Final Program - AIAA`s Aviation 2016

22–26 JUNE 2015 PUSHING THE BOUNDARIES OF THE IMAGINABLE: LEVERAGING THE AVIATION ECOSYSTEM FINAL PROGRAM www.aiaa-aviation.org #aiaaAviation 14-315 DALLAS, TX What is today’s best aircraft investment that ensures profitability? Airbus Widebody aircraft. Offering standard 18 inch wide seats in economy. Unrivalled low operating costs of the A330, 25% less fuel burn with the A350 XWB, up to 65% more profit per flight with the A380. Airbus is the answer. airbus.com © AIRBUS, 2015. All rights reserved. Airbus, its logo and the product names are registered trademarks. 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. Juan Alonso Victoria Cox Stanford University Federal Aviation Administration (retired) Thomas Edwards John O’Leary NASA Ames Research Center Airbus Americas Richard Wahls Todd Zarfos NASA Langley Research Center Boeing Commercial Airplanes Tom Enders will set the tone for us with his opening keynote addressing how the aviation industry can remain a dynamic player in pushing technology forward. Ed Bolton and Bill Ayer will discuss how NextGen will provide the foundation for advancing aviation in the future while engaging the myriad stakeholders that are a part of our ecosystem. Charlie Bolden will share the ways by which NASA historically has and will continue to push boundaries in aviation for the benefit of the entire community. Greg Touhill will discuss one of the more pressing issues of the day – cybersecurity and the importance of securing our ecosystem. Finally, Kurt Erbacher will look back at the design, development, and testing of the award-winning G650, one of the newest airplanes to hit the market while advancing the state of the art. The Forum 360 sessions will provide several opportunities for our community to interact with customers, regulators, and technology leaders in focused, intimate conversations. Two sessions will allow leaders from airlines to discuss issues of importance to them with our design community. Unmanned systems continue to make headlines and we will discuss the challenges facing this sector internationally. Following Administrator Bolden’s discussion of NASA’s aeronautics strategy, we will hear from the center directors responsible for executing those plans. The challenges of widely deploying green aviation technologies to substantially reduce the environmental impact of aviation will be addressed by international experts. The future of supercomputing and particle image velocimetry will be discussed, with an emphasis on their role in advancing the future of aerospace technology. We will also have focused sessions on complex aerospace systems that will tackle the most important system development issues facing chief engineers, program managers, and systems engineers today. As you would expect, with over 1,500 presentations, our technical program is second to none. The scope, breadth, and depth of the cutting-edge aviation and aerospace research being presented is material that you will be unable to find anywhere else. We thank the Forum Organizing and Technical Program Committees and the AIAA staff for their hard work to assemble this first-class program. We hope you will too. AVIATION 2015 will energize, inspire, and sustain our community’s efforts to keep the aviation ecosystem on the glide path to advanced efficiency, safety, and security. We thank you for making the choice to be here with us this week, and we are confident you will find the experience to be a worthwhile one. 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 Ground Testing Conference AIAA Flight Testing Conference 33rd AIAA Applied Aerodynamics Conference AIAA Atmospheric Flight Mechanics Conference 22nd AIAA Lighter-Than-Air Systems Technology Conference 7th AIAA Atmospheric and Space Environments Conference 16th AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference 15th AIAA Aviation Technology, Integration, and Operations Conference AIAA Modeling and Simulation Technologies Conference AIAA Balloon Systems Conference 45th AIAA Thermophysics Conference 45th AIAA Fluid Dynamics Conference 46th AIAA Plasmadynamics and Lasers Conference AIAA Complex Aerospace Systems Exchange www.aiaa-aviation.org 3#aiaaAviation Organizing Committee Intro General Chair Richard Wahls, NASA Langley Research Center Forum 360 Chair Robert Gregg, III, The Boeing Company Technical Co-Chair Vincent Schultz, NASA Langley Research Center Technical Co-Chair Greg Naterer, Memorial University International Konstantinos “Kostas” Kontis, University of Glasgow Member Services Sarah Shull, NASA Johnson Space Center Local Rep Terry Burress, Lockheed Martin Information Systems & Global Solutions Young Professional Greg Johnson, Aerojet Rocketdyne Recognition Dimitri Mavris, Georgia Institute of Technology Public Policy Bob Stuever, Beechcraft Defense Company, LLC Complex Aerospace Systems Exchange (CASE) Chair Sophia Bright, The Boeing Company Technical Program Committee Forum Technical Co-Chairs Greg Naterer (Aerospace Sciences Group), Memorial University Vincent Schultz (Aircraft and Atmospheric Systems Group), NASA Langley Research Center Forum Deputy Technical Co-Chairs LaTunia Melton (Aerospace Sciences Group), NASA Langley Research Center Cees Bil (Aircraft and Atmospheric Systems Group), RMIT University ITAR Chair Katya M. Casper, Sandia National Laboratories www.aiaa-aviation.org Technical Discipline Chairs Aeroacoustics Naval Agarwal, The Boeing Company Aerodynamic Measurement Technology Andrew Cutler, The George Washington University Todd Lowe, Virginia Polytechnic Institute and State University Air Transportation Integration & Operations Cees Bil, RMIT University Kapil Sheth, NASA Ames Research Center Karen Marais, Purdue University Flight Testing Karl Garman, Federal Aviation Administration Fluid Dynamics Jill Klentzman, Baylor University Green Engineering Andrew Gibson, Empirical Systems Aerospace Ground Testing Benjamin Mills, Aerospace Testing Alliance Lighter than Air Systems Rajkumar S. Pant, Indian Institute of Technology Bombay Scot Campbell, Massachusetts Institute of Technology Modeling and Simulation Technologies Gano Broto Chatterji, NASA Ames Research Center Aircraft Design Hernando Jimenez, Georgia Institute of Technology Multidisciplinary Analysis and Optimization Eliot Winer, Iowa State University Danielle (Dani) Soban, Queen’s University Belfast Applied Aerodynamics Brian McGrath, The Johns Hopkins University Applied Physics Laboratory Khaled Abdol-Hamid, NASA Langley Research Center Zifeng Yang, Wright State University Atmospheric and Space Environments Nashat Ahmad, NASA Langley Research Center Vijay Kalivarapu, Iowa State University Plasmadynamics and Lasers Azer Yalin, Colorado State University Thermophysics Chad Boyack, Raytheon Missile Systems Elliott Short, Raytheon Missile Systems Technical Discipline Group Representatives TAC Information Systems Group Sam Adhikari, Sysoft Corporation Matthew Pruis, Northwest Research Associates Inc. Atmospheric Flight Mechanics Soumyo (Som) Dutta, NASA Langley Research Center Kevin Cunningham, NASA Langley Research Center Balloon Systems Debora Fairbrother, NASA Complex Aerospace Systems Exchange (CASE) Sophia Bright, The Boeing Company Computational Fluid Dynamics Krzysztof (Chris) Fidkowski, University of Michigan 4#aiaaAviation Contents Intro Welcome 3 Organizing Committee 4 Contents5 Forum Overview 8 Sponsors 10 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 ITAR Information 21 Exposition Hall 22 www.twitter.com/aiaa www.flickr.com/aiaaevents http://livestream.com/AIAAvideo/ AVIATION2015 www.instagram.com/aiaaerospace Exhibitors24 General Information 27 Author and Session Chair Information 29 Committee Meetings 30 Sessions at a Glance 33 Session Detail Matrix 41 Author and Session Chair Index #aiaaAviation On-Site Wi-Fi Information Network Name: PSAV-Meeting Password: AIAA2015 121 Technical Zones 134 Venue Map 135 www.aiaa-aviation.org Join the conversation! 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. 5#aiaaAviation Get Your Conference Info on the Go! Download the FREE AIAA 2015 Conference Mobile App MY ITINERARY FROM SCHOLARONE Compatible with iPhone/iPad, Android, and BlackBerry! FEATURES Browse Program View the program at your fingertips My Itinerary Create your own conference schedule Conference Info Including special events Take Notes HOW TO DOWNLOAD 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. MyItinerary Mobile App MyItinerary Web App For optimal use, we recommend iPhone 3GS, iPod Touch (3rd generation), iPad iOS 4.0, or later • For optimal use, we recommend: Download the MyItinerary app by searching for “ScholarOne” in the App Store directly from your mobile device. Or, access the link below or scan the QR code to access the iTunes page for the app. Take notes during sessions http://itunes.apple.com/us/app/scholaronemy-itinerary/id497884329?mt=8 City Map Select the meeting “AIAA Aviation 2015” See the surrounding area and the Hilton Anatole Connect to Twitter Tweet about what you’re doing and who you’re meeting with #aiaaAviation s iPhone 3GS, iPod Touch (3rd generation), iPad iOS 4.0, or later sMost mobile devices using Android 2.2 or later with the default browser sB lackBerry Torch or later device using BlackBerry OS 7.0 with the default browser •Download the MyItinerary app by scanning the QR code or accessing http://download.abstractcentral.com/ aiaa-mav15/index.htm • Once downloaded, you can bookmark the site to access it later or add a link to your home screen. Participate in Real-Time Q&A and Polling during AIAA AVIATION 2015 with the Conference IO App! During Plenary and Forum 360 Sessions, go to aiaa1.cnf.io 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 Forum Overview Intro 0730 hrs MONDAY 22 June TUESDAY 23 June Speakers’ Briefing Speakers’ Briefing Plenary Keynote Plenary Panel 0800 hrs 0830 hrs 0900 hrs Networking Break in Exposition Hall Networking Break 0930 hrs 1000 hrs Technical Sessions 1030 hrs Technical Sessions Forum 360 Exposition Hall Open Forum 360 1100 hrs 1130 hrs 1200 hrs 1230 hrs 1300 hrs Awards Luncheon: Celebrating Achievements in Aerospace Sciences Networking Lunch on Own 1330 hrs Networking Lunch on Own 1400 hrs 1430 hrs 1500 hrs 1530 hrs Technical Sessions Networking Break Forum 360 Forum 360 Networking Break in Exposition Hall CFD Flow Visualization Showcase Exposition Hall Open Technical Sessions 1600 hrs 1630 hrs Plasmadynamics and Lasers Award Lecture 1700 hrs 1730 hrs 1800 hrs 1830 hrs 1900 hrs Fluid Dynamics Award Lecture Speed Geek Networking Event and Reception Reception in Exposition Hall Rising Leaders in Aerospace Reception 1930 hrs 2000 hrs 2030 hrs 2100 hrs 2130 hrs 2200 hrs www.aiaa-aviation.org 8#aiaaAviation Forum Overview Intro WEDNESDAY 24 June THURSDAY 25 June FRIDAY 26 June Speakers’ Briefing Speakers’ Briefing Speakers’ Briefing Plenary Keynote Plenary Keynote Plenary Keynote 0730 hrs 0800 hrs 0830 hrs 0900 hrs Networking Break in Exposition Hall Networking Break in Exposition Hall Networking Break 0930 hrs Exposition Hall Open 1000 hrs Technical Sessions 1030 hrs Forum 360 Technical Sessions Forum 360 Exposition Hall Open Technical Sessions 1100 hrs 1130 hrs 1200 hrs 1230 hrs 1300 hrs Awards Luncheon: Celebrating Achievements in Aircraft and Atmospheric Systems Luncheon in Exposition Hall 1330 hrs Networking Lunch on Own 1400 hrs 1430 hrs 1500 hrs 1530 hrs Forum 360 Networking Break in Exposition Hall Technical Sessions 1600 hrs 1630 hrs 1700 hrs 1730 hrs 1800 hrs Aerodynamics Award Lecture Aeroacoustics Lecture Rising Leaders in Aerospace Panel Exposition Hall Open Rising Leaders in Aerospace Leadership Exchange/Speed Networking Thermophysics Award Lecture Forum 360 Networking Break Technical Sessions Wright Brothers Lectureship in Aeronautics 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 Sponsors Intro 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 Keynote Speakers and Plenary Sessions Intro 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 These conversations will cover a spectrum of timely topics including programs, systems, policy, operations, applications, platforms and more! Monday, 22 June 0930–1200 hrs Grand Ballroom E The Voice of the Customer — Designing the Right Aircraft Moderator: Christopher Stonehouse, Senior Vice President, Customer Services, Airbus Americas, Inc. Panelists: Jack Arehart, President of MRO Services, Delta TechOps William “Bill” Meehan, Chief Operating Officer, Frontier Airlines, Inc. Bart Roberts, Vice President, Flight Operations, JetBlue Airways David Seymour, Senior Vice President, Technical Operations, American Airlines 1400–1700 hrs Grand Ballroom E Whatever Happened to the Four-Year Airplane? Moderator: Craig Willis, Group Head for Systems Verification, Gulfstream G500/G600 Program, Gulfstream Aerospace Corporation Panelists: Tim Campbell, Senior Vice President, Air Operations, American Airlines Jim Crites, Executive Vice President of Operations, DFW International Airport Brian Quigley, Managing Director Flight Operations, United Airlines Dan Smiley, Vice President for System Operations, Federal Aviation Administration Air Traffic Office 1400–1630 hrs Grand Ballroom E International UAS Integration Forum Moderator: Rob Hughes, Northrop Grumman, Inc Panelists: Cees Bil, Associate Professor, School of Aerospace, Mechanical and Manufacturing Engineering, RMIT University Chuck Johnson, Vice President of Operations, The Padina Group Marty Rogers, University of Alaska-Fairbanks Marshall Jackson, Project Manager – Aviation Safety Audits, Office of Inspector General, U.S. Department of Transportation Randy Willis, FAA, Co-Chair of ICAO RPAS (Remotely Piloted Aircraft Systems) Dale Richards, Senior Research Fellow, Human Factors, Faculty of Engineering & Computing, Coventry University 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 Intro 360 Forum 1400–1730 hrs Wednesday, 24 June 0930–1200 hrs Grand Ballroom E NACA to NASA: Embarking on the Next 100 Years of Excellence and Innovation in Aeronautics and Beyond Moderator: Robert Pearce, Director, Strategy, Architecture & Analysis, Aeronautics Research Mission Directorate, NASA Headquarters Panelists: David Bowles, Center Director (Acting), NASA Langley Research Center Thomas Edwards, Deputy Center Director, NASA Ames Research Center Janet Kavandi, Deputy Director, NASA Glenn Research Center David McBride, Center Director, NASA Armstrong Flight Research Center Jaiwon Shin, Associate Administrator, Aeronautics Research Mission Directorate, NASA Headquarters 1400–1630 hrs Grand Ballroom E Energy/Environment Panel — The Challenges of Green Aviation Moderator: Marty Bradley, Technical Fellow, Boeing Commercial Airplanes Panelists: Ricky Curran, Faculty of Aerospace Engineering, Delft University of Technology Jay E. Dryer, Director, Advanced Air Vehicles Program Office (Acting), Aeronautics Research Mission Directorate, NASA Headquarters Askin Isikveren, Head of Visionary Aircraft Concepts, Bauhaus Luftfahrt Leslie Perkins, Director, Energy Office, Air Force Research Laboratory Jeanne Yu, Environmental Director, Boeing Commercial Airplanes Grand Ballroom D System Complexity: Government Needs and Practical Research Results Keynote Speaker: Kristen Baldwin, Principal Deputy DASD (SE), Department of Defense Moderators: Frank Serna, Principal Director, Strategic Imperatives, Draper Laboratory Anna-Marie McGowan, Aeronautics Research Directorate, NASA Langley Research Center Panelists: Jeffrey P. Holland, Director of Research and Development and Chief Scientist, U.S. Army Corps of Engineers David Neyland, Consultant Thursday, 25 June 0930–1200 hrs Grand Ballroom E The Impact of Particle Image Velocimetry on Aerospace Technology Moderator: Steven Beresh, Distinguished Member of the Technical Staff, Sandia National Laboratories Panelists: Ronald J. Adrian, Regent’s Professor and Ira A. Fulton Professor of Mechanical and Aerospace Engineering, Arizona State University Susan Gorton, Project Manager, Revolutionary Vertical Lift Technology Project, NASA Langley Research Center Fulvio Scarano, Full Professor and Chair of Aerodynamics, Delft University of Technology Miguel Visbal, Principal Research Aerospace Engineer and Team Leader of Multidisciplinary Computational Aerodynamics, Aerospace Systems Directorate, Air Force Research Laboratory 1400–1630 hrs Grand Ballroom E Supercomputing: Roadmap and Its Future Role in Aerospace 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 Intro 360 Forum 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 day activity of the 2015 CASE Academic Workshop. It will offer rapid-fire discussions of current research efforts in systems knowledge and competency. Sponsored by Boeing Commercial Airplanes Facilitators: 0930–1200 hrs Franz-Josef Kahlen, Ph.D., Associate Professor, Department of Mechanical Engineering, University of Cape Town, Cape Town, South Africa Shannon Flumerfelt, Ph.D., Associate Professor, Educational Leadership, Director of Lean Thinking for Schools, Pawley Learning Institute, Oakland University, Michigan Anabela Alves, Ph.D., Assistant Professor, Departamento de Produção e Sistemas Escola de Engenharia da Universidade do Minho, Centro Interdisciplinar de Tecnologias, da Produção e da Energia (CITPE), Campus de Azurém, Portugal 1400–1700 hrs Grand Ballroom E Whatever Happened to the Four-Year Airplane? This panel will explore the challenges facing aerospace professionals who are directly engaged in leading, developing, producing, and supporting the industry’s most advanced vehicles and systems in the context of a “four-year aircraft” theme. We continue to push the limits of technology to deliver greater performance in all segments of aerospace, in an environment that is increasingly risk averse. These challenges have pushed us to longer development cycles and exponential growth in budgets. In addition, new technical disciplines (e.g., cyber) are being integrated into legacy and emerging systems, while subsystems are gaining in both complexity and interdependency. In the context of this environment, our panel will address how the aerospace industry should position itself to meet the challenges of reducing the cost and schedule and approach a “four-year aircraft” cycle in our increasingly complex world. Moderator: Craig Willis, Group Head for Systems Verification, Gulfstream G500/G600 Program, Gulfstream Aerospace Corporation 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 Tuesday, 23 June Grand Ballroom D Applied Complexity Workshop 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, Systems Engineering & Integration Team 777X, Boeing Commercial Airplanes Steve Holt, Engineering Integrated Strategy, Airplane Level Engineering Integration, The Boeing Company Jim Blohowiak, 777X Airplane Level Integration Team, The Boeing Company Alison Lauderbach, 777X Airplane Level Integration Team, The Boeing Company 1400–1530 hrs Steuben 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 UrbanaChampaign Mat French, Electrical Systems Engineer, Rolls-Royce Corporation Panelists: Rick Mange, F-35 PNR Program Manager, Lockheed Martin Aeronautics Robert (Rob) Simons, Technical Fellow, The Boeing Company Jason Merret, Technical Specialist, Gulfstream Aerospace Performance Engineering, Gulfstream Aerospace Corporation 14#aiaaAviation Forum 360 Intro 1545–1730 hrs Steuben 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 Carmen Schooley, Manager, Systems Engineering and Integration, Gulfstream Aerospace Corporation Panelists: 1045–1230 hrs Grand Ballroom D 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, Chief Engineer of Factories, Raytheon Missile Systems Ed Dolanski, President and CEO, Aviall Jim Gallagher, EIS Program Manager, Gulfstream Aerospace Corporation Fernando Dones, Technical Fellow, The Boeing Company Bernard Dion, CTO, ANSYS Brenda Nuhfer, Program Manager, UTC/Pratt & Whitney 1400–1730 hrs Wednesday, 24 June 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. 0900–1045 hrs Grand Ballroom D 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 transdisciplinary 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 David Loda, Executive Director, NCPS Research, LLC Panelists: Grand Ballroom D System Complexity: Government Needs and Practical Research Results Keynote Speaker: Kristen Baldwin, Principal Deputy DASD (SE), Department of Defense Moderators: Frank Serna, Principal Director, Strategic Initiatives, Draper Laboratory Anna-Maria McGowan, Aeronautics Research Directorate, NASA Langley Research Center Panelists: Jeffrey P. Holland, Director of Research and Development and Chief Scientist, U.S. Army Corps of Engineers David Neyland, Consultant 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 Forum 360 Intro RISING The multidimensional program features a leadership exchange/speed mentoring, panel session, Q&A with top industry leaders, and multiple opportunities for networking. These exciting and energetic activities will provide access to top aerospace leaders and their perspectives with subject matter relevant to your career. Sponsored by: LEADERS in AEROSPACE Program Agenda Networking Reception Panel Discussion: Transitioning to Leadership Monday, 22 June 1830–1930 hrs Emerald 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. Leadership Exchange/Speed Networking Wednesday, 24 June 1530–1700 hrs Metropolitan Ballroom Get your questions answered! Senior Mentors will include: Russ Althof, Chief Engineer, Raytheon Missile Systems Cees Bil, Professor, Royal Melbourne Institute of Technology Dave Bowles, C enter Director (Acting), NASA Langley Research Center Ed Feltrop, Engineer Specialist, Cessna Aircraft Company Susan Gorton, Rotary Wing Project, NASA Langley Research Center Peter Hartwich, Engineering Manager, Boeing Defense, Space and Security Janice Kavandi, Deputy Director, NASA Glenn Research Center 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, Center 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 Thursday, 25 June Emerald 1400–1530 hrs As engineers and aerospace professionals gain experience, there is often the opportunity to do more with the company. Promotions are often a result, but so are management opportunities. As you transition from an engineer on a project to an engineer leading a project, what changes? How about when you are made manager of a department or a division, are there skill sets that you need to hone? What if you are looking to eventually become a chief officer, how can you plan for and make those transitions? This panel will address the changes that accompany moving into a management role, the different skill sets that will need to be acquired, and the changes you can expect in your daily work routine. If you have management or leadership aspirations, come and listen to advice from esteemed panelists. Moderator: Ben Marchionna, Systems Engineer, Lockheed Martin Skunk Works Panelists: Russ Althof, Chief Engineer, Raytheon Missile Systems Douglas Stanley, President and Executive Director, National Institute of Aerospace Frederick Wieland, Director, Air Traffic Management, Intelligent Automation Systems, Inc. 16#aiaaAviation Special Sessions and Events Intro Speed Geek Networking Event and Reception Monday, 22 June Chantilly Ballroom Foyer 1730–1830 hrs, reception to follow 1830–1900 hrs A MILE OF RUNWAY CAN 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 1400–1600 hrs Chantilly Ballroom Foyer 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 largescreen 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 1900 hrs Imperial Ballroom 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 on site, as space is available. NARRATED BY HARRISON FORD See it in Dallas at the Perot Museum of Nature and Science www.airplanesmovie.com www.aiaa-aviation.org 17#aiaaAviation Intro Networking 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 Sunday, 21 June 1800–1930 hrs Reception in the Exposition Hall Emerald Mingle with your peers and hear from AIAA Executive Director Sandy Magnus. This reception provides you with the opportunity to meet your fellow students and learn more about the opportunities available to you as an AIAA student member. Networking Coffee Breaks Networking coffee breaks allow even more time for making new contacts, continuing discussions from sessions, visiting the Exposition Hall, or checking emails and voicemails to keep in touch with the office while you are at the forum. Networking coffee breaks will be held at the following locations and times: Monday, 22 June 0900–0930 hrs and 1530–1600 hrs; Meeting Room Foyers Tuesday, 23 June 0900–0930 hrs and 1530–1600 hrs; Exposition Hall Wednesday, 24 June 0900–0930 hrs and 1530–1600 hrs; Exposition Hall Thursday, 25 June Tuesday, 23 June 1730–1900 hrs Chantilly Ballroom East Take this opportunity to engage new contacts and refresh old ones. A ticket for the reception is required and included in the registration fee where indicated. Additional tickets for guests may be purchased on site, as space is available. Luncheon in the Exposition Hall Wednesday, 24 June Chantilly Ballroom East 1230–1400 hrs A ticket is required and included in the registration fee where indicated. 0900–0930 hrs (Exposition Hall) and 1530–1600 hrs (Meeting Room Foyers) Friday, 26 June www.aiaa-aviation.org 0900–0930 hrs Meeting Room Foyers 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 Fluid Dynamics Award Lecture Searching for Truthiness in Computational Fluid Dynamics Philip Roe, Professor, Department of Aerospace Engineering, University of Michigan Ring Chair & Professor, Mechanical Engineering Department University of Memphis “For significant contributions to gas turbine heat transfer and aerodynamics, investigation of novel cooling schemes and application of emerging computational methodologies for gas turbine cooling.” Certificates of Merit: Tuesday, 23 June 1230–1400 hrs Sumanta Acharya Chantilly Ballroom West Awards Luncheon: Celebrating Achievements in Aerospace Sciences A ticket for the luncheon is required and included in the registration fee where indicated. Additional tickets for guests may be purchased on site, as space is available. The following awards will be presented: Aeroacoustics Award Nigel Peake Professor, Applied Mathematics University of Cambridge “For significant contributions to the understanding and prediction of turbomachinery noise generation and scattering.” Aerodynamics Award Russell M. Cummings Professor of Aeronautics U.S. Air Force Academy “For a career devoted to predicting and understanding the vortical flowfields about aircraft at high angles of attack and during maneuvers.” Fluid Dynamics Award Philip Roe Professor, Department of Aerospace Engineering University of Michigan “For seminal contributions to the design of numerical algorithms for simulations of compressible flows.” Plasmadynamics and Lasers Award Philip E. Cassady Senior Technical Fellow (retired) The Boeing Company “For distinguished contributions to the development of aero-optics and high power laser fluid dynamics.” Aerodynamic Measurement Technology Best Paper AIAA 2015-1696, “Pressure Monitoring using Hybrid fs/ps Rotational CARS,” Sean Kearney, Sandia National Laboratories, and Paul Danehy, NASA Langley Research Center. Applied Aerodynamics Best Paper AIAA 2014-2139, “Uncertainty Quantification and Certification Prediction of Low-Boom Supersonic Aircraft Configurations,” Thomas K. West, Missouri University of Science and Technology; Bryan W. Reuter, University of Texas at Austin; Eric L. Walker, Bill Kleb, and Michael A. Park, NASA Langley Research Center. David Weaver Best Student Paper AIAA 2014-2247, “Microscale Simulations of Porous TPS Materials: Application to Permeability,” Eric C. Stern, Ioannis Nompeli, Thomas Schwartzentruber and Graham Candler, University of Minnesota. Fluid Dynamics Best Paper AIAA Paper 2015-1518, “Large Eddy Simulation of a ThreeDimensional Compression Ramp Shock-Turbulent Boundary Layer Interaction,” David Dawson and Sanjiva Lele, Stanford University. Ground Testing Best Paper AIAA 2014-2800, “Skin Friction Sensor Validation for HighSpeed, High-Enthalpy Flow Applications,” Ryan Meritt and Joseph Schetz, Virginia Polytechnic Institute and State University. Modeling and Simulation Best Paper AIAA 2014-2206, “Transfer of Training on the Vertical Motion Simulator,” Peter Zaal, NASA Ames Research Center; Jeffrey Schroeder, Federal Aviation Administration; and William Chung, SAIC. (continued) www.aiaa-aviation.org 19#aiaaAviation Recognition Events Thursday, 25 June Certificates of Merit (continued) Plasmadynamics and Lasers Best Paper AIAA 2015-0935, “Electric Field Measurements in a Dielectric Barrier Nanosecond Pulse Discharge with Sub-nanosecond Time Resolution,” Benjamin Goldberg and Walter Lempert, Ohio State University; and Sean O’Byrne, University of New South Wales at the Australian Defence Force Academy. Plasmadynamics and Lasers Best Student Paper AIAA 2015-0679, “A Latency-Tolerant Architecture for Airborne Adaptive Optic Systems,” William R. Burns, Eric J. Jumper and Stanislav Gordeyev, University of Notre Dame. Thermophysics Best Paper AIAA 2015-0213, “NASA Langley Experimental Aerothermodynamic Contributions to Slender and Winged Hypersonic Vehicles,” Scott Berry and Karen Berger, NASA Langley Research Center. 1630–1730 hrs Grand Ballroom D Plasmadynamics and Lasers Award Lecture From Plasmadynamics and Shock Tubes to AeroOptics and Laser Radar: An Aerospace Career Philip E. Cassady, Senior Technical Fellow (retired), The Boeing Company Wednesday, 24 June 1630–1730 hrs Chantilly Ballroom West Aerodynamics Award Lecture Still Trying to Understand Aircraft Vortices Russell M. Cummings, Professor of Aeronautics, U.S. Air Force Academy 1730–1830 hrs Grand Ballroom E Thermophysics Award Lecture Aerodynamics and Heat Transfer in Gas Turbine Cooling-Recent Advances Sumanta Acharya, Ring Chair & Professor, Mechanical Engineering Department, University of Memphis 1730–1830 hrs Chantilly Ballroom West Aeroacoustics Lecture Fan Broadband Noise Generation and Suppression 1230–1400 hrs Chantilly Ballroom West Awards Luncheon: Celebrating Achievements in Aircraft and Atmospheric Systems A ticket for the luncheon is required and included in the registration fee where indicated. Additional tickets for guests may be purchased on site, as space is available. The following awards will be presented: Aircraft Design Award Darold B. Cummings Aerospace Consultant Boeing Technical Fellow (retired) “For a career demonstrating exceptional skill and creativity in the configuration and design of aircraft, and inspiring future generations of aircraft designers.” Elmer A. Sperry Award Michael Sinnett, Vice President, Product Development, and the Boeing 787-8 Development Team, Seattle, Washington “For pioneering engineering advances including lightweight composite wing and monolithic composite fuselage construction and advanced systems that have led to significant improvements in fuel efficiency, reduced carbon emission, reduced maintenance costs and increased passenger comfort.” Certificates of Merit: Aircraft Design Best Paper AIAA 2014-3012, “A Requirements-driven Methodology for Integrating Subsystem Architecture Sizing and Analysis into the Conceptual Aircraft Design Phase,” Imon Chakraborty, David Trawick, and Dimitri Mavris, Georgia Institute of Technology; Mathias Emeneth, PACE Americas Inc.; and Alexander Schneegans, PACE GmbH. Multidisciplinary Design Optimization Best Paper AIAA-2014-3274, “Aerostructural Optimization of the Common Research Model Configuration,” Gaetan Kenway and Joaquim Martins, University of Michigan; and Graeme Kennedy, Georgia Institute of Technology. 1730–1830 hrs Chantilly Ballroom West Wright Brothers Lectureship in Aeronautics Development and Testing of the X-47B Pablo Gonzalez II, UCAS-D Program Manager, Northrop Grumman Aerospace Systems Edmane Envia, Acoustics Branch, NASA Glenn Research Center www.aiaa-aviation.org 20#aiaaAviation Intro Information ITAR ITAR-Restricted Sessions On Tuesday, a limited number of oral presentations and papers will be presented in “U.S. Only” technical sessions. In addition to your forum registration, a separate registration process is required to attend these restricted sessions. Please see the detailed information on the ITAR Registration Grid below to determine your individual requirements. Access to ITAR Sessions: Presenting a Paper, Chairing a Session, or Attending an ITARRestricted Presentation Admittance to the restricted technical program is controlled by the U.S. International Traffic in Arms Regulations (ITAR). All attendees, presenters, and session chairs will need to register for the conference, and then visit the ITAR registration desk to complete the additional processes. Anyone wishing to enter the restricted session room MUST abide by the procedures and submission of verified documents mandated by the DoD. No Exceptions! Availability of Manuscripts from ITAR-Restricted Sessions For those who are registered to attend the sessions, a DVD containing the papers from the ITAR sessions will be available for purchase on site at the forum for $25. Those purchasing the DVD must be available to pick it up on Wednesday, 24 June 2015. All DVDs must be picked up in person. There will be no sale or distribution of these papers after the event. ITAR Electronics Policy No phones, computers (other than the presenter), iPads, cameras, or other electronic devices with cameras or recording capabilities will be permitted into the ITAR session room. There will be a check-in desk in front of the room where you can check these devices. Important session information for all attendees wishing to present or attend ITAR papers AIAA Restricted Papers – ITAR Regulations Session Admittance Policy (Revised 10/19/2012) Several papers scheduled to be presented at this conference will be restricted papers governed by ITAR (U.S. International Traffic in Arms Regulations). If you plan to attend any presentations restricted by ITAR, you must bring proof of citizenship PLUS the other verification documents as shown below. Please note that only U.S. Citizens and U.S. Resident Aliens can be considered for attendance at these restricted presentations. Admittance to restricted sessions and access to restricted technical papers is implemented and controlled by ITAR . All restricted session attendees (including speakers and session chairs for these sessions) MUST abide by the procedures and submittal of verification documents as noted below – NO EXCEPTIONS: ATTENDEE CLASSIFICATION U.S. Government Employees U.S. Citizens Resident Aliens (U.S.) IDENTIFICATION & PROOF OF EMPLOYMENT REQUIREMENTS 1. 2. 1. 2. 3. 1. 2. 3. Proof of U.S. Citizenship (for example, passport, birth certificate, voters registration card, naturalization papers), AND Personal photographic identification: U.S. Government/Military Photo ID badge, such as CAC card Proof of U.S. Citizenship (for example, passport, birth certificate, voters registration card, naturalization papers), AND Personal photographic identification (passport, driver’s license, etc.), AND Certification credentials based on DD Form 2345 (see below for details) Resident Alien Card, AND Personal photographic identification (passport, driver’s license, etc.), AND 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 Exposition Hall Intro Exhibitor Lounge MathWorks Altair AIAA Pavilion ANSYS XFlow CFD Kamatics /RWG Desktop ADI 410 SG 309 dSPACE Ennova G.R.A.S. DUNMORE 208 408 307 Software Tecplot Cradle BETA CAE OPAL-RT Pointwise Photron 301 401 303 30 304 302 403 Exa Corp 404 ENTRANCE Exhibitors by Booth Number 217 AIAA North Texas Section 420 Altair 213 ANSYS 410 Applied Dynamics International (ADI) 403 BETA CAE Systems USA, Inc. 219 DARcorporation 209 Desktop Aeronautics 207 dSPACE 408 DUNMORE Corporation 208 Ennova Technologies, Inc. 215 ESI North America 211 ESTECO 404 Exa Corporation 307 G.R.A.S. Sound & Vibration 412 Kamatics/RWG www.aiaa-aviation.org 314 Lockheed Martin 320 MathWorks 301 OPAL-RT Technologies 401 Photron 302 Pointwise, Inc. 309 SG - Space & Ground Engineering Solutions 303 Software Cradle 304 Tecplot Inc. 301 VectorNav Technologies 416 Vision Research 414 XFlow CFD 22#aiaaAviation Intro Exposition 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. 30% Off All Books at AIAA AVIATION 2015 Exposition Hall Hours Tuesday, 23 June Reception* 0900–1230 hrs 1400–1600 hrs 1730–1900 hrs Wednesday, 24 June 0900–1200 hrs 1230–1600 hrs Thursday, 25 June 0900–1200 hrs AIAA Publications is offering a special show discount on all titles featured at AVIATION 2015. Attendees can take advantage of a 30% discount off the list price of all books for sale at the AIAA Bookstore located in the AIAA Pavilion. This show special will only be available during the forum! Take advantage of these super savings and visit the AIAA Bookstore! *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 DARcorporation219 1440 Wakarusa Drive Lawrence, KS 66049 www.darcopr.com Jordan.ashley@darcorp.com Altair420 DARcorporation (Design, Analysis and Research Corporation) is an aeronautical engineering firm, located in Lawrence, Kansas, that has been offering aeronautical engineering consulting services, software and books since 1991. 1820 E Big Beaver Road Troy, MI 48083 www.altair.com yancy@altair.com Desktop Aeronautics Inc. Altair is a leader in developing simulation-driven designs for leading aerospace customers. Our world-class optimization methods provide designs that are lower weight, higher quality, and have better performance vs. traditional designs. ANSYS, Inc. 213 2600 ANSYS Drive Cannonsburg, PA 15317 www.ansys.com jennifer.dorazio@ansys.com ANSYS, Inc. develops and globally markets engineering simulation software used by designers and engineers across the aerospace and defense industry. Our open and flexible simulation solutions enable users to simulate design performance using an open platform for fast, efficient and cost-effective product development. Applied Dynamics International 410 209 1900 Embarcadero Road Suite 101 Palo Alto, CA 94303 www.desktopaero.com sales@desktopaero.com Desktop Aeronautics is a software company that licenses tools for the aerodynamic design and analysis of aerospace vehicles. Our flagship product, GoCart, is an intuitive aerial vehicle design tool built around NASA’s renowned Cartesian Euler CFD solver, Cart3D. Our customers include major players from the aerospace industry and academia. dSPACE207 50131 Pontiac Trail Wixom, MI 48393-2020 www.dspaceinc.com info@dspace.com 3800 Stone School Road Ann Arbor, MI 48108-2499 www.adi.com info@adi.com dSPACE is the world’s leading provider of hardware and software tools for developing and testing sophisticated electronic control systems. dSPACE systems play a vital role in product innovation industries. Learn more at: www.dspaceinc.com. Applied Dynamics helps companies make better use of simulation assets through all stages of product development, verification testing, demonstration, training, and maintenance. Our user base includes more than 50% of the Fortune 500 aerospace and defense companies and extends into marine, power systems, oil & gas, and the automotive industry. DUNMORE Corporation BETA CAE Systems USA, Inc. DUNMORE is a manufacturer of engineered films and tapes for aerospace, supplying multilayer insulation materials to the aerospace industry for over twenty-five years. With a highly technical product base of over 400 certified products, DUNMORE is the trusted source for engineered aerospace films and tapes. 403 29800 Middlebelt Road Suite #100 Farmington Hills, MI 48334 www.ansa-usa.com Deepak@ansa-usa.com 408 145 Wharton Road Bristol, PA 19007 www.dunmore.com amallettjr@dunmore.com R 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 2150 Allston Way, Suite 250 Berkeley, CA 94704 ennova-cfd.com egan@ennova-cfd.com 208 Ennova Scalable Simulation Delivered Ennova Technologies delivers today’s most scalable simulation platform combining the power of cloud based computing, advanced geometry repair tools, and mixed mode meshing to create an extremely efficient pre and post processing simulation environment. ESI North America 215 32605 West Twelve Mile Road, Ste 350 Farmington Hills, MI 48334 www.esi-group.com mmd@esi-group.com ESTECO211 39555 Orchard Hill Place Novi, MI 48375 www.esteco.com marketing@esteco.com ESTECO is a pioneer in numerical optimization solutions, specializing in the research and development of engineering software for all stages of the simulation-driven design process. ESTECO’s top-class products, modeFRONTIER and SOMO, are used worldwide, helping companies increase efficiency in design simulation and accelerate product innovation. 404 55 Network Drive Burlington, MA 01803 www.exa.com info@exa.com Exa Corporation offers a full suite of CFD/CAE simulation design optimization software applications with aerodynamic, thermal and aeroacoustic simulation capabilities in addition to engineering consulting services. Exa’s products and services enable engineers to integrate simulation early in the design process, therefore creating competitive designs, shortening product design cycles and speeding time-to-market. www.aiaa-aviation.org 307 2234 E Enterprise Parkway Twinsburg, OH 44087 www.gras.uk sales@gras.us G.R.A.S. has concentrated its efforts and expertise on the development and production of front-end acoustic products. This includes in principle all products necessary for the precise and reliable measurement, and recording of acoustic signals, from the transducer to the input of the A/D converter. The main line of instrumentation includes a broad range of standard measurement microphones and preamplifiers, all designed and manufactured in accordance with international standards. Kamatics/RWG ESI’s 1,000 Virtual Prototyping and Mfg Simulation specialists serve clients in over 40 countries. For over 40 years, ESI’s simulation software suite has been used to tackle the toughest Acoustics, Crash, VR, Composites, Casting, Welding, Forming, and CFD engineering challenges—earning the slogan “We get it right.” For more info: www. esi-group.com Exa Corporation G.R.A.S. Sound & Vibration 412 1330 Blue Hills Ave Bloomfield, CT 06002 www.kaman.com/engineered John.bertolini@kaman.com For decades, Kamatics (USA) and RWG have been designing, testing, and manufacturing the highest performing bearings and flight critical parts in the industry, excelling under the most demanding conditions. Lockheed Martin Corporation 314 P.O. Box 748 MZ 1500 Fort Worth, TX 76101 www.lockheedmartin.com jon.h.otto@lmco.com Lockheed Martin is principally engaged in the research, design, development, manufacture, integration and sustainment of advance technology systems, products and services. MathWorks320 3 Apple Hill Drive Natick, MA 01760 www.mathworks.com/academia The MATLAB and Simulink product families are fundamental applied math and computational tools at the world’s educational institutions. Adopted by more than 5000 universities and colleges, MathWorks products accelerate the pace of learning, teaching, and research in engineering and science. MathWorks products also help prepare students for careers in industry worldwide, where the tools are widely used for data analysis, mathematical modeling, and algorithm development in collaborative research and new product development. 