22–26 JUNE 2015 DALLAS, TX
PUSHING THE BOUNDARIES OF THE IMAGINABLE: LEVERAGING THE AVIATION ECOSYSTEM
FINAL PROGRAM www.aiaa-aviation.org #aiaaAviation
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12206_AIR_QA_Fuselage_AirbusAmericasProg_11x8.5_1.0.indd 1 04/06/2015 15:29 Executive Steering Committee AIAA AVIATION 2015 Welcome 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 Juan Alonso Victoria Cox 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 Stanford University Federal Aviation Administration (retired) 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 Thomas Edwards John O’Leary design community. Unmanned systems continue to make headlines and we will discuss the NASA Ames Research Airbus Americas challenges facing this sector internationally. Following Administrator Bolden’s discussion Center 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 Richard Wahls Todd Zarfos 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 NASA Langley Boeing Commercial Forum Organizing and Technical Program Committees and the AIAA staff for their hard Research Center Airplanes 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.
AVIATION 2O15 is proud to feature the following conferences: 21st AIAA/CEAS Aeroacoustics Conference 22nd AIAA Computational Fluid Dynamics Conference 31st AIAA Aerodynamic Measurement Technology and AIAA Flight Testing Conference Ground Testing Conference 45th AIAA Fluid Dynamics Conference 33rd AIAA Applied Aerodynamics Conference 22nd AIAA Lighter-Than-Air Systems Technology AIAA Atmospheric Flight Mechanics Conference Conference 7th AIAA Atmospheric and Space Environments 16th AIAA/ISSMO Multidisciplinary Analysis and Conference Optimization Conference 15th AIAA Aviation Technology, Integration, and AIAA Modeling and Simulation Technologies Conference Operations Conference 46th AIAA Plasmadynamics and Lasers Conference AIAA Balloon Systems Conference 45th AIAA Thermophysics Conference AIAA Complex Aerospace Systems Exchange www.aiaa-aviation.org 3 #aiaaAviation IntroOrganizing Committee
General Chair Technical Discipline Chairs Flight Testing Richard Wahls, NASA Langley Research Karl Garman, Federal Aviation Center Aeroacoustics Administration Naval Agarwal, The Boeing Company Forum 360 Chair Fluid Dynamics Robert Gregg, III, The Boeing Company Aerodynamic Measurement Technology Jill Klentzman, Baylor University Andrew Cutler, The George Washington Technical Co-Chair University Green Engineering Vincent Schultz, NASA Langley Research Andrew Gibson, Empirical Systems Center Todd Lowe, Virginia Polytechnic Institute Aerospace and State University Technical Co-Chair Ground Testing Greg Naterer, Memorial University Air Transportation Integration & Operations Benjamin Mills, Aerospace Testing Alliance Cees Bil, RMIT University International Lighter than Air Systems Konstantinos “Kostas” Kontis, University of Kapil Sheth, NASA Ames Research Center Rajkumar S. Pant, Indian Institute of Glasgow Technology Bombay Karen Marais, Purdue University Member Services Modeling and Simulation Technologies Sarah Shull, NASA Johnson Space Center Scot Campbell, Massachusetts Institute of Gano Broto Chatterji, NASA Ames Research Technology Center Local Rep Aircraft Design Terry Burress, Lockheed Martin Information Multidisciplinary Analysis and Optimization Systems & Global Solutions Hernando Jimenez, Georgia Institute of Eliot Winer, Iowa State University Technology Young Professional Vijay Kalivarapu, Iowa State University Greg Johnson, Aerojet Rocketdyne Danielle (Dani) Soban, Queen’s University Belfast Plasmadynamics and Lasers Recognition Azer Yalin, Colorado State University Applied Aerodynamics Dimitri Mavris, Georgia Institute of Technology Brian McGrath, The Johns Hopkins Thermophysics University Applied Physics Laboratory Chad Boyack, Raytheon Missile Systems Public Policy Bob Stuever, Beechcraft Defense Company, Khaled Abdol-Hamid, NASA Langley Elliott Short, Raytheon Missile Systems LLC Research Center Technical Discipline Group Representatives Complex Aerospace Systems Zifeng Yang, Wright State University Exchange (CASE) Chair TAC Information Systems Group Atmospheric and Space Environments Sophia Bright, The Boeing Company Sam Adhikari, Sysoft Corporation Nashat Ahmad, NASA Langley Research Technical Program Committee Center
Forum Technical Co-Chairs Matthew Pruis, Northwest Research Greg Naterer (Aerospace Sciences Group), Associates Inc. Memorial University Atmospheric Flight Mechanics Vincent Schultz (Aircraft and Atmospheric Soumyo (Som) Dutta, NASA Langley Systems Group), NASA Langley Research Research Center Center Kevin Cunningham, NASA Langley Forum Deputy Technical Co-Chairs Research Center LaTunia Melton (Aerospace Sciences Balloon Systems Group), NASA Langley Research Center Debora Fairbrother, NASA
Cees Bil (Aircraft and Atmospheric Systems Complex Aerospace Systems Exchange (CASE) Group), RMIT University Sophia Bright, The Boeing Company ITAR Chair Computational Fluid Dynamics Katya M. Casper, Sandia National Krzysztof (Chris) Fidkowski, University of Laboratories Michigan
www.aiaa-aviation.org 4 #aiaaAviation IntroContents
Welcome 3
Organizing Committee 4
Contents 5
Forum Overview 8
Sponsors 10
www.twitter.com/aiaa Keynote Speakers and Plenary Sessions 11
Forum 360 12 www.facebook.com/AIAAfan
Special Sessions and Events 17 www.youtube.com/AIAATV
Networking Events 18 www.linkedin.com/companies/aiaa
Recognition Events 19 www.flickr.com/aiaaevents
ITAR Information 21 http://livestream.com/AIAAvideo/ AVIATION2015 Exposition Hall 22 www.instagram.com/aiaaerospace Exhibitors 24
General Information 27
Author and Session Chair Information 29 Join the conversation! #aiaaAviation Committee Meetings 30
On-Site Wi-Fi Information Sessions at a Glance 33 Network Name: PSAV-Meeting Session Detail Matrix 41 Password: AIAA2015
Author and Session Chair Index 121 AIAA is the world’s largest aerospace professional Technical Zones 134 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, Venue Map 135 more connected, more accessible, and more prosperous. For more information, visit www.aiaa.org, or follow us on Twitter @AIAA. www.aiaa-aviation.org 5 #aiaaAviation Get Your Conference Info on the Go!
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FEATURES HOW TO DOWNLOAD Browse Program Any version can be run without an active Internet connection! You can also sync an itinerary you created online with the app by entering your unique itinerary name. View the program at your fingertips MyItinerary Mobile App MyItinerary Web App My Itinerary For optimal use, we recommend • For optimal use, we recommend: iPhone 3GS, iPod Touch (3rd generation), Create your own conference s iPhone 3GS, iPod Touch (3rd iPad iOS 4.0, or later schedule generation), iPad iOS 4.0, or later Download the MyItinerary app by s Most mobile devices using Android Conference Info searching for “ScholarOne” in the App 2.2 or later with the default browser Store directly from your mobile device. Or, Including special events access the link below or scan the QR code s BlackBerry Torch or later device to access the iTunes page for the app. using BlackBerry OS 7.0 with the Take Notes http://itunes.apple.com/us/app/scholarone- default browser Take notes during sessions my-itinerary/id497884329?mt=8 • Download the MyItinerary app by Select the meeting “AIAA Aviation 2015” scanning the QR code or accessing City Map http://download.abstractcentral.com/ See the surrounding area and aiaa-mav15/index.htm the Hilton Anatole • Once downloaded, you can bookmark the site to access it later or add a link Connect to Twitter to your home screen. Tweet about what you’re doing and who you’re meeting with #aiaaAviation ParParticipateticipate inin Real-TimeReal-Time Q&AQ&A andand PollingPolling duringduring AIAAAIAA AVIATIONAVIATION 20152015 withwith thethe ConferenceConference IOIO App!App!
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Getting Your Question Answered is as EASY as 1-2-3! 1. Click the “Ask” button to submit a question. 2. Check out the questions that other attendees are asking. 3. If you see a question that you want answered, click on the arrow on the left. The most popular questions automatically rise to the top.
Participate in Session Polls 1. If Polls are available they will appear at the top of the page. Simply click/tap on a Poll to respond. 2. Choose your response(s) and hit “submit”. 3. After responding you will be able to see the results on your own device!* * Some Poll results may be hidden IntroForum Overview
MONDAY TUESDAY 22 June 23 June 0730 hrs Speakers’ Briefing Speakers’ Briefing
0800 hrs Plenary Keynote Plenary Panel 0830 hrs
Networking Break in 0900 hrs Networking Break Exposition Hall
0930 hrs
1000 hrs Exposition Technical Technical Hall 1030 hrs Sessions Forum 360 Sessions Forum 360 Open 1100 hrs
1130 hrs
1200 hrs
1230 hrs Awards Luncheon: 1300 hrs Networking Lunch on Own Celebrating Achievements Networking Lunch on Own in Aerospace Sciences 1330 hrs
1400 hrs
1430 hrs CFD Flow Exposition Hall Visualization Open 1500 hrs Forum 360 Showcase Forum 360 Technical Networking Break Technical 1530 hrs Networking Break Sessions in Exposition Hall Sessions 1600 hrs
1630 hrs Plasmadynamics and Lasers Award Lecture 1700 hrs
1730 hrs Fluid Dynamics Speed Geek Award Lecture 1800 hrs Networking Event Reception in Exposition Hall and Reception 1830 hrs Rising Leaders in Aerospace Reception 1900 hrs
1930 hrs
2000 hrs
2030 hrs
2100 hrs
2130 hrs
2200 hrs
www.aiaa-aviation.org 8 #aiaaAviation IntroForum Overview
WEDNESDAY THURSDAY FRIDAY 24 June 25 June 26 June 0730 hrs Speakers’ Briefing Speakers’ Briefing Speakers’ Briefing
0800 hrs Plenary Keynote Plenary Keynote Plenary Keynote 0830 hrs Networking Break Networking Break in 0900 hrs Networking Break in Exposition Hall Exposition Hall 0930 hrs
1000 hrs Exposition Exposition Hall Hall Technical Technical Technical Open Open 1030 hrs Sessions Forum 360 Sessions Forum 360 Sessions 1100 hrs
1130 hrs
1200 hrs
1230 hrs Awards Luncheon: 1300 hrs Luncheon in Exposition Hall Celebrating Achievements in Aircraft Networking Lunch on Own and Atmospheric Systems 1330 hrs
1400 hrs Rising Leaders 1430 hrs Exposition in Aerospace Hall Panel 1500 hrs Forum 360 Open Forum 360 Networking Break Technical Technical 1530 hrs Rising Leaders Networking Break in Exposition Hall Sessions Sessions in Aerospace 1600 hrs Leadership Exchange/Speed 1630 hrs Networking Aerodynamics Award Lecture 1700 hrs
1730 hrs Aeroacoustics Thermophysics Wright Brothers Lectureship in Aeronautics Lecture Award Lecture 1800 hrs
1830 hrs
1900 hrs
1930 hrs Aeroacoustics Awards Banquet
2000 hrs
2030 hrs
2100 hrs
2130 hrs
2200 hrs
www.aiaa-aviation.org 9 #aiaaAviation IntroSponsors
Premier Sponsor
Speed Geek Networking Event Sponsor
Rising Leaders Program Sponsor Sponsor
Supporting Sponsors
R Crean & Associates Aerospace Consultants
Media Sponsor
www.aiaa-aviation.org 10 #aiaaAviation IntroKeynote Speakers and Plenary Sessions
Get the big picture on aviation from the thought leaders in the field during these high-level discussions and presentations.
Monday, 22 June 0800–0900 hrs Chantilly Ballroom West Opening Keynote: Are We Moving Fast Enough? Tom Enders, Chief Executive Officer, Airbus Group
Tuesday, 23 June 0800–0900 hrs Chantilly Ballroom West NextGen: A Model of Stakeholder Engagement Bill Ayer, Retired Chairman and CEO, Alaska Air Group Edward L. Bolton Jr., Assistant Administrator for NextGen, Federal Aviation Administration
Wednesday, 24 June 0800–0900 hrs Chantilly Ballroom West NASA and the Future of Aerospace Charles F. Bolden Jr., Administrator, National Aeronautics and Space Administration
Thursday, 25 June 0800–0900 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 June 0800–0900 hrs Chantilly Ballroom West The G650 Design, Development, and Test Kurt Erbacher, Vice President, G650 Aircraft Program, Gulfstream Aerospace Corporation
www.aiaa-aviation.org 11 #aiaaAviation Forum 360
Tuesday, 23 June 0930–1200 hrs Grand Ballroom E Day in the Life of Operations – Effectively Managing Disruption Moderator: Neil Planzer, Vice President, Air Traffic Management, Boeing Commercial Airplanes Panelists: These conversations will cover a spectrum of Tim Campbell, Senior Vice President, Air Operations, American timely topics including programs, systems, policy, Airlines operations, applications, platforms and more! Jim Crites, Executive Vice President of Operations, DFW International Airport Brian Quigley, Managing Director Flight Operations, United Monday, 22 June Airlines 0930–1200 hrs Grand Ballroom E Dan Smiley, Vice President for System Operations, Federal Aviation Administration Air Traffic Office The Voice of the Customer — Designing the Right Aircraft 1400–1630 hrs Grand Ballroom E Moderator: Christopher Stonehouse, Senior Vice President, Customer Services, Airbus Americas, Inc. International UAS Integration Forum Panelists: Moderator: Rob Hughes, Northrop Grumman, Inc Jack Arehart, President of MRO Services, Delta TechOps Panelists: William “Bill” Meehan, Chief Operating Officer, Frontier Cees Bil, Associate Professor, School of Aerospace, Mechanical Airlines, Inc. and Manufacturing Engineering, RMIT University Bart Roberts, Vice President, Flight Operations, JetBlue Airways Chuck Johnson, Vice President of Operations, The Padina David Seymour, Senior Vice President, Technical Operations, Group American Airlines Marty Rogers, University of Alaska-Fairbanks Marshall Jackson, Project Manager – Aviation Safety 1400–1700 hrs Grand Ballroom E Audits, Office of Inspector General, U.S. Department of Transportation Whatever Happened to the Four-Year Airplane? Randy Willis, FAA, Co-Chair of ICAO RPAS (Remotely Piloted Moderator: Craig Willis, Group Head for Systems Verification, Aircraft Systems) Gulfstream G500/G600 Program, Gulfstream Aerospace Dale Richards, Senior Research Fellow, Human Factors, Faculty Corporation of Engineering & Computing, Coventry University Panelists: Catherine Ferrie Kilmain, Executive Vice President of Engineering, Bell Helicopter Eric Schrock, Deputy Director, Technology Development and Product Integration, Lockheed Martin Corporation
www.aiaa-aviation.org 12 #aiaaAviation IntroForum 360
Wednesday, 24 June 1400–1730 hrs Grand Ballroom D 0930–1200 hrs Grand Ballroom E System Complexity: Government Needs and Practical Research Results NACA to NASA: Embarking on the Next 100 Keynote Speaker: Kristen Baldwin, Principal Deputy DASD Years of Excellence and Innovation in Aeronautics (SE), Department of Defense and Beyond Moderators: Moderator: Robert Pearce, Director, Strategy, Architecture & Frank Serna, Principal Director, Strategic Imperatives, Draper Analysis, Aeronautics Research Mission Directorate, NASA Laboratory Headquarters Anna-Marie McGowan, Aeronautics Research Directorate, Panelists: NASA Langley Research Center David Bowles, Center Director (Acting), NASA Langley Panelists: Research Center Jeffrey P. Holland, Director of Research and Development and Thomas Edwards, Deputy Center Director, NASA Ames Chief Scientist, U.S. Army Corps of Engineers Research Center David Neyland, Consultant Janet Kavandi, Deputy Director, NASA Glenn Research Center
David McBride, Center Director, NASA Armstrong Flight Research Center Thursday, 25 June Jaiwon Shin, Associate Administrator, Aeronautics Research Mission Directorate, NASA Headquarters 0930–1200 hrs Grand Ballroom E The Impact of Particle Image Velocimetry on 1400–1630 hrs Grand Ballroom E Aerospace Technology Energy/Environment Panel — The Challenges of Moderator: Steven Beresh, Distinguished Member of the Green Aviation Technical Staff, Sandia National Laboratories Panelists: Moderator: Marty Bradley, Technical Fellow, Boeing Commercial Airplanes Ronald J. Adrian, Regent’s Professor and Ira A. Fulton Professor of Mechanical and Aerospace Engineering, Arizona State Panelists: University Ricky Curran, Faculty of Aerospace Engineering, Delft Susan Gorton, Project Manager, Revolutionary Vertical Lift University of Technology Technology Project, NASA Langley Research Center Jay E. Dryer, Director, Advanced Air Vehicles Program Office Fulvio Scarano, Full Professor and Chair of Aerodynamics, (Acting), Aeronautics Research Mission Directorate, NASA Delft University of Technology Headquarters Miguel Visbal, Principal Research Aerospace Engineer Askin Isikveren, Head of Visionary Aircraft Concepts, Bauhaus and Team Leader of Multidisciplinary Computational Luftfahrt Aerodynamics, Aerospace Systems Directorate, Air Force Leslie Perkins, Director, Energy Office, Air Force Research Research Laboratory Laboratory Jeanne Yu, Environmental Director, Boeing Commercial 1400–1630 hrs Grand Ballroom E Airplanes Supercomputing: Roadmap and Its Future Role in Aerospace Engineering Moderator: Doug Cline, Technical Lead, High Performance Computing, Lockheed Martin Aeronautics Panelists: 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 Research Mark Seager, Intel Fellow, CTO, High Performance Computing Ecosystem, Intel Corporation www.aiaa-aviation.org 13 #aiaaAviation IntroForum 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. Monday, 22 June 0900–1200 hrs Batik A-B 1730–1900 hrs Morocco Academic Roundtable CASE Networking Social Expanding on the theme from Sunday, this session is the second Sponsored by Boeing Commercial Airplanes day activity of the 2015 CASE Academic Workshop. It will offer rapid-fire discussions of current research efforts in systems knowledge and competency. Tuesday, 23 June Facilitators: 0930–1200 hrs Grand Ballroom D Franz-Josef Kahlen, Ph.D., Associate Professor, Department Applied Complexity Workshop of Mechanical Engineering, University of Cape Town, Cape Town, South Africa Participants can learn how to embrace and thrive within Shannon Flumerfelt, Ph.D., Associate Professor, Educational technically, socially, and organizationally complex environments. Leadership, Director of Lean Thinking for Schools, Pawley Participants will be immersed in a three-pronged approach to Learning Institute, Oakland University, Michigan learning, with industry examples, applied theory, and interactive practice. Please join us for this engagement, and bring your own Anabela Alves, Ph.D., Assistant Professor, Departamento de experiences to share and a desire to strengthen your complex Produção e Sistemas Escola de Engenharia da Universidade do systems engineering thinking. Minho, Centro Interdisciplinar de Tecnologias, da Produção e da Energia (CITPE), Campus de Azurém, Portugal Panelists: Paul C. Lambertson, Systems Engineering & Integration Team 777X, Boeing Commercial Airplanes 1400–1700 hrs Grand Ballroom E Steve Holt, Engineering Integrated Strategy, Airplane Level Whatever Happened to the Four-Year Airplane? Engineering Integration, The Boeing Company This panel will explore the challenges facing aerospace Jim Blohowiak, 777X Airplane Level Integration Team, The professionals who are directly engaged in leading, developing, Boeing Company producing, and supporting the industry’s most advanced vehicles Alison Lauderbach, 777X Airplane Level Integration Team, The and systems in the context of a “four-year aircraft” theme. We Boeing Company continue to push the limits of technology to deliver greater performance in all segments of aerospace, in an environment 1400–1530 hrs Steuben that is increasingly risk averse. These challenges have pushed us to longer development cycles and exponential growth in budgets. Concept Development of Complex Systems In addition, new technical disciplines (e.g., cyber) are being integrated into legacy and emerging systems, while subsystems This panel addresses the phase of development that includes are gaining in both complexity and interdependency. In the activities from the beginning of decision activities for building context of this environment, our panel will address how the new systems to the transition to the product design at milestone aerospace industry should position itself to meet the challenges “B” (DoD) or the end of Phase B for NASA. of reducing the cost and schedule and approach a “four-year Session Chairs: aircraft” cycle in our increasingly complex world. Steven D’Urso, Program Coordinator and Lecturer, Aerospace Moderator: Craig Willis, Group Head for Systems Verification, Systems Engineering, University of Illinois at Urbana- Gulfstream G500/G600 Program, Gulfstream Aerospace Champaign Corporation Mat French, Electrical Systems Engineer, Rolls-Royce Panelists: Corporation Catherine Ferrie Kilmain, Executive Vice President of Panelists: Engineering, Bell Helicopter Rick Mange, F-35 PNR Program Manager, Lockheed Martin Eric Schrock, Deputy Director, Technology Development and Aeronautics Product Integration, Lockheed Martin Corporation Robert (Rob) Simons, Technical Fellow, The Boeing Company Jason Merret, Technical Specialist, Gulfstream Aerospace Performance Engineering, Gulfstream Aerospace Corporation
www.aiaa-aviation.org 14 #aiaaAviation IntroForum 360
1545–1730 hrs Steuben 1045–1230 hrs Grand Ballroom D Product Design for Complex Systems Across the Entry into Service/End of Life Supply Chain This panel focuses on the complexities that arise once a This session will focus on the challenges and enabling system enters service throughout the life of the system. If these technologies for product design across a supply chain. In complexities are considered and incorporated into the system particular, the session will address the layered chain consisting of development phase, more robust products can be developed and OEM/airframer, Tier 1, Tier 2, and the approaches for designing higher customer satisfaction can be achieved. complex systems that handle the integration aspects. Methods Session Chair: Jeff Jepson, Senior Systems Engineer GNC / and model-based tool approaches will be discussed in terms of Guidance Design & Performance, Raytheon Missile Systems existing capabilities, gaps, and future trends. Panelists: Session Chairs: Tim Adama, Chief Engineer of Factories, Raytheon Missile Eelco Scholte, Manager, Advanced Methods – Electric Systems, Systems UTC Aerospace Systems Ed Dolanski, President and CEO, Aviall Carmen Schooley, Manager, Systems Engineering and Jim Gallagher, EIS Program Manager, Gulfstream Aerospace Integration, Gulfstream Aerospace Corporation Corporation Panelists: Fernando Dones, Technical Fellow, The Boeing Company 1400–1730 hrs Grand Ballroom D Bernard Dion, CTO, ANSYS System Complexity: Government Needs and Brenda Nuhfer, Program Manager, UTC/Pratt & Whitney Practical Research Results This panel is arranged around two application domains – defense Wednesday, 24 June systems and unmanned air systems in the national airspace – and two engineering practice needs – rapid system development 0900–1045 hrs Grand Ballroom D and new theory complex systems engineering. The expectation Integration and Test is that the audience will take away both a cogent statement of needs and challenges along with a concise description of new This panel focuses on the Integration & Test phase of techniques that show promise to meet the stated needs and development. Planning for integration activities of complex challenges. systems is inherently different from traditional systems engineering integration planning activities. Decisions about Keynote Speaker: Kristen Baldwin, Principal Deputy DASD the systems under development have to consider not only the (SE), Department of Defense technical and programmatic viewpoints but also the political, Moderators: societal, operational, and economic viewpoints. Definition of performance measures, found intrinsic in the plan, with trans- Frank Serna, Principal Director, Strategic Initiatives, Draper disciplinary implications will be discussed. A scenario for Laboratory integration of UAS in the NAS will be used as a benchmark for Anna-Maria McGowan, Aeronautics Research Directorate, current views and life-cycle challenges. NASA Langley Research Center Session Chairs: Panelists: Mat French, Electrical Systems Engineer, Rolls-Royce Jeffrey P. Holland, Director of Research and Development and Corporation Chief Scientist, U.S. Army Corps of Engineers Hernando Jiminez, Research Engineer II at Aerospace Systems David Neyland, Consultant Design Laboratory, Georgia Institute of Technology David Loda, Executive Director, NCPS Research, LLC Panelists: 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
www.aiaa-aviation.org 15 #aiaaAviation IntroForum 360
The multidimensional program features a leadership exchange/speed mentoring, panel session, Q&A with top Sponsored by: RISING industry leaders, and multiple opportunities for networking. LEADERS These exciting and energetic activities will provide access inAEROSPACE to top aerospace leaders and their perspectives with subject matter relevant to your career. Program Agenda
Networking Reception Panel Discussion: Transitioning to Leadership Monday, 22 June Emerald Thursday, 25 June Emerald 1830–1930 hrs 1400–1530 hrs The reception will kick off the Rising Leaders in Aerospace As engineers and aerospace professionals gain experience, there is events and is a perfect opportunity for young leaders to mingle often the opportunity to do more with the company. Promotions with others who will be participating in AIAA AVIATION are often a result, but so are management opportunities. 2015 as attendee, presenter, or veteran professional. Come As you transition from an engineer on a project to an engineer meet other participants in a casual environment. You’re bound leading a project, what changes? How about when you are made to see them again. 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? Leadership Exchange/Speed Networking This panel will address the changes that accompany moving Wednesday, 24 June Metropolitan Ballroom into a management role, the different skill sets that will need to 1530–1700 hrs be acquired, and the changes you can expect in your daily work Get your questions answered! Senior Mentors will include: routine. Russ Althof, Chief Engineer, Raytheon Missile Systems If you have management or leadership aspirations, come and listen to advice from esteemed panelists. Cees Bil, Professor, Royal Melbourne Institute of Technology Dave Bowles, Center Director (Acting), NASA Langley Research Moderator: Ben Marchionna, Systems Engineer, Lockheed Center Martin Skunk Works Ed Feltrop, Engineer Specialist , Cessna Aircraft Company Panelists: Susan Gorton, Rotary Wing Project, NASA Langley Research Russ Althof, Chief Engineer, Raytheon Missile Systems Center Douglas Stanley, President and Executive Director, National Peter Hartwich, Engineering Manager, Boeing Defense, Space Institute of Aerospace and Security Frederick Wieland, Director, Air Traffic Management, Janice Kavandi, Deputy Director, NASA Glenn Research Center Intelligent Automation Systems, Inc. Jeff Jepson, Senior Multi-Disciplined Engineer I, Raytheon Missile Systems Samantha A. Magill, Academic Affairs and Inclusion & Diversity, Honda Aircraft Company Sandy Magnus, Executive Director, AIAA David McBride, C enter Director, NASA Armstrong Flight Research Center Charles Smith, Center Director (Acting), NASA Ames Research Center John Valasek, Professor/Director, Vehicle Systems & Control Laboratory, Texas A&M University
www.aiaa-aviation.org 16 #aiaaAviation IntroSpecial Sessions and Events
Speed Geek Networking Event and Reception Monday, 22 June Chantilly Ballroom Foyer A MILE OF RUNWAY CAN 1730–1830 hrs, reception to follow 1830–1900 hrs TAKE YOU ANYWHERE. This 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 Showcase Tuesday, 23 June Chantilly Ballroom Foyer 1400–1600 hrs The 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 Banquet Wednesday, 24 June Imperial Ballroom 1900 hrs The 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 NARRATED BY recognized. Please join us and celebrate the achievements of your peers. Tickets will be available on site, as space is HARRISON FORD available.
See it in Dallas at the Perot Museum of Nature and Science www.airplanesmovie.com www.aiaa-aviation.org 17 #aiaaAviation IntroNetworking Events
Understanding the importance of networking with colleagues new and old, a series of activities have been planned that will help you connect with current colleagues and new acquaintances. Student Welcome Reception Reception in the Exposition Hall Sunday, 21 June Emerald Tuesday, 23 June Chantilly Ballroom East 1800–1930 hrs 1730–1900 hrs Mingle with your peers and hear from AIAA Executive Take this opportunity to engage new contacts and refresh old Director Sandy Magnus. This reception provides you with the ones. A ticket for the reception is required and included in the opportunity to meet your fellow students and learn more about registration fee where indicated. Additional tickets for guests the opportunities available to you as an AIAA student member. may be purchased on site, as space is available. Networking Coffee Breaks Networking coffee breaks allow even more time for making Luncheon in the Exposition Hall new contacts, continuing discussions from sessions, visiting Wednesday, 24 June Chantilly Ballroom East the Exposition Hall, or checking emails and voicemails to keep 1230–1400 hrs in touch with the office while you are at the forum. Networking A ticket is required and included in the registration fee where coffee breaks will be held at the following locations and times: indicated.
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
www.aiaa-aviation.org 18 #aiaaAviation Recognition Events
AIAA 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 June Thermophysics Award 1730–1830 hrs Grand Ballroom D Sumanta Acharya Fluid Dynamics Award Lecture Ring Chair & Professor, Mechanical Engineering Department University of Memphis Searching for Truthiness in Computational Fluid “For significant contributions to gas turbine heat transfer and Dynamics aerodynamics, investigation of novel cooling schemes and application of emerging computational methodologies for gas Philip Roe, Professor, Department of Aerospace Engineering, turbine cooling.” University of Michigan Certificates of Merit: Tuesday, 23 June Aerodynamic Measurement Technology Best Paper 1230–1400 hrs Chantilly Ballroom West AIAA 2015-1696, “Pressure Monitoring using Hybrid fs/ps Rotational CARS,” Sean Kearney, Sandia National Laboratories, Awards Luncheon: Celebrating Achievements and Paul Danehy, NASA Langley Research Center. in Aerospace Sciences Applied Aerodynamics Best Paper A ticket for the luncheon is required and included in the registration fee where indicated. Additional tickets for guests AIAA 2014-2139, “Uncertainty Quantification and may be purchased on site, as space is available. Certification Prediction of Low-Boom Supersonic Aircraft Configurations,” Thomas K. West, Missouri University of The following awards will be presented: Science and Technology; Bryan W. Reuter, University of Texas Aeroacoustics Award at Austin; Eric L. Walker, Bill Kleb, and Michael A. Park, NASA Langley Research Center. Nigel Peake Professor, Applied Mathematics David Weaver Best Student Paper University of Cambridge AIAA 2014-2247, “Microscale Simulations of Porous TPS “For significant contributions to the understanding and prediction Materials: Application to Permeability,” Eric C. Stern, Ioannis of turbomachinery noise generation and scattering.” Nompeli, Thomas Schwartzentruber and Graham Candler, Aerodynamics Award University of Minnesota. Russell M. Cummings Fluid Dynamics Best Paper Professor of Aeronautics AIAA Paper 2015-1518, “Large Eddy Simulation of a Three- U.S. Air Force Academy Dimensional Compression Ramp Shock-Turbulent Boundary “For a career devoted to predicting and understanding the Layer Interaction,” David Dawson and Sanjiva Lele, Stanford vortical flowfields about aircraft at high angles of attack and University. during maneuvers.” Ground Testing Best Paper Fluid Dynamics Award AIAA 2014-2800, “Skin Friction Sensor Validation for High- Philip Roe Speed, High-Enthalpy Flow Applications,” Ryan Meritt Professor, Department of Aerospace Engineering and Joseph Schetz, Virginia Polytechnic Institute and State University of Michigan University. “For seminal contributions to the design of numerical algorithms Modeling and Simulation Best Paper for simulations of compressible flows.” AIAA 2014-2206, “Transfer of Training on the Vertical Motion Plasmadynamics and Lasers Award Simulator,” Peter Zaal, NASA Ames Research Center; Jeffrey Philip E. Cassady Schroeder, Federal Aviation Administration; and William Chung, SAIC. Senior Technical Fellow (retired) The Boeing Company “For distinguished contributions to the development of aero-optics and high power laser fluid dynamics.” (continued) www.aiaa-aviation.org 19 #aiaaAviation Recognition Events
Certificates of Merit (continued) Thursday, 25 June Plasmadynamics and Lasers Best Paper 1230–1400 hrs Chantilly Ballroom West AIAA 2015-0935, “Electric Field Measurements in a Dielectric Barrier Nanosecond Pulse Discharge with Sub-nanosecond Awards Luncheon: Celebrating Achievements in Time Resolution,” Benjamin Goldberg and Walter Lempert, Aircraft and Atmospheric Systems Ohio State University; and Sean O’Byrne, University of New South Wales at the Australian Defence Force Academy. A ticket for the luncheon is required and included in the registration fee where indicated. Additional tickets for guests Plasmadynamics and Lasers Best Student Paper may be purchased on site, as space is available. AIAA 2015-0679, “A Latency-Tolerant Architecture for The following awards will be presented: Airborne Adaptive Optic Systems,” William R. Burns, Eric J. Jumper and Stanislav Gordeyev, University of Notre Dame. Aircraft Design Award Thermophysics Best Paper Darold B. Cummings AIAA 2015-0213, “NASA Langley Experimental Aerospace Consultant Aerothermodynamic Contributions to Slender and Winged Boeing Technical Fellow (retired) Hypersonic Vehicles,” Scott Berry and Karen Berger, NASA “For a career demonstrating exceptional skill and creativity in Langley Research Center. the configuration and design of aircraft, and inspiring future generations of aircraft designers.” 1630–1730 hrs Grand Ballroom D Plasmadynamics and Lasers Award Lecture Elmer A. Sperry Award Michael Sinnett, Vice President, Product Development, and From Plasmadynamics and Shock Tubes to Aero- the Boeing 787-8 Development Team, Seattle, Washington Optics and Laser Radar: An Aerospace Career “For pioneering engineering advances including lightweight Philip E. Cassady, Senior Technical Fellow (retired), The Boeing composite wing and monolithic composite fuselage construction Company and advanced systems that have led to significant improvements in fuel efficiency, reduced carbon emission, reduced maintenance Wednesday, 24 June costs and increased passenger comfort.” 1630–1730 hrs Chantilly Ballroom West Certificates of Merit: Aircraft Design Best Paper Aerodynamics Award Lecture AIAA 2014-3012, “A Requirements-driven Methodology for Still Trying to Understand Aircraft Vortices Integrating Subsystem Architecture Sizing and Analysis into the Conceptual Aircraft Design Phase,” Imon Chakraborty, David Russell M. Cummings, Professor of Aeronautics, U.S. Air Force Trawick, and Dimitri Mavris, Georgia Institute of Technology; Academy Mathias Emeneth, PACE Americas Inc.; and Alexander Schneegans, PACE GmbH. 1730–1830 hrs Grand Ballroom E Multidisciplinary Design Optimization Best Paper Thermophysics Award Lecture AIAA-2014-3274, “Aerostructural Optimization of the Common Research Model Configuration,” Gaetan Kenway and Joaquim Aerodynamics and Heat Transfer in Gas Turbine Martins, University of Michigan; and Graeme Kennedy, Georgia Cooling-Recent Advances Institute of Technology. Sumanta Acharya, Ring Chair & Professor, Mechanical Engineering Department, University of Memphis 1730–1830 hrs Chantilly Ballroom West Wright Brothers Lectureship in Aeronautics 1730–1830 hrs Chantilly Ballroom West Aeroacoustics Lecture Development and Testing of the X-47B Pablo Gonzalez II, UCAS-D Program Manager, Northrop Fan Broadband Noise Generation and Suppression Grumman Aerospace Systems Edmane Envia, Acoustics Branch, NASA Glenn Research Center
www.aiaa-aviation.org 20 #aiaaAviation IntroITAR Information
ITAR-Restricted Sessions Availability of Manuscripts from On Tuesday, a limited number of oral presentations and papers ITAR-Restricted Sessions will be presented in “U.S. Only” technical sessions. In addition For those who are registered to attend the sessions, a DVD to your forum registration, a separate registration process containing the papers from the ITAR sessions will be available is required to attend these restricted sessions. Please see the for purchase on site at the forum for $25. Those purchasing the detailed information on the ITAR Registration Grid below to DVD must be available to pick it up on Wednesday, 24 June determine your individual requirements. 2015. All DVDs must be picked up in person. There will be no sale or distribution of these papers after the event. Access to ITAR Sessions: Presenting a Paper, Chairing a Session, or Attending an ITAR- ITAR Electronics Policy Restricted Presentation No phones, computers (other than the presenter), iPads, Admittance to the restricted technical program is controlled by cameras, or other electronic devices with cameras or recording the U.S. International Traffic in Arms Regulations (ITAR). All capabilities will be permitted into the ITAR session room. attendees, presenters, and session chairs will need to register There will be a check-in desk in front of the room where you for the conference, and then visit the ITAR registration desk can check these devices. 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!
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 otheri ver fication 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.
10/19/2012 www.aiaa-aviation.org 21 #aiaaAviation IntroExposition Hall
Exhibitor Lounge
MathWorks Altair
AIAA Pavilion
ANSYS XFlow CFD
Kamatics /RWG
Desktop SG ADI 309 410 dSPACE Ennova G.R.A.S. DUNMORE 208 307 408
Software Tecplot BETA CAE Exa Corp Cradle 303 304 403 404 OPAL-RT Pointwise Photron 30 301 302 401
ENTRANCE
Exhibitors by Booth Number
217 AIAA North Texas Section 314 Lockheed Martin 420 Altair 320 MathWorks 213 ANSYS 301 OPAL-RT Technologies 410 Applied Dynamics International (ADI) 401 Photron 403 BETA CAE Systems USA, Inc. 302 Pointwise, Inc. 219 DARcorporation 309 SG - Space & Ground Engineering Solutions 209 Desktop Aeronautics 303 Software Cradle 207 dSPACE 304 Tecplot Inc. 408 DUNMORE Corporation 301 VectorNav Technologies 208 Ennova Technologies, Inc. 416 Vision Research 215 ESI North America 414 XFlow CFD 211 ESTECO 404 Exa Corporation 307 G.R.A.S. Sound & Vibration 412 Kamatics/RWG www.aiaa-aviation.org 22 #aiaaAviation IntroExposition Hall
The Exposition Hall is the hub of activity during this event—from seeing exhibitor displays to enjoying networking breaks and other functions. All the major networking events are held in the Exposition Hall to give attendees and exhibitors an opportunity to connect with partners, industry thought leaders, and collaborators who can help move your business forward. The Exposition Hall is located in the Chantilly Ballroom East. Exposition Hall Hours 30% Off All Books at AIAA AVIATION 2015 Tuesday, 23 June 0900–1230 hrs AIAA Publications is offering a special show discount on all titles 1400–1600 hrs featured at AVIATION 2015. Attendees can take advantage of a Reception* 1730–1900 hrs 30% discount off the list price of all books for sale at the AIAA Bookstore located in the AIAA Pavilion. This show special will Wednesday, 24 June 0900–1200 hrs only be available during the forum! Take advantage of these 1230–1600 hrs super savings and visit the AIAA Bookstore! Thursday, 25 June 0900–1200 hrs
*A ticket is required and included in the registration fee where indicated
AIAA Pavilion Stop by the AIAA Pavilion, located in the Exposition Hall, to browse publications and merchandise, learn about your membership benefits, and meet AIAA staff.
www.aiaa-aviation.org 23 #aiaaAviation Exhibitors AIAA North Texas Section 217 DARcorporation 219 1440 Wakarusa Drive Lawrence, KS 66049 www.darcopr.com [email protected]
DARcorporation (Design, Analysis and Research Corporation) is an Altair 420 aeronautical engineering firm, located in Lawrence, Kansas, that has 1820 E Big Beaver Road been offering aeronautical engineering consulting services, software Troy, MI 48083 and books since 1991. www.altair.com [email protected] Desktop Aeronautics Inc. 209 Altair is a leader in developing simulation-driven designs for 1900 Embarcadero Road leading aerospace customers. Our world-class optimization methods Suite 101 provide designs that are lower weight, higher quality, and have better Palo Alto, CA 94303 performance vs. traditional designs. www.desktopaero.com [email protected]
ANSYS, Inc. 213 Desktop Aeronautics is a software company that licenses tools for 2600 ANSYS Drive the aerodynamic design and analysis of aerospace vehicles. Our Cannonsburg, PA 15317 flagship product, GoCart, is an intuitive aerial vehicle design tool built www.ansys.com around NASA’s renowned Cartesian Euler CFD solver, Cart3D. Our [email protected] customers include major players from the aerospace industry and academia. 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 dSPACE 207 users to simulate design performance using an open platform for fast, 50131 Pontiac Trail efficient and cost-effective product development. Wixom, MI 48393-2020 www.dspaceinc.com Applied Dynamics International 410 [email protected] 3800 Stone School Road dSPACE is the world’s leading provider of hardware and software tools Ann Arbor, MI 48108-2499 for developing and testing sophisticated electronic control systems. www.adi.com dSPACE systems play a vital role in product innovation industries. [email protected] Learn more at: www.dspaceinc.com.
Applied Dynamics helps companies make better use of simulation assets through all stages of product development, verification DUNMORE Corporation 408 testing, demonstration, training, and maintenance. Our user base 145 Wharton Road includes more than 50% of the Fortune 500 aerospace and defense Bristol, PA 19007 companies and extends into marine, power systems, oil & gas, and the www.dunmore.com R automotive industry. [email protected]
DUNMORE is a manufacturer of engineered films and tapes for BETA CAE Systems USA, Inc. 403 aerospace, supplying multilayer insulation materials to the aerospace 29800 Middlebelt Road industry for over twenty-five years. With a highly technical product Suite #100 base of over 400 certified products, DUNMORE is the trusted source Farmington Hills, MI 48334 for engineered aerospace films and tapes. www.ansa-usa.com [email protected]
BETA CAE Systems is an engineering services company that distributes & supports the industry leading ANSA & META software. ANSA is CAE pre-processing tool for FE & CFD Analysis, for full-model build, from CAD to solver input file, in one integrated environment. META is a post-processor for analyzing results from ANSYS, NASTRAN, ABAQUS, LS-DYNA, PAMCRASH, RADIOSS, MADYMO, FLUENT, STAR CCM, CFD++ & other solvers.
www.aiaa-aviation.org 24 #aiaaAviation Exhibitors Ennova Technologies Inc 208 G.R.A.S. Sound & Vibration 307 2150 Allston Way, Suite 250 2234 E Enterprise Parkway Berkeley, CA 94704 Twinsburg, OH 44087 ennova-cfd.com ScalableEnnova Simulation Delivered www.gras.uk [email protected] [email protected]
Ennova Technologies delivers today’s most scalable simulation G.R.A.S. has concentrated its efforts and expertise on the platform combining the power of cloud based computing, advanced development and production of front-end acoustic products. This geometry repair tools, and mixed mode meshing to create an includes in principle all products necessary for the precise and reliable extremely efficient pre and post processing simulation environment. 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 ESI North America 215 preamplifiers, all designed and manufactured in accordance with 32605 West Twelve Mile Road, Ste 350 international standards. Farmington Hills, MI 48334 www.esi-group.com [email protected] Kamatics/RWG 412 1330 Blue Hills Ave ESI’s 1,000 Virtual Prototyping and Mfg Simulation specialists serve Bloomfield, CT 06002 clients in over 40 countries. For over 40 years, ESI’s simulation www.kaman.com/engineered software suite has been used to tackle the toughest Acoustics, Crash, [email protected] VR, Composites, Casting, Welding, Forming, and CFD engineering challenges—earning the slogan “We get it right.” For more info: www. For decades, Kamatics (USA) and RWG have been designing, testing, esi-group.com and manufacturing the highest performing bearings and flight critical parts in the industry, excelling under the most demanding conditions. ESTECO 211 39555 Orchard Hill Place Lockheed Martin Corporation 314 Novi, MI 48375 P.O. Box 748 MZ 1500 www.esteco.com Fort Worth, TX 76101 [email protected] www.lockheedmartin.com [email protected] ESTECO is a pioneer in numerical optimization solutions, specializing in the research and development of engineering Lockheed Martin is principally engaged in the research, design, software for all stages of the simulation-driven design process. development, manufacture, integration and sustainment of advance ESTECO’s top-class products, modeFRONTIER and SOMO, are technology systems, products and services. used worldwide, helping companies increase efficiency in design simulation and accelerate product innovation. MathWorks 320 3 Apple Hill Drive Exa Corporation 404 Natick, MA 01760 55 Network Drive www.mathworks.com/academia Burlington, MA 01803 www.exa.com The MATLAB and Simulink product families are fundamental [email protected] applied math and computational tools at the world’s educational institutions. Adopted by more than 5000 universities and colleges, Exa Corporation offers a full suite of CFD/CAE simulation design MathWorks products accelerate the pace of learning, teaching, and optimization software applications with aerodynamic, thermal research in engineering and science. MathWorks products also and aeroacoustic simulation capabilities in addition to engineering help prepare students for careers in industry worldwide, where the consulting services. Exa’s products and services enable engineers to tools are widely used for data analysis, mathematical modeling, and integrate simulation early in the design process, therefore creating algorithm development in collaborative research and new product competitive designs, shortening product design cycles and speeding development. time-to-market.
www.aiaa-aviation.org 25 #aiaaAviation IntroExhibitors
OPAL-RT TECHNOLOGIES 301 Tecplot, Inc 304 1751 Richardson, Suite 2525 3535 Factoria Blvd SE, Suite 550 Montreal Quebec H3K 1G6 Bellevue, WA 98006 www.opal-rt.com www.tecplot.com [email protected] [email protected]
OPAL-RT: From Imagination… to Real-Time. OPAL-RT Tecplot visualization tools—for simulations, analyses, and TECHNOLOGIES is a world leading developer of open, Real-Time experiments—provide insight and understanding into the Digital Simulators and Hardware-in-the-Loop testing equipment mechanisms inside your data. Information critical in pinpointing for electrical, electro-mechanical and power electronics systems. problems, optimizing designs, and explaining physical observations. Our simulators are used by engineers and researchers at leading manufacturers, utilities, universities and research centers around the world. VectorNav Technologies 301 10501 Markison Road Photron 401 Dallas, TX 75238 www.vectornav.com 9520 Padgett Street, Suite 110 [email protected] San Diego, CA 92126 www.photron.com VectorNav specializes in high-performance inertial navigation [email protected] systems using the latest MEMS sensor and GPS/GNSS technology. Since its founding in 2008, we have been providing customers Photron’s wide range of light sensitive high-speed cameras including worldwide fully calibrated inertial sensors with aerospace-grade systems ideally suited to PIV and DIC, mega pixel to 21,000 frames filtering technology, expanding the possibilities of today’s inertial per second (fps) and 4M pixels producing HD to 2,000 fps. Photron navigation technology. has a slow motion camera for every application.
Pointwise, Inc. 302 Vision Research 416 100 Dey Road 213 S. Jennings Avenue Wayne, NJ 07470 Fort Worth, TX 76104 www.visionresearch.com www.pointwise.com [email protected] [email protected] Vision Research designs and manufactures high-speed digital imaging Pointwise is solving the top problem facing engineering analysts systems with unsurpassed light-sensitivity, image resolution, acquisition today: grid generation and preprocessing for computational fluid speed and image quality. Marketed under the Phantom®brand,these dynamics. Since 1994, Pointwise has supplied meshing tools to cameras enable users to visualize and analyze physical phenomena engineers and scientists worldwide. when it’s too fast to see, and too important not to™.
SG-Space & Ground Engineering Solutions 309 XFlow CFD 414 6A Aigiidon Street 40 Chellis Street Athens, Attica Greece 11853 White River Junction, VT 05001 www.sg-incorp.com www.xflowusa.com [email protected] [email protected].
SG Company provides integrated engineering solutions for air/space- XFlow™ CFD is the next-generation, meshless CFD package for based earth monitoring systems and develops special techniques for modeling external aerodynamics of fixed-wing and rotorcraft aircraft. UAS (Unmanned Aerial Systems) earth observation applications in XFlow supports complex motion of complicated moving parts to various disciplines. model dynamic effects of control surface motion in flight, high-lift (take-off and landing) configurations and/or separation of munitions Software Cradle 303 or separable stores. 70 Birch Alley, Suite 240 Beavercreek, OH 45440 www.cradle-cfd.com [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. www.aiaa-aviation.org 26 #aiaaAviation IntroGeneral Information
AIAA Registration and Information Center Hours Conference Proceedings The AIAA Registration and Information Center will be located Proceedings for the forum will be available online. The cost on the Ballroom Level at the Hyatt Regency. Hours are as is included in the registration fee where indicated. Online follows: proceedings will be available on 22 June 2015. Attendees who Sunday, 21 June 1500–1900 hrs register in advance for the online proceedings will be provided with instructions on how to access them. Those registering on site Monday, 22 June – Thursday, 25 June 0700–1730 hrs will be provided with instructions at that time. Friday, 26 June 0700–1200 hrs Proceedings: 1. To view proceedings visit www.aiaa.org >ARC>Meeting Papers. Wi-Fi Internet Access On Site a. Log in with the link at the top right of the page. AIAA is providing limited Wi-Fi service for attendees to use b. Select the appropriate conference from the list. while on site. To keep this service available and optimized for all attendees, please do not download files larger than 2MB, create c. Search for individual papers with the Quick Search multiple sessions across multiple devices, or download multiple toolbar in the upper-right corner of the page: files in one session. If you receive an error message that an AIAA i. By paper number: Click the “Paper Number” link, server is blocking your current IP address, please inform the select the conference year, and enter the paper number. AIAA registration desk. ii. Use the Search textbox to find papers by author, title, or keyword. The Advanced Search link provides Social Media Kiosks additional search information and options. 2. All manuscript files submitted at least four days prior to the Throughout the forum, social media kiosks will display conference are currently in the proceedings. Files submitted content shared by forum attendees! Look for your tweets or after that date, both original and revised manuscripts, will instagrams to be displayed on the screens. AIAA is also hosting not be available until the final proceedings update, which a competition where the user who has posted the most tweets may take up to 15 business days after the last day of the during the forum will win a prize. 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.
www.aiaa-aviation.org 27 #aiaaAviation IntroGeneral Information
Certificate of Attendance Young Professional Guide for Gaining Certificates of Attendance are available for attendees who Management Support request documentation at the forum itself. The Certificates of Young professionals have the unique opportunity to meet and Attendance will be available for attendees to print at a self- learn from some of the most important people in the business service station at the registration desk starting Wednesday, by attending conferences and participating in AIAA activities. 24 June. AIAA offers this service to better serve the needs of A detailed online guide, published by the AIAA Young the professional community. Claims of hours or applicability Professional Committee, is available to help you gain support toward professional education requirements are the and financial backing from your company. The guide explains responsibility of the participant. 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 Employment Opportunities participation. The online guide can be found on the AIAA website at www.aiaa.org/YPGuide. AIAA 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 Nondiscriminatory Practices postings in the Exposition Hall. AIAA accepts registrations irrespective of race, creed, gender, color, sexual orientation, physical handicap, and national or ethnic origin. Membership AIAA is your vital lifelong link to the collective creativity and brainpower of the aerospace profession and a champion for its Restrictions achievements – and nonmembers who pay the full conference Photos, video, or audio recording of sessions or exhibits, as registration fee will receive their first year’s AIAA membership well as the unauthorized sale of AIAA-copyrighted material, is at no additional cost! Students who are not yet members may prohibited. apply their registration fee toward their first year’s student member dues. (Free membership is not included in discounted group-rate registration.) International Traffic in Arms Regulations (ITAR) AIAA speakers and attendees are reminded that some AIAA Foundation topics discussed in the conference could be controlled by the International Traffic in Arms Regulations (ITAR). Since 1996 the AIAA Foundation has provided programs U.S. nationals (U.S. citizens and permanent residents) are and support for educators and students. Through classroom responsible for ensuring that technical data they present grants, scholarships, awards, design competitions, and in open sessions to non-U.S. nationals in attendance or in student conferences, the AIAA Foundation has encouraged conference proceedings are not export restricted by the ITAR. students in grades K-12 and at the university level to discover U.S. nationals are likewise responsible for ensuring that they do the aerospace industry and become the next generation of not discuss ITAR export-restricted information with non-U.S. scientists and engineers. Please consider making a donation nationals in attendance. 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.
www.aiaa-aviation.org 28 #aiaaAviation IntroGeneral Information
Author and Session Chair Information
Speakers’ Briefings in Session Rooms Audiovisual Authors who are presenting papers will meet with session chairs Each session room will be preset with the following: one LCD and co-chairs in their session rooms for a short 30-minute projector, one screen, one microphone and sound system briefing on the day of their sessions to exchange bios and review (if necessitated by room size), and one laser pointer. Laptop final details prior to the session. Please attend on the day of computers will also be provided. You may also use your your session(s). Laptops preloaded with the Speaker Briefing own computer. Any additional audiovisual equipment preparation slides will be provided in each session room. requested onsite will be at cost to the presenter. Please note Speaker’s Briefing schedule is as follows: that AIAA does not provide security in the session rooms and Monday 22 June–Friday 26 June, 0730 hrs recommends that items of value not be left unattended Speakers’ Practice Room “No Paper, No Podium” and “No Podium, No Paper” Policy Speakers who wish to practice their presentations may do so in the Peridot room. A sign-up sheet will be posted on the If a written paper is not submitted by the final manuscript door. In consideration of others, please limit practice time to deadline, authors will not be permitted to present the paper at 30-minute increments. the forum. Also, if the paper is not presented at the forum, it will be withdrawn from the proceedings. It is the responsibility Session Chair Reports of those authors whose papers or presentations are accepted to ensure that a representative attends the conference to present All session chairs are asked to complete a session chair report to the paper. These policies are intended to improve the quality of evaluate their session for future planning. AIAA has partnered the program for attendees.. with Canvas Solutions to provide an electronic Session Chair Report form. You can download the FREE mobile app in Journal Publication your App Store, AppWorld, or Marketplace by searching for “Canvas Solutions, Inc.” The mobile app is free, so please be Authors of appropriate papers are encouraged to submit sure to download it. Detailed instructions will be provided in them for possible publication in one of the Institute’s archival the session rooms. If you do not have a tablet or a smartphone, journals: AIAA Journal; Journal of Aircraft; Journal of Guidance, simply use the report form as a guide and enter your session Control, and Dynamics; Journal of Propulsion and Power; chair report information at the session chair reporting computer Journal of Spacecraft and Rockets; Journal of Thermophysics station located on site near the AIAA registration area. Report and Heat Transfer; or Journal of Aerospace Information Systems data will be collected and used for future planning purposes, (formerly Journal of Aerospace Computing, Information, and including session topics and room allocations. Please submit Communication). You may now submit your paper online at your session chair report electronically by Friday, 26 June 2015. http://mc.manuscriptcentral.com/aiaa.
