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22–26 JUNE 2015 DALLAS, TX
14-315
PUSHING THE BOUNDARIES OF THE IMAGINABLE: LEVERAGING THE AVIATION ECOSYSTEM
FINAL PROGRAM www.aiaa-aviation.org#aiaaAviation
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Welcome
Juan Alonso
Stanford University
Victoria Cox
Federal Aviation Administration (retired)
Thomas Edwards
NASA Ames Research Center
John O’Leary
Airbus Americas
Richard Wahls
NASA Langley Research Center
Todd Zarfos
Boeing Commercial Airplanes
Executive Steering Committee
AIAA AVIATION 2015
21st AIAA/CEAS Aeroacoustics Conference
31st AIAA Aerodynamic Measurement Technology and Ground Testing Conference
33rd AIAA Applied Aerodynamics Conference
AIAA Atmospheric Flight Mechanics Conference
7th AIAA Atmospheric and Space Environments Conference
15th AIAA Aviation Technology, Integration, and Operations Conference
AIAA Balloon Systems Conference
AIAA Complex Aerospace Systems Exchange
22nd AIAA Computational Fluid Dynamics Conference
AIAA Flight Testing Conference
45th AIAA Fluid Dynamics Conference
22nd AIAA Lighter-Than-Air Systems Technology Conference
16th AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference
AIAA Modeling and Simulation Technologies Conference
46th AIAA Plasmadynamics and Lasers Conference
45th AIAA Thermophysics Conference
AVIATION 2O15 is proud to feature the following conferences:
Welcome to Dallas and to AIAA AVIATION 2015! We are excited to share this week’s program with you as we explore recent progress and the most pressing issues facing aviation today. This year’s theme is “Pushing the Boundaries of the Imaginable: Leveraging the Aviation Ecosystem.” More than just a simple slogan, we think this theme provides a good overview of the various sessions planned for you this week.
Tom Enders will set the tone for us with his opening keynote addressing how the aviation industry can remain a dynamic player in pushing technology forward. Ed Bolton and Bill Ayer will discuss how NextGen will provide the foundation for advancing aviation in the future while engaging the myriad stakeholders that are a part of our ecosystem. Charlie Bolden will share the ways by which NASA historically has and will continue to push boundaries in aviation for the benefit of the entire community. Greg Touhill will discuss one of the more pressing issues of the day – cybersecurity and the importance of securing our ecosystem. Finally, Kurt Erbacher will look back at the design, development, and testing of the award-winning G650, one of the newest airplanes to hit the market while advancing the state of the art.
The Forum 360 sessions will provide several opportunities for our community to interact with customers, regulators, and technology leaders in focused, intimate conversations. Two sessions will allow leaders from airlines to discuss issues of importance to them with our design community. Unmanned systems continue to make headlines and we will discuss the challenges facing this sector internationally. Following Administrator Bolden’s discussion of NASA’s aeronautics strategy, we will hear from the center directors responsible for executing those plans. The challenges of widely deploying green aviation technologies to substantially reduce the environmental impact of aviation will be addressed by international experts. The future of supercomputing and particle image velocimetry will be discussed, with an emphasis on their role in advancing the future of aerospace technology. We will also have focused sessions on complex aerospace systems that will tackle the most important system development issues facing chief engineers, program managers, and systems engineers today.
As you would expect, with over 1,500 presentations, our technical program is second to none. The scope, breadth, and depth of the cutting-edge aviation and aerospace research being presented is material that you will be unable to find anywhere else. We thank the Forum Organizing and Technical Program Committees and the AIAA staff for their hard work to assemble this first-class program. We hope you will too.
AVIATION 2015 will energize, inspire, and sustain our community’s efforts to keep the aviation ecosystem on the glide path to advanced efficiency, safety, and security. We thank you for making the choice to be here with us this week, and we are confident you will find the experience to be a worthwhile one.
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IntroOrganizing CommitteeGeneral ChairRichard Wahls, NASA Langley Research Center
Forum 360 ChairRobert Gregg, III, The Boeing Company
Technical Co-ChairVincent Schultz, NASA Langley Research Center
Technical Co-ChairGreg Naterer, Memorial University
InternationalKonstantinos “Kostas” Kontis, University of Glasgow
Member ServicesSarah Shull, NASA Johnson Space Center
Local RepTerry Burress, Lockheed Martin Information Systems & Global Solutions
Young ProfessionalGreg Johnson, Aerojet Rocketdyne
RecognitionDimitri Mavris, Georgia Institute of Technology
Public PolicyBob Stuever, Beechcraft Defense Company, LLC
Complex Aerospace Systems Exchange (CASE) ChairSophia Bright, The Boeing Company
Technical Program Committee
Forum Technical Co-ChairsGreg Naterer (Aerospace Sciences Group), Memorial University
Vincent Schultz (Aircraft and Atmospheric Systems Group), NASA Langley Research Center
Forum Deputy Technical Co-ChairsLaTunia Melton (Aerospace Sciences Group), NASA Langley Research Center
Cees Bil (Aircraft and Atmospheric Systems Group), RMIT University
ITAR ChairKatya M. Casper, Sandia National Laboratories
Technical Discipline Chairs
Aeroacoustics Naval Agarwal, The Boeing Company
Aerodynamic Measurement TechnologyAndrew Cutler, The George Washington University
Todd Lowe, Virginia Polytechnic Institute and State University
Air Transportation Integration & OperationsCees Bil, RMIT University
Kapil Sheth, NASA Ames Research Center
Karen Marais, Purdue University
Scot Campbell, Massachusetts Institute of Technology
Aircraft DesignHernando Jimenez, Georgia Institute of Technology
Danielle (Dani) Soban, Queen’s University Belfast
Applied AerodynamicsBrian McGrath, The Johns Hopkins University Applied Physics Laboratory
Khaled Abdol-Hamid, NASA Langley Research Center
Zifeng Yang, Wright State University
Atmospheric and Space EnvironmentsNashat Ahmad, NASA Langley Research Center
Matthew Pruis, Northwest Research Associates Inc.
Atmospheric Flight Mechanics Soumyo (Som) Dutta, NASA Langley Research Center
Kevin Cunningham, NASA Langley Research Center
Balloon SystemsDebora Fairbrother, NASA
Complex Aerospace Systems Exchange (CASE) Sophia Bright, The Boeing Company
Computational Fluid DynamicsKrzysztof (Chris) Fidkowski, University of Michigan
Flight TestingKarl Garman, Federal Aviation Administration
Fluid DynamicsJill Klentzman, Baylor University
Green EngineeringAndrew Gibson, Empirical Systems Aerospace
Ground TestingBenjamin Mills, Aerospace Testing Alliance
Lighter than Air SystemsRajkumar S. Pant, Indian Institute of Technology Bombay
Modeling and Simulation TechnologiesGano Broto Chatterji, NASA Ames Research Center
Multidisciplinary Analysis and OptimizationEliot Winer, Iowa State University
Vijay Kalivarapu, Iowa State University
Plasmadynamics and LasersAzer Yalin, Colorado State University
ThermophysicsChad Boyack, Raytheon Missile Systems
Elliott Short, Raytheon Missile Systems
Technical Discipline Group Representatives
TAC Information Systems GroupSam Adhikari, Sysoft Corporation
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IntroContents
Welcome 3
Organizing Committee 4
Contents 5
Forum Overview 8
Sponsors 10
Keynote Speakers and Plenary Sessions 11
Forum 360 12
Special Sessions and Events 17
Networking Events 18
Recognition Events 19
ITAR Information 21
Exposition Hall 22
Exhibitors 24
General Information 27
Author and Session Chair Information 29
Committee Meetings 30
Sessions at a Glance 33
Session Detail Matrix 41
Author and Session Chair Index 121
Technical Zones 134
Venue Map 135
AIAA is the world’s largest aerospace professional society, serving a diverse range of more than 30,000 individual members from 88 countries, and 95 corporate members. AIAA members help make the world safer, more connected, more accessible, and more prosperous. For more information, visit www.aiaa.org, or follow us on Twitter @AIAA.
Join the conversation!#aiaaAviation
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IntroForum Overview
MONDAY 22 June
TUESDAY 23 June
0730 hrs Speakers’ Briefing Speakers’ Briefing
0800 hrsPlenary Keynote Plenary Panel
0830 hrs
0900 hrs Networking Break
Technical Sessions
Networking Break in Exposition Hall
Technical Sessions
Exposition Hall Open
0930 hrs
Forum 360 Forum 360
1000 hrs
1030 hrs
1100 hrs
1130 hrs
1200 hrs
1230 hrs
Networking Lunch on OwnAwards Luncheon:
Celebrating Achievements in Aerospace Sciences
Networking Lunch on Own1300 hrs
1330 hrs
1400 hrs
Technical Sessions
Forum 360 Technical Sessions
Forum 360
CFD Flow Visualization Showcase
Exposition Hall Open
1430 hrs
1500 hrs
1530 hrs Networking Break Networking Break in Exposition Hall
1600 hrs
1630 hrs Plasmadynamics and Lasers Award Lecture1700 hrs
1730 hrs Fluid Dynamics Award Lecture Speed Geek
Networking Event and Reception
Reception in Exposition Hall1800 hrs
1830 hrs Rising Leaders in Aerospace Reception1900 hrs
1930 hrs
2000 hrs
2030 hrs
2100 hrs
2130 hrs
2200 hrs
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IntroForum Overview
WEDNESDAY 24 June
THURSDAY 25 June
FRIDAY 26 June
0730 hrs Speakers’ Briefing Speakers’ Briefing Speakers’ Briefing
0800 hrsPlenary Keynote Plenary Keynote Plenary Keynote
0830 hrs
0900 hrs Networking Break in Exposition Hall
Technical Sessions
Exposition Hall Open
Networking Break in Exposition Hall
Technical Sessions
Exposition Hall Open
Networking Break
Technical Sessions
0930 hrs
Forum 360 Forum 360
1000 hrs
1030 hrs
1100 hrs
1130 hrs
1200 hrs
1230 hrs
Luncheon in Exposition HallAwards Luncheon:
Celebrating Achievements in Aircraft and Atmospheric Systems
Networking Lunch on Own1300 hrs
1330 hrs
1400 hrs
Technical Sessions
Forum 360
Exposition Hall Open
Technical Sessions
Forum 360
Rising Leaders in Aerospace
Panel1430 hrs
1500 hrs
1530 hrs Networking Break in Exposition Hall Rising Leaders
in Aerospace Leadership
Exchange/Speed Networking
Networking Break
1600 hrs
1630 hrs Aerodynamics Award Lecture1700 hrs
1730 hrsAeroacoustics
LectureThermophysics Award Lecture Wright Brothers Lectureship in Aeronautics
1800 hrs
1830 hrs
1900 hrs
Aeroacoustics Awards Banquet1930 hrs
2000 hrs
2030 hrs
2100 hrs
2130 hrs
2200 hrs
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IntroSponsors Premier Sponsor
Speed Geek Networking Event Sponsor
Supporting Sponsors
Media Sponsor
R
Crean & AssociatesAerospace Consultants
Rising Leaders Program SponsorSponsor
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IntroKeynote Speakers and Plenary SessionsGet the big picture on aviation from the thought leaders in the field during these high-level discussions and presentations.
Monday, 22 June 0800–0900 hrs Chantilly Ballroom West
Opening Keynote: Are We Moving Fast Enough? Tom Enders, Chief Executive Officer, Airbus Group
Tuesday, 23 June0800–0900 hrs Chantilly Ballroom West
NextGen: A Model of Stakeholder Engagement Bill Ayer, Retired Chairman and CEO, Alaska Air GroupEdward L. Bolton Jr., Assistant Administrator for NextGen, Federal Aviation Administration
Wednesday, 24 June0800–0900 hrs Chantilly Ballroom West
NASA and the Future of AerospaceCharles F. Bolden Jr., Administrator, National Aeronautics and Space Administration
Thursday, 25 June0800–0900 hrs Chantilly Ballroom West
DHS’s Perspectives on Cybersecurity in Aviation Gregory J. Touhill, Deputy Assistant Secretary for Cybersecurity and Communications, Department of Homeland Security
Friday, 26 June0800–0900 hrs Chantilly Ballroom West
The G650 Design, Development, and Test Kurt Erbacher, Vice President, G650 Aircraft Program, Gulfstream Aerospace Corporation
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Forum 360
Monday, 22 June0930–1200 hrs Grand Ballroom E
The Voice of the Customer — Designing the Right Aircraft Moderator: Christopher Stonehouse, Senior Vice President, Customer Services, Airbus Americas, Inc.Panelists:Jack Arehart, President of MRO Services, Delta TechOpsWilliam “Bill” Meehan, Chief Operating Officer, Frontier
Airlines, Inc.Bart Roberts, Vice President, Flight Operations, JetBlue AirwaysDavid Seymour, Senior Vice President, Technical Operations,
American Airlines
1400–1700 hrs Grand Ballroom E
Whatever Happened to the Four-Year Airplane?Moderator: Craig Willis, Group Head for Systems Verification, Gulfstream G500/G600 Program, Gulfstream Aerospace CorporationPanelists:Catherine Ferrie Kilmain, Executive Vice President of
Engineering, Bell HelicopterEric Schrock, Deputy Director, Technology Development and
Product Integration, Lockheed Martin Corporation
Tuesday, 23 June0930–1200 hrs Grand Ballroom E
Day in the Life of Operations – Effectively Managing DisruptionModerator: Neil Planzer, Vice President, Air Traffic Management, Boeing Commercial AirplanesPanelists:Tim Campbell, Senior Vice President, Air Operations, American
AirlinesJim Crites, Executive Vice President of Operations, DFW
International AirportBrian Quigley, Managing Director Flight Operations, United
AirlinesDan Smiley, Vice President for System Operations, Federal
Aviation Administration Air Traffic Office
1400–1630 hrs Grand Ballroom E
International UAS Integration ForumModerator: Rob Hughes, Northrop Grumman, IncPanelists:Cees Bil, Associate Professor, School of Aerospace, Mechanical
and Manufacturing Engineering, RMIT UniversityChuck Johnson, Vice President of Operations, The Padina
GroupMarty Rogers, University of Alaska-FairbanksMarshall Jackson, Project Manager – Aviation Safety
Audits, Office of Inspector General, U.S. Department of Transportation
Randy Willis, FAA, Co-Chair of ICAO RPAS (Remotely Piloted Aircraft Systems)
Dale Richards, Senior Research Fellow, Human Factors, Faculty of Engineering & Computing, Coventry University
These conversations will cover a spectrum of timely topics including programs, systems, policy, operations, applications, platforms and more!
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IntroWednesday, 24 June0930–1200 hrs Grand Ballroom E
NACA to NASA: Embarking on the Next 100 Years of Excellence and Innovation in Aeronautics and BeyondModerator: Robert Pearce, Director, Strategy, Architecture & Analysis, Aeronautics Research Mission Directorate, NASA HeadquartersPanelists:David Bowles, Center Director (Acting), NASA Langley
Research CenterThomas Edwards, Deputy Center Director, NASA Ames
Research CenterJanet Kavandi, Deputy Director, NASA Glenn Research CenterDavid McBride, Center Director, NASA Armstrong Flight
Research CenterJaiwon Shin, Associate Administrator, Aeronautics Research
Mission Directorate, NASA Headquarters
1400–1630 hrs Grand Ballroom E
Energy/Environment Panel — The Challenges of Green AviationModerator: Marty Bradley, Technical Fellow, Boeing Commercial AirplanesPanelists:Ricky Curran, Faculty of Aerospace Engineering, Delft
University of TechnologyJay E. Dryer, Director, Advanced Air Vehicles Program Office
(Acting), Aeronautics Research Mission Directorate, NASA Headquarters
Askin Isikveren, Head of Visionary Aircraft Concepts, Bauhaus Luftfahrt
Leslie Perkins, Director, Energy Office, Air Force Research Laboratory
Jeanne Yu, Environmental Director, Boeing Commercial Airplanes
1400–1730 hrs Grand Ballroom D
System Complexity: Government Needs and Practical Research Results Keynote Speaker: Kristen Baldwin, Principal Deputy DASD (SE), Department of DefenseModerators:Frank Serna, Principal Director, Strategic Imperatives, Draper
LaboratoryAnna-Marie McGowan, Aeronautics Research Directorate,
NASA Langley Research CenterPanelists:Jeffrey P. Holland, Director of Research and Development and
Chief Scientist, U.S. Army Corps of EngineersDavid Neyland, Consultant
Thursday, 25 June0930–1200 hrs Grand Ballroom E
The Impact of Particle Image Velocimetry on Aerospace TechnologyModerator: Steven Beresh, Distinguished Member of the Technical Staff, Sandia National Laboratories Panelists:Ronald J. Adrian, Regent’s Professor and Ira A. Fulton Professor
of Mechanical and Aerospace Engineering, Arizona State University
Susan Gorton, Project Manager, Revolutionary Vertical Lift Technology Project, NASA Langley Research Center
Fulvio Scarano, Full Professor and Chair of Aerodynamics, Delft University of Technology
Miguel Visbal, Principal Research Aerospace Engineer and Team Leader of Multidisciplinary Computational Aerodynamics, Aerospace Systems Directorate, Air Force Research Laboratory
1400–1630 hrs Grand Ballroom E
Supercomputing: Roadmap and Its Future Role in Aerospace EngineeringModerator: Doug Cline, Technical Lead, High Performance Computing, Lockheed Martin AeronauticsPanelists:Jef Dawson, Applications Manager, Cray, Inc.William Gropp, Thomas M. Siebel Chair, Department of
Computer Science and Director, Parallel Computing Institute, University of Illinois at Urbana-Champaign
Brian Mitchell, Senior Principal Engineer, GE Global ResearchMark Seager, Intel Fellow, CTO, High Performance Computing
Ecosystem, Intel Corporation
Forum 360
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Intro
Monday, 22 June0900–1200 hrs Batik A-B
Academic RoundtableExpanding on the theme from Sunday, this session is the second day activity of the 2015 CASE Academic Workshop. It will offer rapid-fire discussions of current research efforts in systems knowledge and competency.Facilitators:Franz-Josef Kahlen, Ph.D., Associate Professor, Department
of Mechanical Engineering, University of Cape Town, Cape Town, South Africa
Shannon Flumerfelt, Ph.D., Associate Professor, Educational Leadership, Director of Lean Thinking for Schools, Pawley Learning Institute, Oakland University, Michigan
Anabela Alves, Ph.D., Assistant Professor, Departamento de Produção e Sistemas Escola de Engenharia da Universidade do Minho, Centro Interdisciplinar de Tecnologias, da Produção e da Energia (CITPE), Campus de Azurém, Portugal
1400–1700 hrs Grand Ballroom E
Whatever Happened to the Four-Year Airplane?This panel will explore the challenges facing aerospace professionals who are directly engaged in leading, developing, producing, and supporting the industry’s most advanced vehicles and systems in the context of a “four-year aircraft” theme. We continue to push the limits of technology to deliver greater performance in all segments of aerospace, in an environment that is increasingly risk averse. These challenges have pushed us to longer development cycles and exponential growth in budgets. In addition, new technical disciplines (e.g., cyber) are being integrated into legacy and emerging systems, while subsystems are gaining in both complexity and interdependency. In the context of this environment, our panel will address how the aerospace industry should position itself to meet the challenges of reducing the cost and schedule and approach a “four-year aircraft” cycle in our increasingly complex world.Moderator: Craig Willis, Group Head for Systems Verification, Gulfstream G500/G600 Program, Gulfstream Aerospace CorporationPanelists:Catherine Ferrie Kilmain, Executive Vice President of
Engineering, Bell HelicopterEric Schrock, Deputy Director, Technology Development and
Product Integration, Lockheed Martin Corporation
1730–1900 hrs Morocco
CASE Networking SocialSponsored by Boeing Commercial Airplanes
Tuesday, 23 June0930–1200 hrs Grand Ballroom D
Applied Complexity WorkshopParticipants can learn how to embrace and thrive within technically, socially, and organizationally complex environments. Participants will be immersed in a three-pronged approach to learning, with industry examples, applied theory, and interactive practice. Please join us for this engagement, and bring your own experiences to share and a desire to strengthen your complex systems engineering thinking. Panelists:Paul C. Lambertson, Systems Engineering & Integration Team
777X, Boeing Commercial AirplanesSteve Holt, Engineering Integrated Strategy, Airplane Level
Engineering Integration, The Boeing CompanyJim Blohowiak, 777X Airplane Level Integration Team, The
Boeing CompanyAlison Lauderbach, 777X Airplane Level Integration Team, The
Boeing Company
1400–1530 hrs Steuben
Concept Development of Complex SystemsThis panel addresses the phase of development that includes activities from the beginning of decision activities for building new systems to the transition to the product design at milestone “B” (DoD) or the end of Phase B for NASA. Session Chairs:Steven D’Urso, Program Coordinator and Lecturer, Aerospace
Systems Engineering, University of Illinois at Urbana-Champaign
Mat French, Electrical Systems Engineer, Rolls-Royce Corporation
Panelists:Rick Mange, F-35 PNR Program Manager, Lockheed Martin
AeronauticsRobert (Rob) Simons, Technical Fellow, The Boeing CompanyJason Merret, Technical Specialist, Gulfstream Aerospace
Performance Engineering, Gulfstream Aerospace Corporation
Forum 360 As the name implies, CASE is an exchange of ideas among professionals on some of the most pertinent issues of the day facing the aerospace industry and the field of systems engineering.
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IntroForum 360 1545–1730 hrs Steuben
Product Design for Complex Systems Across the Supply ChainThis session will focus on the challenges and enabling technologies for product design across a supply chain. In particular, the session will address the layered chain consisting of OEM/airframer, Tier 1, Tier 2, and the approaches for designing complex systems that handle the integration aspects. Methods and model-based tool approaches will be discussed in terms of existing capabilities, gaps, and future trends.Session Chairs:Eelco Scholte, Manager, Advanced Methods – Electric Systems,
UTC Aerospace Systems Carmen Schooley, Manager, Systems Engineering and
Integration, Gulfstream Aerospace CorporationPanelists:Fernando Dones, Technical Fellow, The Boeing CompanyBernard Dion, CTO, ANSYSBrenda Nuhfer, Program Manager, UTC/Pratt & Whitney
Wednesday, 24 June0900–1045 hrs Grand Ballroom D
Integration and TestThis panel focuses on the Integration & Test phase of development. Planning for integration activities of complex systems is inherently different from traditional systems engineering integration planning activities. Decisions about the systems under development have to consider not only the technical and programmatic viewpoints but also the political, societal, operational, and economic viewpoints. Definition of performance measures, found intrinsic in the plan, with trans-disciplinary implications will be discussed. A scenario for integration of UAS in the NAS will be used as a benchmark for current views and life-cycle challenges.Session Chairs:Mat French, Electrical Systems Engineer, Rolls-Royce
CorporationHernando Jiminez, Research Engineer II at Aerospace Systems
Design Laboratory, Georgia Institute of TechnologyDavid Loda, Executive Director, NCPS Research, LLCPanelists:Jim Murphy, Project Engineer for Integrated Test and Evaluation
for the Unmanned Aircraft System Integration, NASA Ames Research Center
David Maroney, Principal Systems Engineer, The Mitre Corporation
1045–1230 hrs Grand Ballroom D
Entry into Service/End of LifeThis panel focuses on the complexities that arise once a system enters service throughout the life of the system. If these complexities are considered and incorporated into the system development phase, more robust products can be developed and higher customer satisfaction can be achieved. Session Chair: Jeff Jepson, Senior Systems Engineer GNC / Guidance Design & Performance, Raytheon Missile SystemsPanelists:Tim Adama, Chief Engineer of Factories, Raytheon Missile
SystemsEd Dolanski, President and CEO, AviallJim Gallagher, EIS Program Manager, Gulfstream Aerospace
Corporation
1400–1730 hrs Grand Ballroom D
System Complexity: Government Needs and Practical Research ResultsThis panel is arranged around two application domains – defense systems and unmanned air systems in the national airspace – and two engineering practice needs – rapid system development and new theory complex systems engineering. The expectation is that the audience will take away both a cogent statement of needs and challenges along with a concise description of new techniques that show promise to meet the stated needs and challenges.Keynote Speaker: Kristen Baldwin, Principal Deputy DASD (SE), Department of DefenseModerators: Frank Serna, Principal Director, Strategic Initiatives, Draper
LaboratoryAnna-Maria McGowan, Aeronautics Research Directorate,
NASA Langley Research CenterPanelists:Jeffrey P. Holland, Director of Research and Development and
Chief Scientist, U.S. Army Corps of EngineersDavid Neyland, Consultant
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IntroForum 360
Program Agenda
Networking ReceptionMonday, 22 June Emerald1830–1930 hrsThe reception will kick off the Rising Leaders in Aerospace events and is a perfect opportunity for young leaders to mingle with others who will be participating in AIAA AVIATION 2015 as attendee, presenter, or veteran professional. Come meet other participants in a casual environment. You’re bound to see them again.
Leadership Exchange/Speed NetworkingWednesday, 24 June Metropolitan Ballroom1530–1700 hrsGet your questions answered! Senior Mentors will include:Russ Althof, Chief Engineer, Raytheon Missile SystemsCees Bil, Professor , Royal Melbourne Institute of TechnologyDave Bowles, Center Director (Acting), NASA Langley Research CenterEd Feltrop, Engineer Specialist , Cessna Aircraft CompanySusan Gorton, Rotary Wing Project, NASA Langley Research CenterPeter Hartwich, Engineering Manager, Boeing Defense, Space and SecurityJanice Kavandi, Deputy Director, NASA Glenn Research CenterJeff Jepson, Senior Multi-Disciplined Engineer I, Raytheon Missile SystemsSamantha A. Magill, Academic Affairs and Inclusion & Diversity, Honda Aircraft CompanySandy Magnus, Executive Director, AIAADavid McBride, Center Director, NASA Armstrong Flight Research CenterCharles Smith, Center Director (Acting), NASA Ames Research Center John Valasek, Professor/Director, Vehicle Systems & Control Laboratory, Texas A&M University
Panel Discussion: Transitioning to Leadership Thursday, 25 June Emerald1400–1530 hrsAs engineers and aerospace professionals gain experience, there is often the opportunity to do more with the company. Promotions are often a result, but so are management opportunities. As you transition from an engineer on a project to an engineer leading a project, what changes? How about when you are made manager of a department or a division, are there skill sets that you need to hone? What if you are looking to eventually become a chief officer, how can you plan for and make those transitions? This panel will address the changes that accompany moving into a management role, the different skill sets that will need to be acquired, and the changes you can expect in your daily work routine.If you have management or leadership aspirations, come and listen to advice from esteemed panelists.Moderator: Ben Marchionna, Systems Engineer, Lockheed Martin Skunk WorksPanelists:Russ Althof, Chief Engineer, Raytheon Missile SystemsDouglas Stanley, President and Executive Director, National Institute of AerospaceFrederick Wieland, Director, Air Traffic Management, Intelligent Automation Systems, Inc.
RISINGLEADERSAEROSPACEin
Sponsored by:
The multidimensional program features a leadership exchange/speed mentoring, panel session, Q&A with top industry leaders, and multiple opportunities for networking. These exciting and energetic activities will provide access to top aerospace leaders and their perspectives with subject matter relevant to your career.
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IntroSpecial Sessions and EventsSpeed Geek Networking Event and ReceptionMonday, 22 June Chantilly Ballroom Foyer1730–1830 hrs, reception to follow 1830–1900 hrsThis casual, high-energy session will give you the opportunity to engage one-on-one with speakers and get a glimpse of things to come in the week ahead at AIAA AVIATION 2015. You’ll travel from speaker to speaker in small groups, listen to a 5-minute overview of their topic, and then have five minutes to have your questions answered.Open to all conference attendees, but space is limited to the first 500 participants.Sponsored by:
CFD Flow Visualization ShowcaseTuesday, 23 June Chantilly Ballroom Foyer1400–1600 hrsThe CFD Flow Visualization Showcase will be held in the foyer area outside the Exposition Hall. Authors of papers containing CFD visualizations will describe their work and the significance of their animation as it plays on a large- screen monitor. Multiple visualizations will be shown during each of the four 30-minute time slots during the event. At the conclusion of the event, awards will be presented for Most Artistic Flow Visualization Animation, Most Quantitatively Descriptive Flow Visualization Animation, and Most Comprehensive Flow Visualization Animation. The visualizations of the three winners will be displayed on a monitor in the Exposition Hall during the remainder of the exposition.
Aeroacoustics Awards Reception and BanquetWednesday, 24 June Imperial Ballroom1900 hrsThe Aeroacoustics Awards Reception and Banquet will begin with a cash bar social period at 1900 hrs, followed by the awards ceremony and banquet where the AIAA and CEAS Aeroacoustics Awards will be presented. The winner of the Aeroacoustics Student Paper Competition also will be recognized. Please join us and celebrate the achievements of your peers. Tickets will be available on site, as space is available.
See it in Dallas at the Perot Museum of Nature and Science
www.airplanesmovie.com
A MILE OF RUNWAY CAN TAKE YOU ANYWHERE.
NARRATED BY
HARRISON FORD
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IntroUnderstanding the importance of networking with colleagues new and old, a series of activities have been planned that will help you connect with current colleagues and new acquaintances.
Student Welcome ReceptionSunday, 21 June Emerald1800–1930 hrs Mingle with your peers and hear from AIAA Executive Director Sandy Magnus. This reception provides you with the opportunity to meet your fellow students and learn more about the opportunities available to you as an AIAA student member.
Networking Coffee BreaksNetworking coffee breaks allow even more time for making new contacts, continuing discussions from sessions, visiting the Exposition Hall, or checking emails and voicemails to keep in touch with the office while you are at the forum. Networking coffee breaks will be held at the following locations and times:
Monday, 22 June 0900–0930 hrs and 1530–1600 hrs; Meeting Room Foyers
Tuesday, 23 June 0900–0930 hrs and 1530–1600 hrs; Exposition Hall
Wednesday, 24 June 0900–0930 hrs and 1530–1600 hrs; Exposition Hall
Thursday, 25 June 0900–0930 hrs (Exposition Hall) and 1530–1600 hrs (Meeting Room Foyers)
Friday, 26 June 0900–0930 hrs Meeting Room Foyers
Reception in the Exposition HallTuesday, 23 June Chantilly Ballroom East 1730–1900 hrsTake this opportunity to engage new contacts and refresh old ones. A ticket for the reception is required and included in the registration fee where indicated. Additional tickets for guests may be purchased on site, as space is available.
Luncheon in the Exposition HallWednesday, 24 June Chantilly Ballroom East1230–1400 hrsA ticket is required and included in the registration fee where indicated.
Networking Events
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Recognition EventsAIAA celebrates our industry’s discoveries and achievements from the small but brilliantly simple innovations that affect everyday life to the major discoveries and missions that fuel our collective human drive to explore and accomplish amazing things.
Monday, 22 June1730–1830 hrs Grand Ballroom D
Fluid Dynamics Award LectureSearching for Truthiness in Computational Fluid DynamicsPhilip Roe, Professor, Department of Aerospace Engineering, University of Michigan
Tuesday, 23 June1230–1400 hrs Chantilly Ballroom West
Awards Luncheon: Celebrating Achievements in Aerospace Sciences A ticket for the luncheon is required and included in the registration fee where indicated. Additional tickets for guests may be purchased on site, as space is available. The following awards will be presented:
Aeroacoustics AwardNigel PeakeProfessor, Applied Mathematics University of Cambridge “For significant contributions to the understanding and prediction of turbomachinery noise generation and scattering.”
Aerodynamics AwardRussell M. CummingsProfessor of Aeronautics U.S. Air Force Academy “For a career devoted to predicting and understanding the vortical flowfields about aircraft at high angles of attack and during maneuvers.”
Fluid Dynamics AwardPhilip RoeProfessor, Department of Aerospace Engineering University of Michigan “For seminal contributions to the design of numerical algorithms for simulations of compressible flows.”
Plasmadynamics and Lasers AwardPhilip E. CassadySenior Technical Fellow (retired) The Boeing Company “For distinguished contributions to the development of aero-optics and high power laser fluid dynamics.”
Thermophysics AwardSumanta AcharyaRing Chair & Professor, Mechanical Engineering Department University of Memphis “For significant contributions to gas turbine heat transfer and aerodynamics, investigation of novel cooling schemes and application of emerging computational methodologies for gas turbine cooling.”
Certificates of Merit:Aerodynamic Measurement Technology Best PaperAIAA 2015-1696, “Pressure Monitoring using Hybrid fs/ps Rotational CARS,” Sean Kearney, Sandia National Laboratories, and Paul Danehy, NASA Langley Research Center.
Applied Aerodynamics Best PaperAIAA 2014-2139, “Uncertainty Quantification and Certification Prediction of Low-Boom Supersonic Aircraft Configurations,” Thomas K. West, Missouri University of Science and Technology; Bryan W. Reuter, University of Texas at Austin; Eric L. Walker, Bill Kleb, and Michael A. Park, NASA Langley Research Center.
David Weaver Best Student PaperAIAA 2014-2247, “Microscale Simulations of Porous TPS Materials: Application to Permeability,” Eric C. Stern, Ioannis Nompeli, Thomas Schwartzentruber and Graham Candler, University of Minnesota.
Fluid Dynamics Best PaperAIAA Paper 2015-1518, “Large Eddy Simulation of a Three-Dimensional Compression Ramp Shock-Turbulent Boundary Layer Interaction,” David Dawson and Sanjiva Lele, Stanford University.
Ground Testing Best PaperAIAA 2014-2800, “Skin Friction Sensor Validation for High-Speed, High-Enthalpy Flow Applications,” Ryan Meritt and Joseph Schetz, Virginia Polytechnic Institute and State University.
Modeling and Simulation Best PaperAIAA 2014-2206, “Transfer of Training on the Vertical Motion Simulator,” Peter Zaal, NASA Ames Research Center; Jeffrey Schroeder, Federal Aviation Administration; and William Chung, SAIC.
(continued)
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Recognition EventsCertificates of Merit (continued)Plasmadynamics and Lasers Best PaperAIAA 2015-0935, “Electric Field Measurements in a Dielectric Barrier Nanosecond Pulse Discharge with Sub-nanosecond Time Resolution,” Benjamin Goldberg and Walter Lempert, Ohio State University; and Sean O’Byrne, University of New South Wales at the Australian Defence Force Academy.Plasmadynamics and Lasers Best Student PaperAIAA 2015-0679, “A Latency-Tolerant Architecture for Airborne Adaptive Optic Systems,” William R. Burns, Eric J. Jumper and Stanislav Gordeyev, University of Notre Dame.Thermophysics Best PaperAIAA 2015-0213, “NASA Langley Experimental Aerothermodynamic Contributions to Slender and Winged Hypersonic Vehicles,” Scott Berry and Karen Berger, NASA Langley Research Center.
1630–1730 hrs Grand Ballroom D
Plasmadynamics and Lasers Award LectureFrom Plasmadynamics and Shock Tubes to Aero-Optics and Laser Radar: An Aerospace CareerPhilip E. Cassady, Senior Technical Fellow (retired), The Boeing Company
Wednesday, 24 June1630–1730 hrs Chantilly Ballroom West
Aerodynamics Award LectureStill Trying to Understand Aircraft VorticesRussell M. Cummings, Professor of Aeronautics, U.S. Air Force Academy
1730–1830 hrs Grand Ballroom E
Thermophysics Award LectureAerodynamics and Heat Transfer in Gas Turbine Cooling-Recent AdvancesSumanta Acharya, Ring Chair & Professor, Mechanical Engineering Department, University of Memphis
1730–1830 hrs Chantilly Ballroom West
Aeroacoustics LectureFan Broadband Noise Generation and SuppressionEdmane Envia, Acoustics Branch, NASA Glenn Research Center
Thursday, 25 June1230–1400 hrs Chantilly Ballroom West
Awards Luncheon: Celebrating Achievements in Aircraft and Atmospheric Systems A ticket for the luncheon is required and included in the registration fee where indicated. Additional tickets for guests may be purchased on site, as space is available. The following awards will be presented:
Aircraft Design AwardDarold B. CummingsAerospace Consultant Boeing Technical Fellow (retired)“For a career demonstrating exceptional skill and creativity in the configuration and design of aircraft, and inspiring future generations of aircraft designers.”
Elmer A. Sperry AwardMichael Sinnett, Vice President, Product Development, and the Boeing 787-8 Development Team, Seattle, Washington“For pioneering engineering advances including lightweight composite wing and monolithic composite fuselage construction and advanced systems that have led to significant improvements in fuel efficiency, reduced carbon emission, reduced maintenance costs and increased passenger comfort.”
Certificates of Merit:Aircraft Design Best PaperAIAA 2014-3012, “A Requirements-driven Methodology for Integrating Subsystem Architecture Sizing and Analysis into the Conceptual Aircraft Design Phase,” Imon Chakraborty, David Trawick, and Dimitri Mavris, Georgia Institute of Technology; Mathias Emeneth, PACE Americas Inc.; and Alexander Schneegans, PACE GmbH.
Multidisciplinary Design Optimization Best PaperAIAA-2014-3274, “Aerostructural Optimization of the Common Research Model Configuration,” Gaetan Kenway and Joaquim Martins, University of Michigan; and Graeme Kennedy, Georgia Institute of Technology.
1730–1830 hrs Chantilly Ballroom West
Wright Brothers Lectureship in Aeronautics Development and Testing of the X-47BPablo Gonzalez II, UCAS-D Program Manager, Northrop Grumman Aerospace Systems
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IntroITAR-Restricted SessionsOn Tuesday, a limited number of oral presentations and papers will be presented in “U.S. Only” technical sessions. In addition to your forum registration, a separate registration process is required to attend these restricted sessions. Please see the detailed information on the ITAR Registration Grid below to determine your individual requirements.
Access to ITAR Sessions: Presenting a Paper, Chairing a Session, or Attending an ITAR-Restricted PresentationAdmittance to the restricted technical program is controlled by the U.S. International Traffic in Arms Regulations (ITAR). All attendees, presenters, and session chairs will need to register for the conference, and then visit the ITAR registration desk to complete the additional processes. Anyone wishing to enter the restricted session room MUST abide by the procedures and submission of verified documents mandated by the DoD. No Exceptions!
Availability of Manuscripts from ITAR-Restricted SessionsFor those who are registered to attend the sessions, a DVD containing the papers from the ITAR sessions will be available for purchase on site at the forum for $25. Those purchasing the DVD must be available to pick it up on Wednesday, 24 June 2015. All DVDs must be picked up in person. There will be no sale or distribution of these papers after the event.
ITAR Electronics PolicyNo phones, computers (other than the presenter), iPads, cameras, or other electronic devices with cameras or recording capabilities will be permitted into the ITAR session room. There will be a check-in desk in front of the room where you can check these devices.
ITAR Information
10/19/2012
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.
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IntroExposition Hall
Exhibitors by Booth Number
217 AIAA North Texas Section420 Altair213 ANSYS410 Applied Dynamics International (ADI)403 BETA CAE Systems USA, Inc.219 DARcorporation209 Desktop Aeronautics207 dSPACE408 DUNMORE Corporation208 Ennova Technologies, Inc.215 ESI North America211 ESTECO404 Exa Corporation307 G.R.A.S. Sound & Vibration412 Kamatics/RWG
314 Lockheed Martin320 MathWorks301 OPAL-RT Technologies401 Photron302 Pointwise, Inc.309 SG - Space & Ground Engineering Solutions303 Software Cradle304 Tecplot Inc.301 VectorNav Technologies416 Vision Research414 XFlow CFD
ENTRANCE
208 307 408
309 410
LoungeExhibitor
ADIDesktop
DUNMORE
30
SG
Altair
301 302
303 304
Software
MathWorks
ANSYS
dSPACE
Cradle
OPAL-RT Pointwise
Tecplot
XFlow CFD
Ennova
401
403 404
BETA CAE
Photron
G.R.A.S.
Exa Corp
Kamatics/RWG
AIAA Pavilion
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IntroThe Exposition Hall is the hub of activity during this event—from seeing exhibitor displays to enjoying networking breaks and other functions. All the major networking events are held in the Exposition Hall to give attendees and exhibitors an opportunity to connect with partners, industry thought leaders, and collaborators who can help move your business forward. The Exposition Hall is located in the Chantilly Ballroom East.
Exposition Hall HoursTuesday, 23 June 0900–1230 hrs
1400–1600 hrs Reception* 1730–1900 hrs
Wednesday, 24 June 0900–1200 hrs 1230–1600 hrs
Thursday, 25 June 0900–1200 hrs
*A ticket is required and included in the registration fee where indicated
AIAA PavilionStop by the AIAA Pavilion, located in the Exposition Hall, to browse publications and merchandise, learn about your membership benefits, and meet AIAA staff.
30% Off All Books at AIAA AVIATION 2015 AIAA Publications is offering a special show discount on all titles featured at AVIATION 2015. Attendees can take advantage of a 30% discount off the list price of all books for sale at the AIAA Bookstore located in the AIAA Pavilion. This show special will only be available during the forum! Take advantage of these super savings and visit the AIAA Bookstore!
Exposition Hall
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ExhibitorsAIAA North Texas Section 217
Altair 4201820 E Big Beaver Road Troy, MI [email protected]
Altair is a leader in developing simulation-driven designs for leading aerospace customers. Our world-class optimization methods provide designs that are lower weight, higher quality, and have better performance vs. traditional designs.
ANSYS, Inc. 2132600 ANSYS Drive Cannonsburg, PA 15317 [email protected]
ANSYS, Inc. develops and globally markets engineering simulation software used by designers and engineers across the aerospace and defense industry. Our open and flexible simulation solutions enable users to simulate design performance using an open platform for fast, efficient and cost-effective product development.
Applied Dynamics International 4103800 Stone School Road Ann Arbor, MI [email protected]
Applied Dynamics helps companies make better use of simulation assets through all stages of product development, verification testing, demonstration, training, and maintenance. Our user base includes more than 50% of the Fortune 500 aerospace and defense companies and extends into marine, power systems, oil & gas, and the automotive industry.
BETA CAE Systems USA, Inc. 40329800 Middlebelt Road Suite #100Farmington Hills, MI [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.
DARcorporation 2191440 Wakarusa Drive Lawrence, KS [email protected]
DARcorporation (Design, Analysis and Research Corporation) is an aeronautical engineering firm, located in Lawrence, Kansas, that has been offering aeronautical engineering consulting services, software and books since 1991.
Desktop Aeronautics Inc. 2091900 Embarcadero Road Suite 101Palo Alto, CA [email protected]
Desktop Aeronautics is a software company that licenses tools for the aerodynamic design and analysis of aerospace vehicles. Our flagship product, GoCart, is an intuitive aerial vehicle design tool built around NASA’s renowned Cartesian Euler CFD solver, Cart3D. Our customers include major players from the aerospace industry and academia.
dSPACE 20750131 Pontiac Trail Wixom, MI [email protected]
dSPACE is the world’s leading provider of hardware and software tools for developing and testing sophisticated electronic control systems. dSPACE systems play a vital role in product innovation industries. Learn more at: www.dspaceinc.com.
DUNMORE Corporation 408145 Wharton Road
R
Bristol, PA [email protected]
DUNMORE is a manufacturer of engineered films and tapes for aerospace, supplying multilayer insulation materials to the aerospace industry for over twenty-five years. With a highly technical product base of over 400 certified products, DUNMORE is the trusted source for engineered aerospace films and tapes.
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Ennova Technologies Inc 2082150 Allston Way, Suite 250
EnnovaScalable Simulation Delivered
Berkeley, CA [email protected]
Ennova Technologies delivers today’s most scalable simulation platform combining the power of cloud based computing, advanced geometry repair tools, and mixed mode meshing to create an extremely efficient pre and post processing simulation environment.
ESI North America 21532605 West Twelve Mile Road, Ste 350 Farmington Hills, MI [email protected]
ESI’s 1,000 Virtual Prototyping and Mfg Simulation specialists serve clients in over 40 countries. For over 40 years, ESI’s simulation software suite has been used to tackle the toughest Acoustics, Crash, VR, Composites, Casting, Welding, Forming, and CFD engineering challenges—earning the slogan “We get it right.” For more info: www.esi-group.com
ESTECO 21139555 Orchard Hill Place Novi, MI [email protected]
ESTECO is a pioneer in numerical optimization solutions, specializing in the research and development of engineering software for all stages of the simulation-driven design process. ESTECO’s top-class products, modeFRONTIER and SOMO, are used worldwide, helping companies increase efficiency in design simulation and accelerate product innovation.
Exa Corporation 40455 Network Drive Burlington, MA [email protected]
Exa Corporation offers a full suite of CFD/CAE simulation design optimization software applications with aerodynamic, 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 process, therefore creating competitive designs, shortening product design cycles and speeding time-to-market.
G.R.A.S. Sound & Vibration 3072234 E Enterprise Parkway Twinsburg, OH [email protected]
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.
Kamatics/RWG 4121330 Blue Hills Ave Bloomfield, CT 06002www.kaman.com/[email protected]
For decades, Kamatics (USA) and RWG have been designing, testing, and manufacturing the highest performing bearings and flight critical parts in the industry, excelling under the most demanding conditions.
Lockheed Martin Corporation 314P.O. Box 748 MZ 1500 Fort Worth, TX 76101 www.lockheedmartin.com [email protected]
Lockheed Martin is principally engaged in the research, design, development, manufacture, integration and sustainment of advance technology systems, products and services.
MathWorks 3203 Apple Hill Drive Natick, MA 01760www.mathworks.com/academia
The MATLAB and Simulink product families are fundamental applied math and computational tools at the world’s educational institutions. Adopted by more than 5000 universities and colleges, MathWorks products accelerate the 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 used for data analysis, mathematical modeling, and algorithm development in collaborative research and new product development.
Exhibitors
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IntroOPAL-RT TECHNOLOGIES 3011751 Richardson, Suite 2525 Montreal Quebec H3K [email protected]
OPAL-RT: From Imagination… to Real-Time. OPAL-RT TECHNOLOGIES is a world leading developer of open, Real-Time Digital Simulators and Hardware-in-the-Loop testing equipment for electrical, electro-mechanical and power electronics systems. Our simulators are used by engineers and researchers at leading manufacturers, utilities, universities and research centers around the world.
Photron 4019520 Padgett Street, Suite 110 San Diego, CA [email protected]
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.
Pointwise, Inc. 302213 S. Jennings Avenue Fort Worth, TX [email protected]
Pointwise is solving the top problem facing engineering analysts today: grid generation and preprocessing for computational fluid dynamics. Since 1994, Pointwise has supplied meshing tools to engineers and scientists worldwide.
SG-Space & Ground Engineering Solutions 3096A Aigiidon Street Athens, Attica Greece [email protected]
SG Company provides integrated engineering solutions for air/space-based earth monitoring systems and develops special techniques for UAS (Unmanned Aerial Systems) earth observation applications in various disciplines.
Software Cradle 30370 Birch Alley, Suite 240 Beavercreek, OH [email protected]
Software Cradle is a leading provider of Computational Fluid Dynamics (CFD) software including SC/Tetra (unstructured mesh), scSTREAM (general purpose Cartesian mesh), and Heat Designer (Cartesian mesh for electronics). Since inception in 1984, Cradle has established itself as a major innovator for advancing the role of simulation in engineering design.
Tecplot, Inc 3043535 Factoria Blvd SE, Suite 550 Bellevue, WA [email protected]
Tecplot visualization tools—for simulations, analyses, and experiments—provide insight and understanding into the mechanisms inside your data. Information critical in pinpointing problems, optimizing designs, and explaining physical observations.
VectorNav Technologies 30110501 Markison Road Dallas, TX [email protected]
VectorNav specializes in high-performance inertial navigation systems using the latest MEMS sensor and GPS/GNSS technology. Since its founding in 2008, we have been providing customers worldwide fully calibrated inertial sensors with aerospace-grade filtering technology, expanding the possibilities of today’s inertial navigation technology.
Vision Research 416100 Dey Road Wayne, NJ 07470 www.visionresearch.com [email protected]
Vision Research designs and manufactures high-speed digital imaging systems with unsurpassed light-sensitivity, image resolution, acquisition speed and image quality. Marketed under the Phantom®brand,these cameras enable users to visualize and analyze physical phenomena when it’s too fast to see, and too important not to™.
XFlow CFD 41440 Chellis Street White River Junction, VT 05001 www.xflowusa.com [email protected].
XFlow™ CFD is the next-generation, meshless CFD package for modeling external aerodynamics of fixed-wing and rotorcraft aircraft. XFlow supports complex motion of complicated moving parts to model dynamic effects of control surface motion in flight, high-lift (take-off and landing) configurations and/or separation of munitions or separable stores.
Exhibitors
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IntroGeneral InformationAIAA Registration and Information Center HoursThe AIAA Registration and Information Center will be located on the Ballroom Level at the Hyatt Regency. Hours are as follows:Sunday, 21 June 1500–1900 hrsMonday, 22 June – Thursday, 25 June 0700–1730 hrsFriday, 26 June 0700–1200 hrs
Wi-Fi Internet Access On SiteAIAA is providing limited Wi-Fi service for attendees to use while on site. To keep this service available and optimized for all attendees, please do not download files larger than 2MB, create multiple sessions across multiple devices, or download multiple files in one session. If you receive an error message that an AIAA server is blocking your current IP address, please inform the AIAA registration desk.
Social Media KiosksThroughout the forum, social media kiosks will display content shared by forum attendees! Look for your tweets or instagrams to be displayed on the screens. AIAA is also hosting a competition where the user who has posted the most tweets during the forum will win a prize.
Conference ProceedingsProceedings for the forum will be available online. The cost is included in the registration fee where indicated. Online proceedings will be available on 22 June 2015. Attendees who register in advance for the online proceedings will be provided with instructions on how to access them. Those registering on site will be provided with instructions at that time. Proceedings:1. To view proceedings visit
www.aiaa.org >ARC>Meeting Papers.a. Log in with the link at the top right of the page.b. Select the appropriate conference from the list.c. Search for individual papers with the Quick Search
toolbar in the upper-right corner of the page:i. By paper number: Click the “Paper Number” link,
select the conference year, and enter the paper number. ii. Use the Search textbox to find papers by author, title,
or keyword. The Advanced Search link provides additional search information and options.
2. All manuscript files submitted at least four days prior to the conference are currently in the proceedings. Files submitted after that date, both original and revised manuscripts, will not be available until the final proceedings update, which may take up to 15 business days after the last day of the conference.
3. Direct any questions concerning access to proceedings and/or ARC to [email protected].
Manuscript Revisions:1. Manuscript revision is open for all presenting authors from
0900 hrs Eastern Time, Monday, 22 June, through 2000 hrs Eastern Time, Wednesday, 8 July.
2. Revisions submitted for manuscripts already online will not refresh until after the proceedings have been updated, which may take up to 15 business days after the last day of the conference.
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IntroGeneral InformationCertificate of Attendance Certificates of Attendance are available for attendees who request documentation at the forum itself. The Certificates of Attendance will be available for attendees to print at a self-service station at the registration desk starting Wednesday, 24 June. AIAA offers this service to better serve the needs of the professional community. Claims of hours or applicability toward professional education requirements are the responsibility of the participant.
Employment OpportunitiesAIAA members can post and browse resumes, browse job listings, and access other online employment resources by visiting the AIAA Career Center at http://careercenter.aiaa.org. Additionally, a message board will be available for postings in the Exposition Hall.
MembershipAIAA is your vital lifelong link to the collective creativity and brainpower of the aerospace profession and a champion for its achievements – and nonmembers who pay the full conference registration fee will receive their first year’s AIAA membership at no additional cost! Students who are not yet members may apply their registration fee toward their first year’s student member dues. (Free membership is not included in discounted group-rate registration.)
AIAA Foundation Since 1996 the AIAA Foundation has provided programs and support for educators and students. Through classroom grants, scholarships, awards, design competitions, and student conferences, the AIAA Foundation has encouraged students in grades K-12 and at the university level to discover the aerospace industry and become the next generation of scientists and engineers. Please consider making a donation so that the Foundation can continue to provide the resources needed to support aerospace education and to recognize innovation at all levels. For more information and to donate online, please visit www.aiaafoundation.org.
Young Professional Guide for Gaining Management SupportYoung professionals have the unique opportunity to meet and learn from some of the most important people in the business by attending conferences and participating in AIAA activities. A detailed online guide, published by the AIAA Young Professional Committee, is available to help you gain support and financial backing from your company. The guide explains the benefits of participation, offers recommendations, and provides an example letter for seeking management support and funding, and shows you how to get the most out of your participation. The online guide can be found on the AIAA website at www.aiaa.org/YPGuide.
Nondiscriminatory PracticesAIAA accepts registrations irrespective of race, creed, gender, color, sexual orientation, physical handicap, and national or ethnic origin.
RestrictionsPhotos, video, or audio recording of sessions or exhibits, as well as the unauthorized sale of AIAA-copyrighted material, is prohibited.
International Traffic in Arms Regulations (ITAR)AIAA speakers and attendees are reminded that some topics discussed in the conference could be controlled by the International Traffic in Arms Regulations (ITAR). U.S. nationals (U.S. citizens and permanent residents) are responsible for ensuring that technical data they present in open sessions to non-U.S. nationals in attendance or in conference proceedings are not export restricted by the ITAR. U.S. nationals are likewise responsible for ensuring that they do not discuss ITAR export-restricted information with non-U.S. nationals in attendance.
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IntroGeneral Information
AIAA is the world’s largest aerospace professional society, serving a diverse range of more than 30,000 individual members from 88 countries, and 95 corporate members. AIAA members help make the world safer, more connected, more accessible, and more prosperous. For more information, visit www.aiaa.org, or follow us on Twitter @AIAA.American Institute of Aeronautics and Astronautics 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
Speakers’ Briefings in Session RoomsAuthors who are presenting papers will meet with session chairs and co-chairs in their session rooms for a short 30-minute briefing on the day of their sessions to exchange bios and review final details prior to the session. Please attend on the day of your session(s). Laptops preloaded with the Speaker Briefing preparation slides will be provided in each session room. Speaker’s Briefing schedule is as follows:Monday 22 June–Friday 26 June, 0730 hrs
Speakers’ Practice RoomSpeakers who wish to practice their presentations may do so in the Peridot room. A sign-up sheet will be posted on the door. In consideration of others, please limit practice time to 30-minute increments.
Session Chair ReportsAll session chairs are asked to complete a session chair report to evaluate their session for future planning. AIAA has partnered with Canvas Solutions to provide an electronic Session Chair Report form. You can download the FREE mobile app in your App Store, AppWorld, or Marketplace by searching for “Canvas Solutions, Inc.” The mobile app is free, so please be sure to download it. Detailed instructions will be provided in the session rooms. If you do not have a tablet or a smartphone, simply use the report form as a guide and enter your session chair report information at the session chair reporting computer station located on site near the AIAA registration area. Report data will be collected and used for future planning purposes, including session topics and room allocations. Please submit your session chair report electronically by Friday, 26 June 2015.
AudiovisualEach session room will be preset with the following: one LCD projector, one screen, one microphone and sound system (if necessitated by room size), and one laser pointer. Laptop computers will also be provided. You may also use your own computer. Any additional audiovisual equipment requested onsite will be at cost to the presenter. Please note that AIAA does not provide security in the session rooms and recommends that items of value not be left unattended
“No Paper, No Podium” and “No Podium, No Paper” PolicyIf a written paper is not submitted by the final manuscript deadline, authors will not be permitted to present the paper at the forum. Also, if the paper is not presented at the forum, it will be withdrawn from the proceedings. It is the responsibility of those authors whose papers or presentations are accepted to ensure that a representative attends the conference to present the paper. These policies are intended to improve the quality of the program for attendees..
Journal PublicationAuthors of appropriate papers are encouraged to submit them for possible publication in one of the Institute’s archival journals: AIAA Journal; Journal of Aircraft; Journal of Guidance, Control, and Dynamics; Journal of Propulsion and Power; Journal of Spacecraft and Rockets; Journal of Thermophysics and Heat Transfer; or Journal of Aerospace Information Systems (formerly Journal of Aerospace Computing, Information, and Communication). You may now submit your paper online at http://mc.manuscriptcentral.com/aiaa.
Author and Session Chair Information
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IntroTime Title Location
Sunday, 21 June 20150900-1600 CASE Academics Batik A & B
1400-1500 GTTC Steering Subcommittee Miro
1400-1500 APATC New Member Orientation Dardanelles
1430-1500 APATC Liaisons Subcommittee Fleur de lis A
1500-1600 APATC Education Subcommittee Milan
1500-1600 APATC Honors and Awards Subcommittee Ming
1500-1600 APATC Membership and Nominations Subcommittee Inverness
1500-1600 APATC Planning Subcommittee Lalique
1500-1600 APATC Publicity and Publications Subcommittee Edelweiss
1500-1600 GTTC Introduction/Overview Miro
1600-1700 GTTC Program Subcommittee Miro
1600-1700 APATC Technical Activities Meeting Edelweiss
1600-1700 FDTC Higher Order Methods WG Dardanelles
1700-1800 APATC Steering Committee Ming
1700-1800 GTTC Conferences Subcommittee Miro
1730-1830 FDTC New Member Orientation Fleur de lis A
1730-2100 Atmospheric Flight Mechanics TC Dardanelles
1800-1900 GTTC Publications Subcommittee Miro
1800-2100 Applied Aerodynamics TC Metropolitan
1830-2000 FDTC Steering Committee Fleur de lis A
1900-2000 GTTC Education and Student Activities Subcommittee Miro
1900-2100 FDTC Transition DG Cardinal A
1900-2100 TAC Aircraft and Atmospheric Systems Group Cardinal B
2000-2100 GTTC Awards Subcommittee Miro
2000-2100 AMTTC Conference Subcommittee Milan
Monday, 22 June 20150800-1200 GTTC WT Model Attitude and Deformation Measurement WG Dardanelles
1100-1400 General Aviation TC Morocco
1200-1400 Aircraft Electric Propulsion Path Forward Batik B
1200-1400 Aviation MDO SPC Dardanelles
1300-1500 GTTC FoGT Experimental and Computational Aero Development Coordination
Cardinal A & B
1500-1600 FDTC Reduced Order Modeling DG Dardanelles
1600-1700 TPTC New Member Meeting Cooper
1600-1700 FDTC Flow Control - Barriers/Challenges to Tech Trans Cardinal A
1630-1800 Atmospheric and Space Environments TC Batik A
1700-1900 Computational Fluid Dynamics Committee on Standards Batik B
1730-1830 GTTC Committee on Standards Cardinal A
1730-1830 APATC Low Boom DG Cooper
1730-1900 APATC Validation of Numerical Models DG Dardanelles
1830-1930 AMTTC Awards Subcommittee Batik A
1830-2030 APATC Rotorcraft Simulations and Performance Predictions DG Cardinal B
Committee Meetings
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IntroTime Title Location
Monday, 22 June 2015 (continued) 1900-2100 TAC Aerospace Sciences Group Batik B
1900-2100 FDTC Computational Fluid Dynamics Subcommittee Dardanelles
1900-2100 FDTC Flow Control and Fluid Applications Subcommittee Cardinal A
1900-2100 FDTC Fundamentals of Flow Phenomena Subcommittee Cooper
1900-2200 Aircraft Design TC Monte Carlo
Tuesday, 23 June 20150800-1600 GTTC Internal Balance WG Cooper
0800-1600 GTTC Dual Flow Reference Nozzle WG - Day 1 Batik A
0930-1200 DETC Subcommittee Batik B
1400-1500 Journal of Thermophysics and Heat Transfer Malta
1500-1600 TPTC Awards Subcommittee Cardinal A
1500-1600 TPTC Publications Subcommittee Dardanelles
1600-1700 TPTC Conferences Subcommittee Cardinal A
1600-1700 TPTC Best Paper Subcommittee Batik B
1700-1800 TPTC Nominations Subcommittee Cardinal A
1700-1800 TPTC Education Subcommittee Cooper
1730-1900 FDTC Low Re DG Dardanelles
1800-1900 FDTC Free Shear Layer Mixing Layer Control DG Batik A
1800-1900 TPTC Publicity Subcommittee Cooper
1800-2100 Design Engineering TC Batik B
1900-2000 APATC Low Reynolds Number Aerodynamics DG Dardanelles
1900-2200 Air Transportation Systems TC Monte Carlo
1900-2200 MVCETC Meshing 2030 Subcommittee Batik A
1900-2200 Fluid Dynamics TC Cardinal A & B
1900-2200 Thermophysics TC Monet Ballroom
1900-2200 Plasmadynamics and Lasers TC Rosetta
1930-2130 Aeroacoustics TC Miro
2000-2300 Aerodynamic Measurement Technology TC Cooper
Wednesday, 24 June 20150800-1200 GTTC Future of Ground Testing WG Cardinal A & B
0800-1200 GTTC Dual Flow Reference Nozzle WG - Day 2 Cooper
1200-1600 GTTC Uncertainty Analysis WG Cooper
1500-1600 AVIATION 2016 Technical Program Committee Dardanelles
1730-1900 GTTC Student Meet and Greet Stemmons A
1730-1830 FDTC Large Eddy Simulation DG Monte Carlo
1730-1830 Green Engineering PC Malta
1800-1900 FDTC Future of Fluids Subcommittee Cooper
1800-1900 FDTC Turbulence Model Benchmarking WG Cardinal A
1830-2000 Plasma Aerodynamics DG Cardinal B
1830-1930 AMTTC Nominations Subcommittee Edelweiss
1830-2000 FDTC Non-Equilibrium DG Dardanelles
1830-2200 Multidisciplinary Design Optimization TC Batik A & B
1900-2000 FDTC Solver Technology for Turbulent Flows Cardinal A
1900-2200 V/STOL Aircraft Systems TC Cooper
1900-2200 Meshing, Visualization and Computational Environments TC Fleur de lis B
Committee Meetings
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IntroTime Title Location
Thursday, 25 June 20150900-1100 CASE Planning Committee Monte Carlo
0900-1700 GTTC Wind Tunnel Flow Quality WG Cooper
1600-1730 APATC Missile and Projectile Aeroprediction DG Dardanelles
1730-1830 AMTTC Conferences Subcommittee Milan
1800-2100 Ground Testing TC Cardinal A & B
1800-2100 Transformational Flight PC Batik A & B
1830-2130 Modeling and Simulation TC Cooper
1900-2200 Flight Testing TC Coral
Committee Meetings
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IntroSessions at a GlanceAbbreviation Title Date Start Time Location
Aeroacoustics3-AA-1 Airframe Noise I 22-Jun 0900 hrs Fleur-de-lis A
4-AA-2 Jet Noise Prediction I 22-Jun 0900 hrs Fleur-de-lis B
5-AA-3 Jet Noise Modeling I 22-Jun 0900 hrs Inverness
6-AA-4 CAA Numerical Techniques I 22-Jun 0900 hrs Lalique
7-AA-5 Duct Acoustics I 22-Jun 0900 hrs Obelisk A
37-AA-6 Open Rotor I 22-Jun 1400 hrs Fleur-de-lis A
38-AA-7 Trailing Edge Noise I 22-Jun 1400 hrs Fleur-de-lis B
39-AA-8 Jet Noise Prediction II 22-Jun 1400 hrs Inverness
40-AA-9 Jet Noise Measurements I 22-Jun 1400 hrs Lalique
41-AA-10 CAA Sound Generation I 22-Jun 1400 hrs Obelisk A
77-AA-11 Fan Noise 23-Jun 0900 hrs Fleur-de-lis A
78-AA-12 Duct Acoustics II 23-Jun 0900 hrs Fleur-de-lis B
79-AA-13 Trailing Edge Noise II 23-Jun 0900 hrs Inverness
80-AA-14 Jet Noise Prediction III 23-Jun 0900 hrs Lalique
81-AA-15 CAA Numerical Techniques II 23-Jun 0900 hrs Obelisk A
112-AA-16 CAA Sound Generation II 23-Jun 1400 hrs Fleur-de-lis A
113-AA-17 CAA Propagation and Scattering I 23-Jun 1400 hrs Fleur-de-lis B
114-AA-18 General Acoustics I 23-Jun 1400 hrs Inverness
115-AA-19 Airframe Noise II 23-Jun 1400 hrs Lalique
116-AA-20 Duct Acoustics III 23-Jun 1400 hrs Obelisk A
151-AA-21 Turbomachinery and Core Noise 24-Jun 0900 hrs Fleur-de-lis B
152-AA-22 General Acoustics II 24-Jun 0900 hrs Inverness
153-AA-23 Jet Noise Near Field and Jet Noise Reduction 24-Jun 0900 hrs Lalique
154-AA-24 CAA Propagation and Scattering II 24-Jun 0900 hrs Obelisk A
155-AA-25 Benchmark Problems for Airframe Noise Computations III (BANC-III) Summary (Invited) 24-Jun 0900 hrs Fleur-de-lis A
185-AA-26 Combustion Noise 24-Jun 1400 hrs Fleur-de-lis B
186-AA-27 Arrays Method Panel Session 24-Jun 1400 hrs Fleur-de-lis A
187-AA-28 Open Rotor II 24-Jun 1400 hrs Inverness
188-AA-29 Airframe Noise III 24-Jun 1400 hrs Lalique
189-AA-30 Jet Noise Measurements II 24-Jun 1400 hrs Obelisk A
226-AA-31 Interior Noise 25-Jun 0900 hrs Edelweiss
227-AA-32 Jet Noise Measurements III 25-Jun 0900 hrs Fleur-de-lis A
228-AA-33 Jet Noise Modeling II 25-Jun 0900 hrs Fleur-de-lis B
229-AA-34 CAA Numerical Techniques III 25-Jun 0900 hrs Inverness
230-AA-35 Airframe Noise IV 25-Jun 0900 hrs Lalique
231-AA-36 General Acoustics III 25-Jun 0900 hrs Obelisk A
259-AA-37 Landing Gear Noise 25-Jun 1400 hrs Edelweiss
260-AA-38 Fluid-Structure Interaction 25-Jun 1400 hrs Fleur-de-lis A
261-AA-39 Fluid Acoustic Phenomena 25-Jun 1400 hrs Fleur-de-lis B
262-AA-40 Advanced Testing Techniques 25-Jun 1400 hrs Inverness
263-AA-41 CAA Numerical Techniques IV 25-Jun 1400 hrs Lalique
264-AA-42 Fan Broadband Noise Prediction 25-Jun 1400 hrs Obelisk A
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IntroSessions at a GlanceAbbreviation Title Date Start Time Location
Aircraft Design42-ACD-1 Aircraft Design for Environmental Impact Reduction 22-Jun 1400 hrs Miro
82-ACD-2 Aircraft Design Methods and Tools 23-Jun 0900 hrs Wyeth
117-ACD-3 Aircraft Performance Studies 23-Jun 1400 hrs Wyeth
156-ACD-4 General Aviation 24-Jun 0900 hrs Morocco
190-ACD-5 Design of Unconventional Aircraft Configurations 24-Jun 1400 hrs Morocco
232-ACD-6 Conceptual Aircraft Design Working Group (CADWG21) Panel 25-Jun 0900 hrs Wyeth
265-ACD-7 Aircraft Subsystems, Integration, and Architectures 25-Jun 1400 hrs Wyeth
293-ACD-8 Aeronautic Discipline Considerations in Aircraft Design 26-Jun 0900 hrs Miro
Atmospheric Flight Mechanics8-AFM-1 Aircraft Flight Dynamics, Control, Handling Qualities and Performance I 22-Jun 0900 hrs Plum Blossom A
9-AFM-2 Aeroservoelastic (ASE) Modeling 22-Jun 0900 hrs Plum Blossom B
43-AFM-3 Unmanned Aircraft Systems I 22-Jun 1400 hrs Plum Blossom A
44-AFM-4 Planetary Entry and Aeroassist Technology 22-Jun 1400 hrs Plum Blossom B
83-AFM-5 Aircraft Flight Dynamics, Control, Handling Qualities and Performance II 23-Jun 0900 hrs Plum Blossom A
84-AFM-6 Aeroservoelastic (ASE) and Aerodynamic Prediction Methods 23-Jun 0900 hrs Plum Blossom B
118-AFM-7 Flight Test, System Identification, and Parameter Estimation 23-Jun 1400 hrs Plum Blossom A
119-AFM-8 Launch Vehicles, Missiles, and Projectile Flight Mechanics 23-Jun 1400 hrs Plum Blossom B
157-AFM-9 Unmanned Aircraft Systems II 24-Jun 0900 hrs Plum Blossom A
Aerodynamic Measurement Technology and Ground Testing10-AMT-1/GT-1 Hap Arnold's New Horizon: The Future Role of Ground Test in High Speed System
Development22-Jun 0900 hrs Obelisk B
11-AMT-2/GT-2 Line of Sight and Density Measurement 22-Jun 0900 hrs Edelweiss
45-AMT-3/GT-3 Advances in Test Methodology and CFD Integration 22-Jun 1400 hrs Obelisk B
46-AMT-4/GT-4 Surface and Inflow Sensing 22-Jun 1400 hrs Edelweiss
85-AMT-5/GT-5 Model Attitude, Deformation, and Data Acquisition Techniques 23-Jun 0900 hrs Obelisk B
86-AMT-6/GT-6 Spatially-Resolved Spectroscopic Techniques 23-Jun 0900 hrs Edelweiss
120-AMT-7/GT-7 Design of Experiment 23-Jun 1400 hrs Obelisk B
121-AMT-8/FD-14/TP-6/GT-8
Molecular-Based Optical Diagnostics for Hypersonic Nonequilibrium Flows 23-Jun 1400 hrs Topaz
158-AMT-9/GT-9 Ground Test Facility Improvements I 24-Jun 0900 hrs Obelisk B
159-AMT-10/GT-10 Particle-Based Velocimetry Applications and Developments 24-Jun 0900 hrs Topaz
191-AMT-11/GT-11 Ground Test Facility Improvements II 24-Jun 1400 hrs Obelisk B
192-AMT-12/GT-12 The Impact of PIV on Aerospace Technology I 24-Jun 1400 hrs Edelweiss
266-AMT-13/GT-13 The Impact of PIV on Aerospace Technology II 25-Jun 1400 hrs Topaz
280-FT-2/GT-14 Optimization Techniques in Flight Test/Ground Test 25-Jun 1400 hrs Obelisk B
294-AMT-14/GT-15 Aerodynamic Measurement Systems: Calibration and Monitoring 26-Jun 0900 hrs Topaz
Applied Aerodynamics12-APA-1 Aerodynamic-Structure Dynamics Interaction 22-Jun 0900 hrs Stemmons C
13-APA-2 Aerodynamic Design Methodologies I 22-Jun 0900 hrs Carpenter Ballroom
14-APA-3 Special Session: Low Boom Activities I 22-Jun 0900 hrs Stemmons A
15-APA-4 Propeller/Rotorcraft/Wind Turbine Aerodynamics I 22-Jun 0900 hrs Stemmons B
47-APA-5 Applied CFD & Numerical Correlations with Experimental Data I 22-Jun 1400 hrs Stemmons B
48-APA-6 Unmanned, Bio-Inspired, Solar Powered Aerial Vehicle Designs I 22-Jun 1400 hrs Carpenter Ballroom
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IntroSessions at a GlanceAbbreviation Title Date Start Time Location
Applied Aerodynamics (continued)49-APA-7 Special Session: Aerodynamic-Structural Modeling, Optimization, and Test Techniques for
Flexible Wing Technology I22-Jun 1400 hrs Stemmons A
50-APA-8 Flow Control Applications & Demonstrations (Active & Passive) I 22-Jun 1400 hrs Stemmons C
87-APA-9 High Angle of Attack and High Lift Aerodynamics 23-Jun 0900 hrs Stemmons C
88-APA-10 Wind Tunnel and Flight Testing 23-Jun 0900 hrs Carpenter Ballroom
89-APA-11 Special Session: Low Boom Activities II 23-Jun 0900 hrs Stemmons A
90-APA-12 Weapons Aerodynamics: Missile/Projectile/Guided-Munitions, Carriage and Store Separation I 23-Jun 0900 hrs Stemmons B
122-APA-13 Applied CFD & Numerical Correlations with Experimental Data II 23-Jun 1400 hrs Stemmons B
123-APA-14 Special Session: Historically Significant/Influential Papers in Applied Aerodynamics 23-Jun 1400 hrs Carpenter Ballroom
124-APA-15 Special Session: Aerodynamic-Structural Modeling, Optimization, and Test Techniques for Flexible Wing Technology II
23-Jun 1400 hrs Stemmons A
125-APA-16 Flow Control Applications & Demonstrations (Active & Passive) II 23-Jun 1400 hrs Stemmons C
160-APA-17 Special Session: Hybrid CFD Method Assessments for F-16XL Aircraft Aerodynamics 24-Jun 0900 hrs Stemmons A
161-APA-18 Aerodynamic Design Methodologies II 24-Jun 0900 hrs Carpenter Ballroom
162-APA-19 Propeller/Rotorcraft/Wind Turbine Aerodynamics II 24-Jun 0900 hrs Stemmons B
180-PDL-8/APA-20 Plasma Aerodynamics & Flow Control IV 24-Jun 0900 hrs Stemmons C
193-APA-21 Transonic & Supersonic Aerodynamics 24-Jun 1400 hrs Stemmons A
194-APA-22 VSTOL/STOL Aerodynamics 24-Jun 1400 hrs Carpenter Ballroom
195-APA-23 Weapons Aerodynamics: Missile/Projectile/Guided-Munitions, Carriage and Store Separation II 24-Jun 1400 hrs Stemmons B
233-APA-25 Applied CFD & Numerical Correlations with Experimental Data III 25-Jun 0900 hrs Stemmons B
234-APA-26 Unmanned, Bio-Inspired, Solar Powered Aerial Vehicle Designs II 25-Jun 0900 hrs Carpenter Ballroom
235-APA-27 Airfoil/Wing/Configuration Aerodynamics 25-Jun 0900 hrs Stemmons C
236-APA-28 Unsteady Aerodynamics I 25-Jun 0900 hrs Stemmons A
267-APA-29 Innovative Aerodynamic Concepts & Designs 25-Jun 1400 hrs Carpenter Ballroom
268-APA-30 Low Speed, Low Reynolds Number Aerodynamics 25-Jun 1400 hrs Grand Ballroom A
269-APA-31 Vortical/Vortex Flow 25-Jun 1400 hrs Stemmons B
270-APA-32 Unsteady Aerodynamics II 25-Jun 1400 hrs Stemmons A
271-APA-33 Flow Control Applications & Demonstrations (Active & Passive) III 25-Jun 1400 hrs Stemmons C
295-APA-34 Icing or Roughness Effects on Vehicle Aerodynamics 26-Jun 0900 hrs Stemmons C
296-APA-35 Aerodynamic Design Methodologies III 26-Jun 0900 hrs Carpenter Ballroom
297-APA-37 Propeller/Rotorcraft/Wind Turbine Aerodynamics III 26-Jun 0900 hrs Stemmons B
Atmospheric and Space Environments163-ASE-1 Numerical Weather Prediction (Invited) 24-Jun 0900 hrs Plum Blossom B
196-ASE-2 Aircraft Icing and Atmospheric Hazards 24-Jun 1400 hrs Plum Blossom B
237-ASE-3 Aircraft Wake Turbulence I (Invited) 25-Jun 0900 hrs Plum Blossom B
272-ASE-4 Aircraft Wake Turbulence II (Invited) 25-Jun 1400 hrs Plum Blossom B
273-ASE-5 Atmospheric and Space Environments 25-Jun 1400 hrs Plum Blossom A
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IntroAbbreviation Title Date Start Time Location
Aviation Technology, Integration, and Operations16-ATIO-1 Terminal & Surface Operations I 22-Jun 0900 hrs Manchester
17-ATIO-2 Separation Assurance 22-Jun 0900 hrs Ming
18-ATIO-3 Trajectory Optimization 22-Jun 0900 hrs Milan
19-ATIO-4 Transformational Flight - Rapid Concept to Flight 22-Jun 0900 hrs Metropolitan Ballroom
51-ATIO-5 Terminal & Surface Operations II 22-Jun 1400 hrs Manchester
52-ATIO-6 Fleet and Route Planning 22-Jun 1400 hrs Ming
53-ATIO-7 Systems Engineering and Analysis 22-Jun 1400 hrs Milan
54-ATIO-8 Transformational Flight - Enabling the Next Billion Dollar Aviation Market through Autonomy
22-Jun 1400 hrs Metropolitan Ballroom
91-ATIO-9 Terminal & Surface Operations III 23-Jun 0900 hrs Manchester
92-ATIO-10 ATM I - Trajectory Enhancements 23-Jun 0900 hrs Milan
93-ATIO-11 Transformational Flight - On-Demand Mobility 23-Jun 0900 hrs Metropolitan Ballroom
126-ATIO-12 ATM II - Air Traffic Analysis 23-Jun 1400 hrs Milan
127-ATIO-13 Transformational Flight - Advanced Concepts 23-Jun 1400 hrs Metropolitan Ballroom
128-ATIO-14 Product Design and Support 23-Jun 1400 hrs Manchester
164-ATIO-15 ATM III - Modeling in ATM 24-Jun 0900 hrs Metropolitan Ballroom
165-ATIO-16 Transformational Flight - Autonomy I 24-Jun 0900 hrs Monet Ballroom
166-ATIO-17 Human Factors in Aviation Operations 24-Jun 0900 hrs Milan
197-ATIO-18 ATM IV - Economic/Benefits Analysis 24-Jun 1400 hrs Ming
198-ATIO-19 Terminal & Surface Operations IV 24-Jun 1400 hrs Milan
199-ATIO-20 Transformational Flight - Autonomy II 24-Jun 1400 hrs Monet Ballroom
238-ATIO-21 En Route Operations 25-Jun 0900 hrs Milan
239-ATIO-22 ATM V - Performance Assessment 25-Jun 0900 hrs Morocco
240-ATIO-23 Transformational Flight - Electric Propulsion 25-Jun 0900 hrs Monet Ballroom
274-ATIO-24 UAS Integration & Operations I 25-Jun 1400 hrs Ming
275-ATIO-25 ATM VI - Management of NAS Resources 25-Jun 1400 hrs Morocco
276-ATIO-26 Transformational Flight - Unconventional VTOL Configurations 25-Jun 1400 hrs Monet Ballroom
298-ATIO-27 ATM VII - Weather Impact 26-Jun 0900 hrs Morocco
299-ATIO-28 Future Concepts 26-Jun 0900 hrs Wyeth
300-ATIO-29 UAS Integration & Operations II 26-Jun 0900 hrs Ming
Balloon Systems167-BAL-1 Balloon Systems I 24-Jun 0900 hrs Steuben
200-BAL-2 Balloon Systems II 24-Jun 1400 hrs Steuben
Complex Aerospace Systems Exchange (CASE)20-CASE-1 Academic Roundtable 22-Jun 0900 hrs Batik
59-F360-2/CASE-2 Whatever Happened to the Four-Year Airplane? 22-Jun 1400 hrs Grand Ballroom E
72-CASE-3 CASE Networking Social 22-Jun 1730 hrs Morocco
94-CASE-4 Applied Complexity Workshop 23-Jun 0900 hrs Grand Ballroom D
129-CASE-5 CASE Session I & II 23-Jun 1400 hrs Steuben
168-CASE-6 CASE Session II & III 24-Jun 0900 hrs Grand Ballroom D
207-F360-7/CASE-7 System Complexity : Government Needs and Practical Research Results 24-Jun 1400 hrs Grand Ballroom D
Sessions at a Glance
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IntroAbbreviation Title Date Start Time Location
Computational Fluid Dynamics 21-CFD-1 Unstructured High-Order Methods I 22-Jun 0900 hrs Grand Ballroom A
22-CFD-2 Unsteady Flow Simulations 22-Jun 0900 hrs Grand Ballroom B
23-CFD-3 Meshing Techniques I 22-Jun 0900 hrs Coral
24-CFD-4 LES, DNS, and Hybrid RANS-LES I 22-Jun 0900 hrs Emerald
55-CFD-5 Unstructured High-Order Methods II 22-Jun 1400 hrs Grand Ballroom A
56-CFD-6 Novel Discretizations 22-Jun 1400 hrs Grand Ballroom B
57-CFD-7 Interdisciplinary CFD I 22-Jun 1400 hrs Coral
58-CFD-8 Turbulence Modeling and Uncertainty Quantification 22-Jun 1400 hrs Emerald
95-CFD-9 Adaptive High-Order Methods 23-Jun 0900 hrs Grand Ballroom A
96-CFD-10 Turbulent Flow Simulations I 23-Jun 0900 hrs Grand Ballroom B
97-CFD-11 Meshing Techniques II 23-Jun 0900 hrs Coral
98-CFD-12 LES, DNS, and Hybrid RANS-LES II 23-Jun 0900 hrs Emerald
130-CFD-13 Flux Reconstruction Methods 23-Jun 1400 hrs Grand Ballroom A
131-CFD-14 Adjoints and Error Estimation 23-Jun 1400 hrs Grand Ballroom B
132-CFD-15 Time Integration Methods 23-Jun 1400 hrs Coral
133-CFD-16 RANS Modeling 23-Jun 1400 hrs Emerald
134-CFD-37 CFD Flow Visualization Showcase 23-Jun 1400 hrs Chantilly Ballroom Foyer
169-CFD-17 Advances in High-Order Methods 24-Jun 0900 hrs Grand Ballroom A
170-CFD-18 Current Trends in CFD Research I (Invited) 24-Jun 0900 hrs Grand Ballroom B
171-CFD-19 LES, DNS, and Hybrid RANS-LES III 24-Jun 0900 hrs Coral
172-CFD-20 Turbulence Model Validation (Invited) 24-Jun 0900 hrs Emerald
201-CFD-21 Discontinuous Galerkin Methods 24-Jun 1400 hrs Grand Ballroom A
202-CFD-22 Future of Fluids: Next Generation CFD (Invited) 24-Jun 1400 hrs Grand Ballroom B
203-CFD-23 Parallel Computing and Novel Architectures 24-Jun 1400 hrs Plum Blossom A
204-CFD-24 Design Optimization 24-Jun 1400 hrs Coral
205-CFD-25 Turbulent Flow Simulations II 24-Jun 1400 hrs Emerald
241-CFD-26 Unstructured High-Order Methods III 25-Jun 0900 hrs Grand Ballroom A
242-CFD-27 Current Trends in CFD Research II (Invited) 25-Jun 0900 hrs Grand Ballroom B
243-CFD-28 Incompressible and Low Speed Flows 25-Jun 0900 hrs Plum Blossom A
244-CFD-29 High-Speed and Reacting Flows 25-Jun 0900 hrs Coral
245-CFD-30 Inflow Turbulence for Wall-Bounded LES (Invited) 25-Jun 0900 hrs Emerald
301-CFD-31 Visualization for CFD 2030 26-Jun 0900 hrs Grand Ballroom A
302-CFD-32 Post-Processing and Model Reduction 26-Jun 0900 hrs Grand Ballroom B
303-CFD-33 Interdisciplinary CFD II 26-Jun 0900 hrs Plum Blossom A
304-CFD-34 Multiphase and Nonequilibrium Flows 26-Jun 0900 hrs Coral
305-CFD-35 Overset and Cartesian Grid Methods 26-Jun 0900 hrs Plum Blossom B
306-CFD-36 LES, DNS, and Hybrid RANS-LES IV 26-Jun 0900 hrs Emerald
Sessions at a Glance
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IntroSessions at a GlanceAbbreviation Title Date Start Time Location
Fluid Dynamics25-FD-1 Wing Aerodynamics 22-Jun 0900 hrs Govenors Lecture
Hall
26-FD-2 Fundamental Fluid Flows 22-Jun 0900 hrs Senators Lecture Hall
27-FD-3 Combustion and Heat Transfer 22-Jun 0900 hrs Topaz
28-FD-4 Boundary Layer Transition: Hypersonic Flows 22-Jun 0900 hrs Sapphire
33-PDL-1/FD-5 Plasma Aerodynamics & Flow Control I 22-Jun 0900 hrs Monet Ballroom
60-FD-6/PDL-2 Plasma Aerodynamics & Flow Control II 22-Jun 1400 hrs Govenors Lecture Hall
61-FD-7 Boundary Layer Transition - Progress and Challenges 22-Jun 1400 hrs Sapphire
62-FD-8 Vortex Flows 22-Jun 1400 hrs Senators Lecture Hall
63-FD-9 Active and Passive Flow Control 22-Jun 1400 hrs Topaz
99-FD-10 Boundary-Layer Transition 23-Jun 0900 hrs Sapphire
100-FD-11 Unsteady Wing Aerodynamics I 23-Jun 0900 hrs Govenors Lecture Hall
101-FD-12 Airfoil Separation Control 23-Jun 0900 hrs Senators Lecture Hall
102-FD-13 Shock-Dominated Flows 23-Jun 0900 hrs Topaz
121-AMT-8/FD-14/TP-6/GT-8
Molecular-Based Optical Diagnostics for Hypersonic Nonequilibrium Flows 23-Jun 1400 hrs Topaz
136-FD-15 Unsteady Wing Aerodynamics II 23-Jun 1400 hrs Govenors Lecture Hall
137-FD-16 Boundary Layer Transition: Crossflow 23-Jun 1400 hrs Sapphire
138-FD-17 Boundary Layer and Bluff Body Control 23-Jun 1400 hrs Senators Lecture Hall
139-FD-18 Turbulence Modeling 23-Jun 1400 hrs Edelweiss
173-FD-19 Turbomachinery - Turbines 24-Jun 0900 hrs Senators Lecture Hall
174-FD-20 Shock Wave / Boundary Layer Interactions 24-Jun 0900 hrs Edelweiss
175-FD-22 Unsteady Flows - Cavity and Shear Flows 24-Jun 0900 hrs Govenors Lecture Hall
208-FD-23 Unsteady Wing Aerodynamics III 24-Jun 1400 hrs Govenors Lecture Hall
209-FD-24 Boundary Layer Transition: Receptivity and Control 24-Jun 1400 hrs Sapphire
210-FD-25 Flow Control Technologies - Barriers/Challenges to Tech Transition 24-Jun 1400 hrs Topaz
211-FD-26 Turbulence Simulations 24-Jun 1400 hrs Senators Lecture Hall
246-FD-27 Turbulence Analysis 25-Jun 0900 hrs Govenors Lecture Hall
247-FD-28 Transition Open Forum 25-Jun 0900 hrs Sapphire
248-FD-29 Flow Control - Aerodynamics 25-Jun 0900 hrs Senators Lecture Hall
278-FD-30 Hypersonic and Chemically-Reacting Flows 25-Jun 1400 hrs Sapphire
279-FD-31 Flow Control - Vortical Flows 25-Jun 1400 hrs Senators Lecture Hall
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IntroSessions at a GlanceAbbreviation Title Date Start Time Location
Flight Testing249-FT-1 Flight Testing 25-Jun 0900 hrs Obelisk B
280-FT-2/GT-14 Optimization Techniques in Flight Test/Ground Test 25-Jun 1400 hrs Obelisk B
Green Engineering281-GEPC-1 Overview of NASA Advanced Air Vehicles Program 25-Jun 1400 hrs Metropolitan
Ballroom
ITAR Sessions103-ITAR-1 ITAR - Hypersonic Flow Phenomena (Invited) 23-Jun 0900 hrs Morocco
140-ITAR-2 ITAR - Aircraft Design and Modeling 23-Jun 1400 hrs Morocco
Lighter-Than-Air Systems250-LTA-1 Lighter-than-Air Systems & Technologies I 25-Jun 0900 hrs Steuben
282-LTA-2 Lighter-than-Air Systems & Technologies II 25-Jun 1400 hrs Steuben
Multidisciplinary Analysis and Optimization29-MAO-1 Vehicle Design Applications I 22-Jun 0900 hrs Madrid
64-MAO-2 Vehicle Design Applications II 22-Jun 1400 hrs Madrid
104-MAO-3 Applications I 23-Jun 0900 hrs Madrid
141-MAO-4 Applications II 23-Jun 1400 hrs Madrid
176-MAO-5 Emerging Methods I 24-Jun 0900 hrs Madrid
212-MAO-6 Emerging Methods II 24-Jun 1400 hrs Madrid
213-MAO-7 Metamodeling I 24-Jun 1400 hrs Manchester
251-MAO-8 Metamodeling II 25-Jun 0900 hrs Manchester
252-MAO-9 Shape and Topology I 25-Jun 0900 hrs Madrid
283-MAO-10 Shape and Topology II 25-Jun 1400 hrs Madrid
284-MAO-11 Uncertainty I 25-Jun 1400 hrs Manchester
307-MAO-12 Shape and Topology III 26-Jun 0900 hrs Madrid
308-MAO-13 Uncertainty II 26-Jun 0900 hrs Manchester
Modeling and Simulation Technologies30-MST-1 Unmanned Aerial Vehicle Systems 22-Jun 0900 hrs Travertine
31-MST-2 Aviation Systems Human Factors 22-Jun 0900 hrs Wyeth
65-MST-3 Air Traffic Management 22-Jun 1400 hrs Travertine
66-MST-4 Guidance, Control, and Dynamics I 22-Jun 1400 hrs Wyeth
105-MST-5 Guidance, Control, and Dynamics II 23-Jun 0900 hrs Travertine
142-MST-6 Shadow Mode Assessment using Realistic Technologies for National Airspace System (SMART NAS) Test Bed Development (Invited)
23-Jun 1400 hrs Travertine
177-MST-7 Flight Simulation 24-Jun 0900 hrs Travertine
178-MST-8 Computational Methods for Fluid Dynamics and Heat Transfer Simulations 24-Jun 0900 hrs Wyeth
214-MST-9 Airframe Damage and Health Monitoring 24-Jun 1400 hrs Travertine
215-MST-10 Sensor and Communications Systems 24-Jun 1400 hrs Wyeth
253-MST-11 Aircraft Systems Design, Verification and Validation 25-Jun 0900 hrs Travertine
285-MST-12 Propulsion Systems 25-Jun 1400 hrs Travertine
www.aiaa-aviation.org 40 #aiaaAviation
IntroSessions at a GlanceAbbreviation Title Date Start Time Location
Plasmadynamics and Lasers 33-PDL-1/FD-5 Plasma Aerodynamics & Flow Control I 22-Jun 0900 hrs Monet Ballroom
60-FD-6/PDL-2 Plasma Aerodynamics & Flow Control II 22-Jun 1400 hrs Govenors Lecture Hall
67-PDL-3 Plasma Computational Methods I 22-Jun 1400 hrs Monet Ballroom
107-PDL-4 Plasma Assisted Combustion 23-Jun 0900 hrs Miro
143-PDL-6 Plasma Diagnostics I 23-Jun 1400 hrs Miro
144-PDL-7 Plasma Aerodynamics & Flow Control III 23-Jun 1400 hrs Monet Ballroom
180-PDL-8/APA-20 Plasma Aerodynamics & Flow Control IV 24-Jun 0900 hrs Stemmons C
181-PDL-9/TP-8 Plasma Diagnostics II 24-Jun 0900 hrs Miro
216-TP-10/PDL-10 Plasma Computational Methods II 24-Jun 1400 hrs Miro
255-PDL-12 Aero-Optics Plasma Diagnostics 25-Jun 0900 hrs Miro
286-PDL-13 Plasma Aerodynamics & Flow Control V 25-Jun 1400 hrs Miro
Thermophysics34-TP-1 Ablation I 22-Jun 0900 hrs Rosetta
35-TP-2 Heat Transfer I 22-Jun 0900 hrs Steuben
68-TP-3 Ablation II 22-Jun 1400 hrs Rosetta
69-TP-4 Aerothermodynamics I 22-Jun 1400 hrs Steuben
108-TP-5 Plasma and Arc Jet Testing, Diagnostics and Computational Methods 23-Jun 0900 hrs Rosetta
121-AMT-8/FD-14/TP-6/GT-8
Molecular-Based Optical Diagnostics for Hypersonic Nonequilibrium Flows 23-Jun 1400 hrs Topaz
145-TP-7 Heat Transfer II 23-Jun 1400 hrs Rosetta
181-PDL-9/TP-8 Plasma Diagnostics II 24-Jun 0900 hrs Miro
182-TP-9 Aerothermodynamics II 24-Jun 0900 hrs Rosetta
216-TP-10/PDL-10 Plasma Computational Methods II 24-Jun 1400 hrs Miro
217-TP-11 Aerothermodynamics III 24-Jun 1400 hrs Rosetta
256-TP-12 Detailed Molecular Process Modeling 25-Jun 0900 hrs Rosetta
288-TP-13 DSMC 25-Jun 1400 hrs Rosetta
Mond
ay
Mond
ay, 2
2 Ju
ne 2
015
1-SB
-1
0730
- 08
00 h
rsSp
eake
rs’ B
riefin
gSe
ssion
Roo
ms
Mond
ay, 2
2 Ju
ne 2
015
2-PL
NRY-1
08
00 -
0900
hrs
Open
ing K
eyno
teCh
antill
y Ball
room
Wes
t
Are W
e Mov
ing Fa
st En
ough
?To
m En
ders
Chief
Exec
utive
Offic
erAir
bus G
roup
Mond
ay, 2
2 Ju
ne 2
015
3-AA
-1Ai
rfram
e Nois
e IFle
ur-d
e-lis
ACh
aired
by: D
. LOC
KARD
, NAS
A-Lan
gley R
esea
rch Ce
nter
0900
hrs
AIAA-2
015-2
200
Aero
acou
stic a
nd A
erod
ynam
ic Pe
rform
ance
s of a
n Ae
rofo
il Su
bjecte
d to S
inuso
idal L
eadin
g Ed
ges
T. Ch
ong,
S. S
iddiqi
, Brun
el Un
iversi
ty,
Uxbri
dge,
Unite
d King
dom
0930
hrs
AIAA-2
015-2
201
Aero
dyna
mic a
nd A
eroa
cous
tic
Perfo
rman
ce of
Serra
ted A
irfoil
sX.
Liu,
M. Az
arpey
vand
, R. T
heun
issen
, Un
iversi
ty of
Brist
ol, B
ristol
, Unit
ed
Kingd
om
1000
hrs
AIAA-2
015-2
202
Broa
dban
d nois
e red
uctio
n th
roug
h lea
ding e
dge s
erra
tions
on re
alisti
c ae
rofo
ilsC.
Paruc
huri,
N. S
ubram
anian
, P.
Jose
ph, C
. Van
derw
el, J.
Kim,
B.
Gana
pathi
subra
mani,
Univ
ersity
of
South
ampto
n, So
utham
pton,
Unite
d Kin
gdom
1030
hrs
AIAA-2
015-2
203
Airfo
il nois
e pre
dictio
n fro
m 2D
3C
PIV d
ata
L. de
San
tana,
Catho
lic Un
iversi
ty of
Leuv
en, L
euve
n, Be
lgium
; C. S
chram
, vo
n Kárm
án In
stitut
e for
Fluid
Dyna
mics,
Rh
ode-S
aint-G
enès
e, Be
lgium
; W. D
esme
t, Ca
tholic
Unive
rsity
of Le
uven
, Leu
ven,
Belgi
um
1100
hrs
AIAA-2
015-2
204
Noise
gene
ratio
n by
turb
ulenc
e int
erac
ting w
ith an
aero
foil w
ith a
serra
ted le
ading
edge
J. Ma
thews
, N. P
eake
, Univ
ersity
of
Camb
ridge
, Cam
bridg
e, Un
ited K
ingdo
m
1130
hrs
AIAA-2
015-2
205
Deta
iled e
xper
imen
tal in
vesti
gatio
n of
the a
eroa
cous
tic fi
eld ar
ound
a Co
ntro
lled-
Diffu
sion
airfo
ilT.
Pado
is, P.
Laffa
y, A.
Idier,
S. M
oreau
, Un
iversi
ty of
Sherb
rooke
, She
rbroo
ke,
Cana
da
1200
hrs
AIAA-2
015-2
206
2D h
igh-li
ft air
foil n
oise
meas
urem
ents
in an
aero
dyna
mic
wind
tunn
elV.
Fleury
, J. B
ulte,
R. Da
vy, E
. Man
oha,
ONER
A, Ch
âtillo
n, Fra
nce;
M. Po
tt-Po
llens
ke, G
erman
Aeros
pace
Cente
r (D
LR),
Brau
nsch
weig,
Germ
any
Mond
ay, 2
2 Ju
ne 2
015
4-AA
-2Je
t Nois
e Pre
dictio
n I
Fleur
-de-
lis B
Chair
ed by
: P. M
ORRIS
, Pen
nsylv
ania
State
Univ
ersity
0900
hrs
AIAA-2
015-2
207
Asse
ssmen
t of J
et-pla
te In
terac
tion
Noise
Usin
g the
Latti
ce B
oltzm
ann
Meth
odF.
da S
ilva,
C. De
scham
ps, A
. da S
ilva,
Fede
ral U
nivers
ity of
San
ta Ca
tarina
, Flo
rianó
polis,
Braz
il; L.
Simõe
s, Em
braer,
Sã
o Jos
é dos
Camp
os, B
razil
0930
hrs
AIAA-2
015-2
208
Insta
llatio
n no
ise of
a tu
rbof
an je
t en
gine u
nder
an ai
rfoil
G. B
riche
t, M.
Koen
ig, S
afran
Grou
p, Mo
issy-C
ramay
el, Fr
ance
; C. B
ailly,
École
Ce
ntrale
de Ly
on, E
cully,
Fran
ce
1000
hrs
AIAA-2
015-2
209
Larg
e-ed
dy si
mulat
ion of
su
perso
nic pl
anar
jets
impin
ging
on a
flat p
late a
t an
angle
of 6
0 to
90
degr
ees
R. Go
jon, C
. Bog
ey, O
. Mars
den,
École
Ce
ntrale
de Ly
on, E
cully,
Fran
ce
1030
hrs
AIAA-2
015-2
210
Larg
e-ed
dy si
mulat
ion of
un
dere
xpan
ded r
ound
jets
impin
ging o
n a fl
at pl
ate 4
to 9
ra
dii do
wnstr
eam
from
the n
ozzle
R. Go
jon, C
. Bog
ey, O
. Mars
den,
École
Ce
ntrale
de Ly
on, E
cully,
Fran
ce
1100
hrs
AIAA-2
015-2
211
Noise
Char
acter
istics
of a
Four
-Jet
Impin
geme
nt D
evice
Insid
e a
Broa
dban
d Eng
ine N
oise S
imula
tor
C. Br
ehm,
J. H
ousm
an, C
. Kiris
, NAS
A Am
es Re
searc
h Cen
ter, M
offett
Field
, CA;
F. Hu
tches
on, N
ASA L
angle
y Res
earch
Ce
nter, H
ampto
n, VA
1130
hrs
AIAA-2
015-2
212
Simula
tion
and s
tabil
ity an
alysis
of
a su
perso
nic im
pingin
g jet
at
vary
ing n
ozzle
-to-w
all di
stanc
esN.
Hild
ebran
d, J.
Nicho
ls, U
nivers
ity of
Mi
nnes
ota, T
win C
ities,
Minn
eapo
lis, M
N
1200
hrs
AIAA-2
015-2
213
Hybr
id ap
proa
ch fo
r the
pred
iction
of
jet n
oise i
nter
actio
n an
d ins
talla
tion
effe
ctsY.
Yang
, Y. S
un, C
. Brea
rd, Co
mmerc
ial
Aircra
ft Co
rporat
ion of
China
, Ltd.
(C
OMAC
), Sh
angh
ai, Ch
ina
41
Mond
ay, 2
2 Ju
ne 2
015
5-AA
-3Je
t Nois
e Mod
eling
IIn
vern
ess
Chair
ed by
: C. B
OGEY
, Eco
le Ce
ntrale
de Ly
on09
00 hr
sAIA
A-201
5-221
4Re
al-tim
e mod
elling
of
wave
pack
ets in
turb
ulent
jets
K. Sa
saki,
Tech
nolog
ical In
stitut
e of
Aeron
autic
s (ITA
), Sã
o Jos
é dos
Camp
os,
Braz
il; S.
Pian
tanida
, Nati
onal
Cente
r for
Scie
ntific
Rese
arch (
CNRS
), Po
itiers,
Fra
nce;
A. Ca
valie
ri, Te
chno
logica
l Ins
titute
of Ae
ronau
tics (
ITA),
São J
osé
dos C
ampo
s, Br
azil;
P. Jo
rdan,
Natio
nal
Cente
r for
Scien
tific R
esea
rch (C
NRS)
, Po
itiers,
Fran
ce
0930
hrs
AIAA-2
015-2
215
Auto
matic
Opt
imize
r vs H
uman
Op
timize
r for
Low-
Orde
r Jet
Noise
Mo
dellin
gY.
Korol
ev, S
. Kara
baso
v, V.
Torop
ov,
Quee
n Mary
Univ
ersity
of Lo
ndon
, Lon
don,
Unite
d King
dom
1000
hrs
AIAA-2
015-2
216
The p
redic
tion
of th
e rad
iated
pr
essu
re sp
ectru
m pr
oduc
ed by
jet
-wing
inter
actio
nJ.
Vera,
J. La
wren
ce, R
. Self
, M. K
ingan
, Un
iversi
ty of
South
ampto
n, So
utham
pton,
Unite
d King
dom
1030
hrs
AIAA-2
015-2
217
Stoch
astic
and n
onlin
ear f
orcin
g of
wave
pack
ets in
a Ma
ch 0
.9 je
tA.
Town
e, T.
Colon
ius, C
alifor
nia In
stitut
e of
Tech
nolog
y, Pa
sade
na, C
A; P.
Jorda
n, Na
tiona
l Cen
ter fo
r Scie
ntific
Rese
arch
(CNR
S), P
oitier
s, Fra
nce;
A. Ca
valie
ri, Te
chno
logica
l Insti
tute o
f Aero
nauti
cs (IT
A), S
ão Jo
sé do
s Cam
pos,
Braz
il; G.
Br
ès, C
asca
de Te
chno
logies
, Inc
., Pa
lo Alt
o, CA
1100
hrs
AIAA-2
015-2
218
Sens
itivity
of w
avep
acke
ts in
jets t
o no
n-line
ar ef
fects:
the r
ole of
the
critic
al lay
erG.
Tissot
, Tech
nolog
ical In
stitute
of Ae
ronau
tics
(ITA)
, São
José
dos C
ampo
s, Bra
zil; M
. Zh
ang,
Natio
nal C
enter
for S
cienti
fic Re
search
(C
NRS)
, Poit
iers,
France
; F. La
jús, A
. Cav
alieri,
Techn
ologic
al Ins
titute
of Ae
ronau
tics (I
TA),
São J
osé do
s Cam
pos,
Brazil;
P. Jor
dan,
Natio
nal C
enter
for S
cienti
fic Re
search
(C
NRS)
, Poit
iers,
France
; T. C
oloniu
s, Ca
liforni
a Ins
titute
of Tec
hnolo
gy, Pa
saden
a, CA
1130
hrs
AIAA-2
015-2
219
Sens
itivity
analy
sis fo
r sub
sonic
jet
using
adjoi
nt of
non
loca
l sta
bility
eq
uatio
nsC.
Airiau
, T. A
nsald
i, Univ
ersity
of To
ulous
e, To
ulous
e, Fra
nce
1200
hrs
AIAA-2
015-2
220
A Co
ntro
l Fra
mewo
rk fo
r Wa
vepa
ckets
in Tu
rbule
nt Je
ts Us
ing Ti
me-D
omain
Tran
sfer
Func
tions
F. Sil
vestr
e, M.
Capre
cci, A
. Cav
alieri
, Te
chno
logica
l Insti
tute o
f Aero
nauti
cs (IT
A), S
ão Jo
sé do
s Cam
pos,
Braz
il; P.
Jorda
n, Éc
ole N
ation
ale S
upéri
eure
des
Mine
s de S
aint-É
tienn
e, Po
itiers,
Fran
ce
Mond
ay, 2
2 Ju
ne 2
015
6-AA
-4CA
A Nu
meric
al Te
chniq
ues I
Laliq
ueCh
aired
by: W
. SCH
ROED
ER, R
WTH
AACH
EN, I
nstitu
te of
Aerod
ynam
ics09
00 hr
sAIA
A-201
5-222
1Ex
perim
enta
l Vali
datio
n of
Ae
ro-V
ibro-
Acou
stic A
nalys
is of
Pr
oduc
tion
Vehic
les (I
nvite
d)S.
Caro,
CD-ad
apco
, Lyo
n, Fra
nce
0930
hrs
AIAA-2
015-2
222
CAA
Study
of A
irfoil
Bro
adba
nd
Inter
actio
n No
ise U
sing S
toch
astic
Tu
rbule
nt Vo
rticit
y Sou
rces
T. Ha
inaut,
G. G
abard
, V. C
lair, U
nivers
ity
of So
utham
pton,
South
ampto
n, Un
ited
Kingd
om
1000
hrs
AIAA-2
015-2
223
CABA
RET G
PU So
lver f
or Fa
st-Tu
rn-
Arou
nd Fl
ow an
d Nois
e Calc
ulatio
nsA.
Marke
steijn
, V. S
emile
tov, S
. Kara
baso
v, Qu
een M
ary U
nivers
ity of
Lond
on, L
ondo
n, Un
ited K
ingdo
m
1030
hrs
AIAA-2
015-2
224
Asse
ssmen
t of F
lap Si
de-Ed
ge Fe
nce
Noise
usin
g SNG
R Me
thod
H. Ya
o, L.
David
son, C
halm
ers Un
iversit
y of
Techn
ology,
Göteb
org, S
wede
n; S.
Peng
, Sw
edish
Defen
se Re
search
Agen
cy (F
OI),
Stockh
olm, S
wede
n; L.
Erikss
on, C
halm
ers
Unive
rsity o
f Tech
nolog
y, Gö
teborg
, Swe
den;
M. Ba
rbarin
o, F. C
apizz
ano,
Italian
Aeros
pace
Re
search
Cente
r (CIR
A), C
apua
, Italy
; et a
l.
1100
hrs
AIAA-2
015-2
225
Verifi
catio
n of
a Vis
cous
Co
mput
ation
al Ae
roac
ousti
cs Co
de
using
Exter
nal V
erifi
catio
n An
alysis
D. In
graha
m, D
. Hixo
n, Un
iversi
ty of
Toled
o, To
ledo,
OH
1130
hrs
AIAA-2
015-2
226
Acou
stic l
oads
pred
iction
for a
co
mmer
cial t
rans
port
aircra
ft un
der
grou
nd an
d fligh
t con
dition
sY.
Sun,
Y. Ya
ng, C
. Brea
rd, Co
mmerc
ial
Aircra
ft Co
rporat
ion of
China
, Ltd.
(C
OMAC
), Sh
angh
ai, Ch
ina
Mond
ay, 2
2 Ju
ne 2
015
7-AA
-5Du
ct Ac
ousti
cs I
Obeli
sk A
Chair
ed by
: W. E
VERS
MAN,
Miss
ouri U
nivers
ity of
Scie
nce a
nd Te
chno
logy
0900
hrs
AIAA-2
015-2
227
Effe
ct of
visco
sity o
n im
peda
nce
educ
tion
and v
alida
tion
L. Zh
ou, H
. Bod
en, R
oyal
Institu
te of
Tech
nolog
y (KT
H), S
tockh
olm, S
wede
n
0930
hrs
AIAA-2
015-2
228
Impe
danc
e Edu
ction
in So
und F
ields
wi
th P
eriph
erall
y Var
ying L
iners
and F
lowW.
Wats
on, M
. Jon
es, N
ASA L
angle
y Re
searc
h Cen
ter, H
ampto
n, VA
1000
hrs
AIAA-2
015-2
229
The E
ffecti
ve Im
peda
nce o
f a
Finite
-Thick
ness
Visco
ther
mal
Boun
dary
Laye
r Ove
r an
Acou
stic
Lining
D. Kh
amis,
E. B
ramble
y, Un
iversi
ty of
Camb
ridge
, Cam
bridg
e, Un
ited K
ingdo
m
1030
hrs
AIAA-2
015-2
230
Acou
stic L
iner D
rag:
A Pa
rame
tric
Study
of Co
nven
tiona
l Co
nfigu
ratio
nsB.
How
erton
, M. J
ones
, NAS
A Lan
gley
Rese
arch C
enter
, Ham
pton,
VA
1100
hrs
AIAA-2
015-2
231
Expe
rimen
tal S
tudy
of th
e Me
chan
isms o
f Sou
nd G
ener
ation
Du
e to a
n In
-duc
t Orifi
ce P
late
F. Ta
o, X.
Zhan
g, P.
Jose
ph, O
. Stal
nov,
Unive
rsity
of So
utham
pton,
South
ampto
n, Un
ited K
ingdo
m; M
. Sier
cke,
H. S
chee
l, Air
bus,
Hamb
urg, G
erman
y
1130
hrs
AIAA-2
015-2
232
Duct
spinn
ing m
ode’s
parti
cle
veloc
ity im
aging
on a
cross
plane
ou
tside
the d
uct
W. Yu
, Q. W
ei, X
. Hua
ng, P
eking
Un
iversi
ty, B
eijing
, Chin
a
1200
hrs
AIAA-2
015-2
233
In-d
uct B
eamf
ormi
ng N
oise
Sour
ce Es
timat
ion M
ode D
etecti
on
Unive
rsity
of Sã
o Pau
lo Fa
n Ri
gL.
Calda
s, L.
Bacca
la, R.
Cuen
ca,
Unive
rsity
of Sã
o Pau
lo, S
ão Pa
ulo,
Braz
il; R.
Queir
oz, E
mbrae
r, São
José
dos
Camp
os, B
razil
42
Mond
ay, 2
2 Ju
ne 2
015
8-AF
M-1
Aircr
aft F
light
Dyn
amics
, Con
trol, H
andli
ng Q
ualiti
es an
d Per
form
ance
IPlu
m Bl
osso
m A
Chair
ed by
: E. G
ILLES
PIE, U
nited
Spa
ce Al
lianc
e09
00 hr
sAIA
A-201
5-223
4Be
nefit
s of F
orma
tion F
light
of
Exten
ded D
urati
on Co
nside
ring F
uel
Burn
W. O
kolo,
A. Do
gan,
Unive
rsity o
f Tex
as,
Arling
ton, A
rlingto
n, TX
; W. B
lake,
Air Fo
rce
Resea
rch La
borat
ory, W
right-
Patte
rson
AFB,
OH
0930
hrs
AIAA-2
015-2
235
Auto
matic
Stall
/Spin
Dete
ction
in
Fixed
-Wing
Airc
raft
R. Bu
nge,
F. Mu
nera
Savin
o, I.
Kroo,
Stan
ford U
nivers
ity, S
tanfor
d, CA
1000
hrs
AIAA-2
015-2
236
Extra
cting
Airp
lane P
erfo
rman
ce
for a
Fata
l Acci
dent
in th
e Abs
ence
of
a Fli
ght D
ata R
ecor
der
T. Bu
rtch,
Natio
nal T
ransp
ortati
on S
afety
Board
, Was
hingto
n, DC
1030
hrs
AIAA-2
015-2
237
Valid
ation
of a
Mode
l Bas
ed St
ructu
ral
Load
s Mon
itorin
g Sys
tem us
ing th
e Fli
ght T
est Ai
rcraft
UW-
9 Spr
intM.
Mon
tel, F.
Thiele
cke, H
ambu
rg Un
iversit
y of
Techn
ology,
Hamb
urg, G
erman
y
1100
hrs
AIAA-2
015-2
238
Roll p
erfo
rman
ce as
sessm
ent o
f a
light
aircr
aft:
fligh
t tes
ts an
d fligh
t sim
ulatio
nF.
Nicolo
si, A.
De M
arco,
V. Sa
betta
, P.
Della
Vecch
ia, U
nivers
ity of
Nap
les
“Fed
erico
II”, N
aples
, Ital
y
Mond
ay, 2
2 Ju
ne 2
015
9-AF
M-2
Aero
serv
oelas
tic (A
SE) M
odeli
ngPlu
m Bl
osso
m B
Chair
ed by
: T. A
LEXE
EV, U
nivers
ity of
Califo
rnia D
avis
and F
. PRIO
LO, M
illenn
ium En
ginee
ring a
nd In
tegrat
ion Co
mpan
y09
00 hr
sAIA
A-201
5-223
9Co
ntro
l of a
Non
linea
r Wing
Secti
on
using
Fly-
by-Fe
el Se
nsing
V. Su
ryaku
mar, Y
. Bab
bar, T
. Strg
anac
, Te
xas A
&M U
nivers
ity, C
olleg
e Stat
ion, T
X;
A. Ma
ngala
m, Ta
o of S
ystem
s Inte
gratio
n, Inc
., Ha
mpton
, VA
0930
hrs
AIAA-2
015-2
240
Aero
elasti
c Sta
te-sp
ace M
odel
Deve
lopme
nt B
ased
on Fr
eque
ncy
Resp
onse
Iden
tifica
tion
and
Integ
ratio
n wi
th Fl
ight D
ynam
icsT.
Buttin
i, F. M
oreira
, Emb
raer, S
ão Jo
sé
dos C
ampo
s, Br
azil;
F. Sil
vestr
e, R.
A. da
Sil
va, T
echn
ologic
al Ins
titute
of Ae
ronau
tics
(ITA)
, São
José
dos C
ampo
s, Br
azil
1000
hrs
AIAA-2
015-2
241
Optim
al Siz
ing an
d Con
figur
ation
s of
the C
ontro
l Sur
face
s for
Acti
ve
Aero
elasti
c Con
trol
R. Br
own,
K. Sin
gh, M
iami U
nivers
ity,
Oxfor
d, OH
1030
hrs
AIAA-2
015-2
242
Aero
elasti
c Tail
oring
for
Maxim
izing
Sailp
lane A
vera
ge
Cros
s-Cou
ntry
Spee
dC.
Lupp
, C. C
esnik
, Univ
ersity
of M
ichiga
n, An
n Arbo
r, Ann
Arbo
r, MI
1100
hrs
AIAA-2
015-2
243
Adap
tive F
eedf
orwa
rd Co
ntro
l De
sign
for G
ust L
oads
Alle
viatio
n of
Hi
ghly
Flexib
le Ai
rcraf
tY.
Wang
, F. L
i, Chin
a Aca
demy
of
Aeros
pace
Aerod
ynam
ics, B
eijing
, Chin
a; A.
Da Ro
nch,
Unive
rsity
of So
utham
pton,
South
ampto
n, Un
ited K
ingdo
m
1130
hrs
AIAA-2
015-2
244
Delta
Ada
ptive
Flex
ible M
otion
Co
ntro
l for
the X
-56A
Airc
raft
K. Ha
shem
i, Univ
ersity
of Te
xas,
Austi
n, Au
stin,
TX; C
. Pak
, NAS
A Arm
stron
g Flig
ht Re
searc
h Cen
ter, E
dward
s, CA
; M. A
kella
, Un
iversi
ty of
Texa
s, Au
stin,
Austi
n, TX
1200
hrs
AIAA-2
015-2
245
Feed
back
Line
ariza
tion
base
d Co
ntro
l of A
eroe
lastic
Syste
ms
repr
esen
ted in
Mod
al Co
ordin
ates
H. S
hukla
, M. P
atil, V
irgini
a Poly
techn
ic Ins
titute
and S
tate U
nivers
ity, B
lacks
burg,
VA
Mond
ay, 2
2 Ju
ne 2
015
10-A
MT-1
/GT-1
Hap A
rnold
’s Ne
w Ho
rizon
: The
Futu
re R
ole of
Gro
und T
est i
n Hi
gh Sp
eed S
ystem
Dev
elopm
ent
Obeli
sk B
Chair
ed by
: J. S
CHMI
SSEU
R and
G. L
ISTON
0900
hrs
Oral
Prese
ntatio
nEn
vision
ing th
e Fut
ure o
f the
T&E
Enter
prise
M. Le
wis,
IDA,
Wash
ington
, DC
0930
hrs
Oral
Prese
ntatio
nCh
allen
ges a
nd O
ppor
tunit
ies in
the
Deve
lopme
nt of
T&E C
apab
ilities
J. Sc
hmiss
eur, U
nivers
ity of
Tenn
esse
e, Tu
llaho
ma, T
ullah
oma,
TN
1000
hrs
Oral
Prese
ntatio
nIn
trodu
ction
to th
e AFR
L High
-Sp
eed E
xper
imen
tatio
n Br
anch
G. Li
ston,
Air Fo
rce Re
searc
h Lab
orator
y, Cle
velan
d, OH
1030
hrs
Oral
Prese
ntatio
nDe
velop
ment
of La
rge-
Scale
Quie
t Tu
nnels
Supp
ortin
g T&E
T. Ju
liano
, Notr
e Dam
e Univ
ersity
, Notr
e Da
me, I
N
1100
hrs
Pane
l Disc
usssi
onTh
e Fut
ure o
f Gro
und T
est w
ithin
T&E
J. Sc
hmiss
eur, U
nivers
ity of
Tenn
esse
e, Tu
llaho
ma, T
ullah
oma,
TN
Mond
ay, 2
2 Ju
ne 2
015
11-A
MT-2
/GT-2
Line o
f Sigh
t and
Den
sity M
easu
reme
ntEd
elweis
sCh
aired
by: S
. O’B
YRNE
, The
Univ
ersity
of N
ew S
outh
Wales
0900
hrs
AIAA-2
015-2
246
Analy
sis of
Focu
sed L
aser
Di
ffere
ntial
Inter
fero
metry
B. S
chmi
dt, J.