25#aiaaAviation Intro Exhibitors OPAL-RT TECHNOLOGIES 301 Tecplot, Inc 304 1751 Richardson, Suite 2525 Montreal Quebec H3K 1G6 www.opal-rt.com sabrina.benzid@opal-rt.com 3535 Factoria Blvd SE, Suite 550 Bellevue, WA 98006 www.tecplot.com info@tecplot.com OPAL-RT: From Imagination… to Real-Time. OPAL-RT TECHNOLOGIES is a world leading developer of open, Real-Time Digital Simulators and Hardware-in-the-Loop testing equipment for electrical, electro-mechanical and power electronics systems. Our simulators are used by engineers and researchers at leading manufacturers, utilities, universities and research centers around the world. Tecplot visualization tools—for simulations, analyses, and experiments—provide insight and understanding into the mechanisms inside your data. Information critical in pinpointing problems, optimizing designs, and explaining physical observations. Photron401 9520 Padgett Street, Suite 110 San Diego, CA 92126 www.photron.com image@photron.com Photron’s wide range of light sensitive high-speed cameras including systems ideally suited to PIV and DIC, mega pixel to 21,000 frames per second (fps) and 4M pixels producing HD to 2,000 fps. Photron has a slow motion camera for every application. Pointwise, Inc. 302 213 S. Jennings Avenue Fort Worth, TX 76104 www.pointwise.com sales@pointwise.com VectorNav Technologies 301 10501 Markison Road Dallas, TX 75238 www.vectornav.com sales@vectornav.com VectorNav specializes in high-performance inertial navigation systems using the latest MEMS sensor and GPS/GNSS technology. Since its founding in 2008, we have been providing customers worldwide fully calibrated inertial sensors with aerospace-grade filtering technology, expanding the possibilities of today’s inertial navigation technology. Vision Research 416 100 Dey Road Wayne, NJ 07470 www.visionresearch.com info@visionresearch.com Pointwise is solving the top problem facing engineering analysts today: grid generation and preprocessing for computational fluid dynamics. Since 1994, Pointwise has supplied meshing tools to engineers and scientists worldwide. Vision Research designs and manufactures high-speed digital imaging systems with unsurpassed light-sensitivity, image resolution, acquisition speed and image quality. Marketed under the Phantom®brand,these cameras enable users to visualize and analyze physical phenomena when it’s too fast to see, and too important not to™. SG-Space & Ground Engineering Solutions XFlow CFD 309 6A Aigiidon Street Athens, Attica Greece 11853 www.sg-incorp.com info@sg-incorp.com 40 Chellis Street White River Junction, VT 05001 www.xflowusa.com info@xflowusa.com. SG Company provides integrated engineering solutions for air/spacebased earth monitoring systems and develops special techniques for UAS (Unmanned Aerial Systems) earth observation applications in various disciplines. Software Cradle 414 303 XFlow™ CFD is the next-generation, meshless CFD package for modeling external aerodynamics of fixed-wing and rotorcraft aircraft. XFlow supports complex motion of complicated moving parts to model dynamic effects of control surface motion in flight, high-lift (take-off and landing) configurations and/or separation of munitions or separable stores. 70 Birch Alley, Suite 240 Beavercreek, OH 45440 www.cradle-cfd.com ando@cradle-cfd.com 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 General Information Intro AIAA Registration and Information Center Hours Conference Proceedings The AIAA Registration and Information Center will be located on the Ballroom Level at the Hyatt Regency. Hours are as follows: Proceedings for the forum will be available online. The cost is included in the registration fee where indicated. Online proceedings will be available on 22 June 2015. Attendees who register in advance for the online proceedings will be provided with instructions on how to access them. Those registering on site will be provided with instructions at that time. Sunday, 21 June 1500–1900 hrs Monday, 22 June – Thursday, 25 June 0700–1730 hrs Friday, 26 June 0700–1200 hrs Wi-Fi Internet Access On Site AIAA is providing limited Wi-Fi service for attendees to use while on site. To keep this service available and optimized for all attendees, please do not download files larger than 2MB, create multiple sessions across multiple devices, or download multiple files in one session. If you receive an error message that an AIAA server is blocking your current IP address, please inform the AIAA registration desk. Social Media Kiosks Throughout the forum, social media kiosks will display content shared by forum attendees! Look for your tweets or instagrams to be displayed on the screens. AIAA is also hosting a competition where the user who has posted the most tweets during the forum will win a prize. Proceedings: 1. To view proceedings visit www.aiaa.org >ARC>Meeting Papers. a. Log in with the link at the top right of the page. b. Select the appropriate conference from the list. c. S earch for individual papers with the Quick Search toolbar in the upper-right corner of the page: i. By paper number: Click the “Paper Number” link, select the conference year, and enter the paper number. ii. Use the Search textbox to find papers by author, title, or keyword. The Advanced Search link provides additional search information and options. 2. All manuscript files submitted at least four days prior to the conference are currently in the proceedings. Files submitted after that date, both original and revised manuscripts, will not be available until the final proceedings update, which may take up to 15 business days after the last day of the conference. 3. Direct any questions concerning access to proceedings and/ or ARC to arcsupport@aiaa.org. 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 General Information Intro Certificate of Attendance Certificates of Attendance are available for attendees who request documentation at the forum itself. The Certificates of Attendance will be available for attendees to print at a selfservice station at the registration desk starting Wednesday, 24 June. AIAA offers this service to better serve the needs of the professional community. Claims of hours or applicability toward professional education requirements are the responsibility of the participant. Employment Opportunities 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 postings in the Exposition Hall. Membership AIAA is your vital lifelong link to the collective creativity and brainpower of the aerospace profession and a champion for its achievements – and nonmembers who pay the full conference registration fee will receive their first year’s AIAA membership at no additional cost! Students who are not yet members may apply their registration fee toward their first year’s student member dues. (Free membership is not included in discounted group-rate registration.) AIAA Foundation Since 1996 the AIAA Foundation has provided programs and support for educators and students. Through classroom grants, scholarships, awards, design competitions, and student conferences, the AIAA Foundation has encouraged students in grades K-12 and at the university level to discover the aerospace industry and become the next generation of scientists and engineers. Please consider making a donation so that the Foundation can continue to provide the resources needed to support aerospace education and to recognize innovation at all levels. For more information and to donate online, please visit www.aiaafoundation.org. www.aiaa-aviation.org Young Professional Guide for Gaining Management Support Young professionals have the unique opportunity to meet and learn from some of the most important people in the business by attending conferences and participating in AIAA activities. A detailed online guide, published by the AIAA Young Professional Committee, is available to help you gain support and financial backing from your company. The guide explains the benefits of participation, offers recommendations, and provides an example letter for seeking management support and funding, and shows you how to get the most out of your participation. The online guide can be found on the AIAA website at www.aiaa.org/YPGuide. Nondiscriminatory Practices AIAA accepts registrations irrespective of race, creed, gender, color, sexual orientation, physical handicap, and national or ethnic origin. Restrictions Photos, video, or audio recording of sessions or exhibits, as well as the unauthorized sale of AIAA-copyrighted material, is prohibited. International Traffic in Arms Regulations (ITAR) AIAA speakers and attendees are reminded that some topics discussed in the conference could be controlled by the International Traffic in Arms Regulations (ITAR). U.S. nationals (U.S. citizens and permanent residents) are responsible for ensuring that technical data they present in open sessions to non-U.S. nationals in attendance or in conference proceedings are not export restricted by the ITAR. U.S. nationals are likewise responsible for ensuring that they do not discuss ITAR export-restricted information with non-U.S. nationals in attendance. 28#aiaaAviation General Information Intro Author and Session Chair Information Speakers’ Briefings in Session Rooms Audiovisual Authors who are presenting papers will meet with session chairs and co-chairs in their session rooms for a short 30-minute briefing on the day of their sessions to exchange bios and review final details prior to the session. Please attend on the day of your session(s). Laptops preloaded with the Speaker Briefing preparation slides will be provided in each session room. Speaker’s Briefing schedule is as follows: Each session room will be preset with the following: one LCD projector, one screen, one microphone and sound system (if necessitated by room size), and one laser pointer. Laptop computers will also be provided. You may also use your own computer. Any additional audiovisual equipment requested onsite will be at cost to the presenter. Please note that AIAA does not provide security in the session rooms and recommends that items of value not be left unattended Monday 22 June–Friday 26 June, 0730 hrs Speakers’ Practice Room Speakers who wish to practice their presentations may do so in the Peridot room. A sign-up sheet will be posted on the door. In consideration of others, please limit practice time to 30-minute increments. Session Chair Reports All session chairs are asked to complete a session chair report to evaluate their session for future planning. AIAA has partnered with Canvas Solutions to provide an electronic Session Chair Report form. You can download the FREE mobile app in your App Store, AppWorld, or Marketplace by searching for “Canvas Solutions, Inc.” The mobile app is free, so please be sure to download it. Detailed instructions will be provided in the session rooms. If you do not have a tablet or a smartphone, simply use the report form as a guide and enter your session chair report information at the session chair reporting computer station located on site near the AIAA registration area. Report data will be collected and used for future planning purposes, including session topics and room allocations. Please submit your session chair report electronically by Friday, 26 June 2015. “No Paper, No Podium” and “No Podium, No Paper” Policy If a written paper is not submitted by the final manuscript deadline, authors will not be permitted to present the paper at the forum. Also, if the paper is not presented at the forum, it will be withdrawn from the proceedings. It is the responsibility of those authors whose papers or presentations are accepted to ensure that a representative attends the conference to present the paper. These policies are intended to improve the quality of the program for attendees.. Journal Publication Authors of appropriate papers are encouraged to submit them for possible publication in one of the Institute’s archival journals: AIAA Journal; Journal of Aircraft; Journal of Guidance, Control, and Dynamics; Journal of Propulsion and Power; Journal of Spacecraft and Rockets; Journal of Thermophysics and Heat Transfer; or Journal of Aerospace Information Systems (formerly Journal of Aerospace Computing, Information, and Communication). You may now submit your paper online at http://mc.manuscriptcentral.com/aiaa. 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 custserv@aiaa.org www.aiaa.org www.aiaa-aviation.org 29#aiaaAviation Intro Committee 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 Coordination Cardinal A & B 1500-1600 FDTC Reduced Order Modeling DG Dardanelles 1600-1700 TPTC New Member Meeting Cooper 1600-1700 FDTC Flow Control - Barriers/Challenges to Tech Trans Cardinal A 1630-1800 Atmospheric and Space Environments TC Batik A 1700-1900 Computational Fluid Dynamics Committee on Standards Batik B 1730-1830 GTTC Committee on Standards Cardinal A 1730-1830 APATC Low Boom DG Cooper 1730-1900 APATC Validation of Numerical Models DG Dardanelles 1830-1930 AMTTC Awards Subcommittee Batik A 1830-2030 APATC Rotorcraft Simulations and Performance Predictions DG Cardinal B www.aiaa-aviation.org 30#aiaaAviation Intro Committee Meetings 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 Intro Committee 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 www.aiaa-aviation.org 32#aiaaAviation Sessions at a Glance Intro Abbreviation Title 3-AA-1 Airframe Noise I Date Start Time Location 22-Jun 0900 hrs Fleur-de-lis A Aeroacoustics 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 www.aiaa-aviation.org 33#aiaaAviation Sessions at a Glance Intro 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 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 10-AMT-1/GT-1 Hap Arnold's New Horizon: The Future Role of Ground Test in High Speed System Development 22-Jun 0900 hrs Obelisk B 11-AMT-2/GT-2 Line of Sight and Density Measurement 22-Jun 0900 hrs Edelweiss Atmospheric Flight Mechanics Aerodynamic Measurement Technology and Ground Testing 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 121-AMT-8/FD-14/ Molecular-Based Optical Diagnostics for Hypersonic Nonequilibrium Flows TP-6/GT-8 158-AMT-9/GT-9 Ground Test Facility Improvements I 23-Jun 1400 hrs Obelisk B 23-Jun 1400 hrs Topaz 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 294-AMT-14/GT-15 Aerodynamic Measurement Systems: Calibration and Monitoring 25-Jun 1400 hrs Obelisk B 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 www.aiaa-aviation.org 34#aiaaAviation Sessions at a Glance Intro Abbreviation Title Date Start Time Location Applied Aerodynamics (continued) 49-APA-7 Special Session: Aerodynamic-Structural Modeling, Optimization, and Test Techniques for Flexible Wing Technology I 22-Jun 1400 hrs Stemmons A 50-APA-8 Flow Control Applications & Demonstrations (Active & Passive) I 22-Jun 1400 hrs Stemmons C 87-APA-9 High Angle of Attack and High Lift Aerodynamics 23-Jun 0900 hrs Stemmons C 88-APA-10 Wind Tunnel and Flight Testing 23-Jun 0900 hrs Carpenter Ballroom 89-APA-11 Special Session: Low Boom Activities II 23-Jun 0900 hrs Stemmons A 90-APA-12 Weapons Aerodynamics: Missile/Projectile/Guided-Munitions, Carriage and Store Separation I 23-Jun 0900 hrs Stemmons B 122-APA-13 Applied CFD & Numerical Correlations with Experimental Data II 23-Jun 1400 hrs Stemmons B 123-APA-14 Special Session: Historically Significant/Influential Papers in Applied Aerodynamics 23-Jun 1400 hrs Carpenter Ballroom 124-APA-15 Special Session: Aerodynamic-Structural Modeling, Optimization, and Test Techniques for Flexible Wing Technology II 23-Jun 1400 hrs Stemmons A 125-APA-16 Flow Control Applications & Demonstrations (Active & Passive) II 23-Jun 1400 hrs Stemmons C 160-APA-17 Special Session: Hybrid CFD Method Assessments for F-16XL Aircraft Aerodynamics 24-Jun 0900 hrs Stemmons A 161-APA-18 Aerodynamic Design Methodologies II 24-Jun 0900 hrs Carpenter Ballroom 162-APA-19 Propeller/Rotorcraft/Wind Turbine Aerodynamics II 24-Jun 0900 hrs Stemmons B 24-Jun 0900 hrs Stemmons C 180-PDL-8/APA-20 Plasma Aerodynamics & Flow Control IV 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 www.aiaa-aviation.org 35#aiaaAviation Intro at a Glance Sessions 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 Autonomy 22-Jun 1400 hrs Metropolitan Ballroom 91-ATIO-9 Terminal & Surface Operations III 23-Jun 0900 hrs Manchester 92-ATIO-10 ATM I - Trajectory Enhancements 23-Jun 0900 hrs Milan 93-ATIO-11 Transformational Flight - On-Demand Mobility 23-Jun 0900 hrs Metropolitan Ballroom 126-ATIO-12 ATM II - Air Traffic Analysis 23-Jun 1400 hrs Milan 127-ATIO-13 Transformational Flight - Advanced Concepts 23-Jun 1400 hrs Metropolitan Ballroom 128-ATIO-14 Product Design and Support 23-Jun 1400 hrs Manchester 164-ATIO-15 ATM III - Modeling in ATM 24-Jun 0900 hrs Metropolitan Ballroom 165-ATIO-16 Transformational Flight - Autonomy I 24-Jun 0900 hrs Monet Ballroom 166-ATIO-17 Human Factors in Aviation Operations 24-Jun 0900 hrs Milan 197-ATIO-18 ATM IV - Economic/Benefits Analysis 24-Jun 1400 hrs Ming 198-ATIO-19 Terminal & Surface Operations IV 24-Jun 1400 hrs Milan 199-ATIO-20 Transformational Flight - Autonomy II 24-Jun 1400 hrs Monet Ballroom 238-ATIO-21 En Route Operations 25-Jun 0900 hrs Milan 239-ATIO-22 ATM V - Performance Assessment 25-Jun 0900 hrs Morocco 240-ATIO-23 Transformational Flight - Electric Propulsion 25-Jun 0900 hrs Monet Ballroom 274-ATIO-24 UAS Integration & Operations I 25-Jun 1400 hrs Ming 275-ATIO-25 ATM VI - Management of NAS Resources 25-Jun 1400 hrs Morocco 276-ATIO-26 Transformational Flight - Unconventional VTOL Configurations 25-Jun 1400 hrs Monet Ballroom 298-ATIO-27 ATM VII - Weather Impact 26-Jun 0900 hrs Morocco 299-ATIO-28 Future Concepts 26-Jun 0900 hrs Wyeth 300-ATIO-29 UAS Integration & Operations II 26-Jun 0900 hrs Ming Balloon 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 59-F360-2/CASE-2 Whatever Happened to the Four-Year Airplane? 72-CASE-3 CASE Networking Social 22-Jun 0900 hrs Batik 22-Jun 1400 hrs Grand Ballroom E 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 207-F360-7/CASE-7 System Complexity : Government Needs and Practical Research Results www.aiaa-aviation.org 24-Jun 0900 hrs Grand Ballroom D 24-Jun 1400 hrs Grand Ballroom D 36#aiaaAviation Intro at a Glance Sessions 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 www.aiaa-aviation.org 37#aiaaAviation Sessions at a Glance Intro 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 121-AMT-8/FD-14/ Molecular-Based Optical Diagnostics for Hypersonic Nonequilibrium Flows TP-6/GT-8 136-FD-15 Unsteady Wing Aerodynamics II 23-Jun 0900 hrs Topaz 23-Jun 1400 hrs Topaz 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 www.aiaa-aviation.org 38#aiaaAviation Sessions at a Glance Intro 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 25-Jun 1400 hrs Metropolitan Ballroom Green Engineering 281-GEPC-1 Overview of NASA Advanced Air Vehicles Program 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 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 Lighter-Than-Air Systems 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 NAS) Test Bed Development (Invited) 1400 hrs Travertine 177-MST-7 Flight Simulation 0900 hrs Travertine 24-Jun 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 Sessions at a Glance Intro 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 121-AMT-8/FD-14/ Molecular-Based Optical Diagnostics for Hypersonic Nonequilibrium Flows TP-6/GT-8 145-TP-7 Heat Transfer II 23-Jun 0900 hrs Rosetta 23-Jun 1400 hrs Topaz 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 41 Kingdom F. da Silva, C. Deschamps, A. da Silva, Federal University of Santa Catarina, Florianópolis, Brazil; L. Simões, Embraer, São José dos Campos, Brazil Moissy-Cramayel, France; C. Bailly, École Centrale de Lyon, Ecully, France Chaired by: P. MORRIS, Pennsylvania State University 0900 hrs 0930 hrs AIAA-2015-2207 AIAA-2015-2208 Assessment of Jet-plate Interaction Installation noise of a turbofan jet Noise Using the Lattice Boltzmann engine under an airfoil G. Brichet, M. Koenig, Safran Group, Method Monday, 22 June 2015 4-AA-2 T. Chong, S. Siddiqi, Brunel University, Uxbridge, United Kingdom Chaired by: D. LOCKARD, NASA-Langley Research Center 0900 hrs 0930 hrs AIAA-2015-2200 AIAA-2015-2201 Aeroacoustic and Aerodynamic Aerodynamic and Aeroacoustic Performances of an Aerofoil Performance of Serrated Airfoils X. Liu, M. Azarpeyvand, R. Theunissen, Subjected to Sinusoidal Leading University of Bristol, Bristol, United Edges Monday, 22 June 2015 3-AA-1 R. Gojon, C. Bogey, O. Marsden, École Centrale de Lyon, Ecully, France 1000 hrs AIAA-2015-2209 Large-eddy simulation of supersonic planar jets impinging on a flat plate at an angle of 60 to 90 degrees C. Paruchuri, N. Subramanian, P. Joseph, C. Vanderwel, J. Kim, B. Ganapathisubramani, University of Southampton, Southampton, United Kingdom 1000 hrs AIAA-2015-2202 Broadband noise reduction through leading edge serrations on realistic aerofoils Opening Keynote Monday, 22 June 2015 2-PLNRY-1 0800 - 0900 hrs 1100 hrs AIAA-2015-2204 Noise generation by turbulence interacting with an aerofoil with a serrated leading edge R. Gojon, C. Bogey, O. Marsden, École Centrale de Lyon, Ecully, France 1030 hrs AIAA-2015-2210 Large-eddy simulation of underexpanded round jets impinging on a flat plate 4 to 9 radii downstream from the nozzle Jet Noise Prediction I C. Brehm, J. Housman, C. Kiris, NASA Ames Research Center, Moffett Field, CA; F. Hutcheson, NASA Langley Research Center, Hampton, VA 1100 hrs AIAA-2015-2211 Noise Characteristics of a Four-Jet Impingement Device Inside a Broadband Engine Noise Simulator L. de Santana, Catholic University of Leuven, Leuven, Belgium; C. Schram, J. Mathews, N. Peake, University of von Kármán Institute for Fluid Dynamics, Cambridge, Cambridge, United Kingdom Rhode-Saint-Genèse, Belgium; W. Desmet, Catholic University of Leuven, Leuven, Belgium 1030 hrs AIAA-2015-2203 Airfoil noise prediction from 2D3C PIV data Airframe Noise I Are We Moving Fast Enough? Tom Enders Chief Executive Officer Airbus Group Speakers’ Briefing Monday, 22 June 2015 1-SB-1 0730 - 0800 hrs Monday N. Hildebrand, J. Nichols, University of Minnesota, Twin Cities, Minneapolis, MN 1130 hrs AIAA-2015-2212 Simulation and stability analysis of a supersonic impinging jet at varying nozzle-to-wall distances T. Padois, P. Laffay, A. Idier, S. Moreau, University of Sherbrooke, Sherbrooke, Canada 1130 hrs AIAA-2015-2205 Detailed experimental investigation of the aeroacoustic field around a Controlled-Diffusion airfoil Y. Yang, Y. Sun, C. Breard, Commercial Aircraft Corporation of China, Ltd. (COMAC), Shanghai, China 1200 hrs AIAA-2015-2213 Hybrid approach for the prediction of jet noise interaction and installation effects Fleur-de-lis B V. Fleury, J. Bulte, R. Davy, E. Manoha, ONERA, Châtillon, France; M. PottPollenske, German Aerospace Center (DLR), Braunschweig, Germany 1200 hrs AIAA-2015-2206 2D high-lift airfoil noise measurements in an aerodynamic wind tunnel Fleur-de-lis A Chantilly Ballroom West Session Rooms 42 T. Hainaut, G. Gabard, V. Clair, University of Southampton, Southampton, United Kingdom Technology (KTH), Stockholm, Sweden W. Watson, M. Jones, NASA Langley Research Center, Hampton, VA Chaired by: W. EVERSMAN, Missouri University of Science and Technology 0930 hrs 0900 hrs AIAA-2015-2228 AIAA-2015-2227 Effect of viscosity on impedance Impedance Eduction in Sound Fields eduction and validation with Peripherally Varying Liners L. Zhou, H. Boden, Royal Institute of and Flow Monday, 22 June 2015 7-AA-5 S. Caro, CD-adapco, Lyon, France 1000 hrs AIAA-2015-2216 The prediction of the radiated pressure spectrum produced by jet-wing interaction 1030 hrs AIAA-2015-2217 Stochastic and nonlinear forcing of wavepackets in a Mach 0.9 jet Jet Noise Modeling I D. Khamis, E. Brambley, University of Cambridge, Cambridge, United Kingdom 1000 hrs AIAA-2015-2229 The Effective Impedance of a Finite-Thickness Viscothermal Boundary Layer Over an Acoustic Lining B. Howerton, M. Jones, NASA Langley Research Center, Hampton, VA 1030 hrs AIAA-2015-2230 Acoustic Liner Drag: A Parametric Study of Conventional Configurations Duct Acoustics I 1030 hrs AIAA-2015-2224 Assessment of Flap Side-Edge Fence Noise using SNGR Method 1130 hrs AIAA-2015-2219 Sensitivity analysis for subsonic jet using adjoint of non local stability equations 1100 hrs AIAA-2015-2225 Verification of a Viscous Computational Aeroacoustics Code using External Verification Analysis 1130 hrs AIAA-2015-2232 Duct spinning mode’s particle velocity imaging on a cross plane outside the duct F. Tao, X. Zhang, P. Joseph, O. Stalnov, W. Yu, Q. Wei, X. Huang, Peking University of Southampton, Southampton, University, Beijing, China United Kingdom; M. Siercke, H. Scheel, Airbus, Hamburg, Germany 1100 hrs AIAA-2015-2231 Experimental Study of the Mechanisms of Sound Generation Due to an In-duct Orifice Plate Y. Sun, Y. Yang, C. Breard, Commercial Aircraft Corporation of China, Ltd. (COMAC), Shanghai, China L. Caldas, L. Baccala, R. Cuenca, University of São Paulo, São Paulo, Brazil; R. Queiroz, Embraer, São José dos Campos, Brazil Obelisk A Lalique 1200 hrs AIAA-2015-2233 In-duct Beamforming Noise Source Estimation Mode Detection University of São Paulo Fan Rig 1130 hrs AIAA-2015-2226 Acoustic loads prediction for a commercial transport aircraft under ground and flight conditions (ITA), São José dos Campos, Brazil; M. Toulouse, France Zhang, National Center for Scientific Research (CNRS), Poitiers, France; F. Lajús, A. Cavalieri, Technological Institute of Aeronautics (ITA), São José dos Campos, Brazil; P. Jordan, National Center for Scientific Research (CNRS), Poitiers, France; T. Colonius, California Institute of Technology, Pasadena, CA F. Silvestre, M. Caprecci, A. Cavalieri, Technological Institute of Aeronautics (ITA), São José dos Campos, Brazil; P. Jordan, École Nationale Supérieure des Mines de Saint-Étienne, Poitiers, France Inverness 1200 hrs AIAA-2015-2220 A Control Framework for Wavepackets in Turbulent Jets Using Time-Domain Transfer G. Tissot, Technological Institute of Aeronautics C. Airiau, T. Ansaldi, University of Toulouse, Functions 1100 hrs AIAA-2015-2218 Sensitivity of wavepackets in jets to non-linear effects: the role of the critical layer A. Markesteijn, V. Semiletov, S. Karabasov, H. Yao, L. Davidson, Chalmers University of Queen Mary University of London, London, Technology, Göteborg, Sweden; S. Peng, D. Ingraham, D. Hixon, University of United Kingdom Swedish Defense Research Agency (FOI), Toledo, Toledo, OH Stockholm, Sweden; L. Eriksson, Chalmers University of Technology, Göteborg, Sweden; M. Barbarino, F. Capizzano, Italian Aerospace Research Center (CIRA), Capua, Italy; et al. 1000 hrs AIAA-2015-2223 CABARET GPU Solver for Fast-TurnAround Flow and Noise Calculations CAA Numerical Techniques I A. Towne, T. Colonius, California Institute Y. Korolev, S. Karabasov, V. Toropov, J. Vera, J. Lawrence, R. Self, M. Kingan, of Technology, Pasadena, CA; P. Jordan, Queen Mary University of London, London, University of Southampton, Southampton, National Center for Scientific Research (CNRS), Poitiers, France; A. Cavalieri, United Kingdom United Kingdom Technological Institute of Aeronautics (ITA), São José dos Campos, Brazil; G. Brès, Cascade Technologies, Inc., Palo Alto, CA Chaired by: W. SCHROEDER, RWTH AACHEN, Institute of Aerodynamics 0900 hrs 0930 hrs AIAA-2015-2221 AIAA-2015-2222 Experimental Validation of CAA Study of Airfoil Broadband Aero-Vibro-Acoustic Analysis of Interaction Noise Using Stochastic Production Vehicles (Invited) Turbulent Vorticity Sources Monday, 22 June 2015 6-AA-4 Aeronautics (ITA), São José dos Campos, Brazil; S. Piantanida, National Center for Scientific Research (CNRS), Poitiers, France; A. Cavalieri, Technological Institute of Aeronautics (ITA), São José dos Campos, Brazil; P. Jordan, National Center for Scientific Research (CNRS), Poitiers, France Chaired by: C. BOGEY, Ecole Centrale de Lyon 0900 hrs 0930 hrs AIAA-2015-2214 AIAA-2015-2215 Automatic Optimizer vs Human Real-time modelling of Optimizer for Low-Order Jet Noise wavepackets in turbulent jets K. Sasaki, Technological Institute of Modelling Monday, 22 June 2015 5-AA-3 43 Stanford University, Stanford, CA T. Burtch, National Transportation Safety Board, Washington, DC 1000 hrs AIAA-2015-2236 Extracting Airplane Performance for a Fatal Accident in the Absence of a Flight Data Recorder J. Schmisseur, University of Tennessee, Tullahoma, Tullahoma, TN Institute of Technology, Pasadena, CA G. Liston, Air Force Research Laboratory, Cleveland, OH 1000 hrs Oral Presentation Introduction to the AFRL HighSpeed Experimentation Branch J. Schmisseur, University of Tennessee, Tullahoma, Tullahoma, TN 1100 hrs Panel Discusssion The Future of Ground Test within T&E 1000 hrs AIAA-2015-2248 Optical Measurements of Velocity, Density, and Mass Flux in a Supersonic Wind Tunnel Y. Krishna, S. Sheehe, S. O’Byrne, University of New South Wales, Canberra, Australia 1030 hrs AIAA-2015-2249 A Time-Resolved Temperature Measurement System for FreePiston Shock Tunnels Line of Sight and Density Measurement T. Juliano, Notre Dame University, Notre Dame, IN 1030 hrs Oral Presentation Development of Large-Scale Quiet Tunnels Supporting T&E Hap Arnold’s New Horizon: The Future Role of Ground Test in High Speed System Development J. George, T. Jenkins, C. Hess, J. Trolinger, D. Plemmons, N. Galyen, Aerospace MetroLaser, Inc., Laguna Hills, CA Testing Alliance, Arnold AFB, TN Chaired by: S. O’BYRNE, The University of New South Wales 0930 hrs 0900 hrs AIAA-2015-2247 AIAA-2015-2246 Simultaneous Measurements Analysis of Focused Laser of Density Field and Wavefront Differential Interferometry B. Schmidt, J. Shepherd, California Distortions in High Speed Jet Flows Monday, 22 June 2015 11-AMT-2/GT-2 M. Lewis, IDA, Washington, DC Chaired by: J. SCHMISSEUR and G. LISTON 0900 hrs 0930 hrs Oral Presentation Oral Presentation Envisioning the Future of the T&E Challenges and Opportunities in the Enterprise Development of T&E Capabilities Monday, 22 June 2015 10-AMT-1/GT-1 A. Mangalam, Tao of Systems Integration, T. Buttini, F. Moreira, Embraer, São José Oxford, OH Inc., Hampton, VA dos Campos, Brazil; F. Silvestre, R. A. da Silva, Technological Institute of Aeronautics (ITA), São José dos Campos, Brazil 1100 hrs AIAA-2015-2243 Adaptive Feedforward Control Design for Gust Loads Alleviation of Highly Flexible Aircraft F. Nicolosi, A. De Marco, V. Sabetta, P. Della Vecchia, University of Naples “Federico II”, Naples, Italy Plum Blossom B Edelweiss Obelisk B 1200 hrs AIAA-2015-2245 Feedback Linearization based Control of Aeroelastic Systems represented in Modal Coordinates Plum Blossom A K. Hashemi, University of Texas, Austin, Austin, TX; C. Pak, NASA Armstrong Flight H. Shukla, M. Patil, Virginia Polytechnic Research Center, Edwards, CA; M. Akella, Institute and State University, Blacksburg, University of Texas, Austin, Austin, TX VA 1130 hrs AIAA-2015-2244 Delta Adaptive Flexible Motion Control for the X-56A Aircraft 1100 hrs AIAA-2015-2238 Roll performance assessment of a light aircraft: flight tests and flight simulation C. Lupp, C. Cesnik, University of Michigan, Y. Wang, F. Li, China Academy of Ann Arbor, Ann Arbor, MI Aerospace Aerodynamics, Beijing, China; A. Da Ronch, University of Southampton, Southampton, United Kingdom 1030 hrs AIAA-2015-2242 Aeroelastic Tailoring for Maximizing Sailplane Average Cross-Country Speed Aeroservoelastic (ASE) Modeling M. Montel, F. Thielecke, Hamburg University of Technology, Hamburg, Germany 1030 hrs AIAA-2015-2237 Validation of a Model Based Structural Loads Monitoring System using the Flight Test Aircraft UW-9 Sprint Aircraft Flight Dynamics, Control, Handling Qualities and Performance I Chaired by: T. ALEXEEV, University of California Davis and F. PRIOLO, Millennium Engineering and Integration Company 0900 hrs 0930 hrs 1000 hrs AIAA-2015-2239 AIAA-2015-2240 AIAA-2015-2241 Control of a Nonlinear Wing Section Aeroelastic State-space Model Optimal Sizing and Configurations using Fly-by-Feel Sensing Development Based on Frequency of the Control Surfaces for Active V. Suryakumar, Y. Babbar, T. Strganac, Response Identification and Aeroelastic Control Texas A&M University, College Station, TX; Integration with Flight Dynamics R. Brown, K. Singh, Miami University, Monday, 22 June 2015 9-AFM-2 W. Okolo, A. Dogan, University of Texas, Arlington, Arlington, TX; W. Blake, Air Force Research Laboratory, Wright-Patterson AFB, OH Chaired by: E. GILLESPIE, United Space Alliance 0900 hrs 0930 hrs AIAA-2015-2234 AIAA-2015-2235 Automatic Stall/Spin Detection in Benefits of Formation Flight of Extended Duration Considering Fuel Fixed-Wing Aircraft R. Bunge, F. Munera Savino, I. Kroo, Burn Monday, 22 June 2015 8-AFM-1 44 C. Fagley, J. Seidel, T. McLaughlin, U.S. Air Force Academy, Colorado Springs, CO Z. Hasnain, J. Hubbard, University of Maryland, College Park, College Park, MD; A. Wissa, University of Illinois, UrbanaChampaign, Urbana, IL M. Wintzer, Analytical Mechanics Associates, Hampton, VA; M. Wintzer, Analytical Inc., Hampton, VA; I. Ordaz, NASA Langley Mechanics Associates, Inc., Hampton, VA; S. Rallabhandi, National Institute of Research Center, Hampton, VA Aerospace, Hampton, VA Hampton, VA D. Franke, German Aerospace Center (DLR), Braunschweig, Germany 1100 hrs AIAA-2015-2258 Investigation on continuously deflectable High-Lift Devices for a 3D High-Lift Configuration 1100 hrs AIAA-2015-2263 Cart3D Analysis of Plume and Shock Interaction Effects on Sonic Boom J. Housman, C. Kiris, NASA Ames Research R. Castner, NASA Glenn Research Center, Center, Moffett Field, CA Cleveland, OH 1030 hrs AIAA-2015-2262 Numerical Simulations of Shock/ Plume Interaction Using Structured Overset Grids Special Session: Low Boom Activities I A. Krumme, German Aerospace Center (DLR), Göttingen, Germany; S. Hegen, German-Dutch Wind Tunnels, Marknesse, The Netherlands; R. Nahuis, National Aerospace Laboratory (NLR), Marknesse, The Netherlands Chaired by: K. WAITHE, Gulfstream Aerospace Corporation and L. BANGERT, NASA Langley Research Center 0930 hrs 1000 hrs 0900 hrs AIAA-2015-2261 Oral Presentation AIAA-2015-2260 Under-Track CFD-Based Shape Full-Carpet Design of a Low-Boom Sonic Boom Variation of a WingOptimization for a Low-Boom Demonstrator Concept Body-Tail-Nacelle Configuration I. Ordaz, NASA Langley Research Center, M. Park, NASA Langley Research Center, Demonstrator Concept Monday, 22 June 2015 14-APA-3 Aerodynamic Design Methodologies I Technology, Daejeon, South Korea; R. Prasad, S. Choi, D. Im, Virginia Polytechnic Institute and State University, Blacksburg, VA; D. Lee, Korea Advanced Institute of Science and Technology, Daejeon, South Korea 1030 hrs AIAA-2015-2253 Analyzing the Pitch Agility of an Ornithopter Undergoing Passive Compliant Element Induced Shape S. Yi, Korea Advanced Institute of Science and Change 1000 hrs AIAA-2015-2252 Spectral Formulation-Based FSI and Coupled Sensitivity Analysis for Dyanmic Aeroelastic Problems Aerodynamic-Structure Dynamics Interaction Chaired by: K. KARA, Khalifa University of Science, Technology & Research and J. MURRAY, Sandia National Laboratories 0900 hrs 0930 hrs 1000 hrs 1030 hrs AIAA-2015-2254 AIAA-2015-2255 AIAA-2015-2256 AIAA-2015-2257 Development of NOVA Aircraft Aircraft directional stability Design of a Multi-Stage Axial Turbine Fuselage Aerodynamic Prediction Configurations for Large Engine prediction method by CFD within the scope of complete System Methods P. Della Vecchia, F. Nicolosi, D. Ciliberti, Integration Studies Design, Manufacturing and Operation F. Nicolosi, P. Della Vecchia, D. Ciliberti, V. 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 Italy “Federico II”, Naples, Italy D. Hue, ONERA, Meudon, France (TPS) Monday, 22 June 2015 13-APA-2 K. Boo, S. Mansor, A. Abdul-Latif, University of Technology, Johor Bahru, Malaysia Chaired by: J. AZEVEDO and C. PASILIAO, AFRL/RWWV 0900 hrs 0930 hrs AIAA-2015-2250 AIAA-2015-2251 Experimental Investigation of the Aerodynamic Damping and Stiffness Determination for Aircraft Aeroelastic Behavior a NACA0018 Cyber-Physical FlexibleWing Wing Flutter Speed Analysis Monday, 22 June 2015 12-APA-1 S. Oliviu, A. Koreanschi, R. Botez, University of Québec, Montréal, Canada 1130 hrs AIAA-2015-2259 Numerical study of UAS-S4 Éhecatl aerodynamic performance improvement obtained with the use of a morphing wing approach Stemmons A Carpenter Ballroom Stemmons C 45 University of Illinois, Urbana-Champaign, Urbana, IL K. Swieringa, NASA Langley Research Center, Hampton, VA Chaired by: H. ARNESON 0900 hrs AIAA-2015-2278 The String Stability of a TrajectoryBased Interval Management Algorithm in the Midterm Airspace Monday, 22 June 2015 18-ATIO-3 1000 hrs AIAA-2015-2280 Branch & Bound-Based Algorithm for Aircraft VNAV Profile Reference Trajectory Optimization H. Tang, NASA Ames Research Center, Moffett Field, CA 1000 hrs AIAA-2015-2277 Conflict Alerts for Aircraft Conducting Visual Approaches H. Lee, W. Malik, University of California, Santa Cruz, Moffett Field, CA; B. Zhang, B. Nagarajan, American Airlines, Fort Worth, TX; Y. Jung, NASA Ames Research Center, Moffett Field, CA 1000 hrs AIAA-2015-2272 Taxi Time Prediction at Charlotte Airport Using Fast-Time Simulation and Machine Learning Techniques H. Ng, University of California, Santa Cruz, A. Murrieta Mendoza, B. Beuze, L. Moffett Field, CA; B. Sridhar, NASA Ames Ternisien, R. Botez, University of Québec, Research Center, Moffett Field, CA Montréal, Canada 0930 hrs AIAA-2015-2279 Computational Approaches to Simulation and Optimization of Global Aircraft Trajectories N. Guerreiro, J. Maddalon, T. Lewis, G. Hagen, A. Sadovsky, M. Jastrzebski, NASA Ames NASA Langley Research Center, Hampton, VA Research Center, Moffett Field, CA Chaired by: M. WILCOXEN, U.S. Air Force 0930 hrs 0900 hrs AIAA-2015-2276 AIAA-2015-2275 Strategic time-based metering that Conflict Detection Performance Analysis for Function Allocation Using assures separation for integrated Time-Shifted Recorded Traffic Data operations in a terminal airspace Monday, 22 June 2015 17-ATIO-2 A. Saraf, V. Felipe, Saab Sensis Corporation, Campbell, CA; B. Sawhill, NextGen Aerosciences LLC, Williamsburg, VA Chaired by: S. CAMPBELL, MIT Lincoln Laboratory 0900 hrs 0930 hrs AIAA-2015-2270 AIAA-2015-2271 A Robust and Practical Decision Identification of Local and Support Tool for Integrated Propagated Queuing Effects at Arrival-Departure-Surface Traffic Major Airports H. Idris, Engility Corporation, Billerica, MA Management Monday, 22 June 2015 16-ATIO-1 Air Force Academy, Colorado Springs, CO; K. Van Treuren, T. Liller, Baylor University, Waco, TX; N. Wisniewski, Rose Hulman Institute of Technology, Terre Haute, IN 1100 hrs AIAA-2015-2268 A Parabolic Method for Accurate and Efficient Wind Farm Simulation 1130 hrs AIAA-2015-2269 Blade Resolved Simulation for a Wind Farm R. Félix Patrón, M. Schindler, R. Botez, University of Québec, Montréal, Canada Trajectory Optimization 1030 hrs AIAA-2015-2281 Aircraft Trajectories Optimization By Genetic Algorithms To Reduce Flight Cost Using A Dynamic Weather Model Separation Assurance M. Xue, University of California, Santa Cruz, Moffett Field, CA; S. Zelinski, NASA Ames Research Center, Moffett Field, CA 1030 hrs AIAA-2015-2273 A Stochastic Scheduler for Integrated Arrival, Departure, and Surface Operations in Los Angeles Terminal & Surface Operations I A. Liv, R. Dancila, R. Botez, University of Québec, Montréal, Canada 1100 hrs AIAA-2015-2282 Trajectory optimization algorithm for a constant altitude cruise flight with a required time of arrival constraint C. Bosson, D. Sun, Purdue University, West Lafayette, IN 1100 hrs AIAA-2015-2274 Optimization of Airport Surface Operations Under Uncertainty A. Mittal, K. Sreenivas, W. Briley, L. Taylor, W. Hassan, K. Sreenivas, A. Mittal, L. Taylor, L. Hereth, University of Tennessee, C. Wisniewski, A. Byerley, W. Heiser, U.S. University of Tennessee, Chattanooga, Chattanooga, Chattanooga, TN C. Wisniewski, A. Byerley, W. Heiser, U.S. Air Force Academy, Colorado Springs, CO; Chattanooga, TN Air Force Academy, Colorado Springs, CO; K. Van Treuren, T. Liller, Baylor University, K. Van Treuren, T. Liller, Baylor University, Waco, TX Waco, TX 1030 hrs AIAA-2015-2267 Designing Small Propellers for Optimum Efficiency and Low Noise Footprint Propeller/Rotorcraft/Wind Turbine Aerodynamics I Chaired by: M. CALVERT, U.S. Army AMRDEC and D. O’BRIEN, US Army RDECOM 0900 hrs 0930 hrs 1000 hrs AIAA-2015-2264 AIAA-2015-2265 AIAA-2015-2266 Slipstream Measurements of Small- The Influence of Airfoil Shape, Experimental Evaluation of Open Propeller Aerodynamic Performance Scale Propellers at Low Reynolds Reynolds Number and Chord Numbers Length on Small Propeller and Aero-acoustic Behavior C. Wisniewski, A. Byerley, W. Heiser, U.S. R. Deters, G. Ananda Krishnan, M. Selig, Performance and Noise Monday, 22 June 2015 15-APA-4 Milan Ming Manchester Stemmons B 46 Mark Page Dzyne Technologies Academic Roundtable JoeBen Bevirt Joby Aviation Transformational Flight - Rapid Concept to Flight Starr Ginn NASA Armstrong Research Center Batik Metropolitan Ballroom A. Jalali, C. Ollivier Gooch, University of British Columbia, Vancouver, Canada K. Bhamidipati, D. Reasor, 412th Test Wing, Edwards AFB, CA; C. Pasiliao, Air Force Research Laboratory, Eglin AFB, FL Kingdom Chaired by: Y. WANG and D. REASOR, Air Force Research Laboratory 0930 hrs 0900 hrs AIAA-2015-2288 AIAA-2015-2287 Unsteady Simulations of Shockwave- Effect of Cavity Flow on Landing Boundary Layer Interaction Induced Gear Aerodynamic Loads Transonic Shockwave Oscillations using U. Oza, Z. Hu, X. Zhang, University of Southampton, Southampton, United Unstructured Grids Monday, 22 June 2015 22-CFD-2 Logan, UT; J. Sitaraman, U.S. Army, Moffett Field, CA Chaired by: S. MURMAN, NASA Ames Research Center and A. KATZ 0900 hrs 0930 hrs AIAA-2015-2283 AIAA-2015-2284 High-Order Strand Grid Methods Higher-order Unstructured Finite for Shock Turbulence Interaction Volume Methods for Turbulent O. Tong, A. Katz, Utah State University, Aerodynamic Flows Monday, 22 June 2015 21-CFD-1 1030 hrs AIAA-2015-2290 Symmetrical and non-symmetrical 3D wing deformation of flapping micro aerial vehicles Unsteady Flow Simulations J. Pan, Y. Ren, Tsinghua University, Beijing, China 1030 hrs AIAA-2015-2286 High order subcell finite volume method in solving hyperbolic conservation laws R. Ritz, T. Schomberg, O. Wünsch, W. Tay, National university of Singapore, University of Kassel, Kassel, Germany; M. Singapore, Singapore Ruetten, R. Kessler, German Aerospace Center (DLR), Göttingen, Germany 1000 hrs AIAA-2015-2289 Numerical Investigation of the Detaching Vortical Flow at Rotating Cylinders with Thom Discs S. Murman, L. Diosady, NASA Ames Research Center, Moffett Field, CA 1000 hrs AIAA-2015-2285 A Spectral-Element Approach for the Eikonal Equation Y. Wang, Z. Hu, Z. Jiang, Chinese Academy of Sciences, Beijing, China 1100 hrs AIAA-2015-2291 Numerical Investigation of the Starting Process in a Long-testduration Hypervelocity Shock Tunnel Unstructured High-Order Methods I Grand Ballroom B Grand Ballroom A 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: Shannon Flumerfelt, Ph.D. Anabela Alves, Ph.D. Franz-Josef Kahlen, Ph.D. Associate Professor, Educational Leadership, Director of Lean Thinking for Schools, Assistant Professor, Departamento de Produção e Sistemas Escola de Engenharia da Universidade Associate Professor, Department of Mechanical Engineering 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 20-CASE-1 0900 - 1200 hrs Neal Willford Textron Aviation Moderator: William Fredericks, NASA Langley Research Center Panelists: Monday, 22 June 2015 19-ATIO-4 0900 - 1100 hrs 47 LES, DNS, and Hybrid RANS-LES I 1030 hrs AIAA-2015-2300 Resolved Scalar Mixing in Large Eddy Simulations of a Low Reynolds Number Plane Mixing Layer Chaired by: A. SESCU, Mississippi State University and W. MCMULLAN, University of Leicester 0900 hrs 0930 hrs 1000 hrs AIAA-2015-2297 AIAA-2015-2298 AIAA-2015-2299 High Order Numerical Methods for Large Eddy Simulation of Resolved Scalar Mixing in Large the Dynamic SGS Model of Turbulent Supersonic Impinging Jets by Eddy Simulations of a Low Flows with Shocks Adaptive, Explicit Filtering Reynolds Number Plane Mixing D. Kotov, Bay Area Environmental Research S. Patel, J. Mathew, Indian Institute of Layer Peking University, Beijing, China J. Zhu, S. Zou, L. Liu, J. Wu, Peking University, Beijing, China; T. Liu, Western Michigan University, Kalamazoo, MI Chaired by: D. YOUNG, Raytheon Missile Systems and U. KAUL, NASA ARC 0930 hrs 0900 hrs AIAA-2015-2303 AIAA-2015-2302 The Origin of Lift Revisited: I. A The Origin of Lift Revisited: II. Complete Physical Theory Physical Processes of AirfoilT. Liu, Western Michigan University, Circulation Formation in Starting Kalamazoo, MI; J. Wu, J. Zhu, L. Liu, Flow Monday, 22 June 2015 25-FD-1 Institute, Petaluma, CA; H. Yee, A. Wray, Science, Bangalore, India NASA Ames Research Center, Moffett Field, CA; B. Sjogreen, Lawrence Livermore National Laboratory, Livermore, CA R. Hajian, J. Jaworski, Lehigh University, Bethlehem, PA 1000 hrs AIAA-2015-2304 The Steady Aerodynamics of Quiet Airfoils with Porosity Gradients J. Haywood, A. Sescu, Mississippi State University, Mississippi State, MS 1100 hrs AIAA-2015-2306 Lift and Drag in Two-Dimensional Steady Viscous and Compressible Flow: II. Fundamental Solution Theory J. Li, Nanjing University of Aeronautics and Astronautics, Nanjing, China; G. Page, J. McGuirk, Loughborough University, Loughborough, United Kingdom 1130 hrs AIAA-2015-2307 Effects of Perturbation on the Flow over Nonslender Delta Wings Govenors Lecture Hall Emerald 1200 hrs AIAA-2015-2308 Interaction of Multiple Vortices over a Double Delta Wing Coral C. Canpolat, B. Sahin, Cukurova University, X. Zhang, Z. Wang, I. Gursul, University of Adana, Turkey; S. Yayla, Yuzuncu Yil Bath, Bath, United Kingdom J. Zhu, L. Liu, Peking University, Beijing, L. Liu, J. Wu, Peking University, Beijing, University, Van, Turkey; H. Akilli, Cukurova China; T. Liu, Western Michigan University, China; T. Liu, Western Michigan University, University, Adana, Turkey Kalamazoo, MI; Y. Shi, W. Su, J. Wu, Kalamazoo, MI Peking University, Beijing, China 1030 hrs AIAA-2015-2305 Lift and Drag in Two-Dimensional Steady Viscous and Compressible Flow: I. Far-Field Formulae Analysis and Numerical Confirmation Wing Aerodynamics S. Hug, W. McMullan, University of Leicester, Leicester, United Kingdom 1100 hrs AIAA-2015-2301 LES Simulation Inflow conditions for Outlet Guide Vane and Prediffuser Flows 1100 hrs AIAA-2015-2296 Construction of Prism and Hex Layers from Anisotropic Tetrahedra J. Steinbrenner, Pointwise, Inc., Fort University of British Columbia, Vancouver, H. Koizumi, S. Tsutsumi, R. Takaki, Japan Worth, TX Canada Aerospace Exploration Agency (JAXA), Sagamihara, Japan; K. Yamamoto, Japan Aerospace Exploration Agency (JAXA), Mitaka, Japan; H. Ito, M. Abe, Ryoyu Systems, Nagoya, Japan; et al. Monday, 22 June 2015 24-CFD-4 M. Park, NASA Langley Research Center, J. Ims, Z. Duan, Z. Wang, University of Hampton, VA; A. Loseille, French National Kansas, Lawrence, Lawrence, KS Institute for Research in Computer Science and Control (INRIA), Le Chesnay, France; J. Krakos, T. Michal, The Boeing Company, St. Louis, MO 1030 hrs AIAA-2015-2295 Automated Massively Refinement Technique for Multi-block Structured Grids Based on NURBS Volume Meshing Techniques I Chaired by: D. THOMPSON, Mississippi State University and B. JOLLY, US Air Force 0900 hrs 0930 hrs 1000 hrs AIAA-2015-2292 AIAA-2015-2293 AIAA-2015-2294 meshCurve: An Automated Target-Edge Based Orthogonal Comparing Anisotropic OutputAnisotropic Mesh Based Grid Adaptation Methods by Low-Order to High-Order Mesh J. Zuniga Vazquez, C. Ollivier Gooch, Generator Decomposition Monday, 22 June 2015 23-CFD-3 48 Berlin, Berlin, Germany; M. Meinke, W. M. Carmine, R. Cheli, F. Cozzi, A. Schroeder, RWTH Aachen University, Aachen, Spinelli, M. Zocca, A. Guardone, Technical Germany; G. Pechlivanoglou, C. Nayeri, University of Milan, Milan, Italy Technical University of Berlin, Berlin, Germany; et al. F. Kok, R. Myose, Wichita State University, Wichita, KS; S. Hayashibara, Embry-Riddle Aeronautical University, Prescott, AZ Schneider, Purdue University, West Lafayette, IN H. Nawroth, C. Paschereit, Technical University of Berlin, Berlin, Germany 1030 hrs AIAA-2015-2316 Flow Fields of Manipulated Shear Layers of a Turbulent Jet Flame Combustion and Heat Transfer Q. Qu, P. Ma, P. Liu, Beihang University, Beijing, China; S. Li, Beijing Institute of Mechanical and Electrical Engineering, Beijing, China; R. Agarwal, Washington University in St. Louis, St. Louis, MO 1030 hrs AIAA-2015-2312 Numerical Study of the Transient Deformation and Drag Characteristics of a Decelerating Droplet Fundamental Fluid Flows 1000 hrs AIAA-2015-2319 Correlation of HIFiRE-5 Flight Data With Computed Pressure and Heat Transfer A. Ramachandran, B. Saikia, K. Sinha, Indian Institute of Technology Bombay, Mumbai, India; R. Govindarajan, Tata Institute of Fundamental Research, Hyderabad, India 1030 hrs AIAA-2015-2320 Linear stability of high-speed boundary layer flows at varying Prandtl numbers Boundary Layer Transition: Hypersonic Flows N. Cymbalist, P. Dimotakis, California Institute of Technology, Pasadena, CA 1000 hrs AIAA-2015-2315 On autoignition-dominated supersonic combustion J. Jewell, J. Miller, R. Kimmel, Air Force L. Salemi, H. Fasel, University of Arizona, Research Laboratory, Wright-Patterson AFB, OH Tucson, Tucson, AZ Chaired by: J. JEWELL, Air Force Research Laboratory and K. CASPER 0930 hrs 0900 hrs AIAA-2015-2318 AIAA-2015-2317 Numerical Investigation of Nonlinear Instability and Transition Experiments in the Boeing/AFOSR Wave-packets in a Hypersonic HighMach 6 Quiet Tunnel Enthalpy Boundary-Layer on a 5 G. McKiernan, B. Chynoweth, S. deg Sharp Cone Monday, 22 June 2015 28-FD-4 A. Ramachandran, V. Narayanaswamy, North Carolina State University, Raleigh, NC Chaired by: J. CHOI, Georgia Institute of Technology and I. LEYVA 0900 hrs 0930 hrs AIAA-2015-2313 AIAA-2015-2314 An Experimental Study of Global Comparison of Theoretical and SemiCharacteristics of Turbulent Empirical Solutions for Dissipation Diffusion Jet Flames for Fuels of Coefficient in a Low Reynolds Number Complex Chemistry Compressor Cascade Monday, 22 June 2015 27-FD-3 Institute and State University, Blacksburg, VA Chaired by: G. DALE, Air Force Research Laboratory and M. GREEN, Syracuse University 0900 hrs 0930 hrs 1000 hrs AIAA-2015-2309 AIAA-2015-2310 AIAA-2015-2311 Evidence of complex flow structures Evolution of Stratified Boundary- Numerical and Experimental Investigation of Wind Turbine Wakes in a converging-diverging nozzle Free Shear Flows Under StokesX. Huang, RWTH Aachen University, Aachen, caused by a recessed step at the Ekman Forcing Germany; S. Vey, Technical University of M. Jones, E. Paterson, Virginia Polytechnic nozzle throat Monday, 22 June 2015 26-FD-2 Sapphire Topaz Senators Lecture Hall 49 Unmanned Aerial Vehicle Systems L. Hale, M. Patil, C. Roy, Virginia Polytechnic Institute and State University, Blacksburg, VA Chaired by: B. LANDRUM and M. PATIL, Virginia Tech 0900 hrs 0930 hrs AIAA-2015-2328 AIAA-2015-2329 Experimental Characterization of Nondeterministic Simulation for Butterfly in Climbing Flight Probability of Loss of Control J. Cranford, University of Alabama, Prediction for Unmanned Aircraft Huntsville, Huntsville, AL; N. Slegers, Systems Monday, 22 June 2015 32-NW-1 0900 - 0930 hrs Networking Coffee Break A. Uehara, D. Niedermeier, German Aerospace Center (DLR), Braunschweig, Germany 1030 hrs AIAA-2015-2338 Influence of coupled sidesticks on the pilot monitoring’s awareness during flare (NLR), Amsterdam, The Netherlands; L. Fucke, B. Correia Grácio, The Boeing Company, Madrid, Spain; M. Varney, Airbus, Toulouse, France Aviation Systems Human Factors J. Suraj Nandiganahalli, I. Hwang, Purdue California, Davis, Davis, CA University, West Lafayette, IN 1100 hrs AIAA-2015-2332 Optimal Object Location by a Fleet of Various UAVs M. Zhelonkin, Y. Dubov, V. Zhelonkin, O. Tkachenko, TsAGI, Zhukovsky, Russia 1100 hrs Oral Presentation Ergonomic evaluation of different principles of position indication and control plane in field B. Kaddouh, W. Crowther, P. Hollingsworth, A. Kopyt, J. Narkiewicz, T. Malecki, P. University of Manchester, Manchester, Radyisyewski, Warsaw University of United Kingdom Technology, Warsaw, Poland 1030 hrs AIAA-2015-2331 Dynamic Resource Allocation for Sharing Multi-UAV Services Chaired by: D. CARTMELL, Boeing Engineering Operations & Technology and S. ROBINSON, UC Davis 0930 hrs 1000 hrs 0900 hrs AIAA-2015-2336 AIAA-2015-2337 AIAA-2015-2335 Formal Extensions to the IntentThe Rapidly Reconfigurable Flight Crew Response to Unexpected Based Mode Confusion Detection Research Cockpit Events: A Simulator Experiment R. Joyce, S. Robinson, University of J. Field, National Aerospace Laboratory Framework J. Narkiewicz, A. Kopyt, P. Radyisyewski, T. Malecki, Warsaw University of Technology, Warsaw, Poland 1000 hrs AIAA-2015-2330 Optimal selection of UAV for ground target tracking Monday, 22 June 2015 31-MST-2 George Fox University, Newberg, OR; B. Landrum, University of Alabama, Huntsville, Huntsville, AL 1100 hrs AIAA-2015-2325 Hybrid Wing Body (HWB) Aircraft Design and Optimization using Stitched Composites E. Rudnick-Cohen, S. Azarm, J. Herrmann, R. Chhabra, Virginia Polytechnic Institute C. Meckstroth, University of Dayton, V. Li, The Boeing Company, Huntington University of Maryland, College Park, and State University, Blacksburg, VA; S. Dayton, OH; W. Blake, Air Force Research Beach, CA College Park, MD Mulani, University of Alabama, Tuscaloosa, Laboratory, Wright-Patterson AFB, OH Tuscaloosa, AL; R. Kapania, J. Schetz, Virginia Polytechnic Institute and State University, Blacksburg, VA Monday, 22 June 2015 30-MST-1 J. Hwang, J. Martins, University of Michigan, Ann Arbor, Ann Arbor, MI 1030 hrs AIAA-2015-2324 Control Focused Multidisciplinary Design Optimization of Tailless Fighter Aircraft Vehicle Design Applications I Chaired by: R. KOLONAY, Air Force Research Laboratory/RQVC/WPAFB and V. KALIVARAPU, Iowa State University 0900 hrs 0930 hrs 1000 hrs AIAA-2015-2321 AIAA-2015-2322 AIAA-2015-2323 Multi-Objective Design and Control Power Optimization using Parallel allocation-mission Path Planning Optimization of Artificial Intelligence for Hybrid optimization of a 128-route Unmanned Aerial Vehicles (UAVs) Wing Body Aircraft network Monday, 22 June 2015 29-MAO-1 E. Ayyad, W. Culbreth, D. Reynolds, University of Nevada, Las Vegas, Las Vegas, NV 1130 hrs AIAA-2015-2339 Equation-System Representation Model for Pneumatic Seat Design Used for Vibration Isolation In Air and Ground Transport D. Ferreira de Castro, J. Santos, M. Batista, D. Antônio dos Santos, L. Góes, Technological Institute of Aeronautics (ITA), São José dos Campos, Brazil 1130 hrs AIAA-2015-2333 Modeling and Control of Tethered Unmanned Multicopters in Hovering Flight A. Ciarella, C. Tsotskas, M. Hahn, Aircraft Research Association, Ltd., Bedford, United Kingdom; N. Werter, R. De Breuker, Delft University of Technology, Delft, The Netherlands; C. Beaverstock, Swansea University, Swansea, United Kingdom; et al. 1130 hrs AIAA-2015-2326 A Multi-Fidelity, Multi-Disciplinary Analysis and Optimization Framework for the Design of Morphing UAV Wing Meeting Room Foyers Y. Zhang, Y. Sun, L. Liu, Nanjing University of Aeronautics and Astronautics, Yangzhou, China 1200 hrs Oral Presentation An approach to establish case base of motions for layout optimization Wyeth Q. Zeng, J. Liu, Y. Wang, Nanjing University of Aeronautics and Astronautics, Nanjing, China 1200 hrs AIAA-2015-2334 MAV Pose Measurement algorithm Based on Visual Systems Travertine S. Gemma, F. Mastroddi, University of Rome “La Sapienza”, Rome, Italy 1200 hrs AIAA-2015-2327 Multi-Disciplinary and MultiObjective Optimization of an Unconventional Aircraft Concept Madrid 50 Japan; K. Suzuki, University of Tokyo, Kashiwa, Japan Alexeenko, Purdue University, West Lafayette, IN Moderator: Christopher Stonehouse, Senior Vice President, Customer Services, Airbus Americas, Inc. Panelists: Jack Arehart President of MRO Services Delta TechOps Monday, 22 June 2015 36-F360-1 0930 - 1200 hrs of L’Aquila, L’Aquila, Italy; J. Beck, S. K. Hanquist, I. Boyd, University of Nallapaneni, Michigan State University, Michigan, Ann Arbor, Ann Arbor, MI E. Lansing, MI; D. Amos, Sandia National Laboratories, Albuquerque, NM; A. Haji-Sheikh, University of Texas, Arlington, Arlington, TX M. Mantelli, J. Florez Mera, F. Milanese, Federal University of Santa Catarina, Florianópolis, Brazil 1030 hrs AIAA-2015-2353 Thermal Model for Sintered Cylindrical Evaporators of Loop Heat Pipes(2150991) Heat Transfer I William “Bill” Meehan Chief Operating Officer Frontier Airlines, Inc. Bart Roberts Vice President, Flight Technical Operations JetBlue Airways J. Hua, Nanjing University of Aeronautics and Astronautics, Nanjing, China Grand Ballroom E Steuben Rosetta J. Zhao, X. Meng, J. Wang, Northwestern Polytechnical University, Xi’an, China; F. Liu, S. Luo, University of California, Irvine, Los Angeles, CA Monet Ballroom 1200 hrs AIAA-2015-2346 Pressure Investigations over a Conical Forebody under DutyCycled Plasma Actuations 1130 hrs AIAA-2015-2355 Studies on thermal conductivity prediction of fiber reinforced material with microscopic structure identification N. Webb, M. Samimy, Ohio State University, Columbus, OH 1130 hrs AIAA-2015-2345 Shock-Trapping Capability of a Cavity in a Supersonic Flow David Seymour Senior Vice President, Technical Operations American Airlines Y. Zhao, S. Chang, Y. Bo, M. Leng, Beihang University, Beijing, China 1100 hrs AIAA-2015-2354 Study of the Minimum Anti-icing Energy Based on Icing Limit State K. Bayoda, N. Benard, E. Moreau, National Center for Scientific Research (CNRS), Futuroscope, France 1100 hrs AIAA-2015-2344 Single Nanosecond Dielectric Barrier Discharge and Pulsed Sliding Discharge Applied to Separation Control Along a NACA 0015 Airfoil The Voice of the Customer - Designing the Right Aircraft Chaired by: M. KIO, National Space Research & Development Agency and A. WILLIAMS, Air Force Reseach Laboratory 0900 hrs 0930 hrs 1000 hrs AIAA-2015-2350 AIAA-2015-2351 AIAA-2015-2352 Diffusion Penetration Time for Comparisons of Computations Heat and Mass Transfer Analysis of Transient Conduction with Experiments for Electron a Film Evaporative MEMS Tuneable R. McMasters, Virginia Military Institute, Transpiration Cooling at High Array Thruster Lexington, VA; F. de Monte, University W. O’Neill, A. Cofer, A. Weaver, A. Enthalpies Monday, 22 June 2015 35-TP-2 Y. Chen, NASA Ames Research Center, Moffett Field, CA; T. Gokcen, ERC, Inc., Moffett Field, CA Ablation I B. Greene, N. Clemens, University of Texas, Austin, Austin, TX; P. Magari, D. Micka, M. Ueckermann, Creare, Inc., Hannover, NH 1030 hrs AIAA-2015-2343 Effect of Pulsed Plasma Jets on Boundary Layer Recovery Downstream of a Reflected Shock Y. Watanabe, University of Tokyo, Bunkyo, Wave-Boundary Layer Interaction 1000 hrs AIAA-2015-2342 Aerodynamic Control Effect of Surface DC Plasma Discharge at Mach-7 Hypersonic Flow Plasma Aerodynamics & Flow Control I S. Lewis, R. Morgan, T. Mcintyre, University Institute for Fluid Dynamics, Rhode-Saintof Queensland, St. Lucia, Australia; C. Alba, R. Genèse, Belgium Greendyke, Air Force Institute of Technology, Wright-Patterson AFB, OH M. Frankhouser, J. Gregory, Ohio State University, Columbus, OH 0930 hrs AIAA-2015-2341 Nanosecond Dielectric Barrier Discharge Plasma Actuator Flow Control of Compressible Dynamic Stall 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 B. Dias, A. Turchi, T. Magin, von Kármán Carbon Based Ablator Surface Temperatures Monday, 22 June 2015 34-TP-1 I. Popov, G. Correale, S. Hulshoff, Delft University of Technology, Delft, The Netherlands Chaired by: M. STANEK, AFRL/RQVI 0900 hrs AIAA-2015-2340 Numerical Simulations of Disturbances in Shear Flows Introduced by NS-DBD Plasma Actuators Monday, 22 June 2015 33-PDL-1/FD-5 51 C. Ekoule, M. Kingan, A. McAlpine, Southampton University, Southampton, United Kingdom; N. Sohoni, Cambridge University, Cambridge, United Kingdom; A. Parry, RollsRoyce Group plc, Derby, United Kingdom 1430 hrs AIAA-2015-2357 Hybrid Use of CFD and Analytical Methods for the Prediction of Advanced Open Rotor Tone Noise N. Lupoglazoff, F. Vuillot, ONERA, Châtillon, France Chaired by: D. MCLAUGHLIN, Retired 1400 hrs AIAA-2015-2369 Recent progress in numerical simulations for jet noise computation using LES on fully unstructured meshes Monday, 22 June 2015 39-AA-8 A. Neifeld, N. Reiche, J. Dierke, R. Ewert, German Aerospace Center (DLR), Braunschweig, Germany 1430 hrs AIAA-2015-2370 Jet Noise Prediction with Eddy Relaxation Source Model B. Lyu, University of Cambridge, J. Serpieri, S. Pröbsting, M. Gupta, F. Cambridge, United Kingdom; M. Scarano, Delft University of Technology, Azarpeyvand, University of Bristol, Bristol, Delft, The Netherlands United Kingdom; S. Sinayoko, University of Southampton, Southampton, United Kingdom Chaired by: R. EWERT, DLR - German Aerospace Center 1400 hrs 1430 hrs AIAA-2015-2362 AIAA-2015-2363 A Trailing-Edge Noise Model for Effect of serrated trailing edge on Serrated Edges boundary layer instability noise Monday, 22 June 2015 38-AA-7 T. Sinnige, K. Lynch, D. Ragni, G. Eitelberg, L. Veldhuis, Delft University of Technology, Delft, The Netherlands Chaired by: A. LYRINTZIS 1400 hrs AIAA-2015-2356 Aerodynamic and Aeroacoustic Effects of Pylon Trailing Edge Blowing on Pusher Propeller Installation Monday, 22 June 2015 37-AA-6 A. West, CD-adapco, London, United Kingdom; M. Caraeni, CD-adapco, Lebanon, NH 1500 hrs AIAA-2015-2371 Jet Noise Prediction using a Permeable FW-H Solver W. Ramirez, W. Wolf, University of Campinas, Campinas, Brazil 1500 hrs AIAA-2015-2364 The Effects of Suction and Blowing on Tonal Noise Generation by Blunt Trailing Edges T. Sinnige, J. van Kuijk, K. Lynch, D. Ragni, G. Eitelberg, L. Veldhuis, Delft University of Technology, Delft, The Netherlands 1500 hrs AIAA-2015-2358 The Effects of Swirl Recovery Vanes on Single-Rotation Propeller Aerodynamics and Aeroacoustics B. Venkatesh, R. Self, University of Southampton, Southampton, United Kingdom 1530 hrs AIAA-2015-2372 Parametric Study of Jet Nozzles Using a RANS-Based Jet Noise Prediction Tool Jet Noise Prediction II I. Clark, W. Alexander, W. Devenport, Virginia Polytechnic Institute and State University, Blacksburg, VA; S. Glegg, Florida Atlantic University, Boca Raton, FL; J. Jaworski, Lehigh University, Bethlehem, PA; C. Daly, University of Cambridge, Cambridge, United Kingdom; et al. 1530 hrs AIAA-2015-2365 Bio-Inspired Trailing Edge Noise Control Trailing Edge Noise I G. Busch, M. Hassan, D. Mavris, Georgia Institute of Technology, Atlanta, GA 1530 hrs AIAA-2015-2359 Aircraft Open Rotor Technology: Analysis from an Operational Perspective Open Rotor I D. Dahl, J. Nichols, University of Minnesota, Minneapolis, Minneapolis, MN Fleur-de-lis B Inverness 1700 hrs AIAA-2015-2368 Impact of Wall Permeability on Trailing-Edge Noise at High Reynolds Number C. Paruchuri, O. Stalnov, P. Joseph, C. S. Koh, M. Meinke, W. Schroeder, RWTH Vanderwel, B. Ganapathisubramani, Aachen University, Aachen, Germany University of Southampton, Southampton, United Kingdom; R. Leung, Defence Science and Technology Laboratory, Southampton, United Kingdom 1630 hrs AIAA-2015-2367 On the robustness of the TNO model for aerofoil self-noise prediction S. Glegg, A. Buono, J. Grant, F. Lachowski, Florida Atlantic University, Boca Raton, FL; W. Devenport, W. Alexander, Virginia Polytechnic Institute and State University, Blacksburg, VA 1600 hrs AIAA-2015-2373 Large Eddy Simulation of a Tactical Aircraft Exhaust Nozzle with Freestream and Wall Turbulence W. van der Velden, S. Pröbsting, A. de Jong, A. van Zuijlen, Delft University of Technology, Delft, The Netherlands; Y. Guan, S. Morris, University of Notre Dame, Notre Dame, IN 1600 hrs AIAA-2015-2366 Numerical and experimental investigation of a beveled trailing edge flow and noise field State University, Stillwater, OK 1630 hrs AIAA-2015-2361 Sound Radiation from a Rotor Partially Immersed in a Turbulent B. Humpert, R. Gaeta, J. Jacob, Oklahoma Boundary Layer 1600 hrs AIAA-2015-2360 Optimal Propeller Design for Quiet Aircraft using Numerical Analysis Fleur-de-lis A 52 A. Sescu, E. Collins, Mississippi State University, Mississippi State, MS; R. Harris, CFD Research Corporation, Huntsville, AL; E. Luke, Mississippi State University, Mississippi State, MS M. James, A. Salton, J. Downing, Blue Ridge Research and Consulting, LLC, Asheville, NC; K. Gee, T. Neilsen, B. Reichman, Brigham Young University, Provo, UT; et al. 1430 hrs AIAA-2015-2375 Acoustic Emissions from F-35 Aircraft during Ground Run-Up A. Wortmann, M. Hoogreef, R. Vos, Delft University of Technology, Delft, The Netherlands I. Chakraborty, M. LeVine, M. Hassan, D. Mavris, Georgia Institute of Technology, Atlanta, GA Chaired by: D. WELLS, NASA Langley Research Center 1430 hrs 1400 hrs AIAA-2015-2386 AIAA-2015-2385 Effect of Wing Loading and Fuel Assessing Taxiing Trade Spaces Type on Optimal Cruise Altitude for from Aircraft, Airport, and Airline Civil Aircraft Perspectives Monday, 22 June 2015 42-ACD-1 S. Schlimpert, S. Koh, A. Feldhusen, B. Roidl, M. Meinke, W. Schroeder, RWTH Aachen University, Aachen, Germany Chaired by: C. TAM, Florida State Univeristy 1400 hrs 1430 hrs AIAA-2015-2380 AIAA-2015-2381 Hydrodynamic instability and shear Assessing Acoustic Source Forcing layer effect on the sound emission Tools for Launch Vehicle Jet Noise of a turbulent jet flame Prediction Monday, 22 June 2015 41-AA-10 R. Powers, D. McLaughlin, P. Morris, Pennsylvania State University, State College, PA Chaired by: S. MILLER, NASA 1400 hrs AIAA-2015-2374 Noise Reduction with Fluidic Inserts in Supersonic Jets Exhausting Over a Simulated Aircraft Carrier Deck Monday, 22 June 2015 40-AA-9 1530 hrs AIAA-2015-2388 Greenhouse Gas Impacts of OnDemand Electric Aircraft C. Bil, A. Gebreegziabher, RMIT University, T. Thompson, LMI, McLean, VA Melbourne, Australia 1500 hrs AIAA-2015-2387 Utilising Secondary Airports for RPT Operations: A Business Case S. Min, D. Lim, D. Mavris, Georgia Institute of Technology, Atlanta, GA 1600 hrs AIAA-2015-2389 Aircraft Noise Reduction Technology and Airport Noise Analysis for General Aviation Revitalization Aircraft Design for Environmental Impact Reduction Garching, Germany; F. Bake, German Aerospace Center (DLR), Berlin, Germany; N. Kings, National Center for Scientific Research (CNRS), Châtenay-Malabry, France; T. Sattelmayer, Technical University of Munich, Garching, Germany 1600 hrs AIAA-2015-2384 A study of mechanisms of sound generation by airfoils using flowacoustic correlations T. Stout, K. Gee, T. Neilsen, A. Wall, Brigham Young University, Provo, UT; M. James, Blue Ridge Research and Consulting, LLC, Asheville, NC 1600 hrs AIAA-2015-2378 Source characterization of full-scale jet noise using vector intensity A. Sano, A. Cavalieri, Technological Institute of Aeronautics (ITA), São José A. Wohlbrandt, S. Guerin, German Aerospace Center (DLR), Berlin, Germany; dos Campos, Brazil; W. Wolf, University of R. Ewert, German Aerospace Center (DLR), Campinas, Campinas, Brazil Braunschweig, Germany CAA Sound Generation I B. Reichman, Brigham Young University, Provo, UT; J. Downing, M. James, Blue Ridge Research and Consulting, LLC, Asheville, NC; A. Aubert, Naval Air Warfare Center, Patuxent River, MD; R. McKinley, A. Wall, Air Force Research Laboratory, Wright-Patterson AFB, OH; et al. 1530 hrs AIAA-2015-2377 Acoustical Environment of an F-35B During Vertical Landings 1530 hrs AIAA-2015-2383 Extension of the Random Particle Mesh method to periodic turbulent flows for fan broadband noise W. Ullrich, Technical University of Munich, prediction 1500 hrs AIAA-2015-2382 Numerical Investigation of Indirect Noise Generation by Accelerated Vorticity B. Harker, T. Neilsen, K. Gee, Brigham Young University, Provo, UT; M. James, Blue Ridge Research and Consulting, LLC, Asheville, NC; A. Wall, Air Force Research Laboratory, Wright-Patterson AFB, OH 1500 hrs AIAA-2015-2376 Spatiotemporal Correlation Analysis of Jet Noise from a HighPerformance Military Aircraft Jet Noise Measurements I M. Brunet, S. Aubry, R. Lafage, ONERA, Toulouse, France 1630 hrs AIAA-2015-2390 The Clean Sky programme: environmental benefits at aircraft level A. Wall, Air Force Research Laboratory, Wright-Patterson AFB, OH; K. Gee, T. Neilsen, Brigham Young University, Provo, UT; S. McInerny, University of Louisiana, Lafayette, Lafayette, LA; M. James, Blue Ridge Research and Consulting, LLC, Asheville, NC 1630 hrs AIAA-2015-2379 Investigation of multi-lobed fighter jet noise sources using acoustical holography and partial field decomposition methods Miro Obelisk A Lalique 53 T. Dief, S. Yoshida, Kyushu University, Kasuga, Japan; M. Abdelhady, Cairo University, Giza, Egypt West Lafayette, IN; M. Bolender, Air Force IN; M. Bolender, Air Force Research Research Laboratory, Wright-Patterson Laboratory, Wright-Patterson AFB, OH AFB, OH B. Martinez, D. Bidino, M. Bastide, C. Demeautis, F. Leopold, P. Wey, FrenchGerman Research Institute of Saint-Louis (ISL), Saint-Louis, France 1530 hrs AIAA-2015-2410 Computational Modeling of Radiation Effects on Total Temperature Probes Surface and Inflow Sensing F. Liu, M. Junkui, Nanjing University of Aeronautics and Astronautics, Nanjing, China 1530 hrs AIAA-2015-2406 Experimental Investigations about Heat Transfer Characteristics of Irregular Impingement Jet Arrays in Typical Active Clearance Control System J. Reardon, J. Schetz, K. Lowe, Virginia 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. Chaired by: Z. ZHANG, University of Tennessee and T. IOPPOLO, Southern Methodist University 1430 hrs 1500 hrs 1400 hrs AIAA-2015-2408 AIAA-2015-2409 AIAA-2015-2407 Development of a Sol-Gel Based A Counter-Propagating Laser Air Shear Stress Sensing with Elastic Nanoporous unsteady Pressure Speed Sensor System for Aircraft Microfence Structures A. Cisotto, F. Palmieri, NASA Langley J. Kurtz, University of New South Wales, Sensitive Paint and Validation in Research Center, Hampton, VA; Y. Lin, the Large Transonic Onera S2MA Canberra, Australia; S. Wittig, OHB System National Institute of Aerospace, Hampton, Windtunnel HB, Munich, Germany; S. O’Byrne, Monday, 22 June 2015 46-AMT-4/GT-4 Corporation, Fort Worth, TX N. Allen, M. Quinn, Aircraft Research Association, Ltd., Bedford, United Kingdom M. Grant, Purdue University, West Lafayette, IN; M. Bolender, Air Force Research Laboratory, Wright-Patterson AFB, OH 1530 hrs AIAA-2015-2402 Minimum Terminal Energy Optimizations of Hypersonic Vehicles Using Indirect Methods Edelweiss Obelisk B Plum Blossom B R. Olson, National Test Pilot School, Mojave, CA Plum Blossom A 1700 hrs AIAA-2015-2397 Flight Test Evaluation of Pilot Control Interfaces for Remotely H. Chao, University of Kansas, Lawrence, Piloted Vehicles 1630 hrs AIAA-2015-2396 Wake Vortex Detection with UAV Close Formation Flight J. Tritschler, Naval Air Systems Command, Lawrence, KS; Y. Gu, West Virginia Patuxent River, MD; J. Horn, Pennsylvania University, Morgantown, WV; P. Tian, Z. Zheng, University of Kansas, Lawrence, State University, State College, PA Lawrence, KS; M. Napolitano, West Virginia University, Morgantown, WV 1600 hrs AIAA-2015-2395 Objective Function Development for Optimized Path Guidance for Rotorcraft Shipboard Recovery Advances in Test Methodology and CFD Integration Chaired by: S. DUNN, Jacobs Technology and S. COLE, NASA Langley Research Center 1400 hrs 1430 hrs 1500 hrs AIAA-2015-2403 AIAA-2015-2404 AIAA-2015-2405 Development of a Transonic Gust F-35 Conventional Mode Jet-Effects Motion measurement of a wind Rig for Simulation of Vertical Gusts Testing Methodology tunnel model by stereovision M. McWaters, Lockheed Martin on Half-models technique Monday, 22 June 2015 45-AMT-3/GT-3 Y. Zheng, H. Cui, Y. Tian, Harbin Institute of Technology, Harbin, China D. Jack, K. Hoffler, S. Johnson, Adaptive Aerospace Group, Inc., Hampton, VA 1530 hrs AIAA-2015-2394 An Assessment of Unmanned Aircraft System Level-Turn Maneuver Performance Requirements In Relation to a Quantified Well-Clear Definition Unmanned Aircraft Systems I Planetary Entry and Aeroassist Technology K. Greene, D. Kunz, Air Force Institute of Technology, Wright-Patterson AFB, OH Chaired by: S. DUTTA, NASA Langley Research Center and C. KARLGAARD, Analytical Mechanics Associates Inc 1400 hrs 1430 hrs 1500 hrs AIAA-2015-2398 AIAA-2015-2399 AIAA-2015-2401 Improvements to Entry Terminal Optimization of Interior Point Cost Rapid, Robust Trajectory Design Using Point Controller for Mars Functions Using Indirect Methods Indirect Optimization Methods T. Antony, M. Grant, Purdue University, M. Grant, Purdue University, West Lafayette, Atmospheric Entry Monday, 22 June 2015 44-AFM-4 P. Santos, P. Gamboa, University of Beira Interior, Covilha, Portugal Chaired by: K. HOFFLER, Adaptive Aerospace Group, Inc. and S. D’SOUZA, NASA-ARC 1400 hrs 1430 hrs 1500 hrs AIAA-2015-2391 AIAA-2015-2392 AIAA-2015-2393 Attitude and altitude stabilization Quickness Criteria for Large Evaluation of Energy Required of quad rotor using parameter Unmanned Aircraft in Nonfor Flight by a UAV Fitted with a Precision Aggressive and NonVariable-Span Wing Performing a estimation and self-tuning Given Mission Profile controller Aggressive Maneuvers Monday, 22 June 2015 43-AFM-3 54 1500 hrs AIAA-2015-2416 System Development for Wildfire SUAS N. Nguyen, NASA Ames Research Center, N. Nguyen, NASA Ames Research Center, Moffett Field, CA Moffett Field, CA; N. Precup, E. Livne, University of Washington, Seattle, Seattle, WA; J. Urnes, The Boeing Company, St. Louis, MO; E. Dickey, The Boeing Company, Huntington Beach, CA; C. Nelson, The Boeing Company, Seattle, WA; et al. B. Stanford, NASA Langley Research Center, Hampton, VA 1500 hrs AIAA-2015-2419 Optimization of an Aeroservoelastic Wing with Distributed Multiple Control Surfaces G. Fujiwara, University of Washington, Seattle, Seattle, WA; N. Nguyen, NASA Ames Research Center, Moffett Field, CA 1530 hrs AIAA-2015-2420 Adaptive Aeroelastic Wing Shape Optimization for High-Lift Configurations Y. Liu, J. Bai, Northwestern Polytechnical University, Xi’an, China; E. Livne, University of Washington, Seattle, Seattle, WA 1600 hrs AIAA-2015-2421 Robust Optimization of VariableCamber Continuous Trailing-Edge Flap System Action Using Stochastic Kriging U. Kaul, N. Nguyen, NASA Ames Research Center, Moffett Field, CA 1630 hrs AIAA-2015-2422 A 3-D Drag Optimization Study of Variable Camber Continuous Trailing Edge Flap (VCCTEF) Using OVERFLOW Special Session: Aerodynamic-Structural Modeling, Optimization, and Test Techniques for Flexible Wing Technology I Unmanned, Bio-Inspired, Solar Powered Aerial Vehicle Designs I Beijing, China; R. Agarwal, Washington University in St. Louis, St. Louis, MO J. Jacob, D. Gabbert, M. Andalibi, Oklahoma State University, Stillwater, OK A. Rege, B. Dennis, K. Subbarao, University of Texas, Arlington, Arlington, TX Chaired by: N. NGUYEN, NASA-Ames Research Center and S. ANDERS 1400 hrs 1430 hrs AIAA-2015-2417 AIAA-2015-2418 Wind Tunnel Investigation of a Flexible Use of a Viscous Flow Simulation Wing High-Lift Configuration with a Code for Static Aeroelastic Analysis Variable Camber Continuous Trailing of a Wing at High-Lift Conditions H. Akaydin, S. Moini-Yekta, J. Housman, Edge Flap Design Monday, 22 June 2015 49-APA-7 T. Young, Naval Research Laboratory, Washington, DC Chaired by: L. UKEILEY, University of Florida 1400 hrs 1430 hrs AIAA-2015-2414 AIAA-2015-2415 Computational Studies for the Force Production by Wing Flapping: Development of a Hybrid UAV/UUV The Role of Stroke Angle of Attack R. Ramamurti, J. Geder, D. Edwards, and Local Reynolds Number Monday, 22 June 2015 48-APA-6 P. Wey, C. Berner, French-German Research J. Xiang, J. Schluter, F. Duan, Nanyang Institute of Saint-Louis (ISL), Saint-Louis, Technological University, Singapore, France; et al. Singapore Applied CFD & Numerical Correlations with Experimental Data I 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 Numerical Simulation of Water Supersonic Projectile Steering using Effects of Tip Clearance on Micro-Actuators: Experimental and Miniature Gas Turbines Compressor Spray Caused by a Rolling Airplane Performance: A Numerical Tire Numerical Study M. Libsig, B. Martinez, C. Rey, T. Gauthier, Approach Q. Qu, F. Zhang, P. Liu, Beihang University, Monday, 22 June 2015 47-APA-5 Stemmons A Carpenter Ballroom Stemmons B 55 Munich, Munich, Germany; C. Jessberger, K. Ploetner, Bauhaus Luftfahrt e.V., Munich, Germany Tokyo, Bunkyo, Japan Arlington, Arlington, TX 1500 hrs AIAA-2015-2442 Parametric Assessment of Aviation Environmental Goals: Implications on R&D Decision Making K. Gatian, D. Mavris, Georgia Institute of Technology, Atlanta, GA 1500 hrs AIAA-2015-2436 Enabling Technology Portfolio Selection through Quantitative Uncertainty Analysis R. Curran, F. Herrema, W. Zhao, Delft University of Technology, Delft, The Netherlands; V. Treve, R. Graham, EUROCONTROL, Bretigny, France M. Hassan, A. Payan, S. O’Sullivan, H. X. Peng, B. Chudoba, University of Texas, Pfaender, D. Mavris, Georgia Institute of Technology, Atlanta, GA Arlington, Arlington, TX Chaired by: P. HOLLINGSWORTH, The University of Manchester 1430 hrs 1400 hrs AIAA-2015-2441 AIAA-2015-2440 Paving the Way from the Past to Knowledge Engineering the Future: AVDKBS, a Software Formalizing the Engineering Science Discipline Development in Knowledge X. Peng, B. Chudoba, University of Texas, Engineering Monday, 22 June 2015 53-ATIO-7 C. Murphy, B. Miller, Metron Aviation, Inc., Dulles, VA; L. Sherry, George Mason University, Fairfax, VA Chaired by: W. CROSSLEY, Purdue University 1430 hrs 1400 hrs AIAA-2015-2435 AIAA-2015-2434 Effects of Fuel Price on Total Fuel Estimating the Fuel Saving Burn and System Capacity- An Potential of Commercial Aircraft Analysis of Advanced Engine and in Future Fleet-Development Airframe Technology and Airline Scenarios Responses to Changes in Fuel Price N. Randt, L. Wache, Technical University of Monday, 22 June 2015 52-ATIO-6 E. Chevalley, B. Parke, J. Kraut, N. Bienert, F. Omar, E. Palmer, NASA Ames Research Center, Moffett Field, CA A. Isikveren, D. Empl, U. Kling, K. Ploetner, C. Pornet, Bauhaus Luftfahrt e.V., Ottobrunn, Germany 1530 hrs AIAA-2015-2443 Selected Array of Technology and Systems Options for Ecologically Responsible Aviation Systems Engineering and Analysis J. Bernardo, T. Zaidi, M. LeVine, H. Jimenez, D. Mavris, Georgia Institute of Technology, Atlanta, GA 1530 hrs AIAA-2015-2437 A Rapid Integrated Interdependent Fleet-Level Environmental Model Fleet and Route Planning C. Hanses, F. Knabe, B. Korn, German Aerospace Center (DLR), Braunschweig, Germany 1530 hrs AIAA-2015-2431 Designing and Evaluating Advanced Approach Procedures for the Concept of Segmented Independent Parallel Approaches 1500 hrs AIAA-2015-2430 Time Based Separation: A study into runway compression and time based separation Terminal & Surface Operations II 1630 hrs AIAA-2015-2439 Landscape Analysis Framework for Low Carbon Energy T. Reynolds, M. McPartland, Y. Rodriguez, M. Sandberg, J. Venuti, Lincoln Laboratory, Massachusetts Institute of Technology, Lexington, MA P. Vascik, Massachusetts Institute of Z. Sha, K. Moolchandani, A. Maheshwari, Technology, Cambridge, MA; R. Pearce, NASA Headquarters, Washington, DC; J. Thekinen, J. Panchal, D. DeLaurentis, D. Rhodes, Massachusetts Institute of Purdue University, West Lafayette, IN Technology, Cambridge, MA 1600 hrs AIAA-2015-2438 Modeling Airline Decisions on Route Planning Using Discrete Choice Models University, Goyang, South Korea 1630 hrs AIAA-2015-2433 Assessment of Delayed Deceleration Approach E. Kim, S. Hong, K. Lee, Korea Aerospace Opportunities at US Airports 1600 hrs AIAA-2015-2432 Optimal Airspace Design for Continuous Climb Operation 1600 hrs AIAA-2015-2427 Stochastic analysis of aerodynamic forces acting on a self-adaptive camber airfoil in turbulent inflow G. Kampers, Carl von Ossietzky University, Oldenburg, Germany; U. Cordes, C. Z. Hasnain, R. Weinstein, L. Trollinger, Tropea, Technical University of Darmstadt, J. Hubbard, A. Flatau, University of Maryland, College Park, College Park, MD Darmstadt, Germany; M. Hoelling, J. Peinke, Carl von Ossietzky University, Oldenburg, Germany Chaired by: A. SARAF, Saab Sensis Corporation 1400 hrs 1430 hrs AIAA-2015-2428 AIAA-2015-2429 Scheduling and Delivering Aircraft Stochastic Near-Optimal Control to Departure Fixes in the NY for Aircraft Arrival Sequencing and Metroplex with Controller-Managed Conflict Resolution Y. Matsuno, T. Tsuchiya, University of Spacing Tools M. Walker, K. Hipp, S. Benton, J. Bons, Ohio State University, Columbus, OH Monday, 22 June 2015 51-ATIO-5 Chennai, India; S. Thanigaiarasu, Madras K. Kara, Khalifa University, Abu Dhabi, Institute of Technology, Chennai, India; S. United Arab Emirates Venkatraman, KCG College of Technology, Chennai, India; E. Srinivasan, Bharath University, Chennai, India; E. Rathakrishnan, Indian Institute of Technology Kanpur, Kanpur, India 1530 hrs AIAA-2015-2426 Dynamic Flow Control over Aerodynamic Bodies using Phased Array Vectored Synthetic Jet Actuation Flow Control Applications & Demonstrations (Active & Passive) I Chaired by: J. GEORGE, Metrolaser Inc. and K. MULLENERS, Leibniz Universitaet Hannover 1400 hrs 1430 hrs 1500 hrs AIAA-2015-2423 AIAA-2015-2424 AIAA-2015-2425 Effect of Spanwise Jet Spacing on Study of slanted perforated shapes in Numerical Study of the Internal Flow Structures Inside the Sweeping Separation Control for Swept and tabs for control of subsonic Jets A. Reyaz Ahmed, KCG College of Technology, Jet Actuator Unswept Airfoils Monday, 22 June 2015 50-APA-8 Milan Ming Manchester Stemmons C 56 National Institute of Aerospace, Hampton, J. Choi, University of Maryland, College VA Park, College Park, MD Danette Allen Autonomy Incubator, NASA Langley Research Center H. Nishikawa, National Institute of Aerospace, Hampton, VA L. Reimer, M. Ritter, R. Heinrich, W. Krüger, German Aerospace Center (DLR), Braunschweig, Germany Institute of Technology, Harbin, China India Chaired by: L. MARTINELLI, Princeton University and S. EYI, Middle East Technical University 1430 hrs 1500 hrs 1400 hrs AIAA-2015-2456 AIAA-2015-2457 AIAA-2015-2455 CFD-based Gust Load Analysis for Influence of Wall Vibration on the Numerical Analysis of Synthetic Jet Aero Performance of Transonic in Crossflow a Free-flying Flexible Passenger A. Gupte, A. Pradeep, P. Mujumdar, Indian Aircraft in Comparison to a DLM- Diffuser Institute of Technology Bombay, Mumbai, C. Yao, G. Zhang, F. Xu, Z. Liu, Harbin based Approach Monday, 22 June 2015 57-CFD-7 Arbor, Ann Arbor, MI Chaired by: J. EKATERIN, IACM and M. CHOUDHARI, NASA-Langley Research Center 1400 hrs 1430 hrs 1500 hrs AIAA-2015-2449 AIAA-2015-2450 AIAA-2015-2451 Investigations of a New Scheme for Active Flux for Advection Diffusion Alternative Formulations for H. Nishikawa, National Institute of Wave Propagation First-, Second-, and Third-Order D. Fan, P. Roe, University of Michigan, Ann Aerospace, Hampton, VA Hyperbolic Navier-Stokes Schemes Monday, 22 June 2015 56-CFD-6 1600 hrs AIAA-2015-2453 A Versatile Nonlinear Predictive Modeling Approach X. Liu, H. Luo, North Carolina State University, Raleigh, NC; Y. Xia, Idaho National Laboratory, Idaho Falls, ID Y. Muslubas, S. Eyi, Middle East Technical University, Ankara, Turkey 1530 hrs AIAA-2015-2458 Performances of Newton and Preconditioned Newton-GMRES Methods in Hypersonic Flow Solutions Interdisciplinary CFD I 1630 hrs AIAA-2015-2454 Dynamical selective filtering for the Lattice Boltzmann Method 1600 hrs AIAA-2015-2448 A Class of Rosenbrock Methods for a Reconstructed Discontinuous Galerkin Method for the Unsteady Compressible Flows Craig Woolsey Virginia Tech Z. Duan, Z. Wang, University of Kansas, M. Liou, NASA Glenn Research Center, S. Marie, National Conservatory of Arts Lawrence, Lawrence, KS; B. Vu, NASA Cleveland, OH; W. Yao, Queen’s University, and Crafts, Paris, France; X. Gloerfelt, Kennedy Space Center, Cape Canaveral, FL Belfast, United Kingdom Paris Institute of Technology, Paris, France 1530 hrs AIAA-2015-2452 Recent Progresses on a Meshless Euler Solver for Compressible Flows Novel Discretizations M. López-Morales, A. Jameson, Stanford University, Stanford, CA 1530 hrs AIAA-2015-2447 Stabilization of High-Order Methods for Unstructured Grids with Local Fourier Spectral Filtering: high-Re Simulations in Coarse Meshes Unstructured High-Order Methods II Nick Roy MIT Transformational Flight - Enabling the Next Billion Dollar Aviation Market through Autonomy Chaired by: H. HUYNH, NASA Glenn Research Center and A. JAMESON, Aeronautics and Astronautics 1400 hrs 1430 hrs 1500 hrs AIAA-2015-2444 AIAA-2015-2445 AIAA-2015-2446 A Survey of the Isentropic Euler High-Order Hyperbolic ResidualHigh-Order Methods for Vortex Problem using High-Order Distribution Schemes on Arbitrary Conservation Laws Employing Methods Triangular Grids Embedded Structured Element S. Spiegel, H. Huynh, J. DeBonis, NASA A. Mazaheri, NASA Langley Research Method on Unstructured Glenn Research Center, Cleveland, OH Center, Hampton, VA; H. Nishikawa, Hexahedral Grid Monday, 22 June 2015 55-CFD-5 Moderator: Mark Ballin, NASA Langley Research Center Panelists: Monday, 22 June 2015 54-ATIO-8 1400 - 1600 hrs Coral Grand Ballroom B Grand Ballroom A Metropolitan Ballroom 57 Michigan, Ann Arbor, Ann Arbor, MI J. Coder, Pennsylvania State University, State College, PA R. Miles, C. Limbach, Princeton University, P. Milan, F. Demers, H. Vo, École Princeton, NJ Polytechnique de Montréal, Montréal, Canada College Station, TX J. Crouch, The Boeing Company, Seattle, WA Technology, Delft, The Netherlands K. Asano, University of Tokyo, Sagamihara, 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 S. Schneider, Purdue University, West Lafayette, IN P. Balakumar, NASA Langley Research Center, Hampton, VA 1530 hrs AIAA-2015-2473 Receptivity of Hypersonic Boundary Layers to Acoustic and Vortical Disturbances (Invited) 1630 hrs AIAA-2015-2475 CFD Transition Modeling: Blending Classical Methods with Modern Tools (Invited) G. Correale, Delft University of Technology, Delft, The Netherlands R. Langtry, The Boeing Company, Seattle, WA J. Coder, M. Maughmer, Pennsylvania State University, State College, PA 1600 hrs AIAA-2015-2474 Extending the Gamma-Rethetat Correlation based Transition Model for Crossflow Effects (Invited) Boundary Layer Transition - Progress and Challenges Chaired by: M. MALIK, NASA-Langley Research Center and M. ROGERS, NASA-Ames Research Center 1430 hrs 1500 hrs 1400 hrs AIAA-2015-2472 Oral Presentation AIAA-2015-2471 Hypersonic Boundary-Layer Receptivity: The Inspiration of Mark Boundary-Layer Transition Prediction for Laminar Flow Control Transition: Towards MechanismMorkovin (Invited) H. Reed, W. Saric, Texas A&M University, (Invited) Based Prediction Methods (Invited) Monday, 22 June 2015 61-FD-7 ONERA, Toulouse, France 1600 hrs AIAA-2015-2469 Contribution of large-scale vortex and fine-scale turbulent structure in separated flow control using DBD R. Winkel, G. Correale, Delft University of plasma actuator 1530 hrs AIAA-2015-2468 Ns-DBD plasma actuator induced density gradient on a laminar boundary layer 1630 hrs AIAA-2015-2470 Flow control over a backward facing step by ns-DBD plasma actuator Eric Schrock Deputy Director, Technology Development and Product Integration Lockheed Martin Corporation Plasma Aerodynamics & Flow Control II Chaired by: D. WILLIAMS, Illinois Institute of Technology and J. LITTLE, The University of Arizona 1400 hrs 1430 hrs 1500 hrs AIAA-2015-2465 AIAA-2015-2466 AIAA-2015-2467 PIV and Electric Characterization of Adjoint Optimization of the Spatial Modeling of Saw-tooth DBD a Plasma Synthetic Jet Actuator Profile of Steady Energy Deposition Plasma Actuators for Flow Control F. Laurendeau, F. Chedevergne, O. Léon, for Supersonic Drag Reduction Simulations Monday, 22 June 2015 60-FD-6/PDL-2 A. Krumbein, N. Krimmelbein, C. Grabe, German Aerospace Center (DLR), Cologne, Germany Sapphire Govenors Lecture Hall Grand Ballroom E Emerald 1700 hrs AIAA-2015-2476 Development and Application of Transition Prediction Techniques in an Unstructured CFD Code (Invited) 1630 hrs AIAA-2015-2464 A logarithmic formulation for low-Reynolds number turbulence models with adaptive wall-functions D. Higuera Caubilla, University of Toulouse, L. Frazza, A. Hay, D. Pelletier, École Toulouse, France; P. Razi, Texas A&M Polytechnique de Montréal, Montréal, University, College Station, TX; S. Sekhar, Canada N. Mansour, NASA Ames Research Center, Moffett Field, CA; S. Girimaji, Texas A&M University, College Station, TX 1600 hrs AIAA-2015-2463 PANS Simulations of Turbulent Separated Flow over a Wallmounted Hump Whatever Happened to the Four-Year Airplane? J. Schaefer, T. West, S. Hosder, Missouri University of Science and Technology, Rolla, MO; C. Rumsey, J. Carlson, W. Kleb, NASA Langley Research Center, Hampton, VA Moderator: Craig Willis, Group Head for Systems Verification, Gulfstream G500/G600 Program, Gulfstream Aerospace Corporation Panelists: Catherine Ferrie Kilmain Executive Vice President of Engineering Bell Helicopter Monday, 22 June 2015 59-F360-2/CASE-2 1400 - 1700 hrs E. Parish, K. Duraisamy, University of Michigan, Ann Arbor, Ann Arbor, MI 1530 hrs AIAA-2015-2462 A Scale-Adaptive Variant of the Spalart-Allmaras Eddy-Viscosity Model Turbulence Modeling and Uncertainty Quantification Chaired by: D. YODER, NASA Glenn Research Center and K. DURAISAMY, Stanford University 1400 hrs 1430 hrs 1500 hrs AIAA-2015-2459 AIAA-2015-2460 AIAA-2015-2461 Machine Learning Methods for Uncertainty Quantification of Quantification of Turbulence Modeling Uncertainties Using Full Data-Driven Turbulence Modeling Turbulence Model Closure Coefficients Z. Zhang, K. Duraisamy, University of for Transonic Wall-Bounded Flows Field Inversion Monday, 22 June 2015 58-CFD-8 58 A. Elham, Delft University of Technology, Delft, The Netherlands; M. van Tooren, University of South Carolina, Columbia, Columbia, SC Vehicle Design Applications II M. Koklu, NASA Langley Research Center, Hampton, VA J. Xie, Y. Wan, University of North Texas, Denton, TX Chaired by: J. SMITH 1400 hrs AIAA-2015-2492 Scalable Multidimensional Uncertainty Evaluation Approach to Strategic Air Traffic Flow Management Monday, 22 June 2015 65-MST-3 DHC Engineering, San Mateo, CA; F. Gilliam, Lipscomb University, Nashville, TN; T. Jung, T. Yechout, U.S. Air Force Academy, Colorado Springs, CO 1500 hrs AIAA-2015-2494 Development of an ATC Tower Simulator to Simulate Ground Operations 1530 hrs AIAA-2015-2495 Multi-Agent Based Air Traffic Simulation System 1600 hrs AIAA-2015-2496 Estimating Benefits of Aviation Alternative Fuels at the System, Route, and Airport Level A. Wildschek, Airbus, Ottobrunn, Germany 1600 hrs AIAA-2015-2490 Concurrent Optimization of a Feed-Forward Gust Loads Controller and Minimization of Wing Box Structural Mass on an Aircraft with Active Winglets S. Beresh, J. Wagner, J. Henfling, R. Spillers, B. Pruett, Sandia National Laboratories, Albuquerque, NM D. Poole, C. Allen, T. Rendall, University of Bristol, Bristol, United Kingdom 1630 hrs AIAA-2015-2491 Free-Form Aerodynamic Wing Optimization Using MathematicallyDerived Design Variables 1600 hrs AIAA-2015-2481 Temporal Evolution of Turbulent Eddies in a Compressible Jet in Crossflow Measured using Pulse-Burst PIV Z. Yue, D. Sui, Y. Lin, J. Zhang, Nanjing Z. Chua, University of Toulouse, Toulouse, University of Aeronautics and Astronautics, B. Miller, C. Murphy, Metron Aviation, Inc., Nanjing, China Dulles, VA; C. Villa, A. Filizola, National V. Kumar, B. Horio, A. DeCicco, S. Hasan, V. France; F. Andre, M. Cousy, French Civil Aviation University, Toulouse, France Civil Aviation Agency (ANAC), Brasilia, Stouffer, LMI, McLean, VA; J. Smith, NASA Brazil Langley Research Center, Hampton, VA; et al. 1430 hrs AIAA-2015-2493 Understanding Air Transportation Market Dynamics using a Search Algorithm for Calibrating Travel Demand and Price Air Traffic Management Technical University, Cankaya, Turkey; E. M. van Tooren, University of South Acar, TOBB University of Economics and Carolina, Columbia, Columbia, SC; A. Technology, Sogutozu, Turkey Elham, Delft University of Technology, Delft, The Netherlands; R. Harik, University of South Carolina, Columbia, Columbia, SC 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 AIAA-2015-2486 AIAA-2015-2487 AIAA-2015-2488 AIAA-2015-2489 The Value of Semi-Empirical Coupled Adjoint Aerostructural Optimal variable stiffness Simulation-Based Optimal Sensor/ Analysis Models in Aircraft Design Wing Optimization Using Quasidistribution for a composite plate Actuator Positioning on a Fin-Like S. Brandt, M. Post, U.S. Air Force Three-Dimensional Aerodynamic with a row of holes subjected to Structure Academy, Colorado Springs, CO; D. Hall, Analysis N. Pedramasl, M. Sahin, Middle East tension/shear load cases Monday, 22 June 2015 64-MAO-2 R. Cummings, Rensselaer Polytechnic Institute, Troy, NY; D. Clingman, The Boeing Company, Seattle, WA; O. Sahni, Rensselaer Polytechnic Institute, Troy, NY C. Leong, E. Cruz, Rensselaer Polytechnic Polytechnic Institute, Troy, NY Institute, Troy, NY; D. Clingman, The Boeing Company, Seattle, WA; M. Amitay, Rensselaer Polytechnic Institute, Troy, NY 1530 hrs AIAA-2015-2485 The Effects of Sweeping Jet Actuator Parameters on Flow Separation Control X. Gloerfelt, Paris Institute of Technology, Paris, France; P. Cinnella, University of Salento, Lecce, Italy Active and Passive Flow Control University, Murfreesboro, TN Chaired by: K. GRANLUND, Air Force Research Laboratory and M. AMITAY, Rensselaer Polytechnic Institute 1400 hrs 1430 hrs 1500 hrs AIAA-2015-2482 AIAA-2015-2483 AIAA-2015-2484 Interactions of a Dynamic Vortex Interactions of a Dynamic Vortex Flow Control in a Diffuser at Generator with a Cross-flow: A Generator with a Cross-flow: An Transonic Conditions J. Gartner, M. Amitay, Rensselaer Numerical Study Experimental Study University, Dallas, TX Monday, 22 June 2015 63-FD-9 Z. Rusak, J. Choi, Rensselaer Polytechnic Institute, Troy, NY; S. Wang, University of Auckland, Auckland, New Zealand 1530 hrs AIAA-2015-2480 Investigation of the flow dynamics in a channel constricted by periodic hills Vortex Flows Chaired by: Z. ZHENG, The University of Kansas and R. GORDNIER, Air Force Reseach Laboratory 1400 hrs 1430 hrs 1500 hrs AIAA-2015-2477 AIAA-2015-2478 AIAA-2015-2479 Vortex Breakdown of Compressible Numerical Study of the Formation Rotating Cylindrical Bodies at of Concentric Vortex Rings Low Re Swirling Flows in a Finite-Length V. Sadri, P. Krueger, Southern Methodist M. Callender, Middle Tennessee State Straight Circular Pipe Monday, 22 June 2015 62-FD-8 Travertine Madrid Topaz Senators Lecture Hall 59 E. Sezer, M. Nalci, ROKETSAN Missile Industries, Inc., Ankara, Turkey; A. Kutay, Middle East Technical University, Ankara, Turkey 1530 hrs AIAA-2015-2508 Development and Qualification of Lightweight Ablator Aeroshell BBM for Martian Mission Ablation II Q. Zhai, Z. Zhang, J. Cai, Northwestern Polytechnical University, Xi’an, China; F. Liu, S. Luo, University of California, Irvine, Los Angeles, CA 1530 hrs AIAA-2015-2504 CFD Validation of PIV-based Estimation of DBD PlasmaActuation Force Plasma Computational Methods I 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 Chaired by: N. DOUGHERTY, ERC Incorporated and A. HASHEMI, Lockheed Martin Space Systems 1430 hrs 1500 hrs 1400 hrs AIAA-2015-2506 AIAA-2015-2507 AIAA-2015-2505 Effects of Water Presence on Low A Multi-Dimensional Finite Element Thermal Protection System Mass Temperature Phenomenon in Based Solver for Decomposing Estimating Relationships For BluntPorous TPS Materials and Non-Decomposing Thermal Body, Earth Entry Spacecraft D. Smith, A. Omidy, H. Weng, University Protection Systems S. Sepka, ERC, Inc., Moffett Field, CA; J. Monday, 22 June 2015 68-TP-3 R. Thompson, T. Moeller, University of Tennessee, Tullahoma, Tullahoma, TN 1500 hrs AIAA-2015-2503 Investigations of Flow over a Hemisphere using Numerical Simulations C. Tam, T. Madden, Air Force Research Technology, Chickballapur, India; P. Moses Laboratory, Kirtland AFB, NM; B. Thurow, John Christy Appolo, T. Sheshadri, Indian Auburn University, Auburn, AL Institute of Science, Bengaluru, India Aircraft Manufacturing and Development Company, Tokyo, Japan; T. Dhaene, Ghent University, Ghent, Belgium Chaired by: M. WHITE, Ohio Aerospace Institute 1400 hrs 1430 hrs AIAA-2015-2501 AIAA-2015-2502 A Non-iterative Hyperbolic, First- Equivalent Electrical Circuit for a 1D order Conservation Law Approach Plasma Engine N. Ramesh, Sri Jagadguru to Divergence-free Solutions to Chandrashekaranatha Swamiji Institute of Maxwell’s Equations Monday, 22 June 2015 67-PDL-3 R. Botez, S. Khan, University of Québec, Montréal, Canada 1500 hrs AIAA-2015-2499 Control validation of a morphing wing in an open loop architecture Guidance, Control, and Dynamics I 1530 hrs AIAA-2015-2500 A Comparative Study of a PseudoFive Degree of Freedom and an M. Tchatchueng Kammegne, D. Nguyen, Adjoint Model Against a Six Degree Hirayama, Yokohama National University, R. Botez, University of Québec, Montréal, of Freedom Model for Fidelity Yokohama, Japan; T. Sakurai, Hiyoh Canada Assessment Chaired by: R. BOTEZ, Ecole de Technologie Superieure 1400 hrs 1430 hrs AIAA-2015-2497 AIAA-2015-2498 A New Method for Tuning PI Gains Longitudinal Stability Augmentation for Position Control of BLDC Motor of Seaplanes in Planing K. Ito, Ghent University, Ghent, Belgium; T. Based Wing Morphing Actuators Monday, 22 June 2015 66-MST-4 Rosetta Monet Ballroom Wyeth 60 T. Zhu, Z. Li, N. Parsons, Pennsylvania State University, State College, PA; D. Levin, M. Panesi, University of Illinois, Urbana-Champaign, Urbana, IL 1600 hrs AIAA-2015-2513 Comparison of Two Hybrid RC-Models for Prediction of Nonequilibrium Radiation from Strong Shock Waves Rising Leaders in Aerospace Networking Reception Searching for Truthiness in Computational Fluid Dynamics Philip Roe Professor, Department of Aerospace Engineering University of Michigan Fluid Dynamics Award Lecture CASE Networking Social Steuben Emerald Grand Ballroom D Morocco Chantilly Ballroom Foyer Meeting Room Foyers 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. Monday, 22 June 2015 74-RLA-1 1830 - 1930 hrs Monday, 22 June 2015 73-LEC-1 1730 - 1830 hrs Sponsored by Boeing Commercial Airplanes Monday, 22 June 2015 72-CASE-3 1730 - 1900 hrs S. Nomura, H. Takayanagi, K. Fujita, H. Tanno, Japan Aerospace Exploration Agency (JAXA), Chofu, Japan 1630 hrs AIAA-2015-2514 Radiative Heat Flux from Metallic Species in Free Piston Shock Tunnel HIEST 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: Lockheed Martin Speed Geek Networking Event and Reception Monday, 22 June 2015 71-AIAA-1 1730 - 1900 hrs B. Cruden, A. Brandis, ERC, Inc., Moffett Field, CA; J. Grinstead, J. Olejniczak, NASA S. Surzhikov, Russian Academy of Ames Research Center, Moffett Field, CA; Sciences, Moscow, Russia L. Kirk, R. Lillard, NASA Johnson Space Center, Houston, TX; et al. 1530 hrs AIAA-2015-2512 Measurement of Ultraviolet Radiative Heating Augmentation in HIEST Reflected Shock Tunnel Networking Coffee Break J. Burt, E. Josyula, Air Force Research Laboratory, Wright-Patterson AFB, OH 1500 hrs AIAA-2015-2511 DSMC Modeling of Nonequilibrium Electronic Excitation and Emission for Hypersonic Sensor Applications Aerothermodynamics I Monday, 22 June 2015 70-NW-2 1530 - 1600 hrs K. Neitzel, D. Andrienko, I. Boyd, University of Michigan, Ann Arbor, Ann Arbor, MI Chaired by: C. JOHNSTON, NASA-Langley Research Center 1400 hrs 1430 hrs AIAA-2015-2509 AIAA-2015-2510 State Specific Modeling of the Modeling Fidelity for Oxygen Nonequilibrium Thermochemistry Energy Transfer in Nitrogen Shocks using High Fidelity Models in Reflected Shock Tube Flows Monday, 22 June 2015 69-TP-4 61 Cleveland, OH X. Liu, H. Jiang, X. Huang, Peking University, Beijing, China B. Fassmann, C. Rautmann, R. Ewert, J. Delfs, German Aerospace Center (DLR), Braunschweig, Germany 1000 hrs AIAA-2015-2527 Parametric Investigations of Tonal Trailing-Edge Noise Generation by Low-Reynolds Number Airfoils. Part I - Experimental Studies A. Maldonado, R. Astley, J. Coupland, G. Gabard, University of Southampton, Southampton, United Kingdom; D. Sutliff, NASA Glenn Research Center, Cleveland, OH 1000 hrs AIAA-2015-2522 Sound Propagation in Lined Annular Ducts with Mean Swirling Flow Aerospace Center (DLR), Berlin, Germany 1100 hrs AIAA-2015-2529 A Model for Jet-Surface Interaction Noise Using Physically Realizable Upstream Turbulence Conditions M. Dahl, NASA Glenn Research Center, Cleveland, OH; D. Hixon, University of Toledo, Toledo, OH 1100 hrs AIAA-2015-2524 Numerical Predictions of Mode Reflections in an Open Circular Duct: Comparison with Theory A. Kozlov, H. Atassi, University of Notre Dame, Notre Dame, IN 1100 hrs AIAA-2015-2519 Effect of Stator Vane Sweep on High Frequency Fan Noise and Comparison with Experiment M. Afsar, Imperial College London, London, L. Nguyen, W. Hiner, S. Salehian, V. Golubev, United Kingdom; S. Leib, Ohio Aerospace Institute, Cleveland, OH R. Mankbadi, Embry-Riddle Aeronautical University, Daytona Beach, FL; G. Yakhina, École Centrale de Lyon, Lyon, France; et al. 1030 hrs AIAA-2015-2528 Parametric Investigations of Tonal Trailing-Edge Noise Generation by Low-Reynolds Number Airfoils. Part II - Numerical Studies Trailing Edge Noise II A. Samanta, Indian Institute of Science, Bangalore, India; J. Freund, University of Illinois, Urbana-Champaign, Urbana, IL 1030 hrs AIAA-2015-2523 Upstream Radiation from Supersonic Buried-nozzle Jets via Scattering at the Shroud Edge Duct Acoustics II B. Pimenta, R. Bobenrieth Miserda, University of Brasília, Brasília, Brazil Fan Noise 1030 hrs AIAA-2015-2518 Validation of a Moving-Body HighOrder Immersed Boundary Method for the Multiple Pure Tone Noise V. Blandeau, V. Pastorelli, Airbus, Toulouse, Generated by Supersonic Rotor France; A. Moreau, S. Guerin, German Cascades 1000 hrs AIAA-2015-2517 Fan noise scaling of static data using semi-analytical methods and assessment against experimental data University of Southampton, Southampton, G. Yakhina, M. Roger, École Centrale de United Kingdom Lyon, Lyon, France; L. Nguyen, V. Golubev, Embry-Riddle Aeronautical University, Daytona Beach, FL Chaired by: J. GALLMAN, Gulfstream Aerospace Corporation 0900 hrs 0930 hrs AIAA-2015-2526 AIAA-2015-2525 Prediction of Porous Trailing Edge Prediction of Broadband TrailingNoise Reduction via Acoustic Edge Noise Based on Blake Model Perturbation Equations and Volume and Amiet Theory O. Stalnov, C. Paruchuri, P. Joseph, Averaging Tuesday, 23 June 2015 79-AA-13 Sweden 0930 hrs AIAA-2015-2521 Theoretical Study of Sound Propagation in Lined Duct with F. Majić, G. Efraimsson, C. O’Reilly, Royal Rigid Splices Using Wiener-Hopf Institute of Technology (KTH), Stockholm, Method Chaired by: C. YEN, Jacobs Technology 0900 hrs AIAA-2015-2520 Aero-Acoustic Performance of Adaptive Nacelle Inlet Tuesday, 23 June 2015 78-AA-12 R. Jaron, A. Moreau, S. Guerin, German Aerospace Center (DLR), Berlin, Germany Chaired by: S. GLEGG, Florida Atlantic University 0930 hrs 0900 hrs AIAA-2015-2515 AIAA-2015-2516 System Noise Prediction of the Extrapolation of RANS flow data for improved analytical fan tone DGEN 380 Turbofan Engine J. Berton, NASA Glenn Research Center, prediction Tuesday, 23 June 2015 77-AA-11 Plenary Panel Tuesday, 23 June 2015 76-PLNRY-2 0800 - 0900 hrs NextGen: A Model of Stakeholder Engagement Bill Ayer Edward L. Bolton Jr. Assistant Administrator for NextGen Retired Chairman and CEO Federal Aviation Administration Alaska Air Group Speakers’ Briefing Tuesday, 23 June 2015 75-SB-2 0730 - 0800 hrs Tuesday B. Zhou, N. Gauger, Technical University of Kaiserslautern, Kaiserslautern, Germany; S. Koh, M. Meinke, W. Schroeder, RWTH Aachen University, Aachen, Germany 1130 hrs AIAA-2015-2530 On the Adjoint-based Control of Trailing-Edge Turbulence and Noise Minimization via Porous Material K. Kucukcoskun, J. Christophe, C. Schram, von Kármán Institute for Fluid Dynamics, RhodeSaint-Genèse, Belgium; S. Moreau, University of Sherbrooke, Sherbrooke, Canada Inverness Fleur-de-lis B 1200 hrs AIAA-2015-2531 Experimental Validation of a SemiAnalytical Trailing-Edge Noise Model Including Broadband Scattering Fleur-de-lis A Chantilly Ballroom West Session Rooms 62 M. Cetin, S. Koh, M. Meinke, W. Schroeder, RWTH Aachen University, Aachen, Germany F. Gern, NASA Langley Research Center, Hampton, VA N. Mansouri, D. Hixon, University of Toledo, Toledo, OH 0930 hrs AIAA-2015-2539 Optimized Explicit Dissipation Operators for Computational Aeroacoustics State University, State College, PA; C. A. Thorsen, J. Horn, Pennsylvania State Thaiss, C. McColl, Technical Data Analysis, University, State College, PA Inc., Marietta, GA Chaired by: M. GRANT, Purdue University 0930 hrs 0900 hrs AIAA-2015-2550 AIAA-2015-2549 Aerobatic Maneuvers of a Damage Mitigating on a Large Rotorcraft using Load Alleviating Conventional and Compound Rotorcraft - Flight Path Generation Flight Control Laws D. Caudle, J. Horn, E. Keller, Pennsylvania and Dynamic Simulation Tuesday, 23 June 2015 83-AFM-5 A. Chaput, University of Texas, Austin, Austin, TX Chaired by: A. CHAPUT, University of Texas at Austin 0930 hrs 0900 hrs AIAA-2015-2544 AIAA-2015-2543 Student Air Vehicle Design and Update on HCDstruct - A Tool for Analysis - A Systems Engineering Hybrid Wing Body Conceptual Model Based Approach Design and Structural Optimization Tuesday, 23 June 2015 82-ACD-2 R. Harris, CFD Research Corporation, Huntsville, AL; E. Collins, A. Sescu, E. Luke, Mississippi State University, Mississippi State, MS Chaired by: X. LI, Beihang University 0900 hrs AIAA-2015-2538 Coupled Overset Unstructured Discontinuous Galerkin Method for Launch Environment Acoustics Prediction (Invited) Tuesday, 23 June 2015 81-AA-15 U. Sasidharan Nair, L. Agostini, D. Gaitonde, Ohio State University, Columbus, OH Chaired by: N. MURRAY, The University of Mississippi 0900 hrs 0930 hrs AIAA-2015-2532 AIAA-2015-2533 Aeroacoustic Analysis of a Analysis of Intermittency of Helicopter Engine Jet Including a Supersonic Jet Noise with Realistic Nozzle Geometry Synchronized LES Tuesday, 23 June 2015 80-AA-14 S. Erturk, A. Dogan, University of Texas, Arlington, Arlington, TX 1000 hrs AIAA-2015-2551 Propeller Torque Effect on Cruise Trim of Standard and MassActuated Airplane 1130 hrs AIAA-2015-2537 Spatial stability characteristics of non-circular jets 1100 hrs AIAA-2015-2547 User Defined Components in the OpenVSP Parametric Geometry Tool D. Hixon, University of Toledo, Toledo, OH 1100 hrs AIAA-2015-2542 Zero-Average Source Terms for Multidimensional Nonlinear Disturbance Equations P. Schmollgruber, N. Bartoli, ONERA, R. McDonald, California Polytechnic Toulouse, France; Y. Gourinat, University of State University, San Luis Obispo, CA; J. Toulouse, Toulouse, France Gloudemans, Self, San Mateo, CA 1030 hrs AIAA-2015-2546 Virtual flight testing in an aircraft sizing and optimization process Aircraft Design Methods and Tools M. Roger, École Centrale de Lyon, Ecully, France; S. Moreau, GAUS, Sherbrooke, Canada 1030 hrs AIAA-2015-2541 Towards Cascade Trailing-Edge Noise Modeling Using a ModeMatching Technique CAA Numerical Techniques II J. Barnes, Pelican Aero Group, San Pedro, CA 1030 hrs AIAA-2015-2552 Energy Gain From an Atmosphere in Motion - Dynamic Soaring and Regen-electric Flight Compared Y. Denieul, D. Alazard, J. Bordeneuve, University of Toulouse, Toulouse, France; C. Toussaint, ONERA, Toulouse, France; G. Taquin, Airbus, Toulouse, France 1100 hrs AIAA-2015-2553 Interactions of Aircraft Design and Control: Actuators Sizing and Optimization for an Unstable Blended Wing-Body R. Gezer, ROKETSAN Missile Industries, Inc., Ankara, Turkey; A. Kutay, Middle East Technical University, Ankara, Turkey 1130 hrs AIAA-2015-2554 Finite Series Based Model Reference Adaptive Control M. Waddington, R. McDonald, California Polytechnic State University, San Luis Obispo, CA 1130 hrs AIAA-2015-2548 Development of an Interactive Wave Drag Capability for the OpenVSP Parametric Geometry Tool F. Lajús, Federal University of Santa Catarina, Florianópolis, Brazil; A. Cavalieri, Technological Institute of Aeronautics (ITA), São José dos Campos, Brazil; C. Center for Scientific Research (CNRS), Poitiers, V. Semiletov, S. Karabasov, A. France; T. Colonius, California Institute of Chintagunta, A. Markesteijn, Queen Mary Deschamps, Federal University of Santa Catarina, Florianópolis, Brazil Technology, Pasadena, CA; S. Lele, Stanford University of London, London, United University, Stanford, CA Kingdom 1100 hrs AIAA-2015-2536 Empiricism-free noise calculation from LES solution based on Goldstein generalized acoustic G. Brès, Cascade Technologies, Inc., Palo Alto, analogy: volume noise sources and CA; V. Jaunet, M. Le Rallic, P. Jordan, National meanflow effects 1030 hrs AIAA-2015-2535 Large eddy simulation for jet noise: the importance of getting the boundary layer right Aircraft Flight Dynamics, Control, Handling Qualities and Performance II P. Govindaraju, W. Crossley, Purdue University, West Lafayette, IN 1000 hrs AIAA-2015-2545 Simultaneous Aircraft Design and Trip Assignment under Design Parameter and Demand Uncertainty E. Brambley, University of Cambridge, Cambridge, United Kingdom 1000 hrs AIAA-2015-2540 DRP schemes perform poorly for decaying or growing oscillations F. Feng, Q. Wang, China Academy of Aerospace Aerodynamics, Beijing, China 1000 hrs AIAA-2015-2534 Large-scale structure evolution and sound generation in a hotjet Jet Noise Prediction III Plum Blossom A Wyeth Obelisk A Lalique 63 1000 hrs Oral Presentation New Wings level Yaw Capability in the AEDC PWT 16T Tunnel N. Calvert, A. Dogariu, M. Edwards, R. Miles, Princeton University, Princeton, NJ C. Guo, Y. Ren, Tsinghua University, Beijing, China R. Guyton, Air Force Research Laboratory, Wright-Patterson AFB, OH 1030 hrs Oral Presentation Model Deformation Measurements on a Flexible Wing H. Quix, J. Semmelmann, M. Wright, European Transonic Windtunnel, Cologne, Germany 1100 hrs AIAA-2015-2562 Model Deformation Measurement Capabilities at ETW Hampton, VA; P. Danehy, S. Jones, NASA Langley Research Center, Hampton, VA; B. Halls, N. Jiang, Spectral Energies, LLC, Dayton, OH Center, Hampton, VA; N. Jiang, Spectral Energies, LLC, Dayton, OH; N. Calvert, R. Miles, Princeton University, Princeton, NJ C. Ground, D. Thumiah, L. Maddalena, University of Texas, Arlington, Arlington, TX D. Lacy, The Boeing Company, Everett, WA; E. Dickey, A. Sclafani, The Boeing Company, Huntington Beach, CA Center (DLR), Braunschweig, Germany D. Keller, R. Rudnik, German Aerospace Center (DLR), Braunschweig, Germany 1100 hrs AIAA-2015-2571 Numerical Investigation of the Dynamic Behavior of a High-Lift Configuration with Circulation D. Rohlmann, S. Keye, German Aerospace Control 1030 hrs AIAA-2015-2570 Stall Maneuver Simulation of an elastic Transport Aircraft based on Flight Test Data High Angle of Attack and High Lift Aerodynamics 1030 hrs AIAA-2015-2566 Application of FLEET Velocimetry in the NASA Langley 0.3-Meter Transonic Cryogenic Tunnel 1000 hrs AIAA-2015-2565 Precision of FLEET Velocimetry using High-Speed CMOS Camera Systems 1100 hrs AIAA-2015-2567 Design and Application of Filtered Rayleigh Scattering Experiments C. Peters, Princeton University, Princeton, NJ; for Mixing Studies of New Strut P. Danehy, B. Bathel, NASA Langley Research R. Burns, National Institute of Aerospace, Injectors for Scramjets Spatially-Resolved Spectroscopic Techniques Chaired by: D. LACY, Boeing Commercial Airplanes and P. HARTWICH, Boeing Research & Technology 0930 hrs 1000 hrs 0900 hrs AIAA-2015-2569 Oral Presentation AIAA-2015-2568 Pressure Measurements of Burst Development Status of the High Lift High Angle of Attack Flight of a Wakes Over a Three-Element Airfoil Common Research Model (HL-CRM): A Subscale Aerobatic Aircraft O. Dantsker, M. Selig, University of Illinois, B. Pomeroy, M. Selig, University of Illinois, Representative High Lift Configuration Urbana-Champaign, Urbana, IL Urbana-Champaign, Urbana, IL for Transonic Transports Tuesday, 23 June 2015 87-APA-9 A. Cutler, E. Gallo, L. Cantu, George Washington University, Washington, DC D. Communier, M. Salinas, O. Carranza Moyao, R. Botez, University of Québec, Montréal, Canada C. Zwerger, S. Hickel, C. Breitsamter, N. Adams, Technical University of Munich, Munich, Germany 1130 hrs AIAA-2015-2572 Wall modeled large eddy simulation of the VFE-2 delta wing 1100 hrs AIAA-2015-2559 On the Calculation of Pitch Damping Stability Derivatives of Aircrafts Using Unsteady Sensitivity Equations Model Attitude, Deformation, and Data Acquisition Techniques B. Mills, Arnold Engineering Development P. Hebert, D. Davis, M. Turowski, W. Holladay, Complex, Tullahoma, TN NASA Stennis Space Center, Stennis, MS; P. Marshall, M. Duncan, Arctic Slope Regional Corporation (ASRC), Stennis, MS; et al. Chaired by: R. BURNS and A. CUTLER, The George Washington University 0900 hrs 0930 hrs AIAA-2015-2563 AIAA-2015-2564 WIDECARS Spectra Fitting in a Density Scaling and Calibration of Premixed Ethylene-Air Flame FLEET Temperature Measurements Tuesday, 23 June 2015 86-AMT-6/GT-6 D. Liu, J. Jin, F. Wang, W. Jin, Beihang University, Beijing, China Chaired by: R. GUYTON, USAF Wright Lab 0900 hrs 0930 hrs AIAA-2015-2560 AIAA-2015-2561 Temperature Measurement at the NASA Data Acquisition System Exit of Annular Combustor with Software Development for Rocket Slinger in Turbojet Engine Propulsion Test Facilities Tuesday, 23 June 2015 85-AMT-5/GT-5 Vegas, Las Vegas, NV; K. Lee, Catholic Force Engineering University, Xi’an, China F. Bocola, V. Muscarello, G. Quaranta, P. Kwandong University, Gangnung, South Masarati, Technical University of Milan, Korea; S. Singh, University of Nevada, Las Milano, Italy Vegas, Las Vegas, NV 1030 hrs AIAA-2015-2558 Aero structural modeling of a wing using CATIA V5 and XFLR5 software and experimental validation using the Price- Païdoussis wing tunnel Aeroservoelastic (ASE) and Aerodynamic Prediction Methods Chaired by: A. DA RONCH, University of Southampton and T. RICHARDSON, University of Bristol 0900 hrs 0930 hrs 1000 hrs AIAA-2015-2555 AIAA-2015-2556 AIAA-2015-2557 Pilot In The Loop Aeroservoelastic Adaptive Chebyshev Neural Control Modeling and Simulation for of a Multi-Input Aeroelastic System Autonomous Aerial Refueling Using Simulation In Support To The a Probe-Drogue System Conceptual Design Of A Fly By Wire Despite Gust Load P. Ghorawat, University of Nevada, Las H. Wang, X. Dong, J. Liu, J. Wang, Air Airplane Tuesday, 23 June 2015 84-AFM-6 Stemmons C Edelweiss Obelisk B Plum Blossom B 64 W. Li, NASA Langley Research Center, Hampton, VA S. Rallabhandi, National Institute of Aerospace, Hampton, VA M. Rennie, M. Nguyen, S. Gordeyev, E. K. Kanistras, P. Saka, K. Valavanis, N. Jumper, University of Notre Dame, Notre Vitzilaios, M. Rutherford, University of Dame, IN; A. Cain, Innovative Technology Denver, Denver, CO Applications Company, LLC, Chesterfield, MO; T. Hayden, U.S. Air Force Academy, Colorado Springs, CO B. Aponso, R. Coppenbarger, Y. Jung, NASA Ames Research Center, Moffett Field, CA; C. O’Connor, G. Lohr, NASA Langley Research Center, Hampton, VA; L. Quon, NASA Ames Research Center, Moffett Field, CA; et al. J. Coupe, D. Milutinovic, University of California, Santa Cruz, Santa Cruz, CA; W. Malik, UARC at NASA Ames Research Center, Moffett Field, CA; Y. Jung, NASA Ames Research Center, Moffet Field, CA Chaired by: A. SARAF, Saab Sensis Corporation 0930 hrs 0900 hrs AIAA-2015-2591 AIAA-2015-2590 Identifying Key Issues and Potential Integration of Uncertain Ramp Area Aircraft Trajectories and Generation Solutions for Integrated Arrival, of Optimal Taxiway Schedules at Departure, Surface Operations by Charlotte Douglas (CLT) Airport Surveying Stakeholder Preferences Tuesday, 23 June 2015 91-ATIO-9 Aberdeen Proving Ground, MD; C. Coyle, J. Sahu, F. Fresconi, Army Research Laboratory, Aberdeen Proving Ground, MD U.S. Military Academy, West Point, NY Chaired by: C. PASILIAO, AFRL/RWWV and C. ROSEMA, US Army AMRDEC 0900 hrs 0930 hrs AIAA-2015-2585 AIAA-2015-2586 Flight Behaviors of a Complex Effect of Canard Deflection on Fin Projectile using a Coupled CFDPerformance of a Fin-Stabilized based Simulation Technique: Free Projectile S. Silton, Army Research Laboratory, Motion Tuesday, 23 June 2015 90-APA-12 C. Ocheltree, S. Choi, Virginia Polytechnic Institute and State University, Blacksburg, VA R. Yamashita, K. Suzuki, University of Tokyo, Kashiwa, Japan 1030 hrs AIAA-2015-2583 Rise Time Prediction of Sonic Boom by Full-Field Simulation with Thermal Nonequilibrium A. Iwakawa, D. Furukawa, Y. Aoki, A. Sasoh, Nagoya University, Nagoya, Japan 1100 hrs AIAA-2015-2584 Free Flight Measurement of Aircraft Model using Aero Ballistic Range Special Session: Low Boom Activities II Technology, Delft, The Netherlands P. Roling, P. Sillekens, R. Curran, Delft University of Technology, Delft, The Netherlands; W. Wilder, KLM Royal Dutch Airlines, Schiphol, The Netherlands 1000 hrs AIAA-2015-2592 The effects of Electric Taxi Systems on airport surface congestion J. Doyle, C. Rosema, Army Aviation and Missile Research Development and Engineering Center, Redstone Arsenal, AL 1000 hrs AIAA-2015-2587 Enhanced Body Vortex Modeling Within Missile Datcom S. Loth, S. Helm, German Aerospace Center (DLR), Braunschweig, Germany 1030 hrs AIAA-2015-2593 Punctuality as KPI for Performance Based Airport Management Terminal & Surface Operations III C. Rosema, Army Aviation and Missile Research Development and Engineering Center, Redstone Arsenal, AL 1030 hrs AIAA-2015-2588 A Comparison of Predictive Methodologies for Missile Configurations with Strakes 1130 hrs AIAA-2015-2578 Development, Startup Operations and Tests of a Propeller Wind Tunnel Test Rig S. Speck, S. Herbst, H. Kim, F. Stein, M. T. Kuhn, ENERCON GmbH, Bremen, Germany; Hornung, Technical University of Munich, Garching, Germany A. Altmikus, ENERCON GmbH, Aurich, Germany; N. Balaresque, Deutsche WindGuard GmbH, Varel, Germany; M. Lippert, University of Applied Sciences, Kiel, Germany C. Schinwald, M. Hornung, Technical University of Munich, Munich, Germany 1100 hrs AIAA-2015-2594 Determining Airport Airside Capacity Utilization: A DemandDriven Approach J. Gan, G. Zha, University of Miami, Coral Gables, FL M. Ellejmi, EUROCONTROL, Brussels, Belgium; B. Weiss, F. Schmitt, S. Straub, Deutsche Flugsicherung GmbH (DFS), Frankfurt, Germany 1130 hrs AIAA-2015-2595 Integration of a Routing Tool in an Advanced Airport Controller Working Position 1100 hrs AIAA-2015-2589 Delayed Detached Eddy Simulation of Projectile Flows Weapons Aerodynamics: Missile/Projectile/Guided-Munitions, Carriage and Store Separation I Chaired by: S. CLIFF, NASA-Ames and K. WAITHE, Gulfstream Aerospace Corporation 0900 hrs 0930 hrs 1000 hrs AIAA-2015-2580 AIAA-2015-2581 AIAA-2015-2582 Design of Optimum EquivalentFeasibility of Supersonic Aircraft Uncertainty Analysis and Robust Area Target for High-Fidelity Low- Concepts for Low-Boom and Flight Design of Low-Boom Concepts Boom Aircraft Design Trim Constraints using Atmospheric Adjoints Tuesday, 23 June 2015 89-APA-11 M. Almond, P. Render, A. Walker, Loughborough University, Loughborough, United Kingdom 1030 hrs AIAA-2015-2576 Design of a swept wing wind tunnel model for study of cross-flow instability Chaired by: J. PINIER, NASA Langley Research Center and G. GATLIN, NASA Langley Research Center 0900 hrs 0930 hrs 1000 hrs AIAA-2015-2573 AIAA-2015-2574 AIAA-2015-2575 Low Speed Wind Tunnel Analysis of Single Hole Simulated Windspeed and Flow Angle Measurement by Tracking of a Investigation of a Circulation Battle Damage on a Wing Using Laser-Induced Breakdown Spark Control Wing for Enhanced Lift Particle Image Velocimetry 1100 hrs AIAA-2015-2577 Numerical Replication and Improvement of Wind Tunnel Tests for Design and Off-Design Operating J. Serpieri, M. Kotsonis, Delft University of Points of Wind Turbine Airfoils Wind Tunnel and Flight Testing Tuesday, 23 June 2015 88-APA-10 Manchester Stemmons B Stemmons A J. Katz, San Diego State University, San Diego, CA 1200 hrs AIAA-2015-2579 Study of the flow field near the AOA sensor of an A320 aircraft Carpenter Ballroom 65 S. Torres, Lockheed Martin Corporation, Rockville, MD 1030 hrs AIAA-2015-2599 Trajectory Accuracy Sensitivity to Modeling Factors S. Tsao, R. Mayer, A. Mahashabde, MITRE Corporation, McLean, VA 1100 hrs AIAA-2015-2600 Trajectory Inefficiency Metric for Measuring Operational Performance of Flights in the National Airspace System M. Moore, NASA Langley Research Center, Hampton, VA 1000 hrs Oral Presentation On-Demand Mobility Technical Pathway: Enabling Low Community Noise, Low Operating Costs, Robust Control, and Ride Quality Applied Complexity Workshop Transformational Flight - On-Demand Mobility J. Li, N. Chen, B. Sridhar, H. Ng, NASA Ames Research Center, Moffett Field, CA 1000 hrs AIAA-2015-2598 Simple Tool for Aircraft NoiseReduction Route Design ATM I - Trajectory Enhancements Grand Ballroom D Metropolitan Ballroom Milan M. Woopen, A. Balan, G. May, RWTH Aachen University, Aachen, Germany 1000 hrs AIAA-2015-2603 An Adjoint-Based hp-Adaptive Petrov-Galerkin Method for Turbulent Flows S. Ojeda, H. Sun, S. Allmaras, D. Darmofal, Massachusetts Institute of Technology, Cambridge, MA Adaptive High-Order Methods Arbor, Ann Arbor, MI University of Tennessee, Chattanooga, Chattanooga, TN 1030 hrs AIAA-2015-2604 An Adaptive Simplex Cut-Cell Method for High-Order Discontinuous Galerkin Discretizations of Conjugate Heat K. Fidkowski, University of Michigan, Ann B. Reza Ahrabi, W. Anderson, J. Newman, Transfer Problems Chaired by: G. MAY, RWTH Aachen and S. ALLMARAS, MIT 0930 hrs 0900 hrs AIAA-2015-2602 AIAA-2015-2601 An Output-Based Adaptive A Unifying Computational Hybridized Discontinuous Galerkin Framework for Adaptive HighMethod on Deforming Domains Order Finite Element Methods Tuesday, 23 June 2015 95-CFD-9 D. Sanjaya, K. Fidkowski, University of Michigan, Ann Arbor, Ann Arbor, MI 1100 hrs AIAA-2015-2605 Improving High-Order Finite Element Approximation Through Geometrical Warping A. Balan, M. Woopen, G. May, RWTH Aachen University, Aachen, Germany 1130 hrs AIAA-2015-2606 Hp-Adaptivity on Anisotropic Meshes for Hybridized Discontinuous Galerkin Scheme Grand Ballroom A 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: Jim Blohowiak Alison Lauderbach Paul C. Lambertson Steve Holt 777X Airplane Level Integration Team 777X Airplane Level Integration Team Systems Engineering & Integration Team 777X Engineering Integrated Strategy, Airplane Level Engineering Integration The Boeing Company The Boeing Company The Boeing Company Boeing Commercial Airplanes Tuesday, 23 June 2015 94-CASE-4 0900 - 1200 hrs M. Moore, NASA Langley Research Center, K. Goodrich, M. Moore, NASA Langley Hampton, VA Research Center, Hampton, VA Chaired by: B. GERMAN, Georgia Institute of Technology 0900 hrs 0930 hrs Oral Presentation Oral Presentation On-Demand Mobility: Aviation’s On-Demand Mobility Technical Future Path to High Speed Regional Pathway: Enabling Ease of Use Mobility and Safety Tuesday, 23 June 2015 93-ATIO-11 F. Linke, German Aerospace Center (DLR), B. Beulze, B. Dancila, R. Botez, University Hamburg, Germany; N. Chen, NASA Ames of Québec, Montréal, Canada Research Center, Moffett Field, CA Chaired by: S. ROY, Washington State Univ 0900 hrs 0930 hrs AIAA-2015-2596 AIAA-2015-2597 Presentation of three methods Impact of Airspace Charges on Transatlantic Aircraft Trajectories results comparison for Vertical B. Sridhar, NASA Ames Research Center, Navigation VNAV trajectory Moffett Field, CA; H. Ng, University of optimization for the Flight California, Santa Cruz, Moffett Field, CA; Management System FMS Tuesday, 23 June 2015 92-ATIO-10 66 University of Kassel, Kassel, Germany; M. A. Porteous, R. Habbit, J. Colmenares, Ruetten, R. Kessler, German Aerospace S. Poroseva, University of New Mexico, Center (DLR), Göttingen, Germany Albuquerque, Albuquerque, NM; S. Murman, NASA Ames Research Center, Moffett Field, CA Y. Yang, S. Özgen, Middle East Technical University, Ankara, Turkey L. Freret, C. Groth, University of Toronto, Toronto, Canada W. McMullan, S. Garrett, University of Leicester, Leicester, United Kingdom C. Roussel, F. Alizard, F. Grasso, Paris Institute of Technology, Paris, France A. Jesus, Technological Institute of Aeronautics (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 1030 hrs AIAA-2015-2619 Further Studies of Adverse Pressure Gradient Effects in Turbulent Channel Flows R. Mittal, Johns Hopkins University, Baltimore, MD LES, DNS, and Hybrid RANS-LES II S. Deng, Delft University of Technology, Delft, The Netherlands; T. Xiao, Nanjing University of Aeronautics and Astronautics, Nanjing, China; M. Percin, B. van Oudheusden, H. Bijl, B. Remes, Delft University of Technology, Delft, The Netherlands 1100 hrs AIAA-2015-2615 Numerical simulation of an X-wing flapping wing MAV by means of a deforming overset grid method Chaired by: N. BISEK, Air Force Reseach Laboratory and A. SESCU, Mississippi State University 0930 hrs 1000 hrs 0900 hrs AIAA-2015-2617 AIAA-2015-2618 AIAA-2015-2616 Simulation of Boundary Layer The Effect of Initial Conditions on Turbulent inflow generation in flows over Biofouled Surfaces Streamwise Vortices in the Plane square duct at supersonic Mach J. Sadique, X. Yang, C. Meneveau, Turbulent Mixing Layer number N. Arora, A. Gupta, Indian Institute of Technology Delhi, New Delhi, India; W. Shyy, Hong Kong University of Science and Technology, Hong Kong, Hong Kong 1030 hrs AIAA-2015-2614 A shifting discontinuous-grid-block lattice Boltzmann method for moving boundary simulations Meshing Techniques II G. Gherman, I. Malael, COMOTI Romanian Research & Development Institute for Gas Turbines, Bucharest, Romania; M. Mihaescu, Royal Institute of Technology (KTH), Stockholm, Sweden; I. Porumbel, COMOTI Romanian Research & Development Institute for Gas Turbines, Bucharest, Romania 1030 hrs AIAA-2015-2610 Jet pump optimization through Reynolds averaged Navier-Stokes Simulation Analysis Turbulent Flow Simulations I Tuesday, 23 June 2015 98-CFD-12 State University, Blacksburg, VA Chaired by: M. PARK, NASA-Langley Research Center and D. THOMPSON, Mississippi State University 0900 hrs 0930 hrs 1000 hrs AIAA-2015-2611 AIAA-2015-2612 AIAA-2015-2613 Comparison of r-Adaptation Implementation of Ball-Center Anisotropic Non-Uniform BlockTechniques for 2-D CFD Applications Spring Analogy Mesh Deformation Based Adaptive Mesh Refinement W. Tyson, J. Derlaga, A. Choudhary, C. Technique with CFD Design for Three-Dimensional Inviscid and Roy, Virginia Polytechnic Institute and Optimization Viscous Flows Tuesday, 23 June 2015 97-CFD-11 Liverpool, Liverpool, United Kingdom Chaired by: S. POROSEVA, The University of New Mexico and S. TIMME, The University of Liverpool 0900 hrs 0930 hrs 1000 hrs AIAA-2015-2607 AIAA-2015-2608 AIAA-2015-2609 Delayed Detached-Eddy Simulation Flow Control of a Rotating Cylinder Simulations of Incompressible of Shock Buffet on Half Wing-Body by the Use of a Structured Surface: Separated Turbulent Flows around A Visualization of Flow Structures Two-Dimensional Bodies with Configuration F. Sartor, S. Timme, University of T. Schomberg, R. Ritz, O. Wünsch, URANS Models in OpenFOAM Tuesday, 23 June 2015 96-CFD-10 Emerald Coral Grand Ballroom B 67 Z. Huang, Tianjin University, Tianjin, China; A. Novikov, Moscow Institute of Physics X. Wu, Imperial College London, London, and Technology, Zhukovsky, Russia; I. United Kingdom Egorov, TsAGI, Zhukovsky, Russia; A. Fedorov, Moscow Institute of Physics and Technology, Zhukovsky, Russia Tuna, M. Amitay, Rensselaer Polytechnic Institute, Troy, NY Nashville, TN; B. Tobalske, University of Montana, Missoula, Missoula, MT; T. Hedrick, University of North Carolina, Chapel Hill, Chapel Hill, NC D. Williams, Illinois Institute of Technology, P. Munday, K. Taira, Florida State Chicago, IL; F. Reissner, Technical University University, Tallahassee, FL of Berlin, Berlin, Germany; D. Greenblatt, H. Muehler-Vahl, Technion--Israel Institute of Technology, Haifa, Israel; C. Strangfeld, Technical University of Berlin, Berlin, Germany Chaired by: M. VISBAL, USAF AFRL/RQVA and K. TAIRA, Florida State University 0930 hrs 1000 hrs 0900 hrs AIAA-2015-2632 AIAA-2015-2633 AIAA-2015-2631 Surface vorticity flux analysis in Measurements of 3-D Stall Cells on Modeling Lift Hysteresis with a Modified Goman-Khrabrov Model on separation control on NACA 0012 2-D Airfoil E. Demauro, H. Dell’Orso, V. Sivaneri, B. Pitching Airfoils airfoil Tuesday, 23 June 2015 101-FD-12 A. Lambert, S. Yarusevych, University of Waterloo, Waterloo, Canada S. Gildersleeve, C. Leong, M. Amitay, Rensselaer Polytechnic Institute, Troy, NY 1030 hrs AIAA-2015-2634 Interactions of a Low Aspect Ratio Dynamic Pin with a Laminar Boundary Layer Airfoil Separation Control S. Hosseinverdi, R. Jacobi, H. Fasel, University of Arizona, Tucson, Tucson, AZ D. Rizzetta, M. Visbal, Air Force Research Laboratory, Wright-Patterson AFB, OH 1100 hrs AIAA-2015-2635 Simulation of a Laminar-Flow Compatible High-Lift Configuration with Flow Control 1030 hrs AIAA-2015-2630 Topology and Flow Structures of Three-Dimensional Separation Bubbles: The Effect of Aspect Ratio J. Kurelek, A. Lambert, S. Yarusevych, University of Waterloo, Waterloo, Canada Unsteady Wing Aerodynamics I Chaired by: K. MOORED, Lehigh University and M. RINGUETTE, University at Buffalo 0900 hrs 0930 hrs 1000 hrs AIAA-2015-2627 AIAA-2015-2628 AIAA-2015-2629 Development of coherent structures Analyzing Vortex Dynamics in the Analysis of cruise flight of the within the laminar separation Laminar Separation Bubble vis calliope hummingbird J. Song, H. Luo, Vanderbilt University, bubble of a NACA0018 airfoil Surface Pressure Measurements Tran, Dassault Group, Saint Cloud, France; China (AVIC), Shanghai, China D. Arnal, ONERA, Toulouse, France; et al. 1100 hrs AIAA-2015-2624 Numerical Simulation of ThreeDimensional Wave Packet in Supersonic Flow over a Compression Corner Tuesday, 23 June 2015 100-FD-11 J. Panda, NASA Ames Research Center, Moffett Field, CA Boundary-Layer Transition 1030 hrs AIAA-2015-2623 A local scattering approach for the effect of abrupt changes on boundary-layer instability and R. Gross, F. Chalot, J. Courty, M. Mallet, D. Z. Wang, Aviation Industry Corporation of transition: a numerical method Chaired by: E. MARINEAU, AEDC White Oak and J. KLENTZMAN, Baylor University 0900 hrs 0930 hrs 1000 hrs AIAA-2015-2620 AIAA-2015-2621 AIAA-2015-2622 Turbulent Density Fluctuations in Automatic transition prediction in Large-Eddy Simulation of Thermal Boundary Layers Studied an industrial Navier-Stokes solver Transitional Flows on a Compressor via Molecular Rayleigh scattering using higher-order finite elements Blade Tuesday, 23 June 2015 99-FD-10 M. Iorio, Airbus, Madrid, Spain; L. Gonzalez, Technical University of Madrid, Madrid, Spain; A. Martinez, Airbus, Filton, United Kingdom 1130 hrs AIAA-2015-2636 Global stability analysis of a compressible turbulent flow around a high-lift configuration Senators Lecture Hall Govenors Lecture Hall 1200 hrs AIAA-2015-2626 Acoustic radiation due to scattering of T-S wave by nonlinear roughness in subsonic boundary layer flows M. Dong, Tianjin University, Tianjin, China; X. Wu, Imperial College London, London, M. Choudhari, F. Li, NASA Langley Research Center, Hampton, VA; M. Bynum, United Kingdom AMA Research Associates, Hampton, VA; M. Kegerise, R. King, NASA Langley Research Center, Hampton, VA 1130 hrs AIAA-2015-2625 Computations of Disturbance Amplification Behind Isolated Roughness Elements and Comparison with Measurements Sapphire 68 A. Vashishtha, University of Tokyo, Kashiwa, Japan; Y. Watanabe, University of Tokyo, Bunkyo, Japan; K. Suzuki, University of Tokyo, Kashiwa, Japan 0930 hrs Oral Presentation STABL-3D Software Overview A. Renner, F. Thompson, V. Kalivarapu, E. Winer, J. Oliver, Iowa State University, Ames, IA; B. Gilmore, Deere & Company, Moline, IL; et al. CO; M. Hafez, University of California, Davis, Davis, CA J. Knowles, Loughborough University, Loughborough, United Kingdom; E. Coetzee, Airbus, Bristol, United Kingdom 1030 hrs AIAA-2015-2640 Numerical Simulation Exploring Supersonic Flow Over a WallMounted Half-Cylinder Turret Shock-Dominated Flows 1100 hrs AIAA-2015-2641 Numerical Investigation of Shockinduced Laminar Separation Bubble in Supersonic Flows N. Bhagat, Wright State University, Beavercreek, OH; E. Alyanak, Air Force Research Laboratory, Wright-Patterson AFB, OH; D. Allison, Optimal Flight Sciences, LLC, Dayton, OH 1000 hrs AIAA-2015-2648 Geometry Driven High Fidelity Stability Derivatives Obtained Using Automated CFD Analysis Process E. Marineau, D. Lewis, J. Lafferty, G. Moraru, Arnold Engineering Development Center, Silver Spring, MD 1000 hrs Oral Presentation Mach 10 Boundary Layer Transition Experiments on Sharp and Blunted Cones P. Albuquerque, P. Gamboa, M. Silvestre, University of Beira Interior, Covilha, Portugal 1100 hrs AIAA-2015-2650 Multidisciplinary and Multilevel Aircraft Design Methodology Using Enhanced Collaborative Optimization W. Yang, S. Tang, Z. Xu, Northwestern Aerospace Center (DLR), Braunschweig, Polytechnical University, Xi’an, China Germany; W. Krüger, H. Schmidt, German Aerospace Center (DLR), Göttingen, Germany 1030 hrs AIAA-2015-2655 Control Enhanced and Parameterized Load Relief technology for a Launch Vehicle Q. Xiaojie, W. Su, Y. Tang, Aviation Industry Corporation of China (AVIC), Wuxi, China F. Nicolosi, A. De Marco, L. Attanasio, D. Gambardella, University of Naples “Federico II”, Naples, Italy 1130 hrs AIAA-2015-2651 Development of a Java-based framework for aircraft preliminary design and optimization 1100 hrs AIAA-2015-2656 The mode switch control research of small-type parallel TBCC engine based on SQP method Guidance, Control, and Dynamics II R. Entz, G. Scherer Schwening, R. Fernandes de Oliveira, Airbus, Munich, Germany 1030 hrs AIAA-2015-2649 Application of automatic algorithm generation to air-to-air refueling scheduling Applications I B. Wheaton, Johns Hopkins University Applied Physics Laboratory, Laurel, MD; H. Johnson, GoHypersonic, Inc., Dayton, OH; R. Wagnild, Sandia National Laboratories, Albuquerque, NM 1030 hrs Oral Presentation Stability Analysis of Hypersonic Flows Using STABL-3D ITAR - Hypersonic Flow Phenomena (Invited) 1130 hrs AIAA-2015-2642 On unsteady shock wave reflections from wedges with straight and concave tips R. Kimmel, Air Force Research Laboratory, P. Morgan, Ohio Aerospace Institute, J. Sivasubramanian, H. Fasel, University of F. Alzamora Previtali, E. Timofeev, McGill Wright-Patterson AFB, OH; D. Prabhu, ERC, Dayton, OH; M. Visbal, Air Force Research Arizona, Tucson, Tucson, AZ University, Montréal, Canada; H. Kleine, Inc., Moffett Field, CA Laboratory, Wright-Patterson AFB, OH University of New South Wales at the Australian Defence Force Academy, Canberra, Australia Chaired by: T. ALEXEEV, University of California Davis and J. KNOWLES, Loughborough University 0930 hrs 1000 hrs 0900 hrs AIAA-2015-2653 AIAA-2015-2654 AIAA-2015-2652 A Bifurcation Study of a Dynamic Multi-Fidelity Simulation of Cargo Semi-Implicit Numerical Airdrop: From the Payload Bay to the Simulations of Nonlinear Dynamics Model of a Nose Landing Gear Mechanism Subjected to External Ground of Beams, Plates, and Shells T. Alexeev, Siemens Energy, Inc., Boulder, Disturbances T. Jann, S. Geisbauer, N. Bier, German Tuesday, 23 June 2015 105-MST-5 North Carolina State University, Raleigh, NC Chaired by: A. NAJAFI, ANSYS, Inc. and P. PIPERNI, Bombardier Inc 0930 hrs 0900 hrs AIAA-2015-2647 AIAA-2015-2646 Optimization of System Evolvability An Application of Conceptual Design and Multidisciplinary Under Uncertainty J. Watson, J. Allen, C. Mattson, Brigham Analysis Transitioning to Detailed Young University, Provo, UT; S. Ferguson, Design Stages Tuesday, 23 June 2015 104-MAO-3 H. Johnson, GoHypersonic, Inc., R. Kimmel, Air Force Research Laboratory, Minneapolis, MN Wright-Patterson AFB, OH Chaired by: K. CASPER 0900 hrs Oral Presentation HTV-2 Boundary Layer Transition Summary and Lessons Learned Tuesday, 23 June 2015 103-ITAR-1 Washington, DC; T. Young, Berkeley Research Associates, Beltsville, MD; D. Schwer, P. Matic, Naval Research Laboratory, Washington, DC Chaired by: M. GAMBA, University of Michigan and J. POGGIE, USAF AFRL/RBAC 0900 hrs 0930 hrs 1000 hrs AIAA-2015-2637 AIAA-2015-2638 AIAA-2015-2639 Study of Bow-Shock Instabilities HIFiRE-1 Turbulent Shock Boundary Assessing Blast Loading Within in front of Hemispherical Shell at Layer Interaction -Flight Data and Obstacle Arrays D. Mott, Naval Research Laboratory, Hypersonic Mach Number 7 Computations Tuesday, 23 June 2015 102-FD-13 Travertine Madrid Morocco Topaz 69 D. Smith, University of Kentucky, Lexington, Lexington, KY; T. White, ERC, Inc., Moffett Field, CA; A. Martin, University of Kentucky, Lexington, Lexington, KY D. Driver, NASA Ames Research Center, Moffett Field, CA; S. Sepka, ERC, Inc., Moffett Field, CA A ticket is required and included in the conference registration fee where indicated. Tuesday, 23 June 2015 111-LNCH-1 1230 - 1400 hrs Awards Luncheon: Celebrating Achievements in Aerospace Sciences BrianQuigley Managing Director Flight Operations United Airlines Grand Ballroom E Rosetta Miro Chantilly Ballroom East Chantilly Ballroom West Dan Smiley Vice President for Systems Operations, Federal Aviation Administration Air Traffic Office Moffett Field, CA; R. Lewis, NASA Johnson B. Helber, T. Alessandro, O. Chazot, M. Space Center, Houston, TX Thierry, von Kármán Institute for Fluid Dynamics, Rhode-Saint-Genèse, Belgium 1130 hrs AIAA-2015-2668 Physico-Chemistry of CN in the J. Balboni, T. Gokcen, F. Hui, P. Graube, P. Boundary Layer of Graphite in Morrissey, NASA Ames Research Center, Nitrogen Plasmas 1100 hrs AIAA-2015-2667 Consolidating NASA’s Arc-Jet 1130 hrs AIAA-2015-2662 Investigation of Thermal Cycling Property of Thermal Barrier Coatings with Laser Deposited Mesh Structure A. Palla, J. Zimmerman, D. Carroll, CU Aerospace, Champaign, IL; C. Mitsingas, S. Shi, W. Chen, Z. Hong, D. Gao, Aviation S. Hammack, T. Lee, University of Illinois, Industry Corporation of China (AVIC), Urbana-Champaign, Urbana, IL Shanghai, China 1100 hrs AIAA-2015-2661 Multiphysics simulations of plasmaassisted combustion dynamics in a direct-coupled microwave reactor Day in the Life of Operations - Effectively Managing Disruption P. Bauman, State University of New York, Buffalo, NY 1030 hrs AIAA-2015-2666 Side Arm Reactor Study of Copper Catalysis Moderator: Neil Planzer, Vice President, Air Traffic Management, Boeing Commercial Airplanes Panelits: Tim Campbell Jim Crites Senior Vice President, Air Operations Executive Vice President of Operations DFW International Airport American Airlines Tuesday, 23 June 2015 109-F360-3 0930 - 1200 hrs AL; I. Terrazas-Salinas, NASA Ames Research Center, Moffett Field, CA C. Dumitrache, A. Yalin, Colorado State University, Fort Collins, CO 1030 hrs AIAA-2015-2660 Towards Laser Ignition by Rapid Heating of Water Vapor Plasma Assisted Combustion Networking Coffee Break Plasma and Arc Jet Testing, Diagnostics and Computational Methods C. Dumitrache, C. Rose, A. Yalin, Colorado A. Firsov, Russian Academy of Sciences, State University, Fort Collins, CO Moscow, Russia; S. Leonov, University of Notre Dame, Notre Dame, IN 1000 hrs AIAA-2015-2659 Magnetic positioning of the electric discharge in the volume of supersonic flow Chaired by: M. WINTER, University of Kentucky and P. YEE, The Aerospace Corporation 0930 hrs 1000 hrs 0900 hrs AIAA-2015-2664 AIAA-2015-2665 AIAA-2015-2663 Comparisons of PICA In-depth Material Enabling the Statistical Calibration Arc Jet Facility Test Condition Performance and Ablator Response of Active Nitridation of Graphite by Predictions Using the ADSI Code G. Palmer, D. Prabhu, ERC, Inc., Huntsville, Modeling from MEDLI Arc Jet Tests Atomic Nitrogen Tuesday, 23 June 2015 108-TP-5 S. Jacobs, K. Xu, University of Alabama, Huntsville, Huntsville, AL Chaired by: K. XU, University of Alabama in Huntsville 0900 hrs 0930 hrs AIAA-2015-2657 AIAA-2015-2658 Electron Temperature in a Laser-Induced Heating Using a Methane-Air Flame under a DC Non-Resonant Dual-Pulse Approach Electric Field with Application to Laser Ignition Tuesday, 23 June 2015 107-PDL-4 Tuesday, 23 June 2015 106-NW-3 0900 - 0930 hrs 70 1430 hrs AIAA-2015-2676 Stabilized Time-domain Impedance Model and the Application in Bypass Duct Noise Simulations 1500 hrs AIAA-2015-2684 The Acoustic Environment of the NASA Glenn 9- by 15-Foot LowSpeed Wind Tunnel P. Salas, S. Moreau, University of Sherbrooke, Sherbrooke, Canada 1500 hrs AIAA-2015-2688 Wall Pressure Spectra on a DU96-W-180 Profile From Low to Pre-Stall Angles of Attack Y. Yauwenas, N. Ahmed, University of New A. Suryadi, M. Herr, German Aerospace South Wales, Kensington, Australia Center (DLR), Braunschweig, Germany Chaired by: C. DOOLAN, The University of Adelaide 1430 hrs 1400 hrs AIAA-2015-2687 AIAA-2015-2686 Aerodynamic Noise Simulation Aeroacoustic Simulations of of an Airfoil in a Periodically a Simplified High-Lift Device Accounting for Installations Effects Fluctuating Freestream Tuesday, 23 June 2015 115-AA-19 D. Stephens, NASA Glenn Research Center, H. Murray, D. Wisda, W. Alexander, M. T. Tatsukawa, T. Nonomura, A. Oyama, K. Cleveland, OH Nelson, W. Devenport, Virginia Polytechnic Fujii, Japan Aerospace Exploration Agency Institute and State University, Blacksburg, (JAXA), Kanagawa, Japan VA; S. Glegg, Florida Atlantic University, Boca Raton, FL Chaired by: C. BAILLY, Ecole Centrale de Lyon 1400 hrs 1430 hrs AIAA-2015-2682 AIAA-2015-2683 Sound and Distortion Produced Nozzle-to-Ground Distance Effect by a Braking Rotor Operating in on Nondominated Solutions of a Planar Boundary Layer with Multiobjective Aeroacoustic Flame Application to Wind Turbines Deflector Design Problem Tuesday, 23 June 2015 114-AA-18 J. Gill, R. Fattah, X. Zhang, University of Southampton, Southampton, United Kingdom 1500 hrs AIAA-2015-2677 Evaluation and Development of Non-Reflective Boundary Conditions for Aeroacoustic Simulations 1500 hrs AIAA-2015-2671 Prediction of Slat Broadband Noise with RANS Results B. Bai, X. Li, Y. Guo, Beihang University, University of Southampton, Southampton, Beijing, China; F. Thiele, Technical United Kingdom; T. Nodé-Langlois, Airbus, University of Berlin, Berlin, Germany Toulouse, France P. Cinnella, Università del Salento, Lecce, X. Liu, X. Huang, Peking University, Italy; X. Gloerfelt, X. Merle, Paris Institute Beijing, China of Technology, Paris, France Chaired by: S. CARO, CD-Adapco 1400 hrs AIAA-2015-2675 Direct and inverse uncertainty quantification of acoustic refraction phenomena through a shear layer Tuesday, 23 June 2015 113-AA-17 G. Grasso, J. Christophe, C. Schram, von Kármán Institute for Fluid Dynamics, Rhode-Saint-Genèse, Belgium Chaired by: J. DELFS, DLR - German Aerospace Center 1400 hrs 1430 hrs AIAA-2015-2669 AIAA-2015-2670 Synthetic Turbulence Methods for Prediction of low-speed fan trailing-edge noise based on RANS Leading Edge Noise Predictions and on scale resolved simulations F. Gea-Aguilera, X. Zhang, X. Chen, J. Gill, Tuesday, 23 June 2015 112-AA-16 I. Belyaev, G. Faranosov, N. Ostrikov, TsAGI, Moscow, Russia; G. Paranin, OJS Irkut Corporation, Moscow, Russia C. Temmler, M. Schulze, T. Sattelmayer, Technical University of Munich, Munich, Germany 1600 hrs AIAA-2015-2679 Acoustic Scattering Matrices for Higher-Order Modes for Simple Orifice Configurations with Flow L. Lopes, NASA Langley Research Center, Hampton, VA 1600 hrs AIAA-2015-2673 Compact Assumption Applied to the Monopole Term of Farassat’s Formulation (NLR), Emmeloord, The Netherlands; P. Sijtsma, Pieter Sijtsma Advanced AeroAcoustics, Wezep, The Netherlands 1600 hrs AIAA-2015-2690 A parametric experimental study of jet-flap interaction noise for a realistic small-scale swept wing M. Tuinstra, National Aerospace Laboratory model 1530 hrs AIAA-2015-2689 Suppression of spurious noise sources in airfoil self-noise measurements Airframe Noise II D. Luquet, R. Marchiano, F. Coulouvrat, Pierre and Marie Curie University, Paris, France; I. Salah El Din, ONERA, Meudon, France; A. Loseille, French National Institute for Research in Computer Science and Control (INRIA), Le Chesnay, France 1530 hrs AIAA-2015-2685 Sonic Boom Assessment of a Hypersonic Transport Vehicle with Advanced Numerical Methods General Acoustics I M. Muriel Gracia, W. De Roeck, W. Desmet, Catholic University of Leuven, Leuven, Belgium 1530 hrs AIAA-2015-2678 Implementation of a surface based coupling approach in a high-order DG aeroacoustics propagation solver CAA Propagation and Scattering I N. Reiche, M. Lummer, R. Ewert, German Aerospace Center (DLR), Braunschweig, Germany 1530 hrs AIAA-2015-2672 Towards high-lift noise from Fast Multipole BEM with anisotropic synthetic turbulence sources CAA Sound Generation II N. Ostrikov, S. Denisov, TsAGI, Moscow, Russia 1630 hrs AIAA-2015-2691 Airframe Shielding of Noncompact Aviation Noise Sources: Theory and Experiment V. Clair, G. Gabard, University of Southampton, Southampton, United Kingdom 1630 hrs AIAA-2015-2680 Numerical assessment of the scattering of acoustic waves by turbulent structures E. Sundström, M. Mihaescu, Royal Institute of Technology (KTH), Stockholm, Sweden H. Yao, L. Davidson, Chalmers University of Technology, Göteborg, Sweden; S. Peng, Swedish Defense Research Agency (FOI), Stockholm, Sweden; F. Capizzano, M. Barbarino, G. Mingione, Italian Aerospace Research Center (CIRA), Capua, Italy Lalique 1700 hrs AIAA-2015-2692 Assessment of Conceptual Noise Reduction Devices for A Main Landing Gear using SNGR Method Inverness S. Swift, G. Blaisdell, Purdue University, West Lafayette, IN; A. Lyrintzis, EmbryRiddle Aeronautical University, Daytona Beach, FL Fleur-de-lis B 1700 hrs AIAA-2015-2681 Enhancements of a time-domain equivalent source method for acoustic scattering 1630 hrs AIAA-2015-2674 Centrifugal Compressor: The Sound of Surge Fleur-de-lis A 71 J. Dias, Brazilian Air Force, São José dos Campos, Brazil of Aeronautics (ITA), São José dos Campos, Brazil; L. Santos, Embraer, São José dos Campos, Brazil Research Laboratory, Aberdeen Proving Ground, MD Z. Enjiao, T. Chao, S. Wang, M. Yang, Harbin Institute of Technology, Harbin, China L. Sherry, George Mason University, Fairfax, VA R. Kumar, PEC University of Technology, Chandigarh, India; A. Ghosh, Indian Institute of Technology Kanpur, Kanpur, India 1530 hrs AIAA-2015-2707 Nonlinear Aerodynamic Modeling from Flight Data at High Angles of Attack Using Neural-Gauss-Newton Method E. Oliveira, Aeronautics and Space Institute (IAE), São José dos Campos, Brazil; P. Gasbarri, University of Rome “La Sapienza”, Rome, Italy; I. Milagre da Fonseca, Technological Institute of Aeronautics (ITA), São José dos Campos, Brazil Ann Arbor, Ann Arbor, MI J. Pei, P. Rothhaar, NASA Langley Research Center, Hampton, VA 1600 hrs AIAA-2015-2712 Demonstration of Launch Vehicle Slosh Instability on a Pole-Cart R. Klock, C. Cesnik, University of Michigan, Platform 1530 hrs AIAA-2015-2711 Aerothermoelastic Reduced-Order Model of a Hypersonic Vehicle Launch Vehicles, Missiles, and Projectile Flight Mechanics D. Kaya, A. Kutay, Middle East Technical University, Ankara, Turkey Chaired by: T. LAVIN, Sandia National Laboratories and F. FRESCONI, US Army Research Lab 1430 hrs 1500 hrs 1400 hrs AIAA-2015-2709 AIAA-2015-2710 AIAA-2015-2708 Delivery of Modular Lethality via a An Adaptive Parameter Cooperative Flight Dynamics Numerical Guidance Law for Multiple flight Computation of a Sounding Rocket Parent-Child Concept F. Fresconi, M. Fermen-Coker, Army vehicles Including Elastic Deformation Model Tuesday, 23 June 2015 119-AFM-8 J. Grauer, E. Morelli, NASA Langley Research Center, Hampton, VA T. Takahashi, Arizona State University, Tempe, AZ 1600 hrs AIAA-2015-2702 Design for Resilience in Autonomous Systems: Lessons Learned from Controlled Flight into Stall Accidents M. Jones, W. Watson, D. Nark, B. Howerton, NASA Langley Research Center, Hampton, VA 1600 hrs AIAA-2015-2697 Evaluation of Variable-Depth Liner Configurations for Increased Broadband Noise Reduction Flight Test, System Identification, and Parameter Estimation L. Young, NASA Ames Research Center, Moffett Field, CA Chaired by: J. GRAUER, NASA Langley Research Center and J. BRANDON, NASA-Langley Research Center 1400 hrs 1430 hrs 1500 hrs AIAA-2015-2704 AIAA-2015-2705 AIAA-2015-2706 A New Formulation of the FilterUnsteady and Post-Stall Model Modeling and Simulation of a Error Method for Aerodynamic Identification Using Dynamic Stall Quadrotor using Curve Fitting Parameter Estimation in Turbulence Maneuvers Method Tuesday, 23 June 2015 118-AFM-7 Tempe, AZ 1530 hrs AIAA-2015-2701 Optimal Climb Trajectories Through Explicit Simulation Aircraft Performance Studies 1530 hrs AIAA-2015-2696 Nonlinear impedance modeling of resonator with high intensity incident acoustic wave Duct Acoustics III J. Xu, X. Li, Y. Guo, Beihang University, Beijing, China C. Ji, D. Zhao, S. Li, X. Li, Nanyang Technological University, Singapore, Singapore 1500 hrs AIAA-2015-2695 Effect of Porosity and Joint Biasgrazing Flow on the Acoustic Damping Performance of Double- and Singlelayer Perforated Liners 1500 hrs AIAA-2015-2700 Simulated Tiltrotor Aircraft Operation in Close Proximity to a Building in Wind and Ground-Effect R. Silva, D. Ferrari, Technological Institute Conditions Chaired by: C. BIL, RMIT University and W. ANEMAAT, DARcorporation 1400 hrs 1430 hrs AIAA-2015-2698 AIAA-2015-2699 The Impact of ATTCS on Reduced- Uncertainty Modeling and Thrust Takeoff Field Performance Assessment in Aircraft Evacuation T. Takahashi, Arizona State University, Simulation Tuesday, 23 June 2015 117-ACD-3 D. Nark, M. Jones, NASA Langley Research K. Mitchell, Virginia Polytechnic Institute Center, Hampton, VA; D. Sutliff, NASA and State University, Blacksburg, VA Glenn Research Center, Cleveland, OH Chaired by: C. ROYALTY, Honeywell International, Inc. 1400 hrs 1430 hrs AIAA-2015-2693 AIAA-2015-2694 Design Optimization of Broadband Modeling of Broadband Liners Acoustic Liners Through Finite Applied to the Advanced Noise Element Efficacy Studies Control Fan Tuesday, 23 June 2015 116-AA-20 S. Lazarus, Eaton Corporation, Pune, India; S. Frischemeier, M. Holland, J. Skinner, A. Smith, Eaton Corporation, Jackson, MS 1630 hrs AIAA-2015-2703 Adaptive and Intelligent power control allocation and scheduling for a More Electric Aircraft Plum Blossom B Plum Blossom A Wyeth Obelisk A 72 G. Garrard, M. Mills, Arnold Engineering Development Complex, Tullahoma, TN S. Kamali, B. Reza Ahrabi, R. Webster, K. Sreenivas, University of Tennessee, Chattanooga, Chattanooga, TN R. Liebeck, The Boeing Company, Huntington Beach, CA B. Bathel, NASA Langley Research Center, C. Johansen, University of Calgary, Hampton, VA Calgary, Canada 1600 hrs Oral Presentation Introduction to Laser Induced Fluorescence Spectroscopy for Hypersonic Nonequilibrium Flows J. Cheng, M. Lowenberg, University of Bristol, Bristol, United Kingdom; X. Wang, J. Yu, Nanjing University of Science and Technology, Nanjing, China 1530 hrs AIAA-2015-2717 Wind Tunnel Wall Interference Effects on an Oscillating Aerofoil in the Stall Regime P. Spalart, The Boeing Company, Seattle, WA; S. Allmaras, Massachusetts Institute of Technology, Cambridge, MA Topaz Carpenter Ballroom Stemmons B 1700 hrs Oral Presentation Introduction to CARS Spectroscopy for Hypersonic Nonequilibrium Flows Obelisk B P. Danehy, NASA Langley Research Center, A. Cutler, George Washington University, Hampton, VA Washington, DC 1630 hrs Oral Presentation Introduction to Raman Rayleigh Spectroscopy for Hypersonic Nonequilibrium Flows 1600 hrs AIAA-2015-2718 Origins and Further Development of the Jameson-Schmidt-Turkel Scheme (Invited) A. Jameson, Stanford University, Stanford, CA Special Session: Historically Significant/Influential Papers in Applied Aerodynamics Y. Zhang, A. van Zuijlen, G. van Bussel, Delft University of Technology, Delft, The Netherlands 1500 hrs AIAA-2015-2716 Massively separated turbulent flow simulation around non-rotating MEXICO blade by means of RANS and DDES approaches in OpenFOAM Applied CFD & Numerical Correlations with Experimental Data II Wales, Canberra, Australia 1530 hrs Oral Presentation Introduction to Molecular Tagging Velocimetry for Hypersonic Nonequilibrium Flows Chaired by: B. MCGRATH, JHU/Applied Physics Laboratory and J. PINIER, NASA Langley Research Center 1500 hrs 1400 hrs Oral Presentation Oral Presentation The Spalart-Allmaras Turbulence Model Paper of 1992 (Invited) Thoughts on working with AMO Smith (Invited) Tuesday, 23 June 2015 123-APA-14 University in St. Louis, St. Louis, MO Chaired by: N. HARIHARAN, CREATE-AV and C. SHENG, University of Toledo 1400 hrs 1430 hrs AIAA-2015-2714 AIAA-2015-2715 CFD Analysis of Counter-Rotating Numerical Simulation of Open Rotors Using a Rotating Compressible Flow in a Diffusing Actuator Disk Model S-duct with and without Vortex M. Malick, R. Agarwal, Washington Generators Tuesday, 23 June 2015 122-APA-13 P. Danehy, NASA Langley Research Center, Lexington, Lexington, KY Hampton, VA Design of Experiment Molecular-Based Optical Diagnostics for Hypersonic Nonequilibrium Flows Chaired by: P. DANEHY, NASA Langley Research Center and M. WINTER, University of Kentucky 1400 hrs 1430 hrs 1500 hrs Oral Presentation Oral Presentation Oral Presentation Introduction and Application Introduction to Emission Introduction to Absorption Considerations for Optical Spectroscopy for Hypersonic Spectroscopy for Hypersonic Diagnostics in Hypersonic Nonequilibrium Flows Nonequilibrium Flows M. Winter, University of Kentucky, S. O’Byrne, University of New South Nonequilibrium Flows Tuesday, 23 June 2015 121-AMT-8/FD-14/TP-6/GT-8 Commo, NASA Langley Research Center, Hampton, VA Chaired by: G. GARRARD, Aerospace Testing Alliance (ATA) and D. YODER 1400 hrs 1430 hrs AIAA-2015-2713 Oral Presentation Comparison between DOE and Case Studies for the Statistical 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 Tuesday, 23 June 2015 120-AMT-7/GT-7 73 N. Namura, K. Shimoyama, S. Obayashi, Tohoku University, Sendai, Japan R. Bartels, R. Scott, NASA Langley Research Center, Hampton, VA W. Fredericks, NASA Langley Research Center, Hampton, VA ATM II - Air Traffic Analysis (DLR), Braunschweig, Germany; M. Bauer, T. N. Findanis, University of New South Grund, Technical University of Berlin, Berlin, Wales, Sydney, Australia Germany; C. Huehne, P. Scholz, Technical University of Braunschweig, Braunschweig, Germany; et al. 1600 hrs AIAA-2015-2729 Passive Flow Control Applied to a NACA23012 Airfoil In A Subsonic V. Ciobaca, J. Wild, German Aerospace Center Flow 1530 hrs AIAA-2015-2728 Wind Tunnel Experiments with Active Flow Control for an Outer Wing Model M. Patterson, N. Borer, NASA Langley Research Center, Hampton, VA; B. German, Georgia Institute of Technology, Atlanta, GA 1500 hrs Oral Presentation Comparison of Computational Aerodynamics Tools for Predicting M. Moore, NASA Langley Research Center, Low-Speed Performance of a Hampton, VA Distributed Propeller Concept Hampton, VA 1600 hrs Oral Presentation Hoverless VTOL Hyper Commuter Mission Concept V. Ahuja, R. Hartfield, Flightstream, Auburn, AL J. Seidel, C. Fagley, T. McLaughlin, U.S. Air Force Academy, Colorado Springs, CO J. Selfridge, G. Tao, University of Virginia, Charlottesville, Charlottesville, VA Metropolitan Ballroom Milan Stemmons C Stemmons A 1700 hrs AIAA-2015-2735 Centrifugally Stiffened Rotor: A Complete Derivation of the Plant Model with Nonlinear Dynamics 1630 hrs AIAA-2015-2730 Computations of Active Open-Loop Flow Control on a Fluttering Wing Y. Babbar, V. Suryakumar, T. Strganac, Texas A&M University, College Station, TX; A. Mangalam, Tao of Systems Integration, Inc., Hampton, VA 1630 hrs AIAA-2015-2724 Measurement and Modeling of Aeroelastic Response under Gust 1630 hrs AIAA-2015-2734 Predicting the Aero Loads Behind a Propeller in the Presence of a Wing S. Bousfield, Samson Aircraft, Auburn, CA M. Moore, NASA Langley Research Center, Using Flightstream 1530 hrs Oral Presentation The Samson Switchblade MultiMode Aircraft Concept Transformational Flight - Advanced Concepts 1500 hrs AIAA-2015-2733 Identification of Aircraft Conflict ResolutionTypes from Recorded Flight Data Institute of Technology Madras, Chennai, India J. Busquets, City University London, London, United Kingdom; A. Evans, S. Shin, K. Kim, I. Hwang, Purdue University College London, London, University, West Lafayette, IN United Kingdom; E. Alonso, City University London, London, United Kingdom 1430 hrs AIAA-2015-2732 Application of Data Mining in Air Traffic Forecasting Chaired by: N. BORER, NASA Langley Research Center 1430 hrs 1400 hrs Oral Presentation Oral Presentation LEAPTech Distributed Electric NASA GL-10 Tilt-Wing Tilt-Tail Propulsion Integration Concept Concept Tuesday, 23 June 2015 127-ATIO-13 M. Drew, University of California, Santa Cruz, Moffett Field, CA; K. Sheth, NASA Ames Research Center, Moffett Field, CA Chaired by: A. RAO, Purdue University 1400 hrs AIAA-2015-2731 A Wavelet Analysis Approach for Categorizing Air Traffic Behavior Tuesday, 23 June 2015 126-ATIO-12 R. Bevan, D. Poole, C. Allen, T. Rendall, University of Bristol, Bristol, United Kingdom S. Lebofsky, E. Ting, K. Trinh, Stinger E. Tal, Delft University of Technology, Delft, Ghaffarian Technologies, Inc., Mountain The Netherlands; N. Nguyen, NASA Ames View, CA; N. Nguyen, NASA Ames Research Center, Moffett Field, CA Research Center, Moffett Field, CA 1600 hrs AIAA-2015-2723 Optimization for Load Alleviation of Truss-Braced Wing Aircraft With Variable Camber Continuous Trailing Edge Flap Flow Control Applications & Demonstrations (Active & Passive) II Langley Research Center, Hampton, VA Chaired by: M. OL, US Air Force Reseach Laboratory and G. ZHA, University of Miami 1400 hrs 1430 hrs 1500 hrs AIAA-2015-2725 AIAA-2015-2726 AIAA-2015-2727 Simulation and Surrogate-Based Multipoint Design of Vortex Flow Control in a Mach 4.0 Inlet Design of Rectangular Vortex Generators on a Swept Infiniteby Slotted Wedge-shaped Vortex Generators for Tiltrotor Aircraft Wing under Cruise and Critical Generators D. Varma, S. Saurav, S. Ghosh, Indian Wings Condition Tuesday, 23 June 2015 125-APA-16 Heeg, J. Hur, M. Sanetrik, NASA Langley Research Center, Hampton, VA; et al. 1530 hrs AIAA-2015-2722 Unsteady Aeroservoelastic Modeling of Flexible Wing Generic Transport Aircraft with Variable Camber Continuous Trailing Edge Flap Special Session: Aerodynamic-Structural Modeling, Optimization, and Test Techniques for Flexible Wing Technology II Chaired by: W. SILVA, NASA-Langley Research Center and B. STANFORD, NASA Langley Research Center 1400 hrs 1430 hrs 1500 hrs AIAA-2015-2719 AIAA-2015-2720 AIAA-2015-2721 Analysis of Limit Cycle Oscillation Computational Aeroelastic Analyses Ongoing Fixed Wing Research Data from the Aeroelastic Test of a Low-Boom Supersonic within the NASA Langley of the SUGAR Truss-Braced Wing Configuration Aeroelasticity Branch R. Bartels, P. Chwalowski, C. Funk, J. W. Silva, M. Sanetrik, P. Chwalowski, NASA Model Tuesday, 23 June 2015 124-APA-15 74 1500 hrs AIAA-2015-2738 Development and Application of a Parametric Design Tool for Design Iterations of Large Turboprop Aircraft CASE Session I & II U. Rehmanjan, Qantas Airways, Ltd., Sydney, Australia 1530 hrs AIAA-2015-2739 3D Printed Parts for Quick Turnaround Aircraft Projects and Legacy Issues Product Design and Support 1630 hrs AIAA-2015-2741 Toward Efficient Model-Based Development of Aerospace Applications B. Vermeire, F. Witherden, P. Vincent, Imperial College London, London, United Kingdom S. Spiegel, H. Huynh, J. DeBonis, NASA Glenn Research Center, Cleveland, OH Chaired by: Z. WANG, University of Kansas and B. VERMEIRE, McGill University 1430 hrs 1400 hrs AIAA-2015-2744 AIAA-2015-2743 De-Aliasing through OverOn the Utility of High-Order Integration Applied to the Flux Methods for Unstructured Grids: A Comparison Between PyFR and Reconstruction and Discontinuous Galerkin Methods Industry Standard Tools Tuesday, 23 June 2015 130-CFD-13 Y. Abe, University of Tokyo, Sagamihara, Japan; T. Haga, T. Nonomura, K. Fujii, Japan Aerospace Exploration Agency (JAXA), Sagamihara, Japan 1500 hrs AIAA-2015-2745 Fully-conservative High-order FR Scheme on Moving and Deforming Grids Z. Sun, F. Xiao, Tokyo Institute of Technology, Yokohama, Japan 1530 hrs AIAA-2015-2746 A WENO-type Limiter for 4th Order Constrained Derivative Flux Reconstruction Method Flux Reconstruction Methods 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 Technical Fellow CTO The Boeing Company ANSYS Brenda Nuhfer Program Manager UTC/Pratt & Whitney Grand Ballroom A 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. 1545-1730 hrs 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: Robert (Rob) Simons Jason Merret Rick Mange Technical Fellow Technical Specialist, Gulfstream Aerospace Performance Engineering F-35 PNR Program Manager The Boeing Company Gulfstream Aerospace Corporation Lockheed Martin Aeronautics Steuben 1700 hrs AIAA-2015-2742 Reliability Analysis of the Integrated Modular Avionics System Using AADL and GSPN Manchester 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 Texas, Arlington, Arlington, TX Nowak, Eaton Corporation, Cleveland, OH Aviation University of China, Tianjin, China 1600 hrs AIAA-2015-2740 UGV and UAV Cooperation for Constructing Probabilistic Threat Exposure Map (PTEM) 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. 1400-1530 hrs Tuesday, 23 June 2015 129-CASE-5 1400 - 1730 hrs University of Southampton, Southampton, D. Bianchi, T. Orra, Embraer, São José dos M. Kügler, N. Randt, Technical University United Kingdom Campos, Brazil; P. Paglione, Technological of Munich, Munich, Germany Institute of Aeronautics (ITA), São José dos Campos, Brazil Chaired by: A. CHAPUT, University of Texas at Austin 1400 hrs 1430 hrs AIAA-2015-2736 AIAA-2015-2737 Value Driven Conceptual Design of Monte Carlo based Robust MDO Unmanned Air System for Defense applied to Aircraft Conceptual Design: a technical-financial Applications E. Papageorgio, M. Eres, J. Scanlan, coupling optimization strategy Tuesday, 23 June 2015 128-ATIO-14 75 M. Sharbatdar, C. Ollivier Gooch, University of British Columbia, Vancouver, Canada C. Morsbach, German Aerospace Center (DLR), Cologne, Germany 1530 hrs AIAA-2015-2761 Turbulent Flow Simulations on Unstructured Grids using a Reynolds Stress Models RANS Modeling D. Im, S. Choi, J. McClure, J. Choi, F. Skies, Virginia Polytechnic Institute and State University, Blacksburg, VA 1530 hrs AIAA-2015-2755 A Mapped Chebyshev Pseudospectral Method for Unsteady Flow Analysis Time Integration Methods The Netherlands; G. Gori, Technical University of Milan, Milan, Italy; M. Pini, Delft University of Technology, Delft, The Netherlands; A. Guardone, Technical University of Milan, Milan, Italy; T. Economon, F. Palacios, Stanford University, Palo Alto, CA; et al. CFD Flow Visualization Showcase P. Boom, D. Zingg, University of Toronto, Toronto, Canada 1630 hrs AIAA-2015-2763 Proper orthogonal decomposition closure models for Burgers and Navier-Stokes Equations H. Imtiaz, I. Akhtar, M. Saif Ullah Khalid, National University of Sciences and J. Choi, O. Kwon, Korea Advanced Institute Technology, Rawalpindi, Pakistan of Science and Technology, Daejeon, South Korea Hampton, VA 1630 hrs AIAA-2015-2757 Investigation of Efficient HighOrder Implicit Runge-Kutta Methods Based on Generalized P. Gnoffo, NASA Langley Research Center, Summation-by-Parts Operators 1600 hrs AIAA-2015-2756 Unsteady Solutions of Non-Linear Differential Equations Using Walsh Function Series Chantilly Ballroom Foyer Emerald Coral Grand Ballroom B 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 134-CFD-37 1400 - 1600 hrs Langley Research Center, Hampton, VA 1600 hrs AIAA-2015-2751 Convergence Acceleration Using Convergence Error Estimation S. Akbarzadeh, Y. Wang, J. Mueller, S. Eyi, Middle East Technical University, Queen Mary University of London, London, Ankara, Turkey United Kingdom 1530 hrs AIAA-2015-2750 Fixed point discrete adjoint of SIMPLE-like solvers Adjoints and Error Estimation 1600 hrs AIAA-2015-2762 Recent Improvement of a Correlation-Based Transition Turbulence Model for Simulating Y. Mor-Yossef, Israeli CFD Center, Caesarea Three-Dimensional Boundary S. Vitale, Delft University of Technology, Delft, Industrial Park, Israel Layers Chaired by: P. HARTWICH, Boeing Research & Technology and J. CARLSON, Computational Aerosciences Branch 1400 hrs 1430 hrs 1500 hrs AIAA-2015-2758 AIAA-2015-2759 AIAA-2015-2760 Node-Centered Wall Function Analysis of a low Reynolds Extension of the SU2 open source CFD Models for the Unstructured FLow differential Reynolds stress model code to the simulation of turbulent Code Fun3D in homogeneous shear flow with flows of fuids modelled with complex J. Carlson, V. Vatsa, J. White, NASA respect to numerical stability thermophysical laws Tuesday, 23 June 2015 133-CFD-16 Edoh, University of California, Los Angeles, A. Jameson, Stanford University, Stanford, Lecce, Italy; C. Cedric, Paris Institute of Los Angeles, CA; V. Sankaran, Air Force Technology, Paris, France CA Research Laboratory, Edwards AFB, CA Chaired by: X. WANG, Air Force Research Laboratory, Wright-Patterson AFB and J. NORDSTROM, Linköping University 1400 hrs 1430 hrs 1500 hrs AIAA-2015-2752 AIAA-2015-2753 AIAA-2015-2754 Optimal Runge-Kutta Schemes for Application of Dual Time Stepping Assessment of time implicit High-order Spatial and Temporal to Fully Implicit Runge Kutta discretizations for the computation Discretizations Schemes for Unsteady Flow of turbulent compressible flows N. Mundis, ERC, Inc., Edwards AFB, CA; A. Calculations P. Cinnella, Università del Salento, Tuesday, 23 June 2015 132-CFD-15 British Columbia, Vancouver, Canada Chaired by: C. ROY, Virginia Tech and C. OLLIVIER GOOCH, University of British Columbia 1400 hrs 1430 hrs 1500 hrs AIAA-2015-2747 AIAA-2015-2748 AIAA-2015-2749 Comparison of Truncation Error Stabilisation of Discrete Adjoint Accuracy of Discretization Error Solvers for Incompressible Flow Estimation by the Error Transport Estimators for Defect Correction Y. Wang, S. Akbarzadeh, J. Mueller, Equation on Unstructured Meshes - and Output Error Estimation in the Queen Mary University of London, London, Nonlinear Systems of Equations Unstructured Mesh Finite Volume United Kingdom G. Yan, C. Ollivier Gooch, University of Method Tuesday, 23 June 2015 131-CFD-14 76 S. Yoon, N. Chaderjian, T. Pulliam, T. Holst, NASA Ames Research Center, Moffett Field, CA N. Oliviero, T. Kocian, A. Moyes, H. Reed, C. Ward, R. Henderson, S. Schneider, Texas A&M University, College Station, TX Purdue University, West Lafayette, IN C. Kroninger, A. Harrington, M. Munson, Army Research Laboratory, Aberdeen Proving Ground, MD (DLR), Göttingen, Germany College Station, TX W. Saric, Texas A&M University, College Station, TX R. Giepman, A. Srivastava, F. Schrijer, B. van Oudheusden, Delft University of Technology, Delft, The Netherlands R. Giepman, R. Louman, F. Schrijer, B. van Oudheusden, Delft University of Technology, Delft, The Netherlands 1530 hrs AIAA-2015-2780 Experimental investigation of boundary layer tripping devices for shock wave - boundary layer control J. Eppink, NASA Langley Research Center, Hampton, VA; R. Wlezien, Iowa State University, Ames, IA; R. King, M. Choudhari, NASA Langley Research Center, Hampton, VA A. Iwakawa, T. Tamba, P. Son, T. Shoda, A. Sasoh, Nagoya University, Nagoya, Japan 1600 hrs AIAA-2015-2781 Control of Shock Wave Boundary Layer Interaction using Laser Pulse Energy Depositions 1630 hrs AIAA-2015-2776 The Effect of Backward-facing Step Height on Instability Growth and Breakdown in Swept-Wing BoundaryM. Tufts, H. Reed, B. Crawford, G. Duncan, Layer Transition 1600 hrs AIAA-2015-2775 Computational Investigation of Step Excrescence Sensitivity in a SweptS. Craig, W. Saric, Texas A&M University, Wing Boundary Layer 1530 hrs AIAA-2015-2774 Experimental study of crossflow instability on a Mach 6 yawed cone Senators Lecture Hall Sapphire 1700 hrs AIAA-2015-2770 Analysis of Deflected Vortex Street Produced by an Oscillating Airfoil Govenors Lecture Hall Dale Richards Senior Research Fellow, Human Factors Faculty of Engineering & Computing Coventry University, United Kingdom Grand Ballroom E M. Khalid, I. Akhtar, National University of S. Badrinath, S. Sarkar, Indian Institute of S. Badrinath, S. Sarkar, Indian Institute of Sciences and Technology, Islamabad, Pakistan; Technology Madras, Chennai, India Technology Madras, Chennai, India H. Dong, University of Virginia, Charlottesville, Charlottesville, VA; N. Ahsan, Institute of Space Technology, Islamabad, Pakistan Boundary Layer and Bluff Body Control Chaired by: Z. ZHANG, University of Tennessee and J. LIN, NASA-Langley Research Center 1430 hrs 1500 hrs 1400 hrs AIAA-2015-2778 AIAA-2015-2779 AIAA-2015-2777 Simplified model for flow-heating The effects of Mach and Reynolds Control of Afterbody Vortices by effect on wave drag of blunt bodies number on the flow mixing properties Blowing R. Jackson, Z. Wang, I. Gursul, University and its validation of micro-ramp vortex generators in a of Bath, Bath, United Kingdom E. Schülein, German Aerospace Center supersonic boundary layer Tuesday, 23 June 2015 138-FD-17 F. Li, M. Choudhari, NASA Langley Research Center, Hampton, VA; L. Duan, Missouri University of Science and Technology, Rolla, MO S. Dawson, N. Schiavone, C. Rowley, Princeton University, Princeton, NJ; D. Williams, Illinois Institute of Technology, Chicago, IL 1630 hrs AIAA-2015-2769 Intermittency Behaviour in the Flow Past an Oscillating Airfoil Randy Willis FAA, Co-Chair of ICAO RPAS (Remotely Piloted Aircraft Systems) 1600 hrs AIAA-2015-2768 Nonlinear Characterization of Flow over Oscillating Elliptic Airfoils Boundary Layer Transition: Crossflow Chaired by: M. BORG, Air Force Research Laboratory and T. JULIANO, University of Notre Dame 1400 hrs 1430 hrs 1500 hrs AIAA-2015-2771 AIAA-2015-2772 AIAA-2015-2773 Direct Numerical Simulation EPIC: NPSE Analysis of Hypersonic Secondary Instability of Stationary of Transition due to Traveling Crossflow Instability on Yawed Crossflow Vortices on an Inclined Crossflow Vortices Straight Circular Cone Cone at Mach 6 Tuesday, 23 June 2015 137-FD-16 Ganapathisubramani, University of Southampton, Southampton, United Kingdom 1530 hrs AIAA-2015-2767 A Data-Driven Modeling Framework for Predicting Forces and Pressures on a Rapidly Pitching Airfoil 1500 hrs AIAA-2015-2766 Effect of Turbulence Modeling on Hovering Rotor Flows Marshall Jackson Project Manager - Aviation Safety Audits Office of Inspector General U.S. Department of Transportation Unsteady Wing Aerodynamics II Marty Rogers University of Alaska-Fairbanks Chaired by: K. TAIRA, Florida State University and B. JOLLY, US Air Force 1400 hrs 1430 hrs AIAA-2015-2764 AIAA-2015-2765 Aeromechanics of Membrane Wings The Influence of Streamline in Ground-Effect Curvature on Low Aspect Ratio R. Bleischwitz, R. De Kat, B. Rotating Wings Chuck Johnson Vice President of Operations The Padina Group International UAS Integration Forum Tuesday, 23 June 2015 136-FD-15 Moderator: Rob Hughes, Northrop Grumman, Inc. Panelists: Cees Bil Associate Professor, School of Aerospace, Mechanical and Manufacturing Engineering RMIT University Tuesday, 23 June 2015 135-F360-4 1400 - 1630 hrs 77 University, Palo Alto, CA J. Ray, S. Lefantzi, Sandia National Laboratories, Livermore, CA; S. Arunajatesan, L. DeChant, Sandia National Laboratories, Albuquerque, NM F. Zajaczkowski, J. Tarter, T. Bagwell, Applied Research Laboratory, State College, PA 1430 hrs AIAA-2015-2788 Airfield Lifting Loads a CFD/Full Scale Rotary Wing Test Study K. Palopo, NASA Ames Research Center, Moffett Field, CA; G. Chatterji, University of California, Santa Cruz, Moffett Field, CA; M. Guminsky, P. Glaab, NASA Langley Research Center, Hampton, VA C. Humphreys, R. Cobb, D. Jacques, J. Reeger, Air Force Institute of Technology, Wright-Patterson AFB, OH Applications II 1530 hrs AIAA-2015-2792 Optimal Mission Path for the Uninhabited Loyal Wingman S. Andrews, R. Perez, Royal Military College of Canada, Kingston, Canada 1600 hrs AIAA-2015-2793 Multidisciplinary Analysis of a Box-Wing Aircraft Designed for a Regional-Jet Mission M. Rahman, Aalto University, Helsinki, Finland; R. Agarwal, Washington University in St. Louis, St. Louis, MO; M. Lampinen, T. Siikonen, Aalto University, Helsinki, Finland 1600 hrs AIAA-2015-2786 An Improved Version of OneEquation RAS Turbulence Model VA; J. Krozel, Innovation Laboratory, Inc., Portland, OR; D. Miller, J. Smith, Metron Aviation, Inc., Dulles, VA Arlington, VA 1600 hrs AIAA-2015-2798 A Data Exchange and Transformation System for SMART NAS (Invited) 1630 hrs AIAA-2015-2799 Parallel Simulation of Agent-Based Model for Air Traffic Network Y. Kim, O. Pinon-Fischer, D. Mavris, P. Cobb, Crown Consulting, Inc., Arlington, Georgia Institute of Technology, Atlanta, P. Kostiuk, Robust Analytics, Gambrills, MD VA; M. Garland, Mosaic ATM, Leesburg, VA GA 1530 hrs AIAA-2015-2797 Architecture Development for Shadow Mode Assessments of Air Traffic Management Technologies (Invited) Shadow Mode Assessment using Realistic Technologies for National Airspace System (SMART NAS) Test Bed Development (Invited) Chaired by: K. PALOPO, NASA Ames Research Center and G. CHATTERJI, NASA Ames Research Center 1430 hrs 1500 hrs 1400 hrs AIAA-2015-2795 AIAA-2015-2796 AIAA-2015-2794 Design Challenges for a Shadow Platform As A Service (PAAS) Shadow Mode Assessment using Architecture for NASA’s SMART NAS Realistic Technologies for the National Mode Assessment Tool for Air Traffic Management (Invited) (Invited) Airspace System (SMART NAS) R. Hoffman, Metron Aviation, Inc., Dulles, P. Cobb, M. Blake, Crown Consulting, Inc., Test Bed Development (Invited) Tuesday, 23 June 2015 142-MST-6 C. Potter, Georgia Institute of Technology, G. Kenway, J. Martins, University of Atlanta, GA; S. Russell, Triumph Aerostructures, Michigan, Ann Arbor, Ann Arbor, MI Dallas, TX; V. Kim, Z. Liu, D. Mavris, Georgia Institute of Technology, Atlanta, GA T. Wray, R. Agarwal, Washington University in St. Louis, St. Louis, MO 1530 hrs AIAA-2015-2785 Extension of Wray-Agarwal Turbulence Model for Flow Over Rough Surfaces Turbulence Modeling ITAR - Aircraft Design and Modeling C. Pak, NASA Armstrong Flight Research Center, Edwards, CA Chaired by: R. KHIRE, United Technologies Research Center and E. WINER, Iowa State University 1430 hrs 1500 hrs 1400 hrs AIAA-2015-2790 AIAA-2015-2791 AIAA-2015-2789 Aeroelastic Tailoring Study of Design Space Exploration of Wingbox High-Fidelity Aerostructural Otimization Considering Buffet an N+2 Low-boom Supersonic Substructures Configuration Using Onset Commercial Transport Aircraft SPANDSET Tuesday, 23 June 2015 141-MAO-4 J. Jacob, Oklahoma State University, Stillwater, OK; J. Grimsley, S. Atkins, Design Intelligence, Inc., Norman, OK Chaired by: K. CASPER 1400 hrs AIAA-2015-2787 Development and Testing of a Solar Powered Aircraft Tuesday, 23 June 2015 140-ITAR-2 Minnesota, Minneapolis, Minneapolis, MN; P. Dimotakis, California Institute of Technology, Pasadena, CA Chaired by: C. RUMSEY, NASA-Langley Research Center and G. BLAISDELL, Purdue University 1400 hrs 1430 hrs 1500 hrs AIAA-2015-2782 AIAA-2015-2783 AIAA-2015-2784 DNS/LES Simulations of Separated Bayesian Calibration of a RANS Stretched-Vortex based Subgridscale Modeling of Variable-Density Flows at High Reynolds Numbers Model with a Complex Response P. Balakumar, NASA Langley Research Surface - A Case Study with Jet-inFlows Center, Hampton, VA; G. Park, Stanford G. Sidharth, G. Candler, University of Crossflow Configuration Tuesday, 23 June 2015 139-FD-18 B. Horio, V. Kumar, V. Stouffer, S. Hasan, A. DeCicco, LMI, Tysons Corner, VA; J. Smith, NASA Langley Research Center, Hampton, VA; et al. Travertine Madrid Morocco 1700 hrs AIAA-2015-2800 An Integrated Framework for Modeling Air Carrier Behavior, Policy, and Impacts in the U.S. Air Transportation System Edelweiss 78 N. Bisek, M. Brown, Air Force Research Laboratory, Wright-Patterson AFB, OH S. Leonov, University of Notre Dame, Notre Dame, IN From Plasmadynamics and Shock Tubes to Aero-Optics and Laser Radar: An Aerospace Career Philip E. Cassady Senior Technical Fellow (Retired) The Boeing Company Plasmadynamics and Lasers Award Lecture Tuesday, 23 June 2015 147-LEC-2 1630 - 1730 hrs W. Cai, C. Yang, B. Qi, H. Ma, L. Yu, X. Chen, Nanjing University of Science and Technology, Nanjing, China 1600 hrs AIAA-2015-2815 POD Analysis of the Transient Flow Field at Pulse Engine Exhaust Region X. Han, H. Li, X. Meng, Northwestern Polytechnical University, Xi’an, China; F. Liu, S. Luo, University of California, Irvine, Los Angeles, CA Rosetta Monet Ballroom Miro Grand Ballroom D Chantilly Ballroom East 1700 hrs AIAA-2015-2817 Numerical and experimental analysis of heat transfer of piccolo tube jet impingement on a concave surface J. Bai, Q. Pan, Aviation Industry Corporation of Y. Bo, S. Chang, Y. Zhao, M. Leng, China (AVIC), Shanghai, China Beihang University, Beijing, China 1630 hrs AIAA-2015-2816 Fluid flow and heat transfer in a rotating two-pass square channel with smooth walls and axial inward/outward flow 1600 hrs AIAA-2015-2810 Effect of Voltage and Frequency on Starting Repetitive Nanosecond Pulsed DBD Networking Coffee Break S. Martinez, M. Ricklick, Embry-Riddle Aeronautical University, Daytona Beach, FL Q. Pan, H. Tang, J. Bai, Aviation Industry Corporation of China (AVIC), Shanghai, China 1530 hrs AIAA-2015-2814 Numerical Analysis of Film Cooling Characteristic on a Turbine Nonaxisymmetric Contoured Endwall Heat Transfer II H. Nishida, M. Tamura, Tokyo University H. Otsu, Ryukoku University, Otsu, Japan; K. of Agriculture and Technology, Koganei, Yamada, T. Abe, Japan Aerospace Exploration Japan; T. Matsuno, Tottori University, Tottori, Japan Agency (JAXA), Sagamihara, Japan 1530 hrs AIAA-2015-2809 Numerical Study on Performance Improvement Mechanism of TriElectrode Plasma Actuator Tuesday, 23 June 2015 146-NW-4 1530 - 1600 hrs G. Jackson, K. Smith, P. Mccarthy, T. Fisher, Purdue University, West Lafayette, IN 1600 hrs AIAA-2015-2805 Langmuir Probe Diagnostics of an Atmospheric-Pressure Microplasma L. Blair, K. Xu, University of Alabama, Huntsville, Huntsville, AL M. Nguyen, M. Rennie, S. Gordeyev, E. Jumper, University of Notre Dame, Notre Dame, IN; A. Cain, Innovative Technology Applications Company, LLC, Chesterfield, MO; T. Hayden, U.S. Air Force Academy, Colorado Springs, CO 1530 hrs AIAA-2015-2804 Wavefront Measurements of a Supersonic Boundary Layer Using a Laser-Induced Breakdown Spark Plasma Diagnostics I Plasma Aerodynamics & Flow Control III 1500 hrs AIAA-2015-2808 Effect of New Electron Impact Ionization on the Aerodynamic Heating Environment for Super-Orbital Reentry Vehicles T. Chng, R. Miles, Princeton University, Princeton, NJ 1500 hrs AIAA-2015-2803 Understanding the Impact of Buffer Gases on the Radar REMPI Diagnostic 1500 hrs AIAA-2015-2813 Benchmarking of Computational Models For Adiabatic Film-Cooling Effectiveness For Large Spacing B. Upalkar, M. Ricklick, Embry-Riddle Compound Angle Full Coverage Aeronautical University, Daytona Beach, FL Film Cooling Arrays Chaired by: E. SHORT, Raytheon Company and E. KHALIL, Cairo University 1400 hrs 1430 hrs AIAA-2015-2811 AIAA-2015-2812 Response of porous foams filled Evaluation of different Turbulence with phase change material under Models for analysis of Jet transient heating Impingement in Gas Turbine Blades Tuesday, 23 June 2015 145-TP-7 Technology, Haifa, Israel Chaired by: T. MOELLER, University of Tennessee Space Institute 1400 hrs 1430 hrs AIAA-2015-2806 AIAA-2015-2807 Investigation of Cathodic-Arc-Jet Dynamics of Charge Transfer in Influence on Cross Flow using Atmospheric Pressure Barrier Particle Image Velocimetry Discharge at Single and Alternative I. Kronhaus, Technion--Israel Institute of Polarities of Supplying Voltage Tuesday, 23 June 2015 144-PDL-7 D. Zelenak, F. Kidd, V. Narayanaswamy, North Carolina State University, Raleigh, NC Chaired by: C. DUMITRACHE, Colorado State University 1400 hrs 1430 hrs AIAA-2015-2801 AIAA-2015-2802 Computational and Experimental Composition-Independent Laser Differential Interferometry Temperature and Pressure for Supersonic Turbulent BoundaryMeasurements using Lineshape Scaling Information from Kr PLIF Layer Flow Tuesday, 23 June 2015 143-PDL-6 79 Plenary Keynote Wednesday, 24 June 2015 150-PLNRY-3 0800 - 0900 hrs Lacor, Vrije Universiteit Brussel, Brussels, S. Bouley, B. François, M. Roger, École Centrale de Lyon, Ecully, France; S. Moreau, Belgium University of Sherbrooke, Sherbrooke, Canada L. Siozos-Rousoulis, G. Ghorbaniasl, C. Lacor, Vrije Universiteit Brussel, Brussels, Belgium 1000 hrs AIAA-2015-2827 Acoustic effects of a rotationally oscillating rod in a rod-airfoil configuration N. Kings, L. Enghardt, F. Bake, German Aerospace Center (DLR), Berlin, Germany W. Schuster, Honeywell International, Inc., Phoenix, AZ; L. Hultgren, NASA Glenn Research Center, Cleveland, OH Chaired by: S. RIZZI, NASA Langley Research Center 0900 hrs 0930 hrs AIAA-2015-2825 AIAA-2015-2826 On a mode-matching technique for Noise control by a rotating rod in a sound generation and transmission in rod-airfoil configuration a linear cascade of outlet guide vanes L. Siozos-Rousoulis, G. Ghorbaniasl, C. Wednesday, 24 June 2015 152-AA-22 Aerospace Center (DLR), Berlin, Germany 1100 hrs AIAA-2015-2829 Acoustic Resonance Phenomena in a Three-Dimensional Cascade Interacting with Oncoming Unsteady Wakes D. Broszat, M. Höger, MTU Aero Engines, Munich, Germany; A. Marn, T. Selic, F. Schönleitner, F. Heitmeir, Graz University of Technology, Graz, Austria 1100 hrs AIAA-2015-2822 Acoustic Comparison of Different Turbine Exit Guide Vane Designs - Part 1: Design Philosophy and Numerical Predictions L. Enghardt, P. Kausche, A. Moreau, German Aerospace Center (DLR), Berlin, Germany; T. Carolus, University of Siegen, H. Kodama, IHI Corporation, Nishitama, Siegen, Germany Japan; M. Namba, Kyusyu University, Fukuoka, Japan 1030 hrs AIAA-2015-2828 Active Control of Fan Tones by means of Trailing Edge Blowing General Acoustics II J. O’Brien, J. Kim, M. Ihme, Stanford University, Stanford, CA 1030 hrs AIAA-2015-2821 Linear Analysis of Engine Core Noise Using a Hybrid Modeling Approach Chaired by: H. ATASSI, University of Notre Dame 0930 hrs 0900 hrs AIAA-2015-2818 AIAA-2015-2819 Dynamic Temperature and Pressure Entropy Noise Generation and Reduction in a Heated Nozzle Flow Measurements in the Core of a K. Knobloch, T. Werner, F. Bake, German Propulsion Engine 1000 hrs AIAA-2015-2820 Broadband indirect noise generation by accelerated vorticity Turbomachinery and Core Noise Wednesday, 24 June 2015 151-AA-21 NASA and the Future of Aerospace Charles F. Bolden Jr. Administrator National Aeronautics and Space Administration Speakers’ Briefing Wednesday Reception in the Exposition Hall Wednesday, 24 June 2015 149-SB-3 0730 - 0800 hrs A ticket is required and included in the conference registration fee where indicated. Tuesday, 23 June 2015 148-NW-5 1730 - 1900 hrs C. Paruchuri, J. Gill, N. Subramanian, P. Joseph, C. Vanderwel, X. Zhang, University of Southampton, Southampton, United Kingdom; et al. 1130 hrs AIAA-2015-2830 Aerofoil geometry effects on turbulence interaction noise A. Marn, T. Selic, F. Schönleitner, S. Zerobin, Graz University of Technology, Graz, Austria; D. Broszat, M. Höger, MTU Aero Engines, Munich, Germany; et al. 1130 hrs AIAA-2015-2823 Acoustic Comparison of Different Turbine Exit Guide Vane Designs Part 2: Experimental Analysis D. Moreau, C. Doolan, University of New South Wales, Sydney, Australia; W. Alexander, T. Meyers, W. Devenport, Virginia Polytechnic Institute and State University, Blacksburg, VA 1200 hrs AIAA-2015-2831 Wall-Mounted Finite Airfoil Noise Production and Prediction Inverness W. Qiao, L. Wang, W. Chen, F. Tong, L. Ji, Northwestern Polytechnical University, Xi’an, China 1200 hrs AIAA-2015-2824 Experimental Study on the Turbomachinery Trailing Edge Noise Reduction Based on Linear Cascade Test with Phased Array Fleur-de-lis B Chantilly Ballroom West Session Rooms Chantilly Ballroom East 80 State University, Columbus, OH Center, Hampton, VA M. Choudhari, D. Lockard, NASA Langley Research Center, Hampton, VA Chaired by: M. CHOUDHARI, NASA-Langley Research Center 0900 hrs 0930 hrs Oral Presentation AIAA-2015-2844 An Overview of Contributions on Assessment of Slat Noise Nose Landing Gear Configuration Predictions for 30P30N High-Lift for BANC-III Workshop Configuration from BANC-III M. Khorrami, NASA Langley Research Workshop Wednesday, 24 June 2015 155-AA-25 S. Peng, L. Tysell, Swedish Defense Research S. Lee, General Electric Company, Agency (FOI), Stockholm, Sweden; H. Yao, L. Niskayuna, NY Davidson, L. Eriksson, Chalmers University of Technology, Göteborg, Sweden Chaired by: M. ROGER, Ecole Centrale de Lyon 0900 hrs 0930 hrs AIAA-2015-2839 AIAA-2015-2840 CAA analysis of a Wing Section with Prediction of Far-Field Wind Turbine Flap Side-Edges Based on Hybrid Noise Propagation with Parabolic RANS-LES Computation Equation Wednesday, 24 June 2015 154-AA-24 S. Miller, NASA Langley Research Center, Hampton, VA Chaired by: A. PILON, Lockheed Martin Aeronautics 0900 hrs 0930 hrs AIAA-2015-2832 AIAA-2015-2833 On Theoretical Broadband Shock- Near-field Pressure Waveform Associated Noise Near-Field Cross- Analysis of an Excited Mach 0.9 Jet C. Kuo, M. Crawley, M. Samimy, Ohio Spectra Wednesday, 24 June 2015 153-AA-23 1030 hrs AIAA-2015-2846 Summary of the LAGOON Solutions from the Benchmark problems for Airframe Noise Computations-III Workshop L. Lopes, NASA Langley Research Center, E. Manoha, ONERA, Châtillon, France; B. Hampton, VA; S. Redonnet, ONERA, Toulouse, Caruelle, Airbus, Toulouse, France France; T. Imamura, University of Tokyo, Tokyo, Japan; T. Ikeda, Japan Aerospace Exploration Agency (JAXA), Chofu, Japan; N. Zawodny, NASA Langley Research Center, Hampton, VA; G. Cunha, ONERA, Toulouse, France 1000 hrs AIAA-2015-2845 Variability in the Propagation Phase of CFD-Based Noise Prediction: Summary of Results from Category 8 of the BANC-III Workshop J. Cluts, C. Kuo, M. Samimy, Ohio State University, Columbus, OH 1130 hrs AIAA-2015-2837 An Investigation of Twin Supersonic Jets’ Near-field 1100 hrs AIAA-2015-2843 Numerical and Analytical Investigation of Orthogonal Blade/ Vortex Interaction Noise A. Subramanyam, K. Natarajan, National Aerospace Laboratories, Bangalore, India 1100 hrs AIAA-2015-2836 Effect of Inverted Triangular Tabs on Mitigation of Jet Noise from Axisymmetric Convergent Nozzles F. Falissard, P. Zehner, ONERA, Châtillon, C. Durand, D. Hixon, University of Toledo, France; M. Roger, École Centrale de Lyon, Ecully, France; X. Gloerfelt, Arts Metiers Toledo, OH ParisTech, Paris, France 1030 hrs AIAA-2015-2842 Comparison of Computational Aeroacoustics Prediction of Vortical Gust Scattering by a 2D Stator with Flat Plate Theory CAA Propagation and Scattering II J. Liu, A. Corrigan, K. Kailasanath, Naval Research Laboratory, Washington, DC; E. Gutmark, University of Cincinnati, Cincinnati, OH 1030 hrs AIAA-2015-2835 Impact of Chevrons on Noise Source Characteristics In Imperfectly Expanded Jet Flows M. Herr, R. Ewert, C. Rautmann, German Aerospace Center (DLR), Braunschweig, Germany; M. Kamruzzaman, ENERCON GmbH, Aurich, Germany; D. Bekiropoulos, University of Stuttgart, Stuttgart, Germany; R. Arina, Technical University of Turin, Torino, Italy; et al. 1100 hrs AIAA-2015-2847 Broadband Trailing-Edge Noise Predictions—Overview of BANC-III Results Benchmark Problems for Airframe Noise Computations III (BANC-III) Summary (Invited) I. Bennaceur, D. Mincu, I. Mary, M. Terracol, ONERA, Châtillon, France; L. Larcheveque, D. Pierre, Aix-Marseille University, Marseille, France 1000 hrs AIAA-2015-2841 Numerical simulation of spectral broadening of an acoustic wave by a spatially growing turbulent mixing layer D. Edgington-Mitchell, O. Amili, D. Honnery, J. Soria, Monash University, Melbourne, Australia 1000 hrs AIAA-2015-2834 Measuring shear layer growth rates in aeroacoustically forced axisymmetric supersonic jets Jet Noise Near Field and Jet Noise Reduction Fleur-de-lis A Obelisk A J. Kreitzman, J. Nichols, University of Minnesota, Minneapolis, Minneapolis, MN 1200 hrs AIAA-2015-2838 Acoustic source analysis of a supersonic rectangular chevron jet Lalique 81 Colorado, Boulder, Boulder, CO C. Montalvo, J. Richardson, J. Marshall, University of South Alabama, Mobile, AL E. Harrison, S. Min, H. Jimenez, D. Mavris, Georgia Institute of Technology, Atlanta, GA 1000 hrs AIAA-2015-2850 Implementataion and Validation of an Internal Combustion Engine and Propeller Model for General Aviation Aircraft Performance Studies Technology, Haifa, Israel T. Jenkins, MetroLaser, Inc., Laguna Hills, CA; J. Seitzman, S. Adusumilli, Georgia Institute of Technology, Atlanta, GA M. Nelson, K. Lowe, W. O’Brien, C. Kirk, Virginia Polytechnic Institute and State University, Blacksburg, VA Chaired by: K. LOWE, Virginia Tech and C. GOYNE, University of Virginia 0930 hrs 0900 hrs AIAA-2015-2866 AIAA-2015-2865 Stereoscopic PIV measurements Velocity Measurements in an Unseeded Turbojet Engine Exhaust in a turbofan engine inlet with Using Planar Doppler Velocimetry tailored swirl distortion Wednesday, 24 June 2015 159-AMT-10/GT-10 F. Lou, W. Murray, N. Key, Purdue University, West Lafayette, IN G. Hammock, Arnold Engineering Development Complex, Arnold AFB, TN A. Patterson, A. Arena, Oklahoma State University, Stillwater, OK 1100 hrs AIAA-2015-2858 A Launch System Design Methodology for Small Unmanned Aircraft Applications I. Chakraborty, B. Lozano, D. Mavris, Georgia Institute of Technology, Atlanta, GA 1100 hrs AIAA-2015-2852 Pilot-Friendliness Considerations for Personal Air Vehicle Flight Control Systems 1100 hrs AIAA-2015-2864 Upgrades to the Texas A&M Oran W. Nicks Low-Speed Wind Tunnel for M=0.4 Operation M. Novara, R. Geisler, A. Schroeder, German Aerospace Center (DLR), Göttingen, Germany 1000 hrs AIAA-2015-2867 Multi-stereo PIV measurement of propeller wake flow in industrial facility 1130 hrs Oral Presentation NASA Langley Aeroacoustic Wind Tunnel Capability Moving Forward T. Hays, A. Arena, Oklahoma State University, Stillwater, OK 1130 hrs AIAA-2015-2859 Feasibility Study of Closed Cycle Propulsion for Unmanned Aerial Systems S. Min, E. Harrison, H. Jimenez, D. Mavris, Georgia Institute of Technology, Atlanta, GA 1100 hrs AIAA-2015-2869 Biological Flow Measurement using Optical Flow Method Z. Yang, H. Yu, G. Huang, B. Ludwig, H. Rochlitz, P. Scholz, Technical University Wright State University, Beavercreek, OH of Braunschweig, Braunschweig, Germany 1030 hrs AIAA-2015-2868 Application of Particle Image Velocimetry and Laser Induced Fluorescence in a cooling duct flow D. Lincoln, K. Murari, C. Johansen, University of Calgary, Calgary, Canada 1130 hrs AIAA-2015-2870 Development and characterization of an inexpensive LED-based light source for high-frame-rate schlieren imaging 1130 hrs AIAA-2015-2853 Development of Aerodynamic Modeling and Calibration Methods for General Aviation Aircraft Performance Analysis - a Survey and Comparison of Models M. Doty, F. Hutcheson, H. Haskin, P. Quinto, D. Smith, NASA Langley Research J. Lancaster, M. Reeder, Air Force Institute A. Herring, D. Kutz, L. Brown, E. White, 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 1030 hrs AIAA-2015-2863 Experiments with the Model Test Apparatus Installed in the AFIT Low Speed Tunnel Ground Test Facility Improvements I K. Subbarao, C. Tule, P. Ru, University of Texas, Arlington, Arlington, TX 1030 hrs AIAA-2015-2857 Nonlinear Model Predictive Control Applied to Trajectory Tracking for Unmanned Aerial Vehicles Unmanned Aircraft Systems II N. Fala, V. Goblet, K. Marais, Purdue University, West Lafayette, IN 1030 hrs AIAA-2015-2851 Identifying Phases of Flight in General Aviation Operations General Aviation Particle-Based Velocimetry Applications and Developments Chaired by: R. RHEW, NASA-Langley Research Center and S. SIMERLY, NASA Glenn Research Center 0900 hrs 0930 hrs 1000 hrs AIAA-2015-2860 AIAA-2015-2861 AIAA-2015-2862 Development of a Research Facility Development and Testing of an Expansion of the AEDC H2 Arc to Study the Flow Field in an APU- Unsteady Low-Speed Wind Tunnel Heater Facility Test Envelope Using D. Greenblatt, Technion--Israel Institute of Cold-Air Mixing Style Inlet Wednesday, 24 June 2015 158-AMT-9/GT-9 University of Minnesota, Minneapolis, Minneapolis, MN Chaired by: T. FIELDS, University of Missouri and G. SHAH, NASA-Langley Research Center 0900 hrs 0930 hrs 1000 hrs AIAA-2015-2854 AIAA-2015-2855 AIAA-2015-2856 Unsteady Aerodynamics Modeling A Comparison of Filters for UAS-Based Robust Three-Dimensional for a Flexible Unmanned Air Localization of Stationary RF Sources Characterization of a Complex M. Stachura, Black Swift Technologies, LLC, Atmosphere at High Resolution Vehicle Boulder, CO; N. Wagle, E. Frew, University of using Multi-Agent Windmappers A. Kotikalpudi, H. Pfifer, G. Balas, Wednesday, 24 June 2015 157-AFM-9 A. Rao, K. Marais, Purdue University, West S. Silva, L. Jensen, R. Hansman, Lafayette, IN Massachusetts Institute of Technology, Cambridge, MA Chaired by: M. ORR, Boeing Commercial Airplanes 0900 hrs 0930 hrs AIAA-2015-2848 AIAA-2015-2849 Identifying High-Risk Occurrence Pilot Perception and Use of ADS-B In Traffic and Weather Services Chains in Helicopter Operations (TIS-B and FIS-B) from Accident Data Wednesday, 24 June 2015 156-ACD-4 Topaz Obelisk B Plum Blossom A Morocco 82 Z. Gao, K. Zhao, C. Wang, Northwestern Polytechnical University, Xi’an, China Aviation University, Toulouse, France of Technology, Pasadena, CA Z. Janjic, National Oceanic and Atmospheric Administration, College Park, MD Chaired by: N. AHMAD, NASA Langley Research Center and D. GHOSH 0900 hrs AIAA-2015-2888 Challenges and Opportunities in Modeling of the Global Atmosphere Wednesday, 24 June 2015 163-ASE-1 Abdul Malik, University of Glasgow, Glasgow, United Kingdom L. King, R. Hartfield, Auburn University, Auburn, AL; V. Ahuja, Research in Flight, Auburn, AL 1030 hrs AIAA-2015-2880 Aerodynamic Optimization of Integrated Wing-Engine Geometry using an Unstructured Vorticity Solver Aerodynamic Design Methodologies II D. Ghosh, E. Constantinescu, Argonne National Laboratory, Lemont, IL 1000 hrs AIAA-2015-2889 Well-Balanced Formulation of Gravitational Source Terms for Conservative Finite-Difference Atmospheric Flow Solvers B. Passe, A. Sridharan, J. Baeder, University of Maryland, College Park, College Park, MD 1130 hrs AIAA-2015-2876 A Synthesis of Hybrid CFD Results for F-16XL Aircraft Aerodynamics S. Troxel, T. Reynolds, Lincoln Laboratory, Massachusetts Institute of Technology, Lexington, MA J. Szmelter, Loughborough University, Loughborough, United Kingdom; P. Smolarkiewicz, European Centre for MediumRange Forecasting, Reading, United Kingdom; A. Wyszogrodzki, National Research Institute, Warsaw, Poland 1100 hrs AIAA-2015-2891 Simulations of orographic flows using unstructured and structured meshes (Invited) Numerical Weather Prediction (Invited) 1030 hrs AIAA-2015-2890 Use of Numerical Weather Prediction Models for NextGen ATC Wind Impact Studies (Invited) A. Stuermer, German Aerospace Center (DLR), Braunschweig, Germany 1130 hrs AIAA-2015-2886 Validation of Installation Effect Predictions through Simulations M. Gennaretti, R. Gori, J. Serafini, G. of Contra-Rotating Open Rotors at Bernardini, F. Cardito, Roma Tre University, Low-Speed Flight Conditions 1100 hrs AIAA-2015-2885 Rotor Dynamic Wake Inflow Modelling in State-Space Format R. Singh, H. Kang, Army Research Laboratory, Rome, Italy Aberdeen Proving Ground, MD; J. Sirohi, University of Texas, Austin, Austin, TX 1030 hrs AIAA-2015-2884 Computational Investigations of Transient Loads and Blade Deformations on Coaxial Rotor Systems Propeller/Rotorcraft/Wind Turbine Aerodynamics II Chaired by: J. FARNSWORTH, University of Colorado Boulder and M. POST, USAF Academy 0900 hrs 0930 hrs 1000 hrs AIAA-2015-2881 AIAA-2015-2882 AIAA-2015-2883 Development of UGS Monocopter: A study of separation on airfoils Computational Investigation Platform Design and Trajectory undergoing pitch, surge and of Coaxial Rotor Interactional Tracking combined motions Aerodynamics in Steady Forward S. Srigrarom, K. Lee, S. Chng, M. Bin R. Dunne, B. McKeon, California Institute Flight Wednesday, 24 June 2015 162-APA-19 Meudon, France Chaired by: J. LATZ, Northrop Grumman Aerospace Systems and D. FINLEY, Lockheed Martin Aeronautics 0900 hrs 0930 hrs 1000 hrs AIAA-2015-2877 AIAA-2015-2878 AIAA-2015-2879 Improvements in the New Unsteady Aerodynamic shape optimization of Design of A High-Performance Far-Field Drag Breakdown Method BWB aircraft based on multizone Tailless MAV Through Planform and Application to Complex Cases collaborative optimization design Optimization H. Toubin, D. Bailly, M. Costes, ONERA, M. Bronz, G. Hattenberger, French Civil method Wednesday, 24 June 2015 161-APA-18 NASA Langley Research Center, Hampton, S. Morton, D. McDaniel, CREATE Kestrel VA Team, Eglin AFB, FL 1100 hrs AIAA-2015-2875 Numerical Simulation of the F-16XL at Full-Scale Flight Test Conditions Using Delayed Detached-Eddy Simulation J. Luckring, NASA Langley Research Center, Hampton, VA M. Tomac, A. Rizzi, Royal Institute of Technology (KTH), Stockholm, Sweden; A. A. Lofthouse, R. Cummings, U.S. Air Force Jirasek, P. Eliasson, Swedish Defense Research Academy, Colorado Springs, CO Agency (FOI), Stockholm, Sweden 1030 hrs AIAA-2015-2874 Hybrid RANS-LES Simulations of F-16XL Aircraft in Low-speed Highalpha Flight Special Session: Hybrid CFD Method Assessments for F-16XL Aircraft Aerodynamics Chaired by: J. LUCKRING, NASA-Langley Research Center and A. RIZZI, KTH Royal Institute Technology 0900 hrs 0930 hrs 1000 hrs AIAA-2015-2871 AIAA-2015-2872 AIAA-2015-2873 F-16XL Hybrid Reynolds-Averaged Numerical Simulation of the F-16XL Free-Flight High AoA Flows at Full-Scale Flight Test Conditions Simulation at Sub- and Transonic Navier-Stokes/Large Eddy Simulation on Unstructured Grids Using a Near-Body Off-Body CFD Speeds - F-16XL (CAWAPI-3) S. Hitzel, Airbus, Manching, Germany M. Park, A. Elmiligui, K. Abdol-Hamid, Approach Wednesday, 24 June 2015 160-APA-17 Plum Blossom B Y. Yang, G. Huang, D. Zhao, C. Tang, Aviation Industry Corporation of China (AVIC), Xi’an, China Stemmons B Carpenter Ballroom 1200 hrs AIAA-2015-2887 A New Whirl Flutter Analysis Method Stemmons A 83 R. Palumbo, A. Errico, D. Pascarella, F. Gargiulo, E. Filippone, Italian Aerospace Research Center (CIRA), Capua, Italy E. Dill, S. Young, NASA Langley Research Center, Hampton, VA 1000 hrs Oral Presentation Balloon Systems Application LLC, Mesa, AZ J. Guo, K. Marais, S. Landry, Purdue University, West Lafayette, IN 1100 hrs AIAA-2015-2910 Non-Linear Analysis of the NASA Super Pressure Balloons: Implementation of a Large Strain Material Model C. Surakitbanharn, C. Surakitbanharn, S. Landry, Purdue University, West Lafayette, IN 1130 hrs AIAA-2015-2911 Returning to Hydrogen Gas : a Strategic Decision to Continue Achievement of Stratospheric Balloons Flights F. Schmidt-Skipiol, Technical University of Braunschweig, Braunschweig, Germany 1130 hrs AIAA-2015-2905 Tactile Feedback and Situation Awareness - Improving Adherence to an Envelope in SidestickControlled Fly-by-Wire Aircrafts H. Cathey, New Mexico State University, Wallops Island, VA; J. Tuttle, D. Fairbrother, M. Said, NASA Goddard Space A. Bown, D. Wakefield, Tensys Dynamics, J. Gary, French Space Agency (CNES), 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 1030 hrs AIAA-2015-2909 Qualification of the NASA Super Pressure Balloon Balloon Systems I C. Surakitbanharn, S. Landry, Purdue University, West Lafayette, IN 1100 hrs AIAA-2015-2904 A Comparison of an Intensity Control Measure Versus Dynamic Density to Capture Complexity Within a Sector Human Factors in Aviation Operations M. Motter, J. High, C. Cross, H. Fan, W. Fehlman, L. Hempley, NASA Langley Research Center, Hampton, VA; et al. 1100 hrs AIAA-2015-2896 Assessing Air Traffic Control System Safety with System Controllability 1030 hrs Oral Presentation “His actions indicate twodimensional thinking” - Deciding to Go Around via Machine Learning 1030 hrs AIAA-2015-2903 Evaluating Intensity as a NextGen Controller Function for Increased D. Carroll, Aviation Performance Solutions, Traffic Scenarios T. Gerber, Applied Technology Associates, D. Fairbrother, NASA Goddard Space Flight A. Vargas, V. Dubourg, D. Vassaux, French Albuquerque, NM Center, Greenbelt, MD Space Agency (CNES), Toulouse, France Chaired by: J. NOTT, Nott Technology LLC 0930 hrs 0900 hrs AIAA-2015-2908 AIAA-2015-2907 The French balloon program 2013 The NASA Balloon Program - 2015 Positioning For the Future Wednesday, 24 June 2015 167-BAL-1 A. Oztekin, Hi-Tec Systems, Inc., Egg Harbor Twp, NJ 1030 hrs AIAA-2015-2895 A Data-Driven Quantitative Framework for Safety Assessment of Air Traffic Control System ATM III - Modeling in ATM Transformational Flight - Autonomy I 1000 hrs AIAA-2015-2902 Threat and Error Management Applied to Loss of Control - Inflight 1000 hrs AIAA-2015-2899 Reinforcement Learning with Autonomous Small Unmanned Aerial Vehicles in Cluttered Environments - “After all these years among humans, you still haven’t learned to smile.” S. Geuther, A. Shih, NASA Langley Research Center, Hampton, VA 1000 hrs AIAA-2015-2894 Risk-based Causal Modeling of Airborne Loss of Separation C. Cross, H. Fan, W. Fehlman, L. Hempley, L. Tran, C. Cross, M. Motter, J. Neilan, M. Motter, J. Neilan, NASA Langley G. Qualls, P. Rothhaar, NASA Langley Research Center, Hampton, VA; et al. Research Center, Hampton, VA; et al. Chaired by: L. BOWERS, Purdue University 0900 hrs 0930 hrs AIAA-2015-2900 AIAA-2015-2901 A Model for Situational Awareness Analysis of Eye-Tracking Data with in Aircraft Upset Prevention and Regards to the Complexity of Flight Recovery Deck Information Automation K. Schlimm, Aviation Performance and Management - Inattentional Solutions, LLC, Mesa, AZ Blindness, System State Awareness, and EFB Usage Wednesday, 24 June 2015 166-ATIO-17 B. Allen, C. Cross, H. Fan, W. Fehlman, L. Hempley, M. Motter, NASA Langley Research Center, Hampton, VA; et al. Chaired by: B. ALLEN, NASA Langley Research Center 0900 hrs 0930 hrs AIAA-2015-2897 AIAA-2015-2898 Who’s got the bridge? Towards Towards an Open, Distributed Safe, Robust Autonomous Software Architecture for UxS Operations - “Data, you’ve got Operations - “It’s difficult to the bridge.” - First Officer Thomas work in groups when you’re “Will” Riker Star Trek: The Next omnipotent,” - Q Star Trek: The Generation:: Coming of Age (1988) Next Generation:: Deja Q (1990) Wednesday, 24 June 2015 165-ATIO-16 M. Kreuz, M. Schultz, German Aerospace Center (DLR), Braunschweig, Germany Chaired by: S. LANDRY, Purdue University 0900 hrs 0930 hrs AIAA-2015-2892 AIAA-2015-2893 Modeling Approach for Resilience A System Dynamics Approach Engineering of the Future ATM System towards ANSP Modeling Wednesday, 24 June 2015 164-ATIO-15 T. Lachenmeier, R. Dewey, Near Space Corporation, Tillamook, OR 1200 hrs AIAA-2015-2912 Suitability of ADS-B as a Beacon for Stratospheric Balloon Platforms and Payloads Steuben S. Hong, S. Jung, K. Lee, Korea Aerospace University, Goyang, South Korea Milan Monet Ballroom 1200 hrs AIAA-2015-2906 Modeling the Air Traffic Controller’s Direct-to Operation Using Logistic Regression Metropolitan Ballroom 84 CASE Session II & III Grand Ballroom D Arbor, Ann Arbor, MI of Toronto, Toronto, Canada of Toronto, Toronto, Canada H. Carson, S. Allmaras, M. Galbraith, D. Darmofal, Massachusetts Institute of Technology, Cambridge, MA 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 J. Newman, W. Anderson, University of P. Persson, University of California, Tennessee, Chattanooga, Chattanooga, TN Berkeley, Berkeley, CA 1030 hrs Oral Presentation High-order Discontinuous Galerkin Simulations on Domains with Large Deformations (Invited) M. Visbal, Air Force Research Laboratory, Wright-Patterson AFB, OH 1100 hrs Oral Presentation Probing Complex Unsteady Flow Physics Using a High-Fidelity Computational Framework (Invited) Current Trends in CFD Research I (Invited) Chaired by: H. HUYNH, NASA Glenn Research Center and Z. WANG, University of Kansas 0930 hrs 1000 hrs 0900 hrs Oral Presentation AIAA-2015-2917 Oral Presentation Comparison of Output Error Estimation Novel Adaptive Mechanics for High- Investigation of Unstructured for Finite Element Discretizations of Order Unstructured CFD (Invited) Higher-Order Methods for Unsteady Convection-dominated Flows (Invited) K. Fidkowski, University of Michigan, Ann flow and Moving Domains Wednesday, 24 June 2015 170-CFD-18 1000 hrs AIAA-2015-2915 Development of Generalized Summation-by-Parts Operators for the Second Derivative with Variable Coefficients Advances in High-Order Methods 1030 hrs AIAA-2015-2916 A Finite Difference WENO Scheme Maintaining Velocity, Pressure and Temperature Equilibrium in Multicomponent Compressible Fluid D. Del Rey Fernández, D. Zingg, University D. Del Rey Fernández, D. Zingg, University Analysis Chaired by: D. ZINGG, University of Toronto and P. ROE, University of Michigan 0930 hrs 0900 hrs AIAA-2015-2913 AIAA-2015-2914 New Diagonal-Norm SummationNew Approaches to Limiting P. Roe, T. Lung, J. Maeng, University of by-Parts Operators for the First Michigan, Ann Arbor, Ann Arbor, MI Derivative with Increased Order of Accuracy Wednesday, 24 June 2015 169-CFD-17 Grand Ballroom B Grand Ballroom A 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 1045-1230 hrs 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 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. 0900-1045 hrs Wednesday, 24 June 2015 168-CASE-6 0900 - 1230 hrs 85 Johns Hopkins University, Baltimore, MD Kingdom Space Center, Houston, TX; T. Coakley, NASA Ames Research Center, Moffett Field, CA B. Eisfeld, German Aerospace Center (DLR), Braunschweig, Germany; C. Rumsey, NASA Langley Research Center, Hampton, VA R. Berdanier, N. Key, Purdue University, West Lafayette, IN B. Pardowitz, German Aerospace Center (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 1000 hrs AIAA-2015-2930 Visualization of Secondary Flow Structures Caused by Rotating Instability: Synchronized Stereo High-Speed PIV and Unsteady General Electric Company, Niskayuna, NY Pressure Measurements Chaired by: Z. RUSAK, Rensselaer Polytechnic Institute and Q. WANG, MIT 0900 hrs 0930 hrs AIAA-2015-2928 AIAA-2015-2929 Data Processing Techniques for Flowfield and Film Performance Measurements Collected from Measurements of Axial Shaped a Single Slanted Hot-Wire for Cooling Holes on a Flat Plate D. Getsinger, J. Dees, G. Rodebaugh, Turbomachinery Applications Wednesday, 24 June 2015 173-FD-19 B. Smith, Lockheed Martin Corporation, Fort Worth, TX J. West, C. Groth, University of Toronto, Toronto, Canada; J. Hu, Pratt & Whitney, Mississauga, Canada 1030 hrs AIAA-2015-2921 Assessment of Hybrid RANS/LES Methods For Gas-Turbine CombustorRelevant Turbulent Flows LES, DNS, and Hybrid RANS-LES III H. Tang, S. Liu, H. Luo, Aviation Industry Corporation of China (AVIC), Shanghai, China 1030 hrs AIAA-2015-2931 Design Optimization of Profiled Endwall with Consideration of Cooling and Rim Seal Flow Effects Turbomachinery - Turbines V. Togiti, B. Eisfeld, German Aerospace Center (DLR), Braunschweig, Germany 1030 hrs AIAA-2015-2925 Assessment of g-Equation Formulation for a Second-Moment Reynolds Stress Turbulence Model (Invited) M. Stoellinger, R. Roy, University of Wyoming, Laramie, Laramie, WY; N. Ashton, University of Manchester, Manchester, United Kingdom 1100 hrs AIAA-2015-2926 Application of an Elliptic Blending Reynolds Stress Model in Attached and Separated flows (Invited) Turbulence Model Validation (Invited) Chaired by: C. RUMSEY, NASA-Langley Research Center and B. SMITH, Lockheed Martin Aeronautics 0900 hrs 0930 hrs 1000 hrs AIAA-2015-2922 AIAA-2015-2923 AIAA-2015-2924 Modification of the k-kl Two LagRST Model Predictions of a Second-Moment RANS Model Equation Turbulence Model for Wingtip Vortex Flowfield (Invited) Verification and Validation using the M. Olsen, NASA Ames Research Center, Improved Jet Flow Predictions Turbulence Modeling Resource Website Moffett Field, CA; R. Lillard, NASA Johnson (Invited) (Invited) Wednesday, 24 June 2015 172-CFD-20 N. Jain, J. Baeder, University of Maryland, College Park, College Park, MD Chaired by: J. BAEDER, University of Maryland and C. GROTH, University of Toronto 0900 hrs 0930 hrs 1000 hrs AIAA-2015-2918 AIAA-2015-2919 AIAA-2015-2920 Applications of the integral Wall Model An Embedded LES-RANS Solver for Aerodynamic Characteristics of SC1095 Airfoil using Hybrid RANS-LES in LES of flow over surfaces including Aerodynamic Simulations K. Anupindi, R. Sandberg, University of resolved and subgrid roughness Methods Implemented into a GPU X. Yang, J. Sadique, C. Meneveau, R. Mittal, Southampton, Southampton, United Accelerated Navier-Stokes Solver Wednesday, 24 June 2015 171-CFD-19 C. Rumsey, NASA Langley Research Center, Hampton, VA 1130 hrs AIAA-2015-2927 Recent Developments on the Turbulence Modeling Resource Website (Invited) Senators Lecture Hall Emerald Coral 86 University of Arizona, Tucson, Tucson, AZ Carolina State University, Raleigh, NC K. Bilimoria, S. Reardon, NASA Ames Research Center, Moffett Field, CA Chaired by: K. BILIMORIA 0900 hrs AIAA-2015-2946 Motion Parameter Selection for Flight Simulators Wednesday, 24 June 2015 177-MST-7 Institute and State University, Blacksburg, VA; E. Alyanak, Air Force Research Laboratory, Wright-Patterson AFB, OH T. Gerlach, U. Durak, German Aerospace Center (DLR), Braunschweig, Germany 0930 hrs AIAA-2015-2947 AVES SDK: Bridging the Gap between Simulator and Flight Systems Designer W. Tong, Syracuse University, Syracuse, NY; S. Chowdhury, A. Messac, Mississippi State University, Mississippi State, MS M. Mankbadi, J. DeBonis, N. Georgiadis, NASA Glenn Research Center, Cleveland, OH 1000 hrs AIAA-2015-2939 Comparison of High-Order and Low-Order Methods for Large-Eddy Simulation of a Compressible Shear Layer 1000 hrs AIAA-2015-2948 Model-Based Testing for Objective Fidelity Evaluation of Engineering and Research Flight Simulators U. Durak, German Aerospace Center (DLR), Braunschweig, Germany; A. Schmidt, T. Pawletta, University of Wismar, Wismar, Germany G. Robertson, R. Kumar, Florida State University, Tallahassee, FL; T. Eymann, S. Morton, CREATE Kestrel Team, Eglin AFB, FL H. Tabanli, K. Yuceil, Istanbul Technical University, Istanbul, Turkey 1100 hrs AIAA-2015-2936 An Experimental Investigation of the Effect of Boundary Layer on an Internal Compression Inlet Flight Simulation M. Hoogreef, G. La Rocca, Delft University of Technology, Delft, The Netherlands F. Kok, R. Myose, K. Hoffmann, Wichita State University, Wichita, KS 1100 hrs AIAA-2015-2941 Shear-Thinning Properties of Blood in Large Arteries 1030 hrs AIAA-2015-2945 An MDO advisory system supported by knowledge-based technologies Emerging Methods I J. Chabot, E. Caraballo, Miami University, Oxford, OH; J. Little, University of Arizona, Tucson, Tucson, AZ 1030 hrs AIAA-2015-2940 Reduced Order Modeling of a Dielectric Barrier Discharge Controlled Shear Layer using Minimum Basis Rotations Unsteady Flows - Cavity and Shear Flows Chaired by: E. WINER, Iowa State University and V. LI, Boeing Engineering Operations & Technology 0900 hrs 0930 hrs 1000 hrs AIAA-2015-2942 AIAA-2015-2943 AIAA-2015-2944 Multidisciplinary Design Space Arnoldi-based Sampling for High- Multi-Domain Diversity Exploration Using Additive dimensional Optimization using Preservation to Mitigate Particle Manufacturing and Rapid Prototype Imperfect Data Stagnation and Enable Better J. Hicken, A. Ashley, Rensselaer Testing Pareto Coverage in Mixed-Discrete Polytechnic Institute, Troy, NY A. Friedman, P. Raj, Virginia Polytechnic Particle Swarm Optimization Wednesday, 24 June 2015 176-MAO-5 J. Wagner, K. Casper, S. Beresh, B. Pruett, National Laboratories, Albuquerque, NM R. Spillers, J. Henfling, Sandia National Laboratories, Albuquerque, NM Chaired by: K. CASPER and K. GRANLUND, Air Force Research Laboratory 0900 hrs 0930 hrs AIAA-2015-2937 AIAA-2015-2938 Relationship between Acoustic Modal Decomposition of Pressure Tones and Flow Structure in Data in Cavity Flows Transonic Rectangular Cavity Flow K. Casper, S. Arunajatesan, Sandia Wednesday, 24 June 2015 175-FD-22 L. Vanstone, M. Saleem, S. Seckin, N. Clemens, University of Texas, Austin, Austin, TX 1030 hrs AIAA-2015-2935 Experimental and Numerical Study of Shock-Wave Boundary Layer Interactions on an Axisymmetric Body Shock Wave / Boundary Layer Interactions Chaired by: N. CLEMENS, The University of Texas at Austin and D. GAITONDE, The Ohio State University 0900 hrs 0930 hrs 1000 hrs AIAA-2015-2932 AIAA-2015-2933 AIAA-2015-2934 Effects of Sweep on Impinging Experimental Investigation of Experimental Investigation of Oblique Shock-Turbulent Boundary shock-induced corner boundary Unsteadiness of Swept-Ramp layer separation Shock/Boundary Layer Interactions Layer Interaction R. Dawson, C. Pederson, J. Little, A. Hegde, V. Narayanaswamy, North at Mach 2 Wednesday, 24 June 2015 174-FD-20 Travertine Madrid Govenors Lecture Hall Edelweiss 87 A. Osman, A. Aly, Cairo University, Cairo, Egypt; I. El baialy, Qatar University, Doha, Qatar; O. Abdellatif, Banha University, Cairo, Egypt; E. Khalil, Cairo University, Cairo, Egypt D. Zhang, X. Meng, J. Wang, Northwestern Polytechnical University, Xi’an, China; F. Liu, S. Luo, University of California, Irvine, Los Angeles, CA J. Meyers, D. Fletcher, University of Vermont, Burlington, Burlington, VT Brazil Networking Coffee Break Q. Liu, Chinese Academy of Sciences, Beijing, China; Z. Li, Y. Yang, J. Cai, Academy of Opto-Electronics, Chinese Academy of Sciences, Beijing, China 1030 hrs AIAA-2015-2952 Thermal simulation and experiments for a stratospheric balloon gondola B. Sasanapuri, ANSYS, Inc., Pune, India H. Hu, H. Li, X. Meng, J. Wang, Northwestern Polytechnical University, Xi’an, China; F. Liu, S. Luo, University of California, Irvine, Los Angeles, CA 1000 hrs AIAA-2015-2956 Starting Flow by Repetitive Nanosecond Pulsed DBD Actuation at Microseconds and Milliseconds in Quiescent Air 1100 hrs AIAA-2015-2963 Non-Equilibrium Analysis of Emission Spectroscopy Data Taken in the Freestream of the NASA IHF Arc Jet Facility D. Mei, Aviation Industry Corporation of China (AVIC), Shenyang, China; Y. Fan, C. Jiang, Beihang University, Beijing, China 1100 hrs AIAA-2015-2958 The Effect of Plasma Clouds on Aerodynamic Performance of Subsonic/Supersonic Inlets C. Dedic, J. Michael, T. Meyer, Iowa State M. Winter, C. Srinivasan, R. Charnigo, University, Ames, IA University of Kentucky, Lexington, Lexington, KY 1030 hrs AIAA-2015-2962 Hybrid fs/ps coherent anti-Stokes Raman scattering in a nonequilibrium environment initiated by a ns laser spark Plasma Diagnostics II N. Benard, National Center for Scientific Research (CNRS), Futuroscope, France; J. Pons-Prat, J. Periaux, G. Bugeda, CIMNE, Barcelona, Spain; J. Bonnet, E. Moreau, National Center for Scientific Research (CNRS), Futuroscope, France 1030 hrs AIAA-2015-2957 Multi-Input Genetic Algorithm for Experimental Optimization of the Reattachment Downstream of a Backward-Facing-Step with Surface Plasma Actuator L. Su, Y. Wu, J. Sawyer, Z. Zhang, University of Tennessee, Knoxville, Knoxville, TN 1130 hrs AIAA-2015-2964 Quantitative Measurements of Electron Number Density and Threshold for Laser Induced Breakdown in Air 1100 hrs AIAA-2015-2953 Real Time Multiple Fidelity Physics Based Simulation of Aircraft Environmental Control System Plasma Aerodynamics & Flow Control IV W. Yan, Aviation Industry Corporation of China (AVIC), Beijing, China; X. Luo, Aviation Industry Corporation of China (AVIC), Chengdu, China; D. Cui, Aviation Industry Corporation of China (AVIC), Beijing, China 1000 hrs AIAA-2015-2951 Strength Analysis and Optimization Technique for Thermal Protection System using 3 Dimensional Element Model Computational Methods for Fluid Dynamics and Heat Transfer Simulations Chaired by: N. HARADA, Nagaoka University of Technology and J. BURT, Universal Technology Corporation 0900 hrs 0930 hrs 1000 hrs AIAA-2015-2959 AIAA-2015-2960 AIAA-2015-2961 Planar Two-Photon LIF Particle Vaporization Velocimetry Investigation of Non-Equilibrium Measurements of Atomic Species for LPG Diffusion Flames Nitrogen Plasmas A. Lutz, D. Fletcher, University of Vermont, in a High-Temperature Inductively L. Tolomelli, Technological Institute of Aeronautics (ITA), São José dos Campos, Burlington, Burlington, VT Couple Plasma Environment Wednesday, 24 June 2015 181-PDL-9/TP-8 X. Meng, X. Yan, H. Hu, Northwestern Polytechnical University, Xi’an, China; F. Liu, S. Luo, University of California, Irvine, Irvine, CA Chaired by: T. DOUVILLE, TLG Aerospace, LLC. 0900 hrs 0930 hrs AIAA-2015-2954 AIAA-2015-2955 Plasma Laminar-SeparationPressures over a Conical Forebody Bubble Control over Airfoil at Low under Repetitive Nanosecond Pulse Reynolds Numbers SDBD Actuations Wednesday, 24 June 2015 180-PDL-8/APA-20 Wednesday, 24 June 2015 179-NW-6 0900 - 0930 hrs B. Jaffrezic, M. Ruetten, H. Rosemann, German Aerospace Center (DLR), Göttingen, Germany Chaired by: M. KOKALY and B. JAFFREZIC 0900 hrs 0930 hrs AIAA-2015-2949 AIAA-2015-2950 Investigation of the effect of grid Aerodynamics Flight Mechanics Approach on Compact Domains for size on external store separation trajectory using CFD Air Vehicle Separation Wednesday, 24 June 2015 178-MST-8 Miro Stemmons C Chantilly Ballroom East Wyeth 88 M. Wilder, NASA Ames Research Center, Moffett Field, CA; D. Bogdanoff, D. Saunders, ERC, Inc., Moffett Field, CA K. Naitoh, Y. Tanaka, T. Tamura, T. Okamoto, Y. Nojima, K. Yamagishi, Waseda University, Shinjuku, Japan 1030 hrs AIAA-2015-2968 Fugine cycle theory: predicting high efficiency of the supermultijetconvergence engine working from startup to hypersonic scram mode 1500 hrs AIAA-2015-2971 Numerical investigation of combustion noise generation in a full annular combustion chamber W. Ullrich, T. Sattelmayer, Technical University of Munich, Garching, Germany Combustion Noise Luncheon in the Exposition Hall State University, Raleigh, NC Toulouse, France; E. Bouty, Turbomeca, Bordes, France 1530 hrs AIAA-2015-2972 Transfer Functions of Acoustic, Entropy and Vorticity Waves in an Annular Model Combustor and T. Livebardon, CERFACS, Toulouse, France; Nozzle for the Prediction of the S. Moreau, University of Sherbrooke, Y. Liu, University of Surrey, Guildford, Ratio Between Indirect and Direct United Kingdom; T. Echekki, North Carolina Sherbrooke, Canada; T. Poinsot, CERFACS, Combustion Noise Chaired by: J. MENDOZA, United Technologies Research Center 1400 hrs 1430 hrs AIAA-2015-2970 AIAA-2015-2969 Modelling of combustion noise On the spectrum of combustion noise spectrum using temporal C. Tam, Florida State University, correlations of heat release rate Tallahassee, FL from turbulent premixed flames Wednesday, 24 June 2015 185-AA-26 A ticket is required and included in the conference registration fee where indicated. Wednesday, 24 June 2015 184-LNCH-2 1230 - 1400 hrs F. Grimm, German Aerospace Center (DLR), Stuttgart, Germany; R. Ewert, J. Dierke, German Aerospace Center (DLR), Braunschweig, Germany; B. Noll, M. Aigner, German Aerospace Center (DLR), Stuttgart, Germany 1600 hrs AIAA-2015-2973 Efficient Full 3D Turbulent Combustion Noise Simulation Based on Stochastic Sound Sources Grand Ballroom E Rosetta J. Zheng, M. Huet, ONERA, Châtillon, France; A. Giauque, National Center for Scientific Research (CNRS), Ecully, France; F. Cléro, ONERA, Châtillon, France; S. Ducruix, National Center for Scientific Research (CNRS), Châtenay-Malabry, France Fleur-de-lis B Chantilly Ballroom East Jaiwon Shin Associate Administrator, Aeronautics Research Mission Directorate NASA Headquarters 1630 hrs AIAA-2015-2974 A 2D-axisymmetric analytical model for the estimation of indirect combustion noise in nozzle flows David McBride Center Director NASA Armstrong Flight Research Center NACA to NASA: Embarking on the Next 100 Years of Excellence and Innovation in Aeronautics and Beyond E. Zishka, R. Agarwal, Washington University in St. Louis, St. Louis, MO 1000 hrs AIAA-2015-2967 Shape Optimization of a Blunt Body in Reacting Hypersonic flow in Thermal Non-Equilibrium for Reducing Both Drag and Heat Transfer Aerothermodynamics II Moderator: Robert Pearce, Director, Strategy, Architecture & Analysis, Aeronautics Research Mission Directorate, NASA Headquarters Panelists: David Bowles Thomas Edwards Janet Kavandi Center Director (Acting) Deputy Center Director Deputy Director NASA Langley Research Center NASA Ames Rsearch Center NASA Glenn Research Center Wednesday, 24 June 2015 183-F360-5 0930 - 1200 hrs Chaired by: A. MARTIN, University of Kentucky 0900 hrs 0930 hrs AIAA-2015-2965 AIAA-2015-2966 Heat Transfer Measurements on the Shock Radiation Tests for Saturn Afterbody of Spheres in Hypersonic and Uranus Entry Probes B. Cruden, D. Bogdanoff, ERC, Inc., Free-Flight in Air and Carbon Moffett Field, CA Dioxide Wednesday, 24 June 2015 182-TP-9 89 Germany 1430 hrs AIAA-2015-2988 Evaluation of Airframe Noise Reduction Concepts via Simulations Using a Lattice Boltzmann Approach Hampton, VA; R. Mineck, Self, Yorktown, VA; E. Fares, Exa GmbH, Stuttgart, Germany; C. Yao, L. Jenkins, NASA Langley Research Center, Hampton, VA 1630 hrs AIAA-2015-2985 Analytical Prediction of the PylonWake Effect on the Tonal Noise radiated by the Front-Rotor of CROR Propulsion Systems 1600 hrs AIAA-2015-2991 Characterization of Flap Edge Noise Radiation from a High-Fidelity Airframe Model 1700 hrs AIAA-2015-2993 Simulations of LAGOON landinggear noise using Lattice Boltzmann Solver Lalique I. Belyaev, V. Kopiev, R. Skvortsov, I. Pankratov, TsAGI, Moscow, Russia; V. Titarev, Russian Academy of Sciences, Moscow, Russia; M. Zaytsev, TsAGI, Moscow, Russia 1700 hrs AIAA-2015-2986 Comparison of rotor noise measurement results in large-scale and small-scale anechoic facilities Inverness Fleur-de-lis A D. Casalino, E. Fares, B. Duda, A. Hazir, A. Sengissen, J. Giret, Airbus, Toulouse, Exa GmbH, Stuttgart, Germany; M. France; C. Coreixas, J. Boussuge, Khorrami, NASA Langley Research Center, CERFACS, Toulouse, France Hampton, VA 1630 hrs AIAA-2015-2992 On the Connection between Flap Side-Edge Noise and Tip Vortex Dynamics S. Moreau, M. Quaglia, Sherbrooke University, Sherbrooke, Canada; R. N. Jaouani, Sogeti High Tech, Issy Les Fernando, Safran Group, Moissy-Cramayel, Moulineaux, France; M. Roger, École Centrale France de Lyon, Lyon, France; T. Nodé-Langlois, Airbus, Toulouse, France; G. Serre, Sogeti High Tech, Issy Les Moulineaux, France 1600 hrs AIAA-2015-2984 A 3D analytical approach for Open rotor Blade Vortex Interaction(BVI) tonal noise B. Tester, K. Holland, University of Southampton, Southampton, United Kingdom 1600 hrs 1630 AIAA-2015-2979 Discussion Estimating the sound power radiated by a nozzle-based source in a test cell using a phased array W. Humphreys, M. Khorrami, D. Lockard, D. Lockard, W. Humphreys, M. Khorrami, D. Neuhart, C. Bahr, NASA Langley NASA Langley Research Center, Hampton, Research Center, Hampton, VA VA; E. Fares, D. Casalino, Exa GmbH, Stuttgart, Germany; P. Ravetta, AVEC, Inc., Blacksburg, VA 1530 hrs AIAA-2015-2990 Comparison of Computational and Experimental Microphone Array Results for an 18%-Scale Aircraft M. Khorrami, NASA Langley Research Center, Model 1500 hrs AIAA-2015-2989 A Comparative Study of Simulated and measured Gear-Flap Flow Interaction Airframe Noise III S. Sinayoko, University of Southampton, Southampton, United Kingdom Open Rotor II J. Underbrink, The Boeing Company, Seattle, WA 1530 hrs AIAA-2015-2978 Pletharrays for Aeroacoustic Phased Array Applications Arrays Method Panel Session 1530 hrs AIAA-2015-2983 Broadband noise for rotating blades: analysis of acceleration effects in the time and frequency J. Wang, K. Wang, M. Wang, University of domains 1500 hrs AIAA-2015-2982 Computation of Rotor Noise Generation in Grid Turbulence Using Large-Eddy Simulation G. Herold, E. Sarradj, Brandenburg University of Technology, Cottbus, Germany 1500 hrs AIAA-2015-2977 An Approach to Estimate the Reliability of Microphone Array Methods D. Wisda, H. Murray, W. Alexander, M. Nelson, W. Devenport, Virginia Polytechnic Notre Dame, Notre Dame, IN Institute and State University, Blacksburg, VA; S. Glegg, Florida Atlantic University, Boca Raton, FL M. Khorrami, W. Humphreys, D. Lockard, NASA Langley Research Center, Hampton, VA E. Fares, D. Casalino, Exa GmbH, Stuttgart, Germany; M. Khorrami, NASA Langley Research Center, Hampton, VA Chaired by: S. NOELTING, EXA 1400 hrs AIAA-2015-2987 An Assessment of Flap and Main Landing Gear Noise Abatement Concepts Wednesday, 24 June 2015 188-AA-29 Châtillon, France Chaired by: W. DEVENPORT, Virginia Tech 1400 hrs 1430 hrs AIAA-2015-2980 AIAA-2015-2981 Open-Rotor Noise Assessment with Flow Distortion and Noise Produced CFD/CAA Chaining by a Thrusting Rotor Ingesting a A. Chelius, T. Le Garrec, D. Mincu, ONERA, Planar Turbulent Boundary Layer Wednesday, 24 June 2015 187-AA-28 W. Horne, N. Burnside, NASA Ames Research Center, Moffett Field, CA Chaired by: C. BAHR, NASA-Langley Research Center 1400 hrs 1430 hrs AIAA-2015-2975 AIAA-2015-2976 Development of New Wall-mounted Decorrelation of Acoustic Wave Propagation through the Shear and Strut-mounted Phased Layer in Open Jet Wind Tunnel Microphone Arrays for Acoustic D. Ernst, C. Spehr, T. Berkefeld, German Measurements in Closed TestAerospace Center (DLR), Göttingen, section Wind Tunnels Wednesday, 24 June 2015 186-AA-27 90 V. Kopiev, I. Belyaev, G. Faranosov, M. Zaytsev, TsAGI, Moscow, Russia; A. Aleksentsev, Y. Bersenev, OJSC Aviadvigatel, Perm, Russia; et al. Institute of Technology, Atlanta, GA K. Xie, F. Wang, N. Chen, L. Chen, Q. Shen, China Academy of Aerospace Aerodynamics, Beijing, China L. Zientarski, C. Marks, University of Dayton, Dayton, OH; J. Joo, Air Force Research Laboratory, Wright-Patterson AFB, OH R. Shi, J. Peng, Tsinghua University, Beijing, China 1500 hrs AIAA-2015-3002 Morphing Strategy Design for Variable-Wing Aircraft L. Jenkins, G. Yamauchi, NASA Langley Research Center, Hampton, VA (DLR), Cologne, Germany Delft, The Netherlands L. Gonzalez-Linero, Embry-Riddle Aeronautical University, Daytona Beach, FL 1600 hrs AIAA-2015-3004 The Hoops on the Way to a Supersonic Business Jet (Performance Drivers for a Commercially Viable Product) G. Hammock, Arnold Engineering Development Complex, Arnold AFB, TN 1530 hrs AIAA-2015-3008 Comparison of Freejet Data between a Contoured and Conical Nozzle in the AEDC H1 Facility J. Stephens, E. Hubbard, NASA Langley Research Center, Hampton, VA 1600 hrs Oral Presentation Overview of Uncertainty Analysis Activities at NASA Glenn’s Aeropropulsion Facilities Ground Test Facility Improvements II I. Roy Salam, C. Bil, RMIT University, Melbourne, Australia 1530 hrs AIAA-2015-3003 A Methodology for MultiDisciplinary Analysis of the Box Wing Concept J. Heineck, NASA Ames Research Center, Moffett Field, CA 1530 hrs Oral Presentation Subsonic Wake Characterization of the Orion Capsule using PIV in the Ames UPWT 11-foot Wind Tunnel (Invited) H. Kato, S. Koike, Japan Aerospace Exploration Agency (JAXA), Tokyo, Japan 1600 hrs Oral Presentation Industrial Applications of PIV in JAXA Large-Scale Wind Tunnels (Invited) F. de Souza, National Research Council Canada, Ottawa, Canada 1630 hrs Oral Presentation Recent Applications of PIV in Large NRC Wind Tunnels S. Dunn, NASA Langley Research Center, Hampton, VA Y. Michou, ONERA, Chambery, France Edelweiss Obelisk B Morocco Obelisk A 1700 hrs Oral Presentation Applications of PIV measurements in the ONERA large wind tunnels (Invited) 1630 hrs AIAA-2015-3009 Reactivation of the NTF 3000 Ton Liquid Nitrogen Tank from Ambient Condition 1630 hrs AIAA-2015-2999 Investigating the feedback path in a jet-surface resonant interaction S. Piantanida, V. Jaunet, P. Jordan, J. Huber, K. Zaman, A. Fagan, J. Bridges, C. Brown, National Center for Scientific Research (CNRS), NASA Glenn Research Center, Cleveland, Poitiers, France; A. Cavalieri, Technological OH Institute of Aeronautics (ITA), São José dos Campos, Brazil; W. Wolf, University of Campinas, Campinas, Brazil 1600 hrs AIAA-2015-2998 Scattering of turbulent-jet wavepackets by a swept trailing edge The Impact of PIV on Aerospace Technology I Chaired by: S. BERESH, Sandia National Laboratories and K. LOWE, Virginia Tech 1430 hrs 1500 hrs 1400 hrs Oral Presentation Oral Presentation Oral Presentation PIV for helicopter aerodynamics Time-resolved PIV in the buffeting Application of Particle Image regime of ARIANE V (Invited) Velocimetry at NASA for Rotorcraft (Invited) M. Raffel, German Aerospace Center F. Scarano, Delft University of Technology, Research (Invited) Wednesday, 24 June 2015 192-AMT-12/GT-12 M. Sadraey, Daniel Webster College, Nashua, NH A. Karon, D. Dickey, K. Ahuja, Georgia Institute of Technology, Atlanta, GA 1530 hrs AIAA-2015-2997 Role of Nozzle’s Proximity to Plenum Chambers or Other Nonline-of-sight Devices on Measured Jet Noise Jet Noise Measurements II Design of Unconventional Aircraft Configurations U. Michel, CFD Software GmbH, Berlin, Germany 1500 hrs AIAA-2015-2996 On the systematic error in measurements of jet noise flight effects using open jet wind tunnels Chaired by: R. RHEW, NASA-Langley Research Center and J. HOPF, Aerospace Testing Alliance 1400 hrs 1430 hrs 1500 hrs AIAA-2015-3005 AIAA-2015-3006 AIAA-2015-3007 Lyapunov-Based Nonlinear Control Development and Demonstration Wind Tunnel Testing of Variable of Wind Tunnel Supersonic Nozzle of A Continuous Beta Sweep Test & Camber Compliant Wing with Multiple Contour Analysis Technique(CBSTAT) Rig Load Cell Test Fixture Wednesday, 24 June 2015 191-AMT-11/GT-11 V. Mirochnitchenko, T. Takahashi, Arizona State University, Tempe, AZ Chaired by: M. LOGAN, NASA Langley Research Center 1400 hrs 1430 hrs AIAA-2015-3000 AIAA-2015-3001 An Investigation into the Design of Advanced General Aviation Concept an Efficient In Ground Effect Flying Study for a Roadable Aircraft D. Lim, C. Justin, D. Mavris, Georgia Vehicle Planform Wednesday, 24 June 2015 190-ACD-5 National Center for Scientific Research (CNRS), Poitiers, France; A. Cavalieri, Technological Institute of Aeronautics (ITA), São José dos Campos, Brazil Chaired by: D. JUVE, Ecole Centrale de Lyon 1400 hrs 1430 hrs AIAA-2015-2994 AIAA-2015-2995 Dual-plane, time-resolved, stereo PIV Adaptation of the Azimuthal for wavepacket eduction in a turbulent Decomposition Technique to Jet Noise Measuerements of an Aircraft subsonic jet V. Jaunet, P. Braud, F. Boissonneau, P. Jordan, Engine in the Ground Tests Wednesday, 24 June 2015 189-AA-30 91 K. Lo, K. Kontis, University of Glasgow, Glasgow, United Kingdom Q. Zhao, C. Sheng, University of Toledo, Toledo, OH M. Kotov, I. Kryukov, L. Ruleva, S. Solodovnikov, S. Surzhikov, Russian Academy of Sciences, Moscow, Russia G. Gori, M. Zocca, A. Guardone, Technical University of Milan, Milan, Italy Canada; C. Aliaga, Newmerical Technologies International, Montréal, Canada; W. Habashi, McGill University, Montréal, Canada E. Sheta, R. Harris, CFD Research Corporation, Huntsville, AL; E. Luke, Mississippi State University, Mississippi State, MS; L. Ukeiley, University of Florida, Gainesville, Gainesville, FL 1530 hrs AIAA-2015-3018 Loads and Acoustics Prediction on Deployed Weapons Bay Doors M. Hughes, S. McClain, Baylor University, State University, Stillwater, OK Waco, TX; M. Vargas, A. Broeren, NASA Glenn Research Center, Cleveland, OH T. Misaka, S. Obayashi, Tohoku University, Sendai, Japan; A. Stephan, F. Holzäpfel, T. Gerz, German Aerospace Center (DLR), Oberpfaffenhofen, Germany 1600 hrs AIAA-2015-3023 Sensitivity Analysis of Wake Vortex Parameters Measured by Doppler J. Hathaway, A. Avery, J. Jacob, Oklahoma Lidar 1530 hrs AIAA-2015-3022 Sensor Suite Development for a Weather UAV Aircraft Icing and Atmospheric Hazards Chaired by: W. VAUGHAN, William W Vaughan Consultant and J. OWENS, NASA (Retired) 1430 hrs 1500 hrs 1400 hrs AIAA-2015-3020 AIAA-2015-3021 AIAA-2015-3019 A model for in-flight ice accretion Quasi-Unsteady Icing Simulation of Convective Enhancement of Icing Roughness Elements in Stagnation based on the exact solution of the an Oscillating Airfoil H. Fouladi, McGill University, Montréal, Region Flows unsteady Stefan problem Wednesday, 24 June 2015 196-ASE-2 VSTOL/STOL Aerodynamics Weapons Aerodynamics: Missile/Projectile/Guided-Munitions, Carriage and Store Separation II 1500 hrs AIAA-2015-3017 Cavity-Store Interaction under Supersonic Freestream Conditions 1500 hrs AIAA-2015-3012 Supersonic Air Flows Around Some Geometrical Primitives Transonic & Supersonic Aerodynamics J. Merrick, M. Reeder, Air Force Institute of Point, NY; S. Silton, Army Research Technology, Wright-Patterson AFB, OH S. Geisbauer, German Aerospace Center Laboratory, Aberdeen Proving Ground, MD (DLR), Braunschweig, Germany; H. Schmidt, German Aerospace Center (DLR), Göttingen, Germany Chaired by: K. DENISSEN, Sandia National Labs 1400 hrs 1430 hrs AIAA-2015-3015 AIAA-2015-3016 CFD Aerodynamic Characterization Development and Validation of a of a High Maneuverability Airframe RANS-based Airdrop Simulation C. Coyle, U.S. Military Academy, West Approach Wednesday, 24 June 2015 195-APA-23 M. Duffy, A. Samaritano, The Boeing Company, Ridley Park, PA 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 Wednesday, 24 June 2015 194-APA-22 Aerospace, Hampton, VA; M. Mullane, University of Alabama, Birmingham, Birmingham, AL; G. Cheng, University of Alabama, Tuscaloosa, Tuscaloosa, AL; C. Chang, NASA Langley Research Center, Hampton, VA Chaired by: M. JURKOVICH, US Air Force 1400 hrs 1430 hrs AIAA-2015-3010 AIAA-2015-3011 Numerical Study of Counterflowing Flow Physics of a ThreeJet Effects on Supersonic Slender- Dimensional Rounded Contour Bump in a Mach 1.3 Supersonic Body Configurations B. Venkatachari, National Institute of Free-stream Wednesday, 24 June 2015 193-APA-21 Plum Blossom B Stemmons B Carpenter Ballroom Stemmons A 92 A. Mahashabde, MITRE Corporation, McLean, VA J. Neilan, C. Cross, H. Fan, W. Fehlman, L. Hempley, M. Motter, NASA Langley Research Center, Hampton, VA; et al. Chaired by: B. ALLEN, NASA Langley Research Center 1400 hrs 1430 hrs AIAA-2015-3032 AIAA-2015-3033 Using Multimodal Input for Collaborating with Autonomous Autonomous Decision Making Agents A. Trujillo, NASA Langley Research for Unmanned Systems - “What Center, Hampton, VA; H. Fan, Analytical it needs in order to evolve, is a human quality. Our capacity to leap Mechanics Associates, Inc., Hampton, VA; L. Hempley, C. Cross, Northrop Grumman beyond logic.” - Capt. Kirk, Star Corporation, Hampton, VA; W. Fehlman, Trek: The Motion Picture M. Motter, NASA Langley Research Center, Hampton, VA; et al. California, Santa Cruz, Santa Cruz, CA; W. A. Wilson, M. LeVine, J. Bernardo, M. Malik, University of California, Santa Cruz, Kirby, D. Mavris, Georgia Institute of Moffett Field, CA; Y. Jung, NASA Ames Technology, Atlanta, GA Research Center, Moffett Field, CA Wednesday, 24 June 2015 199-ATIO-20 H. Yang, Civil Aviation Flight University of China, Guanghan, China S. Sidiropoulos, A. Majumdar, K. Han, W. Schuster, W. Ochieng, Imperial College London, London, United Kingdom 1530 hrs AIAA-2015-3031 A framework for the classification and prioritization of arrival and departure routes in Multi-Airport Systems Terminal Manoeuvring Areas G. Qualls, C. Cross, H. Fan, W. Fehlman, L. Hempley, M. Motter, NASA Langley Research Center, Hampton, VA; et al. 1530 hrs AIAA-2015-3035 Operating in “Strange New Worlds” and Measuring Success - Test and Evaluation in Complex P. Rothhaar, C. Cross, H. Fan, W. Fehlman, Environments L. Hempley, M. Motter, NASA Langley Research Center, Hampton, VA; et al. V. Stouffer, LMI, McLean, VA; K. Goodrich, NASA Langley Research Center, Hampton, VA 1600 hrs AIAA-2015-3036 State of the Art of Autonomous Platforms and Human-Machine Systems: Only a Fool Would Stand In the Way of Progress Transformational Flight - Autonomy II 1500 hrs AIAA-2015-3034 A Flexible Flight Control System for Rapid GNC and Distributed Control Deployment F. Wieland, W. Krueger, W. Peng, Y. Zhang, A. Tyagi, C. Ye, Intelligent Automation, Inc., Rockville, MD; et al. 1500 hrs AIAA-2015-3030 Implementing a Combined Arrival, Departure, and Surface Scheduler for a Metroplex Terminal & Surface Operations IV R. Mayer, B. Crow, D. Zondervan, MITRE Corporation, McLean, VA; J. Allerdice, Federal Aviation Administration, Peachtree City, GA 1530 hrs AIAA-2015-3027 Concept and Benefits of PBN-Enabled Parallel Approach Operations ATM IV - Economic/Benefits Analysis 1500 hrs AIAA-2015-3026 Airfare Determinants on the Kangaroo Route (Australia-UK Market): A Case Study of the Influences of Airlines, S. Tsao, J. DeArmon, S. Agbolosu-Amison, Alliances and Airports 1430 hrs AIAA-2015-3025 Assessing Departure Efficiency at U.S. Airports: a Comparison of Methods Chaired by: R. CURRAN, Delft Technical University of Technology 1400 hrs 1430 hrs AIAA-2015-3028 AIAA-2015-3029 Optimization of Push Back Time Development of Generic Ground Windows That Ensure Conflict Free Tracks of Performance Based Ramp Area Aircraft Trajectories Navigation Operations for FleetJ. Coupe, D. Milutinovic, University of Level Airport Noise Analysis Wednesday, 24 June 2015 198-ATIO-19 S. Landry, D. Peng, Purdue University, West Lafayette, IN Chaired by: S. HASAN, LMI 1400 hrs AIAA-2015-3024 Identifying benefit mechanisms for NextGen technologies and concepts Wednesday, 24 June 2015 197-ATIO-18 Monet Ballroom Milan Ming 93 J. Marsh, Columbia Scientific Balloon Facility, Palestine, TX; M. Giles, Raven Aerostar, Sulphur Springs, TX G. Candler, University of Minnesota, Minneapolis, Minneapolis, MN Champaign, Urbana, IL A. Pandare, H. Luo, North Carolina State University, Raleigh, NC H. Shah, Wichita State University, Wichita, KS Carolina State University, Raleigh, NC Fairbrother, M. Said, S. Lang, NASA Wallops Flight Facility, Wallops Island, VA P. Vincent, F. Witherden, A. Farrington, G. Q. Wang, Massachusetts Institute of Ntemos, B. Vermeire, J. Park, Imperial College Technology, Cambridge, MA London, London, United Kingdom; et al. 1600 hrs AIAA-2015-3051 Towards high-fidelity aerospace design in the age of extreme scale supercomputing (Invited) Technology, Melbourne, FL; T. Jackson, University of Florida, Gainesville, Gainesville, FL R. Jambunathan, D. Levin, University of Illinois, Urbana-Champaign, Urbana, IL 1530 hrs AIAA-2015-3057 A Hybrid CPU-GPU Parallel Octree Direct Simulation Monte Carlo Approach C. Stone, Computational Science and Engineering, LLC, Chicago, IL; R. Davis, University of California, Davis, Davis, CA 1600 hrs AIAA-2015-3058 High-Performance 3D MultiDisciplinary Fluid/Thermal Prediction using Combined MultiCore/Multi-GPGPU Computer Systems Parallel Computing and Novel Architectures Chaired by: L. LUO, North Carolina State University and C. STONE, Computational Science and Engineering 1430 hrs 1500 hrs 1400 hrs AIAA-2015-3055 AIAA-2015-3056 AIAA-2015-3054 Optimization of A Fine-grained GPU Parallelization of a High Order Parallel Techniques for NavierImmersed Boundary Method Fluid Stokes Solver based on 4th Order BILU by CUDA Inter-block Synchronization Solver Modified Runge-Kutta Scheme L. Luo, J. Edwards, H. Luo, F. Mueller, North A. Jost, J. Zhang, Florida Institute of with TVD Wednesday, 24 June 2015 203-CFD-23 CA; F. Ham, Cascade Technologies, Inc., Palo Alto, CA 1630 hrs AIAA-2015-3042 Shape Analysis of the 1/20-Scale ExaVolt Antenna Test Balloon Grand Ballroom B L. Mangani, G. Romanelli, University of Applied Sciences and Arts, Luzern, Switzerland; A. Gaddai, Technical University of Milan, Milan, Switzerland; E. Casartelli, University of Applied Sciences and Arts, Luzern, Switzerland 1630 hrs AIAA-2015-3059 Comparison Of Acceleration Techniques on CFD Open-Source Software for Aerospace Applications Plum Blossom A 1700 hrs AIAA-2015-3053 CFD for Next Generation Hardware: Experiences with Proxy Applications Grand Ballroom A K. Franko, T. Fisher, P. Lin, S. Bova, J. Alonso, Stanford University, Stanford, CA Sandia National Laboratories, Albuquerque, NM 1630 hrs AIAA-2015-3052 Opportunities and Challenges for Multi-Disciplinary Analysis and Optimization at Exascale (Invited) Washington, DC E. Bering, R. Gamblin, University of Houston, Houston, TX Steuben 1700 hrs AIAA-2015-3043 An Undergraduate Student Instrumentation Project (USIP) to F. Baginski, George Washington Develop New Instrument Technology F. Baginski, George Washington University, University, Washington, DC; K. Brakke, to Study the Auroral Ionosphere and Susquehanna University, Selinsgrove, PA; Stratospheric Ozone Layer Using Washington, DC; P. Gorham, University K. Zhao, George Washington University, of Hawaii, Honolulu, Honolulu, HI; D. Ultralight Balloon Payloads 1600 hrs AIAA-2015-3041 Technology Development for the ExaVolt Antenna (EVA). 1/20-Scale Deployment Test Future of Fluids: Next Generation CFD (Invited) Laramie, Laramie, WY; A. Wissink, Army Aviation and Missile Research Development and Engineering Center, Moffett Field, CA Chaired by: M. MALIK, NASA-Langley Research Center and A. KHODADOUST, Boeing Engineering Operations & Technology 1400 hrs 1430 hrs 1500 hrs 1530 hrs Oral Presentation AIAA-2015-3048 AIAA-2015-3049 AIAA-2015-3050 Impacting Design with Large Eddy Next-Generation CFD for Scaling Limits for PDE-Based PyFR: Next-Generation High-Order Simulation (Invited) Hypersonic and Aerothermal Flows Simulation (Invited) Computational Fluid Dynamics on P. Moin, Stanford University, Stanford, P. Fischer, University of Illinois, Urbana(Invited) Many-Core Hardware (Invited) Wednesday, 24 June 2015 202-CFD-22 University of Michigan, Ann Arbor, Ann Arbor, MI 1530 hrs AIAA-2015-3047 A Hybrid Reconstructed Discontinuous Galerkin and Continuous Galerkin method for Incompressible Flows L. Diosady, S. Murman, NASA Ames Research Center, Moffett Field, CA Discontinuous Galerkin Methods D. Varga, NASA Glenn Research Center, Cleveland, OH; E. Young, Southwest Research Institute, Boulder, CO 1530 hrs AIAA-2015-3040 Current Status of a NASA HighAltitude Balloon-Based Observatory for Planetary Science Chaired by: C. SCHROCK, Air Firce Research Laboratory and L. DIOSADY, NASA Ames Research Center 1400 hrs 1430 hrs 1500 hrs AIAA-2015-3044 AIAA-2015-3045 AIAA-2015-3046 General element shapes within High-order Discontinuous Galerkin An Adaptive Explicit 3D Discontinuous a tensor-product higher-order Methods Applied to Multiphase Galerkin Solver for Unsteady space-time discontinuous-Galerkin Flows Problems M. Henry de Frahan, E. Johnsen, A. Kirby, D. Mavriplis, University of Wyoming, formulation D. Stuchlik, NASA Goddard Space Flight Center, Greenbelt, MD 1500 hrs AIAA-2015-3039 The Wallops Arc Second Pointer - A Balloon Borne Fine Pointing System Balloon Systems II Wednesday, 24 June 2015 201-CFD-21 CA Chaired by: J. RAND, Winzen Engineering Inc 1400 hrs 1430 hrs AIAA-2015-3037 AIAA-2015-3038 Recent Improvements to the Design Balloon Aspect of StratEx World and Manufacture of High Altitude Record Skydive J. Nott, Nott Technology, Santa Barbara, Zero-Pressure Balloons Wednesday, 24 June 2015 200-BAL-2 94 1500 hrs AIAA-2015-3062 A Continuous Sensitivity Equation of Arbitrary High Order S. Spagnolo, X. Zhang, Z. Hu, D. Angland, S. Poroseva, J. Colmenares, University of University of Southampton, Southampton, New Mexico, Albuquerque, Albuquerque, United Kingdom NM; S. Murman, NASA Ames Research Center, Moffett Field, NM 1600 hrs AIAA-2015-3064 Design and Optimization of a Supersonic Business Jet Leslie Perkins Director, Energy Office Air Force Research Laboratory System Complexity : Government Needs and Practical Research Results Askin Isikveren Head of Visionary Aircraft Concepts Bauhaus Luftfahrt The Challenges of Green Aviation J. Sudani, R. Prasad, M. Damodaran, Indian Institute of Technology Gandhinagar, Ahmedabad, India 1530 hrs AIAA-2015-3068 High-Fidelity Computational Assessment of the Performance of a Vertical Axis Wind Turbine Turbulent Flow Simulations II S. Qiu, D. Yang, Aviation Industry Corporation F. Kiyici, S. Aradag, TOBB University of of China (AVIC), Shanghai, China Economics and Technology, Ankara, Turkey 1530 hrs AIAA-2015-3063 Design optimization of a high bypass ratio fan rotor against water ingestion Design Optimization Emerald Grand Ballroom E Grand Ballroom D Jeanne Yu Environmental Director Boeing Commercial Airplanes Coral 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 207-F360-7/CASE-7 1400 - 1730 hrs Moderator: Marty Bradley, Technical Fellow, Boeing Commercial Airplanes Panelists: Ricky Curran Jay E. Dryer Director, Advanced Air Vehicles Program Office (Acting) Faculty of Aerospace Engineering Aeronautics Research Mission Directorate Delft University of Technology NASA Headquarters Wednesday, 24 June 2015 206-F360-6 1400 - 1630 hrs K. Goparaju, D. Gaitonde, S. Bhaumik, Ohio State University, Columbus, OH Chaired by: F. VERGINE and L. DUAN, Missouri University of Science and Technology 1400 hrs 1430 hrs 1500 hrs AIAA-2015-3065 AIAA-2015-3066 AIAA-2015-3067 Investigation of a Twinjet Numerical Simulations of RANS Simulations of a Channel Configuration with and without Single and Tandem Wheels for Flow with a New Velocity/PressureFlow Control Aerodynamic Loads Prediction Gradient Model Wednesday, 24 June 2015 205-CFD-25 C. Belley, A. Hay, D. Pelletier, École F. Palacios, The Boeing Company, Everett, R. Rashad, D. Zingg, University of Toronto, Polytechnique de Montréal, Montréal, WA; T. Economon, J. Alonso, Stanford Canada Toronto, Canada University, Stanford, CA Chaired by: L. TAO, GE Global Research 1400 hrs 1430 hrs AIAA-2015-3060 AIAA-2015-3061 Aerodynamic Shape Optimization Adjoint-Based Optimization of a for Natural Laminar Flow Using a Hypersonic Inlet H. Kline, Stanford University, Stanford, CA; Discrete-Adjoint Approach Wednesday, 24 June 2015 204-CFD-24 95 Y. Hu, H. Zhang, Northwestern Polytechnical University, Xi’an, China M. Percin, B. van Oudheusden, Delft University of Technology, Delft, The Netherlands 1630 hrs AIAA-2015-3080 Delaying transition in rotating boundary-layer flows P. Griffiths, University of Birmingham, H. Kurz, M. Kloker, University of Stuttgart, Birmingham, United Kingdom; S. Garrett, University of Leicester, Leicester, United Stuttgart, Germany Kingdom; S. Stephen, University of New South Wales, Sydney, Australia 1600 hrs AIAA-2015-3079 Swept-Wing Boundary-Layer Receptivity to Steady Free-Stream Disturbances Flow Control Technologies - Barriers/Challenges to Tech Transition C. Mortensen, X. Zhong, University of California, Los Angeles, Los Angeles, CA A. Cerminara, N. Sandham, University of Southampton, Southampton, United Kingdom 1530 hrs AIAA-2015-3078 Leading-Edge Receptivity to Acoustic Waves for High-Speed Flows over a Blunt Wedge Boundary Layer Transition: Receptivity and Control Laboratory, Wright-Patterson AFB, OH Topaz Sapphire Govenors Lecture Hall 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 210-FD-25 1400 - 1730 hrs Mississippi State, MS; M. Afsar, Imperial A. Chou, NASA Langley Research Center, College London, London, United Kingdom; Hampton, VA; S. Schneider, Purdue V. Sassanis, Mississippi State University, University, West Lafayette, IN Mississippi State, MS 1600 hrs AIAA-2015-3073 Transient Encounters of a NACA0012 Wing with a Streamwise-Oriented Vortex 1630 hrs AIAA-2015-3074 Flow Visualization and Force Measurements on Accelerated Revolving Flat Plates at Low R. Gordnier, M. Visbal, Air Force Research D. Garmann, M. Visbal, Air Force Research Reynolds Numbers 1530 hrs AIAA-2015-3072 Impact of a Vortical Gust on the Aerodynamics of a Finite AspectRatio Wing Unsteady Wing Aerodynamics III Technology, Haifa, Israel; C. Rumsey, NASA Laboratory, Wright-Patterson AFB, OH Langley Research Center, Hampton, VA; H. Mueller-Vahl, Technion--Israel Institute of Technology, Haifa, Israel; C. Stangfeld, Technical University of Berlin, Berlin, Germany Chaired by: E. WHITE, Texas A&M University and A. CHOU, NASA Langley Research Center 1400 hrs 1430 hrs 1500 hrs AIAA-2015-3075 AIAA-2015-3076 AIAA-2015-3077 On the Effect of Small Steps on Pre- Time-Frequency Analysis of Numerical Simulation of Hypersonic transitional Streamwise Elongated Boundary Layer Instabilities Boundary-Layer Instability in a Streaks Generated by Freestream Laser Real Gas with Two-Dimensional A. Sescu, Mississippi State University, Perturbations Surface Roughness Wednesday, 24 June 2015 209-FD-24 University, Las Cruces, NM; H. Fasel, University of Arizona, Tucson, AZ Chaired by: S. YARUSEVYCH, University of Waterloo and H. LUO, Vanderbilt University 1400 hrs 1430 hrs 1500 hrs AIAA-2015-3069 AIAA-2015-3070 AIAA-2015-3071 The effect of the blade chord length Unsteady Thick Airfoil Aerodynamics: Numerical Simulation of Circular on the aerodynamics of the MAV Experiments, Computation, and Cylinders and Wing Sections in scale cycloidal propeller under Theory Unsteady Motion A. Gross, J. Zhou, New Mexico State D. Greenblatt, Technion--Israel Institute of hovering status Wednesday, 24 June 2015 208-FD-23 96 J. Poggie, Air Force Research Laboratory, Wright-Patterson AFB, OH University in St. Louis, St. Louis, MO Institute of Technology, Atlanta, GA; S. Coggon, Airbus, Filton, United Kingdom 1530 hrs AIAA-2015-3088 A Full-Space Method with Matrix Aggregates for Stress-Constrained Structural Optimization Emerging Methods II C. Chang, NASA Langley Research Center, Hampton, VA; B. Venkatachari, National Institute of Aerospace, Hampton, VA; G. Cheng, University of Alabama, Tuscaloosa, Tuscaloosa, AL 1530 hrs AIAA-2015-3084 Tetrahedral-Mesh Simulation of Turbulent Flows with the SpaceTime Conservative Schemes Turbulence Simulations S. Ghosh, D. Rancourt, D. Mavris, Georgia Institute of Technology, Atlanta, GA; S. Coggon, Airbus, Filton, United Kingdom José dos Campos, Brazil; D. Ferrari, Technological Institute of Aeronautics (ITA), São José dos Campos, Brazil Z. Gao, C. Wang, Northwestern Polytechnical University, Xi’an, China 1530 hrs AIAA-2015-3094 HDMR-based Surrogate Model for High Dimensional Aerodynamic Design Problems Metamodeling I G. Kennedy, Georgia Institute of H. Kannan, E. Tibor, Iowa State University, Economon, J. Alonso, Stanford University, Technology, Atlanta, GA Stanford, CA; T. Orra, Embraer, São José Ames, IA; B. Mesmer, University of dos Campos, Brazil; et al. Alabama, Huntsville, Huntsville, AL; C. Bloebaum, Iowa State University, Ames, IA Chaired by: S. CHOWDHURY, Mississippi State University and P. PIPERNI, Bombardier Inc 1430 hrs 1500 hrs 1400 hrs AIAA-2015-3092 AIAA-2015-3093 AIAA-2015-3091 Principal Component Analysis Assisted Auxiliary Air Inlet Design: NonA Methodology to Create Approximate Models of Load Surrogate Modeling (PCA-SM) of Linearity, Surrogate Envelopes Under Uncertainty Correlated Loads for Uncertainty Modeling and Optimization Aspects D. Rancourt, S. Ghosh, D. Mavris, Georgia Analysis of Design Load Envelopes A. Lombardi, L. Santos, Embraer, São Wednesday, 24 June 2015 213-MAO-7 T. Richardson, E. Winer, Iowa State University, Ames, IA Chaired by: B. MESMER, University of Alabama and J. HICKEN, Rensselaer Polytechnic Institute 1400 hrs 1430 hrs 1500 hrs AIAA-2015-3085 AIAA-2015-3086 AIAA-2015-3087 Increasing Feasibility of the Self- Incorporation of Coupling Strength SUAVE: An Open-Source Organizing Map as a Design Tool Models in a Value-based Systems Environment for Multi-Fidelity through a Novel Convergence Engineering framework for Conceptual Vehicle Design T. Lukaczyk, A. Wendorff, M. Colonno, T. Heuristic optimization Wednesday, 24 June 2015 212-MAO-6 E. Johnsen, University of Michigan, Ann Arbor, Ann Arbor, MI; P. Movahed, University of Illinois, Urbana-Champaign, Urbana, IL; D. Dowling, University of Michigan, Ann Arbor, Ann Arbor, MI Chaired by: P. SPALART, Boeing Commercial Airplanes and E. JOHNSEN, University of Michigan 1400 hrs 1430 hrs 1500 hrs AIAA-2015-3081 AIAA-2015-3082 AIAA-2015-3083 Surface Roughness Effects in Application of the Wray-Agarwal A numerical study of turbulence Model to Compressible Flows in boxes with no-slip walls and of Hypersonic Turbulent Boundary T. Wray, R. Agarwal, Washington varying volume-to-surface ratios Layers Wednesday, 24 June 2015 211-FD-26 D. Wu, T. Long, Y. Wang, L. Liu, Beijing Institute of Technology, Beijing, China 1600 hrs AIAA-2015-3095 A Sequential Maximin Latin Hypercube Sampling Method And Its Application to Aircraft Design J. Lin, Control Research Corporation, Lexington, MA 1600 hrs AIAA-2015-3089 Reducing Induced Drag and Maneuver Loads by Active Aeroelastic Alteration F. Daoud, S. Deinert, R. Maierl, Ö. Petersson, Airbus, Manching, Germany 1630 hrs AIAA-2015-3090 Integrated Multidisciplinary Aircraft Design Process Supported by a Decentral MDO Framework Manchester Madrid Senators Lecture Hall 97 X. Zhang, X. Jinwu, M. Li, Beihang University, Beijing, China; Y. Ren, Hunan University, Changsha, China of China (AVIC), Xi’an, China; Z. Zhai, X. Jianchun, Aviation Industry Corporation Northwestern Polytechnical University, Xi’an, of China (AVIC), Xi’an, China China; L. Zhang, Aviation Industry Corporation of China (AVIC), Xi’an, China B. Parent, Pusan National University, Busan, South Korea; S. Macheret, Purdue University, West Lafayette, IN; M. Shneider, Princeton University, Princeton, NJ A. Bellemans, T. Magin, von Kármán Institute for Fluid Dynamics, Rhode-SaintGenèse, Belgium; G. Degrez, A. Parente, University of Brussels, Brussels, Belgium Plasma Computational Methods II J. Balboni, NASA Ames Research Center, Moffett Field, CA; A. Alunni, ERC, Inc., Moffett Field, CA A. Viladegut, von Kármán Institute for Fluid Dynamics, Rhode-Saint-Genèse, Belgium Arlington, Arlington, TX 1600 hrs AIAA-2015-3107 Enthalpy Characterization and Assessment of Copper Catalysis Determination in Inductively E. Cisneros, L. Massa, University of Texas, Coupled Plasma Facility Chaired by: K. STEPHANI, University of Illinois at Urbana-Champaign and T. MOELLER, University of Tennessee Space Institute 1430 hrs 1500 hrs 1530 hrs 1400 hrs AIAA-2015-3104 AIAA-2015-3105 AIAA-2015-3106 AIAA-2015-3103 Computational Simulations of TP3 Simulation of Plasma Flow Control: MG-local-PCA Method for the Reduced-Order Models of LowArc-Jet Facility Flow A New Computationally Efficient Reduction of a Collisional-Radiative Temperature Gas Discharges in T. Gokcen, ERC, Inc., Moffett Field, CA; Approach Argon Plasma Mechanism Glow Mode Wednesday, 24 June 2015 216-TP-10/PDL-10 J. Zambrano, O. Yeste-Ojeda, R. Landry, University of Québec, Montréal, Canada Sensor and Communications Systems 1530 hrs AIAA-2015-3099 A Vehicle Management End-to-End Testing and Analysis Platform for Validation of Mission and Fault Management Algorithms to Reduce Risk for NASA’s Space Launch System P. Mehta, University of Strathclyde, Glasgow, United Kingdom; A. Walker, Los Alamos National Laboratory, Los Alamos, NM; M. 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 1500 hrs AIAA-2015-3098 Sensitivity Analysis towards Probabilistic Re-Entry Modeling of Spacecraft and Space Debris Airframe Damage and Health Monitoring 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 Y. Cheng, W. Niu, Aviation Industry Corporation Embedded Parallel Computing Airborne Network Wednesday, 24 June 2015 215-MST-10 V. Mukhopadhyay, M. Sorokach, NASA Langley Research Center, Hampton, VA Chaired by: V. MUKHOPADHYAY, NASA Langley Research Center 1400 hrs 1430 hrs AIAA-2015-3096 AIAA-2015-3097 Numerical Simulation and Analysis Composite Structure Modeling and Analysis of Advanced Aircraft of the Aircraft Pilot Seat Impact Resistance Fuselage Concepts Wednesday, 24 June 2015 214-MST-9 S. Surzhikov, D. Storozhev, Russian Academy of Sciences, Moscow, Russia 1630 hrs AIAA-2015-3108 Numerical Simulation of TwoDimensional Structure of Glow Discharge in Molecular Hydrogen Miro Wyeth Travertine 98 Center, Hampton, VA; A. Brandis, ERC, Inc., Moffett Field, CA Wednesday, 24 June 2015 221-LEC-4 1730 - 1830 hrs Wednesday, 24 June 2015 220-LEC-3 1630 - 1730 hrs Jeff Jepson Senior Multi-Disciplined Engineer I Raytheon Missile Systems Susan Gorton Rotary Wing Project NASA Langley Research Center David McBride Center Director NASA Armstrong Flight Research Center Ed Feltrop Engineer Specialist Cessna Aircraft Company Fan Broadband Noise Generation and Suppression Edmane Envia Aeroacoustics Branch NASA Glenn Research Center Aeroacoustics Lecture Still Trying to Understand Aircraft Vortices Russell M. Cummings Professor of Aeronautics Department of Aeronautics U.S. Air Force Academy Aerodynamics Award Lecture Sandy Magnus Executive Director AIAA Dave Bowles Center Director (Acting) NASA Langley Research Center Samantha A. Magill Academic Affairs and Inclusion & Diversity Honda Aircraft Company Get your questions answered! Senior Mentors will include: Russ Althof Cees Bil Chief Engineer Professor, Royal Melbourne Institute of Technology Raytheon Missile Systems Rising Leaders in Aerospace: Leadership Exchange/Speed Networking Wednesday, 24 June 2015 219-RLA-2 1530 - 1700 hrs J. Scoggins, L. Soucasse, von Kármán Institute 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-SaintGenèse, Belgium Networking Coffee Break Johnston, NASA Langley Research Center, Hampton, VA 1530 hrs AIAA-2015-3112 Coupled Flow, Radiation, and Ablation Simulations of Atmospheric Entry A. Brandis, B. Cruden, T. White, D. Vehicles using the Hybrid Statistical Saunders, ERC, Inc., Moffett Field, CA; C. Narrow Band Model 1500 hrs AIAA-2015-3111 Radiative Heating on the AfterBody of Martian Entry Vehicles Aerothermodynamics III Wednesday, 24 June 2015 218-NW-7 1530 - 1600 hrs M. Mason, S. Berry, NASA Langley Research Center, Hampton, VA Chaired by: T. LAM, The Aerospace Corporation 1400 hrs 1430 hrs AIAA-2015-3109 AIAA-2015-3110 Global Aeroheating Measurements Aerothermodynamic Characteristics of Shock-Shock Interactions on a of 16-22 km/s Earth Entry C. Johnston, NASA Langley Research Swept Cylinder Wednesday, 24 June 2015 217-TP-11 Charles Smith Center Director (Acting) NASA Ames Research Center Janice Kavandi Deputy Director NASA Glenn Research Center Metropolitan Ballroom Chantilly Ballroom East Chantilly Ballroom West Chantilly Ballroom West John Valasek Professor/Director, Vehicle Systems & Control Laboratory Texas A&M University Peter Hartwich Engineering Manager Boeing Defense, Space and Security Rosetta 99 Aeroacoustics Awards Reception and Banquet Aerodynamics and Heat Transfer in Gas Turbine Cooling-Recent Advances Sumanta Acharya Ring Chair & Professor Mechanical Engineering Department University of Memphis Thermophysics Award Lecture C. Fuller, Virginia Polytechnic Institute and State University, Blacksburg, VA Chaired by: N. AGARWAL, Boeing Defense, Space & Security 0900 hrs Oral Presentation Poroelastic Acoustic Meta Materials (Invited) Thursday, 25 June 2015 226-AA-31 Plenary Keynote Thursday, 25 June 2015 225-PLNRY-4 0800 - 0900 hrs A. Slagle, C. Fuller, Virginia Polytechnic Institute and State University, Blacksburg, VA 1000 hrs AIAA-2015-3113 Low Frequency Noise Reduction Using Poro-Elastic Acoustic Metamaterials 1100 hrs AIAA-2015-3115 Fuselage Excitation During Cruise Flight Conditions: Measurement and Prediction of Pressure Point Spectra A. Klabes, M. Herr, C. Appel, German R. Abdrashitov, Sukhoi Civil Aircraft Company, Aerospace Center (DLR), Braunschweig, Germany; M. Bouhaj, Airbus Operations Moscow, Russia; A. Golubev, TsAGI, GmbH, Hamburg, Germany Zhukovsky, Russia 1030 hrs AIAA-2015-3114 Identification of sources of noise in the cabin and the definition of the local passage of sound energy through fuselage based on the results of in-flight measurements of the Superjet Interior Noise DHS’s Perspectives on Cybersecurity in Aviation Gregory J. Touhill Deputy Assistant Secretary for Office of Cybersecurity and Communications Department of Homeland Security Speakers’ Briefing Thursday, 25 June 2015 224-SB-4 0730 - 0800 hrs Thursday M. Alaoui, X. Gloerfelt, Paris Institute of Technology, Paris, France; O. Collery, M. Etchessahar, Airbus, Toulouse, France 1130 hrs AIAA-2015-3116 Effect of pressure gradients on turbulent boundary layer vortical structures and wall-pressure fluctuations E. Cohen, X. Gloerfelt, Paris Institute of Technology, Paris, France Edelweiss Chantilly Ballroom West Session Rooms Imperial Ballroom Grand Ballroom E 1200 hrs AIAA-2015-3117 Effect of pressure gradients on turbulent boundary layer noise and wall-pressure fluctuations 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. Wednesday, 24 June 2015 223-BANQ-1 1900 - 2030 hrs Wednesday, 24 June 2015 222-LEC-5 1730 - 1830 hrs 100 J. Bridges, M. Wernet, NASA Glenn Research Center, Cleveland, OH A. Sinha, Indian Institute of Technology Bombay, Mumbai, India; T. Colonius, California Institute of Technology, Pasadena, CA VA; A. Fernando, Norfolk State University, M. Terracol, E. Manoha, ONERA, Châtillon, Norfolk, VA France; M. Murayama, K. Yamamoto, Japan Aerospace Exploration Agency (JAXA), Tokyo, Japan Chaired by: S. ARUNAJATESAN, Sandia National Labs 0930 hrs 0900 hrs AIAA-2015-3132 AIAA-2015-3131 A study of accuracy on numerical Aeroacoustic Calculations of the methods for nonuniform meshes 30P30N High-lift Airfoil using Hybrid (Invited) RANS/LES methods: Modeling and F. Hu, Old Dominion University, Norfolk, Grid Resolution Effects Thursday, 25 June 2015 229-AA-34 M. Itasse, J. Brazier, O. Léon, G. Casalis, ONERA, Toulouse, France Chaired by: C. BROWN, NASA Glenn Research Center 0900 hrs 0930 hrs AIAA-2015-3124 AIAA-2015-3125 Nonlinear interaction analysis of Linear Stability Implications of subsonic jet instabilities with forced Mean Flow Variations in Turbulent eigenmodes using PSE Jets Issuing from Serrated Nozzles Thursday, 25 June 2015 228-AA-33 J. Lawrence, R. Self, University of Southampton, Southampton, United Kingdom Chaired by: D. PAPAMOSCHOU, University of California Irvine 0900 hrs 0930 hrs AIAA-2015-3118 AIAA-2015-3119 Noise measurements of high aspect Installed jet-flap impingement ratio distributed exhaust systems tonal noise Thursday, 25 June 2015 227-AA-32 M. Schlottke, H. Cheng, V. Pauz, M. Meinke, W. Schroeder, RWTH Aachen University, Aachen, Germany 1000 hrs AIAA-2015-3133 A direct-hybrid method for computational aeroacoustics 1100 hrs AIAA-2015-3122 An Experimental Study of Coaxial Jets Using Acoustic PIV and LDA Methods (CoJeN) S. Le Bras, CERFACS, Toulouse, France; H. Deniau, ONERA, Toulouse, France; C. Bogey, École Centrale de Lyon, Ecully, France; G. Daviller, CERFACS, Toulouse, France C. Brown, NASA Glenn Research Center, Cleveland, OH 1100 hrs AIAA-2015-3128 Empirical Models for the Shielding and Reflection of Jet Mixing Noise by a Surface Toledo, OH 1100 hrs AIAA-2015-3135 Development of compressible largeeddy simulations combining highS. Yazdani, D. Hixon, University of Toledo, order schemes and wall modeling 1030 hrs AIAA-2015-3134 Hybrid MacCormack-type Schemes for Computational Aeroacoustics CAA Numerical Techniques III 1030 hrs AIAA-2015-3127 Theoretical Modelling Of Broadband Shock Associated Noise in Asymmetric Jets Jet Noise Modeling II Inverness V. Kopiev, S. Chernyshev, TsAGI, Moscow, Russia V. Semiletov, Queen Mary University of London, London, United Kingdom; P. Yakovlev, North-Eastern Federal University, Yakutsk, Russia; S. Karabasov, Queen Mary University of London, London, United Kingdom; G. Faranosov, V. Kopiev, TsAGI, Moscow, Russia 1130 hrs AIAA-2015-3129 Computational modelling of jet-wing interaction: the effect of asymmetries from the jet inflow conditions and the wing Fleur-de-lis B Fleur-de-lis A 1200 hrs AIAA-2015-3130 Refraction Effect in Correlation Model of Quadrupole Noise Sources in Turbulent Jet 1130 hrs AIAA-2015-3123 Experimental and numerical study of the noise generation in an outflow butterfly valve K. Natarajan, L. Venkatakrishnan, National C. Mead, Aero Acoustics, Ltd., Elstead, United A. Chauvin, Y. Pasco, M. Sanjose, G. 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 1030 hrs AIAA-2015-3121 Flow Field and Acoustic Investigations of the Launch Vehicle Environment during Lift-off A. Kalyan, S. Karabasov, Queen Mary University of London, London, United R. Farr, NASA Marshall Space Flight Kingdom Center, Huntsville, AL; C. Chang, NASA Langley Research Center, Hampton, VA; J. Jones, AI Signal Research, Inc., Huntsville, AL; N. Dougherty, ERC, Inc., Huntsville, AL 1000 hrs AIAA-2015-3126 On the Comparison of the Long Penetration Mode (LPM) Supersonic Counterflowing Jet to the Supersonic Screech Jet B. Henderson, S. Leib, NASA Glenn Research Center, Cleveland, OH 1000 hrs AIAA-2015-3120 Measurements and Predictions of the Noise from Three-Stream Jets Jet Noise Measurements III 101 0930 hrs AIAA-2015-3137 LEISA2: an experimental database for the validation of numerical predictions of slat unsteady flow and noise M. Catlett, J. Anderson, Naval Surface Warfare Center, West Bethesda, MD Jason Welstead NASA Langley S. Alter, G. Brauckmann, W. Kleb, C. Streett, School of Engineering, Brooklyn, NY C. Glass, D. Schuster, NASA Langley Research Center, Hampton, VA T. Geyer, E. Sarradj, G. Herold, Brandenburg University of Technology, Cottbus, Germany 1100 hrs AIAA-2015-3147 Flow Noise Generation of Cylinders with Soft Porous Cover Mark Page DZYNE Technologies Research Laboratory, Washington, DC D. Dalle, Science and Technology Corporation, P. Vrchota, A. Prachar, Aerospace Research and Moffett Field, CA; S. Rogers, NASA Ames Test Establishment, Prague, Czech Republic Research Center, Moffett Field, CA 1100 hrs AIAA-2015-3153 Improvement of CFD results of NASA CRM by on-line mesh deformation using modal analysis of a wing Applied CFD & Numerical Correlations with Experimental Data III Joaquim Martins University of Michigan The Need of Community-Accepted Public Domain / Open Source Sizing Codes Conceptual Aircraft Design Working Group (CADWG21) Panel 1030 hrs AIAA-2015-3146 On the Relevance of Convection Effects for a Laser-Generated Sound Source General Acoustics III Chaired by: K. ABDOL-HAMID, NASA Langley Research Center and A. SCLAFANI, Boeing Engineering Operations & Technology 0930 hrs 1000 hrs 1030 hrs 0900 hrs AIAA-2015-3150 AIAA-2015-3151 AIAA-2015-3152 AIAA-2015-3149 Time-Accurate Unsteady Pressure Continuous Radial Jet in Annular Simulation of a Flapping Wing UAV Output-Based Adaptive Meshing Loads Simulated for the Space Launch Cross-flow using a Coupled CFD-Control Tool Applied to Space Launch System P. Rajput, I. Kalkhoran, NYU Polytechnic J. Geder, R. Ramamurti, K. Viswanath, Naval Booster Separation Analysis System at Wind Tunnel Conditions Thursday, 25 June 2015 233-APA-25 Clif Davis Lockheed Martin Aeronautics Panelists: 1100 hrs AIAA-2015-3140 Large-Scale Studies on Slat Noise Reduction M. Herr, M. Pott-Pollenske, R. Ewert, B. Dirk, J. Siebert, J. Delfs, German N. Ashton, University of Manchester, Aerospace Center (DLR), Braunschweig, Manchester, United Kingdom; A. West, Germany; et al. CD-adapco, London, United Kingdom; F. Mendonca, Self, London, United Kingdom 1030 hrs AIAA-2015-3139 Slat Noise Prediction using Hybrid RANS-LES methods on Structured and Unstructured Grids Airframe Noise IV J. Callicoat, R. Gaeta, J. Jacob, Oklahoma K. Rossignol, J. Delfs, L. Rossian, F. State University, Stillwater, OK Boden, German Aerospace Center (DLR), Braunschweig, Germany 1000 hrs AIAA-2015-3145 An Experimental Study of Composite Materials for the Design of Quiet UAVs F. Amaral, D. Souza, C. Pagani, M. Medeiros, University of São Paulo, São José dos Campos, Brazil 1000 hrs AIAA-2015-3138 Experimental study of the effect of a small 2D excrescence placed on the slat cove surface of an airfoil on its acoustic noise Chaired by: W. ANEMAAT, DARcorporation and T. TAKAHASHI, Arizona State University Thursday, 25 June 2015 232-ACD-6 0900 - 1200 hrs 0930 hrs AIAA-2015-3144 Experimental Investigation of the Unsteady Pressure on a Hydrofoil A. Mimani, D. Moreau, C. Doolan, due to the Ingestion of Turbulence University of Adelaide, Adelaide, Australia and Hydro-elastic Motion Chaired by: C. SCHRAM 0900 hrs AIAA-2015-3143 Experimental Application of Aeroacoustic Time-Reversal Thursday, 25 June 2015 231-AA-36 D. Lockard, M. Choudhari, P. Buning, NASA E. Manoha, ONERA, Châtillon, France; M. Langley Research Center, Hampton, VA Pott-Pollenske, German Aerospace Center (DLR), Braunschweig, Germany Chaired by: T. VAN DE VEN, Gulfstream 0900 hrs AIAA-2015-3136 Influence of Spanwise Boundary Conditions on Slat Noise Simulations Thursday, 25 June 2015 230-AA-35 Steve Komadina Northrop-Grumman E. Salze, C. Bailly, O. Marsden, E. Jondeau, D. Juve, École Centrale de Lyon, Ecully, France Rob McDonald CalPoly Stemmons B Wyeth Obelisk A M. Pott-Pollenske, J. Wild, German Aerospace Center (DLR), Braunschweig, Germany 1200 hrs AIAA-2015-3142 On the Noise Generation of Krueger Leading Edge Devices 1130 hrs AIAA-2015-3148 An experimental investigation of wall pressure fluctuations beneath pressure gradients M. Murayama, Y. Yokokawa, Y. Ito, K. Yamamoto, T. Takaishi, H. Ura, Japan Aerospace Exploration Agency (JAXA), Mitaka, Japan 1130 hrs AIAA-2015-3141 Study on Noise Generation from Slat Tracks Using a High-Lift Wing Model Lalique 102 B. Nieto, X. Alfonso, K. Basto, J. Escobar, University of San Buenaventura, Bogota, Colombia University, Bangkok, Thailand M. Zakaria, Virginia Polytechnic Institute and State University, Blacksburg, VA; D. Pereira, University of São Paulo, São Paulo, Brazil; S. Ragab, M. Hajj, Virginia Polytechnic Institute and State University, Blacksburg, VA; F. Marques, University of São Paulo, São Paulo, Brazil M. Zakaria, Virginia Polytechnic Institute and State University, Blacksburg, VA; H. Taha, University of California, Irvine, Irvine, CA; M. Hajj, A. Hussein, Virginia Polytechnic Institute and State University, Blacksburg, VA South Korea; K. Cho, Korea University P. Gilge, K. Mulleners, Leibniz University, of Science and Technology, Daejeon, Hannover, Germany South Korea; K. Jung, Agency for Defense Development, Daejeon, South Korea Unsteady Aerodynamics I M. Kerho, Rolling Hills Research Corporation, El Segundo, CA 1030 hrs AIAA-2015-3162 Aero-Propulsive Coupling of an Embedded, Distributed Propulsion System University, Washington, DC; M. Snyder, U.S. Naval Academy, Annapolis, MD La Plata, La Plata, Argentina 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 AIAA-2015-3165 AIAA-2015-3166 AIAA-2015-3167 AIAA-2015-3168 Measurements of Dynamic An Experimental Study of Added Experimental-Based Unified Experimental Dynamic Stall study Interface Between Ship and Mass on a Plunging Airfoil Unsteady Nonlinear Aerodynamic on a low Reynolds number airfoil S. Algozino, J. Marañon Di Leo, J. Helicopter Air Wakes Oscillating with High Frequencies at Modeling For Two-Dimensional Delnero, G. Capittini, National University of C. Friedman, George Washington High Angles of Attack Airfoils Thursday, 25 June 2015 236-APA-28 North Carolina State University, Raleigh, NC Kanpur, Kanpur, India D. Kumar, S. Kumar, T. Goyal, P. Mohite, S. Kamle, Indian Institute of Technology Kanpur, Kanpur, India M. Ghoreyshi, U.S. Air Force Academy, Colorado Springs, CO; K. Bergeron, Army Research, Development and Engineering Command, Natick, MA; J. Seidel, A. Lofthouse, R. Cummings, U.S. Air Force Academy, Colorado Springs, CO 1100 hrs AIAA-2015-3169 Unsteady Aerodynamic Modeling of Rolling Parachutes Using the Indicial Method Stemmons A Stemmons C 1200 hrs AIAA-2015-3171 Implementation of Vortex-type Gust Model Through Boundary Conditions Carpenter Ballroom E. Eljack, I. AlQadi, King Abdulaziz University, Jeedah, Saudi Arabia M. Righi, Zurich University of Applied Sciences, Winterthur, Switzerland; M. Berci, University of Leeds, Leeds, United Kingdom; J. Koch, Zurich University of Applied Sciences, Winterthur, Switzerland 1130 hrs AIAA-2015-3170 Subsonic Indicial Aerodynamics for Unsteady Loads Calculation via Numerical and Analytical Methods: a Preliminary Assessment Institute of Technology (KTH), Stockholm, H. Sharma, S. Harshe, S. Vekaria, M. Sweden Singh, M. Damodaran, Indian Institute of Technology Gandhinagar, Ahmedabad, India; B. Khoo, National University of Singapore, Singapore, Singapore 1130 hrs AIAA-2015-3164 Computational Assessment of Rainfall Effects on Aircraft F. Majić, G. Efraimsson, C. O’Reilly, Royal Aerodynamic Characteristics 1100 hrs AIAA-2015-3163 Aerodynamic Performance of the Adaptive Nacelle Inlet Airfoil/Wing/Configuration Aerodynamics Chaired by: A. MCCOMAS, TLG Aerospace and J. GUGLIELMO, Boeing Defense, Space & Security 0900 hrs 0930 hrs 1000 hrs AIAA-2015-3159 AIAA-2015-3160 AIAA-2015-3161 Improved Stall Prediction for Modeling and Prediction of On the resulting aerodynamic Swept Wings Using Low-Order the Crossflow Transition Using loss of combinations of localized Aerodynamics Transition Transport Equations surface roughness patches on a P. Hosangadi, R. Paul, A. Gopalarathnam, J. Sa, S. Park, Konkuk University, Seoul, turbine blade Thursday, 25 June 2015 235-APA-27 C. Planck, F. Siala, J. Liburdy, Oregon State University, Corvallis, OR 1100 hrs AIAA-2015-3158 Development and Aero-structural Analysis of Light and Strong D. Kumar, T. Goyal, S. Vemuri, P. Mohite, Carbon Fiber-CNT/PP Hummingbird S. Kamle, Indian Institute of Technology Inspired MAV Wings 1030 hrs AIAA-2015-3157 Development and Analysis of Gull Inspired UAV Flapping Wing Unmanned, Bio-Inspired, Solar Powered Aerial Vehicle Designs II Chaired by: M. OL, US Air Force Reseach Laboratory and A. MITTAL, The University of Tennessee at Chattanooga 0900 hrs 0930 hrs 1000 hrs AIAA-2015-3154 AIAA-2015-3155 AIAA-2015-3156 Numerical Simulation of a Flapping Aerodynamics of Southern Hawker Dynamical Characterization of a Wing in Ansys-Fluent Based on the Dragonfly: Aeshna cyanea Bio-Inspired Wing with Passively S. Srigrarom, C. Thipyopas, Kasetsart Fruit Fly Wing Kinematics Actuated Edges Thursday, 25 June 2015 234-APA-26 103 Oberpfaffenhofen, Germany; N. Ahmad, NASA Langley Research Center, Hampton, VA; F. Holzäpfel, German Aerospace Center (DLR), Oberpfaffenhofen, Germany; R. VanValkenburg, NASA Langley Research Center, Hampton, VA M. Gautier, R. Botez, University of Québec, Montréal, Canada T. Foster, Empirical Systems Aerospace, Inc., Pismo Beach, CA Chaired by: S. GINN, NASA 0900 hrs Oral Presentation HEIST LEAPTech Instrumentation Design, Development, and Initial Results Thursday, 25 June 2015 240-ATIO-23 D. Zeng, J. Gonda, MITRE Corporation, McLean, VA S. Sharma, J. Robinson III, NASA Ames Research Center, Moffett Field, CA S. Clarke, Y. Lin, A. Samuel, K. Papathakis, NASA Armstrong Flight Research Center, Edwards, CA 0930 hrs Oral Presentation LEAPTech HEIST Power Architecture and Testing Chaired by: D. DELAURENTIS, Purdue University 0930 hrs 0900 hrs AIAA-2015-3182 AIAA-2015-3181 Verifying Required Communication Methodology to Define Delivery Performance in Air Traffic Accuracy Under Current Day ATC Management Operations Thursday, 25 June 2015 239-ATIO-22 B. Marr, K. Lindsay, MITRE Corporation, McLean, VA Chaired by: M. KOCH, NASA Langley Research Center 0900 hrs 0930 hrs AIAA-2015-3178 AIAA-2015-3179 Controller Workload-based Optimization of the Cruise Regime Calculation of Monitor Alert of Flight Airplane Trajectory using Parameters for En Route Sectors Deterministic Algorithms Thursday, 25 June 2015 238-ATIO-21 J. Hallock, Department of Transportation, Cambridge, MA; G. Greene, J. Tittsworth, P. Strande, Federal Aviation Administration, Washington, DC; F. Wang, Department of Transportation, Cambridge, MA F. Holzäpfel, N. Tchipev, A. Stephan, German Aerospace Center (DLR), Oberpfaffenhofen, Germany A. Stoll, Joby Aviation, Santa Cruz, CA 1000 hrs AIAA-2015-3188 Comparison of CFD and Experimental Results of the LEAPTech Distributed Electric Propulsion Blown Wing B. Seeley, CAFE Foundation, Santa Rosa, CA 1030 hrs AIAA-2015-3184 Regional Sky Transit ATM V - Performance Assessment M. Weiss, N. Dzikus, German Aerospace Center (DLR), Hamburg, Germany 1100 hrs AIAA-2015-3185 An Airport Assessment Approach in the Conceptual Design Stage D. Jacob, Coherent Research Group, Ormond Beach, FL; D. Lai, M. Pruis, D. Delisi, NorthWest Research Associates, Redmond, WA 1100 hrs AIAA-2015-3190 Optimal Propeller Pitch Scheduling and Propeller--Airframe Matching for Conceptual Design R. McDonald, California Polytechnic State M. Olson, Georgia Institute of Technology, University, San Luis Obispo, CA Atlanta, GA 1030 hrs AIAA-2015-3189 A Conceptual Approach to FlightTraining Mission and Cost Analysis of an All-Electric Aircraft Equipped with Regenerative Energy Devices Transformational Flight - Electric Propulsion L. Bowers, L. Mockus, S. Tamaskar, D. DeLaurentis, Purdue University, West Lafayette, IN 1000 hrs AIAA-2015-3183 Investigation of Connectivity: Definition, Application, and Formulation H. Blom, B. Bakker, National Aerospace Laboratory (NLR), Amsterdam, The Netherlands En Route Operations of Berlin, Berlin, Germany 1100 hrs AIAA-2015-3176 Assessment of WakeMod 4: A New Standalone Wake Vortex Algorithm for Estimating Circulation Strength D. Bieniek, R. Luckner, Technical University and Position (Invited) 1030 hrs AIAA-2015-3175 Sensitivity Analysis of Aircraft Encounters with Deformed Wake Vortices (Invited) Aircraft Wake Turbulence I (Invited) 1000 hrs AIAA-2015-3180 Can ground-based separation accommodate very high en route traffic demand as well as advanced self-separation? Chaired by: M. PRUIS, Northwest Research Associates Inc and N. AHMAD, NASA Langley Research Center 0900 hrs 0930 hrs 1000 hrs AIAA-2015-3172 AIAA-2015-3173 AIAA-2015-3174 Use of Simple Models to Determine Multi-Model Ensemble Wake Vortex Wind Impact on Single Vortices and Prediction (Invited) Counter-Rotating Vortex Pairs in Wake Vortex Categories for New S. Koerner, German Aerospace Center (DLR), Ground Proximity (Invited) Aircraft (Invited) Thursday, 25 June 2015 237-ASE-3 C. Green, R. McDonald, California Polytechnic State University, San Luis Obispo, CA Monet Ballroom M. Hassan, A. Payan, H. Pfaender, D. Mavris, E. Garcia, J. Schutte, Georgia Institute of Technology, Atlanta, GA Morocco Milan 1200 hrs AIAA-2015-3187 Framework Development for Performance Evaluation of the Future National Airspace System 1130 hrs AIAA-2015-3191 Modeling and Test of the Efficiency of Electronic Speed Controllers for Brushless DC Motors A. Wing, W. Felder, R. Cloutier, Stevens Institute of Technology, Hoboken, NJ 1130 hrs AIAA-2015-3186 Modeling a Ramp Area Support System M. Pruis, D. Delisi, NorthWest Research Associates, Redmond, WA; D. Jacob, Coherent Research Group, Ormond Beach, FL 1130 hrs AIAA-2015-3177 Observations of Wake Vortices from Upward Looking Pulsed Doppler Lidar Data (Invited) Plum Blossom B 104 Q. Wang, Y. Ren, Tsinghua University, Beijing, China; W. Li, Sun Yat-Sen University, Guangzhou, China J. Nordstrom, Linköping University, Linköping, Sweden Y. Tamaki, T. Imamura, University of Tokyo, Tokyo, Japan A. Kartha, P. Subbareddy, G. Candler, University of Minnesota, Minneapolis, Minneapolis, MN; P. Dimotakis, California Institute of Technology, Pasadena, CA M. Evans, P. Medwell, Z. Tian, University of Adelaide, Adelaide, Australia; A. Frassoldati, A. Cuoci, A. Stagni, Technical University of Milan, Milan, Italy 1030 hrs AIAA-2015-3210 Ignition Characteristics in Spatially Zero-, One- and Two-Dimensional Laminar Ethylene Flames J. Quinlan, T. Drozda, NASA Langley Research N. Williams, R. Thompson, T. Moeller, Center, Hampton, VA; J. McDaniel, University University of Tennessee, Tullahoma, of Virginia, Charlottesville, Charlottesville, Tullahoma, TN VA; G. Lacaze, J. Oefelein, Sandia National Laboratories, Livermore, CA High-Speed and Reacting Flows M. Fischels, R. Rajagopalan, Iowa State University, Ames, IA Chaired by: G. CANDLER, University of Minnesota and B. RATHAKRISHNAN, GE Global Research 0930 hrs 1000 hrs 0900 hrs AIAA-2015-3208 AIAA-2015-3209 AIAA-2015-3207 A Priori Analysis of a Compressible Numerical Investigations of Pulsed LES of reacting mixing layers: influence of inflow conditions and Flamelet Model using RANS Data for a Fuel Injection into Supersonic Dual-Mode Scramjet Combustor Crossflow heat release R. Djeddi, K. Ekici, University of Tennessee, Knoxville, Knoxville, TN Thursday, 25 June 2015 244-CFD-29 J. Thorne, A. Katz, Utah State University, Logan, UT Z. Xu, University of Science and Technology, Hefei, China; Q. Zhao, Chinese Academy of Sciences, Beijing, China; Q. Lin, University of Science and Technology, Hefei, China; J. Xu, Chinese Academy of Sciences, Beijing, China 1100 hrs AIAA-2015-3196 A new high-order unstructured numerical scheme for large eddy simulation Z. Wang, University of Kansas, Lawrence, Lawrence, KS 1100 hrs Oral Presentation Large Eddy Simulations of Turbulent Flows Using Discontinuous High Order Methods (Invited) H. Wang, Y. Piao, J. Niu, Tsinghua University, Beijing, China 1100 hrs AIAA-2015-3211 IDDES simulation of supersonic combustion using flamelet modeling V. Ivanov, B. Makarov, ANSYS, Inc., Lebanon, NH 1100 hrs AIAA-2015-3204 Applying Non-Reflecting Boundary Conditions in Pressure-Based Solvers Incompressible and Low Speed Flows M. Ihme, Y. Lv, Stanford University, Stanford, CA 1030 hrs AIAA-2015-3203 Comparison of Pressure-Based Runge-Kutta Schemes for Unsteady Incompressible Flows University, Ames, IA J. Hicken, Rensselaer Polytechnic Institute, Troy, NY; D. Del Rey Fernández, D. Zingg, University of Toronto, Toronto, Canada 1030 hrs Oral Presentation Role of Entropy-Residual in HighOrder Numerical Methods for GasDynamics Calculations: Shock Detector and Adaptation Indicator (Invited) Chaired by: M. YU, University of Maryland, Baltimore County and R. RAJAGOPALAN, Iowa State University 0900 hrs 0930 hrs 1000 hrs AIAA-2015-3200 AIAA-2015-3201 AIAA-2015-3202 High-Order Strand Grid Methods An Explicit Pressure-Based A Turbulent Low-Speed for Low Mach and Incompressible Algorithm for Incompressible Flows Preconditioner for Unsteady Flows D. Garrick, R. Rajagopalan, Iowa State Flows About Wind Turbine Airfoils Thursday, 25 June 2015 243-CFD-28 P. Vincent, Imperial College London, London, United Kingdom F. Moreira, C. Breviglieri, Technological Institute of Aeronautics (ITA), São José dos Campos, Brazil; J. Azevedo, Aeronautics and Space Institute (IAE), São José dos Campos, Brazil 1030 hrs AIAA-2015-3195 High-Order Compressible Flow Simulations with the Unstructured Spectral Difference Method Current Trends in CFD Research II (Invited) 1000 hrs AIAA-2015-3194 Locally-Defined High-Resolution Scheme for Shock-Capturing Problems on Unstructured Cartesian Grids Unstructured High-Order Methods III Chaired by: H. HUYNH, NASA Glenn Research Center and Z. WANG, University of Kansas 0900 hrs 0930 hrs 1000 hrs Oral Presentation AIAA-2015-3197 AIAA-2015-3198 Theoretical Aspects of High-Order Well Posed Problems and Boundary Opportunities for efficient high-order Flux Reconstruction Schemes Conditions in Computational Fluid methods based on the summation-by(Invited) Dynamics (Invited) parts property (Invited) Thursday, 25 June 2015 242-CFD-27 H. Yang, R. Harris, CFD Research Corporation, Huntsville, AL Chaired by: R. HARRIS, CFD Research Corporation and B. JOLLY, US Air Force 0900 hrs 0930 hrs AIAA-2015-3192 AIAA-2015-3193 Development of Vertex-Centered, A compact high order finite volume method for hyperbolic conservation High-Order Schemes and laws on unstructured grids Implementation in FUN3D Thursday, 25 June 2015 241-CFD-26 R. Rouzbar, S. Eyi, Middle East Technical University, Ankara, Turkey Coral C. Falcão, University of Rio Grande do Sul, Porto Alegre, Brazil; F. Medeiros, Military Institute of Engineering (IME), Rio de Janeiro, Brazil; L. Alves, Fluminese Federal University (UFF), Niterói, Brazil Plum Blossom A Grand Ballroom B 1200 hrs AIAA-2015-3206 Robustness to Inaccurate Initial Conditions in Low Mach Preconditioned Density-Based Methods 1130 hrs AIAA-2015-3212 Three Dimensional Flow Analysis of a Cavity-Based Scramjet Combustor V. Przulj, Ricardo Software, Shoreham by Sea, United Kingdom 1130 hrs AIAA-2015-3205 Generalised SIMPLE-Based Pressure Correction Method for Unstructured Co-located Grids C. Kim, Seoul National University, Seoul, South Korea; J. Park, Imperial College London, London, United Kingdom 1130 hrs AIAA-2015-3199 Multi-dimensional Limiting Strategy for Higher-order CFD Methods Progress and Issue (Invited) Grand Ballroom A 105 P. Chakraborty, A. Roy, Indian Institute of Technology Kharagpur, Kolkata, India Minneapolis, Minneapolis, MN P. Batten, U. Goldberg, O. Peroomian, S. Chakravarthy, Metacomp Technologies, Inc., Agoura Hills, CA Y. Zhang, N. Arora, Y. Sun, L. Cattafesta, K. Taira, Florida State University, Tallahassee, FL; L. Ukeiley, University of Florida, Gainesville, Gainesville, FL C. Yuan, G. Liu, Y. Ren, H. Dong, University of Virginia, Charlottesville, Charlottesville, VA Aerospace, Hampton, VA; S. Wilkinson, P. Balakumar, NASA Langley Research Center, Hampton, VA Chaired by: H. DONG, University of Virginia and E. WHALEN, Boeing Engineering Operations & Technology 0900 hrs 0930 hrs 1000 hrs AIAA-2015-3220 AIAA-2015-3221 AIAA-2015-3219 Three-dimensional Control via Mass Propulsive Performance and Vortex On the Effect of Rigid Swept Injection for Suppression of Cavity Interactions of Multiple Tandem Surface Waves on Turbulent Drag M. Denison, National Institute of Oscillations Foils Pitching In Line Thursday, 25 June 2015 248-FD-29 Chaired by: H. REED, Texas A&M University Thursday, 25 June 2015 247-FD-28 0900 - 1230 hrs Arlington, Arlington, TX H. Dell’Orso, B. Tuna, M. Amitay, Rensselaer Polytechnic Institute, Troy, NY Flow Control - Aerodynamics Transition Open Forum Turbulence Analysis 1030 hrs AIAA-2015-3222 Control of Tollmien-Schlichting Waves Using Piezoelectrically Driven Oscillating Surface 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 Threeturbulent compressible shear flows A. Neville, I. Nompelis, P. Subbareddy, Detonation-Turbulence Interaction Dimensional Wing Using Large G. Candler, University of Minnesota, S. Hussein, F. Lu, University of Texas, Eddy Simulation Data Thursday, 25 June 2015 246-FD-27 N. Dhamankar, G. Blaisdell, Purdue D. Gaitonde, M. Waindim, M. Adler, Ohio University, West Lafayette, IN; A. Lyrintzis, State University, Columbus, OH Embry-Riddle Aeronautical University, Daytona Beach, FL 1030 hrs Q&A Panel Discussion Inflow Turbulence for Wall-Bounded LES (Invited) Chaired by: N. BISEK, Air Force Reseach Laboratory and L. TAO, GE Global Research 0900 hrs 0930 hrs 1000 hrs AIAA-2015-3213 AIAA-2015-3214 AIAA-2015-3215 A Counter-Flow Force Based Method Generating Synthetic An Overview of Turbulent Inflow to Generate Equilibrium Turbulent Inhomogeneous Turbulence from Boundary Conditions for Large Inflow Conditions (Invited) RANS Statistics (Invited) Eddy Simulations (Invited) Thursday, 25 June 2015 245-CFD-30 Senators Lecture Hall Sapphire Govenors Lecture Hall Emerald 106 J. Spravka, T. Jorris, 412th Test Wing, Edwards AFB, CA R. Bunge, F. Munera Savino, I. Kroo, Stanford University, Stanford, CA Y. Korolev, V. Toropov, Queen Mary University of London, London, United Kingdom; S. Shahpar, Rolls-Royce Group plc, Derby, United Kingdom A. Suñol, T. Yang, D. Vucinic, Vrije Universiteit Brussel, Brussels, Belgium 0930 hrs AIAA-2015-3229 Numerical Feasibility Analysis of the Extra-light Weight Structure Tensairity on Large Airships M. Kulkarni, R. Canfield, M. Patil, Virginia E. Olson, NASA Langley Research Center, Polytechnic Institute and State University, Hampton, VA Blacksburg, VA 1030 hrs AIAA-2015-3236 Study of Hybrid Radial Basis Function for Design Optimization Problems Metamodeling II 1030 hrs AIAA-2015-3231 Disturbance Rejection Based Path Following Control for A Stratospheric Airship with Actuator Saturation T. Köthe, S. Herzog, C. Wagner, German Aerospace Center (DLR), Göttingen, Germany H. Su, L. Gu, C. Gong, Northwestern Polytechnical University, Xi’an, China 1100 hrs AIAA-2015-3232 A Long Endurance, Highly Maneuverable, Collaborative, Unmanned Airborne System University of Kaiserslautern, Kaiserslautern, Germany 1100 hrs AIAA-2015-3241 The Research on Geometry Modeling Method Based on Threedimensional CST Parameterization T. Albring, M. Sagebaum, N. Gauger, Technical Technology 1030 hrs AIAA-2015-3240 Development of a Consistent Discrete Adjoint Solver in an Evolving Aerodynamic Design Framework Shape and Topology I R. Shi, L. Liu, T. Long, J. Liu, Beijing Institute of Technology, Beijing, China Y. Jo, J. Park, C. Ocheltree, J. Choi, S. Choi, P. Raj, Virginia Polytechnic Institute and State University, Blacksburg, VA; et al. Chaired by: J. MARTINS, University of Michigan and R. KOLONAY, Air Force Research Laboratory/RQVC/WPAFB 0930 hrs 1000 hrs 0900 hrs AIAA-2015-3238 AIAA-2015-3239 AIAA-2015-3237 Multi-objective shape optimization Nonintrusive Continuum Sensitivity Three-Dimensional PiecewiseContinuous Class-Shape of aircraft cabin ventilation Analysis for Aerodynamic Shape Transformation of Wings components using adjoint CFD Optimization Thursday, 25 June 2015 252-MAO-9 Syracuse, NY; S. Chowdhury, A. Messac, Mississippi State University, Mississippi State, MS J. Zanette, Brazilian Air Force, São José dos Campos, Brazil; F. Almeida, Technological Institute of Aeronautics (ITA), São José dos Campos, Brazil 1100 hrs AIAA-2015-3227 Lateral-Directional Aerodynamic Model Identification of a SingleEngine Propeller Aircraft Using Partial Orthogonal Least Squares A. Kanoria, K. Panchal, R. Dongre, M. W. King, D. Landrum, J. Alcorn, A. Damodaran, Indian Institute of Technology K. Yan, Z. Zheng, M. Zhu, Z. Wu, Beihang Jarzembski, University of Alabama, Gandhinagar, Ahmedabad, India Huntsville, Huntsville, AL University, Beijing, China 1000 hrs AIAA-2015-3230 Computational Modelling of Aerodynamic Characteristics of Airships in Arbitrary Motion P. Bolds-Moorehead, V. Chaney, The Boeing Company, Seattle, WA; T. Lutz, S. Vaux, Airbus, Toulouse, France 1030 hrs AIAA-2015-3226 Ground Minimum Control Speed (VMCG) Testing of Transport Aircraft Flight Testing Lighter-than-Air Systems & Technologies I Chaired by: B. ROTH, Walla Walla Univ and J. HICKEN, Rensselaer Polytechnic Institute 0900 hrs 0930 hrs 1000 hrs AIAA-2015-3233 AIAA-2015-3234 AIAA-2015-3235 Adaptive Switching of VariableLarge-scale CFD Optimization Adaptive Variable-Fidelity Fidelity Models in Population-based based on the FFD Parametrization Aerodynamic Analysis and Design Optimization Algorithms using the Multipoint Approximation for Tailless Aircraft under ModelA. Mehmani, Syracuse University, Method in an HPC Environment Form Uncertainty Thursday, 25 June 2015 251-MAO-8 L. Chen, Y. Wen, H. Zhou, X. Wang, P. Zhou, D. Duan, Shanghai Jiao Tong University, Shanghai, China Chaired by: R. VAN TREUREN 0900 hrs AIAA-2015-3228 Design and Control of a Multivectored Thrust Airship Thursday, 25 June 2015 250-LTA-1 J. Newcamp, U.S. Air Force Academy, Colorado Springs, CO Chaired by: K. GARMAN, Federal Aviation Administration and J. BRANDON, NASA-Langley Research Center 0900 hrs 0930 hrs 1000 hrs AIAA-2015-3223 AIAA-2015-3224 AIAA-2015-3225 Current Hypersonic and Space Stall/Spin Flight Test Techniques A Framework for Applying the Vehicle Flight Test Instrumentation with COTS Model Aircraft and Flight OODA Loop to Mission Control Challenges Data Systems Room Execution Thursday, 25 June 2015 249-FT-1 C. Jing, S. Yuan-pei, China Aerodynamics Research and Development Center, Mianyang, China 1130 hrs AIAA-2015-3242 Concurrent Subspace Optimization Design of Hypersonic Cruise Vehicle Madrid Manchester Steuben Obelisk B 107 B. Jie, Q. Mei, C. Zhang, Aviation Industry Corporation of China (AVIC), Zhuzhou, China E. Mathews, K. Wang, M. Wang, E. Jumper, University of Notre Dame, Notre Dame, IN Michigan, Ann Arbor, Ann Arbor, MI M. White, Ohio Aerospace Institute, Dayton, OH; M. Visbal, Air Force Research Laboratory, Wright-Patterson AFB, OH Fulvio Scarano Full Professor and Chair of Aerodynamics Delft University of Technology The Impact of Particle Image Velocimetry on Aerospace Technology 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 1030 hrs AIAA-2015-3254 Direct molecular simulation of high-temperature nitrogen dissociation due to both N-N2 and N2-N2 collisions Moderator: Steven Beresh, Distinguished Member of the Technical Staff, Sandia National Laboratories Panelists: Susan Gorton Ronald J. Adrian Project Manager, Revolutionary Vertical Lift Technology Project Regent’s Professor and Ira A. Fulton Professor of Mechanical and Aerospace Engineering NASA Langley Research Center Arizona State University Thursday, 25 June 2015 257-F360-8 0930 - 1200 hrs Michigan, Ann Arbor, Ann Arbor, MI B. Singh, M. Belmouss, S. Bane, Purdue University, West Lafayette, IN 1100 hrs AIAA-2015-3250 Investigation of shock / turbulent boundary interaction unsteadiness with various obstructions for aerooptics Detailed Molecular Process Modeling Chaired by: R. WAGNILD, Sandia National Laboratories and T. SCHWARTZENTRUBER, University of Minnesota 0900 hrs 0930 hrs 1000 hrs AIAA-2015-3251 AIAA-2015-3252 AIAA-2015-3253 Vibrational Relaxation and Master Equation Study of Characterization of Vibrational and Dissociation of Oxygen in Molecule- Vibrational and Rotational Rotational Energy Transfer in N2-N2 Atom Collisions Relaxation of Oxygen Dissociative Collisions Using the D. Andrienko, I. Boyd, University of D. Andrienko, I. Boyd, University of Quasiclassical Trajectory Method Thursday, 25 June 2015 256-TP-12 Technology Applications Company, LLC, Chesterfield, MO; T. Hayden, U.S. Air Force Academy, Colorado Springs, CO 1030 hrs AIAA-2015-3249 Characterization of Flow Control Actuators Based on Spark Discharge Plasmas Using Particle Image Velocimetry Networking Coffee Break Aero-Optics Plasma Diagnostics Chaired by: R. MILES, Princeton University and M. RENNIE, University of Notre Dame 0900 hrs 0930 hrs 1000 hrs AIAA-2015-3246 AIAA-2015-3247 AIAA-2015-3248 Aero-Optical Measurements of High- Non-intrusive Velocity and Density Numerical Investigation of Mach Supersonic Boundary Layers Measurements in Subsonic Aero-Optical Distortions over a S. Gordeyev, M. Rennie, University of Notre Turbulent Boundary Layer Hemisphere-on-Cylinder Turret Dame, Notre Dame, IN; A. Cain, Innovative J. Sontag, S. Gordeyev, University of Notre with Gaps Dame, Notre Dame, IN Aircraft Systems Design, Verification and Validation Thursday, 25 June 2015 255-PDL-12 Thursday, 25 June 2015 254-NW-8 0900 - 0930 hrs S. Herbst, M. Hornung, Technical University of Munich, Munich, Germany 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 a simulation casing based on Model for an Aircraft Design experimental modal parameters Environment in MATLAB Thursday, 25 June 2015 253-MST-11 Grand Ballroom E Rosetta Miro Chantilly Ballroom East Miguel Visbal Principal Research Aerospace Engineer and Team Leader of Multidisciplinary Computational Aerodynamics, Aerospace Systems Directorate Air Force Research Laboratory Travertine 108 W. Alexander, W. Devenport, Virginia Polytechnic Institute and State University, Blacksburg, VA H. Boden, Royal Institute of Technology (KTH), Stockholm, Sweden Chaired by: K. AHUJA, Georgia Institute of Technology 1400 hrs 1430 hrs AIAA-2015-3267 AIAA-2015-3266 Vortex Scattering Effects on Non-linear System Identification Techniques for Determination Acoustic Wave Propagation G. Ke, W. Li, Z. Zheng, University of of the Acoustic Properties of Kansas, Lawrence, Lawrence, KS Perforates Thursday, 25 June 2015 261-AA-39 W. Wolf, University of Campinas, Campinas, Brazil; A. Cavalieri, Technological Institute of Aeronautics (ITA), São José dos Campos, Brazil Chaired by: J. ALONSO-MIRALLES, UTC Aerospace Systems 1400 hrs 1430 hrs AIAA-2015-3260 AIAA-2015-3261 A fast numerical framework Noise Produced by Fabric and Wire for acoustic scattering by 3D Mesh Covered Panels in Low-Speed poroelastic plates Anechoic Wind Tunnels Thursday, 25 June 2015 260-AA-38 Research Center, Hampton, VA; J. Rhoads, F. De La Puente, L. Sanders, F. Vuillot, E. Pointwise, Inc., Fort Worth, TX; D. Manoha, ONERA, Châtillon, France Lockard, NASA Langley Research Center, Hampton, VA Chaired by: T. SPALT, NASA Langley Research Center 1430 hrs 1400 hrs AIAA-2015-3256 AIAA-2015-3255 Aeroacoustic Simulations of a Nose Nose landing gear flow and noise predictions on unstructured grid Landing Gear using FUN3D on using a cell-centered Navier-Stokes Pointwise Unstructured Grids V. Vatsa, M. Khorrami, NASA Langley code Thursday, 25 June 2015 259-AA-37 S. Redonnet, J. Bulte, ONERA, Châtillon, France 1500 hrs AIAA-2015-3268 Numerical Investigation of the Refraction Effects by Jet Flows in Anechoic Wind Tunnels, with Application to NASA/LaRC Quiet Flow Facility S. Haeri, J. Kim, P. Joseph, University of Southampton, Southampton, United Kingdom 1530 hrs AIAA-2015-3269 On the mechanisms of noise reduction in aerofoil-turbulence interaction by using wavy leading edges Fluid Acoustic Phenomena 1530 hrs AIAA-2015-3263 Experimental Investigation of FlowInduced Panel Vibrations at Cruise Mach Number Fluid-Structure Interaction P. McCarthy, A. Ekmekci, University of Toronto, Toronto, Canada A. Cavalieri, M. Donadon, Technological Institute of Aeronautics (ITA), São José T. Berkefeld, C. Spehr, K. Ehrenfried, S. dos Campos, Brazil; W. Wolf, University of Haxter, German Aerospace Center (DLR), Campinas, Campinas, Brazil Göttingen, Germany; S. Kroeber, Daimler AG, Stuttgart, Germany 1500 hrs AIAA-2015-3262 Acoustic scattering by finite composite plates T. Heffernon, D. Angland, X. Zhang, M. Smith, University of Southampton, Southampton, United Kingdom 1530 hrs AIAA-2015-3258 The Effect of Strut Geometry on the Inter-Wheel Flow for a Two-Wheel Landing Gear Landing Gear Noise B. Bryan, S. Glegg, Florida Atlantic University, Boca Raton, FL; M. Awasthi, W. Alexander, W. Devenport, Virginia Polytechnic Institute and State University, Blacksburg, VA 1600 hrs AIAA-2015-3270 Noise Radiation from a Cylindrical Embossment Immersed in Turbulent Boundary Layer Flow W. Chen, W. Qiao, L. Wang, F. Tong, Northwestern Polytechnical University, Xi’an, China; X. Wang, State Key Laboratory of Aerodynamics, Mianyang, China 1600 hrs AIAA-2015-3264 Rod-Airfoil Interaction Noise Reduction Using Leading Edge Serrations T. Rougier, Safran Group, Vélizy-Villacoublay, France; Q. Bouvy, Safran Group, Gloucester, United Kingdom; D. Casalino, J. Appelbaum, Exa GmbH, Stuttgart, Germany; C. Kleinclaus, Exa GmbH, Munich, Germany 1600 hrs AIAA-2015-3259 Design of quieter landing gears through lattice-Boltzmann CFD simulations Awards Luncheon: Celebrating Achievements in Aircraft and Atmospheric Systems 1500 hrs AIAA-2015-3257 The Effect of Flow Circulation on the Scattering of Landing Gear Noise A ticket is required and included in the conference registration fee where indicated. Thursday, 25 June 2015 258-LNCH-3 1230 - 1400 hrs L. Ayton, University of Cambridge, Cambridge, United Kingdom; J. Gill, University of Southampton, Southampton, United Kingdom; N. Peake, University of Cambridge, Cambridge, United Kingdom 1630 hrs AIAA-2015-3265 Comparison of Analytical, Numerical, and Experimental Results for Unsteady Aerofoil Interaction Noise Fleur-de-lis B Fleur-de-lis A Edelweiss Chantilly Ballroom West 109 J. Jiao, J. Delfs, J. Dierke, German Aerospace Center (DLR), Braunschweig, Germany C. Bahr, NASA Langley Research Center, Hampton, VA; W. Horne, NASA Ames Research Center, Moffett Field, CA 1430 hrs AIAA-2015-3272 Advanced Background Subtraction Applied to Aeroacoustic Wind Tunnel Testing S. Grace, Boston University, Boston, MA Q. Gu, G. Wang, J. Wu, M. Wang, China National Aeronautical Radio Electronics Research Institute, Shanghai, China Fan Broadband Noise Prediction Italy; C. Testa, Italian Institute for Naval Hydrodynamic Research and Ship Model Basin, Rome, Italy; M. Gennaretti, Roma Tre University, Rome, Italy Aachen, Germany K. Hamiche, H. Bériot, Siemens, Leuven, Belgium; G. Gabard, University of Southampton, Southampton, United Kingdom 1600 hrs AIAA-2015-3281 A Stabilised High-Order Finite Element Model for the Linearised G. Bernardini, Roma Tre University, Rome, Euler Equations 1530 hrs AIAA-2015-3280 A Spectral-BEM Formulation for Compact Sources Aeroacoustics N. Goli, B. Landrum, University of Alabama, Huntsville, Huntsville, AL M. Ozcan, I. Chakraborty, D. Mavris, Georgia Institute of Technology, Atlanta, GA S. Srigrarom, H. Lin, Z. Saw, J. Zhang, C. Lim, University of Glasgow, Singapore, Singapore 1600 hrs AIAA-2015-3288 Design and Build of Swarm Quadrotor UAVs at UGS Aircraft Subsystems, Integration, and Architectures in Computer Science and Control (INRIA), Pau, K. Chelliah, G. Raman, R. Muehleisen, Illinois France; F. Simon, ONERA, Toulouse, France Institute of Technology, Chicago, IL 1630 hrs AIAA-2015-3276 Effects of Hologram Distance and Regularization Techniques on Various Methods of Nearfield Acoustic V. Popie, E. Piot, ONERA, Toulouse, France; S. Holography Applied to Building Tordeux, French National Institute for Research Leakage Detection/Quantification 1600 hrs AIAA-2015-3275 Impedance eduction of perforated plates at low Stouhal numbers and high bias flow Mach number E. Envia, NASA Glenn Research Center, Cleveland, OH; J. Coupland, University of Southampton, Southampton, United Kingdom 1500 hrs Panel Fan Broadband Noise Prediction Panel M. Wang, R. Fattah, D. Angland, X. Zhang, University of Southampton, Southampton, United Kingdom 1500 hrs AIAA-2015-3279 High-Order Hybrid Cell-Centered Method for Computational Aeroacoustics CAA Numerical Techniques IV 1530 hrs AIAA-2015-3274 Beamforming-based noise level dereverberation solution for S1MA sonic wind-tunnel : metrology, methodology and validation A. Herron, D. Reed, D. Nance, NASA Marshall F. Mery, ONERA, Modane, France; R. Space Flight Center, Huntsville, AL Davy, V. Fleury, J. Bulte, M. Rey, ONERA, Châtillon, France 1500 hrs AIAA-2015-3273 Reducing the Effect of Transducer Mount Induced Noise on Aeroacoustic Wind Tunnel Testing Data with a New Transducer Mount Design Advanced Testing Techniques Chaired by: P. RAJ, Virginia Polytechnic Institute and State University and E. DIGIROLAMO, Lockheed Martin Aeronautics 1430 hrs 1500 hrs 1530 hrs 1400 hrs AIAA-2015-3285 AIAA-2015-3286 AIAA-2015-3287 AIAA-2015-3284 Dynamic Reconfiguration mechanism Development of an Integrated Major Aircraft Subsystem Effects on An Innovative All-Active Hybrid for Distributed Integrated Modular UAS for Agricultural Imaging Gas Turbine Performance in More Actuation System T. Röben, RWTH Aachen University, Avionics System Applications Electric Aircraft Architectures Thursday, 25 June 2015 265-ACD-7 A. Truong, D. Papamoschou, University of California, Irvine, Irvine, CA Chaired by: E. ENVIA, NASA Glenn Research Center 1400 hrs 1430 hrs AIAA-2015-3282 AIAA-2015-3283 Harmonic and Broadband Further Investigations Into a LowSeparation of Noise from a Small Order Model of Fan Broadband Ducted Fan Noise Thursday, 25 June 2015 264-AA-42 M. Williamschen, G. Gabard, University of Southampton, Southampton, United Kingdom Chaired by: P. MORRIS, Pennsylvania State University 1400 hrs 1430 hrs AIAA-2015-3277 AIAA-2015-3278 Performance of the DGM for the Towards CAA Based Acoustic Wind Linearized Euler Equations With Tunnel Corrections for Realistic Non-Uniform Mean-Flow Shear Layers Thursday, 25 June 2015 263-AA-41 M. Jones, W. Watson, NASA Langley Research Center, Hampton, VA; J. June, University of Florida, Gainesville, Gainesville, FL Chaired by: J. UNDERBRINK 1400 hrs AIAA-2015-3271 Optimization of Microphone Locations for Acoustic Liner Impedance Eduction Thursday, 25 June 2015 262-AA-40 Wyeth Obelisk A Lalique Inverness 110 M. Visbal, Air Force Research Laboratory, Wright-Patterson AFB, OH Netherlands A. Saini, A. Gopalarathnam, North Carolina State University, Raleigh, NC S. Chen, R. Chue, J. Schluter, Nanyang Technological University, Singapore, Singapore; S. Yu, Singapore Institute of Technology, Singapore, Singapore E. Saheby, G. Huang, W. Qiao, W. Tang, Nanjing University of Aeronautics and Astronautics, Nanjing, China 1600 hrs AIAA-2015-3293 A novel aerodynamic surface for redirecting the boundary layer Y. Yang, L. Veldhuis, G. Eitelberg, Delft University of Technology, Delft, The Netherlands 1600 hrs AIAA-2015-3302 Investigation of propeller induced ground vortices by numerical and D. Schauerhamer, S. Robinson, University experimental methods 1530 hrs AIAA-2015-3301 Simulating Aircraft Wake Vortices with OVERFLOW Vortical/Vortex Flow A. Medina, Army Research Laboratory, Aberdeen Proving Ground, MD; A. Jones, University of Maryland, College Park, College Park, MD 1530 hrs AIAA-2015-3297 Stereoscopic PIV analysis on rotary plates in bursting M. Mendenhall, D. Lesieutre, Nielsen Engineering & Research, Inc., Santa Clara, of California, Davis, Davis, CA CA; M. Kelly, NASA Langley Research Center, Hampton, VA Chaired by: M. JURKOVICH, US Air Force and T. DOUVILLE, TLG Aerospace, LLC. 1430 hrs 1500 hrs 1400 hrs AIAA-2015-3299 AIAA-2015-3300 AIAA-2015-3298 Effects of Spinning Motion on the Trailing Vortex-Induced Loads Near Ground Aircraft Wake Trapped Vortex Combustors During Close Encounters in Cruise Dissipation with Obstacles C. Wang, J. Schluter, Nanyang Technological University, Singapore, Singapore T. Reist, D. Zingg, University of Toronto, Toronto, Canada 1530 hrs AIAA-2015-3292 Optimization of the Aerodynamic Performance of Regional and WideBody-Class Blended Wing-Body Aircraft Low Speed, Low Reynolds Number Aerodynamics S. Andrews, R. Perez, Royal Military College of Canada, Kingston, Canada Technology Delhi, New Delhi, India; H. A. Medina, R. Singh, Army Research M. McCrink, J. Gregory, Ohio State Laboratory, Aberdeen Proving Ground, MD Aono, Japan Aerospace Exploration Agency University, Columbus, OH (JAXA), Sagamihara, Japan; W. Shyy, Hong Kong University of Science and Technology, Clear Water Bay, Hong Kong Thursday, 25 June 2015 269-APA-31 S. Peltier, C. Carter, Air Force Research Laboratory, Wright-Patterson AFB, OH 1600 hrs Oral Presentation PIV Applications in Supersonic Combustion Wind Tunnels at AFRL (Invited) Innovative Aerodynamic Concepts & Designs Chaired by: Z. YANG, Wright State University and A. JONES, University of Maryland 1400 hrs 1430 hrs 1500 hrs AIAA-2015-3294 AIAA-2015-3295 AIAA-2015-3296 Numerical investigation of finite- Propulsion of a Plunging Flexible Blade Element Momentum aspect ratio plate flows in ground Airfoil using a Torsion Spring Model Modeling of Low-Re Small UAS N. Arora, A. Gupta, Indian Institute of effect Electric Propulsion Systems Thursday, 25 June 2015 268-APA-30 Boeing Company, Berkeley, MO Chaired by: V. BHAGWANDIN, US Army Research Laboratory and J. LATZ, Northrop Grumman Aerospace Systems 1400 hrs 1430 hrs 1500 hrs AIAA-2015-3289 AIAA-2015-3290 AIAA-2015-3291 Evaluation of Adaptive Compliant Determination of Section Aerodynamic Parametric Study of Box-Wing Trailing Edge Technology Operating Condition on Wings and Aerodynamics for Minimum S. Wakayama, The Boeing Company, Rotor Blades From Leading-Edge Drag Under Stability and Huntington Beach, CA; E. White, The Pressure Measurements Maneuverability Constraints Thursday, 25 June 2015 267-APA-29 Columbus, OH K. Lynch, F. Scarano, Delft University of Technology, Delft, The Netherlands 1530 hrs Oral Presentation Tomographic and time-resolved PIV: Adding dimensions to flow diagnostics (Invited) The Impact of PIV on Aerospace Technology II Chaired by: S. BERESH, Sandia National Laboratories and K. LOWE, Virginia Tech 1400 hrs 1430 hrs 1500 hrs Oral Presentation Oral Presentation Oral Presentation PIV uncertainty: how good are PIV Use of PIV to anchor computational Synergistic Interactions of HighResolution CFD and PIV to Reveal measurements? (Invited) analysis of free shear and wall A. Sciacchitano, F. Scarano, Delft Complex Unsteady Flow Physics bounded flows (Invited) University of Technology, Delft, The D. Gaitonde, Ohio State University, (Invited) Thursday, 25 June 2015 266-AMT-13/GT-13 M. Stohr, I. Boxx, O. Lammel, K. Oberleithner, C. Arndt, W. Meier, German Aerospace Center (DLR), Stuttgart, Germany 1630 hrs Oral Presentation PIV in gas turbine combustion chambers: New insights into flow physics and its importance for combustor development Stemmons B Grand Ballroom A Carpenter Ballroom S. Gogineni, Spectral Energies, LLC, Dayton, OH 1700 hrs Oral Presentation A Tribute to Ron Adrian: Three Decades of PIV Innovation (Invited) Topaz 111 P. Zachos, Cranfield University, Cranfield, United Kingdom A. Shmilovich, Y. Yadlin, E. