdaragh, R., 115-ATIO-11 Menier, V., 256-FD-24 Livingston, D., 95-MST-3 Ma, J., 99-FC-7 Marn, A., 153-APA-25, 360-AA-48 McAlpine, A., 261-AA-23 Meon, C., 90-AA-3 Livne, E., 121-APA-23 Ma, Y., 68-TP-6, 223-TP-16 Marner, W., 105-TP-7 McCabe, G., 18-ASE-2 Mercer, J., 116-ATIO-12, 242-ATIO-19 Lizanich, P., 250-ASE-14/GT-10 MacDonald, M., 66-TP-4 Marotta, E., 33-TP-2 McCarthy, P., 299-TP-19 Mercurio, U., 84-ACD-4 Lo, K., 269-APA-40 Mace, W., 128-AA-9 Marotta, T., 288-AA-31 McCartney, E., 290-FD-28 Meritt, R., 216-AMT-11/GT-9 Lobbia, M., 98-HYTASP-2 Mach, J., 104-AFM-7 Marquart, E., 211-FD-20 McClain, S., 91-ASE-5, 125-ASE-7 Merkle, C., 329-FD-34 Lobel, G., 350-AA-43 Machado, D., 140-AMT-7/PDL-10 Marques, S., 88-FD-9, 346-MAO-15 McComas, A., 26-APA-6, 309-APA-47 Merle, J., 204-ASE-11 Locatelli, D., 10-ACD-1 Machado, H., 223-TP-16 Marsan, A., 333-AA-41 McCrink, M., 220-AFM-14 Merlen, A., 156-APA-28 Lock, J., 159-ATIO-14 Macheret, S., 100-AMT-4/GT-3 Marsden, O., 164-AA-10, 253-AA-21 McDaniel, M., 79-APA-16, 309-APA-47 Merret, J., 277-ACD-12 Author/Session Chair Index Merrifield, J., 221-TP-14 Mockus, L., 21-MST-1 Mulfinger, D., 314-ATIO-24 Naughton, J., 39-APA-9/FC-4, 216-AMT-11/GT-9, Norris, A., 132-FD-12 Mery, F., 354-AA-47 Modena, M., 155-APA-27 Munafó, A., 325-FD-31 339-APA-53 North, S., 61-AMT-3/GT-2 Mesh, M., 48-FD-5 Moder, J., 363-TP-25 Munafò, A., 32-TP-1, 103-PDL-8 Nawaz, K., 221-TP-14, 266-TP-18 Notario, A., 316-ANERS-6 Meskine, M., 267-AA-25 Modest, M., 67-TP-5 Munakata, T., 57-FD-8 Nawroth, H., 67-TP-5, 127-AA-8 Nottebrock, B., 25-FC-2 Mesmer, B., 46-MAO-4, 119-MAO-7, 278-MAO-12 Mogavero, A., 98-HYTASP-2, 213-HYTASP-6 Munday, P., 189-APA-30 Nayani, S., 78-APA-15 Nourgaliev, R., 329-FD-34 Messac, A., 120-MAO-8, 199-MAO-10 Moitra, A., 111-APA-21, 339-APA-53 Mundt, C., 137-AMT-6/GT-5, 184-TP-12 Nayeri, C., 153-APA-25, 257-FD-25 Nouri, B., 106-TP-8 Meyer, M., 112-APA-22 Molder, S., 331-HYTASP-13 Mungal, G., 296-HYTASP-11 Neale, T., 131-PDL-9 Noyes, E., 104-AFM-7 Meyer, T., 136-AMT-5/GT-4 Monastero, M., 166-ASE-9 Munoz, C., 115-ATIO-11, 242-ATIO-19 Neeb, D., 221-TP-14 Nysetvold, T., 46-MAO-4 Meyers, T., 124-AA-7 Mongeau, L., 326-FD-32, 353-AA-46 Munoz, F., 211-FD-20 Neece, R., 53-ASE-4/FT-1 O’Brien, D., 154-APA-26 Miake-Lye, R., 316-ANERS-6 Moore, J., 212-FD-21 Munz, C., 202-AA-14, 290-FD-28 Neergaard, L., 84-ACD-4 O’Brien, E., 34-TP-3 Mian, H., 340-APA-54 Moore, K., 12-MAO-2 Muppidi, S., 32-TP-1, 271-APA-42 Neifeld, A., 285-AA-28, 286-AA-29 O’Brien, T., 292-HYTASP-10 Mian, Z., 194-BA-1, 195-LTA-1, 197-ACD-8 Moore, M., 113-ATIO-9, 114-ATIO-10, 157-ATIO-13, Murayama, M., 20-AA-1, 111-APA-21 Neilsen, T., 288-AA-31, 323-AA-38 O’Neal, A., 273-ATIO-20 Miao, S., 89-AA-2 240-ATIO-17 Murman, S., 55-FD-6, 136-AMT-5/GT-4, 212-FD-21, Neitzel, K., 265-TP-17 O’Reilly, C., 20-AA-1 Michael, J., 61-AMT-3/GT-2, 100-AMT-4/GT-3 Moosavi, R., 33-TP-2, 299-TP-19, 363-TP-25 342-APA-56 Nelson, C., 110-APA-20, 121-APA-23 Obayashi, S., 92-ASE-6/AFM-6/FT-2 Michel, B., 270-APA-41 Mor, M., 121-APA-23 Murphy, P., 51-AFM-5, 154-APA-26, 273-ATIO-20 Nelson, E., 251-ASE-15 Ocker, J., 349-AA-42 Michel, U., 93-AA-4 Mora Sanchez, P., 123-AA-6 Murray, J., 18-ASE-2, 167-ASE-10/FT-5, 239-APA-38, Nemili, A., 135-FC-8/APA-24 Ocokoljic, G., 310-APA-48 Micheli, F., 125-ASE-7 Moradian, N., 331-HYTASP-13 251-ASE-15 Nepak, A., 6-APA-3 Oerlemans, S., 319-AA-34 Michelis, T., 355-FD-35 Morandini, M., 122-FD-11 Murrieta Mendoza, A., 279-ANERS-4 Neretti, G., 181-PDL-6/FC-6, 189-APA-30 Ofosu, J., 19-PDL-1 Miguel, E., 353-AA-46 Morando, A., 159-ATIO-14 Mutuel, L., 92-ASE-6/AFM-6/FT-2 Neuhart, D., 128-AA-9 Ogata, S., 181-PDL-6/FC-6 Mikkelsen, C., 201-APA-34 Moraru, G., 296-HYTASP-11 Myers, L., 323-AA-38 Neville, A., 325-FD-31 Ogawa, H., 98-HYTASP-2 Miklosovic, D., 214-FC-11 Moreau, A., 261-AA-23 Na, W., 264-AA-24 Newman, B., 51-AFM-5 Ogino, Y., 142-TP-9 Miles, R., 30-AMT-2/PDL-2, 61-AMT-3/GT-2, Moreau, D., 254-AA-22, 349-AA-42, 350-AA-43 Nabawy, M., 79-APA-16 Newman, J., 270-APA-41 Ogus, G., 334-AA-40 100-AMT-4/GT-3, 140-AMT-7/PDL-10 Moreau, S., 90-AA-3, 206-AA-16, 261-AA-23, Nadarajah, S., 318-APA-51 Newman, T., 261-AA-23 Ohira, K., 294-APA-45 Milholen, W., 112-APA-22 282-AA-26, 320-AA-35, 333-AA-41, 350-AA-43 Nagaraja, S., 65-PDL-4 Newton, M., 15-AFM-1 Ohnishi, N., 142-TP-9 142 Miller, J., 136-AMT-5/GT-4 Moreira, F., 270-APA-41 Naghib Lahouti, A., 219-PDL-12 Ng, H., 83-ATIO-7, 159-ATIO-14, 279-ANERS-4 Ohno, D., 135-FC-8/APA-24 Miller, N., 182-AFM-13 Morelli, E., 144-AFM-12, 209-ITAR-5 Nagle, G., 9-ATIO-2 Ng, J., 175-FC-9 Ohta, S., 115-ATIO-11 Miller, R., 130-ITAR-2 Morgan, P., 31-FC-3/PDL-3, 156-APA-28, 270-APA-41 Naguib, A., 133-FD-13 Nguyen, L., 259-FC-12, 352-AA-45 Okabe, T., 260-AMT-12/GT-11 Miller, S., 46-MAO-4, 93-AA-4 Morgan-Ruszkowski, L., 196-ATIO-16 Nair, A., 293-FD-30 Nguyen, N., 121-APA-23, 162-APA-29 Okamine, S., 308-APA-46 Miller, V., 296-HYTASP-11 Morgand, S., 109-APA-19 Najafiyazdi, A., 326-FD-32 Nichols, J., 252-AA-20 Ol, M., 79-APA-16, 246-APA-39, 308-APA-46 Mills, B., 176-AMT-8/GT-6 Morgenstern, J., 5-APA-2, 38-APA-8, 110-APA-20 Najafiyazdi, M., 326-FD-32 Nickels, A., 358-FD-38 Oliden, D., 52-ASE-3 Milluzzo, J., 342-APA-56 Morin, P., 21-MST-1 Nakakita, K., 20-AA-1 Nicolosi, F., 6-APA-3 Oliveira, A., 140-AMT-7/PDL-10 Mimani, A., 89-AA-2, 254-AA-22 Morris, P., 127-AA-8, 164-AA-10, 248-AA-18, Nakano, T., 284-ASE-16 Niedermeier, D., 160-ACD-7 Oliver, M., 204-ASE-11, 250-ASE-14/GT-10, 284-ASE-16 Mincu, D., 321-AA-36 358-FD-38 Nalci, M., 15-AFM-1 Nies, J., 339-APA-53 Olivetti, S., 123-AA-6 Mineck, R., 128-AA-9 Morris, S., 47-APA-11, 237-APA-36, 351-AA-44 Nam, T., 46-MAO-4, 117-ACD-5, 241-ATIO-18 Niesse, H., 347-ANERS-7 Olivier, H., 339-APA-53 Minervino, M., 321-AA-36 Morton, M., 203-AA-15 Nam, Y., 134-HYTASP-4 Nikam, S., 168-AA-12 Oliviero, N., 211-FD-20 Ming, X., 269-APA-40 Moser, R., 91-ASE-5 Namgoong, H., 123-AA-6, 267-AA-25 Nikishkov, Y., 217-HYTASP-7 Oliviu, S., 79-APA-16, 317-APA-50 Mingbo, S., 175-FC-9 Moss, N., 289-FD-27 Nance, D., 93-AA-4 Nikolay, B., 272-APA-43 Ollar, J., 120-MAO-8 Minisci, E., 98-HYTASP-2 Moss, R., 95-MST-3 Nangia, R., 198-ACD-9 Nikoleris, A., 242-ATIO-19 Omais, M., 267-AA-25 Minnich, A., 106-TP-8, 300-TP-20, 337-TP-23, Mößner, M., 283-AA-27 Nara, K., 310-APA-48 Nikoueeyan, P., 39-APA-9/FC-4 Omar, A., 190-APA-31, 195-LTA-1 364-TP-26 Mosson, A., 321-AA-36 Narayanan, P., 87-APA-18, 246-APA-39 Nishida, S., 213-HYTASP-6 Omran, A., 51-AFM-5 Minto, D., 176-AMT-8/GT-6 Motta, V., 340-APA-54 Narayanan, S., 90-AA-3 Nishijima, H., 190-APA-31 Ong, W., 34-TP-3 Misaka, T., 92-ASE-6/AFM-6/FT-2, Motter, M., 193-ATIO-15 Narayanarao, B., 155-APA-27 Nishikawa, H., 23-FD-3 Onofri, M., 217-HYTASP-7 126-ASE-8/AFM-9/FT-3 Moule, Y., 58-HYTASP-1, 258-HYTASP-8 Narayanaswamy, A., 34-TP-3, 185-TP-13, 300-TP-20, Nizenkov, P., 292-HYTASP-10 Onuma, T., 308-APA-46 Mitchell, D., 248-AA-18 Mouries, F., 254-AA-22 364-TP-26 Node-Langlois, T., 90-AA-3, 165-AA-11, 267-AA-25 Oorebeek, J., 214-FC-11, 269-APA-40 Mitsuo, K., 190-APA-31 Mueller, E., 115-ATIO-11 Narayanaswamy, V., 31-FC-3/PDL-3, 176-AMT-8/GT-6, Noeding, P., 142-TP-9 Oosthuizen, P., 142-TP-9, 223-TP-16, 362-TP-24 Mittal, A., 80-APA-17 Mueller, F., 291-FD-29 177-AMT-9/GT-7 Noelting, S., 295-AA-32 Ordaz, I., 38-APA-8 Mittelman, J., 286-AA-29 Mueller-Vahl, H., 153-APA-25, 257-FD-25 Nark, D., 240-ATIO-17, 295-AA-32, 333-AA-41, Noll, B., 123-AA-6 Orkwis, P., 249-AA-19, 269-APA-40 Miyazaki, T., 141-AFM-11, 222-TP-15 Muhlestein, M., 323-AA-38 360-AA-48, 361-AA-49 Nompelis, I., 66-TP-4, 96-FD-10, 291-FD-29, Orr, J., 141-AFM-11 Miyazazki, T., 260-AMT-12/GT-11 Mukherjee, A., 196-ATIO-16, 242-ATIO-19 Narkawicz, A., 115-ATIO-11, 242-ATIO-19 325-FD-31, 327-FD-33, 359-FD-39 Oseguera-Lohr, R., 159-ATIO-14 Miyoshi, Y., 348-APA-57 Mukhopadhyay, V., 118-ACD-6 Narkus-Kramer, M., 114-ATIO-10, 345-ATIO-26 Nomura, S., 142-TP-9 Oshman, Y., 25-FC-2 Mizoguchi, M., 7-APA-4, 348-APA-57 Mukkamala, Y., 6-APA-3 Narsipur, S., 192-APA-33 Nonomura, T., 180-FC-10/PDL-11, 189-APA-30 Ostoich, C., 48-FD-5 Mizukaki, T., 136-AMT-5/GT-4 Mula, S., 342-APA-56 Natarajan, M., 25-FC-2 Norde, E., 298-AA-33 Ostrikov, N., 286-AA-29 Author/Session Chair Index Osuka, T., 99-FC-7 Parrish, S., 206-AA-16, 354-AA-47 Petrosino, F., 103-PDL-8 Pott-Pollenske, M., 20-AA-1, 319-AA-34, 321-AA-36 Rahromostaqim, M., 311-APA-49 Ota, S., 308-APA-46 Parry, A., 165-AA-11, 203-AA-15 Pezzella, G., 103-PDL-8, 238-APA-37 Potturi, A., 24-FD-4 Raj, P., 243-ACD-10 Otanicar, T., 143-TP-10, 299-TP-19 Parsons, N., 325-FD-31 Pfaender, H., 245-ANERS-3, 316-ANERS-6, Powell, H., 95-MST-3 Rajashesan, A., 246-APA-39 Otero, E., 23-FD-3 Paschereit, C., 67-TP-5, 153-APA-25, 257-FD-25, 345-ATIO-26, 347-ANERS-7 Powers, R., 127-AA-8 Rajguru, A., 64-PDL-5 Otsu, H., 103-PDL-8 319-AA-34 Pfeiffer, J., 112-APA-22 Prabhu, D., 131-PDL-9, 265-TP-17, 327-FD-33, Rajnarayan, D., 45-MAO-3 Ou, K., 257-FD-25 Pascioni, K., 287-AA-30 Pfeiffer, N., 243-ACD-10 359-FD-39 Rajvanshi, D., 111-APA-21 Outtier, P., 270-APA-41 Pasco, Y., 320-AA-35 Phillips, B., 176-AMT-8/GT-6 Prakasha, P., 46-MAO-4 Rakotoarisoa, I., 254-AA-22 Owens, L., 99-FC-7, 172-FD-16 Páscoa, J., 122-FD-11 Phillips, C., 158-FT-4 Prasad, J., 284-ASE-16 Rallabhandi, S., 78-APA-15 Ozawa, H., 296-HYTASP-11 Pasiliao, C., 84-ACD-4, 112-APA-22 Phillips, T., 156-APA-28 Prasad, R., 26-APA-6 Ramachandran, R., 254-AA-22 Ozawa, T., 104-AFM-7 Pate, D., 243-ACD-10 Phinney, L., 184-TP-12, 299-TP-19 Prata, F., 167-ASE-10/FT-5 Ramamoorthy, K., 9-ATIO-2 Ozbay, A., 80-APA-17 Patel, M., 84-ACD-4 Phojanamongkolkij, N., 159-ATIO-14 Prats, X., 8-ATIO-1, 314-ATIO-24 Ramamurti, R., 127-AA-8, 168-AA-12, 220-AFM-14 Özkaya, E., 135-FC-8/APA-24 Patel, R., 46-MAO-4 Phung, K., 21-MST-1 Prax, C., 254-AA-22 Raman, G., 254-AA-22, 288-AA-31 Ozoroski, L., 38-APA-8, 78-APA-15 Patel, V., 299-TP-19 Piantanida, S., 286-AA-29 Prazenica, R., 49-AFM-3 Raman, V., 163-FD-14 Ozturk, O., 158-FT-4 Patil, M., 12-MAO-2 Pichon, R., 27-AMT-1/GT-1 Precup, N., 121-APA-23 Rambaud, P., 211-FD-20 Özyörük, Y., 254-AA-22 Patil, Y., 155-APA-27 Pidaparti, S., 362-TP-24 Preller, D., 262-HYTASP-9 Ramchandran, G., 6-APA-3 Pack Melton, L., 99-FC-7, 214-FC-11 Patnaik, S., 143-TP-10 Piellard, M., 123-AA-6 Prevot, T., 116-ATIO-12, 242-ATIO-19 Ramesh, G., 246-APA-39 Padois, T., 282-AA-26 Patrick, J., 250-ASE-14/GT-10 Pierce, F., 67-TP-5 Price, M., 345-ATIO-26 Ramos, N., 259-FC-12 Padron, A., 278-MAO-12 Patterson, M., 240-ATIO-17 Pieri, D., 167-ASE-10/FT-5 Prime, Z., 254-AA-22, 349-AA-42, 350-AA-43 Rampurawala, A., 6-APA-3 Pak, C., 15-AFM-1, 315-MAO-14 Patton, C., 55-FD-6 Pignatiello, A., 79-APA-16 Prisell, E., 123-AA-6 Ramu, A., 68-TP-6 Palacios, F., 85-MAO-5, 110-APA-20, 112-APA-22, Paukner, D., 292-HYTASP-10, 328-HYTASP-12 Pilon, A., 353-AA-46 Probst, A., 156-APA-28 Ran, H., 6-APA-3 278-MAO-12, 331-HYTASP-13 Paul, M., 97-PDL-7 Pimenta, B., 261-AA-23 Probst, F., 316-ANERS-6 Ranade, A., 41-ATIO-3 Palacios, J., 17-ASE-1, 52-ASE-3, 125-ASE-7, Paul, S., 335-TP-21 Pimentel, R., 219-PDL-12 Pröbsting, S., 7-APA-4, 351-AA-44 Rancourt, D., 44-ACD-3, 244-MAO-11, 274-DE-1 284-ASE-16 Paula, L., 270-APA-41 Pinaud, G., 101-HYTASP-3 Proctor, F., 92-ASE-6/AFM-6/FT-2, Ranjan, D., 362-TP-24 Paletta, N., 84-ACD-4 Pavolonis, M., 167-ASE-10/FT-5 Pinier, J., 47-APA-11, 340-APA-54 126-ASE-8/AFM-9/FT-3 Raps, D., 91-ASE-5 143 Palmer, E., 242-ATIO-19 Payan, A., 316-ANERS-6 Pinna, F., 171-FD-15, 211-FD-20 Protat, A., 204-ASE-11 Rarata, Z., 123-AA-6 Palmer, G., 32-TP-1 Pazmany, A., 53-ASE-4/FT-1 Pinon-Fischer, O., 82-ATIO-6, 345-ATIO-26 Pruett, B., 177-AMT-9/GT-7, 280-APA-44, 293-FD-30 Rasmussen, R., 30-AMT-2/PDL-2 Palumbo, D., 240-ATIO-17 Peake, N., 90-AA-3, 253-AA-21 Pintado-Peno, A., 282-AA-26 Pruis, M., 126-ASE-8/AFM-9/FT-3 Rasquin, M., 155-APA-27 Pan, B., 134-HYTASP-4 Pei, P., 113-ATIO-9 Piotrowski, M., 348-APA-57 Przekwas, A., 212-FD-21 Rasuo, B., 310-APA-48 Pan, C., 331-HYTASP-13 Peijin, L., 292-HYTASP-10 Piskin, T., 330-APA-52 Pu, D., 114-ATIO-10 Rath, J., 19-PDL-1 Pan, Y., 362-TP-24 Pekoz, H., 79-APA-16 Plassman, G., 94-AA-5 Pulliam, T., 191-APA-32, 342-APA-56 Rauleder, J., 255-FD-23 Panahi, A., 7-APA-4 Pelletier, D., 222-TP-15, 270-APA-41 Plemmons, D., 170-ITAR-3 Pustelnik, M., 336-TP-22 Rautmann, C., 351-AA-44 Panda, J., 137-AMT-6/GT-5 Pendenza, A., 289-FD-27 Pliavaka, K., 65-PDL-4 Putnam, Z., 104-AFM-7 Ravetta, P., 128-AA-9 Panda, R., 51-AFM-5 Pendleton, E., 315-MAO-14 Plogmann, B., 247-FD-22 Pytel, D., 105-TP-7 Ravichandran, N., 364-TP-26 Panesi, M., 64-PDL-5, 103-PDL-8, 131-PDL-9, 325-FD-31 Pendyala, R., 247-FD-22 Poehlmann, F., 61-AMT-3/GT-2 Pytka, J., 241-ATIO-18 Ravindra, K., 155-APA-27 Pankow, M., 315-MAO-14 Peng, L., 120-MAO-8 Poggie, J., 14-FD-1, 30-AMT-2/PDL-2, Qiao, L., 163-FD-14 Ray, J., 22-FD-2 Pankratov, I., 287-AA-30 Peng, S., 131-PDL-9, 189-APA-30 140-AMT-7/PDL-10, 326-FD-32, 356-FD-36 Qiao, W., 351-AA-44, 360-AA-48 Razzaqi, S., 258-HYTASP-8 Pant, R., 41-ATIO-3, 198-ACD-9 Percin, M., 154-APA-26 Polacsek, C., 123-AA-6, 285-AA-28, 295-AA-32 Qin, T., 363-TP-25 Reba, R., 295-AA-32 Pantano, C., 256-FD-24 Perebatov, V., 160-ACD-7 Polet, D., 236-APA-35 Qin, Y., 271-APA-42 Reboul, G., 295-AA-32 Paolo, S., 189-APA-30 Peres, P., 101-HYTASP-3 Polifke, W., 334-AA-40 Qiu Shi, Z., 26-APA-6 Reddy, A., 43-ACD-2 Papadimitriou, C., 318-APA-51 Perez, B., 101-HYTASP-3 Politovich, M., 18-ASE-2, 251-ASE-15 Qu, Q., 192-APA-33 Reddy, K., 134-HYTASP-4 Papadimitriou, D., 318-APA-51 Perez, R., 160-ACD-7, 200-ANERS-1 Pomeroy, B., 308-APA-46 Qu, S., 122-FD-11 Redonnet, S., 93-AA-4, 169-AA-13, 285-AA-28 Papalambros, P., 312-MAO-13 Perez-Batlle, M., 314-ATIO-24 Ponnappan, R., 14-FD-1 Quaranta, G., 51-AFM-5, 122-FD-11, 340-APA-54 Reed, D., 91-ASE-5 Papamoschou, D., 168-AA-12 Peroomian, O., 289-FD-27 Pont, G., 190-APA-31 Qureshi, H., 26-APA-6 Reed, H., 211-FD-20, 231-FD-18 Paquet, C., 203-AA-15 Perot, F., 123-AA-6, 267-AA-25, 295-AA-32 Pontelandolfo, P., 79-APA-16 Rabadan, E., 258-HYTASP-8 Reed, P., 199-MAO-10 Parchment, O., 89-AA-2 Perry, M., 214-FC-11 Poole, D., 10-ACD-1, 330-APA-52 Rabinovitch, J., 66-TP-4 Reeder, M., 177-AMT-9/GT-7, 260-AMT-12/GT-11 Pardowitz, B., 354-AA-47 Persoons, T., 177-AMT-9/GT-7 Pope, D., 169-AA-13 Radespiel, R., 96-FD-10, 156-APA-28, 173-FD-17, Reese, B., 99-FC-7 Paredes, P., 211-FD-20 Perullo, C., 46-MAO-4, 117-ACD-5 Poroseva, S., 22-FD-2, 55-FD-6, 80-APA-17, 340-APA-54 211-FD-20, 246-APA-39 Reger, R., 358-FD-38 Parente, A., 325-FD-31 Pescetelli, F., 98-HYTASP-2 Porteous, A., 80-APA-17 Raghunath, K., 244-MAO-11 Regert, T., 211-FD-20 Parezanovic, V., 59-FC-5 Peschke, P., 219-PDL-12 Porter, R., 61-AMT-3/GT-2 Rahai, H., 289-FD-27 Reich, G., 130-ITAR-2, 207-AA-17, 351-AA-44 Park, C., 115-ATIO-11, 363-TP-25 Peter, H., 335-TP-21 Posa, A., 311-APA-49 Rahimi, M., 137-AMT-6/GT-5 Reichman, B., 323-AA-38 Park, M., 5-APA-2, 38-APA-8, 111-APA-21 Petersen, J., 159-ATIO-14 Post, J., 159-ATIO-14 Rahman, M., 326-FD-32, 356-FD-36 Reimann, B., 101-HYTASP-3 Parmhed, O., 131-PDL-9 Petrone, G., 318-APA-51 Potapczuk, M., 52-ASE-3, 166-ASE-9 Rahnamoun, A., 222-TP-15 Reimann, C., 295-AA-32 Author/Session Chair Index Reimer, T., 66-TP-4, 292-HYTASP-10 Robinet, J., 190-APA-31 Saeki, H., 260-AMT-12/GT-11 Scalo, C., 358-FD-38 Seeley, B., 241-ATIO-18 Rein, M., 4-APA-1 Robinson, F., 299-TP-19 Saffari, H., 363-TP-25 Scarano, F., 351-AA-44 Segal, C., 262-HYTASP-9 Reinartz, B., 122-FD-11 Robinson III, J., 242-ATIO-19 Sagaut, P., 156-APA-28 Schaefer, M., 245-ANERS-3 Segawa, T., 181-PDL-6/FC-6 Reinhart, T., 80-APA-17 Rodi, P., 251-ASE-15, 312-MAO-13 Sahai, A., 20-AA-1, 325-FD-31 Schaeffler, N., 153-APA-25 Seidel, J., 88-FD-9, 236-APA-35 Remes, B., 154-APA-26 Rodio, J., 55-FD-6 Sahu, J., 50-AFM-4, 175-FC-9, 280-APA-44 Schaffner, P., 205-ASE-12 Seifert, A., 112-APA-22 Ren, H., 344-ATIO-25 Rodriguez Segura, D., 137-AMT-6/GT-5 Saile, D., 310-APA-48 Scheelhaase, J., 347-ANERS-7 Self, R., 206-AA-16 Ren, J., 173-FD-17 Rodriguez-Garcia, P., 349-AA-42 Sakai, M., 355-FD-35 Schery, S., 137-AMT-6/GT-5 Selic, T., 360-AA-48 Ren, L., 8-ATIO-1, 159-ATIO-14 Roe, P., 23-FD-3 Sakai, T., 99-FC-7 Schetz, J., 10-ACD-1, 15-AFM-1, 117-ACD-5, Selig, M., 40-APA-10, 154-APA-26, 239-APA-38 Ren, Q., 337-TP-23 Roe, R., 197-ACD-8 Sakaue, H., 17-ASE-1, 91-ASE-5, 141-AFM-11, 216-AMT-11/GT-9, 257-FD-25 Selvaraj, S., 134-HYTASP-4 Ren, T., 67-TP-5 Roettgen, A., 30-AMT-2/PDL-2 222-TP-15, 260-AMT-12/GT-11 Schilden, T., 96-FD-10, 173-FD-17 Semaan, R., 25-FC-2, 135-FC-8/APA-24 Ren, Y., 13-APA-5/FC-1 Roger, M., 124-AA-7, 333-AA-41, 352-AA-45 Sakaue, S., 328-HYTASP-12 Schiltgen, B., 157-ATIO-13 Semiletov, V., 89-AA-2, 127-AA-8 Rendall, T., 10-ACD-1, 330-APA-52 Rogers, J., 141-AFM-11, 174-MST-4, 182-AFM-13 Sakraker, I., 154-APA-26 Schirra, J., 271-APA-42 Senda, F., 143-TP-10 Rennie, M., 27-AMT-1/GT-1, 131-PDL-9 Rogers, M., 121-APA-23 Sakuranaka, N., 57-FD-8 Schleeh, J., 337-TP-23 Sengupta, P., 242-ATIO-19 Reppenhagen, A., 202-AA-14 Rogier, F., 219-PDL-12 Salah El Din, I., 5-APA-2 Schmidt, B., 132-FD-12 Senocak, I., 205-ASE-12 Reulet, P., 125-ASE-7 Rohl, P., 312-MAO-13 Saldívar Massimi, H., 134-HYTASP-4 Schmidt-Wimmer, S., 101-HYTASP-3 Seong, T., 134-HYTASP-4 Reuter, B., 38-APA-8 Röhle, I., 354-AA-47 Salemi, L., 211-FD-20 Schmisseur, J., 217-HYTASP-7, 325-FD-31 Sepahi Younsi, J., 47-APA-11 Reverdy, P., 43-ACD-2 Rohlf, D., 4-APA-1 Salvage, R., 195-LTA-1 Schmit, R., 177-AMT-9/GT-7, 293-FD-30 Serre, L., 138-HYTASP-5 Rexius, S., 209-ITAR-5 Rohlmann, D., 238-APA-37 Salze, E., 253-AA-21 Schneegans, A., 277-ACD-12 Sescu, A., 56-FD-7, 247-FD-22, 285-AA-28 Reyhanoglu, M., 320-AA-35 Roisman, I., 68-TP-6, 222-TP-15, 284-ASE-16 Samimy, M., 39-APA-9/FC-4, 93-AA-4, 293-FD-30 Schneider, G., 105-TP-7 Seyed-Yagoobi, J., 143-TP-10, 299-TP-19 Reynolds, K., 162-APA-29 Rokhsaz, K., 271-APA-42, 272-APA-43 Sampson, Z., 289-FD-27 Schneider, S., 173-FD-17, 211-FD-20, Shang, J., 64-PDL-5, 103-PDL-8, 131-PDL-9 Reynolds, T., 275-ATIO-22 Roling, P., 41-ATIO-3, 344-ATIO-25, 345-ATIO-26 Samuel, P., 220-AFM-14 296-HYTASP-11 Sharan, N., 256-FD-24 Reza Ahrabi, B., 270-APA-41 Romero, J., 317-APA-50 Sanchez-Gonzalez, R., 61-AMT-3/GT-2 Schnepf, C., 294-APA-45 Sharifzadeh, S., 84-ACD-4 Rhew, R., 215-AMT-10/GT-8 Rona, A., 93-AA-4 Sandberg, R., 123-AA-6 Scholz, P., 39-APA-9/FC-4, 135-FC-8/APA-24, Sharma, A., 247-FD-22, 350-AA-43 Rhudy, M., 95-MST-3, 174-MST-4 Rorie, R., 115-ATIO-11 Sander, T., 137-AMT-6/GT-5 308-APA-46 Sharma, S., 51-AFM-5, 168-AA-12, 353-AA-46 144 Ribeiro, A., 249-AA-19, 295-AA-32 Rosema, C., 271-APA-42, 280-APA-44 Sanders, L., 207-AA-17, 321-AA-36 Schram, C., 90-AA-3, 165-AA-11, 298-AA-33, 334-AA-40 Sharman, R., 53-ASE-4/FT-1, 205-ASE-12 Ricci, M., 157-ATIO-13 Rosenbaum, R., 313-ATIO-23 Sandham, N., 132-FD-12 Schrijer, F., 357-FD-37 Shaw, S., 38-APA-8 Ricci, Y., 92-ASE-6/AFM-6/FT-2 Rosine, B., 250-ASE-14/GT-10 Sanghi, S., 40-APA-10 Schroeder, J., 54-MST-2 Shay, R., 8-ATIO-1 Ricciardi, G., 222-TP-15 Rosseel, E., 89-AA-2 Sanjose, M., 90-AA-3, 206-AA-16, 261-AA-23, Schroeder, M., 41-ATIO-3 Sheets, D., 241-ATIO-18 Richardson, T., 119-MAO-7, 199-MAO-10 Rossetti, A., 189-APA-30 282-AA-26, 350-AA-43 Schroeder, W., 25-FC-2, 96-FD-10, 173-FD-17, Shen, H., 134-HYTASP-4 Richwine, D., 110-APA-20 Rossignol, K., 164-AA-10, 283-AA-27 Sanna, F., 321-AA-36 206-AA-16, 212-FD-21, 283-AA-27 Shen, N., 41-ATIO-3 Ricot, D., 156-APA-28 Roth, B., 12-MAO-2 Santos, L., 336-TP-22 Schuelein, E., 294-APA-45, 357-FD-37 Shende, N., 155-APA-27 Ricouard, J., 203-AA-15 Rothacker, B., 156-APA-28 Saraf, A., 9-ATIO-2, 41-ATIO-3 Schuette, A., 4-APA-1, 37-APA-7, 109-APA-19 Sheng, C., 56-FD-7, 210-FD-19 Riedel, U., 65-PDL-4 Rothhaar, P., 273-ATIO-20 Saric, W., 260-AMT-12/GT-11 Schuetz, J., 212-FD-21 Shepherd, J., 132-FD-12 Riehmer, J., 258-HYTASP-8 Rothmayer, A., 91-ASE-5, 135-FC-8/APA-24 Sarradj, E., 283-AA-27 Schultheis, S., 116-ATIO-12 Sherwin, S., 256-FD-24 Rienstra, S., 333-AA-41, 361-AA-49 Rotter, T., 364-TP-26 Sashittal, P., 358-FD-38 Schultz, V., 82-ATIO-6, 115-ATIO-11 Sheshadri, A., 190-APA-31, 317-APA-50 Rigby, D., 91-ASE-5, 204-ASE-11 Roux, J., 106-TP-8, 295-AA-32 Sasoh, A., 99-FC-7 Schulze, M., 292-HYTASP-10 Sheth, K., 116-ATIO-12, 159-ATIO-14 Rigby, G., 4-APA-1 Rowe, S., 274-DE-1 Sasuga, N., 308-APA-46 Schutte, J., 245-ANERS-3 Shi, R., 120-MAO-8 Riggins, B., 10-ACD-1 Roy, A., 133-FD-13 Sathre, P., 236-APA-35 Schutte, P., 193-ATIO-15 Shi, W., 26-APA-6, 87-APA-18 Righi, M., 356-FD-36 Roy, C., 156-APA-28, 291-FD-29 Sato, K., 296-HYTASP-11 Schwanekamp, T., 101-HYTASP-3 Shih, T., 67-TP-5 Rigney, S., 129-HYTASP-23 Roy, S., 42-ATIO-4, 136-AMT-5/GT-4, 219-PDL-12 Sato, M., 180-FC-10/PDL-11, 189-APA-30 Schwartz, A., 18-ASE-2 Shimamura, K., 19-PDL-1 Ringuette, T., 219-PDL-12 Roy, X., 34-TP-3 Sato, S., 57-FD-8 Schwartz, H., 243-ACD-10 Shimoyama, K., 201-APA-34 Rinoie, K., 355-FD-35 Rozenfeld, T., 33-TP-2 Satori, S., 115-ATIO-11 Schwartzentruber, T., 66-TP-4 Shiryaeva, A., 24-FD-4 Ristori, A., 58-HYTASP-1 Rudnik, R., 155-APA-27, 238-APA-37 Sattelmayer, T., 292-HYTASP-10, 322-AA-37, Schwetzler, D., 238-APA-37 Shively, R., 115-ATIO-11 Rival, D., 162-APA-29, 192-APA-33, 236-APA-35 Ruetten, M., 237-APA-36 328-HYTASP-12, 358-FD-38 Schwing, A., 291-FD-29 Shkarayev, S., 236-APA-35 Rivers, M., 310-APA-48 Ruffin, S., 190-APA-31 Sattler, S., 135-FC-8/APA-24 Sciacchitano, A., 87-APA-18 Shkurenkov, I., 30-AMT-2/PDL-2 Rizzetta, D., 56-FD-7, 180-FC-10/PDL-11 Ruleva, L., 176-AMT-8/GT-6 Sausen, R., 347-ANERS-7 Sclafani, A., 111-APA-21, 191-APA-32, 237-APA-36, Shmueli, H., 68-TP-6, 223-TP-16 Rizzi, A., 6-APA-3 Rumpfkeil, M., 161-MAO-9, 351-AA-44 Sauti, G., 219-PDL-12 317-APA-50 Shneider, M., 19-PDL-1, 100-AMT-4/GT-3 Rizzi, S., 203-AA-15, 240-ATIO-17 Rumsey, C., 22-FD-2, 111-APA-21 Savaglio, C., 21-MST-1 Scoggins, J., 265-TP-17 Shock, R., 206-AA-16 Roach, K., 196-ATIO-16 Rutherford, M., 87-APA-18 Savill, A., 6-APA-3 Scott, K., 61-AMT-3/GT-2, 136-AMT-5/GT-4 Shorstov, V., 111-APA-21 Robertson, D., 130-ITAR-2, 207-AA-17 Ryzhkov, S., 19-PDL-1 Sawada, K., 142-TP-9 Scott, R., 122-FD-11 Shorter, P., 322-AA-37 Robertson, P., 276-ACD-11 Sack, S., 298-AA-33 Saxena, S., 238-APA-37, 284-ASE-16, 348-APA-57 Séchaud, J., 215-AMT-10/GT-8 Shrestha, P., 281-FD-26 Robic, B., 10-ACD-1 Sadraey, M., 197-ACD-8 Saxton-Fox, T., 131-PDL-9 Seehof, C., 54-MST-2 Sidharth, G., 326-FD-32 Author/Session Chair Index Siebenhaar, A., 28-HYTASP-15, 35-HYTASP-16, Song, M., 350-AA-43 Stilson, E., 113-ATIO-9 Sytsma, M., 84-ACD-4, 246-APA-39 Thakur, S., 67-TP-5 62-HYTASP-17, 178-HYTASP-19, 186-HYTASP-20 Sopek, T., 65-PDL-4 Stimpson, R., 261-AA-23 Szmuk, M., 259-FC-12 Thandavamoorthy, G., 156-APA-28 Siefers, T., 210-FD-19 Sor, S., 363-TP-25 Stoellinger, M., 355-FD-35 Tabata, M., 104-AFM-7 Thangawng, A., 220-AFM-14 Sieglaff, J., 167-ASE-10/FT-5 Soria, J., 248-AA-18 Stoll, A., 113-ATIO-9, 240-ATIO-17 Tafti, D., 236-APA-35 Theiss, A., 96-FD-10, 211-FD-20 Siikonen, T., 326-FD-32, 356-FD-36 Sotiropoulos, F., 133-FD-13 Stone, J., 206-AA-16 Taghinia, J., 326-FD-32 Theofilis, V., 211-FD-20 Sijtsma, P., 288-AA-31, 319-AA-34 Soudakov, V., 132-FD-12 Storm, S., 17-ASE-1 Taguchi, H., 213-HYTASP-6 Thévenin, D., 65-PDL-4 Sikarwar, N., 127-AA-8 Soutade, J., 58-HYTASP-1 Stouffer, V., 313-ATIO-23, 345-ATIO-26 Taha, H., 243-ACD-10 Thiele, F., 135-FC-8/APA-24 Siller, H., 288-AA-31 Sovardi, C., 334-AA-40 Strangfeld, C., 257-FD-25 Taherian, S., 289-FD-27 Thipphavong, D., 313-ATIO-23 Silton, S., 13-APA-5/FC-1, 88-FD-9, 280-APA-44 Sozer, E., 5-APA-2 Strapp, J., 204-ASE-11 Tahir, R., 331-HYTASP-13 Thipphavong, J., 42-ATIO-4 Silva, C., 111-APA-21 Spalt, T., 94-AA-5 Strike, J., 39-APA-9/FC-4, 339-APA-53 Tai, J., 316-ANERS-6 Thirifay, F., 84-ACD-4 Simon, A., 79-APA-16 Sparrow, V., 110-APA-20 Strobl, T., 17-ASE-1, 91-ASE-5 Taira, K., 189-APA-30, 293-FD-30 Thisse, J., 295-AA-32 Simpson, J., 198-ACD-9 Spears, Z., 127-AA-8 Struk, P., 91-ASE-5, 204-ASE-11, 284-ASE-16 Takahashi, H., 57-FD-8 Thomas, D., 323-AA-38 Simpson, T., 46-MAO-4, 199-MAO-10 Speer, S., 55-FD-6 Stuermer, A., 309-APA-47 Takahashi, S., 92-ASE-6/AFM-6/FT-2 Thomas, G., 157-ATIO-13 Sinayoko, S., 351-AA-44 Spehr, C., 287-AA-30, 349-AA-42 Stump, G., 46-MAO-4 Takahashi, T., 10-ACD-1, 117-ACD-5, 118-ACD-6, Thomas, J., 85-MAO-5 Singh, A., 40-APA-10 Spiegel, P., 203-AA-15, 267-AA-25 Stumpf, E., 20-AA-1 241-ATIO-18, 292-HYTASP-10, 315-MAO-14, Thomason, C., 177-AMT-9/GT-7 Singh, D., 246-APA-39, 361-AA-49 Spillers, R., 48-FD-5, 177-AMT-9/GT-7, 280-APA-44, Sturdza, P., 45-MAO-3 317-APA-50, 344-ATIO-25 Thompson, D., 17-ASE-1, 52-ASE-3, 91-ASE-5, Singh, K., 15-AFM-1 293-FD-30 Stutts, J., 97-PDL-7, 271-APA-42 Takahashi, Y., 348-APA-57 247-FD-22 Singh, P., 237-APA-36 Spinder, C., 298-AA-33 Su, C., 172-FD-16 Takayanagi, H., 142-TP-9, 183-TP-11, 190-APA-31, Thompson, G., 18-ASE-2, 205-ASE-12 Singh, R., 255-FD-23, 284-ASE-16 Spitalny, M., 360-AA-48 Suarez, C., 111-APA-21 265-TP-17 Thompson, K., 50-AFM-4 Singh, S., 87-APA-18, 237-APA-36 Spottswood, S., 14-FD-1 Subbareddy, P., 281-FD-26, 325-FD-31 Takeshima, Y., 92-ASE-6/AFM-6/FT-2 Thompson, T., 245-ANERS-3, 279-ANERS-4, Singhal, A., 39-APA-9/FC-4 Sree, D., 203-AA-15 Subia, S., 222-TP-15 Talamelli, A., 189-APA-30 347-ANERS-7 Sinha, K., 358-FD-38 Sreenivas, K., 23-FD-3, 80-APA-17, 222-TP-15, Subramanian, S., 199-MAO-10 Tam, C., 164-AA-10, 170-ITAR-3, 206-AA-16, 354-AA-47 Thurow, B., 136-AMT-5/GT-4, 177-AMT-9/GT-7, Siochi, E., 219-PDL-12 291-FD-29 Suchomel, C., 107-AFM-8, 181-PDL-6/FC-6, Tam, W., 106-TP-8 247-FD-22 Sirohi, J., 342-APA-56 Sridhar, B., 9-ATIO-2, 83-ATIO-7, 159-ATIO-14, 219-PDL-12 Tamaki, Y., 352-AA-45 Tian, W., 80-APA-17 145 Sitaraman, J., 256-FD-24, 339-APA-53 196-ATIO-16, 279-ANERS-4 Suchyta, C., 357-FD-37 Tan, C., 284-ASE-16 Tibbe, T., 319-AA-34 Siu, N., 154-APA-26 Sridhar, M., 88-FD-9 Sud, V., 42-ATIO-4 Tanaka, K., 111-APA-21 Tibor, E., 46-MAO-4 Sivasubramanian, J., 211-FD-20 Staebler, T., 66-TP-4 Sudhir Kumar, B., 138-HYTASP-5 Tanaka, M., 91-ASE-5 Tien, S., 9-ATIO-2, 42-ATIO-4, 196-ATIO-16 Skokova, K., 221-TP-14 Stanek, M., 97-PDL-7 Suehiro, E., 59-FC-5 Tanba, T., 99-FC-7 Tilmann, C., 201-APA-34 Skomorokhov, S., 272-APA-43 Stanford, B., 162-APA-29 Sugai, S., 115-ATIO-11 Tandale, M., 242-ATIO-19 Timofeev, E., 331-HYTASP-13 Skoog, M., 193-ATIO-15 Stanisak, M., 92-ASE-6/AFM-6/FT-2 Sugimoto, R., 123-AA-6, 298-AA-33 Tang, C., 271-APA-42 Ting, E., 121-APA-23, 162-APA-29 Slipchenko, M., 136-AMT-5/GT-4 Stanlov, O., 249-AA-19 Suh, P., 15-AFM-1 Tang, H., 8-ATIO-1 Tinker, M., 45-MAO-3 Slotnick, J., 191-APA-32, 270-APA-41 Starikovskiy, A., 65-PDL-4 Sulaeman, E., 195-LTA-1 Tang, W., 45-MAO-3 Tinney, C., 252-AA-20, 342-APA-56 Sluis, J., 345-ATIO-26 Starkey, R., 262-HYTASP-9, 296-HYTASP-11 Sullivan, T., 135-FC-8/APA-24 Tang, Z., 345-ATIO-26 Titchener, N., 154-APA-26 Smart, M., 65-PDL-4, 258-HYTASP-8, Starzmann, R., 267-AA-25 Sultana, K., 135-FC-8/APA-24 Tanner, P., 153-APA-25 Tixier, E., 222-TP-15 262-HYTASP-9, 292-HYTASP-10 Stead, D., 94-AA-5, 169-AA-13, 207-AA-17 Sun, T., 104-AFM-7 Tanno, H., 142-TP-9, 296-HYTASP-11 Toal, D., 161-MAO-9 Smith, A., 97-PDL-7, 131-PDL-9 Steelant, J., 238-APA-37 Sun, X., 264-AA-24, 350-AA-43 Tantaroudas, N., 160-ACD-7 Tobin, E., 158-FT-4 Smith, B., 22-FD-2, 177-AMT-9/GT-7 Steen, M., 92-ASE-6/AFM-6/FT-2 Sun, Y., 293-FD-30 Tanvir, S., 163-FD-14 Tognaccini, R., 112-APA-22 Smith, D., 39-APA-9/FC-4 Steger, M., 286-AA-29 Sun, Z., 88-FD-9 Tapken, U., 354-AA-47 Toker, K., 213-HYTASP-6 Smith, J., 313-ATIO-23 Steglinski, M., 51-AFM-5 Sunada, Y., 355-FD-35 Taubert, L., 59-FC-5, 135-FC-8/APA-24 Tokuno, H., 349-AA-42 Smith, K., 82-ATIO-6, 281-FD-26, 299-TP-19 Steiner, M., 153-APA-25, 251-ASE-15 Sundaramoorthy, B., 87-APA-18 Taylor, C., 9-ATIO-2, 42-ATIO-4, 196-ATIO-16 Tomac, M., 109-APA-19 Smith, N., 159-ATIO-14, 242-ATIO-19 Steinfeld, A., 105-TP-7 Suñol, A., 13-APA-5/FC-1, 194-BA-1 Taylor, I., 213-HYTASP-6 Tomioka, S., 57-FD-8, 98-HYTASP-2 Smith, R., 299-TP-19 Steinhoff, J., 322-AA-37 Suraj Nandiganahalli, J., 95-MST-3 Taylor, L., 80-APA-17, 222-TP-15, 326-FD-32 Tomita, T., 57-FD-8 Snyder, M., 294-APA-45 Steinle, F., 54-MST-2 Sureshkumar, P., 165-AA-11 Tchipev, N., 126-ASE-8/AFM-9/FT-3 Tong, F., 351-AA-44, 360-AA-48 Sobester, A., 161-MAO-9 Stemmer, C., 173-FD-17 Surzhikov, S., 64-PDL-5, 103-PDL-8, 131-PDL-9, Tecson, L., 125-ASE-7 Tong, W., 199-MAO-10 Sobolewski, M., 46-MAO-4 Stengel, R., 82-ATIO-6 171-FD-15, 176-AMT-8/GT-6 Tekinalp, O., 21-MST-1 Tong, X., 52-ASE-3 Sokhey, J., 17-ASE-1, 343-ACD-13 Stephan, A., 126-ASE-8/AFM-9/FT-3 Sutcliffe, P., 27-AMT-1/GT-1 Tenaglia, A., 154-APA-26 Tormalm, M., 109-APA-19 Soleimani, S., 67-TP-5, 335-TP-21 Stephen, E., 290-FD-28 Sutliff, D., 94-AA-5, 295-AA-32, 333-AA-41, 354-AA-47 Terracol, M., 285-AA-28 Toropov, V., 85-MAO-5, 120-MAO-8 Soliman, M., 58-HYTASP-1 Stephens, D., 203-AA-15 Suzuki, K., 78-APA-15, 98-HYTASP-2 Tesfahunegn, Y., 330-APA-52 Toubin, H., 271-APA-42 Solodovnikov, S., 176-AMT-8/GT-6 Stern, E., 66-TP-4 Suzuki, T., 104-AFM-7, 177-AMT-9/GT-7 Testa, C., 320-AA-35 Tournadre, J., 264-AA-24 Soltani, M., 47-APA-11 Stevens, P., 47-APA-11 Sventitskiy, A., 184-TP-12 Tester, B., 123-AA-6, 254-AA-22, 288-AA-31, 349-AA-42 Toussaint, S., 82-ATIO-6 Song, J., 40-APA-10 Stevenson, G., 157-ATIO-13 Swieringa, K., 8-ATIO-1, 313-ATIO-23 Tetzloff, I., 245-ANERS-3 Towery, C., 281-FD-26 Song, K., 344-ATIO-25 Stewart, D., 165-AA-11, 253-AA-21 Swift, S., 202-AA-14 Tewes, P., 135-FC-8/APA-24 Towne, A., 252-AA-20 Author/Session Chair Index Trainelli, L., 200-ANERS-1 Van Aken, J., 27-AMT-1/GT-1 Vitagliano, P., 321-AA-36 Watanabe, T., 57-FD-8 Williams, C., 11-MAO-1 Trajkov, S., 114-ATIO-10, 345-ATIO-26 Van Antwerpen, B., 89-AA-2 Vitale, A., 238-APA-37 Watjen, J., 300-TP-20 Williams, D., 259-FC-12, 355-FD-35 Trani, A., 114-ATIO-10, 159-ATIO-14 Van Bavel, L., 16-AFM-2 Vitzilaios, N., 87-APA-18 Watkins, J., 317-APA-50 Williams, J., 53-ASE-4/FT-1 Trapani, G., 6-APA-3 Van de Ven, T., 128-AA-9 Viviani, A., 262-HYTASP-9 Watmuff, J., 271-APA-42 Williams, R., 193-ATIO-15 Trawick, D., 118-ACD-6, 277-ACD-12 Van den Eynde, J., 132-FD-12 Vlasenko, V., 270-APA-41 Watson, J., 12-MAO-2 Williams, W., 131-PDL-9 Trebs, A., 303-HYTASP-22 Van Dommelen, L., 99-FC-7 Von Hagel, K., 315-MAO-14 Watson, W., 361-AA-49 Wilson, A., 200-ANERS-1, 322-AA-37 Trevino, L., 141-AFM-11 van Duin, A., 185-TP-13, 222-TP-15 von Wolfersdorf, J., 262-HYTASP-9, 292-HYTASP-10, Weaver, B., 136-AMT-5/GT-4 Wilson, J., 299-TP-19 Trier, S., 205-ASE-12 Van Norman, J., 271-APA-42 328-HYTASP-12 Weber, M., 204-ASE-11 Wilson, S., 8-ATIO-1 Trinh, K., 121-APA-23 van Oudheusden, B., 154-APA-26, 357-FD-37 Vorobiev, A., 27-AMT-1/GT-1, 97-PDL-7 Weckmüller, C., 298-AA-33 Wilson Chan, Y., 258-HYTASP-8 Triscone, G., 79-APA-16 Van Schoor, M., 281-FD-26 Voutsinas, S., 239-APA-38 Weckner, O., 86-MAO-6 Winer, E., 86-MAO-6, 119-MAO-7, 199-MAO-10 Trolier, J., 84-ACD-4 Van Zante, D., 203-AA-15 Vu, B., 289-FD-27 Wehrmeyer, J., 61-AMT-3/GT-2, 136-AMT-5/GT-4 Wing, D., 42-ATIO-4 Trontin, P., 17-ASE-1, 52-ASE-3 Van Zante, J., 250-ASE-14/GT-10 Vucinic, D., 13-APA-5/FC-1, 194-BA-1 Wei, J., 122-FD-11, 350-AA-43 Winkleman, B., 136-AMT-5/GT-4 Tropea, C., 68-TP-6, 222-TP-15, 284-ASE-16 Vanden, K., 271-APA-42, 340-APA-54 Vuillot, F., 207-AA-17, 286-AA-29 Wei, M., 13-APA-5/FC-1 Winkler, J., 295-AA-32 Troshin, A., 270-APA-41 Vane, Z., 55-FD-6 Vyas, V., 48-FD-5 Wei, Q., 254-AA-22, 298-AA-33 Winski, C., 38-APA-8 Trujillo, A., 115-ATIO-11, 193-ATIO-15 VanPelt, T., 136-AMT-5/GT-4 Wadefalk, N., 337-TP-23 Weidong, L., 175-FC-9 Winter, M., 131-PDL-9, 217-HYTASP-7 Truong, S., 315-MAO-14 VanValkenburg, R., 126-ASE-8/AFM-9/FT-3 Wadel, M., 225-ASE-13 Weigand, B., 134-HYTASP-4, 258-HYTASP-8 Wisda, D., 165-AA-11, 203-AA-15 Tsai, C., 255-FD-23 Vanyai, T., 213-HYTASP-6 Wadhams, T., 215-AMT-10/GT-8, 327-FD-33, Weiner, A., 214-FC-11 Wise, D., 258-HYTASP-8 Tsakiris, D., 133-FD-13 Vargas, A., 194-BA-1 359-FD-39 Weitz, L., 313-ATIO-23, 344-ATIO-25 Witeof, Z., 84-ACD-4 Tsao, J., 52-ASE-3, 91-ASE-5, 166-ASE-9, 284-ASE-16 Vargas, M., 91-ASE-5, 125-ASE-7, 284-ASE-16 Waggoner, E., 78-APA-15 Welge, H., 110-APA-20 Witherden, F., 256-FD-24 Tsoi, A., 162-APA-29 Vassberg, J., 257-FD-25 Wagner, A., 296-HYTASP-11 Wells, D., 197-ACD-8, 198-ACD-9, 276-ACD-11 Wittich, D., 97-PDL-7, 131-PDL-9 Tsubokura, M., 308-APA-46, 310-APA-48 Vathylakis, A., 349-AA-42 Wagner, J., 48-FD-5, 177-AMT-9/GT-7, 280-APA-44, Wen, C., 134-HYTASP-4 Wlassow, F., 165-AA-11, 267-AA-25 Tu, Q., 262-HYTASP-9 Vatsa, V., 39-APA-9/FC-4 293-FD-30 Weng, H., 32-TP-1 Wojno, J., 203-AA-15, 249-AA-19 Turchi, A., 32-TP-1 Vechtel, D., 92-ASE-6/AFM-6/FT-2 Waithe, K., 5-APA-2 Wenzel, S., 313-ATIO-23 Wokoeck, R., 246-APA-39 Turgut, E., 316-ANERS-6 Veeraravagan, A., 65-PDL-4, 134-HYTASP-4, Waldron, T., 41-ATIO-3 Wernet, M., 323-AA-38 Wolf, A., 352-AA-45 146 Turnbull, A., 240-ATIO-17 262-HYTASP-9 Walker, B., 94-AA-5 Wernz, S., 211-FD-20 Wolf, W., 124-AA-7, 270-APA-41, 319-AA-34 Tyagi, A., 42-ATIO-4 Velandia, J., 111-APA-21 Walker, C., 125-ASE-7 West, D., 260-AMT-12/GT-11 Wolfe, D., 177-AMT-9/GT-7 Tyl, C., 138-HYTASP-5 Veldhuis, L., 87-APA-18 Walker, E., 38-APA-8 West, T., 38-APA-8, 183-TP-11, 217-HYTASP-7 Wolff, C., 18-ASE-2 Übelacker, S., 237-APA-36 Vellaramkalayil, J., 292-HYTASP-10, 328-HYTASP-12 Walker, G., 68-TP-6 Westmoreland, W., 309-APA-47 Wolkov, A., 270-APA-41 Ucarsu, M., 316-ANERS-6 Vellore, R., 205-ASE-12 Wall, A., 288-AA-31 Wey, P., 136-AMT-5/GT-4 Wollenheit, R., 245-ANERS-3 Ueda, S., 98-HYTASP-2 Venkatapathy, E., 104-AFM-7 Wallin, S., 131-PDL-9 Weymouth, G., 236-APA-35 Wolpert, D., 42-ATIO-4 Ugolotti, M., 269-APA-40 Venkataraman, K., 91-ASE-5 Wan, H., 143-TP-10 Whalen, E., 135-FC-8/APA-24 Wong, C., 180-FC-10/PDL-11 Uhlig, D., 308-APA-46 Venuti, J., 275-ATIO-22 Wan, Y., 9-ATIO-2 Wheatley, V., 65-PDL-4, 262-HYTASP-9 Wong, J., 162-APA-29, 192-APA-33 Uhlmann, F., 101-HYTASP-3 Verbeke, J., 16-AFM-2 Wang, B., 175-FC-9 Whelan, A., 336-TP-22 Wong, O., 153-APA-25 Uijt De Haag, M., 8-ATIO-1 Veres, J., 250-ASE-14/GT-10 Wang, C., 7-APA-4, 65-PDL-4, 329-FD-34 White, E., 23-FD-3, 132-FD-12, 247-FD-22 Woo, G., 99-FC-7 Ukeiley, L., 293-FD-30, 358-FD-38 Vergine, F., 217-HYTASP-7, 328-HYTASP-12 Wang, D., 223-TP-16 White, M., 97-PDL-7 Woodard, B., 166-ASE-9 Ulbrich, N., 215-AMT-10/GT-8 Vermeland, R., 190-APA-31, 317-APA-50 Wang, G., 60-ATIO-8, 282-AA-26, 340-APA-54 White, T., 104-AFM-7, 130-ITAR-2 Woodruff, M., 199-MAO-10 Ullrich, W., 322-AA-37 Vermillion, C., 195-LTA-1 Wang, J., 56-FD-7, 133-FD-13, 210-FD-19 Whiteley, M., 97-PDL-7, 131-PDL-9 Woopen, M., 212-FD-21 Umrigar, E., 362-TP-24 Vernier, J., 167-ASE-10/FT-5 Wang, L., 180-FC-10/PDL-11, 190-APA-31, Whitfield, C., 94-AA-5 Woszidlo, R., 25-FC-2 Underwood, M., 313-ATIO-23 Verstraete, D., 84-ACD-4 237-APA-36, 272-APA-43, 326-FD-32 Wiberg, B., 166-ASE-9 Wray, T., 55-FD-6 Upchurch, J., 115-ATIO-11 Verstraete, T., 165-AA-11 Wang, M., 124-AA-7 Wickern, G., 349-AA-42 Wright, W., 52-ASE-3, 125-ASE-7 Ura, H., 20-AA-1 Vicroy, D., 4-APA-1, 51-AFM-5, 77-APA-14, Wang, S., 7-APA-4 Wiebenga, J., 32-TP-1 Wu, D., 86-MAO-6, 134-HYTASP-4 Uranga, A., 154-APA-26, 216-AMT-11/GT-9 109-APA-19, 154-APA-26 Wang, T., 135-FC-8/APA-24 Wieland, F., 42-ATIO-4, 82-ATIO-6, 345-ATIO-26 Wu, J., 60-ATIO-8, 86-MAO-6, 173-FD-17 Urnes, J., 121-APA-23 Vidal, V., 123-AA-6 Wang, W., 133-FD-13, 135-FC-8/APA-24 Wigger, F., 101-HYTASP-3 Wu, L., 350-AA-43 Usanmaz, O., 316-ANERS-6 Viguier, P., 58-HYTASP-1 Wang, X., 48-FD-5, 264-AA-24 Wijnterp, C., 344-ATIO-25 Wu, S., 64-PDL-5, 134-HYTASP-4 Usoh, C., 339-APA-53 Vilardaga, S., 8-ATIO-1, 314-ATIO-24 Wang, Y., 9-ATIO-2, 26-APA-6, 87-APA-18, Wild, J., 20-AA-1, 112-APA-22 Wu, W., 65-PDL-4 Utt, L., 166-ASE-9 Villedieu, P., 17-ASE-1, 52-ASE-3, 125-ASE-7 134-HYTASP-4, 271-APA-42 Wilde, W., 344-ATIO-25 Wu, X., 247-FD-22, 348-APA-57, 358-FD-38 Uzol, O., 39-APA-9/FC-4 Vincent, P., 256-FD-24 Wang, Z., 86-MAO-6, 272-APA-43 Wiley, S., 78-APA-15 Wu, Y., 31-FC-3/PDL-3 Vaddi, S., 314-ATIO-24 Vincent-Randonnier, A., 258-HYTASP-8 Wanke, C., 9-ATIO-2, 42-ATIO-4, 196-ATIO-16 Wilhemi, C., 101-HYTASP-3 Wu, Z., 180-FC-10/PDL-11 Vaddi, V., 242-ATIO-19 Vinokur, M., 325-FD-31 Ward, C., 173-FD-17 Wilk, G., 106-TP-8 Wuerz, W., 247-FD-22 Valavanis, K., 87-APA-18 Visbal, M., 13-APA-5/FC-1, 14-FD-1, 26-APA-6, Washabaugh, K., 317-APA-50 Wilkinson, S., 219-PDL-12 Wuilbercq, R., 98-HYTASP-2 Valeau, V., 254-AA-22 31-FC-3/PDL-3, 56-FD-7, 88-FD-9, 97-PDL-7, Wassmer, D., 319-AA-34 Williams, A., 299-TP-19 Wukie, N., 249-AA-19 Valenzuela-del Río, J., 10-ACD-1 180-FC-10/PDL-11, 352-AA-45 Watanabe, M., 190-APA-31 Williams, B., 82-ATIO-6 Wygnanski, I., 59-FC-5, 135-FC-8/APA-24 Author/Session Chair Index Wysocki, O., 294-APA-45 Ye, Z., 340-APA-54 Zhang, Y., 155-APA-27 Xia, Y., 291-FD-29, 329-FD-34 Yee, P., 222-TP-15 Zhang, Z., 34-TP-3, 100-AMT-4/GT-3, 269-APA-40, Xiang, L., 134-HYTASP-4, 292-HYTASP-10 Yeong, Y., 17-ASE-1 300-TP-20 Xiang, X., 260-AMT-12/GT-11 Yeste, O., 242-ATIO-19 Zhao, B., 300-TP-20 Xiang Geng, W., 134-HYTASP-4, 292-HYTASP-10 Yi, S., 223-TP-16 Zhao, D., 264-AA-24, 320-AA-35, 354-AA-47 Xiao, X., 55-FD-6 Yildizlar, B., 318-APA-51 Zhao, J., 34-TP-3 Xiao, Z., 132-FD-12 Yilmaz, E., 182-AFM-13, 316-ANERS-6 Zhao, S., 134-HYTASP-4 Xiaosong, G., 86-MAO-6 Yoda, M., 222-TP-15 Zhao, W., 325-FD-31, 335-TP-21 Xie, D., 42-ATIO-4 Yokoyama, H., 322-AA-37 Zhao, X., 10-ACD-1, 47-APA-11, 221-TP-14 Xie, J., 9-ATIO-2 You, Y., 331-HYTASP-13 Zhao, Y., 175-FC-9 Xin, M., 104-AFM-7, 141-AFM-11 Young, A., 205-ASE-12 Zhengze, Z., 292-HYTASP-10 Xing, J., 88-FD-9 Young, J., 7-APA-4, 339-APA-53 Zhong, S., 176-AMT-8/GT-6, 334-AA-40 Xiong, J., 168-AA-12 Young, M., 37-APA-7, 77-APA-14 Zhou, B., 283-AA-27 Xisto, C., 122-FD-11 Young, S., 53-ASE-4/FT-1, 205-ASE-12 Zhou, L., 264-AA-24 Xu, G., 172-FD-16 Young, T., 158-FT-4, 197-ACD-8 Zhou, N., 155-APA-27 Xu, J., 361-AA-49 Yu, C., 283-AA-27 Zhou, Y., 7-APA-4, 9-ATIO-2, 120-MAO-8, Xu, K., 351-AA-44, 360-AA-48 Yu, H., 246-APA-39 180-FC-10/PDL-11 Xu, L., 329-FD-34 Yu, J., 260-AMT-12/GT-11 Zhu, C., 40-APA-10 Xu, M., 13-APA-5/FC-1 Yu, M., 210-FD-19, 272-APA-43 Zhu, T., 325-FD-31 Xu, T., 219-PDL-12 Yu, W., 176-AMT-8/GT-6, 254-AA-22, 319-AA-34 Zhu, W., 262-HYTASP-9 Xu, Y., 360-AA-48 Yu, Y., 308-APA-46 Zhuang, F., 281-FD-26 Xue, M., 8-ATIO-1 Yuan, M., 260-AMT-12/GT-11 Zilberter, I., 19-PDL-1 Xueying, D., 87-APA-18 Yuen, W., 106-TP-8 Zimper, D., 4-APA-1, 77-APA-14 Ya Jun, W., 134-HYTASP-4 Yumusak, M., 318-APA-51, 330-APA-52 Zingg, D., 45-MAO-3 147 Yadav, P., 343-ACD-13 Zaal, P., 54-MST-2 Ziskind, G., 33-TP-2, 68-TP-6, 223-TP-16, Yadav, R., 343-ACD-13 Zähringer, K., 65-PDL-4 336-TP-22, 362-TP-24 Yakeno, A., 180-FC-10/PDL-11, 189-APA-30 Zaichik, L., 160-ACD-7 Yalin, A., 19-PDL-1, 100-AMT-4/GT-3 Zaidi, T., 44-ACD-3 Yamada, K., 103-PDL-8, 183-TP-11, 265-TP-17, Zakaria, M., 243-ACD-10 348-APA-57 Zaki, T., 56-FD-7 Yamada, Y., 141-AFM-11, 260-AMT-12/GT-11 Zalewski, N., 59-FC-5 Yamagishi, Y., 17-ASE-1 Zaman, K., 136-AMT-5/GT-4, 323-AA-38 Yamamoto, F., 177-AMT-9/GT-7 Zaman, R., 7-APA-4 Yamamoto, H., 322-AA-37 Zambrano, J., 242-ATIO-19 Yamamoto, K., 20-AA-1, 111-APA-21, 168-AA-12 Zander, F., 66-TP-4, 140-AMT-7/PDL-10 Yamashita, R., 78-APA-15 Zang, W., 64-PDL-5 Yamauchi, Y., 328-HYTASP-12 Zare-Behtash, H., 219-PDL-12, 269-APA-40 Yan, S., 284-ASE-16 Zaytsev, M., 20-AA-1, 286-AA-29, 287-AA-30 Yang, B., 95-MST-3 Zelinski, S., 8-ATIO-1, 314-ATIO-24 Yang, H., 212-FD-21, 283-AA-27 Zerobin, S., 360-AA-48 Yang, J., 198-ACD-9 Zha, G., 26-APA-6, 189-APA-30, 330-APA-52 Yang, K., 167-ASE-10/FT-5 Zhang, B., 99-FC-7 Yang, V., 65-PDL-4, 255-FD-23 Zhang, F., 127-AA-8 Yang, X., 137-AMT-6/GT-5 Zhang, G., 122-FD-11 Yang, Y., 87-APA-18 Zhang, K., 91-ASE-5, 133-FD-13, 237-APA-36 Yang, Z., 47-APA-11, 79-APA-16, 266-TP-18 Zhang, L., 65-PDL-4, 237-APA-36, 345-ATIO-26 Yao, C., 122-FD-11, 128-AA-9 Zhang, M., 6-APA-3, 286-AA-29 Yao, W., 88-FD-9, 346-MAO-15 Zhang, Q., 361-AA-49 Yapalparvi, R., 99-FC-7 Zhang, R., 206-AA-16 Yarusevych, S., 7-APA-4, 133-FD-13 Zhang, S., 99-FC-7 Yashin, Y., 160-ACD-7 Zhang, X., 89-AA-2, 90-AA-3, 249-AA-19, 259-FC-12, Yay, O., 316-ANERS-6 352-AA-45 IntroTechnical Zones

AVIATION 2014 Technical Zones (see Venue Map)

The Technical Program, which consists of more than 1500 papers in over 20 technical tracks, has been placed within the hotel in zones to keep related session topics and technical conferences together. Please visit one of the zones to listen to a technical paper that is of interest to you! Zone 1 Zone 5 19th AIAA International Space Planes and Hypersonic 20th AIAA/CEAS Aeroacoustics Conference Systems and Technologies Conference AIAA Atmospheric Flight Mechanics Conference 14th AIAA Aviation Technology, Integration, and Operations Zone 2 Conference 7th AIAA Flow Control Conference 20th AIAA/CEAS Aeroacoustics Conference 45th AIAA Plasmadynamics and Lasers Conference AIAA Atmospheric Flight Mechanics Conference 30th AIAA Aerodynamic Measurement Technology and 6th AIAA Atmospheric and Space Environments Conference Ground Testing Conference 14th AIAA Aviation Technology, Integration, and Operations 32nd AIAA Applied Aerodynamics Conference Conference 11th AIAA/ASME Joint Thermophysics and Heat Transfer 44th AIAA Fluid Dynamics Conference Conference AIAA Modeling and Simulation Technologies Conference 44th AIAA Fluid Dynamics Conference 19th AIAA International Space Planes and Hypersonic Systems and Technologies Conference 45th AIAA Plasmadynamics and Lasers Conference Zone 6 14th AIAA Aviation Technology, Integration, and Operations Conference Zone 3 AIAA Balloon Systems Conference 32nd AIAA Applied Aerodynamics Conference AIAA Flight Testing Conference 44th AIAA Fluid Dynamics Conference 21st AIAA Lighter-Than-Air Systems Technology Conference 7th AIAA Theoretical Fluid Mechanics Conference 45th AIAA Plasmadynamics and Lasers Conference 45th AIAA Plasmadynamics and Lasers Conference AIAA/3AF Aircraft Noise and Emissions Reduction Symposium 15th AIAA/ISSMO Multidisciplinary Analysis and Zone 4 Optimization Conference 7th AIAA Flow Control Conference 44th AIAA Fluid Dynamics Conference 7th AIAA Theoretical Fluid Mechanics Conference 45th AIAA Plasmadynamics and Lasers Conference

www.aiaa-aviation.org 14842 #aiaaAviation IntroVenue Map

Hyatt Regency Atlanta LOBBY LEVEL ESCALATOR TO SKYWAY BRIDGE MAIN ENTRANCE BALLROOM ATRIUM LOBBY LEVEL (LL1)

ELEVATORS

INTERNATIONAL TOWER TO RADIUS TOWER REGISTRATION & SKYWAY BRIDGE

S TO BALLROOM GIFT LEVEL ATOR V SHOP E L LOBBY E

TO ATRIUM LOBBY ESCALATOR

TO INTERNATIONAL BALLROOM CENTENNIAL BALLROOM III III IV Exposition Hall

LOAD-IN VEHICLE BALLROOM LEVEL (LL1) ELEVATOR PRE-FUNCTION AREA Registration

ESCALATOR TO ATRIUM LOBBY POOL ESCALATOR TO POOL DECK THE EXHIBIT LEVEL LEARNING CENTER ELEVATORS REGENCY Zone 1 V TO TO EXHIBIT LEVEL LOBBY VI LEVEL Zone 1 INTERNATIONAL NORTH VII LOBBY BALLROOM ELEVATORS SOUTH ESCALATOR BALLROOM

TO TO BALLROOM LEVEL EMBASSY LEVEL

VEHICLE ABCD ELEVATOR TO BALLROOM LEVEL (LL1) WEST GRAND HALL EAST

LOADING EXHIBIT LEVEL (LL2) DOCKS LOAD-IN VEHICLE RAMP ELEVATOR

ESCALATOR A PRE-FUNCTION TO A B B AREA BALLROOM LEVEL C D ESCALATOR TO E ELEVATORS CONFERENCE LEVEL HANOVER Zone 2 C TO EMBASSY HALL CONFERENCE LEVEL (LL3) CHICAGO D F TO Zone 6 INTERNATIONAL BALLROOM G AB C E HALL G LOBBY H ATORS

ELEV FE D

ESCALATOR

TO TO CONFERENCE Zone 4 EXHIBIT LEVEL (LL2) LEVEL (LL3) ESCALATOR TO INMAN EXHIBIT LEVEL HARRIS GREENBRIAR FAIRLIE EDGEWOOD

ATLANTA CONFERENCE CENTER ELEVATORS KENNESAW TO (LL3) EMBASSY HALL (LL2) Zone 3 LENOX COURTLAND DUNWOODY VININGS

HERITAGE UNIVERSITY TECHWOOD SPRING BOARDROOM WILLIAMS

ELEVATORS BAKERAUBURN INTERNATIONAL Zone 5 ROSWELL PIEDMONT MARIETTA ESCALATOR

www.aiaa-aviation.org 14951 #aiaaAviation 22–26 JUNE 2015 DALLAS, TX AVIATION 2O15 WILL FEATURE: PLAN NOW FOR NEXT YEAR! 21st AIAA/CEAS Aeroacoustics Conference 31st AIAA Aerodynamic Measurement Technology What makes Dallas the perfect and Ground Testing Conference location for AVIATION 2O15? 33rd AIAA Applied Aerodynamics Conference 7th AIAA Atmospheric and Space Texas is: Environments Conference • No. 1 in Air Transportation Jobs AIAA Atmospheric Flight Mechanics Conference • No. 1 in Air Force Personnel 15th AIAA Aviation Technology, Integration, • No. 2 in Aerospace Manufacturing Output and Operations Conference AIAA Balloon Systems Conference The Hilton Anatole is conveniently located in the Design AIAA Complex Aerospace Systems Exchange (CASE) District near many attractions, making it ideal for 22nd AIAA Computational Fluid the family. It stands on 45 lush acres with an array Dynamics Conference of indoor and outdoor facilities, including pools, AIAA Flight Testing Conference restaurants, indoor basketball court, and Sculpture Park. Summer activities on the property include Bocce 45th AIAA Fluid Dynamics Conference ball, croquet, dive-in movies, volleyball, and more. 22nd AIAA Lighter-Than-Air Systems Technology Conference AIAA Modeling and Simulation Technologies Conference 16th AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference 46th AIAA Plasmadynamics and Lasers Conference 45th AIAA Thermophysics Conference

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