She
pherd
, Cali
fornia
Ins
titute
of Te
chno
logy,
Pasa
dena
, CA
0930
hrs
AIAA-2
015-2
247
Simult
aneo
us M
easu
reme
nts
of D
ensit
y Fiel
d and
Wav
efro
nt
Disto
rtion
s in
High
Spee
d Jet
Flows
J. Ge
orge,
T. Je
nkins
, C. H
ess,
J. Tro
linge
r, Me
troLa
ser, I
nc.,
Lagu
na H
ills, C
A
1000
hrs
AIAA-2
015-2
248
Optic
al Me
asur
emen
ts of
Veloc
ity,
Dens
ity, a
nd M
ass F
lux in
a Su
perso
nic W
ind Tu
nnel
D. Pl
emmo
ns, N
. Galy
en, A
erosp
ace
Testi
ng Al
lianc
e, Arn
old AF
B, TN
1030
hrs
AIAA-2
015-2
249
A Tim
e-Re
solve
d Tem
pera
ture
Me
asur
emen
t Sys
tem fo
r Fre
e-Pis
ton
Shoc
k Tu
nnels
Y. Kri
shna
, S. S
heeh
e, S.
O’B
yrne,
Unive
rsity
of Ne
w So
uth W
ales,
Canb
erra,
Austr
alia
43
Mond
ay, 2
2 Ju
ne 2
015
12-A
PA-1
Aero
dyna
mic-S
tructu
re D
ynam
ics In
terac
tion
Stemm
ons C
Chair
ed by
: J. A
ZEVE
DO an
d C. P
ASILI
AO, A
FRL/
RWW
V09
00 hr
sAIA
A-201
5-225
0Ae
rody
nami
c Dam
ping a
nd
Stiffn
ess D
eterm
inatio
n fo
r Airc
raft
Wing
Flut
ter Sp
eed A
nalys
isK.
Boo,
S. M
anso
r, A. A
bdul-
Latif,
Un
iversi
ty of
Tech
nolog
y, Jo
hor B
ahru,
Ma
laysia
0930
hrs
AIAA-2
015-2
251
Expe
rimen
tal I
nves
tigat
ion of
the
Aero
elasti
c Beh
avior
a NA
CA00
18
Cybe
r-Phy
sical
Flexib
leWing
C. Fa
gley,
J. Se
idel, T
. McLa
ughli
n, U.
S.
Air Fo
rce Ac
adem
y, Co
lorad
o Spri
ngs,
CO
1000
hrs
AIAA-2
015-2
252
Spec
tral F
ormu
lation
-Bas
ed FS
I and
Co
upled
Sens
itivity
Ana
lysis
for
Dyan
mic A
eroe
lastic
Pro
blems
S. Yi,
Korea
Adva
nced I
nstitu
te of
Scien
ce an
d Tec
hnolo
gy, Da
ejeon
, Sou
th Ko
rea; R
. Pras
ad,
S. Ch
oi, D.
Im, V
irginia
Polyt
echnic
Instit
ute
and S
tate U
nivers
ity, Bl
acksbu
rg, VA
; D. L
ee,
Korea
Adva
nced I
nstitu
te of
Scien
ce an
d Tec
hnolo
gy, Da
ejeon
, Sou
th Ko
rea
1030
hrs
AIAA-2
015-2
253
Analy
zing t
he P
itch
Agilit
y of a
n Or
nitho
pter
Und
ergo
ing P
assiv
e Co
mplia
nt El
emen
t Ind
uced
Shap
e Ch
ange
Z. Ha
snain
, J. H
ubba
rd, U
nivers
ity of
Ma
rylan
d, Co
llege
Park,
Colle
ge Pa
rk, M
D;
A. W
issa,
Unive
rsity
of Illi
nois,
Urba
na-
Cham
paign
, Urba
na, I
L
Mond
ay, 2
2 Ju
ne 2
015
13-A
PA-2
Aero
dyna
mic D
esign
Meth
odolo
gies I
Carp
enter
Ball
room
Chair
ed by
: K. K
ARA,
Khali
fa Un
iversi
ty of
Scien
ce, T
echn
ology
& Re
searc
h and
J. M
URRA
Y, Sa
ndia
Natio
nal L
abora
tories
0900
hrs
AIAA-2
015-2
254
Deve
lopme
nt of
NOV
A Ai
rcraf
t Co
nfigu
ratio
ns fo
r Lar
ge En
gine
Integ
ratio
n Stu
dies
L. W
iart,
O. At
inault
, R. G
renon
, B. P
aluch
, D.
Hue
, ONE
RA, M
eudo
n, Fra
nce
0930
hrs
AIAA-2
015-2
255
Aircr
aft d
irecti
onal
stabil
ity
pred
iction
meth
od by
CFD
P. De
lla Ve
cchia,
F. N
icolos
i, D. C
ilibert
i, Un
iversi
ty of
Naple
s “Fe
deric
o II”,
Nap
les,
Italy
1000
hrs
AIAA-2
015-2
256
Desig
n of a
Mult
i-Stag
e Axia
l Tur
bine
withi
n the
scop
e of c
omple
te Sy
stem
Desig
n, Ma
nufac
turing
and O
pera
tion
of a n
ew Tu
rbine
Prop
ulsion
Simu
lator
(TP
S)A.
Krumm
e, Ge
rman
Aeros
pace
Cente
r (DL
R),
Göttin
gen,
Germ
any;
S. He
gen,
Germ
an-Du
tch
Wind
Tunn
els, M
arkne
sse, T
he N
etherl
ands;
R.
Nahu
is, Na
tiona
l Aero
space
Labo
ratory
(NLR
), Ma
rkness
e, Th
e Neth
erlan
ds
1030
hrs
AIAA-2
015-2
257
Fuse
lage A
erod
ynam
ic Pr
edict
ion
Meth
ods
F. Nic
olosi,
P. D
ella V
ecch
ia, D
. Cilib
erti, V
. Cu
sati,
L. Att
anas
io, U
nivers
ity of
Nap
les
“Fed
erico
II”, N
aples
, Ital
y
1100
hrs
AIAA-2
015-2
258
Inve
stiga
tion
on co
ntinu
ously
de
flecta
ble H
igh-Li
ft De
vices
for a
3D
High
-Lift
Confi
gura
tion
D. Fr
anke
, Germ
an Ae
rospa
ce Ce
nter
(DLR
), Br
auns
chwe
ig, G
erman
y
1130
hrs
AIAA-2
015-2
259
Nume
rical
study
of U
AS-S
4 Éh
ecat
l aer
odyn
amic
perfo
rman
ce
impr
ovem
ent o
btain
ed w
ith th
e use
of
a mo
rphin
g wing
appr
oach
S. O
liviu,
A. Ko
reans
chi, R
. Bote
z, Un
iversi
ty of
Québ
ec, M
ontré
al, Ca
nada
Mond
ay, 2
2 Ju
ne 2
015
14-A
PA-3
Spec
ial Se
ssion
: Low
Boo
m Ac
tivitie
s ISte
mmon
s ACh
aired
by: K
. WAIT
HE, G
ulfstr
eam
Aeros
pace
Corpo
ration
and L
. BAN
GERT
, NAS
A Lan
gley R
esea
rch Ce
nter
0900
hrs
AIAA-2
015-2
260
Unde
r-Tra
ck CF
D-Ba
sed S
hape
Op
timiza
tion
for a
Low-
Boom
De
mons
trato
r Con
cept
M. W
intze
r, Ana
lytica
l Mec
hanic
s Asso
ciates
, Inc
., Ha
mpton
, VA;
I. Orda
z, NA
SA La
ngley
Re
searc
h Cen
ter, H
ampto
n, VA
0930
hrs
AIAA-2
015-2
261
Full-
Carp
et De
sign
of a
Low-
Boom
De
mons
trato
r Con
cept
I. Or
daz,
NASA
Lang
ley Re
searc
h Cen
ter,
Hamp
ton, V
A; M.
Wint
zer, A
nalyt
ical
Mech
anics
Asso
ciates
, Inc
., Ha
mpton
, VA
; S. R
allab
hand
i, Nati
onal
Institu
te of
Aeros
pace
, Ham
pton,
VA
1000
hrs
Oral
Prese
ntatio
nSo
nic B
oom
Varia
tion
of a
Wing
-Bo
dy-Ta
il-Na
celle
Confi
gura
tion
M. Pa
rk, N
ASA L
angle
y Res
earch
Cente
r, Ha
mpton
, VA
1030
hrs
AIAA-2
015-2
262
Nume
rical
Simula
tions
of Sh
ock/
Plume
Inter
actio
n Us
ing St
ructu
red
Over
set G
rids
J. Ho
usma
n, C.
Kiris,
NAS
A Ame
s Res
earch
Ce
nter, M
offett
Field
, CA
1100
hrs
AIAA-2
015-2
263
Cart3
D An
alysis
of P
lume a
nd
Shoc
k In
terac
tion
Effe
cts on
Sonic
Bo
omR.
Castn
er, N
ASA G
lenn R
esea
rch Ce
nter,
Cleve
land,
OH
44
Mond
ay, 2
2 Ju
ne 2
015
15-A
PA-4
Prop
eller
/Rot
orcra
ft/Wi
nd Tu
rbine
Aer
odyn
amics
ISte
mmon
s BCh
aired
by: M
. CAL
VERT
, U.S
. Arm
y AMR
DEC a
nd D
. O’B
RIEN,
US
Army R
DECO
M09
00 hr
sAIA
A-201
5-226
4Ex
perim
ental
Evalu
ation
of O
pen
Prop
eller
Aero
dyna
mic P
erfor
manc
e an
d Aero
-acou
stic B
ehav
iorC.
Wisni
ewski
, A. B
yerle
y, W.
Heise
r, U.S.
Air
Force
Acad
emy,
Color
ado S
pring
s, CO
; K.
Van T
reuren
, T. L
iller, B
aylor
Unive
rsity,
Waco,
TX
; N. W
isniew
ski, R
ose Hu
lman
Instit
ute of
Tec
hnolo
gy, Te
rre Ha
ute, IN
0930
hrs
AIAA-2
015-2
265
Slips
tream
Mea
sure
ment
s of S
mall-
Scale
Pro
pelle
rs at
Low
Reyn
olds
Numb
ers
R. De
ters,
G. An
anda
Krish
nan,
M. S
elig,
Unive
rsity
of Illi
nois,
Urba
na-Ch
ampa
ign,
Urba
na, I
L
1000
hrs
AIAA-2
015-2
266
The I
nflue
nce o
f Airf
oil Sh
ape,
Reyn
olds N
umbe
r and
Chor
d Le
ngth
on Sm
all P
rope
ller
Perfo
rman
ce an
d Nois
eC.
Wisn
iewsk
i, A. B
yerle
y, W.
Heis
er, U
.S.
Air Fo
rce Ac
adem
y, Co
lorad
o Spri
ngs,
CO;
K. Va
n Treu
ren, T
. Lille
r, Bay
lor U
nivers
ity,
Waco
, TX
1030
hrs
AIAA-2
015-2
267
Desig
ning S
mall P
rope
llers
for
Optim
um Ef
ficien
cy an
d Low
Nois
e Fo
otpr
intC.
Wisn
iewsk
i, A. B
yerle
y, W.
Heis
er, U
.S.
Air Fo
rce Ac
adem
y, Co
lorad
o Spri
ngs,
CO;
K. Va
n Treu
ren, T
. Lille
r, Bay
lor U
nivers
ity,
Waco
, TX
1100
hrs
AIAA-2
015-2
268
A Pa
rabo
lic M
ethod
for A
ccura
te an
d Effi
cient
Wind
Farm
Simu
lation
A. Mi
ttal, K
. Sree
nivas
, W. B
riley,
L. Ta
ylor,
Unive
rsity
of Te
nnes
see,
Chatt
anoo
ga,
Chatt
anoo
ga, T
N
1130
hrs
AIAA-2
015-2
269
Blad
e Res
olved
Simu
lation
for a
Wi
nd Fa
rmW.
Has
san,
K. Sr
eeniv
as, A
. Mitta
l, L.
Taylo
r, L. H
ereth,
Univ
ersity
of Te
nnes
see,
Chatt
anoo
ga, C
hatta
noog
a, TN
Mond
ay, 2
2 Ju
ne 2
015
16-A
TIO-1
Term
inal &
Surfa
ce O
pera
tions
IMa
nche
ster
Chair
ed by
: S. C
AMPB
ELL,
MIT L
incoln
Labo
ratory
0900
hrs
AIAA-2
015-2
270
A Rob
ust a
nd Pr
actic
al De
cision
Su
ppor
t Too
l for I
ntegr
ated
Arriv
al-De
partu
re-Su
rface
Traffi
c Ma
nage
ment
A. Sa
raf, V
. Felip
e, Sa
ab Se
nsis C
orpora
tion,
Camp
bell,
CA; B
. Saw
hill, N
extGe
n Ae
roscie
nces L
LC, W
illiams
burg,
VA
0930
hrs
AIAA-2
015-2
271
Iden
tifica
tion
of Lo
cal a
nd
Prop
agat
ed Q
ueuin
g Effe
cts at
Ma
jor A
irpor
tsH.
Idris
, Eng
ility C
orpora
tion,
Biller
ica, M
A
1000
hrs
AIAA-2
015-2
272
Taxi
Time P
redic
tion
at Ch
arlot
te Ai
rpor
t Usin
g Fas
t-Tim
e Sim
ulatio
n an
d Mac
hine L
earn
ing Te
chniq
ues
H. Le
e, W.
Mali
k, Un
iversi
ty of
Califo
rnia,
Santa
Cruz
, Moff
ett Fi
eld, C
A; B.
Zhan
g, B.
Nag
arajan
, Ame
rican
Airlin
es, F
ort
Worth
, TX;
Y. Ju
ng, N
ASA A
mes R
esea
rch
Cente
r, Moff
ett Fi
eld, C
A
1030
hrs
AIAA-2
015-2
273
A Sto
chas
tic Sc
hedu
ler fo
r In
tegra
ted A
rriva
l, Dep
artu
re, a
nd
Surfa
ce O
pera
tions
in Lo
s Ang
eles
M. X
ue, U
nivers
ity of
Califo
rnia,
Santa
Cru
z, Mo
ffett
Field,
CA; S
. Zeli
nski,
NAS
A Am
es Re
searc
h Cen
ter, M
offett
Field
, CA
1100
hrs
AIAA-2
015-2
274
Optim
izatio
n of
Airp
ort S
urfa
ce
Oper
ation
s Und
er U
ncer
taint
yC.
Bosso
n, D.
Sun
, Purd
ue U
nivers
ity, W
est
Lafay
ette,
IN
Mond
ay, 2
2 Ju
ne 2
015
17-A
TIO-2
Sepa
ratio
n As
sura
nce
Ming
Chair
ed by
: M. W
ILCOX
EN, U
.S. A
ir Forc
e09
00 hr
sAIA
A-201
5-227
5Co
nflict
Dete
ction
Perfo
rman
ce
Analy
sis fo
r Fun
ction
Alloc
ation
Usin
g Tim
e-Shif
ted Re
cord
ed Tr
affic D
ataN.
Guerr
eiro,
J. Ma
ddalo
n, T.
Lewis,
G. Ha
gen,
NASA
Lang
ley Re
search
Cente
r, Ham
pton,
VA
0930
hrs
AIAA-2
015-2
276
Strat
egic
time-
base
d mete
ring t
hat
assu
res s
epar
ation
for i
nteg
rated
op
erat
ions i
n a t
ermi
nal a
irspa
ceA.
Sado
vsky
, M. J
astrz
ebsk
i, NAS
A Ame
s Re
searc
h Cen
ter, M
offett
Field
, CA
1000
hrs
AIAA-2
015-2
277
Confl
ict A
lerts
for A
ircra
ft Co
nduc
ting V
isual
Appr
oach
esH.
Tang
, NAS
A Ame
s Res
earch
Cente
r, Mo
ffett
Field,
CA
Mond
ay, 2
2 Ju
ne 2
015
18-A
TIO-3
Trajec
tory
Opt
imiza
tion
Milan
Chair
ed by
: H. A
RNES
ON09
00 hr
sAIA
A-201
5-227
8Th
e Stri
ng St
abilit
y of a
Traje
ctory
-Ba
sed I
nter
val M
anag
emen
t Al
gorit
hm in
the M
idter
m Ai
rspac
eK.
Swier
inga,
NASA
Lang
ley Re
searc
h Ce
nter, H
ampto
n, VA
0930
hrs
AIAA-2
015-2
279
Comp
utat
ional
Appr
oach
es to
Sim
ulatio
n an
d Opt
imiza
tion
of
Glob
al Ai
rcraf
t Tra
jecto
ries
H. N
g, Un
iversi
ty of
Califo
rnia,
Santa
Cruz
, Mo
ffett
Field,
CA; B
. Srid
har, N
ASA A
mes
Rese
arch C
enter
, Moff
ett Fi
eld, C
A
1000
hrs
AIAA-2
015-2
280
Bran
ch &
Bou
nd-B
ased
Algo
rithm
fo
r Airc
raft
VNAV
Pro
file R
efer
ence
Tra
jecto
ry O
ptim
izatio
nA.
Murrie
ta Me
ndoz
a, B.
Beu
ze, L
. Te
rnisie
n, R.
Botez
, Univ
ersity
of Q
uébe
c, Mo
ntréa
l, Can
ada
1030
hrs
AIAA-2
015-2
281
Aircr
aft T
rajec
torie
s Opt
imiza
tion
By G
eneti
c Algo
rithm
s To R
educ
e Fli
ght C
ost U
sing A
Dyn
amic
Weat
her M
odel
R. Fé
lix Pa
trón,
M. S
chind
ler, R
. Bote
z, Un
iversi
ty of
Québ
ec, M
ontré
al, Ca
nada
1100
hrs
AIAA-2
015-2
282
Trajec
tory
optim
izatio
n alg
orith
m fo
r a co
nsta
nt al
titud
e cru
ise fl
ight
with
a re
quire
d tim
e of a
rriva
l co
nstra
intA.
Liv, R
. Dan
cila, R
. Bote
z, Un
iversi
ty of
Québ
ec, M
ontré
al, Ca
nada
45
Mond
ay, 2
2 Ju
ne 2
015
19-A
TIO-4
09
00 -
1100
hrs
Trans
form
ation
al Fli
ght -
Rap
id Co
ncep
t to F
light
Metro
polita
n Ba
llroo
m
Mode
rator:
Willi
am Fr
ederi
cks,
NASA
Lang
ley Re
searc
h Cen
ter
Pan
elists
:Ne
al Wi
llfor
dTe
xtron
Aviat
ionMa
rk P
age
Dzyn
e Tec
hnolo
gies
JoeB
en B
evirt
Joby
Aviat
ionSta
rr Gi
nnNA
SA Ar
mstro
ng Re
searc
h Cen
ter
Mond
ay, 2
2 Ju
ne 2
015
20-C
ASE-1
09
00 -
1200
hrs
Acad
emic
Roun
dtab
leBa
tik
Expa
nding
on th
e the
me fr
om S
unda
y, thi
s ses
sion i
s the
seco
nd da
y acti
vity o
f the
201
5 CA
SE Ac
adem
ic Wo
rksho
p. It
will o
ffer r
apid-
fire di
scussi
ons o
f curr
ent r
esea
rch ef
forts
in sy
stems
know
ledge
and c
ompe
tency.
F
acilit
ators:
Fran
z-Jos
ef K
ahlen
, Ph.
D.As
socia
te Pro
fesso
r, Dep
artme
nt of
Mech
anica
l Eng
ineeri
ngUn
iversi
ty of
Cape
Town
, Cap
e Tow
n, So
uth Af
rica
Shan
non
Flume
rfelt,
Ph.
D.As
socia
te Pro
fesso
r, Edu
catio
nal L
eade
rship,
Dire
ctor o
f Lea
n Thin
king f
or Sc
hools
, Pa
wley
Learn
ing In
stitut
e, Oa
kland
Univ
ersity
, Mich
igan
Anab
ela A
lves,
Ph.D
.As
sistan
t Prof
essor,
Depa
rtame
nto de
Prod
ução e
Siste
mas E
scola
de En
genh
aria d
a Univ
ersida
de
do M
inho,
Centr
o Inte
rdisci
plinar
de Te
cnolog
ias, d
a Prod
ução e
da En
ergia
(CITP
E)Ca
mpus
de Az
urém,
Portu
gal
Mond
ay, 2
2 Ju
ne 2
015
21-C
FD-1
Unstr
uctu
red H
igh-O
rder
Meth
ods I
Gran
d Ball
room
ACh
aired
by: S
. MUR
MAN,
NAS
A Ame
s Res
earch
Cente
r and
A. KA
TZ09
00 hr
sAIA
A-201
5-228
3Hi
gh-O
rder
Stra
nd G
rid M
ethod
s fo
r Sho
ck Tu
rbule
nce I
nter
actio
nO.
Tong
, A. K
atz, U
tah S
tate U
nivers
ity,
Loga
n, UT
; J. S
itaram
an, U
.S. A
rmy,
Moffe
tt Fie
ld, CA
0930
hrs
AIAA-2
015-2
284
High
er-o
rder
Uns
tructu
red F
inite
Volum
e Meth
ods f
or Tu
rbule
nt
Aero
dyna
mic F
lows
A. Ja
lali, C
. Olliv
ier G
ooch
, Univ
ersity
of
Britis
h Colu
mbia,
Vanc
ouve
r, Can
ada
1000
hrs
AIAA-2
015-2
285
A Sp
ectra
l-Elem
ent A
ppro
ach
for
the E
ikona
l Equ
ation
S. M
urman
, L. D
iosad
y, NA
SA Am
es
Rese
arch C
enter
, Moff
ett Fi
eld, C
A
1030
hrs
AIAA-2
015-2
286
High
orde
r sub
cell fi
nite v
olume
me
thod
in so
lving
hyp
erbo
lic
cons
erva
tion
laws
J. Pa
n, Y.
Ren,
Tsing
hua U
nivers
ity,
Beijin
g, Ch
ina
Mond
ay, 2
2 Ju
ne 2
015
22-C
FD-2
Unste
ady F
low Si
mulat
ions
Gran
d Ball
room
BCh
aired
by: Y
. WAN
G an
d D. R
EASO
R, Air
Force
Rese
arch L
abora
tory
0900
hrs
AIAA-2
015-2
287
Unste
ady S
imula
tions
of Sh
ockw
ave-
Boun
dary
Laye
r Inte
racti
on In
duced
Tra
nson
ic Sho
ckwa
ve O
scilla
tions
using
Un
struc
tured
Grid
sK.
Bham
idipati
, D. R
easor
, 412
th Tes
t Wing
, Ed
wards
AFB,
CA; C
. Pasi
liao, A
ir Forc
e Re
search
Labo
ratory
, Eglin
AFB,
FL
0930
hrs
AIAA-2
015-2
288
Effe
ct of
Cavit
y Flow
on La
nding
Ge
ar A
erod
ynam
ic Lo
ads
U. O
za, Z
. Hu,
X. Zh
ang,
Unive
rsity
of So
utham
pton,
South
ampto
n, Un
ited
Kingd
om
1000
hrs
AIAA-2
015-2
289
Nume
rical
Inve
stiga
tion
of th
e De
tach
ing Vo
rtica
l Flow
at R
otat
ing
Cylin
ders
with
Thom
Disc
sR.
Ritz,
T. Sc
homb
erg, O
. Wün
sch,
Unive
rsity
of Ka
ssel, K
asse
l, Germ
any;
M.
Ruett
en, R
. Kes
sler, G
erman
Aeros
pace
Ce
nter (
DLR)
, Gött
ingen
, Germ
any
1030
hrs
AIAA-2
015-2
290
Symm
etrica
l and
non
-symm
etrica
l 3D
wing
defo
rmat
ion of
flap
ping
micro
aeria
l veh
icles
W. Ta
y, Na
tiona
l univ
ersity
of S
ingap
ore,
Singa
pore,
Sing
apore
1100
hrs
AIAA-2
015-2
291
Nume
rical
Inve
stiga
tion
of th
e Sta
rting
Pro
cess
in a L
ong-
test-
dura
tion
Hype
rvelo
city S
hock
Tu
nnel
Y. Wa
ng, Z
. Hu,
Z. Jia
ng, C
hines
e Ac
adem
y of S
cienc
es, B
eijing
, Chin
a
46
Mond
ay, 2
2 Ju
ne 2
015
23-C
FD-3
Mesh
ing Te
chniq
ues I
Cora
lCh
aired
by: D
. THO
MPSO
N, M
ississ
ippi S
tate U
nivers
ity an
d B. J
OLLY,
US
Air Fo
rce09
00 hr
sAIA
A-201
5-229
2Co
mpar
ing A
nisot
ropic
Out
put-
Base
d Grid
Ada
ptat
ion M
ethod
s by
Deco
mpos
ition
M. Pa
rk, N
ASA L
angle
y Res
earch
Cente
r, Ha
mpton
, VA;
A. Lo
seille
, Fren
ch N
ation
al Ins
titute
for Re
searc
h in C
ompu
ter S
cienc
e an
d Con
trol (
INRIA
), Le
Ches
nay,
Franc
e; J.
Krako
s, T.
Mich
al, Th
e Boe
ing Co
mpan
y, St
. Lou
is, M
O
0930
hrs
AIAA-2
015-2
293
mesh
Curv
e: An
Aut
omat
ed
Low-
Orde
r to H
igh-O
rder
Mes
h Ge
nera
tor
J. Im
s, Z.
Duan
, Z. W
ang,
Unive
rsity
of Ka
nsas
, Law
rence
, Law
rence
, KS
1000
hrs
AIAA-2
015-2
294
Targ
et-Ed
ge B
ased
Orth
ogon
al An
isotro
pic M
esh
J. Zu
niga V
azqu
ez, C
. Olliv
ier G
ooch
, Un
iversi
ty of
Britis
h Colu
mbia,
Vanc
ouve
r, Ca
nada
1030
hrs
AIAA-2
015-2
295
Autom
ated M
assiv
ely Re
finem
ent
Techn
ique f
or M
ulti-b
lock S
tructu
red
Grids
Based
on N
URBS
Volum
eH.
Koizu
mi, S
. Tsu
tsumi
, R. T
akak
i, Jap
an
Aeros
pace
Explo
ration
Agen
cy (J
AXA)
, Sa
gami
hara,
Japa
n; K.
Yama
moto,
Japa
n Ae
rospa
ce Ex
plorat
ion Ag
ency
(JAX
A),
Mitak
a, Ja
pan;
H. It
o, M.
Abe,
Ryoy
u Sy
stems
, Nag
oya,
Japa
n; et
al.
1100
hrs
AIAA-2
015-2
296
Cons
tructi
on of
Pris
m an
d Hex
La
yers
from
Aniso
tropic
Tetra
hedr
aJ.
Stein
brenn
er, Po
intwi
se, I
nc.,
Fort
Worth
, TX
Mond
ay, 2
2 Ju
ne 2
015
24-C
FD-4
LES,
DNS,
and H
ybrid
RAN
S-LE
S IEm
erald
Chair
ed by
: A. S
ESCU
, Miss
issipp
i Stat
e Univ
ersity
and W
. MCM
ULLA
N, U
nivers
ity of
Leice
ster
0900
hrs
AIAA-2
015-2
297
High
Ord
er Nu
meric
al Me
thods
for
the D
ynam
ic SGS
Mod
el of
Turb
ulent
Flows
with
Shoc
ksD.
Kotov
, Bay
Area
Envir
onme
ntal R
esearc
h Ins
titute,
Petal
uma,
CA; H
. Yee
, A. W
ray,
NASA
Ames
Resea
rch Ce
nter, M
offett
Field
, CA
; B. S
jogree
n, La
wren
ce Liv
ermore
Nati
onal
Labo
ratory
, Live
rmore
, CA
0930
hrs
AIAA-2
015-2
298
Larg
e Edd
y Sim
ulatio
n of
Su
perso
nic Im
pingin
g Jets
by
Adap
tive,
Expli
cit Fi
lterin
gS.
Patel
, J. M
athew
, Ind
ian In
stitut
e of
Scien
ce, B
anga
lore,
India
1000
hrs
AIAA-2
015-2
299
Reso
lved S
calar
Mixi
ng in
Larg
e Ed
dy Si
mulat
ions o
f a Lo
w Re
ynold
s Num
ber P
lane M
ixing
La
yer
J. Ha
ywoo
d, A.
Sescu
, Miss
issipp
i Stat
e Un
iversi
ty, M
ississ
ippi S
tate,
MS
1030
hrs
AIAA-2
015-2
300
Reso
lved S
calar
Mixi
ng in
Larg
e Ed
dy Si
mulat
ions o
f a Lo
w Re
ynold
s Num
ber P
lane M
ixing
La
yer
S. H
ug, W
. McM
ullan
, Univ
ersity
of
Leice
ster, L
eices
ter, U
nited
King
dom
1100
hrs
AIAA-2
015-2
301
LES S
imula
tion
Inflo
w co
nditio
ns
for O
utlet
Guid
e Van
e and
Pr
ediff
user
Flow
sJ.
Li, N
anjin
g Univ
ersity
of Ae
ronau
tics
and A
stron
autic
s, Na
njing
, Chin
a; G.
Page
, J.
McGu
irk, L
ough
borou
gh U
nivers
ity,
Loug
hboro
ugh,
Unite
d King
dom
Mond
ay, 2
2 Ju
ne 2
015
25-FD
-1Wi
ng A
erod
ynam
icsGo
veno
rs Le
cture
Hall
Chair
ed by
: D. Y
OUNG
, Ray
theon
Miss
ile S
ystem
s and
U. K
AUL,
NASA
ARC
0900
hrs
AIAA-2
015-2
302
The O
rigin
of Li
ft Re
visite
d: I.
A Co
mplet
e Phy
sical
Theo
ryT.
Liu, W
ester
n Mich
igan U
nivers
ity,
Kalam
azoo
, MI;
J. W
u, J.
Zhu,
L. Liu
, Pe
king U
nivers
ity, B
eijing
, Chin
a
0930
hrs
AIAA-2
015-2
303
The O
rigin
of Li
ft Re
visite
d: II.
Ph
ysica
l Pro
cesse
s of A
irfoil
-Cir
culat
ion Fo
rmat
ion in
Star
ting
Flow
J. Zh
u, S.
Zou,
L. Liu
, J. W
u, Pe
king
Unive
rsity,
Beij
ing, C
hina;
T. Liu
, Wes
tern
Mich
igan U
nivers
ity, K
alama
zoo,
MI
1000
hrs
AIAA-2
015-2
304
The S
teady
Aer
odyn
amics
of Q
uiet
Airfo
ils w
ith P
oros
ity G
radie
nts
R. Ha
jian,
J. Ja
worsk
i, Leh
igh U
nivers
ity,
Bethl
ehem
, PA
1030
hrs
AIAA-2
015-2
305
Lift a
nd D
rag i
n Tw
o-Di
mens
ional
Stead
y Visc
ous a
nd Co
mpre
ssible
Flo
w: I.
Far-F
ield F
ormu
lae A
nalys
is an
d Num
erica
l Con
firma
tion
J. Zh
u, L.
Liu, P
eking
Univ
ersity
, Beij
ing,
China
; T. L
iu, W
ester
n Mich
igan U
nivers
ity,
Kalam
azoo
, MI;
Y. Sh
i, W. S
u, J.
Wu,
Pekin
g Univ
ersity
, Beij
ing, C
hina
1100
hrs
AIAA-2
015-2
306
Lift a
nd D
rag i
n Tw
o-Di
mens
ional
Stead
y Visc
ous a
nd Co
mpre
ssible
Flo
w: II
. Fun
dame
ntal
Solut
ion
Theo
ryL.
Liu, J
. Wu,
Pekin
g Univ
ersity
, Beij
ing,
China
; T. L
iu, W
ester
n Mich
igan U
nivers
ity,
Kalam
azoo
, MI
1130
hrs
AIAA-2
015-2
307
Effe
cts of
Per
turb
ation
on th
e Flow
ov
er N
onsle
nder
Delt
a Wing
sC.
Canp
olat,
B. Sa
hin, C
ukuro
va U
nivers
ity,
Adan
a, Tu
rkey;
S. Ya
yla, Y
uzun
cu Y
il Un
iversi
ty, Va
n, Tu
rkey;
H. Ak
illi, C
ukuro
va
Unive
rsity,
Adan
a, Tu
rkey
1200
hrs
AIAA-2
015-2
308
Inter
actio
n of
Mult
iple V
ortic
es ov
er
a Dou
ble D
elta W
ingX.
Zhan
g, Z.
Wang
, I. G
ursul,
Univ
ersity
of
Bath,
Bath
, Unit
ed Ki
ngdo
m
47
Mond
ay, 2
2 Ju
ne 2
015
26-FD
-2Fu
ndam
enta
l Flui
d Flow
sSe
nato
rs Le
cture
Hall
Chair
ed by
: G. D
ALE,
Air Fo
rce Re
searc
h Lab
orator
y and
M. G
REEN
, Syra
cuse
Univ
ersity
0900
hrs
AIAA-2
015-2
309
Evolu
tion
of St
ratifi
ed B
ound
ary-
Free
Shea
r Flow
s Und
er St
okes
-Ek
man
Forci
ngM.
Jone
s, E.
Pater
son, V
irginia
Polyt
echnic
Ins
titute
and S
tate U
nivers
ity, Bl
acksbu
rg, VA
0930
hrs
AIAA-2
015-2
310
Nume
rical
and E
xperi
menta
l Inv
estiga
tion o
f Wind
Turb
ine W
akes
X. Hu
ang,
RWTH
Aache
n Univ
ersity,
Aache
n, Ge
rman
y; S.
Vey,
Techn
ical U
nivers
ity of
Be
rlin, B
erlin,
Germ
any;
M. M
einke
, W.
Schro
eder,
RWTH
Aache
n Univ
ersity,
Aache
n, Ge
rman
y; G.
Pechl
ivano
glou,
C. Na
yeri,
Techn
ical U
nivers
ity of
Berlin
, Berl
in, Ge
rman
y; et
al.
1000
hrs
AIAA-2
015-2
311
Evide
nce o
f com
plex
flow
struc
ture
s in
a con
verg
ing-d
iverg
ing n
ozzle
ca
used
by a
rece
ssed s
tep at
the
nozz
le th
roat
M. Ca
rmine
, R. C
heli,
F. Co
zzi, A
. Sp
inelli,
M. Z
occa
, A. G
uardo
ne, T
echn
ical
Unive
rsity
of Mi
lan, M
ilan,
Italy
1030
hrs
AIAA-2
015-2
312
Nume
rical
Study
of th
e Tra
nsien
t De
forma
tion a
nd D
rag C
hara
cteris
tics
of a D
eceler
ating
Dro
plet
Q. Q
u, P.
Ma, P
. Liu,
Beih
ang U
nivers
ity,
Beijin
g, Ch
ina; S
. Li, B
eijing
Insti
tute o
f Me
chan
ical a
nd El
ectric
al En
ginee
ring,
Beijin
g, Ch
ina; R
. Aga
rwal,
Was
hingto
n Un
iversi
ty in
St. L
ouis,
St.
Louis
, MO
Mond
ay, 2
2 Ju
ne 2
015
27-FD
-3Co
mbus
tion
and H
eat T
rans
fer
Topa
zCh
aired
by: J
. CHO
I, Ge
orgia
Institu
te of
Tech
nolog
y and
I. LE
YVA
0900
hrs
AIAA-2
015-2
313
An Ex
perim
enta
l Stu
dy of
Glob
al Ch
arac
terist
ics of
Turb
ulent
Di
ffusio
n Je
t Flam
es fo
r Fue
ls of
Co
mplex
Chem
istry
A. Ra
mach
andra
n, V.
Naray
anas
wamy
, No
rth Ca
rolina
Stat
e Univ
ersity
, Rale
igh,
NC
0930
hrs
AIAA-2
015-2
314
Comp
ariso
n of T
heor
etica
l and
Semi
-Em
pirica
l Solu
tions
for D
issipa
tion
Coeffi
cient
in a L
ow Re
ynold
s Num
ber
Comp
resso
r Cas
cade
F. Ko
k, R.
Myos
e, W
ichita
Stat
e Univ
ersity
, W
ichita
, KS;
S. H
ayas
hibara
, Emb
ry-Rid
dle
Aeron
autic
al Un
iversi
ty, Pr
esco
tt, AZ
1000
hrs
AIAA-2
015-2
315
On au
toign
ition-
domi
nated
su
perso
nic co
mbus
tion
N. Cy
mbali
st, P.
Dim
otakis
, Cali
fornia
Ins
titute
of Te
chno
logy,
Pasa
dena
, CA
1030
hrs
AIAA-2
015-2
316
Flow
Fields
of M
anipu
lated
Shea
r La
yers
of a
Turb
ulent
Jet F
lame
H. N
awrot
h, C.
Pasch
ereit,
Tech
nical
Unive
rsity
of Be
rlin, B
erlin,
Germ
any
Mond
ay, 2
2 Ju
ne 2
015
28-FD
-4Bo
unda
ry La
yer T
rans
ition:
Hyp
erso
nic Fl
ows
Sapp
hire
Chair
ed by
: J. J
EWEL
L, Air
Force
Rese
arch L
abora
tory a
nd K.
CASP
ER09
00 hr
sAIA
A-201
5-231
7In
stabil
ity an
d Tra
nsitio
n Ex
perim
ents
in th
e Boe
ing/A
FOSR
Ma
ch 6
Quie
t Tun
nel
G. M
cKier
nan,
B. Ch
ynow
eth, S
. Sc
hneid
er, Pu
rdue U
nivers
ity, W
est
Lafay
ette,
IN
0930
hrs
AIAA-2
015-2
318
Nume
rical
Inves
tigati
on of
Non
linea
r Wa
ve-p
acke
ts in
a Hyp
erso
nic H
igh-
Entha
lpy B
ound
ary-
Laye
r on a
5
deg S
harp
Cone
L. Sa
lemi, H
. Fas
el, U
nivers
ity of
Arizo
na,
Tucso
n, Tu
cson,
AZ
1000
hrs
AIAA-2
015-2
319
Corre
lation
of H
IFiRE
-5 Fl
ight D
ata
With
Comp
uted
Pre
ssure
and H
eat
Trans
fer
J. Je
well,
J. Mi
ller, R
. Kim
mel, A
ir Forc
e Re
searc
h Lab
orator
y, W
right-
Patte
rson
AFB,
OH
1030
hrs
AIAA-2
015-2
320
Linea
r sta
bility
of h
igh-sp
eed
boun
dary
laye
r flow
s at v
aryin
g Pr
andt
l num
bers
A. Ra
macha
ndran
, B. S
aikia,
K. Si
nha,
Indian
Ins
titute
of Tec
hnolo
gy Bo
mbay,
Mum
bai,
India;
R. Go
vinda
rajan
, Tata
Instit
ute of
Fu
ndam
ental
Resea
rch, H
ydera
bad,
India
48
Mond
ay, 2
2 Ju
ne 2
015
29-M
AO-1
Vehic
le De
sign
Appli
catio
ns I
Madr
idCh
aired
by: R
. KOL
ONAY
, Air F
orce R
esea
rch La
borat
ory/R
QVC/
WPA
FB an
d V. K
ALIVA
RAPU
, Iow
a Stat
e Univ
ersity
0900
hrs
AIAA-2
015-2
321
Para
llel a
lloca
tion-
missi
on
optim
izatio
n of
a 12
8-ro
ute
netw
ork
J. Hw
ang,
J. Ma
rtins,
Unive
rsity
of Mi
chiga
n, An
n Arbo
r, Ann
Arbo
r, MI
0930
hrs
AIAA-2
015-2
322
Multi-
Objec
tive D
esign
and
Path
Plan
ning O
ptim
izatio
n of
Un
mann
ed A
erial
Vehic
les (U
AVs)
E. Ru
dnick
-Cohe
n, S.
Azarm
, J. H
errma
nn,
Unive
rsity
of Ma
rylan
d, Co
llege
Park,
Co
llege
Park,
MD
1000
hrs
AIAA-2
015-2
323
Cont
rol P
ower
Opt
imiza
tion
using
Ar
tificia
l Int
ellige
nce f
or H
ybrid
Wi
ng B
ody A
ircra
ftR.
Chha
bra, V
irgini
a Poly
techn
ic Ins
titute
and S
tate U
nivers
ity, B
lacks
burg,
VA; S
. Mu
lani, U
nivers
ity of
Alab
ama,
Tusca
loosa
, Tu
scaloo
sa, A
L; R.
Kapa
nia, J
. Sch
etz,
Virgin
ia Po
lytec
hnic
Institu
te an
d Stat
e Un
iversi
ty, B
lacks
burg,
VA
1030
hrs
AIAA-2
015-2
324
Cont
rol F
ocus
ed M
ultidi
scipli
nary
De
sign
Optim
izatio
n of
Taille
ss Fig
hter
Airc
raft
C. Me
ckstr
oth, U
nivers
ity of
Day
ton,
Dayto
n, OH
; W. B
lake,
Air Fo
rce Re
searc
h La
borat
ory, W
right-
Patte
rson A
FB, O
H
1100
hrs
AIAA-2
015-2
325
Hybr
id Wi
ng B
ody (
HWB)
Airc
raft
Desig
n an
d Opt
imiza
tion
using
Sti
tched
Comp
osite
sV.
Li, Th
e Boe
ing Co
mpan
y, Hu
nting
ton
Beac
h, CA
1130
hrs
AIAA-2
015-2
326
A Mu
lti-Fid
elity,
Mult
i-Disc
iplina
ry
Analy
sis an
d Opt
imiza
tion
Fram
ewor
k fo
r the
Des
ign of
Mo
rphin
g UAV
Wing
A. Cia
rella,
C. Ts
otska
s, M.
Hahn
, Aircr
aft
Resea
rch As
sociat
ion, L
td., B
edfor
d, Un
ited
Kingd
om; N
. Wert
er, R.
De Br
euke
r, De
lft Un
iversit
y of T
echno
logy,
Delft,
The
Nethe
rland
s; C.
Beav
erstoc
k, Sw
ansea
Un
iversit
y, Sw
ansea
, Unit
ed Ki
ngdo
m; et
al.
1200
hrs
AIAA-2
015-2
327
Multi-
Disci
plina
ry an
d Mult
i-Ob
jectiv
e Opt
imiza
tion
of an
Un
conv
entio
nal A
ircra
ft Co
ncep
tS.
Gem
ma, F
. Mas
trodd
i, Univ
ersity
of
Rome
“La S
apien
za”,
Rome
, Ital
y
Mond
ay, 2
2 Ju
ne 2
015
30-M
ST-1
Unma
nned
Aer
ial Ve
hicle
Syste
msTra
verti
neCh
aired
by: B
. LAN
DRUM
and M
. PAT
IL, V
irgini
a Tec
h09
00 hr
sAIA
A-201
5-232
8Ex
perim
enta
l Cha
racte
rizat
ion of
Bu
tterfl
y in
Climb
ing Fl
ight
J. Cra
nford,
Univ
ersity
of Al
abam
a, Hu
ntsvil
le, H
untsv
ille, A
L; N.
Sleg
ers,
Georg
e Fox
Univ
ersity
, New
berg,
OR;
B. La
ndrum
, Univ
ersity
of Al
abam
a, Hu
ntsvil
le, H
untsv
ille, A
L
0930
hrs
AIAA-2
015-2
329
Nond
eterm
inisti
c Sim
ulatio
n for
Pr
obab
ility o
f Los
s of C
ontro
l Pr
edict
ion fo
r Unm
anne
d Airc
raft
Syste
msL.
Hale,
M. P
atil, C
. Roy,
Virgi
nia Po
lytech
nic
Institu
te an
d Stat
e Univ
ersity,
Black
sburg,
VA
1000
hrs
AIAA-2
015-2
330
Optim
al se
lectio
n of
UAV
for
grou
nd ta
rget
track
ingJ.
Narki
ewicz
, A. K
opyt,
P. Ra
dyisy
ewsk
i, T.
Malec
ki, W
arsaw
Univ
ersity
of
Tech
nolog
y, Wa
rsaw,
Polan
d
1030
hrs
AIAA-2
015-2
331
Dyna
mic R
esou
rce A
lloca
tion
for
Shar
ing M
ulti-U
AV Se
rvice
sB.
Kadd
ouh,
W. Cr
owthe
r, P. H
olling
swort
h, Un
iversi
ty of
Manc
heste
r, Man
ches
ter,
Unite
d King
dom
1100
hrs
AIAA-2
015-2
332
Optim
al Ob
ject L
ocat
ion by
a Fle
et of
Vario
us U
AVs
A. Ko
pyt,
J. Na
rkiew
icz, T
. Male
cki, P
. Ra
dyisy
ewsk
i, Wars
aw U
nivers
ity of
Te
chno
logy,
Warsa
w, Po
land
1130
hrs
AIAA-2
015-2
333
Mode
ling a
nd Co
ntro
l of T
ether
ed
Unma
nned
Mult
icopt
ers i
n Ho
verin
g Flig
htD.
Ferre
ira de
Castr
o, J.
Santo
s, M.
Ba
tista,
D. A
ntônio
dos S
antos
, L. G
óes,
Tech
nolog
ical In
stitut
e of A
erona
utics
(ITA)
, São
José
dos C
ampo
s, Br
azil
1200
hrs
AIAA-2
015-2
334
MAV P
ose M
easu
reme
nt al
gorit
hm
Base
d on
Visua
l Sys
tems
Q. Ze
ng, J
. Liu,
Y. W
ang,
Nanji
ng
Unive
rsity
of Ae
ronau
tics a
nd As
trona
utics,
Na
njing
, Chin
a
Mond
ay, 2
2 Ju
ne 2
015
31-M
ST-2
Aviat
ion Sy
stems
Hum
an Fa
ctors
Wyeth
Chair
ed by
: D. C
ARTM
ELL,
Boein
g Eng
ineeri
ng O
perat
ions &
Tech
nolog
y and
S. R
OBIN
SON,
UC D
avis
0900
hrs
AIAA-2
015-2
335
Form
al Ex
tensio
ns to
the I
nten
t-Ba
sed M
ode C
onfu
sion
Detec
tion
Fram
ewor
kJ.
Suraj
Nan
digan
ahall
i, I. H
wang
, Purd
ue
Unive
rsity,
Wes
t Lafa
yette
, IN
0930
hrs
AIAA-2
015-2
336
The R
apidl
y Rec
onfig
urab
le Re
sear
ch Co
ckpit
R. Jo
yce,
S. Ro
binso
n, Un
iversi
ty of
Califo
rnia,
Davis
, Dav
is, CA
1000
hrs
AIAA-2
015-2
337
Fligh
t Crew
Resp
onse
to Un
expe
cted
Even
ts: A
Simula
tor Ex
perim
ent
J. Fie
ld, N
ation
al Ae
rospa
ce La
borat
ory
(NLR
), Am
sterda
m, Th
e Neth
erlan
ds;
L. Fu
cke,
B. Co
rreia
Grác
io, Th
e Boe
ing
Comp
any,
Madri
d, Sp
ain; M
. Varn
ey,
Airbu
s, To
ulous
e, Fra
nce
1030
hrs
AIAA-2
015-2
338
Influ
ence
of co
upled
side
stick
s on
the p
ilot m
onito
ring’s
awar
enes
s du
ring fl
are
A. Ue
hara,
D. N
iederm
eier, G
erman
Ae
rospa
ce Ce
nter (
DLR)
, Brau
nsch
weig,
Ge
rman
y
1100
hrs
Oral
Prese
ntatio
nEr
gono
mic e
valua
tion
of di
ffere
nt
princ
iples
of po
sition
indic
ation
and
cont
rol p
lane i
n fie
ldM.
Zhelo
nkin,
Y. D
ubov
, V. Z
helon
kin, O
. Tk
ache
nko,
TsAGI
, Zhu
kovs
ky, R
ussia
1130
hrs
AIAA-2
015-2
339
Equa
tion-
Syste
m Re
pres
enta
tion
Mode
l for
Pne
umat
ic Se
at D
esign
Us
ed fo
r Vibr
ation
Isola
tion
In A
ir an
d Gro
und T
rans
port
E. Ay
yad,
W. Cu
lbreth
, D. R
eyno
lds,
Unive
rsity
of Ne
vada
, Las
Vega
s, La
s Ve
gas,
NV
1200
hrs
Oral
Prese
ntatio
nAn
appr
oach
to es
tabli
sh ca
se ba
se
of m
otion
s for
layo
ut op
timiza
tion
Y. Zh
ang,
Y. Su
n, L.
Liu, N
anjin
g Univ
ersity
of
Aeron
autic
s and
Astro
nauti
cs, Ya
ngzh
ou,
China
Mond
ay, 2
2 Ju
ne 2
015
32-N
W-1
0900
- 09
30 h
rsNe
twor
king C
offe
e Bre
akMe
eting
Roo
m Fo
yers
49
Mond
ay, 2
2 Ju
ne 2
015
33-P
DL-1
/FD-
5Pla
sma A
erod
ynam
ics &
Flow
Cont
rol I
Mone
t Ball
room
Chair
ed by
: M. S
TANE
K, AF
RL/R
QVI
0900
hrs
AIAA-2
015-2
340
Nume
rical
Simula
tions
of
Distu
rban
ces i
n Sh
ear F
lows
Intro
duce
d by N
S-DB
D Pla
sma
Actu
ator
sI.
Popo
v, G.
Corre
ale, S
. Huls
hoff,
Delf
t Un
iversi
ty of
Tech
nolog
y, De
lft, Th
e Ne
therla
nds
0930
hrs
AIAA-2
015-2
341
Nano
seco
nd D
ielec
tric B
arrie
r Di
schar
ge P
lasma
Actu
ator
Flow
Co
ntro
l of C
ompr
essib
le Dy
nami
c Sta
llM.
Fran
khou
ser, J
. Greg
ory, O
hio S
tate
Unive
rsity,
Colum
bus,
OH
1000
hrs
AIAA-2
015-2
342
Aero
dyna
mic C
ontro
l Effe
ct of
Su
rface
DC P
lasma
Disc
harg
e at
Mach
-7 H
yper
sonic
Flow
Y. Wa
tanab
e, Un
iversi
ty of
Toky
o, Bu
nkyo
, Ja
pan;
K. Su
zuki,
Univ
ersity
of To
kyo,
Kash
iwa,
Japa
n
1030
hrs
AIAA-2
015-2
343
Effect
of Pu
lsed P
lasma
Jets
on Bo
unda
ry La
yer R
ecove
ry
Down
strea
m of
a Refl
ected
Shoc
k Wa
ve-B
ound
ary L
ayer
Intera
ction
B. Gre
ene,
N. Cl
emen
s, Un
iversit
y of T
exas,
Au
stin, A
ustin,
TX; P.
Mag
ari, D
. Mick
a, M.
Ue
ckerm
ann,
Creare
, Inc.,
Hann
over,
NH
1100
hrs
AIAA-2
015-2
344
Single
Nan
oseco
nd D
ielect
ric Ba
rrier
Di
schar
ge an
d Puls
ed Sl
iding
Di
schar
ge Ap
plied
to Se
para
tion
Contr
ol Alo
ng a
NACA
0015
Airfo
ilK.
Bayo
da, N
. Ben
ard, E
. More
au, N
ation
al Ce
nter fo
r Scie
ntific
Resea
rch (C
NRS)
, Fu
turosc
ope,
France
1130
hrs
AIAA-2
015-2
345
Shoc
k-Tra
pping
Capa
bility
of a
Cavit
y in
a Sup
erso
nic Fl
owN.
Web
b, M.
Sam
imy,
Ohio
State
Un
iversi
ty, Co
lumbu
s, OH
1200
hrs
AIAA-2
015-2
346
Pres
sure
Inve
stiga
tions
over
a Co
nical
Fore
body
und
er D
uty-
Cycle
d Plas
ma A
ctuat
ions
J. Zh
ao, X
. Men
g, J.
Wang
, Nort
hwes
tern
Polyt
echn
ical U
nivers
ity, X
i’an,
China
; F.
Liu, S
. Luo
, Univ
ersity
of Ca
liforni
a, Irv
ine,
Los A
ngele
s, CA
Mond
ay, 2
2 Ju
ne 2
015
34-TP
-1Ab
lation
IRo
setta
Chair
ed by
: D. K
UNTZ
, San
dia N
ation
al La
borat
ories
and D
. PYT
EL, L
ockh
eed M
artin
Spac
e Sys
tems
0900
hrs
AIAA-2
015-2
347
Evalu
ation
of Fi
nite-
Rate
Gas/
Surfa
ce In
terac
tion
Mode
ls fo
r a
Carb
on B
ased
Abla
tor
Y. Ch
en, N
ASA A
mes R
esea
rch Ce
nter,
Moffe
tt Fie
ld, CA
; T. G
okce
n, ER
C, Inc
., Mo
ffett
Field,
CA
0930
hrs
AIAA-2
015-2
348
Comp
ariso
n of
Carb
on A
blativ
e Sh
ock-
Laye
r Rad
iation
with
High
Su
rface
Temp
erat
ures
S. Lew
is, R.
Morga
n, T.
Mcint
yre, U
nivers
ity
of Qu
eensl
and,
St. Lu
cia, A
ustral
ia; C.
Alba
, R.
Green
dyke
, Air F
orce I
nstitu
te of
Techn
ology,
Wr
ight-P
atters
on AF
B, OH
1000
hrs
AIAA-2
015-2
349
Stagn
ation
-Line
Simu
lation
s of
Meteo
r Abla
tion
B. D
ias, A
. Turc
hi, T.
Mag
in, vo
n Kárm
án
Institu
te for
Fluid
Dyn
amics
, Rho
de-Sa
int-
Genè
se, B
elgium
Mond
ay, 2
2 Ju
ne 2
015
35-TP
-2He
at Tr
ansfe
r ISte
uben
Chair
ed by
: M. K
IO, N
ation
al Sp
ace R
esea
rch &
Dev
elopm
ent A
genc
y and
A. W
ILLIAM
S, Ai
r Forc
e Res
each
Labo
ratory
0900
hrs
AIAA-2
015-2
350
Diffu
sion
Pene
tratio
n Tim
e for
Tra
nsien
t Con
ducti
onR.
McMa
sters,
Virgi
nia M
ilitary
Institu
te,
Lexing
ton, V
A; F. d
e Mon
te, Un
iversit
y of
L’Aqu
ila, L’A
quila,
Italy;
J. Be
ck, S.
Na
llapan
eni, M
ichiga
n Stat
e Univ
ersity,
E.
Lansi
ng, M
I; D. A
mos,
Sand
ia Na
tiona
l La
borat
ories,
Albu
querq
ue, N
M; A.
Haji-S
heikh
, Un
iversit
y of T
exas,
Arling
ton, A
rlingto
n, TX
0930
hrs
AIAA-2
015-2
351
Comp
ariso
ns of
Comp
utat
ions
with
Expe
rimen
ts fo
r Elec
tron
Trans
pirat
ion Co
oling
at H
igh
Enth
alpies
K. Ha
nquis
t, I.
Boyd
, Univ
ersity
of
Mich
igan,
Ann A
rbor, A
nn Ar
bor, M
I
1000
hrs
AIAA-2
015-2
352
Heat
and M
ass T
rans
fer A
nalys
is of
a F
ilm Ev
apor
ative
MEM
S Tun
eable
Ar
ray T
hrus
terW.
O’N
eill, A
. Cofe
r, A. W
eave
r, A.
Alexe
enko
, Purd
ue U
nivers
ity, W
est
Lafay
ette,
IN
1030
hrs
AIAA-2
015-2
353
Ther
mal M
odel
for S
inter
ed
Cylin
drica
l Eva
pora
tors
of Lo
op
Heat
Pipe
s(215
0991
)M.
Man
telli,
J. Flo
rez M
era, F
. Mila
nese
, Fe
deral
Univ
ersity
of S
anta
Catar
ina,
Floria
nópo
lis, B
razil
1100
hrs
AIAA-2
015-2
354
Study
of th
e Mini
mum
Anti-
icing
En
ergy
Bas
ed on
Icing
Limi
t Sta
teY.
Zhao
, S. C
hang
, Y. B
o, M.
Leng
, Be
ihang
Univ
ersity
, Beij
ing, C
hina
1130
hrs
AIAA-2
015-2
355
Studie
s on
ther
mal c
ondu
ctivit
y pr
edict
ion of
fibe
r rein
force
d ma
terial
with
micr
osco
pic st
ructu
re
ident
ifica
tion
J. Hu
a, Na
njing
Univ
ersity
of Ae
ronau
tics
and A
stron
autic
s, Na
njing
, Chin
a
Mond
ay, 2
2 Ju
ne 2
015
36-F3
60-1
09
30 -
1200
hrs
The V
oice o
f the
Custo
mer -
Des
igning
the R
ight A
ircra
ftGr
and B
allro
om E
Mode
rator:
Chris
tophe
r Ston
ehou
se, S
enior
Vice
Pres
ident,
Custo
mer S
ervice
s, Air
bus A
meric
as, I
nc.
P
aneli
sts:
Jack
Are
hart
Presid
ent o
f MRO
Serv
ices
Delta
Tech
Ops
Willia
m “B
ill” M
eeha
nCh
ief O
perat
ing O
fficer
Fronti
er Air
lines
, Inc
.
Bart
Robe
rtsVic
e Pres
ident,
Fligh
t Tec
hnica
l Ope
ration
sJe
tBlue
Airw
ays
David
Seym
our
Senio
r Vice
Pres
ident,
Tech
nical
Opera
tions
Ameri
can A
irline
s
50
Mond
ay, 2
2 Ju
ne 2
015
37-A
A-6
Open
Rot
or I
Fleur
-de-
lis A
Chair
ed by
: A. L
YRIN
TZIS
1400
hrs
AIAA-2
015-2
356
Aero
dyna
mic a
nd A
eroa
cous
tic
Effe
cts of
Pylo
n Tra
iling E
dge
Blow
ing on
Pus
her P
rope
ller
Insta
llatio
nT.
Sinnig
e, K.
Lync
h, D.
Ragn
i, G.
Eitelb
erg, L
. Veld
huis,
Delf
t Univ
ersity
of
Tech
nolog
y, De
lft, Th
e Neth
erlan
ds
1430
hrs
AIAA-2
015-2
357
Hybr
id Us
e of C
FD an
d Ana
lytica
l Me
thod
s for
the P
redic
tion
of
Adva
nced
Ope
n Ro
tor T
one N
oise
C. Ek
oule,
M. K
ingan
, A. M
cAlpin
e, So
utham
pton U
nivers
ity, So
utham
pton,
Unite
d Kin
gdom
; N. S
ohon
i, Cam
bridg
e Univ
ersity,
Ca
mbrid
ge, U
nited
King
dom;
A. Pa
rry, R
olls-
Royce
Grou
p plc,
Derby
, Unit
ed Ki
ngdo
m
1500
hrs
AIAA-2
015-2
358
The E
ffects
of Sw
irl R
ecov
ery
Vane
s on
Single
-Rot
ation
Pro
pelle
r Ae
rody
nami
cs an
d Aer
oaco
ustic
sT.
Sinnig
e, J.
van K
uijk,
K. Ly
nch,
D.
Ragn
i, G. E
itelbe
rg, L.
Veldh
uis, D
elft
Unive
rsity
of Te
chno
logy,
Delft,
The
Nethe
rland
s
1530
hrs
AIAA-2
015-2
359
Aircr
aft O
pen
Roto
r Tec
hnolo
gy:
Analy
sis fr
om an
Ope
ratio
nal
Persp
ectiv
eG.
Bus
ch, M
. Has
san,
D. M
avris
, Geo
rgia
Institu
te of
Tech
nolog
y, Atl
anta,
GA
1600
hrs
AIAA-2
015-2
360
Optim
al Pr
opell
er D
esign
for Q
uiet
Aircr
aft u
sing N
umer
ical A
nalys
isB.
Hum
pert,
R. G
aeta,
J. Ja
cob,
Oklah
oma
State
Univ
ersity
, Still
water
, OK
1630
hrs
AIAA-2
015-2
361
Soun
d Rad
iation
from
a Ro
tor
Parti
ally I
mmer
sed i
n a T
urbu
lent
Boun
dary
Laye
rS.
Gleg
g, A.
Buon
o, J.
Gran
t, F.
Lach
owsk
i, Flo
rida A
tlanti
c Univ
ersity
, Boc
a Rato
n, FL
; W. D
even
port,
W. A
lexan
der, V
irgini
a Po
lytec
hnic
Institu
te an
d Stat
e Univ
ersity
, Bla
cksb
urg, V
A
Mond
ay, 2
2 Ju
ne 2
015
38-A
A-7
Trailin
g Edg
e Nois
e IFle
ur-d
e-lis
BCh
aired
by: R
. EW
ERT,
DLR -
Germ
an Ae
rospa
ce Ce
nter
1400
hrs
AIAA-2
015-2
362
A Tra
iling-
Edge
Nois
e Mod
el fo
r Se
rrated
Edge
sB.
Lyu,
Unive
rsity
of Ca
mbrid
ge,
Camb
ridge
, Unit
ed Ki
ngdo
m; M
. Az
arpey
vand
, Univ
ersity
of B
ristol
, Bris
tol,
Unite
d King
dom;
S. S
inayo
ko, U
nivers
ity
of So
utham
pton,
South
ampto
n, Un
ited
Kingd
om
1430
hrs
AIAA-2
015-2
363
Effe
ct of
serra
ted tr
ailing
edge
on
boun
dary
laye
r ins
tabil
ity n
oise
J. Se
rpieri
, S. P
röbsti
ng, M
. Gup
ta, F.
Sc
arano
, Delf
t Univ
ersity
of Te
chno
logy,
Delft,
The N
etherl
ands
1500
hrs
AIAA-2
015-2
364
The E
ffects
of Su
ction
and B
lowing
on
Tona
l Nois
e Gen
erat
ion by
Blun
t Tra
iling E
dges
W. Ra
mirez
, W. W
olf, U
nivers
ity of
Ca
mpina
s, Ca
mpina
s, Br
azil
1530
hrs
AIAA-2
015-2
365
Bio-
Insp
ired T
railin
g Edg
e Nois
e Co
ntro
lI.
Clark,
W. A
lexan
der, W
. Dev
enpo
rt,
Virgin
ia Po
lytec
hnic
Institu
te an
d Stat
e Un
iversi
ty, B
lacks
burg,
VA; S
. Gleg
g, Flo
rida A
tlanti
c Univ
ersity
, Boc
a Rato
n, FL
; J.
Jawo
rski, L
ehigh
Univ
ersity
, Beth
lehem
, PA
; C. D
aly, U
nivers
ity of
Camb
ridge
, Ca
mbrid
ge, U
nited
King
dom;
et al
.
1600
hrs
AIAA-2
015-2
366
Nume
rical
and e
xper
imen
tal
inves
tigat
ion of
a be
veled
trail
ing
edge
flow
and n
oise fi
eldW.
van d
er Ve
lden,
S. Pr
öbsti
ng, A
. de
Jong
, A. v
an Zu
ijlen,
Delft
Unive
rsity
of Te
chno
logy,
Delft,
The N
etherl
ands
; Y.
Guan
, S. M
orris,
Univ
ersity
of N
otre D
ame,
Notre
Dam
e, IN
1630
hrs
AIAA-2
015-2
367
On th
e rob
ustn
ess o
f the
TNO
mode
l for
aero
foil s
elf-n
oise
pred
iction
C. Pa
ruchu
ri, O.
Stal
nov,
P. Jo
seph
, C.
Vand
erwel,
B. G
anap
athisu
brama
ni,
Unive
rsity
of So
utham
pton,
South
ampto
n, Un
ited K
ingdo
m; R.
Leun
g, De
fence
Sc
ience
and T
echn
ology
Labo
ratory
, So
utham
pton,
Unite
d King
dom
1700
hrs
AIAA-2
015-2
368
Impa
ct of
Wall
Per
meab
ility
on Tr
ailing
-Edge
Nois
e at H
igh
Reyn
olds N
umbe
rS.
Koh,
M. M
einke
, W. S
chroe
der, R
WTH
Aa
chen
Univ
ersity
, Aac
hen,
Germ
any
Mond
ay, 2
2 Ju
ne 2
015
39-A
A-8
Jet N
oise P
redic
tion
IIIn
vern
ess
Chair
ed by
: D. M
CLAU
GHLIN
, Reti
red14
00 hr
sAIA
A-201
5-236
9Re
cent
prog
ress
in nu
meric
al sim
ulatio
ns fo
r jet
noise
co
mput
ation
usin
g LES
on fu
lly
unstr
uctu
red m
eshe
sN.
Lupo
glazo
ff, F.
Vuillo
t, ON
ERA,
Châti
llon,
Franc
e
1430
hrs
AIAA-2
015-2
370
Jet N
oise P
redic
tion
with
Eddy
Re
laxat
ion So
urce
Mod
elA.
Neife
ld, N
. Reic
he, J
. Dier
ke, R
. Ew
ert, G
erman
Aeros
pace
Cente
r (DL
R),
Brau
nsch
weig,
Germ
any
1500
hrs
AIAA-2
015-2
371
Jet N
oise P
redic
tion
using
a Pe
rmea
ble FW
-H So
lver
A. We
st, CD
-adap
co, L
ondo
n, Un
ited
Kingd
om; M
. Cara
eni, C
D-ada
pco,
Leba
non,
NH
1530
hrs
AIAA-2
015-2
372
Para
metri
c Stu
dy of
Jet N
ozzle
s Us
ing a
RANS
-Bas
ed Je
t Nois
e Pr
edict
ion To
olB.
Venk
atesh
, R. S
elf, U
nivers
ity of
So
utham
pton,
South
ampto
n, Un
ited
Kingd
om
1600
hrs
AIAA-2
015-2
373
Larg
e Edd
y Sim
ulatio
n of
a Ta
ctica
l Ai
rcraf
t Exh
aust
Nozz
le wi
th Fr
ee-
strea
m an
d Wall
Turb
ulenc
eD.
Dah
l, J. N
ichols
, Univ
ersity
of
Minn
esota
, Minn
eapo
lis, M
innea
polis,
MN
51
Mond
ay, 2
2 Ju
ne 2
015
40-A
A-9
Jet N
oise M
easu
reme
nts I
Laliq
ueCh
aired
by: S
. MILL
ER, N
ASA
1400
hrs
AIAA-2
015-2
374
Noise
Red
uctio
n wi
th Fl
uidic
Inse
rts
in Su
perso
nic Je
ts Ex
haus
ting O
ver
a Sim
ulated
Airc
raft
Carri
er D
eck
R. Po
wers,
D. M
cLaug
hlin,
P. Mo
rris,
Penn
sylva
nia S
tate U
nivers
ity, S
tate
Colle
ge, P
A
1430
hrs
AIAA-2
015-2
375
Acou
stic E
missi
ons f
rom
F-35
Aircr
aft d
uring
Gro
und R
un-U
pM.
Jame
s, A.
Salto
n, J.
Down
ing, B
lue
Ridge
Rese
arch a
nd Co
nsult
ing, L
LC,
Ashe
ville,
NC;
K. Ge
e, T.
Neilse
n, B.
Re
ichma
n, Br
igham
Youn
g Univ
ersity
, Pro
vo, U
T; et
al.
1500
hrs
AIAA-2
015-2
376
Spat
iotem
pora
l Cor
relat
ion
Analy
sis of
Jet N
oise f
rom
a High
-Pe
rform
ance
Milit
ary A
ircra
ftB.
Hark
er, T.
Neil
sen,
K. Ge
e, Br
igham
Yo
ung U
nivers
ity, P
rovo,
UT; M
. Jam
es,
Blue R
idge R
esea
rch an
d Con
sultin
g, LLC
, As
hevil
le, N
C; A.
Wall,
Air Fo
rce Re
searc
h La
borat
ory, W
right-
Patte
rson A
FB, O
H
1530
hrs
AIAA-2
015-2
377
Acou
stica
l Env
ironm
ent o
f an
F-35B
Du
ring V
ertic
al La
nding
sB.
Reich
man,
Brigh
am Yo
ung U
nivers
ity,
Provo
, UT;
J. Do
wning
, M. J
ames
, Blue
Rid
ge Re
searc
h and
Cons
ulting
, LLC
, As
hevil
le, N
C; A.
Aube
rt, N
aval
Air W
arfare
Ce
nter, P
atuxe
nt Riv
er, M
D; R.
McK
inley
, A.
Wall,
Air Fo
rce Re
searc
h Lab
orator
y, W
right-
Patte
rson A
FB, O
H; et
al.
1600
hrs
AIAA-2
015-2
378
Sour
ce ch
arac
teriza
tion
of fu
ll-sca
le jet
nois
e usin
g vec
tor i
nten
sity
T. St
out,
K. Ge
e, T.
Neilse
n, A.
Wall,
Brigh
am Yo
ung U
nivers
ity, P
rovo,
UT;
M. Ja
mes,
Blue R
idge R
esea
rch an
d Co
nsult
ing, L
LC, A
shev
ille, N
C
1630
hrs
AIAA-2
015-2
379
Invest
igatio
n of m
ulti-lo
bed fi
ghter
jet
noise
sour
ces us
ing ac
ousti
cal
holog
raph
y and
parti
al fie
ld de
comp
ositio
n meth
ods
A. Wa
ll, Air
Force
Resea
rch La
borat
ory,
Wrigh
t-Patt
erson
AFB,
OH; K
. Gee
, T. N
eilsen
, Bri
gham
Youn
g Univ
ersity,
Prov
o, UT
; S.
McIne
rny, U
nivers
ity of
Louis
iana,
Lafay
ette,
Lafay
ette,
LA; M
. Jam
es, Bl
ue Ri
dge R
esearc
h an
d Con
sultin
g, LLC
, Ashe
ville,
NC
Mond
ay, 2
2 Ju
ne 2
015
41-A
A-10
CAA
Soun
d Gen
erat
ion I
Obeli
sk A
Chair
ed by
: C. T
AM, F
lorida
Stat
e Univ
eristy
1400
hrs
AIAA-2
015-2
380
Hydr
odyn
amic
insta
bility
and s
hear
lay
er ef
fect
on th
e sou
nd em
ission
of
a tu
rbule
nt je
t flam
eS.
Sch
limpe
rt, S
. Koh
, A. F
eldhu
sen,
B.
Roidl
, M. M
einke
, W. S
chroe
der, R
WTH
Aa
chen
Univ
ersity
, Aac
hen,
Germ
any
1430
hrs
AIAA-2
015-2
381
Asse
ssing
Aco
ustic
Sour
ce Fo
rcing
To
ols fo
r Lau
nch
Vehic
le Je
t Nois
e Pr
edict
ionA.
Sescu
, E. C
ollins
, Miss
issipp
i Stat
e Un
iversi
ty, M
ississ
ippi S
tate,
MS; R
. Harr
is,
CFD
Rese
arch C
orpora
tion,
Hunts
ville,
AL
; E. L
uke,
Missi
ssipp
i Stat
e Univ
ersity
, Mi
ssissi
ppi S
tate,
MS
1500
hrs
AIAA-2
015-2
382
Nume
rical
Inve
stiga
tion
of In
direc
t No
ise G
ener
ation
by A
cceler
ated
Vo
rticit
yW.
Ullri
ch, T
echn
ical U
nivers
ity of
Mun
ich,
Garch
ing, G
erman
y; F.
Bake
, Germ
an
Aeros
pace
Cente
r (DL
R), B
erlin,
Germ
any;
N. Ki
ngs,
Natio
nal C
enter
for S
cienti
fic
Rese
arch (
CNRS
), Ch
âtena
y-Mala
bry,
Franc
e; T.
Satte
lmay
er, Te
chnic
al Un
iversi
ty of
Munic
h, Ga
rching
, Germ
any
1530
hrs
AIAA-2
015-2
383
Exten
sion
of th
e Ran
dom
Parti
cle
Mesh
meth
od to
perio
dic tu
rbule
nt
flows
for f
an br
oadb
and n
oise
pred
iction
A. Wo
hlbran
dt, S
. Gue
rin, G
erman
Ae
rospa
ce Ce
nter (
DLR)
, Berl
in, G
erman
y; R.
Ewert
, Germ
an Ae
rospa
ce Ce
nter (
DLR)
, Br
auns
chwe
ig, G
erman
y
1600
hrs
AIAA-2
015-2
384
A stu
dy of
mec
hanis
ms of
soun
d ge
nera
tion
by ai
rfoils
usin
g flow
-ac
ousti
c cor
relat
ions
A. Sa
no, A
. Cav
alieri
, Tec
hnolo
gical
Institu
te of
Aeron
autic
s (ITA
), Sã
o Jos
é do
s Cam
pos,
Braz
il; W.
Wolf
, Univ
ersity
of
Camp
inas,
Camp
inas,
Braz
il
Mond
ay, 2
2 Ju
ne 2
015
42-A
CD-1
Aircr
aft D
esign
for E
nviro
nmen
tal I
mpac
t Red
uctio
nMi
roCh
aired
by: D
. WEL
LS, N
ASA L
angle
y Res
earch
Cente
r14
00 hr
sAIA
A-201
5-238
5Ef
fect
of W
ing Lo
ading
and F
uel
Type
on O
ptim
al Cr
uise A
ltitud
e for
Civ
il Airc
raft
A. Wo
rtman
n, M.
Hoo
greef,
R. Vo
s, De
lft Un
iversi
ty of
Tech
nolog
y, De
lft, Th
e Ne
therla
nds
1430
hrs
AIAA-2
015-2
386
Asse
ssing
Taxii
ng Tr
ade S
pace
s fro
m Ai
rcraf
t, Ai
rpor
t, an
d Airl
ine
Persp
ectiv
esI.
Chak
rabort
y, M.
LeVin
e, M.
Has
san,
D.
Mavri
s, Ge
orgia
Institu
te of
Tech
nolog
y, Atl
anta,
GA
1500
hrs
AIAA-2
015-2
387
Utilis
ing Se
cond
ary A
irpor
ts fo
r RPT
Op
erat
ions:
A Bu
sines
s Cas
eC.
Bil, A
. Geb
reegz
iabhe
r, RMI
T Univ
ersity
, Me
lbourn
e, Au
strali
a
1530
hrs
AIAA-2
015-2
388
Gree
nhou
se G
as Im
pacts
of O
n-De
mand
Elec
tric A
ircra
ftT.
Thom
pson
, LMI
, McLe
an, V
A
1600
hrs
AIAA-2
015-2
389
Aircr
aft N
oise R
educ
tion
Tech
nolog
y an
d Airp
ort N
oise A
nalys
is fo
r Ge
nera
l Avia
tion
Revit
aliza
tion
S. M
in, D
. Lim
, D. M
avris
, Geo
rgia
Institu
te of
Tech
nolog
y, Atl
anta,
GA
1630
hrs
AIAA-2
015-2
390
The C
lean
Sky p
rogr
amme
: en
viron
ment
al be
nefit
s at a
ircra
ft lev
elM.
Brun
et, S
. Aub
ry, R.
Lafag
e, ON
ERA,
Toulo
use,
Franc
e
52
Mond
ay, 2
2 Ju
ne 2
015
43-A
FM-3
Unma
nned
Airc
raft
Syste
ms I
Plum
Blos
som
ACh
aired
by: K
. HOF
FLER
, Ada
ptive
Aeros
pace
Grou
p, Inc
. and
S. D
’SOU
ZA, N
ASA-A
RC14
00 hr
sAIA
A-201
5-239
1Ev
aluat
ion of
Ener
gy R
equir
ed
for F
light
by a
UAV F
itted
with
a Va
riable
-Spa
n Wi
ng P
erfo
rming
a Gi
ven
Missi
on P
rofil
eP.
Santo
s, P.
Gamb
oa, U
nivers
ity of
Beir
a Int
erior,
Covil
ha, P
ortug
al
1430
hrs
AIAA-2
015-2
392
Attit
ude a
nd al
titud
e sta
biliza
tion
of qu
ad ro
tor u
sing p
aram
eter
estim
ation
and s
elf-tu
ning
cont
rolle
rT.
Dief,
S. Yo
shida
, Kyu
shu U
nivers
ity,
Kasu
ga, J
apan
; M. A
bdelh
ady,
Cairo
Un
iversi
ty, G
iza, E
gypt
1500
hrs
AIAA-2
015-2
393
Quick
ness
Crite
ria fo
r Lar
ge
Unma
nned
Airc
raft
in No
n-Pr
ecisi
on A
ggre
ssive
and N
on-
Aggr
essiv
e Man
euve
rsK.
Gree
ne, D
. Kun
z, Air
Force
Insti
tute o
f Te
chno
logy,
Wrig
ht-Pa
tterso
n AFB
, OH
1530
hrs
AIAA-2
015-2
394
An A
ssessm
ent o
f Unm
anne
d Ai
rcraf
t Sys
tem Le
vel-T
urn
Mane
uver
Per
form
ance
Re
quire
ment
s In
Relat
ion to
a Qu
antifi
ed W
ell-C
lear D
efinit
ionD.
Jack
, K. H
offler,
S. J
ohns
on, A
dapti
ve
Aeros
pace
Grou
p, Inc
., Ha
mpton
, VA
1600
hrs
AIAA-2
015-2
395
Objec
tive F
uncti
on D
evelo
pmen
t fo
r Opt
imize
d Pat
h Gu
idanc
e for
Ro
torcr
aft S
hipbo
ard R
ecov
ery
J. Tri
tschle
r, Nav
al Air
Sys
tems C
omma
nd,
Patux
ent R
iver, M
D; J.
Horn
, Pen
nsylv
ania
State
Univ
ersity
, Stat
e Coll
ege,
PA
1630
hrs
AIAA-2
015-2
396
Wake
Vorte
x De
tectio
n wi
th U
AV
Close
Form
ation
Fligh
tH.
Chao
, Univ
ersity
of Ka
nsas
, Law
rence
, La
wren
ce, K
S; Y.
Gu,
West
Virgin
ia Un
iversi
ty, M
organ
town,
WV;
P. Tia
n, Z.
Zhen
g, Un
iversi
ty of
Kans
as, L
awren
ce,
Lawr
ence
, KS;
M. N
apoli
tano,
West
Virgin
ia Un
iversi
ty, M
organ
town,
WV
1700
hrs
AIAA-2
015-2
397
Fligh
t Tes
t Eva
luatio
n of
Pilo
t Co
ntro
l Int
erfa
ces f
or R
emot
ely
Pilot
ed Ve
hicles
R. Ol
son,
Natio
nal T
est P
ilot S
choo
l, Mo
jave,
CA
Mond
ay, 2
2 Ju
ne 2
015
44-A
FM-4
Plane
tary
Entry
and A
eroa
ssist
Tech
nolog
yPlu
m Bl
osso
m B
Chair
ed by
: S. D
UTTA
, NAS
A Lan
gley R
esea
rch Ce
nter a
nd C.
KARL
GAAR
D, An
alytic
al Me
chan
ics As
socia
tes In
c14
00 hr
sAIA
A-201
5-239
8Im
prov
emen
ts to
Entry
Term
inal
Point
Cont
rolle
r for
Mar
s At
mosp
heric
Entry
Y. Zh
eng,
H. Cu
i, Y. T
ian, H
arbin
Institu
te of
Tech
nolog
y, Ha
rbin,
China
1430
hrs
AIAA-2
015-2
399
Optim
izatio
n of
Inter
ior P
oint C
ost
Func
tions
Usin
g Ind
irect
Meth
ods
T. An
tony,
M. G
rant,
Purdu
e Univ
ersity
, We
st La
fayett
e, IN
; M. B
olend
er, Ai
r Forc
e Re
searc
h Lab
orator
y, W
right-
Patte
rson
AFB,
OH
1500
hrs
AIAA-2
015-2
401
Rapid
, Rob
ust T
rajec
tory D
esign
Usin
g Ind
irect
Optim
izatio
n Meth
ods
M. Gr
ant, P
urdue
Unive
rsity,
West
Lafay
ette,
IN; M
. Bole
nder,
Air F
orce R
esearc
h La
borat
ory, W
right-
Patte
rson A
FB, O
H
1530
hrs
AIAA-2
015-2
402
Minim
um Te
rmina
l Ene
rgy
Optim
izatio
ns of
Hyp
erson
ic Veh
icles
Using
Indir
ect M
ethod
sM.
Gran
t, Purd
ue Un
iversit
y, We
st La
fayett
e, IN;
M. B
olend
er, Ai
r Forc
e Rese
arch
Labo
ratory
, Wrig
ht-Pa
tterso
n AFB
, OH
Mond
ay, 2
2 Ju
ne 2
015
45-A
MT-3
/GT-3
Adva
nces
in Te
st Me
thod
ology
and C
FD In
tegra
tion
Obeli
sk B
Chair
ed by
: S. D
UNN,
Jaco
bs Te
chno
logy a
nd S
. COL
E, NA
SA La
ngley
Rese
arch C
enter
1400
hrs
AIAA-2
015-2
403
Deve
lopme
nt of
a Tra
nson
ic Gu
st Ri
g for
Simu
lation
of Ve
rtica
l Gus
ts on
Half
-mod
elsN.
Allen
, M. Q
uinn,
Aircra
ft Re
searc
h As
socia
tion,
Ltd.,
Bedfo
rd, U
nited
King
dom
1430
hrs
AIAA-2
015-2
404
F-35
Conv
entio
nal M
ode J
et-Ef
fects
Te
sting
Meth
odolo
gyM.
McW
aters,
Lock
heed
Mart
in Co
rporat
ion, F
ort W
orth,
TX
1500
hrs
AIAA-2
015-2
405
Motio
n me
asur
emen
t of a
wind
tu
nnel
mode
l by s
tereo
vision
tec
hniqu
eB.
Mart
inez,
D. B
idino
, M. B
astid
e, C.
Deme
autis
, F. L
eopo
ld, P.
Wey
, Fren
ch-
Germ
an Re
searc
h Ins
titute
of Sa
int-Lo
uis
(ISL)
, Sain
t-Lou
is, Fr
ance
1530
hrs
AIAA-2
015-2
406
Expe
rimen
tal In
vesti
gatio
ns ab
out
Heat
Trans
fer Ch
arac
terist
ics of
Irr
egula
r Imp
ingem
ent J
et Ar
rays
in
Typic
al Ac
tive C
leara
nce C
ontro
l Sy
stem
F. Liu,
M. J
unku
i, Nan
jing Un
iversit
y of
Aeron
autics
and A
stron
autics
, Nan
jing, C
hina
Mond
ay, 2
2 Ju
ne 2
015
46-A
MT-4
/GT-4
Surfa
ce an
d Infl
ow Se
nsing
Edelw
eiss
Chair
ed by
: Z. Z
HANG
, Univ
ersity
of Te
nnes
see a
nd T.
IOPP
OLO,
Sou
thern
Metho
dist U
nivers
ity14
00 hr
sAIA
A-201
5-240
7Sh
ear S
tress
Sens
ing w
ith El
astic
Mi
crofe
nce S
tructu
res
A. Cis
otto,
F. Pa
lmier
i, NAS
A Lan
gley
Rese
arch C
enter
, Ham
pton,
VA; Y
. Lin,
Na
tiona
l Insti
tute o
f Aero
spac
e, Ha
mpton
, VA
; A. S
aini, J
. Kim
, T. K
im, N
orth C
arolin
a St
ate U
nivers
ity, R
aleigh
, NC;
et al.
1430
hrs
AIAA-2
015-2
408
Deve
lopme
nt of
a So
l-Gel
Base
d Na
nopo
rous
uns
teady
Pre
ssure
Se
nsitiv
e Pain
t and
Valid
ation
in
the L
arge
Tran
sonic
One
ra S2
MA
Wind
tunn
elY.
Mich
ou, B
. Dele
glise
, F. L
ebrun
, ONE
RA,
Moda
ne, F
rance
; E. S
colan
, A. G
rivel,
R.
Steig
er, S
wiss
Cente
r for
Electr
onics
and
Micro
techn
ology
(CSE
M), N
eûch
atel,
Switz
erlan
d; et
al.
1500
hrs
AIAA-2
015-2
409
A Co
unter
-Pro
paga
ting L
aser
Air
Spee
d Sen
sor S
ystem
for A
ircra
ftJ.
Kurtz
, Univ
ersity
of N
ew S
outh
Wales
, Ca
nberr
a, Au
strali
a; S.
Witti
g, OH
B Sy
stem
HB, M
unich
, Germ
any;
S. O
’Byrn
e, Un
iversi
ty of
New
South
Wale
s, Ca
nberr
a, Au
strali
a
1530
hrs
AIAA-2
015-2
410
Comp
utat
ional
Mode
ling o
f Ra
diatio
n Ef
fects
on To
tal
Temp
erat
ure P
robe
sJ.
Reard
on, J
. Sch
etz, K
. Low
e, Vir
ginia
Polyt
echn
ic Ins
titute
and S
tate U
nivers
ity,
Black
sburg
, VA
53
Mond
ay, 2
2 Ju
ne 2
015
47-A
PA-5
Appli
ed CF
D &
Nume
rical
Corre
lation
s with
Expe
rimen
tal D
ata I
Stemm
ons B
Chair
ed by
: D. F
INLE
Y, Lo
ckhe
ed M
artin
Aeron
autic
s and
J. S
LOTN
ICK, B
oeing
Engin
eerin
g Ope
ration
s & Te
chno
logy
1400
hrs
AIAA-2
015-2
411
Supe
rsonic
Pro
jectile
Stee
ring u
sing
Micro
-Actu
ator
s: Ex
perim
enta
l and
Nu
meric
al Stu
dyM.
Libs
ig, B
. Mart
inez,
C. Re
y, T.
Gauth
ier,
P. We
y, C.
Berne
r, Fren
ch-Ge
rman
Rese
arch
Institu
te of
Saint
-Louis
(ISL
), Sa
int-Lo
uis,
Franc
e; et
al.
1430
hrs
AIAA-2
015-2
412
Effe
cts of
Tip C
leara
nce o
n Mi
niatu
re G
as Tu
rbine
s Com
pres
sor
Perfo
rman
ce: A
Num
erica
l Ap
proa
chJ.
Xiang
, J. S
chlut
er, F.
Dua
n, Na
nyan
g Te
chno
logica
l Univ
ersity
, Sing
apore
, Sin
gapo
re
1500
hrs
AIAA-2
015-2
413
Nume
rical
Simula
tion
of W
ater
Sp
ray C
ause
d by a
Roll
ing A
irplan
e Tir
eQ.
Qu,
F. Zh
ang,
P. Liu
, Beih
ang U
nivers
ity,
Beijin
g, Ch
ina; R
. Aga
rwal,
Was
hingto
n Un
iversi
ty in
St. L
ouis,
St.
Louis
, MO
Mond
ay, 2
2 Ju
ne 2
015
48-A
PA-6
Unma
nned
, Bio-
Insp
ired,
Solar
Pow
ered
Aer
ial Ve
hicle
Desig
ns I
Carp
enter
Ball
room
Chair
ed by
: L. U
KEILE
Y, Un
iversi
ty of
Florid
a14
00 hr
sAIA
A-201
5-241
4Co
mput
ation
al Stu
dies f
or th
e De
velop
ment
of a
Hybr
id UA
V/UU
VR.
Rama
murti,
J. G
eder,
D. E
dward
s, T.
Youn
g, Na
val R
esea
rch La
borat
ory,
Wash
ington
, DC
1430
hrs
AIAA-2
015-2
415
Force
Pro
ducti
on by
Wing
Flap
ping:
The R
ole of
Stro
ke A
ngle
of A
ttack
an
d Loc
al Re
ynold
s Num
ber
A. Re
ge, B
. Den
nis, K
. Sub
barao
, Un
iversi
ty of
Texa
s, Arl
ington
, Arlin
gton,
TX 15
00 hr
sAIA
A-201
5-241
6Sy
stem
Deve
lopme
nt fo
r Wild
fire
SUAS
J. Ja
cob,
D. G
abbe
rt, M
. And
alibi,
Ok
lahom
a Stat
e Univ
ersity
, Still
water
, OK
Mond
ay, 2
2 Ju
ne 2
015
49-A
PA-7
Spec
ial Se
ssion
: Aer
odyn
amic-
Struc
tura
l Mod
eling
, Opt
imiza
tion,
and T
est T
echn
iques
for F
lexibl
e Wing
Tech
nolog
y ISte
mmon
s ACh
aired
by: N
. NGU
YEN,
NAS
A-Ame
s Res
earch
Cente
r and
S. A
NDER
S14
00 hr
sAIA
A-201
5-241
7Wi
nd Tu
nnel
Invest
igatio
n of a
Flex
ible
Wing
High
-Lift
Confi
gura
tion w
ith a
Varia
ble Ca
mber
Conti
nuou
s Tra
iling
Edge
Flap
Desi
gnN.
Ngu
yen,
NASA
Ames
Resea
rch Ce
nter,
Moffe
tt Field
, CA;
N. Pr
ecup,
E. Liv
ne,
Unive
rsity o
f Wash
ington
, Sea
ttle, S
eattle
, WA
; J. U
rnes,
The B
oeing
Comp
any,
St.
Louis
, MO;
E. Di
ckey,
The B
oeing
Comp
any,
Hunti
ngton
Beach
, CA;
C. Ne
lson,
The B
oeing
Co
mpan
y, Se
attle,
WA;
et al.
1430
hrs
AIAA-2
015-2
418
Use o
f a Vi
scous
Flow
Simu
lation
Co
de fo
r Sta
tic A
eroe
lastic
Ana
lysis
of a
Wing
at H
igh-Li
ft Co
nditio
nsH.
Akay
din, S
. Moin
i-Yek
ta, J.
Hou
sman
, N.
Ngu
yen,
NASA
Ames
Rese
arch C
enter
, Mo
ffett
Field,
CA
1500
hrs
AIAA-2
015-2
419
Optim
izatio
n of
an A
eros
ervo
elasti
c Wi
ng w
ith D
istrib
uted
Mult
iple
Cont
rol S
urfa
ces
B. S
tanfor
d, NA
SA La
ngley
Rese
arch
Cente
r, Ham
pton,
VA
1530
hrs
AIAA-2
015-2
420
Adap
tive A
eroe
lastic
Wing
Sh
ape O
ptim
izatio
n fo
r High
-Lift
Confi
gura
tions
G. Fu
jiwara
, Univ
ersity
of W
ashin
gton,
Seatt
le, S
eattle
, WA;
N. N
guye
n, NA
SA
Ames
Rese
arch C
enter
, Moff
ett Fi
eld, C
A
1600
hrs
AIAA-2
015-2
421
Robu
st Op
timiza
tion
of Va
riable
-Ca
mber
Cont
inuou
s Tra
iling-
Edge
Fla
p Sys
tem A
ction
Usin
g Sto
chas
tic
Krigi
ngY.
Liu, J
. Bai,
Nort
hwes
tern P
olytec
hnica
l Un
iversi
ty, X
i’an,
China
; E. L
ivne,
Unive
rsity
of Wa
shing
ton, S
eattle
, Se
attle,
WA
1630
hrs
AIAA-2
015-2
422
A 3-
D Dr
ag O
ptim
izatio
n Stu
dy
of Va
riable
Camb
er Co
ntinu
ous
Trailin
g Edg
e Flap
(VCC
TEF)
Usin
g OV
ERFL
OWU.
Kaul,
N. N
guye
n, NA
SA Am
es Re
searc
h Ce
nter, M
offett
Field
, CA
54
Mond
ay, 2
2 Ju
ne 2
015
50-A
PA-8
Flow
Cont
rol A
pplic
ation
s & D
emon
strat
ions (
Activ
e & P
assiv
e) I
Stemm
ons C
Chair
ed by
: J. G
EORG
E, Me
trolas
er Inc
. and
K. M
ULLE
NERS
, Leib
niz U
nivers
itaet
Hann
over
1400
hrs
AIAA-2
015-2
423
Study
of sla
nted p
erfor
ated s
hape
s in
tabs f
or co
ntrol
of su
bson
ic Jets
A. Re
yaz A
hmed
, KCG
Colleg
e of T
echno
logy,
Chen
nai, I
ndia;
S. Th
aniga
iarasu
, Mad
ras
Institu
te of
Techn
ology,
Chen
nai, I
ndia;
S.
Venk
atram
an, K
CG Co
llege o
f Tech
nolog
y, Ch
enna
i, Ind
ia; E.
Sriniv
asan,
Bhara
th Un
iversit
y, Ch
enna
i, Ind
ia; E.
Ratha
krishn
an,
Indian
Instit
ute of
Techn
ology
Kanp
ur, Ka
npur,
Ind
ia
1430
hrs
AIAA-2
015-2
424
Nume
rical
Study
of th
e Int
erna
l Flo
w Str
uctu
res I
nside
the S
weep
ing
Jet A
ctuat
orK.
Kara,
Khali
fa Un
iversi
ty, Ab
u Dha
bi,
Unite
d Arab
Emira
tes
1500
hrs
AIAA-2
015-2
425
Effe
ct of
Span
wise
Jet S
pacin
g on
Sepa
ratio
n Co
ntro
l for
Swep
t and
Un
swep
t Airf
oils
M. W
alker,
K. H
ipp, S
. Ben
ton, J
. Bon
s, Oh
io St
ate U
nivers
ity, C
olumb
us, O
H
1530
hrs
AIAA-2
015-2
426
Dyna
mic F
low Co
ntro
l ove
r Ae
rody
nami
c Bod
ies u
sing P
hase
d Ar
ray V
ecto
red S
ynth
etic J
et Ac
tuat
ionZ.
Hasn
ain, R
. Wein
stein,
L. Tr
olling
er,
J. Hu
bbard
, A. F
latau
, Univ
ersity
of
Maryl
and,
Colle
ge Pa
rk, Co
llege
Park,
MD
1600
hrs
AIAA-2
015-2
427
Stoch
astic
analy
sis of
aero
dyna
mic
force
s acti
ng on
a se
lf-ad
aptiv
e ca
mber
airfo
il in
turb
ulent
inflo
wG.
Kamp
ers, C
arl vo
n Ossi
etzky
Univ
ersity
, Ol
denb
urg, G
erman
y; U.
Corde
s, C.
Trope
a, Te
chnic
al Un
iversi
ty of
Darm
stadt,
Da
rmsta
dt, G
erman
y; M.
Hoe
lling,
J. Pe
inke,
Carl v
on O
ssietz
ky U
nivers
ity,
Olde
nburg
, Germ
any
Mond
ay, 2
2 Ju
ne 2
015
51-A
TIO-5
Term
inal &
Surfa
ce O
pera
tions
IIMa
nche
ster
Chair
ed by
: A. S
ARAF
, Saa
b Sen
sis Co
rporat
ion14
00 hr
sAIA
A-201
5-242
8Sc
hedu
ling a
nd D
elive
ring A
ircra
ft to
Dep
artu
re Fi
xes i
n th
e NY
Metro
plex
with
Cont
rolle
r-Man
aged
Sp
acing
Tools
E. Ch
evall
ey, B
. Park
e, J.
Kraut,
N.
Biene
rt, F.
Oma
r, E. P
almer,
NAS
A Ame
s Re
searc
h Cen
ter, M
offett
Field
, CA
1430
hrs
AIAA-2
015-2
429
Stoch
astic
Nea
r-Opt
imal
Cont
rol
for A
ircra
ft Ar
rival
Sequ
encin
g and
Co
nflict
Res
olutio
nY.
Matsu
no, T
. Tsu
chiya
, Univ
ersity
of
Toky
o, Bu
nkyo
, Jap
an
1500
hrs
AIAA-2
015-2
430
Time B
ased
Sepa
ratio
n: A
stud
y int
o run
way c
ompr
essio
n an
d tim
e ba
sed s
epar
ation
R. Cu
rran,
F. He
rrema
, W. Z
hao,
Delft
Unive
rsity
of Te
chno
logy,
Delft,
The
Nethe
rland
s; V.
Treve
, R. G
raham
, EU
ROCO
NTRO
L, Br
etign
y, Fra
nce
1530
hrs
AIAA-2
015-2
431
Desig
ning a
nd Ev
aluat
ing A
dvan
ced
Appr
oach
Pro
cedu
res f
or th
e Co
ncep
t of S
egme
nted
Inde
pend
ent
Para
llel A
ppro
ache
sC.
Hans
es, F
. Kna
be, B
. Korn
, Germ
an
Aeros
pace
Cente
r (DL
R), B
rauns
chwe
ig,
Germ
any
1600
hrs
AIAA-2
015-2
432
Optim
al Ai
rspac
e Des
ign fo
r Co
ntinu
ous C
limb O
pera
tion
E. Kim
, S. H
ong,
K. Le
e, Ko
rea Ae
rospa
ce
Unive
rsity,
Goy
ang,
South
Korea
1630
hrs
AIAA-2
015-2
433
Asse
ssmen
t of D
elaye
d De
celer
ation
App
roac
h Op
portu
nities
at U
S Airp
orts
T. Re
ynold
s, M.
McP
artlan
d, Y.
Rodri
guez
, M.
San
dberg
, J. V
enuti
, Linc
oln La
borat
ory,
Massa
chus
etts I
nstitu
te of
Tech
nolog
y, Le
xingto
n, MA
Mond
ay, 2
2 Ju
ne 2
015
52-A
TIO-6
Fleet
and R
oute
Plann
ingMi
ngCh
aired
by: W
. CRO
SSLE
Y, Pu
rdue U
nivers
ity14
00 hr
sAIA
A-201
5-243
4Ef
fects
of Fu
el Pr
ice on
Tota
l Fue
l Bu
rn an
d Sys
tem Ca
pacit
y- A
n An
alysis
of A
dvan
ced E
ngine
and
Airfr
ame T
echn
ology
and A
irline
Re
spon
ses t
o Cha
nges
in Fu
el Pr
iceC.
Murph
y, B.
Mille
r, Metr
on Av
iation
, Inc
., Du
lles,
VA; L
. She
rry, G
eorge
Mas
on
Unive
rsity,
Fairfa
x, VA
1430
hrs
AIAA-2
015-2
435
Estim
ating
the F
uel S
aving
Po
tentia
l of C
omme
rcial
Aircr
aft
in Fu
ture
Flee
t-Dev
elopm
ent
Scen
arios
N. Ra
ndt,
L. Wa
che,
Tech
nical
Unive
rsity
of Mu
nich,
Munic
h, Ge
rman
y; C.
Jessb
erger,
K.
Ploetn
er, B
auha
us Lu
ftfah
rt e.V
., Mu
nich,
Germ
any
1500
hrs
AIAA-2
015-2
436
Enab
ling T
echn
ology
Por
tfolio
Se
lectio
n th
roug
h Qu
antit
ative
Un
certa
inty A
nalys
isK.
Gatia
n, D.
Mav
ris, G
eorgi
a Ins
titute
of Te
chno
logy,
Atlan
ta, G
A
1530
hrs
AIAA-2
015-2
437
A Ra
pid In
tegra
ted In
terde
pend
ent
Fleet-
Leve
l Env
ironm
enta
l Mod
elJ.
Berna
rdo, T
. Zaid
i, M. L
eVine
, H.
Jimen
ez, D
. Mav
ris, G
eorgi
a Ins
titute
of Te
chno
logy,
Atlan
ta, G
A
1600
hrs
AIAA-2
015-2
438
Mode
ling A
irline
Dec
ision
s on
Rout
e Pla
nning
Usin
g Disc
rete
Choic
e Mo
dels
Z. Sh
a, K.
Moolc
hand
ani, A
. Mah
eshw
ari,
J. Th
ekine
n, J.
Panc
hal, D
. DeL
auren
tis,
Purdu
e Univ
ersity
, Wes
t Lafa
yette
, IN
1630
hrs
AIAA-2
015-2
439
Land
scape
Ana
lysis
Fram
ewor
k fo
r Lo
w Ca
rbon
Ener
gyP.
Vasci
k, Ma
ssach
usett
s Ins
titute
of Te
chno
logy,
Camb
ridge
, MA;
R. Pe
arce,
NASA
Hea
dqua
rters,
Was
hingto
n, DC
; D.
Rhod
es, M
assa
chus
etts I
nstitu
te of
Tech
nolog
y, Ca
mbrid
ge, M
A
Mond
ay, 2
2 Ju
ne 2
015
53-A
TIO-7
Syste
ms En
ginee
ring a
nd A
nalys
isMi
lanCh
aired
by: P
. HOL
LINGS
WOR
TH, T
he U
nivers
ity of
Man
ches
ter14
00 hr
sAIA
A-201
5-244
0Kn
owled
ge En
ginee
ring -
Fo
rmali
zing t
he En
ginee
ring
Scien
ce D
iscipl
ineX.
Peng
, B. C
hudo
ba, U
nivers
ity of
Texa
s, Arl
ington
, Arlin
gton,
TX
1430
hrs
AIAA-2
015-2
441
Pavin
g the
Way
from
the P
ast t
o th
e Fut
ure:
AVDKB
S , a So
ftwar
e De
velop
ment
in K
nowl
edge
En
ginee
ring
X. Pe
ng, B
. Chu
doba
, Univ
ersity
of Te
xas,
Arling
ton, A
rlingto
n, TX
1500
hrs
AIAA-2
015-2
442
Para
metri
c Asse
ssmen
t of A
viatio
n En
viron
ment
al Go
als: I
mplic
ation
s on
R&D
Dec
ision
Mak
ingM.
Has
san,
A. Pa
yan,
S. O
’Sull
ivan,
H.
Pfaen
der, D
. Mav
ris, G
eorgi
a Ins
titute
of Te
chno
logy,
Atlan
ta, G
A
1530
hrs
AIAA-2
015-2
443
Selec
ted A
rray o
f Tec
hnolo
gy an
d Sy
stems
Opt
ions f
or Ec
ologic
ally
Resp
onsib
le Av
iation
A. Isi
kvere
n, D.
Empl,
U. K
ling,
K. Plo
etner,
C. Po
rnet,
Bauh
aus L
uftfah
rt e.V
., Ot
tobrun
n, Ge
rman
y
55
Mond
ay, 2
2 Ju
ne 2
015
54-A
TIO-8
14
00 -
1600
hrs
Trans
form
ation
al Fli
ght -
Enab
ling t
he N
ext B
illion
Doll
ar A
viatio
n Ma
rket
thro
ugh
Auto
nomy
Metro
polita
n Ba
llroo
m
Mode
rator:
Mark
Ball
in, N
ASA L
angle
y Res
earch
Cente
r
Pan
elists
:Da
nette
Alle
nAu
tonom
y Inc
ubato
r, NAS
A Lan
gley R
esea
rch Ce
nter
Nick
Roy
MIT
Craig
Woo
lsey
Virgin
ia Te
ch
Mond
ay, 2
2 Ju
ne 2
015
55-C
FD-5
Unstr
uctu
red H
igh-O
rder
Meth
ods I
IGr
and B
allro
om A
Chair
ed by
: H. H
UYNH
, NAS
A Glen
n Res
earch
Cente
r and
A. JA
MESO
N, Ae
ronau
tics a
nd As
trona
utics
1400
hrs
AIAA-2
015-2
444
A Su
rvey
of th
e Ise
ntro
pic Eu
ler
Vorte
x Pr
oblem
usin
g High
-Ord
er
Meth
ods
S. S
piege
l, H. H
uynh
, J. D
eBon
is, N
ASA
Glenn
Rese
arch C
enter
, Clev
eland
, OH
1430
hrs
AIAA-2
015-2
445
High
-Ord
er H
yper
bolic
Res
idual-
Distr
ibutio
n Sc
heme
s on
Arbit
rary
Tri
angu
lar G
rids
A. Ma
zahe
ri, NA
SA La
ngley
Rese
arch
Cente
r, Ham
pton,
VA; H
. Nish
ikawa
, Na
tiona
l Insti
tute o
f Aero
spac
e, Ha
mpton
, VA
1500
hrs
AIAA-2
015-2
446
High
-Ord
er M
ethod
s for
Co
nser
vatio
n La
ws Em
ployin
g Em
bedd
ed St
ructu
red E
lemen
t Me
thod
on U
nstru
cture
d He
xahe
dral
Grid
J. Ch
oi, U
nivers
ity of
Mary
land,
Colle
ge
Park,
Colle
ge Pa
rk, M
D
1530
hrs
AIAA-2
015-2
447
Stabil
izatio
n of
High
-Ord
er
Meth
ods f
or U
nstru
cture
d Grid
s wi
th Lo
cal F
ourie
r Spe
ctral
Filter
ing: h
igh-R
e Sim
ulatio
ns in
Co
arse
Mes
hes
M. Ló
pez-M
orales
, A. J
ames
on, S
tanfor
d Un
iversi
ty, S
tanfor
d, CA
1600
hrs
AIAA-2
015-2
448
A Cla
ss of
Ros
enbr
ock
Meth
ods
for a
Rec
onstr
ucted
Disc
ontin
uous
Ga
lerkin
Meth
od fo
r the
Uns
teady
Co
mpre
ssible
Flow
sX.
Liu,
H. Lu
o, No
rth Ca
rolina
Stat
e Un
iversi
ty, Ra
leigh
, NC;
Y. Xia
, Ida
ho
Natio
nal L
abora
tory,
Idaho
Falls,
ID
Mond
ay, 2
2 Ju
ne 2
015
56-C
FD-6
Nove
l Disc
retiz
ation
sGr
and B
allro
om B
Chair
ed by
: J. E
KATE
RIN, I
ACM
and M
. CHO
UDHA
RI, N
ASA-L
angle
y Res
earch
Cente
r14
00 hr
sAIA
A-201
5-244
9In
vesti
gatio
ns of
a Ne
w Sc
heme
for
Wave
Pro
paga
tion
D. Fa
n, P.
Roe,
Unive
rsity
of Mi
chiga
n, An
n Arb
or, An
n Arbo
r, MI
1430
hrs
AIAA-2
015-2
450
Activ
e Flux
for A
dvec
tion
Diffu
sion
H. N
ishika
wa, N
ation
al Ins
titute
of Ae
rospa
ce, H
ampto
n, VA
1500
hrs
AIAA-2
015-2
451
Alter
nativ
e For
mulat
ions f
or
First-
, Sec
ond-
, and
Third
-Ord
er
Hype
rboli
c Nav
ier-S
toke
s Sch
emes
H. N
ishika
wa, N
ation
al Ins
titute
of Ae
rospa
ce, H
ampto
n, VA
1530
hrs
AIAA-2
015-2
452
Rece
nt P
rogr
esse
s on
a Mes
hless
Euler
Solve
r for
Comp
ressi
ble Fl
ows
Z. Du
an, Z
. Wan
g, Un
iversi
ty of
Kans
as,
Lawr
ence
, Law
rence
, KS;
B. V
u, NA
SA
Kenn
edy S
pace
Cente
r, Cap
e Can
avera
l, FL
1600
hrs
AIAA-2
015-2
453
A Ve
rsatile
Non
linea
r Pre
dictiv
e Mo
delin
g App
roac
hM.
Liou
, NAS
A Glen
n Res
earch
Cente
r, Cle
velan
d, OH
; W. Y
ao, Q
ueen
’s Un
iversi
ty,
Belfa
st, U
nited
King
dom
1630
hrs
AIAA-2
015-2
454
Dyna
mica
l sele
ctive
filte
ring f
or th
e La
ttice
Bolt
zman
n Me
thod
S. M
arie,
Natio
nal C
onse
rvator
y of A
rts
and C
rafts,
Paris
, Fran
ce; X
. Gloe
rfelt,
Paris
Insti
tute o
f Tec
hnolo
gy, P
aris,
Franc
e
Mond
ay, 2
2 Ju
ne 2
015
57-C
FD-7
Inter
discip
linar
y CFD
ICo
ral
Chair
ed by
: L. M
ARTIN
ELLI,
Princ
eton U
nivers
ity an
d S. E
YI, M
iddle
East
Tech
nical
Unive
rsity
1400
hrs
AIAA-2
015-2
455
CFD-
base
d Gus
t Loa
d Ana
lysis
for
a Fre
e-fly
ing Fl
exibl
e Pas
seng
er
Aircr
aft i
n Co
mpar
ison
to a
DLM-
base
d App
roac
hL.
Reim
er, M
. Ritte
r, R. H
einric
h, W.
Krü
ger, G
erman
Aeros
pace
Cente
r (DL
R),
Brau
nsch
weig,
Germ
any
1430
hrs
AIAA-2
015-2
456
Influ
ence
of W
all Vi
brat
ion on
the
Aero
Per
form
ance
of Tr
anso
nic
Diffu
ser
C. Ya
o, G.
Zhan
g, F.
Xu, Z
. Liu,
Harb
in Ins
titute
of Te
chno
logy,
Harbi
n, Ch
ina
1500
hrs
AIAA-2
015-2
457
Nume
rical
Analy
sis of
Synt
hetic
Jet
in Cr
ossfl
owA.
Gupte
, A. P
radee
p, P.
Mujum
dar, I
ndian
Ins
titute
of Te
chno
logy B
omba
y, Mu
mbai,
Ind
ia
1530
hrs
AIAA-2
015-2
458
Perfo
rman
ces o
f New
ton
and
Prec
ondit
ioned
New
ton-
GMRE
S Me
thod
s in
Hype
rsonic
Flow
So
lution
sY.
Muslu
bas,
S. Ey
i, Midd
le Ea
st Te
chnic
al Un
iversi
ty, An
kara,
Turke
y
56
Mond
ay, 2
2 Ju
ne 2
015
58-C
FD-8
Turb
ulenc
e Mod
eling
and U
ncer
taint
y Qua
ntifi
catio
nEm
erald
Chair
ed by
: D. Y
ODER
, NAS
A Glen
n Res
earch
Cente
r and
K. D
URAIS
AMY,
Stan
ford U
nivers
ity14
00 hr
sAIA
A-201
5-245
9Qu
antifi
catio
n of
Turb
ulenc
e Mo
delin
g Unc
erta
inties
Usin
g Full
Fie
ld In
versi
onE.
Paris
h, K.
Durai
samy
, Univ
ersity
of
Mich
igan,
Ann A
rbor, A
nn Ar
bor, M
I
1430
hrs
AIAA-2
015-2
460
Mach
ine Le
arnin
g Meth
ods f
or
Data
-Driv
en Tu
rbule
nce M
odeli
ngZ.
Zhan
g, K.
Durai
samy
, Univ
ersity
of
Mich
igan,
Ann A
rbor, A
nn Ar
bor, M
I
1500
hrs
AIAA-2
015-2
461
Uncer
tainty
Qua
ntific
ation
of
Turb
ulenc
e Mod
el Clo
sure
Coeffi
cients
for
Tran
sonic
Wall
-Bou
nded
Flow
sJ.
Scha
efer, T
. West
, S. H
osder,
Miss
ouri
Unive
rsity o
f Scie
nce an
d Tech
nolog
y, Ro
lla,
MO; C
. Rum
sey, J
. Carl
son, W
. Kleb
, NAS
A La
ngley
Resea
rch Ce
nter, H
ampto
n, VA
1530
hrs
AIAA-2
015-2
462
A Sc
ale-A
dapt
ive Va
riant
of th
e Sp
alart-
Allm
aras
Eddy
-Visc
osity
Mo
del
J. Co
der, P
enns
ylvan
ia St
ate U
nivers
ity,
State
Colle
ge, P
A
1600
hrs
AIAA-2
015-2
463
PANS
Simu
lation
s of T
urbu
lent
Sepa
rated
Flow
over
a Wa
ll-mo
unted
Hum
pD.
Higu
era Ca
ubilla
, Univ
ersity
of To
ulous
e, To
ulous
e, Fra
nce;
P. Ra
zi, Te
xas A
&M
Unive
rsity,
Colle
ge S
tation
, TX;
S. S
ekha
r, N.
Man
sour,
NAS
A Ame
s Res
earch
Cente
r, Mo
ffett
Field,
CA; S
. Girim
aji, T
exas
A&M
Unive
rsity,
Colle
ge S
tation
, TX
1630
hrs
AIAA-2
015-2
464
A log
arith
mic f
ormu
lation
for
low-R
eyno
lds n
umbe
r tur
bulen
ce
mode
ls wi
th ad
aptiv
e wall
-func
tions
L. Fra
zza,
A. Ha
y, D.
Pelle
tier, É
cole
Polyt
echn
ique d
e Mon
tréal,
Mon
tréal,
Ca
nada
Mond
ay, 2
2 Ju
ne 2
015
59-F3
60-2
/CAS
E-2
1400
- 17
00 h
rsWh
atev
er H
appe
ned t
o the
Four
-Year
Airp
lane?
Gran
d Ball
room
E
Mode
rator:
Craig
Willi
s, Gr
oup H
ead f
or Sy
stems
Verifi
catio
n, Gu
lfstre
am G
500/
G600
Prog
ram, G
ulfstr
eam
Aeros
pace
Corpo
ration
P
aneli
sts:
Cath
erine
Ferri
e Kilm
ainEx
ecuti
ve V
ice Pr
eside
nt of
Engin
eerin
gBe
ll Heli
copte
r
Eric
Schr
ock
Depu
ty Dir
ector
, Tec
hnolo
gy D
evelo
pmen
t and
Prod
uct I
ntegra
tion
Lock
heed
Mart
in Co
rporat
ion
Mond
ay, 2
2 Ju
ne 2
015
60-FD
-6/P
DL-2
Plasm
a Aer
odyn
amics
& Fl
ow Co
ntro
l II
Gove
nors
Lectu
re H
allCh
aired
by: D
. WILL
IAMS,
Illino
is Ins
titute
of Te
chno
logy a
nd J.
LITT
LE, T
he U
nivers
ity of
Arizo
na14
00 hr
sAIA
A-201
5-246
5PI
V and
Elec
tric C
hara
cteriz
ation
of
a Plas
ma Sy
nthe
tic Je
t Actu
ator
F. La
urend
eau,
F. Ch
edev
ergne
, O. L
éon,
ONER
A, To
ulous
e, Fra
nce
1430
hrs
AIAA-2
015-2
466
Adjoi
nt O
ptim
izatio
n of
the S
patia
l Pr
ofile
of St
eady
Ener
gy D
epos
ition
for S
uper
sonic
Dra
g Red
uctio
nR.
Miles
, C. L
imba
ch, P
rince
ton U
nivers
ity,
Princ
eton,
NJ
1500
hrs
AIAA-2
015-2
467
Mode
ling o
f Saw
-toot
h DB
D Pla
sma A
ctuat
ors f
or Fl
ow Co
ntro
l Sim
ulatio
nsP.
Milan
, F. D
emers
, H. V
o, Éc
ole
Polyt
echn
ique d
e Mon
tréal,
Mon
tréal,
Ca
nada
1530
hrs
AIAA-2
015-2
468
Ns-D
BD pl
asma
actu
ator
indu
ced
dens
ity gr
adien
t on
a lam
inar
boun
dary
laye
rR.
Wink
el, G
. Corr
eale,
Delf
t Univ
ersity
of
Tech
nolog
y, De
lft, Th
e Neth
erlan
ds
1600
hrs
AIAA-2
015-2
469
Contr
ibutio
n of la
rge-s
cale
vorte
x an
d fine
-scale
turb
ulent
struc
ture i
n sep
arate
d flow
contr
ol us
ing D
BD
plasm
a actu
ator
K. As
ano,
Unive
rsity o
f Tok
yo, S
agam
ihara,
Jap
an; K
. Asad
a, Oh
io Sta
te Un
iversit
y, Co
lumbu
s, OH
; H. K
ato, U
nivers
ity of
Toky
o, Sa
gami
hara,
Japa
n; M.
Sato,
T. N
onom
ura,
K. Fu
jii, Jap
an Ae
rospa
ce Ex
plorat
ion Ag
ency
(JAXA
), Sa
gami
hara,
Japa
n
1630
hrs
AIAA-2
015-2
470
Flow
cont
rol o
ver a
back
ward
fa
cing s
tep by
ns-D
BD pl
asma
ac
tuat
orG.
Corre
ale, D
elft U
nivers
ity of
Tech
nolog
y, De
lft, Th
e Neth
erlan
ds
Mond
ay, 2
2 Ju
ne 2
015
61-FD
-7Bo
unda
ry La
yer T
rans
ition
- Pro
gres
s and
Chall
enge
sSa
pphir
eCh
aired
by: M
. MAL
IK, N
ASA-L
angle
y Res
earch
Cente
r and
M. R
OGER
S, N
ASA-A
mes R
esea
rch Ce
nter
1400
hrs
AIAA-2
015-2
471
Rece
ptivi
ty: T
he In
spira
tion o
f Mar
k Mo
rkov
in (In
vited
)H.
Reed
, W. S
aric,
Texa
s A&M
Univ
ersity
, Co
llege
Stat
ion, T
X
1430
hrs
AIAA-2
015-2
472
Boun
dary
-Laye
r Tra
nsitio
n Pr
edict
ion fo
r Lam
inar F
low Co
ntro
l (In
vited
)J.
Crouch
, The
Boein
g Com
pany,
Seatt
le, W
A
1500
hrs
Oral
Prese
ntatio
nHy
perso
nic B
ound
ary-
Laye
r Tra
nsitio
n: To
ward
s Mec
hanis
m-Ba
sed P
redic
tion
Meth
ods (
Invit
ed)
S. S
chne
ider, P
urdue
Univ
ersity
, Wes
t La
fayett
e, IN
1530
hrs
AIAA-2
015-2
473
Rece
ptivi
ty of
Hyp
erso
nic B
ound
ary
Laye
rs to
Aco
ustic
and V
ortic
al Di
sturb
ance
s (In
vited
)P.
Balak
umar,
NAS
A Lan
gley R
esea
rch
Cente
r, Ham
pton,
VA
1600
hrs
AIAA-2
015-2
474
Exten
ding t
he G
amma
-Reth
etat
Corre
lation
base
d Tra
nsitio
n Mo
del
for C
rossfl
ow Ef
fects
(Inv
ited)
R. La
ngtry
, The
Boein
g Com
pany,
Seatt
le, W
A
1630
hrs
AIAA-2
015-2
475
CFD
Trans
ition
Mode
ling:
Blen
ding
Classi
cal M
ethod
s with
Mod
ern
Tools
(Inv
ited)
J. Co
der, M
. Mau
ghme
r, Pen
nsylv
ania
State
Univ
ersity
, Stat
e Coll
ege,
PA
1700
hrs
AIAA-2
015-2
476
Deve
lopme
nt an
d App
licat
ion of
Tra
nsitio
n Pr
edict
ion Te
chniq
ues i
n an
Uns
tructu
red C
FD Co
de (I
nvite
d)A.