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
www.aiaa-aviation.org 29 #aiaaAviation IntroCommittee Meetings
Time Title Location Sunday, 21 June 2015 0900-1600 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 2015 0800-1200 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 Cardinal A & B Coordination 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
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Time 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 2015 0800-1600 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 2015 0800-1200 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 www.aiaa-aviation.org 31 #aiaaAviation IntroCommittee Meetings
Time Title Location Thursday, 25 June 2015 0900-1100 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
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Abbreviation Title Date Start Time Location Aeroacoustics 3-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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Abbreviation Title Date Start Time Location Aircraft Design 42-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 Mechanics 8-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 Testing 10-AMT-1/GT-1 Hap Arnold's New Horizon: The Future Role of Ground Test in High Speed System 22-Jun 0900 hrs Obelisk B Development 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/ Molecular-Based Optical Diagnostics for Hypersonic Nonequilibrium Flows 23-Jun 1400 hrs Topaz TP-6/GT-8 158-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 Aerodynamics 12-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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Abbreviation Title Date Start Time Location Applied Aerodynamics (continued) 49-APA-7 Special Session: Aerodynamic-Structural Modeling, Optimization, and Test Techniques for 22-Jun 1400 hrs Stemmons A Flexible Wing Technology I 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 23-Jun 1400 hrs Stemmons A Flexible Wing Technology II 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 Environments 163-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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Abbreviation Title Date Start Time Location Aviation Technology, Integration, and Operations 16-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 22-Jun 1400 hrs Metropolitan Autonomy 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 Systems 167-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
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Abbreviation 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
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Abbreviation Title Date Start Time Location Fluid Dynamics 25-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/ Molecular-Based Optical Diagnostics for Hypersonic Nonequilibrium Flows 23-Jun 1400 hrs Topaz TP-6/GT-8 136-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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Abbreviation Title Date Start Time Location Flight Testing 249-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 Engineering 281-GEPC-1 Overview of NASA Advanced Air Vehicles Program 25-Jun 1400 hrs Metropolitan Ballroom ITAR Sessions 103-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 Systems 250-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 Optimization 29-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 Technologies 30-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 23-Jun 1400 hrs Travertine NAS) Test Bed Development (Invited) 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 39 #aiaaAviation IntroSessions at a Glance
Abbreviation 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 Thermophysics 34-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/ Molecular-Based Optical Diagnostics for Hypersonic Nonequilibrium Flows 23-Jun 1400 hrs Topaz TP-6/GT-8 145-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
www.aiaa-aviation.org 40 #aiaaAviation Monday Monday, 22 June 2015 1-SB-1 Speakers’ Briefing Session Rooms 0730 - 0800 hrs Monday, 22 June 2015 2-PLNRY-1 Opening Keynote Chantilly Ballroom West 0800 - 0900 hrs
Are We Moving Fast Enough? Tom Enders Chief Executive Officer Airbus Group Monday, 22 June 2015 3-AA-1 Airframe Noise I Fleur-de-lis A Chaired by: D. LOCKARD, NASA-Langley Research Center 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2015-2200 AIAA-2015-2201 AIAA-2015-2202 AIAA-2015-2203 AIAA-2015-2204 AIAA-2015-2205 AIAA-2015-2206 Aeroacoustic and Aerodynamic Aerodynamic and Aeroacoustic Broadband noise reduction through Airfoil noise prediction from 2D3C Noise generation by turbulence Detailed experimental investigation 2D high-lift airfoil noise Performances of an Aerofoil Performance of Serrated Airfoils leading edge serrations on realistic PIV data interacting with an aerofoil with a of the aeroacoustic field around a measurements in an aerodynamic Subjected to Sinusoidal Leading X. Liu, M. Azarpeyvand, R. Theunissen, aerofoils L. de Santana, Catholic University of serrated leading edge Controlled-Diffusion airfoil wind tunnel Edges University of Bristol, Bristol, United C. Paruchuri, N. Subramanian, P. Leuven, Leuven, Belgium; C. Schram, J. Mathews, N. Peake, University of T. Padois, P. Laffay, A. Idier, S. Moreau, V. Fleury, J. Bulte, R. Davy, E. Manoha, T. Chong, S. Siddiqi, Brunel University, Kingdom Joseph, C. Vanderwel, J. Kim, B. von Kármán Institute for Fluid Dynamics, Cambridge, Cambridge, United Kingdom University of Sherbrooke, Sherbrooke, ONERA, Châtillon, France; M. Pott- Rhode-Saint-Genèse, Belgium; W. Desmet, 41 Uxbridge, United Kingdom Ganapathisubramani, University of Canada Pollenske, German Aerospace Center Southampton, Southampton, United Catholic University of Leuven, Leuven, (DLR), Braunschweig, Germany Kingdom Belgium Monday, 22 June 2015 4-AA-2 Jet Noise Prediction I Fleur-de-lis B Chaired by: P. MORRIS, Pennsylvania State University 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2015-2207 AIAA-2015-2208 AIAA-2015-2209 AIAA-2015-2210 AIAA-2015-2211 AIAA-2015-2212 AIAA-2015-2213 Assessment of Jet-plate Interaction Installation noise of a turbofan jet Large-eddy simulation of Large-eddy simulation of Noise Characteristics of a Four-Jet Simulation and stability analysis Hybrid approach for the prediction Noise Using the Lattice Boltzmann engine under an airfoil supersonic planar jets impinging underexpanded round jets Impingement Device Inside a of a supersonic impinging jet at of jet noise interaction and Method G. Brichet, M. Koenig, Safran Group, on a flat plate at an angle of 60 to impinging on a flat plate 4 to 9 Broadband Engine Noise Simulator varying nozzle-to-wall distances installation effects F. da Silva, C. Deschamps, A. da Silva, Moissy-Cramayel, France; C. Bailly, École 90 degrees radii downstream from the nozzle C. Brehm, J. Housman, C. Kiris, NASA N. Hildebrand, J. Nichols, University of Y. Yang, Y. Sun, C. Breard, Commercial Federal University of Santa Catarina, Centrale de Lyon, Ecully, France R. Gojon, C. Bogey, O. Marsden, École R. Gojon, C. Bogey, O. Marsden, École Ames Research Center, Moffett Field, CA; Minnesota, Twin Cities, Minneapolis, MN Aircraft Corporation of China, Ltd. Florianópolis, Brazil; L. Simões, Embraer, Centrale de Lyon, Ecully, France Centrale de Lyon, Ecully, France F. Hutcheson, NASA Langley Research (COMAC), Shanghai, China São José dos Campos, Brazil Center, Hampton, VA Monday, 22 June 2015 5-AA-3 Jet Noise Modeling I Inverness Chaired by: C. BOGEY, Ecole Centrale de Lyon 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2015-2214 AIAA-2015-2215 AIAA-2015-2216 AIAA-2015-2217 AIAA-2015-2218 AIAA-2015-2219 AIAA-2015-2220 Real-time modelling of Automatic Optimizer vs Human The prediction of the radiated Stochastic and nonlinear forcing of Sensitivity of wavepackets in jets to Sensitivity analysis for subsonic jet A Control Framework for wavepackets in turbulent jets Optimizer for Low-Order Jet Noise pressure spectrum produced by wavepackets in a Mach 0.9 jet non-linear effects: the role of the using adjoint of non local stability Wavepackets in Turbulent Jets K. Sasaki, Technological Institute of Modelling jet-wing interaction A. Towne, T. Colonius, California Institute critical layer equations Using Time-Domain Transfer Aeronautics (ITA), São José dos Campos, Y. Korolev, S. Karabasov, V. Toropov, J. Vera, J. Lawrence, R. Self, M. Kingan, of Technology, Pasadena, CA; P. Jordan, G. Tissot, Technological Institute of Aeronautics C. Airiau, T. Ansaldi, University of Toulouse, Functions Brazil; S. Piantanida, National Center Queen Mary University of London, London, University of Southampton, Southampton, National Center for Scientific Research (ITA), São José dos Campos, Brazil; M. Toulouse, France F. Silvestre, M. Caprecci, A. Cavalieri, for Scientific Research (CNRS), Poitiers, United Kingdom United Kingdom (CNRS), Poitiers, France; A. Cavalieri, Zhang, National Center for Scientific Research Technological Institute of Aeronautics France; A. Cavalieri, Technological Technological Institute of Aeronautics (CNRS), Poitiers, France; F. Lajús, A. Cavalieri, (ITA), São José dos Campos, Brazil; P. Institute of Aeronautics (ITA), São José (ITA), São José dos Campos, Brazil; G. Technological Institute of Aeronautics (ITA), Jordan, École Nationale Supérieure des dos Campos, Brazil; P. Jordan, National Brès, Cascade Technologies, Inc., Palo São José dos Campos, Brazil; P. Jordan, Mines de Saint-Étienne, Poitiers, France Center for Scientific Research (CNRS), Alto, CA National Center for Scientific Research Poitiers, France (CNRS), Poitiers, France; T. Colonius, California Institute of Technology, Pasadena, CA Monday, 22 June 2015 6-AA-4 CAA Numerical Techniques I Lalique Chaired by: W. SCHROEDER, RWTH AACHEN, Institute of Aerodynamics 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2015-2221 AIAA-2015-2222 AIAA-2015-2223 AIAA-2015-2224 AIAA-2015-2225 AIAA-2015-2226 Experimental Validation of CAA Study of Airfoil Broadband CABARET GPU Solver for Fast-Turn- Assessment of Flap Side-Edge Fence Verification of a Viscous Acoustic loads prediction for a Aero-Vibro-Acoustic Analysis of Interaction Noise Using Stochastic Around Flow and Noise Calculations Noise using SNGR Method Computational Aeroacoustics Code commercial transport aircraft under A. Markesteijn, V. Semiletov, S. Karabasov, H. Yao, L. Davidson, Chalmers University of
42 Production Vehicles (Invited) Turbulent Vorticity Sources using External Verification Analysis ground and flight conditions S. Caro, CD-adapco, Lyon, France T. Hainaut, G. Gabard, V. Clair, University Queen Mary University of London, London, Technology, Göteborg, Sweden; S. Peng, D. Ingraham, D. Hixon, University of Y. Sun, Y. Yang, C. Breard, Commercial of Southampton, Southampton, United United Kingdom Swedish Defense Research Agency (FOI), Toledo, Toledo, OH Aircraft Corporation of China, Ltd. Kingdom Stockholm, Sweden; L. Eriksson, Chalmers (COMAC), Shanghai, China University of Technology, Göteborg, Sweden; M. Barbarino, F. Capizzano, Italian Aerospace Research Center (CIRA), Capua, Italy; et al. Monday, 22 June 2015 7-AA-5 Duct Acoustics I Obelisk A Chaired by: W. EVERSMAN, Missouri University of Science and Technology 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2015-2227 AIAA-2015-2228 AIAA-2015-2229 AIAA-2015-2230 AIAA-2015-2231 AIAA-2015-2232 AIAA-2015-2233 Effect of viscosity on impedance Impedance Eduction in Sound Fields The Effective Impedance of a Acoustic Liner Drag: A Parametric Experimental Study of the Duct spinning mode’s particle In-duct Beamforming Noise eduction and validation with Peripherally Varying Liners Finite-Thickness Viscothermal Study of Conventional Mechanisms of Sound Generation velocity imaging on a cross plane Source Estimation Mode Detection L. Zhou, H. Boden, Royal Institute of and Flow Boundary Layer Over an Acoustic Configurations Due to an In-duct Orifice Plate outside the duct University of São Paulo Fan Rig Technology (KTH), Stockholm, Sweden W. Watson, M. Jones, NASA Langley Lining B. Howerton, M. Jones, NASA Langley F. Tao, X. Zhang, P. Joseph, O. Stalnov, W. Yu, Q. Wei, X. Huang, Peking L. Caldas, L. Baccala, R. Cuenca, Research Center, Hampton, VA D. Khamis, E. Brambley, University of Research Center, Hampton, VA University of Southampton, Southampton, University, Beijing, China University of São Paulo, São Paulo, Cambridge, Cambridge, United Kingdom United Kingdom; M. Siercke, H. Scheel, Brazil; R. Queiroz, Embraer, São José dos Airbus, Hamburg, Germany Campos, Brazil Monday, 22 June 2015 8-AFM-1 Aircraft Flight Dynamics, Control, Handling Qualities and Performance I Plum Blossom A Chaired by: E. GILLESPIE, United Space Alliance 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2015-2234 AIAA-2015-2235 AIAA-2015-2236 AIAA-2015-2237 AIAA-2015-2238 Benefits of Formation Flight of Automatic Stall/Spin Detection in Extracting Airplane Performance Validation of a Model Based Structural Roll performance assessment of a Extended Duration Considering Fuel Fixed-Wing Aircraft for a Fatal Accident in the Absence Loads Monitoring System using the light aircraft: flight tests and flight Burn R. Bunge, F. Munera Savino, I. Kroo, of a Flight Data Recorder Flight Test Aircraft UW-9 Sprint simulation W. Okolo, A. Dogan, University of Texas, Stanford University, Stanford, CA T. Burtch, National Transportation Safety M. Montel, F. Thielecke, Hamburg University F. Nicolosi, A. De Marco, V. Sabetta, Arlington, Arlington, TX; W. Blake, Air Force Board, Washington, DC of Technology, Hamburg, Germany P. Della Vecchia, University of Naples Research Laboratory, Wright-Patterson “Federico II”, Naples, Italy AFB, OH Monday, 22 June 2015 9-AFM-2 Aeroservoelastic (ASE) Modeling Plum Blossom B Chaired by: T. ALEXEEV, University of California Davis and F. PRIOLO, Millennium Engineering and Integration Company 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2015-2239 AIAA-2015-2240 AIAA-2015-2241 AIAA-2015-2242 AIAA-2015-2243 AIAA-2015-2244 AIAA-2015-2245 Control of a Nonlinear Wing Section Aeroelastic State-space Model Optimal Sizing and Configurations Aeroelastic Tailoring for Adaptive Feedforward Control Delta Adaptive Flexible Motion Feedback Linearization based using Fly-by-Feel Sensing Development Based on Frequency of the Control Surfaces for Active Maximizing Sailplane Average Design for Gust Loads Alleviation of Control for the X-56A Aircraft Control of Aeroelastic Systems V. Suryakumar, Y. Babbar, T. Strganac, Response Identification and Aeroelastic Control Cross-Country Speed Highly Flexible Aircraft K. Hashemi, University of Texas, Austin, represented in Modal Coordinates Texas A&M University, College Station, TX; Integration with Flight Dynamics R. Brown, K. Singh, Miami University, C. Lupp, C. Cesnik, University of Michigan, Y. Wang, F. Li, China Academy of Austin, TX; C. Pak, NASA Armstrong Flight H. Shukla, M. Patil, Virginia Polytechnic A. Mangalam, Tao of Systems Integration, T. Buttini, F. Moreira, Embraer, São José Oxford, OH Ann Arbor, Ann Arbor, MI Aerospace Aerodynamics, Beijing, China; Research Center, Edwards, CA; M. Akella, Institute and State University, Blacksburg, Inc., Hampton, VA dos Campos, Brazil; F. Silvestre, R. A. da A. Da Ronch, University of Southampton, University of Texas, Austin, Austin, TX VA Silva, Technological Institute of Aeronautics Southampton, United Kingdom
43 (ITA), São José dos Campos, Brazil Monday, 22 June 2015 10-AMT-1/GT-1 Hap Arnold’s New Horizon: The Future Role of Ground Test in High Speed System Development Obelisk B Chaired by: J. SCHMISSEUR and G. LISTON 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs Oral Presentation Oral Presentation Oral Presentation Oral Presentation Panel Discusssion Envisioning the Future of the T&E Challenges and Opportunities in the Introduction to the AFRL High- Development of Large-Scale Quiet The Future of Ground Test within Enterprise Development of T&E Capabilities Speed Experimentation Branch Tunnels Supporting T&E T&E M. Lewis, IDA, Washington, DC J. Schmisseur, University of Tennessee, G. Liston, Air Force Research Laboratory, T. Juliano, Notre Dame University, Notre J. Schmisseur, University of Tennessee, Tullahoma, Tullahoma, TN Cleveland, OH Dame, IN Tullahoma, Tullahoma, TN Monday, 22 June 2015 11-AMT-2/GT-2 Line of Sight and Density Measurement Edelweiss Chaired by: S. O’BYRNE, The University of New South Wales 0900 hrs 0930 hrs 1000 hrs 1030 hrs AIAA-2015-2246 AIAA-2015-2247 AIAA-2015-2248 AIAA-2015-2249 Analysis of Focused Laser Simultaneous Measurements Optical Measurements of Velocity, A Time-Resolved Temperature Differential Interferometry of Density Field and Wavefront Density, and Mass Flux in a Measurement System for Free- B. Schmidt, J. Shepherd, California Distortions in High Speed Jet Flows Supersonic Wind Tunnel Piston Shock Tunnels Institute of Technology, Pasadena, CA J. George, T. Jenkins, C. Hess, J. Trolinger, D. Plemmons, N. Galyen, Aerospace Y. Krishna, S. Sheehe, S. O’Byrne, MetroLaser, Inc., Laguna Hills, CA Testing Alliance, Arnold AFB, TN University of New South Wales, Canberra, Australia Monday, 22 June 2015 12-APA-1 Aerodynamic-Structure Dynamics Interaction Stemmons C Chaired by: J. AZEVEDO and C. PASILIAO, AFRL/RWWV 0900 hrs 0930 hrs 1000 hrs 1030 hrs AIAA-2015-2250 AIAA-2015-2251 AIAA-2015-2252 AIAA-2015-2253 Aerodynamic Damping and Experimental Investigation of the Spectral Formulation-Based FSI and Analyzing the Pitch Agility of an Stiffness Determination for Aircraft Aeroelastic Behavior a NACA0018 Coupled Sensitivity Analysis for Ornithopter Undergoing Passive Wing Flutter Speed Analysis Cyber-Physical FlexibleWing Dyanmic Aeroelastic Problems Compliant Element Induced Shape K. Boo, S. Mansor, A. Abdul-Latif, C. Fagley, J. Seidel, T. McLaughlin, U.S. S. Yi, Korea Advanced Institute of Science and Change University of Technology, Johor Bahru, Air Force Academy, Colorado Springs, CO Technology, Daejeon, South Korea; R. Prasad, Z. Hasnain, J. Hubbard, University of Malaysia S. Choi, D. Im, Virginia Polytechnic Institute Maryland, College Park, College Park, MD; and State University, Blacksburg, VA; D. Lee, A. Wissa, University of Illinois, Urbana- Korea Advanced Institute of Science and Champaign, Urbana, IL Technology, Daejeon, South Korea Monday, 22 June 2015 13-APA-2 Aerodynamic Design Methodologies I Carpenter Ballroom Chaired by: K. KARA, Khalifa University of Science, Technology & Research and J. MURRAY, Sandia National Laboratories 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2015-2254 AIAA-2015-2255 AIAA-2015-2256 AIAA-2015-2257 AIAA-2015-2258 AIAA-2015-2259 Development of NOVA Aircraft Aircraft directional stability Design of a Multi-Stage Axial Turbine Fuselage Aerodynamic Prediction Investigation on continuously Numerical study of UAS-S4 Configurations for Large Engine prediction method by CFD within the scope of complete System Methods deflectable High-Lift Devices for a Éhecatl aerodynamic performance Integration Studies P. Della Vecchia, F. Nicolosi, D. Ciliberti, Design, Manufacturing and Operation F. Nicolosi, P. Della Vecchia, D. Ciliberti, V. 3D High-Lift Configuration improvement obtained with the use L. Wiart, O. Atinault, R. Grenon, B. Paluch, University of Naples “Federico II”, Naples, of a new Turbine Propulsion Simulator Cusati, L. Attanasio, University of Naples D. Franke, German Aerospace Center of a morphing wing approach D. Hue, ONERA, Meudon, France Italy (TPS) “Federico II”, Naples, Italy (DLR), Braunschweig, Germany S. Oliviu, A. Koreanschi, R. Botez,
44 A. Krumme, German Aerospace Center (DLR), University of Québec, Montréal, Canada Göttingen, Germany; S. Hegen, German-Dutch Wind Tunnels, Marknesse, The Netherlands; R. Nahuis, National Aerospace Laboratory (NLR), Marknesse, The Netherlands Monday, 22 June 2015 14-APA-3 Special Session: Low Boom Activities I Stemmons A Chaired by: K. WAITHE, Gulfstream Aerospace Corporation and L. BANGERT, NASA Langley Research Center 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2015-2260 AIAA-2015-2261 Oral Presentation AIAA-2015-2262 AIAA-2015-2263 Under-Track CFD-Based Shape Full-Carpet Design of a Low-Boom Sonic Boom Variation of a Wing- Numerical Simulations of Shock/ Cart3D Analysis of Plume and Optimization for a Low-Boom Demonstrator Concept Body-Tail-Nacelle Configuration Plume Interaction Using Structured Shock Interaction Effects on Sonic Demonstrator Concept I. Ordaz, NASA Langley Research Center, M. Park, NASA Langley Research Center, Overset Grids Boom M. Wintzer, Analytical Mechanics Associates, Hampton, VA; M. Wintzer, Analytical Hampton, VA J. Housman, C. Kiris, NASA Ames Research R. Castner, NASA Glenn Research Center, Inc., Hampton, VA; I. Ordaz, NASA Langley Mechanics Associates, Inc., Hampton, Center, Moffett Field, CA Cleveland, OH Research Center, Hampton, VA VA; S. Rallabhandi, National Institute of Aerospace, Hampton, VA Monday, 22 June 2015 15-APA-4 Propeller/Rotorcraft/Wind Turbine Aerodynamics I Stemmons B Chaired by: M. CALVERT, U.S. Army AMRDEC and D. O’BRIEN, US Army RDECOM 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2015-2264 AIAA-2015-2265 AIAA-2015-2266 AIAA-2015-2267 AIAA-2015-2268 AIAA-2015-2269 Experimental Evaluation of Open Slipstream Measurements of Small- The Influence of Airfoil Shape, Designing Small Propellers for A Parabolic Method for Accurate Blade Resolved Simulation for a Propeller Aerodynamic Performance Scale Propellers at Low Reynolds Reynolds Number and Chord Optimum Efficiency and Low Noise and Efficient Wind Farm Simulation Wind Farm and Aero-acoustic Behavior Numbers Length on Small Propeller Footprint A. Mittal, K. Sreenivas, W. Briley, L. Taylor, W. Hassan, K. Sreenivas, A. Mittal, L. C. Wisniewski, A. Byerley, W. Heiser, U.S. R. Deters, G. Ananda Krishnan, M. Selig, Performance and Noise C. Wisniewski, A. Byerley, W. Heiser, U.S. University of Tennessee, Chattanooga, Taylor, L. Hereth, University of Tennessee, Air Force Academy, Colorado Springs, CO; K. University of Illinois, Urbana-Champaign, C. Wisniewski, A. Byerley, W. Heiser, U.S. Air Force Academy, Colorado Springs, CO; Chattanooga, TN Chattanooga, Chattanooga, TN Van Treuren, T. Liller, Baylor University, Waco, Urbana, IL Air Force Academy, Colorado Springs, CO; K. Van Treuren, T. Liller, Baylor University, TX; N. Wisniewski, Rose Hulman Institute of K. Van Treuren, T. Liller, Baylor University, Waco, TX Technology, Terre Haute, IN Waco, TX Monday, 22 June 2015 16-ATIO-1 Terminal & Surface Operations I Manchester Chaired by: S. CAMPBELL, MIT Lincoln Laboratory 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2015-2270 AIAA-2015-2271 AIAA-2015-2272 AIAA-2015-2273 AIAA-2015-2274 A Robust and Practical Decision Identification of Local and Taxi Time Prediction at Charlotte A Stochastic Scheduler for Optimization of Airport Surface Support Tool for Integrated Propagated Queuing Effects at Airport Using Fast-Time Simulation Integrated Arrival, Departure, and Operations Under Uncertainty Arrival-Departure-Surface Traffic Major Airports and Machine Learning Techniques Surface Operations in Los Angeles C. Bosson, D. Sun, Purdue University, West Management H. Idris, Engility Corporation, Billerica, MA H. Lee, W. Malik, University of California, M. Xue, University of California, Santa Lafayette, IN A. Saraf, V. Felipe, Saab Sensis Corporation, Santa Cruz, Moffett Field, CA; B. Zhang, Cruz, Moffett Field, CA; S. Zelinski, NASA Campbell, CA; B. Sawhill, NextGen B. Nagarajan, American Airlines, Fort Ames Research Center, Moffett Field, CA
45 Aerosciences LLC, Williamsburg, VA Worth, TX; Y. Jung, NASA Ames Research Center, Moffett Field, CA Monday, 22 June 2015 17-ATIO-2 Separation Assurance Ming Chaired by: M. WILCOXEN, U.S. Air Force 0900 hrs 0930 hrs 1000 hrs AIAA-2015-2275 AIAA-2015-2276 AIAA-2015-2277 Conflict Detection Performance Strategic time-based metering that Conflict Alerts for Aircraft Analysis for Function Allocation Using assures separation for integrated Conducting Visual Approaches Time-Shifted Recorded Traffic Data operations in a terminal airspace H. Tang, NASA Ames Research Center, N. Guerreiro, J. Maddalon, T. Lewis, G. Hagen, A. Sadovsky, M. Jastrzebski, NASA Ames Moffett Field, CA NASA Langley Research Center, Hampton, VA Research Center, Moffett Field, CA Monday, 22 June 2015 18-ATIO-3 Trajectory Optimization Milan Chaired by: H. ARNESON 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2015-2278 AIAA-2015-2279 AIAA-2015-2280 AIAA-2015-2281 AIAA-2015-2282 The String Stability of a Trajectory- Computational Approaches to Branch & Bound-Based Algorithm Aircraft Trajectories Optimization Trajectory optimization algorithm Based Interval Management Simulation and Optimization of for Aircraft VNAV Profile Reference By Genetic Algorithms To Reduce for a constant altitude cruise flight Algorithm in the Midterm Airspace Global Aircraft Trajectories Trajectory Optimization Flight Cost Using A Dynamic with a required time of arrival K. Swieringa, NASA Langley Research H. Ng, University of California, Santa Cruz, A. Murrieta Mendoza, B. Beuze, L. Weather Model constraint Center, Hampton, VA Moffett Field, CA; B. Sridhar, NASA Ames Ternisien, R. Botez, University of Québec, R. Félix Patrón, M. Schindler, R. Botez, A. Liv, R. Dancila, R. Botez, University of Research Center, Moffett Field, CA Montréal, Canada University of Québec, Montréal, Canada Québec, Montréal, Canada Monday, 22 June 2015 19-ATIO-4 Transformational Flight - Rapid Concept to Flight Metropolitan Ballroom 0900 - 1100 hrs Moderator: William Fredericks, NASA Langley Research Center Panelists: Neal Willford Mark Page JoeBen Bevirt Starr Ginn Textron Aviation Dzyne Technologies Joby Aviation NASA Armstrong Research Center
Monday, 22 June 2015 20-CASE-1 Academic Roundtable Batik 0900 - 1200 hrs Expanding 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. Shannon Flumerfelt, Ph.D. Anabela Alves, Ph.D. Associate Professor, Department of Mechanical Engineering Associate Professor, Educational Leadership, Director of Lean Thinking for Schools, Assistant Professor, Departamento de Produção e Sistemas Escola de Engenharia da Universidade University of Cape Town, Cape Town, South Africa Pawley Learning Institute, Oakland University, Michigan do Minho, Centro Interdisciplinar de Tecnologias, da Produção e da Energia (CITPE) Campus de Azurém, Portugal
Monday, 22 June 2015 21-CFD-1 Unstructured High-Order Methods I Grand Ballroom A Chaired by: S. MURMAN, NASA Ames Research Center and A. KATZ 0900 hrs 0930 hrs 1000 hrs 1030 hrs
46 AIAA-2015-2283 AIAA-2015-2284 AIAA-2015-2285 AIAA-2015-2286 High-Order Strand Grid Methods Higher-order Unstructured Finite A Spectral-Element Approach for High order subcell finite volume for Shock Turbulence Interaction Volume Methods for Turbulent the Eikonal Equation method in solving hyperbolic O. Tong, A. Katz, Utah State University, Aerodynamic Flows S. Murman, L. Diosady, NASA Ames conservation laws Logan, UT; J. Sitaraman, U.S. Army, A. Jalali, C. Ollivier Gooch, University of Research Center, Moffett Field, CA J. Pan, Y. Ren, Tsinghua University, Moffett Field, CA British Columbia, Vancouver, Canada Beijing, China Monday, 22 June 2015 22-CFD-2 Unsteady Flow Simulations Grand Ballroom B Chaired by: Y. WANG and D. REASOR, Air Force Research Laboratory 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2015-2287 AIAA-2015-2288 AIAA-2015-2289 AIAA-2015-2290 AIAA-2015-2291 Unsteady Simulations of Shockwave- Effect of Cavity Flow on Landing Numerical Investigation of the Symmetrical and non-symmetrical Numerical Investigation of the Boundary Layer Interaction Induced Gear Aerodynamic Loads Detaching Vortical Flow at Rotating 3D wing deformation of flapping Starting Process in a Long-test- Transonic Shockwave Oscillations using U. Oza, Z. Hu, X. Zhang, University of Cylinders with Thom Discs micro aerial vehicles duration Hypervelocity Shock Unstructured Grids Southampton, Southampton, United R. Ritz, T. Schomberg, O. Wünsch, W. Tay, National university of Singapore, Tunnel K. Bhamidipati, D. Reasor, 412th Test Wing, Kingdom University of Kassel, Kassel, Germany; M. Singapore, Singapore Y. Wang, Z. Hu, Z. Jiang, Chinese Edwards AFB, CA; C. Pasiliao, Air Force Ruetten, R. Kessler, German Aerospace Academy of Sciences, Beijing, China Research Laboratory, Eglin AFB, FL Center (DLR), Göttingen, Germany Monday, 22 June 2015 23-CFD-3 Meshing Techniques I Coral Chaired by: D. THOMPSON, Mississippi State University and B. JOLLY, US Air Force 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2015-2292 AIAA-2015-2293 AIAA-2015-2294 AIAA-2015-2295 AIAA-2015-2296 Comparing Anisotropic Output- meshCurve: An Automated Target-Edge Based Orthogonal Automated Massively Refinement Construction of Prism and Hex Based Grid Adaptation Methods by Low-Order to High-Order Mesh Anisotropic Mesh Technique for Multi-block Structured Layers from Anisotropic Tetrahedra Decomposition Generator J. Zuniga Vazquez, C. Ollivier Gooch, Grids Based on NURBS Volume J. Steinbrenner, Pointwise, Inc., Fort M. Park, NASA Langley Research Center, J. Ims, Z. Duan, Z. Wang, University of University of British Columbia, Vancouver, H. Koizumi, S. Tsutsumi, R. Takaki, Japan Worth, TX Hampton, VA; A. Loseille, French National Kansas, Lawrence, Lawrence, KS Canada Aerospace Exploration Agency (JAXA), Institute for Research in Computer Science Sagamihara, Japan; K. Yamamoto, Japan and Control (INRIA), Le Chesnay, France; Aerospace Exploration Agency (JAXA), J. Krakos, T. Michal, The Boeing Company, Mitaka, Japan; H. Ito, M. Abe, Ryoyu St. Louis, MO Systems, Nagoya, Japan; et al. Monday, 22 June 2015 24-CFD-4 LES, DNS, and Hybrid RANS-LES I Emerald Chaired by: A. SESCU, Mississippi State University and W. MCMULLAN, University of Leicester 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2015-2297 AIAA-2015-2298 AIAA-2015-2299 AIAA-2015-2300 AIAA-2015-2301 High Order Numerical Methods for Large Eddy Simulation of Resolved Scalar Mixing in Large Resolved Scalar Mixing in Large LES Simulation Inflow conditions the Dynamic SGS Model of Turbulent Supersonic Impinging Jets by Eddy Simulations of a Low Eddy Simulations of a Low for Outlet Guide Vane and Flows with Shocks Adaptive, Explicit Filtering Reynolds Number Plane Mixing Reynolds Number Plane Mixing Prediffuser Flows D. Kotov, Bay Area Environmental Research S. Patel, J. Mathew, Indian Institute of Layer Layer J. Li, Nanjing University of Aeronautics Institute, Petaluma, CA; H. Yee, A. Wray, Science, Bangalore, India J. Haywood, A. Sescu, Mississippi State S. Hug, W. McMullan, University of and Astronautics, Nanjing, China; G. Page,
47 NASA Ames Research Center, Moffett Field, University, Mississippi State, MS Leicester, Leicester, United Kingdom J. McGuirk, Loughborough University, CA; B. Sjogreen, Lawrence Livermore National Loughborough, United Kingdom Laboratory, Livermore, CA Monday, 22 June 2015 25-FD-1 Wing Aerodynamics Govenors Lecture Hall Chaired by: D. YOUNG, Raytheon Missile Systems and U. KAUL, NASA ARC 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2015-2302 AIAA-2015-2303 AIAA-2015-2304 AIAA-2015-2305 AIAA-2015-2306 AIAA-2015-2307 AIAA-2015-2308 The Origin of Lift Revisited: I. A The Origin of Lift Revisited: II. The Steady Aerodynamics of Quiet Lift and Drag in Two-Dimensional Lift and Drag in Two-Dimensional Effects of Perturbation on the Flow Interaction of Multiple Vortices over Complete Physical Theory Physical Processes of Airfoil- Airfoils with Porosity Gradients Steady Viscous and Compressible Steady Viscous and Compressible over Nonslender Delta Wings a Double Delta Wing T. Liu, Western Michigan University, Circulation Formation in Starting R. Hajian, J. Jaworski, Lehigh University, Flow: I. Far-Field Formulae Analysis Flow: II. Fundamental Solution C. Canpolat, B. Sahin, Cukurova University, X. Zhang, Z. Wang, I. Gursul, University of Kalamazoo, MI; J. Wu, J. Zhu, L. Liu, Flow Bethlehem, PA and Numerical Confirmation Theory Adana, Turkey; S. Yayla, Yuzuncu Yil Bath, Bath, United Kingdom Peking University, Beijing, China J. Zhu, S. Zou, L. Liu, J. Wu, Peking J. Zhu, L. Liu, Peking University, Beijing, L. Liu, J. Wu, Peking University, Beijing, University, Van, Turkey; H. Akilli, Cukurova University, Beijing, China; T. Liu, Western China; T. Liu, Western Michigan University, China; T. Liu, Western Michigan University, University, Adana, Turkey Michigan University, Kalamazoo, MI Kalamazoo, MI; Y. Shi, W. Su, J. Wu, Kalamazoo, MI Peking University, Beijing, China Monday, 22 June 2015 26-FD-2 Fundamental Fluid Flows Senators Lecture Hall Chaired by: G. DALE, Air Force Research Laboratory and M. GREEN, Syracuse University 0900 hrs 0930 hrs 1000 hrs 1030 hrs AIAA-2015-2309 AIAA-2015-2310 AIAA-2015-2311 AIAA-2015-2312 Evolution of Stratified Boundary- Numerical and Experimental Evidence of complex flow structures Numerical Study of the Transient Free Shear Flows Under Stokes- Investigation of Wind Turbine Wakes in a converging-diverging nozzle Deformation and Drag Characteristics Ekman Forcing X. Huang, RWTH Aachen University, Aachen, caused by a recessed step at the of a Decelerating Droplet M. Jones, E. Paterson, Virginia Polytechnic Germany; S. Vey, Technical University of nozzle throat Q. Qu, P. Ma, P. Liu, Beihang University, Institute and State University, Blacksburg, VA Berlin, Berlin, Germany; M. Meinke, W. M. Carmine, R. Cheli, F. Cozzi, A. Beijing, China; S. Li, Beijing Institute of Schroeder, RWTH Aachen University, Aachen, Spinelli, M. Zocca, A. Guardone, Technical Mechanical and Electrical Engineering, Germany; G. Pechlivanoglou, C. Nayeri, University of Milan, Milan, Italy Beijing, China; R. Agarwal, Washington Technical University of Berlin, Berlin, Germany; University in St. Louis, St. Louis, MO et al. Monday, 22 June 2015 27-FD-3 Combustion and Heat Transfer Topaz Chaired by: J. CHOI, Georgia Institute of Technology and I. LEYVA 0900 hrs 0930 hrs 1000 hrs 1030 hrs AIAA-2015-2313 AIAA-2015-2314 AIAA-2015-2315 AIAA-2015-2316 An Experimental Study of Global Comparison of Theoretical and Semi- On autoignition-dominated Flow Fields of Manipulated Shear Characteristics of Turbulent Empirical Solutions for Dissipation supersonic combustion Layers of a Turbulent Jet Flame Diffusion Jet Flames for Fuels of Coefficient in a Low Reynolds Number N. Cymbalist, P. Dimotakis, California H. Nawroth, C. Paschereit, Technical Complex Chemistry Compressor Cascade Institute of Technology, Pasadena, CA University of Berlin, Berlin, Germany A. Ramachandran, V. Narayanaswamy, F. Kok, R. Myose, Wichita State University,
48 North Carolina State University, Raleigh, Wichita, KS; S. Hayashibara, Embry-Riddle NC Aeronautical University, Prescott, AZ Monday, 22 June 2015 28-FD-4 Boundary Layer Transition: Hypersonic Flows Sapphire Chaired by: J. JEWELL, Air Force Research Laboratory and K. CASPER 0900 hrs 0930 hrs 1000 hrs 1030 hrs AIAA-2015-2317 AIAA-2015-2318 AIAA-2015-2319 AIAA-2015-2320 Instability and Transition Numerical Investigation of Nonlinear Correlation of HIFiRE-5 Flight Data Linear stability of high-speed Experiments in the Boeing/AFOSR Wave-packets in a Hypersonic High- With Computed Pressure and Heat boundary layer flows at varying Mach 6 Quiet Tunnel Enthalpy Boundary-Layer on a 5 Transfer Prandtl numbers G. McKiernan, B. Chynoweth, S. deg Sharp Cone J. Jewell, J. Miller, R. Kimmel, Air Force A. Ramachandran, B. Saikia, K. Sinha, Indian Schneider, Purdue University, West L. Salemi, H. Fasel, University of Arizona, Research Laboratory, Wright-Patterson Institute of Technology Bombay, Mumbai, Lafayette, IN Tucson, Tucson, AZ AFB, OH India; R. Govindarajan, Tata Institute of Fundamental Research, Hyderabad, India Monday, 22 June 2015 29-MAO-1 Vehicle Design Applications I Madrid Chaired by: R. KOLONAY, Air Force Research Laboratory/RQVC/WPAFB and V. KALIVARAPU, Iowa State University 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2015-2321 AIAA-2015-2322 AIAA-2015-2323 AIAA-2015-2324 AIAA-2015-2325 AIAA-2015-2326 AIAA-2015-2327 Parallel allocation-mission Multi-Objective Design and Control Power Optimization using Control Focused Multidisciplinary Hybrid Wing Body (HWB) Aircraft A Multi-Fidelity, Multi-Disciplinary Multi-Disciplinary and Multi- optimization of a 128-route Path Planning Optimization of Artificial Intelligence for Hybrid Design Optimization of Tailless Design and Optimization using Analysis and Optimization Objective Optimization of an network Unmanned Aerial Vehicles (UAVs) Wing Body Aircraft Fighter Aircraft Stitched Composites Framework for the Design of Unconventional Aircraft Concept J. Hwang, J. Martins, University of E. Rudnick-Cohen, S. Azarm, J. Herrmann, R. Chhabra, Virginia Polytechnic Institute C. Meckstroth, University of Dayton, V. Li, The Boeing Company, Huntington Morphing UAV Wing S. Gemma, F. Mastroddi, University of Michigan, Ann Arbor, Ann Arbor, MI University of Maryland, College Park, and State University, Blacksburg, VA; S. Dayton, OH; W. Blake, Air Force Research Beach, CA A. Ciarella, C. Tsotskas, M. Hahn, Aircraft Rome “La Sapienza”, Rome, Italy College Park, MD Mulani, University of Alabama, Tuscaloosa, Laboratory, Wright-Patterson AFB, OH Research Association, Ltd., Bedford, United Tuscaloosa, AL; R. Kapania, J. Schetz, Kingdom; N. Werter, R. De Breuker, Virginia Polytechnic Institute and State Delft University of Technology, Delft, The University, Blacksburg, VA Netherlands; C. Beaverstock, Swansea University, Swansea, United Kingdom; et al. Monday, 22 June 2015 30-MST-1 Unmanned Aerial Vehicle Systems Travertine Chaired by: B. LANDRUM and M. PATIL, Virginia Tech 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2015-2328 AIAA-2015-2329 AIAA-2015-2330 AIAA-2015-2331 AIAA-2015-2332 AIAA-2015-2333 AIAA-2015-2334 Experimental Characterization of Nondeterministic Simulation for Optimal selection of UAV for Dynamic Resource Allocation for Optimal Object Location by a Fleet Modeling and Control of Tethered MAV Pose Measurement algorithm Butterfly in Climbing Flight Probability of Loss of Control ground target tracking Sharing Multi-UAV Services of Various UAVs Unmanned Multicopters in Based on Visual Systems J. Cranford, University of Alabama, Prediction for Unmanned Aircraft J. Narkiewicz, A. Kopyt, P. Radyisyewski, B. Kaddouh, W. Crowther, P. Hollingsworth, A. Kopyt, J. Narkiewicz, T. Malecki, P. Hovering Flight Q. Zeng, J. Liu, Y. Wang, Nanjing Huntsville, Huntsville, AL; N. Slegers, Systems T. Malecki, Warsaw University of University of Manchester, Manchester, Radyisyewski, Warsaw University of D. Ferreira de Castro, J. Santos, M. University of Aeronautics and Astronautics,
49 George Fox University, Newberg, OR; L. Hale, M. Patil, C. Roy, Virginia Polytechnic Technology, Warsaw, Poland United Kingdom Technology, Warsaw, Poland Batista, D. Antônio dos Santos, L. Góes, Nanjing, China B. Landrum, University of Alabama, Institute and State University, Blacksburg, VA Technological Institute of Aeronautics Huntsville, Huntsville, AL (ITA), São José dos Campos, Brazil Monday, 22 June 2015 31-MST-2 Aviation Systems Human Factors Wyeth Chaired by: D. CARTMELL, Boeing Engineering Operations & Technology and S. ROBINSON, UC Davis 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2015-2335 AIAA-2015-2336 AIAA-2015-2337 AIAA-2015-2338 Oral Presentation AIAA-2015-2339 Oral Presentation Formal Extensions to the Intent- The Rapidly Reconfigurable Flight Crew Response to Unexpected Influence of coupled sidesticks on Ergonomic evaluation of different Equation-System Representation An approach to establish case base Based Mode Confusion Detection Research Cockpit Events: A Simulator Experiment the pilot monitoring’s awareness principles of position indication and Model for Pneumatic Seat Design of motions for layout optimization Framework R. Joyce, S. Robinson, University of J. Field, National Aerospace Laboratory during flare control plane in field Used for Vibration Isolation In Air Y. Zhang, Y. Sun, L. Liu, Nanjing University J. Suraj Nandiganahalli, I. Hwang, Purdue California, Davis, Davis, CA (NLR), Amsterdam, The Netherlands; A. Uehara, D. Niedermeier, German M. Zhelonkin, Y. Dubov, V. Zhelonkin, O. and Ground Transport of Aeronautics and Astronautics, Yangzhou, University, West Lafayette, IN L. Fucke, B. Correia Grácio, The Boeing Aerospace Center (DLR), Braunschweig, Tkachenko, TsAGI, Zhukovsky, Russia E. Ayyad, W. Culbreth, D. Reynolds, China Company, Madrid, Spain; M. Varney, Germany University of Nevada, Las Vegas, Las Airbus, Toulouse, France Vegas, NV Monday, 22 June 2015 32-NW-1 Networking Coffee Break Meeting Room Foyers 0900 - 0930 hrs Monday, 22 June 2015 33-PDL-1/FD-5 Plasma Aerodynamics & Flow Control I Monet Ballroom Chaired by: M. STANEK, AFRL/RQVI 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2015-2340 AIAA-2015-2341 AIAA-2015-2342 AIAA-2015-2343 AIAA-2015-2344 AIAA-2015-2345 AIAA-2015-2346 Numerical Simulations of Nanosecond Dielectric Barrier Aerodynamic Control Effect of Effect of Pulsed Plasma Jets Single Nanosecond Dielectric Barrier Shock-Trapping Capability of a Pressure Investigations over a Disturbances in Shear Flows Discharge Plasma Actuator Flow Surface DC Plasma Discharge at on Boundary Layer Recovery Discharge and Pulsed Sliding Cavity in a Supersonic Flow Conical Forebody under Duty- Introduced by NS-DBD Plasma Control of Compressible Dynamic Mach-7 Hypersonic Flow Downstream of a Reflected Shock Discharge Applied to Separation N. Webb, M. Samimy, Ohio State Cycled Plasma Actuations Actuators Stall Y. Watanabe, University of Tokyo, Bunkyo, Wave-Boundary Layer Interaction Control Along a NACA 0015 Airfoil University, Columbus, OH J. Zhao, X. Meng, J. Wang, Northwestern I. Popov, G. Correale, S. Hulshoff, Delft M. Frankhouser, J. Gregory, Ohio State Japan; K. Suzuki, University of Tokyo, B. Greene, N. Clemens, University of Texas, K. Bayoda, N. Benard, E. Moreau, National Polytechnical University, Xi’an, China; F. University of Technology, Delft, The University, Columbus, OH Kashiwa, Japan Austin, Austin, TX; P. Magari, D. Micka, M. Center for Scientific Research (CNRS), Liu, S. Luo, University of California, Irvine, Netherlands Ueckermann, Creare, Inc., Hannover, NH Futuroscope, France Los Angeles, CA Monday, 22 June 2015 34-TP-1 Ablation I Rosetta Chaired by: D. KUNTZ, Sandia National Laboratories and D. PYTEL, Lockheed Martin Space Systems 0900 hrs 0930 hrs 1000 hrs AIAA-2015-2347 AIAA-2015-2348 AIAA-2015-2349 Evaluation of Finite-Rate Gas/ Comparison of Carbon Ablative Stagnation-Line Simulations of Surface Interaction Models for a Shock-Layer Radiation with High Meteor Ablation Carbon Based Ablator Surface Temperatures B. Dias, A. Turchi, T. Magin, von Kármán Y. Chen, NASA Ames Research Center, S. Lewis, R. Morgan, T. Mcintyre, University Institute for Fluid Dynamics, Rhode-Saint- Moffett Field, CA; T. Gokcen, ERC, Inc., of Queensland, St. Lucia, Australia; C. Alba, R. Genèse, Belgium Moffett Field, CA Greendyke, Air Force Institute of Technology, Wright-Patterson AFB, OH 50 Monday, 22 June 2015 35-TP-2 Heat Transfer I Steuben Chaired by: M. KIO, National Space Research & Development Agency and A. WILLIAMS, Air Force Reseach Laboratory 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2015-2350 AIAA-2015-2351 AIAA-2015-2352 AIAA-2015-2353 AIAA-2015-2354 AIAA-2015-2355 Diffusion Penetration Time for Comparisons of Computations Heat and Mass Transfer Analysis of Thermal Model for Sintered Study of the Minimum Anti-icing Studies on thermal conductivity Transient Conduction with Experiments for Electron a Film Evaporative MEMS Tuneable Cylindrical Evaporators of Loop Energy Based on Icing Limit State prediction of fiber reinforced R. McMasters, Virginia Military Institute, Transpiration Cooling at High Array Thruster Heat Pipes(2150991) Y. Zhao, S. Chang, Y. Bo, M. Leng, material with microscopic structure Lexington, VA; F. de Monte, University Enthalpies W. O’Neill, A. Cofer, A. Weaver, A. M. Mantelli, J. Florez Mera, F. Milanese, Beihang University, Beijing, China identification of L’Aquila, L’Aquila, Italy; J. Beck, S. K. Hanquist, I. Boyd, University of Alexeenko, Purdue University, West Federal University of Santa Catarina, J. Hua, Nanjing University of Aeronautics Nallapaneni, Michigan State University, Michigan, Ann Arbor, Ann Arbor, MI Lafayette, IN Florianópolis, Brazil and Astronautics, Nanjing, China E. Lansing, MI; D. Amos, Sandia National Laboratories, Albuquerque, NM; A. Haji-Sheikh, University of Texas, Arlington, Arlington, TX Monday, 22 June 2015 36-F360-1 The Voice of the Customer - Designing the Right Aircraft Grand Ballroom E 0930 - 1200 hrs Moderator: Christopher Stonehouse, Senior Vice President, Customer Services, Airbus Americas, Inc. Panelists: Jack Arehart William “Bill” Meehan Bart Roberts David Seymour President of MRO Services Chief Operating Officer Vice President, Flight Technical Operations Senior Vice President, Technical Operations Delta TechOps Frontier Airlines, Inc. JetBlue Airways American Airlines Monday, 22 June 2015 37-AA-6 Open Rotor I Fleur-de-lis A Chaired by: A. LYRINTZIS 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2015-2356 AIAA-2015-2357 AIAA-2015-2358 AIAA-2015-2359 AIAA-2015-2360 AIAA-2015-2361 Aerodynamic and Aeroacoustic Hybrid Use of CFD and Analytical The Effects of Swirl Recovery Aircraft Open Rotor Technology: Optimal Propeller Design for Quiet Sound Radiation from a Rotor Effects of Pylon Trailing Edge Methods for the Prediction of Vanes on Single-Rotation Propeller Analysis from an Operational Aircraft using Numerical Analysis Partially Immersed in a Turbulent Blowing on Pusher Propeller Advanced Open Rotor Tone Noise Aerodynamics and Aeroacoustics Perspective B. Humpert, R. Gaeta, J. Jacob, Oklahoma Boundary Layer Installation C. Ekoule, M. Kingan, A. McAlpine, T. Sinnige, J. van Kuijk, K. Lynch, D. G. Busch, M. Hassan, D. Mavris, Georgia State University, Stillwater, OK S. Glegg, A. Buono, J. Grant, F. Lachowski, T. Sinnige, K. Lynch, D. Ragni, G. Southampton University, Southampton, United Ragni, G. Eitelberg, L. Veldhuis, Delft Institute of Technology, Atlanta, GA Florida Atlantic University, Boca Raton, Eitelberg, L. Veldhuis, Delft University of Kingdom; N. Sohoni, Cambridge University, University of Technology, Delft, The FL; W. Devenport, W. Alexander, Virginia Technology, Delft, The Netherlands Cambridge, United Kingdom; A. Parry, Rolls- Netherlands Polytechnic Institute and State University, Royce Group plc, Derby, United Kingdom Blacksburg, VA Monday, 22 June 2015 38-AA-7 Trailing Edge Noise I Fleur-de-lis B Chaired by: R. EWERT, DLR - German Aerospace Center 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs AIAA-2015-2362 AIAA-2015-2363 AIAA-2015-2364 AIAA-2015-2365 AIAA-2015-2366 AIAA-2015-2367 AIAA-2015-2368 A Trailing-Edge Noise Model for Effect of serrated trailing edge on The Effects of Suction and Blowing Bio-Inspired Trailing Edge Noise Numerical and experimental On the robustness of the TNO Impact of Wall Permeability Serrated Edges boundary layer instability noise on Tonal Noise Generation by Blunt Control investigation of a beveled trailing model for aerofoil self-noise on Trailing-Edge Noise at High B. Lyu, University of Cambridge, J. Serpieri, S. Pröbsting, M. Gupta, F. Trailing Edges I. Clark, W. Alexander, W. Devenport, edge flow and noise field prediction Reynolds Number Cambridge, United Kingdom; M. Scarano, Delft University of Technology, W. Ramirez, W. Wolf, University of Virginia Polytechnic Institute and State W. van der Velden, S. Pröbsting, A. de C. Paruchuri, O. Stalnov, P. Joseph, C. S. Koh, M. Meinke, W. Schroeder, RWTH Azarpeyvand, University of Bristol, Bristol, Delft, The Netherlands Campinas, Campinas, Brazil University, Blacksburg, VA; S. Glegg, Jong, A. van Zuijlen, Delft University of Vanderwel, B. Ganapathisubramani, Aachen University, Aachen, Germany United Kingdom; S. Sinayoko, University Florida Atlantic University, Boca Raton, FL; Technology, Delft, The Netherlands; Y. University of Southampton, Southampton, of Southampton, Southampton, United J. Jaworski, Lehigh University, Bethlehem,
51 Guan, S. Morris, University of Notre Dame, United Kingdom; R. Leung, Defence Kingdom PA; C. Daly, University of Cambridge, Notre Dame, IN Science and Technology Laboratory, Cambridge, United Kingdom; et al. Southampton, United Kingdom Monday, 22 June 2015 39-AA-8 Jet Noise Prediction II Inverness Chaired by: D. MCLAUGHLIN, Retired 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs AIAA-2015-2369 AIAA-2015-2370 AIAA-2015-2371 AIAA-2015-2372 AIAA-2015-2373 Recent progress in numerical Jet Noise Prediction with Eddy Jet Noise Prediction using a Parametric Study of Jet Nozzles Large Eddy Simulation of a Tactical simulations for jet noise Relaxation Source Model Permeable FW-H Solver Using a RANS-Based Jet Noise Aircraft Exhaust Nozzle with Free- computation using LES on fully A. Neifeld, N. Reiche, J. Dierke, R. A. West, CD-adapco, London, United Prediction Tool stream and Wall Turbulence unstructured meshes Ewert, German Aerospace Center (DLR), Kingdom; M. Caraeni, CD-adapco, B. Venkatesh, R. Self, University of D. Dahl, J. Nichols, University of N. Lupoglazoff, F. Vuillot, ONERA, Braunschweig, Germany Lebanon, NH Southampton, Southampton, United Minnesota, Minneapolis, Minneapolis, MN Châtillon, France Kingdom Monday, 22 June 2015 40-AA-9 Jet Noise Measurements I Lalique Chaired by: S. MILLER, NASA 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2015-2374 AIAA-2015-2375 AIAA-2015-2376 AIAA-2015-2377 AIAA-2015-2378 AIAA-2015-2379 Noise Reduction with Fluidic Inserts Acoustic Emissions from F-35 Spatiotemporal Correlation Acoustical Environment of an F-35B Source characterization of full-scale Investigation of multi-lobed fighter in Supersonic Jets Exhausting Over Aircraft during Ground Run-Up Analysis of Jet Noise from a High- During Vertical Landings jet noise using vector intensity jet noise sources using acoustical a Simulated Aircraft Carrier Deck M. James, A. Salton, J. Downing, Blue Performance Military Aircraft B. Reichman, Brigham Young University, T. Stout, K. Gee, T. Neilsen, A. Wall, holography and partial field R. Powers, D. McLaughlin, P. Morris, Ridge Research and Consulting, LLC, B. Harker, T. Neilsen, K. Gee, Brigham Provo, UT; J. Downing, M. James, Blue Brigham Young University, Provo, UT; decomposition methods Pennsylvania State University, State Asheville, NC; K. Gee, T. Neilsen, B. Young University, Provo, UT; M. James, Ridge Research and Consulting, LLC, M. James, Blue Ridge Research and A. Wall, Air Force Research Laboratory, College, PA Reichman, Brigham Young University, Blue Ridge Research and Consulting, LLC, Asheville, NC; A. Aubert, Naval Air Warfare Consulting, LLC, Asheville, NC Wright-Patterson AFB, OH; K. Gee, T. Neilsen, Provo, UT; et al. Asheville, NC; A. Wall, Air Force Research Center, Patuxent River, MD; R. McKinley, Brigham Young University, Provo, UT; S. Laboratory, Wright-Patterson AFB, OH A. Wall, Air Force Research Laboratory, McInerny, University of Louisiana, Lafayette, Wright-Patterson AFB, OH; et al. Lafayette, LA; M. James, Blue Ridge Research and Consulting, LLC, Asheville, NC Monday, 22 June 2015 41-AA-10 CAA Sound Generation I Obelisk A Chaired by: C. TAM, Florida State Univeristy 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs AIAA-2015-2380 AIAA-2015-2381 AIAA-2015-2382 AIAA-2015-2383 AIAA-2015-2384 Hydrodynamic instability and shear Assessing Acoustic Source Forcing Numerical Investigation of Indirect Extension of the Random Particle A study of mechanisms of sound layer effect on the sound emission Tools for Launch Vehicle Jet Noise Noise Generation by Accelerated Mesh method to periodic turbulent generation by airfoils using flow- of a turbulent jet flame Prediction Vorticity flows for fan broadband noise acoustic correlations S. Schlimpert, S. Koh, A. Feldhusen, B. A. Sescu, E. Collins, Mississippi State W. Ullrich, Technical University of Munich, prediction A. Sano, A. Cavalieri, Technological
52 Roidl, M. Meinke, W. Schroeder, RWTH University, Mississippi State, MS; R. Harris, Garching, Germany; F. Bake, German A. Wohlbrandt, S. Guerin, German Institute of Aeronautics (ITA), São José Aachen University, Aachen, Germany CFD Research Corporation, Huntsville, Aerospace Center (DLR), Berlin, Germany; Aerospace Center (DLR), Berlin, Germany; dos Campos, Brazil; W. Wolf, University of AL; E. Luke, Mississippi State University, N. Kings, National Center for Scientific R. Ewert, German Aerospace Center (DLR), Campinas, Campinas, Brazil Mississippi State, MS Research (CNRS), Châtenay-Malabry, Braunschweig, Germany France; T. Sattelmayer, Technical University of Munich, Garching, Germany Monday, 22 June 2015 42-ACD-1 Aircraft Design for Environmental Impact Reduction Miro Chaired by: D. WELLS, NASA Langley Research Center 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2015-2385 AIAA-2015-2386 AIAA-2015-2387 AIAA-2015-2388 AIAA-2015-2389 AIAA-2015-2390 Effect of Wing Loading and Fuel Assessing Taxiing Trade Spaces Utilising Secondary Airports for RPT Greenhouse Gas Impacts of On- Aircraft Noise Reduction Technology The Clean Sky programme: Type on Optimal Cruise Altitude for from Aircraft, Airport, and Airline Operations: A Business Case Demand Electric Aircraft and Airport Noise Analysis for environmental benefits at aircraft Civil Aircraft Perspectives C. Bil, A. Gebreegziabher, RMIT University, T. Thompson, LMI, McLean, VA General Aviation Revitalization level A. Wortmann, M. Hoogreef, R. Vos, I. Chakraborty, M. LeVine, M. Hassan, D. Melbourne, Australia S. Min, D. Lim, D. Mavris, Georgia M. Brunet, S. Aubry, R. Lafage, ONERA, Delft University of Technology, Delft, The Mavris, Georgia Institute of Technology, Institute of Technology, Atlanta, GA Toulouse, France Netherlands Atlanta, GA Monday, 22 June 2015 43-AFM-3 Unmanned Aircraft Systems I Plum Blossom A Chaired by: K. HOFFLER, Adaptive Aerospace Group, Inc. and S. D’SOUZA, NASA-ARC 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs AIAA-2015-2391 AIAA-2015-2392 AIAA-2015-2393 AIAA-2015-2394 AIAA-2015-2395 AIAA-2015-2396 AIAA-2015-2397 Evaluation of Energy Required Attitude and altitude stabilization Quickness Criteria for Large An Assessment of Unmanned Objective Function Development Wake Vortex Detection with UAV Flight Test Evaluation of Pilot for Flight by a UAV Fitted with a of quad rotor using parameter Unmanned Aircraft in Non- Aircraft System Level-Turn for Optimized Path Guidance for Close Formation Flight Control Interfaces for Remotely Variable-Span Wing Performing a estimation and self-tuning Precision Aggressive and Non- Maneuver Performance Rotorcraft Shipboard Recovery H. Chao, University of Kansas, Lawrence, Piloted Vehicles Given Mission Profile controller Aggressive Maneuvers Requirements In Relation to a J. Tritschler, Naval Air Systems Command, Lawrence, KS; Y. Gu, West Virginia R. Olson, National Test Pilot School, P. Santos, P. Gamboa, University of Beira T. Dief, S. Yoshida, Kyushu University, K. Greene, D. Kunz, Air Force Institute of Quantified Well-Clear Definition Patuxent River, MD; J. Horn, Pennsylvania University, Morgantown, WV; P. Tian, Z. Mojave, CA Interior, Covilha, Portugal Kasuga, Japan; M. Abdelhady, Cairo Technology, Wright-Patterson AFB, OH D. Jack, K. Hoffler, S. Johnson, Adaptive State University, State College, PA Zheng, University of Kansas, Lawrence, University, Giza, Egypt Aerospace Group, Inc., Hampton, VA Lawrence, KS; M. Napolitano, West Virginia University, Morgantown, WV Monday, 22 June 2015 44-AFM-4 Planetary Entry and Aeroassist Technology Plum Blossom B Chaired by: S. DUTTA, NASA Langley Research Center and C. KARLGAARD, Analytical Mechanics Associates Inc 1400 hrs 1430 hrs 1500 hrs 1530 hrs AIAA-2015-2398 AIAA-2015-2399 AIAA-2015-2401 AIAA-2015-2402 Improvements to Entry Terminal Optimization of Interior Point Cost Rapid, Robust Trajectory Design Using Minimum Terminal Energy Point Controller for Mars Functions Using Indirect Methods Indirect Optimization Methods Optimizations of Hypersonic Vehicles Atmospheric Entry T. Antony, M. Grant, Purdue University, M. Grant, Purdue University, West Lafayette, Using Indirect Methods Y. Zheng, H. Cui, Y. Tian, Harbin Institute West Lafayette, IN; M. Bolender, Air Force IN; M. Bolender, Air Force Research M. Grant, Purdue University, West Lafayette, of Technology, Harbin, China Research Laboratory, Wright-Patterson Laboratory, Wright-Patterson AFB, OH IN; M. Bolender, Air Force Research AFB, OH Laboratory, Wright-Patterson AFB, OH
53 Monday, 22 June 2015 45-AMT-3/GT-3 Advances in Test Methodology and CFD Integration Obelisk B Chaired by: S. DUNN, Jacobs Technology and S. COLE, NASA Langley Research Center 1400 hrs 1430 hrs 1500 hrs 1530 hrs AIAA-2015-2403 AIAA-2015-2404 AIAA-2015-2405 AIAA-2015-2406 Development of a Transonic Gust F-35 Conventional Mode Jet-Effects Motion measurement of a wind Experimental Investigations about Rig for Simulation of Vertical Gusts Testing Methodology tunnel model by stereovision Heat Transfer Characteristics of on Half-models M. McWaters, Lockheed Martin technique Irregular Impingement Jet Arrays N. Allen, M. Quinn, Aircraft Research Corporation, Fort Worth, TX B. Martinez, D. Bidino, M. Bastide, C. in Typical Active Clearance Control Association, Ltd., Bedford, United Kingdom Demeautis, F. Leopold, P. Wey, French- System German Research Institute of Saint-Louis F. Liu, M. Junkui, Nanjing University of (ISL), Saint-Louis, France Aeronautics and Astronautics, Nanjing, China Monday, 22 June 2015 46-AMT-4/GT-4 Surface and Inflow Sensing Edelweiss Chaired by: Z. ZHANG, University of Tennessee and T. IOPPOLO, Southern Methodist University 1400 hrs 1430 hrs 1500 hrs 1530 hrs AIAA-2015-2407 AIAA-2015-2408 AIAA-2015-2409 AIAA-2015-2410 Shear Stress Sensing with Elastic Development of a Sol-Gel Based A Counter-Propagating Laser Air Computational Modeling of Microfence Structures Nanoporous unsteady Pressure Speed Sensor System for Aircraft Radiation Effects on Total A. Cisotto, F. Palmieri, NASA Langley Sensitive Paint and Validation in J. Kurtz, University of New South Wales, Temperature Probes Research Center, Hampton, VA; Y. Lin, the Large Transonic Onera S2MA Canberra, Australia; S. Wittig, OHB System J. Reardon, J. Schetz, K. Lowe, Virginia National Institute of Aerospace, Hampton, Windtunnel HB, Munich, Germany; S. O’Byrne, Polytechnic Institute and State University, VA; A. Saini, J. Kim, T. Kim, North Carolina Y. Michou, B. Deleglise, F. Lebrun, ONERA, University of New South Wales, Canberra, Blacksburg, VA State University, Raleigh, NC; et al. Modane, France; E. Scolan, A. Grivel, R. Australia Steiger, Swiss Center for Electronics and Microtechnology (CSEM), Neûchatel, Switzerland; et al. Monday, 22 June 2015 47-APA-5 Applied CFD & Numerical Correlations with Experimental Data I Stemmons B Chaired by: D. FINLEY, Lockheed Martin Aeronautics and J. SLOTNICK, Boeing Engineering Operations & Technology 1400 hrs 1430 hrs 1500 hrs AIAA-2015-2411 AIAA-2015-2412 AIAA-2015-2413 Supersonic Projectile Steering using Effects of Tip Clearance on Numerical Simulation of Water Micro-Actuators: Experimental and Miniature Gas Turbines Compressor Spray Caused by a Rolling Airplane Numerical Study Performance: A Numerical Tire M. Libsig, B. Martinez, C. Rey, T. Gauthier, Approach Q. Qu, F. Zhang, P. Liu, Beihang University, P. Wey, C. Berner, French-German Research J. Xiang, J. Schluter, F. Duan, Nanyang Beijing, China; R. Agarwal, Washington Institute of Saint-Louis (ISL), Saint-Louis, Technological University, Singapore, University in St. Louis, St. Louis, MO France; et al. Singapore Monday, 22 June 2015 48-APA-6 Unmanned, Bio-Inspired, Solar Powered Aerial Vehicle Designs I Carpenter Ballroom Chaired by: L. UKEILEY, University of Florida 1400 hrs 1430 hrs 1500 hrs AIAA-2015-2414 AIAA-2015-2415 AIAA-2015-2416 Computational Studies for the Force Production by Wing Flapping: System Development for Wildfire Development of a Hybrid UAV/UUV The Role of Stroke Angle of Attack SUAS R. Ramamurti, J. Geder, D. Edwards, and Local Reynolds Number J. Jacob, D. Gabbert, M. Andalibi, T. Young, Naval Research Laboratory, A. Rege, B. Dennis, K. Subbarao, Oklahoma State University, Stillwater, OK Washington, DC University of Texas, Arlington, Arlington, TX Monday, 22 June 2015
54 49-APA-7 Special Session: Aerodynamic-Structural Modeling, Optimization, and Test Techniques for Flexible Wing Technology I Stemmons A Chaired by: N. NGUYEN, NASA-Ames Research Center and S. ANDERS 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2015-2417 AIAA-2015-2418 AIAA-2015-2419 AIAA-2015-2420 AIAA-2015-2421 AIAA-2015-2422 Wind Tunnel Investigation of a Flexible Use of a Viscous Flow Simulation Optimization of an Aeroservoelastic Adaptive Aeroelastic Wing Robust Optimization of Variable- A 3-D Drag Optimization Study Wing High-Lift Configuration with a Code for Static Aeroelastic Analysis Wing with Distributed Multiple Shape Optimization for High-Lift Camber Continuous Trailing-Edge of Variable Camber Continuous Variable Camber Continuous Trailing of a Wing at High-Lift Conditions Control Surfaces Configurations Flap System Action Using Stochastic Trailing Edge Flap (VCCTEF) Using Edge Flap Design H. Akaydin, S. Moini-Yekta, J. Housman, B. Stanford, NASA Langley Research G. Fujiwara, University of Washington, Kriging OVERFLOW N. Nguyen, NASA Ames Research Center, N. Nguyen, NASA Ames Research Center, Center, Hampton, VA Seattle, Seattle, WA; N. Nguyen, NASA Y. Liu, J. Bai, Northwestern Polytechnical U. Kaul, N. Nguyen, NASA Ames Research Moffett Field, CA; N. Precup, E. Livne, Moffett Field, CA Ames Research Center, Moffett Field, CA University, Xi’an, China; E. Livne, Center, Moffett Field, CA University of Washington, Seattle, Seattle, University of Washington, Seattle, WA; J. Urnes, The Boeing Company, St. Seattle, WA Louis, MO; E. Dickey, The Boeing Company, Huntington Beach, CA; C. Nelson, The Boeing Company, Seattle, WA; et al. Monday, 22 June 2015 50-APA-8 Flow Control Applications & Demonstrations (Active & Passive) I Stemmons C Chaired by: J. GEORGE, Metrolaser Inc. and K. MULLENERS, Leibniz Universitaet Hannover 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs AIAA-2015-2423 AIAA-2015-2424 AIAA-2015-2425 AIAA-2015-2426 AIAA-2015-2427 Study of slanted perforated shapes in Numerical Study of the Internal Effect of Spanwise Jet Spacing on Dynamic Flow Control over Stochastic analysis of aerodynamic tabs for control of subsonic Jets Flow Structures Inside the Sweeping Separation Control for Swept and Aerodynamic Bodies using Phased forces acting on a self-adaptive A. Reyaz Ahmed, KCG College of Technology, Jet Actuator Unswept Airfoils Array Vectored Synthetic Jet camber airfoil in turbulent inflow Chennai, India; S. Thanigaiarasu, Madras K. Kara, Khalifa University, Abu Dhabi, M. Walker, K. Hipp, S. Benton, J. Bons, Actuation G. Kampers, Carl von Ossietzky University, Institute of Technology, Chennai, India; S. United Arab Emirates Ohio State University, Columbus, OH Z. Hasnain, R. Weinstein, L. Trollinger, Oldenburg, Germany; U. Cordes, C. Venkatraman, KCG College of Technology, J. Hubbard, A. Flatau, University of Tropea, Technical University of Darmstadt, Chennai, India; E. Srinivasan, Bharath Maryland, College Park, College Park, MD Darmstadt, Germany; M. Hoelling, J. University, Chennai, India; E. Rathakrishnan, Peinke, Carl von Ossietzky University, Indian Institute of Technology Kanpur, Kanpur, Oldenburg, Germany India Monday, 22 June 2015 51-ATIO-5 Terminal & Surface Operations II Manchester Chaired by: A. SARAF, Saab Sensis Corporation 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2015-2428 AIAA-2015-2429 AIAA-2015-2430 AIAA-2015-2431 AIAA-2015-2432 AIAA-2015-2433 Scheduling and Delivering Aircraft Stochastic Near-Optimal Control Time Based Separation: A study Designing and Evaluating Advanced Optimal Airspace Design for Assessment of Delayed to Departure Fixes in the NY for Aircraft Arrival Sequencing and into runway compression and time Approach Procedures for the Continuous Climb Operation Deceleration Approach Metroplex with Controller-Managed Conflict Resolution based separation Concept of Segmented Independent E. Kim, S. Hong, K. Lee, Korea Aerospace Opportunities at US Airports Spacing Tools Y. Matsuno, T. Tsuchiya, University of R. Curran, F. Herrema, W. Zhao, Delft Parallel Approaches University, Goyang, South Korea T. Reynolds, M. McPartland, Y. Rodriguez, Tokyo, Bunkyo, Japan University of Technology, Delft, The M. Sandberg, J. Venuti, Lincoln Laboratory,
55 E. Chevalley, B. Parke, J. Kraut, N. C. Hanses, F. Knabe, B. Korn, German Bienert, F. Omar, E. Palmer, NASA Ames Netherlands; V. Treve, R. Graham, Aerospace Center (DLR), Braunschweig, Massachusetts Institute of Technology, Research Center, Moffett Field, CA EUROCONTROL, Bretigny, France Germany Lexington, MA Monday, 22 June 2015 52-ATIO-6 Fleet and Route Planning Ming Chaired by: W. CROSSLEY, Purdue University 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2015-2434 AIAA-2015-2435 AIAA-2015-2436 AIAA-2015-2437 AIAA-2015-2438 AIAA-2015-2439 Effects of Fuel Price on Total Fuel Estimating the Fuel Saving Enabling Technology Portfolio A Rapid Integrated Interdependent Modeling Airline Decisions on Route Landscape Analysis Framework for Burn and System Capacity- An Potential of Commercial Aircraft Selection through Quantitative Fleet-Level Environmental Model Planning Using Discrete Choice Low Carbon Energy Analysis of Advanced Engine and in Future Fleet-Development Uncertainty Analysis J. Bernardo, T. Zaidi, M. LeVine, H. Models P. Vascik, Massachusetts Institute of Airframe Technology and Airline Scenarios K. Gatian, D. Mavris, Georgia Institute of Jimenez, D. Mavris, Georgia Institute of Z. Sha, K. Moolchandani, A. Maheshwari, Technology, Cambridge, MA; R. Pearce, Responses to Changes in Fuel Price N. Randt, L. Wache, Technical University of Technology, Atlanta, GA Technology, Atlanta, GA J. Thekinen, J. Panchal, D. DeLaurentis, NASA Headquarters, Washington, DC; C. Murphy, B. Miller, Metron Aviation, Munich, Munich, Germany; C. Jessberger, Purdue University, West Lafayette, IN D. Rhodes, Massachusetts Institute of Inc., Dulles, VA; L. Sherry, George Mason K. Ploetner, Bauhaus Luftfahrt e.V., Technology, Cambridge, MA University, Fairfax, VA Munich, Germany Monday, 22 June 2015 53-ATIO-7 Systems Engineering and Analysis Milan Chaired by: P. HOLLINGSWORTH, The University of Manchester 1400 hrs 1430 hrs 1500 hrs 1530 hrs AIAA-2015-2440 AIAA-2015-2441 AIAA-2015-2442 AIAA-2015-2443 Knowledge Engineering - Paving the Way from the Past to Parametric Assessment of Aviation Selected Array of Technology and Formalizing the Engineering the Future: AVDKBS, a Software Environmental Goals: Implications Systems Options for Ecologically Science Discipline Development in Knowledge on R&D Decision Making Responsible Aviation X. Peng, B. Chudoba, University of Texas, Engineering M. Hassan, A. Payan, S. O’Sullivan, H. A. Isikveren, D. Empl, U. Kling, K. Arlington, Arlington, TX X. Peng, B. Chudoba, University of Texas, Pfaender, D. Mavris, Georgia Institute of Ploetner, C. Pornet, Bauhaus Luftfahrt e.V., Arlington, Arlington, TX Technology, Atlanta, GA Ottobrunn, Germany Monday, 22 June 2015 54-ATIO-8 Transformational Flight - Enabling the Next Billion Dollar Aviation Market through Autonomy Metropolitan Ballroom 1400 - 1600 hrs Moderator: Mark Ballin, NASA Langley Research Center Panelists: Danette Allen Nick Roy Craig Woolsey Autonomy Incubator, NASA Langley Research Center MIT Virginia Tech
Monday, 22 June 2015 55-CFD-5 Unstructured High-Order Methods II Grand Ballroom A Chaired by: H. HUYNH, NASA Glenn Research Center and A. JAMESON, Aeronautics and Astronautics 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs AIAA-2015-2444 AIAA-2015-2445 AIAA-2015-2446 AIAA-2015-2447 AIAA-2015-2448 A Survey of the Isentropic Euler High-Order Hyperbolic Residual- High-Order Methods for Stabilization of High-Order A Class of Rosenbrock Methods Vortex Problem using High-Order Distribution Schemes on Arbitrary Conservation Laws Employing Methods for Unstructured Grids for a Reconstructed Discontinuous Methods Triangular Grids Embedded Structured Element with Local Fourier Spectral Galerkin Method for the Unsteady S. Spiegel, H. Huynh, J. DeBonis, NASA A. Mazaheri, NASA Langley Research Method on Unstructured Filtering: high-Re Simulations in Compressible Flows Glenn Research Center, Cleveland, OH Center, Hampton, VA; H. Nishikawa, Hexahedral Grid Coarse Meshes X. Liu, H. Luo, North Carolina State National Institute of Aerospace, Hampton, J. Choi, University of Maryland, College M. López-Morales, A. Jameson, Stanford University, Raleigh, NC; Y. Xia, Idaho VA Park, College Park, MD University, Stanford, CA National Laboratory, Idaho Falls, ID Monday, 22 June 2015 56-CFD-6 Novel Discretizations Grand Ballroom B Chaired by: J. EKATERIN, IACM and M. CHOUDHARI, NASA-Langley Research Center 56 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2015-2449 AIAA-2015-2450 AIAA-2015-2451 AIAA-2015-2452 AIAA-2015-2453 AIAA-2015-2454 Investigations of a New Scheme for Active Flux for Advection Diffusion Alternative Formulations for Recent Progresses on a Meshless A Versatile Nonlinear Predictive Dynamical selective filtering for the Wave Propagation H. Nishikawa, National Institute of First-, Second-, and Third-Order Euler Solver for Compressible Flows Modeling Approach Lattice Boltzmann Method D. Fan, P. Roe, University of Michigan, Ann Aerospace, Hampton, VA Hyperbolic Navier-Stokes Schemes Z. Duan, Z. Wang, University of Kansas, M. Liou, NASA Glenn Research Center, S. Marie, National Conservatory of Arts Arbor, Ann Arbor, MI H. Nishikawa, National Institute of Lawrence, Lawrence, KS; B. Vu, NASA Cleveland, OH; W. Yao, Queen’s University, and Crafts, Paris, France; X. Gloerfelt, Aerospace, Hampton, VA Kennedy Space Center, Cape Canaveral, FL Belfast, United Kingdom Paris Institute of Technology, Paris, France Monday, 22 June 2015 57-CFD-7 Interdisciplinary CFD I Coral Chaired by: L. MARTINELLI, Princeton University and S. EYI, Middle East Technical University 1400 hrs 1430 hrs 1500 hrs 1530 hrs AIAA-2015-2455 AIAA-2015-2456 AIAA-2015-2457 AIAA-2015-2458 CFD-based Gust Load Analysis for Influence of Wall Vibration on the Numerical Analysis of Synthetic Jet Performances of Newton and a Free-flying Flexible Passenger Aero Performance of Transonic in Crossflow Preconditioned Newton-GMRES Aircraft in Comparison to a DLM- Diffuser A. Gupte, A. Pradeep, P. Mujumdar, Indian Methods in Hypersonic Flow based Approach C. Yao, G. Zhang, F. Xu, Z. Liu, Harbin Institute of Technology Bombay, Mumbai, Solutions L. Reimer, M. Ritter, R. Heinrich, W. Institute of Technology, Harbin, China India Y. Muslubas, S. Eyi, Middle East Technical Krüger, German Aerospace Center (DLR), University, Ankara, Turkey Braunschweig, Germany Monday, 22 June 2015 58-CFD-8 Turbulence Modeling and Uncertainty Quantification Emerald Chaired by: D. YODER, NASA Glenn Research Center and K. DURAISAMY, Stanford University 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2015-2459 AIAA-2015-2460 AIAA-2015-2461 AIAA-2015-2462 AIAA-2015-2463 AIAA-2015-2464 Quantification of Turbulence Machine Learning Methods for Uncertainty Quantification of A Scale-Adaptive Variant of the PANS Simulations of Turbulent A logarithmic formulation for Modeling Uncertainties Using Full Data-Driven Turbulence Modeling Turbulence Model Closure Coefficients Spalart-Allmaras Eddy-Viscosity Separated Flow over a Wall- low-Reynolds number turbulence Field Inversion Z. Zhang, K. Duraisamy, University of for Transonic Wall-Bounded Flows Model mounted Hump models with adaptive wall-functions E. Parish, K. Duraisamy, University of Michigan, Ann Arbor, Ann Arbor, MI J. Schaefer, T. West, S. Hosder, Missouri J. Coder, Pennsylvania State University, D. Higuera Caubilla, University of Toulouse, L. Frazza, A. Hay, D. Pelletier, École Michigan, Ann Arbor, Ann Arbor, MI University of Science and Technology, Rolla, State College, PA Toulouse, France; P. Razi, Texas A&M Polytechnique de Montréal, Montréal, MO; C. Rumsey, J. Carlson, W. Kleb, NASA University, College Station, TX; S. Sekhar, Canada Langley Research Center, Hampton, VA N. Mansour, NASA Ames Research Center, Moffett Field, CA; S. Girimaji, Texas A&M University, College Station, TX Monday, 22 June 2015 59-F360-2/CASE-2 Whatever Happened to the Four-Year Airplane? Grand Ballroom E 1400 - 1700 hrs Moderator: Craig Willis, Group Head for Systems Verification, Gulfstream G500/G600 Program, Gulfstream Aerospace Corporation Panelists: Catherine Ferrie Kilmain Eric Schrock Executive Vice President of Engineering Deputy Director, Technology Development and Product Integration Bell Helicopter Lockheed Martin Corporation
Monday, 22 June 2015 57 60-FD-6/PDL-2 Plasma Aerodynamics & Flow Control II Govenors Lecture Hall Chaired by: D. WILLIAMS, Illinois Institute of Technology and J. LITTLE, The University of Arizona 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2015-2465 AIAA-2015-2466 AIAA-2015-2467 AIAA-2015-2468 AIAA-2015-2469 AIAA-2015-2470 PIV and Electric Characterization of Adjoint Optimization of the Spatial Modeling of Saw-tooth DBD Ns-DBD plasma actuator induced Contribution of large-scale vortex Flow control over a backward a Plasma Synthetic Jet Actuator Profile of Steady Energy Deposition Plasma Actuators for Flow Control density gradient on a laminar and fine-scale turbulent structure in facing step by ns-DBD plasma F. Laurendeau, F. Chedevergne, O. Léon, for Supersonic Drag Reduction Simulations boundary layer separated flow control using DBD actuator ONERA, Toulouse, France R. Miles, C. Limbach, Princeton University, P. Milan, F. Demers, H. Vo, École R. Winkel, G. Correale, Delft University of plasma actuator G. Correale, Delft University of Technology, Princeton, NJ Polytechnique de Montréal, Montréal, Technology, Delft, The Netherlands K. Asano, University of Tokyo, Sagamihara, Delft, The Netherlands Canada Japan; K. Asada, Ohio State University, Columbus, OH; H. Kato, University of Tokyo, Sagamihara, Japan; M. Sato, T. Nonomura, K. Fujii, Japan Aerospace Exploration Agency (JAXA), Sagamihara, Japan Monday, 22 June 2015 61-FD-7 Boundary Layer Transition - Progress and Challenges Sapphire Chaired by: M. MALIK, NASA-Langley Research Center and M. ROGERS, NASA-Ames Research Center 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs AIAA-2015-2471 AIAA-2015-2472 Oral Presentation AIAA-2015-2473 AIAA-2015-2474 AIAA-2015-2475 AIAA-2015-2476 Receptivity: The Inspiration of Mark Boundary-Layer Transition Hypersonic Boundary-Layer Receptivity of Hypersonic Boundary Extending the Gamma-Rethetat CFD Transition Modeling: Blending Development and Application of Morkovin (Invited) Prediction for Laminar Flow Control Transition: Towards Mechanism- Layers to Acoustic and Vortical Correlation based Transition Model Classical Methods with Modern Transition Prediction Techniques in H. Reed, W. Saric, Texas A&M University, (Invited) Based Prediction Methods (Invited) Disturbances (Invited) for Crossflow Effects (Invited) Tools (Invited) an Unstructured CFD Code (Invited) College Station, TX J. Crouch, The Boeing Company, Seattle, WA S. Schneider, Purdue University, West P. Balakumar, NASA Langley Research R. Langtry, The Boeing Company, Seattle, WA J. Coder, M. Maughmer, Pennsylvania A. Krumbein, N. Krimmelbein, C. Grabe, Lafayette, IN Center, Hampton, VA State University, State College, PA German Aerospace Center (DLR), Cologne, Germany Monday, 22 June 2015 62-FD-8 Vortex Flows Senators Lecture Hall Chaired by: Z. ZHENG, The University of Kansas and R. GORDNIER, Air Force Reseach Laboratory 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs AIAA-2015-2477 AIAA-2015-2478 AIAA-2015-2479 AIAA-2015-2480 AIAA-2015-2481 Vortex Breakdown of Compressible Numerical Study of the Formation Rotating Cylindrical Bodies at Investigation of the flow dynamics Temporal Evolution of Turbulent Eddies Swirling Flows in a Finite-Length of Concentric Vortex Rings Low Re in a channel constricted by periodic in a Compressible Jet in Crossflow Straight Circular Pipe V. Sadri, P. Krueger, Southern Methodist M. Callender, Middle Tennessee State hills Measured using Pulse-Burst PIV Z. Rusak, J. Choi, Rensselaer Polytechnic University, Dallas, TX University, Murfreesboro, TN X. Gloerfelt, Paris Institute of Technology, S. Beresh, J. Wagner, J. Henfling, R. Institute, Troy, NY; S. Wang, University of Paris, France; P. Cinnella, University of Spillers, B. Pruett, Sandia National Auckland, Auckland, New Zealand Salento, Lecce, Italy Laboratories, Albuquerque, NM Monday, 22 June 2015 63-FD-9 Active and Passive Flow Control Topaz Chaired by: K. GRANLUND, Air Force Research Laboratory and M. AMITAY, Rensselaer Polytechnic Institute 1400 hrs 1430 hrs 1500 hrs 1530 hrs AIAA-2015-2482 AIAA-2015-2483 AIAA-2015-2484 AIAA-2015-2485 Interactions of a Dynamic Vortex Interactions of a Dynamic Vortex Flow Control in a Diffuser at The Effects of Sweeping Jet Generator with a Cross-flow: A Generator with a Cross-flow: An Transonic Conditions Actuator Parameters on Flow Numerical Study Experimental Study J. Gartner, M. Amitay, Rensselaer Separation Control R. Cummings, Rensselaer Polytechnic C. Leong, E. Cruz, Rensselaer Polytechnic Polytechnic Institute, Troy, NY M. Koklu, NASA Langley Research Center, Institute, Troy, NY; D. Clingman, The Institute, Troy, NY; D. Clingman, The Hampton, VA Boeing Company, Seattle, WA; O. Sahni, Boeing Company, Seattle, WA; M. Amitay, Rensselaer Polytechnic Institute, Troy, NY Rensselaer Polytechnic Institute, Troy, NY
58 Monday, 22 June 2015 64-MAO-2 Vehicle Design Applications II Madrid Chaired by: S. CHOI, Virginia Polytechnic Institute and State University and S. FERGUSON, North Carolina State University 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2015-2486 AIAA-2015-2487 AIAA-2015-2488 AIAA-2015-2489 AIAA-2015-2490 AIAA-2015-2491 The Value of Semi-Empirical Coupled Adjoint Aerostructural Optimal variable stiffness Simulation-Based Optimal Sensor/ Concurrent Optimization of a Free-Form Aerodynamic Wing Analysis Models in Aircraft Design Wing Optimization Using Quasi- distribution for a composite plate Actuator Positioning on a Fin-Like Feed-Forward Gust Loads Controller Optimization Using Mathematically- S. Brandt, M. Post, U.S. Air Force Three-Dimensional Aerodynamic with a row of holes subjected to Structure and Minimization of Wing Box Derived Design Variables Academy, Colorado Springs, CO; D. Hall, Analysis tension/shear load cases N. Pedramasl, M. Sahin, Middle East Structural Mass on an Aircraft with D. Poole, C. Allen, T. Rendall, University of DHC Engineering, San Mateo, CA; F. A. Elham, Delft University of Technology, M. van Tooren, University of South Technical University, Cankaya, Turkey; E. Active Winglets Bristol, Bristol, United Kingdom Gilliam, Lipscomb University, Nashville, Delft, The Netherlands; M. van Tooren, Carolina, Columbia, Columbia, SC; A. Acar, TOBB University of Economics and A. Wildschek, Airbus, Ottobrunn, Germany TN; T. Jung, T. Yechout, U.S. Air Force University of South Carolina, Columbia, Elham, Delft University of Technology, Technology, Sogutozu, Turkey Academy, Colorado Springs, CO Columbia, SC Delft, The Netherlands; R. Harik, University of South Carolina, Columbia, Columbia, SC Monday, 22 June 2015 65-MST-3 Air Traffic Management Travertine Chaired by: J. SMITH 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs AIAA-2015-2492 AIAA-2015-2493 AIAA-2015-2494 AIAA-2015-2495 AIAA-2015-2496 Scalable Multidimensional Understanding Air Transportation Development of an ATC Tower Multi-Agent Based Air Traffic Estimating Benefits of Aviation Uncertainty Evaluation Approach Market Dynamics using a Search Simulator to Simulate Ground Simulation System Alternative Fuels at the System, to Strategic Air Traffic Flow Algorithm for Calibrating Travel Operations Z. Yue, D. Sui, Y. Lin, J. Zhang, Nanjing Route, and Airport Level Management Demand and Price Z. Chua, University of Toulouse, Toulouse, University of Aeronautics and Astronautics, B. Miller, C. Murphy, Metron Aviation, Inc., J. Xie, Y. Wan, University of North Texas, V. Kumar, B. Horio, A. DeCicco, S. Hasan, V. France; F. Andre, M. Cousy, French Civil Nanjing, China Dulles, VA; C. Villa, A. Filizola, National Denton, TX Stouffer, LMI, McLean, VA; J. Smith, NASA Aviation University, Toulouse, France Civil Aviation Agency (ANAC), Brasilia, Langley Research Center, Hampton, VA; et al. Brazil Monday, 22 June 2015 66-MST-4 Guidance, Control, and Dynamics I Wyeth Chaired by: R. BOTEZ, Ecole de Technologie Superieure 1400 hrs 1430 hrs 1500 hrs 1530 hrs AIAA-2015-2497 AIAA-2015-2498 AIAA-2015-2499 AIAA-2015-2500 A New Method for Tuning PI Gains Longitudinal Stability Augmentation Control validation of a morphing A Comparative Study of a Pseudo- for Position Control of BLDC Motor of Seaplanes in Planing wing in an open loop architecture Five Degree of Freedom and an Based Wing Morphing Actuators K. Ito, Ghent University, Ghent, Belgium; T. M. Tchatchueng Kammegne, D. Nguyen, Adjoint Model Against a Six Degree R. Botez, S. Khan, University of Québec, Hirayama, Yokohama National University, R. Botez, University of Québec, Montréal, of Freedom Model for Fidelity Montréal, Canada Yokohama, Japan; T. Sakurai, Hiyoh Canada Assessment Aircraft Manufacturing and Development E. Sezer, M. Nalci, ROKETSAN Missile Company, Tokyo, Japan; T. Dhaene, Ghent Industries, Inc., Ankara, Turkey; A. Kutay, University, Ghent, Belgium Middle East Technical University, Ankara, Turkey Monday, 22 June 2015 67-PDL-3 Plasma Computational Methods I Monet Ballroom Chaired by: M. WHITE, Ohio Aerospace Institute 1400 hrs 1430 hrs 1500 hrs 1530 hrs AIAA-2015-2501 AIAA-2015-2502 AIAA-2015-2503 AIAA-2015-2504 A Non-iterative Hyperbolic, First- Equivalent Electrical Circuit for a 1D Investigations of Flow over a CFD Validation of PIV-based order Conservation Law Approach Plasma Engine Hemisphere using Numerical Estimation of DBD Plasma- to Divergence-free Solutions to N. Ramesh, Sri Jagadguru Simulations Actuation Force Maxwell’s Equations Chandrashekaranatha Swamiji Institute of C. Tam, T. Madden, Air Force Research Q. Zhai, Z. Zhang, J. Cai, Northwestern R. Thompson, T. Moeller, University of Technology, Chickballapur, India; P. Moses Laboratory, Kirtland AFB, NM; B. Thurow, Polytechnical University, Xi’an, China; F.
59 Tennessee, Tullahoma, Tullahoma, TN John Christy Appolo, T. Sheshadri, Indian Auburn University, Auburn, AL Liu, S. Luo, University of California, Irvine, Institute of Science, Bengaluru, India Los Angeles, CA Monday, 22 June 2015 68-TP-3 Ablation II Rosetta Chaired by: N. DOUGHERTY, ERC Incorporated and A. HASHEMI, Lockheed Martin Space Systems 1400 hrs 1430 hrs 1500 hrs 1530 hrs AIAA-2015-2505 AIAA-2015-2506 AIAA-2015-2507 AIAA-2015-2508 Effects of Water Presence on Low A Multi-Dimensional Finite Element Thermal Protection System Mass Development and Qualification of Temperature Phenomenon in Based Solver for Decomposing Estimating Relationships For Blunt- Lightweight Ablator Aeroshell BBM Porous TPS Materials and Non-Decomposing Thermal Body, Earth Entry Spacecraft for Martian Mission D. Smith, A. Omidy, H. Weng, University Protection Systems S. Sepka, ERC, Inc., Moffett Field, CA; J. K. Fujita, T. Suzuki, T. Aoki, T. Ogasawara, of Kentucky, Lexington, Lexington, KY; M. Howard, B. Blackwell, Sandia National Samareh, NASA Langley Research Center, Y. Ishida, Japan Aerospace Exploration T. White, ERC, Inc., Moffett Field, CA; A. Laboratories, Albuquerque, NM Hampton, VA Agency (JAXA), Chofu, Japan Martin, University of Kentucky, Lexington, Lexington, KY Monday, 22 June 2015 69-TP-4 Aerothermodynamics I Steuben Chaired by: C. JOHNSTON, NASA-Langley Research Center 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2015-2509 AIAA-2015-2510 AIAA-2015-2511 AIAA-2015-2512 AIAA-2015-2513 AIAA-2015-2514 Modeling Fidelity for Oxygen State Specific Modeling of the DSMC Modeling of Nonequilibrium Measurement of Ultraviolet Comparison of Two Hybrid Radiative Heat Flux from Metallic Nonequilibrium Thermochemistry Energy Transfer in Nitrogen Shocks Electronic Excitation and Emission Radiative Heating Augmentation in RC-Models for Prediction of Species in Free Piston Shock Tunnel in Reflected Shock Tube Flows using High Fidelity Models for Hypersonic Sensor Applications HIEST Reflected Shock Tunnel Nonequilibrium Radiation from HIEST K. Neitzel, D. Andrienko, I. Boyd, T. Zhu, Z. Li, N. Parsons, Pennsylvania J. Burt, E. Josyula, Air Force Research B. Cruden, A. Brandis, ERC, Inc., Moffett Strong Shock Waves S. Nomura, H. Takayanagi, K. Fujita, University of Michigan, Ann Arbor, Ann State University, State College, PA; D. Laboratory, Wright-Patterson AFB, OH Field, CA; J. Grinstead, J. Olejniczak, NASA S. Surzhikov, Russian Academy of H. Tanno, Japan Aerospace Exploration Arbor, MI Levin, M. Panesi, University of Illinois, Ames Research Center, Moffett Field, CA; Sciences, Moscow, Russia Agency (JAXA), Chofu, Japan Urbana-Champaign, Urbana, IL L. Kirk, R. Lillard, NASA Johnson Space Center, Houston, TX; et al. Monday, 22 June 2015 70-NW-2 Networking Coffee Break Meeting Room Foyers 1530 - 1600 hrs Monday, 22 June 2015 71-AIAA-1 Speed Geek Networking Event and Reception Chantilly Ballroom Foyer 1730 - 1900 hrs This 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.
60 Sponsored by: Lockheed Martin Monday, 22 June 2015 72-CASE-3 CASE Networking Social Morocco 1730 - 1900 hrs Sponsored by Boeing Commercial Airplanes Monday, 22 June 2015 73-LEC-1 Fluid Dynamics Award Lecture Grand Ballroom D 1730 - 1830 hrs
Searching for Truthiness in Computational Fluid Dynamics Philip Roe Professor, Department of Aerospace Engineering University of Michigan Monday, 22 June 2015 74-RLA-1 Rising Leaders in Aerospace Networking Reception Emerald 1830 - 1930 hrs The 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. Tuesday Tuesday, 23 June 2015 75-SB-2 Speakers’ Briefing Session Rooms 0730 - 0800 hrs Tuesday, 23 June 2015 76-PLNRY-2 Plenary Panel Chantilly Ballroom West 0800 - 0900 hrs
NextGen: A Model of Stakeholder Engagement Bill Ayer Edward L. Bolton Jr. Retired Chairman and CEO Assistant Administrator for NextGen Alaska Air Group Federal Aviation Administration
Tuesday, 23 June 2015 77-AA-11 Fan Noise Fleur-de-lis A Chaired by: S. GLEGG, Florida Atlantic University 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2015-2515 AIAA-2015-2516 AIAA-2015-2517 AIAA-2015-2518 AIAA-2015-2519 Extrapolation of RANS flow data System Noise Prediction of the Fan noise scaling of static data Validation of a Moving-Body High- Effect of Stator Vane Sweep on for improved analytical fan tone DGEN 380 Turbofan Engine using semi-analytical methods and Order Immersed Boundary Method High Frequency Fan Noise and prediction J. Berton, NASA Glenn Research Center, assessment against experimental data for the Multiple Pure Tone Noise Comparison with Experiment R. Jaron, A. Moreau, S. Guerin, German Cleveland, OH V. Blandeau, V. Pastorelli, Airbus, Toulouse, Generated by Supersonic Rotor A. Kozlov, H. Atassi, University of Notre Aerospace Center (DLR), Berlin, Germany France; A. Moreau, S. Guerin, German Dame, Notre Dame, IN
61 Cascades Aerospace Center (DLR), Berlin, Germany B. Pimenta, R. Bobenrieth Miserda, University of Brasília, Brasília, Brazil Tuesday, 23 June 2015 78-AA-12 Duct Acoustics II Fleur-de-lis B Chaired by: C. YEN, Jacobs Technology 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2015-2520 AIAA-2015-2521 AIAA-2015-2522 AIAA-2015-2523 AIAA-2015-2524 Aero-Acoustic Performance of Theoretical Study of Sound Sound Propagation in Lined Annular Upstream Radiation from Numerical Predictions of Mode Adaptive Nacelle Inlet Propagation in Lined Duct with Ducts with Mean Swirling Flow Supersonic Buried-nozzle Jets via Reflections in an Open Circular F. Majić, G. Efraimsson, C. O’Reilly, Royal Rigid Splices Using Wiener-Hopf A. Maldonado, R. Astley, J. Coupland, Scattering at the Shroud Edge Duct: Comparison with Theory Institute of Technology (KTH), Stockholm, Method G. Gabard, University of Southampton, A. Samanta, Indian Institute of Science, M. Dahl, NASA Glenn Research Center, Sweden X. Liu, H. Jiang, X. Huang, Peking Southampton, United Kingdom; D. Sutliff, Bangalore, India; J. Freund, University of Cleveland, OH; D. Hixon, University of University, Beijing, China NASA Glenn Research Center, Cleveland, OH Illinois, Urbana-Champaign, Urbana, IL Toledo, Toledo, OH Tuesday, 23 June 2015 79-AA-13 Trailing Edge Noise II Inverness Chaired by: J. GALLMAN, Gulfstream Aerospace Corporation 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2015-2525 AIAA-2015-2526 AIAA-2015-2527 AIAA-2015-2528 AIAA-2015-2529 AIAA-2015-2530 AIAA-2015-2531 Prediction of Porous Trailing Edge Prediction of Broadband Trailing- Parametric Investigations of Tonal Parametric Investigations of Tonal A Model for Jet-Surface Interaction On the Adjoint-based Control of Experimental Validation of a Semi- Noise Reduction via Acoustic Edge Noise Based on Blake Model Trailing-Edge Noise Generation by Trailing-Edge Noise Generation by Noise Using Physically Realizable Trailing-Edge Turbulence and Noise Analytical Trailing-Edge Noise Model Perturbation Equations and Volume and Amiet Theory Low-Reynolds Number Airfoils. Part Low-Reynolds Number Airfoils. Part Upstream Turbulence Conditions Minimization via Porous Material Including Broadband Scattering Averaging O. Stalnov, C. Paruchuri, P. Joseph, I - Experimental Studies II - Numerical Studies M. Afsar, Imperial College London, London, B. Zhou, N. Gauger, Technical University of K. Kucukcoskun, J. Christophe, C. Schram, von B. Fassmann, C. Rautmann, R. Ewert, J. University of Southampton, Southampton, G. Yakhina, M. Roger, École Centrale de L. Nguyen, W. Hiner, S. Salehian, V. Golubev, United Kingdom; S. Leib, Ohio Aerospace Kaiserslautern, Kaiserslautern, Germany; Kármán Institute for Fluid Dynamics, Rhode- Delfs, German Aerospace Center (DLR), United Kingdom Lyon, Lyon, France; L. Nguyen, V. Golubev, R. Mankbadi, Embry-Riddle Aeronautical Institute, Cleveland, OH S. Koh, M. Meinke, W. Schroeder, RWTH Saint-Genèse, Belgium; S. Moreau, University Braunschweig, Germany Embry-Riddle Aeronautical University, University, Daytona Beach, FL; G. Yakhina, Aachen University, Aachen, Germany of Sherbrooke, Sherbrooke, Canada Daytona Beach, FL École Centrale de Lyon, Lyon, France; et al. Tuesday, 23 June 2015 80-AA-14 Jet Noise Prediction III Lalique Chaired by: N. MURRAY, The University of Mississippi 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2015-2532 AIAA-2015-2533 AIAA-2015-2534 AIAA-2015-2535 AIAA-2015-2536 AIAA-2015-2537 Analysis of Intermittency of Aeroacoustic Analysis of a Large-scale structure evolution and Large eddy simulation for jet noise: Empiricism-free noise calculation Spatial stability characteristics of Supersonic Jet Noise with Helicopter Engine Jet Including a sound generation in a hotjet the importance of getting the from LES solution based on non-circular jets Synchronized LES Realistic Nozzle Geometry F. Feng, Q. Wang, China Academy of boundary layer right Goldstein generalized acoustic F. Lajús, Federal University of Santa U. Sasidharan Nair, L. Agostini, D. Gaitonde, M. Cetin, S. Koh, M. Meinke, W. Aerospace Aerodynamics, Beijing, China G. Brès, Cascade Technologies, Inc., Palo Alto, analogy: volume noise sources and Catarina, Florianópolis, Brazil; A. Cavalieri, Ohio State University, Columbus, OH Schroeder, RWTH Aachen University, CA; V. Jaunet, M. Le Rallic, P. Jordan, National meanflow effects Technological Institute of Aeronautics Aachen, Germany Center for Scientific Research (CNRS), Poitiers, V. Semiletov, S. Karabasov, A. (ITA), São José dos Campos, Brazil; C. France; T. Colonius, California Institute of Chintagunta, A. Markesteijn, Queen Mary Deschamps, Federal University of Santa Technology, Pasadena, CA; S. Lele, Stanford University of London, London, United Catarina, Florianópolis, Brazil University, Stanford, CA Kingdom Tuesday, 23 June 2015 81-AA-15 CAA Numerical Techniques II Obelisk A Chaired by: X. LI, Beihang University 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2015-2538 AIAA-2015-2539 AIAA-2015-2540 AIAA-2015-2541 AIAA-2015-2542 Coupled Overset Unstructured Optimized Explicit Dissipation DRP schemes perform poorly for Towards Cascade Trailing-Edge Zero-Average Source Terms for Discontinuous Galerkin Method Operators for Computational decaying or growing oscillations Noise Modeling Using a Mode- Multidimensional Nonlinear for Launch Environment Acoustics Aeroacoustics E. Brambley, University of Cambridge, Matching Technique Disturbance Equations Prediction (Invited) N. Mansouri, D. Hixon, University of Cambridge, United Kingdom M. Roger, École Centrale de Lyon, Ecully, D. Hixon, University of Toledo, Toledo, OH R. Harris, CFD Research Corporation, Toledo, Toledo, OH France; S. Moreau, GAUS, Sherbrooke,
62 Huntsville, AL; E. Collins, A. Sescu, Canada E. Luke, Mississippi State University, Mississippi State, MS Tuesday, 23 June 2015 82-ACD-2 Aircraft Design Methods and Tools Wyeth Chaired by: A. CHAPUT, University of Texas at Austin 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2015-2543 AIAA-2015-2544 AIAA-2015-2545 AIAA-2015-2546 AIAA-2015-2547 AIAA-2015-2548 Student Air Vehicle Design and Update on HCDstruct - A Tool for Simultaneous Aircraft Design Virtual flight testing in an aircraft User Defined Components in the Development of an Interactive Analysis - A Systems Engineering Hybrid Wing Body Conceptual and Trip Assignment under sizing and optimization process OpenVSP Parametric Geometry Tool Wave Drag Capability for the Model Based Approach Design and Structural Optimization Design Parameter and Demand P. Schmollgruber, N. Bartoli, ONERA, R. McDonald, California Polytechnic OpenVSP Parametric Geometry Tool A. Chaput, University of Texas, Austin, F. Gern, NASA Langley Research Center, Uncertainty Toulouse, France; Y. Gourinat, University of State University, San Luis Obispo, CA; J. M. Waddington, R. McDonald, California Austin, TX Hampton, VA P. Govindaraju, W. Crossley, Purdue Toulouse, Toulouse, France Gloudemans, Self, San Mateo, CA Polytechnic State University, San Luis University, West Lafayette, IN Obispo, CA Tuesday, 23 June 2015 83-AFM-5 Aircraft Flight Dynamics, Control, Handling Qualities and Performance II Plum Blossom A Chaired by: M. GRANT, Purdue University 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2015-2549 AIAA-2015-2550 AIAA-2015-2551 AIAA-2015-2552 AIAA-2015-2553 AIAA-2015-2554 Damage Mitigating on a Large Aerobatic Maneuvers of a Propeller Torque Effect on Cruise Energy Gain From an Atmosphere Interactions of Aircraft Design Finite Series Based Model Rotorcraft using Load Alleviating Conventional and Compound Trim of Standard and Mass- in Motion - Dynamic Soaring and and Control: Actuators Sizing and Reference Adaptive Control Flight Control Laws Rotorcraft - Flight Path Generation Actuated Airplane Regen-electric Flight Compared Optimization for an Unstable R. Gezer, ROKETSAN Missile Industries, D. Caudle, J. Horn, E. Keller, Pennsylvania and Dynamic Simulation S. Erturk, A. Dogan, University of Texas, J. Barnes, Pelican Aero Group, San Blended Wing-Body Inc., Ankara, Turkey; A. Kutay, Middle East State University, State College, PA; C. A. Thorsen, J. Horn, Pennsylvania State Arlington, Arlington, TX Pedro, CA Y. Denieul, D. Alazard, J. Bordeneuve, Technical University, Ankara, Turkey Thaiss, C. McColl, Technical Data Analysis, University, State College, PA University of Toulouse, Toulouse, France; Inc., Marietta, GA C. Toussaint, ONERA, Toulouse, France; G. Taquin, Airbus, Toulouse, France Tuesday, 23 June 2015 84-AFM-6 Aeroservoelastic (ASE) and Aerodynamic Prediction Methods Plum Blossom B Chaired by: A. DA RONCH, University of Southampton and T. RICHARDSON, University of Bristol 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2015-2555 AIAA-2015-2556 AIAA-2015-2557 AIAA-2015-2558 AIAA-2015-2559 Adaptive Chebyshev Neural Control Modeling and Simulation for Pilot In The Loop Aeroservoelastic Aero structural modeling of a wing On the Calculation of Pitch of a Multi-Input Aeroelastic System Autonomous Aerial Refueling Using Simulation In Support To The using CATIA V5 and XFLR5 software Damping Stability Derivatives of Despite Gust Load a Probe-Drogue System Conceptual Design Of A Fly By Wire and experimental validation using Aircrafts Using Unsteady Sensitivity P. Ghorawat, University of Nevada, Las H. Wang, X. Dong, J. Liu, J. Wang, Air Airplane the Price- Païdoussis wing tunnel Equations Vegas, Las Vegas, NV; K. Lee, Catholic Force Engineering University, Xi’an, China F. Bocola, V. Muscarello, G. Quaranta, P. D. Communier, M. Salinas, O. Carranza C. Guo, Y. Ren, Tsinghua University, Kwandong University, Gangnung, South Masarati, Technical University of Milan, Moyao, R. Botez, University of Québec, Beijing, China Korea; S. Singh, University of Nevada, Las Milano, Italy Montréal, Canada Vegas, Las Vegas, NV Tuesday, 23 June 2015 85-AMT-5/GT-5 Model Attitude, Deformation, and Data Acquisition Techniques Obelisk B Chaired by: R. GUYTON, USAF Wright Lab 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2015-2560 AIAA-2015-2561 Oral Presentation Oral Presentation AIAA-2015-2562 Temperature Measurement at the NASA Data Acquisition System New Wings level Yaw Capability in Model Deformation Measurements Model Deformation Measurement Exit of Annular Combustor with Software Development for Rocket the AEDC PWT 16T Tunnel on a Flexible Wing Capabilities at ETW Slinger in Turbojet Engine Propulsion Test Facilities B. Mills, Arnold Engineering Development R. Guyton, Air Force Research Laboratory, H. Quix, J. Semmelmann, M. Wright, D. Liu, J. Jin, F. Wang, W. Jin, Beihang P. Hebert, D. Davis, M. Turowski, W. Holladay, Complex, Tullahoma, TN Wright-Patterson AFB, OH European Transonic Windtunnel, Cologne, University, Beijing, China NASA Stennis Space Center, Stennis, MS; P. Germany Marshall, M. Duncan, Arctic Slope Regional
63 Corporation (ASRC), Stennis, MS; et al. Tuesday, 23 June 2015 86-AMT-6/GT-6 Spatially-Resolved Spectroscopic Techniques Edelweiss Chaired by: R. BURNS and A. CUTLER, The George Washington University 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2015-2563 AIAA-2015-2564 AIAA-2015-2565 AIAA-2015-2566 AIAA-2015-2567 WIDECARS Spectra Fitting in a Density Scaling and Calibration of Precision of FLEET Velocimetry using Application of FLEET Velocimetry Design and Application of Filtered Premixed Ethylene-Air Flame FLEET Temperature Measurements High-Speed CMOS Camera Systems in the NASA Langley 0.3-Meter Rayleigh Scattering Experiments A. Cutler, E. Gallo, L. Cantu, George N. Calvert, A. Dogariu, M. Edwards, R. C. Peters, Princeton University, Princeton, NJ; Transonic Cryogenic Tunnel for Mixing Studies of New Strut Washington University, Washington, DC Miles, Princeton University, Princeton, NJ P. Danehy, B. Bathel, NASA Langley Research R. Burns, National Institute of Aerospace, Injectors for Scramjets Center, Hampton, VA; N. Jiang, Spectral Hampton, VA; P. Danehy, S. Jones, NASA C. Ground, D. Thumiah, L. Maddalena, Energies, LLC, Dayton, OH; N. Calvert, R. Langley Research Center, Hampton, VA; University of Texas, Arlington, Arlington, TX Miles, Princeton University, Princeton, NJ B. Halls, N. Jiang, Spectral Energies, LLC, Dayton, OH Tuesday, 23 June 2015 87-APA-9 High Angle of Attack and High Lift Aerodynamics Stemmons C Chaired by: D. LACY, Boeing Commercial Airplanes and P. HARTWICH, Boeing Research & Technology 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2015-2568 AIAA-2015-2569 Oral Presentation AIAA-2015-2570 AIAA-2015-2571 AIAA-2015-2572 High Angle of Attack Flight of a Pressure Measurements of Burst Development Status of the High Lift Stall Maneuver Simulation of an Numerical Investigation of the Wall modeled large eddy Subscale Aerobatic Aircraft Wakes Over a Three-Element Airfoil Common Research Model (HL-CRM): A elastic Transport Aircraft based on Dynamic Behavior of a High-Lift simulation of the VFE-2 delta wing O. Dantsker, M. Selig, University of Illinois, B. Pomeroy, M. Selig, University of Illinois, Representative High Lift Configuration Flight Test Data Configuration with Circulation C. Zwerger, S. Hickel, C. Breitsamter, N. Urbana-Champaign, Urbana, IL Urbana-Champaign, Urbana, IL for Transonic Transports D. Rohlmann, S. Keye, German Aerospace Control Adams, Technical University of Munich, D. Lacy, The Boeing Company, Everett, WA; Center (DLR), Braunschweig, Germany D. Keller, R. Rudnik, German Aerospace Munich, Germany E. Dickey, A. Sclafani, The Boeing Company, Center (DLR), Braunschweig, Germany Huntington Beach, CA Tuesday, 23 June 2015 88-APA-10 Wind Tunnel and Flight Testing Carpenter Ballroom Chaired by: J. PINIER, NASA Langley Research Center and G. GATLIN, NASA Langley Research Center 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2015-2573 AIAA-2015-2574 AIAA-2015-2575 AIAA-2015-2576 AIAA-2015-2577 AIAA-2015-2578 AIAA-2015-2579 Analysis of Single Hole Simulated Windspeed and Flow Angle Low Speed Wind Tunnel Design of a swept wing wind tunnel Numerical Replication and Development, Startup Operations Study of the flow field near the Battle Damage on a Wing Using Measurement by Tracking of a Investigation of a Circulation model for study of cross-flow Improvement of Wind Tunnel Tests and Tests of a Propeller Wind AOA sensor of an A320 aircraft Particle Image Velocimetry Laser-Induced Breakdown Spark Control Wing for Enhanced Lift instability for Design and Off-Design Operating Tunnel Test Rig J. Katz, San Diego State University, San M. Almond, P. Render, A. Walker, M. Rennie, M. Nguyen, S. Gordeyev, E. K. Kanistras, P. Saka, K. Valavanis, N. J. Serpieri, M. Kotsonis, Delft University of Points of Wind Turbine Airfoils S. Speck, S. Herbst, H. Kim, F. Stein, M. Diego, CA Loughborough University, Loughborough, Jumper, University of Notre Dame, Notre Vitzilaios, M. Rutherford, University of Technology, Delft, The Netherlands T. Kuhn, ENERCON GmbH, Bremen, Germany; Hornung, Technical University of Munich, United Kingdom Dame, IN; A. Cain, Innovative Technology Denver, Denver, CO A. Altmikus, ENERCON GmbH, Aurich, Garching, Germany Applications Company, LLC, Chesterfield, Germany; N. Balaresque, Deutsche WindGuard MO; T. Hayden, U.S. Air Force Academy, GmbH, Varel, Germany; M. Lippert, University Colorado Springs, CO of Applied Sciences, Kiel, Germany Tuesday, 23 June 2015 89-APA-11 Special Session: Low Boom Activities II Stemmons A Chaired by: S. CLIFF, NASA-Ames and K. WAITHE, Gulfstream Aerospace Corporation 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2015-2580 AIAA-2015-2581 AIAA-2015-2582 AIAA-2015-2583 AIAA-2015-2584 Design of Optimum Equivalent- Feasibility of Supersonic Aircraft Uncertainty Analysis and Robust Rise Time Prediction of Sonic Free Flight Measurement of Aircraft Area Target for High-Fidelity Low- Concepts for Low-Boom and Flight Design of Low-Boom Concepts Boom by Full-Field Simulation with Model using Aero Ballistic Range Boom Aircraft Design Trim Constraints using Atmospheric Adjoints Thermal Nonequilibrium A. Iwakawa, D. Furukawa, Y. Aoki, A. C. Ocheltree, S. Choi, Virginia Polytechnic W. Li, NASA Langley Research Center, S. Rallabhandi, National Institute of R. Yamashita, K. Suzuki, University of Sasoh, Nagoya University, Nagoya, Japan Institute and State University, Blacksburg, Hampton, VA Aerospace, Hampton, VA Tokyo, Kashiwa, Japan
64 VA Tuesday, 23 June 2015 90-APA-12 Weapons Aerodynamics: Missile/Projectile/Guided-Munitions, Carriage and Store Separation I Stemmons B Chaired by: C. PASILIAO, AFRL/RWWV and C. ROSEMA, US Army AMRDEC 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2015-2585 AIAA-2015-2586 AIAA-2015-2587 AIAA-2015-2588 AIAA-2015-2589 Flight Behaviors of a Complex Effect of Canard Deflection on Fin Enhanced Body Vortex Modeling A Comparison of Predictive Delayed Detached Eddy Simulation Projectile using a Coupled CFD- Performance of a Fin-Stabilized Within Missile Datcom Methodologies for Missile of Projectile Flows based Simulation Technique: Free Projectile J. Doyle, C. Rosema, Army Aviation Configurations with Strakes J. Gan, G. Zha, University of Miami, Coral Motion S. Silton, Army Research Laboratory, and Missile Research Development and C. Rosema, Army Aviation and Missile Gables, FL J. Sahu, F. Fresconi, Army Research Aberdeen Proving Ground, MD; C. Coyle, Engineering Center, Redstone Arsenal, AL Research Development and Engineering Laboratory, Aberdeen Proving Ground, MD U.S. Military Academy, West Point, NY Center, Redstone Arsenal, AL Tuesday, 23 June 2015 91-ATIO-9 Terminal & Surface Operations III Manchester Chaired by: A. SARAF, Saab Sensis Corporation 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2015-2590 AIAA-2015-2591 AIAA-2015-2592 AIAA-2015-2593 AIAA-2015-2594 AIAA-2015-2595 Identifying Key Issues and Potential Integration of Uncertain Ramp Area The effects of Electric Taxi Systems Punctuality as KPI for Performance Determining Airport Airside Integration of a Routing Tool in Solutions for Integrated Arrival, Aircraft Trajectories and Generation on airport surface congestion Based Airport Management Capacity Utilization: A Demand- an Advanced Airport Controller Departure, Surface Operations by of Optimal Taxiway Schedules at P. Roling, P. Sillekens, R. Curran, Delft S. Loth, S. Helm, German Aerospace Driven Approach Working Position Surveying Stakeholder Preferences Charlotte Douglas (CLT) Airport University of Technology, Delft, The Center (DLR), Braunschweig, Germany C. Schinwald, M. Hornung, Technical M. Ellejmi, EUROCONTROL, Brussels, B. Aponso, R. Coppenbarger, Y. Jung, NASA J. Coupe, D. Milutinovic, University of Netherlands; W. Wilder, KLM Royal Dutch University of Munich, Munich, Germany Belgium; B. Weiss, F. Schmitt, S. Straub, Ames Research Center, Moffett Field, CA; C. California, Santa Cruz, Santa Cruz, CA; W. Airlines, Schiphol, The Netherlands Deutsche Flugsicherung GmbH (DFS), O’Connor, G. Lohr, NASA Langley Research Malik, UARC at NASA Ames Research Center, Frankfurt, Germany Center, Hampton, VA; L. Quon, NASA Ames Moffett Field, CA; Y. Jung, NASA Ames Research Center, Moffett Field, CA; et al. Research Center, Moffet Field, CA Tuesday, 23 June 2015 92-ATIO-10 ATM I - Trajectory Enhancements Milan Chaired by: S. ROY, Washington State Univ 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2015-2596 AIAA-2015-2597 AIAA-2015-2598 AIAA-2015-2599 AIAA-2015-2600 Impact of Airspace Charges on Presentation of three methods Simple Tool for Aircraft Noise- Trajectory Accuracy Sensitivity to Trajectory Inefficiency Metric Transatlantic Aircraft Trajectories results comparison for Vertical Reduction Route Design Modeling Factors for Measuring Operational B. Sridhar, NASA Ames Research Center, Navigation VNAV trajectory J. Li, N. Chen, B. Sridhar, H. Ng, NASA S. Torres, Lockheed Martin Corporation, Performance of Flights in the Moffett Field, CA; H. Ng, University of optimization for the Flight Ames Research Center, Moffett Field, CA Rockville, MD National Airspace System California, Santa Cruz, Moffett Field, CA; Management System FMS S. Tsao, R. Mayer, A. Mahashabde, MITRE F. Linke, German Aerospace Center (DLR), B. Beulze, B. Dancila, R. Botez, University Corporation, McLean, VA Hamburg, Germany; N. Chen, NASA Ames of Québec, Montréal, Canada Research Center, Moffett Field, CA Tuesday, 23 June 2015 93-ATIO-11 Transformational Flight - On-Demand Mobility Metropolitan Ballroom Chaired by: B. GERMAN, Georgia Institute of Technology 0900 hrs 0930 hrs 1000 hrs Oral Presentation Oral Presentation Oral Presentation On-Demand Mobility: Aviation’s On-Demand Mobility Technical On-Demand Mobility Technical Future Path to High Speed Regional Pathway: Enabling Ease of Use Pathway: Enabling Low Community Mobility and Safety Noise, Low Operating Costs, Robust M. Moore, NASA Langley Research Center, K. Goodrich, M. Moore, NASA Langley Control, and Ride Quality Hampton, VA Research Center, Hampton, VA M. Moore, NASA Langley Research Center, Hampton, VA 65 Tuesday, 23 June 2015 94-CASE-4 Applied Complexity Workshop Grand Ballroom D 0900 - 1200 hrs Participants 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 Steve Holt Jim Blohowiak Alison Lauderbach Systems Engineering & Integration Team 777X Engineering Integrated Strategy, Airplane Level Engineering Integration 777X Airplane Level Integration Team 777X Airplane Level Integration Team Boeing Commercial Airplanes The Boeing Company The Boeing Company The Boeing Company
Tuesday, 23 June 2015 95-CFD-9 Adaptive High-Order Methods Grand Ballroom A Chaired by: G. MAY, RWTH Aachen and S. ALLMARAS, MIT 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2015-2601 AIAA-2015-2602 AIAA-2015-2603 AIAA-2015-2604 AIAA-2015-2605 AIAA-2015-2606 A Unifying Computational An Output-Based Adaptive An Adjoint-Based hp-Adaptive An Adaptive Simplex Cut-Cell Method Improving High-Order Finite Hp-Adaptivity on Anisotropic Framework for Adaptive High- Hybridized Discontinuous Galerkin Petrov-Galerkin Method for for High-Order Discontinuous Galerkin Element Approximation Through Meshes for Hybridized Order Finite Element Methods Method on Deforming Domains Turbulent Flows Discretizations of Conjugate Heat Geometrical Warping Discontinuous Galerkin Scheme M. Woopen, A. Balan, G. May, RWTH K. Fidkowski, University of Michigan, Ann B. Reza Ahrabi, W. Anderson, J. Newman, Transfer Problems D. Sanjaya, K. Fidkowski, University of A. Balan, M. Woopen, G. May, RWTH Aachen University, Aachen, Germany Arbor, Ann Arbor, MI University of Tennessee, Chattanooga, S. Ojeda, H. Sun, S. Allmaras, D. Darmofal, Michigan, Ann Arbor, Ann Arbor, MI Aachen University, Aachen, Germany Chattanooga, TN Massachusetts Institute of Technology, Cambridge, MA Tuesday, 23 June 2015 96-CFD-10 Turbulent Flow Simulations I Grand Ballroom B Chaired by: S. POROSEVA, The University of New Mexico and S. TIMME, The University of Liverpool 0900 hrs 0930 hrs 1000 hrs 1030 hrs AIAA-2015-2607 AIAA-2015-2608 AIAA-2015-2609 AIAA-2015-2610 Delayed Detached-Eddy Simulation Flow Control of a Rotating Cylinder Simulations of Incompressible Jet pump optimization through of Shock Buffet on Half Wing-Body by the Use of a Structured Surface: Separated Turbulent Flows around Reynolds averaged Navier-Stokes Configuration A Visualization of Flow Structures Two-Dimensional Bodies with Simulation Analysis F. Sartor, S. Timme, University of T. Schomberg, R. Ritz, O. Wünsch, URANS Models in OpenFOAM G. Gherman, I. Malael, COMOTI Romanian Liverpool, Liverpool, United Kingdom University of Kassel, Kassel, Germany; M. A. Porteous, R. Habbit, J. Colmenares, Research & Development Institute for Gas Ruetten, R. Kessler, German Aerospace S. Poroseva, University of New Mexico, Turbines, Bucharest, Romania; M. Mihaescu, Center (DLR), Göttingen, Germany Albuquerque, Albuquerque, NM; S. Royal Institute of Technology (KTH), Murman, NASA Ames Research Center, Stockholm, Sweden; I. Porumbel, COMOTI Moffett Field, CA Romanian Research & Development Institute for Gas Turbines, Bucharest, Romania Tuesday, 23 June 2015 97-CFD-11 Meshing Techniques II Coral Chaired by: M. PARK, NASA-Langley Research Center and D. THOMPSON, Mississippi State University 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2015-2611 AIAA-2015-2612 AIAA-2015-2613 AIAA-2015-2614 AIAA-2015-2615 Comparison of r-Adaptation Implementation of Ball-Center Anisotropic Non-Uniform Block- A shifting discontinuous-grid-block Numerical simulation of an X-wing Techniques for 2-D CFD Applications Spring Analogy Mesh Deformation Based Adaptive Mesh Refinement lattice Boltzmann method for flapping wing MAV by means of a W. Tyson, J. Derlaga, A. Choudhary, C. Technique with CFD Design for Three-Dimensional Inviscid and moving boundary simulations deforming overset grid method Roy, Virginia Polytechnic Institute and Optimization Viscous Flows N. Arora, A. Gupta, Indian Institute of S. Deng, Delft University of Technology, Delft, State University, Blacksburg, VA 66 Y. Yang, S. Özgen, Middle East Technical L. Freret, C. Groth, University of Toronto, Technology Delhi, New Delhi, India; W. The Netherlands; T. Xiao, Nanjing University of University, Ankara, Turkey Toronto, Canada Shyy, Hong Kong University of Science and Aeronautics and Astronautics, Nanjing, China; Technology, Hong Kong, Hong Kong M. Percin, B. van Oudheusden, H. Bijl, B. Remes, Delft University of Technology, Delft, The Netherlands Tuesday, 23 June 2015 98-CFD-12 LES, DNS, and Hybrid RANS-LES II Emerald Chaired by: N. BISEK, Air Force Reseach Laboratory and A. SESCU, Mississippi State University 0900 hrs 0930 hrs 1000 hrs 1030 hrs AIAA-2015-2616 AIAA-2015-2617 AIAA-2015-2618 AIAA-2015-2619 Simulation of Boundary Layer The Effect of Initial Conditions on Turbulent inflow generation in Further Studies of Adverse Pressure flows over Biofouled Surfaces Streamwise Vortices in the Plane square duct at supersonic Mach Gradient Effects in Turbulent Channel J. Sadique, X. Yang, C. Meneveau, Turbulent Mixing Layer number Flows R. Mittal, Johns Hopkins University, W. McMullan, S. Garrett, University of C. Roussel, F. Alizard, F. Grasso, Paris A. Jesus, Technological Institute of Aeronautics Baltimore, MD Leicester, Leicester, United Kingdom Institute of Technology, Paris, France (ITA), São José dos Campos, Brazil; L. Schiavo, University of Campinas, Campinas, Brazil; J. Azevedo, Aeronautics and Space Institute (IAE), São José dos Campos, Brazil; J. Laval, National Center for Scientific Research (CNRS), Villeneuve d’Ascq, France Tuesday, 23 June 2015 99-FD-10 Boundary-Layer Transition Sapphire Chaired by: E. MARINEAU, AEDC White Oak and J. KLENTZMAN, Baylor University 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2015-2620 AIAA-2015-2621 AIAA-2015-2622 AIAA-2015-2623 AIAA-2015-2624 AIAA-2015-2625 AIAA-2015-2626 Turbulent Density Fluctuations in Automatic transition prediction in Large-Eddy Simulation of A local scattering approach for Numerical Simulation of Three- Computations of Disturbance Acoustic radiation due to scattering Thermal Boundary Layers Studied an industrial Navier-Stokes solver Transitional Flows on a Compressor the effect of abrupt changes on Dimensional Wave Packet Amplification Behind Isolated of T-S wave by nonlinear roughness via Molecular Rayleigh scattering using higher-order finite elements Blade boundary-layer instability and in Supersonic Flow over a Roughness Elements and in subsonic boundary layer flows J. Panda, NASA Ames Research Center, R. Gross, F. Chalot, J. Courty, M. Mallet, D. Z. Wang, Aviation Industry Corporation of transition: a numerical method Compression Corner Comparison with Measurements M. Dong, Tianjin University, Tianjin, China; Moffett Field, CA Tran, Dassault Group, Saint Cloud, France; China (AVIC), Shanghai, China Z. Huang, Tianjin University, Tianjin, China; A. Novikov, Moscow Institute of Physics M. Choudhari, F. Li, NASA Langley X. Wu, Imperial College London, London, D. Arnal, ONERA, Toulouse, France; et al. X. Wu, Imperial College London, London, and Technology, Zhukovsky, Russia; I. Research Center, Hampton, VA; M. Bynum, United Kingdom United Kingdom Egorov, TsAGI, Zhukovsky, Russia; A. AMA Research Associates, Hampton, Fedorov, Moscow Institute of Physics and VA; M. Kegerise, R. King, NASA Langley Technology, Zhukovsky, Russia Research Center, Hampton, VA Tuesday, 23 June 2015 100-FD-11 Unsteady Wing Aerodynamics I Govenors Lecture Hall Chaired by: K. MOORED, Lehigh University and M. RINGUETTE, University at Buffalo 0900 hrs 0930 hrs 1000 hrs 1030 hrs AIAA-2015-2627 AIAA-2015-2628 AIAA-2015-2629 AIAA-2015-2630 Development of coherent structures Analyzing Vortex Dynamics in the Analysis of cruise flight of the Topology and Flow Structures of within the laminar separation Laminar Separation Bubble vis calliope hummingbird Three-Dimensional Separation bubble of a NACA0018 airfoil Surface Pressure Measurements J. Song, H. Luo, Vanderbilt University, Bubbles: The Effect of Aspect Ratio J. Kurelek, A. Lambert, S. Yarusevych, A. Lambert, S. Yarusevych, University of Nashville, TN; B. Tobalske, University S. Hosseinverdi, R. Jacobi, H. Fasel, University of Waterloo, Waterloo, Canada Waterloo, Waterloo, Canada of Montana, Missoula, Missoula, MT; T. University of Arizona, Tucson, Tucson, AZ
67 Hedrick, University of North Carolina, Chapel Hill, Chapel Hill, NC Tuesday, 23 June 2015 101-FD-12 Airfoil Separation Control Senators Lecture Hall Chaired by: M. VISBAL, USAF AFRL/RQVA and K. TAIRA, Florida State University 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2015-2631 AIAA-2015-2632 AIAA-2015-2633 AIAA-2015-2634 AIAA-2015-2635 AIAA-2015-2636 Modeling Lift Hysteresis with a Surface vorticity flux analysis in Measurements of 3-D Stall Cells on Interactions of a Low Aspect Ratio Simulation of a Laminar-Flow Global stability analysis of a Modified Goman-Khrabrov Model on separation control on NACA 0012 2-D Airfoil Dynamic Pin with a Laminar Compatible High-Lift Configuration compressible turbulent flow around Pitching Airfoils airfoil E. Demauro, H. Dell’Orso, V. Sivaneri, B. Boundary Layer with Flow Control a high-lift configuration D. Williams, Illinois Institute of Technology, P. Munday, K. Taira, Florida State Tuna, M. Amitay, Rensselaer Polytechnic S. Gildersleeve, C. Leong, M. Amitay, D. Rizzetta, M. Visbal, Air Force Research M. Iorio, Airbus, Madrid, Spain; L. Chicago, IL; F. Reissner, Technical University University, Tallahassee, FL Institute, Troy, NY Rensselaer Polytechnic Institute, Troy, NY Laboratory, Wright-Patterson AFB, OH Gonzalez, Technical University of Madrid, of Berlin, Berlin, Germany; D. Greenblatt, Madrid, Spain; A. Martinez, Airbus, Filton, H. Muehler-Vahl, Technion--Israel Institute United Kingdom of Technology, Haifa, Israel; C. Strangfeld, Technical University of Berlin, Berlin, Germany Tuesday, 23 June 2015 102-FD-13 Shock-Dominated Flows Topaz Chaired by: M. GAMBA, University of Michigan and J. POGGIE, USAF AFRL/RBAC 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2015-2637 AIAA-2015-2638 AIAA-2015-2639 AIAA-2015-2640 AIAA-2015-2641 AIAA-2015-2642 Assessing Blast Loading Within Study of Bow-Shock Instabilities HIFiRE-1 Turbulent Shock Boundary Numerical Simulation Exploring Numerical Investigation of Shock- On unsteady shock wave reflections Obstacle Arrays in front of Hemispherical Shell at Layer Interaction -Flight Data and Supersonic Flow Over a Wall- induced Laminar Separation Bubble from wedges with straight and D. Mott, Naval Research Laboratory, Hypersonic Mach Number 7 Computations Mounted Half-Cylinder Turret in Supersonic Flows concave tips Washington, DC; T. Young, Berkeley A. Vashishtha, University of Tokyo, R. Kimmel, Air Force Research Laboratory, P. Morgan, Ohio Aerospace Institute, J. Sivasubramanian, H. Fasel, University of F. Alzamora Previtali, E. Timofeev, McGill Research Associates, Beltsville, MD; Kashiwa, Japan; Y. Watanabe, University Wright-Patterson AFB, OH; D. Prabhu, ERC, Dayton, OH; M. Visbal, Air Force Research Arizona, Tucson, Tucson, AZ University, Montréal, Canada; H. Kleine, D. Schwer, P. Matic, Naval Research of Tokyo, Bunkyo, Japan; K. Suzuki, Inc., Moffett Field, CA Laboratory, Wright-Patterson AFB, OH University of New South Wales at the Laboratory, Washington, DC University of Tokyo, Kashiwa, Japan Australian Defence Force Academy, Canberra, Australia Tuesday, 23 June 2015 103-ITAR-1 ITAR - Hypersonic Flow Phenomena (Invited) Morocco Chaired by: K. CASPER 0900 hrs 0930 hrs 1000 hrs 1030 hrs Oral Presentation Oral Presentation Oral Presentation Oral Presentation HTV-2 Boundary Layer Transition - STABL-3D Software Overview Mach 10 Boundary Layer Transition Stability Analysis of Hypersonic Summary and Lessons Learned H. Johnson, GoHypersonic, Inc., Experiments on Sharp and Blunted Flows Using STABL-3D R. Kimmel, Air Force Research Laboratory, Minneapolis, MN Cones B. Wheaton, Johns Hopkins University Wright-Patterson AFB, OH E. Marineau, D. Lewis, J. Lafferty, G. Applied Physics Laboratory, Laurel, MD; H. Moraru, Arnold Engineering Development Johnson, GoHypersonic, Inc., Dayton, OH; Center, Silver Spring, MD R. Wagnild, Sandia National Laboratories, Albuquerque, NM 68 Tuesday, 23 June 2015 104-MAO-3 Applications I Madrid Chaired by: A. NAJAFI, ANSYS, Inc. and P. PIPERNI, Bombardier Inc 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2015-2646 AIAA-2015-2647 AIAA-2015-2648 AIAA-2015-2649 AIAA-2015-2650 AIAA-2015-2651 Optimization of System Evolvability An Application of Conceptual Geometry Driven High Fidelity Application of automatic algorithm Multidisciplinary and Multilevel Development of a Java-based Under Uncertainty Design and Multidisciplinary Stability Derivatives Obtained Using generation to air-to-air refueling Aircraft Design Methodology framework for aircraft preliminary J. Watson, J. Allen, C. Mattson, Brigham Analysis Transitioning to Detailed Automated CFD Analysis Process scheduling Using Enhanced Collaborative design and optimization Young University, Provo, UT; S. Ferguson, Design Stages N. Bhagat, Wright State University, R. Entz, G. Scherer Schwening, R. Optimization F. Nicolosi, A. De Marco, L. Attanasio, North Carolina State University, Raleigh, A. Renner, F. Thompson, V. Kalivarapu, Beavercreek, OH; E. Alyanak, Air Force Fernandes de Oliveira, Airbus, Munich, P. Albuquerque, P. Gamboa, M. Silvestre, D. Gambardella, University of Naples NC E. Winer, J. Oliver, Iowa State University, Research Laboratory, Wright-Patterson AFB, Germany University of Beira Interior, Covilha, “Federico II”, Naples, Italy Ames, IA; B. Gilmore, Deere & Company, OH; D. Allison, Optimal Flight Sciences, LLC, Portugal Moline, IL; et al. Dayton, OH Tuesday, 23 June 2015 105-MST-5 Guidance, Control, and Dynamics II Travertine Chaired by: T. ALEXEEV, University of California Davis and J. KNOWLES, Loughborough University 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2015-2652 AIAA-2015-2653 AIAA-2015-2654 AIAA-2015-2655 AIAA-2015-2656 Semi-Implicit Numerical A Bifurcation Study of a Dynamic Multi-Fidelity Simulation of Cargo Control Enhanced and The mode switch control research Simulations of Nonlinear Dynamics Model of a Nose Landing Gear Airdrop: From the Payload Bay to the Parameterized Load Relief of small-type parallel TBCC engine of Beams, Plates, and Shells Mechanism Subjected to External Ground technology for a Launch Vehicle based on SQP method T. Alexeev, Siemens Energy, Inc., Boulder, Disturbances T. Jann, S. Geisbauer, N. Bier, German W. Yang, S. Tang, Z. Xu, Northwestern Q. Xiaojie, W. Su, Y. Tang, Aviation CO; M. Hafez, University of California, J. Knowles, Loughborough University, Aerospace Center (DLR), Braunschweig, Polytechnical University, Xi’an, China Industry Corporation of China (AVIC), Davis, Davis, CA Loughborough, United Kingdom; E. Germany; W. Krüger, H. Schmidt, German Wuxi, China Coetzee, Airbus, Bristol, United Kingdom Aerospace Center (DLR), Göttingen, Germany Tuesday, 23 June 2015 106-NW-3 Networking Coffee Break Chantilly Ballroom East 0900 - 0930 hrs Tuesday, 23 June 2015 107-PDL-4 Plasma Assisted Combustion Miro Chaired by: K. XU, University of Alabama in Huntsville 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2015-2657 AIAA-2015-2658 AIAA-2015-2659 AIAA-2015-2660 AIAA-2015-2661 AIAA-2015-2662 Electron Temperature in a Laser-Induced Heating Using a Magnetic positioning of the Towards Laser Ignition by Rapid Multiphysics simulations of plasma- Investigation of Thermal Cycling Methane-Air Flame under a DC Non-Resonant Dual-Pulse Approach electric discharge in the volume of Heating of Water Vapor assisted combustion dynamics in a Property of Thermal Barrier Electric Field with Application to Laser Ignition supersonic flow C. Dumitrache, A. Yalin, Colorado State direct-coupled microwave reactor Coatings with Laser Deposited Mesh S. Jacobs, K. Xu, University of Alabama, C. Dumitrache, C. Rose, A. Yalin, Colorado A. Firsov, Russian Academy of Sciences, University, Fort Collins, CO A. Palla, J. Zimmerman, D. Carroll, CU Structure Huntsville, Huntsville, AL State University, Fort Collins, CO Moscow, Russia; S. Leonov, University of Aerospace, Champaign, IL; C. Mitsingas, S. Shi, W. Chen, Z. Hong, D. Gao, Aviation Notre Dame, Notre Dame, IN S. Hammack, T. Lee, University of Illinois, Industry Corporation of China (AVIC), Urbana-Champaign, Urbana, IL Shanghai, China Tuesday, 23 June 2015 108-TP-5 Plasma and Arc Jet Testing, Diagnostics and Computational Methods Rosetta Chaired by: M. WINTER, University of Kentucky and P. YEE, The Aerospace Corporation 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2015-2663 AIAA-2015-2664 AIAA-2015-2665 AIAA-2015-2666 AIAA-2015-2667 AIAA-2015-2668 Arc Jet Facility Test Condition Comparisons of PICA In-depth Material Enabling the Statistical Calibration Side Arm Reactor Study of Copper Consolidating NASA’s Arc-Jet Physico-Chemistry of CN in the Predictions Using the ADSI Code Performance and Ablator Response of Active Nitridation of Graphite by Catalysis J. Balboni, T. Gokcen, F. Hui, P. Graube, P. Boundary Layer of Graphite in G. Palmer, D. Prabhu, ERC, Inc., Huntsville, Modeling from MEDLI Arc Jet Tests Atomic Nitrogen D. Driver, NASA Ames Research Center, Morrissey, NASA Ames Research Center, Nitrogen Plasmas 69 AL; I. Terrazas-Salinas, NASA Ames D. Smith, University of Kentucky, Lexington, P. Bauman, State University of New York, Moffett Field, CA; S. Sepka, ERC, Inc., Moffett Field, CA; R. Lewis, NASA Johnson B. Helber, T. Alessandro, O. Chazot, M. Research Center, Moffett Field, CA Lexington, KY; T. White, ERC, Inc., Moffett Buffalo, NY Moffett Field, CA Space Center, Houston, TX Thierry, von Kármán Institute for Fluid Field, CA; A. Martin, University of Kentucky, Dynamics, Rhode-Saint-Genèse, Belgium Lexington, Lexington, KY Tuesday, 23 June 2015 109-F360-3 Day in the Life of Operations - Effectively Managing Disruption Grand Ballroom E 0930 - 1200 hrs Moderator: Neil Planzer, Vice President, Air Traffic Management, Boeing Commercial Airplanes Panelits: Tim Campbell Jim Crites BrianQuigley Dan Smiley Senior Vice President, Air Operations Executive Vice President of Operations Managing Director Flight Operations Vice President for Systems Operations, Federal Aviation American Airlines DFW International Airport United Airlines Administration Air Traffic Office
Tuesday, 23 June 2015 111-LNCH-1 Awards Luncheon: Celebrating Achievements in Aerospace Sciences Chantilly Ballroom West 1230 - 1400 hrs A ticket is required and included in the conference registration fee where indicated. Tuesday, 23 June 2015 112-AA-16 CAA Sound Generation II Fleur-de-lis A Chaired by: J. DELFS, DLR - German Aerospace Center 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2015-2669 AIAA-2015-2670 AIAA-2015-2671 AIAA-2015-2672 AIAA-2015-2673 AIAA-2015-2674 Prediction of low-speed fan Synthetic Turbulence Methods for Prediction of Slat Broadband Noise Towards high-lift noise from Fast Compact Assumption Applied to Centrifugal Compressor: The Sound trailing-edge noise based on RANS Leading Edge Noise Predictions with RANS Results Multipole BEM with anisotropic the Monopole Term of Farassat’s of Surge and on scale resolved simulations F. Gea-Aguilera, X. Zhang, X. Chen, J. Gill, B. Bai, X. Li, Y. Guo, Beihang University, synthetic turbulence sources Formulation E. Sundström, M. Mihaescu, Royal G. Grasso, J. Christophe, C. Schram, von University of Southampton, Southampton, Beijing, China; F. Thiele, Technical N. Reiche, M. Lummer, R. Ewert, German L. Lopes, NASA Langley Research Center, Institute of Technology (KTH), Stockholm, Kármán Institute for Fluid Dynamics, United Kingdom; T. Nodé-Langlois, Airbus, University of Berlin, Berlin, Germany Aerospace Center (DLR), Braunschweig, Hampton, VA Sweden Rhode-Saint-Genèse, Belgium Toulouse, France Germany Tuesday, 23 June 2015 113-AA-17 CAA Propagation and Scattering I Fleur-de-lis B Chaired by: S. CARO, CD-Adapco 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs AIAA-2015-2675 AIAA-2015-2676 AIAA-2015-2677 AIAA-2015-2678 AIAA-2015-2679 AIAA-2015-2680 AIAA-2015-2681 Direct and inverse uncertainty Stabilized Time-domain Impedance Evaluation and Development Implementation of a surface based Acoustic Scattering Matrices for Numerical assessment of the Enhancements of a time-domain quantification of acoustic refraction Model and the Application in of Non-Reflective Boundary coupling approach in a high-order Higher-Order Modes for Simple scattering of acoustic waves by equivalent source method for phenomena through a shear layer Bypass Duct Noise Simulations Conditions for Aeroacoustic DG aeroacoustics propagation Orifice Configurations with Flow turbulent structures acoustic scattering P. Cinnella, Università del Salento, Lecce, X. Liu, X. Huang, Peking University, Simulations solver C. Temmler, M. Schulze, T. Sattelmayer, V. Clair, G. Gabard, University of S. Swift, G. Blaisdell, Purdue University, Italy; X. Gloerfelt, X. Merle, Paris Institute Beijing, China J. Gill, R. Fattah, X. Zhang, University M. Muriel Gracia, W. De Roeck, W. Technical University of Munich, Munich, Southampton, Southampton, United West Lafayette, IN; A. Lyrintzis, Embry- of Technology, Paris, France of Southampton, Southampton, United Desmet, Catholic University of Leuven, Germany Kingdom Riddle Aeronautical University, Daytona Kingdom Leuven, Belgium Beach, FL
70 Tuesday, 23 June 2015 114-AA-18 General Acoustics I Inverness Chaired by: C. BAILLY, Ecole Centrale de Lyon 1400 hrs 1430 hrs 1500 hrs 1530 hrs AIAA-2015-2682 AIAA-2015-2683 AIAA-2015-2684 AIAA-2015-2685 Sound and Distortion Produced Nozzle-to-Ground Distance Effect The Acoustic Environment of the Sonic Boom Assessment of a by a Braking Rotor Operating in on Nondominated Solutions of NASA Glenn 9- by 15-Foot Low- Hypersonic Transport Vehicle with a Planar Boundary Layer with Multiobjective Aeroacoustic Flame Speed Wind Tunnel Advanced Numerical Methods Application to Wind Turbines Deflector Design Problem D. Stephens, NASA Glenn Research Center, D. Luquet, R. Marchiano, F. Coulouvrat, H. Murray, D. Wisda, W. Alexander, M. T. Tatsukawa, T. Nonomura, A. Oyama, K. Cleveland, OH Pierre and Marie Curie University, Paris, Nelson, W. Devenport, Virginia Polytechnic Fujii, Japan Aerospace Exploration Agency France; I. Salah El Din, ONERA, Meudon, Institute and State University, Blacksburg, (JAXA), Kanagawa, Japan France; A. Loseille, French National VA; S. Glegg, Florida Atlantic University, Institute for Research in Computer Science Boca Raton, FL and Control (INRIA), Le Chesnay, France Tuesday, 23 June 2015 115-AA-19 Airframe Noise II Lalique Chaired by: C. DOOLAN, The University of Adelaide 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs AIAA-2015-2686 AIAA-2015-2687 AIAA-2015-2688 AIAA-2015-2689 AIAA-2015-2690 AIAA-2015-2691 AIAA-2015-2692 Aeroacoustic Simulations of Aerodynamic Noise Simulation Wall Pressure Spectra on a Suppression of spurious noise A parametric experimental study Airframe Shielding of Noncompact Assessment of Conceptual Noise a Simplified High-Lift Device of an Airfoil in a Periodically DU96-W-180 Profile From Low to sources in airfoil self-noise of jet-flap interaction noise for a Aviation Noise Sources: Theory and Reduction Devices for A Main Landing Accounting for Installations Effects Fluctuating Freestream Pre-Stall Angles of Attack measurements realistic small-scale swept wing Experiment Gear using SNGR Method P. Salas, S. Moreau, University of Y. Yauwenas, N. Ahmed, University of New A. Suryadi, M. Herr, German Aerospace M. Tuinstra, National Aerospace Laboratory model N. Ostrikov, S. Denisov, TsAGI, Moscow, H. Yao, L. Davidson, Chalmers University of Sherbrooke, Sherbrooke, Canada South Wales, Kensington, Australia Center (DLR), Braunschweig, Germany (NLR), Emmeloord, The Netherlands; I. Belyaev, G. Faranosov, N. Ostrikov, Russia Technology, Göteborg, Sweden; S. Peng, P. Sijtsma, Pieter Sijtsma Advanced TsAGI, Moscow, Russia; G. Paranin, OJS Swedish Defense Research Agency (FOI), AeroAcoustics, Wezep, The Netherlands Irkut Corporation, Moscow, Russia Stockholm, Sweden; F. Capizzano, M. Barbarino, G. Mingione, Italian Aerospace Research Center (CIRA), Capua, Italy Tuesday, 23 June 2015 116-AA-20 Duct Acoustics III Obelisk A Chaired by: C. ROYALTY, Honeywell International, Inc. 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs AIAA-2015-2693 AIAA-2015-2694 AIAA-2015-2695 AIAA-2015-2696 AIAA-2015-2697 Modeling of Broadband Liners Design Optimization of Broadband Effect of Porosity and Joint Bias- Nonlinear impedance modeling Evaluation of Variable-Depth Applied to the Advanced Noise Acoustic Liners Through Finite grazing Flow on the Acoustic Damping of resonator with high intensity Liner Configurations for Increased Control Fan Element Efficacy Studies Performance of Double- and Single- incident acoustic wave Broadband Noise Reduction D. Nark, M. Jones, NASA Langley Research K. Mitchell, Virginia Polytechnic Institute layer Perforated Liners J. Xu, X. Li, Y. Guo, Beihang University, M. Jones, W. Watson, D. Nark, B. Center, Hampton, VA; D. Sutliff, NASA and State University, Blacksburg, VA C. Ji, D. Zhao, S. Li, X. Li, Nanyang Beijing, China Howerton, NASA Langley Research Center, Glenn Research Center, Cleveland, OH Technological University, Singapore, Singapore Hampton, VA Tuesday, 23 June 2015 117-ACD-3 Aircraft Performance Studies Wyeth Chaired by: C. BIL, RMIT University and W. ANEMAAT, DARcorporation 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2015-2698 AIAA-2015-2699 AIAA-2015-2700 AIAA-2015-2701 AIAA-2015-2702 AIAA-2015-2703 The Impact of ATTCS on Reduced- Uncertainty Modeling and Simulated Tiltrotor Aircraft Optimal Climb Trajectories Through Design for Resilience in Adaptive and Intelligent power Thrust Takeoff Field Performance Assessment in Aircraft Evacuation Operation in Close Proximity to a Explicit Simulation Autonomous Systems: Lessons control allocation and scheduling T. Takahashi, Arizona State University, Simulation Building in Wind and Ground-Effect T. Takahashi, Arizona State University, Learned from Controlled Flight into for a More Electric Aircraft Tempe, AZ R. Silva, D. Ferrari, Technological Institute Conditions Tempe, AZ Stall Accidents S. Lazarus, Eaton Corporation, Pune, of Aeronautics (ITA), São José dos L. Young, NASA Ames Research Center, L. Sherry, George Mason University, India; S. Frischemeier, M. Holland, J. Campos, Brazil; L. Santos, Embraer, São Moffett Field, CA Fairfax, VA Skinner, A. Smith, Eaton Corporation, José dos Campos, Brazil Jackson, MS
71 Tuesday, 23 June 2015 118-AFM-7 Flight Test, System Identification, and Parameter Estimation Plum Blossom A Chaired by: J. GRAUER, NASA Langley Research Center and J. BRANDON, NASA-Langley Research Center 1400 hrs 1430 hrs 1500 hrs 1530 hrs AIAA-2015-2704 AIAA-2015-2705 AIAA-2015-2706 AIAA-2015-2707 A New Formulation of the Filter- Unsteady and Post-Stall Model Modeling and Simulation of a Nonlinear Aerodynamic Modeling Error Method for Aerodynamic Identification Using Dynamic Stall Quadrotor using Curve Fitting from Flight Data at High Angles of Parameter Estimation in Turbulence Maneuvers Method Attack Using Neural-Gauss-Newton J. Grauer, E. Morelli, NASA Langley J. Dias, Brazilian Air Force, São José dos D. Kaya, A. Kutay, Middle East Technical Method Research Center, Hampton, VA Campos, Brazil University, Ankara, Turkey R. Kumar, PEC University of Technology, Chandigarh, India; A. Ghosh, Indian Institute of Technology Kanpur, Kanpur, India Tuesday, 23 June 2015 119-AFM-8 Launch Vehicles, Missiles, and Projectile Flight Mechanics Plum Blossom B Chaired by: T. LAVIN, Sandia National Laboratories and F. FRESCONI, US Army Research Lab 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs AIAA-2015-2708 AIAA-2015-2709 AIAA-2015-2710 AIAA-2015-2711 AIAA-2015-2712 Delivery of Modular Lethality via a An Adaptive Parameter Cooperative Flight Dynamics Numerical Aerothermoelastic Reduced-Order Demonstration of Launch Vehicle Parent-Child Concept Guidance Law for Multiple flight Computation of a Sounding Rocket Model of a Hypersonic Vehicle Slosh Instability on a Pole-Cart F. Fresconi, M. Fermen-Coker, Army vehicles Including Elastic Deformation Model R. Klock, C. Cesnik, University of Michigan, Platform Research Laboratory, Aberdeen Proving Z. Enjiao, T. Chao, S. Wang, M. Yang, E. Oliveira, Aeronautics and Space Institute Ann Arbor, Ann Arbor, MI J. Pei, P. Rothhaar, NASA Langley Research Ground, MD Harbin Institute of Technology, Harbin, (IAE), São José dos Campos, Brazil; P. Center, Hampton, VA China Gasbarri, University of Rome “La Sapienza”, Rome, Italy; I. Milagre da Fonseca, Technological Institute of Aeronautics (ITA), São José dos Campos, Brazil Tuesday, 23 June 2015 120-AMT-7/GT-7 Design of Experiment Obelisk B Chaired by: G. GARRARD, Aerospace Testing Alliance (ATA) and D. YODER 1400 hrs 1430 hrs AIAA-2015-2713 Oral Presentation Case Studies for the Statistical Comparison between DOE and Design of Experiments Applied to Traditional 1-Factor at a Time Powered Rotor Wind Tunnel Tests Calibration of a Transonic Wind A. Overmeyer, P. Martin, P. Tanner, S. Tunnel Commo, NASA Langley Research Center, G. Garrard, M. Mills, Arnold Engineering Hampton, VA Development Complex, Tullahoma, TN Tuesday, 23 June 2015 121-AMT-8/FD-14/TP-6/GT-8 Molecular-Based Optical Diagnostics for Hypersonic Nonequilibrium Flows Topaz Chaired by: P. DANEHY, NASA Langley Research Center and M. WINTER, University of Kentucky 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs Oral Presentation Oral Presentation Oral Presentation Oral Presentation Oral Presentation Oral Presentation Oral Presentation Introduction and Application Introduction to Emission Introduction to Absorption Introduction to Molecular Tagging Introduction to Laser Induced Introduction to Raman Rayleigh Introduction to CARS Spectroscopy Considerations for Optical Spectroscopy for Hypersonic Spectroscopy for Hypersonic Velocimetry for Hypersonic Fluorescence Spectroscopy for Spectroscopy for Hypersonic for Hypersonic Nonequilibrium Diagnostics in Hypersonic Nonequilibrium Flows Nonequilibrium Flows Nonequilibrium Flows Hypersonic Nonequilibrium Flows Nonequilibrium Flows Flows Nonequilibrium Flows M. Winter, University of Kentucky, S. O’Byrne, University of New South B. Bathel, NASA Langley Research Center, C. Johansen, University of Calgary, P. Danehy, NASA Langley Research Center, A. Cutler, George Washington University, P. Danehy, NASA Langley Research Center, Lexington, Lexington, KY Wales, Canberra, Australia Hampton, VA Calgary, Canada Hampton, VA Washington, DC Hampton, VA Tuesday, 23 June 2015
72 122-APA-13 Applied CFD & Numerical Correlations with Experimental Data II Stemmons B Chaired by: N. HARIHARAN, CREATE-AV and C. SHENG, University of Toledo 1400 hrs 1430 hrs 1500 hrs 1530 hrs AIAA-2015-2714 AIAA-2015-2715 AIAA-2015-2716 AIAA-2015-2717 CFD Analysis of Counter-Rotating Numerical Simulation of Massively separated turbulent flow Wind Tunnel Wall Interference Open Rotors Using a Rotating Compressible Flow in a Diffusing simulation around non-rotating Effects on an Oscillating Aerofoil in Actuator Disk Model S-duct with and without Vortex MEXICO blade by means of RANS and the Stall Regime M. Malick, R. Agarwal, Washington Generators DDES approaches in OpenFOAM J. Cheng, M. Lowenberg, University of University in St. Louis, St. Louis, MO S. Kamali, B. Reza Ahrabi, R. Webster, Y. Zhang, A. van Zuijlen, G. van Bussel, Bristol, Bristol, United Kingdom; X. Wang, K. Sreenivas, University of Tennessee, Delft University of Technology, Delft, The J. Yu, Nanjing University of Science and Chattanooga, Chattanooga, TN Netherlands Technology, Nanjing, China Tuesday, 23 June 2015 123-APA-14 Special Session: Historically Significant/Influential Papers in Applied Aerodynamics Carpenter Ballroom Chaired by: B. MCGRATH, JHU/Applied Physics Laboratory and J. PINIER, NASA Langley Research Center 1400 hrs 1500 hrs 1600 hrs Oral Presentation Oral Presentation AIAA-2015-2718 Thoughts on working with AMO Smith (Invited) The Spalart-Allmaras Turbulence Model Paper of 1992 (Invited) Origins and Further Development of the Jameson-Schmidt-Turkel R. Liebeck, The Boeing Company, Huntington Beach, CA P. Spalart, The Boeing Company, Seattle, WA; S. Allmaras, Massachusetts Institute of Scheme (Invited) Technology, Cambridge, MA A. Jameson, Stanford University, Stanford, CA Tuesday, 23 June 2015 124-APA-15 Special Session: Aerodynamic-Structural Modeling, Optimization, and Test Techniques for Flexible Wing Technology II Stemmons A Chaired by: W. SILVA, NASA-Langley Research Center and B. STANFORD, NASA Langley Research Center 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2015-2719 AIAA-2015-2720 AIAA-2015-2721 AIAA-2015-2722 AIAA-2015-2723 AIAA-2015-2724 Ongoing Fixed Wing Research Analysis of Limit Cycle Oscillation Computational Aeroelastic Analyses Unsteady Aeroservoelastic Optimization for Load Alleviation Measurement and Modeling of within the NASA Langley Data from the Aeroelastic Test of a Low-Boom Supersonic Modeling of Flexible Wing Generic of Truss-Braced Wing Aircraft Aeroelastic Response under Gust Aeroelasticity Branch of the SUGAR Truss-Braced Wing Configuration Transport Aircraft with Variable With Variable Camber Continuous Y. Babbar, V. Suryakumar, T. Strganac, R. Bartels, P. Chwalowski, C. Funk, J. Model W. Silva, M. Sanetrik, P. Chwalowski, NASA Camber Continuous Trailing Edge Trailing Edge Flap Texas A&M University, College Station, TX; Heeg, J. Hur, M. Sanetrik, NASA Langley R. Bartels, R. Scott, NASA Langley Langley Research Center, Hampton, VA Flap S. Lebofsky, E. Ting, K. Trinh, Stinger A. Mangalam, Tao of Systems Integration, Research Center, Hampton, VA; et al. Research Center, Hampton, VA E. Tal, Delft University of Technology, Delft, Ghaffarian Technologies, Inc., Mountain Inc., Hampton, VA The Netherlands; N. Nguyen, NASA Ames View, CA; N. Nguyen, NASA Ames Research Center, Moffett Field, CA Research Center, Moffett Field, CA Tuesday, 23 June 2015 125-APA-16 Flow Control Applications & Demonstrations (Active & Passive) II Stemmons C Chaired by: M. OL, US Air Force Reseach Laboratory and G. ZHA, University of Miami 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2015-2725 AIAA-2015-2726 AIAA-2015-2727 AIAA-2015-2728 AIAA-2015-2729 AIAA-2015-2730 Simulation and Surrogate-Based Multipoint Design of Vortex Flow Control in a Mach 4.0 Inlet Wind Tunnel Experiments with Active Passive Flow Control Applied to a Computations of Active Open-Loop Design of Rectangular Vortex Generators on a Swept Infinite- by Slotted Wedge-shaped Vortex Flow Control for an Outer Wing Model NACA23012 Airfoil In A Subsonic Flow Control on a Fluttering Wing Generators for Tiltrotor Aircraft Wing under Cruise and Critical Generators V. Ciobaca, J. Wild, German Aerospace Center Flow J. Seidel, C. Fagley, T. McLaughlin, U.S. Wings Condition D. Varma, S. Saurav, S. Ghosh, Indian (DLR), Braunschweig, Germany; M. Bauer, T. N. Findanis, University of New South Air Force Academy, Colorado Springs, CO R. Bevan, D. Poole, C. Allen, T. Rendall, N. Namura, K. Shimoyama, S. Obayashi, Institute of Technology Madras, Chennai, Grund, Technical University of Berlin, Berlin, Wales, Sydney, Australia University of Bristol, Bristol, United Tohoku University, Sendai, Japan India Germany; C. Huehne, P. Scholz, Technical
73 Kingdom University of Braunschweig, Braunschweig, Germany; et al. Tuesday, 23 June 2015 126-ATIO-12 ATM II - Air Traffic Analysis Milan Chaired by: A. RAO, Purdue University 1400 hrs 1430 hrs 1500 hrs AIAA-2015-2731 AIAA-2015-2732 AIAA-2015-2733 A Wavelet Analysis Approach for Application of Data Mining in Air Identification of Aircraft Conflict Categorizing Air Traffic Behavior Traffic Forecasting ResolutionTypes from Recorded M. Drew, University of California, Santa J. Busquets, City University London, Flight Data Cruz, Moffett Field, CA; K. Sheth, NASA London, United Kingdom; A. Evans, S. Shin, K. Kim, I. Hwang, Purdue Ames Research Center, Moffett Field, CA University College London, London, University, West Lafayette, IN United Kingdom; E. Alonso, City University London, London, United Kingdom Tuesday, 23 June 2015 127-ATIO-13 Transformational Flight - Advanced Concepts Metropolitan Ballroom Chaired by: N. BORER, NASA Langley Research Center 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs Oral Presentation Oral Presentation Oral Presentation Oral Presentation Oral Presentation AIAA-2015-2734 AIAA-2015-2735 NASA GL-10 Tilt-Wing Tilt-Tail LEAPTech Distributed Electric Comparison of Computational The Samson Switchblade Multi- Hoverless VTOL Hyper Commuter Predicting the Aero Loads Behind a Centrifugally Stiffened Rotor: A Concept Propulsion Integration Concept Aerodynamics Tools for Predicting Mode Aircraft Concept Mission Concept Propeller in the Presence of a Wing Complete Derivation of the Plant W. Fredericks, NASA Langley Research M. Moore, NASA Langley Research Center, Low-Speed Performance of a S. Bousfield, Samson Aircraft, Auburn, CA M. Moore, NASA Langley Research Center, Using Flightstream Model with Nonlinear Dynamics Center, Hampton, VA Hampton, VA Distributed Propeller Concept Hampton, VA V. Ahuja, R. Hartfield, Flightstream, J. Selfridge, G. Tao, University of Virginia, M. Patterson, N. Borer, NASA Langley Auburn, AL Charlottesville, Charlottesville, VA Research Center, Hampton, VA; B. German, Georgia Institute of Technology, Atlanta, GA Tuesday, 23 June 2015 128-ATIO-14 Product Design and Support Manchester Chaired by: A. CHAPUT, University of Texas at Austin 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs AIAA-2015-2736 AIAA-2015-2737 AIAA-2015-2738 AIAA-2015-2739 AIAA-2015-2740 AIAA-2015-2741 AIAA-2015-2742 Value Driven Conceptual Design of Monte Carlo based Robust MDO Development and Application of a 3D Printed Parts for Quick UGV and UAV Cooperation for Toward Efficient Model-Based Reliability Analysis of the Unmanned Air System for Defense applied to Aircraft Conceptual Parametric Design Tool for Design Turnaround Aircraft Projects and Constructing Probabilistic Threat Development of Aerospace Integrated Modular Avionics Applications Design: a technical-financial Iterations of Large Turboprop Legacy Issues Exposure Map (PTEM) Applications System Using AADL and GSPN E. Papageorgio, M. Eres, J. Scanlan, coupling optimization strategy Aircraft U. Rehmanjan, Qantas Airways, Ltd., O. Daskiran, H. Sevil, A. Dogan, B. Huff, I. Amundson, L. Shipton, A. Liu, M. P. Wang, F. Yan, R. Liu, C. Zhao, Z. Ma, Civil University of Southampton, Southampton, D. Bianchi, T. Orra, Embraer, São José dos M. Kügler, N. Randt, Technical University Sydney, Australia University of Texas, Arlington, Arlington, TX Nowak, Eaton Corporation, Cleveland, OH Aviation University of China, Tianjin, China United Kingdom Campos, Brazil; P. Paglione, Technological of Munich, Munich, Germany Institute of Aeronautics (ITA), São José dos Campos, Brazil Tuesday, 23 June 2015 129-CASE-5 CASE Session I & II Steuben 1400 - 1730 hrs 1400-1530 hrs Concept Development of Complex Systems This 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 and Mat French, Electrical Systems Engineer, Rolls-Royce Corporation Panelists: Rick Mange Robert (Rob) Simons Jason Merret F-35 PNR Program Manager Technical Fellow Technical Specialist, Gulfstream Aerospace Performance Engineering
74 Lockheed Martin Aeronautics The Boeing Company Gulfstream Aerospace Corporation
1545-1730 hrs Product Design for Complex Systems Across the Supply Chain This 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 and Carmen Schooley, Manager, Systems Engineering and Integration, Gulfstream Aerospace Corporation Panelists: Fernando Dones Bernard Dion Brenda Nuhfer Technical Fellow CTO Program Manager The Boeing Company ANSYS UTC/Pratt & Whitney
Tuesday, 23 June 2015 130-CFD-13 Flux Reconstruction Methods Grand Ballroom A Chaired by: Z. WANG, University of Kansas and B. VERMEIRE, McGill University 1400 hrs 1430 hrs 1500 hrs 1530 hrs AIAA-2015-2743 AIAA-2015-2744 AIAA-2015-2745 AIAA-2015-2746 On the Utility of High-Order De-Aliasing through Over- Fully-conservative High-order FR A WENO-type Limiter for 4th Methods for Unstructured Grids: Integration Applied to the Flux Scheme on Moving and Deforming Order Constrained Derivative Flux A Comparison Between PyFR and Reconstruction and Discontinuous Grids Reconstruction Method Industry Standard Tools Galerkin Methods Y. Abe, University of Tokyo, Sagamihara, Z. Sun, F. Xiao, Tokyo Institute of B. Vermeire, F. Witherden, P. Vincent, S. Spiegel, H. Huynh, J. DeBonis, NASA Japan; T. Haga, T. Nonomura, K. Fujii, Technology, Yokohama, Japan Imperial College London, London, United Glenn Research Center, Cleveland, OH Japan Aerospace Exploration Agency Kingdom (JAXA), Sagamihara, Japan Tuesday, 23 June 2015 131-CFD-14 Adjoints and Error Estimation Grand Ballroom B Chaired by: C. ROY, Virginia Tech and C. OLLIVIER GOOCH, University of British Columbia 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs AIAA-2015-2747 AIAA-2015-2748 AIAA-2015-2749 AIAA-2015-2750 AIAA-2015-2751 Accuracy of Discretization Error Comparison of Truncation Error Stabilisation of Discrete Adjoint Fixed point discrete adjoint of Convergence Acceleration Using Estimation by the Error Transport Estimators for Defect Correction Solvers for Incompressible Flow SIMPLE-like solvers Convergence Error Estimation Equation on Unstructured Meshes - and Output Error Estimation in the Y. Wang, S. Akbarzadeh, J. Mueller, S. Akbarzadeh, Y. Wang, J. Mueller, S. Eyi, Middle East Technical University, Nonlinear Systems of Equations Unstructured Mesh Finite Volume Queen Mary University of London, London, Queen Mary University of London, London, Ankara, Turkey G. Yan, C. Ollivier Gooch, University of Method United Kingdom United Kingdom British Columbia, Vancouver, Canada M. Sharbatdar, C. Ollivier Gooch, University of British Columbia, Vancouver, Canada Tuesday, 23 June 2015 132-CFD-15 Time Integration Methods Coral Chaired by: X. WANG, Air Force Research Laboratory, Wright-Patterson AFB and J. NORDSTROM, Linköping University 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2015-2752 AIAA-2015-2753 AIAA-2015-2754 AIAA-2015-2755 AIAA-2015-2756 AIAA-2015-2757 Optimal Runge-Kutta Schemes for Application of Dual Time Stepping Assessment of time implicit A Mapped Chebyshev Unsteady Solutions of Non-Linear Investigation of Efficient High- High-order Spatial and Temporal to Fully Implicit Runge Kutta discretizations for the computation Pseudospectral Method for Differential Equations Using Walsh Order Implicit Runge-Kutta Discretizations Schemes for Unsteady Flow of turbulent compressible flows Unsteady Flow Analysis Function Series Methods Based on Generalized N. Mundis, ERC, Inc., Edwards AFB, CA; A. Calculations P. Cinnella, Università del Salento, D. Im, S. Choi, J. McClure, J. Choi, F. P. Gnoffo, NASA Langley Research Center, Summation-by-Parts Operators Edoh, University of California, Los Angeles, A. Jameson, Stanford University, Stanford, Lecce, Italy; C. Cedric, Paris Institute of Skies, Virginia Polytechnic Institute and Hampton, VA P. Boom, D. Zingg, University of Toronto, Los Angeles, CA; V. Sankaran, Air Force CA Technology, Paris, France State University, Blacksburg, VA Toronto, Canada Research Laboratory, Edwards AFB, CA 75 Tuesday, 23 June 2015 133-CFD-16 RANS Modeling Emerald Chaired by: P. HARTWICH, Boeing Research & Technology and J. CARLSON, Computational Aerosciences Branch 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2015-2758 AIAA-2015-2759 AIAA-2015-2760 AIAA-2015-2761 AIAA-2015-2762 AIAA-2015-2763 Node-Centered Wall Function Analysis of a low Reynolds Extension of the SU2 open source CFD Turbulent Flow Simulations Recent Improvement of a Proper orthogonal decomposition Models for the Unstructured FLow differential Reynolds stress model code to the simulation of turbulent on Unstructured Grids using a Correlation-Based Transition closure models for Burgers and Code Fun3D in homogeneous shear flow with flows of fuids modelled with complex Reynolds Stress Models Turbulence Model for Simulating Navier-Stokes Equations J. Carlson, V. Vatsa, J. White, NASA respect to numerical stability thermophysical laws Y. Mor-Yossef, Israeli CFD Center, Caesarea Three-Dimensional Boundary H. Imtiaz, I. Akhtar, M. Saif Ullah Khalid, Langley Research Center, Hampton, VA C. Morsbach, German Aerospace Center S. Vitale, Delft University of Technology, Delft, Industrial Park, Israel Layers National University of Sciences and (DLR), Cologne, Germany The Netherlands; G. Gori, Technical University J. Choi, O. Kwon, Korea Advanced Institute Technology, Rawalpindi, Pakistan of Milan, Milan, Italy; M. Pini, Delft University of Science and Technology, Daejeon, of Technology, Delft, The Netherlands; A. South Korea Guardone, Technical University of Milan, Milan, Italy; T. Economon, F. Palacios, Stanford University, Palo Alto, CA; et al. Tuesday, 23 June 2015 134-CFD-37 CFD Flow Visualization Showcase Chantilly Ballroom Foyer 1400 - 1600 hrs The 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, 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. Tuesday, 23 June 2015 135-F360-4 International UAS Integration Forum Grand Ballroom E 1400 - 1630 hrs Moderator: Rob Hughes, Northrop Grumman, Inc. Panelists: Cees Bil Chuck Johnson Marty Rogers Marshall Jackson Randy Willis Dale Richards Associate Professor, School of Aerospace, Vice President of Operations University of Alaska-Fairbanks Project Manager - Aviation Safety Audits FAA, Co-Chair of ICAO RPAS Senior Research Fellow, Human Factors Mechanical and Manufacturing Engineering The Padina Group Office of Inspector General (Remotely Piloted Aircraft Systems) Faculty of Engineering & Computing RMIT University U.S. Department of Transportation Coventry University, United Kingdom
Tuesday, 23 June 2015 136-FD-15 Unsteady Wing Aerodynamics II Govenors Lecture Hall Chaired by: K. TAIRA, Florida State University and B. JOLLY, US Air Force 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs AIAA-2015-2764 AIAA-2015-2765 AIAA-2015-2766 AIAA-2015-2767 AIAA-2015-2768 AIAA-2015-2769 AIAA-2015-2770 Aeromechanics of Membrane Wings The Influence of Streamline Effect of Turbulence Modeling on A Data-Driven Modeling Framework Nonlinear Characterization of Flow Intermittency Behaviour in the Analysis of Deflected Vortex Street in Ground-Effect Curvature on Low Aspect Ratio Hovering Rotor Flows for Predicting Forces and Pressures on over Oscillating Elliptic Airfoils Flow Past an Oscillating Airfoil Produced by an Oscillating Airfoil R. Bleischwitz, R. De Kat, B. Rotating Wings S. Yoon, N. Chaderjian, T. Pulliam, T. a Rapidly Pitching Airfoil M. Khalid, I. Akhtar, National University of S. Badrinath, S. Sarkar, Indian Institute of S. Badrinath, S. Sarkar, Indian Institute of Ganapathisubramani, University of C. Kroninger, A. Harrington, M. Munson, Holst, NASA Ames Research Center, S. Dawson, N. Schiavone, C. Rowley, Sciences and Technology, Islamabad, Pakistan; Technology Madras, Chennai, India Technology Madras, Chennai, India Southampton, Southampton, United Army Research Laboratory, Aberdeen Moffett Field, CA Princeton University, Princeton, NJ; D. H. Dong, University of Virginia, Charlottesville, Kingdom Proving Ground, MD Williams, Illinois Institute of Technology, Charlottesville, VA; N. Ahsan, Institute of Space Chicago, IL Technology, Islamabad, Pakistan Tuesday, 23 June 2015
76 137-FD-16 Boundary Layer Transition: Crossflow Sapphire Chaired by: M. BORG, Air Force Research Laboratory and T. JULIANO, University of Notre Dame 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2015-2771 AIAA-2015-2772 AIAA-2015-2773 AIAA-2015-2774 AIAA-2015-2775 AIAA-2015-2776 Direct Numerical Simulation EPIC: NPSE Analysis of Hypersonic Secondary Instability of Stationary Experimental study of crossflow Computational Investigation of Step The Effect of Backward-facing Step of Transition due to Traveling Crossflow Instability on Yawed Crossflow Vortices on an Inclined instability on a Mach 6 yawed cone Excrescence Sensitivity in a Swept- Height on Instability Growth and Crossflow Vortices Straight Circular Cone Cone at Mach 6 S. Craig, W. Saric, Texas A&M University, Wing Boundary Layer Breakdown in Swept-Wing Boundary- F. Li, M. Choudhari, NASA Langley N. Oliviero, T. Kocian, A. Moyes, H. Reed, C. Ward, R. Henderson, S. Schneider, College Station, TX M. Tufts, H. Reed, B. Crawford, G. Duncan, Layer Transition Research Center, Hampton, VA; L. Duan, Texas A&M University, College Station, TX Purdue University, West Lafayette, IN W. Saric, Texas A&M University, College J. Eppink, NASA Langley Research Center, Missouri University of Science and Station, TX Hampton, VA; R. Wlezien, Iowa State Technology, Rolla, MO University, Ames, IA; R. King, M. Choudhari, NASA Langley Research Center, Hampton, VA Tuesday, 23 June 2015 138-FD-17 Boundary Layer and Bluff Body Control Senators Lecture Hall Chaired by: Z. ZHANG, University of Tennessee and J. LIN, NASA-Langley Research Center 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs AIAA-2015-2777 AIAA-2015-2778 AIAA-2015-2779 AIAA-2015-2780 AIAA-2015-2781 Control of Afterbody Vortices by Simplified model for flow-heating The effects of Mach and Reynolds Experimental investigation of Control of Shock Wave Boundary Blowing effect on wave drag of blunt bodies number on the flow mixing properties boundary layer tripping devices Layer Interaction using Laser Pulse R. Jackson, Z. Wang, I. Gursul, University and its validation of micro-ramp vortex generators in a for shock wave - boundary layer Energy Depositions of Bath, Bath, United Kingdom E. Schülein, German Aerospace Center supersonic boundary layer control A. Iwakawa, T. Tamba, P. Son, T. Shoda, (DLR), Göttingen, Germany R. Giepman, A. Srivastava, F. Schrijer, B. van R. Giepman, R. Louman, F. Schrijer, B. A. Sasoh, Nagoya University, Nagoya, Oudheusden, Delft University of Technology, van Oudheusden, Delft University of Japan Delft, The Netherlands Technology, Delft, The Netherlands Tuesday, 23 June 2015 139-FD-18 Turbulence Modeling Edelweiss Chaired by: C. RUMSEY, NASA-Langley Research Center and G. BLAISDELL, Purdue University 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs AIAA-2015-2782 AIAA-2015-2783 AIAA-2015-2784 AIAA-2015-2785 AIAA-2015-2786 Stretched-Vortex based Subgrid- DNS/LES Simulations of Separated Bayesian Calibration of a RANS Extension of Wray-Agarwal An Improved Version of One- scale Modeling of Variable-Density Flows at High Reynolds Numbers Model with a Complex Response Turbulence Model for Flow Over Equation RAS Turbulence Model Flows P. Balakumar, NASA Langley Research Surface - A Case Study with Jet-in- Rough Surfaces M. Rahman, Aalto University, Helsinki, G. Sidharth, G. Candler, University of Center, Hampton, VA; G. Park, Stanford Crossflow Configuration T. Wray, R. Agarwal, Washington Finland; R. Agarwal, Washington Minnesota, Minneapolis, Minneapolis, University, Palo Alto, CA J. Ray, S. Lefantzi, Sandia National University in St. Louis, St. Louis, MO University in St. Louis, St. Louis, MO; M. MN; P. Dimotakis, California Institute of Laboratories, Livermore, CA; S. Lampinen, T. Siikonen, Aalto University, Technology, Pasadena, CA Arunajatesan, L. DeChant, Sandia National Helsinki, Finland Laboratories, Albuquerque, NM Tuesday, 23 June 2015 140-ITAR-2 ITAR - Aircraft Design and Modeling Morocco Chaired by: K. CASPER 1400 hrs 1430 hrs AIAA-2015-2787 AIAA-2015-2788 Development and Testing of a Solar Airfield Lifting Loads a CFD/Full Powered Aircraft Scale Rotary Wing Test Study J. Jacob, Oklahoma State University, F. Zajaczkowski, J. Tarter, T. Bagwell, Stillwater, OK; J. Grimsley, S. Atkins, Applied Research Laboratory, State Design Intelligence, Inc., Norman, OK College, PA Tuesday, 23 June 2015 77 141-MAO-4 Applications II Madrid Chaired by: R. KHIRE, United Technologies Research Center and E. WINER, Iowa State University 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs AIAA-2015-2789 AIAA-2015-2790 AIAA-2015-2791 AIAA-2015-2792 AIAA-2015-2793 Design Space Exploration of Wingbox High-Fidelity Aerostructural Aeroelastic Tailoring Study of Optimal Mission Path for the Multidisciplinary Analysis of a Substructures Configuration Using Otimization Considering Buffet an N+2 Low-boom Supersonic Uninhabited Loyal Wingman Box-Wing Aircraft Designed for a SPANDSET Onset Commercial Transport Aircraft C. Humphreys, R. Cobb, D. Jacques, J. Regional-Jet Mission C. Potter, Georgia Institute of Technology, G. Kenway, J. Martins, University of C. Pak, NASA Armstrong Flight Research Reeger, Air Force Institute of Technology, S. Andrews, R. Perez, Royal Military Atlanta, GA; S. Russell, Triumph Aerostructures, Michigan, Ann Arbor, Ann Arbor, MI Center, Edwards, CA Wright-Patterson AFB, OH College of Canada, Kingston, Canada Dallas, TX; V. Kim, Z. Liu, D. Mavris, Georgia Institute of Technology, Atlanta, GA Tuesday, 23 June 2015 142-MST-6 Shadow Mode Assessment using Realistic Technologies for National Airspace System (SMART NAS) Test Bed Development (Invited) Travertine Chaired by: K. PALOPO, NASA Ames Research Center and G. CHATTERJI, NASA Ames Research Center 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs AIAA-2015-2794 AIAA-2015-2795 AIAA-2015-2796 AIAA-2015-2797 AIAA-2015-2798 AIAA-2015-2799 AIAA-2015-2800 Shadow Mode Assessment using Design Challenges for a Shadow Platform As A Service (PAAS) Architecture Development for A Data Exchange and Parallel Simulation of Agent-Based An Integrated Framework for Realistic Technologies for the National Mode Assessment Tool for Air Architecture for NASA’s SMART NAS Shadow Mode Assessments of Air Transformation System for SMART Model for Air Traffic Network Modeling Air Carrier Behavior, Airspace System (SMART NAS) Traffic Management (Invited) (Invited) Traffic Management Technologies NAS (Invited) Y. Kim, O. Pinon-Fischer, D. Mavris, Policy, and Impacts in the U.S. Air Test Bed Development (Invited) R. Hoffman, Metron Aviation, Inc., Dulles, P. Cobb, M. Blake, Crown Consulting, Inc., (Invited) P. Cobb, Crown Consulting, Inc., Arlington, Georgia Institute of Technology, Atlanta, Transportation System K. Palopo, NASA Ames Research Center, VA; J. Krozel, Innovation Laboratory, Inc., Arlington, VA P. Kostiuk, Robust Analytics, Gambrills, MD VA; M. Garland, Mosaic ATM, Leesburg, VA GA B. Horio, V. Kumar, V. Stouffer, S. Hasan, Moffett Field, CA; G. Chatterji, University of Portland, OR; D. Miller, J. Smith, Metron A. DeCicco, LMI, Tysons Corner, VA; J. California, Santa Cruz, Moffett Field, CA; M. Aviation, Inc., Dulles, VA Smith, NASA Langley Research Center, Guminsky, P. Glaab, NASA Langley Research Hampton, VA; et al. Center, Hampton, VA Tuesday, 23 June 2015 143-PDL-6 Plasma Diagnostics I Miro Chaired by: C. DUMITRACHE, Colorado State University 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs AIAA-2015-2801 AIAA-2015-2802 AIAA-2015-2803 AIAA-2015-2804 AIAA-2015-2805 Composition-Independent Computational and Experimental Understanding the Impact of Wavefront Measurements of a Langmuir Probe Diagnostics of an Temperature and Pressure Laser Differential Interferometry Buffer Gases on the Radar REMPI Supersonic Boundary Layer Using a Atmospheric-Pressure Microplasma Measurements using Lineshape for Supersonic Turbulent Boundary- Diagnostic Laser-Induced Breakdown Spark L. Blair, K. Xu, University of Alabama, Scaling Information from Kr PLIF Layer Flow T. Chng, R. Miles, Princeton University, M. Nguyen, M. Rennie, S. Gordeyev, E. Huntsville, Huntsville, AL D. Zelenak, F. Kidd, V. Narayanaswamy, N. Bisek, M. Brown, Air Force Research Princeton, NJ Jumper, University of Notre Dame, Notre North Carolina State University, Raleigh, Laboratory, Wright-Patterson AFB, OH Dame, IN; A. Cain, Innovative Technology NC Applications Company, LLC, Chesterfield, MO; T. Hayden, U.S. Air Force Academy, Colorado Springs, CO Tuesday, 23 June 2015 144-PDL-7 Plasma Aerodynamics & Flow Control III Monet Ballroom Chaired by: T. MOELLER, University of Tennessee Space Institute 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs AIAA-2015-2806 AIAA-2015-2807 AIAA-2015-2808 AIAA-2015-2809 AIAA-2015-2810 Investigation of Cathodic-Arc-Jet Dynamics of Charge Transfer in Effect of New Electron Impact Numerical Study on Performance Effect of Voltage and Frequency Influence on Cross Flow using Atmospheric Pressure Barrier Ionization on the Aerodynamic Improvement Mechanism of Tri- on Starting Repetitive Nanosecond Particle Image Velocimetry Discharge at Single and Alternative Heating Environment for Super-Orbital Electrode Plasma Actuator Pulsed DBD I. Kronhaus, Technion--Israel Institute of Polarities of Supplying Voltage Reentry Vehicles H. Nishida, M. Tamura, Tokyo University X. Han, H. Li, X. Meng, Northwestern Technology, Haifa, Israel S. Leonov, University of Notre Dame, H. Otsu, Ryukoku University, Otsu, Japan; K. of Agriculture and Technology, Koganei, Polytechnical University, Xi’an, China; F.
78 Notre Dame, IN Yamada, T. Abe, Japan Aerospace Exploration Japan; T. Matsuno, Tottori University, Liu, S. Luo, University of California, Irvine, Agency (JAXA), Sagamihara, Japan Tottori, Japan Los Angeles, CA Tuesday, 23 June 2015 145-TP-7 Heat Transfer II Rosetta Chaired by: E. SHORT, Raytheon Company and E. KHALIL, Cairo University 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs AIAA-2015-2811 AIAA-2015-2812 AIAA-2015-2813 AIAA-2015-2814 AIAA-2015-2815 AIAA-2015-2816 AIAA-2015-2817 Response of porous foams filled Evaluation of different Turbulence Benchmarking of Computational Numerical Analysis of Film Cooling POD Analysis of the Transient Fluid flow and heat transfer in a Numerical and experimental with phase change material under Models for analysis of Jet Models For Adiabatic Film-Cooling Characteristic on a Turbine Non- Flow Field at Pulse Engine Exhaust rotating two-pass square channel analysis of heat transfer of piccolo transient heating Impingement in Gas Turbine Blades Effectiveness For Large Spacing axisymmetric Contoured Endwall Region with smooth walls and axial tube jet impingement on a concave G. Jackson, K. Smith, P. Mccarthy, T. Fisher, B. Upalkar, M. Ricklick, Embry-Riddle Compound Angle Full Coverage Q. Pan, H. Tang, J. Bai, Aviation Industry W. Cai, C. Yang, B. Qi, H. Ma, L. Yu, X. inward/outward flow surface Purdue University, West Lafayette, IN Aeronautical University, Daytona Beach, FL Film Cooling Arrays Corporation of China (AVIC), Shanghai, Chen, Nanjing University of Science and J. Bai, Q. Pan, Aviation Industry Corporation of Y. Bo, S. Chang, Y. Zhao, M. Leng, S. Martinez, M. Ricklick, Embry-Riddle China Technology, Nanjing, China China (AVIC), Shanghai, China Beihang University, Beijing, China Aeronautical University, Daytona Beach, FL Tuesday, 23 June 2015 146-NW-4 Networking Coffee Break Chantilly Ballroom East 1530 - 1600 hrs Tuesday, 23 June 2015 147-LEC-2 Plasmadynamics and Lasers Award Lecture Grand Ballroom D 1630 - 1730 hrs
From Plasmadynamics and Shock Tubes to Aero-Optics and Laser Radar: An Aerospace Career Philip E. Cassady Senior Technical Fellow (Retired) The Boeing Company Tuesday, 23 June 2015 148-NW-5 Reception in the Exposition Hall Chantilly Ballroom East 1730 - 1900 hrs A ticket is required and included in the conference registration fee where indicated. Wednesday Wednesday, 24 June 2015 149-SB-3 Speakers’ Briefing Session Rooms 0730 - 0800 hrs Wednesday, 24 June 2015 150-PLNRY-3 Plenary Keynote Chantilly Ballroom West 0800 - 0900 hrs
NASA and the Future of Aerospace Charles F. Bolden Jr. Administrator National Aeronautics and Space Administration Wednesday, 24 June 2015 151-AA-21 Turbomachinery and Core Noise Fleur-de-lis B Chaired by: H. ATASSI, University of Notre Dame 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2015-2818 AIAA-2015-2819 AIAA-2015-2820 AIAA-2015-2821 AIAA-2015-2822 AIAA-2015-2823 AIAA-2015-2824 79 Entropy Noise Generation and Dynamic Temperature and Pressure Broadband indirect noise Linear Analysis of Engine Core Acoustic Comparison of Different Acoustic Comparison of Different Experimental Study on the Reduction in a Heated Nozzle Flow Measurements in the Core of a generation by accelerated vorticity Noise Using a Hybrid Modeling Turbine Exit Guide Vane Designs Turbine Exit Guide Vane Designs Turbomachinery Trailing Edge Noise K. Knobloch, T. Werner, F. Bake, German Propulsion Engine N. Kings, L. Enghardt, F. Bake, German Approach - Part 1: Design Philosophy and Part 2: Experimental Analysis Reduction Based on Linear Cascade Aerospace Center (DLR), Berlin, Germany W. Schuster, Honeywell International, Aerospace Center (DLR), Berlin, Germany J. O’Brien, J. Kim, M. Ihme, Stanford Numerical Predictions A. Marn, T. Selic, F. Schönleitner, S. Test with Phased Array Inc., Phoenix, AZ; L. Hultgren, NASA Glenn University, Stanford, CA D. Broszat, M. Höger, MTU Aero Engines, Zerobin, Graz University of Technology, W. Qiao, L. Wang, W. Chen, F. Tong, L. Research Center, Cleveland, OH Munich, Germany; A. Marn, T. Selic, F. Graz, Austria; D. Broszat, M. Höger, MTU Ji, Northwestern Polytechnical University, Schönleitner, F. Heitmeir, Graz University Aero Engines, Munich, Germany; et al. Xi’an, China of Technology, Graz, Austria Wednesday, 24 June 2015 152-AA-22 General Acoustics II Inverness Chaired by: S. RIZZI, NASA Langley Research Center 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2015-2825 AIAA-2015-2826 AIAA-2015-2827 AIAA-2015-2828 AIAA-2015-2829 AIAA-2015-2830 AIAA-2015-2831 On a mode-matching technique for Noise control by a rotating rod in a Acoustic effects of a rotationally Active Control of Fan Tones by Acoustic Resonance Phenomena Aerofoil geometry effects on Wall-Mounted Finite Airfoil Noise sound generation and transmission in rod-airfoil configuration oscillating rod in a rod-airfoil means of Trailing Edge Blowing in a Three-Dimensional Cascade turbulence interaction noise Production and Prediction a linear cascade of outlet guide vanes L. Siozos-Rousoulis, G. Ghorbaniasl, C. configuration L. Enghardt, P. Kausche, A. Moreau, Interacting with Oncoming C. Paruchuri, J. Gill, N. Subramanian, D. Moreau, C. Doolan, University of S. Bouley, B. François, M. Roger, École Lacor, Vrije Universiteit Brussel, Brussels, L. Siozos-Rousoulis, G. Ghorbaniasl, C. German Aerospace Center (DLR), Berlin, Unsteady Wakes P. Joseph, C. Vanderwel, X. Zhang, New South Wales, Sydney, Australia; Centrale de Lyon, Ecully, France; S. Moreau, Belgium Lacor, Vrije Universiteit Brussel, Brussels, Germany; T. Carolus, University of Siegen, H. Kodama, IHI Corporation, Nishitama, University of Southampton, Southampton, W. Alexander, T. Meyers, W. Devenport, University of Sherbrooke, Sherbrooke, Canada Belgium Siegen, Germany Japan; M. Namba, Kyusyu University, United Kingdom; et al. Virginia Polytechnic Institute and State Fukuoka, Japan University, Blacksburg, VA Wednesday, 24 June 2015 153-AA-23 Jet Noise Near Field and Jet Noise Reduction Lalique Chaired by: A. PILON, Lockheed Martin Aeronautics 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2015-2832 AIAA-2015-2833 AIAA-2015-2834 AIAA-2015-2835 AIAA-2015-2836 AIAA-2015-2837 AIAA-2015-2838 On Theoretical Broadband Shock- Near-field Pressure Waveform Measuring shear layer growth Impact of Chevrons on Noise Effect of Inverted Triangular Tabs An Investigation of Twin Supersonic Acoustic source analysis of a Associated Noise Near-Field Cross- Analysis of an Excited Mach 0.9 Jet rates in aeroacoustically forced Source Characteristics In on Mitigation of Jet Noise from Jets’ Near-field supersonic rectangular chevron jet Spectra C. Kuo, M. Crawley, M. Samimy, Ohio axisymmetric supersonic jets Imperfectly Expanded Jet Flows Axisymmetric Convergent Nozzles J. Cluts, C. Kuo, M. Samimy, Ohio State J. Kreitzman, J. Nichols, University of S. Miller, NASA Langley Research Center, State University, Columbus, OH D. Edgington-Mitchell, O. Amili, D. J. Liu, A. Corrigan, K. Kailasanath, Naval A. Subramanyam, K. Natarajan, National University, Columbus, OH Minnesota, Minneapolis, Minneapolis, MN Hampton, VA Honnery, J. Soria, Monash University, Research Laboratory, Washington, DC; Aerospace Laboratories, Bangalore, India Melbourne, Australia E. Gutmark, University of Cincinnati, Cincinnati, OH Wednesday, 24 June 2015 154-AA-24 CAA Propagation and Scattering II Obelisk A Chaired by: M. ROGER, Ecole Centrale de Lyon 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2015-2839 AIAA-2015-2840 AIAA-2015-2841 AIAA-2015-2842 AIAA-2015-2843 CAA analysis of a Wing Section with Prediction of Far-Field Wind Turbine Numerical simulation of spectral Comparison of Computational Numerical and Analytical Flap Side-Edges Based on Hybrid Noise Propagation with Parabolic broadening of an acoustic wave Aeroacoustics Prediction of Vortical Investigation of Orthogonal Blade/ RANS-LES Computation Equation by a spatially growing turbulent Gust Scattering by a 2D Stator with Vortex Interaction Noise S. Peng, L. Tysell, Swedish Defense Research S. Lee, General Electric Company, mixing layer Flat Plate Theory F. Falissard, P. Zehner, ONERA, Châtillon, Agency (FOI), Stockholm, Sweden; H. Yao, L. Niskayuna, NY I. Bennaceur, D. Mincu, I. Mary, M. C. Durand, D. Hixon, University of Toledo, France; M. Roger, École Centrale de Lyon, Davidson, L. Eriksson, Chalmers University of Terracol, ONERA, Châtillon, France; L. Toledo, OH Ecully, France; X. Gloerfelt, Arts Metiers Technology, Göteborg, Sweden Larcheveque, D. Pierre, Aix-Marseille ParisTech, Paris, France
80 University, Marseille, France Wednesday, 24 June 2015 155-AA-25 Benchmark Problems for Airframe Noise Computations III (BANC-III) Summary (Invited) Fleur-de-lis A Chaired by: M. CHOUDHARI, NASA-Langley Research Center 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs Oral Presentation AIAA-2015-2844 AIAA-2015-2845 AIAA-2015-2846 AIAA-2015-2847 An Overview of Contributions on Assessment of Slat Noise Variability in the Propagation Phase of Summary of the LAGOON Solutions Broadband Trailing-Edge Noise Nose Landing Gear Configuration Predictions for 30P30N High-Lift CFD-Based Noise Prediction: Summary from the Benchmark problems for Predictions—Overview of BANC-III for BANC-III Workshop Configuration from BANC-III of Results from Category 8 of the Airframe Noise Computations-III Results M. Khorrami, NASA Langley Research Workshop BANC-III Workshop Workshop M. Herr, R. Ewert, C. Rautmann, German Center, Hampton, VA M. Choudhari, D. Lockard, NASA Langley L. Lopes, NASA Langley Research Center, E. Manoha, ONERA, Châtillon, France; B. Aerospace Center (DLR), Braunschweig, Research Center, Hampton, VA Hampton, VA; S. Redonnet, ONERA, Toulouse, Caruelle, Airbus, Toulouse, France Germany; M. Kamruzzaman, ENERCON France; T. Imamura, University of Tokyo, GmbH, Aurich, Germany; D. Bekiropoulos, Tokyo, Japan; T. Ikeda, Japan Aerospace University of Stuttgart, Stuttgart, Exploration Agency (JAXA), Chofu, Japan; Germany; R. Arina, Technical University of N. Zawodny, NASA Langley Research Center, Turin, Torino, Italy; et al. Hampton, VA; G. Cunha, ONERA, Toulouse, France Wednesday, 24 June 2015 156-ACD-4 General Aviation Morocco Chaired by: M. ORR, Boeing Commercial Airplanes 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2015-2848 AIAA-2015-2849 AIAA-2015-2850 AIAA-2015-2851 AIAA-2015-2852 AIAA-2015-2853 Identifying High-Risk Occurrence Pilot Perception and Use of ADS-B Implementataion and Validation of Identifying Phases of Flight in Pilot-Friendliness Considerations for Development of Aerodynamic Chains in Helicopter Operations In Traffic and Weather Services an Internal Combustion Engine and General Aviation Operations Personal Air Vehicle Flight Control Modeling and Calibration Methods for from Accident Data (TIS-B and FIS-B) Propeller Model for General Aviation N. Fala, V. Goblet, K. Marais, Purdue Systems General Aviation Aircraft Performance A. Rao, K. Marais, Purdue University, West S. Silva, L. Jensen, R. Hansman, Aircraft Performance Studies University, West Lafayette, IN I. Chakraborty, B. Lozano, D. Mavris, Analysis - a Survey and Comparison Lafayette, IN Massachusetts Institute of Technology, E. Harrison, S. Min, H. Jimenez, D. Mavris, Georgia Institute of Technology, Atlanta, of Models Cambridge, MA Georgia Institute of Technology, Atlanta, GA GA S. Min, E. Harrison, H. Jimenez, D. Mavris, Georgia Institute of Technology, Atlanta, GA Wednesday, 24 June 2015 157-AFM-9 Unmanned Aircraft Systems II Plum Blossom A Chaired by: T. FIELDS, University of Missouri and G. SHAH, NASA-Langley Research Center 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2015-2854 AIAA-2015-2855 AIAA-2015-2856 AIAA-2015-2857 AIAA-2015-2858 AIAA-2015-2859 Unsteady Aerodynamics Modeling A Comparison of Filters for UAS-Based Robust Three-Dimensional Nonlinear Model Predictive Control A Launch System Design Feasibility Study of Closed Cycle for a Flexible Unmanned Air Localization of Stationary RF Sources Characterization of a Complex Applied to Trajectory Tracking for Methodology for Small Unmanned Propulsion for Unmanned Aerial Vehicle M. Stachura, Black Swift Technologies, LLC, Atmosphere at High Resolution Unmanned Aerial Vehicles Aircraft Applications Systems A. Kotikalpudi, H. Pfifer, G. Balas, Boulder, CO; N. Wagle, E. Frew, University of using Multi-Agent Windmappers K. Subbarao, C. Tule, P. Ru, University of A. Patterson, A. Arena, Oklahoma State T. Hays, A. Arena, Oklahoma State University of Minnesota, Minneapolis, Colorado, Boulder, Boulder, CO C. Montalvo, J. Richardson, J. Marshall, Texas, Arlington, Arlington, TX University, Stillwater, OK University, Stillwater, OK Minneapolis, MN University of South Alabama, Mobile, AL
81 Wednesday, 24 June 2015 158-AMT-9/GT-9 Ground Test Facility Improvements I Obelisk B Chaired by: R. RHEW, NASA-Langley Research Center and S. SIMERLY, NASA Glenn Research Center 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2015-2860 AIAA-2015-2861 AIAA-2015-2862 AIAA-2015-2863 AIAA-2015-2864 Oral Presentation Development of a Research Facility Development and Testing of an Expansion of the AEDC H2 Arc Experiments with the Model Test Upgrades to the Texas A&M Oran NASA Langley Aeroacoustic Wind to Study the Flow Field in an APU- Unsteady Low-Speed Wind Tunnel Heater Facility Test Envelope Using Apparatus Installed in the AFIT Low W. Nicks Low-Speed Wind Tunnel Tunnel Capability Moving Forward Style Inlet D. Greenblatt, Technion--Israel Institute of Cold-Air Mixing Speed Tunnel for M=0.4 Operation M. Doty, F. Hutcheson, H. Haskin, P. F. Lou, W. Murray, N. Key, Purdue Technology, Haifa, Israel G. Hammock, Arnold Engineering J. Lancaster, M. Reeder, Air Force Institute A. Herring, D. Kutz, L. Brown, E. White, Quinto, D. Smith, NASA Langley Research University, West Lafayette, IN Development Complex, Arnold AFB, TN of Technology, Wright-Patterson AFB, OH; Texas A&M University, College Station, TX Center, Hampton, VA M. Sytsma, Air Force Research Laboratory, Eglin AFB, FL; P. Rowe, RE2, Inc., Pittsburgh, PA; R. Cobb, Air Force Institute of Technology, Wright-Patterson AFB, OH Wednesday, 24 June 2015 159-AMT-10/GT-10 Particle-Based Velocimetry Applications and Developments Topaz Chaired by: K. LOWE, Virginia Tech and C. GOYNE, University of Virginia 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2015-2865 AIAA-2015-2866 AIAA-2015-2867 AIAA-2015-2868 AIAA-2015-2869 AIAA-2015-2870 Velocity Measurements in an Stereoscopic PIV measurements Multi-stereo PIV measurement of Application of Particle Image Biological Flow Measurement using Development and characterization Unseeded Turbojet Engine Exhaust in a turbofan engine inlet with propeller wake flow in industrial Velocimetry and Laser Induced Optical Flow Method of an inexpensive LED-based Using Planar Doppler Velocimetry tailored swirl distortion facility Fluorescence in a cooling duct flow Z. Yang, H. Yu, G. Huang, B. Ludwig, light source for high-frame-rate T. Jenkins, MetroLaser, Inc., Laguna Hills, M. Nelson, K. Lowe, W. O’Brien, C. Kirk, M. Novara, R. Geisler, A. Schroeder, H. Rochlitz, P. Scholz, Technical University Wright State University, Beavercreek, OH schlieren imaging CA; J. Seitzman, S. Adusumilli, Georgia Virginia Polytechnic Institute and State German Aerospace Center (DLR), of Braunschweig, Braunschweig, Germany D. Lincoln, K. Murari, C. Johansen, Institute of Technology, Atlanta, GA University, Blacksburg, VA Göttingen, Germany University of Calgary, Calgary, Canada Wednesday, 24 June 2015 160-APA-17 Special Session: Hybrid CFD Method Assessments for F-16XL Aircraft Aerodynamics Stemmons A Chaired by: J. LUCKRING, NASA-Langley Research Center and A. RIZZI, KTH Royal Institute Technology 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2015-2871 AIAA-2015-2872 AIAA-2015-2873 AIAA-2015-2874 AIAA-2015-2875 AIAA-2015-2876 Free-Flight High AoA Flows F-16XL Hybrid Reynolds-Averaged Numerical Simulation of the F-16XL Hybrid RANS-LES Simulations of Numerical Simulation of the F-16XL A Synthesis of Hybrid CFD Results Simulation at Sub- and Transonic Navier-Stokes/Large Eddy at Full-Scale Flight Test Conditions F-16XL Aircraft in Low-speed High- at Full-Scale Flight Test Conditions for F-16XL Aircraft Aerodynamics Speeds - F-16XL (CAWAPI-3) Simulation on Unstructured Grids Using a Near-Body Off-Body CFD alpha Flight Using Delayed Detached-Eddy J. Luckring, NASA Langley Research S. Hitzel, Airbus, Manching, Germany M. Park, A. Elmiligui, K. Abdol-Hamid, Approach M. Tomac, A. Rizzi, Royal Institute of Simulation Center, Hampton, VA NASA Langley Research Center, Hampton, S. Morton, D. McDaniel, CREATE Kestrel Technology (KTH), Stockholm, Sweden; A. A. Lofthouse, R. Cummings, U.S. Air Force VA Team, Eglin AFB, FL Jirasek, P. Eliasson, Swedish Defense Research Academy, Colorado Springs, CO Agency (FOI), Stockholm, Sweden Wednesday, 24 June 2015 161-APA-18 Aerodynamic Design Methodologies II Carpenter Ballroom Chaired by: J. LATZ, Northrop Grumman Aerospace Systems and D. FINLEY, Lockheed Martin Aeronautics 0900 hrs 0930 hrs 1000 hrs 1030 hrs AIAA-2015-2877 AIAA-2015-2878 AIAA-2015-2879 AIAA-2015-2880 Improvements in the New Unsteady Aerodynamic shape optimization of Design of A High-Performance Aerodynamic Optimization of Far-Field Drag Breakdown Method BWB aircraft based on multizone Tailless MAV Through Planform Integrated Wing-Engine Geometry and Application to Complex Cases collaborative optimization design Optimization using an Unstructured Vorticity Solver H. Toubin, D. Bailly, M. Costes, ONERA, method M. Bronz, G. Hattenberger, French Civil L. King, R. Hartfield, Auburn University, Meudon, France Z. Gao, K. Zhao, C. Wang, Northwestern Aviation University, Toulouse, France Auburn, AL; V. Ahuja, Research in Flight, Polytechnical University, Xi’an, China Auburn, AL
82 Wednesday, 24 June 2015 162-APA-19 Propeller/Rotorcraft/Wind Turbine Aerodynamics II Stemmons B Chaired by: J. FARNSWORTH, University of Colorado Boulder and M. POST, USAF Academy 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2015-2881 AIAA-2015-2882 AIAA-2015-2883 AIAA-2015-2884 AIAA-2015-2885 AIAA-2015-2886 AIAA-2015-2887 Development of UGS Monocopter: A study of separation on airfoils Computational Investigation Computational Investigations Rotor Dynamic Wake Inflow Validation of Installation Effect A New Whirl Flutter Analysis Platform Design and Trajectory undergoing pitch, surge and of Coaxial Rotor Interactional of Transient Loads and Blade Modelling in State-Space Format Predictions through Simulations Method Tracking combined motions Aerodynamics in Steady Forward Deformations on Coaxial Rotor M. Gennaretti, R. Gori, J. Serafini, G. of Contra-Rotating Open Rotors at Y. Yang, G. Huang, D. Zhao, C. Tang, S. Srigrarom, K. Lee, S. Chng, M. Bin R. Dunne, B. McKeon, California Institute Flight Systems Bernardini, F. Cardito, Roma Tre University, Low-Speed Flight Conditions Aviation Industry Corporation of China Abdul Malik, University of Glasgow, of Technology, Pasadena, CA B. Passe, A. Sridharan, J. Baeder, R. Singh, H. Kang, Army Research Laboratory, Rome, Italy A. Stuermer, German Aerospace Center (AVIC), Xi’an, China Glasgow, United Kingdom University of Maryland, College Park, Aberdeen Proving Ground, MD; J. Sirohi, (DLR), Braunschweig, Germany College Park, MD University of Texas, Austin, Austin, TX Wednesday, 24 June 2015 163-ASE-1 Numerical Weather Prediction (Invited) Plum Blossom B Chaired by: N. AHMAD, NASA Langley Research Center and D. GHOSH 0900 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2015-2888 AIAA-2015-2889 AIAA-2015-2890 AIAA-2015-2891 Challenges and Opportunities in Modeling of the Global Atmosphere Well-Balanced Formulation of Use of Numerical Weather Simulations of orographic flows using Z. Janjic, National Oceanic and Atmospheric Administration, College Park, MD Gravitational Source Terms for Prediction Models for NextGen ATC unstructured and structured meshes Conservative Finite-Difference Wind Impact Studies (Invited) (Invited) Atmospheric Flow Solvers S. Troxel, T. Reynolds, Lincoln Laboratory, J. Szmelter, Loughborough University, D. Ghosh, E. Constantinescu, Argonne Massachusetts Institute of Technology, Loughborough, United Kingdom; P. National Laboratory, Lemont, IL Lexington, MA Smolarkiewicz, European Centre for Medium- Range Forecasting, Reading, United Kingdom; A. Wyszogrodzki, National Research Institute, Warsaw, Poland Wednesday, 24 June 2015 164-ATIO-15 ATM III - Modeling in ATM Metropolitan Ballroom Chaired by: S. LANDRY, Purdue University 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2015-2892 AIAA-2015-2893 AIAA-2015-2894 AIAA-2015-2895 AIAA-2015-2896 A System Dynamics Approach Modeling Approach for Resilience Risk-based Causal Modeling of A Data-Driven Quantitative Assessing Air Traffic Control System towards ANSP Modeling Engineering of the Future ATM System Airborne Loss of Separation Framework for Safety Assessment Safety with System Controllability M. Kreuz, M. Schultz, German Aerospace R. Palumbo, A. Errico, D. Pascarella, F. S. Geuther, A. Shih, NASA Langley of Air Traffic Control System J. Guo, K. Marais, S. Landry, Purdue Center (DLR), Braunschweig, Germany Gargiulo, E. Filippone, Italian Aerospace Research Center, Hampton, VA A. Oztekin, Hi-Tec Systems, Inc., Egg University, West Lafayette, IN Research Center (CIRA), Capua, Italy Harbor Twp, NJ Wednesday, 24 June 2015 165-ATIO-16 Transformational Flight - Autonomy I Monet Ballroom Chaired by: B. ALLEN, NASA Langley Research Center 0900 hrs 0930 hrs 1000 hrs 1030 hrs AIAA-2015-2897 AIAA-2015-2898 AIAA-2015-2899 Oral Presentation Who’s got the bridge? Towards Towards an Open, Distributed Reinforcement Learning with “His actions indicate two- Safe, Robust Autonomous Software Architecture for UxS Autonomous Small Unmanned dimensional thinking” - Deciding to Operations - “Data, you’ve got Operations - “It’s difficult to Aerial Vehicles in Cluttered Go Around via Machine Learning the bridge.” - First Officer Thomas work in groups when you’re Environments - “After all these M. Motter, J. High, C. Cross, H. Fan, “Will” Riker Star Trek: The Next omnipotent,” - Q Star Trek: The years among humans, you still W. Fehlman, L. Hempley, NASA Langley Generation:: Coming of Age (1988) Next Generation:: Deja Q (1990) haven’t learned to smile.” Research Center, Hampton, VA; et al. B. Allen, C. Cross, H. Fan, W. Fehlman, C. Cross, H. Fan, W. Fehlman, L. Hempley, L. Tran, C. Cross, M. Motter, J. Neilan, L. Hempley, M. Motter, NASA Langley M. Motter, J. Neilan, NASA Langley G. Qualls, P. Rothhaar, NASA Langley Research Center, Hampton, VA; et al. Research Center, Hampton, VA; et al. Research Center, Hampton, VA; et al. 83 Wednesday, 24 June 2015 166-ATIO-17 Human Factors in Aviation Operations Milan Chaired by: L. BOWERS, Purdue University 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2015-2900 AIAA-2015-2901 AIAA-2015-2902 AIAA-2015-2903 AIAA-2015-2904 AIAA-2015-2905 AIAA-2015-2906 A Model for Situational Awareness Analysis of Eye-Tracking Data with Threat and Error Management Evaluating Intensity as a NextGen A Comparison of an Intensity Tactile Feedback and Situation Modeling the Air Traffic Controller’s in Aircraft Upset Prevention and Regards to the Complexity of Flight Applied to Loss of Control - Inflight Controller Function for Increased Control Measure Versus Dynamic Awareness - Improving Adherence Direct-to Operation Using Logistic Recovery Deck Information Automation D. Carroll, Aviation Performance Solutions, Traffic Scenarios Density to Capture Complexity to an Envelope in Sidestick- Regression K. Schlimm, Aviation Performance and Management - Inattentional LLC, Mesa, AZ C. Surakitbanharn, S. Landry, Purdue Within a Sector Controlled Fly-by-Wire Aircrafts S. Hong, S. Jung, K. Lee, Korea Aerospace Solutions, LLC, Mesa, AZ Blindness, System State Awareness, University, West Lafayette, IN C. Surakitbanharn, C. Surakitbanharn, F. Schmidt-Skipiol, Technical University of University, Goyang, South Korea and EFB Usage S. Landry, Purdue University, West Braunschweig, Braunschweig, Germany E. Dill, S. Young, NASA Langley Research Lafayette, IN Center, Hampton, VA Wednesday, 24 June 2015 167-BAL-1 Balloon Systems I Steuben Chaired by: J. NOTT, Nott Technology LLC 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2015-2907 AIAA-2015-2908 Oral Presentation AIAA-2015-2909 AIAA-2015-2910 AIAA-2015-2911 AIAA-2015-2912 The NASA Balloon Program - The French balloon program 2013 Balloon Systems Application Qualification of the NASA Super Non-Linear Analysis of the Returning to Hydrogen Gas : a Suitability of ADS-B as a Beacon Positioning For the Future - 2015 T. Gerber, Applied Technology Associates, Pressure Balloon NASA Super Pressure Balloons: Strategic Decision to Continue for Stratospheric Balloon Platforms D. Fairbrother, NASA Goddard Space Flight A. Vargas, V. Dubourg, D. Vassaux, French Albuquerque, NM H. Cathey, New Mexico State University, Implementation of a Large Strain Achievement of Stratospheric and Payloads Center, Greenbelt, MD Space Agency (CNES), Toulouse, France Wallops Island, VA; J. Tuttle, D. Material Model Balloons Flights T. Lachenmeier, R. Dewey, Near Space Fairbrother, M. Said, NASA Goddard Space A. Bown, D. Wakefield, Tensys Dynamics, J. Gary, French Space Agency (CNES), Corporation, Tillamook, OR Flight Center, Wallops Island, VA Ltd., Bath, United Kingdom Aire sur l’Adour, France; B. Dellery, G. Letrenne, S. Venel, A. Vargas, French Space Agency (CNES), Toulouse, France Wednesday, 24 June 2015 168-CASE-6 CASE Session II & III Grand Ballroom D 0900 - 1230 hrs 0900-1045 hrs Integration and Test This 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 Corporation, Hernando Jiminez, Research Engineer II at Aerospace Systems Design Laboratory, Georgia Institute of Technology and David Loda, Executive Director, NCPS Research, LLC Panelists: Jim Murphy David Maroney Project Engineer for Integrated Test and Evaluation for the Unmanned Aircraft System Integration Principal Systems Engineer NASA Ames Research Center The Mitre Corporation
1045-1230 hrs Entry into Service/End of Life This 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 Systems Panelists: Tim Adama Ed Dolanski Jim Gallagher Chief Engineer of Factories President and CEO EIS Program Manager Raytheon Missile Systems Aviall Gulfstream Aerospace Corporation 84 Wednesday, 24 June 2015 169-CFD-17 Advances in High-Order Methods Grand Ballroom A Chaired by: D. ZINGG, University of Toronto and P. ROE, University of Michigan 0900 hrs 0930 hrs 1000 hrs 1030 hrs AIAA-2015-2913 AIAA-2015-2914 AIAA-2015-2915 AIAA-2015-2916 New Approaches to Limiting New Diagonal-Norm Summation- Development of Generalized A Finite Difference WENO Scheme P. Roe, T. Lung, J. Maeng, University of by-Parts Operators for the First Summation-by-Parts Operators for Maintaining Velocity, Pressure Michigan, Ann Arbor, Ann Arbor, MI Derivative with Increased Order of the Second Derivative with Variable and Temperature Equilibrium in Accuracy Coefficients Multicomponent Compressible Fluid D. Del Rey Fernández, D. Zingg, University D. Del Rey Fernández, D. Zingg, University Analysis of Toronto, Toronto, Canada of Toronto, Toronto, Canada T. Nonomura, Japan Aerospace Exploration Agency (JAXA), Sagamihara, Japan; D. Terakado, University of Tokyo, Sagamihara, Japan; K. Fujii, Japan Aerospace Exploration Agency (JAXA), Sagamihara, Japan Wednesday, 24 June 2015 170-CFD-18 Current Trends in CFD Research I (Invited) Grand Ballroom B Chaired by: H. HUYNH, NASA Glenn Research Center and Z. WANG, University of Kansas 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs Oral Presentation Oral Presentation AIAA-2015-2917 Oral Presentation Oral Presentation Comparison of Output Error Estimation Novel Adaptive Mechanics for High- Investigation of Unstructured High-order Discontinuous Galerkin Probing Complex Unsteady Flow for Finite Element Discretizations of Order Unstructured CFD (Invited) Higher-Order Methods for Unsteady Simulations on Domains with Large Physics Using a High-Fidelity Convection-dominated Flows (Invited) K. Fidkowski, University of Michigan, Ann flow and Moving Domains Deformations (Invited) Computational Framework H. Carson, S. Allmaras, M. Galbraith, Arbor, Ann Arbor, MI J. Newman, W. Anderson, University of P. Persson, University of California, (Invited) D. Darmofal, Massachusetts Institute of Tennessee, Chattanooga, Chattanooga, TN Berkeley, Berkeley, CA M. Visbal, Air Force Research Laboratory, Technology, Cambridge, MA Wright-Patterson AFB, OH Wednesday, 24 June 2015 171-CFD-19 LES, DNS, and Hybrid RANS-LES III Coral Chaired by: J. BAEDER, University of Maryland and C. GROTH, University of Toronto 0900 hrs 0930 hrs 1000 hrs 1030 hrs AIAA-2015-2918 AIAA-2015-2919 AIAA-2015-2920 AIAA-2015-2921 Aerodynamic Characteristics of Applications of the integral Wall Model An Embedded LES-RANS Solver for Assessment of Hybrid RANS/LES SC1095 Airfoil using Hybrid RANS-LES in LES of flow over surfaces including Aerodynamic Simulations Methods For Gas-Turbine Combustor- Methods Implemented into a GPU resolved and subgrid roughness K. Anupindi, R. Sandberg, University of Relevant Turbulent Flows Accelerated Navier-Stokes Solver X. Yang, J. Sadique, C. Meneveau, R. Mittal, Southampton, Southampton, United J. West, C. Groth, University of Toronto, N. Jain, J. Baeder, University of Maryland, Johns Hopkins University, Baltimore, MD Kingdom Toronto, Canada; J. Hu, Pratt & Whitney, College Park, College Park, MD Mississauga, Canada Wednesday, 24 June 2015 172-CFD-20 Turbulence Model Validation (Invited) Emerald Chaired by: C. RUMSEY, NASA-Langley Research Center and B. SMITH, Lockheed Martin Aeronautics 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2015-2922 AIAA-2015-2923 AIAA-2015-2924 AIAA-2015-2925 AIAA-2015-2926 AIAA-2015-2927 Modification of the k-kl Two LagRST Model Predictions of a Second-Moment RANS Model Assessment of g-Equation Application of an Elliptic Blending Recent Developments on the Equation Turbulence Model for Wingtip Vortex Flowfield (Invited) Verification and Validation using the Formulation for a Second-Moment Reynolds Stress Model in Attached Turbulence Modeling Resource Improved Jet Flow Predictions M. Olsen, NASA Ames Research Center, Turbulence Modeling Resource Website Reynolds Stress Turbulence Model and Separated flows (Invited) Website (Invited) (Invited) Moffett Field, CA; R. Lillard, NASA Johnson (Invited) (Invited) M. Stoellinger, R. Roy, University of C. Rumsey, NASA Langley Research Center, B. Smith, Lockheed Martin Corporation, Space Center, Houston, TX; T. Coakley, B. Eisfeld, German Aerospace Center (DLR), V. Togiti, B. Eisfeld, German Aerospace Wyoming, Laramie, Laramie, WY; Hampton, VA Fort Worth, TX NASA Ames Research Center, Moffett Braunschweig, Germany; C. Rumsey, NASA Center (DLR), Braunschweig, Germany N. Ashton, University of Manchester, Field, CA Langley Research Center, Hampton, VA Manchester, United Kingdom
85 Wednesday, 24 June 2015 173-FD-19 Turbomachinery - Turbines Senators Lecture Hall Chaired by: Z. RUSAK, Rensselaer Polytechnic Institute and Q. WANG, MIT 0900 hrs 0930 hrs 1000 hrs 1030 hrs AIAA-2015-2928 AIAA-2015-2929 AIAA-2015-2930 AIAA-2015-2931 Data Processing Techniques for Flowfield and Film Performance Visualization of Secondary Flow Design Optimization of Profiled Measurements Collected from Measurements of Axial Shaped Structures Caused by Rotating Endwall with Consideration of a Single Slanted Hot-Wire for Cooling Holes on a Flat Plate Instability: Synchronized Stereo Cooling and Rim Seal Flow Effects Turbomachinery Applications D. Getsinger, J. Dees, G. Rodebaugh, High-Speed PIV and Unsteady H. Tang, S. Liu, H. Luo, Aviation Industry R. Berdanier, N. Key, Purdue University, General Electric Company, Niskayuna, NY Pressure Measurements Corporation of China (AVIC), Shanghai, West Lafayette, IN B. Pardowitz, German Aerospace Center China (DLR), Berlin, Germany; J. Peter, Technical University of Berlin, Berlin, Germany; U. Tapken, German Aerospace Center (DLR), Berlin, Germany; P. Thamsen, Technical University of Berlin, Berlin, Germany; L. Enghardt, German Aerospace Center (DLR), Berlin, Germany Wednesday, 24 June 2015 174-FD-20 Shock Wave / Boundary Layer Interactions Edelweiss Chaired by: N. CLEMENS, The University of Texas at Austin and D. GAITONDE, The Ohio State University 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2015-2932 AIAA-2015-2933 AIAA-2015-2934 AIAA-2015-2935 AIAA-2015-2936 Experimental Investigation of Effects of Sweep on Impinging Experimental Investigation of Experimental and Numerical Study An Experimental Investigation of Unsteadiness of Swept-Ramp Oblique Shock-Turbulent Boundary shock-induced corner boundary of Shock-Wave Boundary Layer the Effect of Boundary Layer on an Shock/Boundary Layer Interactions Layer Interaction layer separation Interactions on an Axisymmetric Body Internal Compression Inlet at Mach 2 R. Dawson, C. Pederson, J. Little, A. Hegde, V. Narayanaswamy, North G. Robertson, R. Kumar, Florida State H. Tabanli, K. Yuceil, Istanbul Technical L. Vanstone, M. Saleem, S. Seckin, N. University of Arizona, Tucson, Tucson, AZ Carolina State University, Raleigh, NC University, Tallahassee, FL; T. Eymann, S. University, Istanbul, Turkey Clemens, University of Texas, Austin, Morton, CREATE Kestrel Team, Eglin AFB, FL Austin, TX Wednesday, 24 June 2015 175-FD-22 Unsteady Flows - Cavity and Shear Flows Govenors Lecture Hall Chaired by: K. CASPER and K. GRANLUND, Air Force Research Laboratory 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2015-2937 AIAA-2015-2938 AIAA-2015-2939 AIAA-2015-2940 AIAA-2015-2941 Relationship between Acoustic Modal Decomposition of Pressure Comparison of High-Order and Reduced Order Modeling of Shear-Thinning Properties of Blood Tones and Flow Structure in Data in Cavity Flows Low-Order Methods for Large-Eddy a Dielectric Barrier Discharge in Large Arteries Transonic Rectangular Cavity Flow K. Casper, S. Arunajatesan, Sandia Simulation of a Compressible Shear Controlled Shear Layer using F. Kok, R. Myose, K. Hoffmann, Wichita J. Wagner, K. Casper, S. Beresh, B. Pruett, National Laboratories, Albuquerque, NM Layer Minimum Basis Rotations State University, Wichita, KS R. Spillers, J. Henfling, Sandia National M. Mankbadi, J. DeBonis, N. Georgiadis, J. Chabot, E. Caraballo, Miami University, Laboratories, Albuquerque, NM NASA Glenn Research Center, Cleveland, OH Oxford, OH; J. Little, University of Arizona, Tucson, Tucson, AZ 86 Wednesday, 24 June 2015 176-MAO-5 Emerging Methods I Madrid Chaired by: E. WINER, Iowa State University and V. LI, Boeing Engineering Operations & Technology 0900 hrs 0930 hrs 1000 hrs 1030 hrs AIAA-2015-2942 AIAA-2015-2943 AIAA-2015-2944 AIAA-2015-2945 Multidisciplinary Design Space Arnoldi-based Sampling for High- Multi-Domain Diversity An MDO advisory system supported Exploration Using Additive dimensional Optimization using Preservation to Mitigate Particle by knowledge-based technologies Manufacturing and Rapid Prototype Imperfect Data Stagnation and Enable Better M. Hoogreef, G. La Rocca, Delft University Testing J. Hicken, A. Ashley, Rensselaer Pareto Coverage in Mixed-Discrete of Technology, Delft, The Netherlands A. Friedman, P. Raj, Virginia Polytechnic Polytechnic Institute, Troy, NY Particle Swarm Optimization Institute and State University, Blacksburg, W. Tong, Syracuse University, Syracuse, VA; E. Alyanak, Air Force Research NY; S. Chowdhury, A. Messac, Mississippi Laboratory, Wright-Patterson AFB, OH State University, Mississippi State, MS Wednesday, 24 June 2015 177-MST-7 Flight Simulation Travertine Chaired by: K. BILIMORIA 0900 hrs 0930 hrs 1000 hrs AIAA-2015-2946 AIAA-2015-2947 AIAA-2015-2948 Motion Parameter Selection for AVES SDK: Bridging the Gap Model-Based Testing for Objective Flight Simulators between Simulator and Flight Fidelity Evaluation of Engineering K. Bilimoria, S. Reardon, NASA Ames Systems Designer and Research Flight Simulators Research Center, Moffett Field, CA T. Gerlach, U. Durak, German Aerospace U. Durak, German Aerospace Center Center (DLR), Braunschweig, Germany (DLR), Braunschweig, Germany; A. Schmidt, T. Pawletta, University of Wismar, Wismar, Germany Wednesday, 24 June 2015 178-MST-8 Computational Methods for Fluid Dynamics and Heat Transfer Simulations Wyeth Chaired by: M. KOKALY and B. JAFFREZIC 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2015-2949 AIAA-2015-2950 AIAA-2015-2951 AIAA-2015-2952 AIAA-2015-2953 Aerodynamics Flight Mechanics Investigation of the effect of grid Strength Analysis and Optimization Thermal simulation and Real Time Multiple Fidelity Physics Approach on Compact Domains for size on external store separation Technique for Thermal Protection experiments for a stratospheric Based Simulation of Aircraft Air Vehicle Separation trajectory using CFD System using 3 Dimensional Element balloon gondola Environmental Control System B. Jaffrezic, M. Ruetten, H. Rosemann, A. Osman, A. Aly, Cairo University, Cairo, Model Q. Liu, Chinese Academy of Sciences, B. Sasanapuri, ANSYS, Inc., Pune, India German Aerospace Center (DLR), Egypt; I. El baialy, Qatar University, Doha, W. Yan, Aviation Industry Corporation of Beijing, China; Z. Li, Y. Yang, J. Cai, Göttingen, Germany Qatar; O. Abdellatif, Banha University, China (AVIC), Beijing, China; X. Luo, Aviation Academy of Opto-Electronics, Chinese Cairo, Egypt; E. Khalil, Cairo University, Industry Corporation of China (AVIC), Academy of Sciences, Beijing, China Cairo, Egypt Chengdu, China; D. Cui, Aviation Industry Corporation of China (AVIC), Beijing, China Wednesday, 24 June 2015 179-NW-6 Networking Coffee Break Chantilly Ballroom East 0900 - 0930 hrs Wednesday, 24 June 2015 180-PDL-8/APA-20 Plasma Aerodynamics & Flow Control IV Stemmons C Chaired by: T. DOUVILLE, TLG Aerospace, LLC. 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2015-2954 AIAA-2015-2955 AIAA-2015-2956 AIAA-2015-2957 AIAA-2015-2958 Plasma Laminar-Separation- Pressures over a Conical Forebody Starting Flow by Repetitive Multi-Input Genetic Algorithm for The Effect of Plasma Clouds on 87 Bubble Control over Airfoil at Low under Repetitive Nanosecond Pulse Nanosecond Pulsed DBD Actuation Experimental Optimization of the Aerodynamic Performance of Reynolds Numbers SDBD Actuations at Microseconds and Milliseconds in Reattachment Downstream of a Subsonic/Supersonic Inlets X. Meng, X. Yan, H. Hu, Northwestern D. Zhang, X. Meng, J. Wang, Quiescent Air Backward-Facing-Step with Surface D. Mei, Aviation Industry Corporation of Polytechnical University, Xi’an, China; F. Northwestern Polytechnical University, H. Hu, H. Li, X. Meng, J. Wang, Plasma Actuator China (AVIC), Shenyang, China; Y. Fan, C. Liu, S. Luo, University of California, Irvine, Xi’an, China; F. Liu, S. Luo, University of Northwestern Polytechnical University, N. Benard, National Center for Scientific Jiang, Beihang University, Beijing, China Irvine, CA California, Irvine, Los Angeles, CA Xi’an, China; F. Liu, S. Luo, University of Research (CNRS), Futuroscope, France; J. California, Irvine, Los Angeles, CA Pons-Prat, J. Periaux, G. Bugeda, CIMNE, Barcelona, Spain; J. Bonnet, E. Moreau, National Center for Scientific Research (CNRS), Futuroscope, France Wednesday, 24 June 2015 181-PDL-9/TP-8 Plasma Diagnostics II Miro Chaired by: N. HARADA, Nagaoka University of Technology and J. BURT, Universal Technology Corporation 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2015-2959 AIAA-2015-2960 AIAA-2015-2961 AIAA-2015-2962 AIAA-2015-2963 AIAA-2015-2964 Planar Two-Photon LIF Particle Vaporization Velocimetry Investigation of Non-Equilibrium Hybrid fs/ps coherent anti-Stokes Non-Equilibrium Analysis of Quantitative Measurements of Measurements of Atomic Species for LPG Diffusion Flames Nitrogen Plasmas Raman scattering in a non- Emission Spectroscopy Data Taken Electron Number Density and in a High-Temperature Inductively L. Tolomelli, Technological Institute of A. Lutz, D. Fletcher, University of Vermont, equilibrium environment initiated in the Freestream of the NASA IHF Threshold for Laser Induced Couple Plasma Environment Aeronautics (ITA), São José dos Campos, Burlington, Burlington, VT by a ns laser spark Arc Jet Facility Breakdown in Air J. Meyers, D. Fletcher, University of Brazil C. Dedic, J. Michael, T. Meyer, Iowa State M. Winter, C. Srinivasan, R. Charnigo, L. Su, Y. Wu, J. Sawyer, Z. Zhang, Vermont, Burlington, Burlington, VT University, Ames, IA University of Kentucky, Lexington, University of Tennessee, Knoxville, Lexington, KY Knoxville, TN Wednesday, 24 June 2015 182-TP-9 Aerothermodynamics II Rosetta Chaired by: A. MARTIN, University of Kentucky 0900 hrs 0930 hrs 1000 hrs 1030 hrs AIAA-2015-2965 AIAA-2015-2966 AIAA-2015-2967 AIAA-2015-2968 Shock Radiation Tests for Saturn Heat Transfer Measurements on the Shape Optimization of a Blunt Fugine cycle theory: predicting high and Uranus Entry Probes Afterbody of Spheres in Hypersonic Body in Reacting Hypersonic flow efficiency of the supermultijet- B. Cruden, D. Bogdanoff, ERC, Inc., Free-Flight in Air and Carbon in Thermal Non-Equilibrium for convergence engine working from Moffett Field, CA Dioxide Reducing Both Drag and Heat startup to hypersonic scram mode M. Wilder, NASA Ames Research Center, Transfer K. Naitoh, Y. Tanaka, T. Tamura, T. Moffett Field, CA; D. Bogdanoff, D. E. Zishka, R. Agarwal, Washington Okamoto, Y. Nojima, K. Yamagishi, Saunders, ERC, Inc., Moffett Field, CA University in St. Louis, St. Louis, MO Waseda University, Shinjuku, Japan Wednesday, 24 June 2015 183-F360-5 NACA to NASA: Embarking on the Next 100 Years of Excellence and Innovation in Aeronautics and Beyond Grand Ballroom E 0930 - 1200 hrs Moderator: Robert Pearce, Director, Strategy, Architecture & Analysis, Aeronautics Research Mission Directorate, NASA Headquarters Panelists: David Bowles Thomas Edwards Janet Kavandi David McBride Jaiwon Shin Center Director (Acting) Deputy Center Director Deputy Director Center Director Associate Administrator, Aeronautics Research Mission Directorate NASA Langley Research Center NASA Ames Rsearch Center NASA Glenn Research Center NASA Armstrong Flight Research Center NASA Headquarters
Wednesday, 24 June 2015
88 184-LNCH-2 Luncheon in the Exposition Hall Chantilly Ballroom East 1230 - 1400 hrs A ticket is required and included in the conference registration fee where indicated. Wednesday, 24 June 2015 185-AA-26 Combustion Noise Fleur-de-lis B Chaired by: J. MENDOZA, United Technologies Research Center 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2015-2969 AIAA-2015-2970 AIAA-2015-2971 AIAA-2015-2972 AIAA-2015-2973 AIAA-2015-2974 On the spectrum of combustion Modelling of combustion noise Numerical investigation of Transfer Functions of Acoustic, Efficient Full 3D Turbulent A 2D-axisymmetric analytical noise spectrum using temporal combustion noise generation in a Entropy and Vorticity Waves in Combustion Noise Simulation Based model for the estimation of indirect C. Tam, Florida State University, correlations of heat release rate full annular combustion chamber an Annular Model Combustor and on Stochastic Sound Sources combustion noise in nozzle flows Tallahassee, FL from turbulent premixed flames T. Livebardon, CERFACS, Toulouse, France; Nozzle for the Prediction of the F. Grimm, German Aerospace Center J. Zheng, M. Huet, ONERA, Châtillon, France; Y. Liu, University of Surrey, Guildford, S. Moreau, University of Sherbrooke, Ratio Between Indirect and Direct (DLR), Stuttgart, Germany; R. Ewert, J. A. Giauque, National Center for Scientific United Kingdom; T. Echekki, North Carolina Sherbrooke, Canada; T. Poinsot, CERFACS, Combustion Noise Dierke, German Aerospace Center (DLR), Research (CNRS), Ecully, France; F. Cléro, State University, Raleigh, NC Toulouse, France; E. Bouty, Turbomeca, W. Ullrich, T. Sattelmayer, Technical Braunschweig, Germany; B. Noll, M. ONERA, Châtillon, France; S. Ducruix, National Bordes, France University of Munich, Garching, Germany Aigner, German Aerospace Center (DLR), Center for Scientific Research (CNRS), Stuttgart, Germany Châtenay-Malabry, France Wednesday, 24 June 2015 186-AA-27 Arrays Method Panel Session Fleur-de-lis A Chaired by: C. BAHR, NASA-Langley Research Center 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 AIAA-2015-2975 AIAA-2015-2976 AIAA-2015-2977 AIAA-2015-2978 AIAA-2015-2979 Discussion Development of New Wall-mounted Decorrelation of Acoustic Wave An Approach to Estimate the Pletharrays for Aeroacoustic Estimating the sound power and Strut-mounted Phased Propagation through the Shear Reliability of Microphone Array Phased Array Applications radiated by a nozzle-based source Microphone Arrays for Acoustic Layer in Open Jet Wind Tunnel Methods J. Underbrink, The Boeing Company, in a test cell using a phased array Measurements in Closed Test- D. Ernst, C. Spehr, T. Berkefeld, German G. Herold, E. Sarradj, Brandenburg Seattle, WA B. Tester, K. Holland, University of section Wind Tunnels Aerospace Center (DLR), Göttingen, University of Technology, Cottbus, Southampton, Southampton, United W. Horne, N. Burnside, NASA Ames Germany Germany Kingdom Research Center, Moffett Field, CA Wednesday, 24 June 2015 187-AA-28 Open Rotor II Inverness Chaired by: W. DEVENPORT, Virginia Tech 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs AIAA-2015-2980 AIAA-2015-2981 AIAA-2015-2982 AIAA-2015-2983 AIAA-2015-2984 AIAA-2015-2985 AIAA-2015-2986 Open-Rotor Noise Assessment with Flow Distortion and Noise Produced Computation of Rotor Noise Broadband noise for rotating A 3D analytical approach for Open Analytical Prediction of the Pylon- Comparison of rotor noise CFD/CAA Chaining by a Thrusting Rotor Ingesting a Generation in Grid Turbulence blades: analysis of acceleration rotor Blade Vortex Interaction(BVI) Wake Effect on the Tonal Noise measurement results in large-scale A. Chelius, T. Le Garrec, D. Mincu, ONERA, Planar Turbulent Boundary Layer Using Large-Eddy Simulation effects in the time and frequency tonal noise radiated by the Front-Rotor of CROR and small-scale anechoic facilities Châtillon, France D. Wisda, H. Murray, W. Alexander, M. J. Wang, K. Wang, M. Wang, University of domains S. Moreau, M. Quaglia, Sherbrooke Propulsion Systems I. Belyaev, V. Kopiev, R. Skvortsov, I. Nelson, W. Devenport, Virginia Polytechnic Notre Dame, Notre Dame, IN S. Sinayoko, University of Southampton, University, Sherbrooke, Canada; R. N. Jaouani, Sogeti High Tech, Issy Les Pankratov, TsAGI, Moscow, Russia; V. Institute and State University, Blacksburg, Southampton, United Kingdom Fernando, Safran Group, Moissy-Cramayel, Moulineaux, France; M. Roger, École Centrale Titarev, Russian Academy of Sciences, VA; S. Glegg, Florida Atlantic University, France de Lyon, Lyon, France; T. Nodé-Langlois, Moscow, Russia; M. Zaytsev, TsAGI,
89 Boca Raton, FL Airbus, Toulouse, France; G. Serre, Sogeti High Moscow, Russia Tech, Issy Les Moulineaux, France Wednesday, 24 June 2015 188-AA-29 Airframe Noise III Lalique Chaired by: S. NOELTING, EXA 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs AIAA-2015-2987 AIAA-2015-2988 AIAA-2015-2989 AIAA-2015-2990 AIAA-2015-2991 AIAA-2015-2992 AIAA-2015-2993 An Assessment of Flap and Main Evaluation of Airframe Noise A Comparative Study of Simulated Comparison of Computational and Characterization of Flap Edge Noise On the Connection between Flap Simulations of LAGOON landing- Landing Gear Noise Abatement Reduction Concepts via Simulations and measured Gear-Flap Flow Experimental Microphone Array Radiation from a High-Fidelity Side-Edge Noise and Tip Vortex gear noise using Lattice Boltzmann Concepts Using a Lattice Boltzmann Interaction Results for an 18%-Scale Aircraft Airframe Model Dynamics Solver M. Khorrami, W. Humphreys, D. Lockard, Approach M. Khorrami, NASA Langley Research Center, Model W. Humphreys, M. Khorrami, D. Lockard, D. Casalino, E. Fares, B. Duda, A. Hazir, A. Sengissen, J. Giret, Airbus, Toulouse, NASA Langley Research Center, Hampton, VA E. Fares, D. Casalino, Exa GmbH, Hampton, VA; R. Mineck, Self, Yorktown, D. Lockard, W. Humphreys, M. Khorrami, D. Neuhart, C. Bahr, NASA Langley Exa GmbH, Stuttgart, Germany; M. France; C. Coreixas, J. Boussuge, Stuttgart, Germany; M. Khorrami, NASA VA; E. Fares, Exa GmbH, Stuttgart, Germany; NASA Langley Research Center, Hampton, Research Center, Hampton, VA Khorrami, NASA Langley Research Center, CERFACS, Toulouse, France Langley Research Center, Hampton, VA C. Yao, L. Jenkins, NASA Langley Research VA; E. Fares, D. Casalino, Exa GmbH, Hampton, VA Center, Hampton, VA Stuttgart, Germany; P. Ravetta, AVEC, Inc., Blacksburg, VA Wednesday, 24 June 2015 189-AA-30 Jet Noise Measurements II Obelisk A Chaired by: D. JUVE, Ecole Centrale de Lyon 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2015-2994 AIAA-2015-2995 AIAA-2015-2996 AIAA-2015-2997 AIAA-2015-2998 AIAA-2015-2999 Dual-plane, time-resolved, stereo PIV Adaptation of the Azimuthal On the systematic error in Role of Nozzle’s Proximity to Scattering of turbulent-jet Investigating the feedback path in for wavepacket eduction in a turbulent Decomposition Technique to Jet measurements of jet noise flight Plenum Chambers or Other Non- wavepackets by a swept trailing edge a jet-surface resonant interaction subsonic jet Noise Measuerements of an Aircraft effects using open jet wind tunnels line-of-sight Devices on Measured S. Piantanida, V. Jaunet, P. Jordan, J. Huber, K. Zaman, A. Fagan, J. Bridges, C. Brown, V. Jaunet, P. Braud, F. Boissonneau, P. Jordan, Engine in the Ground Tests U. Michel, CFD Software GmbH, Berlin, Jet Noise National Center for Scientific Research (CNRS), NASA Glenn Research Center, Cleveland, National Center for Scientific Research V. Kopiev, I. Belyaev, G. Faranosov, Germany A. Karon, D. Dickey, K. Ahuja, Georgia Poitiers, France; A. Cavalieri, Technological OH (CNRS), Poitiers, France; A. Cavalieri, M. Zaytsev, TsAGI, Moscow, Russia; Institute of Technology, Atlanta, GA Institute of Aeronautics (ITA), São José Technological Institute of Aeronautics (ITA), A. Aleksentsev, Y. Bersenev, OJSC dos Campos, Brazil; W. Wolf, University of São José dos Campos, Brazil Aviadvigatel, Perm, Russia; et al. Campinas, Campinas, Brazil Wednesday, 24 June 2015 190-ACD-5 Design of Unconventional Aircraft Configurations Morocco Chaired by: M. LOGAN, NASA Langley Research Center 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs AIAA-2015-3000 AIAA-2015-3001 AIAA-2015-3002 AIAA-2015-3003 AIAA-2015-3004 An Investigation into the Design of Advanced General Aviation Concept Morphing Strategy Design for A Methodology for Multi- The Hoops on the Way to an Efficient In Ground Effect Flying Study for a Roadable Aircraft Variable-Wing Aircraft Disciplinary Analysis of the Box a Supersonic Business Jet Vehicle Planform D. Lim, C. Justin, D. Mavris, Georgia R. Shi, J. Peng, Tsinghua University, Wing Concept (Performance Drivers for a V. Mirochnitchenko, T. Takahashi, Arizona Institute of Technology, Atlanta, GA Beijing, China I. Roy Salam, C. Bil, RMIT University, Commercially Viable Product) State University, Tempe, AZ Melbourne, Australia L. Gonzalez-Linero, Embry-Riddle Aeronautical University, Daytona Beach, FL 90 Wednesday, 24 June 2015 191-AMT-11/GT-11 Ground Test Facility Improvements II Obelisk B Chaired by: R. RHEW, NASA-Langley Research Center and J. HOPF, Aerospace Testing Alliance 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2015-3005 AIAA-2015-3006 AIAA-2015-3007 AIAA-2015-3008 Oral Presentation AIAA-2015-3009 Lyapunov-Based Nonlinear Control Development and Demonstration Wind Tunnel Testing of Variable Comparison of Freejet Data Overview of Uncertainty Analysis Reactivation of the NTF 3000 Ton of Wind Tunnel Supersonic Nozzle of A Continuous Beta Sweep Test & Camber Compliant Wing with Multiple between a Contoured and Conical Activities at NASA Glenn’s Liquid Nitrogen Tank from Ambient Contour Analysis Technique(CBSTAT) Rig Load Cell Test Fixture Nozzle in the AEDC H1 Facility Aeropropulsion Facilities Condition M. Sadraey, Daniel Webster College, K. Xie, F. Wang, N. Chen, L. Chen, Q. L. Zientarski, C. Marks, University of Dayton, G. Hammock, Arnold Engineering J. Stephens, E. Hubbard, NASA Langley S. Dunn, NASA Langley Research Center, Nashua, NH Shen, China Academy of Aerospace Dayton, OH; J. Joo, Air Force Research Development Complex, Arnold AFB, TN Research Center, Hampton, VA Hampton, VA Aerodynamics, Beijing, China Laboratory, Wright-Patterson AFB, OH Wednesday, 24 June 2015 192-AMT-12/GT-12 The Impact of PIV on Aerospace Technology I Edelweiss Chaired by: S. BERESH, Sandia National Laboratories and K. LOWE, Virginia Tech 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs Oral Presentation Oral Presentation Oral Presentation Oral Presentation Oral Presentation Oral Presentation Oral Presentation Application of Particle Image PIV for helicopter aerodynamics Time-resolved PIV in the buffeting Subsonic Wake Characterization of Industrial Applications of PIV in Recent Applications of PIV in Large Applications of PIV measurements Velocimetry at NASA for Rotorcraft (Invited) regime of ARIANE V (Invited) the Orion Capsule using PIV in the JAXA Large-Scale Wind Tunnels NRC Wind Tunnels in the ONERA large wind tunnels Research (Invited) M. Raffel, German Aerospace Center F. Scarano, Delft University of Technology, Ames UPWT 11-foot Wind Tunnel (Invited) F. de Souza, National Research Council (Invited) L. Jenkins, G. Yamauchi, NASA Langley (DLR), Cologne, Germany Delft, The Netherlands (Invited) H. Kato, S. Koike, Japan Aerospace Canada, Ottawa, Canada Y. Michou, ONERA, Chambery, France Research Center, Hampton, VA J. Heineck, NASA Ames Research Center, Exploration Agency (JAXA), Tokyo, Japan Moffett Field, CA Wednesday, 24 June 2015 193-APA-21 Transonic & Supersonic Aerodynamics Stemmons A Chaired by: M. JURKOVICH, US Air Force 1400 hrs 1430 hrs 1500 hrs AIAA-2015-3010 AIAA-2015-3011 AIAA-2015-3012 Numerical Study of Counterflowing Flow Physics of a Three- Supersonic Air Flows Around Some Jet Effects on Supersonic Slender- Dimensional Rounded Contour Geometrical Primitives Body Configurations Bump in a Mach 1.3 Supersonic M. Kotov, I. Kryukov, L. Ruleva, S. B. Venkatachari, National Institute of Free-stream Solodovnikov, S. Surzhikov, Russian Aerospace, Hampton, VA; M. Mullane, K. Lo, K. Kontis, University of Glasgow, Academy of Sciences, Moscow, Russia University of Alabama, Birmingham, Glasgow, United Kingdom Birmingham, AL; G. Cheng, University of Alabama, Tuscaloosa, Tuscaloosa, AL; C. Chang, NASA Langley Research Center, Hampton, VA Wednesday, 24 June 2015 194-APA-22 VSTOL/STOL Aerodynamics Carpenter Ballroom Chaired by: M. CALVERT, U.S. Army AMRDEC 1400 hrs 1430 hrs AIAA-2015-3013 AIAA-2015-3014 The LIFT! Project - Modular, Electric Numerical Investigation and Vertical Lift System with Ground Validation for Open Rotor Hover Power Tether Performance M. Duffy, A. Samaritano, The Boeing Q. Zhao, C. Sheng, University of Toledo,
91 Company, Ridley Park, PA Toledo, OH Wednesday, 24 June 2015 195-APA-23 Weapons Aerodynamics: Missile/Projectile/Guided-Munitions, Carriage and Store Separation II Stemmons B Chaired by: K. DENISSEN, Sandia National Labs 1400 hrs 1430 hrs 1500 hrs 1530 hrs AIAA-2015-3015 AIAA-2015-3016 AIAA-2015-3017 AIAA-2015-3018 CFD Aerodynamic Characterization Development and Validation of a Cavity-Store Interaction under Loads and Acoustics Prediction on of a High Maneuverability Airframe RANS-based Airdrop Simulation Supersonic Freestream Conditions Deployed Weapons Bay Doors C. Coyle, U.S. Military Academy, West Approach J. Merrick, M. Reeder, Air Force Institute of E. Sheta, R. Harris, CFD Research Point, NY; S. Silton, Army Research S. Geisbauer, German Aerospace Center Technology, Wright-Patterson AFB, OH Corporation, Huntsville, AL; E. Luke, Laboratory, Aberdeen Proving Ground, MD (DLR), Braunschweig, Germany; H. Mississippi State University, Mississippi Schmidt, German Aerospace Center (DLR), State, MS; L. Ukeiley, University of Göttingen, Germany Florida, Gainesville, Gainesville, FL Wednesday, 24 June 2015 196-ASE-2 Aircraft Icing and Atmospheric Hazards Plum Blossom B Chaired by: W. VAUGHAN, William W Vaughan Consultant and J. OWENS, NASA (Retired) 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs AIAA-2015-3019 AIAA-2015-3020 AIAA-2015-3021 AIAA-2015-3022 AIAA-2015-3023 A model for in-flight ice accretion Quasi-Unsteady Icing Simulation of Convective Enhancement of Icing Sensor Suite Development for a Sensitivity Analysis of Wake Vortex based on the exact solution of the an Oscillating Airfoil Roughness Elements in Stagnation Weather UAV Parameters Measured by Doppler unsteady Stefan problem H. Fouladi, McGill University, Montréal, Region Flows J. Hathaway, A. Avery, J. Jacob, Oklahoma Lidar G. Gori, M. Zocca, A. Guardone, Technical Canada; C. Aliaga, Newmerical M. Hughes, S. McClain, Baylor University, State University, Stillwater, OK T. Misaka, S. Obayashi, Tohoku University, University of Milan, Milan, Italy Technologies International, Montréal, Waco, TX; M. Vargas, A. Broeren, NASA Sendai, Japan; A. Stephan, F. Holzäpfel, Canada; W. Habashi, McGill University, Glenn Research Center, Cleveland, OH T. Gerz, German Aerospace Center (DLR), Montréal, Canada Oberpfaffenhofen, Germany Wednesday, 24 June 2015 197-ATIO-18 ATM IV - Economic/Benefits Analysis Ming Chaired by: S. HASAN, LMI 1400 hrs 1430 hrs 1500 hrs 1530 hrs AIAA-2015-3024 AIAA-2015-3025 AIAA-2015-3026 AIAA-2015-3027 Identifying benefit mechanisms for Assessing Departure Efficiency Airfare Determinants on the Kangaroo Concept and Benefits of PBN-Enabled NextGen technologies and concepts at U.S. Airports: a Comparison of Route (Australia-UK Market): A Case Parallel Approach Operations S. Landry, D. Peng, Purdue University, Methods Study of the Influences of Airlines, R. Mayer, B. Crow, D. Zondervan, MITRE West Lafayette, IN S. Tsao, J. DeArmon, S. Agbolosu-Amison, Alliances and Airports Corporation, McLean, VA; J. Allerdice, Federal A. Mahashabde, MITRE Corporation, H. Yang, Civil Aviation Flight University of Aviation Administration, Peachtree City, GA McLean, VA China, Guanghan, China Wednesday, 24 June 2015 198-ATIO-19 Terminal & Surface Operations IV Milan Chaired by: R. CURRAN, Delft Technical University of Technology 1400 hrs 1430 hrs 1500 hrs 1530 hrs AIAA-2015-3028 AIAA-2015-3029 AIAA-2015-3030 AIAA-2015-3031 Optimization of Push Back Time Development of Generic Ground Implementing a Combined Arrival, A framework for the classification Windows That Ensure Conflict Free Tracks of Performance Based Departure, and Surface Scheduler and prioritization of arrival and Ramp Area Aircraft Trajectories Navigation Operations for Fleet- for a Metroplex departure routes in Multi-Airport J. Coupe, D. Milutinovic, University of Level Airport Noise Analysis F. Wieland, W. Krueger, W. Peng, Y. Systems Terminal Manoeuvring California, Santa Cruz, Santa Cruz, CA; W. A. Wilson, M. LeVine, J. Bernardo, M. Zhang, A. Tyagi, C. Ye, Intelligent Areas Malik, University of California, Santa Cruz, Kirby, D. Mavris, Georgia Institute of Automation, Inc., Rockville, MD; et al. S. Sidiropoulos, A. Majumdar, K. Han, W. Moffett Field, CA; Y. Jung, NASA Ames Technology, Atlanta, GA Schuster, W. Ochieng, Imperial College Research Center, Moffett Field, CA London, London, United Kingdom 92 Wednesday, 24 June 2015 199-ATIO-20 Transformational Flight - Autonomy II Monet Ballroom Chaired by: B. ALLEN, NASA Langley Research Center 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs AIAA-2015-3032 AIAA-2015-3033 AIAA-2015-3034 AIAA-2015-3035 AIAA-2015-3036 Using Multimodal Input for Collaborating with Autonomous A Flexible Flight Control System for Operating in “Strange New State of the Art of Autonomous Autonomous Decision Making Agents Rapid GNC and Distributed Control Worlds” and Measuring Success Platforms and Human-Machine for Unmanned Systems - “What A. Trujillo, NASA Langley Research Deployment - Test and Evaluation in Complex Systems: Only a Fool Would Stand it needs in order to evolve, is a Center, Hampton, VA; H. Fan, Analytical P. Rothhaar, C. Cross, H. Fan, W. Fehlman, Environments In the Way of Progress human quality. Our capacity to leap Mechanics Associates, Inc., Hampton, VA; L. Hempley, M. Motter, NASA Langley G. Qualls, C. Cross, H. Fan, W. Fehlman, V. Stouffer, LMI, McLean, VA; K. Goodrich, beyond logic.” - Capt. Kirk, Star L. Hempley, C. Cross, Northrop Grumman Research Center, Hampton, VA; et al. L. Hempley, M. Motter, NASA Langley NASA Langley Research Center, Hampton, VA Corporation, Hampton, VA; W. Fehlman, Research Center, Hampton, VA; et al. Trek: The Motion Picture M. Motter, NASA Langley Research Center, J. Neilan, C. Cross, H. Fan, W. Fehlman, Hampton, VA; et al. L. Hempley, M. Motter, NASA Langley Research Center, Hampton, VA; et al. Wednesday, 24 June 2015 200-BAL-2 Balloon Systems II Steuben Chaired by: J. RAND, Winzen Engineering Inc 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs AIAA-2015-3037 AIAA-2015-3038 AIAA-2015-3039 AIAA-2015-3040 AIAA-2015-3041 AIAA-2015-3042 AIAA-2015-3043 Balloon Aspect of StratEx World Recent Improvements to the Design The Wallops Arc Second Pointer - A Current Status of a NASA High- Technology Development for the Shape Analysis of the 1/20-Scale An Undergraduate Student Record Skydive and Manufacture of High Altitude Balloon Borne Fine Pointing System Altitude Balloon-Based Observatory ExaVolt Antenna (EVA). 1/20-Scale ExaVolt Antenna Test Balloon Instrumentation Project (USIP) to J. Nott, Nott Technology, Santa Barbara, Zero-Pressure Balloons D. Stuchlik, NASA Goddard Space Flight for Planetary Science Deployment Test F. Baginski, George Washington Develop New Instrument Technology CA J. Marsh, Columbia Scientific Balloon Center, Greenbelt, MD D. Varga, NASA Glenn Research Center, F. Baginski, George Washington University, University, Washington, DC; K. Brakke, to Study the Auroral Ionosphere and Facility, Palestine, TX; M. Giles, Raven Cleveland, OH; E. Young, Southwest Washington, DC; P. Gorham, University Susquehanna University, Selinsgrove, PA; Stratospheric Ozone Layer Using Aerostar, Sulphur Springs, TX Research Institute, Boulder, CO of Hawaii, Honolulu, Honolulu, HI; D. K. Zhao, George Washington University, Ultralight Balloon Payloads Fairbrother, M. Said, S. Lang, NASA Washington, DC E. Bering, R. Gamblin, University of Houston, Wallops Flight Facility, Wallops Island, VA Houston, TX Wednesday, 24 June 2015 201-CFD-21 Discontinuous Galerkin Methods Grand Ballroom A Chaired by: C. SCHROCK, Air Firce Research Laboratory and L. DIOSADY, NASA Ames Research Center 1400 hrs 1430 hrs 1500 hrs 1530 hrs AIAA-2015-3044 AIAA-2015-3045 AIAA-2015-3046 AIAA-2015-3047 General element shapes within High-order Discontinuous Galerkin An Adaptive Explicit 3D Discontinuous A Hybrid Reconstructed a tensor-product higher-order Methods Applied to Multiphase Galerkin Solver for Unsteady Discontinuous Galerkin and space-time discontinuous-Galerkin Flows Problems Continuous Galerkin method for formulation M. Henry de Frahan, E. Johnsen, A. Kirby, D. Mavriplis, University of Wyoming, Incompressible Flows L. Diosady, S. Murman, NASA Ames University of Michigan, Ann Arbor, Ann Laramie, Laramie, WY; A. Wissink, Army A. Pandare, H. Luo, North Carolina State Research Center, Moffett Field, CA Arbor, MI Aviation and Missile Research Development University, Raleigh, NC
93 and Engineering Center, Moffett Field, CA Wednesday, 24 June 2015 202-CFD-22 Future of Fluids: Next Generation CFD (Invited) Grand Ballroom B Chaired by: M. MALIK, NASA-Langley Research Center and A. KHODADOUST, Boeing Engineering Operations & Technology 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs Oral Presentation AIAA-2015-3048 AIAA-2015-3049 AIAA-2015-3050 AIAA-2015-3051 AIAA-2015-3052 AIAA-2015-3053 Impacting Design with Large Eddy Next-Generation CFD for Scaling Limits for PDE-Based PyFR: Next-Generation High-Order Towards high-fidelity aerospace Opportunities and Challenges for CFD for Next Generation Hardware: Simulation (Invited) Hypersonic and Aerothermal Flows Simulation (Invited) Computational Fluid Dynamics on design in the age of extreme scale Multi-Disciplinary Analysis and Experiences with Proxy Applications P. Moin, Stanford University, Stanford, (Invited) P. Fischer, University of Illinois, Urbana- Many-Core Hardware (Invited) supercomputing (Invited) Optimization at Exascale (Invited) K. Franko, T. Fisher, P. Lin, S. Bova, CA; F. Ham, Cascade Technologies, Inc., G. Candler, University of Minnesota, Champaign, Urbana, IL P. Vincent, F. Witherden, A. Farrington, G. Q. Wang, Massachusetts Institute of J. Alonso, Stanford University, Stanford, CA Sandia National Laboratories, Palo Alto, CA Minneapolis, Minneapolis, MN Ntemos, B. Vermeire, J. Park, Imperial College Technology, Cambridge, MA Albuquerque, NM London, London, United Kingdom; et al. Wednesday, 24 June 2015 203-CFD-23 Parallel Computing and Novel Architectures Plum Blossom A Chaired by: L. LUO, North Carolina State University and C. STONE, Computational Science and Engineering 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2015-3054 AIAA-2015-3055 AIAA-2015-3056 AIAA-2015-3057 AIAA-2015-3058 AIAA-2015-3059 Parallel Techniques for Navier- Optimization of A Fine-grained GPU Parallelization of a High Order A Hybrid CPU-GPU Parallel Octree High-Performance 3D Multi- Comparison Of Acceleration Stokes Solver based on 4th Order BILU by CUDA Inter-block Immersed Boundary Method Fluid Direct Simulation Monte Carlo Disciplinary Fluid/Thermal Techniques on CFD Open-Source Modified Runge-Kutta Scheme Synchronization Solver Approach Prediction using Combined Multi- Software for Aerospace Applications with TVD L. Luo, J. Edwards, H. Luo, F. Mueller, North A. Jost, J. Zhang, Florida Institute of R. Jambunathan, D. Levin, University of Core/Multi-GPGPU Computer L. Mangani, G. Romanelli, University H. Shah, Wichita State University, Carolina State University, Raleigh, NC Technology, Melbourne, FL; T. Jackson, Illinois, Urbana-Champaign, Urbana, IL Systems of Applied Sciences and Arts, Luzern, Wichita, KS University of Florida, Gainesville, C. Stone, Computational Science and Switzerland; A. Gaddai, Technical Gainesville, FL Engineering, LLC, Chicago, IL; R. Davis, University of Milan, Milan, Switzerland; E. University of California, Davis, Davis, CA Casartelli, University of Applied Sciences and Arts, Luzern, Switzerland Wednesday, 24 June 2015 204-CFD-24 Design Optimization Coral Chaired by: L. TAO, GE Global Research 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs AIAA-2015-3060 AIAA-2015-3061 AIAA-2015-3062 AIAA-2015-3063 AIAA-2015-3064 Adjoint-Based Optimization of a Aerodynamic Shape Optimization A Continuous Sensitivity Equation Design optimization of a high bypass Design and Optimization of a Hypersonic Inlet for Natural Laminar Flow Using a of Arbitrary High Order ratio fan rotor against water ingestion Supersonic Business Jet H. Kline, Stanford University, Stanford, CA; Discrete-Adjoint Approach C. Belley, A. Hay, D. Pelletier, École S. Qiu, D. Yang, Aviation Industry Corporation F. Kiyici, S. Aradag, TOBB University of F. Palacios, The Boeing Company, Everett, R. Rashad, D. Zingg, University of Toronto, Polytechnique de Montréal, Montréal, of China (AVIC), Shanghai, China Economics and Technology, Ankara, Turkey WA; T. Economon, J. Alonso, Stanford Toronto, Canada Canada University, Stanford, CA Wednesday, 24 June 2015 205-CFD-25 Turbulent Flow Simulations II Emerald Chaired by: F. VERGINE and L. DUAN, Missouri University of Science and Technology 1400 hrs 1430 hrs 1500 hrs 1530 hrs AIAA-2015-3065 AIAA-2015-3066 AIAA-2015-3067 AIAA-2015-3068 Investigation of a Twinjet Numerical Simulations of RANS Simulations of a Channel High-Fidelity Computational Configuration with and without Single and Tandem Wheels for Flow with a New Velocity/Pressure- Assessment of the Performance of Flow Control Aerodynamic Loads Prediction Gradient Model a Vertical Axis Wind Turbine K. Goparaju, D. Gaitonde, S. Bhaumik, S. Spagnolo, X. Zhang, Z. Hu, D. Angland, S. Poroseva, J. Colmenares, University of J. Sudani, R. Prasad, M. Damodaran, Ohio State University, Columbus, OH University of Southampton, Southampton, New Mexico, Albuquerque, Albuquerque, Indian Institute of Technology United Kingdom NM; S. Murman, NASA Ames Research Gandhinagar, Ahmedabad, India Center, Moffett Field, NM Wednesday, 24 June 2015 94 206-F360-6 The Challenges of Green Aviation Grand Ballroom E 1400 - 1630 hrs Moderator: Marty Bradley, Technical Fellow, Boeing Commercial Airplanes Panelists: Ricky Curran Jay E. Dryer Askin Isikveren Leslie Perkins Jeanne Yu Faculty of Aerospace Engineering Director, Advanced Air Vehicles Program Office (Acting) Head of Visionary Aircraft Concepts Director, Energy Office Environmental Director Delft University of Technology Aeronautics Research Mission Directorate Bauhaus Luftfahrt Air Force Research Laboratory Boeing Commercial Airplanes NASA Headquarters
Wednesday, 24 June 2015 207-F360-7/CASE-7 System Complexity : Government Needs and Practical Research Results Grand Ballroom D 1400 - 1730 hrs This 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 Defense Moderators: Frank Serna, Principal Director, Strategic Initiatives, Draper Laboratory and Anna-Maria McGowan, Aeronautics Research Directorate, NASA Langley Research Center Panelists: Jeffrey P. Holland David Neyland Director of Research and Development and Chief Scientist Consultant U.S. Army Corps of Engineers Wednesday, 24 June 2015 208-FD-23 Unsteady Wing Aerodynamics III Govenors Lecture Hall Chaired by: S. YARUSEVYCH, University of Waterloo and H. LUO, Vanderbilt University 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2015-3069 AIAA-2015-3070 AIAA-2015-3071 AIAA-2015-3072 AIAA-2015-3073 AIAA-2015-3074 Numerical Simulation of Circular The effect of the blade chord length Unsteady Thick Airfoil Aerodynamics: Impact of a Vortical Gust on the Transient Encounters of a Flow Visualization and Force Cylinders and Wing Sections in on the aerodynamics of the MAV Experiments, Computation, and Aerodynamics of a Finite Aspect- NACA0012 Wing with a Measurements on Accelerated Unsteady Motion scale cycloidal propeller under Theory Ratio Wing Streamwise-Oriented Vortex Revolving Flat Plates at Low A. Gross, J. Zhou, New Mexico State hovering status D. Greenblatt, Technion--Israel Institute of R. Gordnier, M. Visbal, Air Force Research D. Garmann, M. Visbal, Air Force Research Reynolds Numbers University, Las Cruces, NM; H. Fasel, Y. Hu, H. Zhang, Northwestern Technology, Haifa, Israel; C. Rumsey, NASA Laboratory, Wright-Patterson AFB, OH Laboratory, Wright-Patterson AFB, OH M. Percin, B. van Oudheusden, Delft University of Arizona, Tucson, AZ Polytechnical University, Xi’an, China Langley Research Center, Hampton, VA; University of Technology, Delft, The H. Mueller-Vahl, Technion--Israel Institute Netherlands of Technology, Haifa, Israel; C. Stangfeld, Technical University of Berlin, Berlin, Germany Wednesday, 24 June 2015 209-FD-24 Boundary Layer Transition: Receptivity and Control Sapphire Chaired by: E. WHITE, Texas A&M University and A. CHOU, NASA Langley Research Center 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2015-3075 AIAA-2015-3076 AIAA-2015-3077 AIAA-2015-3078 AIAA-2015-3079 AIAA-2015-3080 On the Effect of Small Steps on Pre- Time-Frequency Analysis of Numerical Simulation of Hypersonic Leading-Edge Receptivity to Swept-Wing Boundary-Layer Delaying transition in rotating transitional Streamwise Elongated Boundary Layer Instabilities Boundary-Layer Instability in a Acoustic Waves for High-Speed Receptivity to Steady Free-Stream boundary-layer flows Streaks Generated by Freestream Laser Real Gas with Two-Dimensional Flows over a Blunt Wedge Disturbances P. Griffiths, University of Birmingham, A. Sescu, Mississippi State University, Perturbations Surface Roughness A. Cerminara, N. Sandham, University H. Kurz, M. Kloker, University of Stuttgart, Birmingham, United Kingdom; S. Garrett, Mississippi State, MS; M. Afsar, Imperial A. Chou, NASA Langley Research Center, C. Mortensen, X. Zhong, University of of Southampton, Southampton, United Stuttgart, Germany University of Leicester, Leicester, United Kingdom; S. Stephen, University of New 95 College London, London, United Kingdom; Hampton, VA; S. Schneider, Purdue California, Los Angeles, Los Angeles, CA Kingdom V. Sassanis, Mississippi State University, University, West Lafayette, IN South Wales, Sydney, Australia Mississippi State, MS Wednesday, 24 June 2015 210-FD-25 Flow Control Technologies - Barriers/Challenges to Tech Transition Topaz 1400 - 1730 hrs Chaired by: G. DALE, Air Force Research Laboratory and D. SMITH, Air Force Office of Scientific Research AFOSR The session will focus on the hurdles to transitioning flow control technology to platforms based on major case studies. Panel members will present lessons learned and recommendations on flow control technology transitions (approx. 15 minutes each), covering both successful and unsuccessful transitions. A moderated Q&A session will follow the presentations. Session outcome is intended to offer a path forward to fostering more technology transition for flow control. Moderator: Lou Cattafesta, Eminent Scholar and Professor, Florida State University Panelists: Edward Whalen Richard Wlezien Ronald Joslin Fay Collier Flow Control Actuation Manager Professor and Chair of Aerospace Engineering Program Officer Project Manager Boeing Research and Technology Iowa State University Office of Naval Research NASA Environmentally Responsible Aviation Wednesday, 24 June 2015 211-FD-26 Turbulence Simulations Senators Lecture Hall Chaired by: P. SPALART, Boeing Commercial Airplanes and E. JOHNSEN, University of Michigan 1400 hrs 1430 hrs 1500 hrs 1530 hrs AIAA-2015-3081 AIAA-2015-3082 AIAA-2015-3083 AIAA-2015-3084 A numerical study of turbulence Surface Roughness Effects in Application of the Wray-Agarwal Tetrahedral-Mesh Simulation of in boxes with no-slip walls and of Hypersonic Turbulent Boundary Model to Compressible Flows Turbulent Flows with the Space- varying volume-to-surface ratios Layers T. Wray, R. Agarwal, Washington Time Conservative Schemes E. Johnsen, University of Michigan, J. Poggie, Air Force Research Laboratory, University in St. Louis, St. Louis, MO C. Chang, NASA Langley Research Center, Ann Arbor, Ann Arbor, MI; P. Movahed, Wright-Patterson AFB, OH Hampton, VA; B. Venkatachari, National University of Illinois, Urbana-Champaign, Institute of Aerospace, Hampton, VA; G. Urbana, IL; D. Dowling, University of Cheng, University of Alabama, Tuscaloosa, Michigan, Ann Arbor, Ann Arbor, MI Tuscaloosa, AL Wednesday, 24 June 2015 212-MAO-6 Emerging Methods II Madrid Chaired by: B. MESMER, University of Alabama and J. HICKEN, Rensselaer Polytechnic Institute 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2015-3085 AIAA-2015-3086 AIAA-2015-3087 AIAA-2015-3088 AIAA-2015-3089 AIAA-2015-3090 Increasing Feasibility of the Self- Incorporation of Coupling Strength SUAVE: An Open-Source A Full-Space Method with Matrix Reducing Induced Drag and Integrated Multidisciplinary Aircraft Organizing Map as a Design Tool Models in a Value-based Systems Environment for Multi-Fidelity Aggregates for Stress-Constrained Maneuver Loads by Active Design Process Supported by a through a Novel Convergence Engineering framework for Conceptual Vehicle Design Structural Optimization Aeroelastic Alteration Decentral MDO Framework Heuristic optimization T. Lukaczyk, A. Wendorff, M. Colonno, T. G. Kennedy, Georgia Institute of J. Lin, Control Research Corporation, F. Daoud, S. Deinert, R. Maierl, Ö. T. Richardson, E. Winer, Iowa State H. Kannan, E. Tibor, Iowa State University, Economon, J. Alonso, Stanford University, Technology, Atlanta, GA Lexington, MA Petersson, Airbus, Manching, Germany University, Ames, IA Ames, IA; B. Mesmer, University of Stanford, CA; T. Orra, Embraer, São José
96 Alabama, Huntsville, Huntsville, AL; C. dos Campos, Brazil; et al. Bloebaum, Iowa State University, Ames, IA Wednesday, 24 June 2015 213-MAO-7 Metamodeling I Manchester Chaired by: S. CHOWDHURY, Mississippi State University and P. PIPERNI, Bombardier Inc 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs AIAA-2015-3091 AIAA-2015-3092 AIAA-2015-3093 AIAA-2015-3094 AIAA-2015-3095 A Methodology to Create Principal Component Analysis Assisted Auxiliary Air Inlet Design: Non- HDMR-based Surrogate Model for A Sequential Maximin Latin Approximate Models of Load Surrogate Modeling (PCA-SM) of Linearity, Surrogate High Dimensional Aerodynamic Hypercube Sampling Method And Envelopes Under Uncertainty Correlated Loads for Uncertainty Modeling and Optimization Aspects Design Problems Its Application to Aircraft Design D. Rancourt, S. Ghosh, D. Mavris, Georgia Analysis of Design Load Envelopes A. Lombardi, L. Santos, Embraer, São Z. Gao, C. Wang, Northwestern D. Wu, T. Long, Y. Wang, L. Liu, Beijing Institute of Technology, Atlanta, GA; S. S. Ghosh, D. Rancourt, D. Mavris, Georgia José dos Campos, Brazil; D. Ferrari, Polytechnical University, Xi’an, China Institute of Technology, Beijing, China Coggon, Airbus, Filton, United Kingdom Institute of Technology, Atlanta, GA; S. Technological Institute of Aeronautics Coggon, Airbus, Filton, United Kingdom (ITA), São José dos Campos, Brazil Wednesday, 24 June 2015 214-MST-9 Airframe Damage and Health Monitoring Travertine Chaired by: V. MUKHOPADHYAY, NASA Langley Research Center 1400 hrs 1430 hrs 1500 hrs 1530 hrs AIAA-2015-3096 AIAA-2015-3097 AIAA-2015-3098 AIAA-2015-3099 Composite Structure Modeling Numerical Simulation and Analysis Sensitivity Analysis towards A Vehicle Management End-to-End and Analysis of Advanced Aircraft of the Aircraft Pilot Seat Impact Probabilistic Re-Entry Modeling of Testing and Analysis Platform for Fuselage Concepts Resistance Spacecraft and Space Debris Validation of Mission and Fault V. Mukhopadhyay, M. Sorokach, NASA X. Zhang, X. Jinwu, M. Li, Beihang P. Mehta, University of Strathclyde, Glasgow, Management Algorithms to Reduce Langley Research Center, Hampton, VA University, Beijing, China; Y. Ren, Hunan United Kingdom; A. Walker, Los Alamos Risk for NASA’s Space Launch University, Changsha, China National Laboratory, Los Alamos, NM; M. System Brown, University of New South Wales at the L. Trevino, J. Patterson, D. Teare, S. Australian Defence Force Academy, Canberra, Johnson, NASA Marshall Space Flight Australia; E. Minisci, M. Vasile, University of Center, Huntsville, AL Strathclyde, Glasgow, United Kingdom Wednesday, 24 June 2015 215-MST-10 Sensor and Communications Systems Wyeth Chaired by: J. ZAMBRANO and Y. CHENG, AVIC Computing Technique Research Institute 1400 hrs 1430 hrs 1500 hrs AIAA-2015-3100 AIAA-2015-3101 AIAA-2015-3102 Simulation/Optimization Modeling Parallel Image Detail Enhancement The Key algorithm Research of for Robust Satellite Data Unit for For Real-time Applications Enhanced Vision System Base on Airborne Network Y. Cheng, W. Niu, Aviation Industry Corporation Embedded Parallel Computing J. Zambrano, O. Yeste-Ojeda, R. Landry, of China (AVIC), Xi’an, China; Z. Zhai, X. Jianchun, Aviation Industry Corporation Northwestern Polytechnical University, Xi’an,
97 University of Québec, Montréal, Canada of China (AVIC), Xi’an, China China; L. Zhang, Aviation Industry Corporation of China (AVIC), Xi’an, China Wednesday, 24 June 2015 216-TP-10/PDL-10 Plasma Computational Methods II Miro Chaired by: K. STEPHANI, University of Illinois at Urbana-Champaign and T. MOELLER, University of Tennessee Space Institute 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2015-3103 AIAA-2015-3104 AIAA-2015-3105 AIAA-2015-3106 AIAA-2015-3107 AIAA-2015-3108 Computational Simulations of TP3 Simulation of Plasma Flow Control: MG-local-PCA Method for the Reduced-Order Models of Low- Enthalpy Characterization and Numerical Simulation of Two- Arc-Jet Facility Flow A New Computationally Efficient Reduction of a Collisional-Radiative Temperature Gas Discharges in Assessment of Copper Catalysis Dimensional Structure of Glow T. Gokcen, ERC, Inc., Moffett Field, CA; Approach Argon Plasma Mechanism Glow Mode Determination in Inductively Discharge in Molecular Hydrogen J. Balboni, NASA Ames Research Center, B. Parent, Pusan National University, Busan, A. Bellemans, T. Magin, von Kármán E. Cisneros, L. Massa, University of Texas, Coupled Plasma Facility S. Surzhikov, D. Storozhev, Russian Moffett Field, CA; A. Alunni, ERC, Inc., South Korea; S. Macheret, Purdue University, Institute for Fluid Dynamics, Rhode-Saint- Arlington, Arlington, TX A. Viladegut, von Kármán Institute for Academy of Sciences, Moscow, Russia Moffett Field, CA West Lafayette, IN; M. Shneider, Princeton Genèse, Belgium; G. Degrez, A. Parente, Fluid Dynamics, Rhode-Saint-Genèse, University, Princeton, NJ University of Brussels, Brussels, Belgium Belgium Wednesday, 24 June 2015 217-TP-11 Aerothermodynamics III Rosetta Chaired by: T. LAM, The Aerospace Corporation 1400 hrs 1430 hrs 1500 hrs 1530 hrs AIAA-2015-3109 AIAA-2015-3110 AIAA-2015-3111 AIAA-2015-3112 Global Aeroheating Measurements Aerothermodynamic Characteristics Radiative Heating on the After- Coupled Flow, Radiation, and Ablation of Shock-Shock Interactions on a of 16-22 km/s Earth Entry Body of Martian Entry Vehicles Simulations of Atmospheric Entry Swept Cylinder C. Johnston, NASA Langley Research A. Brandis, B. Cruden, T. White, D. Vehicles using the Hybrid Statistical M. Mason, S. Berry, NASA Langley Center, Hampton, VA; A. Brandis, ERC, Saunders, ERC, Inc., Moffett Field, CA; C. Narrow Band Model Research Center, Hampton, VA Inc., Moffett Field, CA Johnston, NASA Langley Research Center, J. Scoggins, L. Soucasse, von Kármán Institute Hampton, VA for Fluid Dynamics, Rhode-Saint-Genèse, Belgium; P. Riviere, A. Soufiani, École Centrale de Paris, Paris, France; T. Magin, von Kármán Institute for Fluid Dynamics, Rhode-Saint- Genèse, Belgium Wednesday, 24 June 2015 218-NW-7 Networking Coffee Break Chantilly Ballroom East 1530 - 1600 hrs Wednesday, 24 June 2015 219-RLA-2 Rising Leaders in Aerospace: Leadership Exchange/Speed Networking Metropolitan Ballroom 1530 - 1700 hrs Get your questions answered! Senior Mentors will include: Russ Althof Cees Bil Dave Bowles Ed Feltrop Susan Gorton Peter Hartwich Janice Kavandi 98 Chief Engineer Professor, Royal Melbourne Institute Center Director (Acting) Engineer Specialist Rotary Wing Project Engineering Manager Deputy Director Raytheon Missile Systems of Technology NASA Langley Research Center Cessna Aircraft Company NASA Langley Research Center Boeing Defense, Space and Security NASA Glenn Research Center Jeff Jepson Samantha A. Magill Sandy Magnus David McBride Charles Smith John Valasek Senior Multi-Disciplined Engineer I Academic Affairs and Inclusion & Diversity Executive Director Center Director Center Director (Acting) Professor/Director, Vehicle Systems & Control Raytheon Missile Systems Honda Aircraft Company AIAA NASA Armstrong Flight Research Center NASA Ames Research Center Laboratory Texas A&M University
Wednesday, 24 June 2015 220-LEC-3 Aerodynamics Award Lecture Chantilly Ballroom West 1630 - 1730 hrs
Still Trying to Understand Aircraft Vortices Russell M. Cummings Professor of Aeronautics Department of Aeronautics U.S. Air Force Academy Wednesday, 24 June 2015 221-LEC-4 Aeroacoustics Lecture Chantilly Ballroom West 1730 - 1830 hrs
Fan Broadband Noise Generation and Suppression Edmane Envia Aeroacoustics Branch NASA Glenn Research Center Wednesday, 24 June 2015 222-LEC-5 Thermophysics Award Lecture Grand Ballroom E 1730 - 1830 hrs
Aerodynamics and Heat Transfer in Gas Turbine Cooling-Recent Advances Sumanta Acharya Ring Chair & Professor Mechanical Engineering Department University of Memphis Wednesday, 24 June 2015 223-BANQ-1 Aeroacoustics Awards Reception and Banquet Imperial Ballroom 1900 - 2030 hrs
The 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 at on site as space is available. Thursday Thursday, 25 June 2015 224-SB-4 Speakers’ Briefing Session Rooms 0730 - 0800 hrs Thursday, 25 June 2015
99 225-PLNRY-4 Plenary Keynote Chantilly Ballroom West 0800 - 0900 hrs
DHS’s Perspectives on Cybersecurity in Aviation Gregory J. Touhill Deputy Assistant Secretary for Office of Cybersecurity and Communications Department of Homeland Security Thursday, 25 June 2015 226-AA-31 Interior Noise Edelweiss Chaired by: N. AGARWAL, Boeing Defense, Space & Security 0900 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs Oral Presentation AIAA-2015-3113 AIAA-2015-3114 AIAA-2015-3115 AIAA-2015-3116 AIAA-2015-3117 Poroelastic Acoustic Meta Materials (Invited) Low Frequency Noise Reduction Identification of sources of noise in the Fuselage Excitation During Cruise Effect of pressure gradients on Effect of pressure gradients on C. Fuller, Virginia Polytechnic Institute and State University, Blacksburg, VA Using Poro-Elastic Acoustic cabin and the definition of the local Flight Conditions: Measurement turbulent boundary layer vortical turbulent boundary layer noise and Metamaterials passage of sound energy through and Prediction of Pressure Point structures and wall-pressure wall-pressure fluctuations A. Slagle, C. Fuller, Virginia Polytechnic fuselage based on the results of Spectra fluctuations E. Cohen, X. Gloerfelt, Paris Institute of Institute and State University, Blacksburg, VA in-flight measurements of the Superjet A. Klabes, M. Herr, C. Appel, German M. Alaoui, X. Gloerfelt, Paris Institute of Technology, Paris, France R. Abdrashitov, Sukhoi Civil Aircraft Company, Aerospace Center (DLR), Braunschweig, Technology, Paris, France; O. Collery, M. Moscow, Russia; A. Golubev, TsAGI, Germany; M. Bouhaj, Airbus Operations Etchessahar, Airbus, Toulouse, France Zhukovsky, Russia GmbH, Hamburg, Germany Thursday, 25 June 2015 227-AA-32 Jet Noise Measurements III Fleur-de-lis A Chaired by: D. PAPAMOSCHOU, University of California Irvine 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2015-3118 AIAA-2015-3119 AIAA-2015-3120 AIAA-2015-3121 AIAA-2015-3122 AIAA-2015-3123 Installed jet-flap impingement Noise measurements of high aspect Measurements and Predictions of Flow Field and Acoustic An Experimental Study of Coaxial Jets Experimental and numerical study tonal noise ratio distributed exhaust systems the Noise from Three-Stream Jets Investigations of the Launch Vehicle Using Acoustic PIV and LDA Methods of the noise generation in an J. Lawrence, R. Self, University of J. Bridges, M. Wernet, NASA Glenn B. Henderson, S. Leib, NASA Glenn Environment during Lift-off (CoJeN) outflow butterfly valve Southampton, Southampton, United Research Center, Cleveland, OH Research Center, Cleveland, OH K. Natarajan, L. Venkatakrishnan, National C. Mead, Aero Acoustics, Ltd., Elstead, United A. Chauvin, Y. Pasco, M. Sanjose, G. Kingdom Aerospace Laboratories, Bangalore, India Kingdom; C. Wrighton, QinetiQ, Farnborough, Lobel, A. Marsan, S. Moreau, University of United Kingdom; K. Britchford, Rolls-Royce Sherbrooke, Sherbrooke, Canada; et al. Group plc, Derby, United Kingdom Thursday, 25 June 2015 228-AA-33 Jet Noise Modeling II Fleur-de-lis B Chaired by: C. BROWN, NASA Glenn Research Center 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2015-3124 AIAA-2015-3125 AIAA-2015-3126 AIAA-2015-3127 AIAA-2015-3128 AIAA-2015-3129 AIAA-2015-3130 Nonlinear interaction analysis of Linear Stability Implications of On the Comparison of the Long Theoretical Modelling Of Empirical Models for the Shielding Computational modelling of jet-wing Refraction Effect in Correlation subsonic jet instabilities with forced Mean Flow Variations in Turbulent Penetration Mode (LPM) Supersonic Broadband Shock Associated Noise and Reflection of Jet Mixing Noise interaction: the effect of asymmetries Model of Quadrupole Noise Sources eigenmodes using PSE Jets Issuing from Serrated Nozzles Counterflowing Jet to the in Asymmetric Jets by a Surface from the jet inflow conditions and in Turbulent Jet M. Itasse, J. Brazier, O. Léon, G. Casalis, A. Sinha, Indian Institute of Technology Supersonic Screech Jet A. Kalyan, S. Karabasov, Queen Mary C. Brown, NASA Glenn Research Center, the wing V. Kopiev, S. Chernyshev, TsAGI, Moscow, ONERA, Toulouse, France Bombay, Mumbai, India; T. Colonius, R. Farr, NASA Marshall Space Flight University of London, London, United Cleveland, OH V. Semiletov, Queen Mary University of Russia California Institute of Technology, Center, Huntsville, AL; C. Chang, NASA Kingdom London, London, United Kingdom; P. Yakovlev, Pasadena, CA Langley Research Center, Hampton, VA; J. North-Eastern Federal University, Yakutsk,
100 Jones, AI Signal Research, Inc., Huntsville, Russia; S. Karabasov, Queen Mary University AL; N. Dougherty, ERC, Inc., Huntsville, AL of London, London, United Kingdom; G. Faranosov, V. Kopiev, TsAGI, Moscow, Russia Thursday, 25 June 2015 229-AA-34 CAA Numerical Techniques III Inverness Chaired by: S. ARUNAJATESAN, Sandia National Labs 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2015-3131 AIAA-2015-3132 AIAA-2015-3133 AIAA-2015-3134 AIAA-2015-3135 A study of accuracy on numerical Aeroacoustic Calculations of the A direct-hybrid method for Hybrid MacCormack-type Schemes Development of compressible large- methods for nonuniform meshes 30P30N High-lift Airfoil using Hybrid computational aeroacoustics for Computational Aeroacoustics eddy simulations combining high- (Invited) RANS/LES methods: Modeling and M. Schlottke, H. Cheng, V. Pauz, M. S. Yazdani, D. Hixon, University of Toledo, order schemes and wall modeling F. Hu, Old Dominion University, Norfolk, Grid Resolution Effects Meinke, W. Schroeder, RWTH Aachen Toledo, OH S. Le Bras, CERFACS, Toulouse, France; H. VA; A. Fernando, Norfolk State University, M. Terracol, E. Manoha, ONERA, Châtillon, University, Aachen, Germany Deniau, ONERA, Toulouse, France; C. Bogey, Norfolk, VA France; M. Murayama, K. Yamamoto, Japan École Centrale de Lyon, Ecully, France; G. Aerospace Exploration Agency (JAXA), Tokyo, Daviller, CERFACS, Toulouse, France Japan Thursday, 25 June 2015 230-AA-35 Airframe Noise IV Lalique Chaired by: T. VAN DE VEN, Gulfstream 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2015-3136 AIAA-2015-3137 AIAA-2015-3138 AIAA-2015-3139 AIAA-2015-3140 AIAA-2015-3141 AIAA-2015-3142 Influence of Spanwise Boundary LEISA2: an experimental database for Experimental study of the effect of Slat Noise Prediction using Hybrid Large-Scale Studies on Slat Noise Study on Noise Generation from On the Noise Generation of Conditions on Slat Noise the validation of numerical predictions a small 2D excrescence placed on RANS-LES methods on Structured Reduction Slat Tracks Using a High-Lift Wing Krueger Leading Edge Devices Simulations of slat unsteady flow and noise the slat cove surface of an airfoil and Unstructured Grids M. Herr, M. Pott-Pollenske, R. Ewert, Model M. Pott-Pollenske, J. Wild, German D. Lockard, M. Choudhari, P. Buning, NASA E. Manoha, ONERA, Châtillon, France; M. on its acoustic noise N. Ashton, University of Manchester, B. Dirk, J. Siebert, J. Delfs, German M. Murayama, Y. Yokokawa, Y. Ito, K. Aerospace Center (DLR), Braunschweig, Langley Research Center, Hampton, VA Pott-Pollenske, German Aerospace Center F. Amaral, D. Souza, C. Pagani, M. Manchester, United Kingdom; A. West, Aerospace Center (DLR), Braunschweig, Yamamoto, T. Takaishi, H. Ura, Japan Germany (DLR), Braunschweig, Germany Medeiros, University of São Paulo, São CD-adapco, London, United Kingdom; F. Germany; et al. Aerospace Exploration Agency (JAXA), José dos Campos, Brazil Mendonca, Self, London, United Kingdom Mitaka, Japan Thursday, 25 June 2015 231-AA-36 General Acoustics III Obelisk A Chaired by: C. SCHRAM 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2015-3143 AIAA-2015-3144 AIAA-2015-3145 AIAA-2015-3146 AIAA-2015-3147 AIAA-2015-3148 Experimental Application of Experimental Investigation of the An Experimental Study of On the Relevance of Convection Flow Noise Generation of Cylinders An experimental investigation of Aeroacoustic Time-Reversal Unsteady Pressure on a Hydrofoil Composite Materials for the Design Effects for a Laser-Generated with Soft Porous Cover wall pressure fluctuations beneath A. Mimani, D. Moreau, C. Doolan, due to the Ingestion of Turbulence of Quiet UAVs Sound Source T. Geyer, E. Sarradj, G. Herold, pressure gradients University of Adelaide, Adelaide, Australia and Hydro-elastic Motion J. Callicoat, R. Gaeta, J. Jacob, Oklahoma K. Rossignol, J. Delfs, L. Rossian, F. Brandenburg University of Technology, E. Salze, C. Bailly, O. Marsden, E. M. Catlett, J. Anderson, Naval Surface State University, Stillwater, OK Boden, German Aerospace Center (DLR), Cottbus, Germany Jondeau, D. Juve, École Centrale de Lyon, Warfare Center, West Bethesda, MD Braunschweig, Germany Ecully, France
101 Thursday, 25 June 2015 232-ACD-6 Conceptual Aircraft Design Working Group (CADWG21) Panel Wyeth 0900 - 1200 hrs Chaired by: W. ANEMAAT, DARcorporation and T. TAKAHASHI, Arizona State University
The Need of Community-Accepted Public Domain / Open Source Sizing Codes Panelists: Clif Davis Jason Welstead Joaquim Martins Mark Page Steve Komadina Rob McDonald Lockheed Martin Aeronautics NASA Langley University of Michigan DZYNE Technologies Northrop-Grumman CalPoly
Thursday, 25 June 2015 233-APA-25 Applied CFD & Numerical Correlations with Experimental Data III Stemmons B Chaired by: K. ABDOL-HAMID, NASA Langley Research Center and A. SCLAFANI, Boeing Engineering Operations & Technology 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2015-3149 AIAA-2015-3150 AIAA-2015-3151 AIAA-2015-3152 AIAA-2015-3153 Time-Accurate Unsteady Pressure Continuous Radial Jet in Annular Simulation of a Flapping Wing UAV Output-Based Adaptive Meshing Improvement of CFD results of NASA Loads Simulated for the Space Launch Cross-flow using a Coupled CFD-Control Tool Applied to Space Launch System CRM by on-line mesh deformation System at Wind Tunnel Conditions P. Rajput, I. Kalkhoran, NYU Polytechnic J. Geder, R. Ramamurti, K. Viswanath, Naval Booster Separation Analysis using modal analysis of a wing S. Alter, G. Brauckmann, W. Kleb, C. Streett, School of Engineering, Brooklyn, NY Research Laboratory, Washington, DC D. Dalle, Science and Technology Corporation, P. Vrchota, A. Prachar, Aerospace Research and C. Glass, D. Schuster, NASA Langley Research Moffett Field, CA; S. Rogers, NASA Ames Test Establishment, Prague, Czech Republic Center, Hampton, VA Research Center, Moffett Field, CA Thursday, 25 June 2015 234-APA-26 Unmanned, Bio-Inspired, Solar Powered Aerial Vehicle Designs II Carpenter Ballroom Chaired by: M. OL, US Air Force Reseach Laboratory and A. MITTAL, The University of Tennessee at Chattanooga 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2015-3154 AIAA-2015-3155 AIAA-2015-3156 AIAA-2015-3157 AIAA-2015-3158 Dynamical Characterization of a Numerical Simulation of a Flapping Aerodynamics of Southern Hawker Development and Analysis of Gull Development and Aero-structural Bio-Inspired Wing with Passively Wing in Ansys-Fluent Based on the Dragonfly: Aeshna cyanea Inspired UAV Flapping Wing Analysis of Light and Strong Actuated Edges Fruit Fly Wing Kinematics S. Srigrarom, C. Thipyopas, Kasetsart D. Kumar, T. Goyal, S. Vemuri, P. Mohite, Carbon Fiber-CNT/PP Hummingbird C. Planck, F. Siala, J. Liburdy, Oregon B. Nieto, X. Alfonso, K. Basto, J. Escobar, University, Bangkok, Thailand S. Kamle, Indian Institute of Technology Inspired MAV Wings State University, Corvallis, OR University of San Buenaventura, Bogota, Kanpur, Kanpur, India D. Kumar, S. Kumar, T. Goyal, P. Mohite, Colombia S. Kamle, Indian Institute of Technology Kanpur, Kanpur, India Thursday, 25 June 2015 235-APA-27 Airfoil/Wing/Configuration Aerodynamics Stemmons C Chaired by: A. MCCOMAS, TLG Aerospace and J. GUGLIELMO, Boeing Defense, Space & Security 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2015-3159 AIAA-2015-3160 AIAA-2015-3161 AIAA-2015-3162 AIAA-2015-3163 AIAA-2015-3164 Improved Stall Prediction for Modeling and Prediction of On the resulting aerodynamic Aero-Propulsive Coupling of an Aerodynamic Performance of the Computational Assessment Swept Wings Using Low-Order the Crossflow Transition Using loss of combinations of localized Embedded, Distributed Propulsion Adaptive Nacelle Inlet of Rainfall Effects on Aircraft Aerodynamics Transition Transport Equations surface roughness patches on a System F. Majić, G. Efraimsson, C. O’Reilly, Royal Aerodynamic Characteristics P. Hosangadi, R. Paul, A. Gopalarathnam, J. Sa, S. Park, Konkuk University, Seoul, turbine blade M. Kerho, Rolling Hills Research Institute of Technology (KTH), Stockholm, H. Sharma, S. Harshe, S. Vekaria, M. North Carolina State University, Raleigh, NC South Korea; K. Cho, Korea University P. Gilge, K. Mulleners, Leibniz University, Corporation, El Segundo, CA Sweden Singh, M. Damodaran, Indian Institute of Science and Technology, Daejeon, Hannover, Germany of Technology Gandhinagar, Ahmedabad, South Korea; K. Jung, Agency for Defense India; B. Khoo, National University of
102 Development, Daejeon, South Korea Singapore, Singapore, Singapore Thursday, 25 June 2015 236-APA-28 Unsteady Aerodynamics I Stemmons A Chaired by: K. KARA, Khalifa University of Science, Technology & Research and J. RAULEDER, Technical University of Munich 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2015-3165 AIAA-2015-3166 AIAA-2015-3167 AIAA-2015-3168 AIAA-2015-3169 AIAA-2015-3170 AIAA-2015-3171 Measurements of Dynamic An Experimental Study of Added Experimental-Based Unified Experimental Dynamic Stall study Unsteady Aerodynamic Modeling Subsonic Indicial Aerodynamics Implementation of Vortex-type Interface Between Ship and Mass on a Plunging Airfoil Unsteady Nonlinear Aerodynamic on a low Reynolds number airfoil of Rolling Parachutes Using the for Unsteady Loads Calculation via Gust Model Through Boundary Helicopter Air Wakes Oscillating with High Frequencies at Modeling For Two-Dimensional S. Algozino, J. Marañon Di Leo, J. Indicial Method Numerical and Analytical Conditions C. Friedman, George Washington High Angles of Attack Airfoils Delnero, G. Capittini, National University of M. Ghoreyshi, U.S. Air Force Academy, Methods: a Preliminary Assessment E. Eljack, I. AlQadi, King Abdulaziz University, Washington, DC; M. Snyder, M. Zakaria, Virginia Polytechnic Institute M. Zakaria, Virginia Polytechnic Institute La Plata, La Plata, Argentina Colorado Springs, CO; K. Bergeron, Army M. Righi, Zurich University of Applied University, Jeedah, Saudi Arabia U.S. Naval Academy, Annapolis, MD and State University, Blacksburg, VA; and State University, Blacksburg, VA; Research, Development and Engineering Sciences, Winterthur, Switzerland; M. D. Pereira, University of São Paulo, São H. Taha, University of California, Irvine, Command, Natick, MA; J. Seidel, A. Berci, University of Leeds, Leeds, United Paulo, Brazil; S. Ragab, M. Hajj, Virginia Irvine, CA; M. Hajj, A. Hussein, Virginia Lofthouse, R. Cummings, U.S. Air Force Kingdom; J. Koch, Zurich University of Polytechnic Institute and State University, Polytechnic Institute and State University, Academy, Colorado Springs, CO Applied Sciences, Winterthur, Switzerland Blacksburg, VA; F. Marques, University of Blacksburg, VA São Paulo, São Paulo, Brazil Thursday, 25 June 2015 237-ASE-3 Aircraft Wake Turbulence I (Invited) Plum Blossom B Chaired by: M. PRUIS, Northwest Research Associates Inc and N. AHMAD, NASA Langley Research Center 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2015-3172 AIAA-2015-3173 AIAA-2015-3174 AIAA-2015-3175 AIAA-2015-3176 AIAA-2015-3177 Use of Simple Models to Determine Multi-Model Ensemble Wake Vortex Wind Impact on Single Vortices and Sensitivity Analysis of Aircraft Assessment of WakeMod 4: A New Observations of Wake Vortices from Wake Vortex Categories for New Prediction (Invited) Counter-Rotating Vortex Pairs in Encounters with Deformed Wake Standalone Wake Vortex Algorithm Upward Looking Pulsed Doppler Aircraft (Invited) S. Koerner, German Aerospace Center (DLR), Ground Proximity (Invited) Vortices (Invited) for Estimating Circulation Strength Lidar Data (Invited) J. Hallock, Department of Transportation, Oberpfaffenhofen, Germany; N. Ahmad, F. Holzäpfel, N. Tchipev, A. Stephan, D. Bieniek, R. Luckner, Technical University and Position (Invited) M. Pruis, D. Delisi, NorthWest Research Cambridge, MA; G. Greene, J. Tittsworth, NASA Langley Research Center, Hampton, German Aerospace Center (DLR), of Berlin, Berlin, Germany D. Jacob, Coherent Research Group, Associates, Redmond, WA; D. Jacob, P. Strande, Federal Aviation Administration, VA; F. Holzäpfel, German Aerospace Center Oberpfaffenhofen, Germany Ormond Beach, FL; D. Lai, M. Pruis, D. Coherent Research Group, Ormond Washington, DC; F. Wang, Department of (DLR), Oberpfaffenhofen, Germany; R. Delisi, NorthWest Research Associates, Beach, FL Transportation, Cambridge, MA VanValkenburg, NASA Langley Research Redmond, WA Center, Hampton, VA Thursday, 25 June 2015 238-ATIO-21 En Route Operations Milan Chaired by: M. KOCH, NASA Langley Research Center 0900 hrs 0930 hrs 1000 hrs AIAA-2015-3178 AIAA-2015-3179 AIAA-2015-3180 Controller Workload-based Optimization of the Cruise Regime Can ground-based separation Calculation of Monitor Alert of Flight Airplane Trajectory using accommodate very high en route Parameters for En Route Sectors Deterministic Algorithms traffic demand as well as advanced B. Marr, K. Lindsay, MITRE Corporation, M. Gautier, R. Botez, University of self-separation? McLean, VA Québec, Montréal, Canada H. Blom, B. Bakker, National Aerospace
103 Laboratory (NLR), Amsterdam, The Netherlands Thursday, 25 June 2015 239-ATIO-22 ATM V - Performance Assessment Morocco Chaired by: D. DELAURENTIS, Purdue University 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2015-3181 AIAA-2015-3182 AIAA-2015-3183 AIAA-2015-3184 AIAA-2015-3185 AIAA-2015-3186 AIAA-2015-3187 Verifying Required Communication Methodology to Define Delivery Investigation of Connectivity: Regional Sky Transit An Airport Assessment Approach in Modeling a Ramp Area Support Framework Development for Performance in Air Traffic Accuracy Under Current Day ATC Definition, Application, and B. Seeley, CAFE Foundation, Santa the Conceptual Design Stage System Performance Evaluation of the Management Operations Formulation Rosa, CA M. Weiss, N. Dzikus, German Aerospace A. Wing, W. Felder, R. Cloutier, Stevens Future National Airspace System D. Zeng, J. Gonda, MITRE Corporation, S. Sharma, J. Robinson III, NASA Ames L. Bowers, L. Mockus, S. Tamaskar, D. Center (DLR), Hamburg, Germany Institute of Technology, Hoboken, NJ M. Hassan, A. Payan, H. Pfaender, D. McLean, VA Research Center, Moffett Field, CA DeLaurentis, Purdue University, West Mavris, E. Garcia, J. Schutte, Georgia Lafayette, IN Institute of Technology, Atlanta, GA Thursday, 25 June 2015 240-ATIO-23 Transformational Flight - Electric Propulsion Monet Ballroom Chaired by: S. GINN, NASA 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs Oral Presentation Oral Presentation AIAA-2015-3188 AIAA-2015-3189 AIAA-2015-3190 AIAA-2015-3191 HEIST LEAPTech Instrumentation LEAPTech HEIST Power Architecture Comparison of CFD and A Conceptual Approach to Flight- Optimal Propeller Pitch Scheduling Modeling and Test of the Efficiency Design, Development, and Initial and Testing Experimental Results of the Training Mission and Cost Analysis and Propeller--Airframe Matching of Electronic Speed Controllers for Results S. Clarke, Y. Lin, A. Samuel, K. LEAPTech Distributed Electric of an All-Electric Aircraft Equipped for Conceptual Design Brushless DC Motors T. Foster, Empirical Systems Aerospace, Papathakis, NASA Armstrong Flight Propulsion Blown Wing with Regenerative Energy Devices R. McDonald, California Polytechnic State C. Green, R. McDonald, California Inc., Pismo Beach, CA Research Center, Edwards, CA A. Stoll, Joby Aviation, Santa Cruz, CA M. Olson, Georgia Institute of Technology, University, San Luis Obispo, CA Polytechnic State University, San Luis Atlanta, GA Obispo, CA Thursday, 25 June 2015 241-CFD-26 Unstructured High-Order Methods III Grand Ballroom A Chaired by: R. HARRIS, CFD Research Corporation and B. JOLLY, US Air Force 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2015-3192 AIAA-2015-3193 AIAA-2015-3194 AIAA-2015-3195 AIAA-2015-3196 Development of Vertex-Centered, A compact high order finite volume Locally-Defined High-Resolution High-Order Compressible Flow A new high-order unstructured High-Order Schemes and method for hyperbolic conservation Scheme for Shock-Capturing Simulations with the Unstructured numerical scheme for large eddy Implementation in FUN3D laws on unstructured grids Problems on Unstructured Cartesian Spectral Difference Method simulation H. Yang, R. Harris, CFD Research Q. Wang, Y. Ren, Tsinghua University, Grids F. Moreira, C. Breviglieri, Technological Z. Xu, University of Science and Technology, Corporation, Huntsville, AL Beijing, China; W. Li, Sun Yat-Sen Y. Tamaki, T. Imamura, University of Institute of Aeronautics (ITA), São Hefei, China; Q. Zhao, Chinese Academy of University, Guangzhou, China Tokyo, Tokyo, Japan José dos Campos, Brazil; J. Azevedo, Sciences, Beijing, China; Q. Lin, University of Aeronautics and Space Institute (IAE), São Science and Technology, Hefei, China; J. Xu, José dos Campos, Brazil Chinese Academy of Sciences, Beijing, China Thursday, 25 June 2015 242-CFD-27 Current Trends in CFD Research II (Invited) Grand Ballroom B Chaired by: H. HUYNH, NASA Glenn Research Center and Z. WANG, University of Kansas 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs Oral Presentation AIAA-2015-3197 AIAA-2015-3198 Oral Presentation Oral Presentation AIAA-2015-3199 Theoretical Aspects of High-Order Well Posed Problems and Boundary Opportunities for efficient high-order Role of Entropy-Residual in High- Large Eddy Simulations Multi-dimensional Limiting Strategy Flux Reconstruction Schemes Conditions in Computational Fluid methods based on the summation-by- Order Numerical Methods for Gas- of Turbulent Flows Using for Higher-order CFD Methods - (Invited) Dynamics (Invited) parts property (Invited) Dynamics Calculations: Shock Detector Discontinuous High Order Methods Progress and Issue (Invited) P. Vincent, Imperial College London, J. Nordstrom, Linköping University, J. Hicken, Rensselaer Polytechnic Institute, and Adaptation Indicator (Invited) (Invited) C. Kim, Seoul National University, Seoul, London, United Kingdom Linköping, Sweden Troy, NY; D. Del Rey Fernández, D. Zingg, M. Ihme, Y. Lv, Stanford University, Stanford, Z. Wang, University of Kansas, Lawrence, South Korea; J. Park, Imperial College University of Toronto, Toronto, Canada CA Lawrence, KS London, London, United Kingdom 104 Thursday, 25 June 2015 243-CFD-28 Incompressible and Low Speed Flows Plum Blossom A Chaired by: M. YU, University of Maryland, Baltimore County and R. RAJAGOPALAN, Iowa State University 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2015-3200 AIAA-2015-3201 AIAA-2015-3202 AIAA-2015-3203 AIAA-2015-3204 AIAA-2015-3205 AIAA-2015-3206 High-Order Strand Grid Methods An Explicit Pressure-Based A Turbulent Low-Speed Comparison of Pressure-Based Applying Non-Reflecting Boundary Generalised SIMPLE-Based Pressure Robustness to Inaccurate Initial for Low Mach and Incompressible Algorithm for Incompressible Flows Preconditioner for Unsteady Flows Runge-Kutta Schemes for Unsteady Conditions in Pressure-Based Correction Method for Unstructured Conditions in Low Mach Preconditioned Flows D. Garrick, R. Rajagopalan, Iowa State About Wind Turbine Airfoils Incompressible Flows Solvers Co-located Grids Density-Based Methods J. Thorne, A. Katz, Utah State University, University, Ames, IA R. Djeddi, K. Ekici, University of M. Fischels, R. Rajagopalan, Iowa State V. Ivanov, B. Makarov, ANSYS, Inc., V. Przulj, Ricardo Software, Shoreham by C. Falcão, University of Rio Grande do Sul, Logan, UT Tennessee, Knoxville, Knoxville, TN University, Ames, IA Lebanon, NH Sea, United Kingdom Porto Alegre, Brazil; F. Medeiros, Military Institute of Engineering (IME), Rio de Janeiro, Brazil; L. Alves, Fluminese Federal University (UFF), Niterói, Brazil Thursday, 25 June 2015 244-CFD-29 High-Speed and Reacting Flows Coral Chaired by: G. CANDLER, University of Minnesota and B. RATHAKRISHNAN, GE Global Research 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2015-3207 AIAA-2015-3208 AIAA-2015-3209 AIAA-2015-3210 AIAA-2015-3211 AIAA-2015-3212 LES of reacting mixing layers: A Priori Analysis of a Compressible Numerical Investigations of Pulsed Ignition Characteristics in Spatially IDDES simulation of supersonic Three Dimensional Flow Analysis of influence of inflow conditions and Flamelet Model using RANS Data for a Fuel Injection into Supersonic Zero-, One- and Two-Dimensional combustion using flamelet a Cavity-Based Scramjet Combustor heat release Dual-Mode Scramjet Combustor Crossflow Laminar Ethylene Flames modeling R. Rouzbar, S. Eyi, Middle East Technical A. Kartha, P. Subbareddy, G. Candler, J. Quinlan, T. Drozda, NASA Langley Research N. Williams, R. Thompson, T. Moeller, M. Evans, P. Medwell, Z. Tian, University H. Wang, Y. Piao, J. Niu, Tsinghua University, Ankara, Turkey University of Minnesota, Minneapolis, Center, Hampton, VA; J. McDaniel, University University of Tennessee, Tullahoma, of Adelaide, Adelaide, Australia; A. University, Beijing, China Minneapolis, MN; P. Dimotakis, California of Virginia, Charlottesville, Charlottesville, Tullahoma, TN Frassoldati, A. Cuoci, A. Stagni, Technical Institute of Technology, Pasadena, CA VA; G. Lacaze, J. Oefelein, Sandia National University of Milan, Milan, Italy Laboratories, Livermore, CA Thursday, 25 June 2015 245-CFD-30 Inflow Turbulence for Wall-Bounded LES (Invited) Emerald Chaired by: N. BISEK, Air Force Reseach Laboratory and L. TAO, GE Global Research 0900 hrs 0930 hrs 1000 hrs 1030 hrs AIAA-2015-3213 AIAA-2015-3214 AIAA-2015-3215 Q&A Panel Discussion An Overview of Turbulent Inflow A Counter-Flow Force Based Method Generating Synthetic Boundary Conditions for Large to Generate Equilibrium Turbulent Inhomogeneous Turbulence from Eddy Simulations (Invited) Inflow Conditions (Invited) RANS Statistics (Invited) N. Dhamankar, G. Blaisdell, Purdue D. Gaitonde, M. Waindim, M. Adler, Ohio P. Batten, U. Goldberg, O. Peroomian, S. University, West Lafayette, IN; A. Lyrintzis, State University, Columbus, OH Chakravarthy, Metacomp Technologies, Embry-Riddle Aeronautical University, Inc., Agoura Hills, CA Daytona Beach, FL Thursday, 25 June 2015 246-FD-27 Turbulence Analysis Govenors Lecture Hall Chaired by: Z. ZHENG, The University of Kansas and S. SILTON, US Army Research Laboratory 0900 hrs 0930 hrs 1000 hrs AIAA-2015-3216 AIAA-2015-3217 AIAA-2015-3218 Single and Multiple-Point Analysis Nonlinear Time Series Analysis of Thermal non-equilibrium effects in of Velocity Fluctuations in a Velocity over NACA 2412 Three- turbulent compressible shear flows Detonation-Turbulence Interaction Dimensional Wing Using Large A. Neville, I. Nompelis, P. Subbareddy, S. Hussein, F. Lu, University of Texas, Eddy Simulation Data G. Candler, University of Minnesota, Arlington, Arlington, TX P. Chakraborty, A. Roy, Indian Institute of Minneapolis, Minneapolis, MN Technology Kharagpur, Kolkata, India
105 Thursday, 25 June 2015 247-FD-28 Transition Open Forum Sapphire 0900 - 1230 hrs Chaired by: H. REED, Texas A&M University Thursday, 25 June 2015 248-FD-29 Flow Control - Aerodynamics Senators Lecture Hall Chaired by: H. DONG, University of Virginia and E. WHALEN, Boeing Engineering Operations & Technology 0900 hrs 0930 hrs 1000 hrs 1030 hrs AIAA-2015-3219 AIAA-2015-3220 AIAA-2015-3221 AIAA-2015-3222 Three-dimensional Control via Mass Propulsive Performance and Vortex On the Effect of Rigid Swept Control of Tollmien-Schlichting Injection for Suppression of Cavity Interactions of Multiple Tandem Surface Waves on Turbulent Drag Waves Using Piezoelectrically Oscillations Foils Pitching In Line M. Denison, National Institute of Driven Oscillating Surface Y. Zhang, N. Arora, Y. Sun, L. Cattafesta, C. Yuan, G. Liu, Y. Ren, H. Dong, Aerospace, Hampton, VA; S. Wilkinson, H. Dell’Orso, B. Tuna, M. Amitay, K. Taira, Florida State University, University of Virginia, Charlottesville, P. Balakumar, NASA Langley Research Rensselaer Polytechnic Institute, Troy, NY Tallahassee, FL; L. Ukeiley, University of Charlottesville, VA Center, Hampton, VA Florida, Gainesville, Gainesville, FL Thursday, 25 June 2015 249-FT-1 Flight Testing Obelisk B Chaired by: K. GARMAN, Federal Aviation Administration and J. BRANDON, NASA-Langley Research Center 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2015-3223 AIAA-2015-3224 AIAA-2015-3225 AIAA-2015-3226 AIAA-2015-3227 A Framework for Applying the Current Hypersonic and Space Stall/Spin Flight Test Techniques Ground Minimum Control Speed Lateral-Directional Aerodynamic OODA Loop to Mission Control Vehicle Flight Test Instrumentation with COTS Model Aircraft and Flight (VMCG) Testing of Transport Model Identification of a Single- Room Execution Challenges Data Systems Aircraft Engine Propeller Aircraft Using J. Newcamp, U.S. Air Force Academy, J. Spravka, T. Jorris, 412th Test Wing, R. Bunge, F. Munera Savino, I. Kroo, P. Bolds-Moorehead, V. Chaney, The Partial Orthogonal Least Squares Colorado Springs, CO Edwards AFB, CA Stanford University, Stanford, CA Boeing Company, Seattle, WA; T. Lutz, S. J. Zanette, Brazilian Air Force, São Vaux, Airbus, Toulouse, France José dos Campos, Brazil; F. Almeida, Technological Institute of Aeronautics (ITA), São José dos Campos, Brazil Thursday, 25 June 2015 250-LTA-1 Lighter-than-Air Systems & Technologies I Steuben Chaired by: R. VAN TREUREN 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2015-3228 AIAA-2015-3229 AIAA-2015-3230 AIAA-2015-3231 AIAA-2015-3232 Design and Control of a Multi- Numerical Feasibility Analysis of Computational Modelling of Disturbance Rejection Based A Long Endurance, Highly vectored Thrust Airship the Extra-light Weight Structure Aerodynamic Characteristics of Path Following Control for A Maneuverable, Collaborative, L. Chen, Y. Wen, H. Zhou, X. Wang, Tensairity on Large Airships Airships in Arbitrary Motion Stratospheric Airship with Actuator Unmanned Airborne System P. Zhou, D. Duan, Shanghai Jiao Tong A. Suñol, T. Yang, D. Vucinic, Vrije A. Kanoria, K. Panchal, R. Dongre, M. Saturation W. King, D. Landrum, J. Alcorn, A. University, Shanghai, China Universiteit Brussel, Brussels, Belgium Damodaran, Indian Institute of Technology K. Yan, Z. Zheng, M. Zhu, Z. Wu, Beihang Jarzembski, University of Alabama, Gandhinagar, Ahmedabad, India University, Beijing, China Huntsville, Huntsville, AL 106 Thursday, 25 June 2015 251-MAO-8 Metamodeling II Manchester Chaired by: B. ROTH, Walla Walla Univ and J. HICKEN, Rensselaer Polytechnic Institute 0900 hrs 0930 hrs 1000 hrs 1030 hrs AIAA-2015-3233 AIAA-2015-3234 AIAA-2015-3235 AIAA-2015-3236 Adaptive Switching of Variable- Large-scale CFD Optimization Adaptive Variable-Fidelity Study of Hybrid Radial Basis Fidelity Models in Population-based based on the FFD Parametrization Aerodynamic Analysis and Design Function for Design Optimization Optimization Algorithms using the Multipoint Approximation for Tailless Aircraft under Model- Problems A. Mehmani, Syracuse University, Method in an HPC Environment Form Uncertainty R. Shi, L. Liu, T. Long, J. Liu, Beijing Syracuse, NY; S. Chowdhury, A. Messac, Y. Korolev, V. Toropov, Queen Mary Y. Jo, J. Park, C. Ocheltree, J. Choi, S. Institute of Technology, Beijing, China Mississippi State University, Mississippi University of London, London, United Choi, P. Raj, Virginia Polytechnic Institute State, MS Kingdom; S. Shahpar, Rolls-Royce Group and State University, Blacksburg, VA; et al. plc, Derby, United Kingdom Thursday, 25 June 2015 252-MAO-9 Shape and Topology I Madrid Chaired by: J. MARTINS, University of Michigan and R. KOLONAY, Air Force Research Laboratory/RQVC/WPAFB 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2015-3237 AIAA-2015-3238 AIAA-2015-3239 AIAA-2015-3240 AIAA-2015-3241 AIAA-2015-3242 Nonintrusive Continuum Sensitivity Three-Dimensional Piecewise- Multi-objective shape optimization Development of a Consistent The Research on Geometry Concurrent Subspace Optimization Analysis for Aerodynamic Shape Continuous Class-Shape of aircraft cabin ventilation Discrete Adjoint Solver in an Evolving Modeling Method Based on Three- Design of Hypersonic Cruise Vehicle Optimization Transformation of Wings components using adjoint CFD Aerodynamic Design Framework dimensional CST Parameterization C. Jing, S. Yuan-pei, China Aerodynamics M. Kulkarni, R. Canfield, M. Patil, Virginia E. Olson, NASA Langley Research Center, T. Köthe, S. Herzog, C. Wagner, German T. Albring, M. Sagebaum, N. Gauger, Technical Technology Research and Development Center, Polytechnic Institute and State University, Hampton, VA Aerospace Center (DLR), Göttingen, University of Kaiserslautern, Kaiserslautern, H. Su, L. Gu, C. Gong, Northwestern Mianyang, China Blacksburg, VA Germany Germany Polytechnical University, Xi’an, China Thursday, 25 June 2015 253-MST-11 Aircraft Systems Design, Verification and Validation Travertine Chaired by: G. CHATTERJI, NASA Ames Research Center 0900 hrs 1000 hrs AIAA-2015-3243 AIAA-2015-3245 ADDAM: An Object Oriented Data Dynamic model updating of Model for an Aircraft Design a simulation casing based on Environment in MATLAB experimental modal parameters S. Herbst, M. Hornung, Technical B. Jie, Q. Mei, C. Zhang, Aviation Industry University of Munich, Munich, Germany Corporation of China (AVIC), Zhuzhou, China Thursday, 25 June 2015 254-NW-8 Networking Coffee Break Chantilly Ballroom East 0900 - 0930 hrs Thursday, 25 June 2015 255-PDL-12 Aero-Optics Plasma Diagnostics Miro Chaired by: R. MILES, Princeton University and M. RENNIE, University of Notre Dame 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2015-3246 AIAA-2015-3247 AIAA-2015-3248 AIAA-2015-3249 AIAA-2015-3250 Aero-Optical Measurements of High- Non-intrusive Velocity and Density Numerical Investigation of Characterization of Flow Control Investigation of shock / turbulent Mach Supersonic Boundary Layers Measurements in Subsonic Aero-Optical Distortions over a Actuators Based on Spark boundary interaction unsteadiness S. Gordeyev, M. Rennie, University of Notre Turbulent Boundary Layer Hemisphere-on-Cylinder Turret Discharge Plasmas Using Particle with various obstructions for aero- Dame, Notre Dame, IN; A. Cain, Innovative J. Sontag, S. Gordeyev, University of Notre with Gaps Image Velocimetry optics Technology Applications Company, LLC, Dame, Notre Dame, IN
107 E. Mathews, K. Wang, M. Wang, E. B. Singh, M. Belmouss, S. Bane, Purdue M. White, Ohio Aerospace Institute, Chesterfield, MO; T. Hayden, U.S. Air Force Jumper, University of Notre Dame, Notre University, West Lafayette, IN Dayton, OH; M. Visbal, Air Force Research Academy, Colorado Springs, CO Dame, IN Laboratory, Wright-Patterson AFB, OH Thursday, 25 June 2015 256-TP-12 Detailed Molecular Process Modeling Rosetta Chaired by: R. WAGNILD, Sandia National Laboratories and T. SCHWARTZENTRUBER, University of Minnesota 0900 hrs 0930 hrs 1000 hrs 1030 hrs AIAA-2015-3251 AIAA-2015-3252 AIAA-2015-3253 AIAA-2015-3254 Vibrational Relaxation and Master Equation Study of Characterization of Vibrational and Direct molecular simulation
Dissociation of Oxygen in Molecule- Vibrational and Rotational Rotational Energy Transfer in N2-N2 of high-temperature nitrogen Atom Collisions Relaxation of Oxygen Dissociative Collisions Using the dissociation due to both N-N2 and D. Andrienko, I. Boyd, University of D. Andrienko, I. Boyd, University of Quasiclassical Trajectory Method N2-N2 collisions Michigan, Ann Arbor, Ann Arbor, MI Michigan, Ann Arbor, Ann Arbor, MI J. Bender, P. Valentini, I. Nompelis, T. P. Valentini, T. Schwartzentruber, Schwartzentruber, G. Candler, University of J. Bender, G. Candler, University of Minnesota, Minneapolis, Minneapolis, MN Minnesota, Minneapolis, Minneapolis, MN Thursday, 25 June 2015 257-F360-8 The Impact of Particle Image Velocimetry on Aerospace Technology Grand Ballroom E 0930 - 1200 hrs Moderator: Steven Beresh, Distinguished Member of the Technical Staff, Sandia National Laboratories Panelists: Ronald J. Adrian Susan Gorton Fulvio Scarano Miguel Visbal Regent’s Professor and Ira A. Fulton Professor of Mechanical and Aerospace Project Manager, Revolutionary Vertical Lift Technology Project Full Professor and Chair of Aerodynamics Principal Research Aerospace Engineer and Team Leader of Multidisciplinary Engineering NASA Langley Research Center Delft University of Technology Computational Aerodynamics, Aerospace Systems Directorate Arizona State University Air Force Research Laboratory Thursday, 25 June 2015 258-LNCH-3 Awards Luncheon: Celebrating Achievements in Aircraft and Atmospheric Systems Chantilly Ballroom West 1230 - 1400 hrs A ticket is required and included in the conference registration fee where indicated. Thursday, 25 June 2015 259-AA-37 Landing Gear Noise Edelweiss Chaired by: T. SPALT, NASA Langley Research Center 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs AIAA-2015-3255 AIAA-2015-3256 AIAA-2015-3257 AIAA-2015-3258 AIAA-2015-3259 Aeroacoustic Simulations of a Nose Nose landing gear flow and noise The Effect of Flow Circulation on The Effect of Strut Geometry on the Design of quieter landing gears Landing Gear using FUN3D on predictions on unstructured grid the Scattering of Landing Gear Inter-Wheel Flow for a Two-Wheel through lattice-Boltzmann CFD Pointwise Unstructured Grids using a cell-centered Navier-Stokes Noise Landing Gear simulations V. Vatsa, M. Khorrami, NASA Langley code T. Heffernon, D. Angland, X. Zhang, P. McCarthy, A. Ekmekci, University of T. Rougier, Safran Group, Vélizy-Villacoublay, Research Center, Hampton, VA; J. Rhoads, F. De La Puente, L. Sanders, F. Vuillot, E. M. Smith, University of Southampton, Toronto, Toronto, Canada France; Q. Bouvy, Safran Group, Gloucester, Pointwise, Inc., Fort Worth, TX; D. Manoha, ONERA, Châtillon, France Southampton, United Kingdom United Kingdom; D. Casalino, J. Appelbaum, Lockard, NASA Langley Research Center, Exa GmbH, Stuttgart, Germany; C. Kleinclaus, Hampton, VA Exa GmbH, Munich, Germany Thursday, 25 June 2015 260-AA-38 Fluid-Structure Interaction Fleur-de-lis A Chaired by: J. ALONSO-MIRALLES, UTC Aerospace Systems 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2015-3260 AIAA-2015-3261 AIAA-2015-3262 AIAA-2015-3263 AIAA-2015-3264 AIAA-2015-3265
108 A fast numerical framework Noise Produced by Fabric and Wire Acoustic scattering by finite Experimental Investigation of Flow- Rod-Airfoil Interaction Noise Comparison of Analytical, for acoustic scattering by 3D Mesh Covered Panels in Low-Speed composite plates Induced Panel Vibrations at Cruise Reduction Using Leading Edge Numerical, and Experimental poroelastic plates Anechoic Wind Tunnels A. Cavalieri, M. Donadon, Technological Mach Number Serrations Results for Unsteady Aerofoil W. Wolf, University of Campinas, W. Alexander, W. Devenport, Virginia Institute of Aeronautics (ITA), São José T. Berkefeld, C. Spehr, K. Ehrenfried, S. W. Chen, W. Qiao, L. Wang, F. Tong, Interaction Noise Campinas, Brazil; A. Cavalieri, Polytechnic Institute and State University, dos Campos, Brazil; W. Wolf, University of Haxter, German Aerospace Center (DLR), Northwestern Polytechnical University, L. Ayton, University of Cambridge, Technological Institute of Aeronautics Blacksburg, VA Campinas, Campinas, Brazil Göttingen, Germany; S. Kroeber, Daimler Xi’an, China; X. Wang, State Key Cambridge, United Kingdom; J. Gill, (ITA), São José dos Campos, Brazil AG, Stuttgart, Germany Laboratory of Aerodynamics, Mianyang, University of Southampton, Southampton, China United Kingdom; N. Peake, University of Cambridge, Cambridge, United Kingdom Thursday, 25 June 2015 261-AA-39 Fluid Acoustic Phenomena Fleur-de-lis B Chaired by: K. AHUJA, Georgia Institute of Technology 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs AIAA-2015-3266 AIAA-2015-3267 AIAA-2015-3268 AIAA-2015-3269 AIAA-2015-3270 Non-linear System Identification Vortex Scattering Effects on Numerical Investigation of the On the mechanisms of noise Noise Radiation from a Cylindrical Techniques for Determination Acoustic Wave Propagation Refraction Effects by Jet Flows reduction in aerofoil-turbulence Embossment Immersed in Turbulent of the Acoustic Properties of G. Ke, W. Li, Z. Zheng, University of in Anechoic Wind Tunnels, with interaction by using wavy leading Boundary Layer Flow Perforates Kansas, Lawrence, Lawrence, KS Application to NASA/LaRC Quiet edges B. Bryan, S. Glegg, Florida Atlantic University, H. Boden, Royal Institute of Technology Flow Facility S. Haeri, J. Kim, P. Joseph, University Boca Raton, FL; M. Awasthi, W. Alexander, W. (KTH), Stockholm, Sweden S. Redonnet, J. Bulte, ONERA, Châtillon, of Southampton, Southampton, United Devenport, Virginia Polytechnic Institute and France Kingdom State University, Blacksburg, VA Thursday, 25 June 2015 262-AA-40 Advanced Testing Techniques Inverness Chaired by: J. UNDERBRINK 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2015-3271 AIAA-2015-3272 AIAA-2015-3273 AIAA-2015-3274 AIAA-2015-3275 AIAA-2015-3276 Optimization of Microphone Advanced Background Subtraction Reducing the Effect of Transducer Beamforming-based noise level Impedance eduction of perforated Effects of Hologram Distance and Locations for Acoustic Liner Applied to Aeroacoustic Wind Mount Induced Noise on Aeroacoustic dereverberation solution for S1MA plates at low Stouhal numbers and Regularization Techniques on Various Impedance Eduction Tunnel Testing Wind Tunnel Testing Data with a New sonic wind-tunnel : metrology, high bias flow Mach number Methods of Nearfield Acoustic M. Jones, W. Watson, NASA Langley C. Bahr, NASA Langley Research Center, Transducer Mount Design methodology and validation V. Popie, E. Piot, ONERA, Toulouse, France; S. Holography Applied to Building Research Center, Hampton, VA; J. Hampton, VA; W. Horne, NASA Ames A. Herron, D. Reed, D. Nance, NASA Marshall F. Mery, ONERA, Modane, France; R. Tordeux, French National Institute for Research Leakage Detection/Quantification June, University of Florida, Gainesville, Research Center, Moffett Field, CA Space Flight Center, Huntsville, AL Davy, V. Fleury, J. Bulte, M. Rey, ONERA, in Computer Science and Control (INRIA), Pau, K. Chelliah, G. Raman, R. Muehleisen, Illinois Gainesville, FL Châtillon, France France; F. Simon, ONERA, Toulouse, France Institute of Technology, Chicago, IL Thursday, 25 June 2015 263-AA-41 CAA Numerical Techniques IV Lalique Chaired by: P. MORRIS, Pennsylvania State University 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs AIAA-2015-3277 AIAA-2015-3278 AIAA-2015-3279 AIAA-2015-3280 AIAA-2015-3281 Performance of the DGM for the Towards CAA Based Acoustic Wind High-Order Hybrid Cell-Centered A Spectral-BEM Formulation for A Stabilised High-Order Finite Linearized Euler Equations With Tunnel Corrections for Realistic Method for Computational Compact Sources Aeroacoustics Element Model for the Linearised Non-Uniform Mean-Flow Shear Layers Aeroacoustics G. Bernardini, Roma Tre University, Rome, Euler Equations M. Williamschen, G. Gabard, University J. Jiao, J. Delfs, J. Dierke, German M. Wang, R. Fattah, D. Angland, X. Italy; C. Testa, Italian Institute for Naval K. Hamiche, H. Bériot, Siemens, Leuven, of Southampton, Southampton, United Aerospace Center (DLR), Braunschweig, Zhang, University of Southampton, Hydrodynamic Research and Ship Model Belgium; G. Gabard, University of Kingdom Germany Southampton, United Kingdom Basin, Rome, Italy; M. Gennaretti, Roma Southampton, Southampton, United Tre University, Rome, Italy Kingdom 109 Thursday, 25 June 2015 264-AA-42 Fan Broadband Noise Prediction Obelisk A Chaired by: E. ENVIA, NASA Glenn Research Center 1400 hrs 1430 hrs 1500 hrs AIAA-2015-3282 AIAA-2015-3283 Panel Harmonic and Broadband Further Investigations Into a Low- Fan Broadband Noise Prediction Panel Separation of Noise from a Small Order Model of Fan Broadband E. Envia, NASA Glenn Research Center, Cleveland, OH; J. Coupland, University of Southampton, Southampton, United Kingdom Ducted Fan Noise A. Truong, D. Papamoschou, University of S. Grace, Boston University, Boston, MA California, Irvine, Irvine, CA
Thursday, 25 June 2015 265-ACD-7 Aircraft Subsystems, Integration, and Architectures Wyeth Chaired by: P. RAJ, Virginia Polytechnic Institute and State University and E. DIGIROLAMO, Lockheed Martin Aeronautics 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs AIAA-2015-3284 AIAA-2015-3285 AIAA-2015-3286 AIAA-2015-3287 AIAA-2015-3288 An Innovative All-Active Hybrid Dynamic Reconfiguration mechanism Development of an Integrated Major Aircraft Subsystem Effects on Design and Build of Swarm Actuation System for Distributed Integrated Modular UAS for Agricultural Imaging Gas Turbine Performance in More Quadrotor UAVs at UGS T. Röben, RWTH Aachen University, Avionics System Applications Electric Aircraft Architectures S. Srigrarom, H. Lin, Z. Saw, J. Zhang, Aachen, Germany Q. Gu, G. Wang, J. Wu, M. Wang, China N. Goli, B. Landrum, University of M. Ozcan, I. Chakraborty, D. Mavris, C. Lim, University of Glasgow, Singapore, National Aeronautical Radio Electronics Alabama, Huntsville, Huntsville, AL Georgia Institute of Technology, Atlanta, Singapore Research Institute, Shanghai, China GA Thursday, 25 June 2015 266-AMT-13/GT-13 The Impact of PIV on Aerospace Technology II Topaz Chaired by: S. BERESH, Sandia National Laboratories and K. LOWE, Virginia Tech 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs Oral Presentation Oral Presentation Oral Presentation Oral Presentation Oral Presentation Oral Presentation Oral Presentation Use of PIV to anchor computational Synergistic Interactions of High- PIV uncertainty: how good are PIV Tomographic and time-resolved PIV Applications in Supersonic PIV in gas turbine combustion A Tribute to Ron Adrian: Three analysis of free shear and wall Resolution CFD and PIV to Reveal measurements? (Invited) PIV: Adding dimensions to flow Combustion Wind Tunnels at AFRL chambers: New insights into flow Decades of PIV Innovation (Invited) bounded flows (Invited) Complex Unsteady Flow Physics A. Sciacchitano, F. Scarano, Delft diagnostics (Invited) (Invited) physics and its importance for S. Gogineni, Spectral Energies, LLC, D. Gaitonde, Ohio State University, (Invited) University of Technology, Delft, The K. Lynch, F. Scarano, Delft University of S. Peltier, C. Carter, Air Force Research combustor development Dayton, OH Columbus, OH M. Visbal, Air Force Research Laboratory, Netherlands Technology, Delft, The Netherlands Laboratory, Wright-Patterson AFB, OH M. Stohr, I. Boxx, O. Lammel, K. Oberleithner, Wright-Patterson AFB, OH C. Arndt, W. Meier, German Aerospace Center (DLR), Stuttgart, Germany Thursday, 25 June 2015 267-APA-29 Innovative Aerodynamic Concepts & Designs Carpenter Ballroom Chaired by: V. BHAGWANDIN, US Army Research Laboratory and J. LATZ, Northrop Grumman Aerospace Systems 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs AIAA-2015-3289 AIAA-2015-3290 AIAA-2015-3291 AIAA-2015-3292 AIAA-2015-3293 Evaluation of Adaptive Compliant Determination of Section Aerodynamic Parametric Study of Box-Wing Optimization of the Aerodynamic A novel aerodynamic surface for Trailing Edge Technology Operating Condition on Wings and Aerodynamics for Minimum Performance of Regional and Wide- redirecting the boundary layer S. Wakayama, The Boeing Company, Rotor Blades From Leading-Edge Drag Under Stability and Body-Class Blended Wing-Body E. Saheby, G. Huang, W. Qiao, W. Tang, Huntington Beach, CA; E. White, The Pressure Measurements Maneuverability Constraints Aircraft Nanjing University of Aeronautics and Boeing Company, Berkeley, MO A. Saini, A. Gopalarathnam, North Carolina S. Andrews, R. Perez, Royal Military T. Reist, D. Zingg, University of Toronto, Astronautics, Nanjing, China State University, Raleigh, NC College of Canada, Kingston, Canada Toronto, Canada
110 Thursday, 25 June 2015 268-APA-30 Low Speed, Low Reynolds Number Aerodynamics Grand Ballroom A Chaired by: Z. YANG, Wright State University and A. JONES, University of Maryland 1400 hrs 1430 hrs 1500 hrs 1530 hrs AIAA-2015-3294 AIAA-2015-3295 AIAA-2015-3296 AIAA-2015-3297 Numerical investigation of finite- Propulsion of a Plunging Flexible Blade Element Momentum Stereoscopic PIV analysis on rotary aspect ratio plate flows in ground Airfoil using a Torsion Spring Model Modeling of Low-Re Small UAS plates in bursting effect N. Arora, A. Gupta, Indian Institute of Electric Propulsion Systems A. Medina, Army Research Laboratory, A. Medina, R. Singh, Army Research Technology Delhi, New Delhi, India; H. M. McCrink, J. Gregory, Ohio State Aberdeen Proving Ground, MD; A. Jones, Laboratory, Aberdeen Proving Ground, MD Aono, Japan Aerospace Exploration Agency University, Columbus, OH University of Maryland, College Park, (JAXA), Sagamihara, Japan; W. Shyy, College Park, MD Hong Kong University of Science and Technology, Clear Water Bay, Hong Kong Thursday, 25 June 2015 269-APA-31 Vortical/Vortex Flow Stemmons B Chaired by: M. JURKOVICH, US Air Force and T. DOUVILLE, TLG Aerospace, LLC. 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs AIAA-2015-3298 AIAA-2015-3299 AIAA-2015-3300 AIAA-2015-3301 AIAA-2015-3302 Near Ground Aircraft Wake Effects of Spinning Motion on the Trailing Vortex-Induced Loads Simulating Aircraft Wake Vortices Investigation of propeller induced Dissipation with Obstacles Trapped Vortex Combustors During Close Encounters in Cruise with OVERFLOW ground vortices by numerical and C. Wang, J. Schluter, Nanyang S. Chen, R. Chue, J. Schluter, Nanyang M. Mendenhall, D. Lesieutre, Nielsen D. Schauerhamer, S. Robinson, University experimental methods Technological University, Singapore, Technological University, Singapore, Engineering & Research, Inc., Santa Clara, of California, Davis, Davis, CA Y. Yang, L. Veldhuis, G. Eitelberg, Delft Singapore Singapore; S. Yu, Singapore Institute of CA; M. Kelly, NASA Langley Research University of Technology, Delft, The Technology, Singapore, Singapore Center, Hampton, VA Netherlands Thursday, 25 June 2015 270-APA-32 Unsteady Aerodynamics II Stemmons A Chaired by: E. FELTROP, The Cessna Aircraft Company and K. VANDEN, USAF 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs AIAA-2015-3303 AIAA-2015-3304 AIAA-2015-3305 AIAA-2015-3306 AIAA-2015-3307 AIAA-2015-3308 AIAA-2015-3309 Effect of Bending-Oscillations on Complex aero-engine intake ducts Flow distortion measurements in Large Eddy Simulations of Unsteady Aerodynamics Coupled 6DoF motion and An Unsteady Aerodynamic Model a Streamwise-Oriented Vortex and dynamic distortion convoluted aero engine intakes Supersonic Jet Flows for Simulations of a Sedan-Type Road Aerodynamics Simulation of Road based on the Leading-Edge Interaction D. MacManus, N. Chiereghin, D. Gil Prieto, P. Zachos, D. MacManus, N. Chiereghin, Aeroacoustic Applications Vehicle during Sinusoidal Steering Vehicles in Crosswind gusts Stagnation Point C. Barnes, M. Visbal, Air Force Research P. Zachos, Cranfield University, Cranfield, Cranfield University, Cranfield, United C. Junqueira-Junior, S. Yamouni, Input H. Ishioka, Hokkaido University, Sapporo, V. Suryakumar, Y. Babbar, T. Strganac, Laboratory, Wright-Patterson AFB, OH; United Kingdom Kingdom Technological Institute of Aeronautics T. Nakashima, Y. Morikawa, Hiroshima Japan; K. Onishi, RIKEN Advanced Institute Texas A&M University, College Station, TX; G. Huang, Wright State University, (ITA), São José dos Campos, Brazil; J. University, Higashi-Hiroshima, Japan; M. for Computational Science, Kobe, Japan; A. Mangalam, Tao of Systems Integration, Dayton, OH Azevedo, Aeronautics and Space Institute Tsubokura, Hokkaido University, Sapporo, K. Nakasato, Nissan Motor Corporation, Inc., Hampton, VA (IAE), São José dos Campos, Brazil; W. Japan; Y. Okada, T. Nouzawa, Mazda Yokohama, Japan; T. Nakashima, Wolf, University of Campinas, Campinas, Motor Corporation, Aki Gun, Japan Hiroshima University, Higashi-Hiroshima, Brazil Japan; M. Tsubokura, Hokkaido University, Sapporo, Japan Thursday, 25 June 2015 271-APA-33 Flow Control Applications & Demonstrations (Active & Passive) III Stemmons C Chaired by: C. TILMANN, Air Force Reseach Laboratory and S. SILTON, US Army Research Laboratory 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs AIAA-2015-3310 AIAA-2015-3311 AIAA-2015-3312 AIAA-2015-3313 AIAA-2015-3314 Nanosecond-SDBD Actuation over a Computational Evaluation of Flow Techniques for the Design of Active Experimental investigation of Passive Plenum design for compact fluidic Conical Forebody at Wind Speed 72 Control for Enhanced Control Flow Control Systems in Heavy Load Reduction under dynamic inflow effectors m/s and Angle of Attack 45 degree Authority af a Vertical Tail Vehicles conditions J. Chard, A. Llopis-Pascual, W. Crowther,
111 J. Wang, H. Li, X. Meng, D. Zhang, A. Shmilovich, Y. Yadlin, E. Whalen, The D. Manosalvas, T. Economon, F. Palacios, A. U. Cordes, K. Hufnagel, C. Tropea, Technical University of Manchester, Manchester, Northwestern Polytechnical University, Boeing Company, Huntington Beach, CA Jameson, Stanford University, Stanford, CA University of Darmstadt, Darmstadt, Germany; United Kingdom Xi’an, China; F. Liu, S. Luo, University of G. Kampers, M. Hölling, J. Peinke, University California, Irvine, Irvine, CA of Oldenburg, Oldenburg, Germany Thursday, 25 June 2015 272-ASE-4 Aircraft Wake Turbulence II (Invited) Plum Blossom B Chaired by: Z. ZHENG, The University of Kansas and M. PRUIS, Northwest Research Associates Inc 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs AIAA-2015-3315 AIAA-2015-3316 AIAA-2015-3317 AIAA-2015-3318 AIAA-2015-3319 Effect of Atmospheric Sheets Fast-time Wake Vortex Model Wind and EDR Measurements Evaluation of Fast-Time Wake Aerodynamic Simulation of Wake and Layers Near the Ground on Predictions Compared with with Scanning Doppler LIDARs for Models using Denver 2006 Field Encounter for Aircraft Close Wake Vortex Transport and Decay Observations Behind Landing Aircraft Preparing Future Weather Dependent Experiment Data Formation Operations (Invited) (Invited) Near the Ground (Invited) Separation Concepts (Invited) N. Ahmad, NASA Langley Research A. He, Z. Zheng, University of Kansas, M. Pruis, D. Delisi, NorthWest Research M. Pruis, D. Delisi, NorthWest Research L. Thobois, R. Krishnamurthy, S. Loaec, J. Center, Hampton, VA; M. Pruis, NorthWest Lawrence, Lawrence, KS Associates, Redmond, WA; D. Jacob, Associates, Redmond, WA; D. Jacob, Coherent Cariou, Leosphere, Orsay, France; A. Dolfi- Research Associates, Seattle, WA Coherent Research Group, Ormond Research Group, Ormond Beach, FL; D. Lai, Bouteyre, M. Valla, ONERA, Palaiseau, France Beach, FL NorthWest Research Associates, Redmond, WA Thursday, 25 June 2015 273-ASE-5 Atmospheric and Space Environments Plum Blossom A Chaired by: W. VAUGHAN, William W Vaughan Consultant and R. SCULLY, NASA 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs AIAA-2015-3320 AIAA-2015-3321 AIAA-2015-3322 AIAA-2015-3323 AIAA-2015-3324 AIAA-2015-3325 AIAA-2015-3326 Lightning Protection for the Orion Advanced Spacecraft Systems Investigation of the Impact of Elastomer Seal Performance after Energy-Aware Path Optimization Ride Quality Within Trail Aircraft In Mathematical Modelling for Carbon Space Vehicle Emulation for Space Environment Surface Blending and Ultraviolet Terrestrial Ultraviolet Radiation for Persistent Sampling of Severe Formation Flight Dioxide Equivalent Prediction of R. Scully, NASA Johnson Space Center, Qualification Testing Radiation Exposure on Elastomer Exposure Storms W. Okolo, A. Dogan, University of Texas, Greenhouse Gases Emitted from a Houston, TX H. Rumann, Bastion Technologies, Inc., Seal Leak Rate Performance for C. Daniels, J. Mather, H. Oravec, University W. Silva, E. Frew, University of Colorado, Arlington, Arlington, TX; W. Blake, Air Small Scale Turbojet Engine Houston, TX Space Seal Applications of Akron, Akron, OH; S. Taylor, University Boulder, Boulder, CO Force Research Laboratory, Wright- Y. Şöhret, T. Karakoc, Anadolu University, S. Taylor, University of Toledo, Toledo, OH; of Toledo, Toledo, OH; P. Dunlap, NASA Patterson AFB, OH Eskisehir, Turkey; N. Karakoç, Osmangazi J. Mather, C. Daniels, University of Akron, Glenn Research Center, Cleveland, OH University, Eskisehir, Turkey Akron, OH Thursday, 25 June 2015 274-ATIO-24 UAS Integration & Operations I Ming Chaired by: V. SCHULTZ, NASA Langley Research Center 1400 hrs 1430 hrs 1500 hrs AIAA-2015-3327 AIAA-2015-3328 AIAA-2015-3329 An Evaluation of Detect and Avoid System Development for the NASA Platform-Independent Geofencing (DAA) Displays for Unmanned Aircraft UAS Airspace Operations Challenge for Low Altitude UAS Operations Systems: The Effect of Information S. Fehrenbach, Z. Barbeau, J. Jacob, G. M. Stevens, B. Coloe, E. Atkins, University Level and Display Location on Pilot Chowdhary, Oklahoma State University, of Michigan, Ann Arbor, Ann Arbor, MI Performance Stillwater, OK L. Fern, R. Rorie, San Jose State University, 112 Moffett Field, CA; J. Pack, Infoscitex Corporation, Dayton, OH; J. Shively, NASA Ames Research Center, Moffett Field, CA; M. Draper, Air Force Research Laboratory, Wright- Patterson AFB, OH Thursday, 25 June 2015 275-ATIO-25 ATM VI - Management of NAS Resources Morocco Chaired by: K. MARAIS, Purdue University 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2015-3330 AIAA-2015-3331 AIAA-2015-3332 AIAA-2015-3333 AIAA-2015-3334 AIAA-2015-3335 Strategic Air Traffic Planning with Performance Impact of Improved Proactive and Reactive Probabilistic Time-Series Models for Analytical Identification and Stakeholder Feedback-Based Frechet Distance Aggregation and Departure Time Prediction Relative Management of Non-Weather Ground Delay Program Decision Ranking of Choke Points in the Identification, Ranking, and Causes of Rerouting to Sector Demand & Arrival Time Capacity Disruption Events in the Support National Airspace System Choke Points in the National Airspace A. Bombelli, L. Soler, K. Mease, University Predictability National Airspace System: A Flow E. Vargo, C. Taylor, C. Wanke, MITRE D. Long, S. Hasan, V. Stouffer, LMI, System of California, Irvine, Irvine, CA R. Curran, E. Konnemann, Delft University Modeling and Design Approach Corporation, McLean, VA McLean, VA; K. Ramamoorthy, Saab M. Alcabin, The Boeing Company, Seattle, of Technology, Delft, The Netherlands; S. S. Roy, Washington State University, Sensis Corporation, East Syracuse, NY; H. WA; R. Golaszewski, GRA, Inc., Jenkintown, Mahlich, EUROCONTROL, Bretigny, France Pullman, WA; Y. Wan, University of North Idris, Engility Corporation, Billerica, MA; B. PA; W. Cotton, Cotton Aviation Enterprises, Texas, Denton, TX Ballard, GRA, Inc., Jenkintown, PA; et al. Lakeway, TX; V. Stouffer, LMI, McLean, VA; J. Musiak, The Boeing Company, Seattle, WA Thursday, 25 June 2015 276-ATIO-26 Transformational Flight - Unconventional VTOL Configurations Monet Ballroom Chaired by: I. CHOUTAPALLI, The University of Texas - Pan American 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs Oral Presentation AIAA-2015-3336 Oral Presentation AIAA-2015-3337 Oral Presentation Flight Test Results for the DZYNE Design and Testing of the Joby Lotus Design and Testing of the Joby S2 Integration of Electric Propulsion in The Centrifugally Stiffened Rotor ROTORwing - A High Endurance Multifunctional Rotor VTOL UAV Electric VTOL PAV Propellers Efficient Heavy-Lift VTOL Concept (CSR) VTOL Long Endurance VTOL Concept P. Sinha, Transition Robotics, Inc., Santa A. Stoll, P. Pei, A. Clark, J. Bevirt, Joby E. Demers Bouchard, D. Rancourt, D. Concept M. Page, DZYNE Technologies, Irvine, CA Cruz, CA; A. Stoll, B. Goldsmith, Joby Aviation, Santa Cruz, CA Mavris, Georgia Institute of Technology, M. Moore, NASA Langley Research Center, Aviation, Santa Cruz, CA Atlanta, GA Hampton, VA Thursday, 25 June 2015 277-F360-9 Supercomputing: Roadmap and its Future Role in Aerospace Engineering Grand Ballroom E 1400 - 1630 hrs Moderator: Doug Cline, Technical Lead, High Performance Computing, Lockheed Martin Aeronautics Panelists: William Gropp Brian Mitchell Mark Seager Jef Dawson Thomas M. Siebel Chair, Department of Computer Science and Senior Principal Engineer Intel Fellow Applications Manager Director, Parallel Computing Institute GE Global Research CTO, High Performance Computing Ecosystem, Cray, Inc. University of Illinois at Urbana-Champaign Intel Corporation
Thursday, 25 June 2015 278-FD-30 Hypersonic and Chemically-Reacting Flows Sapphire
113 Chaired by: B. WHEATON, The Johns Hopkins University Applied Physics Laboratory and J. SMITH, Sandia National Laboratories 1400 hrs 1430 hrs 1500 hrs 1530 hrs AIAA-2015-3338 AIAA-2015-3339 AIAA-2015-3340 AIAA-2015-3341 Starting Characteristics of the US Numerical Modeling and Simulation Large-Eddy Simulation of Autoignition- A Numerical Scheme for Hypersonic Air Force Academy Mach 6 Ludwieg of Combustion Phenomena Related Dominated Supersonic Combustion Turbulent Flow Tube to Thermal Ignition and Flame G. Candler, P. Subbareddy, University of M. Righi, Zurich University of Applied R. Decker, M. Semper, J. Anthony, R. Fronts Minnesota, Minneapolis, Minneapolis, Sciences, Winterthur, Switzerland Cummings, U.S. Air Force Academy, W. Tavernetti, M. Hafez, University of MN; N. Cymbalist, P. Dimotakis, California Colorado Springs, CO California, Davis, Davis, CA Institute of Technology, Pasadena, CA Thursday, 25 June 2015 279-FD-31 Flow Control - Vortical Flows Senators Lecture Hall Chaired by: M. YU, University of Maryland, Baltimore County and L. PACK MELTON, NASA-Langley Research Center 1400 hrs 1430 hrs 1500 hrs 1530 hrs AIAA-2015-3342 AIAA-2015-3343 AIAA-2015-3344 AIAA-2015-3345 Observations on the Mean and Mixing Layer: Numerical and Effects of Pulse Energy on Shear Towards integral boundary layer Turbulent Wake of a Micro-Ramp Experimental Control Strategies Layer Control using Surface Plasma modelling of vane-type vortex Array J. Little, University of Arizona, Tucson, Discharges generators E. Baydar, F. Lu, University of Texas, Tucson, AZ; U. Kaul, NASA Ames Research D. Akins, A. Singh, J. Little, University of D. Baldacchino, C. Simao Ferreira, G. van Arlington, Arlington, TX; J. Slater, NASA Center, Moffett Field, CA Arizona, Tucson, Tucson, AZ Bussel, Delft University of Technology, Glenn Research Center, Cleveland, OH Delft, The Netherlands Thursday, 25 June 2015 280-FT-2/GT-14 Optimization Techniques in Flight Test/Ground Test Obelisk B Chaired by: W. SCHUMAN, AF TSTA/AEDC and B. MILLS, AEDC/ ATA 1400 hrs 1430 hrs 1500 hrs 1530 hrs AIAA-2015-3346 AIAA-2015-3347 AIAA-2015-3348 AIAA-2015-3349 Optimized Calculation of Forces for The design and test result of pressure Evaluation of Low-Cost Autopilots Application of a small UAV fleet for Fullscale Aircraft Structure Fatigue distortion compensation device in for SUAS Operations demonstration of optimized mission Testing Weight and Balance System C. Brown, J. Jacob, Oklahoma State M. Kasprzyk, P. Bibik, M. Malinowski, C. He, Aviation Industry Corporation of Y. Minqiang, C. Yue, Taiyuan Aero- University, Stillwater, OK J. Polaczek, K. Wronowski, Warsaw China (AVIC), Xi’an, China Instruments Company, Ltd., Taiyuan, China University of Technology, Warsaw, Poland Thursday, 25 June 2015 281-GEPC-1 Overview of NASA Advanced Air Vehicles Program Metropolitan Ballroom Chaired by: B. ESKER and R. DEL ROSARIO, NASA Glenn Research Center 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs Oral Presentation Oral Presentation Oral Presentation Oral Presentation Oral Presentation Oral Presentation Advanced Air Vehicles Program NASA’s Advanced Air Transport Commercial Supersonic Technology Revolutionary Vertical Lift Advanced Composites Project NASA Aeronautics Evaluation and Overview Technology Project Project Overview Technology Project Overview Test Capabilities Project J. Dryer, B. Esker, NASA Headquarters, R. Del Rosario, NASA Glenn Research P. Coen, NASA Langley Research Center, S. Gorton, NASA Langley Research R. Young, S. Smeltzer, NASA Langley C. Mouring, NASA Langley Research Washington, DC Center, Cleveland, OH; S. Anders, NASA Hampton, VA; K. Civinskas, L. Povinelli, Center, Hampton, VA; I. López, NASA Research Center, Hampton, VA Center, Hampton, VA; R. Colantonio, NASA Langley Research Center, Hampton, VA; N. NASA Glenn Research Center, Cleveland, Glenn Research Center, Cleveland, OH; C. Glenn Research Center, Cleveland, OH Madavan, NASA Ames Research Center, OH Theodore, NASA Ames Research Center, Moffett Field, CA Moffett Field, CA Thursday, 25 June 2015
114 282-LTA-2 Lighter-than-Air Systems & Technologies II Steuben Chaired by: D. HORKHEIMER, Honeywell International, Inc. 1400 hrs 1430 hrs 1500 hrs 1530 hrs AIAA-2015-3350 AIAA-2015-3351 AIAA-2015-3352 AIAA-2015-3353 Lab-Scale Characterization of a The 12M™ Tethered Aerostat Design and Flight Testing of an Diaphragm Testing of Fabric Lighter-Than-Air Wind Energy System: Rapid Tactical Deployment Autonomous Airship Components & Correlation to System - Closing the Loop for Surveillance Missions J. Santos, D. Garcia, M. Cunha, L. Góes, Analysis J. Deese, T. Muyimbwa, N. Deodhar, C. J. Krausman, D. Miller, TCOM, L.P., Technological Institute of Aeronautics K. Cromer, S. Petersen, TCOM, L.P., Vermillion, P. Tkacik, University of North Columbia, MD (ITA), São José dos Campos, Brazil; Columbia, MD Carolina, Charlotte, Charlotte, NC R. Pant, Indian Institute of Technology Mumbai, Mumbai, India Thursday, 25 June 2015 283-MAO-10 Shape and Topology II Madrid Chaired by: B. MESMER, University of Alabama and V. KALIVARAPU, Iowa State University 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2015-3354 AIAA-2015-3355 AIAA-2015-3356 AIAA-2015-3357 AIAA-2015-3358 AIAA-2015-3359 Volumetric Shape Parameterisation A Discrete Adjoint Framework Towards shape optimization Knowledge-based Integrated Wing Conceptual optimal design of Robust and Reliability-Based for Combined Aerodynamic for Unsteady Aerodynamic and of steady-state fluid-structure Automation and Optimization for environmentally friendly airliners: a Topology Optimization of Wing Geometry and Topology Aeroacoustic Optimization interaction problems using vertex Conceptual Design review of available methodologies Bodies Optimisation B. Zhou, T. Albring, N. Gauger, Technical morphing R. Munjulury, P. Berry, T. Melin, K. and their integration into a consistent D. Papadimitriou, C. Papadimitriou, J. Hall, D. Poole, T. Rendall, C. Allen, University of Kaiserslautern, Kaiserslautern, R. Najian Asl, D. Baumgärtner, K. Amadori, P. Krus, Linköping University, framework for everyday use University of Thessaly, Volos, Greece University of Bristol, Bristol, United Germany; T. Economon, F. Palacios, J. Bletzinger, Technical University of Munich, Linköping, Sweden P. Magalhaes, B. Mattos, Technological Kingdom Alonso, Stanford University, Stanford, CA Munich, Germany Institute of Aeronautics (ITA), São José dos Campos, Brazil Thursday, 25 June 2015 284-MAO-11 Uncertainty I Manchester Chaired by: R. KOLONAY, Air Force Research Laboratory/RQVC/WPAFB and P. PIPERNI, Bombardier Inc 1400 hrs 1430 hrs AIAA-2015-3360 AIAA-2015-3361 High-Fidelity Weight Estimation Surrogate-based Robust Shape for Aircraft Conceptual Design Optimization for Vane Clusters Optimization I. Arsenyev, F. Duddeck, Technical N. Nigam, S. Ayyalasomayajula, X. University of Munich, Munich, Germany; A. Qi, P. Chen, Intelligent Automation, Fischersworring-Bunk, MTU Aero Engines, Inc., Rockville, MD; J. Alonso, Stanford Munich, Germany University, Stanford, CA Thursday, 25 June 2015 285-MST-12 Propulsion Systems Travertine Chaired by: A. ELMILIGUI, NASA Langley Research Center 1400 hrs 1430 hrs 1500 hrs AIAA-2015-3362 AIAA-2015-3363 AIAA-2015-3364 One-dimensional Model of a Individual model identification for Numerical Study of Similarity and Closed-loop Underwater Propulsion turbofan engine based on particle Dimensional Methods in Scaled System swarm optimization Turbine Vane cooling performance J. Lu, China Shipbuilding Industry J. Qian, F. Liu, Nanjing University of experiment Corporation Company, Ltd., Xi’an, China Aeronautics and Astronautics, Nanjing, Y. Liu, M. Junkui, G. Dilan, Nanjing China; X. Qiu, Aviation Motor Control University of Aeronautics and Astronautics, System Institute, Wuxi, China Nanjing, China 115 Thursday, 25 June 2015 286-PDL-13 Plasma Aerodynamics & Flow Control V Miro Chaired by: J. POGGIE, USAF AFRL/RBAC 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs AIAA-2015-3365 AIAA-2015-3366 AIAA-2015-3367 AIAA-2015-3368 AIAA-2015-3369 Numerical Study of Three-dimensional Numerical Modeling DBD Plasma Actuators Numerical Investigation of Several Particle in Cell (PIC) simulations of Thermal Protection Using Simulation of Magnetohydrodynamic in Integral Boundary Layer Alkali Metal Addition Methods for plasma-electrode interactions for Magnetohydrodynamic Flow Flow Control in Reentry Flight Formulation for Application in the Forced Elevation of the Starting Reentry Blackout Alleviation Control in Mars Entry Flight K. Masuda, Y. Shimosawa, University of Panel Methods Altitude in the Electrodynamic S. Krishnamoorthy, S. Close, Stanford T. Takahashi, Y. Shimosawa, K. Masuda, Tsukuba, Tsukuba, Japan; S. Ogawa, T. G. de Oliveira, R. Santos Pereira, D. Aerobraking Declearation University, Stanford, CA T. Fujino, University of Tsukuba, Tsukuba, Yoshino, Toshiba Corporation, Kawasaki, Ragni, M. Kotsonis, Delft University of H. Katsurayama, Yamaguchi University, Japan Japan; T. Fujino, University of Tsukuba, Technology, Delft, The Netherlands Ube, Japan Tsukuba, Japan Thursday, 25 June 2015 287-RLA-3 Rising Leaders in Aerospace Panel Discussion: Transitioning to Leadership Emerald 1400 - 1530 hrs 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. Moderator: Ben Marchionna, Systems Engineer, Lockheed Martin Skunk Works Panelists: Russ Althof Douglas Stanley Frederick Wieland Chief Engineer President and Executive Director Director, Air Traffic Management Raytheon Missile Systems National Institute of Aerospace Intelligent Automation Systems, Inc. Thursday, 25 June 2015 288-TP-13 DSMC Rosetta Chaired by: D. HASH, NASA - ARC 1400 hrs 1430 hrs 1500 hrs 1530 hrs AIAA-2015-3370 AIAA-2015-3371 AIAA-2015-3372 AIAA-2015-3373 DSMC Study of Carbon Fiber Oxidation Sensitivity Analysis of DSMC DSMC Investigation of Calibration of DSMC parameters in Ablative Thermal Protection Systems Parameters for Ionizing, Radiating Nonequilibrium Effects in a H2-O2 for transport processes in ionized A. Borner, NASA Ames Research Center, Hypersonic Flows Unstretched Diffusion Flame air mixtures Moffett Field, CA; F. Panerai, University K. Higdon, D. Goldstein, P. Varghese, I. Borges Sebastiao, A. Alexeenko, Purdue K. Swaminathan Gopalan, K. Stephani, of Kentucky, Lexington, Lexington, KY; N. University of Texas, Austin, Austin, TX University, West Lafayette, IN University of Illinois, Urbana-Champaign, Mansour, NASA Ames Research Center, Urbana, IL Moffett Field, CA Thursday, 25 June 2015 289-NW-9 Networking Coffee Break Meeting Room Foyers 1530 - 1600 hrs Thursday, 25 June 2015 290-LEC-6 Wright Brothers Lectureship in Aeronautics Chantilly Ballroom West 1730 - 1830 hrs
Development and Testing of the X-47B Pablo Gonzalez, II UCAS-D Program Manager Northrop Grumman Aerospace Systems 116 Friday Friday, 26 June 2015 291-SB-5 Speakers’ Briefing Session Rooms 0730 - 0800 hrs Friday, 26 June 2015 292-PLNRY-5 Plenary Keynote Chantilly Ballroom West 0800 - 0900 hrs
The G650 Design, Development, and Test Kurt Erbacher Vice President, G650 Aircraft Program Gulfstream Aerospace Corporation Friday, 26 June 2015 293-ACD-8 Aeronautic Discipline Considerations in Aircraft Design Miro Chaired by: H. JIMENEZ, Georgia Institute of Technology 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2015-3374 AIAA-2015-3375 AIAA-2015-3376 AIAA-2015-3377 AIAA-2015-3378 Prediction of Wing Structural Mass Effective L/D: A Theoretical Revisiting Busemann: The Design A Total Flight Envelope Approach Feasibility Studies on a High-Altitude for Transport Category Aicraft Approach to the Measurement Implications of Inconsistencies to Conceptual Design Stability & Captive Lighter-Than-Air Platform Conceptual Design of Aero-Structural Efficiency in Found Within Simple Sweep Theory Control System T. Takahashi, T. Lemonds, Arizona State Aircraft Design T. Takahashi, S. Kamat, Arizona State M. Swann, T. Takahashi, Arizona State K. Chiba, S. Satori, R. Hiramoto, S. Kase, R. University, Tempe, AZ M. Guynn, NASA Langley Research Center, University, Tempe, AZ University, Tempe, AZ Mitsuhashi, Hokkaido University of Science, Hampton, VA Sapporo, Japan; J. Sasaki, Hokkaido Aerospace Science and Technology Incubation Center, Sapporo, Japan; et al. Friday, 26 June 2015 294-AMT-14/GT-15 Aerodynamic Measurement Systems: Calibration and Monitoring Topaz Chaired by: R. RHEW, NASA-Langley Research Center and G. JONES, NASA-Langley Research Center 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs Oral Presentation AIAA-2015-3379 AIAA-2015-3380 AIAA-2015-3381 AIAA-2015-3382 Measurement System Calibration Improved Regression Analysis of Statistical Process Control Analysis of Five-Hole Probe The Use of Absolute-Value Terms in Fundamentals Temperature-Dependent Strain- Implemented for Long Term Study of Calibration Parameters Regression Modeling of Multi-Piece R. Rhew, P. Parker, G. Jones, NASA Gage Balance Calibration Data Wind Tunnel Balance Calibrations S. Karahan, A. Kutay, Middle East Force Balances (Invited) Langley Research Center, Hampton, VA N. Ulbrich, Jacobs, Moffett Field, CA R. Callahan, D. Landman, Old Dominion Technical University, Ankara, Turkey M. Kammeyer, The Boeing Company, St. University, Norfolk, VA; S. Commo, K. Lynn, Louis, MO; N. Ulbrich, Jacobs, Moffett NASA Langley Research Center, Hampton, VA Field, CA Friday, 26 June 2015 295-APA-34 Icing or Roughness Effects on Vehicle Aerodynamics Stemmons C Chaired by: G. WOO, General Electric Global Research and D. O’BRIEN, US Army RDECOM 0900 hrs 0930 hrs 1000 hrs AIAA-2015-3383 AIAA-2015-3384 AIAA-2015-3385 Data-Driven Low-Dimensional Aerodynamic Effects of Roughness The Characteristics of SLD icing Modeling and Uncertainty on Wind Turbine Blade Sections accretions and aerodynamic effects on Quantification for Airfoil Icing L. Joseph, J. Fenouil, A. Borgoltz, W. high-lift configurations A. DeGennaro, C. Rowley, L. Martinelli, Devenport, Virginia Polytechnic Institute C. Zhang, F. Wang, W. Kong, H. Liu, Shanghai Princeton University, Princeton, NJ and State University, Blacksburg, VA Jiao Tong University, Shanghai, China Friday, 26 June 2015 296-APA-35 Aerodynamic Design Methodologies III Carpenter Ballroom 117 Chaired by: C. ROSEMA, US Army AMRDEC 0900 hrs 0930 hrs 1000 hrs AIAA-2015-3386 AIAA-2015-3387 AIAA-2015-3388 Experimental Validation of a Stability Derivative Computation of Aerodynamic performance study Morphed Wing Geometry Using Tailless Aircraft using Variable-Fidelity of high pressure zone capture wing Small Wind Tunnel Testing Aerodynamic Analysis and Wind- configurations A. Koreanschi, S. Oliviu, R. Botez, Tunnel Experiments K. Cui, G. Li, Y. Xiao, Chinese Academy of University of Québec, Montréal, Canada J. Park, C. Ocheltree, J. Choi, S. Choi, P. Raj, Sciences, Beijing, China A. Friedman, Virginia Polytechnic Institute and State University, Blacksburg, VA Friday, 26 June 2015 297-APA-37 Propeller/Rotorcraft/Wind Turbine Aerodynamics III Stemmons B Chaired by: K. MASSEY, DARPA/TTO and J. MURRAY, Sandia National Laboratories 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2015-3389 AIAA-2015-3390 AIAA-2015-3391 AIAA-2015-3392 AIAA-2015-3393 Sensitivity of Wind Turbine Airfoil Configuration and Numerical Extension of a Parabolic Method Experimental and Numerical Optimization of Wind Turbine Sections to Geometry Variations Investigation of the Adaptive Camber without Pressure Approximations Investigations of a Small Research Airfoils Subject to Particle Erosion Inherent in Modular Blades Airfoil as Passive Load Alleviation for Wind Turbines in ABL Flows Wind Turbine G. Fiore, M. Selig, University of Illinois, K. Brown, N. Molinaro, T. Meyers, Mechanism for Wind Turbines A. Mittal, L. Taylor, K. Sreenivas, W. S. Vey, D. Marten, G. Pechlivanoglou, C. Urbana-Champaign, Urbana, IL A. Borgoltz, W. Devenport, Virginia D. Marten, Technical University of Berlin, Briley, D. Nichols, University of Tennessee, Nayeri, C. Paschereit, Technical University Polytechnic Institute and State University, Berlin, Germany; H. Spiegelberg, Technical Chattanooga, Chattanooga, TN of Berlin, Berlin, Germany Blacksburg, VA; J. Luedke, General Electric University of Darmstadt, Darmstadt, Germany; Company, Greenville, SC; et al. G. Pechlivanoglou, C. Nayeri, C. Paschereit, Technical University of Berlin, Berlin, Germany; C. Tropea, Technical University of Darmstadt, Darmstadt, Germany Friday, 26 June 2015 298-ATIO-27 ATM VII - Weather Impact Morocco Chaired by: Y. JUNG, NASA Ames Research Center 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2015-3394 AIAA-2015-3395 AIAA-2015-3396 AIAA-2015-3397 AIAA-2015-3398 AIAA-2015-3399 Dynamic Arrival Routes: A Initial Analysis of and Predictive Benefits Analysis of Ground- Dynamic Wake Vortex Separation Wind Information Uplink to Aircraft Wind Measurements with ground- Trajectory-Based Weather Model Development for Weather Sourced Convective Weather Combining with AMAN/DMAN Performing Interval Management based fiber-based wind Doppler Avoidance System for Merging Reroute Advisory Use Alerting in the Cockpit Concept Operations LIDAR systems for aviation weather Arrivals and Metering H. Arneson, NASA Ames Research Center, S. Campbell, M. McPartland, M. Ishutkina, N. Matayoshi, E. Yoshikawa, Japan N. Ahmad, B. Barmore, K. Swieringa, NASA applications C. Gong, D. Mcnally, NASA Ames Research Moffett Field, CA Lincoln Laboratory, Massachusetts Institute Aerospace Exploration Agency (JAXA), Langley Research Center, Hampton, VA L. Thobois, Leosphere, Orsay, France Center, Moffett Field, CA of Technology, Lexington, MA Mitaka, Japan Friday, 26 June 2015 299-ATIO-28 Future Concepts Wyeth Chaired by: K. MARAIS, Purdue University 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2015-3400 AIAA-2015-3401 AIAA-2015-3402 AIAA-2015-3403 AIAA-2015-3404 Achieving TASAR Operational A Preliminary Evaluation of Improving Situation Awareness with Dynamic Airspace Configuration The Impact of Mitigation Measures for Readiness Supersonic Transport Category a Traffic Management Portal in SESAR: building a smooth and System Capacity Constraints on the D. Wing, NASA Langley Research Center, Vehicle Operations in the National A. Staley, C. Bolczak, MITRE Corporation, dynamic opening scheme through Future Air Transportation System Hampton, VA Airspace System McLean, VA airspace building blocks assessment N. Dzikus, German Aerospace Center (DLR), M. Underwood, M. Guminsky, NASA T. Dubot, S. Aubry, J. Bedouet, ONERA, Hamburg, Germany; S. Bartosch, RWTH Langley Research Center, Hampton, VA Toulouse, France Aachen University, Aachen, Germany; M. Schaefer, Federal Ministry of Transport and Digital Infrastructure, Bonn, Germany 118 Friday, 26 June 2015 300-ATIO-29 UAS Integration & Operations II Ming Chaired by: D. DELAURENTIS, Purdue University 0900 hrs 0930 hrs 1000 hrs AIAA-2015-3405 AIAA-2015-3406 AIAA-2015-3407 UAS Demand Generation Using Investigation of Simulated UAS RPAS - ATM Integration Subject Matter Expert Interviews Safety Incidents Using UAS Safety Demonstration - Real-Time and Socio-economic Analysis Analysis Model (USAM) Simulation Results S. Ayyalasomayajula, R. Sharma, F. A. Tyagi, F. Wieland, Intelligent E. Filippone, Italian Aerospace Research Wieland, Intelligent Automation, Inc., Automation, Inc., Rockville, MD; S. Center (CIRA), Capua, Italy Rockville, MD; A. Trani, N. Hinze, T. Toussaint, Coherent Technical Services, Spencer, Virginia Polytechnic Institute and Inc., Lexington Park, MD; J. Luxhoj, LCR, State University, Blacksburg, VA LLC, Somerset, NJ Friday, 26 June 2015 301-CFD-31 Visualization for CFD 2030 Grand Ballroom A Chaired by: S. IMLAY, Tecplot, Inc 0900 hrs 1000 hrs 1030 hrs AIAA-2015-3408 AIAA-2015-3409 Panel Industrial Perspectives on Geometry Handling for Aerodynamics The Path to and State of Geometry Panel: The Path to CFD Visualization in 2030 N. Taylor, MBDA, Bristol, United Kingdom and Meshing in 2030: Panel Moderator: Scott Imlay, Tecplot, Inc Summary S. Imlay, Tecplot, Inc., Snohomish, WA; E. Duque, Intelligent Light, Prescott, AZ; K. J. Chawner, Pointwise, Inc., Fort Worth, TX; J. Colburn, Computation Engineering International, Inc., Houston, TX; G. Chen, University Dannenhoffer, Syracuse University, Syracuse, of Houston, Houston, TX NY; S. Dey, Naval Research Laboratory, Washington, DC; W. Jones, NASA Langley Research Center, Hampton, VA; J. Slotnick, The Boeing Company, Huntington Beach, CA; N. Taylor, MBDA, Bristol, United Kingdom Friday, 26 June 2015 302-CFD-32 Post-Processing and Model Reduction Grand Ballroom B Chaired by: S. SPEER, Northrop Grumman Corporation 0900 hrs 0930 hrs 1000 hrs AIAA-2015-3410 AIAA-2015-3411 AIAA-2015-3412 EPIC - An Extract Plug-In Dynamic Mode Decomposition Statistical Analysis and Model Components Toolkit for In-Situ Data of Backward Facing Step Flow Reduction of Surface Pressure Extracts Architecture Simulation Data for Interaction of a Streamwise- E. Duque, `. Hiepler, Intelligent Light, T. Horchler, K. Mani, K. Hannemann, Oriented Vortex with a Wing
119 Rutherford, NJ; R. Haimes, Massachusetts German Aerospace Center (DLR), A. Mohan, L. Agostini, D. Gaitonde, Institute of Technology, Cambridge, MA; Göttingen, Germany Ohio State University, Columbus, OH; D. C. Stone, Computational Science and Garmann, Air Force Research Laboratory, Engineering, LLC, Chicago, IL; S. Gorrell, Wright-Patterson AFB, OH M. Jones, Brigham Young University, Provo, UT; et al. Friday, 26 June 2015 303-CFD-33 Interdisciplinary CFD II Plum Blossom A Chaired by: P. SLABOCH and D. GONZALEZ, Naval Surface Warfare Center 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2015-3413 AIAA-2015-3414 AIAA-2015-3415 AIAA-2015-3416 AIAA-2015-3417 Computational Study of Active Flow Aeroelastic Response of Rocket Finite-Time Lyapunov Exponent Numerical Simulation of the Calculation of Airfoil Anti-icing Heat Control of a Flow-Excited Helmholtz Nozzles Subected to Combined Analysis of Intermittent Acoustic Interaction between Rim Seal and Load in SLD Conditions Resonator Thrust and Side Loads Events in a Round Jet Main Annulus Flow in a Four Stage Z. Wang, Nanjing University of Aeronautics J. Buehn, P. Slaboch, Saint Martin’s X. Zhao, Alabama A&M University, D. Gonzalez, Naval Surface Warfare Low-Pressure Axial Turbine and Astronautics, Nanjing, China University, Lacey, WA Huntsville, AL; S. Zhang, ESI Group, Center, Indian Head, MD; D. Gaitonde, Z. Wei tao, China Gas Turbine Huntsville, AL Ohio State University, Columbus, OH; Establishment, Chengdu, China M. Lewis, Science and Technology Policy Institute, Washington, DC Friday, 26 June 2015 304-CFD-34 Multiphase and Nonequilibrium Flows Coral Chaired by: C. TSAI, Lockheed Martin Space Systems and R. AGARWAL, Washington University in St Louis 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2015-3418 AIAA-2015-3419 AIAA-2015-3420 AIAA-2015-3421 AIAA-2015-3422 Numerical simulation of a scramjet A Multiphase and Multiphysics CFD Application of a Maximum-Entropy- An ALE/FE formulation for high Simulation of the Separated isolator with thermodynamic Technique for Fuel Spurt Prediction Based 14-Moment Closure for Multi- precision interface tracking in flow over a Wall-Mounted Hump nonequilibrium with Cavitation and Fluid-Structure Dimensional Non-Equilibrium Flows separated multiphase flows using Finite-Volume Based Lattice R. Fiévet, H. Koo, V. Raman, University of Interaction B. Tensuda, University of Toronto, A. Hay, S. Etienne, D. Pelletier, École Boltzmann Method Michigan, Ann Arbor, Ann Arbor, MI H. Yang, CFD Research Corporation, Toronto, Canada; J. McDonald, University Polytechnique de Montréal, Montréal, B. Yagiz, G. Guzel, I. Koc, ASELSAN, Inc., Huntsville, AL of Ottawa, Ottawa, Canada; C. Groth, Canada Ankara, Turkey University of Toronto, Toronto, Canada Friday, 26 June 2015 305-CFD-35 Overset and Cartesian Grid Methods Plum Blossom B Chaired by: N. FOSTER, Applied Research Laboratory - Penn State and M. GHOREYSHI, United States Air Force Academy 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2015-3423 AIAA-2015-3424 AIAA-2015-3425 AIAA-2015-3426 AIAA-2015-3427 AIAA-2015-3428 AIAA-2015-3429 Three-Dimensional Dynamic Accuracy of High-Order CFD and Advances in Distance-Based Hole Simulation Validation of Static and Sharp resolution of complex Integrating the Stanford University A Comparative Study of Flow Overset Method for Stabilized Overset Interpolation in Finite Cuts on Overset Grids Forced Motion Flow Physics of a moving geometries using a multi- Unstructured Code (SU2) With around a Circular Cylinder using Finite Elements Volume/Difference Codes W. Chan, S. Pandya, NASA Ames Research Canard Configured TransCruiser cut-cell viscous flow solver Overset Grids Lattice Boltzmann Method C. Liu, J. Newman, W. Anderson, N. Foster, Pennsylvania State University, Center, Moffett Field, CA M. Ghoreyshi, R. Korkis-Kanaan, A. L. Schneiders, C. Guenther, J. Grimmen, A. Kanoria, Indian Institute of Technology D. Hamane, O. Guerri, Renewable Energy University of Tennessse, Chattanooga, State College, PA Jirasek, A. Lofthouse, R. Cummings, U.S. M. Meinke, W. Schroeder, RWTH Aachen Gandhinagar, Gandhinagar, India; D. Development Center Algeria, Bouzareah, Chattanooga, TN Air Force Academy, Colorado Springs, CO University, Aachen, Germany Chandar, Institute of High Performance Algeria; S. Larbi, Polytechnical School of Computing, Singapore, Singapore Algiers, Elharache, Algeria 120 Friday, 26 June 2015 306-CFD-36 LES, DNS, and Hybrid RANS-LES IV Emerald Chaired by: J. POGGIE, USAF AFRL/RBAC and B. THORNBER, The University of Sydney 0900 hrs 0930 hrs 1000 hrs 1030 hrs AIAA-2015-3430 AIAA-2015-3431 AIAA-2015-3432 AIAA-2015-3433 Impact of Computational Direct Numerical Simulation of Supersonic Corner Flow Predictions Assessment of novel DES approach Domain Size in Simulations of Turbulent Flow Around a Surface using the Quadratic Constitutive with enhanced SGS modelling for Homogeneous Decaying Turbulence Mounted Cube Relation prediction of separated flow over a and Mixing Layers A. Curley, M. Uddin, B. Peters, University T. Leger, J. Poggie, Air Force Research delta wing B. Thornber, University of Sydney, Sydney, of North Carolina, Charlotte, Charlotte, NC Laboratory, Wright-Patterson AFB, OH M. Fuchs, Technical University of Berlin, Berlin, Australia Germany; C. Mockett, CFD Software GmbH, Berlin, Germany; J. Sesterhenn, F. Thiele, Technical University of Berlin, Berlin, Germany Friday, 26 June 2015 307-MAO-12 Shape and Topology III Madrid Chaired by: B. ROTH, Walla Walla Univ and S. CHOI, Virginia Polytechnic Institute and State University 0900 hrs 0930 hrs 1000 hrs 1030 hrs AIAA-2015-3434 AIAA-2015-3435 AIAA-2015-3436 AIAA-2015-3437 Adjoint-Enhanced Multi-Level Discrete Adjoint Design Aerodynamic Shape Optimization Considerations about Wintip Optimization: Investigation of Optimization Approach for of a Truss-Braced-Wing Aircraft Devices Design of Transport Algorithm Parameter Settings Increasing Transonic Buffet Onset D. Ivaldi, N. Secco, S. Chen, J. Hwang, J. Airplane Y. Tesfahunegn, S. Koziel, Reykjavik Angle-of-Attack Martins, University of Michigan, Ann Arbor, B. Mattos, A. Paula, P. Komatsu, University, Reykjavik, Iceland; L. Leifsson, J. Thomas, E. Dowell, Duke University, Ann Arbor, MI Technological Institute of Aeronautics Iowa State University, Ames, IA Durham, NC (ITA), São José dos Campos, Brazil Friday, 26 June 2015 308-MAO-13 Uncertainty II Manchester Chaired by: S. CHOWDHURY, Mississippi State University and S. FERGUSON, North Carolina State University 0900 hrs 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2015-3438 AIAA-2015-3439 AIAA-2015-3440 AIAA-2015-3441 AIAA-2015-3442 AIAA-2015-3443 Multi-Objective Optimization Under A Multi-Fidelity Approach to Sculpting: A Fast, Interactive Method Multidisciplinary Uncertainty An Integrated Framework A Strategy for Probabilistic Margin Uncertainty Quantification of Uncertainty in for Probabilistic Design Space Quantification in Aeroelastic for Bayesian Uncertainty Allocation in Aircraft Conceptual C. Liang, S. Mahadevan, Vanderbilt Stability and Control Databases Exploration and Margin Allocation Analyses of Semi-Span Supersonic Quantification and Probabilistic Design University, Nashville, TN for use in Stochastic Aircraft R. Cooke, Resources for the Future, Transport Wing Multi-Criteria Decision Making in T. Zang, Zang M&S Consulting, LLC, Simulations Washington, DC; T. Zang, Zang M&S M. Nikbay, P. Acar, Istanbul Technical Aero-Engine Preliminary Design Zebulon, NC; S. Mahadevan, Vanderbilt A. Wendorff, J. Alonso, Stanford Consulting, LLC, Zebulon, NC; D. Mavris, J. Tai, University, Istanbul, Turkey J. Gramatyka, M. Eres, J. Scanlan, University, Nashville, TN; J. Tai, D. University, Stanford, CA; S. Bieniawski, Georgia Institute of Technology, Atlanta, GA University of Southampton, Southampton, Mavris, Georgia Institute of Technology, The Boeing Company, Seattle, WA United Kingdom; M. Moss, R. Bates, Rolls- Atlanta, GA Royce Group plc, Derby, United Kingdom Friday, 26 June 2015 309-NW-10 Networking Coffee Break Meeting Room Foyers 0900 - 0930 hrs
Author/Session Chair Index 121 A. da Silva, R., 9-AFM-2 Airiau, C., 5-AA-3 Allen, N., 45-AMT-3/GT-3 Anderson, J., 231-AA-36 Asada, K., 60-FD-6/PDL-2 Abdelhady, M., 43-AFM-3 Akaydin, H., 49-APA-7 Allerdice, J., 197-ATIO-18 Anderson, W., 95-CFD-9, 170-CFD-18, 305-CFD-35 Asano, K., 60-FD-6/PDL-2 Abdellatif, O., 178-MST-8 Akbarzadeh, S., 131-CFD-14 Allison, D., 104-MAO-3 Andre, F., 65-MST-3 Ashley, A., 176-MAO-5 Abdol-Hamid, K., 160-APA-17, 233-APA-25 Akella, M., 9-AFM-2 Allmaras, S., 95-CFD-9, 123-APA-14, 170-CFD-18 Andrews, S., 141-MAO-4, 267-APA-29 Ashton, N., 172-CFD-20, 230-AA-35 Abdrashitov, R., 226-AA-31 Akhtar, I., 133-CFD-16, 136-FD-15 Almeida, F., 249-FT-1 Andrienko, D., 69-TP-4, 256-TP-12 Astley, R., 78-AA-12 Abdul-Latif, A., 12-APA-1 Akilli, H., 25-FD-1 Almond, M., 88-APA-10 Anemaat, W., 117-ACD-3, 232-ACD-6 Atassi, H., 77-AA-11, 151-AA-21 Abe, M., 23-CFD-3 Akins, D., 279-FD-31 Alonso, E., 126-ATIO-12 Angland, D., 205-CFD-25, 259-AA-37, 263-AA-41 Atinault, O., 13-APA-2 Abe, T., 144-PDL-7 Alaoui, M., 226-AA-31 Alonso, J., 202-CFD-22, 204-CFD-24, 212-MAO-6, Ansaldi, T., 5-AA-3 Atkins, E., 274-ATIO-24 Abe, Y., 130-CFD-13 Alazard, D., 83-AFM-5 283-MAO-10, 284-MAO-11, 308-MAO-13 Anthony, J., 278-FD-30 Atkins, S., 140-ITAR-2 Acar, E., 64-MAO-2 Alba, C., 34-TP-1 Alonso-Miralles, J., 260-AA-38 Antônio dos Santos, D., 30-MST-1 Attanasio, L., 13-APA-2, 104-MAO-3 Acar, P., 308-MAO-13 Albring, T., 252-MAO-9, 283-MAO-10 AlQadi, I., 236-APA-28 Antony, T., 44-AFM-4 Aubert, A., 40-AA-9 Adams, N., 87-APA-9 Albuquerque, P., 104-MAO-3 Alter, S., 233-APA-25 Anupindi, K., 171-CFD-19 Aubry, S., 42-ACD-1, 299-ATIO-28 Adler, M., 245-CFD-30 Alcabin, M., 275-ATIO-25 Altmikus, A., 88-APA-10 Aoki, T., 68-TP-3 Avery, A., 196-ASE-2 Adusumilli, S., 159-AMT-10/GT-10 Alcorn, J., 250-LTA-1 Alunni, A., 216-TP-10/PDL-10 Aoki, Y., 89-APA-11 Awasthi, M., 261-AA-39 Afsar, M., 79-AA-13, 209-FD-24 Aleksentsev, A., 189-AA-30 Alves, L., 243-CFD-28 Aono, H., 268-APA-30 Ayton, L., 260-AA-38 Agarwal, N., 226-AA-31 Alessandro, T., 108-TP-5 Aly, A., 178-MST-8 Aponso, B., 91-ATIO-9 Ayyad, E., 31-MST-2 Agarwal, R., 26-FD-2, 47-APA-5, 122-APA-13, Alexander, W., 37-AA-6, 38-AA-7, 114-AA-18, Alyanak, E., 104-MAO-3, 176-MAO-5 Appel, C., 226-AA-31 Ayyalasomayajula, S., 284-MAO-11, 300-ATIO-29 139-FD-18, 182-TP-9, 211-FD-26, 304-CFD-34 152-AA-22, 187-AA-28, 260-AA-38, 261-AA-39 Alzamora Previtali, F., 102-FD-13 Appelbaum, J., 259-AA-37 Azarm, S., 29-MAO-1 Agbolosu-Amison, S., 197-ATIO-18 Alexeenko, A., 35-TP-2, 288-TP-13 Amadori, K., 283-MAO-10 Aradag, S., 204-CFD-24 Azarpeyvand, M., 3-AA-1, 38-AA-7 Agostini, L., 80-AA-14, 302-CFD-32 Alexeev, T., 9-AFM-2, 105-MST-5 Amaral, F., 230-AA-35 Arena, A., 157-AFM-9 Azevedo, J., 12-APA-1, 98-CFD-12, 241-CFD-26, Ahmad, N., 163-ASE-1, 237-ASE-3, 272-ASE-4, Alfonso, X., 234-APA-26 Amili, O., 153-AA-23 Arina, R., 155-AA-25 270-APA-32 298-ATIO-27 Algozino, S., 236-APA-28 Amitay, M., 63-FD-9, 101-FD-12, 248-FD-29 Arnal, D., 99-FD-10 Babbar, Y., 9-AFM-2, 124-APA-15, 270-APA-32 Ahmed, N., 115-AA-19 Aliaga, C., 196-ASE-2 Amos, D., 35-TP-2 Arndt, C., 266-AMT-13/GT-13 Baccala, L., 7-AA-5 Ahsan, N., 136-FD-15 Alizard, F., 98-CFD-12 Amundson, I., 128-ATIO-14 Arneson, H., 18-ATIO-3, 298-ATIO-27 Badrinath, S., 136-FD-15 Ahuja, K., 189-AA-30, 261-AA-39 Allen, B., 165-ATIO-16, 199-ATIO-20 Ananda Krishnan, G., 15-APA-4 Arora, N., 97-CFD-11, 248-FD-29, 268-APA-30 Baeder, J., 162-APA-19, 171-CFD-19 Ahuja, V., 127-ATIO-13, 161-APA-18 Allen, C., 64-MAO-2, 125-APA-16, 283-MAO-10 Andalibi, M., 48-APA-6 Arsenyev, I., 284-MAO-11 Baginski, F., 200-BAL-2 Aigner, M., 185-AA-26 Allen, J., 104-MAO-3 Anders, S., 49-APA-7, 281-GEPC-1 Arunajatesan, S., 139-FD-18, 175-FD-22, 229-AA-34 Bagwell, T., 140-ITAR-2 Author/Session Chair Index Bahr, C., 186-AA-27, 188-AA-29, 262-AA-40 Bergeron, K., 236-APA-28 Bombelli, A., 275-ATIO-25 Buehn, J., 303-CFD-33 Castner, R., 14-APA-3 Bai, B., 112-AA-16 Bering, E., 200-BAL-2 Bonnet, J., 180-PDL-8/APA-20 Bugeda, G., 180-PDL-8/APA-20 Cathey, H., 167-BAL-1 Bai, J., 49-APA-7, 145-TP-7 Bériot, H., 263-AA-41 Bons, J., 50-APA-8 Bulte, J., 3-AA-1, 261-AA-39, 262-AA-40 Catlett, M., 231-AA-36 Bailly, C., 4-AA-2, 114-AA-18, 231-AA-36 Berkefeld, T., 186-AA-27, 260-AA-38 Boo, K., 12-APA-1 Bunge, R., 8-AFM-1, 249-FT-1 Cattafesta, L., 248-FD-29 Bailly, D., 161-APA-18 Bernardini, G., 162-APA-19, 263-AA-41 Boom, P., 132-CFD-15 Buning, P., 230-AA-35 Caudle, D., 83-AFM-5 Bake, F., 41-AA-10, 151-AA-21 Bernardo, J., 52-ATIO-6, 198-ATIO-19 Bordeneuve, J., 83-AFM-5 Buono, A., 37-AA-6 Cavalieri, A., 5-AA-3, 41-AA-10, 80-AA-14, 189-AA-30, Bakker, B., 238-ATIO-21 Berner, C., 47-APA-5 Borer, N., 127-ATIO-13 Burns, R., 86-AMT-6/GT-6 260-AA-38 Balakumar, P., 61-FD-7, 139-FD-18, 248-FD-29 Berry, P., 283-MAO-10 Borg, M., 137-FD-16 Burnside, N., 186-AA-27 Cedric, C., 132-CFD-15 Balan, A., 95-CFD-9 Berry, S., 217-TP-11 Borges Sebastiao, I., 288-TP-13 Burt, J., 69-TP-4, 181-PDL-9/TP-8 Cerminara, A., 209-FD-24 Balaresque, N., 88-APA-10 Bersenev, Y., 189-AA-30 Borgoltz, A., 295-APA-34, 297-APA-37 Burtch, T., 8-AFM-1 Cesnik, C., 9-AFM-2, 119-AFM-8 Balas, G., 157-AFM-9 Berton, J., 77-AA-11 Borner, A., 288-TP-13 Busch, G., 37-AA-6 Cetin, M., 80-AA-14 Balboni, J., 108-TP-5, 216-TP-10/PDL-10 Beulze, B., 92-ATIO-10 Bosson, C., 16-ATIO-1 Busquets, J., 126-ATIO-12 Chabot, J., 175-FD-22 Baldacchino, D., 279-FD-31 Beuze, B., 18-ATIO-3 Botez, R., 13-APA-2, 18-ATIO-3, 66-MST-4, 84-AFM-6, Buttini, T., 9-AFM-2 Chaderjian, N., 136-FD-15 Ballard, B., 275-ATIO-25 Bevan, R., 125-APA-16 92-ATIO-10, 238-ATIO-21, 296-APA-35 Byerley, A., 15-APA-4 Chakraborty, I., 42-ACD-1, 156-ACD-4, 265-ACD-7 Bane, S., 255-PDL-12 Bevirt, J., 276-ATIO-26 Bouhaj, M., 226-AA-31 Bynum, M., 99-FD-10 Chakraborty, P., 246-FD-27 Bangert, L., 14-APA-3 Bhagat, N., 104-MAO-3 Bouley, S., 152-AA-22 Cai, J., 67-PDL-3, 178-MST-8 Chakravarthy, S., 245-CFD-30 Barbarino, M., 6-AA-4, 115-AA-19 Bhagwandin, V., 267-APA-29 Bousfield, S., 127-ATIO-13 Cai, W., 145-TP-7 Chalot, F., 99-FD-10 Barbeau, Z., 274-ATIO-24 Bhamidipati, K., 22-CFD-2 Boussuge, J., 188-AA-29 Cain, A., 88-APA-10, 143-PDL-6, 255-PDL-12 Chan, W., 305-CFD-35 Barmore, B., 298-ATIO-27 Bhaumik, S., 205-CFD-25 Bouty, E., 185-AA-26 Caldas, L., 7-AA-5 Chandar, D., 305-CFD-35 Barnes, C., 270-APA-32 Bianchi, D., 128-ATIO-14 Bouvy, Q., 259-AA-37 Callahan, R., 294-AMT-14/GT-15 Chaney, V., 249-FT-1 Barnes, J., 83-AFM-5 Bibik, P., 280-FT-2/GT-14 Bova, S., 202-CFD-22 Callender, M., 62-FD-8 Chang, C., 193-APA-21, 211-FD-26, 228-AA-33 Bartels, R., 124-APA-15 Bidino, D., 45-AMT-3/GT-3 Bowers, L., 166-ATIO-17, 239-ATIO-22 Callicoat, J., 231-AA-36 Chang, S., 35-TP-2, 145-TP-7 Bartoli, N., 82-ACD-2 Bienert, N., 51-ATIO-5 Bown, A., 167-BAL-1 Calvert, M., 15-APA-4, 194-APA-22 Chao, H., 43-AFM-3 Bartosch, S., 299-ATIO-28 Bieniawski, S., 308-MAO-13 Boxx, I., 266-AMT-13/GT-13 Calvert, N., 86-AMT-6/GT-6 Chao, T., 119-AFM-8 122 Bastide, M., 45-AMT-3/GT-3 Bieniek, D., 237-ASE-3 Boyd, I., 35-TP-2, 69-TP-4, 256-TP-12 Campbell, S., 16-ATIO-1, 298-ATIO-27 Chaput, A., 82-ACD-2, 128-ATIO-14 Basto, K., 234-APA-26 Bier, N., 105-MST-5 Brakke, K., 200-BAL-2 Candler, G., 139-FD-18, 202-CFD-22, 244-CFD-29, Chard, J., 271-APA-33 Bates, R., 308-MAO-13 Bijl, H., 97-CFD-11 Brambley, E., 7-AA-5, 81-AA-15 246-FD-27, 256-TP-12, 278-FD-30 Charnigo, R., 181-PDL-9/TP-8 Bathel, B., 86-AMT-6/GT-6, Bil, C., 42-ACD-1, 117-ACD-3, 190-ACD-5 Brandis, A., 69-TP-4, 217-TP-11 Canfield, R., 252-MAO-9 Chatterji, G., 142-MST-6, 253-MST-11 121-AMT-8/FD-14/TP-6/GT-8 Bilimoria, K., 177-MST-7 Brandon, J., 118-AFM-7, 249-FT-1 Canpolat, C., 25-FD-1 Chauvin, A., 227-AA-32 Batista, M., 30-MST-1 Bin Abdul Malik, M., 162-APA-19 Brandt, S., 64-MAO-2 Cantu, L., 86-AMT-6/GT-6 Chawner, J., 301-CFD-31 Batten, P., 245-CFD-30 Bisek, N., 98-CFD-12, 143-PDL-6, 245-CFD-30 Brauckmann, G., 233-APA-25 Capittini, G., 236-APA-28 Chazot, O., 108-TP-5 Bauer, M., 125-APA-16 Blackwell, B., 68-TP-3 Braud, P., 189-AA-30 Capizzano, F., 6-AA-4, 115-AA-19 Chedevergne, F., 60-FD-6/PDL-2 Bauman, P., 108-TP-5 Blair, L., 143-PDL-6 Brazier, J., 228-AA-33 Caprecci, M., 5-AA-3 Cheli, R., 26-FD-2 Baumgärtner, D., 283-MAO-10 Blaisdell, G., 113-AA-17, 139-FD-18, 245-CFD-30 Breard, C., 4-AA-2, 6-AA-4 Caraballo, E., 175-FD-22 Chelius, A., 187-AA-28 Baydar, E., 279-FD-31 Blake, M., 142-MST-6 Brehm, C., 4-AA-2 Caraeni, M., 39-AA-8 Chelliah, K., 262-AA-40 Bayoda, K., 33-PDL-1/FD-5 Blake, W., 8-AFM-1, 29-MAO-1, 273-ASE-5 Breitsamter, C., 87-APA-9 Cardito, F., 162-APA-19 Chen, G., 301-CFD-31 Beaverstock, C., 29-MAO-1 Blandeau, V., 77-AA-11 Brès, G., 5-AA-3, 80-AA-14 Cariou, J., 272-ASE-4 Chen, L., 191-AMT-11/GT-11, 250-LTA-1 Beck, J., 35-TP-2 Bleischwitz, R., 136-FD-15 Breviglieri, C., 241-CFD-26 Carlson, J., 58-CFD-8, 133-CFD-16 Chen, N., 92-ATIO-10, 191-AMT-11/GT-11 Bedouet, J., 299-ATIO-28 Bletzinger, K., 283-MAO-10 Brichet, G., 4-AA-2 Carmine, M., 26-FD-2 Chen, P., 284-MAO-11 Bekiropoulos, D., 155-AA-25 Bloebaum, C., 212-MAO-6 Bridges, J., 189-AA-30, 227-AA-32 Caro, S., 6-AA-4, 113-AA-17 Chen, S., 269-APA-31, 307-MAO-12 Bellemans, A., 216-TP-10/PDL-10 Blom, H., 238-ATIO-21 Briley, W., 15-APA-4, 297-APA-37 Carolus, T., 152-AA-22 Chen, W., 107-PDL-4, 151-AA-21, 260-AA-38 Belley, C., 204-CFD-24 Bo, Y., 35-TP-2, 145-TP-7 Britchford, K., 227-AA-32 Carranza Moyao, O., 84-AFM-6 Chen, X., 112-AA-16, 145-TP-7 Belmouss, M., 255-PDL-12 Bobenrieth Miserda, R., 77-AA-11 Broeren, A., 196-ASE-2 Carroll, D., 107-PDL-4, 166-ATIO-17 Chen, Y., 34-TP-1 Belyaev, I., 115-AA-19, 187-AA-28, 189-AA-30 Bocola, F., 84-AFM-6 Bronz, M., 161-APA-18 Carson, H., 170-CFD-18 Cheng, G., 193-APA-21, 211-FD-26 Benard, N., 33-PDL-1/FD-5, 180-PDL-8/APA-20 Boden, F., 231-AA-36 Broszat, D., 151-AA-21 Carter, C., 266-AMT-13/GT-13 Cheng, H., 229-AA-34 Bender, J., 256-TP-12 Boden, H., 7-AA-5, 261-AA-39 Brown, C., 189-AA-30, 228-AA-33, 280-FT-2/GT-14 Cartmell, D., 31-MST-2 Cheng, J., 122-APA-13 Bennaceur, I., 154-AA-24 Bogdanoff, D., 182-TP-9 Brown, K., 297-APA-37 Caruelle, B., 155-AA-25 Cheng, Y., 215-MST-10 Benton, S., 50-APA-8 Bogey, C., 4-AA-2, 5-AA-3, 229-AA-34 Brown, L., 158-AMT-9/GT-9 Casalino, D., 188-AA-29, 259-AA-37 Chernyshev, S., 228-AA-33 Berci, M., 236-APA-28 Boissonneau, F., 189-AA-30 Brown, M., 143-PDL-6, 214-MST-9 Casalis, G., 228-AA-33 Chevalley, E., 51-ATIO-5 Berdanier, R., 173-FD-19 Bolczak, C., 299-ATIO-28 Brown, R., 9-AFM-2 Casartelli, E., 203-CFD-23 Chhabra, R., 29-MAO-1 Beresh, S., 62-FD-8, 175-FD-22, 192-AMT-12/GT-12, Bolds-Moorehead, P., 249-FT-1 Brunet, M., 42-ACD-1 Casper, K., 28-FD-4, 103-ITAR-1, 140-ITAR-2, Chiba, K., 293-ACD-8 266-AMT-13/GT-13 Bolender, M., 44-AFM-4 Bryan, B., 261-AA-39 175-FD-22 Chiereghin, N., 270-APA-32 Author/Session Chair Index Chintagunta, A., 80-AA-14 Cole, S., 45-AMT-3/GT-3 Cutler, A., 86-AMT-6/GT-6, Del Rosario, R., 281-GEPC-1 Dong, M., 99-FD-10 Chng, S., 162-APA-19 Collery, O., 226-AA-31 121-AMT-8/FD-14/TP-6/GT-8 DeLaurentis, D., 52-ATIO-6, 239-ATIO-22, 300-ATIO-29 Dong, X., 84-AFM-6 Chng, T., 143-PDL-6 Collins, E., 41-AA-10, 81-AA-15 Cymbalist, N., 27-FD-3, 278-FD-30 Deleglise, B., 46-AMT-4/GT-4 Dongre, R., 250-LTA-1 Cho, K., 235-APA-27 Colmenares, J., 96-CFD-10, 205-CFD-25 D’Souza, S., 43-AFM-3 Delfs, J., 79-AA-13, 112-AA-16, 230-AA-35, Doolan, C., 115-AA-19, 152-AA-22, 231-AA-36 Choi, J., 27-FD-3, 55-CFD-5, 62-FD-8, 132-CFD-15, Coloe, B., 274-ATIO-24 Da Ronch, A., 9-AFM-2, 84-AFM-6 231-AA-36, 263-AA-41 Doty, M., 158-AMT-9/GT-9 133-CFD-16, 251-MAO-8, 296-APA-35 Colonius, T., 5-AA-3, 80-AA-14, 228-AA-33 da Silva, A., 4-AA-2 Delisi, D., 237-ASE-3, 272-ASE-4 Dougherty, N., 68-TP-3, 228-AA-33 Choi, S., 12-APA-1, 64-MAO-2, 89-APA-11, 132-CFD-15, Colonno, M., 212-MAO-6 da Silva, F., 4-AA-2 Dell’Orso, H., 101-FD-12, 248-FD-29 Douville, T., 180-PDL-8/APA-20, 269-APA-31 251-MAO-8, 296-APA-35, 307-MAO-12 Commo, S., 120-AMT-7/GT-7, 294-AMT-14/GT-15 Dahl, D., 39-AA-8 Della Vecchia, P., 8-AFM-1, 13-APA-2 Dowell, E., 307-MAO-12 Chong, T., 3-AA-1 Communier, D., 84-AFM-6 Dahl, M., 78-AA-12 Dellery, B., 167-BAL-1 Dowling, D., 211-FD-26 Chou, A., 209-FD-24 Constantinescu, E., 163-ASE-1 Dale, G., 26-FD-2, 210-FD-25 Delnero, J., 236-APA-28 Downing, J., 40-AA-9 Choudhari, M., 56-CFD-6, 99-FD-10, 137-FD-16, Cooke, R., 308-MAO-13 Dalle, D., 233-APA-25 Demauro, E., 101-FD-12 Doyle, J., 90-APA-12 155-AA-25, 230-AA-35 Coppenbarger, R., 91-ATIO-9 Daly, C., 38-AA-7 Demeautis, C., 45-AMT-3/GT-3 Draper, M., 274-ATIO-24 Choudhary, A., 97-CFD-11 Cordes, U., 50-APA-8, 271-APA-33 Damodaran, M., 205-CFD-25, 235-APA-27, 250-LTA-1 Demers, F., 60-FD-6/PDL-2 Drew, M., 126-ATIO-12 Choutapalli, I., 276-ATIO-26 Coreixas, C., 188-AA-29 Dancila, B., 92-ATIO-10 Demers Bouchard, E., 276-ATIO-26 Driver, D., 108-TP-5 Chowdhary, G., 274-ATIO-24 Correale, G., 33-PDL-1/FD-5, 60-FD-6/PDL-2 Dancila, R., 18-ATIO-3 Deng, S., 97-CFD-11 Drozda, T., 244-CFD-29 Chowdhury, S., 176-MAO-5, 213-MAO-7, 251-MAO-8, Correia Grácio, B., 31-MST-2 Danehy, P., 86-AMT-6/GT-6, Deniau, H., 229-AA-34 Dryer, J., 281-GEPC-1 308-MAO-13 Corrigan, A., 153-AA-23 121-AMT-8/FD-14/TP-6/GT-8 Denieul, Y., 83-AFM-5 Duan, D., 250-LTA-1 Christophe, J., 79-AA-13, 112-AA-16 Costes, M., 161-APA-18 Daniels, C., 273-ASE-5 Denison, M., 248-FD-29 Duan, F., 47-APA-5 Chua, Z., 65-MST-3 Cotton, W., 275-ATIO-25 Dannenhoffer, J., 301-CFD-31 Denisov, S., 115-AA-19 Duan, L., 137-FD-16, 205-CFD-25 Chudoba, B., 53-ATIO-7 Coulouvrat, F., 114-AA-18 Dantsker, O., 87-APA-9 Denissen, K., 195-APA-23 Duan, Z., 23-CFD-3, 56-CFD-6 Chue, R., 269-APA-31 Coupe, J., 91-ATIO-9, 198-ATIO-19 Daoud, F., 212-MAO-6 Dennis, B., 48-APA-6 Dubot, T., 299-ATIO-28 Chwalowski, P., 124-APA-15 Coupland, J., 78-AA-12, 264-AA-42 Darmofal, D., 95-CFD-9, 170-CFD-18 Deodhar, N., 282-LTA-2 Dubourg, V., 167-BAL-1 Chynoweth, B., 28-FD-4 Courty, J., 99-FD-10 Daskiran, O., 128-ATIO-14 Derlaga, J., 97-CFD-11 Dubov, Y., 31-MST-2 Ciarella, A., 29-MAO-1 Cousy, M., 65-MST-3 Davidson, L., 6-AA-4, 115-AA-19, 154-AA-24 Deschamps, C., 4-AA-2, 80-AA-14 Ducruix, S., 185-AA-26 123 Ciliberti, D., 13-APA-2 Coyle, C., 90-APA-12, 195-APA-23 Daviller, G., 229-AA-34 Desmet, W., 3-AA-1, 113-AA-17 Duda, B., 188-AA-29 Cinnella, P., 62-FD-8, 113-AA-17, 132-CFD-15 Cozzi, F., 26-FD-2 Davis, D., 85-AMT-5/GT-5 Deters, R., 15-APA-4 Duddeck, F., 284-MAO-11 Ciobaca, V., 125-APA-16 Craig, S., 137-FD-16 Davis, R., 203-CFD-23 Devenport, W., 37-AA-6, 38-AA-7, 114-AA-18, Duffy, M., 194-APA-22 Cisneros, E., 216-TP-10/PDL-10 Cranford, J., 30-MST-1 Davy, R., 3-AA-1, 262-AA-40 152-AA-22, 187-AA-28, 260-AA-38, 261-AA-39, Dumitrache, C., 107-PDL-4, 143-PDL-6 Cisotto, A., 46-AMT-4/GT-4 Crawford, B., 137-FD-16 Dawson, R., 174-FD-20 295-APA-34, 297-APA-37 Duncan, G., 137-FD-16 Civinskas, K., 281-GEPC-1 Crawley, M., 153-AA-23 Dawson, S., 136-FD-15 Dewey, R., 167-BAL-1 Duncan, M., 85-AMT-5/GT-5 Clair, V., 6-AA-4, 113-AA-17 Cromer, K., 282-LTA-2 De Breuker, R., 29-MAO-1 Dey, S., 301-CFD-31 Dunlap, P., 273-ASE-5 Clark, A., 276-ATIO-26 Cross, C., 165-ATIO-16, 199-ATIO-20 de Jong, A., 38-AA-7 Dhaene, T., 66-MST-4 Dunn, S., 45-AMT-3/GT-3, 191-AMT-11/GT-11 Clark, I., 38-AA-7 Crossley, W., 52-ATIO-6, 82-ACD-2 De Kat, R., 136-FD-15 Dhamankar, N., 245-CFD-30 Dunne, R., 162-APA-19 Clarke, S., 240-ATIO-23 Crouch, J., 61-FD-7 De La Puente, F., 259-AA-37 Dias, B., 34-TP-1 Duque, E., 301-CFD-31, 302-CFD-32 Clemens, N., 33-PDL-1/FD-5, 174-FD-20 Crow, B., 197-ATIO-18 De Marco, A., 8-AFM-1, 104-MAO-3 Dias, J., 118-AFM-7 Duraisamy, K., 58-CFD-8 Cléro, F., 185-AA-26 Crowther, W., 30-MST-1, 271-APA-33 de Monte, F., 35-TP-2 Dickey, D., 189-AA-30 Durak, U., 177-MST-7 Cliff, S., 89-APA-11 Cruden, B., 69-TP-4, 182-TP-9, 217-TP-11 de Oliveira, G., 286-PDL-13 Dickey, E., 49-APA-7, 87-APA-9 Durand, C., 154-AA-24 Clingman, D., 63-FD-9 Cruz, E., 63-FD-9 De Roeck, W., 113-AA-17 Dief, T., 43-AFM-3 Dutta, S., 44-AFM-4 Close, S., 286-PDL-13 Cuenca, R., 7-AA-5 de Santana, L., 3-AA-1 Dierke, J., 39-AA-8, 185-AA-26, 263-AA-41 Dzikus, N., 239-ATIO-22, 299-ATIO-28 Cloutier, R., 239-ATIO-22 Cui, D., 178-MST-8 de Souza, F., 192-AMT-12/GT-12 DiGirolamo, E., 265-ACD-7 Echekki, T., 185-AA-26 Cluts, J., 153-AA-23 Cui, H., 44-AFM-4 DeArmon, J., 197-ATIO-18 Dilan, G., 285-MST-12 Economon, T., 133-CFD-16, 204-CFD-24, 212-MAO-6, Coakley, T., 172-CFD-20 Cui, K., 296-APA-35 DeBonis, J., 55-CFD-5, 130-CFD-13, 175-FD-22 Dill, E., 166-ATIO-17 271-APA-33, 283-MAO-10 Cobb, P., 142-MST-6 Culbreth, W., 31-MST-2 DeChant, L., 139-FD-18 Dimotakis, P., 27-FD-3, 139-FD-18, 244-CFD-29, Edgington-Mitchell, D., 153-AA-23 Cobb, R., 141-MAO-4, 158-AMT-9/GT-9 Cummings, R., 63-FD-9, 160-APA-17, 236-APA-28, DeCicco, A., 65-MST-3, 142-MST-6 278-FD-30 Edoh, A., 132-CFD-15 Coder, J., 58-CFD-8, 61-FD-7 278-FD-30, 305-CFD-35 Decker, R., 278-FD-30 Diosady, L., 21-CFD-1, 201-CFD-21 Edwards, D., 48-APA-6 Coen, P., 281-GEPC-1 Cunha, G., 155-AA-25 Dedic, C., 181-PDL-9/TP-8 Dirk, B., 230-AA-35 Edwards, J., 203-CFD-23 Coetzee, E., 105-MST-5 Cunha, M., 282-LTA-2 Dees, J., 173-FD-19 Djeddi, R., 243-CFD-28 Edwards, M., 86-AMT-6/GT-6 Cofer, A., 35-TP-2 Cuoci, A., 244-CFD-29 Deese, J., 282-LTA-2 Dogan, A., 8-AFM-1, 83-AFM-5, 128-ATIO-14, 273-ASE-5 Efraimsson, G., 78-AA-12, 235-APA-27 Coggon, S., 213-MAO-7 Curley, A., 306-CFD-36 DeGennaro, A., 295-APA-34 Dogariu, A., 86-AMT-6/GT-6 Egorov, I., 99-FD-10 Cohen, E., 226-AA-31 Curran, R., 51-ATIO-5, 91-ATIO-9, 198-ATIO-19, Degrez, G., 216-TP-10/PDL-10 Dolfi-Bouteyre, A., 272-ASE-4 Ehrenfried, K., 260-AA-38 Colantonio, R., 281-GEPC-1 275-ATIO-25 Deinert, S., 212-MAO-6 Donadon, M., 260-AA-38 Eisfeld, B., 172-CFD-20 Colburn, K., 301-CFD-31 Cusati, V., 13-APA-2 Del Rey Fernández, D., 169-CFD-17, 242-CFD-27 Dong, H., 136-FD-15, 248-FD-29 Eitelberg, G., 37-AA-6, 269-APA-31 Author/Session Chair Index Ekaterin, J., 56-CFD-6 Felder, W., 239-ATIO-22 Fucke, L., 31-MST-2 Gennaretti, M., 162-APA-19, 263-AA-41 Gonda, J., 239-ATIO-22 Ekici, K., 243-CFD-28 Feldhusen, A., 41-AA-10 Fujii, K., 60-FD-6/PDL-2, 114-AA-18, 130-CFD-13, George, J., 11-AMT-2/GT-2, 50-APA-8 Gong, C., 252-MAO-9, 298-ATIO-27 Ekmekci, A., 259-AA-37 Felipe, V., 16-ATIO-1 169-CFD-17 Georgiadis, N., 175-FD-22 Gonzalez, D., 303-CFD-33 Ekoule, C., 37-AA-6 Félix Patrón, R., 18-ATIO-3 Fujino, T., 286-PDL-13 Gerber, T., 167-BAL-1 Gonzalez, L., 101-FD-12 El baialy, I., 178-MST-8 Feltrop, E., 270-APA-32 Fujita, K., 68-TP-3, 69-TP-4 Gerlach, T., 177-MST-7 Gonzalez-Linero, L., 190-ACD-5 Elham, A., 64-MAO-2 Feng, F., 80-AA-14 Fujiwara, G., 49-APA-7 German, B., 93-ATIO-11, 127-ATIO-13 Goodrich, K., 93-ATIO-11, 199-ATIO-20 Eliasson, P., 160-APA-17 Fenouil, J., 295-APA-34 Fuller, C., 226-AA-31 Gern, F., 82-ACD-2 Gopalarathnam, A., 235-APA-27, 267-APA-29 Eljack, E., 236-APA-28 Ferguson, S., 64-MAO-2, 104-MAO-3, 308-MAO-13 Funk, C., 124-APA-15 Gerz, T., 196-ASE-2 Goparaju, K., 205-CFD-25 Ellejmi, M., 91-ATIO-9 Fermen-Coker, M., 119-AFM-8 Furukawa, D., 89-APA-11 Getsinger, D., 173-FD-19 Gordeyev, S., 88-APA-10, 143-PDL-6, 255-PDL-12 Elmiligui, A., 160-APA-17, 285-MST-12 Fern, L., 274-ATIO-24 Gabard, G., 6-AA-4, 78-AA-12, 113-AA-17, 263-AA-41 Geuther, S., 164-ATIO-15 Gordnier, R., 62-FD-8, 208-FD-23 Empl, D., 53-ATIO-7 Fernandes de Oliveira, R., 104-MAO-3 Gabbert, D., 48-APA-6 Geyer, T., 231-AA-36 Gorham, P., 200-BAL-2 Enghardt, L., 151-AA-21, 152-AA-22, 173-FD-19 Fernando, A., 229-AA-34 Gaddai, A., 203-CFD-23 Gezer, R., 83-AFM-5 Gori, G., 133-CFD-16, 196-ASE-2 Enjiao, Z., 119-AFM-8 Fernando, R., 187-AA-28 Gaeta, R., 37-AA-6, 231-AA-36 Gherman, G., 96-CFD-10 Gori, R., 162-APA-19 Entz, R., 104-MAO-3 Ferrari, D., 117-ACD-3, 213-MAO-7 Gaitonde, D., 80-AA-14, 174-FD-20, 205-CFD-25, Ghorawat, P., 84-AFM-6 Gorrell, S., 302-CFD-32 Envia, E., 264-AA-42 Ferreira de Castro, D., 30-MST-1 245-CFD-30, 266-AMT-13/GT-13, 302-CFD-32, Ghorbaniasl, G., 152-AA-22 Gorton, S., 281-GEPC-1 Eppink, J., 137-FD-16 Fidkowski, K., 95-CFD-9, 170-CFD-18 303-CFD-33 Ghoreyshi, M., 236-APA-28, 305-CFD-35 Gourinat, Y., 82-ACD-2 Eres, M., 128-ATIO-14, 308-MAO-13 Field, J., 31-MST-2 Galbraith, M., 170-CFD-18 Ghosh, A., 118-AFM-7 Govindarajan, R., 28-FD-4 Eriksson, L., 6-AA-4, 154-AA-24 Fields, T., 157-AFM-9 Gallman, J., 79-AA-13 Ghosh, D., 163-ASE-1 Govindaraju, P., 82-ACD-2 Ernst, D., 186-AA-27 Fiévet, R., 304-CFD-34 Gallo, E., 86-AMT-6/GT-6 Ghosh, S., 125-APA-16, 213-MAO-7 Goyal, T., 234-APA-26 Errico, A., 164-ATIO-15 Filippone, E., 164-ATIO-15, 300-ATIO-29 Galyen, N., 11-AMT-2/GT-2 Giauque, A., 185-AA-26 Goyne, C., 159-AMT-10/GT-10 Erturk, S., 83-AFM-5 Filizola, A., 65-MST-3 Gamba, M., 102-FD-13 Giepman, R., 138-FD-17 Grabe, C., 61-FD-7 Escobar, J., 234-APA-26 Findanis, N., 125-APA-16 Gambardella, D., 104-MAO-3 Gil Prieto, D., 270-APA-32 Grace, S., 264-AA-42 Esker, B., 281-GEPC-1 Finley, D., 47-APA-5, 161-APA-18 Gamblin, R., 200-BAL-2 Gildersleeve, S., 101-FD-12 Graham, R., 51-ATIO-5 Etchessahar, M., 226-AA-31 Fiore, G., 297-APA-37 Gamboa, P., 43-AFM-3, 104-MAO-3 Giles, M., 200-BAL-2 Gramatyka, J., 308-MAO-13 124 Etienne, S., 304-CFD-34 Firsov, A., 107-PDL-4 Gan, J., 90-APA-12 Gilge, P., 235-APA-27 Granlund, K., 63-FD-9, 175-FD-22 Evans, A., 126-ATIO-12 Fischels, M., 243-CFD-28 Ganapathisubramani, B., 3-AA-1, 38-AA-7, 136-FD-15 Gill, J., 112-AA-16, 113-AA-17, 152-AA-22, 260-AA-38 Grant, J., 37-AA-6 Evans, M., 244-CFD-29 Fischer, P., 202-CFD-22 Gao, D., 107-PDL-4 Gillespie, E., 8-AFM-1 Grant, M., 44-AFM-4, 83-AFM-5 Eversman, W., 7-AA-5 Fischersworring-Bunk, A., 284-MAO-11 Gao, Z., 161-APA-18, 213-MAO-7 Gilliam, F., 64-MAO-2 Grasso, F., 98-CFD-12 Ewert, R., 38-AA-7, 39-AA-8, 41-AA-10, 79-AA-13, Fisher, T., 145-TP-7, 202-CFD-22 Garcia, D., 282-LTA-2 Gilmore, B., 104-MAO-3 Grasso, G., 112-AA-16 112-AA-16, 155-AA-25, 185-AA-26, 230-AA-35 Flatau, A., 50-APA-8 Garcia, E., 239-ATIO-22 Ginn, S., 240-ATIO-23 Graube, P., 108-TP-5 Eyi, S., 57-CFD-7, 131-CFD-14, 244-CFD-29 Fletcher, D., 181-PDL-9/TP-8 Gargiulo, F., 164-ATIO-15 Giret, J., 188-AA-29 Grauer, J., 118-AFM-7 Eymann, T., 174-FD-20 Fleury, V., 3-AA-1, 262-AA-40 Garland, M., 142-MST-6 Girimaji, S., 58-CFD-8 Green, C., 240-ATIO-23 Fagan, A., 189-AA-30 Florez Mera, J., 35-TP-2 Garman, K., 249-FT-1 Glaab, P., 142-MST-6 Green, M., 26-FD-2 Fagley, C., 12-APA-1, 125-APA-16 Foster, J., 157-AFM-9 Garmann, D., 208-FD-23, 302-CFD-32 Glass, C., 233-APA-25 Greenblatt, D., 101-FD-12, 158-AMT-9/GT-9, 208-FD-23 Fairbrother, D., 167-BAL-1, 200-BAL-2 Foster, N., 305-CFD-35 Garrard, G., 120-AMT-7/GT-7 Glegg, S., 37-AA-6, 38-AA-7, 77-AA-11, 114-AA-18, Greendyke, R., 34-TP-1 Fala, N., 156-ACD-4 Foster, T., 240-ATIO-23 Garrett, S., 98-CFD-12, 209-FD-24 187-AA-28, 261-AA-39 Greene, B., 33-PDL-1/FD-5 Falcão, C., 243-CFD-28 Fouladi, H., 196-ASE-2 Garrick, D., 243-CFD-28 Gloerfelt, X., 56-CFD-6, 62-FD-8, 113-AA-17 Greene, G., 237-ASE-3 Falissard, F., 154-AA-24 François, B., 152-AA-22 Gartner, J., 63-FD-9 , 154-AA-24, 226-AA-31 Greene, K., 43-AFM-3 Fan, D., 56-CFD-6 Franke, D., 13-APA-2 Gary, J., 167-BAL-1 Gloudemans, J., 82-ACD-2 Gregory, J., 33-PDL-1/FD-5, 268-APA-30 Fan, H., 165-ATIO-16, 199-ATIO-20 Frankhouser, M., 33-PDL-1/FD-5 Gasbarri, P., 119-AFM-8 Gnoffo, P., 132-CFD-15 Grenon, R., 13-APA-2 Fan, Y., 180-PDL-8/APA-20 Franko, K., 202-CFD-22 Gatian, K., 52-ATIO-6 Goblet, V., 156-ACD-4 Griffiths, P., 209-FD-24 Faranosov, G., 115-AA-19, 189-AA-30, 228-AA-33 Frassoldati, A., 244-CFD-29 Gatlin, G., 88-APA-10 Góes, L., 30-MST-1, 282-LTA-2 Grimm, F., 185-AA-26 Fares, E., 188-AA-29 Frazza, L., 58-CFD-8 Gauger, N., 79-AA-13, 252-MAO-9, 283-MAO-10 Gogineni, S., 266-AMT-13/GT-13 Grimmen, J., 305-CFD-35 Farnsworth, J., 162-APA-19 Fredericks, W., 19-ATIO-4, 127-ATIO-13 Gauthier, T., 47-APA-5 Gojon, R., 4-AA-2 Grimsley, J., 140-ITAR-2 Farr, R., 228-AA-33 Freret, L., 97-CFD-11 Gautier, M., 238-ATIO-21 Gokcen, T., 34-TP-1, 108-TP-5, 216-TP-10/PDL-10 Grinstead, J., 69-TP-4 Farrington, A., 202-CFD-22 Fresconi, F., 90-APA-12, 119-AFM-8 Gea-Aguilera, F., 112-AA-16 Golaszewski, R., 275-ATIO-25 Grivel, A., 46-AMT-4/GT-4 Fasel, H., 28-FD-4, 100-FD-11, 102-FD-13, 208-FD-23 Freund, J., 78-AA-12 Gebreegziabher, A., 42-ACD-1 Goldberg, U., 245-CFD-30 Gross, A., 208-FD-23 Fassmann, B., 79-AA-13 Frew, E., 157-AFM-9, 273-ASE-5 Geder, J., 48-APA-6, 233-APA-25 Goldsmith, B., 276-ATIO-26 Gross, R., 99-FD-10 Fattah, R., 113-AA-17, 263-AA-41 Friedman, A., 176-MAO-5, 296-APA-35 Gee, K., 40-AA-9 Goldstein, D., 288-TP-13 Groth, C., 97-CFD-11, 171-CFD-19, 304-CFD-34 Fedorov, A., 99-FD-10 Friedman, C., 236-APA-28 Geisbauer, S., 105-MST-5, 195-APA-23 Goli, N., 265-ACD-7 Ground, C., 86-AMT-6/GT-6 Fehlman, W., 165-ATIO-16, 199-ATIO-20 Frischemeier, S., 117-ACD-3 Geisler, R., 159-AMT-10/GT-10 Golubev, A., 226-AA-31 Grund, T., 125-APA-16 Fehrenbach, S., 274-ATIO-24 Fuchs, M., 306-CFD-36 Gemma, S., 29-MAO-1 Golubev, V., 79-AA-13 Gu, L., 252-MAO-9 Author/Session Chair Index Gu, Q., 265-ACD-7 Harker, B., 40-AA-9 Herzog, S., 252-MAO-9 Hua, J., 35-TP-2 Jack, D., 43-AFM-3 Gu, Y., 43-AFM-3 Harrington, A., 136-FD-15 Hess, C., 11-AMT-2/GT-2 Huang, G., 159-AMT-10/GT-10, 162-APA-19, Jackson, G., 145-TP-7 Guan, Y., 38-AA-7 Harris, R., 41-AA-10, 81-AA-15, 195-APA-23, 241-CFD-26 Hickel, S., 87-APA-9 267-APA-29, 270-APA-32 Jackson, R., 138-FD-17 Guardone, A., 26-FD-2, 133-CFD-16, 196-ASE-2 Harrison, E., 156-ACD-4 Hicken, J., 176-MAO-5, 212-MAO-6, 242-CFD-27, Huang, X., 7-AA-5, 26-FD-2, 78-AA-12, 113-AA-17 Jackson, T., 203-CFD-23 Guenther, C., 305-CFD-35 Harshe, S., 235-APA-27 251-MAO-8 Huang, Z., 99-FD-10 Jacob, D., 237-ASE-3, 272-ASE-4 Guerin, S., 41-AA-10, 77-AA-11 Hartfield, R., 127-ATIO-13, 161-APA-18 Hiepler, `., 302-CFD-32 Hubbard, E., 191-AMT-11/GT-11 Jacob, J., 37-AA-6, 48-APA-6, 140-ITAR-2, 196-ASE-2, Guerreiro, N., 17-ATIO-2 Hartwich, P., 87-APA-9, 133-CFD-16 Higdon, K., 288-TP-13 Hubbard, J., 12-APA-1, 50-APA-8 231-AA-36, 274-ATIO-24, 280-FT-2/GT-14 Guerri, O., 305-CFD-35 Hasan, S., 65-MST-3, 142-MST-6, 197-ATIO-18, High, J., 165-ATIO-16 Huber, J., 189-AA-30 Jacobi, R., 100-FD-11 Guglielmo, J., 235-APA-27 275-ATIO-25 Higuera Caubilla, D., 58-CFD-8 Hue, D., 13-APA-2 Jacobs, S., 107-PDL-4 Guminsky, M., 142-MST-6, 299-ATIO-28 Hash, D., 288-TP-13 Hildebrand, N., 4-AA-2 Huehne, C., 125-APA-16 Jacques, D., 141-MAO-4 Guo, C., 84-AFM-6 Hashemi, A., 68-TP-3 Hiner, W., 79-AA-13 Huet, M., 185-AA-26 Jaffrezic, B., 178-MST-8 Guo, J., 164-ATIO-15 Hashemi, K., 9-AFM-2 Hinze, N., 300-ATIO-29 Huff, B., 128-ATIO-14 Jain, N., 171-CFD-19 Guo, Y., 112-AA-16, 116-AA-20 Haskin, H., 158-AMT-9/GT-9 Hipp, K., 50-APA-8 Hufnagel, K., 271-APA-33 Jalali, A., 21-CFD-1 Gupta, A., 97-CFD-11, 268-APA-30 Hasnain, Z., 12-APA-1, 50-APA-8 Hiramoto, R., 293-ACD-8 Hug, S., 24-CFD-4 Jambunathan, R., 203-CFD-23 Gupta, M., 38-AA-7 Hassan, M., 37-AA-6, 42-ACD-1, 53-ATIO-7, 239-ATIO-22 Hirayama, T., 66-MST-4 Hughes, M., 196-ASE-2 James, M., 40-AA-9 Gupte, A., 57-CFD-7 Hassan, W., 15-APA-4 Hitzel, S., 160-APA-17 Hui, F., 108-TP-5 Jameson, A., 55-CFD-5, 123-APA-14, 132-CFD-15, Gursul, I., 25-FD-1, 138-FD-17 Hathaway, J., 196-ASE-2 Hixon, D., 6-AA-4, 78-AA-12, 81-AA-15, 154-AA-24, Hulshoff, S., 33-PDL-1/FD-5 271-APA-33 Gutmark, E., 153-AA-23 Hattenberger, G., 161-APA-18 229-AA-34 Hultgren, L., 151-AA-21 Janjic, Z., 163-ASE-1 Guynn, M., 293-ACD-8 Haxter, S., 260-AA-38 Hoelling, M., 50-APA-8 Humpert, B., 37-AA-6 Jann, T., 105-MST-5 Guyton, R., 85-AMT-5/GT-5 Hay, A., 58-CFD-8, 204-CFD-24, 304-CFD-34 Hoffler, K., 43-AFM-3 Humphreys, C., 141-MAO-4 Jaouani, N., 187-AA-28 Guzel, G., 304-CFD-34 Hayashibara, S., 27-FD-3 Hoffman, R., 142-MST-6 Humphreys, W., 188-AA-29 Jaron, R., 77-AA-11 Habashi, W., 196-ASE-2 Hayden, T., 88-APA-10, 143-PDL-6, 255-PDL-12 Hoffmann, K., 175-FD-22 Hur, J., 124-APA-15 Jarzembski, A., 250-LTA-1 Habbit, R., 96-CFD-10 Hays, T., 157-AFM-9 Höger, M., 151-AA-21 Hussein, A., 236-APA-28 Jastrzebski, M., 17-ATIO-2 Haeri, S., 261-AA-39 Haywood, J., 24-CFD-4 Holladay, W., 85-AMT-5/GT-5 Hussein, S., 246-FD-27 Jaunet, V., 80-AA-14, 189-AA-30 125 Hafez, M., 105-MST-5, 278-FD-30 Hazir, A., 188-AA-29 Holland, K., 186-AA-27 Hutcheson, F., 4-AA-2, 158-AMT-9/GT-9 Jaworski, J., 25-FD-1, 38-AA-7 Haga, T., 130-CFD-13 He, A., 272-ASE-4 Holland, M., 117-ACD-3 Huynh, H., 55-CFD-5, 130-CFD-13, 170-CFD-18, Jenkins, L., 188-AA-29, 192-AMT-12/GT-12 Hagen, G., 17-ATIO-2 He, C., 280-FT-2/GT-14 Hölling, M., 271-APA-33 242-CFD-27 Jenkins, T., 11-AMT-2/GT-2, 159-AMT-10/GT-10 Hahn, M., 29-MAO-1 Hebert, P., 85-AMT-5/GT-5 Hollingsworth, P., 30-MST-1, 53-ATIO-7 Hwang, I., 31-MST-2, 126-ATIO-12 Jensen, L., 156-ACD-4 Haimes, R., 302-CFD-32 Hedrick, T., 100-FD-11 Holst, T., 136-FD-15 Hwang, J., 29-MAO-1, 307-MAO-12 Jessberger, C., 52-ATIO-6 Hainaut, T., 6-AA-4 Heeg, J., 124-APA-15 Holzäpfel, F., 196-ASE-2, 237-ASE-3 Idier, A., 3-AA-1 Jesus, A., 98-CFD-12 Haji-Sheikh, A., 35-TP-2 Heffernon, T., 259-AA-37 Hong, S., 51-ATIO-5, 166-ATIO-17 Idris, H., 16-ATIO-1, 275-ATIO-25 Jewell, J., 28-FD-4 Hajian, R., 25-FD-1 Hegde, A., 174-FD-20 Hong, Z., 107-PDL-4 Ihme, M., 151-AA-21, 242-CFD-27 Ji, C., 116-AA-20 Hajj, M., 236-APA-28 Hegen, S., 13-APA-2 Honnery, D., 153-AA-23 Ikeda, T., 155-AA-25 Ji, L., 151-AA-21 Hale, L., 30-MST-1 Heineck, J., 192-AMT-12/GT-12 Hoogreef, M., 42-ACD-1, 176-MAO-5 Im, D., 12-APA-1, 132-CFD-15 Jianchun, X., 215-MST-10 Hall, D., 64-MAO-2 Heinrich, R., 57-CFD-7 Hopf, J., 191-AMT-11/GT-11 Imamura, T., 155-AA-25, 241-CFD-26 Jiang, C., 180-PDL-8/APA-20 Hall, J., 283-MAO-10 Heiser, W., 15-APA-4 Horchler, T., 302-CFD-32 Imlay, S., 301-CFD-31 Jiang, H., 78-AA-12 Hallock, J., 237-ASE-3 Heitmeir, F., 151-AA-21 Horio, B., 65-MST-3, 142-MST-6 Ims, J., 23-CFD-3 Jiang, N., 86-AMT-6/GT-6 Halls, B., 86-AMT-6/GT-6 Helber, B., 108-TP-5 Horkheimer, D., 282-LTA-2 Imtiaz, H., 133-CFD-16 Jiang, Z., 22-CFD-2 Ham, F., 202-CFD-22 Helm, S., 91-ATIO-9 Horn, J., 43-AFM-3, 83-AFM-5 Ingraham, D., 6-AA-4 Jiao, J., 263-AA-41 Hamane, D., 305-CFD-35 Hempley, L., 165-ATIO-16, 199-ATIO-20 Horne, W., 186-AA-27, 262-AA-40 Ioppolo, T., 46-AMT-4/GT-4 Jie, B., 253-MST-11 Hamiche, K., 263-AA-41 Henderson, B., 227-AA-32 Hornung, M., 88-APA-10, 91-ATIO-9, 253-MST-11 Iorio, M., 101-FD-12 Jimenez, H., 52-ATIO-6, 156-ACD-4, 293-ACD-8 Hammack, S., 107-PDL-4 Henderson, R., 137-FD-16 Hosangadi, P., 235-APA-27 Ishida, Y., 68-TP-3 Jin, J., 85-AMT-5/GT-5 Hammock, G., 158-AMT-9/GT-9, 191-AMT-11/GT-11 Henfling, J., 62-FD-8, 175-FD-22 Hosder, S., 58-CFD-8 Ishioka, H., 270-APA-32 Jin, W., 85-AMT-5/GT-5 Han, K., 198-ATIO-19 Henry de Frahan, M., 201-CFD-21 Hosseinverdi, S., 100-FD-11 Ishutkina, M., 298-ATIO-27 Jing, C., 252-MAO-9 Han, X., 144-PDL-7 Herbst, S., 88-APA-10, 253-MST-11 Housman, J., 4-AA-2, 14-APA-3, 49-APA-7 Isikveren, A., 53-ATIO-7 Jinwu, X., 214-MST-9 Hannemann, K., 302-CFD-32 Hereth, L., 15-APA-4 Howard, M., 68-TP-3 Itasse, M., 228-AA-33 Jirasek, A., 160-APA-17, 305-CFD-35 Hanquist, K., 35-TP-2 Herold, G., 186-AA-27, 231-AA-36 Howerton, B., 7-AA-5, 116-AA-20 Ito, H., 23-CFD-3 Jo, Y., 251-MAO-8 Hanses, C., 51-ATIO-5 Herr, M., 115-AA-19, 155-AA-25, 226-AA-31, 230-AA-35 Hu, F., 229-AA-34 Ito, K., 66-MST-4 Johansen, C., 121-AMT-8/FD-14/TP-6/GT-8, Hansman, R., 156-ACD-4 Herrema, F., 51-ATIO-5 Hu, H., 180-PDL-8/APA-20 Ito, Y., 230-AA-35 159-AMT-10/GT-10 Harada, N., 181-PDL-9/TP-8 Herring, A., 158-AMT-9/GT-9 Hu, J., 171-CFD-19 Ivaldi, D., 307-MAO-12 Johnsen, E., 201-CFD-21, 211-FD-26 Hariharan, N., 122-APA-13 Herrmann, J., 29-MAO-1 Hu, Y., 208-FD-23 Ivanov, V., 243-CFD-28 Johnson, H., 103-ITAR-1 Harik, R., 64-MAO-2 Herron, A., 262-AA-40 Hu, Z., 22-CFD-2, 205-CFD-25 Iwakawa, A., 89-APA-11, 138-FD-17 Johnson, S., 43-AFM-3, 214-MST-9 Author/Session Chair Index Johnston, C., 69-TP-4, 217-TP-11 Karakoç, N., 273-ASE-5 Kirk, L., 69-TP-4 Krimmelbein, N., 61-FD-7 Landrum, D., 250-LTA-1 Jolly, B., 23-CFD-3, 136-FD-15, 241-CFD-26 Karlgaard, C., 44-AFM-4 Kiyici, F., 204-CFD-24 Krishna, Y., 11-AMT-2/GT-2 Landry, R., 215-MST-10 Jondeau, E., 231-AA-36 Karon, A., 189-AA-30 Klabes, A., 226-AA-31 Krishnamoorthy, S., 286-PDL-13 Landry, S., 164-ATIO-15, 166-ATIO-17, 197-ATIO-18 Jones, A., 268-APA-30 Kartha, A., 244-CFD-29 Kleb, W., 58-CFD-8, 233-APA-25 Krishnamurthy, R., 272-ASE-4 Lang, S., 200-BAL-2 Jones, G., 294-AMT-14/GT-15 Kase, S., 293-ACD-8 Kleinclaus, C., 259-AA-37 Kroeber, S., 260-AA-38 Langtry, R., 61-FD-7 Jones, J., 228-AA-33 Kasprzyk, M., 280-FT-2/GT-14 Kleine, H., 102-FD-13 Kronhaus, I., 144-PDL-7 Larbi, S., 305-CFD-35 Jones, M., 7-AA-5, 26-FD-2, 116-AA-20, 262-AA-40, Kato, H., 60-FD-6/PDL-2, 192-AMT-12/GT-12 Klentzman, J., 99-FD-10 Kroninger, C., 136-FD-15 Larcheveque, L., 154-AA-24 302-CFD-32 Katsurayama, H., 286-PDL-13 Kline, H., 204-CFD-24 Kroo, I., 8-AFM-1, 249-FT-1 Latz, J., 161-APA-18, 267-APA-29 Jones, S., 86-AMT-6/GT-6 Katz, A., 21-CFD-1, 243-CFD-28 Kling, U., 53-ATIO-7 Krozel, J., 142-MST-6 Laurendeau, F., 60-FD-6/PDL-2 Jones, W., 301-CFD-31 Katz, J., 88-APA-10 Klock, R., 119-AFM-8 Krueger, P., 62-FD-8 Laval, J., 98-CFD-12 Joo, J., 191-AMT-11/GT-11 Kaul, U., 25-FD-1, 49-APA-7, 279-FD-31 Kloker, M., 209-FD-24 Krueger, W., 198-ATIO-19 Lavin, T., 119-AFM-8 Jordan, P., 5-AA-3, 80-AA-14, 189-AA-30 Kausche, P., 152-AA-22 Knabe, F., 51-ATIO-5 Krüger, W., 57-CFD-7, 105-MST-5 Lawrence, J., 5-AA-3, 227-AA-32 Jorris, T., 249-FT-1 Kaya, D., 118-AFM-7 Knobloch, K., 151-AA-21 Krumbein, A., 61-FD-7 Lazarus, S., 117-ACD-3 Joseph, L., 295-APA-34 Ke, G., 261-AA-39 Knowles, J., 105-MST-5 Krumme, A., 13-APA-2 Le Bras, S., 229-AA-34 Joseph, P., 3-AA-1, 7-AA-5, 38-AA-7, 79-AA-13, Kegerise, M., 99-FD-10 Koc, I., 304-CFD-34 Krus, P., 283-MAO-10 Le Garrec, T., 187-AA-28 152-AA-22, 261-AA-39 Keller, D., 87-APA-9 Koch, J., 236-APA-28 Kryukov, I., 193-APA-21 Le Rallic, M., 80-AA-14 Jost, A., 203-CFD-23 Keller, E., 83-AFM-5 Koch, M., 238-ATIO-21 Kucukcoskun, K., 79-AA-13 Lebofsky, S., 124-APA-15 Josyula, E., 69-TP-4 Kelly, M., 269-APA-31 Kocian, T., 137-FD-16 Kügler, M., 128-ATIO-14 Lebrun, F., 46-AMT-4/GT-4 Joyce, R., 31-MST-2 Kennedy, G., 212-MAO-6 Kodama, H., 152-AA-22 Kuhn, T., 88-APA-10 Lee, D., 12-APA-1 Juliano, T., 10-AMT-1/GT-1, 137-FD-16 Kenway, G., 141-MAO-4 Koenig, M., 4-AA-2 Kulkarni, M., 252-MAO-9 Lee, H., 16-ATIO-1 Jumper, E., 88-APA-10, 143-PDL-6, 255-PDL-12 Kerho, M., 235-APA-27 Koerner, S., 237-ASE-3 Kumar, D., 234-APA-26 Lee, K., 51-ATIO-5, 84-AFM-6, 162-APA-19, 166-ATIO-17 June, J., 262-AA-40 Kessler, R., 22-CFD-2, 96-CFD-10 Koh, S., 38-AA-7, 41-AA-10, 79-AA-13, 80-AA-14 Kumar, R., 118-AFM-7, 174-FD-20 Lee, S., 154-AA-24 Jung, K., 235-APA-27 Key, N., 158-AMT-9/GT-9, 173-FD-19 Koike, S., 192-AMT-12/GT-12 Kumar, S., 234-APA-26 Lee, T., 107-PDL-4 Jung, S., 166-ATIO-17 Keye, S., 87-APA-9 Koizumi, H., 23-CFD-3 Kumar, V., 65-MST-3, 142-MST-6 Lefantzi, S., 139-FD-18 126 Jung, T., 64-MAO-2 Khalid, M., 136-FD-15 Kok, F., 27-FD-3, 175-FD-22 Kuntz, D., 34-TP-1 Leger, T., 306-CFD-36 Jung, Y., 16-ATIO-1, 91-ATIO-9, 198-ATIO-19, Khalil, E., 145-TP-7, 178-MST-8 Kokaly, M., 178-MST-8 Kunz, D., 43-AFM-3 Leib, S., 79-AA-13, 227-AA-32 298-ATIO-27 Khamis, D., 7-AA-5 Koklu, M., 63-FD-9 Kuo, C., 153-AA-23 Leifsson, L., 307-MAO-12 Junkui, M., 45-AMT-3/GT-3, 285-MST-12 Khan, S., 66-MST-4 Kolonay, R., 29-MAO-1, 252-MAO-9, 284-MAO-11 Kurelek, J., 100-FD-11 Lele, S., 80-AA-14 Junqueira-Junior, C., 270-APA-32 Khire, R., 141-MAO-4 Komatsu, P., 307-MAO-12 Kurtz, J., 46-AMT-4/GT-4 Lemonds, T., 293-ACD-8 Jurkovich, M., 193-APA-21, 269-APA-31 Khodadoust, A., 202-CFD-22 Kong, W., 295-APA-34 Kurz, H., 209-FD-24 Leng, M., 35-TP-2, 145-TP-7 Justin, C., 190-ACD-5 Khoo, B., 235-APA-27 Konnemann, E., 275-ATIO-25 Kutay, A., 66-MST-4, 83-AFM-5, 118-AFM-7, Léon, O., 60-FD-6/PDL-2, 228-AA-33 Juve, D., 189-AA-30, 231-AA-36 Khorrami, M., 155-AA-25, 188-AA-29, 259-AA-37 Kontis, K., 193-APA-21 294-AMT-14/GT-15 Leong, C., 63-FD-9, 101-FD-12 Kaddouh, B., 30-MST-1 Kidd, F., 143-PDL-6 Koo, H., 304-CFD-34 Kutz, D., 158-AMT-9/GT-9 Leonov, S., 107-PDL-4, 144-PDL-7 Kailasanath, K., 153-AA-23 Kim, C., 242-CFD-27 Kopiev, V., 187-AA-28, 189-AA-30, 228-AA-33 Kwon, O., 133-CFD-16 Leopold, F., 45-AMT-3/GT-3 Kalivarapu, V., 29-MAO-1, 104-MAO-3, 283-MAO-10 Kim, E., 51-ATIO-5 Kopyt, A., 30-MST-1 La Rocca, G., 176-MAO-5 Lesieutre, D., 269-APA-31 Kalkhoran, I., 233-APA-25 Kim, H., 88-APA-10 Koreanschi, A., 13-APA-2, 296-APA-35 Lacaze, G., 244-CFD-29 Letrenne, G., 167-BAL-1 Kalyan, A., 228-AA-33 Kim, J., 3-AA-1, 46-AMT-4/GT-4, 151-AA-21, 261-AA-39 Korkis-Kanaan, R., 305-CFD-35 Lachenmeier, T., 167-BAL-1 Leung, R., 38-AA-7 Kamali, S., 122-APA-13 Kim, K., 126-ATIO-12 Korn, B., 51-ATIO-5 Lachowski, F., 37-AA-6 Levin, D., 69-TP-4, 203-CFD-23 Kamat, S., 293-ACD-8 Kim, T., 46-AMT-4/GT-4 Korolev, Y., 5-AA-3, 251-MAO-8 Lacor, C., 152-AA-22 LeVine, M., 42-ACD-1, 52-ATIO-6, 198-ATIO-19 Kamle, S., 234-APA-26 Kim, V., 141-MAO-4 Kostiuk, P., 142-MST-6 Lacy, D., 87-APA-9 Lewis, D., 103-ITAR-1 Kammeyer, M., 294-AMT-14/GT-15 Kim, Y., 142-MST-6 Köthe, T., 252-MAO-9 Lafage, R., 42-ACD-1 Lewis, M., 10-AMT-1/GT-1, 303-CFD-33 Kampers, G., 50-APA-8, 271-APA-33 Kimmel, R., 28-FD-4, 102-FD-13, 103-ITAR-1 Kotikalpudi, A., 157-AFM-9 Laffay, P., 3-AA-1 Lewis, R., 108-TP-5 Kamruzzaman, M., 155-AA-25 King, L., 161-APA-18 Kotov, D., 24-CFD-4 Lafferty, J., 103-ITAR-1 Lewis, S., 34-TP-1 Kang, H., 162-APA-19 King, R., 99-FD-10, 137-FD-16 Kotov, M., 193-APA-21 Lai, D., 237-ASE-3, 272-ASE-4 Lewis, T., 17-ATIO-2 Kanistras, K., 88-APA-10 King, W., 250-LTA-1 Kotsonis, M., 88-APA-10, 286-PDL-13 Lajús, F., 5-AA-3, 80-AA-14 Leyva, I., 27-FD-3 Kannan, H., 212-MAO-6 Kingan, M., 5-AA-3, 37-AA-6 Koziel, S., 307-MAO-12 Lam, T., 217-TP-11 Li, F., 9-AFM-2, 99-FD-10, 137-FD-16 Kanoria, A., 250-LTA-1, 305-CFD-35 Kings, N., 41-AA-10, 151-AA-21 Kozlov, A., 77-AA-11 Lambert, A., 100-FD-11 Li, G., 296-APA-35 Kapania, R., 29-MAO-1 Kio, M., 35-TP-2 Krakos, J., 23-CFD-3 Lammel, O., 266-AMT-13/GT-13 Li, H., 144-PDL-7, 180-PDL-8/APA-20, 271-APA-33 Kara, K., 13-APA-2, 50-APA-8, 236-APA-28 Kirby, A., 201-CFD-21 Krausman, J., 282-LTA-2 Lampinen, M., 139-FD-18 Li, J., 24-CFD-4, 92-ATIO-10 Karabasov, S., 5-AA-3, 6-AA-4, 80-AA-14, 228-AA-33 Kirby, M., 198-ATIO-19 Kraut, J., 51-ATIO-5 Lancaster, J., 158-AMT-9/GT-9 Li, M., 214-MST-9 Karahan, S., 294-AMT-14/GT-15 Kiris, C., 4-AA-2, 14-APA-3 Kreitzman, J., 153-AA-23 Landman, D., 294-AMT-14/GT-15 Li, S., 26-FD-2, 116-AA-20 Karakoc, T., 273-ASE-5 Kirk, C., 159-AMT-10/GT-10 Kreuz, M., 164-ATIO-15 Landrum, B., 30-MST-1, 265-ACD-7 Li, V., 29-MAO-1, 176-MAO-5 Author/Session Chair Index Li, W., 89-APA-11, 241-CFD-26, 261-AA-39 Lofthouse, A., 160-APA-17, 236-APA-28, 305-CFD-35 Madden, T., 67-PDL-3 Martinelli, L., 57-CFD-7, 295-APA-34 McLaughlin, T., 12-APA-1, 125-APA-16 Li, X., 81-AA-15, 112-AA-16, 116-AA-20 Logan, M., 190-ACD-5 Maeng, J., 169-CFD-17 Martinez, A., 101-FD-12 McMasters, R., 35-TP-2 Li, Z., 69-TP-4, 178-MST-8 Lohr, G., 91-ATIO-9 Magalhaes, P., 283-MAO-10 Martinez, B., 45-AMT-3/GT-3, 47-APA-5 McMullan, W., 24-CFD-4, 98-CFD-12 Liang, C., 308-MAO-13 Lombardi, A., 213-MAO-7 Magari, P., 33-PDL-1/FD-5 Martinez, S., 145-TP-7 Mcnally, D., 298-ATIO-27 Libsig, M., 47-APA-5 Long, D., 275-ATIO-25 Magin, T., 34-TP-1, 216-TP-10/PDL-10, 217-TP-11 Martins, J., 29-MAO-1, 141-MAO-4, 252-MAO-9, McPartland, M., 51-ATIO-5, 298-ATIO-27 Liburdy, J., 234-APA-26 Long, T., 213-MAO-7, 251-MAO-8 Mahadevan, S., 308-MAO-13 307-MAO-12 McWaters, M., 45-AMT-3/GT-3 Liebeck, R., 123-APA-14 Lopes, L., 112-AA-16, 155-AA-25 Mahashabde, A., 92-ATIO-10, 197-ATIO-18 Mary, I., 154-AA-24 Mead, C., 227-AA-32 Lillard, R., 69-TP-4, 172-CFD-20 López, I., 281-GEPC-1 Maheshwari, A., 52-ATIO-6 Masarati, P., 84-AFM-6 Mease, K., 275-ATIO-25 Liller, T., 15-APA-4 López-Morales, M., 55-CFD-5 Mahlich, S., 275-ATIO-25 Mason, M., 217-TP-11 Meckstroth, C., 29-MAO-1 Lim, C., 265-ACD-7 Loseille, A., 23-CFD-3, 114-AA-18 Maierl, R., 212-MAO-6 Massa, L., 216-TP-10/PDL-10 Medeiros, F., 243-CFD-28 Lim, D., 42-ACD-1, 190-ACD-5 Loth, S., 91-ATIO-9 Majić, F., 78-AA-12, 235-APA-27 Massey, K., 297-APA-37 Medeiros, M., 230-AA-35 Limbach, C., 60-FD-6/PDL-2 Lou, F., 158-AMT-9/GT-9 Majumdar, A., 198-ATIO-19 Mastroddi, F., 29-MAO-1 Medina, A., 268-APA-30 Lin, H., 265-ACD-7 Louman, R., 138-FD-17 Makarov, B., 243-CFD-28 Masuda, K., 286-PDL-13 Medwell, P., 244-CFD-29 Lin, J., 138-FD-17, 212-MAO-6 Lowe, K., 46-AMT-4/GT-4, 159-AMT-10/GT-10, Malael, I., 96-CFD-10 Matayoshi, N., 298-ATIO-27 Mehmani, A., 251-MAO-8 Lin, P., 202-CFD-22 192-AMT-12/GT-12, 266-AMT-13/GT-13 Maldonado, A., 78-AA-12 Mather, J., 273-ASE-5 Mehta, P., 214-MST-9 Lin, Q., 241-CFD-26 Lowenberg, M., 122-APA-13 Malecki, T., 30-MST-1 Mathew, J., 24-CFD-4 Mei, D., 180-PDL-8/APA-20 Lin, Y., 46-AMT-4/GT-4, 65-MST-3, 240-ATIO-23 Lozano, B., 156-ACD-4 Malick, M., 122-APA-13 Mathews, E., 255-PDL-12 Mei, Q., 253-MST-11 Lincoln, D., 159-AMT-10/GT-10 Lu, F., 246-FD-27, 279-FD-31 Malik, M., 61-FD-7, 202-CFD-22 Mathews, J., 3-AA-1 Meier, W., 266-AMT-13/GT-13 Lindsay, K., 238-ATIO-21 Lu, J., 285-MST-12 Malik, W., 16-ATIO-1, 91-ATIO-9, 198-ATIO-19 Matic, P., 102-FD-13 Meinke, M., 26-FD-2, 38-AA-7, 41-AA-10, 79-AA-13, Linke, F., 92-ATIO-10 Luckner, R., 237-ASE-3 Malinowski, M., 280-FT-2/GT-14 Matsuno, T., 144-PDL-7 80-AA-14, 229-AA-34, 305-CFD-35 Liou, M., 56-CFD-6 Luckring, J., 160-APA-17 Mallet, M., 99-FD-10 Matsuno, Y., 51-ATIO-5 Melin, T., 283-MAO-10 Lippert, M., 88-APA-10 Ludwig, B., 159-AMT-10/GT-10 Mangalam, A., 9-AFM-2, 124-APA-15, 270-APA-32 Mattos, B., 283-MAO-10, 307-MAO-12 Mendenhall, M., 269-APA-31 Liston, G., 10-AMT-1/GT-1 Luedke, J., 297-APA-37 Mangani, L., 203-CFD-23 Mattson, C., 104-MAO-3 Mendonca, F., 230-AA-35 Little, J., 60-FD-6/PDL-2, 174-FD-20, 175-FD-22, Lukaczyk, T., 212-MAO-6 Mani, K., 302-CFD-32 Maughmer, M., 61-FD-7 Mendoza, J., 185-AA-26 127 279-FD-31 Luke, E., 41-AA-10, 81-AA-15, 195-APA-23 Mankbadi, M., 175-FD-22 Mavriplis, D., 201-CFD-21 Meneveau, C., 98-CFD-12, 171-CFD-19 Liu, A., 128-ATIO-14 Lummer, M., 112-AA-16 Mankbadi, R., 79-AA-13 Mavris, D., 37-AA-6, 42-ACD-1, 52-ATIO-6, 53-ATIO-7, Meng, X., 33-PDL-1/FD-5, 144-PDL-7, Liu, C., 305-CFD-35 Lung, T., 169-CFD-17 Manoha, E., 3-AA-1, 155-AA-25, 229-AA-34, 141-MAO-4, 142-MST-6, 156-ACD-4, 190-ACD-5, 180-PDL-8/APA-20, 271-APA-33 Liu, D., 85-AMT-5/GT-5 Luo, H., 55-CFD-5, 100-FD-11, 173-FD-19, 230-AA-35, 259-AA-37 198-ATIO-19, 213-MAO-7, 239-ATIO-22, Merle, X., 113-AA-17 Liu, F., 33-PDL-1/FD-5, 45-AMT-3/GT-3, 67-PDL-3, 201-CFD-21, 203-CFD-23, 208-FD-23 Manosalvas, D., 271-APA-33 265-ACD-7, 276-ATIO-26, 308-MAO-13 Merrick, J., 195-APA-23 144-PDL-7, 180-PDL-8/APA-20, 271-APA-33, Luo, L., 203-CFD-23 Mansor, S., 12-APA-1 May, G., 95-CFD-9 Mery, F., 262-AA-40 285-MST-12 Luo, S., 33-PDL-1/FD-5, 67-PDL-3, 144-PDL-7, Mansour, N., 58-CFD-8, 288-TP-13 Mayer, R., 92-ATIO-10, 197-ATIO-18 Mesmer, B., 212-MAO-6, 283-MAO-10 Liu, G., 248-FD-29 180-PDL-8/APA-20, 271-APA-33 Mansouri, N., 81-AA-15 Mazaheri, A., 55-CFD-5 Messac, A., 176-MAO-5, 251-MAO-8 Liu, H., 295-APA-34 Luo, X., 178-MST-8 Mantelli, M., 35-TP-2 McAlpine, A., 37-AA-6 Meyer, T., 181-PDL-9/TP-8 Liu, J., 30-MST-1, 84-AFM-6, 153-AA-23, 251-MAO-8 Lupoglazoff, N., 39-AA-8 Marais, K., 156-ACD-4, 164-ATIO-15, 275-ATIO-25, Mccarthy, P., 145-TP-7 Meyers, J., 181-PDL-9/TP-8 Liu, L., 25-FD-1, 31-MST-2, 213-MAO-7, 251-MAO-8 Lupp, C., 9-AFM-2 299-ATIO-28 McCarthy, P., 259-AA-37 Meyers, T., 152-AA-22, 297-APA-37 Liu, P., 26-FD-2, 47-APA-5 Luquet, D., 114-AA-18 Marañon Di Leo, J., 236-APA-28 McClain, S., 196-ASE-2 Michael, J., 181-PDL-9/TP-8 Liu, Q., 178-MST-8 Lutz, A., 181-PDL-9/TP-8 Marchiano, R., 114-AA-18 McClure, J., 132-CFD-15 Michal, T., 23-CFD-3 Liu, R., 128-ATIO-14 Lutz, T., 249-FT-1 Marie, S., 56-CFD-6 McColl, C., 83-AFM-5 Michel, U., 189-AA-30 Liu, S., 173-FD-19 Luxhoj, J., 300-ATIO-29 Marineau, E., 99-FD-10, 103-ITAR-1 McComas, A., 235-APA-27 Michou, Y., 46-AMT-4/GT-4, 192-AMT-12/GT-12 Liu, T., 25-FD-1 Lv, Y., 242-CFD-27 Markesteijn, A., 6-AA-4, 80-AA-14 McCrink, M., 268-APA-30 Micka, D., 33-PDL-1/FD-5 Liu, X., 3-AA-1, 55-CFD-5, 78-AA-12, 113-AA-17 Lynch, K., 37-AA-6, 266-AMT-13/GT-13 Marks, C., 191-AMT-11/GT-11 McDaniel, D., 160-APA-17 Mihaescu, M., 96-CFD-10, 112-AA-16 Liu, Y., 49-APA-7, 185-AA-26, 285-MST-12 Lynn, K., 294-AMT-14/GT-15 Marn, A., 151-AA-21 McDaniel, J., 244-CFD-29 Milagre da Fonseca, I., 119-AFM-8 Liu, Z., 57-CFD-7, 141-MAO-4 Lyrintzis, A., 37-AA-6, 113-AA-17, 245-CFD-30 Marques, F., 236-APA-28 McDonald, J., 304-CFD-34 Milan, P., 60-FD-6/PDL-2 Liv, A., 18-ATIO-3 Lyu, B., 38-AA-7 Marr, B., 238-ATIO-21 McDonald, R., 82-ACD-2, 240-ATIO-23 Milanese, F., 35-TP-2 Livebardon, T., 185-AA-26 Ma, H., 145-TP-7 Marsan, A., 227-AA-32 McGrath, B., 123-APA-14 Miles, R., 60-FD-6/PDL-2, 86-AMT-6/GT-6, Livne, E., 49-APA-7 Ma, P., 26-FD-2 Marsden, O., 4-AA-2, 231-AA-36 McGuirk, J., 24-CFD-4 143-PDL-6, 255-PDL-12 Llopis-Pascual, A., 271-APA-33 Ma, Z., 128-ATIO-14 Marsh, J., 200-BAL-2 McInerny, S., 40-AA-9 Miller, B., 52-ATIO-6, 65-MST-3 Lo, K., 193-APA-21 Macheret, S., 216-TP-10/PDL-10 Marshall, J., 157-AFM-9 Mcintyre, T., 34-TP-1 Miller, D., 142-MST-6, 282-LTA-2 Loaec, S., 272-ASE-4 MacManus, D., 270-APA-32 Marshall, P., 85-AMT-5/GT-5 McKeon, B., 162-APA-19 Miller, J., 28-FD-4 Lobel, G., 227-AA-32 Madavan, N., 281-GEPC-1 Marten, D., 297-APA-37 McKiernan, G., 28-FD-4 Miller, S., 40-AA-9, 153-AA-23 Lockard, D., 3-AA-1, 155-AA-25, 188-AA-29, Maddalena, L., 86-AMT-6/GT-6 Martin, A., 68-TP-3, 108-TP-5, 182-TP-9 McKinley, R., 40-AA-9 Mills, B., 85-AMT-5/GT-5, 280-FT-2/GT-14 230-AA-35, 259-AA-37 Maddalon, J., 17-ATIO-2 Martin, P., 120-AMT-7/GT-7 McLaughlin, D., 39-AA-8, 40-AA-9 Mills, M., 120-AMT-7/GT-7 Author/Session Chair Index Milutinovic, D., 91-ATIO-9, 198-ATIO-19 Mouring, C., 281-GEPC-1 Nayeri, C., 26-FD-2, 297-APA-37 Oberleithner, K., 266-AMT-13/GT-13 Palopo, K., 142-MST-6 Mimani, A., 231-AA-36 Movahed, P., 211-FD-26 Neifeld, A., 39-AA-8 Ocheltree, C., 89-APA-11, 251-MAO-8, 296-APA-35 Paluch, B., 13-APA-2 Min, S., 42-ACD-1, 156-ACD-4 Moyes, A., 137-FD-16 Neilan, J., 165-ATIO-16, 199-ATIO-20 Ochieng, W., 198-ATIO-19 Palumbo, R., 164-ATIO-15 Mincu, D., 154-AA-24, 187-AA-28 Muehleisen, R., 262-AA-40 Neilsen, T., 40-AA-9 Oefelein, J., 244-CFD-29 Pan, J., 21-CFD-1 Mineck, R., 188-AA-29 Muehler-Vahl, H., 101-FD-12 Neitzel, K., 69-TP-4 Ogasawara, T., 68-TP-3 Pan, Q., 145-TP-7 Mingione, G., 115-AA-19 Mueller, F., 203-CFD-23 Nelson, C., 49-APA-7 Ogawa, S., 286-PDL-13 Panchal, J., 52-ATIO-6 Minisci, E., 214-MST-9 Mueller, J., 131-CFD-14 Nelson, M., 114-AA-18, 159-AMT-10/GT-10, 187-AA-28 Ojeda, S., 95-CFD-9 Panchal, K., 250-LTA-1 Minqiang, Y., 280-FT-2/GT-14 Mueller-Vahl, H., 208-FD-23 Neuhart, D., 188-AA-29 Okada, Y., 270-APA-32 Panda, J., 99-FD-10 Mirochnitchenko, V., 190-ACD-5 Mujumdar, P., 57-CFD-7 Neville, A., 246-FD-27 Okamoto, T., 182-TP-9 Pandare, A., 201-CFD-21 Misaka, T., 196-ASE-2 Mukhopadhyay, V., 214-MST-9 Newcamp, J., 249-FT-1 Okolo, W., 8-AFM-1, 273-ASE-5 Pandya, S., 305-CFD-35 Mitchell, K., 116-AA-20 Mulani, S., 29-MAO-1 Newman, J., 95-CFD-9, 170-CFD-18, 305-CFD-35 Ol, M., 125-APA-16, 234-APA-26 Panerai, F., 288-TP-13 Mitsingas, C., 107-PDL-4 Mullane, M., 193-APA-21 Ng, H., 18-ATIO-3, 92-ATIO-10 Olejniczak, J., 69-TP-4 Panesi, M., 69-TP-4 Mitsuhashi, R., 293-ACD-8 Mulleners, K., 50-APA-8, 235-APA-27 Nguyen, D., 66-MST-4 Oliveira, E., 119-AFM-8 Pankratov, I., 187-AA-28 Mittal, A., 15-APA-4, 234-APA-26, 297-APA-37 Munday, P., 101-FD-12 Nguyen, L., 79-AA-13 Oliver, J., 104-MAO-3 Pant, R., 282-LTA-2 Mittal, R., 98-CFD-12, 171-CFD-19 Mundis, N., 132-CFD-15 Nguyen, M., 88-APA-10, 143-PDL-6 Oliviero, N., 137-FD-16 Papadimitriou, C., 283-MAO-10 Mockett, C., 306-CFD-36 Munera Savino, F., 8-AFM-1, 249-FT-1 Nguyen, N., 49-APA-7, 124-APA-15 Oliviu, S., 13-APA-2, 296-APA-35 Papadimitriou, D., 283-MAO-10 Mockus, L., 239-ATIO-22 Munjulury, R., 283-MAO-10 Nichols, D., 297-APA-37 Ollivier Gooch, C., 21-CFD-1, 23-CFD-3, 131-CFD-14 Papageorgio, E., 128-ATIO-14 Moeller, T., 67-PDL-3, 144-PDL-7, 216-TP-10/PDL-10, Munson, M., 136-FD-15 Nichols, J., 4-AA-2, 39-AA-8, 153-AA-23 Olsen, M., 172-CFD-20 Papamoschou, D., 227-AA-32, 264-AA-42 244-CFD-29 Murari, K., 159-AMT-10/GT-10 Nicolosi, F., 8-AFM-1, 13-APA-2, 104-MAO-3 Olson, E., 252-MAO-9 Papathakis, K., 240-ATIO-23 Mohan, A., 302-CFD-32 Murayama, M., 229-AA-34, 230-AA-35 Niedermeier, D., 31-MST-2 Olson, M., 240-ATIO-23 Paranin, G., 115-AA-19 Mohite, P., 234-APA-26 Muriel Gracia, M., 113-AA-17 Nieto, B., 234-APA-26 Olson, R., 43-AFM-3 Pardowitz, B., 173-FD-19 Moin, P., 202-CFD-22 Murman, S., 21-CFD-1, 96-CFD-10, 201-CFD-21, Nigam, N., 284-MAO-11 Omar, F., 51-ATIO-5 Parent, B., 216-TP-10/PDL-10 Moini-Yekta, S., 49-APA-7 205-CFD-25 Nikbay, M., 308-MAO-13 Omidy, A., 68-TP-3 Parente, A., 216-TP-10/PDL-10 Molinaro, N., 297-APA-37 Murphy, C., 52-ATIO-6, 65-MST-3 Nishida, H., 144-PDL-7 Onishi, K., 270-APA-32 Parish, E., 58-CFD-8 128 Montalvo, C., 157-AFM-9 Murray, H., 114-AA-18, 187-AA-28 Nishikawa, H., 55-CFD-5, 56-CFD-6 Oravec, H., 273-ASE-5 Park, G., 139-FD-18 Montel, M., 8-AFM-1 Murray, J., 13-APA-2, 297-APA-37 Niu, J., 244-CFD-29 Ordaz, I., 14-APA-3 Park, J., 202-CFD-22, 242-CFD-27, 251-MAO-8, Moolchandani, K., 52-ATIO-6 Murray, N., 80-AA-14 Niu, W., 215-MST-10 Orr, M., 156-ACD-4 296-APA-35 Moore, M., 54-ATIO-8, 93-ATIO-11, 127-ATIO-13, Murray, W., 158-AMT-9/GT-9 Nodé-Langlois, T., 112-AA-16, 187-AA-28 Orra, T., 128-ATIO-14, 212-MAO-6 Park, M., 14-APA-3, 23-CFD-3, 97-CFD-11, 160-APA-17 276-ATIO-26 Murrieta Mendoza, A., 18-ATIO-3 Noelting, S., 188-AA-29 Osman, A., 178-MST-8 Park, S., 235-APA-27 Moored, K., 100-FD-11 Muscarello, V., 84-AFM-6 Nojima, Y., 182-TP-9 Ostrikov, N., 115-AA-19 Parke, B., 51-ATIO-5 Mor-Yossef, Y., 133-CFD-16 Musiak, J., 275-ATIO-25 Noll, B., 185-AA-26 Otsu, H., 144-PDL-7 Parker, P., 294-AMT-14/GT-15 Moraru, G., 103-ITAR-1 Muslubas, Y., 57-CFD-7 Nompelis, I., 246-FD-27, 256-TP-12 Overmeyer, A., 120-AMT-7/GT-7 Parry, A., 37-AA-6 Moreau, A., 77-AA-11, 152-AA-22 Muyimbwa, T., 282-LTA-2 Nomura, S., 69-TP-4 Owens, J., 196-ASE-2 Parsons, N., 69-TP-4 Moreau, D., 152-AA-22, 231-AA-36 Myose, R., 27-FD-3, 175-FD-22 Nonomura, T., 60-FD-6/PDL-2, 114-AA-18, Oyama, A., 114-AA-18 Paruchuri, C., 3-AA-1, 38-AA-7, 79-AA-13, 152-AA-22 Moreau, E., 33-PDL-1/FD-5, 180-PDL-8/APA-20 Nagarajan, B., 16-ATIO-1 130-CFD-13, 169-CFD-17 Oza, U., 22-CFD-2 Pascarella, D., 164-ATIO-15 Moreau, S., 3-AA-1, 79-AA-13, 81-AA-15, 115-AA-19, Nahuis, R., 13-APA-2 Nordstrom, J., 132-CFD-15, 242-CFD-27 Ozcan, M., 265-ACD-7 Paschereit, C., 27-FD-3, 297-APA-37 152-AA-22, 185-AA-26, 187-AA-28, 227-AA-32 Naitoh, K., 182-TP-9 Nott, J., 167-BAL-1, 200-BAL-2 Özgen, S., 97-CFD-11 Pasco, Y., 227-AA-32 Moreira, F., 9-AFM-2, 241-CFD-26 Najafi, A., 104-MAO-3 Nouzawa, T., 270-APA-32 Oztekin, A., 164-ATIO-15 Pasiliao, C., 12-APA-1, 22-CFD-2, 90-APA-12 Morelli, E., 118-AFM-7 Najian Asl, R., 283-MAO-10 Novara, M., 159-AMT-10/GT-10 Pack, J., 274-ATIO-24 Passe, B., 162-APA-19 Morgan, P., 102-FD-13 Nakasato, K., 270-APA-32 Novikov, A., 99-FD-10 Pack Melton, L., 279-FD-31 Pastorelli, V., 77-AA-11 Morgan, R., 34-TP-1 Nakashima, T., 270-APA-32 Nowak, M., 128-ATIO-14 Padois, T., 3-AA-1 Patel, S., 24-CFD-4 Morikawa, Y., 270-APA-32 Nalci, M., 66-MST-4 Ntemos, G., 202-CFD-22 Pagani, C., 230-AA-35 Paterson, E., 26-FD-2 Morris, P., 4-AA-2, 40-AA-9, 263-AA-41 Nallapaneni, S., 35-TP-2 O’Brien, D., 15-APA-4, 295-APA-34 Page, G., 24-CFD-4 Patil, M., 9-AFM-2, 30-MST-1, 252-MAO-9 Morris, S., 38-AA-7 Namba, M., 152-AA-22 O’Brien, J., 151-AA-21 Page, M., 276-ATIO-26 Patterson, A., 157-AFM-9 Morrissey, P., 108-TP-5 Namura, N., 125-APA-16 O’Brien, W., 159-AMT-10/GT-10 Paglione, P., 128-ATIO-14 Patterson, J., 214-MST-9 Morsbach, C., 133-CFD-16 Nance, D., 262-AA-40 O’Byrne, S., 11-AMT-2/GT-2, 46-AMT-4/GT-4, Pak, C., 9-AFM-2, 141-MAO-4 Patterson, M., 127-ATIO-13 Mortensen, C., 209-FD-24 Napolitano, M., 43-AFM-3 121-AMT-8/FD-14/TP-6/GT-8 Palacios, F., 133-CFD-16, 204-CFD-24, 271-APA-33, Paul, R., 235-APA-27 Morton, S., 160-APA-17, 174-FD-20 Narayanaswamy, V., 27-FD-3, 143-PDL-6, 174-FD-20 O’Connor, C., 91-ATIO-9 283-MAO-10 Paula, A., 307-MAO-12 Moses John Christy Appolo, P., 67-PDL-3 Nark, D., 116-AA-20 O’Neill, W., 35-TP-2 Palla, A., 107-PDL-4 Pauz, V., 229-AA-34 Moss, M., 308-MAO-13 Narkiewicz, J., 30-MST-1 O’Reilly, C., 78-AA-12, 235-APA-27 Palmer, E., 51-ATIO-5 Pawletta, T., 177-MST-7 Mott, D., 102-FD-13 Natarajan, K., 153-AA-23, 227-AA-32 O’Sullivan, S., 53-ATIO-7 Palmer, G., 108-TP-5 Payan, A., 53-ATIO-7, 239-ATIO-22 Motter, M., 165-ATIO-16, 199-ATIO-20 Nawroth, H., 27-FD-3 Obayashi, S., 125-APA-16, 196-ASE-2 Palmieri, F., 46-AMT-4/GT-4 Peake, N., 3-AA-1, 260-AA-38 Author/Session Chair Index Pearce, R., 52-ATIO-6 Porumbel, I., 96-CFD-10 Randt, N., 52-ATIO-6, 128-ATIO-14 Rizzi, S., 152-AA-22 Sadri, V., 62-FD-8 Pechlivanoglou, G., 26-FD-2, 297-APA-37 Post, M., 64-MAO-2, 162-APA-19 Rao, A., 126-ATIO-12, 156-ACD-4 Röben, T., 265-ACD-7 Sagebaum, M., 252-MAO-9 Pederson, C., 174-FD-20 Pott-Pollenske, M., 3-AA-1, 230-AA-35 Rashad, R., 204-CFD-24 Robertson, G., 174-FD-20 Saheby, E., 267-APA-29 Pedramasl, N., 64-MAO-2 Potter, C., 141-MAO-4 Rathakrishnan, B., 244-CFD-29 Robinson, S., 31-MST-2, 269-APA-31 Sahin, B., 25-FD-1 Pei, J., 119-AFM-8 Povinelli, L., 281-GEPC-1 Rathakrishnan, E., 50-APA-8 Robinson III, J., 239-ATIO-22 Sahin, M., 64-MAO-2 Pei, P., 276-ATIO-26 Powers, R., 40-AA-9 Rauleder, J., 236-APA-28 Rochlitz, H., 159-AMT-10/GT-10 Sahni, O., 63-FD-9 Peinke, J., 50-APA-8, 271-APA-33 Prabhu, D., 102-FD-13, 108-TP-5 Rautmann, C., 79-AA-13, 155-AA-25 Rodebaugh, G., 173-FD-19 Sahu, J., 90-APA-12 Pelletier, D., 58-CFD-8, 204-CFD-24, 304-CFD-34 Prachar, A., 233-APA-25 Ravetta, P., 188-AA-29 Rodriguez, Y., 51-ATIO-5 Said, M., 167-BAL-1, 200-BAL-2 Peltier, S., 266-AMT-13/GT-13 Pradeep, A., 57-CFD-7 Ray, J., 139-FD-18 Roe, P., 56-CFD-6, 169-CFD-17 Saif Ullah Khalid, M., 133-CFD-16 Peng, D., 197-ATIO-18 Prasad, R., 12-APA-1, 205-CFD-25 Razi, P., 58-CFD-8 Roger, M., 79-AA-13, 81-AA-15, 152-AA-22, Saikia, B., 28-FD-4 Peng, J., 190-ACD-5 Precup, N., 49-APA-7 Reardon, J., 46-AMT-4/GT-4 154-AA-24, 187-AA-28 Saini, A., 46-AMT-4/GT-4, 267-APA-29 Peng, S., 6-AA-4, 115-AA-19, 154-AA-24 Priolo, F., 9-AFM-2 Reardon, S., 177-MST-7 Rogers, M., 61-FD-7 Saka, P., 88-APA-10 Peng, W., 198-ATIO-19 Pröbsting, S., 38-AA-7 Reasor, D., 22-CFD-2 Rogers, S., 233-APA-25 Sakurai, T., 66-MST-4 Peng, X., 53-ATIO-7 Pruett, B., 62-FD-8, 175-FD-22 Redonnet, S., 155-AA-25, 261-AA-39 Rohlmann, D., 87-APA-9 Salah El Din, I., 114-AA-18 Percin, M., 97-CFD-11, 208-FD-23 Pruis, M., 237-ASE-3, 272-ASE-4 Reed, D., 262-AA-40 Roidl, B., 41-AA-10 Salas, P., 115-AA-19 Pereira, D., 236-APA-28 Przulj, V., 243-CFD-28 Reed, H., 61-FD-7, 137-FD-16, 247-FD-28 Roling, P., 91-ATIO-9 Saleem, M., 174-FD-20 Perez, R., 141-MAO-4, 267-APA-29 Pulliam, T., 136-FD-15 Reeder, M., 158-AMT-9/GT-9, 195-APA-23 Romanelli, G., 203-CFD-23 Salehian, S., 79-AA-13 Periaux, J., 180-PDL-8/APA-20 Pytel, D., 34-TP-1 Reeger, J., 141-MAO-4 Rorie, R., 274-ATIO-24 Salemi, L., 28-FD-4 Peroomian, O., 245-CFD-30 Qi, B., 145-TP-7 Rege, A., 48-APA-6 Rose, C., 107-PDL-4 Salinas, M., 84-AFM-6 Persson, P., 170-CFD-18 Qi, X., 284-MAO-11 Rehmanjan, U., 128-ATIO-14 Rosema, C., 90-APA-12, 296-APA-35 Salton, A., 40-AA-9 Peter, J., 173-FD-19 Qian, J., 285-MST-12 Reiche, N., 39-AA-8, 112-AA-16 Rosemann, H., 178-MST-8 Salze, E., 231-AA-36 Peters, B., 306-CFD-36 Qiao, W., 151-AA-21, 260-AA-38, 267-APA-29 Reichman, B., 40-AA-9 Rossian, L., 231-AA-36 Samanta, A., 78-AA-12 Peters, C., 86-AMT-6/GT-6 Qiu, S., 204-CFD-24 Reimer, L., 57-CFD-7 Rossignol, K., 231-AA-36 Samareh, J., 68-TP-3 Petersen, S., 282-LTA-2 Qiu, X., 285-MST-12 Reissner, F., 101-FD-12 Roth, B., 251-MAO-8, 307-MAO-12 Samaritano, A., 194-APA-22 129 Petersson, Ö, 212-MAO-6 Qu, Q., 26-FD-2, 47-APA-5 Reist, T., 267-APA-29 Rothhaar, P., 119-AFM-8, 165-ATIO-16, 199-ATIO-20 Samimy, M., 33-PDL-1/FD-5, 153-AA-23 Pfaender, H., 53-ATIO-7, 239-ATIO-22 Quaglia, M., 187-AA-28 Remes, B., 97-CFD-11 Rougier, T., 259-AA-37 Samuel, A., 240-ATIO-23 Pfifer, H., 157-AFM-9 Qualls, G., 165-ATIO-16, 199-ATIO-20 Ren, Y., 21-CFD-1, 84-AFM-6, 214-MST-9, Roussel, C., 98-CFD-12 Sandberg, M., 51-ATIO-5 Piantanida, S., 5-AA-3, 189-AA-30 Quaranta, G., 84-AFM-6 241-CFD-26, 248-FD-29 Rouzbar, R., 244-CFD-29 Sandberg, R., 171-CFD-19 Piao, Y., 244-CFD-29 Queiroz, R., 7-AA-5 Rendall, T., 64-MAO-2, 125-APA-16, 283-MAO-10 Rowe, P., 158-AMT-9/GT-9 Sanders, L., 259-AA-37 Pierre, D., 154-AA-24 Quinlan, J., 244-CFD-29 Render, P., 88-APA-10 Rowley, C., 136-FD-15, 295-APA-34 Sandham, N., 209-FD-24 Pilon, A., 153-AA-23 Quinn, M., 45-AMT-3/GT-3 Renner, A., 104-MAO-3 Roy, A., 246-FD-27 Sanetrik, M., 124-APA-15 Pimenta, B., 77-AA-11 Quinto, P., 158-AMT-9/GT-9 Rennie, M., 88-APA-10, 143-PDL-6, 255-PDL-12 Roy, C., 30-MST-1, 97-CFD-11, 131-CFD-14 Sanjaya, D., 95-CFD-9 Pini, M., 133-CFD-16 Quix, H., 85-AMT-5/GT-5 Rey, C., 47-APA-5 Roy, R., 172-CFD-20 Sanjose, M., 227-AA-32 Pinier, J., 88-APA-10, 123-APA-14 Quon, L., 91-ATIO-9 Rey, M., 262-AA-40 Roy, S., 92-ATIO-10, 275-ATIO-25 Sankaran, V., 132-CFD-15 Pinon-Fischer, O., 142-MST-6 Radyisyewski, P., 30-MST-1 Reyaz Ahmed, A., 50-APA-8 Roy Salam, I., 190-ACD-5 Sano, A., 41-AA-10 Piot, E., 262-AA-40 Raffel, M., 192-AMT-12/GT-12 Reynolds, D., 31-MST-2 Royalty, C., 116-AA-20 Santos, J., 30-MST-1, 282-LTA-2 Piperni, P., 104-MAO-3, 213-MAO-7, 284-MAO-11 Ragab, S., 236-APA-28 Reynolds, T., 51-ATIO-5, 163-ASE-1 Ru, P., 157-AFM-9 Santos, L., 117-ACD-3, 213-MAO-7 Planck, C., 234-APA-26 Ragni, D., 37-AA-6, 286-PDL-13 Reza Ahrabi, B., 95-CFD-9, 122-APA-13 Rudnick-Cohen, E., 29-MAO-1 Santos, P., 43-AFM-3 Plemmons, D., 11-AMT-2/GT-2 Rahman, M., 139-FD-18 Rhew, R., 158-AMT-9/GT-9, Rudnik, R., 87-APA-9 Santos Pereira, R., 286-PDL-13 Ploetner, K., 52-ATIO-6, 53-ATIO-7 Raj, P., 176-MAO-5, 251-MAO-8, 265-ACD-7, 296-APA-35 191-AMT-11/GT-11, 294-AMT-14/GT-15 Ruetten, M., 22-CFD-2, 96-CFD-10, 178-MST-8 Saraf, A., 16-ATIO-1, 51-ATIO-5, 91-ATIO-9 Poggie, J., 102-FD-13, 211-FD-26, 286-PDL-13, Rajagopalan, R., 243-CFD-28 Rhoads, J., 259-AA-37 Ruleva, L., 193-APA-21 Saric, W., 61-FD-7, 137-FD-16 306-CFD-36 Rajput, P., 233-APA-25 Rhodes, D., 52-ATIO-6 Rumann, H., 273-ASE-5 Sarkar, S., 136-FD-15 Poinsot, T., 185-AA-26 Rallabhandi, S., 14-APA-3, 89-APA-11 Richardson, J., 157-AFM-9 Rumsey, C., 58-CFD-8, 139-FD-18, 172-CFD-20, Sarradj, E., 186-AA-27, 231-AA-36 Polaczek, J., 280-FT-2/GT-14 Ramachandran, A., 27-FD-3, 28-FD-4 Richardson, T., 84-AFM-6, 212-MAO-6 208-FD-23 Sartor, F., 96-CFD-10 Pomeroy, B., 87-APA-9 Ramamoorthy, K., 275-ATIO-25 Ricklick, M., 145-TP-7 Rusak, Z., 62-FD-8, 173-FD-19 Sasaki, J., 293-ACD-8 Pons-Prat, J., 180-PDL-8/APA-20 Ramamurti, R., 48-APA-6, 233-APA-25 Righi, M., 236-APA-28, 278-FD-30 Russell, S., 141-MAO-4 Sasaki, K., 5-AA-3 Poole, D., 64-MAO-2, 125-APA-16, 283-MAO-10 Raman, G., 262-AA-40 Ringuette, M., 100-FD-11 Rutherford, M., 88-APA-10 Sasanapuri, B., 178-MST-8 Popie, V., 262-AA-40 Raman, V., 304-CFD-34 Ritter, M., 57-CFD-7 Sa, J., 235-APA-27 Sasidharan Nair, U., 80-AA-14 Popov, I., 33-PDL-1/FD-5 Ramesh, N., 67-PDL-3 Ritz, R., 22-CFD-2, 96-CFD-10 Sabetta, V., 8-AFM-1 Sasoh, A., 89-APA-11, 138-FD-17 Pornet, C., 53-ATIO-7 Ramirez, W., 38-AA-7 Riviere, P., 217-TP-11 Sadique, J., 98-CFD-12, 171-CFD-19 Sassanis, V., 209-FD-24 Poroseva, S., 96-CFD-10, 205-CFD-25 Rancourt, D., 213-MAO-7, 276-ATIO-26 Rizzetta, D., 101-FD-12 Sadovsky, A., 17-ATIO-2 Sato, M., 60-FD-6/PDL-2 Porteous, A., 96-CFD-10 Rand, J., 200-BAL-2 Rizzi, A., 160-APA-17 Sadraey, M., 191-AMT-11/GT-11 Satori, S., 293-ACD-8 Author/Session Chair Index Sattelmayer, T., 41-AA-10, 113-AA-17, 185-AA-26 Sclafani, A., 87-APA-9, 233-APA-25 Shively, J., 274-ATIO-24 Smeltzer, S., 281-GEPC-1 Stephani, K., 216-TP-10/PDL-10, 288-TP-13 Saunders, D., 182-TP-9, 217-TP-11 Scoggins, J., 217-TP-11 Shmilovich, A., 271-APA-33 Smith, A., 117-ACD-3 Stephen, S., 209-FD-24 Saurav, S., 125-APA-16 Scolan, E., 46-AMT-4/GT-4 Shneider, M., 216-TP-10/PDL-10 Smith, B., 172-CFD-20 Stephens, D., 114-AA-18 Saw, Z., 265-ACD-7 Scott, R., 124-APA-15 Shoda, T., 138-FD-17 Smith, D., 68-TP-3, 108-TP-5, 158-AMT-9/GT-9, Stephens, J., 191-AMT-11/GT-11 Sawhill, B., 16-ATIO-1 Scully, R., 273-ASE-5 Short, E., 145-TP-7 210-FD-25 Stevens, M., 274-ATIO-24 Sawyer, J., 181-PDL-9/TP-8 Secco, N., 307-MAO-12 Shukla, H., 9-AFM-2 Smith, J., 65-MST-3, 142-MST-6, 278-FD-30 Stoellinger, M., 172-CFD-20 Scanlan, J., 128-ATIO-14, 308-MAO-13 Seckin, S., 174-FD-20 Shyy, W., 97-CFD-11, 268-APA-30 Smith, K., 145-TP-7 Stohr, M., 266-AMT-13/GT-13 Scarano, F., 38-AA-7, 192-AMT-12/GT-12, Seeley, B., 239-ATIO-22 Siala, F., 234-APA-26 Smith, M., 259-AA-37 Stoll, A., 240-ATIO-23, 276-ATIO-26 266-AMT-13/GT-13 Seidel, J., 12-APA-1, 125-APA-16, 236-APA-28 Siddiqi, S., 3-AA-1 Smolarkiewicz, P., 163-ASE-1 Stone, C., 203-CFD-23, 302-CFD-32 Schaefer, J., 58-CFD-8 Seitzman, J., 159-AMT-10/GT-10 Sidharth, G., 139-FD-18 Snyder, M., 236-APA-28 Storozhev, D., 216-TP-10/PDL-10 Schaefer, M., 299-ATIO-28 Sekhar, S., 58-CFD-8 Sidiropoulos, S., 198-ATIO-19 Sohoni, N., 37-AA-6 Stouffer, V., 65-MST-3, 142-MST-6, 199-ATIO-20, Schauerhamer, D., 269-APA-31 Self, R., 5-AA-3, 39-AA-8, 227-AA-32 Siebert, J., 230-AA-35 Şöhret, Y., 273-ASE-5 275-ATIO-25 Scheel, H., 7-AA-5 Selfridge, J., 127-ATIO-13 Siercke, M., 7-AA-5 Soler, L., 275-ATIO-25 Stout, T., 40-AA-9 Scherer Schwening, G., 104-MAO-3 Selic, T., 151-AA-21 Siikonen, T., 139-FD-18 Solodovnikov, S., 193-APA-21 Strande, P., 237-ASE-3 Schetz, J., 29-MAO-1, 46-AMT-4/GT-4 Selig, M., 15-APA-4, 87-APA-9, 297-APA-37 Sijtsma, P., 115-AA-19 Son, P., 138-FD-17 Strangfeld, C., 101-FD-12 Schiavo, L., 98-CFD-12 Semiletov, V., 6-AA-4, 80-AA-14, 228-AA-33 Sillekens, P., 91-ATIO-9 Song, J., 100-FD-11 Straub, S., 91-ATIO-9 Schiavone, N., 136-FD-15 Semmelmann, J., 85-AMT-5/GT-5 Silton, S., 90-APA-12, 195-APA-23, 246-FD-27, Sontag, J., 255-PDL-12 Streett, C., 233-APA-25 Schindler, M., 18-ATIO-3 Semper, M., 278-FD-30 271-APA-33 Soria, J., 153-AA-23 Strganac, T., 9-AFM-2, 124-APA-15, 270-APA-32 Schinwald, C., 91-ATIO-9 Sengissen, A., 188-AA-29 Silva, R., 117-ACD-3 Sorokach, M., 214-MST-9 Stuchlik, D., 200-BAL-2 Schlimm, K., 166-ATIO-17 Sepka, S., 68-TP-3, 108-TP-5 Silva, S., 156-ACD-4 Soucasse, L., 217-TP-11 Stuermer, A., 162-APA-19 Schlimpert, S., 41-AA-10 Serafini, J., 162-APA-19 Silva, W., 124-APA-15, 273-ASE-5 Soufiani, A., 217-TP-11 Su, H., 252-MAO-9 Schlottke, M., 229-AA-34 Serpieri, J., 38-AA-7, 88-APA-10 Silvestre, F., 5-AA-3, 9-AFM-2 Souza, D., 230-AA-35 Su, L., 181-PDL-9/TP-8 Schluter, J., 47-APA-5, 269-APA-31 Serre, G., 187-AA-28 Silvestre, M., 104-MAO-3 Spagnolo, S., 205-CFD-25 Su, W., 25-FD-1, 105-MST-5 Schmidt, A., 177-MST-7 Sescu, A., 24-CFD-4, 41-AA-10, 81-AA-15, 98-CFD-12, Simao Ferreira, C., 279-FD-31 Spalart, P., 123-APA-14, 211-FD-26 Subbarao, K., 48-APA-6, 157-AFM-9 130 Schmidt, B., 11-AMT-2/GT-2 209-FD-24 Simerly, S., 158-AMT-9/GT-9 Spalt, T., 259-AA-37 Subbareddy, P., 244-CFD-29, 246-FD-27, 278-FD-30 Schmidt, H., 105-MST-5, 195-APA-23 Sesterhenn, J., 306-CFD-36 Simões, L., 4-AA-2 Speck, S., 88-APA-10 Subramanian, N., 3-AA-1, 152-AA-22 Schmidt-Skipiol, F., 166-ATIO-17 Sevil, H., 128-ATIO-14 Simon, F., 262-AA-40 Speer, S., 302-CFD-32 Subramanyam, A., 153-AA-23 Schmisseur, J., 10-AMT-1/GT-1 Sezer, E., 66-MST-4 Sinayoko, S., 38-AA-7, 187-AA-28 Spehr, C., 186-AA-27, 260-AA-38 Sudani, J., 205-CFD-25 Schmitt, F., 91-ATIO-9 Sha, Z., 52-ATIO-6 Singh, A., 279-FD-31 Spencer, T., 300-ATIO-29 Sui, D., 65-MST-3 Schmollgruber, P., 82-ACD-2 Shah, G.,154-AFM-9 Singh, B., 255-PDL-12 Spiegel, S., 55-CFD-5, 130-CFD-13 Sun, D., 16-ATIO-1 Schneider, S., 28-FD-4, 61-FD-7, 137-FD-16, 209-FD-24 Shah, H., 203-CFD-23 Singh, K., 9-AFM-2 Spiegelberg, H., 297-APA-37 Sun, H., 95-CFD-9 Schneiders, L., 305-CFD-35 Shahpar, S., 251-MAO-8 Singh, M., 235-APA-27 Spillers, R., 62-FD-8, 175-FD-22 Sun, Y., 4-AA-2, 6-AA-4, 31-MST-2, 248-FD-29 Scholz, P., 125-APA-16, 159-AMT-10/GT-10 Sharbatdar, M., 131-CFD-14 Singh, R., 162-APA-19, 268-APA-30 Spinelli, A., 26-FD-2 Sun, Z., 130-CFD-13 Schomberg, T., 22-CFD-2, 96-CFD-10 Sharma, H., 235-APA-27 Singh, S., 84-AFM-6 Spravka, J., 249-FT-1 Sundström, E., 112-AA-16 Schönleitner, F., 151-AA-21 Sharma, R., 300-ATIO-29 Sinha, A., 228-AA-33 Sreenivas, K., 15-APA-4, 122-APA-13, 297-APA-37 Suñol, A., 250-LTA-1 Schram, C., 3-AA-1, 79-AA-13, 112-AA-16, 231-AA-36 Sharma, S., 239-ATIO-22 Sinha, K., 28-FD-4 Sridhar, B., 18-ATIO-3, 92-ATIO-10 Suraj Nandiganahalli, J., 31-MST-2 Schrijer, F., 138-FD-17 Sheehe, S., 11-AMT-2/GT-2 Sinha, P., 276-ATIO-26 Sridharan, A., 162-APA-19 Surakitbanharn, C., 166-ATIO-17 Schrock, C., 201-CFD-21 Shen, Q., 191-AMT-11/GT-11 Sinnige, T., 37-AA-6 Srigrarom, S., 162-APA-19, 234-APA-26, 265-ACD-7 Suryadi, A., 115-AA-19 Schroeder, A., 159-AMT-10/GT-10 Sheng, C., 122-APA-13, 194-APA-22 Siozos-Rousoulis, L., 152-AA-22 Srinivasan, C., 181-PDL-9/TP-8 Suryakumar, V., 9-AFM-2, 124-APA-15, 270-APA-32 Schroeder, W., 6-AA-4, 26-FD-2, 38-AA-7, 41-AA-10, Shepherd, J., 11-AMT-2/GT-2 Sirohi, J., 162-APA-19 Srinivasan, E., 50-APA-8 Surzhikov, S., 69-TP-4, 193-APA-21, 216-TP-10/PDL-10 79-AA-13, 80-AA-14, 229-AA-34, 305-CFD-35 Sherry, L., 52-ATIO-6, 117-ACD-3 Sitaraman, J., 21-CFD-1 Srivastava, A., 138-FD-17 Sutliff, D., 78-AA-12, 116-AA-20 Schülein, E., 138-FD-17 Sheshadri, T., 67-PDL-3 Sivaneri, V., 101-FD-12 Stachura, M., 157-AFM-9 Suzuki, K., 33-PDL-1/FD-5, 89-APA-11, 102-FD-13 Schultz, M., 164-ATIO-15 Sheta, E., 195-APA-23 Sivasubramanian, J., 102-FD-13 Stagni, A., 244-CFD-29 Suzuki, T., 68-TP-3 Schultz, V., 274-ATIO-24 Sheth, K., 126-ATIO-12 Sjogreen, B., 24-CFD-4 Staley, A., 299-ATIO-28 Swaminathan Gopalan, K., 288-TP-13 Schulze, M., 113-AA-17 Shi, R., 190-ACD-5, 251-MAO-8 Skies, F., 132-CFD-15 Stalnov, O., 7-AA-5, 38-AA-7, 79-AA-13 Swann, M., 293-ACD-8 Schuman, W., 280-FT-2/GT-14 Shi, S., 107-PDL-4 Skinner, J., 117-ACD-3 Stanek, M., 33-PDL-1/FD-5 Swieringa, K., 18-ATIO-3, 298-ATIO-27 Schuster, D., 233-APA-25 Shi, Y., 25-FD-1 Skvortsov, R., 187-AA-28 Stanford, B., 49-APA-7, 124-APA-15 Swift, S., 113-AA-17 Schuster, W., 151-AA-21, 198-ATIO-19 Shih, A., 164-ATIO-15 Slaboch, P., 303-CFD-33 Stangfeld, C., 208-FD-23 Sytsma, M., 158-AMT-9/GT-9 Schutte, J., 239-ATIO-22 Shimosawa, Y., 286-PDL-13 Slagle, A., 226-AA-31 Steiger, R., 46-AMT-4/GT-4 Szmelter, J., 163-ASE-1 Schwartzentruber, T., 256-TP-12 Shimoyama, K., 125-APA-16 Slater, J., 279-FD-31 Stein, F., 88-APA-10 Tabanli, H., 174-FD-20 Schwer, D., 102-FD-13 Shin, S., 126-ATIO-12 Slegers, N., 30-MST-1 Steinbrenner, J., 23-CFD-3 Taha, H., 236-APA-28 Sciacchitano, A., 266-AMT-13/GT-13 Shipton, L., 128-ATIO-14 Slotnick, J., 47-APA-5, 301-CFD-31 Stephan, A., 196-ASE-2, 237-ASE-3 Tai, J., 308-MAO-13 Author/Session Chair Index Taira, K., 101-FD-12, 136-FD-15, 248-FD-29 Thiele, F., 112-AA-16, 306-CFD-36 Troxel, S., 163-ASE-1 Varney, M., 31-MST-2 Wang, F., 85-AMT-5/GT-5, 191-AMT-11/GT-11, Takahashi, T., 117-ACD-3, 190-ACD-5, 232-ACD-6, Thielecke, F., 8-AFM-1 Trujillo, A., 199-ATIO-20 Vascik, P., 52-ATIO-6 237-ASE-3, 295-APA-34 286-PDL-13, 293-ACD-8 Thierry, M., 108-TP-5 Truong, A., 264-AA-42 Vashishtha, A., 102-FD-13 Wang, G., 265-ACD-7 Takaishi, T., 230-AA-35 Thipyopas, C., 234-APA-26 Tsai, C., 304-CFD-34 Vasile, M., 214-MST-9 Wang, H., 84-AFM-6, 244-CFD-29 Takaki, R., 23-CFD-3 Thobois, L., 272-ASE-4, 298-ATIO-27 Tsao, S., 92-ATIO-10, 197-ATIO-18 Vassaux, D., 167-BAL-1 Wang, J., 33-PDL-1/FD-5, 84-AFM-6, 180-PDL-8/ Takayanagi, H., 69-TP-4 Thomas, J., 307-MAO-12 Tsotskas, C., 29-MAO-1 Vatsa, V., 133-CFD-16, 259-AA-37 APA-20, 187-AA-28, 271-APA-33 Tal, E., 124-APA-15 Thompson, D., 23-CFD-3, 97-CFD-11 Tsubokura, M., 270-APA-32 Vaughan, W., 196-ASE-2, 273-ASE-5 Wang, K., 187-AA-28, 255-PDL-12 Tam, C., 41-AA-10, 67-PDL-3, 185-AA-26 Thompson, F., 104-MAO-3 Tsuchiya, T., 51-ATIO-5 Vaux, S., 249-FT-1 Wang, L., 151-AA-21, 260-AA-38 Tamaki, Y., 241-CFD-26 Thompson, R., 67-PDL-3, 244-CFD-29 Tsutsumi, S., 23-CFD-3 Vekaria, S., 235-APA-27 Wang, M., 187-AA-28, 255-PDL-12, 263-AA-41, Tamaskar, S., 239-ATIO-22 Thompson, T., 42-ACD-1 Tufts, M., 137-FD-16 Veldhuis, L., 37-AA-6, 269-APA-31 265-ACD-7 Tamba, T., 138-FD-17 Thornber, B., 306-CFD-36 Tuinstra, M., 115-AA-19 Vemuri, S., 234-APA-26 Wang, P., 128-ATIO-14 Tamura, M., 144-PDL-7 Thorne, J., 243-CFD-28 Tule, C., 157-AFM-9 Venel, S., 167-BAL-1 Wang, Q., 80-AA-14, 173-FD-19, 202-CFD-22, Tamura, T., 182-TP-9 Thorsen, A., 83-AFM-5 Tuna, B., 101-FD-12, 248-FD-29 Venkatachari, B., 193-APA-21, 211-FD-26 241-CFD-26 Tanaka, Y., 182-TP-9 Thumiah, D., 86-AMT-6/GT-6 Turchi, A., 34-TP-1 Venkatakrishnan, L., 227-AA-32 Wang, S., 62-FD-8, 119-AFM-8 Tang, C., 162-APA-19 Thurow, B., 67-PDL-3 Turowski, M., 85-AMT-5/GT-5 Venkatesh, B., 39-AA-8 Wang, X., 122-APA-13, 132-CFD-15, 250-LTA-1, Tang, H., 17-ATIO-2, 145-TP-7, 173-FD-19 Tian, P., 43-AFM-3 Tuttle, J., 167-BAL-1 Venkatraman, S., 50-APA-8 260-AA-38 Tang, S., 105-MST-5 Tian, Y., 44-AFM-4 Tyagi, A., 198-ATIO-19, 300-ATIO-29 Venuti, J., 51-ATIO-5 Wang, Y., 9-AFM-2, 22-CFD-2, 30-MST-1, 131-CFD-14, Tang, W., 267-APA-29 Tian, Z., 244-CFD-29 Tysell, L., 154-AA-24 Vera, J., 5-AA-3 213-MAO-7 Tang, Y., 105-MST-5 Tibor, E., 212-MAO-6 Tyson, W., 97-CFD-11 Vergine, F., 205-CFD-25 Wang, Z., 23-CFD-3, 25-FD-1, 56-CFD-6, 99-FD-10, Tanner, P., 120-AMT-7/GT-7 Tilmann, C., 271-APA-33 Uddin, M., 306-CFD-36 Vermeire, B., 130-CFD-13, 202-CFD-22 130-CFD-13, 138-FD-17, 170-CFD-18, 242-CFD-27, Tanno, H., 69-TP-4 Timme, S., 96-CFD-10 Ueckermann, M., 33-PDL-1/FD-5 Vermillion, C., 282-LTA-2 303-CFD-33 Tao, F., 7-AA-5 Timofeev, E., 102-FD-13 Uehara, A., 31-MST-2 Vey, S., 26-FD-2, 297-APA-37 Wanke, C., 275-ATIO-25 Tao, G., 127-ATIO-13 Ting, E., 124-APA-15 Ukeiley, L., 48-APA-6, 195-APA-23, 248-FD-29 Viladegut, A., 216-TP-10/PDL-10 Ward, C., 137-FD-16 Tao, L., 204-CFD-24, 245-CFD-30 Tissot, G., 5-AA-3 Ulbrich, N., 294-AMT-14/GT-15 Villa, C., 65-MST-3 Watanabe, Y., 33-PDL-1/FD-5, 102-FD-13 131 Tapken, U., 173-FD-19 Titarev, V., 187-AA-28 Ullrich, W., 41-AA-10, 185-AA-26 Vincent, P., 130-CFD-13, 202-CFD-22, 242-CFD-27 Watson, J., 104-MAO-3 Taquin, G., 83-AFM-5 Tittsworth, J., 237-ASE-3 Underbrink, J., 186-AA-27, 262-AA-40 Visbal, M., 101-FD-12, 102-FD-13, 170-CFD-18, Watson, W., 7-AA-5, 116-AA-20, 262-AA-40 Tarter, J., 140-ITAR-2 Tkachenko, O., 31-MST-2 Underwood, M., 299-ATIO-28 208-FD-23, 255-PDL-12, 266-AMT-13/GT-13, Weaver, A., 35-TP-2 Tatsukawa, T., 114-AA-18 Tkacik, P., 282-LTA-2 Upalkar, B., 145-TP-7 270-APA-32 Webb, N., 33-PDL-1/FD-5 Tavernetti, W., 278-FD-30 Tobalske, B., 100-FD-11 Ura, H., 230-AA-35 Viswanath, K., 233-APA-25 Webster, R., 122-APA-13 Tay, W., 22-CFD-2 Togiti, V., 172-CFD-20 Urnes, J., 49-APA-7 Vitale, S., 133-CFD-16 Wei, Q., 7-AA-5 Taylor, C., 275-ATIO-25 Tolomelli, L., 181-PDL-9/TP-8 Valavanis, K., 88-APA-10 Vitzilaios, N., 88-APA-10 Wei tao, Z., 303-CFD-33 Taylor, L., 15-APA-4, 297-APA-37 Tomac, M., 160-APA-17 Valentini, P., 256-TP-12 Vo, H., 60-FD-6/PDL-2 Weinstein, R., 50-APA-8 Taylor, N., 301-CFD-31 Tong, F., 151-AA-21, 260-AA-38 Valla, M., 272-ASE-4 Vos, R., 42-ACD-1 Weiss, B., 91-ATIO-9 Taylor, S., 273-ASE-5 Tong, O., 21-CFD-1 van Bussel, G., 122-APA-13, 279-FD-31 Vrchota, P., 233-APA-25 Weiss, M., 239-ATIO-22 Tchatchueng Kammegne, M., 66-MST-4 Tong, W., 176-MAO-5 van de Ven, T., 230-AA-35 Vu, B., 56-CFD-6 Wells, D., 42-ACD-1 Tchipev, N., 237-ASE-3 Tordeux, S., 262-AA-40 van der Velden, W., 38-AA-7 Vucinic, D., 250-LTA-1 Wen, Y., 250-LTA-1 Teare, D., 214-MST-9 Toropov, V., 5-AA-3, 251-MAO-8 van Kuijk, J., 37-AA-6 Vuillot, F., 39-AA-8, 259-AA-37 Wendorff, A., 212-MAO-6, 308-MAO-13 Temmler, C., 113-AA-17 Torres, S., 92-ATIO-10 van Oudheusden, B., 97-CFD-11, 138-FD-17, 208-FD-23 Wache, L., 52-ATIO-6 Weng, H., 68-TP-3 Tensuda, B., 304-CFD-34 Toubin, H., 161-APA-18 van Tooren, M., 64-MAO-2 Waddington, M., 82-ACD-2 Werner, T., 151-AA-21 Terakado, D., 169-CFD-17 Toussaint, C., 83-AFM-5 Van Treuren, K., 15-APA-4 Wagle, N., 157-AFM-9 Wernet, M., 227-AA-32 Ternisien, L., 18-ATIO-3 Toussaint, S., 300-ATIO-29 Van Treuren, R., 250-LTA-1 Wagner, C., 252-MAO-9 Werter, N., 29-MAO-1 Terracol, M., 154-AA-24, 229-AA-34 Towne, A., 5-AA-3 van Zuijlen, A., 38-AA-7, 122-APA-13 Wagner, J., 62-FD-8, 175-FD-22 West, A., 39-AA-8, 230-AA-35 Terrazas-Salinas, I., 108-TP-5 Tran, D., 99-FD-10 Vanden, K., 270-APA-32 Wagnild, R., 103-ITAR-1, 256-TP-12 West, J., 171-CFD-19 Tesfahunegn, Y., 307-MAO-12 Tran, L., 165-ATIO-16 Vanderwel, C., 3-AA-1, 38-AA-7, 152-AA-22 Waindim, M., 245-CFD-30 West, T., 58-CFD-8 Testa, C., 263-AA-41 Trani, A., 300-ATIO-29 Vanstone, L., 174-FD-20 Waithe, K., 14-APA-3, 89-APA-11 Wey, P., 45-AMT-3/GT-3, 47-APA-5 Tester, B., 186-AA-27 Treve, V., 51-ATIO-5 VanValkenburg, R., 237-ASE-3 Wakayama, S., 267-APA-29 Whalen, E., 248-FD-29, 271-APA-33 Thaiss, C., 83-AFM-5 Trevino, L., 214-MST-9 Varga, D., 200-BAL-2 Wakefield, D., 167-BAL-1 Wheaton, B., 103-ITAR-1, 278-FD-30 Thamsen, P., 173-FD-19 Trinh, K., 124-APA-15 Vargas, A., 167-BAL-1 Walker, A., 88-APA-10, 214-MST-9 White, E., 158-AMT-9/GT-9, 209-FD-24, 267-APA-29 Thanigaiarasu, S., 50-APA-8 Tritschler, J., 43-AFM-3 Vargas, M., 196-ASE-2 Walker, M., 50-APA-8 White, J., 133-CFD-16 Thekinen, J., 52-ATIO-6 Trolinger, J., 11-AMT-2/GT-2 Varghese, P., 288-TP-13 Wall, A., 40-AA-9 White, M., 67-PDL-3, 255-PDL-12 Theodore, C., 281-GEPC-1 Trollinger, L., 50-APA-8 Vargo, E., 275-ATIO-25 Wan, Y., 65-MST-3, 275-ATIO-25 White, T., 68-TP-3, 108-TP-5, 217-TP-11 Theunissen, R., 3-AA-1 Tropea, C., 50-APA-8, 271-APA-33, 297-APA-37 Varma, D., 125-APA-16 Wang, C., 161-APA-18, 213-MAO-7, 269-APA-31 Wiart, L., 13-APA-2 Author/Session Chair Index Wieland, F., 198-ATIO-19, 300-ATIO-29 Xie, J., 65-MST-3 Yoshino, T., 286-PDL-13 Zhang, Z., 46-AMT-4/GT-4, 58-CFD-8, 67-PDL-3, Wilcoxen, M., 17-ATIO-2 Xie, K., 191-AMT-11/GT-11 Young, D., 25-FD-1 138-FD-17, 181-PDL-9/TP-8 Wild, J., 125-APA-16, 230-AA-35 Xu, F., 57-CFD-7 Young, E., 200-BAL-2 Zhao, C., 128-ATIO-14 Wilder, M., 182-TP-9 Xu, J., 116-AA-20, 241-CFD-26 Young, L., 117-ACD-3 Zhao, D., 116-AA-20, 162-APA-19 Wilder, W., 91-ATIO-9 Xu, K., 107-PDL-4, 143-PDL-6 Young, R., 281-GEPC-1 Zhao, J., 33-PDL-1/FD-5 Wildschek, A., 64-MAO-2 Xu, Z., 105-MST-5, 241-CFD-26 Young, S., 166-ATIO-17 Zhao, K., 161-APA-18, 200-BAL-2 Wilkinson, S., 248-FD-29 Xue, M., 16-ATIO-1 Young, T., 48-APA-6, 102-FD-13 Zhao, Q., 194-APA-22, 241-CFD-26 Williams, A., 35-TP-2 Yadlin, Y., 271-APA-33 Yu, H., 159-AMT-10/GT-10 Zhao, W., 51-ATIO-5 Williams, D., 60-FD-6/PDL-2, 101-FD-12, 136-FD-15 Yagiz, B., 304-CFD-34 Yu, J., 122-APA-13 Zhao, X., 303-CFD-33 Williams, N., 244-CFD-29 Yakhina, G., 79-AA-13 Yu, L., 145-TP-7 Zhao, Y., 35-TP-2, 145-TP-7 Williamschen, M., 263-AA-41 Yakovlev, P., 228-AA-33 Yu, M., 243-CFD-28, 279-FD-31 Zhelonkin, M., 31-MST-2 Wilson, A., 198-ATIO-19 Yalin, A., 107-PDL-4 Yu, S., 269-APA-31 Zhelonkin, V., 31-MST-2 Winer, E., 104-MAO-3, 141-MAO-4, 176-MAO-5, Yamada, K., 144-PDL-7 Yu, W., 7-AA-5 Zheng, J., 185-AA-26 212-MAO-6 Yamagishi, K., 182-TP-9 Yuan, C., 248-FD-29 Zheng, Y., 44-AFM-4 Wing, A., 239-ATIO-22 Yamamoto, K., 23-CFD-3, 229-AA-34, 230-AA-35 Yuan-pei, S., 252-MAO-9 Zheng, Z., 43-AFM-3, 62-FD-8, 246-FD-27, 250-LTA-1, Wing, D., 299-ATIO-28 Yamashita, R., 89-APA-11 Yuceil, K., 174-FD-20 261-AA-39, 272-ASE-4 Winkel, R., 60-FD-6/PDL-2 Yamauchi, G., 192-AMT-12/GT-12 Yue, C., 280-FT-2/GT-14 Zhong, X., 209-FD-24 Winter, M., 108-TP-5, 121-AMT-8/FD-14/TP-6/GT-8, Yamouni, S., 270-APA-32 Yue, Z., 65-MST-3 Zhou, B., 79-AA-13, 283-MAO-10 181-PDL-9/TP-8 Yan, F., 128-ATIO-14 Zachos, P., 270-APA-32 Zhou, H., 250-LTA-1 Wintzer, M., 14-APA-3 Yan, G., 131-CFD-14 Zaidi, T., 52-ATIO-6 Zhou, J., 208-FD-23 Wisda, D., 114-AA-18, 187-AA-28 Yan, K., 250-LTA-1 Zajaczkowski, F., 140-ITAR-2 Zhou, L., 7-AA-5 Wisniewski, C., 15-APA-4 Yan, W., 178-MST-8 Zakaria, M., 236-APA-28 Zhou, P., 250-LTA-1 Wisniewski, N., 15-APA-4 Yan, X., 180-PDL-8/APA-20 Zaman, K., 189-AA-30 Wissa, A., 12-APA-1 Yang, C., 145-TP-7 Zambrano, J., 215-MST-10 Zhu, J., 25-FD-1 132 Wissink, A., 201-CFD-21 Yang, D., 204-CFD-24 Zanette, J., 249-FT-1 Zhu, M., 250-LTA-1 Witherden, F., 130-CFD-13, 202-CFD-22 Yang, H., 197-ATIO-18, 241-CFD-26, 304-CFD-34 Zang, T., 308-MAO-13 Zhu, T., 69-TP-4 Wittig, S., 46-AMT-4/GT-4 Yang, M., 119-AFM-8 Zawodny, N., 155-AA-25 Zientarski, L., 191-AMT-11/GT-11 Wlezien, R., 137-FD-16 Yang, T., 250-LTA-1 Zaytsev, M., 187-AA-28, 189-AA-30 Zimmerman, J., 107-PDL-4 Wohlbrandt, A., 41-AA-10 Yang, W., 105-MST-5 Zehner, P., 154-AA-24 Zingg, D., 132-CFD-15, 169-CFD-17, 204-CFD-24, Wolf, W., 38-AA-7, 41-AA-10, 189-AA-30, 260-AA-38, Yang, X., 98-CFD-12, 171-CFD-19 Zelenak, D., 143-PDL-6 242-CFD-27, 267-APA-29 270-APA-32 Yang, Y., 4-AA-2, 6-AA-4, 97-CFD-11, 162-APA-19, Zelinski, S., 16-ATIO-1 Zishka, E., 182-TP-9 Woo, G., 295-APA-34 178-MST-8, 269-APA-31 Zeng, D., 239-ATIO-22 Zocca, M., 26-FD-2, 196-ASE-2 Woopen, M., 95-CFD-9 Yang, Z., 159-AMT-10/GT-10, 268-APA-30 Zeng, Q., 30-MST-1 Zondervan, D., 197-ATIO-18 Wortmann, A., 42-ACD-1 Yao, C., 57-CFD-7, 188-AA-29 Zerobin, S., 151-AA-21 Zou, S., 25-FD-1 Wray, A., 24-CFD-4 Yao, H., 6-AA-4, 115-AA-19, 154-AA-24 Zha, G., 90-APA-12, 125-APA-16 Zuniga Vazquez, J., 23-CFD-3 Wray, T., 139-FD-18, 211-FD-26 Yao, W., 56-CFD-6 Zhai, Q., 67-PDL-3 Zwerger, C., 87-APA-9 Wright, M., 85-AMT-5/GT-5 Yarusevych, S., 100-FD-11, 208-FD-23 Zhai, Z., 215-MST-10 Wrighton, C., 227-AA-32 Yauwenas, Y., 115-AA-19 Zhang, B., 16-ATIO-1 Wronowski, K., 280-FT-2/GT-14 Yayla, S., 25-FD-1 Zhang, C., 253-MST-11, 295-APA-34 Wu, D., 213-MAO-7 Yazdani, S., 229-AA-34 Zhang, D., 180-PDL-8/APA-20, 271-APA-33 Wu, J., 25-FD-1, 265-ACD-7 Ye, C., 198-ATIO-19 Zhang, F., 47-APA-5 Wu, X., 99-FD-10 Yechout, T., 64-MAO-2 Zhang, G., 57-CFD-7 Wu, Y., 181-PDL-9/TP-8 Yee, H., 24-CFD-4 Zhang, H., 208-FD-23 Wu, Z., 250-LTA-1 Yee, P., 108-TP-5 Zhang, J., 65-MST-3, 203-CFD-23, 265-ACD-7 Wünsch, O., 22-CFD-2, 96-CFD-10 Yen, C., 78-AA-12 Zhang, L., 215-MST-10 Wyszogrodzki, A., 163-ASE-1 Yeste-Ojeda, O., 215-MST-10 Zhang, M., 5-AA-3 Xia, Y., 55-CFD-5 Yi, S., 12-APA-1 Zhang, S., 303-CFD-33 Xiang, J., 47-APA-5 Yoder, D., 58-CFD-8, 120-AMT-7/GT-7 Zhang, X., 7-AA-5, 22-CFD-2, 25-FD-1, 112-AA-16, Xiao, F., 130-CFD-13 Yokokawa, Y., 230-AA-35 113-AA-17, 152-AA-22, 205-CFD-25, 214-MST-9, Xiao, T., 97-CFD-11 Yoon, S., 136-FD-15 259-AA-37, 263-AA-41 Xiao, Y., 296-APA-35 Yoshida, S., 43-AFM-3 Zhang, Y., 31-MST-2, 122-APA-13, 198-ATIO-19, Xiaojie, Q., 105-MST-5 Yoshikawa, E., 298-ATIO-27 248-FD-29 IntroNotes
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AVIATION 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 1 Zone 3 21st AIAA/CEAS Aeroacoustics Conference 33rd AIAA Applied Aerodynamics Conference 31st AIAA Aerodynamic Measurement Technology and Ground Testing Conference 15th AIAA Aviation Technology, Integration, and Operations Zone 4 Conference 31st AIAA Aerodynamic Measurement Technology and AIAA Balloon Systems Conference Ground Testing Conference AIAA Flight Testing Conference AIAA Atmospheric Flight Mechanics Conference 22nd AIAA Lighter-Than-Air Systems Technology Conference 7th AIAA Atmospheric and Space Environments Conference AIAA Modeling and Simulation Technologies Conference AIAA Complex Aerospace Systems Exchange 45th AIAA Thermophysics Conference 22nd AIAA Computational Fluid Dynamics Conference 45th AIAA Fluid Dynamics Conference Zone 2 15th AIAA Aviation Technology, Integration, and Operations Conference AIAA Complex Aerospace Systems Exchange 45th AIAA Fluid Dynamics Conference 16th AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference 46th AIAA Plasmadynamics and Lasers Conference 45th AIAA Thermophysics Conference
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Hilton Anatole ZONE 2 ZONE 4 ZONE 1 ZONE 3
www.aiaa-aviation.org 13551 #aiaaAviation 2O16 13–17 JUNE 2016 WASHINGTON, D.C. See You Next Year! Technical Conferences 32nd AIAA Aerodynamic Measurement We hope that you learned something new, achieved Technology and Ground Testing Conference your goals, caught up with colleagues, and made new connections. We look forward to seeing you 34th AIAA Applied Aerodynamics Conference next year in the Nation’s capital! AIAA Atmospheric Flight Mechanics Conference 8th AIAA Atmospheric and Space Why Washington, D.C.? Environments Conference 16th AIAA Aviation Technology, Integration, It’s the perfect place to combine business and and Operations Conference family fun. It is home to Congress, NASA AIAA Flight Testing Conference Headquarters, NASA Goddard, NOAA, the FAA, 8th AIAA Flow Control Conference NSSC, NRL, and the Pentagon. There are more than 100 free things to do in Washington, D.C.— 46th AIAA Fluid Dynamics Conference including most of the Smithsonian (with TWO 17th AIAA/ISSMO Multidisciplinary Analysis air and space museums, art galleries, and the and Optimization Conference National Zoo) and scores of famous landmarks— AIAA Modeling and Simulation most within walking distance of one another. Technologies Conference 47th AIAA Plasmadynamics and Lasers Conference 46th AIAA Thermophysics Conference
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