Krumb
ein, N
. Krim
melbe
in, C.
Grab
e, Ge
rman
Aeros
pace
Cente
r (DL
R), C
ologn
e, Ge
rman
y
57
Mond
ay, 2
2 Ju
ne 2
015
62-FD
-8Vo
rtex
Flows
Sena
tors
Lectu
re H
allCh
aired
by: Z
. ZHE
NG, T
he U
nivers
ity of
Kans
as an
d R. G
ORDN
IER, A
ir Forc
e Res
each
Labo
ratory
1400
hrs
AIAA-2
015-2
477
Vorte
x Br
eakd
own
of Co
mpre
ssible
Sw
irling
Flow
s in
a Fini
te-Le
ngth
Str
aight
Circu
lar P
ipeZ.
Rusa
k, J.
Choi,
Rens
selae
r Poly
techn
ic Ins
titute,
Troy
, NY;
S. W
ang,
Unive
rsity
of Au
cklan
d, Au
cklan
d, Ne
w Ze
aland
1430
hrs
AIAA-2
015-2
478
Nume
rical
Study
of th
e For
matio
n of
Conc
entri
c Vor
tex R
ings
V. Sa
dri, P
. Krue
ger, S
outhe
rn Me
thodis
t Un
iversi
ty, D
allas
, TX
1500
hrs
AIAA-2
015-2
479
Rota
ting C
ylind
rical
Bodie
s at
Low
ReM.
Calle
nder,
Midd
le Te
nnes
see S
tate
Unive
rsity,
Murf
reesb
oro, T
N
1530
hrs
AIAA-2
015-2
480
Inve
stiga
tion
of th
e flow
dyna
mics
in a c
hann
el co
nstri
cted b
y per
iodic
hills
X. G
loerfe
lt, Pa
ris In
stitut
e of T
echn
ology
, Pa
ris, F
rance
; P. C
innell
a, Un
iversi
ty of
Salen
to, Le
cce, I
taly
1600
hrs
AIAA-2
015-2
481
Tempo
ral E
volut
ion of
Turb
ulent
Eddie
s in
a Com
press
ible J
et in
Crossfl
ow
Meas
ured
using
Pulse
-Bur
st PIV
S. B
eresh
, J. W
agne
r, J. H
enflin
g, R.
Spille
rs, B
. Prue
tt, S
andia
Nati
onal
Labo
ratori
es, A
lbuqu
erque
, NM
Mond
ay, 2
2 Ju
ne 2
015
63-FD
-9Ac
tive a
nd P
assiv
e Flow
Cont
rol
Topa
zCh
aired
by: K
. GRA
NLUN
D, Ai
r Forc
e Res
earch
Labo
ratory
and M
. AMI
TAY, R
ensse
laer P
olytec
hnic
Institu
te14
00 hr
sAIA
A-201
5-248
2In
terac
tions
of a
Dyna
mic V
ortex
Ge
nera
tor w
ith a
Cros
s-flow
: A
Nume
rical
Study
R. Cu
mming
s, Re
nsse
laer P
olytec
hnic
Institu
te, Tr
oy, N
Y; D.
Cling
man,
The
Boein
g Com
pany
, Sea
ttle, W
A; O.
Sah
ni,
Rens
selae
r Poly
techn
ic Ins
titute,
Troy
, NY
1430
hrs
AIAA-2
015-2
483
Inter
actio
ns of
a Dy
nami
c Vor
tex
Gene
rato
r with
a Cr
oss-fl
ow: A
n Ex
perim
enta
l Stu
dyC.
Leon
g, E.
Cruz,
Rens
selae
r Poly
techn
ic Ins
titute,
Troy
, NY;
D. Cl
ingma
n, Th
e Bo
eing C
ompa
ny, S
eattle
, WA;
M. Am
itay,
Rens
selae
r Poly
techn
ic Ins
titute,
Troy
, NY
1500
hrs
AIAA-2
015-2
484
Flow
Cont
rol in
a Di
ffuse
r at
Trans
onic
Cond
itions
J. Ga
rtner,
M. A
mitay
, Ren
sselae
r Po
lytec
hnic
Institu
te, Tr
oy, N
Y
1530
hrs
AIAA-2
015-2
485
The E
ffects
of Sw
eepin
g Jet
Actu
ator
Par
amete
rs on
Flow
Se
para
tion
Cont
rol
M. Ko
klu, N
ASA L
angle
y Res
earch
Cente
r, Ha
mpton
, VA
Mond
ay, 2
2 Ju
ne 2
015
64-M
AO-2
Vehic
le De
sign
Appli
catio
ns II
Madr
idCh
aired
by: S
. CHO
I, Vir
ginia
Polyt
echn
ic Ins
titute
and S
tate U
nivers
ity an
d S. F
ERGU
SON,
Nort
h Caro
lina S
tate U
nivers
ity14
00 hr
sAIA
A-201
5-248
6Th
e Valu
e of S
emi-E
mpiri
cal
Analy
sis M
odels
in A
ircra
ft De
sign
S. B
randt,
M. P
ost,
U.S.
Air F
orce
Acad
emy,
Color
ado S
pring
s, CO
; D. H
all,
DHC E
ngine
ering
, San
Mate
o, CA
; F.
Gillia
m, Li
psco
mb U
nivers
ity, N
ashv
ille,
TN; T
. Jun
g, T.
Yech
out,
U.S.
Air F
orce
Acad
emy,
Color
ado S
pring
s, CO
1430
hrs
AIAA-2
015-2
487
Coup
led A
djoint
Aer
ostru
ctura
l Wi
ng O
ptim
izatio
n Us
ing Q
uasi-
Thre
e-Di
mens
ional
Aero
dyna
mic
Analy
sisA.
Elham
, Delf
t Univ
ersity
of Te
chno
logy,
Delft,
The N
etherl
ands
; M. v
an To
oren,
Unive
rsity
of So
uth Ca
rolina
, Colu
mbia,
Co
lumbia
, SC
1500
hrs
AIAA-2
015-2
488
Optim
al va
riable
stiff
ness
distri
butio
n fo
r a co
mpos
ite pl
ate
with
a ro
w of
hole
s sub
jected
to
tensio
n/sh
ear l
oad c
ases
M. va
n Too
ren, U
nivers
ity of
Sou
th Ca
rolina
, Colu
mbia,
Colum
bia, S
C; A.
Elham
, Delf
t Univ
ersity
of Te
chno
logy,
Delft,
The N
etherl
ands
; R. H
arik,
Unive
rsity
of So
uth Ca
rolina
, Colu
mbia,
Colum
bia, S
C
1530
hrs
AIAA-2
015-2
489
Simula
tion-
Base
d Opt
imal
Sens
or/
Actu
ator
Pos
itionin
g on
a Fin-
Like
Struc
ture
N. Pe
drama
sl, M
. Sah
in, M
iddle
East
Tech
nical
Unive
rsity,
Cank
aya,
Turke
y; E.
Acar,
TOBB
Univ
ersity
of Ec
onom
ics an
d Te
chno
logy,
Sogu
tozu,
Turke
y
1600
hrs
AIAA-2
015-2
490
Conc
urre
nt O
ptim
izatio
n of
a Fe
ed-Fo
rwar
d Gus
t Loa
ds Co
ntro
ller
and M
inimi
zatio
n of
Wing
Box
Str
uctu
ral M
ass o
n an
Airc
raft
with
Ac
tive W
inglet
sA.
Wild
schek
, Airb
us, O
ttobru
nn, G
erman
y
1630
hrs
AIAA-2
015-2
491
Free
-Form
Aer
odyn
amic
Wing
Op
timiza
tion U
sing M
athe
matic
ally-
Deriv
ed D
esign
Varia
bles
D. Po
ole, C
. Alle
n, T.
Rend
all, U
nivers
ity of
Br
istol,
Bris
tol, U
nited
King
dom
Mond
ay, 2
2 Ju
ne 2
015
65-M
ST-3
Air T
raffi
c Man
agem
ent
Trave
rtine
Chair
ed by
: J. S
MITH
1400
hrs
AIAA-2
015-2
492
Scala
ble M
ultidi
mens
ional
Unce
rtaint
y Eva
luatio
n Ap
proa
ch
to St
rateg
ic Ai
r Tra
ffic F
low
Mana
geme
ntJ.
Xie, Y
. Wan
, Univ
ersity
of N
orth T
exas
, De
nton,
TX
1430
hrs
AIAA-2
015-2
493
Unde
rstan
ding A
ir Tra
nspo
rtatio
n Ma
rket
Dyna
mics
using
a Se
arch
Alg
orith
m for
Calib
ratin
g Tra
vel
Dema
nd an
d Pric
eV.
Kuma
r, B. H
orio,
A. De
Cicco,
S. Ha
san, V
. Sto
uffer,
LMI, M
cLean
, VA;
J. Sm
ith, N
ASA
Lang
ley Re
search
Cente
r, Ham
pton,
VA; e
t al.
1500
hrs
AIAA-2
015-2
494
Deve
lopme
nt of
an AT
C Tow
er
Simula
tor t
o Sim
ulate
Grou
nd
Oper
ation
sZ.
Chua
, Univ
ersity
of To
ulous
e, To
ulous
e, Fra
nce;
F. An
dre, M
. Cou
sy, Fr
ench
Civil
Av
iation
Univ
ersity
, Tou
louse
, Fran
ce
1530
hrs
AIAA-2
015-2
495
Multi-
Agen
t Bas
ed A
ir Tra
ffic
Simula
tion
Syste
mZ.
Yue,
D. S
ui, Y.
Lin,
J. Zh
ang,
Nanji
ng
Unive
rsity
of Ae
ronau
tics a
nd As
trona
utics,
Na
njing
, Chin
a
1600
hrs
AIAA-2
015-2
496
Estim
ating
Ben
efits
of A
viatio
n Al
terna
tive F
uels
at th
e Sys
tem,
Rout
e, an
d Airp
ort L
evel
B. M
iller, C
. Murp
hy, M
etron
Aviat
ion, I
nc.,
Dulle
s, VA
; C. V
illa, A
. Filiz
ola, N
ation
al Civ
il Avia
tion A
genc
y (AN
AC),
Bras
ilia,
Braz
il
58
Mond
ay, 2
2 Ju
ne 2
015
66-M
ST-4
Guida
nce,
Cont
rol, a
nd D
ynam
ics I
Wyeth
Chair
ed by
: R. B
OTEZ
, Eco
le de
Tech
nolog
ie Su
perie
ure14
00 hr
sAIA
A-201
5-249
7A
New
Meth
od fo
r Tun
ing P
I Gain
s fo
r Pos
ition
Cont
rol o
f BLD
C Mot
or
Base
d Wing
Mor
phing
Actu
ator
sR.
Botez
, S. K
han,
Unive
rsity
of Qu
ébec
, Mo
ntréa
l, Can
ada
1430
hrs
AIAA-2
015-2
498
Long
itudin
al Sta
bility
Aug
ment
ation
of
Seap
lanes
in P
laning
K. Ito
, Ghe
nt Un
iversi
ty, G
hent,
Belg
ium; T
. Hir
ayam
a, Yo
koha
ma N
ation
al Un
iversi
ty,
Yoko
hama
, Jap
an; T
. Sak
urai, H
iyoh
Aircra
ft Ma
nufac
turing
and D
evelo
pmen
t Co
mpan
y, To
kyo,
Japa
n; T.
Dhae
ne, G
hent
Unive
rsity,
Ghe
nt, B
elgium
1500
hrs
AIAA-2
015-2
499
Cont
rol v
alida
tion
of a
morp
hing
wing
in an
open
loop
arch
itectu
reM.
Tcha
tchue
ng Ka
mmeg
ne, D
. Ngu
yen,
R. Bo
tez, U
nivers
ity of
Qué
bec,
Montr
éal,
Cana
da
1530
hrs
AIAA-2
015-2
500
A Co
mpar
ative
Stud
y of a
Pse
udo-
Five D
egre
e of F
reed
om an
d an
Adjoi
nt M
odel
Again
st a S
ix De
gree
of
Free
dom
Mode
l for
Fide
lity
Asse
ssmen
tE.
Seze
r, M. N
alci, R
OKET
SAN
Missi
le Ind
ustrie
s, Inc
., An
kara,
Turke
y; A.
Kutay
, Mi
ddle
East
Tech
nical
Unive
rsity,
Anka
ra,
Turke
y
Mond
ay, 2
2 Ju
ne 2
015
67-P
DL-3
Plasm
a Com
puta
tiona
l Meth
ods I
Mone
t Ball
room
Chair
ed by
: M. W
HITE
, Ohio
Aeros
pace
Insti
tute
1400
hrs
AIAA-2
015-2
501
A No
n-ite
rativ
e Hyp
erbo
lic, F
irst-
orde
r Con
serv
ation
Law
Appr
oach
to
Dive
rgen
ce-fr
ee So
lution
s to
Maxw
ell’s
Equa
tions
R. Th
omps
on, T
. Moe
ller, U
nivers
ity of
Te
nnes
see,
Tulla
homa
, Tull
ahom
a, TN
1430
hrs
AIAA-2
015-2
502
Equiv
alent
Elec
trica
l Circ
uit fo
r a 1
D Pla
sma E
ngine
N. Ra
mesh
, Sri J
agad
guru
Chan
drash
ekara
natha
Swa
miji I
nstitu
te of
Tech
nolog
y, Ch
ickba
llapu
r, Ind
ia; P.
Mos
es
John
Chris
ty Ap
polo,
T. S
hesh
adri,
Indian
Ins
titute
of Sc
ience
, Ben
galur
u, Ind
ia
1500
hrs
AIAA-2
015-2
503
Inve
stiga
tions
of Fl
ow ov
er a
Hemi
sphe
re u
sing N
umer
ical
Simula
tions
C. Ta
m, T.
Mad
den,
Air Fo
rce Re
searc
h La
borat
ory, K
irtlan
d AFB
, NM;
B. T
hurow
, Au
burn
Unive
rsity,
Aubu
rn, AL
1530
hrs
AIAA-2
015-2
504
CFD
Valid
ation
of P
IV-ba
sed
Estim
ation
of D
BD P
lasma
-Ac
tuat
ion Fo
rceQ.
Zhai,
Z. Zh
ang,
J. Ca
i, Nort
hwes
tern
Polyt
echn
ical U
nivers
ity, X
i’an,
China
; F.
Liu, S
. Luo
, Univ
ersity
of Ca
liforni
a, Irv
ine,
Los A
ngele
s, CA
Mond
ay, 2
2 Ju
ne 2
015
68-TP
-3Ab
lation
IIRo
setta
Chair
ed by
: N. D
OUGH
ERTY
, ERC
Inco
rporat
ed an
d A. H
ASHE
MI, L
ockh
eed M
artin
Spac
e Sys
tems
1400
hrs
AIAA-2
015-2
505
Effe
cts of
Wat
er P
rese
nce o
n Lo
w Te
mper
atur
e Phe
nome
non
in Po
rous
TPS M
ater
ials
D. S
mith,
A. O
midy
, H. W
eng,
Unive
rsity
of Ke
ntuck
y, Le
xingto
n, Le
xingto
n, KY
; T.
Whit
e, ER
C, Inc
., Mo
ffett
Field,
CA; A
. Ma
rtin, U
nivers
ity of
Kentu
cky,
Lexin
gton,
Lexin
gton,
KY
1430
hrs
AIAA-2
015-2
506
A Mu
lti-Di
mens
ional
Finite
Elem
ent
Base
d Solv
er fo
r Dec
ompo
sing
and N
on-D
ecom
posin
g The
rmal
Prot
ectio
n Sy
stems
M. H
oward
, B. B
lackw
ell, S
andia
Nati
onal
Labo
ratori
es, A
lbuqu
erque
, NM
1500
hrs
AIAA-2
015-2
507
Ther
mal P
rotec
tion
Syste
m Ma
ss Es
timat
ing R
elatio
nship
s For
Blun
t-Bo
dy, E
arth
Entry
Spac
ecra
ftS.
Sep
ka, E
RC, I
nc.,
Moffe
tt Fie
ld, CA
; J.
Sama
reh, N
ASA L
angle
y Res
earch
Cente
r, Ha
mpton
, VA
1530
hrs
AIAA-2
015-2
508
Deve
lopme
nt an
d Qua
lifica
tion
of
Light
weigh
t Abla
tor A
eros
hell B
BM
for M
artia
n Mi
ssion
K. Fu
jita, T
. Suz
uki, T
. Aok
i, T. O
gasa
wara,
Y.
Ishida
, Jap
an Ae
rospa
ce Ex
plorat
ion
Agen
cy (J
AXA)
, Cho
fu, Ja
pan
59
Mond
ay, 2
2 Ju
ne 2
015
69-TP
-4Ae
roth
ermo
dyna
mics
ISte
uben
Chair
ed by
: C. J
OHNS
TON,
NAS
A-Lan
gley R
esea
rch Ce
nter
1400
hrs
AIAA-2
015-2
509
Mode
ling F
idelity
for O
xyge
n No
nequ
ilibriu
m Th
ermo
chem
istry
in
Refle
cted S
hock
Tube
Flow
sK.
Neitz
el, D
. And
rienk
o, I.
Boyd
, Un
iversi
ty of
Mich
igan,
Ann A
rbor, A
nn
Arbor,
MI
1430
hrs
AIAA-2
015-2
510
State
Spec
ific M
odeli
ng of
the
Ener
gy Tr
ansfe
r in
Nitro
gen
Shoc
ks
using
High
Fide
lity M
odels
T. Zh
u, Z.
Li, N
. Pars
ons,
Penn
sylva
nia
State
Univ
ersity
, Stat
e Coll
ege,
PA; D
. Le
vin, M
. Pan
esi, U
nivers
ity of
Illino
is,
Urba
na-Ch
ampa
ign, U
rbana
, IL
1500
hrs
AIAA-2
015-2
511
DSMC
Mod
eling
of N
oneq
uilibr
ium
Electr
onic
Excit
ation
and E
missi
on
for H
yper
sonic
Sens
or A
pplic
ation
sJ.
Burt,
E. Jo
syula
, Air F
orce R
esea
rch
Labo
ratory
, Wrig
ht-Pa
tterso
n AFB
, OH
1530
hrs
AIAA-2
015-2
512
Meas
urem
ent o
f Ultr
aviol
et Ra
diativ
e Hea
ting A
ugme
ntat
ion in
HI
EST R
eflec
ted Sh
ock
Tunn
elB.
Crud
en, A
. Bran
dis, E
RC, I
nc.,
Moffe
tt Fie
ld, CA
; J. G
rinste
ad, J
. Olej
nicza
k, NA
SA
Ames
Rese
arch C
enter
, Moff
ett Fi
eld, C
A; L.
Kirk,
R. Lil
lard,
NASA
John
son S
pace
Ce
nter, H
ousto
n, TX
; et a
l.
1600
hrs
AIAA-2
015-2
513
Comp
ariso
n of
Two H
ybrid
RC
-Mod
els fo
r Pre
dictio
n of
No
nequ
ilibriu
m Ra
diatio
n fro
m Str
ong S
hock
Wav
esS.
Surz
hikov
, Rus
sian A
cade
my of
Sc
ience
s, Mo
scow,
Russi
a
1630
hrs
AIAA-2
015-2
514
Radia
tive H
eat F
lux fr
om M
etallic
Sp
ecies
in Fr
ee P
iston
Shoc
k Tu
nnel
HIES
TS.
Nom
ura, H
. Tak
ayan
agi, K
. Fuji
ta,
H. Ta
nno,
Japa
n Aero
spac
e Exp
lorati
on
Agen
cy (J
AXA)
, Cho
fu, Ja
pan
Mond
ay, 2
2 Ju
ne 2
015
70-N
W-2
1530
- 16
00 h
rsNe
twor
king C
offe
e Bre
akMe
eting
Roo
m Fo
yers
Mond
ay, 2
2 Ju
ne 2
015
71-A
IAA-
1 17
30 -
1900
hrs
Spee
d Gee
k Ne
twor
king E
vent
and R
ecep
tion
Chan
tilly B
allro
om Fo
yer
This
casu
al, hi
gh-en
ergy s
essio
n will
give y
ou th
e opp
ortun
ity to
enga
ge on
e-on-o
ne w
ith sp
eake
rs an
d get
a glim
pse o
f thin
gs to
come
in th
e wee
k ahe
ad at
AIAA
AVIAT
ION
2015
. Yo
u’ll tr
avel
from
spea
ker t
o spe
aker
in sm
all gr
oups
, liste
n to a
5-m
inute
overv
iew of
their
topic
, and
then
have
five m
inutes
to ha
ve yo
ur qu
estio
ns an
swere
d.Op
en to
all c
onfer
ence
atten
dees
, but
spac
e is l
imite
d to t
he fir
st 50
0 pa
rticipa
nts.
Spon
sored
by: L
ockh
eed M
artin
Mond
ay, 2
2 Ju
ne 2
015
72-C
ASE-3
17
30 -
1900
hrs
CASE
Netw
orkin
g Soc
ialMo
rocco
Spon
sored
by B
oeing
Comm
ercial
Airpl
anes
Mond
ay, 2
2 Ju
ne 2
015
73-LE
C-1
1730
- 18
30 h
rsFlu
id Dy
nami
cs Aw
ard L
ectu
reGr
and B
allro
om D
Searc
hing f
or Tru
thine
ss in
Comp
utatio
nal F
luid D
ynam
icsPh
ilip R
oePro
fesso
r, Dep
artme
nt of
Aeros
pace
Engin
eerin
gUn
iversi
ty of
Mich
igan
Mond
ay, 2
2 Ju
ne 2
015
74-R
LA-1
18
30 -
1930
hrs
Risin
g Lea
ders
in Ae
rosp
ace N
etwor
king R
ecep
tion
Emer
ald
The r
ecep
tion w
ill kic
k off
the Ri
sing L
eade
rs in
Aeros
pace
even
ts an
d is a
perfe
ct op
portu
nity f
or yo
ung l
eade
rs to
ming
le wi
th oth
ers w
ho w
ill be
partic
ipatin
g in A
IAA AV
IATIO
N 20
15 as
atten
dee,
prese
nter, o
r vete
ran pr
ofessi
onal
Come
mee
t othe
r part
icipan
ts in
a cas
ual e
nviro
nmen
t. Yo
u’re b
ound
to se
e the
m ag
ain.
60
Tues
day
Tues
day,
23 Ju
ne 2
015
75-S
B-2
0730
- 08
00 h
rsSp
eake
rs’ B
riefin
gSe
ssion
Roo
ms
Tues
day,
23 Ju
ne 2
015
76-P
LNRY
-2
0800
- 09
00 h
rsPle
nary
Pan
elCh
antill
y Ball
room
Wes
t
NextG
en: A
Mod
el of
Stake
holde
r Eng
agem
ent
Bill A
yer
Retire
d Cha
irman
and C
EOAla
ska A
ir Grou
p
Edwa
rd L.
Bolt
on Jr
.As
sistan
t Adm
inistr
ator f
or Ne
xtGen
Fede
ral Av
iation
Admi
nistra
tion
Tues
day,
23 Ju
ne 2
015
77-A
A-11
Fan
Noise
Fleur
-de-
lis A
Chair
ed by
: S. G
LEGG
, Flor
ida At
lantic
Univ
ersity
0900
hrs
AIAA-2
015-2
515
Extra
polat
ion of
RAN
S flow
data
fo
r imp
rove
d ana
lytica
l fan
tone
pr
edict
ionR.
Jaron
, A. M
oreau
, S. G
uerin
, Germ
an
Aeros
pace
Cente
r (DL
R), B
erlin,
Germ
any
0930
hrs
AIAA-2
015-2
516
Syste
m No
ise P
redic
tion
of th
e DG
EN 3
80 Tu
rbof
an En
gine
J. Be
rton,
NASA
Glen
n Res
earch
Cente
r, Cle
velan
d, OH
1000
hrs
AIAA-2
015-2
517
Fan n
oise s
calin
g of s
tatic d
ata
using
semi
-analy
tical
metho
ds an
d as
sessm
ent a
gains
t exp
erime
ntal d
ataV.
Bland
eau,
V. Pa
storel
li, Air
bus,
Toulo
use,
Franc
e; A.
Morea
u, S.
Gue
rin, G
erman
Ae
rospa
ce Ce
nter (
DLR)
, Berl
in, G
erman
y
1030
hrs
AIAA-2
015-2
518
Valid
ation
of a
Movin
g-Bo
dy H
igh-
Orde
r Imm
erse
d Bou
ndar
y Meth
od
for t
he M
ultipl
e Pur
e Ton
e Nois
e Ge
nera
ted by
Supe
rsonic
Rot
or
Casca
des
B. Pi
menta
, R. B
oben
rieth
Mise
rda,
Unive
rsity
of Br
asília
, Bras
ília, B
razil
1100
hrs
AIAA-2
015-2
519
Effe
ct of
Stat
or Va
ne Sw
eep o
n Hi
gh Fr
eque
ncy F
an N
oise a
nd
Comp
ariso
n wi
th Ex
perim
ent
A. Ko
zlov,
H. At
assi,
Univ
ersity
of N
otre
Dame
, Notr
e Dam
e, IN
Tues
day,
23 Ju
ne 2
015
78-A
A-12
Duct
Acou
stics
IIFle
ur-d
e-lis
BCh
aired
by: C
. YEN
, Jac
obs T
echn
ology
0900
hrs
AIAA-2
015-2
520
Aero
-Aco
ustic
Per
form
ance
of
Adap
tive N
acell
e Inle
tF.
Majić
, G. E
fraim
sson,
C. O’
Reilly
, Roy
al Ins
titute
of Te
chno
logy (
KTH)
, Stoc
kholm
, Sw
eden
0930
hrs
AIAA-2
015-2
521
Theo
retic
al Stu
dy of
Soun
d Pr
opag
ation
in Li
ned D
uct w
ith
Rigid
Splic
es U
sing W
iener
-Hop
f Me
thod
X. Li
u, H.
Jian
g, X.
Hua
ng, P
eking
Un
iversi
ty, B
eijing
, Chin
a
1000
hrs
AIAA-2
015-2
522
Soun
d Pro
paga
tion i
n Line
d Ann
ular
Ducts
with
Mea
n Swi
rling F
lowA.
Maldo
nado
, R. A
stley,
J. Co
uplan
d, G.
Gaba
rd, Un
iversit
y of S
outha
mpton
, So
utham
pton,
Unite
d King
dom;
D. Su
tliff,
NASA
Glen
n Rese
arch C
enter
, Clev
eland
, OH
1030
hrs
AIAA-2
015-2
523
Upstr
eam
Radia
tion
from
Supe
rsonic
Bur
ied-n
ozzle
Jets
via
Scat
tering
at th
e Shr
oud E
dge
A. Sa
manta
, Ind
ian In
stitut
e of S
cienc
e, Ba
ngalo
re, In
dia; J
. Freu
nd, U
nivers
ity of
Illi
nois,
Urba
na-Ch
ampa
ign, U
rbana
, IL
1100
hrs
AIAA-2
015-2
524
Nume
rical
Pred
iction
s of M
ode
Refle
ction
s in
an O
pen
Circu
lar
Duct:
Comp
ariso
n wi
th Th
eory
M. D
ahl, N
ASA G
lenn R
esea
rch Ce
nter,
Cleve
land,
OH; D
. Hixo
n, Un
iversi
ty of
Toled
o, To
ledo,
OH
Tues
day,
23 Ju
ne 2
015
79-A
A-13
Trailin
g Edg
e Nois
e II
Inve
rnes
sCh
aired
by: J
. GAL
LMAN
, Gulf
strea
m Ae
rospa
ce Co
rporat
ion09
00 hr
sAIA
A-201
5-252
5Pr
edict
ion of
Por
ous T
railin
g Edg
e No
ise R
educ
tion
via A
cous
tic
Pertu
rbat
ion Eq
uatio
ns an
d Volu
me
Aver
aging
B. Fa
ssman
n, C.
Rautm
ann,
R. Ew
ert, J
. De
lfs, G
erman
Aeros
pace
Cente
r (DL
R),
Brau
nsch
weig,
Germ
any
0930
hrs
AIAA-2
015-2
526
Pred
iction
of B
road
band
Trail
ing-
Edge
Nois
e Bas
ed on
Blak
e Mod
el an
d Ami
et Th
eory
O. S
talno
v, C.
Paruc
huri,
P. Jo
seph
, Un
iversi
ty of
South
ampto
n, So
utham
pton,
Unite
d King
dom
1000
hrs
AIAA-2
015-2
527
Para
metri
c Inv
estig
ation
s of T
onal
Trailin
g-Ed
ge N
oise G
ener
ation
by
Low-
Reyn
olds N
umbe
r Airf
oils.
Part
I - Ex
perim
enta
l Stu
dies
G. Ya
khina
, M. R
oger,
École
Centr
ale de
Ly
on, L
yon,
Franc
e; L.
Nguy
en, V
. Golu
bev,
Embry
-Ridd
le Ae
ronau
tical
Unive
rsity,
Da
ytona
Bea
ch, F
L
1030
hrs
AIAA-2
015-2
528
Para
metri
c Inv
estiga
tions
of To
nal
Trailin
g-Edg
e Nois
e Gen
eratio
n by
Low-
Reyn
olds N
umbe
r Airf
oils.
Part
II - N
umeri
cal S
tudies
L. Ng
uyen
, W. H
iner, S
. Sale
hian,
V. Go
lubev,
R.
Mank
badi,
Embry
-Ridd
le Ae
ronau
tical
Unive
rsity,
Dayto
na Be
ach, F
L; G.
Yakh
ina,
École
Centr
ale de
Lyon
, Lyo
n, Fra
nce; e
t al.
1100
hrs
AIAA-2
015-2
529
A Mo
del f
or Je
t-Sur
face
Inter
actio
n No
ise U
sing P
hysic
ally R
ealiz
able
Upstr
eam
Turb
ulenc
e Con
dition
sM.
Afsa
r, Imp
erial
Colle
ge Lo
ndon
, Lon
don,
Unite
d King
dom;
S. L
eib, O
hio Ae
rospa
ce
Institu
te, Cl
evela
nd, O
H
1130
hrs
AIAA-2
015-2
530
On th
e Adjo
int-b
ased
Cont
rol o
f Tra
iling-
Edge
Turb
ulenc
e and
Nois
e Mi
nimiza
tion
via P
orou
s Mat
erial
B. Zh
ou, N
. Gau
ger, T
echn
ical U
nivers
ity of
Ka
isersl
auter
n, Ka
isersl
auter
n, Ge
rman
y; S.
Koh,
M. M
einke
, W. S
chroe
der, R
WTH
Aa
chen
Univ
ersity
, Aac
hen,
Germ
any
1200
hrs
AIAA-2
015-2
531
Expe
rimen
tal Va
lidati
on of
a Se
mi-
Analy
tical
Trailin
g-Edg
e Nois
e Mod
el Inc
luding
Broa
dban
d Sca
tterin
gK.
Kucuk
cosku
n, J.
Christ
ophe
, C. S
chram
, von
Ká
rmán
Instit
ute fo
r Fluid
Dyna
mics,
Rhod
e-Sa
int-Ge
nèse,
Belgiu
m; S.
More
au, U
nivers
ity
of Sh
erbroo
ke, S
herbr
ooke
, Can
ada
61
Tues
day,
23 Ju
ne 2
015
80-A
A-14
Jet N
oise P
redic
tion
IIILa
lique
Chair
ed by
: N. M
URRA
Y, Th
e Univ
ersity
of M
ississ
ippi
0900
hrs
AIAA-2
015-2
532
Analy
sis of
Inter
mitte
ncy o
f Su
perso
nic Je
t Nois
e with
Sy
nchr
onize
d LES
U. Sa
sidha
ran N
air, L
. Ago
stini, D
. Gait
onde
, Oh
io Sta
te Un
iversit
y, Co
lumbu
s, OH
0930
hrs
AIAA-2
015-2
533
Aero
acou
stic A
nalys
is of
a He
licop
ter En
gine J
et In
cludin
g a
Reali
stic N
ozzle
Geo
metry
M. Ce
tin, S
. Koh
, M. M
einke
, W.
Schro
eder,
RWTH
Aach
en U
nivers
ity,
Aach
en, G
erman
y
1000
hrs
AIAA-2
015-2
534
Larg
e-sca
le str
uctu
re ev
olutio
n an
d so
und g
ener
ation
in a
hotje
tF.
Feng
, Q. W
ang,
China
Acad
emy o
f Ae
rospa
ce Ae
rodyn
amics
, Beij
ing, C
hina
1030
hrs
AIAA-2
015-2
535
Larg
e edd
y sim
ulatio
n for
jet n
oise:
the im
porta
nce o
f gett
ing th
e bo
unda
ry la
yer r
ight
G. Brè
s, Ca
scade
Techn
ologie
s, Inc
., Palo
Alto,
CA
; V. J
aune
t, M. L
e Ralli
c, P. J
ordan
, Nati
onal
Cente
r for S
cienti
fic Re
search
(CNR
S), P
oitier
s, Fra
nce; T
. Colo
nius,
Califo
rnia I
nstitu
te of
Techn
ology,
Pasad
ena,
CA; S
. Lele
, Stan
ford
Unive
rsity,
Stanfo
rd, CA
1100
hrs
AIAA-2
015-2
536
Empir
icism
-free
nois
e calc
ulatio
n fro
m LE
S solu
tion
base
d on
Golds
tein
gene
raliz
ed ac
ousti
c an
alogy
: volu
me n
oise s
ource
s and
me
anflo
w ef
fects
V. Se
milet
ov, S
. Kara
baso
v, A.
Chint
agun
ta, A.
Mark
estei
jn, Q
ueen
Mary
Un
iversi
ty of
Lond
on, L
ondo
n, Un
ited
Kingd
om
1130
hrs
AIAA-2
015-2
537
Spat
ial st
abilit
y cha
racte
ristic
s of
non-
circu
lar je
tsF.
Lajús
, Fed
eral U
nivers
ity of
San
ta Ca
tarina
, Flor
ianóp
olis,
Braz
il; A.
Cava
lieri,
Tech
nolog
ical In
stitut
e of A
erona
utics
(ITA)
, São
José
dos C
ampo
s, Br
azil;
C. De
scham
ps, F
edera
l Univ
ersity
of S
anta
Catar
ina, F
lorian
ópoli
s, Br
azil
Tues
day,
23 Ju
ne 2
015
81-A
A-15
CAA
Nume
rical
Tech
nique
s II
Obeli
sk A
Chair
ed by
: X. L
I, Be
ihang
Univ
ersity
0900
hrs
AIAA-2
015-2
538
Coup
led O
verse
t Uns
tructu
red
Disco
ntinu
ous G
alerk
in Me
thod
fo
r Lau
nch
Envir
onme
nt A
cous
tics
Pred
iction
(Inv
ited)
R. Ha
rris, C
FD Re
searc
h Corp
oratio
n, Hu
ntsvil
le, AL
; E. C
ollins
, A. S
escu
, E.
Luke
, Miss
issipp
i Stat
e Univ
ersity
, Mi
ssissi
ppi S
tate,
MS
0930
hrs
AIAA-2
015-2
539
Optim
ized E
xplic
it Di
ssipa
tion
Oper
ator
s for
Comp
utat
ional
Aero
acou
stics
N. M
anso
uri, D
. Hixo
n, Un
iversi
ty of
Toled
o, To
ledo,
OH
1000
hrs
AIAA-2
015-2
540
DRP
schem
es pe
rform
poor
ly fo
r de
cayin
g or g
rowi
ng os
cillat
ions
E. Br
amble
y, Un
iversi
ty of
Camb
ridge
, Ca
mbrid
ge, U
nited
King
dom
1030
hrs
AIAA-2
015-2
541
Towa
rds C
asca
de Tr
ailing
-Edge
No
ise M
odeli
ng U
sing a
Mod
e-Ma
tching
Tech
nique
M. Ro
ger, É
cole
Centr
ale de
Lyon
, Ecu
lly,
Franc
e; S.
More
au, G
AUS,
She
rbroo
ke,
Cana
da
1100
hrs
AIAA-2
015-2
542
Zero
-Ave
rage
Sour
ce Te
rms f
or
Multid
imen
siona
l Non
linea
r Di
sturb
ance
Equa
tions
D. H
ixon,
Unive
rsity
of To
ledo,
Toled
o, OH
Tues
day,
23 Ju
ne 2
015
82-A
CD-2
Aircr
aft D
esign
Meth
ods a
nd To
olsWy
ethCh
aired
by: A
. CHA
PUT,
Unive
rsity
of Te
xas a
t Aus
tin09
00 hr
sAIA
A-201
5-254
3Stu
dent
Air
Vehic
le De
sign
and
Analy
sis -
A Sy
stems
Engin
eerin
g Mo
del B
ased
App
roac
hA.
Chap
ut, U
nivers
ity of
Texa
s, Au
stin,
Austi
n, TX
0930
hrs
AIAA-2
015-2
544
Upda
te on
HCD
struc
t - A
Tool
for
Hybr
id Wi
ng B
ody C
once
ptua
l De
sign
and S
tructu
ral O
ptim
izatio
nF.
Gern,
NAS
A Lan
gley R
esea
rch Ce
nter,
Hamp
ton, V
A
1000
hrs
AIAA-2
015-2
545
Simult
aneo
us A
ircra
ft De
sign
and T
rip A
ssign
ment
und
er
Desig
n Pa
rame
ter an
d Dem
and
Unce
rtaint
yP.
Govin
daraj
u, W.
Cros
sley,
Purdu
e Un
iversi
ty, W
est L
afaye
tte, I
N
1030
hrs
AIAA-2
015-2
546
Virtu
al fli
ght t
estin
g in
an ai
rcraf
t siz
ing an
d opt
imiza
tion
proc
ess
P. Sc
hmoll
grube
r, N. B
artoli
, ONE
RA,
Toulo
use,
Franc
e; Y.
Gouri
nat,
Unive
rsity
of To
ulous
e, To
ulous
e, Fra
nce
1100
hrs
AIAA-2
015-2
547
User
Defi
ned C
ompo
nent
s in
the
Open
VSP
Para
metri
c Geo
metry
Tool
R. Mc
Dona
ld, Ca
liforni
a Poly
techn
ic St
ate U
nivers
ity, S
an Lu
is Ob
ispo,
CA; J
. Glo
udem
ans,
Self,
San M
ateo,
CA
1130
hrs
AIAA-2
015-2
548
Deve
lopme
nt of
an In
terac
tive
Wave
Dra
g Cap
abilit
y for
the
Open
VSP
Para
metri
c Geo
metry
Tool
M. W
addin
gton,
R. Mc
Dona
ld, Ca
liforni
a Po
lytec
hnic
State
Univ
ersity
, San
Luis
Obisp
o, CA
Tues
day,
23 Ju
ne 2
015
83-A
FM-5
Aircr
aft F
light
Dyn
amics
, Con
trol, H
andli
ng Q
ualiti
es an
d Per
form
ance
IIPlu
m Bl
osso
m A
Chair
ed by
: M. G
RANT
, Purd
ue U
nivers
ity09
00 hr
sAIA
A-201
5-254
9Da
mage
Mitig
ating
on a
Larg
e Ro
torcr
aft u
sing L
oad A
llevia
ting
Fligh
t Con
trol L
aws
D. Ca
udle,
J. H
orn, E
. Kell
er, Pe
nnsy
lvania
St
ate U
nivers
ity, S
tate C
olleg
e, PA
; C.
Thais
s, C.
McCo
ll, Te
chnic
al Da
ta An
alysis
, Inc
., Ma
rietta
, GA
0930
hrs
AIAA-2
015-2
550
Aero
batic
Man
euve
rs of
a Co
nven
tiona
l and
Comp
ound
Ro
torcr
aft -
Fligh
t Pat
h Ge
nera
tion
and D
ynam
ic Sim
ulatio
nA.
Thors
en, J
. Horn
, Pen
nsylv
ania
State
Un
iversi
ty, S
tate C
olleg
e, PA
1000
hrs
AIAA-2
015-2
551
Prop
eller
Torq
ue Ef
fect
on Cr
uise
Trim
of St
anda
rd an
d Mas
s-Ac
tuat
ed A
irplan
eS.
Ertur
k, A.
Doga
n, Un
iversi
ty of
Texa
s, Arl
ington
, Arlin
gton,
TX
1030
hrs
AIAA-2
015-2
552
Ener
gy G
ain Fr
om an
Atm
osph
ere
in Mo
tion
- Dyn
amic
Soar
ing an
d Re
gen-
electr
ic Fli
ght C
ompa
red
J. Ba
rnes,
Pelica
n Aero
Grou
p, Sa
n Pe
dro, C
A
1100
hrs
AIAA-2
015-2
553
Inter
actio
ns of
Airc
raft
Desig
n an
d Con
trol: A
ctuat
ors S
izing
and
Optim
izatio
n fo
r an
Unsta
ble
Blen
ded W
ing-B
ody
Y. De
nieul,
D. A
lazard
, J. B
orden
euve
, Un
iversi
ty of
Toulo
use,
Toulo
use,
Franc
e; C.
Tous
saint
, ONE
RA, T
oulou
se, F
rance
; G.
Taqu
in, Ai
rbus,
Toulo
use,
Franc
e
1130
hrs
AIAA-2
015-2
554
Finite
Serie
s Bas
ed M
odel
Refe
renc
e Ada
ptive
Cont
rol
R. Ge
zer, R
OKET
SAN
Missi
le Ind
ustrie
s, Inc
., An
kara,
Turke
y; A.
Kutay
, Midd
le Ea
st Te
chnic
al Un
iversi
ty, An
kara,
Turke
y
62
Tues
day,
23 Ju
ne 2
015
84-A
FM-6
Aero
serv
oelas
tic (A
SE) a
nd A
erod
ynam
ic Pr
edict
ion M
ethod
sPlu
m Bl
osso
m B
Chair
ed by
: A. D
A RON
CH, U
nivers
ity of
Sou
thamp
ton an
d T. R
ICHAR
DSON
, Univ
ersity
of B
ristol
0900
hrs
AIAA-2
015-2
555
Adap
tive C
heby
shev
Neu
ral C
ontro
l of
a Mu
lti-In
put A
eroe
lastic
Syste
m De
spite
Gus
t Loa
dP.
Ghora
wat,
Unive
rsity
of Ne
vada
, Las
Ve
gas,
Las V
egas
, NV;
K. Le
e, Ca
tholic
Kwan
dong
Univ
ersity
, Gan
gnun
g, So
uth
Korea
; S. S
ingh,
Unive
rsity
of Ne
vada
, Las
Ve
gas,
Las V
egas
, NV
0930
hrs
AIAA-2
015-2
556
Mode
ling a
nd Si
mulat
ion fo
r Au
tono
mous
Aer
ial R
efue
ling U
sing
a Pro
be-D
rogu
e Sys
temH.
Wan
g, X.
Don
g, J.
Liu, J
. Wan
g, Air
Fo
rce En
ginee
ring U
nivers
ity, X
i’an,
China
1000
hrs
AIAA-2
015-2
557
Pilot
In Th
e Loo
p Aer
oser
voela
stic
Simula
tion
In Su
ppor
t To T
he
Conc
eptu
al De
sign
Of A
Fly B
y Wire
Ai
rplan
eF.
Boco
la, V.
Mus
carel
lo, G
. Qua
ranta,
P.
Masa
rati, T
echn
ical U
nivers
ity of
Mila
n, Mi
lano,
Italy
1030
hrs
AIAA-2
015-2
558
Aero
stru
ctura
l mod
eling
of a
wing
us
ing CA
TIA V5
and X
FLR5
softw
are
and e
xper
imen
tal v
alida
tion
using
th
e Pric
e- P
aïdou
ssis w
ing tu
nnel
D. Co
mmun
ier, M
. Sali
nas,
O. Ca
rranz
a Mo
yao,
R. Bo
tez, U
nivers
ity of
Qué
bec,
Montr
éal, C
anad
a
1100
hrs
AIAA-2
015-2
559
On th
e Calc
ulatio
n of
Pitc
h Da
mping
Stab
ility D
eriva
tives
of
Aircr
afts
Using
Uns
teady
Sens
itivity
Eq
uatio
nsC.
Guo,
Y. Re
n, Tsi
nghu
a Univ
ersity
, Be
ijing,
China
Tues
day,
23 Ju
ne 2
015
85-A
MT-5
/GT-5
Mode
l Atti
tude
, Def
orma
tion,
and D
ata A
cquis
ition
Tech
nique
sOb
elisk
BCh
aired
by: R
. GUY
TON,
USA
F Wrig
ht La
b09
00 hr
sAIA
A-201
5-256
0Te
mper
atur
e Mea
sure
ment
at th
e Ex
it of
Ann
ular C
ombu
stor w
ith
Sling
er in
Turb
ojet E
ngine
D. Li
u, J.
Jin, F
. Wan
g, W.
Jin,
Beiha
ng
Unive
rsity,
Beij
ing, C
hina
0930
hrs
AIAA-2
015-2
561
NASA
Data
Acqu
isition
Syste
m So
ftwar
e Dev
elopm
ent f
or Ro
cket
Prop
ulsion
Test
Facili
ties
P. Heb
ert, D
. Dav
is, M.
Turow
ski, W
. Holla
day,
NASA
Sten
nis Sp
ace Ce
nter, S
tennis
, MS;
P. Ma
rshall,
M. D
uncan
, Arct
ic Slop
e Reg
ional
Corpo
ration
(ASR
C), S
tennis
, MS;
et al.
1000
hrs
Oral
Prese
ntatio
nNe
w Wi
ngs l
evel
Yaw
Capa
bility
in
the A
EDC P
WT 1
6T Tu
nnel
B. M
ills, A
rnold
Engin
eerin
g Dev
elopm
ent
Comp
lex, T
ullah
oma,
TN
1030
hrs
Oral
Prese
ntatio
nMo
del D
efor
matio
n Me
asur
emen
ts on
a Fle
xible
Wing
R. Gu
yton,
Air Fo
rce Re
searc
h Lab
orator
y, W
right-
Patte
rson A
FB, O
H
1100
hrs
AIAA-2
015-2
562
Mode
l Def
orma
tion
Meas
urem
ent
Capa
bilitie
s at E
TWH.
Quix
, J. S
emme
lman
n, M.
Wrig
ht,
Europ
ean T
ranso
nic W
indtun
nel, C
ologn
e, Ge
rman
y
Tues
day,
23 Ju
ne 2
015
86-A
MT-6
/GT-6
Spat
ially-
Reso
lved S
pectr
osco
pic Te
chniq
ues
Edelw
eiss
Chair
ed by
: R. B
URNS
and A
. CUT
LER,
The G
eorge
Was
hingto
n Univ
ersity
0900
hrs
AIAA-2
015-2
563
WIDE
CARS
Spec
tra Fi
tting
in a
Prem
ixed E
thyle
ne-A
ir Fla
meA.
Cutle
r, E. G
allo,
L. Ca
ntu, G
eorge
Wa
shing
ton U
nivers
ity, W
ashin
gton,
DC
0930
hrs
AIAA-2
015-2
564
Dens
ity Sc
aling
and C
alibr
ation
of
FLEE
T Tem
pera
ture
Mea
sure
ment
sN.
Calve
rt, A.
Dog
ariu,
M. Ed
wards
, R.
Miles
, Prin
ceton
Univ
ersity
, Prin
ceton
, NJ
1000
hrs
AIAA-2
015-2
565
Preci
sion o
f FLE
ET Ve
locim
etry u
sing
High
-Spee
d CMO
S Cam
era Sy
stems
C. Pe
ters,
Prince
ton Un
iversit
y, Pri
nceton
, NJ;
P. Dan
ehy,
B. Ba
thel, N
ASA L
angle
y Rese
arch
Cente
r, Ham
pton,
VA; N
. Jian
g, Sp
ectral
En
ergies
, LLC
, Day
ton, O
H; N.
Calve
rt, R.
Miles
, Prin
ceton
Unive
rsity,
Prince
ton, N
J
1030
hrs
AIAA-2
015-2
566
Appli
catio
n of
FLEE
T Velo
cimetr
y in
the N
ASA
Lang
ley 0
.3-M
eter
Trans
onic
Cryo
genic
Tunn
elR.
Burns
, Nati
onal
Institu
te of
Aeros
pace
, Ha
mpton
, VA;
P. Da
nehy
, S. J
ones
, NAS
A La
ngley
Rese
arch C
enter
, Ham
pton,
VA;
B. H
alls,
N. Ji
ang,
Spec
tral E
nergi
es, L
LC,
Dayto
n, OH
1100
hrs
AIAA-2
015-2
567
Desig
n an
d App
licat
ion of
Filte
red
Rayle
igh Sc
atter
ing Ex
perim
ents
for M
ixing
Stud
ies of
New
Stru
t In
jecto
rs fo
r Scra
mjets
C. Gr
ound
, D. T
humi
ah, L
. Mad
dalen
a, Un
iversi
ty of
Texa
s, Arl
ington
, Arlin
gton,
TX
Tues
day,
23 Ju
ne 2
015
87-A
PA-9
High
Ang
le of
Atta
ck an
d High
Lift
Aero
dyna
mics
Stemm
ons C
Chair
ed by
: D. L
ACY,
Boein
g Com
merci
al Air
plane
s and
P. H
ARTW
ICH, B
oeing
Rese
arch &
Tech
nolog
y09
00 hr
sAIA
A-201
5-256
8Hi
gh A
ngle
of A
ttack
Fligh
t of a
Su
bsca
le Ae
roba
tic A
ircra
ftO.
Dan
tsker,
M. S
elig,
Unive
rsity
of Illi
nois,
Ur
bana
-Cham
paign
, Urba
na, I
L
0930
hrs
AIAA-2
015-2
569
Pres
sure
Mea
sure
ment
s of B
urst
Wake
s Ove
r a Th
ree-
Eleme
nt A
irfoil
B. Po
meroy
, M. S
elig,
Unive
rsity
of Illi
nois,
Ur
bana
-Cham
paign
, Urba
na, I
L
1000
hrs
Oral
Prese
ntatio
nDe
velop
ment
Status
of th
e High
Lift
Comm
on Re
search
Mod
el (H
L-CRM
): A
Repr
esenta
tive H
igh Li
ft Co
nfigu
ratio
n for
Tran
sonic
Tran
spor
tsD.
Lacy,
The B
oeing
Comp
any,
Evere
tt, WA
; E.
Dicke
y, A.
Sclaf
ani, T
he Bo
eing C
ompa
ny,
Hunti
ngton
Beach
, CA
1030
hrs
AIAA-2
015-2
570
Stall M
aneu
ver S
imula
tion
of an
ela
stic T
rans
port
Aircr
aft b
ased
on
Fligh
t Tes
t Dat
aD.
Rohlm
ann,
S. Ke
ye, G
erman
Aeros
pace
Ce
nter (
DLR)
, Brau
nsch
weig,
Germ
any
1100
hrs
AIAA-2
015-2
571
Nume
rical
Inve
stiga
tion
of th
e Dy
nami
c Beh
avior
of a
High
-Lift
Confi
gura
tion
with
Circu
lation
Co
ntro
lD.
Kelle
r, R. R
udnik
, Germ
an Ae
rospa
ce
Cente
r (DL
R), B
rauns
chwe
ig, G
erman
y
1130
hrs
AIAA-2
015-2
572
Wall m
odele
d lar
ge ed
dy
simula
tion
of th
e VFE
-2 de
lta w
ingC.
Zwerg
er, S
. Hick
el, C.
Brei
tsamt
er, N
. Ad
ams,
Tech
nical
Unive
rsity
of Mu
nich,
Munic
h, Ge
rman
y
63
Tues
day,
23 Ju
ne 2
015
88-A
PA-1
0Wi
nd Tu
nnel
and F
light
Testi
ngCa
rpen
ter B
allro
omCh
aired
by: J
. PIN
IER, N
ASA L
angle
y Res
earch
Cente
r and
G. G
ATLIN
, NAS
A Lan
gley R
esea
rch Ce
nter
0900
hrs
AIAA-2
015-2
573
Analy
sis of
Sing
le Ho
le Sim
ulated
Ba
ttle D
amag
e on
a Wing
Usin
g Pa
rticle
Imag
e Velo
cimetr
yM.
Almo
nd, P
. Ren
der, A
. Walk
er,
Loug
hboro
ugh U
nivers
ity, L
ough
borou
gh,
Unite
d King
dom
0930
hrs
AIAA-2
015-2
574
Wind
spee
d and
Flow
Ang
le Me
asur
emen
t by T
rack
ing of
a La
ser-I
nduc
ed B
reak
down
Spar
kM.
Renn
ie, M
. Ngu
yen,
S. G
ordey
ev, E
. Ju
mper,
Univ
ersity
of N
otre D
ame,
Notre
Da
me, I
N; A.
Cain,
Inno
vativ
e Tec
hnolo
gy
Appli
catio
ns Co
mpan
y, LLC
, Che
sterfie
ld,
MO; T
. Hay
den,
U.S.
Air F
orce A
cade
my,
Color
ado S
pring
s, CO
1000
hrs
AIAA-2
015-2
575
Low
Spee
d Wind
Tunn
el In
vesti
gatio
n of
a Cir
culat
ion
Cont
rol W
ing fo
r Enh
ance
d Lift
K. Ka
nistra
s, P.
Saka
, K. V
alava
nis, N
. Vit
zilaio
s, M.
Ruthe
rford,
Univ
ersity
of
Denv
er, D
enve
r, CO
1030
hrs
AIAA-2
015-2
576
Desig
n of
a sw
ept w
ing w
ind tu
nnel
mode
l for
stud
y of c
ross-
flow
insta
bility
J. Se
rpieri
, M. K
otson
is, D
elft U
nivers
ity of
Te
chno
logy,
Delft,
The N
etherl
ands
1100
hrs
AIAA-2
015-2
577
Nume
rical
Repli
catio
n and
Im
prov
emen
t of W
ind Tu
nnel
Tests
for D
esign
and O
ff-De
sign O
pera
ting
Point
s of W
ind Tu
rbine
Airfo
ilsT.
Kuhn
, ENE
RCON
GmbH
, Brem
en, G
erman
y; A.
Altmi
kus,
ENER
CON
GmbH
, Auri
ch,
Germ
any;
N. Ba
laresq
ue, D
eutsc
he W
indGu
ard
GmbH
, Vare
l, Germ
any;
M. Lip
pert,
Unive
rsity
of Ap
plied S
cience
s, Kie
l, Germ
any
1130
hrs
AIAA-2
015-2
578
Deve
lopme
nt, S
tartu
p Ope
ratio
ns
and T
ests
of a
Prop
eller
Wind
Tu
nnel
Test
Rig
S. S
peck
, S. H
erbst,
H. K
im, F
. Stei
n, M.
Ho
rnung
, Tec
hnica
l Univ
ersity
of M
unich
, Ga
rching
, Germ
any
1200
hrs
AIAA-2
015-2
579
Study
of th
e flow
field
nea
r the
AO
A se
nsor
of an
A32
0 air
craft
J. Ka
tz, S
an D
iego S
tate U
nivers
ity, S
an
Diego
, CA
Tues
day,
23 Ju
ne 2
015
89-A
PA-1
1Sp
ecial
Sessi
on: L
ow B
oom
Activ
ities I
ISte
mmon
s ACh
aired
by: S
. CLIF
F, NA
SA-Am
es an
d K. W
AITHE
, Gulf
strea
m Ae
rospa
ce Co
rporat
ion09
00 hr
sAIA
A-201
5-258
0De
sign
of O
ptim
um Eq
uivale
nt-
Area
Targ
et fo
r High
-Fide
lity Lo
w-Bo
om A
ircra
ft De
sign
C. Oc
heltre
e, S.
Choi,
Virgi
nia Po
lytec
hnic
Institu
te an
d Stat
e Univ
ersity
, Blac
ksbu
rg,
VA
0930
hrs
AIAA-2
015-2
581
Feas
ibility
of Su
perso
nic A
ircra
ft Co
ncep
ts fo
r Low
-Boo
m an
d Flig
ht
Trim
Cons
traint
sW.
Li, N
ASA L
angle
y Res
earch
Cente
r, Ha
mpton
, VA
1000
hrs
AIAA-2
015-2
582
Unce
rtaint
y Ana
lysis
and R
obus
t De
sign
of Lo
w-Bo
om Co
ncep
ts us
ing A
tmos
pher
ic Ad
joint
sS.
Ralla
bhan
di, N
ation
al Ins
titute
of Ae
rospa
ce, H
ampto
n, VA
1030
hrs
AIAA-2
015-2
583
Rise
Time
Pre
dictio
n of
Sonic
Bo
om by
Full-
Field
Simula
tion
with
Th
erma
l Non
equil
ibrium
R. Ya
mash
ita, K
. Suz
uki, U
nivers
ity of
To
kyo,
Kash
iwa,
Japa
n
1100
hrs
AIAA-2
015-2
584
Free
Fligh
t Mea
sure
ment
of A
ircra
ft Mo
del u
sing A
ero B
allist
ic Ra
nge
A. Iw
akaw
a, D.
Furuk
awa,
Y. Ao
ki, A.
Sa
soh,
Nago
ya U
nivers
ity, N
agoy
a, Ja
pan
Tues
day,
23 Ju
ne 2
015
90-A
PA-1
2We
apon
s Aer
odyn
amics
: Miss
ile/P
rojec
tile/G
uided
-Mun
itions
, Car
riage
and S
tore
Sepa
ratio
n I
Stemm
ons B
Chair
ed by
: C. P
ASILI
AO, A
FRL/
RWW
V an
d C. R
OSEM
A, US
Army
AMRD
EC09
00 hr
sAIA
A-201
5-258
5Fli
ght B
ehav
iors o
f a Co
mplex
Pr
ojecti
le us
ing a
Coup
led CF
D-ba
sed S
imula
tion
Tech
nique
: Fre
e Mo
tion
J. Sa
hu, F
. Fres
coni,
Army
Rese
arch
Labo
ratory
, Abe
rdeen
Prov
ing G
round
, MD
0930
hrs
AIAA-2
015-2
586
Effe
ct of
Cana
rd D
eflec
tion
on Fi
n Pe
rform
ance
of a
Fin-S
tabil
ized
Proje
ctile
S. S
ilton,
Army R
esea
rch La
borat
ory,
Aberd
een P
roving
Grou
nd, M
D; C.
Coyle
, U.
S. M
ilitary
Acad
emy,
West
Point
, NY
1000
hrs
AIAA-2
015-2
587
Enha
nced
Bod
y Vor
tex M
odeli
ng
With
in Mi
ssile
Datco
mJ.
Doyle
, C. R
osem
a, Arm
y Avia
tion
and M
issile
Rese
arch D
evelo
pmen
t and
En
ginee
ring C
enter
, Red
stone
Arse
nal, A
L
1030
hrs
AIAA-2
015-2
588
A Co
mpar
ison
of P
redic
tive
Meth
odolo
gies f
or M
issile
Co
nfigu
ratio
ns w
ith St
rake
sC.
Rose
ma, A
rmy A
viatio
n and
Miss
ile
Rese
arch D
evelo
pmen
t and
Engin
eerin
g Ce
nter, R
edsto
ne Ar
sena
l, AL
1100
hrs
AIAA-2
015-2
589
Delay
ed D
etach
ed Ed
dy Si
mulat
ion
of P
rojec
tile Fl
ows
J. Ga
n, G.
Zha,
Unive
rsity
of Mi
ami, C
oral
Gable
s, FL
Tues
day,
23 Ju
ne 2
015
91-A
TIO-9
Term
inal &
Surfa
ce O
pera
tions
III
Manc
heste
rCh
aired
by: A
. SAR
AF, S
aab S
ensis
Corpo
ration
0900
hrs
AIAA-2
015-2
590
Identi
fying
Key I
ssues
and P
otenti
al So
lution
s for
Integ
rated
Arriv
al,
Depa
rture,
Surfa
ce Op
eratio
ns by
Su
rvey
ing St
akeh
older
Prefe
rences
B. Ap
onso,
R. Co
ppen
barge
r, Y. J
ung,
NASA
Am
es Re
search
Cente
r, Moff
ett Fi
eld, C
A; C.
O’Co
nnor,
G. Lo
hr, N
ASA L
angle
y Rese
arch
Cente
r, Ham
pton,
VA; L
. Quo
n, NA
SA Am
es
Resea
rch Ce
nter, M
offett
Field
, CA;
et al.
0930
hrs
AIAA-2
015-2
591
Integ
ratio
n of U
ncert
ain Ra
mp Ar
ea
Aircra
ft Tra
jector
ies an
d Gen
eratio
n of
Optim
al Ta
xiway
Sche
dules
at
Char
lotte
Doug
las (C
LT) Ai
rpor
tJ.
Coup
e, D.
Milut
inovic
, Univ
ersity
of
Califo
rnia,
Santa
Cruz
, San
ta Cru
z, CA
; W.
Malik,
UARC
at N
ASA A
mes R
esearc
h Cen
ter,
Moffe
tt Field
, CA;
Y. Jun
g, NA
SA Am
es
Resea
rch Ce
nter, M
offet
Field,
CA
1000
hrs
AIAA-2
015-2
592
The e
ffects
of El
ectri
c Tax
i Sys
tems
on ai
rpor
t sur
face
cong
estio
nP.
Rolin
g, P.
Sillek
ens,
R. Cu
rran,
Delft
Unive
rsity
of Te
chno
logy,
Delft,
The
Nethe
rland
s; W.
Wild
er, KL
M Ro
yal D
utch
Airlin
es, S
chiph
ol, Th
e Neth
erlan
ds
1030
hrs
AIAA-2
015-2
593
Punc
tuali
ty as
KPI
for P
erfo
rman
ce
Base
d Airp
ort M
anag
emen
tS.
Loth,
S. H
elm, G
erman
Aeros
pace
Ce
nter (
DLR)
, Brau
nsch
weig,
Germ
any
1100
hrs
AIAA-2
015-2
594
Deter
minin
g Airp
ort A
irside
Ca
pacit
y Utili
zatio
n: A
Dem
and-
Drive
n Ap
proa
chC.
Schin
wald,
M. H
ornun
g, Te
chnic
al Un
iversi
ty of
Munic
h, Mu
nich,
Germ
any
1130
hrs
AIAA-2
015-2
595
Integ
ratio
n of
a Ro
uting
Tool
in an
Adv
ance
d Airp
ort C
ontro
ller
Work
ing P
ositio
nM.
Ellej
mi, E
UROC
ONTR
OL, B
russe
ls,
Belgi
um; B
. Weis
s, F.
Schm
itt, S
. Stra
ub,
Deuts
che F
lugsic
herun
g Gmb
H (D
FS),
Frank
furt,
Germ
any
64
Tues
day,
23 Ju
ne 2
015
92-A
TIO-1
0AT
M I -
Traje
ctory
Enha
ncem
ents
Milan
Chair
ed by
: S. R
OY, W
ashin
gton S
tate U
niv09
00 hr
sAIA
A-201
5-259
6Im
pact
of A
irspa
ce Ch
arge
s on
Trans
atlan
tic A
ircra
ft Tra
jecto
ries
B. S
ridha
r, NAS
A Ame
s Res
earch
Cente
r, Mo
ffett
Field,
CA; H
. Ng,
Unive
rsity
of Ca
liforni
a, Sa
nta Cr
uz, M
offett
Field
, CA;
F. Lin
ke, G
erman
Aeros
pace
Cente
r (DL
R),
Hamb
urg, G
erman
y; N.
Chen
, NAS
A Ame
s Re
searc
h Cen
ter, M
offett
Field
, CA
0930
hrs
AIAA-2
015-2
597
Pres
enta
tion
of th
ree m
ethod
s re
sults
comp
ariso
n fo
r Ver
tical
Navig
ation
VNAV
traje
ctory
op
timiza
tion
for t
he Fl
ight
Mana
geme
nt Sy
stem
FMS
B. B
eulze
, B. D
ancila
, R. B
otez,
Unive
rsity
of Qu
ébec
, Mon
tréal,
Cana
da
1000
hrs
AIAA-2
015-2
598
Simple
Tool
for A
ircra
ft No
ise-
Redu
ction
Rou
te De
sign
J. Li,
N. C
hen,
B. S
ridha
r, H. N
g, NA
SA
Ames
Rese
arch C
enter
, Moff
ett Fi
eld, C
A
1030
hrs
AIAA-2
015-2
599
Trajec
tory
Accu
racy
Sens
itivity
to
Mode
ling F
acto
rsS.
Torre
s, Lo
ckhe
ed M
artin
Corpo
ration
, Ro
ckvil
le, M
D
1100
hrs
AIAA-2
015-2
600
Trajec
tory
Inef
ficien
cy M
etric
for M
easu
ring O
pera
tiona
l Pe
rform
ance
of Fl
ights
in th
e Na
tiona
l Airs
pace
Syste
mS.
Tsao
, R. M
ayer,
A. M
ahas
habd
e, MI
TRE
Corpo
ration
, McLe
an, V
A
Tues
day,
23 Ju
ne 2
015
93-A
TIO-1
1Tra
nsfo
rmat
ional
Fligh
t - O
n-De
mand
Mob
ility
Metro
polita
n Ba
llroo
mCh
aired
by: B
. GER
MAN,
Geo
rgia I
nstitu
te of
Tech
nolog
y09
00 hr
sOr
al Pre
senta
tion
On-D
eman
d Mob
ility:
Aviat
ion’s
Futu
re P
ath
to H
igh Sp
eed R
egion
al Mo
bility
M. M
oore,
NAS
A Lan
gley R
esea
rch Ce
nter,
Hamp
ton, V
A
0930
hrs
Oral
Prese
ntatio
nOn
-Dem
and M
obilit
y Tec
hnica
l Pa
thwa
y: En
ablin
g Eas
e of U
se
and S
afety
K. Go
odric
h, M.
Moo
re, N
ASA L
angle
y Re
searc
h Cen
ter, H
ampto
n, VA
1000
hrs
Oral
Prese
ntatio
nOn
-Dem
and M
obilit
y Tec
hnica
l Pa
thwa
y: En
ablin
g Low
Comm
unity
No
ise, L
ow O
pera
ting C
osts,
Rob
ust
Cont
rol, a
nd R
ide Q
uality
M. M
oore,
NAS
A Lan
gley R
esea
rch Ce
nter,
Hamp
ton, V
A
Tues
day,
23 Ju
ne 2
015
94-C
ASE-4
09
00 -
1200
hrs
Appli
ed Co
mplex
ity W
orks
hop
Gran
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ring y
our o
wn ex
perie
nces
to sh
are an
d a de
sire t
o stre
ngthe
n you
r com
plex s
ystem
s eng
ineeri
ng th
inking
.
Pan
elists
:Pa
ul C.
Lamb
ertso
nSy
stems
Engin
eerin
g & In
tegrat
ion Te
am 7
77X
Boein
g Com
merci
al Air
plane
s
Steve
Holt
E ngin
eerin
g Inte
grated
Strat
egy,
Airpla
ne Le
vel E
ngine
ering
Integ
ration
The B
oeing
Comp
any
Jim B
lohow
iak77
7X Ai
rplan
e Lev
el Int
egrat
ion Te
amTh
e Boe
ing Co
mpan
y
Aliso
n La
uder
bach
777X
Airpl
ane L
evel
Integ
ration
Team
The B
oeing
Comp
any
Tues
day,
23 Ju
ne 2
015
95-C
FD-9
Adap
tive H
igh-O
rder
Meth
ods
Gran
d Ball
room
ACh
aired
by: G
. MAY
, RW
TH Aa
chen
and S
. ALLM
ARAS
, MIT
0900
hrs
AIAA-2
015-2
601
A Un
ifying
Comp
utat
ional
Fram
ewor
k fo
r Ada
ptive
High
-Or
der F
inite
Eleme
nt M
ethod
sM.
Woo
pen,
A. Ba
lan, G
. May
, RW
TH
Aach
en U
nivers
ity, A
ache
n, Ge
rman
y
0930
hrs
AIAA-2
015-2
602
An O
utpu
t-Bas
ed A
dapt
ive
Hybr
idize
d Disc
ontin
uous
Gale
rkin
Meth
od on
Def
ormi
ng D
omain
sK.
Fidko
wski,
Univ
ersity
of M
ichiga
n, An
n Arb
or, An
n Arbo
r, MI
1000
hrs
AIAA-2
015-2
603
An A
djoint
-Bas
ed h
p-Ad
aptiv
e Pe
trov-
Galer
kin M
ethod
for
Turb
ulent
Flow
sB.
Reza
Ahrab
i, W. A
nders
on, J
. New
man,
Unive
rsity
of Te
nnes
see,
Chatt
anoo
ga,
Chatt
anoo
ga, T
N
1030
hrs
AIAA-2
015-2
604
An Ad
aptiv
e Sim
plex C
ut-Ce
ll Meth
od
for H
igh-O
rder
Disco
ntinu
ous G
alerk
in Di
screti
zatio
ns of
Conju
gate
Heat
Trans
fer Pr
oblem
sS.
Ojeda
, H. S
un, S
. Allm
aras,
D. Da
rmofa
l, Ma
ssachu
setts
Institu
te of
Techn
ology,
Ca
mbrid
ge, M
A
1100
hrs
AIAA-2
015-2
605
Impr
oving
High
-Ord
er Fi
nite
Eleme
nt A
ppro
ximat
ion Th
roug
h Ge
ometr
ical W
arpin
gD.
San
jaya,
K. Fid
kows
ki, U
nivers
ity of
Mi
chiga
n, An
n Arbo
r, Ann
Arbo
r, MI
1130
hrs
AIAA-2
015-2
606
Hp-A
dapt
ivity
on A
nisot
ropic
Me
shes
for H
ybrid
ized
Disco
ntinu
ous G
alerk
in Sc
heme
A. Ba
lan, M
. Woo
pen,
G. M
ay, R
WTH
Aa
chen
Univ
ersity
, Aac
hen,
Germ
any
65
Tues
day,
23 Ju
ne 2
015
96-C
FD-1
0Tu
rbule
nt Fl
ow Si
mulat
ions I
Gran
d Ball
room
BCh
aired
by: S
. POR
OSEV
A, Th
e Univ
ersity
of N
ew M
exico
and S
. TIM
ME, T
he U
nivers
ity of
Live
rpool
0900
hrs
AIAA-2
015-2
607
Delay
ed D
etach
ed-Ed
dy Si
mulat
ion
of Sh
ock
Buffe
t on
Half
Wing
-Bod
y Co
nfigu
ratio
nF.
Sarto
r, S. T
imme
, Univ
ersity
of
Liverp
ool, L
iverpo
ol, U
nited
King
dom
0930
hrs
AIAA-2
015-2
608
Flow
Cont
rol o
f a R
otat
ing Cy
linde
r by
the U
se of
a Str
uctu
red S
urfa
ce:
A Vis
ualiz
ation
of Fl
ow St
ructu
res
T. Sc
homb
erg, R
. Ritz
, O. W
ünsch
, Un
iversi
ty of
Kasse
l, Kas
sel, G
erman
y; M.
Ru
etten
, R. K
essle
r, Germ
an Ae
rospa
ce
Cente
r (DL
R), G
ötting
en, G
erman
y
1000
hrs
AIAA-2
015-2
609
Simula
tions
of In
comp
ressi
ble
Sepa
rated
Turb
ulent
Flow
s aro
und
Two-
Dime
nsion
al Bo
dies w
ith
URAN
S Mod
els in
Ope
nFOA
MA.
Porte
ous,
R. Ha
bbit,
J. Co
lmen
ares,
S. Po
rosev
a, Un
iversi
ty of
New
Mexic
o, Alb
uque
rque,
Albuq
uerqu
e, NM
; S.
Murm
an, N
ASA A
mes R
esea
rch Ce
nter,
Moffe
tt Fie
ld, CA
1030
hrs
AIAA-2
015-2
610
Jet p
ump o
ptimi
zatio
n thr
ough
Re
ynold
s ave
rage
d Nav
ier-St
okes
Sim
ulatio
n Ana
lysis
G. Gh
erman
, I. M
alael,
COMO
TI Ro
mania
n Re
search
& De
velop
ment
Institu
te for
Gas
Turbin
es, Bu
chares
t, Rom
ania;
M. M
ihaesc
u, Ro
yal In
stitute
of Te
chnolo
gy (K
TH),
Stockh
olm, S
wede
n; I. P
orumb
el, CO
MOTI
Roma
nian R
esearc
h & De
velop
ment
Institu
te for
Gas T
urbine
s, Bu
chares
t, Rom
ania
Tues
day,
23 Ju
ne 2
015
97-C
FD-1
1Me
shing
Tech
nique
s II
Cora
lCh
aired
by: M
. PAR
K, NA
SA-La
ngley
Rese
arch C
enter
and D
. THO
MPSO
N, M
ississ
ippi S
tate U
nivers
ity09
00 hr
sAIA
A-201
5-261
1Co
mpar
ison
of r-
Adap
tatio
n Te
chniq
ues f
or 2
-D CF
D Ap
plica
tions
W. Ty
son,
J. De
rlaga
, A. C
houd
hary,
C.
Roy,
Virgin
ia Po
lytec
hnic
Institu
te an
d St
ate U
nivers
ity, B
lacks
burg,
VA
0930
hrs
AIAA-2
015-2
612
Imple
ment
ation
of B
all-C
enter
Sp
ring A
nalog
y Mes
h De
form
ation
Te
chniq
ue w
ith CF
D De
sign
Optim
izatio
nY.
Yang
, S. Ö
zgen
, Midd
le Ea
st Te
chnic
al Un
iversi
ty, An
kara,
Turke
y
1000
hrs
AIAA-2
015-2
613
Aniso
tropic
Non
-Unif
orm
Bloc
k-Ba
sed A
dapt
ive M
esh
Refin
emen
t fo
r Thr
ee-D
imen
siona
l Inv
iscid
and
Visco
us Fl
ows
L. Fre
ret, C
. Grot
h, Un
iversi
ty of
Toron
to,
Toron
to, Ca
nada
1030
hrs
AIAA-2
015-2
614
A sh
ifting
disco
ntinu
ous-g
rid-b
lock
lattic
e Bolt
zman
n me
thod
for
movin
g bou
ndar
y sim
ulatio
nsN.
Arora
, A. G
upta,
India
n Ins
titute
of Te
chno
logy D
elhi, N
ew D
elhi, I
ndia;
W.
Shyy
, Hon
g Kon
g Univ
ersity
of S
cienc
e and
Te
chno
logy,
Hong
Kong
, Hon
g Kon
g
1100
hrs
AIAA-2
015-2
615
Nume
rical
simula
tion o
f an X
-wing
fla
pping
wing
MAV
by m
eans
of a
defor
ming
overs
et gr
id me
thod
S. De
ng, D
elft U
nivers
ity of
Techn
ology,
Delft,
Th
e Neth
erlan
ds; T.
Xiao
, Nan
jing Un
iversit
y of
Aeron
autics
and A
stron
autics
, Nan
jing, C
hina;
M. Pe
rcin, B
. van
Oud
heusd
en, H
. Bijl,
B. Re
mes,
Delft
Unive
rsity o
f Tech
nolog
y, De
lft,
The N
etherl
ands
Tues
day,
23 Ju
ne 2
015
98-C
FD-1
2LE
S, DN
S, an
d Hyb
rid R
ANS-
LES I
IEm
erald
Chair
ed by
: N. B
ISEK,
Air Fo
rce Re
seac
h Lab
orator
y and
A. S
ESCU
, Miss
issipp
i Stat
e Univ
ersity
0900
hrs
AIAA-2
015-2
616
Simula
tion
of B
ound
ary L
ayer
flo
ws ov
er B
iofou
led Su
rface
sJ.
Sadiq
ue, X
. Yan
g, C.
Mene
veau
, R.
Mitta
l, Joh
ns H
opkin
s Univ
ersity
, Ba
ltimore
, MD
0930
hrs
AIAA-2
015-2
617
The E
ffect
of In
itial C
ondit
ions o
n Str
eamw
ise Vo
rtice
s in
the P
lane
Turb
ulent
Mixi
ng La
yer
W. M
cMull
an, S
. Garr
ett, U
nivers
ity of
Le
iceste
r, Leic
ester
, Unit
ed Ki
ngdo
m
1000
hrs
AIAA-2
015-2
618
Turb
ulent
inflo
w ge
nera
tion
in sq
uare
duct
at su
perso
nic M
ach
numb
erC.
Rous
sel, F
. Aliz
ard, F
. Gras
so, P
aris
Institu
te of
Tech
nolog
y, Pa
ris, F
rance
1030
hrs
AIAA-2
015-2
619
Furth
er Stu
dies o
f Adv
erse P
ressu
re
Grad
ient E
ffects
in Tu
rbule
nt Ch
anne
l Flo
wsA.
Jesus,
Techn
ologic
al Ins
titute
of Ae
ronau
tics
(ITA)
, São
José
dos C
ampo
s, Bra
zil; L.
Sc
hiavo
, Univ
ersity
of Ca
mpina
s, Ca
mpina
s, Bra
zil; J.
Azev
edo,
Aeron
autics
and S
pace
Ins
titute
(IAE),
São J
osé do
s Cam
pos,
Brazil;
J.
Lava
l, Nati
onal
Cente
r for S
cienti
fic Re
search
(C
NRS)
, Ville
neuv
e d’As
cq, Fr
ance
66
Tues
day,
23 Ju
ne 2
015
99-FD
-10
Boun
dary
-Laye
r Tra
nsitio
nSa
pphir
eCh
aired
by: E
. MAR
INEA
U, AE
DC W
hite O
ak an
d J. K
LENT
ZMAN
, Bay
lor U
nivers
ity09
00 hr
sAIA
A-201
5-262
0Tu
rbule
nt D
ensit
y Fluc
tuat
ions i
n Th
erma
l Bou
ndar
y Lay
ers S
tudie
d via
Mole
cular
Ray
leigh
scat
tering
J. Pa
nda,
NASA
Ames
Rese
arch C
enter
, Mo
ffett
Field,
CA
0930
hrs
AIAA-2
015-2
621
Auto
matic
tran
sition
pred
iction
in
an in
dustr
ial N
avier
-Sto
kes s
olver
us
ing h
igher
-ord
er fi
nite e
lemen
tsR.
Gros
s, F.
Chalo
t, J.
Court
y, M.
Mall
et, D
. Tra
n, Da
ssault
Grou
p, Sa
int Cl
oud,
Franc
e; D.
Arna
l, ONE
RA, T
oulou
se, F
rance
; et a
l.
1000
hrs
AIAA-2
015-2
622
Larg
e-Ed
dy Si
mulat
ion of
Tra
nsitio
nal F
lows o
n a C
ompr
esso
r Bl
ade
Z. Wa
ng, A
viatio
n Ind
ustry
Corpo
ration
of
China
(AVIC
), Sh
angh
ai, Ch
ina
1030
hrs
AIAA-2
015-2
623
A loc
al sca
tterin
g app
roac
h fo
r th
e effe
ct of
abru
pt ch
ange
s on
boun
dary
-laye
r ins
tabil
ity an
d tra
nsitio
n: a
nume
rical
meth
odZ.
Huan
g, Tia
njin U
nivers
ity, T
ianjin
, Chin
a; X.
Wu,
Impe
rial C
olleg
e Lon
don,
Lond
on,
Unite
d King
dom
1100
hrs
AIAA-2
015-2
624
Nume
rical
Simula
tion
of Th
ree-
Dime
nsion
al Wa
ve P
acke
t in
Supe
rsonic
Flow
over
a Co
mpre
ssion
Corn
erA.
Novik
ov, M
osco
w Ins
titute
of Ph
ysics
an
d Tec
hnolo
gy, Z
huko
vsky
, Rus
sia; I
. Eg
orov,
TsAGI
, Zhu
kovs
ky, R
ussia
; A.
Fedo
rov, M
osco
w Ins
titute
of Ph
ysics
and
Tech
nolog
y, Zh
ukov
sky,
Russi
a
1130
hrs
AIAA-2
015-2
625
Comp
utat
ions o
f Dist
urba
nce
Ampli
ficat
ion B
ehind
Isola
ted
Roug
hnes
s Elem
ents
and
Comp
ariso
n wi
th M
easu
reme
nts
M. Ch
oudh
ari, F
. Li, N
ASA L
angle
y Re
searc
h Cen
ter, H
ampto
n, VA
; M. B
ynum
, AM
A Res
earch
Asso
ciates
, Ham
pton,
VA; M
. Keg
erise
, R. K
ing, N
ASA L
angle
y Re
searc
h Cen
ter, H
ampto
n, VA
1200
hrs
AIAA-2
015-2
626
Acou
stic r
adiat
ion du
e to s
catte
ring
of T-
S wav
e by n
onlin
ear r
ough
ness
in su
bson
ic bo
unda
ry la
yer fl
ows
M. D
ong,
Tianji
n Univ
ersity
, Tian
jin, C
hina;
X. W
u, Im
peria
l Coll
ege L
ondo
n, Lo
ndon
, Un
ited K
ingdo
m
Tues
day,
23 Ju
ne 2
015
100-
FD-1
1Un
stead
y Wing
Aer
odyn
amics
IGo
veno
rs Le
cture
Hall
Chair
ed by
: K. M
OORE
D, Le
high U
nivers
ity an
d M. R
INGU
ETTE
, Univ
ersity
at B
uffalo
0900
hrs
AIAA-2
015-2
627
Deve
lopme
nt of
cohe
rent
stru
cture
s wi
thin
the l
amina
r sep
arat
ion
bubb
le of
a NA
CA00
18 ai
rfoil
J. Ku
relek
, A. L
ambe
rt, S
. Yaru
sevy
ch,
Unive
rsity
of Wa
terloo
, Wate
rloo,
Cana
da
0930
hrs
AIAA-2
015-2
628
Analy
zing V
ortex
Dyn
amics
in th
e La
mina
r Sep
arat
ion B
ubble
vis
Surfa
ce P
ressu
re M
easu
reme
nts
A. La
mbert
, S. Y
aruse
vych
, Univ
ersity
of
Water
loo, W
aterlo
o, Ca
nada
1000
hrs
AIAA-2
015-2
629
Analy
sis of
cruis
e fligh
t of t
he
callio
pe h
ummi
ngbir
dJ.
Song
, H. L
uo, V
ande
rbilt U
nivers
ity,
Nash
ville,
TN; B
. Tob
alske
, Univ
ersity
of
Monta
na, M
issou
la, M
issou
la, M
T; T.
Hedri
ck, U
nivers
ity of
Nort
h Caro
lina,
Chap
el Hil
l, Cha
pel H
ill, N
C
1030
hrs
AIAA-2
015-2
630
Topo
logy a
nd Fl
ow St
ructu
res o
f Th
ree-
Dime
nsion
al Se
para
tion
Bubb
les: T
he Ef
fect
of A
spec
t Rat
ioS.
Hos
seinv
erdi, R
. Jac
obi, H
. Fas
el,
Unive
rsity
of Ari
zona
, Tuc
son,
Tucso
n, AZ
Tues
day,
23 Ju
ne 2
015
101-
FD-1
2Ai
rfoil S
epar
ation
Cont
rol
Sena
tors
Lectu
re H
allCh
aired
by: M
. VISB
AL, U
SAF A
FRL/
RQVA
and K
. TAIR
A, Flo
rida S
tate U
nivers
ity09
00 hr
sAIA
A-201
5-263
1Mo
delin
g Lift
Hyste
resis w
ith a
Modifi
ed G
oman
-Khr
abro
v Mod
el on
Pit
ching
Airfo
ilsD.
Willia
ms, Il
linois I
nstitu
te of
Techn
ology,
Ch
icago
, IL; F.
Reiss
ner, T
echnic
al Un
iversit
y of
Berlin
, Berl
in, Ge
rman
y; D.
Green
blatt,
H. Mu
ehler
-Vahl,
Techn
ion--Is
rael In
stitute
of
Techn
ology,
Haifa
, Israe
l; C. S
trang
feld,
Techn
ical U
nivers
ity of
Berlin
, Berl
in, Ge
rman
y
0930
hrs
AIAA-2
015-2
632
Surfa
ce vo
rticit
y flux
analy
sis in
se
para
tion
cont
rol o
n NA
CA 0
012
airfo
ilP.
Mund
ay, K
. Tair
a, Flo
rida S
tate
Unive
rsity,
Talla
hasse
e, FL
1000
hrs
AIAA-2
015-2
633
Meas
urem
ents
of 3
-D St
all Ce
lls on
2-
D Ai
rfoil
E. De
mauro
, H. D
ell’O
rso, V
. Siva
neri,
B.
Tuna
, M. A
mitay
, Ren
sselae
r Poly
techn
ic Ins
titute,
Troy
, NY
1030
hrs
AIAA-2
015-2
634
Inter
actio
ns of
a Lo
w As
pect
Ratio
Dy
nami
c Pin
with
a La
mina
r Bo
unda
ry La
yer
S. G
ilders
leeve
, C. L
eong
, M. A
mitay
, Re
nsse
laer P
olytec
hnic
Institu
te, Tr
oy, N
Y
1100
hrs
AIAA-2
015-2
635
Simula
tion
of a
Lami
nar-F
low
Comp
atibl
e High
-Lift
Confi
gura
tion
with
Flow
Cont
rol
D. Ri
zzett
a, M.
Visb
al, Ai
r Forc
e Res
earch
La
borat
ory, W
right-
Patte
rson A
FB, O
H
1130
hrs
AIAA-2
015-2
636
Glob
al sta
bility
analy
sis of
a co
mpre
ssible
turb
ulent
flow
arou
nd
a high
-lift
confi
gura
tion
M. Io
rio, A
irbus
, Mad
rid, S
pain;
L.
Gonz
alez,
Tech
nical
Unive
rsity
of Ma
drid,
Madri
d, Sp
ain; A
. Mart
inez,
Airbu
s, Fil
ton,
Unite
d King
dom
67
Tues
day,
23 Ju
ne 2
015
102-
FD-1
3Sh
ock-
Domi
nated
Flow
sTo
paz
Chair
ed by
: M. G
AMBA
, Univ
ersity
of M
ichiga
n and
J. PO
GGIE,
USA
F AFR
L/RB
AC09
00 hr
sAIA
A-201
5-263
7As
sessi
ng B
last L
oadin
g With
in Ob
stacle
Arra
ysD.
Mott
, Nav
al Re
searc
h Lab
orator
y, Wa
shing
ton, D
C; T.
Youn
g, Be
rkeley
Re
searc
h Asso
ciates
, Belt
sville
, MD;
D.
Sch
wer, P
. Mati
c, Na
val R
esea
rch
Labo
ratory
, Was
hingto
n, DC
0930
hrs
AIAA-2
015-2
638
Study
of B
ow-S
hock
Insta
bilitie
s in
front
of H
emisp
heric
al Sh
ell at
Hy
perso
nic M
ach
Numb
er 7
A. Va
shish
tha, U
nivers
ity of
Toky
o, Ka
shiw
a, Ja
pan;
Y. Wa
tanab
e, Un
iversi
ty of
Toky
o, Bu
nkyo
, Jap
an; K
. Suz
uki,
Unive
rsity
of To
kyo,
Kash
iwa,
Japa
n
1000
hrs
AIAA-2
015-2
639
HIFiR
E-1 Tu
rbule
nt Sh
ock
Boun
dary
La
yer I
nter
actio
n -Fl
ight D
ata a
nd
Comp
utat
ions
R. Kim
mel, A
ir Forc
e Res
earch
Labo
ratory
, W
right-
Patte
rson A
FB, O
H; D
. Prab
hu, E
RC,
Inc.,
Moffe
tt Fie
ld, CA
1030
hrs
AIAA-2
015-2
640
Nume
rical
Simula
tion
Explo
ring
Supe
rsonic
Flow
Ove
r a W
all-
Moun
ted H
alf-C
ylind
er Tu
rret
P. Mo
rgan,
Ohio
Aeros
pace
Insti
tute,
Dayto
n, OH
; M. V
isbal,
Air F
orce R
esea
rch
Labo
ratory
, Wrig
ht-Pa
tterso
n AFB
, OH
1100
hrs
AIAA-2
015-2
641
Nume
rical
Inve
stiga
tion
of Sh
ock-
induc
ed La
mina
r Sep
arat
ion B
ubble
in
Supe
rsonic
Flow
sJ.
Sivas
ubram
anian
, H. F
asel,
Univ
ersity
of
Arizo
na, T
ucso
n, Tu
cson,
AZ
1130
hrs
AIAA-2
015-2
642
On u
nstea
dy sh
ock
wave
refle
ction
s fro
m we
dges
with
stra
ight a
nd
conc
ave t
ipsF.
Alzam
ora Pr
evita
li, E.
Timofe
ev, M
cGill
Unive
rsity,
Mon
tréal,
Cana
da; H
. Klei
ne,
Unive
rsity
of Ne
w So
uth W
ales a
t the
Au
strali
an D
efenc
e Forc
e Aca
demy
, Ca
nberr
a, Au
strali
a
Tues
day,
23 Ju
ne 2
015
103-
ITAR-
1ITA
R - H
yper
sonic
Flow
Phe
nome
na (I
nvite
d)
Moro
ccoCh
aired
by: K
. CAS
PER
0900
hrs
Oral
Prese
ntatio
nHT
V-2
Boun
dary
Laye
r Tra
nsitio
n -
Summ
ary a
nd Le
ssons
Lear
ned
R. Kim
mel, A
ir Forc
e Res
earch
Labo
ratory
, W
right-
Patte
rson A
FB, O
H
0930
hrs
Oral
Prese
ntatio
nST
ABL-3
D So
ftwar
e Ove
rview
H. Jo
hnso
n, Go
Hype
rsonic
, Inc
., Mi
nnea
polis,
MN
1000
hrs
Oral
Prese
ntatio
nMa
ch 1
0 Bo
unda
ry La
yer T
rans
ition
Expe
rimen
ts on
Shar
p and
Blun
ted
Cone
sE.
Marin
eau,
D. Le
wis,
J. La
fferty
, G.
Morar
u, Arn
old En
ginee
ring D
evelo
pmen
t Ce
nter, S
ilver
Sprin
g, MD
1030
hrs
Oral
Prese
ntatio
nSta
bility
Ana
lysis
of H
yper
sonic
Flo
ws U
sing S
TABL
-3D
B. W
heato
n, Jo
hns H
opkin
s Univ
ersity
Ap
plied
Phys
ics La
borat
ory, L
aurel
, MD;
H.
John
son,
GoHy
perso
nic, I
nc.,
Dayto
n, OH
; R.
Wagn
ild, S
andia
Nati
onal
Labo
ratori
es,
Albuq
uerqu
e, NM
Tues
day,
23 Ju
ne 2
015
104-
MAO-
3Ap
plica
tions
IMa
drid
Chair
ed by
: A. N
AJAF
I, AN
SYS,
Inc.
and P
. PIPE
RNI,
Bomb
ardier
Inc
0900
hrs
AIAA-2
015-2
646
Optim
izatio
n of
Syste
m Ev
olvab
ility
Unde
r Unc
erta
inty
J. Wa
tson,
J. All
en, C
. Matt
son,
Brigh
am
Youn
g Univ
ersity
, Prov
o, UT
; S. F
ergus
on,
North
Carol
ina S
tate U
nivers
ity, R
aleigh
, NC
0930
hrs
AIAA-2
015-2
647
An A
pplic
ation
of Co
ncep
tual
Desig
n an
d Mult
idisci
plina
ry
Analy
sis Tr
ansit
ioning
to D
etaile
d De
sign
Stage
sA.
Renn
er, F.
Thom
pson
, V. K
aliva
rapu,
E. W
iner, J
. Oliv
er, Io
wa S
tate U
nivers
ity,
Ames
, IA;
B. G
ilmore
, Dee
re &
Comp
any,
Molin
e, IL;
et al
.
1000
hrs
AIAA-2
015-2
648
Geom
etry D
riven
High
Fide
lity
Stabil
ity D
eriva
tives
Obtai
ned U
sing
Autom
ated C
FD An
alysis
Proc
essN.
Bhag
at, W
right
State
Unive
rsity,
Beav
ercree
k, OH
; E. A
lyana
k, Air
Force
Re
search
Labo
ratory
, Wrig
ht-Pa
tterso
n AFB
, OH
; D. A
llison
, Opti
mal F
light S
cience
s, LLC
, Da
yton,
OH
1030
hrs
AIAA-2
015-2
649
Appli
catio
n of
auto
matic
algo
rithm
ge
nera
tion
to ai
r-to-
air re
fueli
ng
sched
uling
R. En
tz, G
. Sch
erer S
chwe
ning,
R. Fe
rnand
es de
Oliv
eira,
Airbu
s, Mu
nich,
Germ
any
1100
hrs
AIAA-2
015-2
650
Multid
iscipl
inary
and M
ultile
vel
Aircr
aft D
esign
Meth
odolo
gy
Using
Enha
nced
Colla
bora
tive
Optim
izatio
nP.
Albuq
uerqu
e, P.
Gamb
oa, M
. Silv
estre
, Un
iversi
ty of
Beira
Inter
ior, C
ovilh
a, Po
rtuga
l
1130
hrs
AIAA-2
015-2
651
Deve
lopme
nt of
a Ja
va-b
ased
fra
mewo
rk fo
r airc
raft
preli
mina
ry
desig
n an
d opt
imiza
tion
F. Nic
olosi,
A. D
e Marc
o, L.
Attan
asio,
D.
Gam
barde
lla, U
nivers
ity of
Nap
les
“Fed
erico
II”, N
aples
, Ital
y
Tues
day,
23 Ju
ne 2
015
105-
MST-5
Guida
nce,
Cont
rol, a
nd D
ynam
ics II
Trave
rtine
Chair
ed by
: T. A
LEXE
EV, U
nivers
ity of
Califo
rnia D
avis
and J
. KNO
WLE
S, Lo
ughb
oroug
h Univ
ersity
0900
hrs
AIAA-2
015-2
652
Semi
-Impli
cit N
umer
ical
Simula
tions
of N
onlin
ear D
ynam
ics
of B
eams
, Plat
es, a
nd Sh
ells
T. Ale
xeev
, Siem
ens E
nergy
, Inc
., Bo
ulder,
CO
; M. H
afez,
Unive
rsity
of Ca
liforni
a, Da
vis, D
avis,
CA
0930
hrs
AIAA-2
015-2
653
A Bi
furca
tion
Study
of a
Dyna
mic
Mode
l of a
Nos
e Lan
ding G
ear
Mech
anism
Subje
cted t
o Ext
erna
l Di
sturb
ance
sJ.
Know
les, L
ough
borou
gh U
nivers
ity,
Loug
hboro
ugh,
Unite
d King
dom;
E.
Coetz
ee, A
irbus
, Bris
tol, U
nited
King
dom
1000
hrs
AIAA-2
015-2
654
Multi-
Fideli
ty Sim
ulatio
n of C
argo
Air
drop
: Fro
m the
Paylo
ad Ba
y to t
he
Grou
ndT.
Jann,
S. Ge
isbau
er, N
. Bier,
Germ
an
Aeros
pace
Cente
r (DL
R), B
raunsc
hweig
, Ge
rman
y; W.
Krüg
er, H.
Schm
idt, G
erman
Ae
rospa
ce Ce
nter (
DLR)
, Gött
ingen
, Germ
any
1030
hrs
AIAA-2
015-2
655
Cont
rol E
nhan
ced a
nd
Para
meter
ized L
oad R
elief
tec
hnolo
gy fo
r a La
unch
Vehic
leW.
Yang
, S. T
ang,
Z. Xu
, Nort
hwes
tern
Polyt
echn
ical U
nivers
ity, X
i’an,
China
1100
hrs
AIAA-2
015-2
656
The m
ode s
witch
cont
rol r
esea
rch
of sm
all-ty
pe pa
ralle
l TBC
C eng
ine
base
d on
SQP
meth
odQ.
Xiao
jie, W
. Su,
Y. Ta
ng, A
viatio
n Ind
ustry
Corpo
ration
of Ch
ina (A
VIC),
Wux
i, Chin
a
68
Tues
day,
23 Ju
ne 2
015
106-
NW-3
09
00 -
0930
hrs
Netw
orkin
g Cof
fee B
reak
Chan
tilly B
allro
om Ea
st
Tues
day,
23 Ju
ne 2
015
107-
PDL-4
Plasm
a Assi
sted C
ombu
stion
Miro
Chair
ed by
: K. X
U, U
nivers
ity of
Alab
ama i
n Hun
tsville
0900
hrs
AIAA-2
015-2
657
Electr
on Te
mper
atur
e in
a Me
than
e-Ai
r Flam
e und
er a
DC
Electr
ic Fie
ldS.
Jaco
bs, K
. Xu,
Unive
rsity
of Ala
bama
, Hu
ntsvil
le, H
untsv
ille, A
L
0930
hrs
AIAA-2
015-2
658
Lase
r-Ind
uced
Hea
ting U
sing a
No
n-Re
sona
nt D
ual-P
ulse A
ppro
ach
with
App
licat
ion to
Lase
r Ign
ition
C. Du
mitra
che,
C. Ro
se, A
. Yali
n, Co
lorad
o St
ate U
nivers
ity, F
ort Co
llins,
CO
1000
hrs
AIAA-2
015-2
659
Magn
etic p
ositio
ning o
f the
ele
ctric
disch
arge
in th
e volu
me of
su
perso
nic fl
owA.
Firso
v, Ru
ssian
Acad
emy o
f Scie
nces
, Mo
scow,
Russi
a; S.
Leon
ov, U
nivers
ity of
No
tre D
ame,
Notre
Dam
e, IN
1030
hrs
AIAA-2
015-2
660
Towa
rds L
aser
Ignit
ion by
Rap
id He
ating
of W
ater
Vapo
rC.
Dumi
trach
e, A.
Yalin
, Colo
rado S
tate
Unive
rsity,
Fort
Collin
s, CO
1100
hrs
AIAA-2
015-2
661
Multip
hysic
s sim
ulatio
ns of
plas
ma-
assis
ted co
mbus
tion
dyna
mics
in a
direc
t-cou
pled m
icrow
ave r
eacto
rA.
Palla
, J. Z
imme
rman
, D. C
arroll
, CU
Aeros
pace
, Cha
mpaig
n, IL;
C. M
itsing
as,
S. H
amma
ck, T
. Lee
, Univ
ersity
of Ill
inois,
Ur
bana
-Cham
paign
, Urba
na, I
L
1130
hrs
AIAA-2
015-2
662
Inve
stiga
tion
of Th
erma
l Cyc
ling
Prop
erty
of Th
erma
l Bar
rier
Coat
ings w
ith La
ser D
epos
ited M
esh
Struc
ture
S. S
hi, W
. Che
n, Z.
Hong
, D. G
ao, A
viatio
n Ind
ustry
Corpo
ration
of Ch
ina (A
VIC),
Shan
ghai,
China
Tues
day,
23 Ju
ne 2
015
108-
TP-5
Plasm
a and
Arc
Jet T
estin
g, Di
agno
stics
and C
ompu
tatio
nal M
ethod
sRo
setta
Chair
ed by
: M. W
INTE
R, Un
iversi
ty of
Kentu
cky a
nd P.
YEE
, The
Aeros
pace
Corpo
ration
0900
hrs
AIAA-2
015-2
663
Arc J
et Fa
cility
Test
Cond
ition
Pred
iction
s Usin
g the
ADS
I Cod
eG.
Palm
er, D
. Prab
hu, E
RC, I
nc.,
Hunts
ville,
AL
; I. T
erraz
as-Sa
linas
, NAS
A Ame
s Re
searc
h Cen
ter, M
offett
Field
, CA
0930
hrs
AIAA-2
015-2
664
Comp
ariso
ns of
PICA
In-de
pth M
ateria
l Pe
rform
ance
and A
blator
Resp
onse
Mo
delin
g fro
m ME
DLI A
rc Je
t Test
sD.
Smith
, Univ
ersity
of Ke
ntucky
, Lex
ington
, Lex
ington
, KY;
T. Wh
ite, E
RC, In
c., M
offett
Fie
ld, CA
; A. M
artin,
Unive
rsity o
f Ken
tucky,
Lex
ington
, Lex
ington
, KY
1000
hrs
AIAA-2
015-2
665
Enab
ling t
he St
atist
ical C
alibr
ation
of
Acti
ve N
itrida
tion
of G
raph
ite by
At
omic
Nitro
gen
P. Ba
uman
, Stat
e Univ
ersity
of N
ew Yo
rk,
Buffa
lo, N
Y
1030
hrs
AIAA-2
015-2
666
Side A
rm R
eacto
r Stu
dy of
Copp
er
Cata
lysis
D. D
river,
NAS
A Ame
s Res
earch
Cente
r, Mo
ffett
Field,
CA; S
. Sep
ka, E
RC, I
nc.,
Moffe
tt Fie
ld, CA
1100
hrs
AIAA-2
015-2
667
Cons
olida
ting N
ASA’s
Arc-
Jet
J. Ba
lboni,
T. G
okce
n, F.
Hui, P
. Grau
be, P
. Mo
rrisse
y, NA
SA Am
es Re
searc
h Cen
ter,
Moffe
tt Fie
ld, CA
; R. L
ewis,
NAS
A Joh
nson
Sp
ace C
enter
, Hou
ston,
TX
1130
hrs
AIAA-2
015-2
668
Phys
ico-C
hemi
stry o
f CN
in th
e Bo
unda
ry La
yer o
f Gra
phite
in
Nitro
gen
Plasm
asB.
Helb
er, T.
Ales
sand
ro, O
. Cha
zot,
M.
Thier
ry, vo
n Kárm
án In
stitut
e for
Fluid
Dyna
mics,
Rhod
e-Sain
t-Gen
èse,
Belgi
um
Tues
day,
23 Ju
ne 2
015
109-
F360
-3
0930
- 12
00 h
rsDa
y in
the L
ife of
Ope
ratio
ns -
Effe
ctive
ly Ma
nagin
g Disr
uptio
nGr
and B
allro
om E
Mode
rator:
Neil
Plan
zer, V
ice Pr
eside
nt, Ai
r Traf
fic M
anag
emen
t, Bo
eing C
omme
rcial
Airpla
nes
Pane
lits:
Tim Ca
mpbe
llSe
nior V
ice Pr
eside
nt, Ai
r Ope
ration
sAm
erica
n Airli
nes
Jim Cr
ites
Exec
utive
Vice
Pres
ident
of Op
eratio
nsDF
W In
terna
tiona
l Airp
ort
Brian
Quigl
eyMa
nagin
g Dire
ctor F
light
Opera
tions
Unite
d Airli
nes
Dan
Smile
yVic
e Pres
ident
for S
ystem
s Ope
ration
s, Fe
deral
Aviat
ion
Admi
nistra
tion A
ir Traf
fic O
ffice
Tues
day,
23 Ju
ne 2
015
111-
LNCH
-1
1230
- 14
00 h
rsAw
ards
Lunc
heon
: Cele
brat
ing A
chiev
emen
ts in
Aero
spac
e Scie
nces
Chan
tilly B
allro
om W
est
A tick
et is
requir
ed an
d inc
luded
in th
e con
feren
ce re
gistra
tion f
ee w
here
indica
ted.
69
Tues
day,
23 Ju
ne 2
015
112-
AA-1
6CA
A So
und G
ener
ation
IIFle
ur-d
e-lis
ACh
aired
by: J
. DEL
FS, D
LR - G
erman
Aeros
pace
Cente
r14
00 hr
sAIA
A-201
5-266
9Pr
edict
ion of
low-
spee
d fan
tra
iling-
edge
nois
e bas
ed on
RAN
S an
d on
scale
reso
lved s
imula
tions
G. G
rasso
, J. C
hristo
phe,
C. Sc
hram,
von
Kárm
án In
stitut
e for
Fluid
Dyna
mics,
Rh
ode-S
aint-G
enès
e, Be
lgium
1430
hrs
AIAA-2
015-2
670
Synt
hetic
Turb
ulenc
e Meth
ods f
or
Lead
ing Ed
ge N
oise P
redic
tions
F. Ge
a-Agu
ilera,
X. Z
hang
, X. C
hen,
J. Gil
l, Un
iversi
ty of
South
ampto
n, So
utham
pton,
Unite
d King
dom;
T. N
odé-L
anglo
is, Ai
rbus,
Toulo
use,
Franc
e
1500
hrs
AIAA-2
015-2
671
Pred
iction
of Sl
at B
road
band
Nois
e wi
th R
ANS R
esult
sB.
Bai,
X. L
i, Y. G
uo, B
eihan
g Univ
ersity
, Be
ijing,
China
; F. T
hiele,
Tech
nical
Unive
rsity
of Be
rlin, B
erlin,
Germ
any
1530
hrs
AIAA-2
015-2
672
Towa
rds h
igh-li
ft no
ise fr
om Fa
st Mu
ltipole
BEM
with
aniso
tropic
sy
nthe
tic tu
rbule
nce s
ource
sN.
Reich
e, M.
Lumm
er, R.
Ewert
, Germ
an
Aeros
pace
Cente
r (DL
R), B
rauns
chwe
ig,
Germ
any
1600
hrs
AIAA-2
015-2
673
Comp
act A
ssump
tion
Appli
ed to
th
e Mon
opole
Term
of Fa
rassa
t’s
Form
ulatio
nL.
Lope
s, NA
SA La
ngley
Rese
arch C
enter
, Ha
mpton
, VA
1630
hrs
AIAA-2
015-2
674
Cent
rifug
al Co
mpre
ssor:
The S
ound
of
Surg
eE.
Sund
ström
, M. M
ihaes
cu, R
oyal
Institu
te of
Tech
nolog
y (KT
H), S
tockh
olm,
Swed
en
Tues
day,
23 Ju
ne 2
015
113-
AA-1
7CA
A Pr
opag
ation
and S
catte
ring I
Fleur
-de-
lis B
Chair
ed by
: S. C
ARO,
CD-Ad
apco
1400
hrs
AIAA-2
015-2
675
Dire
ct an
d inv
erse
unc
erta
inty
quan
tifica
tion
of ac
ousti
c ref
racti
on
phen
omen
a thr
ough
a sh
ear l
ayer
P. Cin
nella
, Univ
ersità
del S
alento
, Lec
ce,
Italy;
X. G
loerfe
lt, X.
Merl
e, Pa
ris In
stitut
e of
Tech
nolog
y, Pa
ris, F
rance
1430
hrs
AIAA-2
015-2
676
Stabil
ized T
ime-
doma
in Im
peda
nce
Mode
l and
the A
pplic
ation
in
Bypa
ss Du
ct No
ise Si
mulat
ions
X. Li
u, X.
Hua
ng, P
eking
Univ
ersity
, Be
ijing,
China
1500
hrs
AIAA-2
015-2
677
Evalu
ation
and D
evelo
pmen
t of
Non
-Refl
ectiv
e Bou
ndar
y Co
nditio
ns fo
r Aer
oaco
ustic
Sim
ulatio
nsJ.
Gill, R
. Fatt
ah, X
. Zha
ng, U
nivers
ity
of So
utham
pton,
South
ampto
n, Un
ited
Kingd
om
1530
hrs
AIAA-2
015-2
678
Imple
ment
ation
of a
surfa
ce ba
sed
coup
ling a
ppro
ach
in a h
igh-o
rder
DG
aero
acou
stics
prop
agat
ion
solve
rM.
Muri
el Gr
acia,
W. D
e Roe
ck, W
. De
smet,
Catho
lic Un
iversi
ty of
Leuv
en,
Leuv
en, B
elgium
1600
hrs
AIAA-2
015-2
679
Acou
stic S
catte
ring M
atric
es fo
r Hi
gher
-Ord
er M
odes
for S
imple
Or
ifice
Confi
gura
tions
with
Flow
C. Te
mmler
, M. S
chulz
e, T.
Satte
lmay
er,
Tech
nical
Unive
rsity
of Mu
nich,
Munic
h, Ge
rman
y
1630
hrs
AIAA-2
015-2
680
Nume
rical
asse
ssmen
t of t
he
scatte
ring o
f aco
ustic
wav
es by
tu
rbule
nt st
ructu
res
V. Cla
ir, G.
Gab
ard, U
nivers
ity of
So
utham
pton,
South
ampto
n, Un
ited
Kingd
om
1700
hrs
AIAA-2
015-2
681
Enha
ncem
ents
of a
time-
doma
in eq
uivale
nt so
urce
meth
od fo
r ac
ousti
c sca
tterin
gS.
Swi
ft, G
. Blai
sdell
, Purd
ue U
nivers
ity,
West
Lafay
ette,
IN; A
. Lyri
ntzis,
Embry
-Rid
dle Ae
ronau
tical
Unive
rsity,
Day
tona
Beac
h, FL
Tues
day,
23 Ju
ne 2
015
114-
AA-1
8Ge
nera
l Aco
ustic
s IIn
vern
ess
Chair
ed by
: C. B
AILLY,
Ecole
Centr
ale de
Lyon
1400
hrs
AIAA-2
015-2
682
Soun
d and
Dist
ortio
n Pr
oduc
ed
by a
Brak
ing R
otor
Ope
ratin
g in
a Plan
ar B
ound
ary L
ayer
with
Ap
plica
tion
to W
ind Tu
rbine
sH.
Murr
ay, D
. Wisd
a, W.
Alex
ande
r, M.
Nelso
n, W.
Dev
enpo
rt, V
irgini
a Poly
techn
ic Ins
titute
and S
tate U
nivers
ity, B
lacks
burg,
VA
; S. G
legg,
Florid
a Atla
ntic U
nivers
ity,
Boca
Raton
, FL
1430
hrs
AIAA-2
015-2
683
Nozz
le-to
-Gro
und D
istan
ce Ef
fect
on N
ondo
mina
ted So
lution
s of
Multio
bjecti
ve A
eroa
cous
tic Fl
ame
Defle
ctor D
esign
Pro
blem
T. Ta
tsuka
wa, T
. Non
omura
, A. O
yama
, K.
Fujii,
Japa
n Aero
spac
e Exp
lorati
on Ag
ency
(JA
XA),
Kana
gawa
, Jap
an
1500
hrs
AIAA-2
015-2
684
The A
cous
tic En
viron
ment
of th
e NA
SA G
lenn
9- by
15-
Foot
Low-
Spee
d Wind
Tunn
elD.
Step
hens
, NAS
A Glen
n Res
earch
Cente
r, Cle
velan
d, OH
1530
hrs
AIAA-2
015-2
685
Sonic
Boo
m As
sessm
ent o
f a
Hype
rsonic
Tran
spor
t Veh
icle w
ith
Adva
nced
Num
erica
l Meth
ods
D. Lu
quet,
R. M
archia
no, F
. Cou
louvra
t, Pie
rre an
d Mari
e Curi
e Univ
ersity
, Pari
s, Fra
nce;
I. Sa
lah El
Din,
ONE
RA, M
eudo
n, Fra
nce;
A. Lo
seille
, Fren
ch N
ation
al Ins
titute
for Re
searc
h in C
ompu
ter S
cienc
e an
d Con
trol (
INRIA
), Le
Ches
nay,
Franc
e
Tues
day,
23 Ju
ne 2
015
115-
AA-1
9Ai
rfram
e Nois
e II
Laliq
ueCh
aired
by: C
. DOO
LAN,
The U
nivers
ity of
Adela
ide14
00 hr
sAIA
A-201
5-268
6Ae
roac
ousti
c Sim
ulatio
ns of
a S
impli
fied H
igh-Li
ft De
vice
Acco
untin
g for
Insta
llatio
ns Ef
fects
P. Sa
las, S
. More
au, U
nivers
ity of
Sh
erbroo
ke, S
herbr
ooke
, Can
ada
1430
hrs
AIAA-2
015-2
687
Aero
dyna
mic N
oise S
imula
tion
of an
Airf
oil in
a Pe
riodic
ally
Fluctu
ating
Free
strea
mY.
Yauw
enas
, N. A
hmed
, Univ
ersity
of N
ew
South
Wale
s, Ke
nsing
ton, A
ustra
lia
1500
hrs
AIAA-2
015-2
688
Wall P
ressu
re Sp
ectra
on a
DU96
-W-1
80 P
rofil
e Fro
m Lo
w to
Pr
e-Sta
ll Ang
les of
Atta
ckA.
Surya
di, M
. Herr
, Germ
an Ae
rospa
ce
Cente
r (DL
R), B
rauns
chwe
ig, G
erman
y
1530
hrs
AIAA-2
015-2
689
Supp
ressi
on of
spur
ious n
oise
sour
ces i
n air
foil s
elf-n
oise
meas
urem
ents
M. Tu
instra
, Nati
onal
Aeros
pace
Labo
ratory
(N
LR),
Emme
loord,
The N
etherl
ands
; P.
Sijtsm
a, Pie
ter S
ijtsma
Adva
nced
Ae
roAco
ustic
s, We
zep,
The N
etherl
ands
1600
hrs
AIAA-2
015-2
690
A pa
rame
tric e
xper
imen
tal s
tudy
of
jet-fl
ap in
terac
tion
noise
for a
re
alisti
c sma
ll-sca
le sw
ept w
ing
mode
lI.
Belya
ev, G
. Fara
noso
v, N.
Ostr
ikov,
TsAGI
, Mos
cow,
Russi
a; G.
Paran
in, O
JS
Irkut
Corpo
ration
, Mos
cow,
Russi
a
1630
hrs
AIAA-2
015-2
691
Airfr
ame S
hieldi
ng of
Non
comp
act
Aviat
ion N
oise S
ource
s: Th
eory
and
Expe
rimen
tN.
Ostr
ikov,
S. D
eniso
v, TsA
GI, M
osco
w,
Russi
a
1700
hrs
AIAA-2
015-2
692
Asses
smen
t of C
oncep
tual N
oise
Redu
ction
Dev
ices f
or A
Main
Land
ing
Gear
using
SNGR
Meth
odH.
Yao,
L. Da
vidson
, Cha
lmers
Unive
rsity o
f Tec
hnolo
gy, Gö
teborg
, Swe
den;
S. Pe
ng,
Swed
ish De
fense
Resea
rch Ag
ency
(FOI)
, Sto
ckholm
, Swe
den;
F. Cap
izzan
o, M.
Ba
rbarin
o, G.
Ming
ione,
Italian
Aeros
pace
Re
search
Cente
r (CIR
A), C
apua
, Italy
70
Tues
day,
23 Ju
ne 2
015
116-
AA-2
0Du
ct Ac
ousti
cs III
Obeli
sk A
Chair
ed by
: C. R
OYAL
TY, H
oney
well I
nterna
tiona
l, Inc
.14
00 hr
sAIA
A-201
5-269
3Mo
delin
g of B
road
band
Line
rs Ap
plied
to th
e Adv
ance
d Nois
e Co
ntro
l Fan
D. N
ark, M
. Jon
es, N
ASA L
angle
y Res
earch
Ce
nter, H
ampto
n, VA
; D. S
utliff,
NAS
A Gle
nn Re
searc
h Cen
ter, C
levela
nd, O
H
1430
hrs
AIAA-2
015-2
694
Desig
n Op
timiza
tion
of B
road
band
Ac
ousti
c Line
rs Th
roug
h Fin
ite
Eleme
nt Ef
ficac
y Stu
dies
K. Mi
tchell
, Virg
inia P
olytec
hnic
Institu
te an
d Stat
e Univ
ersity
, Blac
ksbu
rg, VA
1500
hrs
AIAA-2
015-2
695
Effect
of Po
rosit
y and
Joint
Bias
-gr
azing
Flow
on th
e Aco
ustic
Dam
ping
Perfo
rman
ce of
Doub
le- an
d Sing
le-lay
er Pe
rfora
ted Li
ners
C. Ji,
D. Zh
ao, S
. Li, X
. Li, N
anya
ng
Techn
ologic
al Un
iversit
y, Sin
gapo
re, Si
ngap
ore
1530
hrs
AIAA-2
015-2
696
Nonli
near
impe
danc
e mod
eling
of
reso
nato
r with
high
inten
sity
incide
nt ac
ousti
c wav
eJ.
Xu, X
. Li, Y
. Guo
, Beih
ang U
nivers
ity,
Beijin
g, Ch
ina
1600
hrs
AIAA-2
015-2
697
Evalu
ation
of Va
riable
-Dep
th
Liner
Confi
gura
tions
for I
ncre
ased
Br
oadb
and N
oise R
educ
tion
M. Jo
nes,
W. W
atson
, D. N
ark, B
. Ho
werto
n, NA
SA La
ngley
Rese
arch C
enter
, Ha
mpton
, VA
Tues
day,
23 Ju
ne 2
015
117-
ACD-
3Ai
rcraf
t Per
form
ance
Stud
iesWy
ethCh
aired
by: C
. BIL,
RMIT
Unive
rsity
and W
. ANE
MAAT,
DAR
corpo
ration
1400
hrs
AIAA-2
015-2
698
The I
mpac
t of A
TTCS
on R
educ
ed-
Thru
st Ta
keof
f Fiel
d Per
form
ance
T. Ta
kaha
shi, A
rizon
a Stat
e Univ
ersity
, Te
mpe,
AZ
1430
hrs
AIAA-2
015-2
699
Unce
rtaint
y Mod
eling
and
Asse
ssmen
t in
Aircr
aft E
vacu
ation
Sim
ulatio
nR.
Silva
, D. F
errari
, Tec
hnolo
gical
Institu
te of
Aeron
autic
s (ITA
), Sã
o Jos
é dos
Ca
mpos
, Braz
il; L.
Santo
s, Em
braer,
São
Jo
sé do
s Cam
pos,
Braz
il
1500
hrs
AIAA-2
015-2
700
Simula
ted Ti
ltrot
or A
ircra
ft Op
erat
ion in
Clos
e Pro
ximity
to a
Build
ing in
Wind
and G
roun
d-Ef
fect
Cond
itions
L. Yo
ung,
NASA
Ames
Rese
arch C
enter
, Mo
ffett
Field,
CA
1530
hrs
AIAA-2
015-2
701
Optim
al Cli
mb Tr
ajecto
ries T
hrou
gh
Expli
cit Si
mulat
ionT.
Taka
hash
i, Ariz
ona S
tate U
nivers
ity,
Temp
e, AZ
1600
hrs
AIAA-2
015-2
702
Desig
n fo
r Res
ilienc
e in
Auto
nomo
us Sy
stems
: Les
sons
Le
arne
d fro
m Co
ntro
lled F
light
into
Sta
ll Acci
dent
sL.
Sherr
y, Ge
orge M
ason
Univ
ersity
, Fa
irfax,
VA
1630
hrs
AIAA-2
015-2
703
Adap
tive a
nd In
tellig
ent p
ower
co
ntro
l allo
catio
n an
d sch
eduli
ng
for a
Mor
e Elec
tric A
ircra
ftS.
Laza
rus, E
aton C
orpora
tion,
Pune
, Ind
ia; S
. Fris
chem
eier, M
. Holl
and,
J. Sk
inner,
A. S
mith,
Eaton
Corpo
ration
, Ja
ckso
n, MS
Tues
day,
23 Ju
ne 2
015
118-
AFM-
7Fli
ght T
est,
Syste
m Id
entifi
catio
n, an
d Par
amete
r Esti
matio
nPlu
m Bl
osso
m A
Chair
ed by
: J. G
RAUE
R, NA
SA La
ngley
Rese
arch C
enter
and J
. BRA
NDON
, NAS
A-Lan
gley R
esea
rch Ce
nter
1400
hrs
AIAA-2
015-2
704
A Ne
w Fo
rmula
tion
of th
e Filte
r-Er
ror M
ethod
for A
erod
ynam
ic Pa
rame
ter Es
timat
ion in
Turb
ulenc
eJ.
Grau
er, E.
More
lli, N
ASA L
angle
y Re
searc
h Cen
ter, H
ampto
n, VA
1430
hrs
AIAA-2
015-2
705
Unste
ady a
nd P
ost-S
tall M
odel
Iden
tifica
tion
Using
Dyn
amic
Stall
Mane
uver
sJ.
Dias,
Braz
ilian A
ir Forc
e, Sã
o Jos
é dos
Ca
mpos
, Braz
il
1500
hrs
AIAA-2
015-2
706
Mode
ling a
nd Si
mulat
ion of
a Qu
adro
tor u
sing C
urve
Fitti
ng
Meth
odD.
Kaya
, A. K
utay,
Midd
le Ea
st Te
chnic
al Un
iversi
ty, An
kara,
Turke
y
1530
hrs
AIAA-2
015-2
707
Nonli
near
Aero
dyna
mic M
odeli
ng
from
Fligh
t Data
at H
igh An
gles o
f Att
ack U
sing N
eura
l-Gau
ss-Ne
wton
Me
thod
R. Ku
mar, P
EC Un
iversit
y of T
echno
logy,
Chan
digarh
, India
; A. G
hosh,
India
n Inst
itute
of Tec
hnolo
gy Ka
npur,
Kanp
ur, In
dia
Tues
day,
23 Ju
ne 2
015
119-
AFM-
8La
unch
Vehic
les, M
issile
s, an
d Pro
jectile
Fligh
t Mec
hanic
sPlu
m Bl
osso
m B
Chair
ed by
: T. L
AVIN
, San
dia N
ation
al La
borat
ories
and F
. FRE
SCON
I, US
Army
Rese
arch L
ab14
00 hr
sAIA
A-201
5-270
8De
liver
y of M
odula
r Leth
ality
via a
Pa
rent
-Chil
d Con
cept
F. Fre
sconi,
M. F
ermen
-Coke
r, Arm
y Re
searc
h Lab
orator
y, Ab
erdee
n Prov
ing
Grou
nd, M
D
1430
hrs
AIAA-2
015-2
709
An A
dapt
ive Pa
rame
ter Co
oper
ative
Gu
idanc
e Law
for M
ultipl
e fligh
t ve
hicles
Z. En
jiao,
T. Ch
ao, S
. Wan
g, M.
Yang
, Ha
rbin I
nstitu
te of
Tech
nolog
y, Ha
rbin,
China
1500
hrs
AIAA-2
015-2
710
Fligh
t Dyn
amics
Num
erica
l Co
mputa
tion o
f a So
undin
g Roc
ket
Includ
ing El
astic
Defo
rmati
on M
odel
E. Oli
veira
, Aero
nauti
cs an
d Spa
ce Ins
titute
(IAE),
São J
osé do
s Cam
pos,
Brazil;
P.
Gasba
rri, Un
iversit
y of R
ome “
La Sa
pienz
a”,
Rome
, Italy
; I. M
ilagre
da Fo
nseca,
Tec
hnolo
gical
Institu
te of
Aeron
autics
(ITA)
, Sã
o José
dos C
ampo
s, Bra
zil
1530
hrs
AIAA-2
015-2
711
Aero
ther
moela
stic R
educ
ed-O
rder
Mo
del o
f a H
yper
sonic
Vehic
leR.
Klock
, C. C
esnik
, Univ
ersity
of M
ichiga
n, An
n Arbo
r, Ann
Arbo
r, MI
1600
hrs
AIAA-2
015-2
712
Demo
nstra
tion
of La
unch
Vehic
le Slo
sh In
stabil
ity on
a Po
le-Ca
rt Pla
tform
J. Pe
i, P. R
othha
ar, N
ASA L
angle
y Res
earch
Ce
nter, H
ampto
n, VA
71
Tues
day,
23 Ju
ne 2
015
120-
AMT-7
/GT-7
Desig
n of
Expe
rimen
tOb
elisk
BCh
aired
by: G
. GAR
RARD
, Aero
spac
e Tes
ting A
llianc
e (AT
A) an
d D. Y
ODER
1400
hrs
AIAA-2
015-2
713
Case
Stud
ies fo
r the
Stat
istica
l De
sign
of Ex
perim
ents
Appli
ed to
Po
were
d Rot
or W
ind Tu
nnel
Tests
A. Ov
ermey
er, P.
Mart
in, P.
Tann
er, S
. Co
mmo,
NASA
Lang
ley Re
searc
h Cen
ter,
Hamp
ton, V
A
1430
hrs
Oral
Prese
ntatio
nCo
mpar
ison
betw
een
DOE a
nd
Tradit
ional
1-Fa
ctor a
t a Ti
me
Calib
ratio
n of
a Tra
nson
ic Wi
nd
Tunn
elG.
Garr
ard, M
. Mills
, Arno
ld En
ginee
ring
Deve
lopme
nt Co
mplex
, Tull
ahom
a, TN
Tues
day,
23 Ju
ne 2
015
121-
AMT-8
/FD-
14/T
P-6/
GT-8
Molec
ular-B
ased
Opt
ical D
iagno
stics
for H
yper
sonic
Non
equil
ibrium
Flow
sTo
paz
Chair
ed by
: P. D
ANEH
Y, NA
SA La
ngley
Rese
arch C
enter
and M
. WIN
TER,
Unive
rsity
of Ke
ntuck
y14
00 hr
sOr
al Pre
senta
tion
Intro
ducti
on an
d App
licat
ion
Cons
idera
tions
for O
ptica
l Di
agno
stics
in Hy
perso
nic
None
quilib
rium
Flows
P. Da
nehy
, NAS
A Lan
gley R
esea
rch Ce
nter,
Hamp
ton, V
A
1430
hrs
Oral
Prese
ntatio
nIn
trodu
ction
to Em
ission
Sp
ectro
scopy
for H
yper
sonic
No
nequ
ilibriu
m Flo
wsM.
Wint
er, U
nivers
ity of
Kentu
cky,
Lexin
gton,
Lexin
gton,
KY
1500
hrs
Oral
Prese
ntatio
nIn
trodu
ction
to A
bsor
ption
Sp
ectro
scopy
for H
yper
sonic
No
nequ
ilibriu
m Flo
wsS.
O’B
yrne,
Unive
rsity
of Ne
w So
uth
Wales
, Can
berra
, Aus
tralia
1530
hrs
Oral
Prese
ntatio
nIn
trodu
ction
to M
olecu
lar Ta
gging
Ve
locim
etry f
or H
yper
sonic
No
nequ
ilibriu
m Flo
wsB.
Bath
el, N
ASA L
angle
y Res
earch
Cente
r, Ha
mpton
, VA
1600
hrs
Oral
Prese
ntatio
nIn
trodu
ction
to La
ser I
nduc
ed
Fluor
esce
nce S
pectr
osco
py fo
r Hy
perso
nic N
oneq
uilibr
ium Fl
ows
C. Jo
hans
en, U
nivers
ity of
Calga
ry,
Calga
ry, Ca
nada
1630
hrs
Oral
Prese
ntatio
nIn
trodu
ction
to R
aman
Ray
leigh
Sp
ectro
scopy
for H
yper
sonic
No
nequ
ilibriu
m Flo
wsP.
Dane
hy, N
ASA L
angle
y Res
earch
Cente
r, Ha
mpton
, VA
1700
hrs
Oral
Prese
ntatio
nIn
trodu
ction
to CA
RS Sp
ectro
scopy
fo
r Hyp
erso
nic N
oneq
uilibr
ium
Flows
A. Cu
tler, G
eorge
Was
hingto
n Univ
ersity
, Wa
shing
ton, D
C
Tues
day,
23 Ju
ne 2
015
122-
APA-
13Ap
plied
CFD
& Nu
meric
al Co
rrelat
ions w
ith Ex
perim
enta
l Dat
a II
Stemm
ons B
Chair
ed by
: N. H
ARIH
ARAN
, CRE
ATE-A
V an
d C. S
HENG
, Univ
ersity
of To
ledo
1400
hrs
AIAA-2
015-2
714
CFD
Analy
sis of
Coun
ter-R
otat
ing
Open
Rot
ors U
sing a
Rot
ating
Ac
tuat
or D
isk M
odel
M. M
alick
, R. A
garw
al, W
ashin
gton
Unive
rsity
in St
. Lou
is, S
t. Lo
uis, M
O
1430
hrs
AIAA-2
015-2
715
Nume
rical
Simula
tion
of
Comp
ressi
ble Fl
ow in
a Di
ffusin
g S-
duct
with
and w
ithou
t Vor
tex
Gene
rato
rsS.
Kama
li, B.
Reza
Ahrab
i, R. W
ebste
r, K.
Sree
nivas
, Univ
ersity
of Te
nnes
see,
Chatt
anoo
ga, C
hatta
noog
a, TN
1500
hrs
AIAA-2
015-2
716
Massi
vely
separ
ated t
urbu
lent fl
ow
simula
tion a
roun
d non
-rotat
ing
MEXI
CO bl
ade b
y mea
ns of
RANS
and
DDES
appr
oach
es in
Open
FOAM
Y. Zh
ang,
A. va
n Zuijl
en, G
. van
Busse
l, De
lft Un
iversit
y of T
echno
logy,
Delft,
The
Nethe
rland
s
1530
hrs
AIAA-2
015-2
717
Wind
Tunn
el Wa
ll Int
erfe
renc
e Ef
fects
on an
Osci
llatin
g Aer
ofoil
in
the S
tall R
egim
eJ.
Chen
g, M.
Lowe
nberg
, Univ
ersity
of
Brist
ol, B
ristol
, Unit
ed Ki
ngdo
m; X
. Wan
g, J.
Yu, N
anjin
g Univ
ersity
of S
cienc
e and
Te
chno
logy,
Nanji
ng, C
hina
Tues
day,
23 Ju
ne 2
015
123-
APA-
14Sp
ecial
Sessi
on: H
istor
ically
Sign
ifica
nt/I
nflue
ntial
Pap
ers i
n Ap
plied
Aer
odyn
amics
Carp
enter
Ball
room
Chair
ed by
: B. M
CGRA
TH, J
HU/A
pplie
d Phy
sics L
abora
tory a
nd J.
PINI
ER, N
ASA L
angle
y Res
earch
Cente
r14
00 hr
sOr
al Pre
senta
tion
Thou
ghts
on w
orkin
g with
AMO
Smith
(Inv
ited)
R. Lie
beck
, The
Boe
ing Co
mpan
y, Hu
nting
ton B
each
, CA
1500
hrs
Oral
Prese
ntatio
nTh
e Spa
lart-A
llmar
as Tu
rbule
nce M
odel
Pape
r of 1
992
(Invit
ed)
P. Sp
alart,
The B
oeing
Comp
any,
Seatt
le, W
A; S.
Allm
aras,
Massa
chus
etts I
nstitu
te of
Tech
nolog
y, Ca
mbrid
ge, M
A
1600
hrs
AIAA-2
015-2
718
Origi
ns an
d Fur
ther
Dev
elopm
ent o
f the
Jame
son-
Schm
idt-Tu
rkel
Sche
me (I
nvite
d)A.
Jame
son,
Stan
ford U
nivers
ity, S
tanfor
d, CA
72
Tues
day,
23 Ju
ne 2
015
124-
APA-
15Sp
ecial
Sessi
on: A
erod
ynam
ic-Str
uctu
ral M
odeli
ng, O
ptim
izatio
n, an
d Tes
t Tec
hniqu
es fo
r Flex
ible W
ing Te
chno
logy I
ISte
mmon
s ACh
aired
by: W
. SILV
A, NA
SA-La
ngley
Rese
arch C
enter
and B
. STA
NFOR
D, N
ASA L
angle
y Res
earch
Cente
r14
00 hr
sAIA
A-201
5-271
9On
going
Fixe
d Wing
Res
earch
wi
thin
the N
ASA
Lang
ley
Aero
elasti
city B
ranc
hR.
Barte
ls, P.
Chwa
lowsk
i, C. F
unk,
J. He
eg, J
. Hur,
M. S
anetr
ik, N
ASA L
angle
y Re
searc
h Cen
ter, H
ampto
n, VA
; et a
l.
1430
hrs
AIAA-2
015-2
720
Analy
sis of
Limi
t Cyc
le Os
cillat
ion
Data
from
the A
eroe
lastic
Test
of th
e SUG
AR Tr
uss-B
race
d Wing
Mo
del
R. Ba
rtels,
R. S
cott,
NAS
A Lan
gley
Rese
arch C
enter
, Ham
pton,
VA
1500
hrs
AIAA-2
015-2
721
Comp
utat
ional
Aero
elasti
c Ana
lyses
of
a Lo
w-Bo
om Su
perso
nic
Confi
gura
tion
W. Si
lva, M
. San
etrik,
P. Ch
walow
ski, N
ASA
Lang
ley Re
search
Cente
r, Ham
pton,
VA
1530
hrs
AIAA-2
015-2
722
Unste
ady A
eros
ervo
elasti
c Mo
delin
g of F
lexibl
e Wing
Gen
eric
Trans
port
Aircr
aft w
ith Va
riable
Ca
mber
Cont
inuou
s Tra
iling E
dge
Flap
E. Ta
l, Delf
t Univ
ersity
of Te
chno
logy,
Delft,
Th
e Neth
erlan
ds; N
. Ngu
yen,
NASA
Ames
Re
searc
h Cen
ter, M
offett
Field
, CA
1600
hrs
AIAA-2
015-2
723
Optim
izatio
n fo
r Loa
d Alle
viatio
n of
Trus
s-Bra
ced W
ing A
ircra
ft Wi
th Va
riable
Camb
er Co
ntinu
ous
Trailin
g Edg
e Flap
S. Le
bofsk
y, E.
Ting,
K. Tri
nh, S
tinge
r Gh
affari
an Te
chno
logies
, Inc
., Mo
untai
n Vie
w, CA
; N. N
guye
n, NA
SA Am
es
Rese
arch C
enter
, Moff
ett Fi
eld, C
A
1630
hrs
AIAA-2
015-2
724
Meas
urem
ent a
nd M
odeli
ng of
Ae
roela
stic R
espo
nse u
nder
Gus
tY.
Babb
ar, V.
Sury
akum
ar, T.
Strg
anac
, Te
xas A
&M U
nivers
ity, C
olleg
e Stat
ion, T
X;
A. Ma
ngala
m, Ta
o of S
ystem
s Inte
gratio
n, Inc
., Ha
mpton
, VA
Tues
day,
23 Ju
ne 2
015
125-
APA-
16Flo
w Co
ntro
l App
licat
ions &
Dem
onstr
ation
s (Ac
tive &
Pas
sive)
IISte
mmon
s CCh
aired
by: M
. OL,
US Ai
r Forc
e Res
each
Labo
ratory
and G
. ZHA
, Univ
ersity
of M
iami
1400
hrs
AIAA-2
015-2
725
Simula
tion
and S
urro
gate-
Base
d De
sign
of R
ecta
ngula
r Vor
tex
Gene
rato
rs fo
r Tiltr
otor
Airc
raft
Wing
sR.
Beva
n, D.
Poole
, C. A
llen,
T. Re
ndall
, Un
iversi
ty of
Brist
ol, B
ristol
, Unit
ed
Kingd
om
1430
hrs
AIAA-2
015-2
726
Multip
oint D
esign
of Vo
rtex
Gene
rato
rs on
a Sw
ept I
nfinit
e-Wi
ng u
nder
Cruis
e and
Critic
al Co
nditio
nN.
Nam
ura, K
. Shim
oyam
a, S.
Oba
yash
i, To
hoku
Univ
ersity
, Sen
dai, J
apan
1500
hrs
AIAA-2
015-2
727
Flow
Cont
rol in
a Ma
ch 4
.0 In
let
by Sl
otted
Wed
ge-sh
aped
Vorte
x Ge
nera
tors
D. Va
rma,
S. S
aurav
, S. G
hosh
, Ind
ian
Institu
te of
Tech
nolog
y Mad
ras, C
henn
ai,
India
1530
hrs
AIAA-2
015-2
728
Wind
Tunn
el Ex
perim
ents
with
Activ
e Flo
w Co
ntrol
for an
Oute
r Wing
Mod
elV.
Cioba
ca, J.
Wild,
Germ
an Ae
rospa
ce Ce
nter
(DLR
), Bra
unsch
weig,
Germ
any;
M. Ba
uer, T
. Gru
nd, T
echnic
al Un
iversit
y of B
erlin,
Berlin
, Ge
rman
y; C.
Hueh
ne, P.
Scho
lz, Te
chnica
l Un
iversit
y of B
raunsc
hweig
, Brau
nschw
eig,
Germ
any;
et al.
1600
hrs
AIAA-2
015-2
729
Passi
ve Fl
ow Co
ntro
l App
lied t
o a
NACA
2301
2 Ai
rfoil I
n A
Subs
onic
Flow
N. Fi
ndan
is, U
nivers
ity of
New
Sou
th Wa
les, S
ydne
y, Au
strali
a
1630
hrs
AIAA-2
015-2
730
Comp
utat
ions o
f Acti
ve O
pen-
Loop
Flo
w Co
ntro
l on
a Flut
tering
Wing
J. Se
idel, C
. Fag
ley, T
. McLa
ughli
n, U.
S.
Air Fo
rce Ac
adem
y, Co
lorad
o Spri
ngs,
CO
Tues
day,
23 Ju
ne 2
015
126-
ATIO
-12
ATM
II - A
ir Tra
ffic A
nalys
isMi
lanCh
aired
by: A
. RAO
, Purd
ue U
nivers
ity14
00 hr
sAIA
A-201
5-273
1A
Wave
let A
nalys
is Ap
proa
ch fo
r Ca
tegor
izing
Air
Traffi
c Beh
avior
M. D
rew, U
nivers
ity of
Califo
rnia,
Santa
Cru
z, Mo
ffett
Field,
CA; K
. She
th, N
ASA
Ames
Rese
arch C
enter
, Moff
ett Fi
eld, C
A
1430
hrs
AIAA-2
015-2
732
Appli
catio
n of
Dat
a Mini
ng in
Air
Traffi
c For
ecas
ting
J. Bu
sque
ts, Ci
ty Un
iversi
ty Lo
ndon
, Lo
ndon
, Unit
ed Ki
ngdo
m; A.
Evan
s, Un
iversi
ty Co
llege
Lond
on, L
ondo
n, Un
ited K
ingdo
m; E.
Alon
so, C
ity U
nivers
ity
Lond
on, L
ondo
n, Un
ited K
ingdo
m
1500
hrs
AIAA-2
015-2
733
Iden
tifica
tion
of A
ircra
ft Co
nflict
Re
solut
ionTy
pes f
rom
Reco
rded
Fli
ght D
ata
S. S
hin, K
. Kim
, I. H
wang
, Purd
ue
Unive
rsity,
Wes
t Lafa
yette
, IN
Tues
day,
23 Ju
ne 2
015
127-
ATIO
-13
Trans
form
ation
al Fli
ght -
Adv
ance
d Con
cept
sMe
tropo
litan
Ballr
oom
Chair
ed by
: N. B
ORER
, NAS
A Lan
gley R
esea
rch Ce
nter
1400
hrs
Oral
Prese
ntatio
nNA
SA G
L-10
Tilt-W
ing Ti
lt-Ta
il Co
ncep
tW.
Fred
erick
s, NA
SA La
ngley
Rese
arch
Cente
r, Ham
pton,
VA
1430
hrs
Oral
Prese
ntatio
nLE
APTe
ch D
istrib
uted
Elec
tric
Prop
ulsion
Integ
ratio
n Co
ncep
tM.
Moo
re, N
ASA L
angle
y Res
earch
Cente
r, Ha
mpton
, VA
1500
hrs
Oral
Prese
ntatio
nCo
mpar
ison o
f Com
putat
ional
Aero
dyna
mics
Tools
for P
redict
ing
Low-
Spee
d Perf
orma
nce o
f a
Distr
ibuted
Prop
eller
Conc
ept
M. Pa
tterso
n, N.
Borer
, NAS
A Lan
gley
Resea
rch Ce
nter, H
ampto
n, VA
; B. G
erman
, Ge
orgia
Institu
te of
Techn
ology,
Atlan
ta, GA
1530
hrs
Oral
Prese
ntatio
nTh
e Sam
son
Switc
hblad
e Mult
i-Mo
de A
ircra
ft Co
ncep
tS.
Bou
sfield
, Sam
son A
ircraf
t, Au
burn,
CA
1600
hrs
Oral
Prese
ntatio
nHo
verle
ss VT
OL H
yper
Comm
uter
Mi
ssion
Conc
ept
M. M
oore,
NAS
A Lan
gley R
esea
rch Ce
nter,
Hamp
ton, V
A
1630
hrs
AIAA-2
015-2
734
Pred
icting
the A
ero L
oads
Beh
ind a
Prop
eller
in th
e Pre
senc
e of a
Wing
Us
ing Fl
ightst
ream
V. Ah
uja, R
. Hart
field,
Fligh
tstrea
m,
Aubu
rn, AL
1700
hrs
AIAA-2
015-2
735
Cent
rifug
ally S
tiffe
ned R
otor
: A
Comp
lete D
eriva
tion
of th
e Plan
t Mo
del w
ith N
onlin
ear D
ynam
icsJ.
Selfri
dge,
G. Ta
o, Un
iversi
ty of
Virgin
ia,
Charl
ottes
ville,
Charl
ottes
ville,
VA
73
Tues
day,
23 Ju
ne 2
015
128-
ATIO
-14
Prod
uct D
esign
and S
uppo
rtMa
nche
ster
Chair
ed by
: A. C
HAPU
T, Un
iversi
ty of
Texa
s at A
ustin
1400
hrs
AIAA-2
015-2
736
Value
Driv
en Co
ncep
tual
Desig
n of
Un
mann
ed A
ir Sy
stem
for D
efen
se
Appli
catio
nsE.
Papa
georg
io, M
. Eres
, J. S
canla
n, Un
iversi
ty of
South
ampto
n, So
utham
pton,
Unite
d King
dom
1430
hrs
AIAA-2
015-2
737
Mont
e Car
lo ba
sed R
obus
t MDO
ap
plied
to A
ircra
ft Co
ncep
tual
Desig
n: a
techn
ical-fi
nanc
ial
coup
ling o
ptim
izatio
n str
ateg
yD.
Bian
chi, T
. Orra
, Emb
raer, S
ão Jo
sé do
s Ca
mpos
, Braz
il; P.
Pagli
one,
Tech
nolog
ical
Institu
te of
Aeron
autic
s (ITA
), Sã
o Jos
é do
s Cam
pos,
Braz
il
1500
hrs
AIAA-2
015-2
738
Deve
lopme
nt an
d App
licat
ion of
a Pa
rame
tric D
esign
Tool
for D
esign
Ite
ratio
ns of
Larg
e Tur
bopr
op
Aircr
aft
M. Kü
gler, N
. Ran
dt, Te
chnic
al Un
iversi
ty of
Munic
h, Mu
nich,
Germ
any
1530
hrs
AIAA-2
015-2
739
3D P
rinted
Par
ts fo
r Quic
k Tu
rnar
ound
Airc
raft
Proje
cts an
d Le
gacy
Issu
esU.
Rehm
anjan
, Qan
tas Ai
rway
s, Ltd
., Sy
dney
, Aus
tralia
1600
hrs
AIAA-2
015-2
740
UGV a
nd U
AV Co
oper
ation
for
Cons
tructi
ng P
roba
bilist
ic Th
reat
Ex
posu
re M
ap (P
TEM)
O. D
askir
an, H
. Sev
il, A.
Doga
n, B.
Huff
, Un
iversi
ty of
Texa
s, Arl
ington
, Arlin
gton,
TX 16
30 hr
sAIA
A-201
5-274
1To
ward
Effic
ient M
odel-
Base
d De
velop
ment
of A
eros
pace
Ap
plica
tions
I. Am
unds
on, L
. Ship
ton, A
. Liu,
M.
Nowa
k, Ea
ton Co
rporat
ion, C
levela
nd, O
H
1700
hrs
AIAA-2
015-2
742
Relia
bility
Ana
lysis
of th
e In
tegra
ted M
odula
r Avio
nics
Syste
m Us
ing A
ADL a
nd G
SPN
P. Wa
ng, F.
Yan,
R. Liu
, C. Z
hao,
Z. Ma
, Civil
Av
iation
Unive
rsity o
f Chin
a, Tia
njin, C
hina
Tues
day,
23 Ju
ne 2
015
129-
CASE
-5
1400
- 17
30 h
rsCA
SE Se
ssion
I &
IISte
uben
1400
-1530
hrs
Conc
ept D
evelo
pmen
t of C
omple
x Sys
tems
This
pane
l add
resse
s the
phas
e of d
evelo
pmen
t tha
t inclu
des a
ctivit
ies fr
om th
e beg
inning
of de
cision
activ
ities f
or bu
ilding
new
syste
ms to
the t
ransit
ion to
the p
roduc
t des
ign at
mile
stone
“B” (
DoD)
or th
e end
of Ph
ase B
for N
ASA.
Sessi
on Ch
airs:
Stev
en D
’Urso
, Prog
ram Co
ordina
tor an
d Lec
turer,
Aeros
pace
Sys
tems E
ngine
ering
, Univ
ersity
of Ill
inois
at Ur
bana
-Cham
paign
and M
at Fre
nch,
Electr
ical S
ystem
s Eng
ineer,
Rolls-
Royc
e Corp
oratio
n
Pan
elists
:Ri
ck M
ange
F-35
PNR P
rogram
Man
ager
Lock
heed
Mart
in Ae
ronau
tics
Robe
rt (R
ob) S
imon
sT e
chnic
al Fe
llow
The B
oeing
Comp
any
Jaso
n Me
rret
Tech
nical
Spec
ialist
, Gulf
strea
m Ae
rospa
ce Pe
rform
ance
Engin
eerin
gGu
lfstre
am Ae
rospa
ce Co
rporat
ion
1545
-1730
hrs
Produ
ct De
sign f
or Co
mplex
Sys
tems A
cross
the S
upply
Chain
This
sessi
on w
ill foc
us on
the c
halle
nges
and e
nabli
ng te
chno
logies
for p
roduc
t des
ign ac
ross a
supp
ly ch
ain. I
n part
icular
, the
sessi
on w
ill ad
dress
the la
yered
chain
cons
isting
of O
EM/a
irfram
er, Ti
er 1,
Tier
2, an
d the
appro
ache
s for
desig
ning c
omple
x sys
tems t
hat h
andle
the
integ
ration
aspe
cts. M
ethod
s and
mod
el-ba
sed t
ool a
pproa
ches
will
be di
scusse
d in t
erms o
f exis
ting c
apab
ilities
, gap
s, an
d futu
re tre
nds.
Sessi
on Ch
airs:
Eelco
Sch
olte,
Mana
ger, A
dvan
ced M
ethod
s - El
ectric
Sys
tems,
UTC A
erosp
ace S
ystem
s and
Carm
en S
choo
ley, M
anag
er, S
ystem
s Eng
ineeri
ng an
d Inte
gratio
n, Gu
lfstre
am Ae
rospa
ce Co
rporat
ion
Pan
elists
:Fe
rnan
do D
ones
Tech
nical
Fello
wTh
e Boe
ing Co
mpan
y
Bern
ard D
ionCT
OAN
SYS
Bren
da N
uhfe
rPro
gram
Mana
ger
UTC/
Pratt
& W
hitne
y
Tues
day,
23 Ju
ne 2
015
130-
CFD-
13Flu
x Re
cons
tructi
on M
ethod
sGr
and B
allro
om A
Chair
ed by
: Z. W
ANG,
Univ
ersity
of Ka
nsas
and B
. VER
MEIRE
, McG
ill Un
iversi
ty14
00 hr
sAIA
A-201
5-274
3On
the U
tility
of H
igh-O
rder
Me
thod
s for
Uns
tructu
red G
rids:
A Co
mpar
ison
Betw
een
PyFR
and
Indu
stry S
tand
ard T
ools
B. Ve
rmeir
e, F.
With
erden
, P. V
incen
t, Im
peria
l Coll
ege L
ondo
n, Lo
ndon
, Unit
ed
Kingd
om
1430
hrs
AIAA-2
015-2
744
De-A
liasin
g thr
ough
Ove
r-In
tegra
tion
Appli
ed to
the F
lux
Reco
nstru
ction
and D
iscon
tinuo
us
Galer
kin M
ethod
sS.
Spie
gel, H
. Huy
nh, J
. DeB
onis,
NAS
A Gle
nn Re
searc
h Cen
ter, C
levela
nd, O
H
1500
hrs
AIAA-2
015-2
745
Fully
-cons
erva
tive H
igh-o
rder
FR
Sche
me on
Mov
ing an
d Def
ormi
ng
Grids
Y. Ab
e, Un
iversi
ty of
Toky
o, Sa
gami
hara,
Ja
pan;
T. Ha
ga, T
. Non
omura
, K. F
ujii,
Japa
n Aero
spac
e Exp
lorati
on Ag
ency
(JA
XA),
Saga
miha
ra, Ja
pan
1530
hrs
AIAA-2
015-2
746
A WE
NO-ty
pe Li
miter
for 4
th
Orde
r Con
strain
ed D
eriva
tive F
lux
Reco
nstru
ction
Meth
odZ.
Sun,
F. Xia
o, To
kyo I
nstitu
te of
Tech
nolog
y, Yo
koha
ma, J
apan
74
Tues
day,
23 Ju
ne 2
015
131-
CFD-
14Ad
joint
s and
Erro
r Esti
matio
nGr
and B
allro
om B
Chair
ed by
: C. R
OY, V
irgini
a Tec
h and
C. O
LLIVIE
R GOO
CH, U
nivers
ity of
Briti
sh Co
lumbia
1400
hrs
AIAA-2
015-2
747
Accu
racy
of D
iscre
tizat
ion Er
ror
Estim
ation
by th
e Erro
r Tra
nspo
rt Eq
uatio
n on
Uns
tructu
red M
eshe
s -
Nonli
near
Syste
ms of
Equa
tions
G. Ya
n, C.
Olliv
ier G
ooch
, Univ
ersity
of
Britis
h Colu
mbia,
Vanc
ouve
r, Can
ada
1430
hrs
AIAA-2
015-2
748
Comp
ariso
n of T
runc
ation
Erro
r Est
imato
rs for
Defe
ct Co
rrecti
on
and O
utput
Error
Estim
ation
in th
e Un
struc
tured
Mesh
Finit
e Volu
me
Metho
dM.
Sharb
atdar,
C. O
llivier
Gooch
, Univ
ersity
of
British
Colum
bia, V
ancou
ver, C
anad
a
1500
hrs
AIAA-2
015-2
749
Stabil
isatio
n of
Disc
rete
Adjoi
nt
Solve
rs fo
r Inc
ompr
essib
le Flo
wY.
Wang
, S. A
kbarz
adeh
, J. M
uelle
r, Qu
een M
ary U
nivers
ity of
Lond
on, L
ondo
n, Un
ited K
ingdo
m
1530
hrs
AIAA-2
015-2
750
Fixed
point
discr
ete ad
joint
of
SIMPL
E-like
solve
rsS.
Akba
rzade
h, Y.
Wang
, J. M
uelle
r, Qu
een M
ary U
nivers
ity of
Lond
on, L
ondo
n, Un
ited K
ingdo
m
1600
hrs
AIAA-2
015-2
751
Conv
erge
nce A
cceler
ation
Usin
g Co
nver
genc
e Erro
r Esti
matio
nS.
Eyi, M
iddle
East
Tech
nical
Unive
rsity,
An
kara,
Turke
y
Tues
day,
23 Ju
ne 2
015
132-
CFD-
15Tim
e Int
egra
tion
Meth
ods
Cora
lCh
aired
by: X
. WAN
G, Ai
r Forc
e Res
earch
Labo
ratory
, Wrig
ht-Pa
tterso
n AFB
and J
. NOR
DSTR
OM, L
inköp
ing U
nivers
ity14
00 hr
sAIA
A-201
5-275
2Op
timal
Rung
e-Ku
tta Sc
heme
s for
Hi
gh-o
rder
Spat
ial an
d Tem
pora
l Di
screti
zatio
nsN.
Mun
dis, E
RC, I
nc.,
Edwa
rds AF
B, CA
; A.
Edoh
, Univ
ersity
of Ca
liforni
a, Lo
s Ang
eles,
Los A
ngele
s, CA
; V. S
anka
ran, A
ir Forc
e Re
searc
h Lab
orator
y, Ed
wards
AFB,
CA
1430
hrs
AIAA-2
015-2
753
Appli
catio
n of
Dua
l Tim
e Step
ping
to Fu
lly Im
plicit
Run
ge K
utta
Sc
heme
s for
Uns
teady
Flow
Ca
lculat
ions
A. Ja
meso
n, St
anfor
d Univ
ersity
, Stan
ford,
CA
1500
hrs
AIAA-2
015-2
754
Asse
ssmen
t of t
ime i
mplic
it dis
cretiz
ation
s for
the c
ompu
tatio
n of
turb
ulent
comp
ressi
ble fl
ows
P. Cin
nella
, Univ
ersità
del S
alento
, Le
cce, I
taly;
C. Ce
dric,
Paris
Insti
tute o
f Te
chno
logy,
Paris
, Fran
ce
1530
hrs
AIAA-2
015-2
755
A Ma
pped
Cheb
yshe
v Ps
eudo
spec
tral M
ethod
for
Unste
ady F
low A
nalys
isD.
Im, S
. Cho
i, J. M
cClur
e, J.
Choi,
F.
Skies
, Virg
inia P
olytec
hnic
Institu
te an
d St
ate U
nivers
ity, B
lacks
burg,
VA
1600
hrs
AIAA-2
015-2
756
Unste
ady S
olutio
ns of
Non
-Line
ar
Diffe
rent
ial Eq
uatio
ns U
sing W
alsh
Func
tion
Serie
sP.
Gnoff
o, NA
SA La
ngley
Rese
arch C
enter
, Ha
mpton
, VA
1630
hrs
AIAA-2
015-2
757
Inve
stiga
tion
of Ef
ficien
t High
-Or
der I
mplic
it Ru
nge-
Kutta
Me
thod
s Bas
ed on
Gen
erali
zed
Summ
ation
-by-
Parts
Ope
rato
rsP.
Boom
, D. Z
ingg,
Unive
rsity
of To
ronto,
To
ronto,
Cana
da
Tues
day,
23 Ju
ne 2
015
133-
CFD-
16RA
NS M
odeli
ngEm
erald
Chair
ed by
: P. H
ARTW
ICH, B
oeing
Rese
arch &
Tech
nolog
y and
J. CA
RLSO
N, Co
mputa
tiona
l Aero
scien
ces B
ranch
1400
hrs
AIAA-2
015-2
758
Node
-Cen
tered
Wall
Func
tion
Mode
ls fo
r the
Uns
tructu
red F
Low
Code
Fun3
DJ.
Carls
on, V
. Vats
a, J.
Whit
e, NA
SA
Lang
ley Re
searc
h Cen
ter, H
ampto
n, VA
1430
hrs
AIAA-2
015-2
759
Analy
sis of
a low
Rey
nolds
dif
fere
ntial
Rey
nolds
stre
ss mo
del
in ho
moge
neou
s she
ar fl
ow w
ith
resp
ect t
o num
erica
l sta
bility
C. Mo
rsbac
h, Ge
rman
Aeros
pace
Cente
r (D
LR),
Colog
ne, G
erman
y
1500
hrs
AIAA-2
015-2
760
Exten
sion o
f the
SU2 o
pen s
ource
CFD
code
to th
e sim
ulatio
n of t
urbu
lent
flows
of fu
ids m
odell
ed w
ith co
mplex
the
rmop
hysic
al law
sS.
Vitale
, Delf
t Univ
ersity
of Te
chnolo
gy, De
lft,
The N
etherl
ands;
G. Go
ri, Tec
hnica
l Univ
ersity
of
Milan
, Milan
, Italy
; M. P
ini, De
lft Un
iversit
y of
Techn
ology,
Delft,
The N
etherl
ands;
A.
Guard
one,
Techn
ical U
nivers
ity of
Milan
, Milan
, Ita
ly; T.
Econ
omon
, F. Pa
lacios
, Stan
ford
Unive
rsity,
Palo
Alto,
CA; e
t al.
1530
hrs
AIAA-2
015-2
761
Turb
ulent
Flow
Simu
lation
s on
Uns
tructu
red G
rids u
sing a
Re
ynold
s Stre
ss Mo
dels
Y. Mo
r-Yos
sef,
Israe
li CFD
Cente
r, Cae
sarea
Ind
ustria
l Park
, Isra
el
1600
hrs
AIAA-2
015-2
762
Rece
nt Im
prov
emen
t of a
Co
rrelat
ion-B
ased
Tran
sition
Tu
rbule
nce M
odel
for S
imula
ting
Thre
e-Di
mens
ional
Boun
dary
La
yers
J. Ch
oi, O
. Kwo
n, Ko
rea Ad
vanc
ed In
stitut
e of
Scien
ce an
d Tec
hnolo
gy, D
aejeo
n, So
uth Ko
rea
1630
hrs
AIAA-2
015-2
763
Prop
er or
thog
onal
deco
mpos
ition
closu
re m
odels
for B
urge
rs an
d Na
vier-S
toke
s Equ
ation
sH.
Imtia
z, I.
Akhta
r, M. S
aif U
llah K
halid
, Na
tiona
l Univ
ersity
of S
cienc
es an
d Te
chno
logy,
Rawa
lpind
i, Pak
istan
Tues
day,
23 Ju
ne 2
015
134-
CFD-
37
1400
- 16
00 h
rsCF
D Flo
w Vis
ualiz
ation
Show
case
Chan
tilly B
allro
om Fo
yer
The C
FD Fl
ow V
isuali
zatio
n Sho
wcas
e will
be he
ld in
the fo
yer a
rea ou
tside
the E
xpos
ition H
all. A
uthors
of pa
pers
conta
ining
CFD
visua
lizati
ons w
ill de
scribe
their
work
and t
he si
gnific
ance
of th
eir an
imati
on as
it pla
ys on
a lar
ge-sc
reen m
onito
r. Mult
iple v
isuali
zatio
ns w
ill be
sh
own d
uring
each
of th
e fou
r 30-m
inute
time s
lots d
uring
the e
vent.
At th
e con
clusio
n of t
he ev
ent,
award
s will
be pr
esen
ted fo
r, Mos
t Artis
tic Fl
ow V
isuali
zatio
n Anim
ation
, Mos
t Qua
ntitat
ively
Descr
iptive
Flow
Visu
aliza
tion A
nimati
on, M
ost C
ompre
hens
ive Fl
ow V
isuali
zatio
n An
imati
on. T
he vi
suali
zatio
ns of
the t
hree w
inners
will
be di
splay
ed on
a mo
nitor
in the
Expo
sition
Hall
durin
g the
rema
inder
of the
expo
sition
.
75
Tues
day,
23 Ju
ne 2
015
135-
F360
-4
1400
- 16
30 h
rsIn
terna
tiona
l UAS
Integ
ratio
n Fo
rum
Gran
d Ball
room
E
Mode
rator:
Rob H
ughe
s, No
rthrop
Grum
man,
Inc.
P
aneli
sts:
Cees
Bil
Asso
ciate
Profes
sor, S
choo
l of A
erosp
ace,
Mech
anica
l and
Man
ufactu
ring E
ngine
ering
RMIT
Unive
rsity
Chuc
k Jo
hnso
nVic
e Pres
ident
of Op
eratio
nsTh
e Pad
ina G
roup
Marty
Rog
ers
Unive
rsity
of Ala
ska-F
airba
nks
Marsh
all Ja
ckso
nPro
ject M
anag
er - A
viatio
n Safe
ty Au
dits
Offic
e of I
nspe
ctor G
enera
lU.
S. D
epart
ment
of Tra
nspo
rtatio
n
Rand
y Willi
sFA
A, Co
-Chair
of IC
AO RP
AS(R
emote
ly Pil
oted A
ircraf
t Sys
tems)
Dale
Rich
ards
Senio
r Res
earch
Fello
w, H
uman
Facto
rsFa
culty
of En
ginee
ring &
Comp
uting
Cove
ntry U
nivers
ity, U
nited
King
dom
Tues
day,
23 Ju
ne 2
015
136-
FD-1
5Un
stead
y Wing
Aer
odyn
amics
IIGo
veno
rs Le
cture
Hall
Chair
ed by
: K. T
AIRA,
Florid
a Stat
e Univ
ersity
and B
. JOL
LY, U
S Air
Force
1400
hrs
AIAA-2
015-2
764
Aero
mech
anics
of M
embr
ane W
ings
in Gr
ound
-Effe
ctR.
Bleisc
hwitz
, R. D
e Kat,
B.
Gana
pathi
subra
mani,
Univ
ersity
of
South
ampto
n, So
utham
pton,
Unite
d Kin
gdom
1430
hrs
AIAA-2
015-2
765
The I
nflue
nce o
f Stre
amlin
e Cu
rvat
ure o
n Lo
w As
pect
Ratio
Ro
tatin
g Wing
sC.
Kronin
ger, A
. Harr
ington
, M. M
unso
n, Arm
y Res
earch
Labo
ratory
, Abe
rdeen
Pro
ving G
round
, MD
1500
hrs
AIAA-2
015-2
766
Effe
ct of
Turb
ulenc
e Mod
eling
on
Hove
ring R
otor
Flow
sS.
Yoon
, N. C
hade
rjian,
T. Pu
lliam,
T.
Holst
, NAS
A Ame
s Res
earch
Cente
r, Mo
ffett
Field,
CA
1530
hrs
AIAA-2
015-2
767
A Data
-Driv
en M
odeli
ng Fr
amew
ork
for Pr
edict
ing Fo
rces a
nd Pr
essur
es on
a R
apidl
y Pitc
hing A
irfoil
S. Da
wson
, N. S
chiav
one,
C. Ro
wley,
Pri
nceton
Unive
rsity,
Prince
ton, N
J; D.
Wi
lliams
, Illino
is Inst
itute
of Tec
hnolo
gy,
Chica
go, IL
1600
hrs
AIAA-2
015-2
768
Nonli
near
Char
acter
izatio
n of F
low
over
Oscill
ating
Ellip
tic Ai
rfoils
M. Kh
alid, I.
Akhta
r, Nati
onal
Unive
rsity o
f Sc
iences
and T
echno
logy,
Islama
bad,
Pakis
tan;
H. Do
ng, U
nivers
ity of
Virgi
nia, C
harlo
ttesvi
lle,
Charl
ottesv
ille, V
A; N.
Ahsan
, Instit
ute of
Space
Tec
hnolo
gy, Is
lamab
ad, P
akista
n
1630
hrs
AIAA-2
015-2
769
Inter
mitte
ncy B
ehav
iour i
n th
e Flo
w Pa
st an
Osci
llatin
g Airf
oilS.
Bad
rinath
, S. S
arkar,
India
n Ins
titute
of Te
chno
logy M
adras
, Che
nnai,
India
1700
hrs
AIAA-2
015-2
770
Analy
sis of
Defl
ected
Vorte
x Str
eet
Prod
uced
by an
Osci
llatin
g Airf
oilS.
Bad
rinath
, S. S
arkar,
India
n Ins
titute
of Te
chno
logy M
adras
, Che
nnai,
India
Tues
day,
23 Ju
ne 2
015
137-
FD-1
6Bo
unda
ry La
yer T
rans
ition:
Cros
sflow
Sapp
hire
Chair
ed by
: M. B
ORG,
Air F
orce R
esea
rch La
borat
ory an
d T. J
ULIAN
O, U
nivers
ity of
Notr
e Dam
e14
00 hr
sAIA
A-201
5-277
1Di
rect
Nume
rical
Simula
tion
of Tr
ansit
ion du
e to T
rave
ling
Cros
sflow
Vorti
ces
F. Li,
M. C
houd
hari,
NASA
Lang
ley
Rese
arch C
enter
, Ham
pton,
VA; L
. Dua
n, Mi
ssouri
Univ
ersity
of S
cienc
e and
Te
chno
logy,
Rolla
, MO
1430
hrs
AIAA-2
015-2
772
EPIC:
NPS
E Ana
lysis
of H
yper
sonic
Cr
ossfl
ow In
stabil
ity on
Yawe
d Str
aight
Circu
lar Co
neN.
Oliv
iero,
T. Ko
cian,
A. Mo
yes,
H. Re
ed,
Texa
s A&M
Univ
ersity
, Coll
ege S
tation
, TX
1500
hrs
AIAA-2
015-2
773
Seco
ndar
y Ins
tabil
ity of
Stat
ionar
y Cr
ossfl
ow Vo
rtice
s on
an In
cline
d Co
ne at
Mac
h 6
C. Wa
rd, R.
Hen
derso
n, S.
Sch
neide
r, Pu
rdue U
nivers
ity, W
est L
afaye
tte, I
N
1530
hrs
AIAA-2
015-2
774
Expe
rimen
tal s
tudy
of cr
ossfl
ow
insta
bility
on a
Mach
6 ya
wed c
one
S. Cr
aig, W
. Sari
c, Te
xas A
&M U
nivers
ity,
Colle
ge S
tation
, TX
1600
hrs
AIAA-2
015-2
775
Comp
utat
ional
Inve
stiga
tion o
f Step
Ex
cresce
nce S
ensit
ivity
in a
Swep
t-Wi
ng B
ound
ary L
ayer
M. Tu
fts, H
. Ree
d, B.
Craw
ford,
G. D
unca
n, W.
Sari
c, Te
xas A
&M U
nivers
ity, C
olleg
e St
ation
, TX
1630
hrs
AIAA-2
015-2
776
The E
ffect
of Ba
ckwa
rd-fa
cing S
tep
Heigh
t on I
nstab
ility G
rowt
h and
Br
eakd
own i
n Swe
pt-Wi
ng Bo
unda
ry-
Laye
r Tra
nsitio
nJ.
Eppin
k, NA
SA La
ngley
Resea
rch Ce
nter,
Hamp
ton, V
A; R.
Wlez
ien, Io
wa St
ate
Unive
rsity,
Ames,
IA; R
. King
, M. C
houd
hari,
NASA
Lang
ley Re
search
Cente
r, Ham
pton,
VA
Tues
day,
23 Ju
ne 2
015
138-
FD-1
7Bo
unda
ry La
yer a
nd B
luff B
ody C
ontro
lSe
nato
rs Le
cture
Hall
Chair
ed by
: Z. Z
HANG
, Univ
ersity
of Te
nnes
see a
nd J.
LIN,
NAS
A-Lan
gley R
esea
rch Ce
nter
1400
hrs
AIAA-2
015-2
777
Cont
rol o
f Afte
rbod
y Vor
tices
by
Blow
ingR.
Jack
son,
Z. Wa
ng, I
. Gurs
ul, U
nivers
ity
of Ba
th, B
ath, U
nited
King
dom
1430
hrs
AIAA-2
015-2
778
Simpli
fied m
odel
for fl
ow-h
eatin
g ef
fect
on w
ave d
rag o
f blun
t bod
ies
and i
ts va
lidat
ionE.
Schü
lein,
Germ
an Ae
rospa
ce Ce
nter
(DLR
), Gö
ttinge
n, Ge
rman
y
1500
hrs
AIAA-2
015-2
779
The e
ffects
of M
ach a
nd Re
ynold
s nu
mber
on th
e flow
mixi
ng pr
opert
ies
of mi
cro-ra
mp vo
rtex g
enera
tors in
a su
perso
nic bo
unda
ry la
yer
R. Gie
pman
, A. S
rivast
ava,
F. Schr
ijer, B
. van
Ou
dheu
sden,
Delft
Unive
rsity o
f Tech
nolog
y, De
lft, Th
e Neth
erlan
ds
1530
hrs
AIAA-2
015-2
780
Expe
rimen
tal in
vesti
gatio
n of
bo
unda
ry la
yer t
rippin
g dev
ices
for s
hock
wav
e - bo
unda
ry la
yer
cont
rol
R. Gie
pman
, R. L
ouma
n, F.
Schri
jer, B
. va
n Oud
heus
den,
Delft
Unive
rsity
of Te
chno
logy,
Delft,
The N
etherl
ands
1600
hrs
AIAA-2
015-2
781
Cont
rol o
f Sho
ck W
ave B
ound
ary
Laye
r Int
erac
tion
using
Lase
r Puls
e En
ergy
Dep
ositio
nsA.
Iwak
awa,
T. Ta
mba,
P. So
n, T.
Shod
a, A.
Saso
h, Na
goya
Univ
ersity
, Nag
oya,
Japa
n
76
Tues
day,
23 Ju
ne 2
015
139-
FD-1
8Tu
rbule
nce M
odeli
ngEd
elweis
sCh
aired
by: C
. RUM
SEY,
NASA
-Lang
ley Re
searc
h Cen
ter an
d G. B
LAISD
ELL,
Purdu
e Univ
ersity
1400
hrs
AIAA-2
015-2
782
Stretc
hed-
Vorte
x ba
sed S
ubgr
id-sca
le Mo
delin
g of V
ariab
le-De
nsity
Flo
wsG.
Sidh
arth,
G. Ca
ndler
, Univ
ersity
of
Minn
esota
, Minn
eapo
lis, M
innea
polis,
MN
; P. D
imota
kis, C
alifor
nia In
stitut
e of
Tech
nolog
y, Pa
sade
na, C
A
1430
hrs
AIAA-2
015-2
783
DNS/
LES S
imula
tions
of Se
para
ted
Flows
at H
igh R
eyno
lds N
umbe
rsP.
Balak
umar,
NAS
A Lan
gley R
esea
rch
Cente
r, Ham
pton,
VA; G
. Park
, Stan
ford
Unive
rsity,
Palo
Alto,
CA
1500
hrs
AIAA-2
015-2
784
Baye
sian
Calib
ratio
n of
a RA
NS
Mode
l with
a Co
mplex
Res
pons
e Su
rface
- A
Case
Stud
y with
Jet-i
n-Cr
ossfl
ow Co
nfigu
ratio
nJ.
Ray,
S. Le
fantzi
, San
dia N
ation
al La
borat
ories
, Live
rmore
, CA;
S.
Aruna
jates
an, L
. DeC
hant,
San
dia N
ation
al La
borat
ories
, Albu
querq
ue, N
M
1530
hrs
AIAA-2
015-2
785
Exten
sion
of W
ray-
Agar
wal
Turb
ulenc
e Mod
el fo
r Flow
Ove
r Ro
ugh
Surfa
ces
T. W
ray, R
. Aga
rwal,
Was
hingto
n Un
iversi
ty in
St. L
ouis,
St.
Louis
, MO
1600
hrs
AIAA-2
015-2
786
An Im
prov
ed Ve
rsion
of O
ne-
Equa
tion
RAS T
urbu
lence
Mod
elM.
Rahm
an, A
alto U
nivers
ity, H
elsink
i, Fin
land;
R. Ag
arwal,
Was
hingto
n Un
iversi
ty in
St. L
ouis,
St.
Louis
, MO;
M.
Lamp
inen,
T. Sii
kone
n, Aa
lto U
nivers
ity,
Helsin
ki, Fi
nland
Tues
day,
23 Ju
ne 2
015
140-
ITAR-
2ITA
R - A
ircra
ft De
sign
and M
odeli
ng
Moro
ccoCh
aired
by: K
. CAS
PER
1400
hrs
AIAA-2
015-2
787
Deve
lopme
nt an
d Tes
ting o
f a So
lar
Powe
red A
ircra
ftJ.
Jaco
b, Ok
lahom
a Stat
e Univ
ersity
, St
illwate
r, OK;
J. Gr
imsle
y, S.
Atkin
s, De
sign I
ntellig
ence
, Inc
., No
rman
, OK
1430
hrs
AIAA-2
015-2
788
Airfi
eld Li
fting
Load
s a CF
D/Fu
ll Sc
ale R
otar
y Wing
Test
Study
F. Za
jaczk
owsk
i, J. T
arter,
T. B
agwe
ll, Ap
plied
Rese
arch L
abora
tory,
State
Co
llege
, PA
Tues
day,
23 Ju
ne 2
015
141-
MAO-
4Ap
plica
tions
IIMa
drid
Chair
ed by
: R. K
HIRE
, Unit
ed Te
chno
logies
Rese
arch C
enter
and E
. WIN
ER, I
owa S
tate U
nivers
ity14
00 hr
sAIA
A-201
5-278
9De
sign S
pace
Explo
ratio
n of W
ingbo
x Su
bstru
ctures
Confi
gura
tion U
sing
SPAN
DSET
C. Po
tter, G
eorgi
a Inst
itute
of Tec
hnolo
gy,
Atlan
ta, GA
; S. R
ussell,
Trium
ph Ae
rostru
ctures
, Da
llas, T
X; V.
Kim, Z
. Liu,
D. M
avris,
Georg
ia Ins
titute
of Tec
hnolo
gy, At
lanta,
GA
1430
hrs
AIAA-2
015-2
790
High
-Fide
lity A
eros
tructu
ral
Otim
izatio
n Co
nside
ring B
uffe
t On
set
G. Ke
nway
, J. M
artins
, Univ
ersity
of
Mich
igan,
Ann A
rbor, A
nn Ar
bor, M
I
1500
hrs
AIAA-2
015-2
791
Aero
elasti
c Tail
oring
Stud
y of
an N
+2 Lo
w-bo
om Su
perso
nic
Comm
ercia
l Tra
nspo
rt Ai
rcraf
tC.
Pak,
NASA
Arms
trong
Fligh
t Res
earch
Ce
nter, E
dward
s, CA
1530
hrs
AIAA-2
015-2
792
Optim
al Mi
ssion
Pat
h fo
r the
Un
inhab
ited L
oyal
Wing
man
C. Hu
mphre
ys, R
. Cob
b, D.
Jacq
ues,
J. Re
eger,
Air F
orce I
nstitu
te of
Tech
nolog
y, W
right-
Patte
rson A
FB, O
H
1600
hrs
AIAA-2
015-2
793
Multid
iscipl
inary
Ana
lysis
of a
Box-
Wing
Airc
raft
Desig
ned f
or a
Regio
nal-J
et Mi
ssion
S. An
drews
, R. P
erez,
Roya
l Milit
ary
Colle
ge of
Cana
da, K
ingsto
n, Ca
nada
Tues
day,
23 Ju
ne 2
015
142-
MST-6
Shad
ow M
ode A
ssessm
ent u
sing R
ealis
tic Te
chno
logies
for N
ation
al Ai
rspac
e Sys
tem (S
MART
NAS
) Tes
t Bed
Dev
elopm
ent (
Invit
ed)
Trave
rtine
Chair
ed by
: K. P
ALOP
O, N
ASA A
mes R
esea
rch Ce
nter a
nd G
. CHA
TTER
JI, N
ASA A
mes R
esea
rch Ce
nter
1400
hrs
AIAA-2
015-2
794
Shad
ow M
ode A
ssessm
ent u
sing
Reali
stic T
echno
logies
for t
he N
ation
al Air
spac
e Sys
tem (S
MART
NAS
) Tes
t Bed
Dev
elopm
ent (
Invite
d)K.
Palop
o, NA
SA Am
es Re
search
Cente
r, Mo
ffett F
ield, C
A; G.
Chatt
erji, U
nivers
ity of
Ca
liforni
a, Sa
nta Cr
uz, M
offett
Field
, CA;
M.
Gumi
nsky,
P. Glaa
b, NA
SA La
ngley
Resea
rch
Cente
r, Ham
pton,
VA
1430
hrs
AIAA-2
015-2
795
Desig
n Ch
allen
ges f
or a
Shad
ow
Mode
Asse
ssmen
t Too
l for
Air
Traffi
c Man
agem
ent (
Invit
ed)
R. Ho
ffman
, Metr
on Av
iation
, Inc
., Du
lles,
VA; J
. Kroz
el, In
nova
tion L
abora
tory,
Inc.,
Portla
nd, O
R; D.
Mille
r, J. S
mith,
Metr
on
Aviat
ion, I
nc.,
Dulle
s, VA
1500
hrs
AIAA-2
015-2
796
Platfo
rm A
s A Se
rvice
(PAA
S)
Arch
itectu
re fo
r NAS
A’s SM
ART N
AS
(Invit
ed)
P. Co
bb, M
. Blak
e, Cro
wn Co
nsult
ing, I
nc.,
Arling
ton, V
A
1530
hrs
AIAA-2
015-2
797
Arch
itectu
re D
evelo
pmen
t for
Sh
adow
Mod
e Asse
ssmen
ts of
Air
Traffi
c Man
agem
ent T
echn
ologie
s (In
vited
)P.
Kosti
uk, R
obus
t Ana
lytics
, Gam
brills,
MD
1600
hrs
AIAA-2
015-2
798
A Da
ta Ex
chan
ge an
d Tra
nsfo
rmat
ion Sy
stem
for S
MART
NA
S (In
vited
)P.
Cobb
, Crow
n Con
sultin
g, Inc
., Arl
ington
, VA
; M. G
arlan
d, Mo
saic
ATM,
Lees
burg,
VA
1630
hrs
AIAA-2
015-2
799
Para
llel S
imula
tion
of A
gent
-Bas
ed
Mode
l for
Air
Traffi
c Netw
ork
Y. Kim
, O. P
inon-F
ische
r, D. M
avris
, Ge
orgia
Institu
te of
Tech
nolog
y, Atl
anta,
GA
1700
hrs
AIAA-2
015-2
800
An In
tegra
ted Fr
amew
ork
for
Mode
ling A
ir Ca
rrier
Beh
avior
, Po
licy,
and I
mpac
ts in
the U
.S. A
ir Tra
nspo
rtatio
n Sy
stem
B. H
orio,
V. Ku
mar, V
. Stou
ffer, S
. Has
an,
A. De
Cicco
, LMI
, Tys
ons C
orner,
VA; J
. Sm
ith, N
ASA L
angle
y Res
earch
Cente
r, Ha
mpton
, VA;
et al.
77
Tues
day,
23 Ju
ne 2
015
143-
PDL-6
Plasm
a Diag
nosti
cs I
Miro
Chair
ed by
: C. D
UMITR
ACHE
, Colo
rado S
tate U
nivers
ity14
00 hr
sAIA
A-201
5-280
1Co
mpos
ition-
Inde
pend
ent
Temp
erat
ure a
nd P
ressu
re
Meas
urem
ents
using
Line
shap
e Sc
aling
Info
rmat
ion fr
om K
r PLIF
D. Ze
lenak
, F. K
idd, V
. Nara
yana
swam
y, No
rth Ca
rolina
Stat
e Univ
ersity
, Rale
igh,
NC
1430
hrs
AIAA-2
015-2
802
Comp
utat
ional
and E
xper
imen
tal
Lase
r Diff
eren
tial I
nter
fero
metry
fo
r Sup
erso
nic Tu
rbule
nt B
ound
ary-
Laye
r Flow
N. B
isek,
M. B
rown,
Air Fo
rce Re
searc
h La
borat
ory, W
right-
Patte
rson A
FB, O
H
1500
hrs
AIAA-2
015-2
803
Unde
rstan
ding t
he Im
pact
of
Buffe
r Gas
es on
the R
adar
REM
PI
Diag
nosti
cT.
Chng
, R. M
iles,
Princ
eton U
nivers
ity,
Princ
eton,
NJ
1530
hrs
AIAA-2
015-2
804
Wave
front
Mea
sure
ment
s of a
Su
perso
nic B
ound
ary L
ayer
Usin
g a
Lase
r-Ind
uced
Bre
akdo
wn Sp
ark
M. N
guye
n, M.
Renn
ie, S.
Gorde
yev,
E. Jum
per, U
nivers
ity of
Notr
e Dam
e, No
tre
Dame
, IN; A
. Cain
, Inno
vativ
e Tech
nolog
y Ap
plicati
ons C
ompa
ny, LL
C, Ch
esterfi
eld, M
O;
T. Ha
yden
, U.S.
Air F
orce A
cadem
y, Co
lorad
o Sp
rings,
CO
1600
hrs
AIAA-2
015-2
805
Lang
muir
Prob
e Diag
nosti
cs of
an
Atmo
sphe
ric-P
ressu
re M
icrop
lasma
L. Bla
ir, K.
Xu, U
nivers
ity of
Alab
ama,
Hunts
ville,
Hun
tsville
, AL
Tues
day,
23 Ju
ne 2
015
144-
PDL-7
Plasm
a Aer
odyn
amics
& Fl
ow Co
ntro
l III
Mone
t Ball
room
Chair
ed by
: T. M
OELLE
R, Un
iversi
ty of
Tenn
esse
e Spa
ce In
stitut
e14
00 hr
sAIA
A-201
5-280
6In
vesti
gatio
n of
Cath
odic-
Arc-J
et In
fluen
ce on
Cros
s Flow
usin
g Pa
rticle
Imag
e Velo
cimetr
yI.
Kronh
aus,
Tech
nion--
Israe
l Insti
tute o
f Te
chno
logy,
Haifa
, Isra
el
1430
hrs
AIAA-2
015-2
807
Dyna
mics
of Ch
arge
Tran
sfer i
n At
mosp
heric
Pre
ssure
Bar
rier
Disch
arge
at Si
ngle
and A
ltern
ative
Po
laritie
s of S
upply
ing Vo
ltage
S. Le
onov
, Univ
ersity
of N
otre D
ame,
Notre
Dam
e, IN
1500
hrs
AIAA-2
015-2
808
Effect
of N
ew El
ectro
n Imp
act
Ioniza
tion o
n the
Aero
dyna
mic
Heati
ng En
viron
ment
for Su
per-O
rbita
l Re
entry
Vehic
lesH.
Otsu,
Ryuk
oku U
nivers
ity, O
tsu, J
apan
; K.
Yama
da, T
. Abe
, Jap
an Ae
rospa
ce Ex
plorat
ion
Agen
cy (JA
XA),
Saga
miha
ra, Ja
pan
1530
hrs
AIAA-2
015-2
809
Nume
rical
Study
on P
erfo
rman
ce
Impr
ovem
ent M
echa
nism
of Tr
i-Ele
ctrod
e Plas
ma A
ctuat
orH.
Nish
ida, M
. Tam
ura, T
okyo
Univ
ersity
of
Agric
ulture
and T
echn
ology
, Kog
anei,
Ja
pan;
T. Ma
tsuno
, Tott
ori U
nivers
ity,
Totto
ri, Ja
pan
1600
hrs
AIAA-2
015-2
810
Effe
ct of
Volta
ge an
d Fre
quen
cy
on St
artin
g Rep
etitiv
e Nan
osec
ond
Pulse
d DBD
X. H
an, H
. Li, X
. Men
g, No
rthwe
stern
Polyt
echn
ical U
nivers
ity, X
i’an,
China
; F.
Liu, S
. Luo
, Univ
ersity
of Ca
liforni
a, Irv
ine,
Los A
ngele
s, CA
Tues
day,
23 Ju
ne 2
015
145-
TP-7
Heat
Tran
sfer I
IRo
setta
Chair
ed by
: E. S
HORT
, Ray
theon
Comp
any a
nd E.
KHAL
IL, Ca
iro U
nivers
ity14
00 hr
sAIA
A-201
5-281
1Re
spon
se of
poro
us fo
ams fi
lled
with
phas
e cha
nge m
ater
ial u
nder
tra
nsien
t hea
ting
G. Jac
kson,
K. Sm
ith, P.
Mcca
rthy,
T. Fis
her,
Purdu
e Univ
ersity,
West
Lafay
ette,
IN
1430
hrs
AIAA-2
015-2
812
Evalu
ation
of di
ffere
nt Tu
rbule
nce
Mode
ls fo
r ana
lysis
of Je
t Im
pinge
ment
in G
as Tu
rbine
Blad
esB.
Upa
lkar, M
. Rick
lick, E
mbry-
Riddle
Ae
ronau
tical
Unive
rsity,
Day
tona B
each
, FL
1500
hrs
AIAA-2
015-2
813
Benc
hmar
king o
f Com
puta
tiona
l Mo
dels
For A
diaba
tic Fi
lm-C
oolin
g Ef
fecti
vene
ss Fo
r Lar
ge Sp
acing
Co
mpou
nd A
ngle
Full C
over
age
Film
Cooli
ng A
rrays
S. M
artine
z, M.
Rick
lick, E
mbry-
Riddle
Ae
ronau
tical
Unive
rsity,
Day
tona B
each
, FL
1530
hrs
AIAA-2
015-2
814
Nume
rical
Analy
sis of
Film
Cooli
ng
Char
acter
istic
on a
Turb
ine N
on-
axisy
mmetr
ic Co
ntou
red E
ndwa
llQ.
Pan,
H. Ta
ng, J
. Bai,
Aviat
ion In
dustr
y Co
rporat
ion of
China
(AVIC
), Sh
angh
ai,
China
1600
hrs
AIAA-2
015-2
815
POD
Analy
sis of
the T
rans
ient
Flow
Field
at P
ulse E
ngine
Exha
ust
Regio
nW.
Cai, C
. Yan
g, B.
Qi, H
. Ma,
L. Yu
, X.
Chen
, Nan
jing U
nivers
ity of
Scie
nce a
nd
Tech
nolog
y, Na
njing
, Chin
a
1630
hrs
AIAA-2
015-2
816
Fluid
flow
and h
eat t
rans
fer i
n a
rota
ting t
wo-p
ass s
quar
e cha
nnel
with
smoo
th w
alls a
nd ax
ial
inwar
d/ou
twar
d flow
J. Ba
i, Q. P
an, A
viatio
n Ind
ustry
Corpo
ration
of
China
(AVIC
), Sh
angh
ai, Ch
ina
1700
hrs
AIAA-2
015-2
817
Nume
rical
and e
xper
imen
tal
analy
sis of
hea
t tra
nsfe
r of p
iccolo
tu
be je
t imp
ingem
ent o
n a c
onca
ve
surfa
ceY.
Bo, S
. Cha
ng, Y
. Zha
o, M.
Leng
, Be
ihang
Univ
ersity
, Beij
ing, C
hina
Tues
day,
23 Ju
ne 2
015
146-
NW-4
15
30 -
1600
hrs
Netw
orkin
g Cof
fee B
reak
Chan
tilly B
allro
om Ea
st
Tues
day,
23 Ju
ne 2
015
147-
LEC-
2 16
30 -
1730
hrs
Plasm
adyn
amics
and L
aser
s Awa
rd Le
cture
Gran
d Ball
room
D
From
Plasm
adyn
amics
and S
hock
Tube
s to A
ero-Op
tics a
nd La
ser Ra
dar: A
n Aero
spac
e Care
erPh
ilip E.
Cassa
dySe
nior T
echn
ical F
ellow
(Reti
red)
The B
oeing
Comp
any
78
Tues
day,
23 Ju
ne 2
015
148-
NW-5
17
30 -
1900
hrs
Rece
ption
in th
e Exp
ositio
n Ha
llCh
antill
y Ball
room
East
A tick
et is
requir
ed an
d inc
luded
in th
e con
feren
ce re
gistra
tion f
ee w
here
indica
ted.
Wedn
esda
y
Wedn
esda
y, 24
June
201
514
9-SB
-3
0730
- 08
00 h
rsSp
eake
rs’ B
riefin
gSe
ssion
Roo
ms
Wedn
esda
y, 24
June
201
515
0-PL
NRY-3
08
00 -
0900
hrs
Plena
ry K
eyno
teCh
antill
y Ball
room
Wes
t
NASA
and t
he Fu
ture o
f Aero
spac
eCh
arles
F. B
olden
Jr.
Admi
nistra
torNa
tiona
l Aero
nauti
cs an
d Spa
ce Ad
minis
tratio
n
Wedn
esda
y, 24
June
201
515
1-AA
-21
Turb
omac
hiner
y and
Core
Nois
eFle
ur-d
e-lis
BCh
aired
by: H
. ATA
SSI,
Unive
rsity
of No
tre D
ame
0900
hrs
AIAA-2
015-2
818
Entro
py N
oise G
ener
ation
and
Redu
ction
in a
Heat
ed N
ozzle
Flow
K. Kn
obloc
h, T.
Werne
r, F. B
ake,
Germ
an
Aeros
pace
Cente
r (DL
R), B
erlin,
Germ
any
0930
hrs
AIAA-2
015-2
819
Dyna
mic T
empe
ratu
re an
d Pre
ssure
Me
asur
emen
ts in
the C
ore o
f a
Prop
ulsion
Engin
eW.
Sch
uster
, Hon
eywe
ll Inte
rnatio
nal,
Inc.,
Phoe
nix, A
Z; L.
Hultg
ren, N
ASA G
lenn
Rese
arch C
enter
, Clev
eland
, OH
1000
hrs
AIAA-2
015-2
820
Broa
dban
d ind
irect
noise
ge
nera
tion
by ac
celer
ated
vorti
city
N. Ki
ngs,
L. En
ghard
t, F.
Bake
, Germ
an
Aeros
pace
Cente
r (DL
R), B
erlin,
Germ
any
1030
hrs
AIAA-2
015-2
821
Linea
r Ana
lysis
of En
gine C
ore
Noise
Usin
g a H
ybrid
Mod
eling
Ap
proa
chJ.
O’Br
ien, J
. Kim
, M. I
hme,
Stan
ford
Unive
rsity,
Stan
ford,
CA
1100
hrs
AIAA-2
015-2
822
Acou
stic C
ompa
rison
of D
iffer
ent
Turb
ine Ex
it Gu
ide Va
ne D
esign
s - P
art 1
: Des
ign P
hilos
ophy
and
Nume
rical
Pred
iction
sD.
Bros
zat,
M. H
öger,
MTU
Aero
Engin
es,
Munic
h, Ge
rman
y; A.
Marn,
T. S
elic,
F. Sc
hönle
itner,
F. H
eitme
ir, Gr
az U
nivers
ity
of Te
chno
logy,
Graz
, Aus
tria
1130
hrs
AIAA-2
015-2
823
Acou
stic C
ompa
rison
of D
iffer
ent
Turb
ine Ex
it Gu
ide Va
ne D
esign
s Pa
rt 2:
Expe
rimen
tal A
nalys
isA.
Marn,
T. S
elic,
F. Sc
hönle
itner,
S.
Zerob
in, G
raz U
nivers
ity of
Tech
nolog
y, Gr
az, A
ustria
; D. B
rosza
t, M.
Hög
er, M
TU
Aero
Engin
es, M
unich
, Germ
any;
et al.
1200
hrs
AIAA-2
015-2
824
Expe
rimen
tal S
tudy
on th
e Tu
rbom
achin
ery T
railin
g Edg
e Nois
e Re
ducti
on B
ased
on Li
near
Casca
de
Test
with
Pha
sed A
rray
W. Q
iao, L
. Wan
g, W.
Chen
, F. T
ong,
L. Ji,
Nort
hwes
tern P
olytec
hnica
l Univ
ersity
, Xi’
an, C
hina
Wedn
esda
y, 24
June
201
515
2-AA
-22
Gene
ral A
cous
tics I
IIn
vern
ess
Chair
ed by
: S. R
IZZI,
NASA
Lang
ley Re
searc
h Cen
ter09
00 hr
sAIA
A-201
5-282
5On
a mo
de-m
atchin
g tech
nique
for
soun
d gen
eratio
n and
tran
smiss
ion in
a l
inear
casca
de of
outle
t guid
e van
esS.
Boule
y, B.
Franço
is, M.
Roge
r, Écol
e Ce
ntrale
de Ly
on, E
cully,
France
; S. M
oreau
, Un
iversit
y of S
herbr
ooke
, She
rbroo
ke, C
anad
a
0930
hrs
AIAA-2
015-2
826
Noise
cont
rol b
y a ro
tatin
g rod
in a
rod-
airfo
il con
figur
ation
L. Sio
zos-R
ouso
ulis,
G. G
horba
niasl,
C.
Laco
r, Vrije
Univ
ersite
it Brus
sel, B
russe
ls,
Belgi
um
1000
hrs
AIAA-2
015-2
827
Acou
stic e
ffects
of a
rota
tiona
lly
oscil
lating
rod i
n a r
od-a
irfoil
co
nfigu
ratio
nL.
Siozo
s-Rou
souli
s, G.
Gho
rbania
sl, C.
La
cor, V
rije U
nivers
iteit B
russe
l, Brus
sels,
Be
lgium
1030
hrs
AIAA-2
015-2
828
Activ
e Con
trol o
f Fan
Tone
s by
mean
s of T
railin
g Edg
e Blow
ingL.
Engh
ardt,
P. Ka
usch
e, A.
Morea
u, Ge
rman
Aeros
pace
Cente
r (DL
R), B
erlin,
Ge
rman
y; T.
Carol
us, U
nivers
ity of
Sieg
en,
Siege
n, Ge
rman
y
1100
hrs
AIAA-2
015-2
829
Acou
stic R
eson
ance
Phe
nome
na
in a T
hree
-Dim
ensio
nal C
asca
de
Inter
actin
g with
Onc
oming
Un
stead
y Wak
esH.
Koda
ma, I
HI Co
rporat
ion, N
ishita
ma,
Japa
n; M.
Nam
ba, K
yusy
u Univ
ersity
, Fu
kuok
a, Ja
pan
1130
hrs
AIAA-2
015-2
830
Aero
foil g
eome
try ef
fects
on
turb
ulenc
e int
erac
tion
noise
C. Pa
ruchu
ri, J.
Gill, N
. Sub
raman
ian,
P. Jo
seph
, C. V
ande
rwel,
X. Z
hang
, Un
iversi
ty of
South
ampto
n, So
utham
pton,
Unite
d King
dom;
et al
.
1200
hrs
AIAA-2
015-2
831
Wall-
Moun
ted Fi
nite A
irfoil
Nois
e Pr
oduc
tion
and P
redic
tion
D. M
oreau
, C. D
oolan
, Univ
ersity
of
New
South
Wale
s, Sy
dney
, Aus
tralia
; W.
Alex
ande
r, T. M
eyers
, W. D
even
port,
Vir
ginia
Polyt
echn
ic Ins
titute
and S
tate
Unive
rsity,
Blac
ksbu
rg, VA
79
Wedn
esda
y, 24
June
201
515
3-AA
-23
Jet N
oise N
ear F
ield a
nd Je
t Nois
e Red
uctio
nLa
lique
Chair
ed by
: A. P
ILON,
Lock
heed
Mart
in Ae
ronau
tics
0900
hrs
AIAA-2
015-2
832
On Th
eore
tical
Broa
dban
d Sho
ck-
Asso
ciated
Nois
e Nea
r-Fiel
d Cro
ss-Sp
ectra
S. M
iller, N
ASA L
angle
y Res
earch
Cente
r, Ha
mpton
, VA
0930
hrs
AIAA-2
015-2
833
Near
-field
Pre
ssure
Wav
efor
m An
alysis
of an
Excit
ed M
ach
0.9
Jet
C. Ku
o, M.
Craw
ley, M
. Sam
imy,
Ohio
State
Univ
ersity
, Colu
mbus
, OH
1000
hrs
AIAA-2
015-2
834
Meas
uring
shea
r lay
er gr
owth
ra
tes in
aero
acou
stica
lly fo
rced
axisy
mmetr
ic su
perso
nic je
tsD.
Edgin
gton-M
itche
ll, O.
Amili,
D.
Honn
ery, J
. Sori
a, Mo
nash
Univ
ersity
, Me
lbourn
e, Au
strali
a
1030
hrs
AIAA-2
015-2
835
Impa
ct of
Chev
rons
on N
oise
Sour
ce Ch
arac
terist
ics In
Im
perfe
ctly E
xpan
ded J
et Flo
wsJ.
Liu, A
. Corr
igan,
K. Ka
ilasa
nath,
Nav
al Re
searc
h Lab
orator
y, Wa
shing
ton, D
C; E.
Gutm
ark, U
nivers
ity of
Cinc
innati
, Cin
cinna
ti, OH
1100
hrs
AIAA-2
015-2
836
Effe
ct of
Inve
rted T
riang
ular T
abs
on M
itigat
ion of
Jet N
oise f
rom
Axisy
mmetr
ic Co
nver
gent
Noz
zles
A. Su
brama
nyam
, K. N
ataraj
an, N
ation
al Ae
rospa
ce La
borat
ories
, Ban
galor
e, Ind
ia
1130
hrs
AIAA-2
015-2
837
An In
vesti
gatio
n of
Twin
Supe
rsonic
Je
ts’ N
ear-fi
eldJ.
Cluts,
C. Ku
o, M.
Sam
imy,
Ohio
State
Un
iversi
ty, Co
lumbu
s, OH
1200
hrs
AIAA-2
015-2
838
Acou
stic s
ource
analy
sis of
a su
perso
nic re
ctang
ular c
hevr
on je
tJ.
Kreitz
man,
J. Nic
hols,
Univ
ersity
of
Minn
esota
, Minn
eapo
lis, M
innea
polis,
MN
Wedn
esda
y, 24
June
201
515
4-AA
-24
CAA
Prop
agat
ion an
d Sca
tterin
g II
Obeli
sk A
Chair
ed by
: M. R
OGER
, Eco
le Ce
ntrale
de Ly
on09
00 hr
sAIA
A-201
5-283
9CA
A ana
lysis o
f a W
ing Se
ction
with
Fla
p Side
-Edge
s Bas
ed on
Hyb
rid
RANS
-LES C
ompu
tation
S. Pe
ng, L
. Tyse
ll, Sw
edish
Defen
se Re
search
Ag
ency
(FOI)
, Stoc
kholm
, Swe
den;
H. Ya
o, L.
David
son, L
. Erik
sson,
Chalm
ers Un
iversit
y of
Techn
ology,
Göteb
org, S
wede
n
0930
hrs
AIAA-2
015-2
840
Pred
iction
of Fa
r-Fiel
d Wind
Turb
ine
Noise
Pro
paga
tion
with
Par
aboli
c Eq
uatio
nS.
Lee,
Gene
ral El
ectric
Comp
any,
Niska
yuna
, NY
1000
hrs
AIAA-2
015-2
841
Nume
rical
simula
tion
of sp
ectra
l br
oade
ning o
f an
acou
stic w
ave
by a
spat
ially
grow
ing tu
rbule
nt
mixin
g lay
erI.
Benn
aceu
r, D. M
incu,
I. Ma
ry, M
. Te
rraco
l, ONE
RA, C
hâtill
on, F
rance
; L.
Larch
eveq
ue, D
. Pier
re, Ai
x-Mars
eille
Unive
rsity,
Mars
eille,
Fran
ce
1030
hrs
AIAA-2
015-2
842
Comp
ariso
n of
Comp
utat
ional
Aero
acou
stics
Pred
iction
of Vo
rtica
l Gu
st Sc
atter
ing by
a 2D
Stat
or w
ith
Flat P
late T
heor
yC.
Duran
d, D.
Hixo
n, Un
iversi
ty of
Toled
o, To
ledo,
OH
1100
hrs
AIAA-2
015-2
843
Nume
rical
and A
nalyt
ical
Inve
stiga
tion
of O
rthog
onal
Blad
e/Vo
rtex
Inter
actio
n No
iseF.
Faliss
ard, P
. Zeh
ner, O
NERA
, Châ
tillon
, Fra
nce;
M. Ro
ger, É
cole
Centr
ale de
Lyon
, Ec
ully,
Franc
e; X.
Gloe
rfelt,
Arts M
etiers
Pa
risTe
ch, P
aris,
Franc
e
Wedn
esda
y, 24
June
201
515
5-AA
-25
Benc
hmar
k Pr
oblem
s for
Airf
rame
Nois
e Com
puta
tions
III (
BANC
-III)
Summ
ary (
Invit
ed)
Fleur
-de-
lis A
Chair
ed by
: M. C
HOUD
HARI,
NAS
A-Lan
gley R
esea
rch Ce
nter
0900
hrs
Oral
Prese
ntatio
nAn
Ove
rview
of Co
ntrib
ution
s on
Nose
Land
ing G
ear C
onfig
urat
ion
for B
ANC-
III W
orks
hop
M. Kh
orram
i, NAS
A Lan
gley R
esea
rch
Cente
r, Ham
pton,
VA
0930
hrs
AIAA-2
015-2
844
Asse
ssmen
t of S
lat N
oise
Pred
iction
s for
30P
30N
High
-Lift
Confi
gura
tion
from
BANC
-III
Work
shop
M. Ch
oudh
ari, D
. Loc
kard,
NAS
A Lan
gley
Rese
arch C
enter
, Ham
pton,
VA
1000
hrs
AIAA-2
015-2
845
Varia
bility
in th
e Pro
paga
tion P
hase
of
CFD-
Based
Nois
e Pred
iction
: Sum
mary
of
Resu
lts fr
om Ca
tegor
y 8 of
the
BANC
-III W
orks
hop
L. Lo
pes,
NASA
Lang
ley Re
search
Cente
r, Ha
mpton
, VA;
S. Re
donn
et, O
NERA
, Tou
louse,
Fra
nce; T
. Imam
ura, U
nivers
ity of
Toky
o, Tok
yo, J
apan
; T. Ik
eda,
Japan
Aeros
pace
Ex
plorat
ion Ag
ency
(JAXA
), Ch
ofu, J
apan
; N.
Zawo
dny,
NASA
Lang
ley Re
search
Cente
r, Ha
mpton
, VA;
G. Cu
nha,
ONER
A, Tou
louse,
Fra
nce
1030
hrs
AIAA-2
015-2
846
Summ
ary o
f the
LAGO
ON So
lution
s fro
m th
e Ben
chma
rk pr
oblem
s for
Ai
rfram
e Nois
e Com
puta
tions
-III
Work
shop
E. Ma
noha
, ONE
RA, C
hâtill
on, F
rance
; B.
Carue
lle, A
irbus
, Tou
louse
, Fran
ce
1100
hrs
AIAA-2
015-2
847
Broa
dban
d Tra
iling-
Edge
Nois
e Pr
edict
ions—
Over
view
of B
ANC-
III
Resu
ltsM.
Herr
, R. E
wert,
C. Ra
utman
n, Ge
rman
Ae
rospa
ce Ce
nter (
DLR)
, Brau
nsch
weig,
Ge
rman
y; M.
Kamr
uzza
man,
ENER
CON
GmbH
, Auri
ch, G
erman
y; D.
Bek
iropo
ulos,
Unive
rsity
of St
uttga
rt, S
tuttga
rt,
Germ
any;
R. Ari
na, T
echn
ical U
nivers
ity of
Tu
rin, T
orino
, Ital
y; et
al.
80
Wedn
esda
y, 24
June
201
515
6-AC
D-4
Gene
ral A
viatio
nMo
rocco
Chair
ed by
: M. O
RR, B
oeing
Comm
ercial
Airpl
anes
0900
hrs
AIAA-2
015-2
848
Iden
tifyin
g High
-Risk
Occu
rrenc
e Ch
ains i
n He
licop
ter O
pera
tions
fro
m Ac
ciden
t Dat
aA.
Rao,
K. Ma
rais,
Purdu
e Univ
ersity
, Wes
t La
fayett
e, IN
0930
hrs
AIAA-2
015-2
849
Pilot
Per
cept
ion an
d Use
of A
DS-B
In
Traf
fic an
d Wea
ther
Serv
ices
(TIS-
B an
d FIS-
B)S.
Silv
a, L.
Jens
en, R
. Han
sman
, Ma
ssach
usett
s Ins
titute
of Te
chno
logy,
Camb
ridge
, MA
1000
hrs
AIAA-2
015-2
850
Imple
menta
taion
and V
alida
tion o
f an
Inter
nal C
ombu
stion
Engin
e and
Pr
opell
er Mo
del fo
r Gen
eral A
viatio
n Air
craft
Perfo
rman
ce Stu
dies
E. Ha
rrison
, S. M
in, H.
Jimen
ez, D
. Mav
ris,
Georg
ia Ins
titute
of Tec
hnolo
gy, At
lanta,
GA
1030
hrs
AIAA-2
015-2
851
Iden
tifyin
g Pha
ses o
f Flig
ht in
Ge
nera
l Avia
tion
Oper
ation
sN.
Fala,
V. G
oblet
, K. M
arais,
Purdu
e Un
iversi
ty, W
est L
afaye
tte, I
N
1100
hrs
AIAA-2
015-2
852
Pilot
-Frien
dline
ss Co
nside
ratio
ns fo
r Pe
rsona
l Air
Vehic
le Fli
ght C
ontro
l Sy
stems
I. Ch
akrab
orty,
B. Lo
zano
, D. M
avris
, Ge
orgia
Institu
te of
Tech
nolog
y, Atl
anta,
GA
1130
hrs
AIAA-2
015-2
853
Deve
lopme
nt of
Aero
dyna
mic
Mode
ling a
nd Ca
libra
tion M
ethod
s for
Ge
nera
l Avia
tion A
ircra
ft Pe
rform
ance
An
alysis
- a Su
rvey
and C
ompa
rison
of
Mode
lsS.
Min,
E. Ha
rrison
, H. J
imen
ez, D
. Mav
ris,
Georg
ia Ins
titute
of Tec
hnolo
gy, At
lanta,
GA
Wedn
esda
y, 24
June
201
515
7-AF
M-9
Unma
nned
Airc
raft
Syste
ms II
Plum
Blos
som
ACh
aired
by: T
. FIEL
DS, U
nivers
ity of
Miss
ouri a
nd G
. SHA
H, N
ASA-L
angle
y Res
earch
Cente
r09
00 hr
sAIA
A-201
5-285
4Un
stead
y Aer
odyn
amics
Mod
eling
fo
r a Fl
exibl
e Unm
anne
d Air
Vehic
leA.
Kotik
alpud
i, H. P
fifer, G
. Bala
s, Un
iversi
ty of
Minn
esota
, Minn
eapo
lis,
Minn
eapo
lis, M
N
0930
hrs
AIAA-2
015-2
855
A Com
paris
on of
Filte
rs for
UAS
-Bas
ed
Loca
lizati
on of
Stati
onar
y RF S
ource
sM.
Stach
ura, B
lack S
wift T
echno
logies
, LLC
, Bo
ulder,
CO; N
. Wag
le, E.
Frew
, Univ
ersity
of
Color
ado,
Bould
er, Bo
ulder,
CO
1000
hrs
AIAA-2
015-2
856
Robu
st Th
ree-
Dime
nsion
al Ch
arac
teriza
tion
of a
Comp
lex
Atmo
sphe
re at
High
Res
olutio
n us
ing M
ulti-A
gent
Wind
mapp
ers
C. Mo
ntalvo
, J. R
ichard
son,
J. Ma
rshall
, Un
iversi
ty of
South
Alab
ama,
Mobil
e, AL
1030
hrs
AIAA-2
015-2
857
Nonli
near
Mod
el Pr
edict
ive Co
ntro
l Ap
plied
to Tr
ajecto
ry Tr
ackin
g for
Un
mann
ed A
erial
Vehic
lesK.
Subb
arao,
C. Tu
le, P.
Ru, U
nivers
ity of
Te
xas,
Arling
ton, A
rlingto
n, TX
1100
hrs
AIAA-2
015-2
858
A La
unch
Syste
m De
sign
Meth
odolo
gy fo
r Sma
ll Unm
anne
d Ai
rcraf
t App
licat
ions
A. Pa
tterso
n, A.
Arena
, Okla
homa
Stat
e Un
iversi
ty, S
tillwa
ter, O
K
1130
hrs
AIAA-2
015-2
859
Feas
ibility
Stud
y of C
losed
Cycle
Pr
opuls
ion fo
r Unm
anne
d Aer
ial
Syste
msT.
Hays
, A. A
rena,
Oklah
oma S
tate
Unive
rsity,
Still
water
, OK
Wedn
esda
y, 24
June
201
515
8-AM
T-9/G
T-9Gr
ound
Test
Facil
ity Im
prov
emen
ts I
Obeli
sk B
Chair
ed by
: R. R
HEW,
NAS
A-Lan
gley R
esea
rch Ce
nter a
nd S
. SIM
ERLY,
NAS
A Glen
n Res
earch
Cente
r09
00 hr
sAIA
A-201
5-286
0De
velop
ment
of a
Rese
arch
Facil
ity
to St
udy t
he Fl
ow Fi
eld in
an A
PU-
Style
Inlet
F. Lo
u, W.
Murr
ay, N
. Key
, Purd
ue
Unive
rsity,
Wes
t Lafa
yette
, IN
0930
hrs
AIAA-2
015-2
861
Deve
lopme
nt an
d Tes
ting o
f an
Unste
ady L
ow-S
peed
Wind
Tunn
elD.
Gree
nblat
t, Te
chnio
n--Isr
ael In
stitut
e of
Tech
nolog
y, Ha
ifa, I
srael
1000
hrs
AIAA-2
015-2
862
Expa
nsion
of th
e AED
C H2
Arc
Heat
er Fa
cility
Test
Enve
lope U
sing
Cold-
Air M
ixing
G. H
ammo
ck, A
rnold
Engin
eerin
g De
velop
ment
Comp
lex, A
rnold
AFB,
TN
1030
hrs
AIAA-2
015-2
863
Expe
rimen
ts wi
th th
e Mod
el Te
st Ap
para
tus I
nsta
lled i
n th
e AFIT
Low
Spee
d Tun
nel
J. La
ncas
ter, M
. Ree
der, A
ir Forc
e Ins
titute
of Te
chno
logy,
Wrig
ht-Pa
tterso
n AFB
, OH;
M.
Syts
ma, A
ir Forc
e Res
earch
Labo
ratory
, Eg
lin AF
B, FL
; P. R
owe,
RE2,
Inc.,
Pit
tsburg
h, PA
; R. C
obb,
Air Fo
rce In
stitut
e of
Tech
nolog
y, W
right-
Patte
rson A
FB, O
H
1100
hrs
AIAA-2
015-2
864
Upgr
ades
to th
e Tex
as A
&M O
ran
W. N
icks L
ow-S
peed
Wind
Tunn
el fo
r M=0
.4 O
pera
tion
A. He
rring,
D. Ku
tz, L.
Brow
n, E.
Whit
e, Te
xas A
&M U
nivers
ity, C
olleg
e Stat
ion, T
X
1130
hrs
Oral
Prese
ntatio
nNA
SA La
ngley
Aer
oaco
ustic
Wind
Tu
nnel
Capa
bility
Mov
ing Fo
rwar
dM.
Doty
, F. H
utche
son,
H. H
askin
, P.
Quint
o, D.
Smi
th, N
ASA L
angle
y Res
earch
Ce
nter, H
ampto
n, VA
Wedn
esda
y, 24
June
201
515
9-AM
T-10/
GT-1
0Pa
rticle
-Bas
ed Ve
locim
etry A
pplic
ation
s and
Dev
elopm
ents
Topa
zCh
aired
by: K
. LOW
E, Vir
ginia
Tech
and C
. GOY
NE, U
nivers
ity of
Virg
inia
0900
hrs
AIAA-2
015-2
865
Veloc
ity M
easu
reme
nts i
n an
Un
seed
ed Tu
rboje
t Eng
ine Ex
haus
t Us
ing P
lanar
Dop
pler V
elocim
etry
T. Je
nkins
, Metr
oLas
er, In
c., La
guna
Hills
, CA
; J. S
eitzm
an, S
. Adu
sumi
lli, G
eorgi
a Ins
titute
of Te
chno
logy,
Atlan
ta, G
A
0930
hrs
AIAA-2
015-2
866
Stere
osco
pic P
IV m
easu
reme
nts
in a t
urbo
fan
engin
e inle
t with
ta
ilore
d swi
rl dis
torti
onM.
Nels
on, K
. Low
e, W.
O’B
rien,
C. Kir
k, Vir
ginia
Polyt
echn
ic Ins
titute
and S
tate
Unive
rsity,
Blac
ksbu
rg, VA
1000
hrs
AIAA-2
015-2
867
Multi-
stere
o PIV
mea
sure
ment
of
prop
eller
wak
e flow
in in
dustr
ial
facil
ityM.
Nov
ara, R
. Geis
ler, A
. Sch
roede
r, Ge
rman
Aeros
pace
Cente
r (DL
R),
Göttin
gen,
Germ
any
1030
hrs
AIAA-2
015-2
868
Appli
catio
n of
Par
ticle
Imag
e Ve
locim
etry a
nd La
ser I
nduc
ed
Fluor
esce
nce i
n a c
oolin
g duc
t flow
H. Ro
chlitz
, P. S
cholz
, Tec
hnica
l Univ
ersity
of
Brau
nsch
weig,
Brau
nsch
weig,
Germ
any
1100
hrs
AIAA-2
015-2
869
Biolo
gical
Flow
Meas
urem
ent u
sing
Optic
al Flo
w Me
thod
Z. Ya
ng, H
. Yu,
G. H
uang
, B. L
udwi
g, W
right
State
Univ
ersity
, Bea
vercr
eek,
OH
1130
hrs
AIAA-2
015-2
870
Deve
lopme
nt an
d cha
racte
rizat
ion
of an
inex
pens
ive LE
D-ba
sed
light
sour
ce fo
r high
-fram
e-ra
te sch
liere
n im
aging
D. Li
ncoln
, K. M
urari,
C. Jo
hans
en,
Unive
rsity
of Ca
lgary,
Calga
ry, Ca
nada
81
Wedn
esda
y, 24
June
201
516
0-AP
A-17
Spec
ial Se
ssion
: Hyb
rid CF
D Me
thod
Asse
ssmen
ts fo
r F-1
6XL A
ircra
ft Ae
rody
nami
csSte
mmon
s ACh
aired
by: J
. LUC
KRIN
G, N
ASA-L
angle
y Res
earch
Cente
r and
A. RI
ZZI,
KTH
Roya
l Insti
tute T
echn
ology
0900
hrs
AIAA-2
015-2
871
Free
-Fligh
t High
AoA
Flow
s Sim
ulatio
n at
Sub-
and T
rans
onic
Spee
ds -
F-16X
L (CA
WAPI
-3)
S. H
itzel,
Airbu
s, Ma
nchin
g, Ge
rman
y
0930
hrs
AIAA-2
015-2
872
F-16X
L Hyb
rid R
eyno
lds-A
vera
ged
Navie
r-Sto
kes/
Larg
e Edd
y Sim
ulatio
n on
Uns
tructu
red G
rids
M. Pa
rk, A.
Elmi
ligui,
K. Ab
dol-H
amid,
NA
SA La
ngley
Rese
arch C
enter
, Ham
pton,
VA
1000
hrs
AIAA-2
015-2
873
Nume
rical
Simula
tion o
f the
F-16
XL
at Fu
ll-Sc
ale Fl
ight T
est C
ondit
ions
Using
a Ne
ar-B
ody O
ff-Bo
dy CF
D Ap
proa
chS.
Mort
on, D
. McD
aniel
, CRE
ATE K
estre
l Te
am, E
glin A
FB, F
L
1030
hrs
AIAA-2
015-2
874
Hybr
id RA
NS-LE
S Sim
ulatio
ns of
F-1
6XL A
ircra
ft in
Low-
spee
d High
-alp
ha Fl
ight
M. To
mac,
A. Riz
zi, Ro
yal In
stitute
of
Techn
ology
(KTH
), Sto
ckholm
, Swe
den;
A. Jira
sek, P.
Elias
son, S
wedis
h Defe
nse Re
search
Ag
ency
(FOI)
, Stoc
kholm
, Swe
den
1100
hrs
AIAA-2
015-2
875
Nume
rical
Simula
tion o
f the
F-16
XL
at Fu
ll-Sc
ale Fl
ight T
est C
ondit
ions
Using
Dela
yed D
etach
ed-Ed
dy
Simula
tion
A. Lo
fthou
se, R
. Cum
ming
s, U.
S. Ai
r Forc
e Ac
adem
y, Co
lorad
o Spri
ngs,
CO
1130
hrs
AIAA-2
015-2
876
A Sy
nthe
sis of
Hyb
rid CF
D Re
sults
fo
r F-1
6XL A
ircra
ft Ae
rody
nami
csJ.
Luck
ring,
NASA
Lang
ley Re
searc
h Ce
nter, H
ampto
n, VA
Wedn
esda
y, 24
June
201
516
1-AP
A-18
Aero
dyna
mic D
esign
Meth
odolo
gies I
ICa
rpen
ter B
allro
omCh
aired
by: J
. LAT
Z, No
rthrop
Grum
man A
erosp
ace S
ystem
s and
D. F
INLE
Y, Lo
ckhe
ed M
artin
Aeron
autic
s09
00 hr
sAIA
A-201
5-287
7Im
prov
emen
ts in
the N
ew U
nstea
dy
Far-F
ield D
rag B
reak
down
Meth
od
and A
pplic
ation
to Co
mplex
Case
sH.
Toub
in, D
. Bail
ly, M
. Cos
tes, O
NERA
, Me
udon
, Fran
ce
0930
hrs
AIAA-2
015-2
878
Aero
dyna
mic s
hape
optim
izatio
n of
BW
B air
craft
base
d on
multiz
one
colla
bora
tive o
ptim
izatio
n de
sign
meth
odZ.
Gao,
K. Zh
ao, C
. Wan
g, No
rthwe
stern
Polyt
echn
ical U
nivers
ity, X
i’an,
China
1000
hrs
AIAA-2
015-2
879
Desig
n of
A H
igh-P
erfo
rman
ce
Taille
ss MA
V Thr
ough
Plan
form
Op
timiza
tion
M. B
ronz,
G. H
atten
berge
r, Fren
ch Ci
vil
Aviat
ion U
nivers
ity, T
oulou
se, F
rance
1030
hrs
AIAA-2
015-2
880
Aero
dyna
mic O
ptimi
zatio
n of
Integ
rated
Wing
-Engin
e Geo
metry
us
ing an
Uns
tructu
red Vo
rticit
y Solv
erL.
King,
R. Ha
rtfield
, Aub
urn Un
iversit
y, Au
burn,
AL; V
. Ahu
ja, Re
search
in Fl
ight,
Aubu
rn, AL
Wedn
esda
y, 24
June
201
516
2-AP
A-19
Prop
eller
/Rot
orcra
ft/Wi
nd Tu
rbine
Aer
odyn
amics
IISte
mmon
s BCh
aired
by: J
. FAR
NSW
ORTH
, Univ
ersity
of Co
lorad
o Bou
lder a
nd M
. POS
T, US
AF Ac
adem
y09
00 hr
sAIA
A-201
5-288
1De
velop
ment
of U
GS M
onoc
opter
: Pla
tform
Des
ign an
d Tra
jecto
ry
Track
ingS.
Srig
rarom
, K. L
ee, S
. Chn
g, M.
Bin
Abdu
l Mali
k, Un
iversi
ty of
Glasg
ow,
Glasg
ow, U
nited
King
dom
0930
hrs
AIAA-2
015-2
882
A stu
dy of
sepa
ratio
n on
airfo
ils
unde
rgoin
g pitc
h, su
rge a
nd
comb
ined m
otion
sR.
Dunn
e, B.
McK
eon,
Califo
rnia I
nstitu
te of
Tech
nolog
y, Pa
sade
na, C
A
1000
hrs
AIAA-2
015-2
883
Comp
utat
ional
Inve
stiga
tion
of Co
axial
Rot
or In
terac
tiona
l Ae
rody
nami
cs in
Stead
y For
ward
Fli
ght
B. Pa
sse, A
. Srid
haran
, J. B
aede
r, Un
iversi
ty of
Maryl
and,
Colle
ge Pa
rk,
Colle
ge Pa
rk, M
D
1030
hrs
AIAA-2
015-2
884
Comp
utatio
nal In
vesti
gatio
ns
of Tra
nsien
t Loa
ds an
d Blad
e De
forma
tions
on Co
axial
Rotor
Sy
stems
R. Sin
gh, H
. Kan
g, Arm
y Rese
arch L
abora
tory,
Aberd
een P
roving
Grou
nd, M
D; J.
Siroh
i, Un
iversit
y of T
exas,
Austin
, Aust
in, TX
1100
hrs
AIAA-2
015-2
885
Roto
r Dyn
amic
Wake
Inflo
w Mo
dellin
g in
State-
Spac
e For
mat
M. G
enna
retti,
R. Go
ri, J.
Serafi
ni, G
. Be
rnardi
ni, F.
Cardi
to, Ro
ma Tr
e Univ
ersity
, Ro
me, I
taly
1130
hrs
AIAA-2
015-2
886
Valid
ation
of In
stalla
tion
Effe
ct Pr
edict
ions t
hrou
gh Si
mulat
ions
of Co
ntra
-Rot
ating
Ope
n Ro
tors
at
Low-
Spee
d Flig
ht Co
nditio
nsA.
Stue
rmer,
Germ
an Ae
rospa
ce Ce
nter
(DLR
), Br
auns
chwe
ig, G
erman
y
1200
hrs
AIAA-2
015-2
887
A Ne
w Wh
irl Fl
utter
Ana
lysis
Meth
odY.
Yang
, G. H
uang
, D. Z
hao,
C. Ta
ng,
Aviat
ion In
dustr
y Corp
oratio
n of C
hina
(AVIC
), Xi’
an, C
hina
Wedn
esda
y, 24
June
201
516
3-AS
E-1Nu
meric
al We
athe
r Pre
dictio
n (In
vited
)Plu
m Bl
osso
m B
Chair
ed by
: N. A
HMAD
, NAS
A Lan
gley R
esea
rch Ce
nter a
nd D
. GHO
SH09
00 hr
sAIA
A-201
5-288
8Ch
allen
ges a
nd O
ppor
tunit
ies in
Mod
eling
of th
e Glob
al At
mosp
here
Z. Ja
njic,
Natio
nal O
cean
ic an
d Atm
osph
eric A
dmini
strati
on, C
olleg
e Park
, MD
1000
hrs
AIAA-2
015-2
889
Well-
Balan
ced F
ormu
lation
of
Grav
itatio
nal S
ource
Term
s for
Co
nser
vativ
e Fini
te-Di
ffere
nce
Atmo
sphe
ric Fl
ow So
lvers
D. G
hosh
, E. C
onsta
ntine
scu, A
rgonn
e Na
tiona
l Lab
orator
y, Le
mont,
IL
1030
hrs
AIAA-2
015-2
890
Use o
f Num
erica
l Wea
ther
Pr
edict
ion M
odels
for N
extG
en AT
C Wi
nd Im
pact
Studie
s (In
vited
)S.
Trox
el, T.
Reyn
olds,
Linco
ln La
borat
ory,
Massa
chus
etts I
nstitu
te of
Tech
nolog
y, Le
xingto
n, MA
1100
hrs
AIAA-2
015-2
891
Simula
tions
of or
ogra
phic fl
ows u
sing
unstr
uctur
ed an
d stru
ctured
mesh
es
(Invit
ed)
J. Sz
melte
r, Lou
ghbo
rough
Unive
rsity,
Loug
hboro
ugh,
Unite
d King
dom;
P.
Smola
rkiew
icz, E
urope
an Ce
ntre f
or Me
dium-
Rang
e Fore
castin
g, Re
ading
, Unit
ed Ki
ngdo
m;
A. Wy
szogro
dzki,
Nati
onal
Resea
rch In
stitute
, Wa
rsaw,
Polan
d
82
Wedn
esda
y, 24
June
201
516
4-AT
IO-1
5AT
M III
- Mo
delin
g in
ATM
Metro
polita
n Ba
llroo
mCh
aired
by: S
. LAN
DRY,
Purdu
e Univ
ersity
0900
hrs
AIAA-2
015-2
892
A Sy
stem
Dyna
mics
Appr
oach
to
ward
s ANS
P Mo
delin
gM.
Kreu
z, M.
Sch
ultz,
Germ
an Ae
rospa
ce
Cente
r (DL
R), B
rauns
chwe
ig, G
erman
y
0930
hrs
AIAA-2
015-2
893
Mode
ling A
ppro
ach f
or Re
silien
ce
Engin
eerin
g of t
he Fu
ture A
TM Sy
stem
R. Pa
lumbo
, A. E
rrico,
D. Pa
scarel
la, F.
Ga
rgiulo
, E. F
ilippo
ne, I
talian
Aeros
pace
Re
searc
h Cen
ter (C
IRA),
Capu
a, Ita
ly
1000
hrs
AIAA-2
015-2
894
Risk
-bas
ed Ca
usal
Mode
ling o
f Ai
rbor
ne Lo
ss of
Sepa
ratio
nS.
Geu
ther, A
. Shih
, NAS
A Lan
gley
Rese
arch C
enter
, Ham
pton,
VA
1030
hrs
AIAA-2
015-2
895
A Da
ta-D
riven
Qua
ntita
tive
Fram
ewor
k fo
r Saf
ety A
ssessm
ent
of A
ir Tra
ffic C
ontro
l Sys
temA.
Oztek
in, H
i-Tec S
ystem
s, Inc
., Eg
g Ha
rbor T
wp, N
J
1100
hrs
AIAA-2
015-2
896
Asse
ssing
Air
Traffi
c Con
trol S
ystem
Sa
fety
with
Syste
m Co
ntro
llabil
ityJ.
Guo,
K. Ma
rais,
S. La
ndry,
Purdu
e Un
iversi
ty, W
est L
afaye
tte, I
N
Wedn
esda
y, 24
June
201
516
5-AT
IO-1
6Tra
nsfo
rmat
ional
Fligh
t - A
uton
omy I
Mone
t Ball
room
Chair
ed by
: B. A
LLEN,
NAS
A Lan
gley R
esea
rch Ce
nter
0900
hrs
AIAA-2
015-2
897
Who’s
got t
he br
idge?
Towa
rds
Safe
, Rob
ust A
uton
omou
s Op
erat
ions -
“Dat
a, yo
u’ve
got
the b
ridge
.” - F
irst O
ffice
r Tho
mas
“Will”
Rike
r Sta
r Tre
k: Th
e Nex
t Ge
nera
tion:
: Com
ing of
Age
(198
8)B.
Allen
, C. C
ross,
H. Fa
n, W.
Fehlm
an,
L. He
mpley
, M. M
otter,
NAS
A Lan
gley
Rese
arch C
enter
, Ham
pton,
VA; e
t al.
0930
hrs
AIAA-2
015-2
898
Towa
rds a
n Op
en, D
istrib
uted
So
ftwar
e Arch
itectu
re fo
r UxS
Op
erat
ions -
“It’s
diffi
cult
to
work
in gr
oups
whe
n yo
u’re
om
nipot
ent,”
- Q
Star T
rek:
The
Next
Gen
erat
ion::
Deja
Q (1
990)
C. Cro
ss, H
. Fan
, W. F
ehlm
an, L
. Hem
pley,
M. M
otter,
J. N
eilan
, NAS
A Lan
gley
Rese
arch C
enter
, Ham
pton,
VA; e
t al.
1000
hrs
AIAA-2
015-2
899
Reinf
orce
ment
Lear
ning w
ith
Auto
nomo
us Sm
all U
nman
ned
Aeria
l Veh
icles
in Cl
utter
ed
Envir
onme
nts -
“Afte
r all t
hese
ye
ars a
mong
hum
ans,
you
still
have
n’t l
earn
ed to
smile
.”L.
Tran,
C. Cro
ss, M
. Mott
er, J.
Neil
an,
G. Q
ualls,
P. Ro
thhaa
r, NAS
A Lan
gley
Rese
arch C
enter
, Ham
pton,
VA; e
t al.
1030
hrs
Oral
Prese
ntatio
n“H
is ac
tions
indic
ate t
wo-
dimen
siona
l thin
king”
- De
ciding
to
Go A
roun
d via
Mach
ine Le
arnin
gM.
Mott
er, J.
High
, C. C
ross,
H. Fa
n, W.
Fehlm
an, L
. Hem
pley,
NASA
Lang
ley
Rese
arch C
enter
, Ham
pton,
VA; e
t al.
Wedn
esda
y, 24
June
201
516
6-AT
IO-1
7Hu
man
Facto
rs in
Aviat
ion O
pera
tions
Milan
Chair
ed by
: L. B
OWER
S, Pu
rdue U
nivers
ity09
00 hr
sAIA
A-201
5-290
0A
Mode
l for
Situ
ation
al Aw
aren
ess
in Ai
rcraf
t Ups
et Pr
even
tion
and
Reco
very
K. Sc
hlimm
, Avia
tion P
erform
ance
So
lution
s, LLC
, Mes
a, AZ
0930
hrs
AIAA-2
015-2
901
Analy
sis of
Eye-
Track
ing D
ata w
ith
Rega
rds t
o the
Comp
lexity
of Fl
ight
Deck
Info
rmat
ion A
utom
ation
an
d Man
agem
ent -
Inat
tentio
nal
Blind
ness,
Syste
m Sta
te Aw
aren
ess,
and E
FB U
sage
E. Dil
l, S. Y
oung
, NAS
A Lan
gley R
esea
rch
Cente
r, Ham
pton,
VA
1000
hrs
AIAA-2
015-2
902
Thre
at an
d Erro
r Man
agem
ent
Appli
ed to
Loss
of Co
ntro
l - In
fligh
tD.
Carro
ll, Av
iation
Perfo
rman
ce S
olutio
ns,
LLC, M
esa,
AZ
1030
hrs
AIAA-2
015-2
903
Evalu
ating
Inten
sity a
s a N
extG
en
Cont
rolle
r Fun
ction
for I
ncre
ased
Tra
ffic S
cena
rios
C. Su
rakitb
anha
rn, S
. Lan
dry, P
urdue
Un
iversi
ty, W
est L
afaye
tte, I
N
1100
hrs
AIAA-2
015-2
904
A Co
mpar
ison
of an
Inten
sity
Cont
rol M
easu
re Ve
rsus D
ynam
ic De
nsity
to Ca
ptur
e Com
plexit
y Wi
thin
a Sec
tor
C. Su
rakitb
anha
rn, C.
Sura
kitba
nharn
, S.
Land
ry, Pu
rdue U
nivers
ity, W
est
Lafay
ette,
IN
1130
hrs
AIAA-2
015-2
905
Tacti
le Fe
edba
ck an
d Situ
ation
Aw
aren
ess -
Impr
oving
Adh
eren
ce
to an
Enve
lope i
n Sid
estic
k-Co
ntro
lled F
ly-by
-Wire
Airc
rafts
F. Sc
hmidt
-Skipi
ol, Te
chnic
al Un
iversi
ty of
Brau
nsch
weig,
Brau
nsch
weig,
Germ
any
1200
hrs
AIAA-2
015-2
906
Mode
ling t
he A
ir Tra
ffic C
ontro
ller’s
Di
rect-
to O
pera
tion
Using
Logis
tic
Regr
essio
nS.
Hon
g, S.
Jung
, K. L
ee, K
orea A
erosp
ace
Unive
rsity,
Goy
ang,
South
Korea
Wedn
esda
y, 24
June
201
516
7-BA
L-1Ba
lloon
Syste
ms I
Steub
enCh
aired
by: J
. NOT
T, No
tt Te
chno
logy L
LC09
00 hr
sAIA
A-201
5-290
7Th
e NAS
A Ba
lloon
Pro
gram
- Po
sition
ing Fo
r the
Futu
reD.
Fairb
rothe
r, NAS
A God
dard
Spac
e Flig
ht Ce
nter, G
reenb
elt, M
D
0930
hrs
AIAA-2
015-2
908
The F
renc
h ba
lloon
prog
ram
2013
- 2
015
A. Va
rgas,
V. Du
bourg
, D. V
assa
ux, F
rench
Sp
ace A
genc
y (CN
ES),
Toulo
use,
Franc
e
1000
hrs
Oral
Prese
ntatio
nBa
lloon
Syste
ms A
pplic
ation
T. Ge
rber, A
pplie
d Tec
hnolo
gy As
socia
tes,
Albuq
uerqu
e, NM
1030
hrs
AIAA-2
015-2
909
Quali
ficat
ion of
the N
ASA
Supe
r Pr
essu
re B
alloo
nH.
Cathe
y, Ne
w Me
xico S
tate U
nivers
ity,
Wallo
ps Is
land,
VA; J
. Tutt
le, D
. Fa
irbrot
her, M
. Said
, NAS
A God
dard
Spac
e Fli
ght C
enter
, Wall
ops I
sland
, VA
1100
hrs
AIAA-2
015-2
910
Non-
Linea
r Ana
lysis
of th
e NA
SA Su
per P
ressu
re B
alloo
ns:
Imple
ment
ation
of a
Larg
e Stra
in Ma
terial
Mod
elA.
Bown
, D. W
akefi
eld, T
ensy
s Dyn
amics
, Ltd
., Ba
th, U
nited
King
dom
1130
hrs
AIAA-2
015-2
911
Retu
rning
to H
ydro
gen
Gas :
a Str
ateg
ic De
cision
to Co
ntinu
e Ac
hieve
ment
of St
rato
sphe
ric
Ballo
ons F
light
sJ.
Gary,
Fren
ch S
pace
Agen
cy (C
NES)
, Air
e sur
l’Ado
ur, Fr
ance
; B. D
ellery
, G.
Letre
nne,
S. Ve
nel, A
. Varg
as, F
rench
Sp
ace A
genc
y (CN
ES),
Toulo
use,
Franc
e
1200
hrs
AIAA-2
015-2
912
Suita
bility
of A
DS-B
as a
Beac
on
for S
trato
sphe
ric B
alloo
n Pla
tform
s an
d Pay
loads
T. La
chen
meier
, R. D
ewey
, Nea
r Spa
ce
Corpo
ration
, Tilla
mook
, OR
83
Wedn
esda
y, 24
June
201
516
8-CA
SE-6
09
00 -
1230
hrs
CASE
Sessi
on II
& II
IGr
and B
allro
om D
0900
-1045
hrs
Integ
ration
and T
est
This
pane
l focu
ses o
n the
Integ
ration
& Te
st ph
ase o
f dev
elopm
ent.
Plann
ing fo
r integ
ration
activ
ities o
f com
plex s
ystem
s is i
nhere
ntly d
ifferen
t from
trad
itiona
l sys
tems e
ngine
ering
integ
ration
plan
ning a
ctivit
ies. D
ecisio
ns ab
out t
he sy
stems
unde
r dev
elopm
ent h
ave t
o con
sider
not o
nly th
e tec
hnica
l and
prog
ramma
tic vi
ewpo
ints b
ut als
o the
politi
cal, s
ociet
al, op
eratio
nal, a
nd ec
onom
ic vie
wpoin
ts. D
efinit
ion of
perfo
rman
ce m
easu
res, f
ound
intrin
sic in
the p
lan, w
ith tr
ans-d
iscipl
inary
impli
catio
ns w
ill be
discu
ssed.
A sce
nario
for in
tegrat
ion of
UAS
in th
e NA
S wi
ll be u
sed a
s a be
nchm
ark fo
r curr
ent v
iews a
nd lif
e cyc
le ch
allen
ges.
Sessi
on Ch
airs:
Mat F
rench
, Elec
trical
Syste
ms En
ginee
r, Roll
s-Roy
ce Co
rporat
ion, H
ernan
do Ji
mine
z, Re
searc
h Eng
ineer
II at A
erosp
ace S
ystem
s Des
ign La
borat
ory, G
eorgi
a Ins
titute
of Te
chno
logy a
nd D
avid
Loda
, Exe
cutiv
e Dire
ctor, N
CPS
Rese
arch,
LLC
Pan
elists
:Jim
Mur
phy
Projec
t Eng
ineer
for In
tegrat
ed Te
st an
d Eva
luatio
n for
the U
nman
ned A
ircraf
t Sys
tem In
tegrat
ionNA
SA Am
es Re
searc
h Cen
ter
David
Mar
oney
Princ
ipal S
ystem
s Eng
ineer
The M
itre Co
rporat
ion
1045
-1230
hrs
Entr y
into
Servi
ce/E
nd of
Life
This
pane
l focu
ses o
n the
comp
lexitie
s tha
t aris
e onc
e a sy
stem
enter
s serv
ice th
rough
out t
he lif
e of t
he sy
stem.
If th
ese c
omple
xities
are c
onsid
ered a
nd in
corpo
rated
into
the sy
stem
deve
lopme
nt ph
ase,
more
robus
t prod
ucts
can b
e dev
elope
d and
high
er cu
stome
r sati
sfacti
on
can b
e ach
ieved
.Se
ssion
Chair
: Jeff
Jeps
on, S
enior
Sys
tems E
ngine
er GN
C / G
uidan
ce D
esign
& Pe
rform
ance
, Ray
theon
Miss
ile S
ystem
s
Pan
elists
:Tim
Ada
maCh
ief En
ginee
r of F
actor
iesRa
ytheo
n Miss
ile S
ystem
s
Ed D
olans
kiPre
siden
t and
CEO
Avial
l
Jim G
allag
her
EIS Pr
ogram
Man
ager
Gulfs
tream
Aeros
pace
Corpo
ration
Wedn
esda
y, 24
June
201
516
9-CF
D-17
Adva
nces
in H
igh-O
rder
Meth
ods
Gran
d Ball
room
ACh
aired
by: D
. ZIN
GG, U
nivers
ity of
Toron
to an
d P. R
OE, U
nivers
ity of
Mich
igan
0900
hrs
AIAA-2
015-2
913
New
Appr
oach
es to
Limi
ting
P. Ro
e, T.
Lung
, J. M
aeng
, Univ
ersity
of
Mich
igan,
Ann A
rbor, A
nn Ar
bor, M
I
0930
hrs
AIAA-2
015-2
914
New
Diag
onal-
Norm
Summ
ation
-by
-Par
ts Op
erat
ors f
or th
e Firs
t De
rivat
ive w
ith In
creas
ed O
rder
of
Accu
racy
D. D
el Re
y Fern
ánde
z, D.
Zing
g, Un
iversi
ty of
Toron
to, To
ronto,
Cana
da
1000
hrs
AIAA-2
015-2
915
Deve
lopme
nt of
Gen
erali
zed
Summ
ation
-by-
Parts
Ope
rato
rs fo
r th
e Sec
ond D
eriva
tive w
ith Va
riable
Co
effic
ients
D. D
el Re
y Fern
ánde
z, D.
Zing
g, Un
iversi
ty of
Toron
to, To
ronto,
Cana
da
1030
hrs
AIAA-2
015-2
916
A Fini
te Di
fferen
ce WE
NO Sc
heme
Ma
intain
ing Ve
locity
, Pres
sure
an
d Tem
pera
ture E
quilib
rium
in Mu
lticom
pone
nt Co
mpres
sible
Fluid
Analy
sisT.
Nono
mura,
Japa
n Aero
space
Explo
ration
Ag
ency
(JAXA
), Sa
gami
hara,
Japa
n; D.
Ter
akad
o, Un
iversit
y of T
okyo
, Sag
amiha
ra,
Japan
; K. F
ujii, J
apan
Aeros
pace
Explo
ration
Ag
ency
(JAXA
), Sa
gami
hara,
Japa
n
Wedn
esda
y, 24
June
201
517
0-CF
D-18
Curre
nt Tr
ends
in CF
D Re
sear
ch I
(Invit
ed)
Gran
d Ball
room
BCh
aired
by: H
. HUY
NH, N
ASA G
lenn R
esea
rch Ce
nter a
nd Z.
WAN
G, U
nivers
ity of
Kans
as09
00 hr
sOr
al Pre
senta
tion
Comp
ariso
n of O
utput
Error
Estim
ation
for
Finit
e Elem
ent D
iscret
izatio
ns of
Co
nvect
ion-do
mina
ted Fl
ows (
Invite
d)H.
Carso
n, S.
Allma
ras, M
. Galb
raith,
D.
Darm
ofal, M
assach
usetts
Instit
ute of
Tec
hnolo
gy, Ca
mbrid
ge, M
A
0930
hrs
Oral
Prese
ntatio
nNo
vel A
dapt
ive M
echa
nics f
or H
igh-
Orde
r Uns
tructu
red C
FD (I
nvite
d)K.
Fidko
wski,
Univ
ersity
of M
ichiga
n, An
n Arb
or, An
n Arbo
r, MI
1000
hrs
AIAA-2
015-2
917
Inve
stiga
tion
of U
nstru
cture
d Hi
gher
-Ord
er M
ethod
s for
Uns
teady
flo
w an
d Mov
ing D
omain
sJ.
Newm
an, W
. And
erson
, Univ
ersity
of
Tenn
esse
e, Ch
attan
ooga
, Cha
ttano
oga,
TN
1030
hrs
Oral
Prese
ntatio
nHi
gh-o
rder
Disc
ontin
uous
Gale
rkin
Simula
tions
on D
omain
s with
Larg
e De
form
ation
s (In
vited
)P.
Perss
on, U
nivers
ity of
Califo
rnia,
Berke
ley, B
erkele
y, CA
1100
hrs
Oral
Prese
ntatio
nPr
obing
Comp
lex U
nstea
dy Fl
ow
Phys
ics U
sing a
High
-Fide
lity
Comp
utat
ional
Fram
ewor
k (In
vited
)M.
Visb
al, Ai
r Forc
e Res
earch
Labo
ratory
, W
right-
Patte
rson A
FB, O
H
84
Wedn
esda
y, 24
June
201
517
1-CF
D-19
LES,
DNS,
and H
ybrid
RAN
S-LE
S III
Cora
lCh
aired
by: J
. BAE
DER,
Unive
rsity
of Ma
rylan
d and
C. G
ROTH
, Univ
ersity
of To
ronto
0900
hrs
AIAA-2
015-2
918
Aero
dyna
mic C
hara
cteris
tics o
f SC
1095
Airfo
il usin
g Hyb
rid RA
NS-LE
S Me
thods
Imple
mente
d into
a GP
U Ac
celera
ted N
avier
-Stok
es So
lver
N. Ja
in, J.
Baed
er, Un
iversit
y of M
arylan
d, Co
llege P
ark, C
ollege
Park,
MD
0930
hrs
AIAA-2
015-2
919
Appli
catio
ns of
the i
ntegr
al Wa
ll Mod
el in
LES o
f flow
over
surfa
ces in
cludin
g res
olved
and s
ubgr
id ro
ughn
essX.
Yang
, J. S
adiqu
e, C.
Mene
veau
, R. M
ittal,
Johns
Hopk
ins Un
iversit
y, Ba
ltimore
, MD
1000
hrs
AIAA-2
015-2
920
An Em
bedd
ed LE
S-RA
NS So
lver f
or
Aero
dyna
mic S
imula
tions
K. An
upind
i, R. S
andb
erg, U
nivers
ity of
So
utham
pton,
South
ampto
n, Un
ited
Kingd
om
1030
hrs
AIAA-2
015-2
921
Asse
ssmen
t of H
ybrid
RAN
S/LE
S Me
thods
For G
as-Tu
rbine
Comb
ustor
-Re
levan
t Tur
bulen
t Flow
sJ.
West,
C. Gr
oth, U
nivers
ity of
Toron
to,
Toron
to, Ca
nada
; J. H
u, Pra
tt & W
hitne
y, Mi
ssissa
uga,
Cana
da
Wedn
esda
y, 24
June
201
517
2-CF
D-20
Turb
ulenc
e Mod
el Va
lidat
ion (I
nvite
d)Em
erald
Chair
ed by
: C. R
UMSE
Y, NA
SA-La
ngley
Rese
arch C
enter
and B
. SMI
TH, L
ockh
eed M
artin
Aeron
autic
s09
00 hr
sAIA
A-201
5-292
2Mo
difica
tion
of th
e k-k
l Two
Eq
uatio
n Tu
rbule
nce M
odel
for
Impr
oved
Jet F
low P
redic
tions
(In
vited
)B.
Smi
th, Lo
ckhe
ed M
artin
Corpo
ration
, Fo
rt Wo
rth, T
X
0930
hrs
AIAA-2
015-2
923
LagR
ST M
odel
Pred
iction
s of a
Wi
ngtip
Vorte
x Flo
wfield
(Inv
ited)
M. O
lsen,
NASA
Ames
Rese
arch C
enter
, Mo
ffett
Field,
CA; R
. Lilla
rd, N
ASA J
ohns
on
Spac
e Cen
ter, H
ousto
n, TX
; T. C
oakle
y, NA
SA Am
es Re
searc
h Cen
ter, M
offett
Fie
ld, CA
1000
hrs
AIAA-2
015-2
924
Seco
nd-M
omen
t RAN
S Mod
el Ve
rifica
tion a
nd Va
lidati
on us
ing th
e Tu
rbule
nce M
odeli
ng Re
sour
ce We
bsite
(In
vited
)B.
Eisfel
d, Ge
rman
Aeros
pace
Cente
r (DL
R),
Braun
schwe
ig, Ge
rman
y; C.
Rums
ey, N
ASA
Lang
ley Re
search
Cente
r, Ham
pton,
VA
1030
hrs
AIAA-2
015-2
925
Asse
ssmen
t of g
-Equa
tion
Form
ulatio
n fo
r a Se
cond
-Mom
ent
Reyn
olds S
tress
Turb
ulenc
e Mod
el (In
vited
)V.
Togit
i, B. E
isfeld
, Germ
an Ae
rospa
ce
Cente
r (DL
R), B
rauns
chwe
ig, G
erman
y
1100
hrs
AIAA-2
015-2
926
Appli
catio
n of
an El
liptic
Blen
ding
Reyn
olds S
tress
Mode
l in A
ttach
ed
and S
epar
ated
flow
s (In
vited
)M.
Stoe
llinge
r, R. R
oy, U
nivers
ity of
W
yomi
ng, L
arami
e, La
ramie,
WY;
N. As
hton,
Unive
rsity
of Ma
nche
ster,
Manc
heste
r, Unit
ed Ki
ngdo
m
1130
hrs
AIAA-2
015-2
927
Rece
nt D
evelo
pmen
ts on
the
Turb
ulenc
e Mod
eling
Res
ource
We
bsite
(Inv
ited)
C. Ru
msey
, NAS
A Lan
gley R
esea
rch Ce
nter,
Hamp
ton, V
A
Wedn
esda
y, 24
June
201
517
3-FD
-19
Turb
omac
hiner
y - Tu
rbine
sSe
nato
rs Le
cture
Hall
Chair
ed by
: Z. R
USAK
, Ren
sselae
r Poly
techn
ic Ins
titute
and Q
. WAN
G, M
IT09
00 hr
sAIA
A-201
5-292
8Da
ta P
roce
ssing
Tech
nique
s for
Me
asur
emen
ts Co
llecte
d fro
m a S
ingle
Slant
ed H
ot-W
ire fo
r Tu
rbom
achin
ery A
pplic
ation
sR.
Berda
nier, N
. Key
, Purd
ue U
nivers
ity,
West
Lafay
ette,
IN
0930
hrs
AIAA-2
015-2
929
Flowfi
eld an
d Film
Per
form
ance
Me
asur
emen
ts of
Axia
l Sha
ped
Cooli
ng H
oles o
n a F
lat P
late
D. G
etsing
er, J.
Dee
s, G.
Rode
baug
h, Ge
neral
Elec
tric Co
mpan
y, Nis
kayu
na, N
Y
1000
hrs
AIAA-2
015-2
930
Visua
lizat
ion of
Seco
ndar
y Flow
Str
uctu
res C
ause
d by R
otat
ing
Insta
bility
: Syn
chro
nized
Ster
eo
High
-Spe
ed P
IV an
d Uns
teady
Pr
essu
re M
easu
reme
nts
B. Pa
rdowi
tz, G
erman
Aeros
pace
Cente
r (D
LR),
Berlin
, Germ
any;
J. Pe
ter, T
echn
ical
Unive
rsity
of Be
rlin, B
erlin,
Germ
any;
U.
Tapk
en, G
erman
Aeros
pace
Cente
r (DL
R),
Berlin
, Germ
any;
P. Th
amse
n, Te
chnic
al Un
iversi
ty of
Berlin
, Berl
in, G
erman
y; L.
Engh
ardt,
Germ
an Ae
rospa
ce Ce
nter
(DLR
), Be
rlin, G
erman
y
1030
hrs
AIAA-2
015-2
931
Desig
n Op
timiza
tion
of P
rofil
ed
Endw
all w
ith Co
nside
ratio
n of
Co
oling
and R
im Se
al Flo
w Ef
fects
H. Ta
ng, S
. Liu,
H. L
uo, A
viatio
n Ind
ustry
Co
rporat
ion of
China
(AVIC
), Sh
angh
ai,
China
85
Wedn
esda
y, 24
June
201
517
4-FD
-20
Shoc
k Wa
ve /
Bou
ndar
y Lay
er In
terac
tions
Edelw
eiss
Chair
ed by
: N. C
LEME
NS, T
he U
nivers
ity of
Texa
s at A
ustin
and D
. GAIT
ONDE
, The
Ohio
Stat
e Univ
ersity
0900
hrs
AIAA-2
015-2
932
Expe
rimen
tal I
nves
tigat
ion of
Un
stead
iness
of Sw
ept-R
amp
Shoc
k/Bo
unda
ry La
yer I
nter
actio
ns
at M
ach
2L.
Vans
tone,
M. S
aleem
, S. S
eckin
, N.
Cleme
ns, U
nivers
ity of
Texa
s, Au
stin,
Austi
n, TX
0930
hrs
AIAA-2
015-2
933
Effe
cts of
Swee
p on
Impin
ging
Obliq
ue Sh
ock-
Turb
ulent
Bou
ndar
y La
yer I
nter
actio
nR.
Daws
on, C
. Ped
erson
, J. L
ittle,
Unive
rsity
of Ari
zona
, Tuc
son,
Tucso
n, AZ
1000
hrs
AIAA-2
015-2
934
Expe
rimen
tal I
nves
tigat
ion of
sh
ock-
induc
ed co
rner
boun
dary
lay
er se
para
tion
A. He
gde,
V. Na
rayan
aswa
my, N
orth
Carol
ina S
tate U
nivers
ity, R
aleigh
, NC
1030
hrs
AIAA-2
015-2
935
Expe
rimen
tal an
d Num
erica
l Stud
y of
Shoc
k-Wav
e Bou
ndar
y Lay
er
Intera
ction
s on a
n Axis
ymme
tric B
ody
G. Ro
berts
on, R
. Kum
ar, Fl
orida
State
Un
iversit
y, Tal
lahass
ee, F
L; T.
Eyma
nn, S
. Mo
rton,
CREA
TE Ke
strel
Team,
Eglin
AFB,
FL
1100
hrs
AIAA-2
015-2
936
An Ex
perim
enta
l Inv
estig
ation
of
the E
ffect
of B
ound
ary L
ayer
on an
In
terna
l Com
pres
sion
Inlet
H. Ta
banli
, K. Y
uceil
, Ista
nbul
Tech
nical
Unive
rsity,
Istan
bul, T
urkey
Wedn
esda
y, 24
June
201
517
5-FD
-22
Unste
ady F
lows -
Cavit
y and
Shea
r Flow
sGo
veno
rs Le
cture
Hall
Chair
ed by
: K. C
ASPE
R and
K. G
RANL
UND,
Air F
orce R
esea
rch La
borat
ory09
00 hr
sAIA
A-201
5-293
7Re
lation
ship
betw
een
Acou
stic
Tone
s and
Flow
Stru
cture
in
Trans
onic
Recta
ngula
r Cav
ity Fl
owJ.
Wagn
er, K.
Casp
er, S
. Bere
sh, B
. Prue
tt,
R. Sp
illers,
J. H
enflin
g, Sa
ndia
Natio
nal
Labo
ratori
es, A
lbuqu
erque
, NM
0930
hrs
AIAA-2
015-2
938
Moda
l Dec
ompo
sition
of P
ressu
re
Data
in Ca
vity F
lows
K. Ca
sper,
S. A
runaja
tesan
, San
dia
Natio
nal L
abora
tories
, Albu
querq
ue, N
M
1000
hrs
AIAA-2
015-2
939
Comp
ariso
n of H
igh-O
rder
and
Low-
Orde
r Meth
ods f
or La
rge-E
ddy
Simula
tion o
f a Co
mpres
sible
Shea
r La
yer
M. M
ankb
adi, J
. DeB
onis,
N. Ge
orgiad
is, NA
SA Gl
enn R
esearc
h Cen
ter, C
levela
nd, O
H
1030
hrs
AIAA-2
015-2
940
Redu
ced O
rder
Mod
eling
of
a Diel
ectri
c Bar
rier D
ischa
rge
Cont
rolle
d She
ar La
yer u
sing
Minim
um B
asis
Rota
tions
J. Ch
abot,
E. Ca
raball
o, Mi
ami U
nivers
ity,
Oxfor
d, OH
; J. L
ittle,
Unive
rsity
of Ari
zona
, Tu
cson,
Tucso
n, AZ
1100
hrs
AIAA-2
015-2
941
Shea
r-Thin
ning P
rope
rties
of B
lood
in La
rge A
rterie
sF.
Kok,
R. My
ose,
K. Ho
ffman
n, W
ichita
St
ate U
nivers
ity, W
ichita
, KS
Wedn
esda
y, 24
June
201
517
6-MA
O-5
Emer
ging M
ethod
s IMa
drid
Chair
ed by
: E. W
INER
, Iow
a Stat
e Univ
ersity
and V
. LI,
Boein
g Eng
ineeri
ng O
perat
ions &
Tech
nolog
y09
00 hr
sAIA
A-201
5-294
2Mu
ltidisc
iplina
ry D
esign
Spac
e Ex
plora
tion
Using
Add
itive
Manu
factu
ring a
nd R
apid
Prot
otyp
e Te
sting
A. Fri
edma
n, P.
Raj, V
irgini
a Poly
techn
ic Ins
titute
and S
tate U
nivers
ity, B
lacks
burg,
VA
; E. A
lyana
k, Air
Force
Rese
arch
Labo
ratory
, Wrig
ht-Pa
tterso
n AFB
, OH
0930
hrs
AIAA-2
015-2
943
Arno
ldi-b
ased
Samp
ling f
or H
igh-
dimen
siona
l Opt
imiza
tion
using
Im
perfe
ct Da
taJ.
Hicke
n, A.
Ashle
y, Re
nsse
laer
Polyt
echn
ic Ins
titute,
Troy
, NY
1000
hrs
AIAA-2
015-2
944
Multi-
Doma
in Di
versi
ty
Pres
erva
tion
to M
itigat
e Par
ticle
Stagn
ation
and E
nable
Bett
er
Pare
to Co
vera
ge in
Mixe
d-Di
screte
Pa
rticle
Swar
m Op
timiza
tion
W. To
ng, S
yracu
se U
nivers
ity, S
yracu
se,
NY; S
. Cho
wdhu
ry, A.
Mes
sac,
Missi
ssipp
i St
ate U
nivers
ity, M
ississ
ippi S
tate,
MS
1030
hrs
AIAA-2
015-2
945
An M
DO ad
visor
y sys
tem su
ppor
ted
by k
nowl
edge
-bas
ed te
chno
logies
M. H
oogre
ef, G
. La R
occa
, Delf
t Univ
ersity
of
Tech
nolog
y, De
lft, Th
e Neth
erlan
ds
Wedn
esda
y, 24
June
201
517
7-MS
T-7Fli
ght S
imula
tion
Trave
rtine
Chair
ed by
: K. B
ILIMO
RIA09
00 hr
sAIA
A-201
5-294
6Mo
tion
Para
meter
Selec
tion
for
Fligh
t Sim
ulato
rsK.
Bilim
oria,
S. Re
ardon
, NAS
A Ame
s Re
searc
h Cen
ter, M
offett
Field
, CA
0930
hrs
AIAA-2
015-2
947
AVES
SDK:
Brid
ging t
he G
ap
betw
een
Simula
tor a
nd Fl
ight
Syste
ms D
esign
erT.
Gerla
ch, U
. Dura
k, Ge
rman
Aeros
pace
Ce
nter (
DLR)
, Brau
nsch
weig,
Germ
any
1000
hrs
AIAA-2
015-2
948
Mode
l-Bas
ed Te
sting
for O
bjecti
ve
Fideli
ty Ev
aluat
ion of
Engin
eerin
g an
d Res
earch
Fligh
t Sim
ulato
rsU.
Dura
k, Ge
rman
Aeros
pace
Cente
r (D
LR),
Brau
nsch
weig,
Germ
any;
A. Sc
hmidt
, T. P
awlet
ta, U
nivers
ity of
W
ismar,
Wism
ar, G
erman
y
86
Wedn
esda
y, 24
June
201
517
8-MS
T-8Co
mput
ation
al Me
thod
s for
Fluid
Dyn
amics
and H
eat T
rans
fer S
imula
tions
Wyeth
Chair
ed by
: M. K
OKAL
Y an
d B. J
AFFR
EZIC
0900
hrs
AIAA-2
015-2
949
Aero
dyna
mics
Fligh
t Mec
hanic
s Ap
proa
ch on
Comp
act D
omain
s for
Ai
r Veh
icle S
epar
ation
B. Ja
ffrez
ic, M
. Rue
tten,
H. Ro
sema
nn,
Germ
an Ae
rospa
ce Ce
nter (
DLR)
, Gö
ttinge
n, Ge
rman
y
0930
hrs
AIAA-2
015-2
950
Inve
stiga
tion
of th
e effe
ct of
grid
size o
n ex
terna
l sto
re se
para
tion
trajec
tory
usin
g CFD
A. Os
man,
A. Aly
, Cair
o Univ
ersity
, Cair
o, Eg
ypt;
I. El
baial
y, Qa
tar U
nivers
ity, D
oha,
Qatar
; O. A
bdell
atif,
Banh
a Univ
ersity
, Ca
iro, E
gypt;
E. Kh
alil, C
airo U
nivers
ity,
Cairo
, Egy
pt
1000
hrs
AIAA-2
015-2
951
Stren
gth An
alysis
and O
ptimi
zatio
n Tec
hniqu
e for
Therm
al Pr
otecti
on
Syste
m us
ing 3
Dime
nsion
al Ele
ment
Mode
lW.
Yan,
Aviat
ion In
dustr
y Corp
oratio
n of
China
(AVIC
), Be
ijing,
China
; X. L
uo, A
viatio
n Ind
ustry
Corpo
ration
of Ch
ina (A
VIC),
Chen
gdu,
China
; D. C
ui, Av
iation
Indu
stry
Corpo
ration
of Ch
ina (A
VIC),
Beijin
g, Ch
ina
1030
hrs
AIAA-2
015-2
952
Ther
mal s
imula
tion
and
expe
rimen
ts fo
r a st
rato
sphe
ric
ballo
on go
ndola
Q. Li
u, Ch
inese
Acad
emy o
f Scie
nces
, Be
ijing,
China
; Z. L
i, Y. Y
ang,
J. Ca
i, Ac
adem
y of O
pto-El
ectro
nics,
Chine
se
Acad
emy o
f Scie
nces
, Beij
ing, C
hina
1100
hrs
AIAA-2
015-2
953
Real
Time M
ultipl
e Fide
lity P
hysic
s Ba
sed S
imula
tion
of A
ircra
ft En
viron
ment
al Co
ntro
l Sys
temB.
Sas
anap
uri, A
NSYS
, Inc
., Pu
ne, I
ndia
Wedn
esda
y, 24
June
201
517
9-NW
-6
0900
- 09
30 h
rsNe
twor
king C
offe
e Bre
akCh
antill
y Ball
room
East
Wedn
esda
y, 24
June
201
518
0-PD
L-8/A
PA-2
0Pla
sma A
erod
ynam
ics &
Flow
Cont
rol I
VSte
mmon
s CCh
aired
by: T
. DOU
VILLE
, TLG
Aeros
pace
, LLC
.09
00 hr
sAIA
A-201
5-295
4Pla
sma L
amina
r-Sep
arat
ion-
Bubb
le Co
ntro
l ove
r Airf
oil at
Low
Reyn
olds N
umbe
rsX.
Men
g, X.
Yan,
H. H
u, No
rthwe
stern
Polyt
echn
ical U
nivers
ity, X
i’an,
China
; F.
Liu, S
. Luo
, Univ
ersity
of Ca
liforni
a, Irv
ine,
Irvine
, CA
0930
hrs
AIAA-2
015-2
955
Pres
sure
s ove
r a Co
nical
Fore
body
un
der R
epeti
tive N
anos
econ
d Puls
e SD
BD A
ctuat
ions
D. Zh
ang,
X. M
eng,
J. Wa
ng,
North
weste
rn Po
lytec
hnica
l Univ
ersity
, Xi’
an, C
hina;
F. Liu
, S. L
uo, U
nivers
ity of
Ca
liforni
a, Irv
ine, L
os An
geles
, CA
1000
hrs
AIAA-2
015-2
956
Starti
ng Fl
ow by
Rep
etitiv
e Na
nose
cond
Puls
ed D
BD A
ctuat
ion
at M
icros
econ
ds an
d Milli
seco
nds i
n Qu
iesce
nt A
irH.
Hu,
H. Li
, X. M
eng,
J. Wa
ng,
North
weste
rn Po
lytec
hnica
l Univ
ersity
, Xi’
an, C
hina;
F. Liu
, S. L
uo, U
nivers
ity of
Ca
liforni
a, Irv
ine, L
os An
geles
, CA
1030
hrs
AIAA-2
015-2
957
Multi-
Inpu
t Gen
etic A
lgorit
hm fo
r Ex
perim
enta
l Opt
imiza
tion
of th
e Re
atta
chme
nt D
owns
tream
of a
Back
ward
-Facin
g-Ste
p with
Surfa
ce
Plasm
a Actu
ator
N. B
enard
, Nati
onal
Cente
r for
Scien
tific
Rese
arch (
CNRS
), Fu
turos
cope
, Fran
ce; J
. Po
ns-Pr
at, J.
Peria
ux, G
. Bug
eda,
CIMNE
, Ba
rcelon
a, Sp
ain; J
. Bon
net,
E. Mo
reau,
Natio
nal C
enter
for S
cienti
fic Re
searc
h (C
NRS)
, Futu
rosco
pe, F
rance
1100
hrs
AIAA-2
015-2
958
The E
ffect
of P
lasma
Clou
ds on
Ae
rody
nami
c Per
form
ance
of
Subs
onic/
Supe
rsonic
Inlet
sD.
Mei,
Aviat
ion In
dustr
y Corp
oratio
n of
China
(AVIC
), Sh
enya
ng, C
hina;
Y. Fa
n, C.
Jiang
, Beih
ang U
nivers
ity, B
eijing
, Chin
a
Wedn
esda
y, 24
June
201
518
1-PD
L-9/T
P-8
Plasm
a Diag
nosti
cs II
Miro
Chair
ed by
: N. H
ARAD
A, Na
gaok
a Univ
ersity
of Te
chno
logy a
nd J.
BUR
T, Un
iversa
l Tec
hnolo
gy Co
rporat
ion09
00 hr
sAIA
A-201
5-295
9Pla
nar T
wo-P
hoto
n LIF
Me
asur
emen
ts of
Ato
mic S
pecie
s in
a High
-Temp
erat
ure I
nduc
tively
Co
uple
Plasm
a Env
ironm
ent
J. Me
yers,
D. F
letch
er, U
nivers
ity of
Ve
rmon
t, Bu
rlingto
n, Bu
rlingto
n, VT
0930
hrs
AIAA-2
015-2
960
Parti
cle Va
poriz
ation
Veloc
imetr
y fo
r LPG
Diff
usion
Flam
esL.
Tolom
elli, T
echn
ologic
al Ins
titute
of Ae
ronau
tics (
ITA),
São J
osé d
os Ca
mpos
, Br
azil
1000
hrs
AIAA-2
015-2
961
Inve
stiga
tion
of N
on-Eq
uilibr
ium
Nitro
gen
Plasm
asA.
Lutz,
D. F
letch
er, U
nivers
ity of
Verm
ont,
Burlin
gton,
Burlin
gton,
VT
1030
hrs
AIAA-2
015-2
962
Hybr
id fs/
ps co
here
nt an
ti-Sto
kes
Rama
n sca
tterin
g in
a non
-eq
uilibr
ium en
viron
ment
initia
ted
by a
ns la
ser s
park
C. De
dic, J
. Mich
ael, T
. Mey
er, Io
wa S
tate
Unive
rsity,
Ames
, IA
1100
hrs
AIAA-2
015-2
963
Non-
Equil
ibrium
Ana
lysis
of
Emiss
ion Sp
ectro
scopy
Dat
a Tak
en
in th
e Fre
estre
am of
the N
ASA
IHF
Arc J
et Fa
cility
M. W
inter,
C. S
riniva
san,
R. Ch
arnigo
, Un
iversi
ty of
Kentu
cky,
Lexin
gton,
Lexin
gton,
KY
1130
hrs
AIAA-2
015-2
964
Quan
titat
ive M
easu
reme
nts o
f Ele
ctron
Num
ber D
ensit
y and
Th
resh
old fo
r Las
er In
duce
d Br
eakd
own
in Ai
rL.
Su, Y
. Wu,
J. Sa
wyer,
Z. Zh
ang,
Unive
rsity
of Te
nnes
see,
Knox
ville,
Kn
oxvil
le, TN
87
Wedn
esda
y, 24
June
201
518
2-TP
-9Ae
roth
ermo
dyna
mics
IIRo
setta
Chair
ed by
: A. M
ARTIN
, Univ
ersity
of Ke
ntuck
y09
00 hr
sAIA
A-201
5-296
5Sh
ock
Radia
tion
Tests
for S
atur
n an
d Ura
nus E
ntry
Pro
bes
B. Cr
uden
, D. B
ogda
noff,
ERC,
Inc.,
Moffe
tt Fie
ld, CA
0930
hrs
AIAA-2
015-2
966
Heat
Tran
sfer M
easu
reme
nts o
n th
e Af
terbo
dy of
Sphe
res i
n Hy
perso
nic
Free
-Fligh
t in
Air a
nd Ca
rbon
Di
oxide
M. W
ilder,
NAS
A Ame
s Res
earch
Cente
r, Mo
ffett
Field,
CA; D
. Bog
dano
ff, D
. Sa
unde
rs, ER
C, Inc
., Mo
ffett
Field,
CA
1000
hrs
AIAA-2
015-2
967
Shap
e Opt
imiza
tion
of a
Blun
t Bo
dy in
Rea
cting
Hyp
erso
nic fl
ow
in Th
erma
l Non
-Equil
ibrium
for
Redu
cing B
oth
Drag
and H
eat
Trans
fer
E. Zis
hka,
R. Ag
arwal,
Was
hingto
n Un
iversi
ty in
St. L
ouis,
St.
Louis
, MO
1030
hrs
AIAA-2
015-2
968
Fugin
e cyc
le th
eory
: pre
dictin
g high
ef
ficien
cy of
the s
uper
multij
et-co
nver
genc
e eng
ine w
orkin
g fro
m sta
rtup t
o hyp
erso
nic sc
ram
mode
K. Na
itoh,
Y. Ta
naka
, T. T
amura
, T.
Okam
oto, Y
. Noji
ma, K
. Yam
agish
i, Wa
seda
Univ
ersity
, Shin
juku,
Japa
n
Wedn
esda
y, 24
June
201
518
3-F3
60-5
09
30 -
1200
hrs
NACA
to N
ASA:
Emba
rking
on th
e Nex
t 100
Year
s of E
xcell
ence
and I
nnov
ation
in A
eron
autic
s and
Bey
ond
Gran
d Ball
room
E
Mode
rator:
Robe
rt Pe
arce,
Direc
tor, S
trateg
y, Arc
hitec
ture &
Analy
sis, A
erona
utics
Rese
arch M
ission
Dire
ctorat
e, NA
SA H
eadq
uarte
rs
Pan
elists
:Da
vid B
owles
Cente
r Dire
ctor (
Actin
g)NA
SA La
ngley
Rese
arch C
enter
Thom
as Ed
ward
sDe
puty
Cente
r Dire
ctor
NASA
Ames
Rsea
rch Ce
nter
Jane
t Kav
andi
Depu
ty Dir
ector
NASA
Glen
n Res
earch
Cente
r
David
McB
ride
Cente
r Dire
ctor
NASA
Arms
trong
Fligh
t Res
earch
Cente
r
Jaiw
on Sh
inAs
sociat
e Adm
inistra
tor, A
erona
utics
Resea
rch M
ission
Direc
torate
NASA
Hea
dqua
rters
Wedn
esda
y, 24
June
201
518
4-LN
CH-2
12
30 -
1400
hrs
Lunc
heon
in th
e Exp
ositio
n Ha
llCh
antill
y Ball
room
East
A tick
et is
requir
ed an
d inc
luded
in th
e con
feren
ce re
gistra
tion f
ee w
here
indica
ted.
Wedn
esda
y, 24
June
201
518
5-AA
-26
Comb
ustio
n No
iseFle
ur-d
e-lis
BCh
aired
by: J
. MEN
DOZA
, Unit
ed Te
chno
logies
Rese
arch C
enter
1400
hrs
AIAA-2
015-2
969
On th
e spe
ctrum
of co
mbus
tion
noise
C. Ta
m, Fl
orida
Stat
e Univ
ersity
, Ta
llaha
ssee,
FL
1430
hrs
AIAA-2
015-2
970
Mode
lling o
f com
busti
on n
oise
spec
trum
using
temp
oral
corre
lation
s of h
eat r
eleas
e rat
e fro
m tu
rbule
nt pr
emixe
d flam
esY.
Liu, U
nivers
ity of
Surr
ey, G
uildfo
rd,
Unite
d King
dom;
T. Ec
hekk
i, Nort
h Caro
lina
State
Univ
ersity
, Rale
igh, N
C
1500
hrs
AIAA-2
015-2
971
Nume
rical
inves
tigat
ion of
co
mbus
tion
noise
gene
ratio
n in
a fu
ll ann
ular c
ombu
stion
cham
ber
T. Liv
ebard
on, C
ERFA
CS, T
oulou
se, F
rance
; S.
More
au, U
nivers
ity of
She
rbroo
ke,
Sherb
rooke
, Can
ada;
T. Po
insot,
CERF
ACS,
To
ulous
e, Fra
nce;
E. Bo
uty, T
urbom
eca,
Borde
s, Fra
nce
1530
hrs
AIAA-2
015-2
972
Trans
fer F
uncti
ons o
f Aco
ustic
, En
tropy
and V
ortic
ity W
aves
in
an A
nnula
r Mod
el Co
mbus
tor a
nd
Nozz
le fo
r the
Pre
dictio
n of
the
Ratio
Betw
een
Indir
ect a
nd D
irect
Comb
ustio
n No
iseW.
Ullri
ch, T
. Satt
elmay
er, Te
chnic
al Un
iversi
ty of
Munic
h, Ga
rching
, Germ
any
1600
hrs
AIAA-2
015-2
973
Effic
ient F
ull 3
D Tu
rbule
nt
Comb
ustio
n No
ise Si
mulat
ion B
ased
on
Stoc
hasti
c Sou
nd So
urce
sF.
Grim
m, G
erman
Aeros
pace
Cente
r (D
LR),
Stutt
gart,
Germ
any;
R. Ew
ert, J
. Die
rke, G
erman
Aeros
pace
Cente
r (DL
R),
Brau
nsch
weig,
Germ
any;
B. N
oll, M
. Aig
ner, G
erman
Aeros
pace
Cente
r (DL
R),
Stutt
gart,
Germ
any
1630
hrs
AIAA-2
015-2
974
A 2D
-axis
ymme
tric a
nalyt
ical
mode
l for
the e
stima
tion
of in
direc
t co
mbus
tion
noise
in n
ozzle
flow
sJ.
Zhen
g, M.
Huet,
ONE
RA, C
hâtillo
n, Fra
nce;
A. Gia
uque
, Nati
onal
Cente
r for S
cienti
fic
Resea
rch (C
NRS)
, Ecul
ly, Fra
nce; F.
Cléro
, ON
ERA,
Châti
llon, F
rance;
S. Du
cruix,
Nati
onal
Cente
r for S
cienti
fic Re
search
(CNR
S),
Châte
nay-M
alabry
, Fran
ce
88
Wedn
esda
y, 24
June
201
518
6-AA
-27
Arra
ys M
ethod
Pan
el Se
ssion
Fleur
-de-
lis A
Chair
ed by
: C. B
AHR,
NASA
-Lang
ley Re
searc
h Cen
ter14
00 hr
sAIA
A-201
5-297
5De
velop
ment
of N
ew W
all-m
ount
ed
and S
trut-m
ount
ed P
hase
d Mi
croph
one A
rrays
for A
cous
tic
Meas
urem
ents
in Clo
sed T
est-
secti
on W
ind Tu
nnels
W. H
orne,
N. B
urnsid
e, NA
SA Am
es
Rese
arch C
enter
, Moff
ett Fi
eld, C
A
1430
hrs
AIAA-2
015-2
976
Deco
rrelat
ion of
Aco
ustic
Wav
e Pr
opag
ation
thro
ugh
the S
hear
La
yer i
n Op
en Je
t Wind
Tunn
elD.
Erns
t, C.
Speh
r, T. B
erkefe
ld, G
erman
Ae
rospa
ce Ce
nter (
DLR)
, Gött
ingen
, Ge
rman
y
1500
hrs
AIAA-2
015-2
977
An A
ppro
ach
to Es
timat
e the
Re
liabil
ity of
Micr
opho
ne A
rray
Meth
ods
G. H
erold,
E. S
arrad
j, Bran
denb
urg
Unive
rsity
of Te
chno
logy,
Cottb
us,
Germ
any
1530
hrs
AIAA-2
015-2
978
Pleth
arra
ys fo
r Aer
oaco
ustic
Ph
ased
Arra
y App
licat
ions
J. Un
derbr
ink, T
he B
oeing
Comp
any,
Seatt
le, W
A
1600
hrs
AIAA-2
015-2
979
Estim
ating
the s
ound
powe
r ra
diated
by a
nozz
le-ba
sed s
ource
in
a tes
t cell
usin
g a ph
ased
arra
yB.
Teste
r, K. H
ollan
d, Un
iversi
ty of
South
ampto
n, So
utham
pton,
Unite
d Kin
gdom
1630
Discu
ssion
Wedn
esda
y, 24
June
201
518
7-AA
-28
Open
Rot
or II
Inve
rnes
sCh
aired
by: W
. DEV
ENPO
RT, V
irgini
a Tec
h14
00 hr
sAIA
A-201
5-298
0Op
en-R
otor
Nois
e Asse
ssmen
t with
CF
D/CA
A Ch
aining
A. Ch
elius
, T. L
e Garr
ec, D
. Minc
u, ON
ERA,
Châti
llon,
Franc
e
1430
hrs
AIAA-2
015-2
981
Flow
Disto
rtion
and N
oise P
rodu
ced
by a
Thru
sting
Rot
or In
gesti
ng a
Plana
r Tur
bulen
t Bou
ndar
y Lay
erD.
Wisd
a, H.
Murr
ay, W
. Alex
ande
r, M.
Nelso
n, W.
Dev
enpo
rt, V
irgini
a Poly
techn
ic Ins
titute
and S
tate U
nivers
ity, B
lacks
burg,
VA
; S. G
legg,
Florid
a Atla
ntic U
nivers
ity,
Boca
Raton
, FL
1500
hrs
AIAA-2
015-2
982
Comp
utat
ion of
Rot
or N
oise
Gene
ratio
n in
Grid
Turb
ulenc
e Us
ing La
rge-
Eddy
Simu
lation
J. Wa
ng, K
. Wan
g, M.
Wan
g, Un
iversi
ty of
Notre
Dam
e, No
tre D
ame,
IN
1530
hrs
AIAA-2
015-2
983
Broa
dban
d nois
e for
rota
ting
blade
s: an
alysis
of ac
celer
ation
ef
fects
in th
e tim
e and
freq
uenc
y do
mains
S. S
inayo
ko, U
nivers
ity of
Sou
thamp
ton,
South
ampto
n, Un
ited K
ingdo
m
1600
hrs
AIAA-2
015-2
984
A 3D
analy
tical
appr
oach
for O
pen
roto
r Blad
e Vor
tex In
terac
tion(
BVI)
tona
l nois
eS.
More
au, M
. Qua
glia,
Sherb
rooke
Un
iversi
ty, S
herbr
ooke
, Can
ada;
R. Fe
rnand
o, Sa
fran G
roup,
Moiss
y-Cram
ayel,
Fra
nce
1630
hrs
AIAA-2
015-2
985
Analy
tical
Pred
iction
of th
e Pylo
n-Wa
ke Ef
fect o
n the
Tona
l Nois
e ra
diated
by th
e Fro
nt-Ro
tor of
CROR
Pr
opuls
ion Sy
stems
N. Ja
ouan
i, Sog
eti Hi
gh Te
ch, Is
sy Les
Mo
ulinea
ux, F
rance;
M. R
oger,
École
Centr
ale
de Ly
on, L
yon,
France
; T. N
odé-L
anglo
is, Air
bus,
Toulou
se, Fr
ance;
G. Se
rre, S
ogeti
High
Tec
h, Iss
y Les
Moulin
eaux
, Fran
ce
1700
hrs
AIAA-2
015-2
986
Comp
ariso
n of
roto
r nois
e me
asur
emen
t res
ults i
n lar
ge-sc
ale
and s
mall-
scale
anec
hoic
facil
ities
I. Be
lyaev
, V. K
opiev
, R. S
kvort
sov,
I. Pa
nkrat
ov, T
sAGI
, Mos
cow,
Russi
a; V.
Titare
v, Ru
ssian
Acad
emy o
f Scie
nces
, Mo
scow,
Russi
a; M.
Zayts
ev, T
sAGI
, Mo
scow,
Russi
a
Wedn
esda
y, 24
June
201
518
8-AA
-29
Airfr
ame N
oise I
IILa
lique
Chair
ed by
: S. N
OELTI
NG, E
XA14
00 hr
sAIA
A-201
5-298
7An
Asse
ssmen
t of F
lap an
d Main
La
nding
Gea
r Nois
e Aba
temen
t Co
ncep
tsM.
Khorr
ami, W
. Hum
phrey
s, D.
Locka
rd,
NASA
Lang
ley Re
search
Cente
r, Ham
pton,
VA
1430
hrs
AIAA-2
015-2
988
Evalu
ation
of A
irfra
me N
oise
Redu
ction
Conc
epts
via Si
mulat
ions
Using
a La
ttice
Bolt
zman
n Ap
proa
chE.
Fares
, D. C
asali
no, E
xa G
mbH,
St
uttga
rt, G
erman
y; M.
Khorr
ami, N
ASA
Lang
ley Re
searc
h Cen
ter, H
ampto
n, VA
1500
hrs
AIAA-2
015-2
989
A Co
mpar
ative
Stud
y of S
imula
ted
and m
easu
red G
ear-F
lap Fl
ow
Inter
actio
nM.
Khorr
ami, N
ASA L
angle
y Rese
arch C
enter
, Ha
mpton
, VA;
R. Mi
neck,
Self,
Yorkt
own,
VA; E
. Fare
s, Ex
a Gmb
H, Stu
ttgart
, Germ
any;
C. Ya
o, L.
Jenkin
s, NA
SA La
ngley
Resea
rch
Cente
r, Ham
pton,
VA
1530
hrs
AIAA-2
015-2
990
Comp
ariso
n of
Comp
utat
ional
and
Expe
rimen
tal M
icrop
hone
Arra
y Re
sults
for a
n 18
%-Sc
ale A
ircra
ft Mo
del
D. Lo
ckard
, W. H
umph
reys,
M. Kh
orram
i, NA
SA La
ngley
Rese
arch C
enter
, Ham
pton,
VA; E
. Fare
s, D.
Casa
lino,
Exa G
mbH,
St
uttga
rt, G
erman
y; P.
Rave
tta, A
VEC,
Inc.,
Black
sburg
, VA
1600
hrs
AIAA-2
015-2
991
Char
acter
izatio
n of
Flap
Edge
Nois
e Ra
diatio
n fro
m a H
igh-Fi
delity
Ai
rfram
e Mod
elW.
Hum
phrey
s, M.
Khorr
ami, D
. Loc
kard,
D.
Neu
hart,
C. B
ahr, N
ASA L
angle
y Re
searc
h Cen
ter, H
ampto
n, VA
1630
hrs
AIAA-2
015-2
992
On th
e Con
necti
on be
twee
n Fla
p Sid
e-Ed
ge N
oise a
nd Ti
p Vor
tex
Dyna
mics
D. Ca
salin
o, E.
Fares
, B. D
uda,
A. Ha
zir,
Exa G
mbH,
Stut
tgart,
Germ
any;
M.
Khorr
ami, N
ASA L
angle
y Res
earch
Cente
r, Ha
mpton
, VA
1700
hrs
AIAA-2
015-2
993
Simula
tions
of LA
GOON
land
ing-
gear
nois
e usin
g Lat
tice B
oltzm
ann
Solve
rA.
Seng
issen
, J. G
iret,
Airbu
s, To
ulous
e, Fra
nce;
C. Co
reixa
s, J.
Bous
suge
, CE
RFAC
S, To
ulous
e, Fra
nce
89
Wedn
esda
y, 24
June
201
518
9-AA
-30
Jet N
oise M
easu
reme
nts I
IOb
elisk
ACh
aired
by: D
. JUV
E, Ec
ole Ce
ntrale
de Ly
on14
00 hr
sAIA
A-201
5-299
4Du
al-pla
ne, ti
me-re
solve
d, ste
reo PI
V for
wav
epac
ket e
ducti
on in
a tur
bulen
t su
bson
ic jet
V. Jau
net, P
. Brau
d, F. B
oisson
neau
, P. Jo
rdan,
Natio
nal C
enter
for S
cienti
fic Re
search
(C
NRS)
, Poit
iers,
France
; A. C
avalie
ri, Tec
hnolo
gical
Institu
te of
Aeron
autics
(ITA)
, Sã
o José
dos C
ampo
s, Bra
zil
1430
hrs
AIAA-2
015-2
995
Adap
tatio
n of
the A
zimut
hal
Deco
mpos
ition
Tech
nique
to Je
t No
ise M
easu
erem
ents
of an
Airc
raft
Engin
e in
the G
roun
d Tes
tsV.
Kopie
v, I.
Belya
ev, G
. Fara
noso
v, M.
Zayts
ev, T
sAGI
, Mos
cow,
Russi
a; A.
Aleks
entse
v, Y.
Berse
nev,
OJSC
Av
iadvig
atel, P
erm, R
ussia
; et a
l.
1500
hrs
AIAA-2
015-2
996
On th
e sys
temat
ic er
ror i
n me
asur
emen
ts of
jet n
oise fl
ight
effe
cts u
sing o
pen
jet w
ind tu
nnels
U. M
ichel,
CFD
Softw
are G
mbH,
Berl
in,
Germ
any
1530
hrs
AIAA-2
015-2
997
Role
of N
ozzle
’s Pr
oxim
ity to
Ple
num
Cham
bers
or O
ther
Non
-lin
e-of
-sigh
t Dev
ices o
n Me
asur
ed
Jet N
oise
A. Ka
ron, D
. Dick
ey, K
. Ahu
ja, G
eorgi
a Ins
titute
of Te
chno
logy,
Atlan
ta, G
A
1600
hrs
AIAA-2
015-2
998
Scatte
ring o
f tur
bulen
t-jet
wave
pack
ets by
a sw
ept tr
ailing
edge
S. Pia
ntanid
a, V.
Jaune
t, P. J
ordan
, J. H
uber,
Na
tiona
l Cen
ter fo
r Scie
ntific
Resea
rch (C
NRS)
, Po
itiers,
Fran
ce; A.
Cava
lieri, T
echno
logica
l Ins
titute
of Ae
ronau
tics (I
TA), S
ão Jo
sé
dos C
ampo
s, Bra
zil; W
. Wolf
, Univ
ersity
of
Camp
inas,
Camp
inas,
Brazil
1630
hrs
AIAA-2
015-2
999
Inve
stiga
ting t
he fe
edba
ck pa
th in
a j
et-su
rface
reso
nant
inter
actio
nK.
Zama
n, A.
Faga
n, J.
Bridg
es, C
. Brow
n, NA
SA G
lenn R
esea
rch Ce
nter, C
levela
nd,
OH
Wedn
esda
y, 24
June
201
519
0-AC
D-5
Desig
n of
Unc
onve
ntion
al Ai
rcraf
t Con
figur
ation
sMo
rocco
Chair
ed by
: M. L
OGAN
, NAS
A Lan
gley R
esea
rch Ce
nter
1400
hrs
AIAA-2
015-3
000
An In
vesti
gatio
n int
o the
Des
ign of
an
Effic
ient I
n Gr
ound
Effe
ct Fly
ing
Vehic
le Pla
nfor
mV.
Miroc
hnitc
henk
o, T.
Taka
hash
i, Ariz
ona
State
Univ
ersity
, Tem
pe, A
Z
1430
hrs
AIAA-2
015-3
001
Adva
nced
Gen
eral
Aviat
ion Co
ncep
t Stu
dy fo
r a R
oada
ble A
ircra
ftD.
Lim,
C. Ju
stin,
D. M
avris
, Geo
rgia
Institu
te of
Tech
nolog
y, Atl
anta,
GA
1500
hrs
AIAA-2
015-3
002
Morp
hing S
trateg
y Des
ign fo
r Va
riable
-Wing
Airc
raft
R. Sh
i, J. P
eng,
Tsing
hua U
nivers
ity,
Beijin
g, Ch
ina
1530
hrs
AIAA-2
015-3
003
A Me
thod
ology
for M
ulti-
Disci
plina
ry A
nalys
is of
the B
ox
Wing
Conc
ept
I. Ro
y Sala
m, C.
Bil,
RMIT
Unive
rsity,
Me
lbourn
e, Au
strali
a
1600
hrs
AIAA-2
015-3
004
The H
oops
on th
e Way
to
a Sup
erso
nic B
usine
ss Je
t (P
erfo
rman
ce D
river
s for
a Co
mmer
cially
Viab
le Pr
oduc
t)L.
Gonz
alez-L
inero,
Embry
-Ridd
le Ae
ronau
tical
Unive
rsity,
Day
tona B
each
, FL
Wedn
esda
y, 24
June
201
519
1-AM
T-11/
GT-1
1Gr
ound
Test
Facil
ity Im
prov
emen
ts II
Obeli
sk B
Chair
ed by
: R. R
HEW,
NAS
A-Lan
gley R
esea
rch Ce
nter a
nd J.
HOP
F, Ae
rospa
ce Te
sting
Allia
nce
1400
hrs
AIAA-2
015-3
005
Lyap
unov
-Bas
ed N
onlin
ear C
ontro
l of
Wind
Tunn
el Su
perso
nic N
ozzle
Co
ntou
rM.
Sad
raey,
Danie
l Web
ster C
olleg
e, Na
shua
, NH
1430
hrs
AIAA-2
015-3
006
Deve
lopme
nt an
d Dem
onstr
ation
of
A Co
ntinu
ous B
eta Sw
eep T
est &
An
alysis
Tech
nique
(CBS
TAT)
Rig
K. Xie
, F. W
ang,
N. Ch
en, L
. Che
n, Q.
Sh
en, C
hina A
cade
my of
Aeros
pace
Ae
rodyn
amics
, Beij
ing, C
hina
1500
hrs
AIAA-2
015-3
007
Wind
Tunn
el Tes
ting o
f Var
iable
Camb
er Co
mplia
nt Wi
ng w
ith M
ultipl
e Lo
ad Ce
ll Test
Fixtu
reL.
Zienta
rski, C
. Mark
s, Un
iversit
y of D
ayton
, Da
yton,
OH; J
. Joo
, Air F
orce R
esearc
h La
borat
ory, W
right-
Patte
rson A
FB, O
H
1530
hrs
AIAA-2
015-3
008
Comp
ariso
n of
Free
jet D
ata
betw
een
a Con
tour
ed an
d Con
ical
Nozz
le in
the A
EDC H
1 Fa
cility
G. H
ammo
ck, A
rnold
Engin
eerin
g De
velop
ment
Comp
lex, A
rnold
AFB,
TN
1600
hrs
Oral
Prese
ntatio
nOv
ervie
w of
Unc
erta
inty A
nalys
is Ac
tivitie
s at N
ASA
Glen
n’s
Aero
prop
ulsion
Facil
ities
J. St
ephe
ns, E
. Hub
bard,
NAS
A Lan
gley
Rese
arch C
enter
, Ham
pton,
VA
1630
hrs
AIAA-2
015-3
009
Reac
tivat
ion of
the N
TF 3
000
Ton
Liquid
Nitr
ogen
Tank
from
Amb
ient
Cond
ition
S. D
unn,
NASA
Lang
ley Re
searc
h Cen
ter,
Hamp
ton, V
A
Wedn
esda
y, 24
June
201
519
2-AM
T-12/
GT-1
2Th
e Imp
act o
f PIV
on A
eros
pace
Tech
nolog
y IEd
elweis
sCh
aired
by: S
. BER
ESH,
San
dia N
ation
al La
borat
ories
and K
. LOW
E, Vir
ginia
Tech
1400
hrs
Oral
Prese
ntatio
nAp
plica
tion
of P
artic
le Im
age
Veloc
imetr
y at N
ASA
for R
otor
craft
Rese
arch
(Inv
ited)
L. Je
nkins
, G. Y
amau
chi, N
ASA L
angle
y Re
searc
h Cen
ter, H
ampto
n, VA
1430
hrs
Oral
Prese
ntatio
nPI
V for
heli
copt
er ae
rody
nami
cs (In
vited
)M.
Raffe
l, Germ
an Ae
rospa
ce Ce
nter
(DLR
), Co
logne
, Germ
any
1500
hrs
Oral
Prese
ntatio
nTim
e-re
solve
d PIV
in th
e buf
fetin
g re
gime o
f ARI
ANE V
(Inv
ited)
F. Sc
arano
, Delf
t Univ
ersity
of Te
chno
logy,
Delft,
The N
etherl
ands
1530
hrs
Oral
Prese
ntatio
nSu
bson
ic Wa
ke Ch
arac
teriza
tion
of
the O
rion
Caps
ule u
sing P
IV in
the
Ames
UPW
T 11-
foot
Wind
Tunn
el (In
vited
)J.
Heine
ck, N
ASA A
mes R
esea
rch Ce
nter,
Moffe
tt Fie
ld, CA
1600
hrs
Oral
Prese
ntatio
nIn
dustr
ial A
pplic
ation
s of P
IV in
JA
XA La
rge-
Scale
Wind
Tunn
els
(Invit
ed)
H. Ka
to, S
. Koik
e, Ja
pan A
erosp
ace
Explo
ration
Agen
cy (J
AXA)
, Tok
yo, J
apan
1630
hrs
Oral
Prese
ntatio
nRe
cent
App
licat
ions o
f PIV
in La
rge
NRC W
ind Tu
nnels
F. de
Sou
za, N
ation
al Re
searc
h Cou
ncil
Cana
da, O
ttawa
, Can
ada
1700
hrs
Oral
Prese
ntatio
nAp
plica
tions
of P
IV m
easu
reme
nts
in th
e ONE
RA la
rge w
ind tu
nnels
(In
vited
)Y.
Mich
ou, O
NERA
, Cha
mbery
, Fran
ce
90
Wedn
esda
y, 24
June
201
519
3-AP
A-21
Trans
onic
& Su
perso
nic A
erod
ynam
icsSte
mmon
s ACh
aired
by: M
. JUR
KOVIC
H, U
S Air
Force
1400
hrs
AIAA-2
015-3
010
Nume
rical
Study
of Co
unter
flowi
ng
Jet E
ffects
on Su
perso
nic Sl
ende
r-Bo
dy Co
nfigu
ratio
nsB.
Venk
atach
ari, N
ation
al Ins
titute
of Ae
rospa
ce, H
ampto
n, VA
; M. M
ullan
e, Un
iversi
ty of
Alaba
ma, B
irming
ham,
Bir
ming
ham,
AL; G
. Che
ng, U
nivers
ity of
Ala
bama
, Tus
caloo
sa, T
usca
loosa
, AL;
C. Ch
ang,
NASA
Lang
ley Re
searc
h Cen
ter,
Hamp
ton, V
A
1430
hrs
AIAA-2
015-3
011
Flow
Phys
ics of
a Th
ree-
Dime
nsion
al Ro
unde
d Con
tour
Bu
mp in
a Ma
ch 1
.3 Su
perso
nic
Free
-stre
amK.
Lo, K
. Kon
tis, U
nivers
ity of
Glas
gow,
Gla
sgow
, Unit
ed Ki
ngdo
m
1500
hrs
AIAA-2
015-3
012
Supe
rsonic
Air
Flows
Aro
und S
ome
Geom
etrica
l Prim
itives
M. Ko
tov, I
. Kryu
kov,
L. Ru
leva,
S.
Solod
ovnik
ov, S
. Surz
hikov
, Rus
sian
Acad
emy o
f Scie
nces
, Mos
cow,
Russi
a
Wedn
esda
y, 24
June
201
519
4-AP
A-22
VSTO
L/ST
OL A
erod
ynam
icsCa
rpen
ter B
allro
omCh
aired
by: M
. CAL
VERT
, U.S
. Arm
y AMR
DEC
1400
hrs
AIAA-2
015-3
013
The L
IFT! P
rojec
t - M
odula
r, Ele
ctric
Verti
cal L
ift Sy
stem
with
Gro
und
Powe
r Teth
erM.
Duff
y, A.
Sama
ritano
, The
Boe
ing
Comp
any,
Ridley
Park,
PA
1430
hrs
AIAA-2
015-3
014
Nume
rical
Inve
stiga
tion
and
Valid
ation
for O
pen
Roto
r Hov
er
Perfo
rman
ceQ.
Zhao
, C. S
heng
, Univ
ersity
of To
ledo,
Toled
o, OH
Wedn
esda
y, 24
June
201
519
5-AP
A-23
Weap
ons A
erod
ynam
ics: M
issile
/Pro
jectile
/Guid
ed-M
unitio
ns, C
arria
ge an
d Sto
re Se
para
tion
IISte
mmon
s BCh
aired
by: K
. DEN
ISSEN
, San
dia N
ation
al La
bs14
00 hr
sAIA
A-201
5-301
5CF
D Ae
rody
nami
c Cha
racte
rizat
ion
of a
High
Man
euve
rabil
ity A
irfra
meC.
Coyle
, U.S
. Milit
ary Ac
adem
y, We
st Po
int, N
Y; S.
Silto
n, Arm
y Res
earch
La
borat
ory, A
berde
en Pr
oving
Grou
nd, M
D
1430
hrs
AIAA-2
015-3
016
Deve
lopme
nt an
d Vali
datio
n of
a RA
NS-b
ased
Aird
rop S
imula
tion
Appr
oach
S. G
eisba
uer, G
erman
Aeros
pace
Cente
r (D
LR),
Brau
nsch
weig,
Germ
any;
H.
Schm
idt, G
erman
Aeros
pace
Cente
r (DL
R),
Göttin
gen,
Germ
any
1500
hrs
AIAA-2
015-3
017
Cavit
y-Sto
re In
terac
tion
unde
r Su
perso
nic Fr
eestr
eam
Cond
itions
J. Me
rrick,
M. Re
eder,
Air F
orce I
nstitu
te of
Tech
nolog
y, W
right-
Patte
rson A
FB, O
H
1530
hrs
AIAA-2
015-3
018
Load
s and
Aco
ustic
s Pre
dictio
n on
De
ploye
d Wea
pons
Bay
Doo
rsE.
Sheta
, R. H
arris,
CFD
Rese
arch
Corpo
ration
, Hun
tsville
, AL;
E. Lu
ke,
Missi
ssipp
i Stat
e Univ
ersity
, Miss
issipp
i St
ate, M
S; L.
Uke
iley,
Unive
rsity
of Flo
rida,
Gaine
sville
, Gain
esvil
le, FL
Wedn
esda
y, 24
June
201
519
6-AS
E-2Ai
rcraf
t Icin
g and
Atm
osph
eric
Haza
rds
Plum
Blos
som
BCh
aired
by: W
. VAU
GHAN
, Willi
am W
Vaug
han C
onsu
ltant
and J
. OW
ENS,
NAS
A (Re
tired)
1400
hrs
AIAA-2
015-3
019
A mo
del f
or in
-fligh
t ice
accre
tion
base
d on
the e
xact
solut
ion of
the
unste
ady S
tefan
prob
lemG.
Gori
, M. Z
occa
, A. G
uardo
ne, T
echn
ical
Unive
rsity
of Mi
lan, M
ilan,
Italy
1430
hrs
AIAA-2
015-3
020
Quas
i-Uns
teady
Icing
Simu
lation
of
an O
scilla
ting A
irfoil
H. Fo
uladi,
McG
ill Un
iversi
ty, M
ontré
al,
Cana
da; C
. Alia
ga, N
ewme
rical
Tech
nolog
ies In
terna
tiona
l, Mon
tréal,
Ca
nada
; W. H
abas
hi, M
cGill
Unive
rsity,
Mo
ntréa
l, Can
ada
1500
hrs
AIAA-2
015-3
021
Conv
ectiv
e Enh
ance
ment
of Ic
ing
Roug
hnes
s Elem
ents
in Sta
gnat
ion
Regio
n Flo
wsM.
Hug
hes,
S. M
cClai
n, Ba
ylor U
nivers
ity,
Waco
, TX;
M. V
argas
, A. B
roeren
, NAS
A Gle
nn Re
searc
h Cen
ter, C
levela
nd, O
H
1530
hrs
AIAA-2
015-3
022
Sens
or Su
ite D
evelo
pmen
t for
a We
athe
r UAV
J. Ha
thawa
y, A.
Avery
, J. J
acob
, Okla
homa
St
ate U
nivers
ity, S
tillwa
ter, O
K
1600
hrs
AIAA-2
015-3
023
Sens
itivity
Ana
lysis
of W
ake V
ortex
Pa
rame
ters M
easu
red b
y Dop
pler
Lidar
T. Mi
saka
, S. O
baya
shi, T
ohok
u Univ
ersity
, Se
ndai,
Japa
n; A.
Step
han,
F. Ho
lzäpfe
l, T.
Gerz,
Germ
an Ae
rospa
ce Ce
nter (
DLR)
, Ob
erpfaf
fenho
fen, G
erman
y
91
Wedn
esda
y, 24
June
201
519
7-AT
IO-1
8AT
M IV
- Ec
onom
ic/Be
nefit
s Ana
lysis
Ming
Chair
ed by
: S. H
ASAN
, LMI
1400
hrs
AIAA-2
015-3
024
Iden
tifyin
g ben
efit m
echa
nisms
for
Next
Gen
techn
ologie
s and
conc
epts
S. La
ndry,
D. P
eng,
Purdu
e Univ
ersity
, We
st La
fayett
e, IN
1430
hrs
AIAA-2
015-3
025
Asse
ssing
Dep
artu
re Ef
ficien
cy
at U
.S. A
irpor
ts: a
Comp
ariso
n of
Me
thod
sS.
Tsao
, J. D
eArm
on, S
. Agb
olosu
-Amiso
n, A.
Maha
shab
de, M
ITRE C
orpora
tion,
McLe
an, V
A
1500
hrs
AIAA-2
015-3
026
Airfar
e Dete
rmina
nts on
the K
anga
roo
Route
(Aus
tralia
-UK M
arke
t): A
Case
Stu
dy of
the I
nflue
nces
of Air
lines,
All
iances
and A
irpor
tsH.
Yang
, Civil
Aviat
ion Fl
ight U
nivers
ity of
Ch
ina, G
uang
han,
China
1530
hrs
AIAA-2
015-3
027
Conc
ept a
nd Be
nefit
s of P
BN-En
abled
Pa
ralle
l App
roac
h Ope
ratio
nsR.
Maye
r, B. C
row, D
. Zon
derva
n, MI
TRE
Corpo
ration
, McLe
an, V
A; J.
Allerd
ice, F
edera
l Av
iation
Admi
nistra
tion,
Peach
tree C
ity, GA
Wedn
esda
y, 24
June
201
519
8-AT
IO-1
9Te
rmina
l & Su
rface
Ope
ratio
ns IV
Milan
Chair
ed by
: R. C
URRA
N, D
elft T
echn
ical U
nivers
ity of
Tech
nolog
y14
00 hr
sAIA
A-201
5-302
8Op
timiza
tion
of P
ush
Back
Time
Wi
ndow
s Tha
t Ens
ure C
onfli
ct Fr
ee
Ramp
Are
a Airc
raft
Trajec
torie
sJ.
Coup
e, D.
Milu
tinov
ic, U
nivers
ity of
Ca
liforni
a, Sa
nta Cr
uz, S
anta
Cruz,
CA; W
. Ma
lik, U
nivers
ity of
Califo
rnia,
Santa
Cruz
, Mo
ffett
Field,
CA; Y
. Jun
g, NA
SA Am
es
Rese
arch C
enter
, Moff
ett Fi
eld, C
A
1430
hrs
AIAA-2
015-3
029
Deve
lopme
nt of
Gen
eric
Grou
nd
Track
s of P
erfo
rman
ce B
ased
Na
vigat
ion O
pera
tions
for F
leet-
Leve
l Airp
ort N
oise A
nalys
isA.
Wilso
n, M.
LeVin
e, J.
Berna
rdo, M
. Kir
by, D
. Mav
ris, G
eorgi
a Ins
titute
of Te
chno
logy,
Atlan
ta, G
A
1500
hrs
AIAA-2
015-3
030
Imple
ment
ing a
Comb
ined A
rriva
l, De
partu
re, a
nd Su
rface
Sche
duler
fo
r a M
etrop
lexF.
Wiel
and,
W. Kr
uege
r, W. P
eng,
Y. Zh
ang,
A. Ty
agi, C
. Ye,
Intell
igent
Autom
ation
, Inc
., Ro
ckvil
le, M
D; et
al.
1530
hrs
AIAA-2
015-3
031
A fra
mewo
rk fo
r the
clas
sifica
tion
and p
riorit
izatio
n of
arriv
al an
d de
partu
re ro
utes
in M
ulti-A
irpor
t Sy
stems
Term
inal M
anoe
uvrin
g Ar
eas
S. S
idirop
oulos
, A. M
ajumd
ar, K.
Han
, W.
Schu
ster, W
. Och
ieng,
Impe
rial C
olleg
e Lo
ndon
, Lon
don,
Unite
d King
dom
Wedn
esda
y, 24
June
201
519
9-AT
IO-2
0Tra
nsfo
rmat
ional
Fligh
t - A
uton
omy I
IMo
net B
allro
omCh
aired
by: B
. ALLE
N, N
ASA L
angle
y Res
earch
Cente
r14
00 hr
sAIA
A-201
5-303
2Us
ing M
ultim
odal
Inpu
t for
Au
tono
mous
Dec
ision
Mak
ing
for U
nman
ned S
ystem
s - “W
hat
it ne
eds i
n or
der t
o evo
lve, is
a hu
man q
uality
. Our
capa
city t
o lea
p be
yond
logic
.” - C
apt.
Kirk
, Sta
r Tre
k: Th
e Mot
ion P
ictur
eJ.
Neila
n, C.
Cross,
H. F
an, W
. Feh
lman
, L.
Hemp
ley, M
. Mott
er, N
ASA L
angle
y Re
searc
h Cen
ter, H
ampto
n, VA
; et a
l.
1430
hrs
AIAA-2
015-3
033
Colla
bora
ting w
ith A
uton
omou
s Ag
ents
A. Tru
jillo,
NASA
Lang
ley Re
searc
h Ce
nter, H
ampto
n, VA
; H. F
an, A
nalyt
ical
Mech
anics
Asso
ciates
, Inc
., Ha
mpton
, VA;
L. He
mpley
, C. C
ross,
North
rop G
rumma
n Co
rporat
ion, H
ampto
n, VA
; W. F
ehlm
an,
M. M
otter,
NAS
A Lan
gley R
esea
rch Ce
nter,
Hamp
ton, V
A; et
al.
1500
hrs
AIAA-2
015-3
034
A Fle
xible
Fligh
t Con
trol S
ystem
for
Rapid
GNC
and D
istrib
uted
Cont
rol
Deplo
ymen
tP.
Rothh
aar, C
. Cros
s, H.
Fan,
W. Fe
hlman
, L.
Hemp
ley, M
. Mott
er, N
ASA L
angle
y Re
searc
h Cen
ter, H
ampto
n, VA
; et a
l.
1530
hrs
AIAA-2
015-3
035
Oper
ating
in “S
trang
e New
Wo
rlds”
and M
easu
ring S
ucce
ss - T
est a
nd Ev
aluat
ion in
Comp
lex
Envir
onme
nts
G. Q
ualls,
C. Cr
oss,
H. Fa
n, W.
Fehlm
an,
L. He
mpley
, M. M
otter,
NAS
A Lan
gley
Rese
arch C
enter
, Ham
pton,
VA; e
t al.
1600
hrs
AIAA-2
015-3
036
State
of th
e Art
of A
uton
omou
s Pla
tform
s and
Hum
an-M
achin
e Sy
stems
: Only
a Fo
ol Wo
uld St
and
In th
e Way
of P
rogr
ess
V. Sto
uffer,
LMI, M
cLean
, VA;
K. Go
odrich
, NA
SA La
ngley
Resea
rch Ce
nter, H
ampto
n, VA
92
Wedn
esda
y, 24
June
201
520
0-BA
L-2Ba
lloon
Syste
ms II
Steub
enCh
aired
by: J
. RAN
D, W
inzen
Engin
eerin
g Inc
1400
hrs
AIAA-2
015-3
037
Ballo
on A
spec
t of S
tratEx
Wor
ld Re
cord
Skyd
iveJ.
Nott,
Nott
Tech
nolog
y, Sa
nta B
arbara
, CA
1430
hrs
AIAA-2
015-3
038
Rece
nt Im
prov
emen
ts to
the D
esign
an
d Man
ufac
ture
of H
igh A
ltitud
e Ze
ro-P
ressu
re B
alloo
nsJ.
Marsh
, Colu
mbia
Scien
tific B
alloo
n Fa
cility,
Pales
tine,
TX; M
. Gile
s, Ra
ven
Aeros
tar, S
ulphu
r Spri
ngs,
TX
1500
hrs
AIAA-2
015-3
039
The W
allop
s Arc
Seco
nd P
ointer
- A
Ballo
on B
orne
Fine
Poin
ting S
ystem
D. S
tuchli
k, NA
SA G
odda
rd Sp
ace F
light
Cente
r, Gree
nbelt
, MD
1530
hrs
AIAA-2
015-3
040
Curre
nt St
atus
of a
NASA
High
-Al
titud
e Ball
oon-
Base
d Obs
erva
tory
fo
r Plan
etary
Scien
ceD.
Varga
, NAS
A Glen
n Res
earch
Cente
r, Cle
velan
d, OH
; E. Y
oung
, Sou
thwes
t Re
searc
h Ins
titute,
Bou
lder, C
O
1600
hrs
AIAA-2
015-3
041
Tech
nolog
y Dev
elopm
ent f
or th
e Ex
aVolt
Ant
enna
(EVA
). 1/
20-S
cale
Deplo
ymen
t Tes
tF.
Bagin
ski, G
eorge
Was
hingto
n Univ
ersity
, Wa
shing
ton, D
C; P.
Gorha
m, U
nivers
ity
of Ha
waii,
Hono
lulu,
Hono
lulu,
HI; D
. Fa
irbrot
her, M
. Said
, S. L
ang,
NASA
Wa
llops
Fligh
t Fac
ility,
Wallo
ps Is
land,
VA
1630
hrs
AIAA-2
015-3
042
Shap
e Ana
lysis
of th
e 1/2
0-Sc
ale
ExaV
olt A
nten
na Te
st Ba
lloon
F. Ba
ginsk
i, Geo
rge W
ashin
gton
Unive
rsity,
Was
hingto
n, DC
; K. B
rakke
, Su
sque
hann
a Univ
ersity
, Seli
nsgro
ve, P
A; K.
Zhao
, Geo
rge W
ashin
gton U
nivers
ity,
Wash
ington
, DC
1700
hrs
AIAA-2
015-3
043
An U
nderg
radu
ate St
uden
t Ins
trume
ntatio
n Pro
ject (
USIP)
to
Deve
lop N
ew In
strum
ent T
echno
logy
to Stu
dy th
e Aur
oral
Ionos
phere
and
Strato
sphe
ric O
zone
Laye
r Usin
g Ul
tralig
ht Ba
lloon
Paylo
ads
E. Be
ring,
R. Ga
mblin,
Unive
rsity o
f Hou
ston,
Houst
on, T
X
Wedn
esda
y, 24
June
201
520
1-CF
D-21
Disco
ntinu
ous G
alerk
in Me
thod
sGr
and B
allro
om A
Chair
ed by
: C. S
CHRO
CK, A
ir Firc
e Res
earch
Labo
ratory
and L
. DIO
SADY
, NAS
A Ame
s Res
earch
Cente
r14
00 hr
sAIA
A-201
5-304
4Ge
nera
l elem
ent s
hape
s with
in a t
enso
r-pro
duct
highe
r-ord
er
spac
e-tim
e disc
ontin
uous
-Gale
rkin
form
ulatio
nL.
Diosa
dy, S
. Murm
an, N
ASA A
mes
Rese
arch C
enter
, Moff
ett Fi
eld, C
A
1430
hrs
AIAA-2
015-3
045
High
-ord
er D
iscon
tinuo
us G
alerk
in Me
thod
s App
lied t
o Mult
iphas
e Flo
wsM.
Hen
ry de
Frah
an, E
. Joh
nsen
, Un
iversi
ty of
Mich
igan,
Ann A
rbor, A
nn
Arbor,
MI
1500
hrs
AIAA-2
015-3
046
An Ad
aptiv
e Exp
licit 3
D Di
sconti
nuou
s Ga
lerkin
Solve
r for
Uns
teady
Pr
oblem
sA.
Kirby,
D. M
avrip
lis, Un
iversit
y of W
yomi
ng,
Laram
ie, La
ramie,
WY;
A. Wi
ssink
, Arm
y Av
iation
and M
issile
Resea
rch De
velop
ment
and E
ngine
ering
Cente
r, Moff
ett Fi
eld, C
A
1530
hrs
AIAA-2
015-3
047
A Hy
brid
Reco
nstru
cted
Disco
ntinu
ous G
alerk
in an
d Co
ntinu
ous G
alerk
in me
thod
for
Inco
mpre
ssible
Flow
sA.
Pand
are, H
. Luo
, Nort
h Caro
lina S
tate
Unive
rsity,
Ralei
gh, N
C
Wedn
esda
y, 24
June
201
520
2-CF
D-22
Futu
re of
Fluid
s: Ne
xt G
ener
ation
CFD
(Invit
ed)
Gran
d Ball
room
BCh
aired
by: M
. MAL
IK, N
ASA-L
angle
y Res
earch
Cente
r and
A. KH
ODAD
OUST
, Boe
ing En
ginee
ring O
perat
ions &
Tech
nolog
y14
00 hr
sOr
al Pre
senta
tion
Impa
cting
Des
ign w
ith La
rge E
ddy
Simula
tion
(Invit
ed)
P. Mo
in, S
tanfor
d Univ
ersity
, Stan
ford,
CA; F
. Ham
, Cas
cade
Tech
nolog
ies, I
nc.,
Palo
Alto,
CA
1430
hrs
AIAA-2
015-3
048
Next
-Gen
erat
ion CF
D fo
r Hy
perso
nic an
d Aer
othe
rmal
Flows
(In
vited
)G.
Cand
ler, U
nivers
ity of
Minn
esota
, Mi
nnea
polis,
Minn
eapo
lis, M
N
1500
hrs
AIAA-2
015-3
049
Scali
ng Li
mits
for P
DE-B
ased
Sim
ulatio
n (In
vited
)P.
Fisch
er, U
nivers
ity of
Illino
is, U
rbana
-Ch
ampa
ign, U
rbana
, IL
1530
hrs
AIAA-2
015-3
050
PyFR
: Nex
t-Gen
eratio
n High
-Ord
er
Comp
utatio
nal F
luid D
ynam
ics on
Ma
ny-Co
re Ha
rdwa
re (In
vited
)P. V
incen
t, F. W
itherd
en, A
. Farr
ington
, G.
Ntem
os, B.
Verm
eire,
J. Pa
rk, Im
peria
l Colle
ge
Lond
on, L
ondo
n, Un
ited K
ingdo
m; et
al.
1600
hrs
AIAA-2
015-3
051
Towa
rds h
igh-fi
delity
aero
spac
e de
sign
in th
e age
of ex
treme
scale
su
perco
mput
ing (I
nvite
d)Q.
Wan
g, Ma
ssach
usett
s Ins
titute
of Te
chno
logy,
Camb
ridge
, MA
1630
hrs
AIAA-2
015-3
052
Oppo
rtunit
ies an
d Cha
lleng
es fo
r Mu
lti-Di
scipli
nary
Ana
lysis
and
Optim
izatio
n at
Exas
cale
(Invit
ed)
J. Alo
nso,
Stan
ford U
nivers
ity, S
tanfor
d, CA
1700
hrs
AIAA-2
015-3
053
CFD
for N
ext G
ener
ation
Har
dwar
e: Ex
perie
nces
with
Prox
y App
licat
ions
K. Fra
nko,
T. Fis
her, P
. Lin,
S. B
ova,
Sand
ia Na
tiona
l Lab
orator
ies,
Albuq
uerqu
e, NM
Wedn
esda
y, 24
June
201
520
3-CF
D-23
Para
llel C
ompu
ting a
nd N
ovel
Arch
itectu
res
Plum
Blos
som
ACh
aired
by: L
. LUO
, Nort
h Caro
lina S
tate U
nivers
ity an
d C. S
TONE
, Com
putat
ional
Scien
ce an
d Eng
ineeri
ng14
00 hr
sAIA
A-201
5-305
4Pa
ralle
l Tec
hniqu
es fo
r Nav
ier-
Stoke
s Solv
er ba
sed o
n 4t
h Or
der
Modifi
ed R
unge
-Kut
ta Sc
heme
wi
th TV
DH.
Sha
h, W
ichita
Stat
e Univ
ersity
, W
ichita
, KS
1430
hrs
AIAA-2
015-3
055
Optim
izatio
n of
A Fi
ne-g
raine
d BI
LU by
CUDA
Inter
-bloc
k Sy
nchr
oniza
tion
L. Lu
o, J.
Edwa
rds, H
. Luo
, F. M
ueller
, Nort
h Ca
rolina
State
Unive
rsity,
Raleig
h, NC
1500
hrs
AIAA-2
015-3
056
GPU
Para
lleliz
ation
of a
High
Ord
er
Imme
rsed B
ound
ary M
ethod
Fluid
So
lver
A. Jo
st, J.
Zhan
g, Flo
rida I
nstitu
te of
Tech
nolog
y, Me
lbourn
e, FL
; T. J
acks
on,
Unive
rsity
of Flo
rida,
Gaine
sville
, Ga
inesv
ille, F
L
1530
hrs
AIAA-2
015-3
057
A Hy
brid
CPU-
GPU
Para
llel O
ctree
Di
rect
Simula
tion
Mont
e Car
lo Ap
proa
chR.
Jamb
unath
an, D
. Lev
in, U
nivers
ity of
Illi
nois,
Urba
na-Ch
ampa
ign, U
rbana
, IL
1600
hrs
AIAA-2
015-3
058
High
-Per
form
ance
3D
Multi-
Disci
plina
ry Fl
uid/T
herm
al Pr
edict
ion u
sing C
ombin
ed M
ulti-
Core
/Mult
i-GPG
PU Co
mput
er
Syste
msC.
Ston
e, Co
mputa
tiona
l Scie
nce a
nd
Engin
eerin
g, LLC
, Chic
ago,
IL; R.
Dav
is,
Unive
rsity
of Ca
liforni
a, Da
vis, D
avis,
CA
1630
hrs
AIAA-2
015-3
059
Comp
ariso
n Of
Acce
lerat
ion
Tech
nique
s on
CFD
Open
-Sou
rce
Softw
are f
or A
eros
pace
App
licat
ions
L. Ma
ngan
i, G. R
oman
elli, U
nivers
ity
of Ap
plied
Scie
nces
and A
rts, L
uzern
, Sw
itzerl
and;
A. Ga
ddai,
Tech
nical
Unive
rsity
of Mi
lan, M
ilan,
Switz
erlan
d; E.
Casa
rtelli,
Univ
ersity
of Ap
plied
Scie
nces
an
d Arts
, Luz
ern, S
witze
rland
93
Wedn
esda
y, 24
June
201
520
4-CF
D-24
Desig
n Op
timiza
tion
Cora
lCh
aired
by: L
. TAO
, GE G
lobal
Rese
arch
1400
hrs
AIAA-2
015-3
060
Adjoi
nt-B
ased
Opt
imiza
tion
of a
Hype
rsonic
Inlet
H. Kl
ine, S
tanfor
d Univ
ersity
, Stan
ford,
CA;
F. Pa
lacios
, The
Boe
ing Co
mpan
y, Ev
erett,
WA
; T. E
cono
mon,
J. Alo
nso,
Stan
ford
Unive
rsity,
Stan
ford,
CA
1430
hrs
AIAA-2
015-3
061
Aero
dyna
mic S
hape
Opt
imiza
tion
for N
atur
al La
mina
r Flow
Usin
g a
Discr
ete-A
djoint
App
roac
hR.
Rash
ad, D
. Zing
g, Un
iversi
ty of
Toron
to,
Toron
to, Ca
nada
1500
hrs
AIAA-2
015-3
062
A Co
ntinu
ous S
ensit
ivity
Equa
tion
of A
rbitr
ary H
igh O
rder
C. Be
lley,
A. Ha
y, D.
Pelle
tier, É
cole
Polyt
echn
ique d
e Mon
tréal,
Mon
tréal,
Ca
nada
1530
hrs
AIAA-2
015-3
063
Desig
n opti
miza
tion o
f a hi
gh by
pass
ratio
fan r
otor a
gains
t wate
r inge
stion
S. Qiu
, D. Y
ang,
Aviat
ion In
dustr
y Corp
oratio
n of
China
(AVIC
), Sh
angh
ai, Ch
ina
1600
hrs
AIAA-2
015-3
064
Desig
n an
d Opt
imiza
tion
of a
Supe
rsonic
Bus
iness
Jet
F. Kiy
ici, S
. Arad
ag, T
OBB
Unive
rsity
of Ec
onom
ics an
d Tec
hnolo
gy, A
nkara
, Turk
ey
Wedn
esda
y, 24
June
201
520
5-CF
D-25
Turb
ulent
Flow
Simu
lation
s II
Emer
aldCh
aired
by: F
. VER
GINE
and L
. DUA
N, M
issou
ri Univ
ersity
of S
cienc
e and
Tech
nolog
y14
00 hr
sAIA
A-201
5-306
5In
vesti
gatio
n of
a Tw
injet
Confi
gura
tion
with
and w
ithou
t Flo
w Co
ntro
lK.
Gopa
raju,
D. G
aiton
de, S
. Bha
umik,
Oh
io St
ate U
nivers
ity, C
olumb
us, O
H
1430
hrs
AIAA-2
015-3
066
Nume
rical
Simula
tions
of
Single
and T
ande
m Wh
eels
for
Aero
dyna
mic L
oads
Pre
dictio
nS.
Spa
gnolo
, X. Z
hang
, Z. H
u, D.
Angla
nd,
Unive
rsity
of So
utham
pton,
South
ampto
n, Un
ited K
ingdo
m
1500
hrs
AIAA-2
015-3
067
RANS
Simu
lation
s of a
Chan
nel
Flow
with
a Ne
w Ve
locity
/Pre
ssure
-Gr
adien
t Mod
elS.
Poros
eva,
J. Co
lmen
ares,
Unive
rsity
of Ne
w Me
xico,
Albuq
uerqu
e, Alb
uque
rque,
NM; S
. Murm
an, N
ASA A
mes R
esea
rch
Cente
r, Moff
ett Fi
eld, N
M
1530
hrs
AIAA-2
015-3
068
High
-Fide
lity Co
mput
ation
al As
sessm
ent o
f the
Per
form
ance
of
a Ver
tical
Axis
Wind
Turb
ineJ.
Suda
ni, R.
Pras
ad, M
. Dam
odara
n, Ind
ian In
stitut
e of T
echn
ology
Ga
ndhin
agar,
Ahme
daba
d, Ind
ia
Wedn
esda
y, 24
June
201
520
6-F3
60-6
14
00 -
1630
hrs
The C
halle
nges
of G
reen
Avia
tion
Gran
d Ball
room
E
Mode
rator:
Mart
y Brad
ley, T
echn
ical F
ellow
, Boe
ing Co
mmerc
ial Ai
rplan
es
Pan
elists
:Ri
cky C
urra
nFa
culty
of Ae
rospa
ce En
ginee
ring
Delft
Unive
rsity
of Te
chno
logy
Jay E
. Dry
erDir
ector,
Adva
nced A
ir Veh
icles P
rogram
Offic
e (Ac
ting)
Aeron
autic
s Res
earch
Miss
ion D
irecto
rate
NASA
Hea
dqua
rters
Askin
Isikv
eren
Head
of V
isiona
ry Air
craft
Conc
epts
Bauh
aus L
uftfah
rt
Leslie
Perki
nsDir
ector
, Ene
rgy O
ffice
Air F
orce
Res
earch
Labo
rato
ry
Jean
ne Yu
Envir
onme
ntal D
irecto
rBo
eing C
omme
rcial
Airpla
nes
Wedn
esda
y, 24
June
201
520
7-F3
60-7
/CAS
E-7
1400
- 17
30 h
rsSy
stem
Comp
lexity
: Go
vern
ment
Nee
ds an
d Pra
ctica
l Res
earch
Res
ults
Gran
d Ball
room
D
This
pane
l is ar
range
d arou
nd tw
o app
licatio
n dom
ains -
defen
se sy
stems
and u
nman
ned a
ir sys
tems i
n the
natio
nal a
irspa
ce - a
nd tw
o eng
ineeri
ng pr
actic
e nee
ds - r
apid
syste
m de
velop
ment
and n
ew th
eory
comp
lex sy
stems
engin
eerin
g. Th
e exp
ectat
ion is
that
the au
dienc
e wi
ll tak
e awa
y both
a co
gent
statem
ent o
f nee
ds an
d cha
lleng
es al
ong w
ith a
conc
ise de
script
ion of
new
techn
iques
that
show
prom
ise to
mee
t the
state
d nee
ds an
d cha
lleng
es.
Keyn
ote S
peak
erKr
isten
Bald
win
Princ
ipal D
eputy
DAS
D (S
E), D
epart
ment
of De
fense
Mode
rators
: Fran
k Sern
a, Pri
ncipa
l Dire
ctor, S
trateg
ic Ini
tiativ
es, D
raper
Labo
ratory
and A
nna-M
aria M
cGow
an, A
erona
utics
Rese
arch D
irecto
rate,
NASA
Lang
ley Re
searc
h Cen
ter
Pan
elists
:Je
ffrey
P. H
ollan
dDir
ector
of Re
searc
h and
Dev
elopm
ent a
nd Ch
ief S
cienti
stU.
S. Ar
my Co
rps of
Engin
eers
David
Ney
land
Cons
ultan
t
94
Wedn
esda
y, 24
June
201
520
8-FD
-23
Unste
ady W
ing A
erod
ynam
ics II
IGo
veno
rs Le
cture
Hall
Chair
ed by
: S. Y
ARUS
EVYC
H, U
nivers
ity of
Wate
rloo a
nd H
. LUO
, Van
derbi
lt Univ
ersity
1400
hrs
AIAA-2
015-3
069
Nume
rical
Simula
tion
of Ci
rcular
Cy
linde
rs an
d Wing
Secti
ons i
n Un
stead
y Mot
ionA.
Gros
s, J.
Zhou
, New
Mex
ico S
tate
Unive
rsity,
Las C
ruces
, NM;
H. F
asel,
Un
iversi
ty of
Arizo
na, T
ucso
n, AZ
1430
hrs
AIAA-2
015-3
070
The e
ffect
of th
e blad
e cho
rd le
ngth
on
the a
erod
ynam
ics of
the M
AV
scale
cyclo
idal p
rope
ller u
nder
ho
verin
g sta
tus
Y. Hu
, H. Z
hang
, Nort
hwes
tern
Polyt
echn
ical U
nivers
ity, X
i’an,
China
1500
hrs
AIAA-2
015-3
071
Unste
ady T
hick A
irfoil
Aero
dyna
mics:
Ex
perim
ents,
Comp
utatio
n, an
d Th
eory
D. Gre
enbla
tt, Tec
hnion
--Israe
l Instit
ute of
Tec
hnolo
gy, Ha
ifa, Is
rael; C
. Rum
sey, N
ASA
Lang
ley Re
search
Cente
r, Ham
pton,
VA;
H. Mu
eller-V
ahl, T
echnio
n--Isr
ael In
stitute
of
Techn
ology,
Haifa
, Israe
l; C. S
tangfe
ld,
Techn
ical U
nivers
ity of
Berlin
, Berl
in, Ge
rman
y
1530
hrs
AIAA-2
015-3
072
Impa
ct of
a Vo
rtica
l Gus
t on
the
Aero
dyna
mics
of a
Finite
Asp
ect-
Ratio
Wing
R. Go
rdnier
, M. V
isbal,
Air F
orce R
esea
rch
Labo
ratory
, Wrig
ht-Pa
tterso
n AFB
, OH
1600
hrs
AIAA-2
015-3
073
Trans
ient E
ncou
nter
s of a
NA
CA00
12 W
ing w
ith a
Strea
mwise
-Orie
nted
Vorte
xD.
Garm
ann,
M. V
isbal,
Air F
orce R
esea
rch
Labo
ratory
, Wrig
ht-Pa
tterso
n AFB
, OH
1630
hrs
AIAA-2
015-3
074
Flow
Visua
lizat
ion an
d For
ce
Meas
urem
ents
on A
cceler
ated
Re
volvi
ng Fl
at P
lates
at Lo
w Re
ynold
s Num
bers
M. Pe
rcin,
B. va
n Oud
heus
den,
Delft
Unive
rsity
of Te
chno
logy,
Delft,
The
Nethe
rland
s
Wedn
esda
y, 24
June
201
520
9-FD
-24
Boun
dary
Laye
r Tra
nsitio
n: R
ecep
tivity
and C
ontro
lSa
pphir
eCh
aired
by: E
. WHI
TE, T
exas
A&M
Unive
rsity
and A
. CHO
U, N
ASA L
angle
y Res
earch
Cente
r14
00 hr
sAIA
A-201
5-307
5On
the E
ffect
of Sm
all St
eps o
n Pr
e-tra
nsitio
nal S
tream
wise
Elon
gated
Str
eaks
A. Se
scu, M
ississ
ippi S
tate U
nivers
ity,
Missi
ssipp
i Stat
e, MS
; M. A
fsar, I
mperi
al Co
llege
Lond
on, L
ondo
n, Un
ited K
ingdo
m;
V. Sa
ssanis
, Miss
issipp
i Stat
e Univ
ersity
, Mi
ssissi
ppi S
tate,
MS
1430
hrs
AIAA-2
015-3
076
Time-
Freq
uenc
y Ana
lysis
of
Boun
dary
Laye
r Ins
tabil
ities
Gene
rated
by Fr
eestr
eam
Lase
r Pe
rturb
ation
sA.
Chou
, NAS
A Lan
gley R
esea
rch Ce
nter,
Hamp
ton, V
A; S.
Sch
neide
r, Purd
ue
Unive
rsity,
Wes
t Lafa
yette
, IN
1500
hrs
AIAA-2
015-3
077
Nume
rical
Simula
tion o
f Hyp
erso
nic
Boun
dary
-Laye
r Ins
tabil
ity in
a Re
al Ga
s with
Two-
Dime
nsion
al Su
rface
Rou
ghne
ssC.
Morte
nsen
, X. Z
hong
, Univ
ersity
of
Califo
rnia,
Los A
ngele
s, Lo
s Ang
eles,
CA
1530
hrs
AIAA-2
015-3
078
Lead
ing-Ed
ge R
ecep
tivity
to
Acou
stic W
aves
for H
igh-S
peed
Flo
ws ov
er a
Blun
t Wed
geA.
Cerm
inara,
N. S
andh
am, U
nivers
ity
of So
utham
pton,
South
ampto
n, Un
ited
Kingd
om
1600
hrs
AIAA-2
015-3
079
Swep
t-Wing
Bou
ndar
y-La
yer
Rece
ptivi
ty to
Stea
dy Fr
ee-S
tream
Di
sturb
ance
sH.
Kurz,
M. K
loker,
Univ
ersity
of S
tuttga
rt,
Stutt
gart,
Germ
any
1630
hrs
AIAA-2
015-3
080
Delay
ing tr
ansit
ion in
rota
ting
boun
dary
-laye
r flow
sP.
Griffi
ths, U
nivers
ity of
Birm
ingha
m,
Birmi
ngha
m, U
nited
King
dom;
S. G
arrett
, Un
iversi
ty of
Leice
ster, L
eices
ter, U
nited
Kin
gdom
; S. S
tephe
n, Un
iversi
ty of
New
South
Wale
s, Sy
dney
, Aus
tralia
Wedn
esda
y, 24
June
201
521
0-FD
-25
1400
- 17
30 h
rsFlo
w Co
ntro
l Tec
hnolo
gies -
Bar
riers/
Chall
enge
s to T
ech
Trans
ition
Topa
z
Chair
ed by
: G. D
ALE,
Air Fo
rce Re
searc
h Lab
orator
y and
D. S
MITH
, Air F
orce O
ffice o
f Scie
ntific
Rese
arch A
FOSR
The s
essio
n will
focus
on th
e hurd
les to
tran
sition
ing flo
w co
ntrol
techn
ology
to pl
atform
s bas
ed on
majo
r cas
e stud
ies. P
anel
memb
ers w
ill pre
sent
lesso
ns le
arned
and r
ecom
mend
ation
s on fl
ow co
ntrol
techn
ology
tran
sition
s (ap
prox.
15 m
inutes
each
), co
verin
g both
succe
ssful
and u
nsuc
cessf
ul tra
nsitio
ns. A
mod
erated
Q&A
sessi
on w
ill fol
low th
e pres
entat
ions.
Sessi
on ou
tcome
is in
tende
d to o
ffer a
path
forwa
rd to
foster
ing m
ore te
chno
logy t
ransit
ion fo
r flow
contr
ol.Mo
derat
or: Lo
u Catt
afesta
, Emi
nent
Scho
lar an
d Prof
esso
r, Flor
ida S
tate U
nivers
ity
Pane
lists:
Edwa
rd W
halen
Flow
Contr
ol Ac
tuatio
n Man
ager
Boein
g Res
earch
and T
echn
ology
Rich
ard W
lezien
Profes
sor a
nd Ch
air of
Aeros
pace
Engin
eerin
gIow
a Stat
e Univ
ersity
Rona
ld Jo
slin
Progra
m Of
ficer
Offic
e of N
aval
Rese
arch
Fay C
ollier
Projec
t Man
ager
NASA
Envir
onme
ntally
Resp
onsib
le A v
iation
95
Wedn
esda
y, 24
June
201
521
1-FD
-26
Turb
ulenc
e Sim
ulatio
nsSe
nato
rs Le
cture
Hall
Chair
ed by
: P. S
PALA
RT, B
oeing
Comm
ercial
Airpl
anes
and E
. JOH
NSEN
, Univ
ersity
of M
ichiga
n14
00 hr
sAIA
A-201
5-308
1A
nume
rical
study
of tu
rbule
nce
in bo
xes w
ith n
o-sli
p wall
s and
of
vary
ing vo
lume-
to-su
rface
ratio
sE.
John
sen,
Unive
rsity
of Mi
chiga
n, An
n Arbo
r, Ann
Arbo
r, MI;
P. Mo
vahe
d, Un
iversi
ty of
Illino
is, U
rbana
-Cham
paign
, Ur
bana
, IL;
D. D
owlin
g, Un
iversi
ty of
Mich
igan,
Ann A
rbor, A
nn Ar
bor, M
I
1430
hrs
AIAA-2
015-3
082
Surfa
ce R
ough
ness
Effe
cts in
Hy
perso
nic Tu
rbule
nt B
ound
ary
Laye
rsJ.
Pogg
ie, Ai
r Forc
e Res
earch
Labo
ratory
, W
right-
Patte
rson A
FB, O
H
1500
hrs
AIAA-2
015-3
083
Appli
catio
n of
the W
ray-
Agar
wal
Mode
l to C
ompr
essib
le Flo
wsT.
Wray
, R. A
garw
al, W
ashin
gton
Unive
rsity
in St
. Lou
is, S
t. Lo
uis, M
O
1530
hrs
AIAA-2
015-3
084
Tetra
hedr
al-Me
sh Si
mulat
ion of
Tu
rbule
nt Fl
ows w
ith th
e Spa
ce-
Time C
onse
rvat
ive Sc
heme
sC.
Chan
g, NA
SA La
ngley
Rese
arch C
enter
, Ha
mpton
, VA;
B. Ve
nkata
chari
, Nati
onal
Institu
te of
Aeros
pace
, Ham
pton,
VA; G
. Ch
eng,
Unive
rsity
of Ala
bama
, Tus
caloo
sa,
Tusca
loosa
, AL
Wedn
esda
y, 24
June
201
521
2-MA
O-6
Emer
ging M
ethod
s II
Madr
idCh
aired
by: B
. MES
MER,
Unive
rsity
of Ala
bama
and J
. HICK
EN, R
ensse
laer P
olytec
hnic
Institu
te14
00 hr
sAIA
A-201
5-308
5In
creas
ing Fe
asibi
lity of
the S
elf-
Orga
nizing
Map
as a
Desig
n To
ol th
roug
h a N
ovel
Conv
erge
nce
Heur
istic
T. Ric
hards
on, E
. Wine
r, Iow
a Stat
e Un
iversi
ty, Am
es, I
A
1430
hrs
AIAA-2
015-3
086
Inco
rpor
ation
of Co
uplin
g Stre
ngth
Mo
dels
in a V
alue-
base
d Sys
tems
Engin
eerin
g fra
mewo
rk fo
r op
timiza
tion
H. Ka
nnan
, E. T
ibor, I
owa S
tate U
nivers
ity,
Ames
, IA;
B. M
esme
r, Univ
ersity
of
Alaba
ma, H
untsv
ille, H
untsv
ille, A
L; C.
Bloeb
aum,
Iowa
Stat
e Univ
ersity
, Ame
s, IA
1500
hrs
AIAA-2
015-3
087
SUAV
E: An
Ope
n-So
urce
En
viron
ment
for M
ulti-F
idelity
Co
ncep
tual
Vehic
le De
sign
T. Lu
kacz
yk, A
. Wen
dorff
, M. C
olonn
o, T.
Econ
omon
, J. A
lonso
, Stan
ford U
nivers
ity,
Stan
ford,
CA; T
. Orra
, Emb
raer, S
ão Jo
sé
dos C
ampo
s, Br
azil;
et al.
1530
hrs
AIAA-2
015-3
088
A Fu
ll-Sp
ace M
ethod
with
Mat
rix
Aggr
egat
es fo
r Stre
ss-Co
nstra
ined
Struc
tura
l Opt
imiza
tion
G. Ke
nned
y, Ge
orgia
Institu
te of
Tech
nolog
y, Atl
anta,
GA
1600
hrs
AIAA-2
015-3
089
Redu
cing I
nduc
ed D
rag a
nd
Mane
uver
Load
s by A
ctive
Ae
roela
stic A
ltera
tion
J. Lin
, Con
trol R
esea
rch Co
rporat
ion,
Lexin
gton,
MA
1630
hrs
AIAA-2
015-3
090
Integ
rated
Mult
idisci
plina
ry A
ircra
ft De
sign
Proc
ess S
uppo
rted b
y a
Dece
ntra
l MDO
Fram
ewor
kF.
Daou
d, S.
Dein
ert, R
. Maie
rl, Ö.
Pe
tersso
n, Air
bus,
Manc
hing,
Germ
any
Wedn
esda
y, 24
June
201
521
3-MA
O-7
Meta
mode
ling I
Manc
heste
rCh
aired
by: S
. CHO
WDH
URY,
Missi
ssipp
i Stat
e Univ
ersity
and P
. PIPE
RNI,
Bomb
ardier
Inc
1400
hrs
AIAA-2
015-3
091
A Me
thod
ology
to Cr
eate
Appr
oxim
ate M
odels
of Lo
ad
Enve
lopes
Und
er U
ncer
taint
yD.
Ranc
ourt,
S. G
hosh
, D. M
avris
, Geo
rgia
Institu
te of
Tech
nolog
y, Atl
anta,
GA;
S.
Cogg
on, A
irbus
, Filto
n, Un
ited K
ingdo
m
1430
hrs
AIAA-2
015-3
092
Princ
ipal C
ompo
nent
Analy
sis As
sisted
Su
rroga
te Mo
delin
g (PC
A-SM
) of
Corre
lated
Load
s for
Unc
ertain
ty An
alysis
of D
esign
Load
Enve
lopes
S. Gh
osh, D
. Ran
court,
D. Ma
vris,
Georg
ia Ins
titute
of Tec
hnolo
gy, At
lanta,
GA; S
. Co
ggon
, Airb
us, Fi
lton,
Unite
d King
dom
1500
hrs
AIAA-2
015-3
093
Auxil
iary A
ir In
let D
esign
: Non
-Lin
earit
y, Su
rroga
te Mo
delin
g and
Opt
imiza
tion
Aspe
ctsA.
Lomb
ardi, L
. San
tos, E
mbrae
r, São
Jo
sé do
s Cam
pos,
Braz
il; D.
Ferra
ri, Te
chno
logica
l Insti
tute o
f Aero
nauti
cs (IT
A), S
ão Jo
sé do
s Cam
pos,
Braz
il
1530
hrs
AIAA-2
015-3
094
HDMR
-bas
ed Su
rroga
te Mo
del f
or
High
Dim
ensio
nal A
erod
ynam
ic De
sign
Prob
lems
Z. Ga
o, C.
Wang
, Nort
hwes
tern
Polyt
echn
ical U
nivers
ity, X
i’an,
China
1600
hrs
AIAA-2
015-3
095
A Se
quen
tial M
axim
in La
tin
Hype
rcube
Samp
ling M
ethod
And
Its
App
licat
ion to
Airc
raft
Desig
nD.
Wu,
T. Lo
ng, Y
. Wan
g, L.
Liu, B
eijing
Ins
titute
of Te
chno
logy,
Beijin
g, Ch
ina
96
Wedn
esda
y, 24
June
201
521
4-MS
T-9Ai
rfram
e Dam
age a
nd H
ealth
Mon
itorin
gTra
verti
neCh
aired
by: V
. MUK
HOPA
DHYA
Y, NA
SA La
ngley
Rese
arch C
enter
1400
hrs
AIAA-2
015-3
096
Comp
osite
Stru
cture
Mod
eling
an
d Ana
lysis
of A
dvan
ced A
ircra
ft Fu
selag
e Con
cept
sV.
Mukh
opad
hyay
, M. S
oroka
ch, N
ASA
Lang
ley Re
searc
h Cen
ter, H
ampto
n, VA
1430
hrs
AIAA-2
015-3
097
Nume
rical
Simula
tion
and A
nalys
is of
the A
ircra
ft Pil
ot Se
at Im
pact
Resis
tanc
eX.
Zhan
g, X.
Jinw
u, M.
Li, B
eihan
g Un
iversi
ty, B
eijing
, Chin
a; Y.
Ren,
Huna
n Un
iversi
ty, Ch
angs
ha, C
hina
1500
hrs
AIAA-2
015-3
098
Sens
itivity
Analy
sis to
ward
s Pr
obab
ilistic
Re-En
try M
odeli
ng of
Sp
acecr
aft an
d Spa
ce De
bris
P. Meh
ta, Un
iversit
y of S
trathc
lyde,
Glasgo
w,
Unite
d King
dom;
A. W
alker,
Los A
lamos
Na
tiona
l Labo
ratory
, Los
Alamo
s, NM
; M.
Brown
, Univ
ersity
of N
ew So
uth W
ales a
t the
Austr
alian D
efence
Force
Acad
emy,
Canb
erra,
Austr
alia; E
. Minis
ci, M.
Vasile
, Univ
ersity
of
Strath
clyde
, Glas
gow,
Unite
d King
dom
1530
hrs
AIAA-2
015-3
099
A Ve
hicle
Mana
geme
nt En
d-to
-End
Testi
ng an
d Ana
lysis
Platfo
rm fo
r Va
lidat
ion of
Miss
ion an
d Fau
lt Ma
nage
ment
Algo
rithm
s to R
educ
e Ri
sk fo
r NAS
A’s Sp
ace L
aunc
h Sy
stem
L. Tre
vino,
J. Pa
tterso
n, D.
Teare
, S.
John
son,
NASA
Mars
hall S
pace
Fligh
t Ce
nter, H
untsv
ille, A
L
Wedn
esda
y, 24
June
201
521
5-MS
T-10
Sens
or an
d Com
munic
ation
s Sys
tems
Wyeth
Chair
ed by
: J. Z
AMBR
ANO
and Y
. CHE
NG, A
VIC Co
mputi
ng Te
chniq
ue Re
searc
h Ins
titute
1400
hrs
AIAA-2
015-3
100
Simula
tion/
Optim
izatio
n Mo
delin
g fo
r Rob
ust S
atell
ite D
ata U
nit fo
r Ai
rbor
ne N
etwor
kJ.
Zamb
rano,
O. Ye
ste-O
jeda,
R. La
ndry,
Un
iversi
ty of
Québ
ec, M
ontré
al, Ca
nada
1430
hrs
AIAA-2
015-3
101
Para
llel I
mage
Deta
il Enh
ance
ment
Fo
r Rea
l-tim
e App
licat
ions
Y. Ch
eng,
W. N
iu, Av
iation
Indu
stry C
orpora
tion
of Ch
ina (A
VIC),
Xi’an
, Chin
a; Z.
Zhai,
No
rthwe
stern
Polyt
echnic
al Un
iversit
y, Xi’
an,
China
; L. Z
hang
, Avia
tion I
ndust
ry Co
rporat
ion
of Ch
ina (A
VIC),
Xi’an
, Chin
a
1500
hrs
AIAA-2
015-3
102
The K
ey al
gorit
hm R
esea
rch of
En
hanc
ed Vi
sion
Syste
m Ba
se on
Em
bedd
ed P
arall
el Co
mput
ingX.
Jian
chun
, Avia
tion I
ndus
try Co
rporat
ion
of Ch
ina (A
VIC),
Xi’an
, Chin
a
Wedn
esda
y, 24
June
201
521
6-TP
-10/
PDL-1
0Pla
sma C
ompu
tatio
nal M
ethod
s II
Miro
Chair
ed by
: K. S
TEPH
ANI,
Unive
rsity
of Illi
nois
at Ur
bana
-Cham
paign
and T
. MOE
LLER,
Unive
rsity
of Te
nnes
see S
pace
Insti
tute
1400
hrs
AIAA-2
015-3
103
Comp
utat
ional
Simula
tions
of TP
3 Ar
c-Jet
Facil
ity Fl
owT.
Gokc
en, E
RC, I
nc.,
Moffe
tt Fie
ld, CA
; J.
Balbo
ni, N
ASA A
mes R
esea
rch Ce
nter,
Moffe
tt Fie
ld, CA
; A. A
lunni,
ERC,
Inc.,
Moffe
tt Fie
ld, CA
1430
hrs
AIAA-2
015-3
104
Simula
tion o
f Plas
ma Fl
ow Co
ntrol:
A N
ew Co
mputa
tiona
lly Ef
ficien
t Ap
proa
chB.
Paren
t, Pusa
n Nati
onal
Unive
rsity,
Busan
, So
uth Ko
rea; S
. Mach
eret, P
urdue
Unive
rsity,
West
Lafay
ette,
IN; M
. Shn
eider,
Princ
eton
Unive
rsity,
Prince
ton, N
J
1500
hrs
AIAA-2
015-3
105
MG-lo
cal-P
CA M
ethod
for t
he
Redu
ction
of a
Collis
ional-
Radia
tive
Argo
n Pla
sma M
echa
nism
A. Be
llema
ns, T
. Mag
in, vo
n Kárm
án
Institu
te for
Fluid
Dyn
amics
, Rho
de-Sa
int-
Genè
se, B
elgium
; G. D
egrez
, A. P
arente
, Un
iversi
ty of
Brus
sels,
Brus
sels,
Belg
ium
1530
hrs
AIAA-2
015-3
106
Redu
ced-
Orde
r Mod
els of
Low-
Temp
erat
ure G
as D
ischa
rges
in
Glow
Mod
eE.
Cisne
ros, L
. Mas
sa, U
nivers
ity of
Texa
s, Arl
ington
, Arlin
gton,
TX
1600
hrs
AIAA-2
015-3
107
Enth
alpy C
hara
cteriz
ation
and
Asse
ssmen
t of C
oppe
r Cat
alysis
De
termi
natio
n in
Indu
ctive
ly Co
upled
Plas
ma Fa
cility
A. Vil
adeg
ut, vo
n Kárm
án In
stitut
e for
Fluid
Dyna
mics,
Rhod
e-Sain
t-Gen
èse,
Belgi
um
1630
hrs
AIAA-2
015-3
108
Nume
rical
Simula
tion
of Tw
o-Di
mens
ional
Struc
ture
of G
low
Disch
arge
in M
olecu
lar H
ydro
gen
S. S
urzhik
ov, D
. Stor
ozhe
v, Ru
ssian
Ac
adem
y of S
cienc
es, M
osco
w, Ru
ssia
97
Wedn
esda
y, 24
June
201
521
7-TP
-11
Aero
ther
mody
nami
cs III
Rose
ttaCh
aired
by: T
. LAM
, The
Aeros
pace
Corpo
ration
1400
hrs
AIAA-2
015-3
109
Glob
al Ae
rohe
ating
Mea
sure
ment
s of
Shoc
k-Sh
ock
Inter
actio
ns on
a Sw
ept C
ylind
erM.
Mas
on, S
. Berr
y, NA
SA La
ngley
Re
searc
h Cen
ter, H
ampto
n, VA
1430
hrs
AIAA-2
015-3
110
Aero
ther
mody
nami
c Cha
racte
ristic
s of
16-
22 k
m/s E
arth
Entry
C. Jo
hnsto
n, NA
SA La
ngley
Rese
arch
Cente
r, Ham
pton,
VA; A
. Bran
dis, E
RC,
Inc.,
Moffe
tt Fie
ld, CA
1500
hrs
AIAA-2
015-3
111
Radia
tive H
eatin
g on
the A
fter-
Body
of M
artia
n En
try Ve
hicles
A. Br
andis
, B. C
ruden
, T. W
hite,
D.
Saun
ders,
ERC,
Inc.,
Moffe
tt Fie
ld, CA
; C.
John
ston,
NASA
Lang
ley Re
searc
h Cen
ter,
Hamp
ton, V
A
1530
hrs
AIAA-2
015-3
112
Coup
led Fl
ow, R
adiat
ion, a
nd Ab
lation
Sim
ulatio
ns of
Atmo
sphe
ric En
try
Vehic
les us
ing th
e Hyb
rid St
atisti
cal
Narro
w Ba
nd M
odel
J. Sc
oggin
s, L.
Souca
sse, v
on Ká
rmán
Instit
ute
for Fl
uid Dy
nami
cs, Rh
ode-S
aint-G
enèse
, Be
lgium;
P. Riv
iere,
A. So
ufian
i, Écol
e Cen
trale
de Pa
ris, Pa
ris, Fr
ance;
T. M
agin,
von K
ármán
Ins
titute
for Fl
uid Dy
nami
cs, Rh
ode-S
aint-
Genè
se, Be
lgium
Wedn
esda
y, 24
June
201
521
8-NW
-7
1530
- 16
00 h
rsNe
twor
king C
offe
e Bre
akCh
antill
y Ball
room
East
Wedn
esda
y, 24
June
201
521
9-RL
A-2
1530
- 17
00 h
rsRi
sing L
eade
rs in
Aero
spac
e: Le
ader
ship
Exch
ange
/Spe
ed N
etwor
king
Metro
polita
n Ba
llroo
m
Get y
our q
uesti
ons a
nswe
red!
Senio
r Men
tors w
ill inc
lude:
Russ
Alth
ofCh
ief En
ginee
rRa
ytheo
n Miss
ile S
ystem
s
Cees
Bil
Profes
sor, R
oyal
Melbo
urne I
nstitu
te of
Tech
nolog
y
Dave
Bow
lesCe
nter D
irecto
r (Ac
ting)
NASA
Lang
ley Re
searc
h Cen
ter
Ed Fe
ltrop
Engin
eer S
pecia
listCe
ssna A
ircraf
t Com
pany
Susa
n Go
rton
Rotar
y Wing
Proje
ctNA
SA La
ngley
Rese
arch C
enter
Peter
Har
twich
Engin
eerin
g Man
ager
Boein
g Defe
nse,
Spac
e and
Sec
urity
Janic
e Kav
andi
Depu
ty Dir
ector
NASA
Glen
n Res
earch
Cente
r
Jeff
Jeps
onSe
nior M
ulti-D
iscipl
ined E
ngine
er I
Rayth
eon M
issile
Sys
tems
Sama
ntha
A. M
agill
Acad
emic
Affair
s and
Inclu
sion &
Dive
rsity
Hond
a Airc
raft C
ompa
ny
Sand
y Mag
nus
Exec
utive
Dire
ctor
AIAA
David
McB
ride
Cente
r Dire
ctor
NASA
Arms
trong
Fligh
t Res
earch
Cente
r
Char
les Sm
ithCe
nter D
irecto
r (Ac
ting)
NASA
Ames
Rese
arch C
enter
John
Valas
ekPro
fessor
/Dire
ctor, V
ehicle
Syste
ms &
Contr
ol La
borat
oryTe
xas A
&M U
nivers
ity
Wedn
esda
y, 24
June
201
522
0-LE
C-3
1630
- 17
30 h
rsAe
rody
nami
cs Aw
ard L
ectu
reCh
antill
y Ball
room
Wes
t
Still T
rying
to U
nders
tand A
ircraf
t Vort
ices
Russe
ll M. C
ummi
ngs
Profes
sor o
f Aero
nauti
csDe
partm
ent o
f Aero
nauti
csU.
S. Ai
r Forc
e Aca
demy
Wedn
esda
y, 24
June
201
522
1-LE
C-4
1730
- 18
30 h
rsAe
roac
ousti
cs Le
cture
Chan
tilly B
allro
om W
est
Fan B
roadb
and N
oise G
enera
tion a
nd Su
ppres
sion
Edma
ne En
viaAe
roaco
ustic
s Bran
chNA
SA G
lenn R
esea
rch Ce
nter
98
Wedn
esda
y, 24
June
201
522
2-LE
C-5
1730
- 18
30 h
rsTh
ermo
phys
ics A
ward
Lectu
reGr
and B
allro
om E
Aerod
ynam
ics an
d Hea
t Tran
sfer in
Gas T
urbine
Cooli
ng-Re
cent A
dvan
cesSu
mant
a Ach
arya
Ring C
hair &
Profe
ssor
Mech
anica
l Eng
ineeri
ng D
epart
ment
Unive
rsity
of Me
mphis
Wedn
esda
y, 24
June
201
522
3-BA
NQ-1
19
00 -
2030
hrs
Aero
acou
stics
Awar
ds R
ecep
tion
and B
anqu
etIm
peria
l Ball
room
The A
eroac
ousti
cs Aw
ards R
ecep
tion a
nd B
anqu
et wi
ll beg
in wi
th a c
ash b
ar so
cial p
eriod
at 1
900
hrs, f
ollow
ed by
the a
wards
cerem
ony a
nd ba
nque
t whe
re the
AIAA
and C
EAS
Aeroa
cous
tics A
wards
will
be pr
esen
ted.
The w
inner
of the
Aeroa
cous
tics S
tuden
t Pap
er Co
mpeti
tion a
lso w
ill be
reco
gnize
d. Ple
ase j
oin us
and c
elebra
te the
achie
veme
nts of
your
peers
.Tic
kets
will b
e ava
ilable
at on
site
as sp
ace i
s ava
ilable
.
Thur
sday
Thur
sday
, 25
June
201
522
4-SB
-4
0730
- 08
00 h
rsSp
eake
rs’ B
riefin
gSe
ssion
Roo
ms
Thur
sday
, 25
June
201
522
5-PL
NRY-4
08
00 -
0900
hrs
Plena
ry K
eyno
teCh
antill
y Ball
room
Wes
t
DHS’s
Persp
ective
s on C
ybers
ecurity
in Av
iation
Greg
ory J
. Tou
hill
Depu
ty As
sistan
t Sec
retary
for O
ffice o
f Cyb
ersec
urity
and C
ommu
nicati
ons
Depa
rtmen
t of H
omela
nd S
ecuri
ty
Thur
sday
, 25
June
201
522
6-AA
-31
Inter
ior N
oise
Edelw
eiss
Chair
ed by
: N. A
GARW
AL, B
oeing
Defe
nse,
Spac
e & S
ecuri
ty09
00 hr
sOr
al Pre
senta
tion
Poro
elasti
c Aco
ustic
Meta
Mat
erial
s (In
vited
)C.
Fulle
r, Virg
inia P
olytec
hnic
Institu
te an
d Stat
e Univ
ersity
, Blac
ksbu
rg, VA
1000
hrs
AIAA-2
015-3
113
Low
Freq
uenc
y Nois
e Red
uctio
n Us
ing P
oro-
Elasti
c Aco
ustic
Me
tama
terial
sA.
Slagle
, C. F
uller, V
irginia
Polyt
echnic
Ins
titute
and S
tate U
nivers
ity, Bl
acksbu
rg, VA
1030
hrs
AIAA-2
015-3
114
Identi
ficati
on of
sour
ces of
noise
in th
e ca
bin an
d the
defin
ition o
f the
loca
l pa
ssage
of so
und e
nerg
y thr
ough
fus
elage
based
on th
e resu
lts of
in-
flight
meas
urem
ents
of the
Supe
rjet
R. Ab
drashi
tov, S
ukho
i Civil
Aircr
aft Co
mpan
y, Mo
scow,
Russi
a; A.
Golub
ev, Ts
AGI,
Zhuk
ovsky
, Russ
ia
1100
hrs
AIAA-2
015-3
115
Fuse
lage E
xcita
tion
Durin
g Cru
ise
Fligh
t Con
dition
s: Me
asur
emen
t an
d Pre
dictio
n of
Pre
ssure
Poin
t Sp
ectra
A. Kla
bes,
M. H
err, C
. App
el, G
erman
Ae
rospa
ce Ce
nter (
DLR)
, Brau
nsch
weig,
Ge
rman
y; M.
Bou
haj, A
irbus
Ope
ration
s Gm
bH, H
ambu
rg, G
erman
y
1130
hrs
AIAA-2
015-3
116
Effe
ct of
pres
sure
grad
ients
on
turb
ulent
boun
dary
laye
r vor
tical
struc
ture
s and
wall
-pre
ssure
flu
ctuat
ions
M. Al
aoui,
X. G
loerfe
lt, Pa
ris In
stitut
e of
Tech
nolog
y, Pa
ris, F
rance
; O. C
ollery
, M.
Etche
ssaha
r, Airb
us, T
oulou
se, F
rance
1200
hrs
AIAA-2
015-3
117
Effe
ct of
pres
sure
grad
ients
on
turb
ulent
boun
dary
laye
r nois
e and
wa
ll-pr
essu
re fl
uctu
ation
sE.
Cohe
n, X.
Gloe
rfelt,
Paris
Insti
tute o
f Te
chno
logy,
Paris
, Fran
ce
99
Thur
sday
, 25
June
201
522
7-AA
-32
Jet N
oise M
easu
reme
nts I
IIFle
ur-d
e-lis
ACh
aired
by: D
. PAP
AMOS
CHOU
, Univ
ersity
of Ca
liforni
a Irvi
ne09
00 hr
sAIA
A-201
5-311
8In
stalle
d jet-
flap i
mping
emen
t to
nal n
oise
J. La
wren
ce, R
. Self
, Univ
ersity
of
South
ampto
n, So
utham
pton,
Unite
d Kin
gdom
0930
hrs
AIAA-2
015-3
119
Noise
mea
sure
ment
s of h
igh as
pect
ratio
distr
ibuted
exha
ust s
ystem
sJ.
Bridg
es, M
. Wern
et, N
ASA G
lenn
Rese
arch C
enter
, Clev
eland
, OH
1000
hrs
AIAA-2
015-3
120
Meas
urem
ents
and P
redic
tions
of
the N
oise f
rom
Thre
e-Str
eam
Jets
B. H
ende
rson,
S. Le
ib, N
ASA G
lenn
Rese
arch C
enter
, Clev
eland
, OH
1030
hrs
AIAA-2
015-3
121
Flow
Field
and A
cous
tic
Inve
stiga
tions
of th
e Lau
nch
Vehic
le En
viron
ment
durin
g Lift
-off
K. Na
taraja
n, L.
Venk
atakri
shna
n, Na
tiona
l Ae
rospa
ce La
borat
ories
, Ban
galor
e, Ind
ia
1100
hrs
AIAA-2
015-3
122
An Ex
perim
ental
Stud
y of C
oaxia
l Jets
Us
ing Ac
ousti
c PIV
and L
DA M
ethod
s (C
oJeN
)C.
Mead
, Aero
Acou
stics,
Ltd., E
lstead
, Unit
ed
Kingd
om; C
. Wrig
hton,
Qineti
Q, Fa
rnboro
ugh,
Unite
d King
dom;
K. Br
itchfor
d, Ro
lls-Ro
yce
Group
plc,
Derby
, Unit
ed Ki
ngdo
m
1130
hrs
AIAA-2
015-3
123
Expe
rimen
tal a
nd n
umer
ical s
tudy
of
the n
oise g
ener
ation
in an
ou
tflow
butte
rfly v
alve
A. Ch
auvin
, Y. P
asco
, M. S
anjos
e, G.
Lo
bel, A
. Mars
an, S
. More
au, U
nivers
ity of
Sh
erbroo
ke, S
herbr
ooke
, Can
ada;
et al.
Thur
sday
, 25
June
201
522
8-AA
-33
Jet N
oise M
odeli
ng II
Fleur
-de-
lis B
Chair
ed by
: C. B
ROW
N, N
ASA G
lenn R
esea
rch Ce
nter
0900
hrs
AIAA-2
015-3
124
Nonli
near
inter
actio
n an
alysis
of
subs
onic
jet in
stabil
ities w
ith fo
rced
eigen
mode
s usin
g PSE
M. It
asse
, J. B
razier
, O. L
éon,
G. Ca
salis,
ON
ERA,
Toulo
use,
Franc
e
0930
hrs
AIAA-2
015-3
125
Linea
r Sta
bility
Impli
catio
ns of
Me
an Fl
ow Va
riatio
ns in
Turb
ulent
Je
ts Iss
uing f
rom
Serra
ted N
ozzle
sA.
Sinha
, Ind
ian In
stitut
e of T
echn
ology
Bo
mbay
, Mum
bai, I
ndia;
T. Co
lonius
, Ca
liforni
a Ins
titute
of Te
chno
logy,
Pasa
dena
, CA
1000
hrs
AIAA-2
015-3
126
On th
e Com
paris
on of
the L
ong
Pene
tratio
n Mo
de (L
PM) S
uper
sonic
Co
unter
flowi
ng Je
t to t
he
Supe
rsonic
Scre
ech
Jet
R. Fa
rr, NA
SA M
arsha
ll Spa
ce Fl
ight
Cente
r, Hun
tsville
, AL;
C. Ch
ang,
NASA
La
ngley
Rese
arch C
enter
, Ham
pton,
VA; J
. Jo
nes,
AI Sig
nal R
esea
rch, I
nc.,
Hunts
ville,
AL
; N. D
ough
erty,
ERC,
Inc.,
Hunts
ville,
AL
1030
hrs
AIAA-2
015-3
127
Theo
retic
al Mo
dellin
g Of
Broa
dban
d Sho
ck A
ssocia
ted N
oise
in As
ymme
tric J
etsA.
Kalya
n, S.
Karab
asov
, Que
en M
ary
Unive
rsity
of Lo
ndon
, Lon
don,
Unite
d Kin
gdom
1100
hrs
AIAA-2
015-3
128
Empir
ical M
odels
for t
he Sh
ieldin
g an
d Refl
ectio
n of
Jet M
ixing
Nois
e by
a Su
rface
C. Br
own,
NASA
Glen
n Res
earch
Cente
r, Cle
velan
d, OH
1130
hrs
AIAA-2
015-3
129
Comp
utatio
nal m
odell
ing of
jet-w
ing
intera
ction
: the e
ffect
of as
ymme
tries
fro
m the
jet in
flow
cond
itions
and
the w
ingV.
Semi
letov,
Que
en M
ary Un
iversit
y of
Lond
on, L
ondo
n, Un
ited K
ingdo
m; P.
Yako
vlev,
North
-Easte
rn Fe
deral
Unive
rsity,
Yaku
tsk,
Russi
a; S.
Karab
asov,
Quee
n Mary
Unive
rsity
of Lo
ndon
, Lon
don,
Unite
d King
dom;
G.
Faran
osov,
V. Ko
piev,
TsAGI,
Mosc
ow, R
ussia
1200
hrs
AIAA-2
015-3
130
Refra
ction
Effe
ct in
Corre
lation
Mo
del o
f Qua
drup
ole N
oise S
ource
s in
Turb
ulent
Jet
V. Ko
piev,
S. Ch
ernys
hev,
TsAGI
, Mos
cow,
Ru
ssia
Thur
sday
, 25
June
201
522
9-AA
-34
CAA
Nume
rical
Tech
nique
s III
Inve
rnes
sCh
aired
by: S
. ARU
NAJAT
ESAN
, San
dia N
ation
al La
bs09
00 hr
sAIA
A-201
5-313
1A
study
of ac
cura
cy on
num
erica
l me
thod
s for
non
unifo
rm m
eshe
s (In
vited
)F.
Hu, O
ld Do
minio
n Univ
ersity
, Norf
olk,
VA; A
. Fern
ando
, Norf
olk S
tate U
nivers
ity,
Norfo
lk, VA
0930
hrs
AIAA-2
015-3
132
Aero
acou
stic C
alcula
tions
of th
e 30
P30N
High
-lift A
irfoil
using
Hyb
rid
RANS
/LES
meth
ods:
Mode
ling a
nd
Grid
Reso
lution
Effec
tsM.
Terra
col, E
. Man
oha,
ONER
A, Ch
âtillon
, Fra
nce; M
. Mura
yama
, K. Y
amam
oto, J
apan
Ae
rospa
ce Ex
plorat
ion Ag
ency
(JAXA
), Tok
yo,
Japan
1000
hrs
AIAA-2
015-3
133
A dir
ect-h
ybrid
meth
od fo
r co
mput
ation
al ae
roac
ousti
csM.
Sch
lottke
, H. C
heng
, V. P
auz,
M.
Meink
e, W.
Sch
roede
r, RW
TH Aa
chen
Un
iversi
ty, Aa
chen
, Germ
any
1030
hrs
AIAA-2
015-3
134
Hybr
id Ma
cCor
mack
-type
Sche
mes
for C
ompu
tatio
nal A
eroa
cous
tics
S. Ya
zdan
i, D. H
ixon,
Unive
rsity
of To
ledo,
Toled
o, OH
1100
hrs
AIAA-2
015-3
135
Deve
lopme
nt of
comp
ressib
le lar
ge-
eddy
simula
tions
comb
ining
high
-or
der s
chem
es an
d wall
mod
eling
S. Le
Bras,
CERF
ACS,
Toulou
se, Fr
ance;
H.
Denia
u, ON
ERA,
Toulou
se, Fr
ance;
C. Bo
gey,
École
Centr
ale de
Lyon
, Ecul
ly, Fra
nce; G
. Da
viller,
CERF
ACS,
Toulou
se, Fr
ance
100
Thur
sday
, 25
June
201
523
0-AA
-35
Airfr
ame N
oise I
VLa
lique
Chair
ed by
: T. V
AN D
E VEN
, Gulf
strea
m09
00 hr
sAIA
A-201
5-313
6In
fluen
ce of
Span
wise
Bou
ndar
y Co
nditio
ns on
Slat
Nois
e Sim
ulatio
nsD.
Lock
ard, M
. Cho
udha
ri, P.
Bunin
g, NA
SA
Lang
ley Re
searc
h Cen
ter, H
ampto
n, VA
0930
hrs
AIAA-2
015-3
137
LEISA
2: an
expe
rimen
tal da
tabas
e for
the
valid
ation
of nu
meric
al pr
edict
ions
of sla
t uns
teady
flow
and n
oise
E. Ma
noha
, ONE
RA, C
hâtillo
n, Fra
nce; M
. Po
tt-Polle
nske,
Germ
an Ae
rospa
ce Ce
nter
(DLR
), Bra
unsch
weig,
Germ
any
1000
hrs
AIAA-2
015-3
138
Expe
rimen
tal s
tudy
of th
e effe
ct of
a s
mall 2
D ex
cresce
nce p
laced
on
the s
lat co
ve su
rface
of an
airfo
il on
its a
cous
tic n
oise
F. Am
aral, D
. Sou
za, C
. Pag
ani, M
. Me
deiro
s, Un
iversi
ty of
São P
aulo,
São
Jo
sé do
s Cam
pos,
Braz
il
1030
hrs
AIAA-2
015-3
139
Slat N
oise P
redic
tion
using
Hyb
rid
RANS
-LES m
ethod
s on
Struc
ture
d an
d Uns
tructu
red G
rids
N. As
hton,
Unive
rsity
of Ma
nche
ster,
Manc
heste
r, Unit
ed Ki
ngdo
m; A.
Wes
t, CD
-adap
co, L
ondo
n, Un
ited K
ingdo
m; F.
Me
ndon
ca, S
elf, L
ondo
n, Un
ited K
ingdo
m
1100
hrs
AIAA-2
015-3
140
Larg
e-Sc
ale St
udies
on Sl
at N
oise
Redu
ction
M. H
err, M
. Pott
-Polle
nske
, R. E
wert,
B.
Dirk
, J. S
iebert
, J. D
elfs,
Germ
an
Aeros
pace
Cente
r (DL
R), B
rauns
chwe
ig,
Germ
any;
et al.
1130
hrs
AIAA-2
015-3
141
Study
on N
oise G
ener
ation
from
Sla
t Tra
cks U
sing a
High
-Lift
Wing
Mo
del
M. M
uraya
ma, Y
. Yok
okaw
a, Y.
Ito, K
. Ya
mamo
to, T.
Taka
ishi, H
. Ura,
Japa
n Ae
rospa
ce Ex
plorat
ion Ag
ency
(JAX
A),
Mitak
a, Ja
pan
1200
hrs
AIAA-2
015-3
142
On th
e Nois
e Gen
erat
ion of
Kr
uege
r Lea
ding E
dge D
evice
sM.
Pott-P
ollen
ske,
J. W
ild, G
erman
Ae
rospa
ce Ce
nter (
DLR)
, Brau
nsch
weig,
Ge
rman
y
Thur
sday
, 25
June
201
523
1-AA
-36
Gene
ral A
cous
tics I
IIOb
elisk
ACh
aired
by: C
. SCH
RAM
0900
hrs
AIAA-2
015-3
143
Expe
rimen
tal A
pplic
ation
of
Aero
acou
stic T
ime-
Reve
rsal
A. Mi
mani,
D. M
oreau
, C. D
oolan
, Un
iversi
ty of
Adela
ide, A
delai
de, A
ustra
lia
0930
hrs
AIAA-2
015-3
144
Expe
rimen
tal I
nves
tigat
ion of
the
Unste
ady P
ressu
re on
a Hy
drof
oil
due t
o the
Inge
stion
of Tu
rbule
nce
and H
ydro
-elas
tic M
otion
M. Ca
tlett,
J. An
derso
n, Na
val S
urfac
e Wa
rfare
Cente
r, Wes
t Beth
esda
, MD
1000
hrs
AIAA-2
015-3
145
An Ex
perim
enta
l Stu
dy of
Co
mpos
ite M
ater
ials f
or th
e Des
ign
of Q
uiet U
AVs
J. Ca
llicoa
t, R.
Gaeta
, J. J
acob
, Okla
homa
St
ate U
nivers
ity, S
tillwa
ter, O
K
1030
hrs
AIAA-2
015-3
146
On th
e Rele
vanc
e of C
onve
ction
Ef
fects
for a
Lase
r-Gen
erat
ed
Soun
d Sou
rceK.
Rossi
gnol,
J. D
elfs,
L. Ro
ssian
, F.
Bode
n, Ge
rman
Aeros
pace
Cente
r (DL
R),
Brau
nsch
weig,
Germ
any
1100
hrs
AIAA-2
015-3
147
Flow
Noise
Gen
erat
ion of
Cylin
ders
with
Soft
Poro
us Co
ver
T. Ge
yer, E
. Sarr
adj, G
. Hero
ld,
Bran
denb
urg U
nivers
ity of
Tech
nolog
y, Co
ttbus
, Germ
any
1130
hrs
AIAA-2
015-3
148
An ex
perim
enta
l inve
stiga
tion
of
wall p
ressu
re fl
uctu
ation
s ben
eath
pr
essu
re gr
adien
tsE.
Salze
, C. B
ailly,
O. M
arsde
n, E.
Jond
eau,
D. Ju
ve, É
cole
Centr
ale de
Lyon
, Ec
ully,
Franc
e
Thur
sday
, 25
June
201
523
2-AC
D-6
0900
- 12
00 h
rsCo
ncep
tual
Aircr
aft D
esign
Wor
king G
roup
(CAD
WG21
) Pan
elWy
eth
Chair
ed by
: W. A
NEMA
AT, D
ARco
rporat
ion an
d T. T
AKAH
ASHI
, Ariz
ona S
tate U
nivers
ity
The N
eed o
f Com
munit
y-Acce
pted P
ublic
Doma
in /
Open
Sourc
e Sizi
ng Co
des
P
aneli
sts:
Clif D
avis
Lock
heed
Mart
in Ae
ronau
tics
Jaso
n We
lstea
dNA
SA La
ngley
Joaq
uim M
artin
sUn
iversi
ty of
Mich
igan
Mark
Pag
eDZ
YNE T
echn
ologie
sSte
ve K
omad
inaNo
rthrop
-Grum
man
Rob M
cDon
aldCa
lPoly
Thur
sday
, 25
June
201
523
3-AP
A-25
Appli
ed CF
D &
Nume
rical
Corre
lation
s with
Expe
rimen
tal D
ata I
IISte
mmon
s BCh
aired
by: K
. ABD
OL-HA
MID,
NAS
A Lan
gley R
esea
rch Ce
nter a
nd A.
SCL
AFAN
I, Bo
eing E
ngine
ering
Ope
ration
s & Te
chno
logy
0900
hrs
AIAA-2
015-3
149
Time-A
ccura
te Un
stead
y Pres
sure
Lo
ads S
imula
ted fo
r the
Spac
e Lau
nch
Syste
m at
Wind
Tunn
el Co
nditio
nsS.
Alter,
G. Br
auckm
ann,
W. Kl
eb, C
. Stre
ett,
C. Gla
ss, D.
Schu
ster, N
ASA L
angle
y Rese
arch
Cente
r, Ham
pton,
VA
0930
hrs
AIAA-2
015-3
150
Cont
inuou
s Rad
ial Je
t in
Annu
lar
Cros
s-flow
P. Ra
jput,
I. Ka
lkhora
n, NY
U Po
lytec
hnic
Scho
ol of
Engin
eerin
g, Br
ookly
n, NY
1000
hrs
AIAA-2
015-3
151
Simula
tion
of a
Flapp
ing W
ing U
AV
using
a Co
upled
CFD-
Cont
rol T
ool
J. Ge
der, R
. Ram
amurt
i, K. V
iswan
ath, N
aval
Resea
rch La
borat
ory, W
ashing
ton, D
C
1030
hrs
AIAA-2
015-3
152
Outpu
t-Bas
ed Ad
aptiv
e Mesh
ing
Appli
ed to
Spac
e Lau
nch S
ystem
Bo
oster
Sepa
ratio
n Ana
lysis
D. Da
lle, Sc
ience
and T
echno
logy C
orpora
tion,
Moffe
tt Field
, CA;
S. Ro
gers,
NAS
A Ame
s Re
search
Cente
r, Moff
ett Fi
eld, C
A
1100
hrs
AIAA-2
015-3
153
Impr
ovem
ent o
f CFD
resu
lts of
NAS
A CR
M by
on-lin
e mesh
defor
matio
n us
ing m
odal
analy
sis of
a wi
ngP. V
rchota
, A. P
racha
r, Aero
space
Resea
rch an
d Tes
t Esta
blishm
ent, P
rague
, Cze
ch Re
public
101
Thur
sday
, 25
June
201
523
4-AP
A-26
Unma
nned
, Bio-
Insp
ired,
Solar
Pow
ered
Aer
ial Ve
hicle
Desig
ns II
Carp
enter
Ball
room
Chair
ed by
: M. O
L, US
Air F
orce R
esea
ch La
borat
ory an
d A. M
ITTAL
, The
Univ
ersity
of Te
nnes
see a
t Cha
ttano
oga
0900
hrs
AIAA-2
015-3
154
Dyna
mica
l Cha
racte
rizat
ion of
a Bi
o-In
spire
d Wing
with
Pas
sively
Ac
tuat
ed Ed
ges
C. Pla
nck,
F. Sia
la, J.
Libu
rdy, O
regon
St
ate U
nivers
ity, C
orvall
is, O
R
0930
hrs
AIAA-2
015-3
155
Nume
rical
Simula
tion
of a
Flapp
ing
Wing
in A
nsys
-Flue
nt B
ased
on th
e Fr
uit Fl
y Wing
Kine
matic
sB.
Niet
o, X.
Alfon
so, K
. Bas
to, J.
Esco
bar,
Unive
rsity
of Sa
n Bue
nave
ntura,
Bog
ota,
Colom
bia
1000
hrs
AIAA-2
015-3
156
Aero
dyna
mics
of So
uthe
rn H
awke
r Dr
agon
fly: A
eshn
a cya
nea
S. S
rigrar
om, C
. Thip
yopa
s, Ka
setsa
rt Un
iversi
ty, B
angk
ok, T
haila
nd
1030
hrs
AIAA-2
015-3
157
Deve
lopme
nt an
d Ana
lysis
of G
ull
Insp
ired U
AV Fl
appin
g Wing
D. Ku
mar, T
. Goy
al, S
. Vem
uri, P
. Moh
ite,
S. Ka
mle,
Indian
Insti
tute o
f Tec
hnolo
gy
Kanp
ur, Ka
npur,
India
1100
hrs
AIAA-2
015-3
158
Deve
lopme
nt an
d Aer
o-str
uctu
ral
Analy
sis of
Ligh
t and
Stro
ng
Carb
on Fi
ber-C
NT/P
P Hu
mming
bird
Insp
ired M
AV W
ings
D. Ku
mar, S
. Kum
ar, T.
Goy
al, P.
Moh
ite,
S. Ka
mle,
Indian
Insti
tute o
f Tec
hnolo
gy
Kanp
ur, Ka
npur,
India
Thur
sday
, 25
June
201
523
5-AP
A-27
Airfo
il/Wi
ng/C
onfig
urat
ion A
erod
ynam
icsSte
mmon
s CCh
aired
by: A
. MCC
OMAS
, TLG
Aeros
pace
and J
. GUG
LIELM
O, B
oeing
Defe
nse,
Spac
e & S
ecuri
ty09
00 hr
sAIA
A-201
5-315
9Im
prov
ed St
all P
redic
tion
for
Swep
t Wing
s Usin
g Low
-Ord
er
Aero
dyna
mics
P. Ho
sanga
di, R.
Paul,
A. Go
palar
athna
m,
North
Carol
ina St
ate Un
iversit
y, Ra
leigh,
NC
0930
hrs
AIAA-2
015-3
160
Mode
ling a
nd P
redic
tion
of
the C
rossfl
ow Tr
ansit
ion U
sing
Trans
ition
Trans
port
Equa
tions
J. Sa
, S. P
ark, K
onku
k Univ
ersity
, Seo
ul,
South
Korea
; K. C
ho, K
orea U
nivers
ity
of Sc
ience
and T
echn
ology
, Dae
jeon,
South
Korea
; K. J
ung,
Agen
cy fo
r Defe
nse
Deve
lopme
nt, D
aejeo
n, So
uth Ko
rea
1000
hrs
AIAA-2
015-3
161
On th
e res
ulting
aero
dyna
mic
loss o
f com
binat
ions o
f loc
alize
d su
rface
roug
hnes
s pat
ches
on a
turb
ine bl
ade
P. Gil
ge, K
. Mull
eners
, Leib
niz U
nivers
ity,
Hann
over,
Germ
any
1030
hrs
AIAA-2
015-3
162
Aero
-Pro
pulsi
ve Co
uplin
g of a
n Em
bedd
ed, D
istrib
uted
Pro
pulsi
on
Syste
mM.
Kerho
, Roll
ing H
ills Re
searc
h Co
rporat
ion, E
l Seg
undo
, CA
1100
hrs
AIAA-2
015-3
163
Aero
dyna
mic P
erfo
rman
ce of
the
Adap
tive N
acell
e Inle
tF.
Majić
, G. E
fraim
sson,
C. O’
Reilly
, Roy
al Ins
titute
of Te
chno
logy (
KTH)
, Stoc
kholm
, Sw
eden
1130
hrs
AIAA-2
015-3
164
Comp
utat
ional
Asse
ssmen
t of
Rain
fall E
ffects
on A
ircra
ft Ae
rody
nami
c Cha
racte
ristic
sH.
Sha
rma,
S. H
arshe
, S. V
ekari
a, M.
Sin
gh, M
. Dam
odara
n, Ind
ian In
stitut
e of
Tech
nolog
y Gan
dhina
gar, A
hmed
abad
, Ind
ia; B
. Kho
o, Na
tiona
l Univ
ersity
of
Singa
pore,
Sing
apore
, Sing
apore
Thur
sday
, 25
June
201
523
6-AP
A-28
Unste
ady A
erod
ynam
ics I
Stemm
ons A
Chair
ed by
: K. K
ARA,
Khali
fa Un
iversi
ty of
Scien
ce, T
echn
ology
& Re
searc
h and
J. RA
ULED
ER, T
echn
ical U
nivers
ity of
Mun
ich09
00 hr
sAIA
A-201
5-316
5Me
asur
emen
ts of
Dyn
amic
Inter
face
Betw
een
Ship
and
Helic
opter
Air
Wake
sC.
Fried
man,
Georg
e Was
hingto
n Un
iversi
ty, W
ashin
gton,
DC; M
. Sny
der,
U.S.
Nav
al Ac
adem
y, An
napo
lis, M
D
0930
hrs
AIAA-2
015-3
166
An Ex
perim
enta
l Stu
dy of
Add
ed
Mass
on a
Plung
ing A
irfoil
Os
cillat
ing w
ith H
igh Fr
eque
ncies
at
High
Ang
les of
Atta
ckM.
Zaka
ria, V
irgini
a Poly
techn
ic Ins
titute
and S
tate U
nivers
ity, B
lacks
burg,
VA;
D. Pe
reira,
Univ
ersity
of S
ão Pa
ulo, S
ão
Paulo
, Braz
il; S.
Raga
b, M.
Hajj
, Virg
inia
Polyt
echn
ic Ins
titute
and S
tate U
nivers
ity,
Black
sburg
, VA;
F. Ma
rques
, Univ
ersity
of
São P
aulo,
São
Paulo
, Braz
il
1000
hrs
AIAA-2
015-3
167
Expe
rimen
tal-B
ased
Unifi
ed
Unste
ady N
onlin
ear A
erod
ynam
ic Mo
delin
g For
Two-
Dime
nsion
al Ai
rfoils
M. Za
karia
, Virg
inia P
olytec
hnic
Institu
te an
d Stat
e Univ
ersity
, Blac
ksbu
rg, VA
; H.
Taha
, Univ
ersity
of Ca
liforni
a, Irv
ine,
Irvine
, CA;
M. H
ajj, A
. Hus
sein,
Virg
inia
Polyt
echn
ic Ins
titute
and S
tate U
nivers
ity,
Black
sburg
, VA
1030
hrs
AIAA-2
015-3
168
Expe
rimen
tal D
ynam
ic Sta
ll stu
dy
on a
low R
eyno
lds n
umbe
r airf
oilS.
Algo
zino,
J. Ma
rañon
Di L
eo, J
. De
lnero,
G. C
apitti
ni, N
ation
al Un
iversi
ty of
La Pl
ata, L
a Plat
a, Arg
entin
a
1100
hrs
AIAA-2
015-3
169
Unste
ady A
erod
ynam
ic Mo
delin
g of
Roll
ing P
arac
hutes
Usin
g the
In
dicial
Meth
odM.
Gho
reysh
i, U.S
. Air F
orce A
cade
my,
Color
ado S
pring
s, CO
; K. B
ergero
n, Arm
y Re
searc
h, De
velop
ment
and E
ngine
ering
Co
mman
d, Na
tick,
MA; J
. Seid
el, A.
Lo
fthou
se, R
. Cum
ming
s, U.
S. Ai
r Forc
e Ac
adem
y, Co
lorad
o Spri
ngs,
CO
1130
hrs
AIAA-2
015-3
170
Subs
onic
Indic
ial A
erod
ynam
ics
for U
nstea
dy Lo
ads C
alcula
tion
via
Nume
rical
and A
nalyt
ical
Meth
ods:
a Pre
limina
ry A
ssessm
ent
M. Ri
ghi, Z
urich
Univ
ersity
of Ap
plied
Sc
ience
s, W
intert
hur, S
witze
rland
; M.
Berci
, Univ
ersity
of Le
eds,
Leed
s, Un
ited
Kingd
om; J
. Koc
h, Zu
rich U
nivers
ity of
Ap
plied
Scie
nces
, Wint
erthu
r, Swi
tzerla
nd
1200
hrs
AIAA-2
015-3
171
Imple
ment
ation
of Vo
rtex-
type
Gu
st Mo
del T
hrou
gh B
ound
ary
Cond
itions
E. Elj
ack,
I. AlQ
adi, K
ing Ab
dulaz
iz Un
iversi
ty, Je
edah
, Sau
di Ara
bia
102
Thur
sday
, 25
June
201
523
7-AS
E-3Ai
rcraf
t Wak
e Tur
bulen
ce I
(Invit
ed)
Plum
Blos
som
BCh
aired
by: M
. PRU
IS, N
orthw
est R
esea
rch As
socia
tes In
c and
N. A
HMAD
, NAS
A Lan
gley R
esea
rch Ce
nter
0900
hrs
AIAA-2
015-3
172
Use o
f Sim
ple M
odels
to D
eterm
ine
Wake
Vorte
x Ca
tegor
ies fo
r New
Ai
rcraf
t (In
vited
)J.
Hallo
ck, D
epart
ment
of Tra
nspo
rtatio
n, Ca
mbrid
ge, M
A; G.
Gree
ne, J
. Titts
worth
, P.
Stran
de, F
edera
l Avia
tion A
dmini
strati
on,
Wash
ington
, DC;
F. Wa
ng, D
epart
ment
of Tra
nspo
rtatio
n, Ca
mbrid
ge, M
A
0930
hrs
AIAA-2
015-3
173
Multi-
Mode
l Ens
emble
Wak
e Vor
tex
Pred
iction
(Inv
ited)
S. Ko
erner,
Germ
an Ae
rospa
ce Ce
nter (
DLR)
, Ob
erpfaf
fenho
fen, G
erman
y; N.
Ahma
d, NA
SA La
ngley
Resea
rch Ce
nter, H
ampto
n, VA
; F. Ho
lzäpfe
l, Germ
an Ae
rospa
ce Ce
nter
(DLR
), Ob
erpfaf
fenho
fen, G
erman
y; R.
VanV
alken
burg,
NAS
A Lan
gley R
esearc
h Ce
nter, H
ampto
n, VA
1000
hrs
AIAA-2
015-3
174
Wind
Impa
ct on
Sing
le Vo
rtice
s and
Co
unter
-Rot
ating
Vorte
x Pa
irs in
Gr
ound
Pro
ximity
(Inv
ited)
F. Ho
lzäpfe
l, N. T
chipe
v, A.
Step
han,
Germ
an Ae
rospa
ce Ce
nter (
DLR)
, Ob
erpfaf
fenho
fen, G
erman
y
1030
hrs
AIAA-2
015-3
175
Sens
itivity
Ana
lysis
of A
ircra
ft En
coun
ters w
ith D
efor
med W
ake
Vorti
ces (
Invit
ed)
D. B
ieniek
, R. L
uckn
er, Te
chnic
al Un
iversi
ty of
Berlin
, Berl
in, G
erman
y
1100
hrs
AIAA-2
015-3
176
Asse
ssmen
t of W
akeM
od 4
: A N
ew
Stand
alone
Wak
e Vor
tex A
lgorit
hm
for E
stima
ting C
ircula
tion
Stren
gth
and P
ositio
n (In
vited
)D.
Jaco
b, Co
heren
t Res
earch
Grou
p, Or
mond
Bea
ch, F
L; D.
Lai, M
. Prui
s, D.
De
lisi, N
orthW
est R
esea
rch As
socia
tes,
Redm
ond,
WA
1130
hrs
AIAA-2
015-3
177
Obse
rvat
ions o
f Wak
e Vor
tices
from
Up
ward
Look
ing P
ulsed
Dop
pler
Lidar
Dat
a (In
vited
)M.
Pruis
, D. D
elisi,
Nort
hWes
t Res
earch
As
socia
tes, R
edmo
nd, W
A; D.
Jaco
b, Co
heren
t Res
earch
Grou
p, Or
mond
Be
ach,
FL
Thur
sday
, 25
June
201
523
8-AT
IO-2
1En
Rou
te Op
erat
ions
Milan
Chair
ed by
: M. K
OCH,
NAS
A Lan
gley R
esea
rch Ce
nter
0900
hrs
AIAA-2
015-3
178
Cont
rolle
r Wor
kload
-bas
ed
Calcu
lation
of M
onito
r Aler
t Pa
rame
ters f
or En
Rou
te Se
ctors
B. M
arr, K
. Lind
say,
MITR
E Corp
oratio
n, Mc
Lean
, VA
0930
hrs
AIAA-2
015-3
179
Optim
izatio
n of
the C
ruise
Reg
ime
of Fl
ight A
irplan
e Tra
jecto
ry u
sing
Deter
minis
tic A
lgorit
hms
M. G
autie
r, R. B
otez,
Unive
rsity
of Qu
ébec
, Mon
tréal,
Cana
da
1000
hrs
AIAA-2
015-3
180
Can
grou
nd-b
ased
sepa
ratio
n ac
comm
odat
e ver
y high
en ro
ute
traffi
c dem
and a
s well
as ad
vanc
ed
self-
sepa
ratio
n?H.
Blom
, B. B
akke
r, Nati
onal
Aeros
pace
La
borat
ory (N
LR),
Amste
rdam,
The
Nethe
rland
s
Thur
sday
, 25
June
201
523
9-AT
IO-2
2AT
M V -
Per
form
ance
Asse
ssmen
tMo
rocco
Chair
ed by
: D. D
ELAU
RENT
IS, Pu
rdue U
nivers
ity09
00 hr
sAIA
A-201
5-318
1Ve
rifyin
g Req
uired
Comm
unica
tion
Perfo
rman
ce in
Air
Traffi
c Ma
nage
ment
D. Ze
ng, J
. Gon
da, M
ITRE C
orpora
tion,
McLe
an, V
A
0930
hrs
AIAA-2
015-3
182
Meth
odolo
gy to
Defi
ne D
elive
ry
Accu
racy
Und
er Cu
rrent
Day
ATC
Oper
ation
sS.
Sha
rma,
J. Ro
binso
n III,
NASA
Ames
Re
searc
h Cen
ter, M
offett
Field
, CA
1000
hrs
AIAA-2
015-3
183
Inve
stiga
tion
of Co
nnec
tivity
: De
finitio
n, A
pplic
ation
, and
Fo
rmula
tion
L. Bo
wers,
L. M
ocku
s, S.
Tama
skar,
D.
DeLa
urenti
s, Pu
rdue U
nivers
ity, W
est
Lafay
ette,
IN
1030
hrs
AIAA-2
015-3
184
Regio
nal S
ky Tr
ansit
B. S
eeley
, CAF
E Fou
ndati
on, S
anta
Rosa
, CA
1100
hrs
AIAA-2
015-3
185
An A
irpor
t Asse
ssmen
t App
roac
h in
the C
once
ptua
l Des
ign St
age
M. W
eiss,
N. D
zikus
, Germ
an Ae
rospa
ce
Cente
r (DL
R), H
ambu
rg, G
erman
y
1130
hrs
AIAA-2
015-3
186
Mode
ling a
Ram
p Are
a Sup
port
Syste
mA.
Wing
, W. F
elder,
R. Cl
outie
r, Stev
ens
Institu
te of
Tech
nolog
y, Ho
boke
n, NJ
1200
hrs
AIAA-2
015-3
187
Fram
ewor
k De
velop
ment
for
Perfo
rman
ce Ev
aluat
ion of
the
Futu
re N
ation
al Ai
rspac
e Sys
temM.
Has
san,
A. Pa
yan,
H. Pf
aend
er, D
. Ma
vris,
E. Ga
rcia,
J. Sc
hutte
, Geo
rgia
Institu
te of
Tech
nolog
y, Atl
anta,
GA
Thur
sday
, 25
June
201
524
0-AT
IO-2
3Tra
nsfo
rmat
ional
Fligh
t - El
ectri
c Pro
pulsi
onMo
net B
allro
omCh
aired
by: S
. GIN
N, N
ASA
0900
hrs
Oral
Prese
ntatio
nHE
IST LE
APTe
ch In
strum
enta
tion
Desig
n, D
evelo
pmen
t, an
d Init
ial
Resu
ltsT.
Foste
r, Emp
irical
Syste
ms Ae
rospa
ce,
Inc.,
Pismo
Bea
ch, C
A
0930
hrs
Oral
Prese
ntatio
nLE
APTe
ch H
EIST P
ower
Arch
itectu
re
and T
estin
gS.
Clark
e, Y.
Lin, A
. Sam
uel, K
. Pa
patha
kis, N
ASA A
rmstr
ong F
light
Rese
arch C
enter
, Edw
ards,
CA
1000
hrs
AIAA-2
015-3
188
Comp
ariso
n of
CFD
and
Expe
rimen
tal R
esult
s of t
he
LEAP
Tech
Dist
ribut
ed El
ectri
c Pr
opuls
ion B
lown
Wing
A. St
oll, J
oby A
viatio
n, Sa
nta Cr
uz, C
A
1030
hrs
AIAA-2
015-3
189
A Co
ncep
tual
Appr
oach
to Fl
ight-
Traini
ng M
ission
and C
ost A
nalys
is of
an A
ll-Ele
ctric
Aircr
aft E
quipp
ed
with
Reg
ener
ative
Ener
gy D
evice
sM.
Olso
n, Ge
orgia
Institu
te of
Tech
nolog
y, Atl
anta,
GA
1100
hrs
AIAA-2
015-3
190
Optim
al Pr
opell
er P
itch
Sche
dulin
g an
d Pro
pelle
r--Ai
rfram
e Mat
ching
fo
r Con
cept
ual D
esign
R. Mc
Dona
ld, Ca
liforni
a Poly
techn
ic St
ate
Unive
rsity,
San
Luis
Obisp
o, CA
1130
hrs
AIAA-2
015-3
191
Mode
ling a
nd Te
st of
the E
fficie
ncy
of El
ectro
nic Sp
eed C
ontro
llers
for
Brus
hless
DC M
otor
sC.
Gree
n, R.
McDo
nald,
Califo
rnia
Polyt
echn
ic St
ate U
nivers
ity, S
an Lu
is Ob
ispo,
CA
103
Thur
sday
, 25
June
201
524
1-CF
D-26
Unstr
uctu
red H
igh-O
rder
Meth
ods I
IIGr
and B
allro
om A
Chair
ed by
: R. H
ARRIS
, CFD
Rese
arch C
orpora
tion a
nd B
. JOL
LY, U
S Air
Force
0900
hrs
AIAA-2
015-3
192
Deve
lopme
nt of
Verte
x-Ce
nter
ed,
High
-Ord
er Sc
heme
s and
Im
pleme
ntat
ion in
FUN3
DH.
Yang
, R. H
arris,
CFD
Rese
arch
Corpo
ration
, Hun
tsville
, AL
0930
hrs
AIAA-2
015-3
193
A co
mpac
t high
orde
r finit
e volu
me
meth
od fo
r hyp
erbo
lic co
nser
vatio
n law
s on
unstr
uctu
red g
rids
Q. W
ang,
Y. Re
n, Tsi
nghu
a Univ
ersity
, Be
ijing,
China
; W. L
i, Sun
Yat-S
en
Unive
rsity,
Gua
ngzh
ou, C
hina
1000
hrs
AIAA-2
015-3
194
Loca
lly-D
efine
d High
-Res
olutio
n Sc
heme
for S
hock
-Cap
turin
g Pr
oblem
s on U
nstru
cture
d Car
tesian
Gr
idsY.
Tama
ki, T.
Imam
ura, U
nivers
ity of
To
kyo,
Toky
o, Ja
pan
1030
hrs
AIAA-2
015-3
195
High
-Ord
er Co
mpre
ssible
Flow
Sim
ulatio
ns w
ith th
e Uns
tructu
red
Spec
tral D
iffer
ence
Meth
odF.
Morei
ra, C.
Brev
iglier
i, Tec
hnolo
gical
Institu
te of
Aeron
autic
s (ITA
), Sã
o Jo
sé do
s Cam
pos,
Braz
il; J.
Azev
edo,
Aeron
autic
s and
Spa
ce In
stitut
e (IAE
), Sã
o Jo
sé do
s Cam
pos,
Braz
il
1100
hrs
AIAA-2
015-3
196
A new
high
-orde
r uns
tructu
red
nume
rical
schem
e for
larg
e edd
y sim
ulatio
nZ.
Xu, U
nivers
ity of
Scien
ce an
d Tech
nolog
y, He
fei, C
hina;
Q. Zh
ao, C
hinese
Acad
emy o
f Sc
iences
, Beiji
ng, C
hina;
Q. Lin
, Univ
ersity
of
Scien
ce an
d Tech
nolog
y, He
fei, C
hina;
J. Xu
, Ch
inese
Acad
emy o
f Scie
nces,
Beijin
g, Ch
ina
Thur
sday
, 25
June
201
524
2-CF
D-27
Curre
nt Tr
ends
in CF
D Re
sear
ch II
(Inv
ited)
Gran
d Ball
room
BCh
aired
by: H
. HUY
NH, N
ASA G
lenn R
esea
rch Ce
nter a
nd Z.
WAN
G, U
nivers
ity of
Kans
as09
00 hr
sOr
al Pre
senta
tion
Theo
retic
al As
pects
of H
igh-O
rder
Flu
x Re
cons
tructi
on Sc
heme
s (In
vited
)P.
Vince
nt, Im
peria
l Coll
ege L
ondo
n, Lo
ndon
, Unit
ed Ki
ngdo
m
0930
hrs
AIAA-2
015-3
197
Well P
osed
Pro
blems
and B
ound
ary
Cond
itions
in Co
mput
ation
al Flu
id Dy
nami
cs (In
vited
)J.
Nords
trom,
Link
öping
Univ
ersity
, Lin
köpin
g, Sw
eden
1000
hrs
AIAA-2
015-3
198
Oppo
rtunit
ies fo
r effi
cient
high-o
rder
me
thods
based
on th
e sum
matio
n-by-
parts
prop
erty (
Invite
d)J.
Hicke
n, Re
nssela
er Po
lytech
nic In
stitute
, Tro
y, NY
; D. D
el Re
y Fern
ánde
z, D.
Zingg
, Un
iversit
y of T
oronto
, Toro
nto, C
anad
a
1030
hrs
Oral
Prese
ntatio
nRo
le of
Entro
py-R
esidu
al in
High
-Or
der N
umeri
cal M
ethod
s for
Gas
-Dy
nami
cs Ca
lculat
ions:
Shoc
k Dete
ctor
and A
dapta
tion I
ndica
tor (I
nvite
d)M.
Ihme
, Y. L
v, Sta
nford
Unive
rsity,
Stanfo
rd,
CA
1100
hrs
Oral
Prese
ntatio
nLa
rge E
ddy S
imula
tions
of
Turb
ulent
Flow
s Usin
g Di
scont
inuou
s High
Ord
er M
ethod
s (In
vited
)Z.
Wang
, Univ
ersity
of Ka
nsas
, Law
rence
, La
wren
ce, K
S
1130
hrs
AIAA-2
015-3
199
Multi-
dimen
siona
l Lim
iting S
trateg
y fo
r High
er-o
rder
CFD
Meth
ods -
Pr
ogre
ss an
d Issu
e (In
vited
)C.
Kim, S
eoul
Natio
nal U
nivers
ity, S
eoul,
So
uth Ko
rea; J
. Park
, Imp
erial
Colle
ge
Lond
on, L
ondo
n, Un
ited K
ingdo
m
Thur
sday
, 25
June
201
524
3-CF
D-28
Inco
mpre
ssible
and L
ow Sp
eed F
lows
Plum
Blos
som
ACh
aired
by: M
. YU,
Univ
ersity
of M
arylan
d, Ba
ltimore
Coun
ty an
d R. R
AJAG
OPAL
AN, I
owa S
tate U
nivers
ity09
00 hr
sAIA
A-201
5-320
0Hi
gh-O
rder
Stra
nd G
rid M
ethod
s fo
r Low
Mac
h an
d Inc
ompr
essib
le Flo
wsJ.
Thorn
e, A.
Katz,
Utah
Stat
e Univ
ersity
, Lo
gan,
UT
0930
hrs
AIAA-2
015-3
201
An Ex
plicit
Pre
ssure
-Bas
ed
Algo
rithm
for I
ncom
pres
sible
Flows
D. G
arrick
, R. R
ajago
palan
, Iow
a Stat
e Un
iversi
ty, Am
es, I
A
1000
hrs
AIAA-2
015-3
202
A Tu
rbule
nt Lo
w-Sp
eed
Prec
ondit
ioner
for U
nstea
dy Fl
ows
Abou
t Wind
Turb
ine A
irfoil
sR.
Djedd
i, K. E
kici, U
nivers
ity of
Te
nnes
see,
Knox
ville,
Knox
ville,
TN
1030
hrs
AIAA-2
015-3
203
Comp
ariso
n of
Pre
ssure
-Bas
ed
Rung
e-Ku
tta Sc
heme
s for
Uns
teady
In
comp
ressi
ble Fl
ows
M. Fi
schels
, R. R
ajago
palan
, Iow
a Stat
e Un
iversi
ty, Am
es, I
A
1100
hrs
AIAA-2
015-3
204
Apply
ing N
on-R
eflec
ting B
ound
ary
Cond
itions
in P
ressu
re-B
ased
So
lvers
V. Iva
nov,
B. M
akaro
v, AN
SYS,
Inc.,
Le
bano
n, NH
1130
hrs
AIAA-2
015-3
205
Gene
ralis
ed SI
MPLE
-Bas
ed P
ressu
re
Corre
ction
Meth
od fo
r Uns
tructu
red
Co-lo
cated
Grid
sV.
Przulj
, Rica
rdo S
oftwa
re, S
horeh
am by
Se
a, Un
ited K
ingdo
m
1200
hrs
AIAA-2
015-3
206
Robu
stness
to In
accu
rate
Initia
l Co
nditio
ns in
Low
Mach
Preco
nditio
ned
Dens
ity-B
ased
Meth
ods
C. Fa
lcão,
Unive
rsity o
f Rio
Grand
e do S
ul,
Porto
Aleg
re, Br
azil;
F. Med
eiros,
Milita
ry Ins
titute
of En
ginee
ring (
IME),
Rio d
e Jan
eiro,
Brazil;
L. Al
ves,
Flumi
nese
Fede
ral Un
iversit
y (U
FF),
Niteró
i, Braz
il
Thur
sday
, 25
June
201
524
4-CF
D-29
High
-Spe
ed an
d Rea
cting
Flow
sCo
ral
Chair
ed by
: G. C
ANDL
ER, U
nivers
ity of
Minn
esota
and B
. RAT
HAKR
ISHNA
N, G
E Glob
al Re
searc
h09
00 hr
sAIA
A-201
5-320
7LE
S of r
eacti
ng m
ixing
laye
rs:
influe
nce o
f infl
ow co
nditio
ns an
d he
at re
lease
A. Ka
rtha,
P. Su
bbare
ddy,
G. Ca
ndler
, Un
iversi
ty of
Minn
esota
, Minn
eapo
lis,
Minn
eapo
lis, M
N; P.
Dim
otakis
, Cali
fornia
Ins
titute
of Te
chno
logy,
Pasa
dena
, CA
0930
hrs
AIAA-2
015-3
208
A Prio
ri Ana
lysis o
f a Co
mpres
sible
Flame
let M
odel
using
RANS
Data
for a
Du
al-Mo
de Sc
ramj
et Co
mbus
torJ.
Quinla
n, T.
Drozd
a, NA
SA La
ngley
Resea
rch
Cente
r, Ham
pton,
VA; J
. McD
aniel,
Unive
rsity
of Vir
ginia,
Charl
ottesv
ille, C
harlo
ttesvi
lle,
VA; G
. Laca
ze, J
. Oefe
lein, S
andia
Nati
onal
Labo
ratori
es, Liv
ermore
, CA
1000
hrs
AIAA-2
015-3
209
Nume
rical
Inve
stiga
tions
of P
ulsed
Fu
el In
jectio
n int
o Sup
erso
nic
Cros
sflow
N. W
illiam
s, R.
Thom
pson
, T. M
oelle
r, Un
iversi
ty of
Tenn
esse
e, Tu
llaho
ma,
Tulla
homa
, TN
1030
hrs
AIAA-2
015-3
210
Ignit
ion Ch
arac
terist
ics in
Spat
ially
Zero
-, On
e- an
d Two
-Dim
ensio
nal
Lami
nar E
thyle
ne Fl
ames
M. Ev
ans,
P. Me
dwell
, Z. T
ian, U
nivers
ity
of Ad
elaide
, Ade
laide
, Aus
tralia
; A.
Frasso
ldati,
A. Cu
oci, A
. Stag
ni, Te
chnic
al Un
iversi
ty of
Milan
, Mila
n, Ita
ly
1100
hrs
AIAA-2
015-3
211
IDDE
S sim
ulatio
n of
supe
rsonic
co
mbus
tion
using
flam
elet
mode
ling
H. W
ang,
Y. Pia
o, J.
Niu, T
singh
ua
Unive
rsity,
Beij
ing, C
hina
1130
hrs
AIAA-2
015-3
212
Thre
e Dim
ensio
nal F
low A
nalys
is of
a C
avity
-Bas
ed Sc
ramj
et Co
mbus
tor
R. Ro
uzba
r, S. E
yi, M
iddle
East
Tech
nical
Unive
rsity,
Anka
ra, Tu
rkey
104
Thur
sday
, 25
June
201
524
5-CF
D-30
Inflo
w Tu
rbule
nce f
or W
all-B
ound
ed LE
S (In
vited
)Em
erald
Chair
ed by
: N. B
ISEK,
Air Fo
rce Re
seac
h Lab
orator
y and
L. TA
O, G
E Glob
al Re
searc
h09
00 hr
sAIA
A-201
5-321
3An
Ove
rview
of Tu
rbule
nt In
flow
Boun
dary
Cond
itions
for L
arge
Ed
dy Si
mulat
ions (
Invit
ed)
N. D
hama
nkar,
G. B
laisd
ell, P
urdue
Un
iversi
ty, W
est L
afaye
tte, I
N; A.
Lyrin
tzis,
Embry
-Ridd
le Ae
ronau
tical
Unive
rsity,
Da
ytona
Bea
ch, F
L
0930
hrs
AIAA-2
015-3
214
A Co
unter
-Flow
Force
Bas
ed M
ethod
to
Gen
erat
e Equ
ilibriu
m Tu
rbule
nt
Inflo
w Co
nditio
ns (I
nvite
d)D.
Gait
onde
, M. W
aindim
, M. A
dler, O
hio
State
Univ
ersity
, Colu
mbus
, OH
1000
hrs
AIAA-2
015-3
215
Gene
ratin
g Syn
theti
c In
homo
gene
ous T
urbu
lence
from
RA
NS St
atist
ics (I
nvite
d)P.
Batte
n, U.
Gold
berg,
O. P
eroom
ian, S
. Ch
akrav
arthy
, Meta
comp
Tech
nolog
ies,
Inc.,
Agou
ra Hil
ls, CA
1030
hrs
Q&A P
anel
Discu
ssion
Thur
sday
, 25
June
201
524
6-FD
-27
Turb
ulenc
e Ana
lysis
Gove
nors
Lectu
re H
allCh
aired
by: Z
. ZHE
NG, T
he U
nivers
ity of
Kans
as an
d S. S
ILTON
, US
Army R
esea
rch La
borat
ory09
00 hr
sAIA
A-201
5-321
6Sin
gle an
d Mult
iple-
Point
Ana
lysis
of Ve
locity
Fluc
tuat
ions i
n a
Deto
natio
n-Tu
rbule
nce I
nter
actio
nS.
Hus
sein,
F. Lu
, Univ
ersity
of Te
xas,
Arling
ton, A
rlingto
n, TX
0930
hrs
AIAA-2
015-3
217
Nonli
near
Time
Serie
s Ana
lysis
of
Veloc
ity ov
er N
ACA
2412
Thre
e-Di
mens
ional
Wing
Usin
g Lar
ge
Eddy
Simu
lation
Dat
aP.
Chak
rabort
y, A.
Roy,
Indian
Insti
tute o
f Te
chno
logy K
harag
pur, K
olkata
, Ind
ia
1000
hrs
AIAA-2
015-3
218
Ther
mal n
on-e
quilib
rium
effe
cts in
tu
rbule
nt co
mpre
ssible
shea
r flow
sA.
Nevil
le, I.
Nom
pelis,
P. S
ubba
reddy
, G.
Cand
ler, U
nivers
ity of
Minn
esota
, Mi
nnea
polis,
Minn
eapo
lis, M
N
Thur
sday
, 25
June
201
524
7-FD
-28
0900
- 12
30 h
rsTra
nsitio
n Op
en Fo
rum
Sapp
hire
Chair
ed by
: H. R
EED,
Texa
s A&M
Univ
ersity
Thur
sday
, 25
June
201
524
8-FD
-29
Flow
Cont
rol -
Aer
odyn
amics
Sena
tors
Lectu
re H
allCh
aired
by: H
. DON
G, U
nivers
ity of
Virg
inia a
nd E.
WHA
LEN,
Boe
ing En
ginee
ring O
perat
ions &
Tech
nolog
y09
00 hr
sAIA
A-201
5-321
9Th
ree-
dimen
siona
l Con
trol v
ia Ma
ss In
jectio
n fo
r Sup
pres
sion
of Ca
vity
Oscil
lation
sY.
Zhan
g, N.
Arora
, Y. S
un, L
. Catt
afesta
, K.
Taira
, Flor
ida S
tate U
nivers
ity,
Talla
hasse
e, FL
; L. U
keile
y, Un
iversi
ty of
Florid
a, Ga
inesv
ille, G
aines
ville,
FL
0930
hrs
AIAA-2
015-3
220
Prop
ulsive
Per
form
ance
and V
ortex
In
terac
tions
of M
ultipl
e Tan
dem
Foils
Pitc
hing I
n Lin
eC.
Yuan
, G. L
iu, Y.
Ren,
H. D
ong,
Unive
rsity
of Vir
ginia,
Charl
ottes
ville,
Ch
arlott
esvil
le, VA
1000
hrs
AIAA-2
015-3
221
On th
e Effe
ct of
Rigi
d Swe
pt
Surfa
ce W
aves
on Tu
rbule
nt D
rag
M. D
eniso
n, Na
tiona
l Insti
tute o
f Ae
rospa
ce, H
ampto
n, VA
; S. W
ilkins
on,
P. Ba
lakum
ar, N
ASA L
angle
y Res
earch
Ce
nter, H
ampto
n, VA
1030
hrs
AIAA-2
015-3
222
Cont
rol o
f Toll
mien
-Sch
licht
ing
Wave
s Usin
g Piez
oelec
trica
lly
Drive
n Os
cillat
ing Su
rface
H. D
ell’O
rso, B
. Tun
a, M.
Amita
y, Re
nsse
laer P
olytec
hnic
Institu
te, Tr
oy, N
Y
105
Thur
sday
, 25
June
201
524
9-FT
-1Fli
ght T
estin
gOb
elisk
BCh
aired
by: K
. GAR
MAN,
Fede
ral Av
iation
Admi
nistra
tion a
nd J.
BRA
NDON
, NAS
A-Lan
gley R
esea
rch Ce
nter
0900
hrs
AIAA-2
015-3
223
A Fr
amew
ork
for A
pplyi
ng th
e OO
DA Lo
op to
Miss
ion Co
ntro
l Ro
om Ex
ecut
ionJ.
Newc
amp,
U.S.
Air F
orce A
cade
my,
Color
ado S
pring
s, CO
0930
hrs
AIAA-2
015-3
224
Curre
nt H
yper
sonic
and S
pace
Ve
hicle
Fligh
t Tes
t Ins
trume
ntat
ion
Chall
enge
sJ.
Sprav
ka, T
. Jorr
is, 4
12th
Test
Wing
, Ed
wards
AFB,
CA
1000
hrs
AIAA-2
015-3
225
Stall/
Spin
Fligh
t Tes
t Tec
hniqu
es
with
COTS
Mod
el Ai
rcraf
t and
Fligh
t Da
ta Sy
stems
R. Bu
nge,
F. Mu
nera
Savin
o, I.
Kroo,
Stan
ford U
nivers
ity, S
tanfor
d, CA
1030
hrs
AIAA-2
015-3
226
Grou
nd M
inimu
m Co
ntro
l Spe
ed
(VMC
G) Te
sting
of Tr
ansp
ort
Aircr
aft
P. Bo
lds-M
ooreh
ead,
V. Ch
aney
, The
Bo
eing C
ompa
ny, S
eattle
, WA;
T. Lu
tz, S
. Va
ux, A
irbus
, Tou
louse
, Fran
ce
1100
hrs
AIAA-2
015-3
227
Later
al-Di
recti
onal
Aero
dyna
mic
Mode
l Ide
ntifi
catio
n of
a Sin
gle-
Engin
e Pro
pelle
r Airc
raft
Using
Pa
rtial
Orth
ogon
al Le
ast S
quar
esJ.
Zane
tte, B
razilia
n Air F
orce,
São
José
dos C
ampo
s, Br
azil;
F. Alm
eida,
Tech
nolog
ical In
stitut
e of A
erona
utics
(ITA)
, São
José
dos C
ampo
s, Br
azil
Thur
sday
, 25
June
201
525
0-LTA
-1Lig
hter
-than
-Air
Syste
ms &
Tech
nolog
ies I
Steub
enCh
aired
by: R
. VAN
TREU
REN
0900
hrs
AIAA-2
015-3
228
Desig
n an
d Con
trol o
f a M
ulti-
vecto
red T
hrus
t Airs
hipL.
Chen
, Y. W
en, H
. Zho
u, X.
Wan
g, P.
Zhou
, D. D
uan,
Shan
ghai
Jiao T
ong
Unive
rsity,
Sha
ngha
i, Chin
a
0930
hrs
AIAA-2
015-3
229
Nume
rical
Feas
ibility
Ana
lysis
of
the E
xtra
-ligh
t Weig
ht St
ructu
re
Tens
airity
on La
rge A
irship
sA.
Suño
l, T. Y
ang,
D. Vu
cinic,
Vrije
Un
iversi
teit B
russe
l, Brus
sels,
Belg
ium
1000
hrs
AIAA-2
015-3
230
Comp
utat
ional
Mode
lling o
f Ae
rody
nami
c Cha
racte
ristic
s of
Airsh
ips in
Arb
itrar
y Mot
ionA.
Kano
ria, K
. Pan
chal,
R. D
ongre
, M.
Damo
daran
, Ind
ian In
stitut
e of T
echn
ology
Ga
ndhin
agar,
Ahme
daba
d, Ind
ia
1030
hrs
AIAA-2
015-3
231
Distu
rban
ce R
ejecti
on B
ased
Pa
th Fo
llowi
ng Co
ntro
l for
A
Strat
osph
eric
Airsh
ip wi
th A
ctuat
or
Satu
ratio
nK.
Yan,
Z. Zh
eng,
M. Zh
u, Z.
Wu,
Beiha
ng
Unive
rsity,
Beij
ing, C
hina
1100
hrs
AIAA-2
015-3
232
A Lo
ng En
dura
nce,
High
ly Ma
neuv
erab
le, Co
llabo
rativ
e, Un
mann
ed A
irbor
ne Sy
stem
W. Ki
ng, D
. Lan
drum,
J. Al
corn,
A.
Jarze
mbsk
i, Univ
ersity
of Al
abam
a, Hu
ntsvil
le, H
untsv
ille, A
L
Thur
sday
, 25
June
201
525
1-MA
O-8
Meta
mode
ling I
IMa
nche
ster
Chair
ed by
: B. R
OTH,
Wall
a Wall
a Univ
and J
. HICK
EN, R
ensse
laer P
olytec
hnic
Institu
te09
00 hr
sAIA
A-201
5-323
3Ad
aptiv
e Swi
tching
of Va
riable
-Fid
elity
Mod
els in
Pop
ulatio
n-ba
sed
Optim
izatio
n Al
gorit
hms
A. Me
hman
i, Syra
cuse
Univ
ersity
, Sy
racus
e, NY
; S. C
howd
hury,
A. M
essa
c, Mi
ssissi
ppi S
tate U
nivers
ity, M
ississ
ippi
State
, MS
0930
hrs
AIAA-2
015-3
234
Larg
e-sca
le CF
D Op
timiza
tion
base
d on
the F
FD P
aram
etriza
tion
using
the M
ultipo
int A
ppro
ximat
ion
Meth
od in
an H
PC En
viron
ment
Y. Ko
rolev
, V. T
oropo
v, Qu
een M
ary
Unive
rsity
of Lo
ndon
, Lon
don,
Unite
d Kin
gdom
; S. S
hahp
ar, Ro
lls-Ro
yce G
roup
plc, D
erby,
Unite
d King
dom
1000
hrs
AIAA-2
015-3
235
Adap
tive V
ariab
le-Fid
elity
Ae
rody
nami
c Ana
lysis
and D
esign
fo
r Tail
less A
ircra
ft un
der M
odel-
Form
Unc
erta
inty
Y. Jo
, J. P
ark, C
. Och
eltree
, J. C
hoi, S
. Ch
oi, P.
Raj, V
irgini
a Poly
techn
ic Ins
titute
and S
tate U
nivers
ity, B
lacks
burg,
VA; e
t al.
1030
hrs
AIAA-2
015-3
236
Study
of H
ybrid
Rad
ial B
asis
Func
tion
for D
esign
Opt
imiza
tion
Prob
lems
R. Sh
i, L. L
iu, T.
Long
, J. L
iu, B
eijing
Ins
titute
of Te
chno
logy,
Beijin
g, Ch
ina
Thur
sday
, 25
June
201
525
2-MA
O-9
Shap
e and
Topo
logy I
Madr
idCh
aired
by: J
. MAR
TINS,
Univ
ersity
of M
ichiga
n and
R. KO
LONA
Y, Air
Force
Rese
arch L
abora
tory/
RQVC
/WPA
FB09
00 hr
sAIA
A-201
5-323
7No
nintru
sive C
ontin
uum
Sens
itivity
An
alysis
for A
erod
ynam
ic Sh
ape
Optim
izatio
nM.
Kulka
rni, R
. Can
field,
M. P
atil, V
irgini
a Po
lytec
hnic
Institu
te an
d Stat
e Univ
ersity
, Bla
cksb
urg, V
A
0930
hrs
AIAA-2
015-3
238
Thre
e-Di
mens
ional
Piece
wise
-Co
ntinu
ous C
lass-S
hape
Tra
nsfo
rmat
ion of
Wing
sE.
Olso
n, NA
SA La
ngley
Rese
arch C
enter
, Ha
mpton
, VA
1000
hrs
AIAA-2
015-3
239
Multi-
objec
tive s
hape
optim
izatio
n of
aircr
aft c
abin
vent
ilatio
n co
mpon
ents
using
adjoi
nt CF
DT.
Köthe
, S. H
erzog
, C. W
agne
r, Germ
an
Aeros
pace
Cente
r (DL
R), G
ötting
en,
Germ
any
1030
hrs
AIAA-2
015-3
240
Deve
lopme
nt of
a Con
sisten
t Di
screte
Adjoi
nt So
lver in
an Ev
olving
Ae
rody
nami
c Desi
gn Fr
amew
ork
T. Alb
ring,
M. Sa
geba
um, N
. Gau
ger, T
echnic
al Un
iversit
y of K
aisers
lauter
n, Ka
isersla
utern,
Ge
rman
y
1100
hrs
AIAA-2
015-3
241
The R
esea
rch on
Geo
metry
Mo
delin
g Meth
od B
ased
on Th
ree-
dimen
siona
l CST
Par
amete
rizat
ion
Tech
nolog
yH.
Su,
L. Gu
, C. G
ong,
North
weste
rn Po
lytec
hnica
l Univ
ersity
, Xi’a
n, Ch
ina
1130
hrs
AIAA-2
015-3
242
Conc
urre
nt Su
bspa
ce O
ptim
izatio
n De
sign
of H
yper
sonic
Cruis
e Veh
icle
C. Jin
g, S.
Yuan
-pei, C
hina A
erody
nami
cs Re
searc
h and
Dev
elopm
ent C
enter
, Mi
anya
ng, C
hina
106
Thur
sday
, 25
June
201
525
3-MS
T-11
Aircr
aft S
ystem
s Des
ign, V
erifi
catio
n an
d Vali
datio
nTra
verti
neCh
aired
by: G
. CHA
TTER
JI, N
ASA A
mes R
esea
rch Ce
nter
0900
hrs
AIAA-2
015-3
243
ADDA
M: A
n Ob
ject O
rient
ed D
ata
Mode
l for
an A
ircra
ft De
sign
Envir
onme
nt in
MAT
LAB
S. H
erbst,
M. H
ornun
g, Te
chnic
al Un
iversi
ty of
Munic
h, Mu
nich,
Germ
any
1000
hrs
AIAA-2
015-3
245
Dyna
mic m
odel
upda
ting o
f a s
imula
tion c
asing
based
on
expe
rimen
tal m
odal
para
meter
sB.
Jie, Q
. Mei,
C. Zh
ang,
Aviat
ion In
dustr
y Co
rporat
ion of
China
(AVIC
), Zh
uzho
u, Ch
ina
Thur
sday
, 25
June
201
525
4-NW
-8
0900
- 09
30 h
rsNe
twor
king C
offe
e Bre
akCh
antill
y Ball
room
East
Thur
sday
, 25
June
201
525
5-PD
L-12
Aero
-Opt
ics P
lasma
Diag
nosti
csMi
roCh
aired
by: R
. MILE
S, Pr
inceto
n Univ
ersity
and M
. REN
NIE,
Unive
rsity
of No
tre D
ame
0900
hrs
AIAA-2
015-3
246
Aero
-Opti
cal M
easu
remen
ts of
High
-Ma
ch Su
perso
nic Bo
unda
ry La
yers
S. Go
rdeye
v, M.
Renn
ie, Un
iversit
y of N
otre
Dame
, Notr
e Dam
e, IN;
A. Ca
in, In
nova
tive
Techn
ology
Applic
ation
s Com
pany,
LLC,
Chest
erfield
, MO;
T. Ha
yden
, U.S.
Air F
orce
Acad
emy,
Color
ado S
pring
s, CO
0930
hrs
AIAA-2
015-3
247
Non-
intru
sive V
elocit
y and
Den
sity
Meas
urem
ents
in Su
bson
ic Tu
rbule
nt B
ound
ary L
ayer
J. So
ntag,
S. G
ordey
ev, U
nivers
ity of
Notr
e Da
me, N
otre D
ame,
IN
1000
hrs
AIAA-2
015-3
248
Nume
rical
Inve
stiga
tion
of
Aero
-Opt
ical D
istor
tions
over
a He
misp
here
-on-
Cylin
der T
urre
t wi
th G
aps
E. Ma
thews
, K. W
ang,
M. W
ang,
E. Ju
mper,
Univ
ersity
of N
otre D
ame,
Notre
Da
me, I
N
1030
hrs
AIAA-2
015-3
249
Char
acter
izatio
n of
Flow
Cont
rol
Actu
ator
s Bas
ed on
Spar
k Di
schar
ge P
lasma
s Usin
g Par
ticle
Imag
e Velo
cimetr
yB.
Sing
h, M.
Belm
ouss,
S. B
ane,
Purdu
e Un
iversi
ty, W
est L
afaye
tte, I
N
1100
hrs
AIAA-2
015-3
250
Inve
stiga
tion
of sh
ock
/ tu
rbule
nt
boun
dary
inter
actio
n un
stead
iness
with
vario
us ob
struc
tions
for a
ero-
optic
sM.
Whit
e, Oh
io Ae
rospa
ce In
stitut
e, Da
yton,
OH; M
. Visb
al, Ai
r Forc
e Res
earch
La
borat
ory, W
right-
Patte
rson A
FB, O
H
Thur
sday
, 25
June
201
525
6-TP
-12
Deta
iled M
olecu
lar P
roce
ss Mo
delin
gRo
setta
Chair
ed by
: R. W
AGNI
LD, S
andia
Nati
onal
Labo
ratori
es an
d T. S
CHWA
RTZE
NTRU
BER,
Unive
rsity
of Mi
nnes
ota09
00 hr
sAIA
A-201
5-325
1Vib
ratio
nal R
elaxa
tion
and
Disso
ciatio
n of
Oxy
gen
in Mo
lecule
-At
om Co
llision
sD.
Andri
enko
, I. B
oyd,
Unive
rsity
of Mi
chiga
n, An
n Arbo
r, Ann
Arbo
r, MI
0930
hrs
AIAA-2
015-3
252
Maste
r Equ
ation
Stud
y of
Vibra
tiona
l and
Rot
ation
al Re
laxat
ion of
Oxy
gen
D. An
drien
ko, I
. Boy
d, Un
iversi
ty of
Mich
igan,
Ann A
rbor, A
nn Ar
bor, M
I
1000
hrs
AIAA-2
015-3
253
Char
acter
izatio
n of
Vibr
ation
al an
d Ro
tatio
nal E
nerg
y Tra
nsfe
r in
N 2-N2
Disso
ciativ
e Coll
ision
s Usin
g the
Qu
asicl
assic
al Tra
jecto
ry M
ethod
J. Be
nder,
P. Va
lentin
i, I. N
ompe
lis, T.
Sc
hwart
zentr
uber,
G. C
andle
r, Univ
ersity
of
Minn
esota
, Minn
eapo
lis, M
innea
polis,
MN
1030
hrs
AIAA-2
015-3
254
Dire
ct mo
lecula
r sim
ulatio
n of
high
-temp
erat
ure n
itrog
en
disso
ciatio
n du
e to b
oth
N-N2
and
N2-N
2 co
llision
sP.
Valen
tini, T
. Sch
wartz
entru
ber,
J. Be
nder,
G. C
andle
r, Univ
ersity
of
Minn
esota
, Minn
eapo
lis, M
innea
polis,
MN
Thur
sday
, 25
June
201
525
7-F3
60-8
09
30 -
1200
hrs
The I
mpac
t of P
artic
le Im
age V
elocim
etry o
n Ae
rosp
ace T
echn
ology
Gran
d Ball
room
E
Mode
rator:
Stev
en B
eresh
, Dist
inguis
hed M
embe
r of t
he Te
chnic
al St
aff, S
andia
Nati
onal
Labo
ratori
es
P
aneli
sts:
Rona
ld J.
Adria
nRe
gent’
s Prof
essor
and I
ra A.
Fulto
n Prof
essor
of Me
chanic
al an
d Aero
space
En
ginee
ring
Arizo
na S
tate U
nivers
ity
Susa
n Go
rton
Projec
t Man
ager,
Revo
lution
ary Ve
rtical
Lift Te
chnolo
gy Pr
oject
NASA
Lang
ley Re
searc
h Cen
ter
Fulvi
o Sca
rano
Full P
rofes
sor a
nd Ch
air of
Aerod
ynam
icsDe
lft Un
iversi
ty of
Tech
nolog
y
Migu
el Vis
bal
Princi
pal R
esearc
h Aero
space
Engin
eer a
nd Te
am Le
ader
of Mu
ltidisc
iplina
ry Co
mputa
tiona
l Aero
dyna
mics,
Aeros
pace
Syste
ms Di
rector
ateAir
Force
Rese
arch L
abora
tory
107
Thur
sday
, 25
June
201
525
8-LN
CH-3
12
30 -
1400
hrs
Awar
ds Lu
nche
on: C
elebr
ating
Ach
ievem
ents
in Ai
rcraf
t and
Atm
osph
eric
Syste
msCh
antill
y Ball
room
Wes
t
A tick
et is
requir
ed an
d inc
luded
in th
e con
feren
ce re
gistra
tion f
ee w
here
indica
ted.
Thur
sday
, 25
June
201
525
9-AA
-37
Land
ing G
ear N
oise
Edelw
eiss
Chair
ed by
: T. S
PALT,
NAS
A Lan
gley R
esea
rch Ce
nter
1400
hrs
AIAA-2
015-3
255
Aero
acou
stic S
imula
tions
of a
Nose
La
nding
Gea
r usin
g FUN
3D on
Po
intwi
se U
nstru
cture
d Grid
sV.
Vatsa
, M. K
horra
mi, N
ASA L
angle
y Re
searc
h Cen
ter, H
ampto
n, VA
; J. R
hoad
s, Po
intwi
se, I
nc.,
Fort
Worth
, TX;
D.
Lock
ard, N
ASA L
angle
y Res
earch
Cente
r, Ha
mpton
, VA
1430
hrs
AIAA-2
015-3
256
Nose
land
ing ge
ar fl
ow an
d nois
e pr
edict
ions o
n un
struc
ture
d grid
us
ing a
cell-
cent
ered
Nav
ier-S
toke
s co
deF.
De La
Puen
te, L.
San
ders,
F. Vu
illot,
E. Ma
noha
, ONE
RA, C
hâtill
on, F
rance
1500
hrs
AIAA-2
015-3
257
The E
ffect
of Fl
ow Ci
rculat
ion on
th
e Sca
tterin
g of L
andin
g Gea
r No
iseT.
Heffe
rnon,
D. An
gland
, X. Z
hang
, M.
Smi
th, U
nivers
ity of
Sou
thamp
ton,
South
ampto
n, Un
ited K
ingdo
m
1530
hrs
AIAA-2
015-3
258
The E
ffect
of St
rut G
eome
try on
the
Inter
-Whe
el Flo
w fo
r a Tw
o-Wh
eel
Land
ing G
ear
P. Mc
Carth
y, A.
Ekme
kci, U
nivers
ity of
To
ronto,
Toron
to, Ca
nada
1600
hrs
AIAA-2
015-3
259
Desig
n of q
uieter
land
ing ge
ars
throu
gh la
ttice-B
oltzm
ann C
FD
simula
tions
T. Ro
ugier,
Safra
n Grou
p, Vé
lizy-Vi
llacou
blay,
France
; Q. B
ouvy,
Safra
n Grou
p, Glo
uceste
r, Un
ited K
ingdo
m; D.
Casal
ino, J
. App
elbau
m,
Exa G
mbH,
Stuttg
art, G
erman
y; C.
Kleinc
laus,
Exa G
mbH,
Munic
h, Ge
rman
y
Thur
sday
, 25
June
201
526
0-AA
-38
Fluid-
Struc
ture
Inter
actio
nFle
ur-d
e-lis
ACh
aired
by: J
. ALO
NSO-
MIRA
LLES,
UTC
Aeros
pace
Sys
tems
1400
hrs
AIAA-2
015-3
260
A fa
st nu
meric
al fra
mewo
rk
for a
cous
tic sc
atter
ing by
3D
poro
elasti
c plat
esW.
Wolf
, Univ
ersity
of Ca
mpina
s, Ca
mpina
s, Br
azil;
A. Ca
valie
ri, Te
chno
logica
l Insti
tute o
f Aero
nauti
cs (IT
A), S
ão Jo
sé do
s Cam
pos,
Braz
il
1430
hrs
AIAA-2
015-3
261
Noise
Pro
duce
d by F
abric
and W
ire
Mesh
Cove
red P
anels
in Lo
w-Sp
eed
Anec
hoic
Wind
Tunn
elsW.
Alex
ande
r, W. D
even
port,
Virg
inia
Polyt
echn
ic Ins
titute
and S
tate U
nivers
ity,
Black
sburg
, VA
1500
hrs
AIAA-2
015-3
262
Acou
stic s
catte
ring b
y finit
e co
mpos
ite pl
ates
A. Ca
valie
ri, M.
Don
adon
, Tec
hnolo
gical
Institu
te of
Aeron
autic
s (ITA
), Sã
o Jos
é do
s Cam
pos,
Braz
il; W.
Wolf
, Univ
ersity
of
Camp
inas,
Camp
inas,
Braz
il
1530
hrs
AIAA-2
015-3
263
Expe
rimen
tal I
nves
tigat
ion of
Flow
-In
duce
d Pan
el Vib
ratio
ns at
Cruis
e Ma
ch N
umbe
rT.
Berke
feld,
C. Sp
ehr, K
. Ehre
nfried
, S.
Haxte
r, Germ
an Ae
rospa
ce Ce
nter (
DLR)
, Gö
ttinge
n, Ge
rman
y; S.
Kroe
ber, D
aimler
AG
, Stut
tgart,
Germ
any
1600
hrs
AIAA-2
015-3
264
Rod-
Airfo
il Int
erac
tion
Noise
Re
ducti
on U
sing L
eadin
g Edg
e Se
rratio
nsW.
Chen
, W. Q
iao, L
. Wan
g, F.
Tong
, No
rthwe
stern
Polyt
echn
ical U
nivers
ity,
Xi’an
, Chin
a; X.
Wan
g, St
ate Ke
y La
borat
ory of
Aerod
ynam
ics, M
ianya
ng,
China
1630
hrs
AIAA-2
015-3
265
Comp
ariso
n of
Ana
lytica
l, Nu
meric
al, an
d Exp
erim
enta
l Re
sults
for U
nstea
dy A
erof
oil
Inter
actio
n No
iseL.
Ayton
, Univ
ersity
of Ca
mbrid
ge,
Camb
ridge
, Unit
ed Ki
ngdo
m; J.
Gill,
Un
iversi
ty of
South
ampto
n, So
utham
pton,
Unite
d King
dom;
N. P
eake
, Univ
ersity
of
Camb
ridge
, Cam
bridg
e, Un
ited K
ingdo
m
Thur
sday
, 25
June
201
526
1-AA
-39
Fluid
Acou
stic P
heno
mena
Fleur
-de-
lis B
Chair
ed by
: K. A
HUJA
, Geo
rgia I
nstitu
te of
Tech
nolog
y14
00 hr
sAIA
A-201
5-326
6No
n-lin
ear S
ystem
Iden
tifica
tion
Tech
nique
s for
Dete
rmina
tion
of th
e Aco
ustic
Pro
perti
es of
Pe
rfora
tesH.
Bod
en, R
oyal
Institu
te of
Tech
nolog
y (K
TH),
Stoc
kholm
, Swe
den
1430
hrs
AIAA-2
015-3
267
Vorte
x Sc
atter
ing Ef
fects
on
Acou
stic W
ave P
ropa
gatio
nG.
Ke, W
. Li, Z
. Zhe
ng, U
nivers
ity of
Ka
nsas
, Law
rence
, Law
rence
, KS
1500
hrs
AIAA-2
015-3
268
Nume
rical
Inve
stiga
tion
of th
e Re
fracti
on Ef
fects
by Je
t Flow
s in
Anec
hoic
Wind
Tunn
els, w
ith
Appli
catio
n to
NAS
A/La
RC Q
uiet
Flow
Facil
ityS.
Redo
nnet,
J. B
ulte,
ONER
A, Ch
âtillo
n, Fra
nce
1530
hrs
AIAA-2
015-3
269
On th
e mec
hanis
ms of
nois
e re
ducti
on in
aero
foil-
turb
ulenc
e int
erac
tion
by u
sing w
avy l
eadin
g ed
ges
S. H
aeri,
J. Kim
, P. J
osep
h, Un
iversi
ty of
South
ampto
n, So
utham
pton,
Unite
d Kin
gdom
1600
hrs
AIAA-2
015-3
270
Noise
Radia
tion f
rom
a Cyli
ndric
al Em
bossm
ent Im
merse
d in T
urbu
lent
Boun
dary
Laye
r Flow
B. Bry
an, S
. Gleg
g, Flo
rida A
tlanti
c Univ
ersity,
Bo
ca Ra
ton, F
L; M.
Awast
hi, W
. Alex
ande
r, W.
Deve
nport
, Virg
inia Po
lytech
nic In
stitute
and
State
Unive
rsity,
Blacks
burg,
VA
108
Thur
sday
, 25
June
201
526
2-AA
-40
Adva
nced
Testi
ng Te
chniq
ues
Inve
rnes
sCh
aired
by: J
. UND
ERBR
INK
1400
hrs
AIAA-2
015-3
271
Optim
izatio
n of
Micr
opho
ne
Loca
tions
for A
cous
tic Li
ner
Impe
danc
e Edu
ction
M. Jo
nes,
W. W
atson
, NAS
A Lan
gley
Rese
arch C
enter
, Ham
pton,
VA; J
. Ju
ne, U
nivers
ity of
Flori
da, G
aines
ville,
Ga
inesv
ille, F
L
1430
hrs
AIAA-2
015-3
272
Adva
nced
Bac
kgro
und S
ubtra
ction
Ap
plied
to A
eroa
cous
tic W
ind
Tunn
el Te
sting
C. Ba
hr, N
ASA L
angle
y Res
earch
Cente
r, Ha
mpton
, VA;
W. H
orne,
NASA
Ames
Re
searc
h Cen
ter, M
offett
Field
, CA
1500
hrs
AIAA-2
015-3
273
Redu
cing t
he Ef
fect o
f Tra
nsdu
cer
Moun
t Indu
ced N
oise o
n Aero
acou
stic
Wind
Tunn
el Tes
ting D
ata w
ith a
New
Trans
ducer
Mou
nt De
sign
A. He
rron,
D. Re
ed, D
. Nan
ce, N
ASA M
arsha
ll Sp
ace Fl
ight C
enter
, Hun
tsville
, AL
1530
hrs
AIAA-2
015-3
274
Beam
form
ing-b
ased
nois
e lev
el de
reve
rber
ation
solut
ion fo
r S1M
A so
nic w
ind-tu
nnel
: metr
ology
, me
thod
ology
and v
alida
tion
F. Me
ry, O
NERA
, Mod
ane,
Franc
e; R.
Davy
, V. F
leury,
J. B
ulte,
M. Re
y, ON
ERA,
Châti
llon,
Franc
e
1600
hrs
AIAA-2
015-3
275
Impe
danc
e edu
ction
of pe
rfora
ted
plates
at lo
w Sto
uhal
numb
ers an
d hig
h bias
flow
Mac
h num
ber
V. Po
pie, E
. Piot
, ONE
RA, T
oulou
se, Fr
ance;
S.
Torde
ux, F
rench
Natio
nal In
stitute
for R
esearc
h in
Comp
uter S
cience
and C
ontro
l (INR
IA), P
au,
France
; F. Si
mon,
ONER
A, Tou
louse,
Fran
ce
1630
hrs
AIAA-2
015-3
276
Effect
s of H
ologr
am D
istan
ce an
d Re
gular
izatio
n Tech
nique
s on V
ariou
s Me
thods
of N
earfi
eld Ac
ousti
c Ho
logra
phy A
pplie
d to B
uildin
g Le
akag
e Dete
ction
/Qua
ntific
ation
K. Ch
elliah
, G. R
aman
, R. M
uehle
isen,
Illinois
Ins
titute
of Tec
hnolo
gy, Ch
icago
, IL
Thur
sday
, 25
June
201
526
3-AA
-41
CAA
Nume
rical
Tech
nique
s IV
Laliq
ueCh
aired
by: P
. MOR
RIS, P
enns
ylvan
ia St
ate U
nivers
ity14
00 hr
sAIA
A-201
5-327
7Pe
rform
ance
of th
e DGM
for t
he
Linea
rized
Euler
Equa
tions
With
No
n-Un
iform
Mea
n-Flo
wM.
Willi
amsch
en, G
. Gab
ard, U
nivers
ity
of So
utham
pton,
South
ampto
n, Un
ited
Kingd
om
1430
hrs
AIAA-2
015-3
278
Towa
rds C
AA B
ased
Aco
ustic
Wind
Tu
nnel
Corre
ction
s for
Rea
listic
Sh
ear L
ayer
sJ.
Jiao,
J. De
lfs, J
. Dier
ke, G
erman
Ae
rospa
ce Ce
nter (
DLR)
, Brau
nsch
weig,
Ge
rman
y
1500
hrs
AIAA-2
015-3
279
High
-Ord
er H
ybrid
Cell-
Cent
ered
Me
thod
for C
ompu
tatio
nal
Aero
acou
stics
M. W
ang,
R. Fa
ttah,
D. An
gland
, X.
Zhan
g, Un
iversi
ty of
South
ampto
n, So
utham
pton,
Unite
d King
dom
1530
hrs
AIAA-2
015-3
280
A Sp
ectra
l-BEM
Form
ulatio
n fo
r Co
mpac
t Sou
rces A
eroa
cous
tics
G. B
ernard
ini, R
oma T
re Un
iversi
ty, Ro
me,
Italy;
C. Te
sta, I
talian
Insti
tute f
or Na
val
Hydro
dyna
mic R
esea
rch an
d Ship
Mod
el Ba
sin, R
ome,
Italy;
M. G
enna
retti,
Roma
Tre
Univ
ersity
, Rom
e, Ita
ly
1600
hrs
AIAA-2
015-3
281
A Sta
bilise
d High
-Ord
er Fi
nite
Eleme
nt M
odel
for t
he Li
near
ised
Euler
Equa
tions
K. Ha
mich
e, H.
Béri
ot, S
iemen
s, Le
uven
, Be
lgium
; G. G
abard
, Univ
ersity
of
South
ampto
n, So
utham
pton,
Unite
d Kin
gdom
Thur
sday
, 25
June
201
526
4-AA
-42
Fan
Broa
dban
d Nois
e Pre
dictio
nOb
elisk
ACh
aired
by: E
. ENV
IA, N
ASA G
lenn R
esea
rch Ce
nter
1400
hrs
AIAA-2
015-3
282
Harm
onic
and B
road
band
Se
para
tion
of N
oise f
rom
a Sma
ll Du
cted F
anA.
Truon
g, D.
Papa
mosch
ou, U
nivers
ity of
Ca
liforni
a, Irv
ine, I
rvine
, CA
1430
hrs
AIAA-2
015-3
283
Furth
er In
vesti
gatio
ns In
to a
Low-
Orde
r Mod
el of
Fan
Broa
dban
d No
iseS.
Grac
e, Bo
ston U
nivers
ity, B
oston
, MA
1500
hrs
Pane
lFa
n Bro
adba
nd N
oise P
redict
ion Pa
nel
E. En
via, N
ASA G
lenn R
esearc
h Cen
ter, C
levela
nd, O
H; J.
Coup
land,
Unive
rsity o
f Sou
thamp
ton, S
outha
mpton
, Unit
ed Ki
ngdo
m
Thur
sday
, 25
June
201
526
5-AC
D-7
Aircr
aft S
ubsy
stems
, Int
egra
tion,
and A
rchite
cture
sWy
ethCh
aired
by: P
. RAJ
, Virg
inia P
olytec
hnic
Institu
te an
d Stat
e Univ
ersity
and E
. DIG
IROLA
MO, L
ockh
eed M
artin
Aeron
autic
s14
00 hr
sAIA
A-201
5-328
4An
Inno
vativ
e All-
Activ
e Hyb
rid
Actu
ation
Syste
mT.
Röbe
n, RW
TH Aa
chen
Univ
ersity
, Aa
chen
, Germ
any
1430
hrs
AIAA-2
015-3
285
Dyna
mic R
econfi
gura
tion m
echan
ism
for D
istrib
uted I
ntegr
ated M
odula
r Av
ionics
Syste
mQ.
Gu,
G. W
ang,
J. W
u, M.
Wan
g, Ch
ina
Natio
nal A
erona
utica
l Rad
io Ele
ctron
ics
Rese
arch I
nstitu
te, S
hang
hai, C
hina
1500
hrs
AIAA-2
015-3
286
Deve
lopme
nt of
an In
tegra
ted
UAS f
or A
gricu
ltura
l Ima
ging
Appli
catio
nsN.
Goli
, B. L
andru
m, U
nivers
ity of
Ala
bama
, Hun
tsville
, Hun
tsville
, AL
1530
hrs
AIAA-2
015-3
287
Major
Airc
raft
Subs
ystem
Effe
cts on
Ga
s Tur
bine P
erfo
rman
ce in
Mor
e Ele
ctric
Aircr
aft A
rchite
cture
sM.
Ozc
an, I
. Cha
krabo
rty, D
. Mav
ris,
Georg
ia Ins
titute
of Te
chno
logy,
Atlan
ta,
GA
1600
hrs
AIAA-2
015-3
288
Desig
n an
d Buil
d of S
warm
Qu
adro
tor U
AVs a
t UGS
S. S
rigrar
om, H
. Lin,
Z. S
aw, J
. Zha
ng,
C. Lim
, Univ
ersity
of G
lasgo
w, S
ingap
ore,
Singa
pore
109
Thur
sday
, 25
June
201
526
6-AM
T-13/
GT-1
3Th
e Imp
act o
f PIV
on A
eros
pace
Tech
nolog
y II
Topa
zCh
aired
by: S
. BER
ESH,
San
dia N
ation
al La
borat
ories
and K
. LOW
E, Vir
ginia
Tech
1400
hrs
Oral
Prese
ntatio
nUs
e of P
IV to
anch
or co
mput
ation
al an
alysis
of fr
ee sh
ear a
nd w
all
boun
ded fl
ows (
Invit
ed)
D. G
aiton
de, O
hio S
tate U
nivers
ity,
Colum
bus,
OH
1430
hrs
Oral
Prese
ntatio
nSy
nerg
istic
Inter
actio
ns of
High
-Re
solut
ion CF
D an
d PIV
to R
evea
l Co
mplex
Uns
teady
Flow
Phy
sics
(Invit
ed)
M. V
isbal,
Air F
orce R
esea
rch La
borat
ory,
Wrig
ht-Pa
tterso
n AFB
, OH
1500
hrs
Oral
Prese
ntatio
nPI
V unc
erta
inty:
how
good
are P
IV
meas
urem
ents?
(Inv
ited)
A. Sc
iacch
itano
, F. S
caran
o, De
lft Un
iversi
ty of
Tech
nolog
y, De
lft, Th
e Ne
therla
nds
1530
hrs
Oral
Prese
ntatio
nTo
mogr
aphic
and t
ime-
reso
lved
PIV:
Addin
g dim
ensio
ns to
flow
dia
gnos
tics (
Invit
ed)
K. Ly
nch,
F. Sc
arano
, Delf
t Univ
ersity
of
Tech
nolog
y, De
lft, Th
e Neth
erlan
ds
1600
hrs
Oral
Prese
ntatio
nPI
V App
licat
ions i
n Su
perso
nic
Comb
ustio
n Wi
nd Tu
nnels
at A
FRL
(Invit
ed)
S. Pe
ltier, C
. Cart
er, Ai
r Forc
e Res
earch
La
borat
ory, W
right-
Patte
rson A
FB, O
H
1630
hrs
Oral
Prese
ntatio
nPIV
in ga
s tur
bine c
ombu
stion
ch
ambe
rs: N
ew in
sights
into
flow
phys
ics an
d its
impo
rtanc
e for
co
mbus
tor de
velop
ment
M. St
ohr, I
. Box
x, O.
Lamm
el, K.
Obe
rleith
ner,
C. Arn
dt, W
. Meie
r, Germ
an Ae
rospa
ce Ce
nter
(DLR
), Stu
ttgart
, Germ
any
1700
hrs
Oral
Prese
ntatio
nA
Tribu
te to
Ron
Adr
ian: T
hree
De
cade
s of P
IV In
nova
tion
(Invit
ed)
S. G
ogine
ni, S
pectr
al En
ergies
, LLC
, Da
yton,
OH
Thur
sday
, 25
June
201
526
7-AP
A-29
Inno
vativ
e Aer
odyn
amic
Conc
epts
& De
signs
Carp
enter
Ball
room
Chair
ed by
: V. B
HAGW
ANDI
N, U
S Arm
y Res
earch
Labo
ratory
and J
. LAT
Z, No
rthrop
Grum
man A
erosp
ace S
ystem
s14
00 hr
sAIA
A-201
5-328
9Ev
aluat
ion of
Ada
ptive
Comp
liant
Tra
iling E
dge T
echn
ology
S. W
akay
ama,
The B
oeing
Comp
any,
Hunti
ngton
Bea
ch, C
A; E.
Whit
e, Th
e Bo
eing C
ompa
ny, B
erkele
y, MO
1430
hrs
AIAA-2
015-3
290
Deter
mina
tion o
f Sect
ion Ae
rody
nami
c Op
eratin
g Con
dition
on W
ings a
nd
Rotor
Blad
es Fro
m Le
ading
-Edge
Pr
essur
e Mea
surem
ents
A. Sa
ini, A.
Gopa
larath
nam,
Nort
h Caro
lina
State
Unive
rsity,
Raleig
h, NC
1500
hrs
AIAA-2
015-3
291
Para
metri
c Stu
dy of
Box
-Wing
Ae
rody
nami
cs fo
r Mini
mum
Drag
Und
er St
abilit
y and
Ma
neuv
erab
ility C
onstr
aints
S. An
drews
, R. P
erez,
Roya
l Milit
ary
Colle
ge of
Cana
da, K
ingsto
n, Ca
nada
1530
hrs
AIAA-2
015-3
292
Optim
izatio
n of
the A
erod
ynam
ic Pe
rform
ance
of R
egion
al an
d Wide
-Bo
dy-C
lass B
lende
d Wing
-Bod
y Ai
rcraf
tT.
Reist
, D. Z
ingg,
Unive
rsity
of To
ronto,
To
ronto,
Cana
da
1600
hrs
AIAA-2
015-3
293
A no
vel a
erod
ynam
ic su
rface
for
redir
ectin
g the
boun
dary
laye
rE.
Sahe
by, G
. Hua
ng, W
. Qiao
, W. T
ang,
Nanji
ng U
nivers
ity of
Aeron
autic
s and
As
trona
utics,
Nan
jing,
China
Thur
sday
, 25
June
201
526
8-AP
A-30
Low
Spee
d, Lo
w Re
ynold
s Num
ber A
erod
ynam
icsGr
and B
allro
om A
Chair
ed by
: Z. Y
ANG,
Wrig
ht St
ate U
nivers
ity an
d A. J
ONES
, Univ
ersity
of M
arylan
d14
00 hr
sAIA
A-201
5-329
4Nu
meric
al inv
estig
ation
of fi
nite-
aspe
ct ra
tio pl
ate fl
ows i
n gr
ound
ef
fect
A. Me
dina,
R. Sin
gh, A
rmy R
esea
rch
Labo
ratory
, Abe
rdeen
Prov
ing G
round
, MD
1430
hrs
AIAA-2
015-3
295
Prop
ulsion
of a
Plung
ing Fl
exibl
e Ai
rfoil u
sing a
Torsi
on Sp
ring M
odel
N. Ar
ora, A
. Gup
ta, In
dian I
nstitu
te of
Tech
nolog
y Delh
i, New
Delh
i, Ind
ia; H
. Ao
no, J
apan
Aeros
pace
Explo
ration
Agen
cy
(JAXA
), Sa
gami
hara,
Japa
n; W.
Shy
y, Ho
ng Ko
ng U
nivers
ity of
Scie
nce a
nd
Tech
nolog
y, Cle
ar Wa
ter B
ay, H
ong K
ong
1500
hrs
AIAA-2
015-3
296
Blad
e Elem
ent M
omen
tum
Mode
ling o
f Low
-Re S
mall U
AS
Electr
ic Pr
opuls
ion Sy
stems
M. M
cCrin
k, J.
Greg
ory, O
hio S
tate
Unive
rsity,
Colum
bus,
OH
1530
hrs
AIAA-2
015-3
297
Stere
osco
pic P
IV an
alysis
on ro
tary
pla
tes in
burst
ingA.
Medin
a, Arm
y Res
earch
Labo
ratory
, Ab
erdee
n Prov
ing G
round
, MD;
A. Jo
nes,
Unive
rsity
of Ma
rylan
d, Co
llege
Park,
Co
llege
Park,
MD
Thur
sday
, 25
June
201
526
9-AP
A-31
Vorti
cal/V
ortex
Flow
Stemm
ons B
Chair
ed by
: M. J
URKO
VICH,
US
Air Fo
rce an
d T. D
OUVIL
LE, T
LG Ae
rospa
ce, L
LC.
1400
hrs
AIAA-2
015-3
298
Near
Gro
und A
ircra
ft Wa
ke
Dissi
patio
n wi
th O
bsta
cles
C. Wa
ng, J
. Sch
luter,
Nan
yang
Te
chno
logica
l Univ
ersity
, Sing
apore
, Sin
gapo
re
1430
hrs
AIAA-2
015-3
299
Effe
cts of
Spinn
ing M
otion
on th
e Tra
pped
Vorte
x Co
mbus
tors
S. Ch
en, R
. Chu
e, J.
Schlu
ter, N
anya
ng
Tech
nolog
ical U
nivers
ity, S
ingap
ore,
Singa
pore;
S. Y
u, Sin
gapo
re Ins
titute
of Te
chno
logy,
Singa
pore,
Sing
apore
1500
hrs
AIAA-2
015-3
300
Trailin
g Vor
tex-In
duce
d Loa
ds
Durin
g Clos
e Enc
ount
ers i
n Cr
uise
M. M
ende
nhall
, D. L
esieu
tre, N
ielse
n En
ginee
ring &
Rese
arch,
Inc.,
Santa
Clara
, CA
; M. K
elly,
NASA
Lang
ley Re
searc
h Ce
nter, H
ampto
n, VA
1530
hrs
AIAA-2
015-3
301
Simula
ting A
ircra
ft Wa
ke Vo
rtice
s wi
th O
VERF
LOW
D. S
chau
erham
er, S
. Rob
inson
, Univ
ersity
of
Califo
rnia,
Davis
, Dav
is, CA
1600
hrs
AIAA-2
015-3
302
Inve
stiga
tion
of pr
opell
er in
duce
d gr
ound
vorti
ces b
y num
erica
l and
ex
perim
enta
l meth
ods
Y. Ya
ng, L
. Veld
huis,
G. E
itelbe
rg, D
elft
Unive
rsity
of Te
chno
logy,
Delft,
The
Nethe
rland
s
110
Thur
sday
, 25
June
201
527
0-AP
A-32
Unste
ady A
erod
ynam
ics II
Stemm
ons A
Chair
ed by
: E. F
ELTR
OP, T
he Ce
ssna A
ircraf
t Com
pany
and K
. VAN
DEN,
USA
F14
00 hr
sAIA
A-201
5-330
3Ef
fect
of B
endin
g-Os
cillat
ions o
n a S
tream
wise
-Orie
nted
Vorte
x In
terac
tion
C. Ba
rnes,
M. V
isbal,
Air F
orce R
esea
rch
Labo
ratory
, Wrig
ht-Pa
tterso
n AFB
, OH;
G.
Hua
ng, W
right
State
Univ
ersity
, Da
yton,
OH
1430
hrs
AIAA-2
015-3
304
Comp
lex ae
ro-e
ngine
inta
ke du
cts
and d
ynam
ic dis
torti
onD.
Mac
Manu
s, N.
Chier
eghin
, D. G
il Prie
to,
P. Za
chos
, Cran
field
Unive
rsity,
Cran
field,
Un
ited K
ingdo
m
1500
hrs
AIAA-2
015-3
305
Flow
disto
rtion
mea
sure
ment
s in
conv
oluted
aero
engin
e int
akes
P. Za
chos
, D. M
acMa
nus,
N. Ch
iereg
hin,
Cranfi
eld U
nivers
ity, C
ranfie
ld, U
nited
Kin
gdom
1530
hrs
AIAA-2
015-3
306
Larg
e Edd
y Sim
ulatio
ns of
Su
perso
nic Je
t Flow
s for
Ae
roac
ousti
c App
licat
ions
C. Ju
nque
ira-Ju
nior, S
. Yam
ouni,
Te
chno
logica
l Insti
tute o
f Aero
nauti
cs (IT
A), S
ão Jo
sé do
s Cam
pos,
Braz
il; J.
Azev
edo,
Aeron
autic
s and
Spa
ce In
stitut
e (IA
E), S
ão Jo
sé do
s Cam
pos,
Braz
il; W.
Wo
lf, Un
iversi
ty of
Camp
inas,
Camp
inas,
Braz
il
1600
hrs
AIAA-2
015-3
307
Unste
ady A
erod
ynam
ics
Simula
tions
of a
Seda
n-Ty
pe R
oad
Vehic
le du
ring S
inuso
idal S
teerin
g In
put
T. Na
kash
ima,
Y. Mo
rikaw
a, Hir
oshim
a Un
iversi
ty, H
igash
i-Hiro
shim
a, Ja
pan;
M.
Tsubo
kura,
Hok
kaido
Univ
ersity
, Sap
poro,
Ja
pan;
Y. Ok
ada,
T. No
uzaw
a, Ma
zda
Motor
Corpo
ration
, Aki
Gun,
Japa
n
1630
hrs
AIAA-2
015-3
308
Coup
led 6
DoF m
otion
and
Aero
dyna
mics
Simula
tion
of R
oad
Vehic
les in
Cros
swind
gusts
H. Is
hioka
, Hok
kaido
Univ
ersity
, Sap
poro,
Ja
pan;
K. On
ishi, R
IKEN
Adva
nced
Insti
tute
for Co
mputa
tiona
l Scie
nce,
Kobe
, Jap
an;
K. Na
kasa
to, N
issan
Moto
r Corp
oratio
n, Yo
koha
ma, J
apan
; T. N
akas
hima,
Hiros
hima U
nivers
ity, H
igash
i-Hiro
shim
a, Ja
pan;
M. Ts
ubok
ura, H
okka
ido U
nivers
ity,
Sapp
oro, J
apan
1700
hrs
AIAA-2
015-3
309
An U
nstea
dy A
erod
ynam
ic Mo
del
base
d on
the L
eadin
g-Ed
ge
Stagn
ation
Poin
tV.
Surya
kuma
r, Y. B
abba
r, T. S
trgan
ac,
Texa
s A&M
Univ
ersity
, Coll
ege S
tation
, TX;
A.
Mang
alam,
Tao o
f Sys
tems I
ntegra
tion,
Inc.,
Hamp
ton, V
A
Thur
sday
, 25
June
201
527
1-AP
A-33
Flow
Cont
rol A
pplic
ation
s & D
emon
strat
ions (
Activ
e & P
assiv
e) II
ISte
mmon
s CCh
aired
by: C
. TILM
ANN,
Air F
orce R
esea
ch La
borat
ory an
d S. S
ILTON
, US
Army R
esea
rch La
borat
ory14
00 hr
sAIA
A-201
5-331
0Na
nose
cond
-SDB
D Ac
tuat
ion ov
er a
Conic
al Fo
rebo
dy at
Wind
Spee
d 72
m/s a
nd A
ngle
of A
ttack
45
degr
eeJ.
Wang
, H. L
i, X. M
eng,
D. Zh
ang,
North
weste
rn Po
lytec
hnica
l Univ
ersity
, Xi’
an, C
hina;
F. Liu
, S. L
uo, U
nivers
ity of
Ca
liforni
a, Irv
ine, I
rvine
, CA
1430
hrs
AIAA-2
015-3
311
Comp
utat
ional
Evalu
ation
of Fl
ow
Cont
rol f
or En
hanc
ed Co
ntro
l Au
thor
ity af
a Ve
rtica
l Tail
A. Sh
milov
ich, Y
. Yad
lin, E
. Wha
len, T
he
Boein
g Com
pany
, Hun
tingto
n Bea
ch, C
A
1500
hrs
AIAA-2
015-3
312
Tech
nique
s for
the D
esign
of A
ctive
Flo
w Co
ntro
l Sys
tems i
n He
avy
Vehic
lesD.
Mano
salva
s, T.
Econo
mon,
F. Pala
cios,
A. Jam
eson,
Stanfo
rd Un
iversit
y, Sta
nford,
CA
1530
hrs
AIAA-2
015-3
313
Expe
rimen
tal in
vesti
gatio
n of P
assiv
e Lo
ad Re
ducti
on un
der d
ynam
ic infl
ow
cond
itions
U. Co
rdes,
K. Hu
fnage
l, C. T
ropea
, Tech
nical
Unive
rsity o
f Darm
stadt,
Darm
stadt,
Germ
any;
G. Ka
mpers
, M. H
ölling
, J. P
einke
, Univ
ersity
of
Olden
burg,
Olde
nburg
, Germ
any
1600
hrs
AIAA-2
015-3
314
Plenu
m de
sign
for c
ompa
ct flu
idic
effe
ctors
J. Ch
ard, A
. Llop
is-Pas
cual,
W. C
rowthe
r, Un
iversi
ty of
Manc
heste
r, Man
ches
ter,
Unite
d King
dom
Thur
sday
, 25
June
201
527
2-AS
E-4Ai
rcraf
t Wak
e Tur
bulen
ce II
(Inv
ited)
Plum
Blos
som
BCh
aired
by: Z
. ZHE
NG, T
he U
nivers
ity of
Kans
as an
d M. P
RUIS,
Nort
hwes
t Res
earch
Asso
ciates
Inc
1400
hrs
AIAA-2
015-3
315
Effe
ct of
Atm
osph
eric
Shee
ts an
d Lay
ers N
ear t
he G
roun
d on
Wake
Vorte
x Tra
nspo
rt an
d Dec
ay
(Invit
ed)
M. Pr
uis, D
. Deli
si, N
orthW
est R
esea
rch
Asso
ciates
, Red
mond
, WA;
D. Ja
cob,
Cohe
rent R
esea
rch G
roup,
Ormo
nd
Beac
h, FL
1430
hrs
AIAA-2
015-3
316
Fast-
time W
ake V
ortex
Mod
el Pr
edict
ions C
ompa
red w
ith
Obser
vatio
ns Be
hind L
andin
g Airc
raft
Near
the G
roun
d (Inv
ited)
M. Pr
uis, D
. Delis
i, Nort
hWest
Resea
rch
Assoc
iates,
Redm
ond,
WA; D
. Jaco
b, Co
heren
t Re
search
Grou
p, Or
mond
Beach
, FL;
D. La
i, No
rthWe
st Re
search
Assoc
iates,
Redm
ond,
WA 15
00 hr
sAIA
A-201
5-331
7Wi
nd an
d EDR
Mea
surem
ents
with
Scann
ing D
opple
r LID
ARs f
or
Prep
aring
Futur
e Wea
ther D
epen
dent
Sepa
ratio
n Con
cepts
(Invit
ed)
L. Th
obois
, R. K
rishna
murth
y, S.
Loae
c, J.
Cario
u, Leo
sphere
, Orsa
y, Fra
nce; A
. Dolfi
-Bo
uteyre
, M. V
alla, O
NERA
, Pala
iseau
, Fran
ce
1530
hrs
AIAA-2
015-3
318
Evalu
ation
of Fa
st-Tim
e Wak
e Mo
dels
using
Den
ver 2
006
Field
Expe
rimen
t Dat
aN.
Ahma
d, NA
SA La
ngley
Rese
arch
Cente
r, Ham
pton,
VA; M
. Prui
s, No
rthWe
st Re
searc
h Asso
ciates
, Sea
ttle, W
A
1600
hrs
AIAA-2
015-3
319
Aero
dyna
mic S
imula
tion
of W
ake
Enco
unter
for A
ircra
ft Clo
se
Form
ation
Ope
ratio
ns (I
nvite
d)A.
He, Z
. Zhe
ng, U
nivers
ity of
Kans
as,
Lawr
ence
, Law
rence
, KS
111
Thur
sday
, 25
June
201
527
3-AS
E-5At
mosp
heric
and S
pace
Envir
onme
nts
Plum
Blos
som
ACh
aired
by: W
. VAU
GHAN
, Willi
am W
Vaug
han C
onsu
ltant
and R
. SCU
LLY, N
ASA
1400
hrs
AIAA-2
015-3
320
Light
ning P
rotec
tion
for t
he O
rion
Spac
e Veh
icle
R. Sc
ully,
NASA
John
son S
pace
Cente
r, Ho
uston
, TX
1430
hrs
AIAA-2
015-3
321
Adva
nced
Spac
ecra
ft Sy
stems
Em
ulatio
n fo
r Spa
ce En
viron
ment
Qu
alific
ation
Testi
ngH.
Ruma
nn, B
astio
n Tec
hnolo
gies,
Inc.,
Hous
ton, T
X
1500
hrs
AIAA-2
015-3
322
Inve
stiga
tion
of th
e Imp
act o
f Su
rface
Blen
ding a
nd U
ltrav
iolet
Radia
tion
Expo
sure
on El
asto
mer
Seal
Leak
Rat
e Per
form
ance
for
Spac
e Sea
l App
licat
ions
S. Ta
ylor, U
nivers
ity of
Toled
o, To
ledo,
OH;
J. Ma
ther, C
. Dan
iels,
Unive
rsity
of Ak
ron,
Akron
, OH
1530
hrs
AIAA-2
015-3
323
Elasto
mer S
eal P
erfo
rman
ce af
ter
Terre
strial
Ultr
aviol
et Ra
diatio
n Ex
posu
reC.
Danie
ls, J.
Math
er, H
. Orav
ec, U
nivers
ity
of Ak
ron, A
kron,
OH; S
. Tay
lor, U
nivers
ity
of To
ledo,
Toled
o, OH
; P. D
unlap
, NAS
A Gle
nn Re
searc
h Cen
ter, C
levela
nd, O
H
1600
hrs
AIAA-2
015-3
324
Ener
gy-A
ware
Pat
h Op
timiza
tion
for P
ersis
tent S
ampli
ng of
Seve
re
Storm
sW.
Silv
a, E.
Frew,
Univ
ersity
of Co
lorad
o, Bo
ulder,
Bou
lder, C
O
1630
hrs
AIAA-2
015-3
325
Ride
Qua
lity W
ithin
Trail A
ircra
ft In
Fo
rmat
ion Fl
ight
W. O
kolo,
A. D
ogan
, Univ
ersity
of Te
xas,
Arling
ton, A
rlingto
n, TX
; W. B
lake,
Air
Force
Rese
arch L
abora
tory,
Wrig
ht-Pa
tterso
n AFB
, OH
1700
hrs
AIAA-2
015-3
326
Math
emat
ical M
odell
ing fo
r Car
bon
Diox
ide Eq
uivale
nt P
redic
tion
of
Gree
nhou
se G
ases
Emitt
ed fr
om a
Small
Scale
Turb
ojet E
ngine
Y. Ş
öhret
, T. K
arako
c, An
adolu
Univ
ersity
, Es
kiseh
ir, Tu
rkey;
N. Ka
rakoç
, Osm
anga
zi Un
iversi
ty, Es
kiseh
ir, Tu
rkey
Thur
sday
, 25
June
201
527
4-AT
IO-2
4UA
S Int
egra
tion
& Op
erat
ions I
Ming
Chair
ed by
: V. S
CHUL
TZ, N
ASA L
angle
y Res
earch
Cente
r14
00 hr
sAIA
A-201
5-332
7An
Evalu
ation
of D
etect
and A
void
(DAA
) Disp
lays f
or U
nman
ned A
ircra
ft Sy
stems
: The
Effec
t of I
nform
ation
Le
vel a
nd D
isplay
Loca
tion o
n Pilo
t Pe
rform
ance
L. Fe
rn, R.
Rorie
, San
Jose
State
Unive
rsity,
Moffe
tt Field
, CA;
J. Pa
ck, In
foscite
x Co
rporat
ion, D
ayton
, OH;
J. Sh
ively,
NASA
Am
es Re
search
Cente
r, Moff
ett Fi
eld, C
A; M.
Dra
per, A
ir Forc
e Rese
arch L
abora
tory,
Wrigh
t-Pa
tterso
n AFB
, OH
1430
hrs
AIAA-2
015-3
328
Syste
m De
velop
ment
for t
he N
ASA
UAS A
irspa
ce O
pera
tions
Chall
enge
S. Fe
hrenb
ach,
Z. Ba
rbeau
, J. J
acob
, G.
Chow
dhary
, Okla
homa
Stat
e Univ
ersity
, St
illwate
r, OK
1500
hrs
AIAA-2
015-3
329
Platfo
rm-In
depe
nden
t Geo
fenc
ing
for L
ow A
ltitud
e UAS
Ope
ratio
nsM.
Stev
ens,
B. Co
loe, E
. Atki
ns, U
nivers
ity
of Mi
chiga
n, An
n Arbo
r, Ann
Arbo
r, MI
Thur
sday
, 25
June
201
527
5-AT
IO-2
5AT
M VI
- Ma
nage
ment
of N
AS R
esou
rces
Moro
ccoCh
aired
by: K
. MAR
AIS, P
urdue
Univ
ersity
1400
hrs
AIAA-2
015-3
330
Strat
egic
Air T
raffi
c Plan
ning w
ith
Frec
het D
istan
ce A
ggre
gatio
n an
d Re
rout
ingA.
Bomb
elli, L
. Sole
r, K. M
ease
, Univ
ersity
of
Califo
rnia,
Irvine
, Irvi
ne, C
A
1430
hrs
AIAA-2
015-3
331
Perfo
rman
ce Im
pact
of Im
prov
ed
Depa
rture
Time
Pre
dictio
n Re
lative
to
Secto
r Dem
and &
Arri
val T
ime
Pred
ictab
ility
R. Cu
rran,
E. Ko
nnem
ann,
Delft
Unive
rsity
of Te
chno
logy,
Delft,
The N
etherl
ands
; S.
Mahli
ch, E
UROC
ONTR
OL, B
retign
y, Fra
nce
1500
hrs
AIAA-2
015-3
332
Proa
ctive
and R
eacti
ve
Mana
geme
nt of
Non
-Wea
ther
Ca
pacit
y Disr
uptio
n Ev
ents
in th
e Na
tiona
l Airs
pace
Syste
m: A
Flow
Mo
delin
g and
Des
ign A
ppro
ach
S. Ro
y, Wa
shing
ton S
tate U
nivers
ity,
Pullm
an, W
A; Y.
Wan,
Unive
rsity
of No
rth
Texa
s, De
nton,
TX
1530
hrs
AIAA-2
015-3
333
Prob
abilis
tic Ti
me-S
eries
Mod
els fo
r Gr
ound
Dela
y Pro
gram
Dec
ision
Su
ppor
tE.
Vargo
, C. T
aylor
, C. W
anke
, MITR
E Co
rporat
ion, M
cLean
, VA
1600
hrs
AIAA-2
015-3
334
Analy
tical
Iden
tifica
tion
and
Rank
ing of
Chok
e Poin
ts in
the
Natio
nal A
irspa
ce Sy
stem
D. Lo
ng, S
. Has
an, V
. Stou
ffer, L
MI,
McLe
an, V
A; K.
Rama
moort
hy, S
aab
Sens
is Co
rporat
ion, E
ast S
yracu
se, N
Y; H.
Idr
is, En
gility
Corpo
ration
, Bille
rica,
MA; B
. Ba
llard,
GRA
, Inc
., Je
nkint
own,
PA; e
t al.
1630
hrs
AIAA-2
015-3
335
Stake
holde
r Fee
dbac
k-Bas
ed
Identi
ficati
on, R
ankin
g, an
d Cau
ses of
Ch
oke P
oints
in the
Nati
onal
Airsp
ace
Syste
mM.
Alcab
in, Th
e Boe
ing Co
mpan
y, Se
attle,
WA
; R. G
olasze
wski,
GRA,
Inc., J
enkin
town,
PA; W
. Cott
on, C
otton
Aviat
ion En
terpri
ses,
Lake
way,
TX; V
. Stou
ffer, L
MI, M
cLean
, VA;
J. Mu
siak,
The B
oeing
Comp
any,
Seatt
le, W
A
112
Thur
sday
, 25
June
201
527
6-AT
IO-2
6Tra
nsfo
rmat
ional
Fligh
t - U
ncon
vent
ional
VTOL
Confi
gura
tions
Mone
t Ball
room
Chair
ed by
: I. C
HOUT
APAL
LI, Th
e Univ
ersity
of Te
xas -
Pan A
meric
an14
00 hr
sOr
al Pre
senta
tion
Fligh
t Tes
t Res
ults f
or th
e DZY
NE
ROTO
Rwing
- A
High
Endu
ranc
e VT
OL Co
ncep
tM.
Page
, DZY
NE Te
chno
logies
, Irvi
ne, C
A
1430
hrs
AIAA-2
015-3
336
Desig
n and
Testi
ng of
the J
oby L
otus
Multif
uncti
onal
Rotor
VTOL
UAV
P. Sin
ha, T
ransit
ion Ro
botic
s, Inc
., Sa
nta
Cruz,
CA; A
. Stol
l, B. G
oldsm
ith, J
oby
Aviat
ion, S
anta
Cruz,
CA
1500
hrs
Oral
Prese
ntatio
nDe
sign
and T
estin
g of t
he Jo
by S2
Ele
ctric
VTOL
PAV P
rope
llers
A. St
oll, P
. Pei,
A. Cl
ark, J
. Bev
irt, Jo
by
Aviat
ion, S
anta
Cruz,
CA
1530
hrs
AIAA-2
015-3
337
Integ
ratio
n of
Elec
tric P
ropu
lsion
in
Effic
ient H
eavy
-Lift
VTOL
Conc
ept
E. De
mers
Bouc
hard,
D. R
anco
urt, D
. Ma
vris,
Georg
ia Ins
titute
of Te
chno
logy,
Atlan
ta, G
A
1600
hrs
Oral
Prese
ntatio
nTh
e Cen
trifu
gally
Stiff
ened
Rot
or
(CSR
) VTO
L Lon
g End
uran
ce
Conc
ept
M. M
oore,
NAS
A Lan
gley R
esea
rch Ce
nter,
Hamp
ton, V
A
Thur
sday
, 25
June
201
527
7-F3
60-9
14
00 -
1630
hrs
Supe
rcomp
uting
: Roa
dmap
and i
ts Fu
ture
Role
in A
eros
pace
Engin
eerin
gGr
and B
allro
om E
Mode
rator:
Dou
g Clin
e, Te
chnic
al Le
ad, H
igh Pe
rform
ance
Comp
uting
, Loc
khee
d Mart
in Ae
ronau
tics
P
aneli
sts:
Willia
m Gr
opp
Thom
as M
. Sieb
el Ch
air, D
epart
ment
of Co
mpute
r Scie
nce a
nd
Direc
tor, P
aralle
l Com
putin
g Ins
titute
Unive
rsity
of Illi
nois
at Ur
bana
-Cham
paign
Brian
Mitc
hell
Senio
r Prin
cipal
Engin
eer
GE G
lobal
Rese
arch
Mark
Seag
erInt
el Fe
llow
CTO,
High
Perfo
rman
ce Co
mputi
ng Ec
osys
tem,
Intel
Corpo
ration
Jef D
awso
nAp
plica
tions
Man
ager
Cray,
Inc.
Thur
sday
, 25
June
201
527
8-FD
-30
Hype
rsonic
and C
hemi
cally
-Rea
cting
Flow
sSa
pphir
eCh
aired
by: B
. WHE
ATON
, The
John
s Hop
kins U
nivers
ity Ap
plied
Phys
ics La
borat
ory an
d J. S
MITH
, San
dia N
ation
al La
borat
ories
1400
hrs
AIAA-2
015-3
338
Starti
ng Ch
arac
terist
ics of
the U
S Ai
r For
ce A
cade
my M
ach
6 Lu
dwieg
Tu
beR.
Deck
er, M
. Sem
per, J
. Anth
ony,
R. Cu
mming
s, U.
S. Ai
r Forc
e Aca
demy
, Co
lorad
o Spri
ngs,
CO
1430
hrs
AIAA-2
015-3
339
Nume
rical
Mode
ling a
nd Si
mulat
ion
of Co
mbus
tion
Phen
omen
a Rela
ted
to Th
erma
l Ign
ition
and F
lame
Fron
tsW.
Tave
rnetti,
M. H
afez,
Unive
rsity
of Ca
liforni
a, Da
vis, D
avis,
CA
1500
hrs
AIAA-2
015-3
340
Larg
e-Edd
y Sim
ulatio
n of A
utoign
ition-
Domi
nated
Supe
rsonic
Comb
ustio
nG.
Cand
ler, P
. Sub
bared
dy, U
nivers
ity of
Mi
nnes
ota, M
innea
polis,
Minn
eapo
lis,
MN; N
. Cym
balist
, P. D
imota
kis, C
alifor
nia
Institu
te of
Tech
nolog
y, Pa
sade
na, C
A
1530
hrs
AIAA-2
015-3
341
A Nu
meric
al Sc
heme
for H
yper
sonic
Tu
rbule
nt Fl
owM.
Righ
i, Zuri
ch U
nivers
ity of
Appli
ed
Scien
ces,
Wint
erthu
r, Swi
tzerla
nd
Thur
sday
, 25
June
201
527
9-FD
-31
Flow
Cont
rol -
Vorti
cal F
lows
Sena
tors
Lectu
re H
allCh
aired
by: M
. YU,
Univ
ersity
of M
arylan
d, Ba
ltimore
Coun
ty an
d L. P
ACK M
ELTO
N, N
ASA-L
angle
y Res
earch
Cente
r14
00 hr
sAIA
A-201
5-334
2Ob
serv
ation
s on
the M
ean
and
Turb
ulent
Wak
e of a
Micr
o-Ra
mp
Arra
yE.
Bayd
ar, F.
Lu, U
nivers
ity of
Texa
s, Arl
ington
, Arlin
gton,
TX; J
. Slat
er, N
ASA
Glenn
Rese
arch C
enter
, Clev
eland
, OH
1430
hrs
AIAA-2
015-3
343
Mixin
g Lay
er: N
umer
ical a
nd
Expe
rimen
tal C
ontro
l Stra
tegies
J. Lit
tle, U
nivers
ity of
Arizo
na, T
ucso
n, Tu
cson,
AZ; U
. Kau
l, NAS
A Ame
s Res
earch
Ce
nter, M
offett
Field
, CA
1500
hrs
AIAA-2
015-3
344
Effe
cts of
Puls
e Ene
rgy o
n Sh
ear
Laye
r Con
trol u
sing S
urfa
ce P
lasma
Di
schar
ges
D. Ak
ins, A
. Sing
h, J.
Little
, Univ
ersity
of
Arizo
na, T
ucso
n, Tu
cson,
AZ
1530
hrs
AIAA-2
015-3
345
Towa
rds i
nteg
ral b
ound
ary l
ayer
mo
dellin
g of v
ane-
type
vorte
x ge
nera
tors
D. B
aldac
chino
, C. S
imao
Ferre
ira, G
. van
Bu
ssel, D
elft U
nivers
ity of
Tech
nolog
y, De
lft, Th
e Neth
erlan
ds
113
Thur
sday
, 25
June
201
528
0-FT
-2/G
T-14
Optim
izatio
n Te
chniq
ues i
n Fli
ght T
est/
Grou
nd Te
stOb
elisk
BCh
aired
by: W
. SCH
UMAN
, AF T
STA/
AEDC
and B
. MILL
S, AE
DC/
ATA
1400
hrs
AIAA-2
015-3
346
Optim
ized C
alcula
tion
of Fo
rces f
or
Fulls
cale
Aircr
aft S
tructu
re Fa
tigue
Te
sting
C. He
, Avia
tion I
ndus
try Co
rporat
ion of
Ch
ina (A
VIC),
Xi’an
, Chin
a
1430
hrs
AIAA-2
015-3
347
The d
esign
and t
est re
sult o
f pres
sure
dis
tortio
n com
pens
ation
devic
e in
Weigh
t and
Balan
ce Sy
stem
Y. Mi
nqian
g, C.
Yue,
Taiyu
an Ae
ro-Ins
trume
nts Co
mpan
y, Ltd
., Ta
iyuan
, Chin
a
1500
hrs
AIAA-2
015-3
348
Evalu
ation
of Lo
w-Co
st Au
topil
ots
for S
UAS O
pera
tions
C. Br
own,
J. Ja
cob,
Oklah
oma S
tate
Unive
rsity,
Still
water
, OK
1530
hrs
AIAA-2
015-3
349
Appli
catio
n of
a sm
all U
AV fl
eet f
or
demo
nstra
tion
of op
timize
d miss
ionM.
Kasp
rzyk,
P. Bib
ik, M
. Mali
nows
ki,
J. Po
lacze
k, K.
Wron
owsk
i, Wars
aw
Unive
rsity
of Te
chno
logy,
Warsa
w, Po
land
Thur
sday
, 25
June
201
528
1-GE
PC-1
Over
view
of N
ASA
Adva
nced
Air
Vehic
les P
rogr
amMe
tropo
litan
Ballr
oom
Chair
ed by
: B. E
SKER
and R
. DEL
ROSA
RIO, N
ASA G
lenn R
esea
rch Ce
nter
1400
hrs
Oral
Prese
ntatio
nAd
vanc
ed A
ir Ve
hicles
Pro
gram
Ov
ervie
wJ.
Drye
r, B. E
sker,
NAS
A Hea
dqua
rters,
Wa
shing
ton, D
C
1430
hrs
Oral
Prese
ntatio
nNA
SA’s
Adva
nced
Air
Trans
port
Tech
nolog
y Pro
ject
R. De
l Ros
ario,
NASA
Glen
n Res
earch
Ce
nter, C
levela
nd, O
H; S
. And
ers, N
ASA
Lang
ley Re
searc
h Cen
ter, H
ampto
n, VA
; N.
Mada
van,
NASA
Ames
Rese
arch C
enter
, Mo
ffett
Field,
CA
1500
hrs
Oral
Prese
ntatio
nCo
mmer
cial S
uper
sonic
Tech
nolog
y Pr
oject
Over
view
P. Co
en, N
ASA L
angle
y Res
earch
Cente
r, Ha
mpton
, VA;
K. Civ
inska
s, L.
Povin
elli,
NASA
Glen
n Res
earch
Cente
r, Clev
eland
, OH
1530
hrs
Oral
Prese
ntatio
nRe
volut
ionar
y Ver
tical
Lift
Tech
nolog
y Pro
ject
S. G
orton
, NAS
A Lan
gley R
esea
rch
Cente
r, Ham
pton,
VA; I
. Lóp
ez, N
ASA
Glenn
Rese
arch C
enter
, Clev
eland
, OH;
C.
Theo
dore,
NAS
A Ame
s Res
earch
Cente
r, Mo
ffett
Field,
CA
1600
hrs
Oral
Prese
ntatio
nAd
vanc
ed Co
mpos
ites P
rojec
t Ov
ervie
wR.
Youn
g, S.
Sme
ltzer,
NAS
A Lan
gley
Rese
arch C
enter
, Ham
pton,
VA
1630
hrs
Oral
Prese
ntatio
nNA
SA A
eron
autic
s Eva
luatio
n an
d Te
st Ca
pabil
ities P
rojec
tC.
Mouri
ng, N
ASA L
angle
y Res
earch
Ce
nter, H
ampto
n, VA
; R. C
olanto
nio, N
ASA
Glenn
Rese
arch C
enter
, Clev
eland
, OH
Thur
sday
, 25
June
201
528
2-LTA
-2Lig
hter
-than
-Air
Syste
ms &
Tech
nolog
ies II
Steub
enCh
aired
by: D
. HOR
KHEIM
ER, H
oney
well I
nterna
tiona
l, Inc
.14
00 hr
sAIA
A-201
5-335
0La
b-Sc
ale Ch
arac
teriza
tion
of a
Light
er-Th
an-A
ir Wi
nd En
ergy
Sy
stem
- Clos
ing th
e Loo
pJ.
Dees
e, T.
Muyim
bwa,
N. D
eodh
ar, C.
Ve
rmilli
on, P
. Tka
cik, U
nivers
ity of
Nort
h Ca
rolina
, Cha
rlotte
, Cha
rlotte
, NC
1430
hrs
AIAA-2
015-3
351
The 1
2M™
Teth
ered
Aer
osta
t Sy
stem:
Rap
id Ta
ctica
l Dep
loyme
nt
for S
urve
illanc
e Miss
ions
J. Kra
usma
n, D.
Mille
r, TCO
M, L.
P.,
Colum
bia, M
D
1500
hrs
AIAA-2
015-3
352
Desig
n an
d Flig
ht Te
sting
of an
Au
tono
mous
Airs
hipJ.
Santo
s, D.
Garc
ia, M
. Cun
ha, L
. Góe
s, Te
chno
logica
l Insti
tute o
f Aero
nauti
cs (IT
A), S
ão Jo
sé do
s Cam
pos,
Braz
il; R.
Pant,
India
n Ins
titute
of Te
chno
logy
Mumb
ai, M
umba
i, Ind
ia
1530
hrs
AIAA-2
015-3
353
Diap
hrag
m Te
sting
of Fa
bric
Comp
onen
ts &
Corre
lation
to
Analy
sisK.
Crome
r, S. P
eterse
n, TC
OM, L
.P.,
Colum
bia, M
D
Thur
sday
, 25
June
201
528
3-MA
O-10
Shap
e and
Topo
logy I
IMa
drid
Chair
ed by
: B. M
ESME
R, Un
iversi
ty of
Alaba
ma an
d V. K
ALIVA
RAPU
, Iow
a Stat
e Univ
ersity
1400
hrs
AIAA-2
015-3
354
Volum
etric
Shap
e Par
amete
risat
ion
for C
ombin
ed A
erod
ynam
ic Ge
ometr
y and
Topo
logy
Optim
isatio
nJ.
Hall,
D. Po
ole, T
. Ren
dall,
C. All
en,
Unive
rsity
of Br
istol,
Bris
tol, U
nited
Kin
gdom
1430
hrs
AIAA-2
015-3
355
A Di
screte
Adjo
int Fr
amew
ork
for U
nstea
dy A
erod
ynam
ic an
d Ae
roac
ousti
c Opt
imiza
tion
B. Zh
ou, T
. Albr
ing, N
. Gau
ger, T
echn
ical
Unive
rsity
of Ka
isersl
auter
n, Ka
isersl
auter
n, Ge
rman
y; T.
Econ
omon
, F. P
alacio
s, J.
Alons
o, St
anfor
d Univ
ersity
, Stan
ford,
CA
1500
hrs
AIAA-2
015-3
356
Towa
rds s
hape
optim
izatio
n of
stea
dy-st
ate fl
uid-st
ructu
re
inter
actio
n pr
oblem
s usin
g ver
tex
morp
hing
R. Na
jian A
sl, D
. Bau
mgärt
ner, K
. Ble
tzing
er, Te
chnic
al Un
iversi
ty of
Munic
h, Mu
nich,
Germ
any
1530
hrs
AIAA-2
015-3
357
Know
ledge
-bas
ed In
tegra
ted W
ing
Auto
matio
n an
d Opt
imiza
tion
for
Conc
eptu
al De
sign
R. Mu
njulur
y, P.
Berry
, T. M
elin,
K. Am
adori
, P. K
rus, L
inköp
ing U
nivers
ity,
Linkö
ping,
Swed
en
1600
hrs
AIAA-2
015-3
358
Conc
eptua
l opti
mal d
esign
of
envir
onme
ntally
frien
dly ai
rliners
: a
review
of av
ailab
le me
thodo
logies
an
d the
ir inte
grati
on in
to a c
onsis
tent
frame
work
for e
very
day u
seP. M
agalh
aes,
B. Ma
ttos,
Techn
ologic
al Ins
titute
of Ae
ronau
tics (I
TA), S
ão Jo
sé do
s Ca
mpos,
Braz
il
1630
hrs
AIAA-2
015-3
359
Robu
st an
d Reli
abilit
y-Ba
sed
Topo
logy O
ptim
izatio
n of
Wing
Bo
dies
D. Pa
padim
itriou
, C. P
apad
imitri
ou,
Unive
rsity
of Th
essa
ly, Vo
los, G
reece
114
Thur
sday
, 25
June
201
528
4-MA
O-11
Unce
rtaint
y IMa
nche
ster
Chair
ed by
: R. K
OLON
AY, A
ir Forc
e Res
earch
Labo
ratory
/RQV
C/W
PAFB
and P
. PIPE
RNI,
Bomb
ardier
Inc
1400
hrs
AIAA-2
015-3
360
High
-Fide
lity W
eight
Estim
ation
fo
r Airc
raft
Conc
eptu
al De
sign
Optim
izatio
nN.
Niga
m, S
. Ayy
alaso
maya
jula,
X.
Qi, P
. Che
n, Int
ellige
nt Au
tomati
on,
Inc.,
Rock
ville,
MD;
J. Al
onso
, Stan
ford
Unive
rsity,
Stan
ford,
CA
1430
hrs
AIAA-2
015-3
361
Surro
gate-
base
d Rob
ust S
hape
Op
timiza
tion
for V
ane C
luster
sI.
Arsen
yev,
F. Du
ddec
k, Te
chnic
al Un
iversi
ty of
Munic
h, Mu
nich,
Germ
any;
A. Fis
chers
worrin
g-Bun
k, MT
U Ae
ro En
gines
, Mu
nich,
Germ
any
Thur
sday
, 25
June
201
528
5-MS
T-12
Prop
ulsion
Syste
msTra
verti
neCh
aired
by: A
. ELM
ILIGU
I, NA
SA La
ngley
Rese
arch C
enter
1400
hrs
AIAA-2
015-3
362
One-
dimen
siona
l Mod
el of
a Clo
sed-
loop U
nder
water
Pro
pulsi
on
Syste
mJ.
Lu, C
hina S
hipbu
ilding
Indu
stry
Corpo
ration
Comp
any,
Ltd.,
Xi’an
, Chin
a
1430
hrs
AIAA-2
015-3
363
Indiv
idual
mode
l iden
tifica
tion
for
turb
ofan
engin
e bas
ed on
parti
cle
swar
m op
timiza
tion
J. Qi
an, F
. Liu,
Nan
jing U
nivers
ity of
Ae
ronau
tics a
nd As
trona
utics,
Nan
jing,
China
; X. Q
iu, Av
iation
Moto
r Con
trol
Syste
m Ins
titute,
Wux
i, Chin
a
1500
hrs
AIAA-2
015-3
364
Nume
rical
Study
of Si
milar
ity an
d Di
mens
ional
Meth
ods i
n Sc
aled
Turb
ine Va
ne co
oling
perfo
rman
ce
expe
rimen
tY.
Liu, M
. Jun
kui, G
. Dila
n, Na
njing
Un
iversi
ty of
Aeron
autic
s and
Astro
nauti
cs,
Nanji
ng, C
hina
Thur
sday
, 25
June
201
528
6-PD
L-13
Plasm
a Aer
odyn
amics
& Fl
ow Co
ntro
l VMi
roCh
aired
by: J
. POG
GIE,
USAF
AFRL
/RBA
C14
00 hr
sAIA
A-201
5-336
5Nu
meric
al Stu
dy of
Th
erma
l Pro
tectio
n Us
ing
Magn
etohy
drod
ynam
ic Flo
w Co
ntro
l in M
ars E
ntry
Fligh
tT.
Taka
hash
i, Y. S
himos
awa,
K. Ma
suda
, T.
Fujin
o, Un
iversi
ty of
Tsuku
ba, T
suku
ba,
Japa
n
1430
hrs
AIAA-2
015-3
366
Three
-dime
nsion
al Nu
meric
al Sim
ulatio
n of M
agne
tohyd
rody
nami
c Flo
w Co
ntrol
in Re
entry
Fligh
tK.
Masud
a, Y.
Shim
osawa
, Univ
ersity
of
Tsuku
ba, T
sukub
a, Jap
an; S
. Oga
wa, T
. Yo
shino
, Tosh
iba Co
rporat
ion, K
awasa
ki,
Japan
; T. F
ujino,
Unive
rsity o
f Tsuk
uba,
Tsuku
ba, J
apan
1500
hrs
AIAA-2
015-3
367
Mode
ling D
BD P
lasma
Actu
ator
s in
Integ
ral B
ound
ary L
ayer
Fo
rmula
tion
for A
pplic
ation
in
Pane
l Meth
ods
G. de
Oliv
eira,
R. Sa
ntos P
ereira
, D.
Ragn
i, M. K
otson
is, D
elft U
nivers
ity of
Te
chno
logy,
Delft,
The N
etherl
ands
1530
hrs
AIAA-2
015-3
368
Nume
rical
Inve
stiga
tion
of Se
vera
l Al
kali M
etal A
dditio
n Me
thod
s for
th
e For
ced E
levat
ion of
the S
tarti
ng
Altit
ude i
n th
e Elec
trody
nami
c Ae
robr
aking
Dec
leara
tion
H. Ka
tsuray
ama,
Yama
guch
i Univ
ersity
, Ub
e, Ja
pan
1600
hrs
AIAA-2
015-3
369
Parti
cle in
Cell (
PIC)
simu
lation
s of
plasm
a-ele
ctrod
e int
erac
tions
for
Reen
try B
lacko
ut A
llevia
tion
S. Kr
ishna
moort
hy, S
. Clos
e, St
anfor
d Un
iversi
ty, S
tanfor
d, CA
Thur
sday
, 25
June
201
528
7-RL
A-3
1400
- 15
30 h
rsRi
sing L
eade
rs in
Aero
spac
e Pan
el Di
scussi
on: T
rans
itionin
g to L
eade
rship
Emer
ald
This
pane
l will
addre
ss the
chan
ges t
hat a
ccomp
any m
oving
into
a man
agem
ent r
ole, t
he di
fferen
t skil
l sets
that
will n
eed t
o be a
cquir
ed, a
nd th
e cha
nges
you c
an ex
pect
in yo
ur da
ily w
ork ro
utine
.Mo
derat
or: B
en M
archio
nna,
Syste
ms En
ginee
r, Loc
khee
d Mart
in Sk
unk W
orks
P
aneli
sts:
Russ
Alth
ofCh
ief En
ginee
rRa
ytheo
n Miss
ile S
ystem
s
Doug
las St
anley
Presid
ent a
nd Ex
ecuti
ve D
irecto
rNa
tiona
l Insti
tute o
f Aero
spac
e
Fred
erick
Wiel
and
Direc
tor, A
ir Traf
fic M
anag
emen
tInt
ellige
nt Au
tomati
on S
ystem
s, Inc
.
115
Thur
sday
, 25
June
201
528
8-TP
-13
DSMC
Rose
ttaCh
aired
by: D
. HAS
H, N
ASA -
ARC
1400
hrs
AIAA-2
015-3
370
DSMC
Stud
y of C
arbo
n Fibe
r Oxid
ation
in
Ablat
ive Th
ermal
Prote
ction
Syste
msA.
Borne
r, NAS
A Ame
s Rese
arch C
enter
, Mo
ffett F
ield, C
A; F. P
anera
i, Univ
ersity
of
Kentu
cky, L
exing
ton, L
exing
ton, K
Y; N.
Ma
nsour,
NAS
A Ame
s Rese
arch C
enter
, Mo
ffett F
ield, C
A
1430
hrs
AIAA-2
015-3
371
Sens
itivity
Ana
lysis
of D
SMC
Para
meter
s for
Ioniz
ing, R
adiat
ing
Hype
rsonic
Flow
sK.
Higdo
n, D.
Gold
stein,
P. Va
rghes
e, Un
iversi
ty of
Texa
s, Au
stin,
Austi
n, TX
1500
hrs
AIAA-2
015-3
372
DSMC
Inve
stiga
tion
of
None
quilib
rium
Effe
cts in
a H2
-O2
Unstr
etche
d Diff
usion
Flam
eI.
Borge
s Seb
astia
o, A.
Alexe
enko
, Purd
ue
Unive
rsity,
Wes
t Lafa
yette
, IN
1530
hrs
AIAA-2
015-3
373
Calib
ratio
n of
DSM
C par
amete
rs fo
r tra
nspo
rt pr
oces
ses i
n ion
ized
air m
ixtur
esK.
Swam
inatha
n Gop
alan,
K. St
epha
ni,
Unive
rsity
of Illi
nois,
Urba
na-Ch
ampa
ign,
Urba
na, I
L
Thur
sday
, 25
June
201
528
9-NW
-9
1530
- 16
00 h
rsNe
twor
king C
offe
e Bre
akMe
eting
Roo
m Fo
yers
Thur
sday
, 25
June
201
529
0-LE
C-6
1730
- 18
30 h
rsWr
ight B
roth
ers L
ectu
resh
ip in
Aero
naut
icsCh
antill
y Ball
room
Wes
t
Deve
lopme
nt an
d Test
ing of
the X
-47B
Pablo
Gon
zalez
, II
UCAS
-D Pro
gram
Mana
ger
North
rop G
rumma
n Aero
spac
e Sys
tems
Frida
y
Frida
y, 26
June
201
529
1-SB
-5
0730
- 08
00 h
rsSp
eake
rs’ B
riefin
gSe
ssion
Roo
ms
Frida
y, 26
June
201
529
2-PL
NRY-5
08
00 -
0900
hrs
Plena
ry K
eyno
teCh
antill
y Ball
room
Wes
t
The G
650 D
esign
, Dev
elopm
ent,
and T
estKu
rt Er
bach
erVic
e Pres
ident,
G65
0 Air
craft
Progra
mGu
lfstre
am Ae
rospa
ce Co
rporat
ion
Frida
y, 26
June
201
529
3-AC
D-8
Aero
naut
ic Di
scipli
ne Co
nside
ratio
ns in
Airc
raft
Desig
nMi
roCh
aired
by: H
. JIM
ENEZ
, Geo
rgia I
nstitu
te of
Tech
nolog
y09
00 hr
sAIA
A-201
5-337
4Pr
edict
ion of
Wing
Stru
ctura
l Mas
s fo
r Tra
nspo
rt Ca
tegor
y Aicr
aft
Conc
eptu
al De
sign
T. Ta
kaha
shi, T
. Lem
onds
, Ariz
ona S
tate
Unive
rsity,
Temp
e, AZ
0930
hrs
AIAA-2
015-3
375
Effe
ctive
L/D:
A Th
eore
tical
Appr
oach
to th
e Mea
sure
ment
of
Aer
o-Str
uctu
ral E
fficie
ncy i
n Ai
rcraf
t Des
ignM.
Guy
nn, N
ASA L
angle
y Res
earch
Cente
r, Ha
mpton
, VA
1000
hrs
AIAA-2
015-3
376
Revis
iting B
usem
ann:
The D
esign
Im
plica
tions
of In
cons
isten
cies
Foun
d With
in Sim
ple Sw
eep T
heor
yT.
Taka
hash
i, S. K
amat,
Arizo
na S
tate
Unive
rsity,
Temp
e, AZ
1030
hrs
AIAA-2
015-3
377
A To
tal F
light
Enve
lope A
ppro
ach
to Co
ncep
tual
Desig
n Sta
bility
&
Cont
rol
M. S
wann
, T. T
akah
ashi,
Arizo
na S
tate
Unive
rsity,
Temp
e, AZ
1100
hrs
AIAA-2
015-3
378
Feas
ibility
Stud
ies on
a Hi
gh-A
ltitud
e Ca
ptive
Ligh
ter-Th
an-A
ir Plat
form
Syste
mK.
Chiba
, S. S
atori,
R. Hir
amoto
, S. K
ase, R
. Mi
tsuha
shi, H
okka
ido Un
iversit
y of S
cience
, Sa
pporo
, Jap
an; J
. Sasa
ki, Ho
kkaid
o Ae
rospa
ce Sc
ience
and T
echno
logy I
ncuba
tion
Cente
r, Sap
poro,
Japa
n; et
al.
116
Frida
y, 26
June
201
529
4-AM
T-14/
GT-1
5Ae
rody
nami
c Mea
sure
ment
Syste
ms: C
alibr
ation
and M
onito
ring
Topa
zCh
aired
by: R
. RHE
W, N
ASA-L
angle
y Res
earch
Cente
r and
G. J
ONES
, NAS
A-Lan
gley R
esea
rch Ce
nter
0900
hrs
Oral
Prese
ntatio
nMe
asur
emen
t Sys
tem Ca
libra
tion
Fund
amen
tals
R. Rh
ew, P
. Park
er, G
. Jon
es, N
ASA
Lang
ley Re
searc
h Cen
ter, H
ampto
n, VA
0930
hrs
AIAA-2
015-3
379
Impr
oved
Reg
ressi
on A
nalys
is of
Te
mper
atur
e-De
pend
ent S
train-
Gage
Bala
nce C
alibr
ation
Dat
aN.
Ulbr
ich, J
acob
s, Mo
ffett
Field,
CA
1000
hrs
AIAA-2
015-3
380
Statis
tical
Proc
ess Co
ntrol
Imple
mente
d for
Long
Term
Stud
y of
Wind
Tunn
el Ba
lance
Calib
ratio
nsR.
Callah
an, D
. Lan
dman
, Old
Domi
nion
Unive
rsity,
Norfo
lk, VA
; S. C
ommo
, K. L
ynn,
NASA
Lang
ley Re
search
Cente
r, Ham
pton,
VA
1030
hrs
AIAA-2
015-3
381
Analy
sis of
Five
-Hole
Pro
be
Calib
ratio
n Pa
rame
ters
S. Ka
rahan
, A. K
utay,
Midd
le Ea
st Te
chnic
al Un
iversi
ty, An
kara,
Turke
y
1100
hrs
AIAA-2
015-3
382
The U
se of
Abs
olute-
Value
Term
s in
Regr
essio
n Mo
delin
g of M
ulti-P
iece
Force
Bala
nces
(Inv
ited)
M. Ka
mmey
er, Th
e Boe
ing Co
mpan
y, St
. Lo
uis, M
O; N
. Ulbr
ich, J
acob
s, Mo
ffett
Field,
CA
Frida
y, 26
June
201
529
5-AP
A-34
Icing
or R
ough
ness
Effe
cts on
Vehic
le Ae
rody
nami
csSte
mmon
s CCh
aired
by: G
. WOO
, Gen
eral E
lectric
Glob
al Re
searc
h and
D. O
’BRIE
N, U
S Arm
y RDE
COM
0900
hrs
AIAA-2
015-3
383
Data
-Driv
en Lo
w-Di
mens
ional
Mode
ling a
nd U
ncer
taint
y Qu
antifi
catio
n fo
r Airf
oil Ic
ingA.
DeGe
nnaro
, C. R
owley
, L. M
artine
lli,
Princ
eton U
nivers
ity, P
rince
ton, N
J
0930
hrs
AIAA-2
015-3
384
Aero
dyna
mic E
ffects
of R
ough
ness
on W
ind Tu
rbine
Blad
e Sec
tions
L. Jo
seph
, J. F
enou
il, A.
Borgo
ltz, W
. De
venp
ort, V
irgini
a Poly
techn
ic Ins
titute
and S
tate U
nivers
ity, B
lacks
burg,
VA
1000
hrs
AIAA-2
015-3
385
The C
hara
cteris
tics o
f SLD
icing
ac
cretio
ns an
d aero
dyna
mic e
ffects
on
high-l
ift co
nfigu
ratio
nsC.
Zhan
g, F. W
ang,
W. Ko
ng, H
. Liu,
Shan
ghai
Jiao T
ong U
nivers
ity, Sh
angh
ai, Ch
ina
Frida
y, 26
June
201
529
6-AP
A-35
Aero
dyna
mic D
esign
Meth
odolo
gies I
IICa
rpen
ter B
allro
omCh
aired
by: C
. ROS
EMA,
US Ar
my AM
RDEC
0900
hrs
AIAA-2
015-3
386
Expe
rimen
tal V
alida
tion
of a
Morp
hed W
ing G
eome
try U
sing
Small
Wind
Tunn
el Te
sting
A. Ko
reans
chi, S
. Oliv
iu, R.
Bote
z, Un
iversi
ty of
Québ
ec, M
ontré
al, Ca
nada
0930
hrs
AIAA-2
015-3
387
Stabil
ity D
eriva
tive C
ompu
tation
of
Taille
ss Air
craft
using
Varia
ble-Fi
delity
Ae
rody
nami
c Ana
lysis a
nd W
ind-
Tunn
el Ex
perim
ents
J. Pa
rk, C.
Oche
ltree,
J. Ch
oi, S.
Choi,
P. Ra
j, A.
Fried
man,
Virgin
ia Po
lytech
nic In
stitute
and
State
Unive
rsity,
Blacks
burg,
VA
1000
hrs
AIAA-2
015-3
388
Aero
dyna
mic p
erfo
rman
ce st
udy
of h
igh pr
essu
re zo
ne ca
ptur
e wing
co
nfigu
ratio
nsK.
Cui, G
. Li, Y
. Xiao
, Chin
ese A
cade
my of
Sc
ience
s, Be
ijing,
China
Frida
y, 26
June
201
529
7-AP
A-37
Prop
eller
/Rot
orcra
ft/Wi
nd Tu
rbine
Aer
odyn
amics
III
Stemm
ons B
Chair
ed by
: K. M
ASSE
Y, DA
RPA/
TTO
and J
. MUR
RAY,
Sand
ia Na
tiona
l Lab
orator
ies09
00 hr
sAIA
A-201
5-338
9Se
nsitiv
ity of
Wind
Turb
ine A
irfoil
Se
ction
s to G
eome
try Va
riatio
ns
Inhe
rent
in M
odula
r Blad
esK.
Brow
n, N.
Moli
naro,
T. M
eyers
, A.
Borgo
ltz, W
. Dev
enpo
rt, V
irgini
a Po
lytec
hnic
Institu
te an
d Stat
e Univ
ersity
, Bla
cksb
urg, V
A; J.
Lued
ke, G
enera
l Elec
tric
Comp
any,
Gree
nville
, SC;
et al.
0930
hrs
AIAA-2
015-3
390
Confi
gura
tion a
nd N
umeri
cal
Invest
igatio
n of t
he Ad
aptiv
e Cam
ber
Airfoi
l as P
assiv
e Loa
d Alle
viatio
n Me
chan
ism fo
r Wind
Turb
ines
D. Ma
rten,
Techn
ical U
nivers
ity of
Berlin
, Be
rlin, G
erman
y; H.
Spieg
elberg
, Tech
nical
Unive
rsity o
f Darm
stadt,
Darm
stadt,
Germ
any;
G. Pe
chliva
noglo
u, C.
Naye
ri, C.
Pasch
ereit,
Techn
ical U
nivers
ity of
Berlin
, Berl
in, Ge
rman
y; C.
Trope
a, Tec
hnica
l Univ
ersity
of Da
rmsta
dt,
Darm
stadt,
Germ
any
1000
hrs
AIAA-2
015-3
391
Exten
sion
of a
Para
bolic
Meth
od
with
out P
ressu
re A
ppro
ximat
ions
for W
ind Tu
rbine
s in
ABL F
lows
A. Mi
ttal, L
. Tay
lor, K
. Sree
nivas
, W.
Brile
y, D.
Nich
ols, U
nivers
ity of
Tenn
esse
e, Ch
attan
ooga
, Cha
ttano
oga,
TN
1030
hrs
AIAA-2
015-3
392
Expe
rimen
tal a
nd N
umer
ical
Inve
stiga
tions
of a
Small
Res
earch
Wi
nd Tu
rbine
S. Ve
y, D.
Mart
en, G
. Pec
hliva
noglo
u, C.
Naye
ri, C.
Pasch
ereit,
Tech
nical
Unive
rsity
of Be
rlin, B
erlin,
Germ
any
1100
hrs
AIAA-2
015-3
393
Optim
izatio
n of
Wind
Turb
ine
Airfo
ils Su
bject
to P
artic
le Er
osion
G. Fi
ore, M
. Seli
g, Un
iversi
ty of
Illino
is,
Urba
na-Ch
ampa
ign, U
rbana
, IL
117
Frida
y, 26
June
201
529
8-AT
IO-2
7AT
M VI
I - W
eath
er Im
pact
Moro
ccoCh
aired
by: Y
. JUN
G, N
ASA A
mes R
esea
rch Ce
nter
0900
hrs
AIAA-2
015-3
394
Dyna
mic A
rriva
l Rou
tes: A
Tra
jecto
ry-B
ased
Wea
ther
Av
oidan
ce Sy
stem
for M
ergin
g Ar
rivals
and M
eterin
gC.
Gong
, D. M
cnall
y, NA
SA Am
es Re
searc
h Ce
nter, M
offett
Field
, CA
0930
hrs
AIAA-2
015-3
395
Initia
l Ana
lysis
of an
d Pre
dictiv
e Mo
del D
evelo
pmen
t for
Wea
ther
Re
rout
e Adv
isory
Use
H. Ar
neso
n, NA
SA Am
es Re
searc
h Cen
ter,
Moffe
tt Fie
ld, CA
1000
hrs
AIAA-2
015-3
396
Bene
fits A
nalys
is of
Gro
und-
Sour
ced C
onve
ctive
Wea
ther
Al
ertin
g in
the C
ockp
itS.
Camp
bell,
M. M
cPart
land,
M. Is
hutki
na,
Linco
ln La
borat
ory, M
assa
chus
etts I
nstitu
te of
Tech
nolog
y, Le
xingto
n, MA
1030
hrs
AIAA-2
015-3
397
Dyna
mic W
ake V
ortex
Sepa
ratio
n Co
mbini
ng w
ith A
MAN/
DMAN
Co
ncep
tN.
Mata
yosh
i, E. Y
oshik
awa,
Japa
n Ae
rospa
ce Ex
plorat
ion Ag
ency
(JAX
A),
Mitak
a, Ja
pan
1100
hrs
AIAA-2
015-3
398
Wind
Info
rmat
ion U
plink
to A
ircra
ft Pe
rform
ing In
terva
l Man
agem
ent
Oper
ation
sN.
Ahma
d, B.
Barm
ore, K
. Swi
ering
a, NA
SA
Lang
ley Re
search
Cente
r, Ham
pton,
VA
1130
hrs
AIAA-2
015-3
399
Wind
Mea
sure
ment
s with
grou
nd-
base
d fibe
r-bas
ed w
ind D
opple
r LID
AR sy
stems
for a
viatio
n we
athe
r ap
plica
tions
L. Th
obois
, Leo
sphe
re, O
rsay,
Franc
e
Frida
y, 26
June
201
529
9-AT
IO-2
8Fu
ture
Conc
epts
Wyeth
Chair
ed by
: K. M
ARAIS
, Purd
ue U
nivers
ity09
00 hr
sAIA
A-201
5-340
0Ac
hievin
g TAS
AR O
pera
tiona
l Re
adine
ssD.
Wing
, NAS
A Lan
gley R
esea
rch Ce
nter,
Hamp
ton, V
A
0930
hrs
AIAA-2
015-3
401
A Pr
elimi
nary
Evalu
ation
of
Supe
rsonic
Tran
spor
t Cat
egor
y Ve
hicle
Oper
ation
s in
the N
ation
al Ai
rspac
e Sys
temM.
Und
erwoo
d, M.
Gum
insky
, NAS
A La
ngley
Rese
arch C
enter
, Ham
pton,
VA
1000
hrs
AIAA-2
015-3
402
Impr
oving
Situ
ation
Awa
rene
ss wi
th
a Tra
ffic M
anag
emen
t Por
tal
A. St
aley,
C. Bo
lczak
, MITR
E Corp
oratio
n, Mc
Lean
, VA
1030
hrs
AIAA-2
015-3
403
Dyna
mic A
irspa
ce Co
nfigu
ratio
n in
SESA
R: bu
ilding
a sm
ooth
and
dyna
mic o
penin
g sch
eme t
hrou
gh
airsp
ace b
uildin
g bloc
ks as
sessm
ent
T. Du
bot,
S. Au
bry, J
. Bed
ouet,
ONE
RA,
Toulo
use,
Franc
e
1100
hrs
AIAA-2
015-3
404
The I
mpac
t of M
itigati
on M
easu
res fo
r Sy
stem
Capa
city C
onstr
aints
on th
e Fu
ture A
ir Tra
nspo
rtatio
n Sys
temN.
Dziku
s, Ge
rman
Aeros
pace
Cente
r (DL
R),
Hamb
urg, G
erman
y; S.
Barto
sch, R
WTH
Aache
n Univ
ersity,
Aache
n, Ge
rman
y; M.
Sc
haefe
r, Fed
eral M
inistry
of Tra
nsport
and
Digita
l Infra
struct
ure, B
onn,
Germ
any
Frida
y, 26
June
201
530
0-AT
IO-2
9UA
S Int
egra
tion
& Op
erat
ions I
IMi
ngCh
aired
by: D
. DEL
AURE
NTIS,
Purdu
e Univ
ersity
0900
hrs
AIAA-2
015-3
405
UAS D
eman
d Gen
erat
ion U
sing
Subje
ct Ma
tter E
xper
t Int
ervie
ws
and S
ocio-
econ
omic
Analy
sisS.
Ayya
lasom
ayaju
la, R.
Sha
rma,
F. W
ielan
d, Int
ellige
nt Au
tomati
on, I
nc.,
Rock
ville,
MD;
A. Tr
ani, N
. Hinz
e, T.
Spen
cer, V
irgini
a Poly
techn
ic Ins
titute
and
State
Univ
ersity
, Blac
ksbu
rg, VA
0930
hrs
AIAA-2
015-3
406
Inve
stiga
tion
of Si
mulat
ed U
AS
Safe
ty In
ciden
ts Us
ing U
AS Sa
fety
An
alysis
Mod
el (U
SAM)
A. Ty
agi, F
. Wiel
and,
Intell
igent
Autom
ation
, Inc
., Ro
ckvil
le, M
D; S
. To
ussa
int, C
ohere
nt Te
chnic
al Se
rvice
s, Inc
., Le
xingto
n Park
, MD;
J. Lu
xhoj,
LCR,
LLC, S
omers
et, N
J
1000
hrs
AIAA-2
015-3
407
RPAS
- AT
M In
tegra
tion
Demo
nstra
tion
- Rea
l-Tim
e Sim
ulatio
n Re
sults
E. Fil
ippon
e, Ita
lian A
erosp
ace R
esea
rch
Cente
r (CIR
A), C
apua
, Ital
y
118
Frida
y, 26
June
201
530
1-CF
D-31
Visua
lizat
ion fo
r CFD
203
0Gr
and B
allro
om A
Chair
ed by
: S. I
MLAY
, Tec
plot,
Inc09
00 hr
sAIA
A-201
5-340
8In
dustr
ial P
ersp
ectiv
es on
Geo
metry
Han
dling
for A
erod
ynam
icsN.
Taylo
r, MBD
A, Br
istol,
Unit
ed Ki
ngdo
m
1000
hrs
AIAA-2
015-3
409
The P
ath to
and S
tate o
f Geo
metry
an
d Mesh
ing in
2030
: Pan
el Su
mmar
yJ.
Chaw
ner, P
ointw
ise, In
c., Fo
rt Wort
h, TX
; J.
Dann
enho
ffer, S
yracus
e Univ
ersity,
Syrac
use,
NY; S
. Dey,
Nav
al Re
search
Labo
ratory
, Wa
shing
ton, D
C; W.
Jone
s, NA
SA La
ngley
Re
search
Cente
r, Ham
pton,
VA; J
. Slot
nick,
The B
oeing
Comp
any,
Hunti
ngton
Beach
, CA;
N. Ta
ylor, M
BDA,
Bristo
l, Unit
ed Ki
ngdo
m
1030
hrs
Pane
lPa
nel: T
he P
ath
to CF
D Vis
ualiz
ation
in 2
030
Mode
rato
r: Sc
ott I
mlay
, Tec
plot,
Inc
S. Im
lay, T
ecplo
t, Inc
., Sn
ohom
ish, W
A; E.
Duqu
e, Int
ellige
nt Lig
ht, Pr
esco
tt, AZ
; K.
Colbu
rn, Co
mputa
tion E
ngine
ering
Inter
natio
nal, I
nc.,
Hous
ton, T
X; G
. Che
n, Un
iversi
ty of
Hous
ton, H
ousto
n, TX
Frida
y, 26
June
201
530
2-CF
D-32
Post-
Proc
essin
g and
Mod
el Re
ducti
onGr
and B
allro
om B
Chair
ed by
: S. S
PEER
, Nort
hrop G
rumma
n Corp
oratio
n09
00 hr
sAIA
A-201
5-341
0EP
IC - A
n Ex
tract
Plug-
In
Comp
onen
ts To
olkit
for I
n-Sit
u Da
ta
Extra
cts A
rchite
cture
E. Du
que,
`. Hie
pler, I
ntellig
ent L
ight,
Ruthe
rford,
NJ;
R. Ha
imes
, Mas
sach
usett
s Ins
titute
of Te
chno
logy,
Camb
ridge
, MA;
C. St
one,
Comp
utatio
nal S
cienc
e and
En
ginee
ring,
LLC, C
hicag
o, IL;
S. G
orrell
, M.
Jone
s, Br
igham
Youn
g Univ
ersity
, Pro
vo, U
T; et
al.
0930
hrs
AIAA-2
015-3
411
Dyna
mic M
ode D
ecom
posit
ion
of B
ackw
ard F
acing
Step
Flow
Sim
ulatio
n Da
taT.
Horch
ler, K
. Man
i, K. H
anne
mann
, Ge
rman
Aeros
pace
Cente
r (DL
R),
Göttin
gen,
Germ
any
1000
hrs
AIAA-2
015-3
412
Statis
tical
Analy
sis an
d Mod
el Re
ducti
on of
Surfa
ce P
ressu
re
for I
nter
actio
n of
a Str
eamw
ise-
Orien
ted Vo
rtex
with
a Wi
ngA.
Moha
n, L.
Agos
tini, D
. Gait
onde
, Oh
io St
ate U
nivers
ity, C
olumb
us, O
H; D
. Ga
rman
n, Air
Force
Rese
arch L
abora
tory,
Wrig
ht-Pa
tterso
n AFB
, OH
Frida
y, 26
June
201
530
3-CF
D-33
Inter
discip
linar
y CFD
IIPlu
m Bl
osso
m A
Chair
ed by
: P. S
LABO
CH an
d D. G
ONZA
LEZ,
Nava
l Surf
ace W
arfare
Cente
r09
00 hr
sAIA
A-201
5-341
3Co
mput
ation
al Stu
dy of
Acti
ve Fl
ow
Cont
rol o
f a Fl
ow-Ex
cited
Helm
holtz
Re
sona
tor
J. Bu
ehn,
P. Sla
boch
, Sain
t Mart
in’s
Unive
rsity,
Lace
y, WA
0930
hrs
AIAA-2
015-3
414
Aero
elasti
c Res
pons
e of R
ocke
t No
zzles
Sube
cted t
o Com
bined
Th
rust
and S
ide Lo
ads
X. Zh
ao, A
labam
a A&M
Univ
ersity
, Hu
ntsvil
le, AL
; S. Z
hang
, ESI
Grou
p, Hu
ntsvil
le, AL
1000
hrs
AIAA-2
015-3
415
Finite
-Time
Lyap
unov
Expo
nent
An
alysis
of In
termi
ttent
Aco
ustic
Ev
ents
in a R
ound
Jet
D. G
onza
lez, N
aval
Surfa
ce W
arfare
Ce
nter, I
ndian
Hea
d, MD
; D. G
aiton
de,
Ohio
State
Univ
ersity
, Colu
mbus
, OH;
M.
Lewi
s, Sc
ience
and T
echn
ology
Policy
Ins
titute,
Was
hingto
n, DC
1030
hrs
AIAA-2
015-3
416
Nume
rical
Simula
tion
of th
e In
terac
tion
betw
een
Rim
Seal
and
Main
Annu
lus Fl
ow in
a Fo
ur St
age
Low-
Pres
sure
Axia
l Tur
bine
Z. We
i tao,
China
Gas
Turbi
ne
Estab
lishme
nt, Ch
engd
u, Ch
ina
1100
hrs
AIAA-2
015-3
417
Calcu
lation
of A
irfoil
Ant
i-icin
g Hea
t Lo
ad in
SLD
Cond
itions
Z. Wa
ng, N
anjin
g Univ
ersity
of Ae
ronau
tics
and A
stron
autic
s, Na
njing
, Chin
a
119
Frida
y, 26
June
201
530
4-CF
D-34
Multip
hase
and N
oneq
uilibr
ium Fl
ows
Cora
lCh
aired
by: C
. TSA
I, Lo
ckhe
ed M
artin
Spac
e Sys
tems a
nd R.
AGAR
WAL,
Wash
ington
Univ
ersity
in S
t Lou
is09
00 hr
sAIA
A-201
5-341
8Nu
meric
al sim
ulatio
n of
a scr
amjet
iso
lator
with
ther
mody
nami
c no
nequ
ilibriu
mR.
Fiéve
t, H.
Koo,
V. Ra
man,
Unive
rsity
of Mi
chiga
n, An
n Arbo
r, Ann
Arbo
r, MI
0930
hrs
AIAA-2
015-3
419
A Mu
ltipha
se an
d Mult
iphys
ics CF
D Te
chniq
ue fo
r Fue
l Spu
rt Pr
edict
ion
with
Cavit
ation
and F
luid-
Struc
ture
In
terac
tion
H. Ya
ng, C
FD Re
searc
h Corp
oratio
n, Hu
ntsvil
le, AL
1000
hrs
AIAA-2
015-3
420
Appli
catio
n of a
Max
imum
-Entro
py-
Based
14-M
omen
t Clos
ure f
or M
ulti-
Dime
nsion
al No
n-Equ
ilibriu
m Flo
wsB.
Tens
uda,
Unive
rsity
of To
ronto,
To
ronto,
Cana
da; J
. McD
onald
, Univ
ersity
of
Ottaw
a, Ot
tawa,
Cana
da; C
. Grot
h, Un
iversi
ty of
Toron
to, To
ronto,
Cana
da
1030
hrs
AIAA-2
015-3
421
An A
LE/F
E for
mulat
ion fo
r high
pr
ecisi
on in
terfa
ce tr
ackin
g in
sepa
rated
mult
iphas
e flow
sA.
Hay,
S. Et
ienne
, D. P
elleti
er, Éc
ole
Polyt
echn
ique d
e Mon
tréal,
Mon
tréal,
Ca
nada
1100
hrs
AIAA-2
015-3
422
Simula
tion
of th
e Sep
arat
ed
flow
over
a Wa
ll-Mo
unted
Hum
p us
ing Fi
nite-
Volum
e Bas
ed La
ttice
Bo
ltzma
nn M
ethod
B. Ya
giz, G
. Guz
el, I.
Koc,
ASEL
SAN,
Inc.,
An
kara,
Turke
y
Frida
y, 26
June
201
530
5-CF
D-35
Over
set a
nd Ca
rtesia
n Gr
id Me
thod
sPlu
m Bl
osso
m B
Chair
ed by
: N. F
OSTE
R, Ap
plied
Rese
arch L
abora
tory -
Penn
Stat
e and
M. G
HORE
YSHI
, Unit
ed S
tates
Air F
orce A
cade
my09
00 hr
sAIA
A-201
5-342
3Th
ree-
Dime
nsion
al Dy
nami
c Ov
erse
t Meth
od fo
r Sta
bilize
d Fin
ite El
emen
tsC.
Liu, J
. New
man,
W. An
derso
n, Un
iversi
ty of
Tenn
essse
, Cha
ttano
oga,
Chatt
anoo
ga, T
N
0930
hrs
AIAA-2
015-3
424
Accu
racy
of H
igh-O
rder
CFD
and
Over
set I
nter
polat
ion in
Finit
e Vo
lume/
Diffe
renc
e Cod
esN.
Foste
r, Pen
nsylv
ania
State
Univ
ersity
, St
ate Co
llege
, PA
1000
hrs
AIAA-2
015-3
425
Adva
nces
in D
istan
ce-B
ased
Hole
Cu
ts on
Ove
rset G
rids
W. Ch
an, S
. Pan
dya,
NASA
Ames
Rese
arch
Cente
r, Moff
ett Fi
eld, C
A
1030
hrs
AIAA-2
015-3
426
Simula
tion
Valid
ation
of St
atic
and
Force
d Mot
ion Fl
ow P
hysic
s of a
Ca
nard
Confi
gure
d Tra
nsCr
uiser
M. G
horey
shi, R
. Kork
is-Kan
aan,
A. Jir
asek
, A. L
oftho
use,
R. Cu
mming
s, U.
S.
Air Fo
rce Ac
adem
y, Co
lorad
o Spri
ngs,
CO
1100
hrs
AIAA-2
015-3
427
Shar
p res
olutio
n of
comp
lex
movin
g geo
metri
es u
sing a
mult
i-cu
t-cell
visco
us fl
ow so
lver
L. Sc
hneid
ers, C
. Gue
nther,
J. G
rimme
n, M.
Mein
ke, W
. Sch
roede
r, RW
TH Aa
chen
Un
iversi
ty, Aa
chen
, Germ
any
1130
hrs
AIAA-2
015-3
428
Integ
ratin
g the
Stan
ford
Univ
ersit
y Un
struc
ture
d Cod
e (SU
2) W
ith
Over
set G
rids
A. Ka
noria
, Ind
ian In
stitut
e of T
echn
ology
Ga
ndhin
agar,
Gan
dhina
gar, I
ndia;
D.
Chan
dar, I
nstitu
te of
High P
erform
ance
Co
mputi
ng, S
ingap
ore, S
ingap
ore
1200
hrs
AIAA-2
015-3
429
A Co
mpar
ative
Stud
y of F
low
arou
nd a
Circu
lar Cy
linde
r usin
g La
ttice
Bolt
zman
n Me
thod
D. H
aman
e, O.
Gue
rri, Re
newa
ble En
ergy
Deve
lopme
nt Ce
nter A
lgeria
, Bou
zarea
h, Alg
eria;
S. La
rbi, P
olytec
hnica
l Sch
ool o
f Alg
iers,
Elhara
che,
Algeri
a
Frida
y, 26
June
201
530
6-CF
D-36
LES,
DNS,
and H
ybrid
RAN
S-LE
S IV
Emer
aldCh
aired
by: J
. POG
GIE,
USAF
AFRL
/RBA
C and
B. T
HORN
BER,
The U
nivers
ity of
Syd
ney
0900
hrs
AIAA-2
015-3
430
Impa
ct of
Comp
utat
ional
Doma
in Siz
e in
Simula
tions
of
Homo
gene
ous D
ecay
ing Tu
rbule
nce
and M
ixing
Laye
rsB.
Thorn
ber, U
nivers
ity of
Syd
ney,
Sydn
ey,
Austr
alia
0930
hrs
AIAA-2
015-3
431
Dire
ct Nu
meric
al Sim
ulatio
n of
Tu
rbule
nt Fl
ow A
roun
d a Su
rface
Mo
unted
Cube
A. Cu
rley,
M. U
ddin,
B. P
eters,
Univ
ersity
of
North
Carol
ina, C
harlo
tte, C
harlo
tte, N
C
1000
hrs
AIAA-2
015-3
432
Supe
rsonic
Corn
er Fl
ow P
redic
tions
us
ing th
e Qua
drat
ic Co
nstit
utive
Re
lation
T. Le
ger, J
. Pog
gie, A
ir Forc
e Res
earch
La
borat
ory, W
right-
Patte
rson A
FB, O
H
1030
hrs
AIAA-2
015-3
433
Asses
smen
t of n
ovel
DES a
ppro
ach
with
enha
nced
SGS m
odell
ing fo
r pr
edict
ion of
sepa
rated
flow
over
a de
lta w
ingM.
Fuchs
, Tech
nical
Unive
rsity o
f Berl
in, Be
rlin,
Germ
any;
C. Mo
ckett,
CFD S
oftwa
re Gm
bH,
Berlin
, Germ
any;
J. Se
sterhe
nn, F.
Thiele
, Tec
hnica
l Univ
ersity
of Be
rlin, B
erlin,
Germ
any
Frida
y, 26
June
201
530
7-MA
O-12
Shap
e and
Topo
logy I
IIMa
drid
Chair
ed by
: B. R
OTH,
Wall
a Wall
a Univ
and S
. CHO
I, Vir
ginia
Polyt
echn
ic Ins
titute
and S
tate U
nivers
ity09
00 hr
sAIA
A-201
5-343
4Ad
joint
-Enha
nced
Mult
i-Lev
el Op
timiza
tion:
Inve
stiga
tion
of
Algo
rithm
Par
amete
r Sett
ings
Y. Te
sfahu
negn
, S. K
oziel
, Rey
kjavik
Un
iversi
ty, Re
ykjav
ik, Ic
eland
; L. L
eifsso
n, Iow
a Stat
e Univ
ersity
, Ame
s, IA
0930
hrs
AIAA-2
015-3
435
Discr
ete A
djoint
Des
ign
Optim
izatio
n Ap
proa
ch fo
r In
creas
ing Tr
anso
nic B
uffe
t Ons
et An
gle-o
f-Atta
ckJ.
Thom
as, E
. Dow
ell, D
uke U
nivers
ity,
Durha
m, N
C
1000
hrs
AIAA-2
015-3
436
Aero
dyna
mic S
hape
Opt
imiza
tion
of a
Truss-
Brac
ed-W
ing A
ircra
ftD.
Ivald
i, N. S
ecco
, S. C
hen,
J. Hw
ang,
J. Ma
rtins,
Unive
rsity
of Mi
chiga
n, An
n Arbo
r, An
n Arbo
r, MI
1030
hrs
AIAA-2
015-3
437
Cons
idera
tions
abou
t Wint
ip De
vices
Des
ign of
Tran
spor
t Ai
rplan
eB.
Matt
os, A
. Pau
la, P.
Koma
tsu,
Tech
nolog
ical In
stitut
e of A
erona
utics
(ITA)
, São
José
dos C
ampo
s, Br
azil
120
Frida
y, 26
June
201
530
8-MA
O-13
Unce
rtaint
y II
Manc
heste
rCh
aired
by: S
. CHO
WDH
URY,
Missi
ssipp
i Stat
e Univ
ersity
and S
. FER
GUSO
N, N
orth C
arolin
a Stat
e Univ
ersity
0900
hrs
AIAA-2
015-3
438
Multi-
Objec
tive O
ptim
izatio
n Un
der
Unce
rtaint
yC.
Liang
, S. M
ahad
evan
, Van
derbi
lt Un
iversi
ty, N
ashv
ille, T
N
0930
hrs
AIAA-2
015-3
439
A Mu
lti-Fid
elity
App
roac
h to
Qu
antifi
catio
n of
Unc
erta
inty i
n Sta
bility
and C
ontro
l Dat
abas
es
for u
se in
Stoc
hasti
c Airc
raft
Simula
tions
A. We
ndorf
f, J.
Alons
o, St
anfor
d Un
iversi
ty, S
tanfor
d, CA
; S. B
ieniaw
ski,
The B
oeing
Comp
any,
Seatt
le, W
A
1000
hrs
AIAA-2
015-3
440
Sculpt
ing: A
Fast,
Inter
activ
e Meth
od
for Pr
obab
ilistic
Desi
gn Sp
ace
Explo
ratio
n and
Mar
gin Al
locati
onR.
Cook
e, Re
source
s for
the Fu
ture,
Washi
ngton
, DC;
T. Za
ng, Z
ang M
&S
Consu
lting,
LLC, Z
ebulo
n, NC
; D. M
avris,
J. Ta
i, Ge
orgia
Institu
te of
Techn
ology,
Atlan
ta, GA
1030
hrs
AIAA-2
015-3
441
Multid
iscipl
inary
Unc
erta
inty
Quan
tifica
tion
in Ae
roela
stic
Analy
ses o
f Sem
i-Spa
n Su
perso
nic
Trans
port
Wing
M. N
ikbay
, P. A
car, I
stanb
ul Te
chnic
al Un
iversi
ty, Is
tanbu
l, Turk
ey
1100
hrs
AIAA-2
015-3
442
An In
tegra
ted Fr
amew
ork
for B
ayes
ian U
ncer
taint
y Qu
antifi
catio
n an
d Pro
babil
istic
Multi-
Crite
ria D
ecisi
on M
aking
in
Aero
-Engin
e Pre
limina
ry D
esign
J. Gr
amaty
ka, M
. Eres
, J. S
canla
n, Un
iversi
ty of
South
ampto
n, So
utham
pton,
Unite
d King
dom;
M. M
oss,
R. Ba
tes, R
olls-
Royc
e Grou
p plc,
Derb
y, Un
ited K
ingdo
m
1130
hrs
AIAA-2
015-3
443
A Str
ateg
y for
Pro
babil
istic
Marg
in Al
locat
ion in
Airc
raft
Conc
eptu
al De
sign
T. Za
ng, Z
ang M
&S Co
nsult
ing, L
LC,
Zebu
lon, N
C; S.
Mah
adev
an, V
ande
rbilt
Unive
rsity,
Nas
hville
, TN;
J. Ta
i, D.
Mavri
s, Ge
orgia
Institu
te of
Tech
nolog
y, Atl
anta,
GA
Frida
y, 26
June
201
530
9-NW
-10
0900
- 09
30 h
rsNe
twor
king C
offe
e Bre
akMe
eting
Roo
m Fo
yers
Auth
or/S
essio
n Ch
air In
dex
A. da
Silv
a, R.,
9-AF
M-2
Abde
lhady
, M.,
43-AF
M-3
Abde
llatif,
O.,
178-M
ST-8
Abdo
l-Ham
id, K.
, 160
-APA-1
7, 2
33-AP
A-25
Abdra
shito
v, R.,
226
-AA-31
Abdu
l-Lati
f, A.,
12-A
PA-1
Abe,
M., 2
3-CFD
-3Ab
e, T.,
144
-PDL-7
Abe,
Y., 1
30-CF
D-13
Acar,
E., 6
4-MAO
-2Ac
ar, P.
, 308
-MAO
-13Ad
ams,
N., 8
7-APA
-9Ad
ler, M
., 24
5-CFD
-30Ad
usum
illi, S
., 15
9-AMT
-10/G
T-10
Afsar,
M.,
79-AA
-13, 2
09-FD
-24Ag
arwal,
N.,
226-A
A-31
Agarw
al, R.
, 26-F
D-2, 4
7-APA
-5, 1
22-AP
A-13,
1
39-FD
-18, 1
82-TP
-9, 2
11-FD
-26, 3
04-CF
D-34
Agbo
losu-A
miso
n, S.
, 197
-ATIO
-18Ag
ostin
i, L.,
80-AA
-14, 3
02-CF
D-32
Ahma
d, N.
, 163
-ASE-1
, 237
-ASE-3
, 272
-ASE-4
, 2
98-AT
IO-27
Ahme
d, N.
, 115
-AA-19
Ahsa
n, N.
, 136
-FD-15
Ahuja
, K.,
189-A
A-30,
261
-AA-39
Ahuja
, V.,
127-A
TIO-13
, 161
-APA-1
8Aig
ner, M
., 18
5-AA-2
6
Airiau
, C.,
5-AA-3
Akay
din, H
., 49
-APA-7
Akba
rzade
h, S.
, 131
-CFD-1
4Ak
ella,
M., 9
-AFM-
2Ak
htar, I
., 13
3-CFD
-16, 1
36-FD
-15Ak
illi, H
., 25
-FD-1
Akins
, D.,
279-F
D-31
Alaou
i, M.,
226-A
A-31
Alaza
rd, D
., 83
-AFM-
5Alb
a, C.,
34-T
P-1Alb
ring,
T., 2
52-M
AO-9,
283
-MAO
-10Alb
uque
rque,
P., 1
04-M
AO-3
Alcab
in, M
., 27
5-ATIO
-25Alc
orn, J
., 25
0-LTA
-1Ale
ksen
tsev,
A., 1
89-AA
-30Ale
ssand
ro, T.
, 108
-TP-5
Alexa
nder,
W.,
37-AA
-6, 3
8-AA-7
, 114
-AA-18
, 1
52-AA
-22, 1
87-AA
-28, 2
60-AA
-38, 2
61-AA
-39Ale
xeen
ko, A
., 35
-TP-2,
288
-TP-13
Alexe
ev, T
., 9-A
FM-2,
105
-MST
-5Alf
onso
, X.,
234-A
PA-26
Algoz
ino, S
., 23
6-APA
-28Ali
aga,
C., 1
96-AS
E-2Ali
zard,
F., 9
8-CFD
-12All
en, B
., 16
5-ATIO
-16, 1
99-AT
IO-20
Allen
, C.,
64-M
AO-2,
125
-APA-1
6, 2
83-M
AO-10
Allen
, J.,
104-M
AO-3
Allen
, N.,
45-AM
T-3/G
T-3All
erdice
, J.,
197-A
TIO-18
Alliso
n, D.
, 104
-MAO
-3All
maras
, S.,
95-CF
D-9, 1
23-AP
A-14,
170
-CFD-1
8Alm
eida,
F., 2
49-FT
-1Alm
ond,
M., 8
8-APA
-10Alo
nso,
E., 1
26-AT
IO-12
Alons
o, J.,
202
-CFD-2
2, 2
04-CF
D-24,
212
-MAO
-6,
283
-MAO
-10, 2
84-M
AO-11
, 308
-MAO
-13Alo
nso-M
iralle
s, J.,
260
-AA-38
AlQad
i, I.,
236-A
PA-28
Alter,
S.,
233-A
PA-25
Altmi
kus,
A., 8
8-APA
-10Alu
nni, A
., 21
6-TP-1
0/PD
L-10
Alves
, L.,
243-C
FD-28
Aly, A
., 17
8-MST
-8Aly
anak
, E.,
104-M
AO-3,
176
-MAO
-5Alz
amora
Prev
itali,
F., 1
02-FD
-13Am
adori
, K.,
283-M
AO-10
Amara
l, F.,
230-A
A-35
Amili,
O.,
153-A
A-23
Amita
y, M.
, 63-F
D-9, 1
01-FD
-12, 2
48-FD
-29Am
os, D
., 35
-TP-2
Amun
dson
, I.,
128-A
TIO-14
Anan
da Kr
ishna
n, G.
, 15-A
PA-4
Anda
libi, M
., 48
-APA-6
Ande
rs, S
., 49
-APA-7
, 281
-GEPC
-1
Ande
rson,
J., 2
31-AA
-36An
derso
n, W.
, 95-C
FD-9,
170
-CFD-1
8, 3
05-CF
D-35
Andre
, F.,
65-M
ST-3
Andre
ws, S
., 14
1-MAO
-4, 2
67-AP
A-29
Andri
enko
, D.,
69-TP
-4, 2
56-TP
-12An
emaa
t, W.
, 117
-ACD-3
, 232
-ACD-6
Angla
nd, D
., 20
5-CFD
-25, 2
59-AA
-37, 2
63-AA
-41An
saldi
, T.,
5-AA-3
Antho
ny, J
., 27
8-FD-3
0An
tônio
dos S
antos
, D.,
30-M
ST-1
Anton
y, T.,
44-A
FM-4
Anup
indi, K
., 17
1-CFD
-19Ao
ki, T.
, 68-T
P-3Ao
ki, Y.
, 89-A
PA-11
Aono
, H.,
268-A
PA-30
Apon
so, B
., 91
-ATIO
-9Ap
pel, C
., 22
6-AA-3
1Ap
pelba
um, J
., 25
9-AA-3
7Ara
dag,
S., 2
04-CF
D-24
Arena
, A.,
157-A
FM-9
Arina
, R.,
155-A
A-25
Arnal,
D.,
99-FD
-10Arn
dt, C.
, 266
-AMT-1
3/GT
-13Arn
eson
, H.,
18-AT
IO-3,
298
-ATIO
-27Aro
ra, N
., 97
-CFD-1
1, 2
48-FD
-29, 2
68-AP
A-30
Arsen
yev,
I., 2
84-M
AO-11
Aru
najat
esan
, S.,
139-F
D-18,
175
-FD-22
, 229
-AA-34
Asad
a, K.,
60-F
D-6/P
DL-2
Asan
o, K.,
60-F
D-6/P
DL-2
Ashle
y, A.,
176
-MAO
-5As
hton,
N., 1
72-CF
D-20,
230
-AA-35
Astle
y, R.,
78-A
A-12
Atassi
, H.,
77-AA
-11, 1
51-AA
-21Ati
nault
, O.,
13-AP
A-2Atk
ins, E
., 27
4-ATIO
-24Atk
ins, S
., 14
0-ITA
R-2Att
anas
io, L.
, 13-A
PA-2,
104
-MAO
-3Au
bert,
A., 4
0-AA-9
Aubry
, S.,
42-AC
D-1, 2
99-AT
IO-28
Avery
, A.,
196-A
SE-2
Awas
thi, M
., 26
1-AA-3
9Ay
ton, L
., 26
0-AA-3
8Ay
yad,
E., 3
1-MST
-2Ay
yalas
omay
ajula,
S.,
284-M
AO-11
, 300
-ATIO
-29Az
arm, S
., 29
-MAO
-1Az
arpey
vand
, M.,
3-AA-1
, 38-A
A-7Az
eved
o, J.,
12-A
PA-1,
98-C
FD-12
, 241
-CFD-2
6,
270
-APA-3
2Ba
bbar,
Y., 9
-AFM-
2, 1
24-AP
A-15,
270
-APA-3
2Ba
ccala,
L., 7
-AA-5
Badri
nath,
S.,
136-F
D-15
Baed
er, J.
, 162
-APA-1
9, 1
71-CF
D-19
Bagin
ski, F
., 20
0-BAL
-2Ba
gwell
, T.,
140-I
TAR-2
121
Auth
or/S
essio
n Ch
air In
dex
Bahr,
C., 1
86-AA
-27, 1
88-AA
-29, 2
62-AA
-40Ba
i, B.,
112-A
A-16
Bai, J
., 49
-APA-7
, 145
-TP-7
Bailly
, C.,
4-AA-2
, 114
-AA-18
, 231
-AA-36
Bailly
, D.,
161-A
PA-18
Bake
, F.,
41-AA
-10, 1
51-AA
-21Ba
kker,
B.,
238-A
TIO-21
Balak
umar,
P., 6
1-FD-7
, 139
-FD-18
, 248
-FD-29
Balan
, A.,
95-CF
D-9Ba
lares
que,
N., 8
8-APA
-10Ba
las, G
., 15
7-AFM
-9Ba
lboni,
J., 1
08-TP
-5, 2
16-TP
-10/P
DL-10
Balda
cchino
, D.,
279-F
D-31
Balla
rd, B
., 27
5-ATIO
-25Ba
ne, S
., 25
5-PDL
-12Ba
ngert
, L.,
14-AP
A-3Ba
rbarin
o, M.
, 6-AA
-4, 1
15-AA
-19Ba
rbeau
, Z.,
274-A
TIO-24
Barm
ore, B
., 29
8-ATIO
-27Ba
rnes,
C., 2
70-AP
A-32
Barne
s, J.,
83-A
FM-5
Barte
ls, R.
, 124
-APA-1
5Ba
rtoli,
N., 8
2-ACD
-2Ba
rtosch
, S.,
299-A
TIO-28
Basti
de, M
., 45
-AMT-3
/GT-3
Basto
, K.,
234-A
PA-26
Bates
, R.,
308-M
AO-13
Bathe
l, B.,
86-AM
T-6/G
T-6,
121
-AMT-8
/FD-1
4/TP
-6/GT
-8Ba
tista,
M.,
30-M
ST-1
Batte
n, P.,
245
-CFD-3
0Ba
uer, M
., 12
5-APA
-16Ba
uman
, P.,
108-T
P-5Ba
umgä
rtner,
D.,
283-M
AO-10
Bayd
ar, E.
, 279
-FD-31
Bayo
da, K
., 33
-PDL-1
/FD-5
Beav
erstoc
k, C.,
29-M
AO-1
Beck
, J.,
35-TP
-2Be
doue
t, J.,
299
-ATIO
-28Be
kirop
oulos
, D.,
155-A
A-25
Belle
mans
, A.,
216-T
P-10/
PDL-1
0Be
lley,
C., 2
04-CF
D-24
Belm
ouss,
M.,
255-P
DL-12
Belya
ev, I
., 11
5-AA-1
9, 1
87-AA
-28, 1
89-AA
-30Be
nard,
N.,
33-PD
L-1/F
D-5, 1
80-PD
L-8/A
PA-20
Bend
er, J.
, 256
-TP-12
Benn
aceu
r, I.,
154-A
A-24
Bento
n, S.
, 50-A
PA-8
Berci
, M.,
236-A
PA-28
Berda
nier, R
., 17
3-FD-1
9Be
resh,
S., 62
-FD-8,
175-F
D-22,
192-A
MT-12
/GT-1
2,
266
-AMT-1
3/GT
-13
Berge
ron, K
., 23
6-APA
-28Be
ring,
E., 2
00-BA
L-2Bé
riot,
H., 2
63-AA
-41Be
rkefel
d, T.,
186
-AA-27
, 260
-AA-38
Berna
rdini,
G.,
162-A
PA-19
, 263
-AA-41
Berna
rdo, J
., 52
-ATIO
-6, 1
98-AT
IO-19
Berne
r, C.,
47-AP
A-5Be
rry, P
., 28
3-MAO
-10Be
rry, S
., 21
7-TP-1
1Be
rsene
v, Y.,
189
-AA-30
Berto
n, J.,
77-A
A-11
Beulz
e, B.
, 92-A
TIO-10
Beuz
e, B.
, 18-A
TIO-3
Beva
n, R.,
125
-APA-1
6Be
virt,
J., 2
76-AT
IO-26
Bhag
at, N
., 10
4-MAO
-3Bh
agwa
ndin,
V., 2
67-AP
A-29
Bham
idipa
ti, K.,
22-C
FD-2
Bhau
mik,
S., 2
05-CF
D-25
Bianc
hi, D
., 12
8-ATIO
-14Bib
ik, P.
, 280
-FT-2/
GT-14
Bidino
, D.,
45-AM
T-3/G
T-3Bie
nert,
N.,
51-AT
IO-5
Bienia
wski,
S.,
308-M
AO-13
Bienie
k, D.
, 237
-ASE-3
Bier, N
., 10
5-MST
-5Bij
l, H.,
97-CF
D-11
Bil, C
., 42
-ACD-1
, 117
-ACD-3
, 190
-ACD-5
Bilim
oria,
K., 1
77-M
ST-7
Bin Ab
dul M
alik,
M., 1
62-AP
A-19
Bisek
, N.,
98-CF
D-12,
143
-PDL-6
, 245
-CFD-3
0Bla
ckwe
ll, B.
, 68-T
P-3Bla
ir, L.,
143
-PDL-6
Blaisd
ell, G
., 11
3-AA-1
7, 1
39-FD
-18, 2
45-CF
D-30
Blake
, M.,
142-M
ST-6
Blake
, W.,
8-AFM
-1, 2
9-MAO
-1, 2
73-AS
E-5Bla
ndea
u, V.,
77-A
A-11
Bleisc
hwitz
, R.,
136-F
D-15
Bletzi
nger,
K., 2
83-M
AO-10
Bloeb
aum,
C., 2
12-M
AO-6
Blom,
H.,
238-A
TIO-21
Bo, Y
., 35
-TP-2,
145
-TP-7
Bobe
nrieth
Mise
rda, R
., 77
-AA-11
Boco
la, F.
, 84-A
FM-6
Bode
n, F.,
231
-AA-36
Bode
n, H.
, 7-AA
-5, 2
61-AA
-39Bo
gdan
off, D
., 18
2-TP-9
Boge
y, C.,
4-AA
-2, 5
-AA-3,
229
-AA-34
Boiss
onne
au, F
., 18
9-AA-3
0Bo
lczak
, C.,
299-A
TIO-28
Bolds
-Moo
rehea
d, P.,
249
-FT-1
Bolen
der, M
., 44
-AFM-
4
Bomb
elli, A
., 27
5-ATIO
-25Bo
nnet,
J., 1
80-PD
L-8/A
PA-20
Bons
, J.,
50-AP
A-8Bo
o, K.,
12-A
PA-1
Boom
, P.,
132-C
FD-15
Borde
neuv
e, J.,
83-A
FM-5
Borer
, N.,
127-A
TIO-13
Borg,
M.,
137-F
D-16
Borge
s Seb
astia
o, I.,
288
-TP-13
Borgo
ltz, A
., 29
5-APA
-34, 2
97-AP
A-37
Borne
r, A.,
288-T
P-13
Bosso
n, C.,
16-A
TIO-1
Botez
, R., 1
3-APA
-2, 18
-ATIO-
3, 66
-MST
-4, 84
-AFM-
6,
92-A
TIO-10
, 238
-ATIO
-21, 2
96-AP
A-35
Bouh
aj, M
., 22
6-AA-3
1Bo
uley,
S., 1
52-AA
-22Bo
usfie
ld, S
., 12
7-ATIO
-13Bo
ussu
ge, J
., 18
8-AA-2
9Bo
uty, E
., 18
5-AA-2
6Bo
uvy,
Q., 2
59-AA
-37Bo
va, S
., 20
2-CFD
-22Bo
wers,
L., 1
66-AT
IO-17
, 239
-ATIO
-22Bo
wn, A
., 16
7-BAL
-1Bo
xx, I
., 26
6-AMT
-13/G
T-13
Boyd
, I.,
35-TP
-2, 6
9-TP-4
, 256
-TP-12
Brak
ke, K
., 20
0-BAL
-2Br
amble
y, E.,
7-AA
-5, 8
1-AA-1
5Br
andis
, A.,
69-TP
-4, 2
17-TP
-11Br
ando
n, J.,
118
-AFM-
7, 2
49-FT
-1Br
andt,
S.,
64-M
AO-2
Brau
ckma
nn, G
., 23
3-APA
-25Br
aud,
P., 1
89-AA
-30Br
azier
, J.,
228-A
A-33
Brea
rd, C.
, 4-AA
-2, 6
-AA-4
Breh
m, C.
, 4-AA
-2Br
eitsa
mter,
C., 8
7-APA
-9Br
ès, G
., 5-A
A-3, 8
0-AA-1
4Br
evigl
ieri, C
., 24
1-CFD
-26Br
ichet,
G.,
4-AA-2
Bridg
es, J
., 18
9-AA-3
0, 2
27-AA
-32Br
iley,
W., 1
5-APA
-4, 2
97-AP
A-37
Britc
hford,
K., 2
27-AA
-32Br
oeren
, A.,
196-A
SE-2
Bron
z, M.
, 161
-APA-1
8Br
osza
t, D.
, 151
-AA-21
Brow
n, C.,
189
-AA-30
, 228
-AA-33
, 280
-FT-2/
GT-14
Brow
n, K.,
297
-APA-3
7Br
own,
L., 1
58-AM
T-9/G
T-9Br
own,
M., 1
43-PD
L-6, 2
14-M
ST-9
Brow
n, R.,
9-AF
M-2
Brun
et, M
., 42
-ACD-1
Brya
n, B.
, 261
-AA-39
Bueh
n, J.,
303
-CFD-3
3Bu
geda
, G.,
180-P
DL-8/
APA-2
0Bu
lte, J
., 3-A
A-1, 2
61-AA
-39, 2
62-AA
-40Bu
nge,
R., 8
-AFM-
1, 2
49-FT
-1Bu
ning,
P., 2
30-AA
-35Bu
ono,
A., 3
7-AA-6
Burns
, R.,
86-AM
T-6/G
T-6Bu
rnside
, N.,
186-A
A-27
Burt,
J., 6
9-TP-4
, 181
-PDL-9
/TP-8
Burtc
h, T.,
8-AF
M-1
Busch
, G.,
37-AA
-6Bu
sque
ts, J.
, 126
-ATIO
-12Bu
ttini, T
., 9-A
FM-2
Byerl
ey, A
., 15
-APA-4
Bynu
m, M
., 99
-FD-10
Cai, J
., 67
-PDL-3
, 178
-MST
-8Ca
i, W.,
145-T
P-7Ca
in, A.
, 88-A
PA-10
, 143
-PDL-6
, 255
-PDL-1
2Ca
ldas,
L., 7
-AA-5
Calla
han,
R., 2
94-AM
T-14/
GT-15
Calle
nder,
M.,
62-FD
-8Ca
llicoa
t, J.,
231
-AA-36
Calve
rt, M
., 15
-APA-4
, 194
-APA-2
2Ca
lvert,
N.,
86-AM
T-6/G
T-6Ca
mpbe
ll, S.
, 16-A
TIO-1,
298
-ATIO
-27Ca
ndler
, G.,
139-F
D-18,
202
-CFD-2
2, 2
44-CF
D-29,
2
46-FD
-27, 2
56-TP
-12, 2
78-FD
-30Ca
nfield
, R.,
252-M
AO-9
Canp
olat,
C., 2
5-FD-1
Cantu
, L.,
86-AM
T-6/G
T-6Ca
pittin
i, G.,
236-A
PA-28
Capiz
zano
, F.,
6-AA-4
, 115
-AA-19
Capre
cci, M
., 5-A
A-3Ca
raball
o, E.,
175
-FD-22
Carae
ni, M
., 39
-AA-8
Cardi
to, F.
, 162
-APA-1
9Ca
riou,
J., 2
72-AS
E-4Ca
rlson
, J.,
58-CF
D-8, 1
33-CF
D-16
Carm
ine, M
., 26
-FD-2
Caro,
S.,
6-AA-4
, 113
-AA-17
Carol
us, T
., 15
2-AA-2
2Ca
rranz
a Moy
ao, O
., 84
-AFM-
6Ca
rroll,
D., 1
07-PD
L-4, 1
66-AT
IO-17
Carso
n, H.
, 170
-CFD-1
8Ca
rter, C
., 26
6-AMT
-13/G
T-13
Cartm
ell, D
., 31
-MST
-2Ca
ruelle
, B.,
155-A
A-25
Casa
lino,
D., 1
88-AA
-29, 2
59-AA
-37Ca
salis,
G.,
228-A
A-33
Casa
rtelli,
E., 2
03-CF
D-23
Casp
er, K.
, 28-F
D-4, 1
03-IT
AR-1,
140
-ITAR
-2,
175
-FD-22
Castn
er, R.
, 14-A
PA-3
Cathe
y, H.
, 167
-BAL-1
Catle
tt, M
., 23
1-AA-3
6Ca
ttafes
ta, L.
, 248
-FD-29
Caud
le, D
., 83
-AFM-
5Ca
valie
ri, A.,
5-AA
-3, 41
-AA-10
, 80-A
A-14,
189-A
A-30,
2
60-AA
-38Ce
dric,
C., 1
32-CF
D-15
Cerm
inara,
A., 2
09-FD
-24Ce
snik,
C., 9
-AFM-
2, 1
19-AF
M-8
Cetin
, M.,
80-AA
-14Ch
abot,
J., 1
75-FD
-22Ch
aderj
ian, N
., 13
6-FD-1
5Ch
akrab
orty,
I., 4
2-ACD
-1, 1
56-AC
D-4, 2
65-AC
D-7Ch
akrab
orty,
P., 2
46-FD
-27Ch
akrav
arthy
, S.,
245-C
FD-30
Chalo
t, F.,
99-F
D-10
Chan
, W.,
305-C
FD-35
Chan
dar, D
., 30
5-CFD
-35Ch
aney
, V.,
249-F
T-1Ch
ang,
C., 1
93-AP
A-21,
211
-FD-26
, 228
-AA-33
Chan
g, S.
, 35-T
P-2, 1
45-TP
-7Ch
ao, H
., 43
-AFM-
3Ch
ao, T
., 11
9-AFM
-8Ch
aput,
A., 8
2-ACD
-2, 1
28-AT
IO-14
Chard
, J.,
271-A
PA-33
Charn
igo, R
., 18
1-PDL
-9/TP
-8Ch
atterj
i, G.,
142-M
ST-6,
253
-MST
-11Ch
auvin
, A.,
227-A
A-32
Chaw
ner, J
., 30
1-CFD
-31Ch
azot,
O.,
108-T
P-5Ch
edev
ergne
, F.,
60-FD
-6/PD
L-2Ch
eli, R
., 26
-FD-2
Cheli
us, A
., 18
7-AA-2
8Ch
elliah
, K.,
262-A
A-40
Chen
, G.,
301-C
FD-31
Chen
, L.,
191-A
MT-11
/GT-1
1, 2
50-LT
A-1Ch
en, N
., 92
-ATIO
-10, 1
91-AM
T-11/
GT-11
Chen
, P.,
284-M
AO-11
Chen
, S.,
269-A
PA-31
, 307
-MAO
-12Ch
en, W
., 10
7-PDL
-4, 1
51-AA
-21, 2
60-AA
-38Ch
en, X
., 11
2-AA-1
6, 1
45-TP
-7Ch
en, Y
., 34
-TP-1
Chen
g, G.
, 193
-APA-2
1, 2
11-FD
-26Ch
eng,
H., 2
29-AA
-34Ch
eng,
J., 1
22-AP
A-13
Chen
g, Y.,
215
-MST
-10Ch
ernys
hev,
S., 2
28-AA
-33Ch
evall
ey, E
., 51
-ATIO
-5Ch
habra
, R.,
29-M
AO-1
Chiba
, K.,
293-A
CD-8
Chier
eghin
, N.,
270-A
PA-32
122
Auth
or/S
essio
n Ch
air In
dex
Chint
agun
ta, A.
, 80-A
A-14
Chng
, S.,
162-A
PA-19
Chng
, T.,
143-P
DL-6
Cho,
K., 2
35-AP
A-27
Choi,
J., 2
7-FD-3
, 55-C
FD-5,
62-F
D-8, 1
32-CF
D-15,
1
33-CF
D-16,
251
-MAO
-8, 2
96-AP
A-35
Choi,
S., 1
2-APA
-1, 64
-MAO
-2, 89
-APA-1
1, 13
2-CFD
-15,
251
-MAO
-8, 2
96-AP
A-35,
307
-MAO
-12Ch
ong,
T., 3
-AA-1
Chou
, A.,
209-F
D-24
Chou
dhari
, M.,
56-CF
D-6, 9
9-FD-1
0, 1
37-FD
-16,
155
-AA-25
, 230
-AA-35
Chou
dhary
, A.,
97-CF
D-11
Chou
tapall
i, I.,
276-A
TIO-26
Chow
dhary
, G.,
274-A
TIO-24
Chow
dhury
, S., 1
76-M
AO-5,
213-M
AO-7,
251-M
AO-8,
3
08-M
AO-13
Chris
tophe
, J.,
79-AA
-13, 1
12-AA
-16Ch
ua, Z
., 65
-MST
-3Ch
udob
a, B.
, 53-A
TIO-7
Chue
, R.,
269-A
PA-31
Chwa
lowsk
i, P.,
124-A
PA-15
Chyn
oweth
, B.,
28-FD
-4Cia
rella,
A., 2
9-MAO
-1Cil
iberti,
D.,
13-AP
A-2Cin
nella
, P.,
62-FD
-8, 1
13-AA
-17, 1
32-CF
D-15
Cioba
ca, V
., 12
5-APA
-16Cis
neros
, E.,
216-T
P-10/
PDL-1
0Cis
otto,
A., 4
6-AMT
-4/GT
-4Civ
inska
s, K.,
281
-GEPC
-1Cla
ir, V.,
6-AA
-4, 1
13-AA
-17Cla
rk, A.
, 276
-ATIO
-26Cla
rk, I.
, 38-A
A-7Cla
rke, S
., 24
0-ATIO
-23Cle
mens
, N.,
33-PD
L-1/F
D-5, 1
74-FD
-20Clé
ro, F.
, 185
-AA-26
Cliff,
S.,
89-AP
A-11
Cling
man,
D., 6
3-FD-9
Close
, S.,
286-P
DL-13
Clouti
er, R.
, 239
-ATIO
-22Clu
ts, J.
, 153
-AA-23
Coak
ley, T
., 17
2-CFD
-20Co
bb, P
., 14
2-MST
-6Co
bb, R
., 14
1-MAO
-4, 1
58-AM
T-9/G
T-9Co
der, J
., 58
-CFD-8
, 61-F
D-7Co
en, P
., 28
1-GEP
C-1Co
etzee
, E.,
105-M
ST-5
Cofer
, A.,
35-TP
-2Co
ggon
, S.,
213-M
AO-7
Cohe
n, E.,
226
-AA-31
Colan
tonio,
R., 2
81-GE
PC-1
Colbu
rn, K.
, 301
-CFD-3
1
Cole,
S.,
45-AM
T-3/G
T-3Co
llery,
O.,
226-A
A-31
Collin
s, E.,
41-A
A-10,
81-A
A-15
Colm
enare
s, J.,
96-C
FD-10
, 205
-CFD-2
5Co
loe, B
., 27
4-ATIO
-24Co
lonius
, T.,
5-AA-3
, 80-A
A-14,
228
-AA-33
Colon
no, M
., 21
2-MAO
-6Co
mmo,
S., 1
20-AM
T-7/G
T-7, 2
94-AM
T-14/
GT-15
Comm
unier
, D.,
84-AF
M-6
Cons
tantin
escu
, E.,
163-A
SE-1
Cook
e, R.,
308
-MAO
-13Co
ppen
barge
r, R.,
91-AT
IO-9
Corde
s, U.
, 50-A
PA-8,
271
-APA-3
3Co
reixa
s, C.,
188
-AA-29
Corre
ale, G
., 33
-PDL-1
/FD-5
, 60-F
D-6/P
DL-2
Corre
ia Gr
ácio,
B.,
31-M
ST-2
Corrig
an, A
., 15
3-AA-2
3Co
stes,
M., 1
61-AP
A-18
Cotto
n, W.
, 275
-ATIO
-25Co
ulouv
rat, F
., 11
4-AA-1
8Co
upe,
J., 9
1-ATIO
-9, 1
98-AT
IO-19
Coup
land,
J., 7
8-AA-1
2, 2
64-AA
-42Co
urty,
J., 9
9-FD-1
0Co
usy,
M., 6
5-MST
-3Co
yle, C
., 90
-APA-1
2, 1
95-AP
A-23
Cozz
i, F.,
26-FD
-2Cra
ig, S
., 13
7-FD-1
6Cra
nford,
J., 3
0-MST
-1Cra
wford
, B.,
137-F
D-16
Crawl
ey, M
., 15
3-AA-2
3Cro
mer, K
., 28
2-LTA
-2Cro
ss, C.
, 165
-ATIO
-16, 1
99-AT
IO-20
Crossl
ey, W
., 52
-ATIO
-6, 8
2-ACD
-2Cro
uch,
J., 6
1-FD-7
Crow,
B.,
197-A
TIO-18
Crowt
her, W
., 30
-MST
-1, 2
71-AP
A-33
Crude
n, B.
, 69-T
P-4, 1
82-TP
-9, 2
17-TP
-11Cru
z, E.,
63-F
D-9Cu
enca
, R.,
7-AA-5
Cui, D
., 17
8-MST
-8Cu
i, H.,
44-AF
M-4
Cui, K
., 29
6-APA
-35Cu
lbreth
, W.,
31-M
ST-2
Cumm
ings,
R., 6
3-FD-9
, 160
-APA-1
7, 2
36-AP
A-28,
2
78-FD
-30, 3
05-CF
D-35
Cunh
a, G.
, 155
-AA-25
Cunh
a, M.
, 282
-LTA-2
Cuoc
i, A.,
244-C
FD-29
Curle
y, A.,
306
-CFD-3
6Cu
rran,
R., 5
1-ATIO
-5, 9
1-ATIO
-9, 1
98-AT
IO-19
, 2
75-AT
IO-25
Cusa
ti, V.,
13-A
PA-2
Cutle
r, A.,
86-AM
T-6/G
T-6,
121
-AMT-8
/FD-1
4/TP
-6/GT
-8Cy
mbali
st, N
., 27
-FD-3,
278
-FD-30
D’So
uza,
S., 4
3-AFM
-3Da
Ronc
h, A.,
9-AF
M-2,
84-A
FM-6
da S
ilva,
A., 4
-AA-2
da S
ilva,
F., 4
-AA-2
Dahl,
D.,
39-AA
-8Da
hl, M
., 78
-AA-12
Dale,
G.,
26-FD
-2, 2
10-FD
-25Da
lle, D
., 23
3-APA
-25Da
ly, C.
, 38-A
A-7Da
moda
ran, M
., 20
5-CFD
-25, 2
35-AP
A-27,
250
-LTA-1
Danc
ila, B
., 92
-ATIO
-10Da
ncila
, R.,
18-AT
IO-3
Dane
hy, P
., 86
-AMT-6
/GT-6
, 1
21-AM
T-8/F
D-14/
TP-6/
GT-8
Danie
ls, C.
, 273
-ASE-5
Dann
enho
ffer, J
., 30
1-CFD
-31Da
ntske
r, O.,
87-AP
A-9Da
oud,
F., 2
12-M
AO-6
Darm
ofal, D
., 95
-CFD-9
, 170
-CFD-1
8Da
skira
n, O.
, 128
-ATIO
-14Da
vidso
n, L.,
6-AA
-4, 1
15-AA
-19, 1
54-AA
-24Da
viller
, G.,
229-A
A-34
Davis
, D.,
85-AM
T-5/G
T-5Da
vis, R
., 20
3-CFD
-23Da
vy, R
., 3-A
A-1, 2
62-AA
-40Da
wson
, R.,
174-F
D-20
Daws
on, S
., 13
6-FD-1
5De
Breu
ker, R
., 29
-MAO
-1de
Jong
, A.,
38-AA
-7De
Kat,
R., 1
36-FD
-15De
La Pu
ente,
F., 2
59-AA
-37De
Marc
o, A.,
8-AF
M-1,
104
-MAO
-3de
Mon
te, F.
, 35-T
P-2de
Oliv
eira,
G., 2
86-PD
L-13
De Ro
eck,
W., 1
13-AA
-17de
San
tana,
L., 3
-AA-1
de S
ouza
, F.,
192-A
MT-12
/GT-1
2De
Armon
, J.,
197-A
TIO-18
DeBo
nis, J
., 55
-CFD-5
, 130
-CFD-1
3, 1
75-FD
-22De
Chan
t, L.,
139
-FD-18
DeCic
co, A
., 65
-MST
-3, 1
42-M
ST-6
Deck
er, R.
, 278
-FD-30
Dedic
, C.,
181-P
DL-9/
TP-8
Dees
, J.,
173-F
D-19
Dees
e, J.,
282
-LTA-2
DeGe
nnaro
, A.,
295-A
PA-34
Degre
z, G.
, 216
-TP-10
/PDL
-10De
inert,
S.,
212-M
AO-6
Del R
ey Fe
rnánd
ez, D
., 16
9-CFD
-17, 2
42-CF
D-27
Del R
osari
o, R.,
281
-GEPC
-1De
Laure
ntis,
D., 5
2-ATIO
-6, 23
9-ATIO
-22, 3
00-AT
IO-29
Deleg
lise, B
., 46
-AMT-4
/GT-4
Delfs
, J.,
79-AA
-13, 1
12-AA
-16, 2
30-AA
-35,
231
-AA-36
, 263
-AA-41
Delisi
, D.,
237-A
SE-3,
272
-ASE-4
Dell’O
rso, H
., 10
1-FD-1
2, 2
48-FD
-29De
lla Ve
cchia,
P., 8
-AFM-
1, 1
3-APA
-2De
llery,
B.,
167-B
AL-1
Delne
ro, J.
, 236
-APA-2
8De
mauro
, E.,
101-F
D-12
Deme
autis
, C.,
45-AM
T-3/G
T-3De
mers,
F., 6
0-FD-6
/PDL
-2De
mers
Bouc
hard,
E., 2
76-AT
IO-26
Deng
, S.,
97-CF
D-11
Denia
u, H.
, 229
-AA-34
Denie
ul, Y.
, 83-A
FM-5
Denis
on, M
., 24
8-FD-2
9De
nisov
, S.,
115-A
A-19
Denis
sen,
K., 1
95-AP
A-23
Denn
is, B
., 48
-APA-6
Deod
har, N
., 28
2-LTA
-2De
rlaga
, J.,
97-CF
D-11
Desch
amps
, C.,
4-AA-2
, 80-A
A-14
Desm
et, W
., 3-A
A-1, 1
13-AA
-17De
ters,
R., 1
5-APA
-4De
venp
ort, W
., 37
-AA-6,
38-A
A-7, 1
14-AA
-18,
152
-AA-22
, 187
-AA-28
, 260
-AA-38
, 261
-AA-39
, 2
95-AP
A-34,
297
-APA-3
7De
wey,
R., 1
67-BA
L-1De
y, S.
, 301
-CFD-3
1Dh
aene
, T.,
66-M
ST-4
Dham
anka
r, N.,
245-C
FD-30
Dias,
B., 3
4-TP-1
Dias,
J., 1
18-AF
M-7
Dicke
y, D.
, 189
-AA-30
Dicke
y, E.,
49-A
PA-7,
87-A
PA-9
Dief,
T., 4
3-AFM
-3Die
rke, J
., 39
-AA-8,
185
-AA-26
, 263
-AA-41
DiGiro
lamo,
E., 2
65-AC
D-7Dil
an, G
., 28
5-MST
-12Dil
l, E.,
166-A
TIO-17
Dimota
kis, P
., 27
-FD-3,
139
-FD-18
, 244
-CFD-2
9,
278
-FD-30
Diosa
dy, L
., 21
-CFD-1
, 201
-CFD-2
1Dir
k, B.
, 230
-AA-35
Djedd
i, R.,
243-C
FD-28
Doga
n, A.,
8-AF
M-1,
83-AF
M-5,
128-A
TIO-14
, 273
-ASE-5
Doga
riu, A
., 86
-AMT-6
/GT-6
Dolfi-
Boute
yre, A
., 27
2-ASE
-4Do
nado
n, M.
, 260
-AA-38
Dong
, H.,
136-F
D-15,
248
-FD-29
Dong
, M.,
99-FD
-10Do
ng, X
., 84
-AFM-
6Do
ngre,
R., 2
50-LT
A-1Do
olan,
C., 1
15-AA
-19, 1
52-AA
-22, 2
31-AA
-36Do
ty, M
., 15
8-AMT
-9/GT
-9Do
ughe
rty, N
., 68
-TP-3,
228
-AA-33
Douv
ille, T
., 18
0-PDL
-8/AP
A-20,
269
-APA-3
1Do
well,
E., 3
07-M
AO-12
Dowl
ing, D
., 21
1-FD-2
6Do
wning
, J.,
40-AA
-9Do
yle, J
., 90
-APA-1
2Dr
aper,
M.,
274-A
TIO-24
Drew
, M.,
126-A
TIO-12
Drive
r, D.,
108-T
P-5Dr
ozda
, T.,
244-C
FD-29
Drye
r, J.,
281-G
EPC-1
Duan
, D.,
250-L
TA-1
Duan
, F.,
47-AP
A-5Du
an, L
., 13
7-FD-1
6, 2
05-CF
D-25
Duan
, Z.,
23-CF
D-3, 5
6-CFD
-6Du
bot,
T., 2
99-AT
IO-28
Dubo
urg, V
., 16
7-BAL
-1Du
bov,
Y., 3
1-MST
-2Du
cruix,
S.,
185-A
A-26
Duda
, B.,
188-A
A-29
Dudd
eck,
F., 2
84-M
AO-11
Duffy
, M.,
194-A
PA-22
Dumi
trach
e, C.,
107
-PDL-4
, 143
-PDL-6
Dunc
an, G
., 13
7-FD-1
6Du
ncan
, M.,
85-AM
T-5/G
T-5Du
nlap,
P., 2
73-AS
E-5Du
nn, S
., 45
-AMT-3
/GT-3
, 191
-AMT-1
1/GT
-11Du
nne,
R., 1
62-AP
A-19
Duqu
e, E.,
301
-CFD-3
1, 3
02-CF
D-32
Durai
samy
, K.,
58-CF
D-8Du
rak, U
., 17
7-MST
-7Du
rand,
C., 1
54-AA
-24Du
tta, S
., 44
-AFM-
4Dz
ikus,
N., 2
39-AT
IO-22
, 299
-ATIO
-28Ec
hekk
i, T.,
185-A
A-26
Econ
omon
, T., 1
33-CF
D-16,
204-C
FD-24
, 212
-MAO
-6,
271
-APA-3
3, 2
83-M
AO-10
Edgin
gton-M
itche
ll, D.
, 153
-AA-23
Edoh
, A.,
132-C
FD-15
Edwa
rds, D
., 48
-APA-6
Edwa
rds, J
., 20
3-CFD
-23Ed
wards
, M.,
86-AM
T-6/G
T-6Efr
aimsso
n, G.
, 78-A
A-12,
235
-APA-2
7Eg
orov,
I., 9
9-FD-1
0Eh
renfrie
d, K.,
260
-AA-38
Eisfel
d, B.
, 172
-CFD-2
0Eit
elberg
, G.,
37-AA
-6, 2
69-AP
A-31
123
Auth
or/S
essio
n Ch
air In
dex
Ekate
rin, J
., 56
-CFD-6
Ekici,
K., 2
43-CF
D-28
Ekme
kci, A
., 25
9-AA-3
7Ek
oule,
C., 3
7-AA-6
El ba
ialy,
I., 1
78-M
ST-8
Elham
, A.,
64-M
AO-2
Elias
son,
P., 1
60-AP
A-17
Eljac
k, E.,
236
-APA-2
8Ell
ejmi, M
., 91
-ATIO
-9Elm
iligui,
A., 1
60-AP
A-17,
285
-MST
-12Em
pl, D
., 53
-ATIO
-7En
ghard
t, L.,
151
-AA-21
, 152
-AA-22
, 173
-FD-19
Enjia
o, Z.,
119
-AFM-
8En
tz, R.
, 104
-MAO
-3En
via, E
., 26
4-AA-4
2Ep
pink,
J., 1
37-FD
-16Ere
s, M.
, 128
-ATIO
-14, 3
08-M
AO-13
Eriks
son,
L., 6
-AA-4,
154
-AA-24
Ernst,
D.,
186-A
A-27
Errico
, A.,
164-A
TIO-15
Erturk
, S.,
83-AF
M-5
Esco
bar, J
., 23
4-APA
-26Es
ker, B
., 28
1-GEP
C-1Etc
hessa
har, M
., 22
6-AA-3
1Eti
enne
, S.,
304-C
FD-34
Evan
s, A.,
126
-ATIO
-12Ev
ans,
M., 2
44-CF
D-29
Evers
man,
W., 7
-AA-5
Ewert
, R.,
38-AA
-7, 3
9-AA-8
, 41-A
A-10,
79-A
A-13,
1
12-AA
-16, 1
55-AA
-25, 1
85-AA
-26, 2
30-AA
-35Ey
i, S.,
57-CF
D-7, 1
31-CF
D-14,
244
-CFD-2
9Ey
mann
, T.,
174-F
D-20
Faga
n, A.,
189
-AA-30
Fagle
y, C.,
12-A
PA-1,
125
-APA-1
6Fa
irbrot
her, D
., 16
7-BAL
-1, 2
00-BA
L-2Fa
la, N
., 15
6-ACD
-4Fa
lcão,
C., 2
43-CF
D-28
Faliss
ard, F
., 15
4-AA-2
4Fa
n, D.
, 56-C
FD-6
Fan,
H., 1
65-AT
IO-16
, 199
-ATIO
-20Fa
n, Y.,
180
-PDL-8
/APA
-20Fa
ranos
ov, G
., 11
5-AA-1
9, 1
89-AA
-30, 2
28-AA
-33Fa
res, E
., 18
8-AA-2
9Fa
rnswo
rth, J
., 16
2-APA
-19Fa
rr, R.,
228
-AA-33
Farrin
gton,
A., 2
02-CF
D-22
Fase
l, H., 2
8-FD-4
, 100
-FD-11
, 102
-FD-13
, 208
-FD-23
Fassm
ann,
B., 7
9-AA-1
3Fa
ttah,
R., 1
13-AA
-17, 2
63-AA
-41Fe
dorov
, A.,
99-FD
-10Fe
hlman
, W.,
165-A
TIO-16
, 199
-ATIO
-20Fe
hrenb
ach,
S., 2
74-AT
IO-24
Felde
r, W.,
239-A
TIO-22
Feldh
usen
, A.,
41-AA
-10Fe
lipe,
V., 1
6-ATIO
-1Fé
lix Pa
trón,
R., 1
8-ATIO
-3Fe
ltrop,
E., 2
70-AP
A-32
Feng
, F.,
80-AA
-14Fe
nouil
, J.,
295-A
PA-34
Fergu
son,
S., 6
4-MAO
-2, 1
04-M
AO-3,
308
-MAO
-13Fe
rmen
-Coke
r, M.,
119-A
FM-8
Fern,
L., 2
74-AT
IO-24
Ferna
ndes
de O
liveir
a, R.,
104
-MAO
-3Fe
rnand
o, A.,
229
-AA-34
Ferna
ndo,
R., 1
87-AA
-28Fe
rrari,
D., 1
17-AC
D-3, 2
13-M
AO-7
Ferre
ira de
Castr
o, D.
, 30-M
ST-1
Fidko
wski,
K., 9
5-CFD
-9, 1
70-CF
D-18
Field,
J., 3
1-MST
-2Fie
lds, T
., 15
7-AFM
-9Fié
vet,
R., 3
04-CF
D-34
Filipp
one,
E., 1
64-AT
IO-15
, 300
-ATIO
-29Fil
izola,
A., 6
5-MST
-3Fin
danis
, N.,
125-A
PA-16
Finley
, D.,
47-AP
A-5, 1
61-AP
A-18
Fiore,
G.,
297-A
PA-37
Firso
v, A.,
107
-PDL-4
Fisch
els, M
., 24
3-CFD
-28Fis
cher,
P., 2
02-CF
D-22
Fisch
erswo
rring-B
unk,
A., 2
84-M
AO-11
Fishe
r, T.,
145-T
P-7, 2
02-CF
D-22
Flatau
, A.,
50-AP
A-8Fle
tcher,
D.,
181-P
DL-9/
TP-8
Fleury
, V.,
3-AA-1
, 262
-AA-40
Florez
Mera
, J.,
35-TP
-2Fo
ster, J
., 15
7-AFM
-9Fo
ster, N
., 30
5-CFD
-35Fo
ster, T
., 24
0-ATIO
-23Fo
uladi,
H.,
196-A
SE-2
Franç
ois, B
., 15
2-AA-2
2Fra
nke,
D., 1
3-APA
-2Fra
nkho
user,
M.,
33-PD
L-1/F
D-5Fra
nko,
K., 2
02-CF
D-22
Frasso
ldati,
A., 2
44-CF
D-29
Frazz
a, L.,
58-C
FD-8
Frede
ricks
, W.,
19-AT
IO-4,
127
-ATIO
-13Fre
ret, L
., 97
-CFD-1
1Fre
sconi,
F., 9
0-APA
-12, 1
19-AF
M-8
Freun
d, J.,
78-A
A-12
Frew,
E., 1
57-AF
M-9,
273
-ASE-5
Fried
man,
A., 1
76-M
AO-5,
296
-APA-3
5Fri
edma
n, C.,
236
-APA-2
8Fri
schem
eier, S
., 11
7-ACD
-3Fu
chs,
M., 3
06-CF
D-36
Fuck
e, L.,
31-M
ST-2
Fujii,
K., 6
0-FD-6
/PDL
-2, 1
14-AA
-18, 1
30-CF
D-13,
1
69-CF
D-17
Fujin
o, T.,
286
-PDL-1
3Fu
jita, K
., 68
-TP-3,
69-T
P-4Fu
jiwara
, G.,
49-AP
A-7Fu
ller, C
., 22
6-AA-3
1Fu
nk, C
., 12
4-APA
-15Fu
rukaw
a, D.
, 89-A
PA-11
Gaba
rd, G
., 6-A
A-4, 7
8-AA-1
2, 1
13-AA
-17, 2
63-AA
-41Ga
bbert
, D.,
48-AP
A-6Ga
ddai,
A., 2
03-CF
D-23
Gaeta
, R.,
37-AA
-6, 2
31-AA
-36Ga
itond
e, D.
, 80-A
A-14,
174
-FD-20
, 205
-CFD-2
5,
245
-CFD-3
0, 2
66-AM
T-13/
GT-13
, 302
-CFD-3
2,
303
-CFD-3
3Ga
lbrait
h, M.
, 170
-CFD-1
8Ga
llman
, J.,
79-AA
-13Ga
llo, E
., 86
-AMT-6
/GT-6
Galye
n, N.
, 11-A
MT-2/
GT-2
Gamb
a, M.
, 102
-FD-13
Gamb
ardell
a, D.
, 104
-MAO
-3Ga
mblin
, R.,
200-B
AL-2
Gamb
oa, P
., 43
-AFM-
3, 1
04-M
AO-3
Gan,
J., 9
0-APA
-12Ga
napa
thisu
brama
ni, B
., 3-A
A-1, 3
8-AA-7
, 136
-FD-15
Gao,
D., 1
07-PD
L-4Ga
o, Z.,
161
-APA-1
8, 2
13-M
AO-7
Garci
a, D.
, 282
-LTA-2
Garci
a, E.,
239
-ATIO
-22Ga
rgiulo
, F.,
164-A
TIO-15
Garla
nd, M
., 14
2-MST
-6Ga
rman
, K.,
249-F
T-1Ga
rman
n, D.
, 208
-FD-23
, 302
-CFD-3
2Ga
rrard,
G.,
120-A
MT-7/
GT-7
Garre
tt, S
., 98
-CFD-1
2, 2
09-FD
-24Ga
rrick,
D., 2
43-CF
D-28
Gartn
er, J.
, 63-F
D-9Ga
ry, J.
, 167
-BAL-1
Gasb
arri, P
., 11
9-AFM
-8Ga
tian,
K., 5
2-ATIO
-6Ga
tlin, G
., 88
-APA-1
0Ga
uger,
N.,
79-AA
-13, 2
52-M
AO-9,
283
-MAO
-10Ga
uthier
, T.,
47-AP
A-5Ga
utier,
M.,
238-A
TIO-21
Gea-A
guile
ra, F.
, 112
-AA-16
Gebre
egzia
bher,
A., 4
2-ACD
-1Ge
der, J
., 48
-APA-6
, 233
-APA-2
5Ge
e, K.,
40-A
A-9Ge
isbau
er, S
., 10
5-MST
-5, 1
95-AP
A-23
Geisle
r, R.,
159-A
MT-10
/GT-1
0Ge
mma,
S., 2
9-MAO
-1
Genn
aretti,
M.,
162-A
PA-19
, 263
-AA-41
Georg
e, J.,
11-A
MT-2/
GT-2,
50-A
PA-8
Georg
iadis,
N.,
175-F
D-22
Gerbe
r, T.,
167-B
AL-1
Gerla
ch, T
., 17
7-MST
-7Ge
rman
, B.,
93-AT
IO-11
, 127
-ATIO
-13Ge
rn, F.
, 82-A
CD-2
Gerz,
T., 1
96-AS
E-2Ge
tsing
er, D
., 17
3-FD-1
9Ge
uther,
S.,
164-A
TIO-15
Geye
r, T.,
231-A
A-36
Geze
r, R.,
83-AF
M-5
Gherm
an, G
., 96
-CFD-1
0Gh
orawa
t, P.,
84-A
FM-6
Ghorb
anias
l, G.,
152-A
A-22
Ghore
yshi,
M.,
236-A
PA-28
, 305
-CFD-3
5Gh
osh,
A., 1
18-AF
M-7
Ghos
h, D.
, 163
-ASE-1
Ghos
h, S.
, 125
-APA-1
6, 2
13-M
AO-7
Giauq
ue, A
., 18
5-AA-2
6Gie
pman
, R.,
138-F
D-17
Gil Pr
ieto,
D., 2
70-AP
A-32
Gilde
rslee
ve, S
., 10
1-FD-1
2Gil
es, M
., 20
0-BAL
-2Gil
ge, P
., 23
5-APA
-27Gil
l, J., 1
12-AA
-16, 1
13-AA
-17, 1
52-AA
-22, 2
60-AA
-38Gil
lespie
, E.,
8-AFM
-1Gil
liam,
F., 6
4-MAO
-2Gil
more,
B.,
104-M
AO-3
Ginn,
S., 2
40-AT
IO-23
Giret,
J., 1
88-AA
-29Gir
imaji
, S.,
58-CF
D-8Gla
ab, P
., 14
2-MST
-6Gla
ss, C.
, 233
-APA-2
5Gle
gg, S
., 37
-AA-6,
38-A
A-7, 7
7-AA-1
1, 1
14-AA
-18,
187
-AA-28
, 261
-AA-39
Gloerf
elt, X
., 56
-CFD-6
, 62-F
D-8, 1
13-AA
-17 ,
154
-AA-24
, 226
-AA-31
Gloud
eman
s, J.,
82-A
CD-2
Gnoff
o, P.,
132
-CFD-1
5Go
blet,
V., 1
56-AC
D-4Gó
es, L
., 30
-MST
-1, 2
82-LT
A-2Go
ginen
i, S.,
266-A
MT-13
/GT-1
3Go
jon, R
., 4-A
A-2Go
kcen
, T.,
34-TP
-1, 1
08-TP
-5, 2
16-TP
-10/P
DL-10
Golas
zews
ki, R.
, 275
-ATIO
-25Go
ldberg
, U.,
245-C
FD-30
Golds
mith,
B.,
276-A
TIO-26
Golds
tein,
D., 2
88-TP
-13Go
li, N.
, 265
-ACD-7
Golub
ev, A
., 22
6-AA-3
1Go
lubev
, V.,
79-AA
-13
Gond
a, J.,
239
-ATIO
-22Go
ng, C
., 25
2-MAO
-9, 2
98-AT
IO-27
Gonz
alez,
D., 3
03-CF
D-33
Gonz
alez,
L., 1
01-FD
-12Go
nzale
z-Line
ro, L.
, 190
-ACD-5
Good
rich,
K., 9
3-ATIO
-11, 1
99-AT
IO-20
Gopa
larath
nam,
A., 2
35-AP
A-27,
267
-APA-2
9Go
paraj
u, K.,
205
-CFD-2
5Go
rdeye
v, S.
, 88-A
PA-10
, 143
-PDL-6
, 255
-PDL-1
2Go
rdnier
, R.,
62-FD
-8, 2
08-FD
-23Go
rham,
P., 2
00-BA
L-2Go
ri, G.
, 133
-CFD-1
6, 1
96-AS
E-2Go
ri, R.,
162
-APA-1
9Go
rrell,
S., 3
02-CF
D-32
Gorto
n, S.
, 281
-GEPC
-1Go
urina
t, Y.,
82-A
CD-2
Govin
daraj
an, R
., 28
-FD-4
Govin
daraj
u, P.,
82-A
CD-2
Goya
l, T.,
234-A
PA-26
Goyn
e, C.,
159
-AMT-1
0/GT
-10Gr
abe,
C., 6
1-FD-7
Grac
e, S.
, 264
-AA-42
Grah
am, R
., 51
-ATIO
-5Gr
amaty
ka, J
., 30
8-MAO
-13Gr
anlun
d, K.,
63-F
D-9, 1
75-FD
-22Gr
ant,
J., 3
7-AA-6
Gran
t, M.
, 44-A
FM-4,
83-A
FM-5
Gras
so, F
., 98
-CFD-1
2Gr
asso
, G.,
112-A
A-16
Grau
be, P
., 10
8-TP-5
Grau
er, J.
, 118
-AFM-
7Gr
een,
C., 2
40-AT
IO-23
Gree
n, M.
, 26-F
D-2Gr
eenb
latt,
D., 1
01-FD
-12, 1
58-AM
T-9/G
T-9, 2
08-FD
-23Gr
eend
yke,
R., 3
4-TP-1
Gree
ne, B
., 33
-PDL-1
/FD-5
Gree
ne, G
., 23
7-ASE
-3Gr
eene
, K.,
43-AF
M-3
Greg
ory, J
., 33
-PDL-1
/FD-5
, 268
-APA-3
0Gr
enon
, R.,
13-AP
A-2Gr
iffiths
, P.,
209-F
D-24
Grim
m, F.
, 185
-AA-26
Grim
men,
J., 3
05-CF
D-35
Grim
sley,
J., 1
40-IT
AR-2
Grins
tead,
J., 6
9-TP-4
Grive
l, A.,
46-AM
T-4/G
T-4Gr
oss,
A., 2
08-FD
-23Gr
oss,
R., 9
9-FD-1
0Gr
oth, C
., 97
-CFD-1
1, 1
71-CF
D-19,
304
-CFD-3
4Gr
ound
, C.,
86-AM
T-6/G
T-6Gr
und,
T., 1
25-AP
A-16
Gu, L
., 25
2-MAO
-9
124
Auth
or/S
essio
n Ch
air In
dex
Gu, Q
., 26
5-ACD
-7Gu
, Y.,
43-AF
M-3
Guan
, Y.,
38-AA
-7Gu
ardon
e, A.,
26-F
D-2, 1
33-CF
D-16,
196
-ASE-2
Guen
ther, C
., 30
5-CFD
-35Gu
erin,
S., 4
1-AA-1
0, 7
7-AA-1
1Gu
erreir
o, N.
, 17-A
TIO-2
Guerr
i, O.,
305-C
FD-35
Gugli
elmo,
J., 2
35-AP
A-27
Gumi
nsky
, M.,
142-M
ST-6,
299
-ATIO
-28Gu
o, C.,
84-A
FM-6
Guo,
J., 1
64-AT
IO-15
Guo,
Y., 1
12-AA
-16, 1
16-AA
-20Gu
pta, A
., 97
-CFD-1
1, 2
68-AP
A-30
Gupta
, M.,
38-AA
-7Gu
pte, A
., 57
-CFD-7
Gursu
l, I.,
25-FD
-1, 1
38-FD
-17Gu
tmark
, E.,
153-A
A-23
Guyn
n, M.
, 293
-ACD-8
Guyto
n, R.,
85-A
MT-5/
GT-5
Guze
l, G.,
304-C
FD-34
Haba
shi, W
., 19
6-ASE
-2Ha
bbit,
R., 9
6-CFD
-10Ha
eri, S
., 26
1-AA-3
9Ha
fez, M
., 10
5-MST
-5, 2
78-FD
-30Ha
ga, T
., 13
0-CFD
-13Ha
gen,
G., 1
7-ATIO
-2Ha
hn, M
., 29
-MAO
-1Ha
imes
, R.,
302-C
FD-32
Haina
ut, T.
, 6-AA
-4Ha
ji-She
ikh, A
., 35
-TP-2
Hajia
n, R.,
25-F
D-1Ha
jj, M.
, 236
-APA-2
8Ha
le, L.
, 30-M
ST-1
Hall,
D., 6
4-MAO
-2Ha
ll, J.,
283
-MAO
-10Ha
llock
, J.,
237-A
SE-3
Halls,
B.,
86-AM
T-6/G
T-6Ha
m, F.
, 202
-CFD-2
2Ha
mane
, D.,
305-C
FD-35
Hami
che,
K., 2
63-AA
-41Ha
mmac
k, S.
, 107
-PDL-4
Hamm
ock,
G., 1
58-AM
T-9/G
T-9, 1
91-AM
T-11/
GT-11
Han,
K., 1
98-AT
IO-19
Han,
X., 1
44-PD
L-7Ha
nnem
ann,
K., 3
02-CF
D-32
Hanq
uist,
K., 3
5-TP-2
Hans
es, C
., 51
-ATIO
-5Ha
nsma
n, R.,
156
-ACD-4
Harad
a, N.
, 181
-PDL-9
/TP-8
Harih
aran,
N., 1
22-AP
A-13
Harik
, R.,
64-M
AO-2
Harke
r, B.,
40-AA
-9Ha
rringto
n, A.,
136
-FD-15
Harris
, R., 4
1-AA-1
0, 81
-AA-15
, 195
-APA-2
3, 24
1-CFD
-26Ha
rrison
, E.,
156-A
CD-4
Harsh
e, S.
, 235
-APA-2
7Ha
rtfield
, R.,
127-A
TIO-13
, 161
-APA-1
8Ha
rtwich
, P.,
87-AP
A-9, 1
33-CF
D-16
Hasa
n, S.
, 65-M
ST-3,
142
-MST
-6, 1
97-AT
IO-18
, 2
75-AT
IO-25
Hash
, D.,
288-T
P-13
Hash
emi, A
., 68
-TP-3
Hash
emi, K
., 9-A
FM-2
Hask
in, H
., 15
8-AMT
-9/GT
-9Ha
snain
, Z.,
12-AP
A-1, 5
0-APA
-8Ha
ssan,
M., 3
7-AA-6
, 42-A
CD-1,
53-AT
IO-7,
239-A
TIO-22
Hassa
n, W.
, 15-A
PA-4
Hatha
way,
J., 1
96-AS
E-2Ha
ttenb
erger,
G.,
161-A
PA-18
Haxte
r, S.,
260-A
A-38
Hay,
A., 5
8-CFD
-8, 2
04-CF
D-24,
304
-CFD-3
4Ha
yash
ibara,
S.,
27-FD
-3Ha
yden
, T.,
88-AP
A-10,
143
-PDL-6
, 255
-PDL-1
2Ha
ys, T
., 15
7-AFM
-9Ha
ywoo
d, J.,
24-C
FD-4
Hazir
, A.,
188-A
A-29
He, A
., 27
2-ASE
-4He
, C.,
280-F
T-2/G
T-14
Hebe
rt, P.
, 85-A
MT-5/
GT-5
Hedri
ck, T
., 10
0-FD-1
1He
eg, J
., 12
4-APA
-15He
fferno
n, T.,
259
-AA-37
Hegd
e, A.,
174
-FD-20
Hege
n, S.
, 13-A
PA-2
Heine
ck, J
., 19
2-AMT
-12/G
T-12
Heinr
ich, R
., 57
-CFD-7
Heise
r, W.,
15-AP
A-4He
itmeir
, F.,
151-A
A-21
Helbe
r, B.,
108-T
P-5He
lm, S
., 91
-ATIO
-9He
mpley
, L.,
165-A
TIO-16
, 199
-ATIO
-20He
nders
on, B
., 22
7-AA-3
2He
nders
on, R
., 13
7-FD-1
6He
nfling
, J.,
62-FD
-8, 1
75-FD
-22He
nry de
Frah
an, M
., 20
1-CFD
-21He
rbst,
S., 8
8-APA
-10, 2
53-M
ST-11
Heret
h, L.,
15-A
PA-4
Herol
d, G.
, 186
-AA-27
, 231
-AA-36
Herr,
M., 1
15-AA
-19, 1
55-AA
-25, 2
26-AA
-31, 2
30-AA
-35He
rrema
, F.,
51-AT
IO-5
Herrin
g, A.,
158
-AMT-9
/GT-9
Herrm
ann,
J., 2
9-MAO
-1He
rron,
A., 2
62-AA
-40
Herzo
g, S.
, 252
-MAO
-9He
ss, C.
, 11-A
MT-2/
GT-2
Hicke
l, S.,
87-AP
A-9Hic
ken,
J., 1
76-M
AO-5,
212
-MAO
-6, 2
42-CF
D-27,
2
51-M
AO-8
Hieple
r, `.,
302-C
FD-32
Higdo
n, K.,
288
-TP-13
High,
J., 1
65-AT
IO-16
Higue
ra Ca
ubilla
, D.,
58-CF
D-8Hil
debra
nd, N
., 4-A
A-2Hin
er, W
., 79
-AA-13
Hinze
, N.,
300-A
TIO-29
Hipp,
K., 5
0-APA
-8Hir
amoto
, R.,
293-A
CD-8
Hiray
ama,
T., 6
6-MST
-4Hit
zel, S
., 16
0-APA
-17Hix
on, D
., 6-A
A-4, 7
8-AA-1
2, 8
1-AA-1
5, 1
54-AA
-24,
229
-AA-34
Hoell
ing, M
., 50
-APA-8
Hoffle
r, K.,
43-AF
M-3
Hoffm
an, R
., 14
2-MST
-6Ho
ffman
n, K.,
175
-FD-22
Höge
r, M.,
151-A
A-21
Holla
day,
W., 8
5-AMT
-5/GT
-5Ho
lland
, K.,
186-A
A-27
Holla
nd, M
., 11
7-ACD
-3Hö
lling,
M., 2
71-AP
A-33
Hollin
gswo
rth, P
., 30
-MST
-1, 5
3-ATIO
-7Ho
lst, T
., 13
6-FD-1
5Ho
lzäpfe
l, F.,
196-A
SE-2,
237
-ASE-3
Hong
, S.,
51-AT
IO-5,
166
-ATIO
-17Ho
ng, Z
., 10
7-PDL
-4Ho
nnery
, D.,
153-A
A-23
Hoog
reef,
M., 4
2-ACD
-1, 1
76-M
AO-5
Hopf,
J., 1
91-AM
T-11/
GT-11
Horch
ler, T
., 30
2-CFD
-32Ho
rio, B
., 65
-MST
-3, 1
42-M
ST-6
Horkh
eimer,
D.,
282-L
TA-2
Horn,
J., 4
3-AFM
-3, 8
3-AFM
-5Ho
rne, W
., 18
6-AA-2
7, 2
62-AA
-40Ho
rnung
, M.,
88-AP
A-10,
91-A
TIO-9,
253
-MST
-11Ho
sang
adi, P
., 23
5-APA
-27Ho
sder,
S.,
58-CF
D-8Ho
sseinv
erdi, S
., 10
0-FD-1
1Ho
usma
n, J.,
4-AA
-2, 1
4-APA
-3, 4
9-APA
-7Ho
ward,
M.,
68-TP
-3Ho
werto
n, B.
, 7-AA
-5, 1
16-AA
-20Hu
, F.,
229-A
A-34
Hu, H
., 18
0-PDL
-8/AP
A-20
Hu, J
., 17
1-CFD
-19Hu
, Y.,
208-F
D-23
Hu, Z
., 22
-CFD-2
, 205
-CFD-2
5
Hua,
J., 3
5-TP-2
Huan
g, G.
, 159
-AMT-1
0/GT
-10, 1
62-AP
A-19,
2
67-AP
A-29,
270
-APA-3
2Hu
ang,
X., 7
-AA-5,
26-F
D-2, 7
8-AA-1
2, 1
13-AA
-17Hu
ang,
Z., 9
9-FD-1
0Hu
bbard
, E.,
191-A
MT-11
/GT-1
1Hu
bbard
, J.,
12-AP
A-1, 5
0-APA
-8Hu
ber, J
., 18
9-AA-3
0Hu
e, D.
, 13-A
PA-2
Hueh
ne, C
., 12
5-APA
-16Hu
et, M
., 18
5-AA-2
6Hu
ff, B
., 12
8-ATIO
-14Hu
fnage
l, K.,
271-A
PA-33
Hug,
S., 2
4-CFD
-4Hu
ghes
, M.,
196-A
SE-2
Hui, F
., 10
8-TP-5
Hulsh
off, S
., 33
-PDL-1
/FD-5
Hultg
ren, L
., 15
1-AA-2
1Hu
mpert
, B.,
37-AA
-6Hu
mphre
ys, C
., 14
1-MAO
-4Hu
mphre
ys, W
., 18
8-AA-2
9Hu
r, J.,
124-A
PA-15
Husse
in, A.
, 236
-APA-2
8Hu
ssein,
S.,
246-F
D-27
Hutch
eson
, F.,
4-AA-2
, 158
-AMT-9
/GT-9
Huyn
h, H.
, 55-C
FD-5,
130
-CFD-1
3, 1
70-CF
D-18,
2
42-CF
D-27
Hwan
g, I.,
31-M
ST-2,
126
-ATIO
-12Hw
ang,
J., 2
9-MAO
-1, 3
07-M
AO-12
Idier,
A., 3
-AA-1
Idris,
H.,
16-AT
IO-1,
275
-ATIO
-25Ihm
e, M.
, 151
-AA-21
, 242
-CFD-2
7Ike
da, T
., 15
5-AA-2
5Im
, D.,
12-AP
A-1, 1
32-CF
D-15
Imam
ura, T
., 15
5-AA-2
5, 2
41-CF
D-26
Imlay
, S.,
301-C
FD-31
Ims,
J., 2
3-CFD
-3Im
tiaz,
H., 1
33-CF
D-16
Ingrah
am, D
., 6-A
A-4Iop
polo,
T., 4
6-AMT
-4/GT
-4Ior
io, M
., 10
1-FD-1
2Ish
ida, Y
., 68
-TP-3
Ishiok
a, H.
, 270
-APA-3
2Ish
utkina
, M.,
298-A
TIO-27
Isikv
eren,
A., 5
3-ATIO
-7Ita
sse, M
., 22
8-AA-3
3Ito
, H.,
23-CF
D-3Ito
, K.,
66-M
ST-4
Ito, Y
., 23
0-AA-3
5Iva
ldi, D
., 30
7-MAO
-12Iva
nov,
V., 2
43-CF
D-28
Iwak
awa,
A., 8
9-APA
-11, 1
38-FD
-17
Jack
, D.,
43-AF
M-3
Jack
son,
G., 1
45-TP
-7Ja
ckso
n, R.,
138
-FD-17
Jack
son,
T., 2
03-CF
D-23
Jaco
b, D.
, 237
-ASE-3
, 272
-ASE-4
Jaco
b, J.,
37-A
A-6, 4
8-APA
-6, 1
40-IT
AR-2,
196
-ASE-2
, 2
31-AA
-36, 2
74-AT
IO-24
, 280
-FT-2/
GT-14
Jaco
bi, R.
, 100
-FD-11
Jaco
bs, S
., 10
7-PDL
-4Ja
cque
s, D.
, 141
-MAO
-4Ja
ffrez
ic, B
., 17
8-MST
-8Ja
in, N
., 17
1-CFD
-19Ja
lali, A
., 21
-CFD-1
Jamb
unath
an, R
., 20
3-CFD
-23Ja
mes,
M., 4
0-AA-9
Jame
son,
A., 5
5-CFD
-5, 1
23-AP
A-14,
132
-CFD-1
5,
271
-APA-3
3Ja
njic,
Z., 1
63-AS
E-1Ja
nn, T
., 10
5-MST
-5Ja
ouan
i, N.,
187-A
A-28
Jaron
, R.,
77-AA
-11Ja
rzemb
ski, A
., 25
0-LTA
-1Ja
strze
bski,
M.,
17-AT
IO-2
Jaun
et, V.
, 80-A
A-14,
189
-AA-30
Jawo
rski, J
., 25
-FD-1,
38-A
A-7Je
nkins
, L.,
188-A
A-29,
192
-AMT-1
2/GT
-12Je
nkins
, T.,
11-AM
T-2/G
T-2, 1
59-AM
T-10/
GT-10
Jens
en, L
., 15
6-ACD
-4Je
ssberg
er, C.
, 52-A
TIO-6
Jesu
s, A.,
98-C
FD-12
Jewe
ll, J.,
28-F
D-4Ji,
C., 1
16-AA
-20Ji,
L., 1
51-AA
-21Jia
nchu
n, X.
, 215
-MST
-10Jia
ng, C
., 18
0-PDL
-8/AP
A-20
Jiang
, H.,
78-AA
-12Jia
ng, N
., 86
-AMT-6
/GT-6
Jiang
, Z.,
22-CF
D-2Jia
o, J.,
263
-AA-41
Jie, B
., 25
3-MST
-11Jim
enez
, H.,
52-AT
IO-6,
156
-ACD-4
, 293
-ACD-8
Jin, J
., 85
-AMT-5
/GT-5
Jin, W
., 85
-AMT-5
/GT-5
Jing,
C., 2
52-M
AO-9
Jinwu
, X.,
214-M
ST-9
Jiras
ek, A
., 16
0-APA
-17, 3
05-CF
D-35
Jo, Y
., 25
1-MAO
-8Jo
hans
en, C
., 12
1-AMT
-8/FD
-14/T
P-6/G
T-8,
159
-AMT-1
0/GT
-10Jo
hnse
n, E.,
201
-CFD-2
1, 2
11-FD
-26Jo
hnso
n, H.
, 103
-ITAR
-1Jo
hnso
n, S.
, 43-A
FM-3,
214
-MST
-9
125
Auth
or/S
essio
n Ch
air In
dex
John
ston,
C., 6
9-TP-4
, 217
-TP-11
Jolly,
B.,
23-CF
D-3, 1
36-FD
-15, 2
41-CF
D-26
Jond
eau,
E., 2
31-AA
-36Jo
nes,
A., 2
68-AP
A-30
Jone
s, G.
, 294
-AMT-1
4/GT
-15Jo
nes,
J., 2
28-AA
-33Jo
nes,
M., 7
-AA-5,
26-F
D-2, 1
16-AA
-20, 2
62-AA
-40,
302
-CFD-3
2Jo
nes,
S., 8
6-AMT
-6/GT
-6Jo
nes,
W., 3
01-CF
D-31
Joo,
J., 1
91-AM
T-11/
GT-11
Jorda
n, P.,
5-AA
-3, 8
0-AA-1
4, 1
89-AA
-30Jo
rris, T
., 24
9-FT-1
Jose
ph, L
., 29
5-APA
-34Jo
seph
, P.,
3-AA-1
, 7-AA
-5, 3
8-AA-7
, 79-A
A-13,
1
52-AA
-22, 2
61-AA
-39Jo
st, A.
, 203
-CFD-2
3Jo
syula
, E.,
69-TP
-4Jo
yce,
R., 3
1-MST
-2Ju
liano
, T.,
10-AM
T-1/G
T-1, 1
37-FD
-16Ju
mper,
E., 8
8-APA
-10, 1
43-PD
L-6, 2
55-PD
L-12
June
, J.,
262-A
A-40
Jung
, K.,
235-A
PA-27
Jung
, S.,
166-A
TIO-17
Jung
, T.,
64-M
AO-2
Jung
, Y.,
16-AT
IO-1,
91-A
TIO-9,
198
-ATIO
-19,
298
-ATIO
-27Ju
nkui,
M.,
45-AM
T-3/G
T-3, 2
85-M
ST-12
Junq
ueira
-Junio
r, C.,
270-A
PA-32
Jurko
vich,
M., 1
93-AP
A-21,
269
-APA-3
1Ju
stin,
C., 1
90-AC
D-5Ju
ve, D
., 18
9-AA-3
0, 2
31-AA
-36Ka
ddou
h, B.
, 30-M
ST-1
Kaila
sana
th, K.
, 153
-AA-23
Kaliv
arapu
, V.,
29-M
AO-1,
104
-MAO
-3, 2
83-M
AO-10
Kalkh
oran,
I., 2
33-AP
A-25
Kalya
n, A.,
228
-AA-33
Kama
li, S.
, 122
-APA-1
3Ka
mat,
S., 2
93-AC
D-8Ka
mle,
S., 2
34-AP
A-26
Kamm
eyer,
M.,
294-A
MT-14
/GT-1
5Ka
mpers
, G.,
50-AP
A-8, 2
71-AP
A-33
Kamr
uzza
man,
M., 1
55-AA
-25Ka
ng, H
., 16
2-APA
-19Ka
nistra
s, K.,
88-A
PA-10
Kann
an, H
., 21
2-MAO
-6Ka
noria
, A.,
250-L
TA-1,
305
-CFD-3
5Ka
pania
, R.,
29-M
AO-1
Kara,
K., 1
3-APA
-2, 5
0-APA
-8, 2
36-AP
A-28
Karab
asov
, S.,
5-AA-3
, 6-AA
-4, 8
0-AA-1
4, 2
28-AA
-33Ka
rahan
, S.,
294-A
MT-14
/GT-1
5Ka
rakoc
, T.,
273-A
SE-5
Karak
oç, N
., 27
3-ASE
-5Ka
rlgaa
rd, C.
, 44-A
FM-4
Karon
, A.,
189-A
A-30
Karth
a, A.,
244
-CFD-2
9Ka
se, S
., 29
3-ACD
-8Ka
sprzy
k, M.
, 280
-FT-2/
GT-14
Kato,
H.,
60-FD
-6/PD
L-2, 1
92-AM
T-12/
GT-12
Katsu
rayam
a, H.
, 286
-PDL-1
3Ka
tz, A.
, 21-C
FD-1,
243
-CFD-2
8Ka
tz, J.
, 88-A
PA-10
Kaul,
U.,
25-FD
-1, 4
9-APA
-7, 2
79-FD
-31Ka
usch
e, P.,
152
-AA-22
Kaya
, D.,
118-A
FM-7
Ke, G
., 26
1-AA-3
9Ke
geris
e, M.
, 99-F
D-10
Kelle
r, D.,
87-AP
A-9Ke
ller, E
., 83
-AFM-
5Ke
lly, M
., 26
9-APA
-31Ke
nned
y, G.
, 212
-MAO
-6Ke
nway
, G.,
141-M
AO-4
Kerho
, M.,
235-A
PA-27
Kessl
er, R.
, 22-C
FD-2,
96-C
FD-10
Key,
N., 1
58-AM
T-9/G
T-9, 1
73-FD
-19Ke
ye, S
., 87
-APA-9
Khali
d, M.
, 136
-FD-15
Khali
l, E.,
145-T
P-7, 1
78-M
ST-8
Kham
is, D
., 7-A
A-5Kh
an, S
., 66
-MST
-4Kh
ire, R
., 14
1-MAO
-4Kh
odad
oust,
A., 2
02-CF
D-22
Khoo
, B.,
235-A
PA-27
Khorr
ami, M
., 15
5-AA-2
5, 1
88-AA
-29, 2
59-AA
-37Kid
d, F.,
143
-PDL-6
Kim, C
., 24
2-CFD
-27Kim
, E.,
51-AT
IO-5
Kim, H
., 88
-APA-1
0Kim
, J., 3
-AA-1,
46-AM
T-4/G
T-4, 1
51-AA
-21, 2
61-AA
-39Kim
, K.,
126-A
TIO-12
Kim, T
., 46
-AMT-4
/GT-4
Kim, V
., 14
1-MAO
-4Kim
, Y.,
142-M
ST-6
Kimme
l, R.,
28-FD
-4, 1
02-FD
-13, 1
03-IT
AR-1
King,
L., 1
61-AP
A-18
King,
R., 9
9-FD-1
0, 1
37-FD
-16Kin
g, W.
, 250
-LTA-1
Kinga
n, M.
, 5-AA
-3, 3
7-AA-6
Kings
, N.,
41-AA
-10, 1
51-AA
-21Kio
, M.,
35-TP
-2Kir
by, A
., 20
1-CFD
-21Kir
by, M
., 19
8-ATIO
-19Kir
is, C.
, 4-AA
-2, 1
4-APA
-3Kir
k, C.,
159
-AMT-1
0/GT
-10
Kirk,
L., 6
9-TP-4
Kiyici,
F., 2
04-CF
D-24
Klabe
s, A.,
226
-AA-31
Kleb,
W., 5
8-CFD
-8, 2
33-AP
A-25
Kleinc
laus,
C., 2
59-AA
-37Kle
ine, H
., 10
2-FD-1
3Kle
ntzma
n, J.,
99-F
D-10
Kline
, H.,
204-C
FD-24
Kling
, U.,
53-AT
IO-7
Klock
, R.,
119-A
FM-8
Kloke
r, M.,
209-F
D-24
Knab
e, F.,
51-A
TIO-5
Knob
loch,
K., 1
51-AA
-21Kn
owles
, J.,
105-M
ST-5
Koc,
I., 3
04-CF
D-34
Koch
, J.,
236-A
PA-28
Koch
, M.,
238-A
TIO-21
Kocia
n, T.,
137
-FD-16
Koda
ma, H
., 15
2-AA-2
2Ko
enig,
M.,
4-AA-2
Koern
er, S
., 23
7-ASE
-3Ko
h, S.
, 38-A
A-7, 4
1-AA-1
0, 7
9-AA-1
3, 8
0-AA-1
4Ko
ike, S
., 19
2-AMT
-12/G
T-12
Koizu
mi, H
., 23
-CFD-3
Kok,
F., 2
7-FD-3
, 175
-FD-22
Koka
ly, M
., 17
8-MST
-8Ko
klu, M
., 63
-FD-9
Kolon
ay, R
., 29
-MAO
-1, 2
52-M
AO-9,
284
-MAO
-11Ko
matsu
, P.,
307-M
AO-12
Kong
, W.,
295-A
PA-34
Konn
eman
n, E.,
275
-ATIO
-25Ko
ntis,
K., 1
93-AP
A-21
Koo,
H., 3
04-CF
D-34
Kopie
v, V.,
187
-AA-28
, 189
-AA-30
, 228
-AA-33
Kopy
t, A.,
30-M
ST-1
Korea
nsch
i, A.,
13-AP
A-2, 2
96-AP
A-35
Korki
s-Kan
aan,
R., 3
05-CF
D-35
Korn,
B.,
51-AT
IO-5
Korol
ev, Y
., 5-A
A-3, 2
51-M
AO-8
Kosti
uk, P
., 14
2-MST
-6Kö
the, T
., 25
2-MAO
-9Ko
tikalp
udi, A
., 15
7-AFM
-9Ko
tov, D
., 24
-CFD-4
Kotov
, M.,
193-A
PA-21
Kotso
nis, M
., 88
-APA-1
0, 2
86-PD
L-13
Kozie
l, S.,
307-M
AO-12
Kozlo
v, A.,
77-A
A-11
Krako
s, J.,
23-C
FD-3
Kraus
man,
J., 2
82-LT
A-2Kra
ut, J.
, 51-A
TIO-5
Kreitz
man,
J., 1
53-AA
-23Kre
uz, M
., 16
4-ATIO
-15
Krimm
elbein
, N.,
61-FD
-7Kri
shna
, Y.,
11-AM
T-2/G
T-2Kri
shna
moort
hy, S
., 28
6-PDL
-13Kri
shna
murth
y, R.,
272
-ASE-4
Kroeb
er, S
., 26
0-AA-3
8Kro
nhau
s, I.,
144
-PDL-7
Kronin
ger, C
., 13
6-FD-1
5Kro
o, I.,
8-AF
M-1,
249
-FT-1
Kroze
l, J.,
142-M
ST-6
Krueg
er, P.
, 62-F
D-8Kru
eger,
W.,
198-A
TIO-19
Krüge
r, W.,
57-CF
D-7, 1
05-M
ST-5
Krumb
ein, A
., 61
-FD-7
Krumm
e, A.,
13-A
PA-2
Krus,
P., 2
83-M
AO-10
Kryu
kov,
I., 1
93-AP
A-21
Kucu
kcos
kun,
K., 7
9-AA-1
3Kü
gler, M
., 12
8-ATIO
-14Ku
hn, T
., 88
-APA-1
0Ku
lkarni
, M.,
252-M
AO-9
Kuma
r, D.,
234-A
PA-26
Kuma
r, R.,
118-A
FM-7,
174
-FD-20
Kuma
r, S.,
234-A
PA-26
Kuma
r, V.,
65-M
ST-3,
142
-MST
-6Ku
ntz, D
., 34
-TP-1
Kunz
, D.,
43-AF
M-3
Kuo,
C., 1
53-AA
-23Ku
relek
, J.,
100-F
D-11
Kurtz
, J.,
46-AM
T-4/G
T-4Ku
rz, H
., 20
9-FD-2
4Ku
tay, A
., 66
-MST
-4, 8
3-AFM
-5, 1
18-AF
M-7,
2
94-AM
T-14/
GT-15
Kutz,
D.,
158-A
MT-9/
GT-9
Kwon
, O.,
133-C
FD-16
La Ro
cca, G
., 17
6-MAO
-5La
caze
, G.,
244-C
FD-29
Lach
enme
ier, T
., 16
7-BAL
-1La
chow
ski, F
., 37
-AA-6
Laco
r, C.,
152-A
A-22
Lacy,
D.,
87-AP
A-9La
fage,
R., 4
2-ACD
-1La
ffay,
P., 3
-AA-1
Laffe
rty, J
., 10
3-ITA
R-1La
i, D.,
237-A
SE-3,
272
-ASE-4
Lajús
, F.,
5-AA-3
, 80-A
A-14
Lam,
T., 2
17-TP
-11La
mbert
, A.,
100-F
D-11
Lamm
el, O
., 26
6-AMT
-13/G
T-13
Lamp
inen,
M., 1
39-FD
-18La
ncas
ter, J
., 15
8-AMT
-9/GT
-9La
ndma
n, D.
, 294
-AMT-1
4/GT
-15La
ndrum
, B.,
30-M
ST-1,
265
-ACD-7
Land
rum, D
., 25
0-LTA
-1La
ndry,
R., 2
15-M
ST-10
Land
ry, S
., 16
4-ATIO
-15, 1
66-AT
IO-17
, 197
-ATIO
-18La
ng, S
., 20
0-BAL
-2La
ngtry
, R.,
61-FD
-7La
rbi, S
., 30
5-CFD
-35La
rchev
eque
, L.,
154-A
A-24
Latz,
J., 1
61-AP
A-18,
267
-APA-2
9La
urend
eau,
F., 6
0-FD-6
/PDL
-2La
val, J
., 98
-CFD-1
2La
vin, T
., 11
9-AFM
-8La
wren
ce, J
., 5-A
A-3, 2
27-AA
-32La
zarus
, S.,
117-A
CD-3
Le B
ras, S
., 22
9-AA-3
4Le
Garr
ec, T
., 18
7-AA-2
8Le
Rallic
, M.,
80-AA
-14Le
bofsk
y, S.
, 124
-APA-1
5Le
brun,
F., 4
6-AMT
-4/GT
-4Le
e, D.
, 12-A
PA-1
Lee,
H., 1
6-ATIO
-1Le
e, K.,
51-AT
IO-5,
84-AF
M-6,
162-A
PA-19
, 166
-ATIO-
17Le
e, S.
, 154
-AA-24
Lee,
T., 1
07-PD
L-4Le
fantzi
, S.,
139-F
D-18
Lege
r, T.,
306-C
FD-36
Leib,
S.,
79-AA
-13, 2
27-AA
-32Le
ifsso
n, L.,
307
-MAO
-12Le
le, S
., 80
-AA-14
Lemo
nds,
T., 2
93-AC
D-8Le
ng, M
., 35
-TP-2,
145
-TP-7
Léon
, O.,
60-FD
-6/PD
L-2, 2
28-AA
-33Le
ong,
C., 6
3-FD-9
, 101
-FD-12
Leon
ov, S
., 10
7-PDL
-4, 1
44-PD
L-7Le
opold
, F.,
45-AM
T-3/G
T-3Le
sieutr
e, D.
, 269
-APA-3
1Le
trenn
e, G.
, 167
-BAL-1
Leun
g, R.,
38-A
A-7Le
vin, D
., 69
-TP-4,
203
-CFD-2
3Le
Vine,
M., 4
2-ACD
-1, 5
2-ATIO
-6, 1
98-AT
IO-19
Lewi
s, D.
, 103
-ITAR
-1Le
wis,
M., 1
0-AMT
-1/GT
-1, 3
03-CF
D-33
Lewi
s, R.,
108
-TP-5
Lewi
s, S.
, 34-T
P-1Le
wis,
T., 1
7-ATIO
-2Le
yva,
I., 2
7-FD-3
Li, F.
, 9-AF
M-2,
99-F
D-10,
137
-FD-16
Li, G
., 29
6-APA
-35Li,
H.,
144-P
DL-7,
180
-PDL-8
/APA
-20, 2
71-AP
A-33
Li, J.
, 24-C
FD-4,
92-A
TIO-10
Li, M
., 21
4-MST
-9Li,
S.,
26-FD
-2, 1
16-AA
-20Li,
V., 2
9-MAO
-1, 1
76-M
AO-5
126
Auth
or/S
essio
n Ch
air In
dex
Li, W
., 89
-APA-1
1, 2
41-CF
D-26,
261
-AA-39
Li, X
., 81
-AA-15
, 112
-AA-16
, 116
-AA-20
Li, Z.
, 69-T
P-4, 1
78-M
ST-8
Liang
, C.,
308-M
AO-13
Libsig
, M.,
47-AP
A-5Lib
urdy,
J., 2
34-AP
A-26
Liebe
ck, R
., 12
3-APA
-14Lil
lard,
R., 6
9-TP-4
, 172
-CFD-2
0Lil
ler, T
., 15
-APA-4
Lim, C
., 26
5-ACD
-7Lim
, D.,
42-AC
D-1, 1
90-AC
D-5Lim
bach
, C.,
60-FD
-6/PD
L-2Lin
, H.,
265-A
CD-7
Lin, J
., 13
8-FD-1
7, 2
12-M
AO-6
Lin, P
., 20
2-CFD
-22Lin
, Q.,
241-C
FD-26
Lin, Y
., 46
-AMT-4
/GT-4
, 65-M
ST-3,
240
-ATIO
-23Lin
coln,
D.,
159-A
MT-10
/GT-1
0Lin
dsay
, K.,
238-A
TIO-21
Linke
, F.,
92-AT
IO-10
Liou,
M., 5
6-CFD
-6Lip
pert,
M.,
88-AP
A-10
Liston
, G.,
10-AM
T-1/G
T-1Lit
tle, J
., 60
-FD-6/
PDL-2
, 174
-FD-20
, 175
-FD-22
, 2
79-FD
-31Liu
, A.,
128-A
TIO-14
Liu, C
., 30
5-CFD
-35Liu
, D.,
85-AM
T-5/G
T-5Liu
, F., 3
3-PDL
-1/FD
-5, 45
-AMT-3
/GT-3
, 67-P
DL-3,
1
44-PD
L-7, 1
80-PD
L-8/A
PA-20
, 271
-APA-3
3,
285
-MST
-12Liu
, G.,
248-F
D-29
Liu, H
., 29
5-APA
-34Liu
, J.,
30-M
ST-1,
84-A
FM-6,
153
-AA-23
, 251
-MAO
-8Liu
, L.,
25-FD
-1, 3
1-MST
-2, 2
13-M
AO-7,
251
-MAO
-8Liu
, P.,
26-FD
-2, 4
7-APA
-5Liu
, Q.,
178-M
ST-8
Liu, R
., 12
8-ATIO
-14Liu
, S.,
173-F
D-19
Liu, T
., 25
-FD-1
Liu, X
., 3-A
A-1, 5
5-CFD
-5, 7
8-AA-1
2, 1
13-AA
-17Liu
, Y.,
49-AP
A-7, 1
85-AA
-26, 2
85-M
ST-12
Liu, Z
., 57
-CFD-7
, 141
-MAO
-4Liv
, A.,
18-AT
IO-3
Liveb
ardon
, T.,
185-A
A-26
Livne
, E.,
49-AP
A-7Llo
pis-Pa
scual,
A., 2
71-AP
A-33
Lo, K
., 19
3-APA
-21Lo
aec,
S., 2
72-AS
E-4Lo
bel, G
., 22
7-AA-3
2Lo
ckard
, D.,
3-AA-1
, 155
-AA-25
, 188
-AA-29
, 2
30-AA
-35, 2
59-AA
-37
Lofth
ouse
, A.,
160-A
PA-17
, 236
-APA-2
8, 3
05-CF
D-35
Loga
n, M.
, 190
-ACD-5
Lohr,
G.,
91-AT
IO-9
Lomb
ardi, A
., 21
3-MAO
-7Lo
ng, D
., 27
5-ATIO
-25Lo
ng, T
., 21
3-MAO
-7, 2
51-M
AO-8
Lope
s, L.,
112
-AA-16
, 155
-AA-25
Lópe
z, I.,
281
-GEPC
-1Ló
pez-M
orales
, M.,
55-CF
D-5Lo
seille
, A.,
23-CF
D-3, 1
14-AA
-18Lo
th, S
., 91
-ATIO
-9Lo
u, F.,
158
-AMT-9
/GT-9
Loum
an, R
., 13
8-FD-1
7Lo
we, K
., 46
-AMT-4
/GT-4
, 159
-AMT-1
0/GT
-10,
192
-AMT-1
2/GT
-12, 2
66-AM
T-13/
GT-13
Lowe
nberg
, M.,
122-A
PA-13
Loza
no, B
., 15
6-ACD
-4Lu
, F.,
246-F
D-27,
279
-FD-31
Lu, J
., 28
5-MST
-12Lu
ckne
r, R.,
237-A
SE-3
Luck
ring,
J., 1
60-AP
A-17
Ludw
ig, B
., 15
9-AMT
-10/G
T-10
Lued
ke, J
., 29
7-APA
-37Lu
kacz
yk, T
., 21
2-MAO
-6Lu
ke, E
., 41
-AA-10
, 81-A
A-15,
195
-APA-2
3Lu
mmer,
M.,
112-A
A-16
Lung
, T.,
169-C
FD-17
Luo,
H., 5
5-CFD
-5, 1
00-FD
-11, 1
73-FD
-19,
201
-CFD-2
1, 2
03-CF
D-23,
208
-FD-23
Luo,
L., 2
03-CF
D-23
Luo,
S., 3
3-PDL
-1/FD
-5, 6
7-PDL
-3, 1
44-PD
L-7,
180
-PDL-8
/APA
-20, 2
71-AP
A-33
Luo,
X., 1
78-M
ST-8
Lupo
glazo
ff, N
., 39
-AA-8
Lupp
, C.,
9-AFM
-2Lu
quet,
D.,
114-A
A-18
Lutz,
A., 1
81-PD
L-9/T
P-8Lu
tz, T.
, 249
-FT-1
Luxh
oj, J.
, 300
-ATIO
-29Lv,
Y., 2
42-CF
D-27
Lync
h, K.,
37-A
A-6, 2
66-AM
T-13/
GT-13
Lynn
, K.,
294-A
MT-14
/GT-1
5Ly
rintzi
s, A.,
37-A
A-6, 1
13-AA
-17, 2
45-CF
D-30
Lyu,
B., 3
8-AA-7
Ma, H
., 14
5-TP-7
Ma, P
., 26
-FD-2
Ma, Z
., 12
8-ATIO
-14Ma
chere
t, S.
, 216
-TP-10
/PDL
-10Ma
cMan
us, D
., 27
0-APA
-32Ma
dava
n, N.
, 281
-GEPC
-1Ma
ddale
na, L
., 86
-AMT-6
/GT-6
Madd
alon,
J., 1
7-ATIO
-2
Madd
en, T
., 67
-PDL-3
Maen
g, J.,
169
-CFD-1
7Ma
galha
es, P
., 28
3-MAO
-10Ma
gari,
P., 3
3-PDL
-1/FD
-5Ma
gin, T
., 34
-TP-1,
216
-TP-10
/PDL
-10, 2
17-TP
-11Ma
hade
van,
S., 3
08-M
AO-13
Maha
shab
de, A
., 92
-ATIO
-10, 1
97-AT
IO-18
Mahe
shwa
ri, A.,
52-A
TIO-6
Mahli
ch, S
., 27
5-ATIO
-25Ma
ierl, R
., 21
2-MAO
-6Ma
jić, F
., 78
-AA-12
, 235
-APA-2
7Ma
jumda
r, A.,
198-A
TIO-19
Maka
rov, B
., 24
3-CFD
-28Ma
lael, I
., 96
-CFD-1
0Ma
ldona
do, A
., 78
-AA-12
Malec
ki, T.
, 30-M
ST-1
Malick
, M.,
122-A
PA-13
Malik
, M.,
61-FD
-7, 2
02-CF
D-22
Malik
, W.,
16-AT
IO-1,
91-A
TIO-9,
198
-ATIO
-19Ma
linow
ski, M
., 28
0-FT-2
/GT-1
4Ma
llet,
M., 9
9-FD-1
0Ma
ngala
m, A.
, 9-AF
M-2,
124
-APA-1
5, 2
70-AP
A-32
Mang
ani, L
., 20
3-CFD
-23Ma
ni, K.
, 302
-CFD-3
2Ma
nkba
di, M
., 17
5-FD-2
2Ma
nkba
di, R.
, 79-A
A-13
Mano
ha, E
., 3-A
A-1, 1
55-AA
-25, 2
29-AA
-34,
230
-AA-35
, 259
-AA-37
Mano
salva
s, D.
, 271
-APA-3
3Ma
nsor,
S.,
12-AP
A-1Ma
nsou
r, N.,
58-CF
D-8, 2
88-TP
-13Ma
nsou
ri, N.
, 81-A
A-15
Mante
lli, M
., 35
-TP-2
Marai
s, K.,
156
-ACD-4
, 164
-ATIO
-15, 2
75-AT
IO-25
, 2
99-AT
IO-28
Marañ
on D
i Leo
, J.,
236-A
PA-28
March
iano,
R., 1
14-AA
-18Ma
rie, S
., 56
-CFD-6
Marin
eau,
E., 9
9-FD-1
0, 1
03-IT
AR-1
Marke
steijn
, A.,
6-AA-4
, 80-A
A-14
Marks
, C.,
191-A
MT-11
/GT-1
1Ma
rn, A.
, 151
-AA-21
Marqu
es, F
., 23
6-APA
-28Ma
rr, B.
, 238
-ATIO
-21Ma
rsan,
A., 2
27-AA
-32Ma
rsden
, O.,
4-AA-2
, 231
-AA-36
Marsh
, J.,
200-B
AL-2
Marsh
all, J
., 15
7-AFM
-9Ma
rshall
, P.,
85-AM
T-5/G
T-5Ma
rten,
D., 2
97-AP
A-37
Martin
, A.,
68-TP
-3, 1
08-TP
-5, 1
82-TP
-9Ma
rtin, P
., 12
0-AMT
-7/GT
-7
Martin
elli, L
., 57
-CFD-7
, 295
-APA-3
4Ma
rtinez
, A.,
101-F
D-12
Martin
ez, B
., 45
-AMT-3
/GT-3
, 47-A
PA-5
Martin
ez, S
., 14
5-TP-7
Martin
s, J.,
29-M
AO-1,
141
-MAO
-4, 2
52-M
AO-9,
3
07-M
AO-12
Mary,
I., 1
54-AA
-24Ma
sarat
i, P.,
84-AF
M-6
Maso
n, M.
, 217
-TP-11
Massa
, L.,
216-T
P-10/
PDL-1
0Ma
ssey,
K., 2
97-AP
A-37
Mastr
oddi,
F., 2
9-MAO
-1Ma
suda
, K.,
286-P
DL-13
Matay
oshi,
N.,
298-A
TIO-27
Mathe
r, J.,
273-A
SE-5
Mathe
w, J.
, 24-C
FD-4
Mathe
ws, E
., 25
5-PDL
-12Ma
thews
, J.,
3-AA-1
Matic
, P.,
102-F
D-13
Matsu
no, T
., 14
4-PDL
-7Ma
tsuno
, Y.,
51-AT
IO-5
Matto
s, B.
, 283
-MAO
-10, 3
07-M
AO-12
Matts
on, C
., 10
4-MAO
-3Ma
ughm
er, M
., 61
-FD-7
Mavri
plis,
D., 2
01-CF
D-21
Mavri
s, D.
, 37-A
A-6, 4
2-ACD
-1, 5
2-ATIO
-6, 5
3-ATIO
-7,
141
-MAO
-4, 1
42-M
ST-6,
156
-ACD-4
, 190
-ACD-5
, 1
98-AT
IO-19
, 213
-MAO
-7, 2
39-AT
IO-22
, 2
65-AC
D-7, 2
76-AT
IO-26
, 308
-MAO
-13Ma
y, G.
, 95-C
FD-9
Maye
r, R.,
92-AT
IO-10
, 197
-ATIO
-18Ma
zahe
ri, A.,
55-C
FD-5
McAlp
ine, A
., 37
-AA-6
Mcca
rthy,
P., 1
45-TP
-7Mc
Carth
y, P.,
259
-AA-37
McCla
in, S
., 19
6-ASE
-2Mc
Clure,
J., 1
32-CF
D-15
McCo
ll, C.,
83-A
FM-5
McCo
mas,
A., 2
35-AP
A-27
McCri
nk, M
., 26
8-APA
-30Mc
Danie
l, D.,
160-A
PA-17
McDa
niel, J
., 24
4-CFD
-29Mc
Dona
ld, J.
, 304
-CFD-3
4Mc
Dona
ld, R.
, 82-A
CD-2,
240
-ATIO
-23Mc
Grath
, B.,
123-A
PA-14
McGu
irk, J
., 24
-CFD-4
McIne
rny, S
., 40
-AA-9
Mcint
yre, T
., 34
-TP-1
McKe
on, B
., 16
2-APA
-19Mc
Kierna
n, G.
, 28-F
D-4Mc
Kinley
, R.,
40-AA
-9Mc
Laug
hlin,
D., 3
9-AA-8
, 40-A
A-9
McLa
ughli
n, T.,
12-A
PA-1,
125
-APA-1
6Mc
Maste
rs, R.
, 35-T
P-2Mc
Mulla
n, W.
, 24-C
FD-4,
98-C
FD-12
Mcna
lly, D
., 29
8-ATIO
-27Mc
Partla
nd, M
., 51
-ATIO
-5, 2
98-AT
IO-27
McWa
ters,
M., 4
5-AMT
-3/GT
-3Me
ad, C
., 22
7-AA-3
2Me
ase,
K., 2
75-AT
IO-25
Meck
stroth
, C.,
29-M
AO-1
Mede
iros,
F., 2
43-CF
D-28
Mede
iros,
M., 2
30-AA
-35Me
dina,
A., 2
68-AP
A-30
Medw
ell, P
., 24
4-CFD
-29Me
hman
i, A.,
251-M
AO-8
Mehta
, P.,
214-M
ST-9
Mei, D
., 18
0-PDL
-8/AP
A-20
Mei, Q
., 25
3-MST
-11Me
ier, W
., 26
6-AMT
-13/G
T-13
Meink
e, M.
, 26-F
D-2, 3
8-AA-7
, 41-A
A-10,
79-A
A-13,
8
0-AA-1
4, 2
29-AA
-34, 3
05-CF
D-35
Melin
, T.,
283-M
AO-10
Mend
enha
ll, M.
, 269
-APA-3
1Me
ndon
ca, F
., 23
0-AA-3
5Me
ndoz
a, J.,
185
-AA-26
Mene
veau
, C.,
98-CF
D-12,
171
-CFD-1
9Me
ng, X
., 33
-PDL-1
/FD-5
, 144
-PDL-7
, 1
80-PD
L-8/A
PA-20
, 271
-APA-3
3Me
rle, X
., 11
3-AA-1
7Me
rrick,
J., 1
95-AP
A-23
Mery,
F., 2
62-AA
-40Me
smer,
B.,
212-M
AO-6,
283
-MAO
-10Me
ssac,
A., 1
76-M
AO-5,
251
-MAO
-8Me
yer, T
., 18
1-PDL
-9/TP
-8Me
yers,
J., 1
81-PD
L-9/T
P-8Me
yers,
T., 1
52-AA
-22, 2
97-AP
A-37
Mich
ael, J
., 18
1-PDL
-9/TP
-8Mi
chal,
T., 2
3-CFD
-3Mi
chel,
U.,
189-A
A-30
Mich
ou, Y
., 46
-AMT-4
/GT-4
, 192
-AMT-1
2/GT
-12Mi
cka,
D., 3
3-PDL
-1/FD
-5Mi
haes
cu, M
., 96
-CFD-1
0, 1
12-AA
-16Mi
lagre
da Fo
nsec
a, I.,
119
-AFM-
8Mi
lan, P
., 60
-FD-6/
PDL-2
Milan
ese,
F., 3
5-TP-2
Miles
, R.,
60-FD
-6/PD
L-2, 8
6-AMT
-6/GT
-6,
143
-PDL-6
, 255
-PDL-1
2Mi
ller, B
., 52
-ATIO
-6, 6
5-MST
-3Mi
ller, D
., 14
2-MST
-6, 2
82-LT
A-2Mi
ller, J
., 28
-FD-4
Mille
r, S.,
40-AA
-9, 1
53-AA
-23Mi
lls, B
., 85
-AMT-5
/GT-5
, 280
-FT-2/
GT-14
Mills,
M.,
120-A
MT-7/
GT-7
127
Auth
or/S
essio
n Ch
air In
dex
Milut
inovic
, D.,
91-AT
IO-9,
198
-ATIO
-19Mi
mani,
A., 2
31-AA
-36Mi
n, S.
, 42-A
CD-1,
156
-ACD-4
Minc
u, D.
, 154
-AA-24
, 187
-AA-28
Mine
ck, R
., 18
8-AA-2
9Mi
ngion
e, G.
, 115
-AA-19
Minis
ci, E.
, 214
-MST
-9Mi
nqian
g, Y.,
280
-FT-2/
GT-14
Miroc
hnitc
henk
o, V.,
190
-ACD-5
Misa
ka, T
., 19
6-ASE
-2Mi
tchell
, K.,
116-A
A-20
Mitsi
ngas
, C.,
107-P
DL-4
Mitsu
hash
i, R.,
293-A
CD-8
Mitta
l, A.,
15-AP
A-4, 2
34-AP
A-26,
297
-APA-3
7Mi
ttal, R
., 98
-CFD-1
2, 1
71-CF
D-19
Mock
ett, C
., 30
6-CFD
-36Mo
ckus
, L.,
239-A
TIO-22
Moell
er, T.
, 67-P
DL-3,
144-P
DL-7,
216-T
P-10/
PDL-1
0,
244
-CFD-2
9Mo
han,
A., 3
02-CF
D-32
Mohit
e, P.,
234
-APA-2
6Mo
in, P.
, 202
-CFD-2
2Mo
ini-Ye
kta, S
., 49
-APA-7
Molin
aro, N
., 29
7-APA
-37Mo
ntalvo
, C.,
157-A
FM-9
Monte
l, M.,
8-AFM
-1Mo
olcha
ndan
i, K.,
52-AT
IO-6
Moore
, M.,
54-AT
IO-8,
93-A
TIO-11
, 127
-ATIO
-13,
276
-ATIO
-26Mo
ored,
K., 1
00-FD
-11Mo
r-Yos
sef,
Y., 1
33-CF
D-16
Morar
u, G.
, 103
-ITAR
-1Mo
reau,
A., 7
7-AA-1
1, 1
52-AA
-22Mo
reau,
D., 1
52-AA
-22, 2
31-AA
-36Mo
reau,
E., 3
3-PDL
-1/FD
-5, 1
80-PD
L-8/A
PA-20
Morea
u, S.
, 3-AA
-1, 7
9-AA-1
3, 8
1-AA-1
5, 1
15-AA
-19,
152
-AA-22
, 185
-AA-26
, 187
-AA-28
, 227
-AA-32
Morei
ra, F.
, 9-AF
M-2,
241
-CFD-2
6Mo
relli,
E., 1
18-AF
M-7
Morga
n, P.,
102
-FD-13
Morga
n, R.,
34-T
P-1Mo
rikaw
a, Y.,
270
-APA-3
2Mo
rris, P
., 4-A
A-2, 4
0-AA-9
, 263
-AA-41
Morris
, S.,
38-AA
-7Mo
rrisse
y, P.,
108
-TP-5
Morsb
ach,
C., 1
33-CF
D-16
Morte
nsen
, C.,
209-F
D-24
Morto
n, S.
, 160
-APA-1
7, 1
74-FD
-20Mo
ses J
ohn C
hristy
Appo
lo, P.
, 67-P
DL-3
Moss,
M.,
308-M
AO-13
Mott,
D.,
102-F
D-13
Motte
r, M.,
165-A
TIO-16
, 199
-ATIO
-20
Mouri
ng, C
., 28
1-GEP
C-1Mo
vahe
d, P.,
211
-FD-26
Moye
s, A.,
137
-FD-16
Mueh
leise
n, R.,
262
-AA-40
Mueh
ler-Va
hl, H
., 10
1-FD-1
2Mu
eller,
F., 2
03-CF
D-23
Muell
er, J.
, 131
-CFD-1
4Mu
eller-
Vahl,
H.,
208-F
D-23
Mujum
dar, P
., 57
-CFD-7
Mukh
opad
hyay
, V.,
214-M
ST-9
Mulan
i, S.,
29-M
AO-1
Mulla
ne, M
., 19
3-APA
-21Mu
llene
rs, K.
, 50-A
PA-8,
235
-APA-2
7Mu
nday
, P.,
101-F
D-12
Mund
is, N
., 13
2-CFD
-15Mu
nera
Savin
o, F.,
8-AF
M-1,
249
-FT-1
Munju
lury,
R., 2
83-M
AO-10
Muns
on, M
., 13
6-FD-1
5Mu
rari, K
., 15
9-AMT
-10/G
T-10
Muray
ama,
M., 2
29-AA
-34, 2
30-AA
-35Mu
riel G
racia,
M.,
113-A
A-17
Murm
an, S
., 21
-CFD-1
, 96-C
FD-10
, 201
-CFD-2
1,
205
-CFD-2
5Mu
rphy,
C., 5
2-ATIO
-6, 6
5-MST
-3Mu
rray,
H., 1
14-AA
-18, 1
87-AA
-28Mu
rray,
J., 1
3-APA
-2, 2
97-AP
A-37
Murra
y, N.
, 80-A
A-14
Murra
y, W.
, 158
-AMT-9
/GT-9
Murrie
ta Me
ndoz
a, A.,
18-A
TIO-3
Musca
rello,
V., 8
4-AFM
-6Mu
siak,
J., 2
75-AT
IO-25
Muslu
bas,
Y., 5
7-CFD
-7Mu
yimbw
a, T.,
282
-LTA-2
Myos
e, R.,
27-F
D-3, 1
75-FD
-22Na
garaj
an, B
., 16
-ATIO
-1Na
huis,
R., 1
3-APA
-2Na
itoh,
K., 1
82-TP
-9Na
jafi, A
., 10
4-MAO
-3Na
jian A
sl, R.
, 283
-MAO
-10Na
kasa
to, K.
, 270
-APA-3
2Na
kash
ima,
T., 2
70-AP
A-32
Nalci,
M.,
66-M
ST-4
Nalla
pane
ni, S
., 35
-TP-2
Namb
a, M.
, 152
-AA-22
Namu
ra, N
., 12
5-APA
-16Na
nce,
D., 2
62-AA
-40Na
polita
no, M
., 43
-AFM-
3Na
rayan
aswa
my, V
., 27
-FD-3,
143
-PDL-6
, 174
-FD-20
Nark,
D.,
116-A
A-20
Narki
ewicz
, J.,
30-M
ST-1
Natar
ajan,
K., 1
53-AA
-23, 2
27-AA
-32Na
wroth
, H.,
27-FD
-3
Naye
ri, C.,
26-F
D-2, 2
97-AP
A-37
Neife
ld, A.
, 39-A
A-8Ne
ilan,
J., 1
65-AT
IO-16
, 199
-ATIO
-20Ne
ilsen,
T., 4
0-AA-9
Neitz
el, K.
, 69-T
P-4Ne
lson,
C., 4
9-APA
-7Ne
lson,
M., 1
14-AA
-18, 1
59-AM
T-10/
GT-10
, 187
-AA-28
Neuh
art, D
., 18
8-AA-2
9Ne
ville,
A., 2
46-FD
-27Ne
wcam
p, J.,
249
-FT-1
Newm
an, J
., 95
-CFD-9
, 170
-CFD-1
8, 3
05-CF
D-35
Ng, H
., 18
-ATIO
-3, 9
2-ATIO
-10Ng
uyen
, D.,
66-M
ST-4
Nguy
en, L
., 79
-AA-13
Nguy
en, M
., 88
-APA-1
0, 1
43-PD
L-6Ng
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, N.,
49-AP
A-7, 1
24-AP
A-15
Nicho
ls, D
., 29
7-APA
-37Nic
hols,
J., 4
-AA-2,
39-A
A-8, 1
53-AA
-23Nic
olosi,
F., 8
-AFM-
1, 1
3-APA
-2, 1
04-M
AO-3
Niede
rmeie
r, D.,
31-M
ST-2
Nieto,
B.,
234-A
PA-26
Nigam
, N.,
284-M
AO-11
Nikba
y, M.
, 308
-MAO
-13Nis
hida,
H., 1
44-PD
L-7Nis
hikaw
a, H.
, 55-C
FD-5,
56-C
FD-6
Niu, J
., 24
4-CFD
-29Niu
, W.,
215-M
ST-10
Nodé
-Lang
lois,
T., 1
12-AA
-16, 1
87-AA
-28No
elting
, S.,
188-A
A-29
Nojim
a, Y.,
182
-TP-9
Noll,
B., 1
85-AA
-26No
mpeli
s, I.,
246
-FD-27
, 256
-TP-12
Nomu
ra, S
., 69
-TP-4
Nono
mura,
T., 6
0-FD-6
/PDL
-2, 1
14-AA
-18,
130
-CFD-1
3, 1
69-CF
D-17
Nords
trom,
J., 1
32-CF
D-15,
242
-CFD-2
7No
tt, J.
, 167
-BAL-1
, 200
-BAL-2
Nouz
awa,
T., 2
70-AP
A-32
Nova
ra, M
., 15
9-AMT
-10/G
T-10
Novik
ov, A
., 99
-FD-10
Nowa
k, M.
, 128
-ATIO
-14Nt
emos
, G.,
202-C
FD-22
O’Br
ien, D
., 15
-APA-4
, 295
-APA-3
4O’
Brien
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151-A
A-21
O’Br
ien, W
., 15
9-AMT
-10/G
T-10
O’By
rne, S
., 11
-AMT-2
/GT-2
, 46-A
MT-4/
GT-4,
1
21-AM
T-8/F
D-14/
TP-6/
GT-8
O’Co
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C., 9
1-ATIO
-9O’
Neill,
W.,
35-TP
-2O’
Reilly
, C.,
78-AA
-12, 2
35-AP
A-27
O’Su
llivan
, S.,
53-AT
IO-7
Obay
ashi,
S.,
125-A
PA-16
, 196
-ASE-2
Oberl
eithn
er, K.
, 266
-AMT-1
3/GT
-13Oc
heltre
e, C.,
89-A
PA-11
, 251
-MAO
-8, 2
96-AP
A-35
Ochie
ng, W
., 19
8-ATIO
-19Oe
felein
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244-C
FD-29
Ogas
awara
, T.,
68-TP
-3Og
awa,
S., 2
86-PD
L-13
Ojed
a, S.
, 95-C
FD-9
Okad
a, Y.,
270
-APA-3
2Ok
amoto
, T.,
182-T
P-9Ok
olo, W
., 8-A
FM-1,
273
-ASE-5
Ol, M
., 12
5-APA
-16, 2
34-AP
A-26
Olejn
iczak
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69-TP
-4Ol
iveira
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119-A
FM-8
Olive
r, J.,
104-M
AO-3
Olivi
ero, N
., 13
7-FD-1
6Ol
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S., 1
3-APA
-2, 2
96-AP
A-35
Olliv
ier G
ooch
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21-CF
D-1, 2
3-CFD
-3, 1
31-CF
D-14
Olse
n, M.
, 172
-CFD-2
0Ol
son,
E., 2
52-M
AO-9
Olso
n, M.
, 240
-ATIO
-23Ol
son,
R., 4
3-AFM
-3Om
ar, F.
, 51-A
TIO-5
Omidy
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68-TP
-3On
ishi, K
., 27
0-APA
-32Or
avec
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273-A
SE-5
Orda
z, I.,
14-A
PA-3
Orr, M
., 15
6-ACD
-4Or
ra, T.
, 128
-ATIO
-14, 2
12-M
AO-6
Osma
n, A.,
178
-MST
-8Os
trikov
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115-A
A-19
Otsu
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144-P
DL-7
Overm
eyer,
A., 1
20-AM
T-7/G
T-7Ow
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J., 1
96-AS
E-2Oy
ama,
A., 1
14-AA
-18Oz
a, U.
, 22-C
FD-2
Ozca
n, M.
, 265
-ACD-7
Özge
n, S.
, 97-C
FD-11
Oztek
in, A.
, 164
-ATIO
-15Pa
ck, J
., 27
4-ATIO
-24Pa
ck M
elton
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279-F
D-31
Pado
is, T.
, 3-AA
-1Pa
gani,
C., 2
30-AA
-35Pa
ge, G
., 24
-CFD-4
Page
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276-A
TIO-26
Pagli
one,
P., 1
28-AT
IO-14
Pak,
C., 9
-AFM-
2, 1
41-M
AO-4
Palac
ios, F
., 13
3-CFD
-16, 2
04-CF
D-24,
271
-APA-3
3,
283
-MAO
-10Pa
lla, A
., 10
7-PDL
-4Pa
lmer,
E., 5
1-ATIO
-5Pa
lmer,
G.,
108-T
P-5Pa
lmier
i, F.,
46-AM
T-4/G
T-4
Palop
o, K.,
142
-MST
-6Pa
luch,
B., 1
3-APA
-2Pa
lumbo
, R.,
164-A
TIO-15
Pan,
J., 2
1-CFD
-1Pa
n, Q.
, 145
-TP-7
Panc
hal, J
., 52
-ATIO
-6Pa
ncha
l, K.,
250-L
TA-1
Pand
a, J.,
99-F
D-10
Pand
are, A
., 20
1-CFD
-21Pa
ndya
, S.,
305-C
FD-35
Pane
rai, F
., 28
8-TP-1
3Pa
nesi,
M.,
69-TP
-4Pa
nkrat
ov, I
., 18
7-AA-2
8Pa
nt, R.
, 282
-LTA-2
Papa
dimitri
ou, C
., 28
3-MAO
-10Pa
padim
itriou
, D.,
283-M
AO-10
Papa
georg
io, E.
, 128
-ATIO
-14Pa
pamo
schou
, D.,
227-A
A-32,
264
-AA-42
Papa
thakis
, K.,
240-A
TIO-23
Paran
in, G
., 11
5-AA-1
9Pa
rdowi
tz, B
., 17
3-FD-1
9Pa
rent,
B., 2
16-TP
-10/P
DL-10
Paren
te, A.
, 216
-TP-10
/PDL
-10Pa
rish,
E., 5
8-CFD
-8Pa
rk, G
., 13
9-FD-1
8Pa
rk, J.
, 202
-CFD-2
2, 2
42-CF
D-27,
251
-MAO
-8,
296
-APA-3
5Pa
rk, M
., 14-A
PA-3,
23-CF
D-3, 9
7-CFD
-11, 1
60-AP
A-17
Park,
S.,
235-A
PA-27
Parke
, B.,
51-AT
IO-5
Parke
r, P.,
294-A
MT-14
/GT-1
5Pa
rry, A
., 37
-AA-6
Parso
ns, N
., 69
-TP-4
Paruc
huri,
C., 3
-AA-1,
38-A
A-7, 7
9-AA-1
3, 1
52-AA
-22Pa
scarel
la, D
., 16
4-ATIO
-15Pa
schere
it, C.,
27-F
D-3, 2
97-AP
A-37
Pasco
, Y.,
227-A
A-32
Pasili
ao, C
., 12
-APA-1
, 22-C
FD-2,
90-A
PA-12
Passe
, B.,
162-A
PA-19
Pasto
relli,
V., 7
7-AA-1
1Pa
tel, S
., 24
-CFD-4
Pater
son,
E., 2
6-FD-2
Patil,
M.,
9-AFM
-2, 3
0-MST
-1, 2
52-M
AO-9
Patte
rson,
A., 1
57-AF
M-9
Patte
rson,
J., 2
14-M
ST-9
Patte
rson,
M., 1
27-AT
IO-13
Paul,
R., 2
35-AP
A-27
Paula
, A.,
307-M
AO-12
Pauz
, V.,
229-A
A-34
Pawl
etta,
T., 1
77-M
ST-7
Paya
n, A.,
53-A
TIO-7,
239
-ATIO
-22Pe
ake,
N., 3
-AA-1,
260
-AA-38
128
Auth
or/S
essio
n Ch
air In
dex
Pearc
e, R.,
52-A
TIO-6
Pech
livan
oglou
, G.,
26-FD
-2, 2
97-AP
A-37
Pede
rson,
C., 1
74-FD
-20Pe
drama
sl, N
., 64
-MAO
-2Pe
i, J.,
119-A
FM-8
Pei, P
., 27
6-ATIO
-26Pe
inke,
J., 5
0-APA
-8, 2
71-AP
A-33
Pelle
tier, D
., 58
-CFD-8
, 204
-CFD-2
4, 3
04-CF
D-34
Peltie
r, S.,
266-A
MT-13
/GT-1
3Pe
ng, D
., 19
7-ATIO
-18Pe
ng, J
., 19
0-ACD
-5Pe
ng, S
., 6-A
A-4, 1
15-AA
-19, 1
54-AA
-24Pe
ng, W
., 19
8-ATIO
-19Pe
ng, X
., 53
-ATIO
-7Pe
rcin,
M., 9
7-CFD
-11, 2
08-FD
-23Pe
reira,
D.,
236-A
PA-28
Perez
, R.,
141-M
AO-4,
267
-APA-2
9Pe
riaux
, J.,
180-P
DL-8/
APA-2
0Pe
roomi
an, O
., 24
5-CFD
-30Pe
rsson
, P.,
170-C
FD-18
Peter
, J.,
173-F
D-19
Peter
s, B.
, 306
-CFD-3
6Pe
ters,
C., 8
6-AMT
-6/GT
-6Pe
terse
n, S.
, 282
-LTA-2
Peter
sson,
Ö, 2
12-M
AO-6
Pfaen
der, H
., 53
-ATIO
-7, 2
39-AT
IO-22
Pfifer
, H.,
157-A
FM-9
Pianta
nida,
S., 5
-AA-3,
189
-AA-30
Piao,
Y., 2
44-CF
D-29
Pierre
, D.,
154-A
A-24
Pilon
, A.,
153-A
A-23
Pimen
ta, B
., 77
-AA-11
Pini, M
., 13
3-CFD
-16Pin
ier, J
., 88
-APA-1
0, 1
23-AP
A-14
Pinon
-Fisch
er, O
., 14
2-MST
-6Pio
t, E.,
262
-AA-40
Pipern
i, P.,
104-M
AO-3,
213
-MAO
-7, 2
84-M
AO-11
Planc
k, C.,
234
-APA-2
6Ple
mmon
s, D.
, 11-A
MT-2/
GT-2
Ploetn
er, K.
, 52-A
TIO-6,
53-A
TIO-7
Pogg
ie, J.
, 102
-FD-13
, 211
-FD-26
, 286
-PDL-1
3,
306
-CFD-3
6Po
insot,
T., 1
85-AA
-26Po
lacze
k, J.,
280
-FT-2/
GT-14
Pome
roy, B
., 87
-APA-9
Pons
-Prat,
J., 1
80-PD
L-8/A
PA-20
Poole
, D.,
64-M
AO-2,
125
-APA-1
6, 2
83-M
AO-10
Popie
, V.,
262-A
A-40
Popo
v, I.,
33-P
DL-1/
FD-5
Porne
t, C.,
53-A
TIO-7
Poros
eva,
S., 9
6-CFD
-10, 2
05-CF
D-25
Porte
ous,
A., 9
6-CFD
-10
Porum
bel, I
., 96
-CFD-1
0Po
st, M
., 64
-MAO
-2, 1
62-AP
A-19
Pott-P
ollen
ske,
M., 3
-AA-1,
230
-AA-35
Potte
r, C.,
141-M
AO-4
Povin
elli, L
., 28
1-GEP
C-1Po
wers,
R., 4
0-AA-9
Prabh
u, D.
, 102
-FD-13
, 108
-TP-5
Prach
ar, A.
, 233
-APA-2
5Pra
deep
, A.,
57-CF
D-7Pra
sad,
R., 1
2-APA
-1, 2
05-CF
D-25
Precu
p, N.
, 49-A
PA-7
Priolo
, F.,
9-AFM
-2Prö
bstin
g, S.
, 38-A
A-7Pru
ett, B
., 62
-FD-8,
175
-FD-22
Pruis,
M.,
237-A
SE-3,
272
-ASE-4
Przulj
, V.,
243-C
FD-28
Pullia
m, T.
, 136
-FD-15
Pytel
, D.,
34-TP
-1Qi
, B.,
145-T
P-7Qi
, X.,
284-M
AO-11
Qian
, J.,
285-M
ST-12
Qiao
, W.,
151-A
A-21,
260
-AA-38
, 267
-APA-2
9Qi
u, S.
, 204
-CFD-2
4Qi
u, X.
, 285
-MST
-12Qu
, Q.,
26-FD
-2, 4
7-APA
-5Qu
aglia
, M.,
187-A
A-28
Quall
s, G.
, 165
-ATIO
-16, 1
99-AT
IO-20
Quara
nta, G
., 84
-AFM-
6Qu
eiroz
, R.,
7-AA-5
Quinl
an, J
., 24
4-CFD
-29Qu
inn, M
., 45
-AMT-3
/GT-3
Quint
o, P.,
158
-AMT-9
/GT-9
Quix,
H.,
85-AM
T-5/G
T-5Qu
on, L
., 91
-ATIO
-9Ra
dyisy
ewsk
i, P.,
30-M
ST-1
Raffe
l, M.,
192-A
MT-12
/GT-1
2Ra
gab,
S., 2
36-AP
A-28
Ragn
i, D.,
37-AA
-6, 2
86-PD
L-13
Rahm
an, M
., 13
9-FD-1
8Ra
j, P., 1
76-M
AO-5,
251-M
AO-8,
265-A
CD-7,
296-A
PA-35
Rajag
opala
n, R.,
243
-CFD-2
8Ra
jput,
P., 2
33-AP
A-25
Ralla
bhan
di, S
., 14
-APA-3
, 89-A
PA-11
Rama
chan
dran,
A., 2
7-FD-3
, 28-F
D-4Ra
mamo
orthy
, K.,
275-A
TIO-25
Rama
murti,
R., 4
8-APA
-6, 2
33-AP
A-25
Rama
n, G.
, 262
-AA-40
Rama
n, V.,
304
-CFD-3
4Ra
mesh
, N.,
67-PD
L-3Ra
mirez
, W.,
38-AA
-7Ra
ncou
rt, D
., 21
3-MAO
-7, 2
76-AT
IO-26
Rand
, J.,
200-B
AL-2
Rand
t, N.
, 52-A
TIO-6,
128
-ATIO
-14Ra
o, A.,
126
-ATIO
-12, 1
56-AC
D-4Ra
shad
, R.,
204-C
FD-24
Ratha
krish
nan,
B., 2
44-CF
D-29
Ratha
krish
nan,
E., 5
0-APA
-8Ra
ulede
r, J.,
236-A
PA-28
Rautm
ann,
C., 7
9-AA-1
3, 1
55-AA
-25Ra
vetta
, P.,
188-A
A-29
Ray,
J., 1
39-FD
-18Ra
zi, P.
, 58-C
FD-8
Reard
on, J
., 46
-AMT-4
/GT-4
Reard
on, S
., 17
7-MST
-7Re
asor,
D.,
22-CF
D-2Re
donn
et, S
., 15
5-AA-2
5, 2
61-AA
-39Re
ed, D
., 26
2-AA-4
0Re
ed, H
., 61
-FD-7,
137
-FD-16
, 247
-FD-28
Reed
er, M
., 15
8-AMT
-9/GT
-9, 1
95-AP
A-23
Reeg
er, J.
, 141
-MAO
-4Re
ge, A
., 48
-APA-6
Rehm
anjan
, U.,
128-A
TIO-14
Reich
e, N.
, 39-A
A-8, 1
12-AA
-16Re
ichma
n, B.
, 40-A
A-9Re
imer,
L., 5
7-CFD
-7Re
issne
r, F.,
101-F
D-12
Reist
, T.,
267-A
PA-29
Reme
s, B.
, 97-C
FD-11
Ren,
Y., 2
1-CFD
-1, 8
4-AFM
-6, 2
14-M
ST-9,
2
41-CF
D-26,
248
-FD-29
Rend
all, T
., 64
-MAO
-2, 1
25-AP
A-16,
283
-MAO
-10Re
nder,
P., 8
8-APA
-10Re
nner,
A., 1
04-M
AO-3
Renn
ie, M
., 88
-APA-1
0, 1
43-PD
L-6, 2
55-PD
L-12
Rey,
C., 4
7-APA
-5Re
y, M.
, 262
-AA-40
Reya
z Ahm
ed, A
., 50
-APA-8
Reyn
olds,
D., 3
1-MST
-2Re
ynold
s, T.,
51-A
TIO-5,
163
-ASE-1
Reza
Ahrab
i, B.,
95-CF
D-9, 1
22-AP
A-13
Rhew
, R.,
158-A
MT-9/
GT-9,
1
91-AM
T-11/
GT-11
, 294
-AMT-1
4/GT
-15Rh
oads
, J.,
259-A
A-37
Rhod
es, D
., 52
-ATIO
-6Ric
hards
on, J
., 15
7-AFM
-9Ric
hards
on, T
., 84
-AFM-
6, 2
12-M
AO-6
Rickli
ck, M
., 14
5-TP-7
Righi,
M.,
236-A
PA-28
, 278
-FD-30
Ringu
ette,
M., 1
00-FD
-11Rit
ter, M
., 57
-CFD-7
Ritz,
R., 2
2-CFD
-2, 9
6-CFD
-10Riv
iere,
P., 2
17-TP
-11Riz
zetta
, D.,
101-F
D-12
Rizzi,
A., 1
60-AP
A-17
Rizzi,
S.,
152-A
A-22
Röbe
n, T.,
265
-ACD-7
Robe
rtson
, G.,
174-F
D-20
Robin
son,
S., 3
1-MST
-2, 2
69-AP
A-31
Robin
son I
II, J.,
239
-ATIO
-22Ro
chlitz
, H.,
159-A
MT-10
/GT-1
0Ro
deba
ugh,
G., 1
73-FD
-19Ro
drigu
ez, Y
., 51
-ATIO
-5Ro
e, P.,
56-C
FD-6,
169
-CFD-1
7Ro
ger, M
., 79
-AA-13
, 81-A
A-15,
152
-AA-22
, 1
54-AA
-24, 1
87-AA
-28Ro
gers,
M.,
61-FD
-7Ro
gers,
S.,
233-A
PA-25
Rohlm
ann,
D., 8
7-APA
-9Ro
idl, B
., 41
-AA-10
Rolin
g, P.,
91-A
TIO-9
Roma
nelli,
G.,
203-C
FD-23
Rorie
, R.,
274-A
TIO-24
Rose
, C.,
107-P
DL-4
Rose
ma, C
., 90
-APA-1
2, 2
96-AP
A-35
Rose
mann
, H.,
178-M
ST-8
Rossi
an, L
., 23
1-AA-3
6Ro
ssign
ol, K.
, 231
-AA-36
Roth,
B.,
251-M
AO-8,
307
-MAO
-12Ro
thhaa
r, P.,
119-A
FM-8,
165
-ATIO
-16, 1
99-AT
IO-20
Roug
ier, T
., 25
9-AA-3
7Ro
usse
l, C.,
98-CF
D-12
Rouz
bar, R
., 24
4-CFD
-29Ro
we, P
., 15
8-AMT
-9/GT
-9Ro
wley
, C.,
136-F
D-15,
295
-APA-3
4Ro
y, A.,
246
-FD-27
Roy,
C., 3
0-MST
-1, 9
7-CFD
-11, 1
31-CF
D-14
Roy,
R., 1
72-CF
D-20
Roy,
S., 9
2-ATIO
-10, 2
75-AT
IO-25
Roy S
alam,
I., 1
90-AC
D-5Ro
yalty
, C.,
116-A
A-20
Ru, P
., 15
7-AFM
-9Ru
dnick
-Cohe
n, E.,
29-M
AO-1
Rudn
ik, R.
, 87-A
PA-9
Ruett
en, M
., 22
-CFD-2
, 96-C
FD-10
, 178
-MST
-8Ru
leva,
L., 1
93-AP
A-21
Ruma
nn, H
., 27
3-ASE
-5Ru
msey
, C.,
58-CF
D-8, 1
39-FD
-18, 1
72-CF
D-20,
2
08-FD
-23Ru
sak,
Z., 6
2-FD-8
, 173
-FD-19
Russe
ll, S.
, 141
-MAO
-4Ru
therfo
rd, M
., 88
-APA-1
0Sa
, J.,
235-A
PA-27
Sabe
tta, V
., 8-A
FM-1
Sadiq
ue, J
., 98
-CFD-1
2, 1
71-CF
D-19
Sado
vsky
, A.,
17-AT
IO-2
Sadra
ey, M
., 19
1-AMT
-11/G
T-11
Sadri
, V.,
62-FD
-8Sa
geba
um, M
., 25
2-MAO
-9Sa
heby
, E.,
267-A
PA-29
Sahin
, B.,
25-FD
-1Sa
hin, M
., 64
-MAO
-2Sa
hni, O
., 63
-FD-9
Sahu
, J.,
90-AP
A-12
Said,
M.,
167-B
AL-1,
200
-BAL-2
Saif U
llah K
halid
, M.,
133-C
FD-16
Saiki
a, B.
, 28-F
D-4Sa
ini, A
., 46
-AMT-4
/GT-4
, 267
-APA-2
9Sa
ka, P
., 88
-APA-1
0Sa
kurai
, T.,
66-M
ST-4
Salah
El D
in, I.
, 114
-AA-18
Salas
, P.,
115-A
A-19
Salee
m, M
., 17
4-FD-2
0Sa
lehian
, S.,
79-AA
-13Sa
lemi, L
., 28
-FD-4
Salin
as, M
., 84
-AFM-
6Sa
lton,
A., 4
0-AA-9
Salze
, E.,
231-A
A-36
Sama
nta, A
., 78
-AA-12
Sama
reh, J
., 68
-TP-3
Sama
ritano
, A.,
194-A
PA-22
Sami
my, M
., 33
-PDL-1
/FD-5
, 153
-AA-23
Samu
el, A.
, 240
-ATIO
-23Sa
ndbe
rg, M
., 51
-ATIO
-5Sa
ndbe
rg, R.
, 171
-CFD-1
9Sa
nders
, L.,
259-A
A-37
Sand
ham,
N.,
209-F
D-24
Sane
trik, M
., 12
4-APA
-15Sa
njaya
, D.,
95-CF
D-9Sa
njose
, M.,
227-A
A-32
Sank
aran,
V., 1
32-CF
D-15
Sano
, A.,
41-AA
-10Sa
ntos,
J., 3
0-MST
-1, 2
82-LT
A-2Sa
ntos,
L., 1
17-AC
D-3, 2
13-M
AO-7
Santo
s, P.,
43-A
FM-3
Santo
s Pere
ira, R
., 28
6-PDL
-13Sa
raf, A
., 16
-ATIO
-1, 5
1-ATIO
-5, 9
1-ATIO
-9Sa
ric, W
., 61
-FD-7,
137
-FD-16
Sarka
r, S.,
136-F
D-15
Sarra
dj, E.
, 186
-AA-27
, 231
-AA-36
Sarto
r, F.,
96-CF
D-10
Sasa
ki, J.
, 293
-ACD-8
Sasa
ki, K.
, 5-AA
-3Sa
sana
puri,
B., 1
78-M
ST-8
Sasid
haran
Nair
, U.,
80-AA
-14Sa
soh,
A., 8
9-APA
-11, 1
38-FD
-17Sa
ssanis
, V.,
209-F
D-24
Sato,
M.,
60-FD
-6/PD
L-2Sa
tori, S
., 29
3-ACD
-8
129
Auth
or/S
essio
n Ch
air In
dex
Satte
lmay
er, T.
, 41-A
A-10,
113
-AA-17
, 185
-AA-26
Saun
ders,
D.,
182-T
P-9, 2
17-TP
-11Sa
urav,
S., 1
25-AP
A-16
Saw,
Z., 2
65-AC
D-7Sa
whill,
B.,
16-AT
IO-1
Sawy
er, J.
, 181
-PDL-9
/TP-8
Scan
lan, J
., 12
8-ATIO
-14, 3
08-M
AO-13
Scara
no, F
., 38
-AA-7,
192
-AMT-1
2/GT
-12,
266
-AMT-1
3/GT
-13Sc
haefe
r, J.,
58-CF
D-8Sc
haefe
r, M.,
299-A
TIO-28
Scha
uerha
mer, D
., 26
9-APA
-31Sc
heel,
H.,
7-AA-5
Sche
rer S
chwe
ning,
G., 1
04-M
AO-3
Sche
tz, J.
, 29-M
AO-1,
46-A
MT-4/
GT-4
Schia
vo, L
., 98
-CFD-1
2Sc
hiavo
ne, N
., 13
6-FD-1
5Sc
hindle
r, M.,
18-AT
IO-3
Schin
wald,
C., 9
1-ATIO
-9Sc
hlimm
, K.,
166-A
TIO-17
Schli
mpert
, S.,
41-AA
-10Sc
hlottk
e, M.
, 229
-AA-34
Schlu
ter, J
., 47
-APA-5
, 269
-APA-3
1Sc
hmidt
, A.,
177-M
ST-7
Schm
idt, B
., 11
-AMT-2
/GT-2
Schm
idt, H
., 10
5-MST
-5, 1
95-AP
A-23
Schm
idt-Sk
ipiol,
F., 1
66-AT
IO-17
Schm
isseu
r, J.,
10-AM
T-1/G
T-1Sc
hmitt,
F., 9
1-ATIO
-9Sc
hmoll
grube
r, P.,
82-AC
D-2Sc
hneid
er, S
., 28-F
D-4, 6
1-FD-7
, 137
-FD-16
, 209
-FD-24
Schn
eiders
, L.,
305-C
FD-35
Scho
lz, P.
, 125
-APA-1
6, 1
59-AM
T-10/
GT-10
Scho
mberg
, T.,
22-CF
D-2, 9
6-CFD
-10Sc
hönle
itner,
F., 1
51-AA
-21Sc
hram,
C., 3
-AA-1,
79-AA
-13, 1
12-AA
-16, 2
31-AA
-36Sc
hrijer
, F.,
138-F
D-17
Schro
ck, C
., 20
1-CFD
-21Sc
hroed
er, A.
, 159
-AMT-1
0/GT
-10Sc
hroed
er, W
., 6-A
A-4, 2
6-FD-2
, 38-A
A-7, 4
1-AA-1
0,
79-A
A-13,
80-A
A-14,
229
-AA-34
, 305
-CFD-3
5Sc
hülei
n, E.,
138
-FD-17
Schu
ltz, M
., 16
4-ATIO
-15Sc
hultz
, V.,
274-A
TIO-24
Schu
lze, M
., 11
3-AA-1
7Sc
huma
n, W.
, 280
-FT-2/
GT-14
Schu
ster, D
., 23
3-APA
-25Sc
huste
r, W.,
151-A
A-21,
198
-ATIO
-19Sc
hutte
, J.,
239-A
TIO-22
Schw
artze
ntrub
er, T.
, 256
-TP-12
Schw
er, D
., 10
2-FD-1
3Sc
iacch
itano
, A.,
266-A
MT-13
/GT-1
3
Sclaf
ani, A
., 87
-APA-9
, 233
-APA-2
5Sc
oggin
s, J.,
217
-TP-11
Scola
n, E.,
46-A
MT-4/
GT-4
Scott
, R.,
124-A
PA-15
Scull
y, R.,
273
-ASE-5
Secco
, N.,
307-M
AO-12
Seck
in, S
., 17
4-FD-2
0Se
eley,
B., 2
39-AT
IO-22
Seide
l, J.,
12-AP
A-1, 1
25-AP
A-16,
236
-APA-2
8Se
itzma
n, J.,
159
-AMT-1
0/GT
-10Se
khar,
S.,
58-CF
D-8Se
lf, R.,
5-AA
-3, 3
9-AA-8
, 227
-AA-32
Selfri
dge,
J., 1
27-AT
IO-13
Selic,
T., 1
51-AA
-21Se
lig, M
., 15
-APA-4
, 87-A
PA-9,
297
-APA-3
7Se
milet
ov, V
., 6-A
A-4, 8
0-AA-1
4, 2
28-AA
-33Se
mmelm
ann,
J., 8
5-AMT
-5/GT
-5Se
mper,
M.,
278-F
D-30
Seng
issen
, A.,
188-A
A-29
Sepk
a, S.
, 68-T
P-3, 1
08-TP
-5Se
rafini,
J., 1
62-AP
A-19
Serpi
eri, J
., 38
-AA-7,
88-A
PA-10
Serre
, G.,
187-A
A-28
Sescu
, A., 2
4-CFD
-4, 41
-AA-10
, 81-A
A-15,
98-CF
D-12,
2
09-FD
-24Se
sterhe
nn, J
., 30
6-CFD
-36Se
vil, H
., 12
8-ATIO
-14Se
zer, E
., 66
-MST
-4Sh
a, Z.,
52-A
TIO-6
Shah
, G.,1
54-AF
M-9
Shah
, H.,
203-C
FD-23
Shah
par, S
., 25
1-MAO
-8Sh
arbatd
ar, M
., 13
1-CFD
-14Sh
arma,
H., 2
35-AP
A-27
Sharm
a, R.,
300
-ATIO
-29Sh
arma,
S., 2
39-AT
IO-22
Shee
he, S
., 11
-AMT-2
/GT-2
Shen
, Q.,
191-A
MT-11
/GT-1
1Sh
eng,
C., 1
22-AP
A-13,
194
-APA-2
2Sh
ephe
rd, J.
, 11-A
MT-2/
GT-2
Sherr
y, L.,
52-A
TIO-6,
117
-ACD-3
Shes
hadri
, T.,
67-PD
L-3Sh
eta, E
., 19
5-APA
-23Sh
eth, K
., 12
6-ATIO
-12Sh
i, R.,
190-A
CD-5,
251
-MAO
-8Sh
i, S.,
107-P
DL-4
Shi, Y
., 25
-FD-1
Shih,
A., 1
64-AT
IO-15
Shim
osaw
a, Y.,
286
-PDL-1
3Sh
imoy
ama,
K., 1
25-AP
A-16
Shin,
S.,
126-A
TIO-12
Shipt
on, L
., 12
8-ATIO
-14
Shive
ly, J.
, 274
-ATIO
-24Sh
milov
ich, A
., 27
1-APA
-33Sh
neide
r, M.,
216-T
P-10/
PDL-1
0Sh
oda,
T., 1
38-FD
-17Sh
ort, E
., 14
5-TP-7
Shuk
la, H
., 9-A
FM-2
Shyy
, W.,
97-CF
D-11,
268
-APA-3
0Sia
la, F.
, 234
-APA-2
6Sid
diqi, S
., 3-A
A-1Sid
harth
, G.,
139-F
D-18
Sidiro
poulo
s, S.
, 198
-ATIO
-19Sie
bert,
J., 2
30-AA
-35Sie
rcke,
M., 7
-AA-5
Siiko
nen,
T., 1
39-FD
-18Sij
tsma,
P., 1
15-AA
-19Sil
leken
s, P.,
91-A
TIO-9
Silton
, S.,
90-AP
A-12,
195
-APA-2
3, 2
46-FD
-27,
271
-APA-3
3Sil
va, R
., 11
7-ACD
-3Sil
va, S
., 15
6-ACD
-4Sil
va, W
., 12
4-APA
-15, 2
73-AS
E-5Sil
vestr
e, F.,
5-AA
-3, 9
-AFM-
2Sil
vestr
e, M.
, 104
-MAO
-3Sim
ao Fe
rreira
, C.,
279-F
D-31
Simerl
y, S.
, 158
-AMT-9
/GT-9
Simõe
s, L.,
4-AA
-2Sim
on, F
., 26
2-AA-4
0Sin
ayok
o, S.
, 38-A
A-7, 1
87-AA
-28Sin
gh, A
., 27
9-FD-3
1Sin
gh, B
., 25
5-PDL
-12Sin
gh, K
., 9-A
FM-2
Singh
, M.,
235-A
PA-27
Singh
, R.,
162-A
PA-19
, 268
-APA-3
0Sin
gh, S
., 84
-AFM-
6Sin
ha, A
., 22
8-AA-3
3Sin
ha, K
., 28
-FD-4
Sinha
, P.,
276-A
TIO-26
Sinnig
e, T.,
37-A
A-6Sio
zos-R
ouso
ulis,
L., 1
52-AA
-22Sir
ohi, J
., 16
2-APA
-19Sit
arama
n, J.,
21-C
FD-1
Sivan
eri, V
., 10
1-FD-1
2Siv
asub
raman
ian, J
., 10
2-FD-1
3Sjo
green
, B.,
24-CF
D-4Sk
ies, F
., 13
2-CFD
-15Sk
inner,
J., 1
17-AC
D-3Sk
vorts
ov, R
., 18
7-AA-2
8Sla
boch
, P.,
303-C
FD-33
Slagle
, A.,
226-A
A-31
Slater
, J.,
279-F
D-31
Slege
rs, N
., 30
-MST
-1Slo
tnick
, J.,
47-AP
A-5, 3
01-CF
D-31
Smelt
zer, S
., 28
1-GEP
C-1Sm
ith, A
., 11
7-ACD
-3Sm
ith, B
., 17
2-CFD
-20Sm
ith, D
., 68
-TP-3,
108
-TP-5,
158
-AMT-9
/GT-9
, 2
10-FD
-25Sm
ith, J
., 65
-MST
-3, 1
42-M
ST-6,
278
-FD-30
Smith
, K.,
145-T
P-7Sm
ith, M
., 25
9-AA-3
7Sm
olarki
ewicz
, P.,
163-A
SE-1
Snyd
er, M
., 23
6-APA
-28So
honi,
N.,
37-AA
-6Şö
hret,
Y., 2
73-AS
E-5So
ler, L
., 27
5-ATIO
-25So
lodov
nikov
, S.,
193-A
PA-21
Son,
P., 1
38-FD
-17So
ng, J
., 10
0-FD-1
1So
ntag,
J., 2
55-PD
L-12
Soria
, J.,
153-A
A-23
Sorok
ach,
M., 2
14-M
ST-9
Souc
asse
, L.,
217-T
P-11
Soufi
ani, A
., 21
7-TP-1
1So
uza,
D., 2
30-AA
-35Sp
agno
lo, S
., 20
5-CFD
-25Sp
alart,
P., 1
23-AP
A-14,
211
-FD-26
Spalt
, T.,
259-A
A-37
Spec
k, S.
, 88-A
PA-10
Spee
r, S.,
302-C
FD-32
Speh
r, C.,
186-A
A-27,
260
-AA-38
Spen
cer, T
., 30
0-ATIO
-29Sp
iegel,
S.,
55-CF
D-5, 1
30-CF
D-13
Spieg
elberg
, H.,
297-A
PA-37
Spille
rs, R.
, 62-F
D-8, 1
75-FD
-22Sp
inelli,
A., 2
6-FD-2
Sprav
ka, J
., 24
9-FT-1
Sree
nivas
, K.,
15-AP
A-4, 1
22-AP
A-13,
297
-APA-3
7Sr
idhar,
B.,
18-AT
IO-3,
92-A
TIO-10
Sridh
aran,
A., 1
62-AP
A-19
Srigr
arom,
S.,
162-A
PA-19
, 234
-APA-2
6, 2
65-AC
D-7Sr
iniva
san,
C., 1
81-PD
L-9/T
P-8Sr
iniva
san,
E., 5
0-APA
-8Sr
ivasta
va, A
., 13
8-FD-1
7St
achu
ra, M
., 15
7-AFM
-9St
agni,
A., 2
44-CF
D-29
Stale
y, A.,
299
-ATIO
-28St
alnov
, O.,
7-AA-5
, 38-A
A-7, 7
9-AA-1
3St
anek
, M.,
33-PD
L-1/F
D-5St
anfor
d, B.
, 49-A
PA-7,
124
-APA-1
5St
angfe
ld, C.
, 208
-FD-23
Steig
er, R.
, 46-A
MT-4/
GT-4
Stein
, F.,
88-AP
A-10
Stein
brenn
er, J.
, 23-C
FD-3
Step
han,
A., 1
96-AS
E-2, 2
37-AS
E-3
Step
hani,
K., 2
16-TP
-10/P
DL-10
, 288
-TP-13
Step
hen,
S., 2
09-FD
-24St
ephe
ns, D
., 11
4-AA-1
8St
ephe
ns, J
., 19
1-AMT
-11/G
T-11
Stev
ens,
M., 2
74-AT
IO-24
Stoe
llinge
r, M.,
172-C
FD-20
Stoh
r, M.,
266-A
MT-13
/GT-1
3St
oll, A
., 24
0-ATIO
-23, 2
76-AT
IO-26
Ston
e, C.,
203
-CFD-2
3, 3
02-CF
D-32
Storo
zhev
, D.,
216-T
P-10/
PDL-1
0St
ouffe
r, V.,
65-M
ST-3,
142
-MST
-6, 1
99-AT
IO-20
, 2
75-AT
IO-25
Stou
t, T.,
40-A
A-9St
rande
, P.,
237-A
SE-3
Stran
gfeld,
C., 1
01-FD
-12St
raub,
S., 9
1-ATIO
-9St
reett,
C., 2
33-AP
A-25
Strga
nac,
T., 9
-AFM-
2, 1
24-AP
A-15,
270
-APA-3
2St
uchli
k, D.
, 200
-BAL-2
Stue
rmer,
A., 1
62-AP
A-19
Su, H
., 25
2-MAO
-9Su
, L.,
181-P
DL-9/
TP-8
Su, W
., 25
-FD-1,
105
-MST
-5Su
bbara
o, K.,
48-A
PA-6,
157
-AFM-
9Su
bbare
ddy,
P., 2
44-CF
D-29,
246
-FD-27
, 278
-FD-30
Subra
mania
n, N.
, 3-AA
-1, 1
52-AA
-22Su
brama
nyam
, A.,
153-A
A-23
Suda
ni, J.
, 205
-CFD-2
5Su
i, D.,
65-M
ST-3
Sun,
D., 1
6-ATIO
-1Su
n, H.
, 95-C
FD-9
Sun,
Y., 4
-AA-2,
6-AA
-4, 3
1-MST
-2, 2
48-FD
-29Su
n, Z.,
130
-CFD-1
3Su
ndstr
öm, E
., 11
2-AA-1
6Su
ñol, A
., 25
0-LTA
-1Su
raj N
andig
anah
alli, J
., 31
-MST
-2Su
rakitb
anha
rn, C.
, 166
-ATIO
-17Su
ryadi,
A., 1
15-AA
-19Su
ryaku
mar, V
., 9-A
FM-2,
124
-APA-1
5, 2
70-AP
A-32
Surzh
ikov,
S., 69
-TP-4,
193-A
PA-21
, 216
-TP-10
/PDL
-10Su
tliff,
D., 7
8-AA-1
2, 1
16-AA
-20Su
zuki,
K., 3
3-PDL
-1/FD
-5, 8
9-APA
-11, 1
02-FD
-13Su
zuki,
T., 6
8-TP-3
Swam
inatha
n Gop
alan,
K., 2
88-TP
-13Sw
ann,
M., 2
93-AC
D-8Sw
iering
a, K.,
18-A
TIO-3,
298
-ATIO
-27Sw
ift, S
., 11
3-AA-1
7Sy
tsma,
M., 1
58-AM
T-9/G
T-9Sz
melte
r, J.,
163-A
SE-1
Taba
nli, H
., 17
4-FD-2
0Ta
ha, H
., 23
6-APA
-28Ta
i, J.,
308-M
AO-13
130
Auth
or/S
essio
n Ch
air In
dex
Taira
, K.,
101-F
D-12,
136
-FD-15
, 248
-FD-29
Taka
hash
i, T.,
117-A
CD-3,
190
-ACD-5
, 232
-ACD-6
, 2
86-PD
L-13,
293
-ACD-8
Taka
ishi, T
., 23
0-AA-3
5Ta
kaki,
R., 2
3-CFD
-3Ta
kaya
nagi,
H.,
69-TP
-4Ta
l, E.,
124-A
PA-15
Tam,
C., 4
1-AA-1
0, 6
7-PDL
-3, 1
85-AA
-26Ta
maki,
Y., 2
41-CF
D-26
Tama
skar,
S.,
239-A
TIO-22
Tamb
a, T.,
138
-FD-17
Tamu
ra, M
., 14
4-PDL
-7Ta
mura,
T., 1
82-TP
-9Ta
naka
, Y.,
182-T
P-9Ta
ng, C
., 16
2-APA
-19Ta
ng, H
., 17
-ATIO
-2, 1
45-TP
-7, 1
73-FD
-19Ta
ng, S
., 10
5-MST
-5Ta
ng, W
., 26
7-APA
-29Ta
ng, Y
., 10
5-MST
-5Ta
nner,
P., 1
20-AM
T-7/G
T-7Ta
nno,
H., 6
9-TP-4
Tao,
F., 7
-AA-5
Tao,
G., 1
27-AT
IO-13
Tao,
L., 2
04-CF
D-24,
245
-CFD-3
0Ta
pken
, U.,
173-F
D-19
Taqu
in, G
., 83
-AFM-
5Ta
rter, J
., 14
0-ITA
R-2Ta
tsuka
wa, T
., 11
4-AA-1
8Ta
verne
tti, W
., 27
8-FD-3
0Ta
y, W.
, 22-C
FD-2
Taylo
r, C.,
275-A
TIO-25
Taylo
r, L.,
15-AP
A-4, 2
97-AP
A-37
Taylo
r, N.,
301-C
FD-31
Taylo
r, S.,
273-A
SE-5
Tchatc
huen
g Kam
megn
e, M.
, 66-M
ST-4
Tchipe
v, N.
, 237
-ASE-3
Teare
, D.,
214-M
ST-9
Temm
ler, C
., 11
3-AA-1
7Te
nsud
a, B.
, 304
-CFD-3
4Te
rakad
o, D.
, 169
-CFD-1
7Te
rnisie
n, L.,
18-A
TIO-3
Terra
col, M
., 15
4-AA-2
4, 2
29-AA
-34Te
rraza
s-Sali
nas,
I., 1
08-TP
-5Te
sfahu
negn
, Y.,
307-M
AO-12
Testa
, C.,
263-A
A-41
Teste
r, B.,
186-A
A-27
Thais
s, C.,
83-A
FM-5
Tham
sen,
P., 1
73-FD
-19Th
aniga
iaras
u, S.
, 50-A
PA-8
Thek
inen,
J., 5
2-ATIO
-6Th
eodo
re, C.
, 281
-GEPC
-1Th
eunis
sen,
R., 3
-AA-1
Thiel
e, F.,
112
-AA-16
, 306
-CFD-3
6Th
ielec
ke, F
., 8-A
FM-1
Thier
ry, M
., 10
8-TP-5
Thipy
opas
, C.,
234-A
PA-26
Thob
ois, L
., 27
2-ASE
-4, 2
98-AT
IO-27
Thom
as, J
., 30
7-MAO
-12Th
omps
on, D
., 23
-CFD-3
, 97-C
FD-11
Thom
pson
, F.,
104-M
AO-3
Thom
pson
, R.,
67-PD
L-3, 2
44-CF
D-29
Thom
pson
, T.,
42-AC
D-1Th
ornbe
r, B.,
306-C
FD-36
Thorn
e, J.,
243
-CFD-2
8Th
orsen
, A.,
83-AF
M-5
Thum
iah, D
., 86
-AMT-6
/GT-6
Thuro
w, B
., 67
-PDL-3
Tian,
P., 4
3-AFM
-3Tia
n, Y.,
44-A
FM-4
Tian,
Z., 2
44-CF
D-29
Tibor,
E., 2
12-M
AO-6
Tilma
nn, C
., 27
1-APA
-33Tim
me, S
., 96
-CFD-1
0Tim
ofeev
, E.,
102-F
D-13
Ting,
E., 1
24-AP
A-15
Tisso
t, G.
, 5-AA
-3Tit
arev,
V., 1
87-AA
-28Tit
tswort
h, J.,
237
-ASE-3
Tkac
henk
o, O.
, 31-M
ST-2
Tkac
ik, P.
, 282
-LTA-2
Toba
lske,
B., 1
00-FD
-11To
giti, V
., 17
2-CFD
-20To
lomell
i, L.,
181-P
DL-9/
TP-8
Toma
c, M.
, 160
-APA-1
7To
ng, F
., 15
1-AA-2
1, 2
60-AA
-38To
ng, O
., 21
-CFD-1
Tong
, W.,
176-M
AO-5
Torde
ux, S
., 26
2-AA-4
0To
ropov
, V.,
5-AA-3
, 251
-MAO
-8To
rres,
S., 9
2-ATIO
-10To
ubin,
H.,
161-A
PA-18
Tous
saint
, C.,
83-AF
M-5
Tous
saint
, S.,
300-A
TIO-29
Town
e, A.,
5-AA
-3Tra
n, D.
, 99-F
D-10
Tran,
L., 1
65-AT
IO-16
Trani,
A., 3
00-AT
IO-29
Treve
, V.,
51-AT
IO-5
Trevin
o, L.,
214
-MST
-9Tri
nh, K
., 12
4-APA
-15Tri
tschle
r, J.,
43-AF
M-3
Trolin
ger, J
., 11
-AMT-2
/GT-2
Trollin
ger, L
., 50
-APA-8
Trope
a, C.,
50-A
PA-8,
271
-APA-3
3, 2
97-AP
A-37
Troxe
l, S.,
163-A
SE-1
Trujill
o, A.,
199
-ATIO
-20Tru
ong,
A., 2
64-AA
-42Tsa
i, C.,
304-C
FD-34
Tsao,
S., 9
2-ATIO
-10, 1
97-AT
IO-18
Tsotsk
as, C
., 29
-MAO
-1Tsu
boku
ra, M
., 27
0-APA
-32Tsu
chiya
, T.,
51-AT
IO-5
Tsutsu
mi, S
., 23
-CFD-3
Tufts
, M.,
137-F
D-16
Tuins
tra, M
., 11
5-AA-1
9Tu
le, C.
, 157
-AFM-
9Tu
na, B
., 10
1-FD-1
2, 2
48-FD
-29Tu
rchi, A
., 34
-TP-1
Turow
ski, M
., 85
-AMT-5
/GT-5
Tuttle
, J.,
167-B
AL-1
Tyag
i, A.,
198-A
TIO-19
, 300
-ATIO
-29Ty
sell,
L., 1
54-AA
-24Ty
son,
W., 9
7-CFD
-11Ud
din, M
., 30
6-CFD
-36Ue
ckerm
ann,
M., 3
3-PDL
-1/FD
-5Ue
hara,
A., 3
1-MST
-2Uk
eiley
, L.,
48-AP
A-6, 1
95-AP
A-23,
248
-FD-29
Ulbric
h, N.
, 294
-AMT-1
4/GT
-15Ull
rich,
W., 4
1-AA-1
0, 1
85-AA
-26Un
derbr
ink, J
., 18
6-AA-2
7, 2
62-AA
-40Un
derw
ood,
M., 2
99-AT
IO-28
Upalk
ar, B
., 14
5-TP-7
Ura,
H., 2
30-AA
-35Ur
nes,
J., 4
9-APA
-7Va
lavan
is, K.
, 88-A
PA-10
Valen
tini, P
., 25
6-TP-1
2Va
lla, M
., 27
2-ASE
-4va
n Bus
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., 12
2-APA
-13, 2
79-FD
-31va
n de V
en, T
., 23
0-AA-3
5va
n der
Velde
n, W.
, 38-A
A-7va
n Kuij
k, J.,
37-A
A-6va
n Oud
heus
den,
B., 97
-CFD-1
1, 13
8-FD-1
7, 20
8-FD-2
3va
n Too
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., 64
-MAO
-2Va
n Treu
ren, K
., 15
-APA-4
Van T
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, R.,
250-L
TA-1
van Z
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, A.,
38-AA
-7, 1
22-AP
A-13
Vand
en, K
., 27
0-APA
-32Va
nderw
el, C.
, 3-AA
-1, 3
8-AA-7
, 152
-AA-22
Vans
tone,
L., 1
74-FD
-20Va
nValk
enbu
rg, R.
, 237
-ASE-3
Varga
, D.,
200-B
AL-2
Varga
s, A.,
167
-BAL-1
Varga
s, M.
, 196
-ASE-2
Vargh
ese,
P., 2
88-TP
-13Va
rgo, E
., 27
5-ATIO
-25Va
rma,
D., 1
25-AP
A-16
Varne
y, M.
, 31-M
ST-2
Vasci
k, P.,
52-A
TIO-6
Vash
ishtha
, A.,
102-F
D-13
Vasile
, M.,
214-M
ST-9
Vassa
ux, D
., 16
7-BAL
-1Va
tsa, V
., 13
3-CFD
-16, 2
59-AA
-37Va
ugha
n, W.
, 196
-ASE-2
, 273
-ASE-5
Vaux
, S.,
249-F
T-1Ve
karia
, S.,
235-A
PA-27
Veldh
uis, L
., 37
-AA-6,
269
-APA-3
1Ve
muri,
S., 2
34-AP
A-26
Vene
l, S.,
167-B
AL-1
Venk
atach
ari, B
., 19
3-APA
-21, 2
11-FD
-26Ve
nkata
krish
nan,
L., 2
27-AA
-32Ve
nkate
sh, B
., 39
-AA-8
Venk
atram
an, S
., 50
-APA-8
Venu
ti, J.,
51-A
TIO-5
Vera,
J., 5
-AA-3
Vergi
ne, F
., 20
5-CFD
-25Ve
rmeir
e, B.
, 130
-CFD-1
3, 2
02-CF
D-22
Verm
illion
, C.,
282-L
TA-2
Vey,
S., 2
6-FD-2
, 297
-APA-3
7Vil
adeg
ut, A.
, 216
-TP-10
/PDL
-10Vil
la, C.
, 65-M
ST-3
Vince
nt, P.
, 130
-CFD-1
3, 2
02-CF
D-22,
242
-CFD-2
7Vis
bal, M
., 101
-FD-12
, 102
-FD-13
, 170
-CFD-1
8,
208
-FD-23
, 255
-PDL-1
2, 26
6-AMT
-13/G
T-13,
2
70-AP
A-32
Viswa
nath,
K., 2
33-AP
A-25
Vitale
, S.,
133-C
FD-16
Vitzil
aios,
N., 8
8-APA
-10Vo
, H.,
60-FD
-6/PD
L-2Vo
s, R.,
42-A
CD-1
Vrcho
ta, P.
, 233
-APA-2
5Vu
, B.,
56-CF
D-6Vu
cinic,
D.,
250-L
TA-1
Vuillo
t, F.,
39-A
A-8, 2
59-AA
-37Wa
che,
L., 5
2-ATIO
-6Wa
dding
ton, M
., 82
-ACD-2
Wagle
, N.,
157-A
FM-9
Wagn
er, C.
, 252
-MAO
-9Wa
gner,
J., 6
2-FD-8
, 175
-FD-22
Wagn
ild, R
., 10
3-ITA
R-1, 2
56-TP
-12Wa
indim
, M.,
245-C
FD-30
Waith
e, K.,
14-A
PA-3,
89-A
PA-11
Waka
yama
, S.,
267-A
PA-29
Wake
field,
D.,
167-B
AL-1
Walke
r, A.,
88-AP
A-10,
214
-MST
-9Wa
lker, M
., 50
-APA-8
Wall,
A., 4
0-AA-9
Wan,
Y., 6
5-MST
-3, 2
75-AT
IO-25
Wang
, C.,
161-A
PA-18
, 213
-MAO
-7, 2
69-AP
A-31
Wang
, F.,
85-AM
T-5/G
T-5, 1
91-AM
T-11/
GT-11
, 2
37-AS
E-3, 2
95-AP
A-34
Wang
, G.,
265-A
CD-7
Wang
, H.,
84-AF
M-6,
244
-CFD-2
9Wa
ng, J
., 33
-PDL-1
/FD-5
, 84-A
FM-6,
180
-PDL-8
/AP
A-20,
187
-AA-28
, 271
-APA-3
3Wa
ng, K
., 18
7-AA-2
8, 2
55-PD
L-12
Wang
, L.,
151-A
A-21,
260
-AA-38
Wang
, M.,
187-A
A-28,
255
-PDL-1
2, 2
63-AA
-41,
265
-ACD-7
Wang
, P.,
128-A
TIO-14
Wang
, Q.,
80-AA
-14, 1
73-FD
-19, 2
02-CF
D-22,
2
41-CF
D-26
Wang
, S.,
62-FD
-8, 1
19-AF
M-8
Wang
, X.,
122-A
PA-13
, 132
-CFD-1
5, 2
50-LT
A-1,
260
-AA-38
Wang
, Y., 9
-AFM-
2, 22
-CFD-2
, 30-M
ST-1,
131-C
FD-14
, 2
13-M
AO-7
Wang
, Z., 2
3-CFD
-3, 25
-FD-1,
56-CF
D-6, 9
9-FD-1
0,
130
-CFD-1
3, 13
8-FD-1
7, 17
0-CFD
-18, 2
42-CF
D-27,
303
-CFD-3
3Wa
nke,
C., 2
75-AT
IO-25
Ward,
C., 1
37-FD
-16Wa
tanab
e, Y.,
33-P
DL-1/
FD-5,
102
-FD-13
Watso
n, J.,
104
-MAO
-3Wa
tson,
W., 7
-AA-5,
116
-AA-20
, 262
-AA-40
Weav
er, A.
, 35-T
P-2We
bb, N
., 33
-PDL-1
/FD-5
Webs
ter, R
., 12
2-APA
-13We
i, Q.,
7-AA-5
Wei ta
o, Z.,
303
-CFD-3
3We
instei
n, R.,
50-A
PA-8
Weiss
, B.,
91-AT
IO-9
Weiss
, M.,
239-A
TIO-22
Wells,
D.,
42-AC
D-1We
n, Y.,
250
-LTA-1
Wend
orff,
A., 2
12-M
AO-6,
308
-MAO
-13We
ng, H
., 68
-TP-3
Werne
r, T.,
151-A
A-21
Werne
t, M.
, 227
-AA-32
Werte
r, N.,
29-M
AO-1
West,
A., 3
9-AA-8
, 230
-AA-35
West,
J., 1
71-CF
D-19
West,
T., 5
8-CFD
-8We
y, P.,
45-A
MT-3/
GT-3,
47-A
PA-5
Wha
len, E
., 24
8-FD-2
9, 2
71-AP
A-33
Whe
aton,
B., 1
03-IT
AR-1,
278
-FD-30
Whit
e, E.,
158
-AMT-9
/GT-9
, 209
-FD-24
, 267
-APA-2
9W
hite,
J., 1
33-CF
D-16
Whit
e, M.
, 67-P
DL-3,
255
-PDL-1
2W
hite,
T., 6
8-TP-3
, 108
-TP-5,
217
-TP-11
Wiar
t, L.,
13-A
PA-2
131
Auth
or/S
essio
n Ch
air In
dex
Wiel
and,
F., 1
98-AT
IO-19
, 300
-ATIO
-29W
ilcoxe
n, M.
, 17-A
TIO-2
Wild
, J.,
125-A
PA-16
, 230
-AA-35
Wild
er, M
., 18
2-TP-9
Wild
er, W
., 91
-ATIO
-9W
ildsch
ek, A
., 64
-MAO
-2W
ilkins
on, S
., 24
8-FD-2
9W
illiam
s, A.,
35-T
P-2W
illiam
s, D.
, 60-F
D-6/P
DL-2,
101
-FD-12
, 136
-FD-15
Willi
ams,
N., 2
44-CF
D-29
Willi
amsch
en, M
., 26
3-AA-4
1W
ilson,
A., 1
98-AT
IO-19
Wine
r, E.,
104-M
AO-3,
141
-MAO
-4, 1
76-M
AO-5,
2
12-M
AO-6
Wing
, A.,
239-A
TIO-22
Wing
, D.,
299-A
TIO-28
Wink
el, R.
, 60-F
D-6/P
DL-2
Wint
er, M
., 10
8-TP-5
, 121
-AMT-8
/FD-1
4/TP
-6/GT
-8,
181
-PDL-9
/TP-8
Wint
zer, M
., 14
-APA-3
Wisd
a, D.
, 114
-AA-18
, 187
-AA-28
Wisn
iewsk
i, C.,
15-AP
A-4W
isniew
ski, N
., 15
-APA-4
Wiss
a, A.,
12-A
PA-1
Wiss
ink, A
., 20
1-CFD
-21W
itherd
en, F
., 13
0-CFD
-13, 2
02-CF
D-22
Witti
g, S.
, 46-A
MT-4/
GT-4
Wlez
ien, R
., 13
7-FD-1
6Wo
hlbran
dt, A.
, 41-A
A-10
Wolf,
W., 3
8-AA-7
, 41-A
A-10,
189-A
A-30,
260-A
A-38,
2
70-AP
A-32
Woo,
G., 2
95-AP
A-34
Woop
en, M
., 95
-CFD-9
Wortm
ann,
A., 4
2-ACD
-1W
ray, A
., 24
-CFD-4
Wray
, T.,
139-F
D-18,
211
-FD-26
Wrig
ht, M
., 85
-AMT-5
/GT-5
Wrig
hton,
C., 2
27-AA
-32W
ronow
ski, K
., 28
0-FT-2
/GT-1
4W
u, D.
, 213
-MAO
-7W
u, J.,
25-F
D-1, 2
65-AC
D-7W
u, X.
, 99-F
D-10
Wu,
Y., 1
81-PD
L-9/T
P-8W
u, Z.,
250
-LTA-1
Wün
sch, O
., 22
-CFD-2
, 96-C
FD-10
Wys
zogro
dzki,
A., 1
63-AS
E-1Xia
, Y.,
55-CF
D-5Xia
ng, J
., 47
-APA-5
Xiao,
F., 1
30-CF
D-13
Xiao,
T., 9
7-CFD
-11Xia
o, Y.,
296
-APA-3
5Xia
ojie,
Q., 1
05-M
ST-5
Xie, J
., 65
-MST
-3Xie
, K.,
191-A
MT-11
/GT-1
1Xu
, F.,
57-CF
D-7Xu
, J.,
116-A
A-20,
241
-CFD-2
6Xu
, K.,
107-P
DL-4,
143
-PDL-6
Xu, Z
., 10
5-MST
-5, 2
41-CF
D-26
Xue,
M., 1
6-ATIO
-1Ya
dlin,
Y., 2
71-AP
A-33
Yagiz
, B.,
304-C
FD-34
Yakh
ina, G
., 79
-AA-13
Yako
vlev,
P., 2
28-AA
-33Ya
lin, A
., 10
7-PDL
-4Ya
mada
, K.,
144-P
DL-7
Yama
gishi,
K., 1
82-TP
-9Ya
mamo
to, K.
, 23-C
FD-3,
229
-AA-34
, 230
-AA-35
Yama
shita
, R.,
89-AP
A-11
Yama
uchi,
G.,
192-A
MT-12
/GT-1
2Ya
moun
i, S.,
270-A
PA-32
Yan,
F., 1
28-AT
IO-14
Yan,
G., 1
31-CF
D-14
Yan,
K., 2
50-LT
A-1Ya
n, W.
, 178
-MST
-8Ya
n, X.
, 180
-PDL-8
/APA
-20Ya
ng, C
., 14
5-TP-7
Yang
, D.,
204-C
FD-24
Yang
, H.,
197-A
TIO-18
, 241
-CFD-2
6, 3
04-CF
D-34
Yang
, M.,
119-A
FM-8
Yang
, T.,
250-L
TA-1
Yang
, W.,
105-M
ST-5
Yang
, X.,
98-CF
D-12,
171
-CFD-1
9Ya
ng, Y
., 4-A
A-2, 6
-AA-4,
97-C
FD-11
, 162
-APA-1
9,
178
-MST
-8, 2
69-AP
A-31
Yang
, Z.,
159-A
MT-10
/GT-1
0, 2
68-AP
A-30
Yao,
C., 5
7-CFD
-7, 1
88-AA
-29Ya
o, H.
, 6-AA
-4, 1
15-AA
-19, 1
54-AA
-24Ya
o, W.
, 56-C
FD-6
Yarus
evyc
h, S.
, 100
-FD-11
, 208
-FD-23
Yauw
enas
, Y.,
115-A
A-19
Yayla
, S.,
25-FD
-1Ya
zdan
i, S.,
229-A
A-34
Ye, C
., 19
8-ATIO
-19Ye
chou
t, T.,
64-M
AO-2
Yee,
H., 2
4-CFD
-4Ye
e, P.,
108
-TP-5
Yen,
C., 7
8-AA-1
2Ye
ste-O
jeda,
O., 2
15-M
ST-10
Yi, S
., 12
-APA-1
Yode
r, D.,
58-CF
D-8, 1
20-AM
T-7/G
T-7Yo
koka
wa, Y
., 23
0-AA-3
5Yo
on, S
., 13
6-FD-1
5Yo
shida
, S.,
43-AF
M-3
Yosh
ikawa
, E.,
298-A
TIO-27
Yosh
ino, T
., 28
6-PDL
-13Yo
ung,
D., 2
5-FD-1
Youn
g, E.,
200
-BAL-2
Youn
g, L.,
117
-ACD-3
Youn
g, R.,
281
-GEPC
-1Yo
ung,
S., 1
66-AT
IO-17
Youn
g, T.,
48-A
PA-6,
102
-FD-13
Yu, H
., 15
9-AMT
-10/G
T-10
Yu, J
., 12
2-APA
-13Yu
, L.,
145-T
P-7Yu
, M.,
243-C
FD-28
, 279
-FD-31
Yu, S
., 26
9-APA
-31Yu
, W.,
7-AA-5
Yuan
, C.,
248-F
D-29
Yuan
-pei, S
., 25
2-MAO
-9Yu
ceil,
K., 1
74-FD
-20Yu
e, C.,
280
-FT-2/
GT-14
Yue,
Z., 6
5-MST
-3Za
chos
, P.,
270-A
PA-32
Zaidi
, T.,
52-AT
IO-6
Zajac
zkow
ski, F
., 14
0-ITA
R-2Za
karia
, M.,
236-A
PA-28
Zama
n, K.,
189
-AA-30
Zamb
rano,
J., 2
15-M
ST-10
Zane
tte, J
., 24
9-FT-1
Zang
, T.,
308-M
AO-13
Zawo
dny,
N., 1
55-AA
-25Za
ytsev
, M.,
187-A
A-28,
189
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Zehn
er, P.
, 154
-AA-24
Zelen
ak, D
., 14
3-PDL
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i, S.,
16-AT
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, D.,
239-A
TIO-22
Zeng
, Q.,
30-M
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in, S
., 15
1-AA-2
1Zh
a, G.
, 90-A
PA-12
, 125
-APA-1
6Zh
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., 67
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Zhai,
Z., 2
15-M
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g, B.
, 16-A
TIO-1
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g, C.,
253
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95-AP
A-34
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, 180
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71-AP
A-33
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47-A
PA-5
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, 57-C
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, 208
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Zhan
g, J.,
65-M
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203
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3, 2
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L., 2
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S., 3
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, 7-AA
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, 112
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52-AA
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05-CF
D-25,
214
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259
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, 263
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122
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., 12
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., 11
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., 16
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., 19
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41-CF
D-26
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, W.,
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Zhao
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303-C
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., 31
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elonk
in, V.
, 31-M
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g, J.,
185
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44-A
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g, Z.,
43-AF
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7, 25
0-LTA-
1,
261
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, 272
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g, X.
, 209
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Zhou
, B.,
79-AA
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83-M
AO-10
Zhou
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250-L
TA-1
Zhou
, J.,
208-F
D-23
Zhou
, L.,
7-AA-5
Zhou
, P.,
250-L
TA-1
Zhu,
J., 2
5-FD-1
Zhu,
M., 2
50-LT
A-1Zh
u, T.,
69-T
P-4Zie
ntarsk
i, L.,
191-A
MT-11
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merm
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., 10
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gg, D
., 13
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69-CF
D-17,
204
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4,
242
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7, 2
67-AP
A-29
Zishk
a, E.,
182
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26-FD
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., 19
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, 25-F
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niga V
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ez, J
., 23
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Zwerg
er, C.
, 87-A
PA-9
132
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Technical ZonesAVIATION 2015 Technical Zones (see Venue Map)
The technical program, which consists of more than 1,500 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 121st AIAA/CEAS Aeroacoustics Conference 31st AIAA Aerodynamic Measurement Technology and Ground Testing Conference15th AIAA Aviation Technology, Integration, and Operations Conference AIAA Balloon Systems Conference AIAA Flight Testing Conference 22nd AIAA Lighter-Than-Air Systems Technology Conference AIAA Modeling and Simulation Technologies Conference 45th AIAA Thermophysics Conference
Zone 215th AIAA Aviation Technology, Integration, and Operations Conference AIAA Complex Aerospace Systems Exchange45th AIAA Fluid Dynamics Conference 16th AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference 46th AIAA Plasmadynamics and Lasers Conference45th AIAA Thermophysics Conference
Zone 333rd AIAA Applied Aerodynamics Conference
Zone 431st AIAA Aerodynamic Measurement Technology and Ground Testing ConferenceAIAA Atmospheric Flight Mechanics Conference 7th AIAA Atmospheric and Space Environments Conference AIAA Complex Aerospace Systems Exchange22nd AIAA Computational Fluid Dynamics Conference45th AIAA Fluid Dynamics Conference
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Reserve your sponsorship and exhibit space today!Contact Tobey Jackson, 703.264.7570 or [email protected]
2O1613–17 JUNE 2016 WASHINGTON, D.C.
See You Next Year!We hope that you learned something new, achieved your goals, caught up with colleagues, and made new connections. We look forward to seeing you next year in the Nation’s capital!
32nd AIAA Aerodynamic Measurement Technology and Ground Testing Conference
34th AIAA Applied Aerodynamics Conference
AIAA Atmospheric Flight Mechanics Conference
8th AIAA Atmospheric and Space Environments Conference
16th AIAA Aviation Technology, Integration, and Operations Conference
AIAA Flight Testing Conference
8th AIAA Flow Control Conference
46th AIAA Fluid Dynamics Conference
17th AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference
AIAA Modeling and Simulation Technologies Conference
47th AIAA Plasmadynamics and Lasers Conference
46th AIAA Thermophysics Conference
It’s the perfect place to combine business and family fun. It is home to Congress, NASA Headquarters, NASA Goddard, NOAA, the FAA, NSSC, NRL, and the Pentagon. There are more than 100 free things to do in Washington, D.C.— including most of the Smithsonian (with TWO air and space museums, art galleries, and the National Zoo) and scores of famous landmarks—most within walking distance of one another.
Technical Conferences
Why Washington, D.C.?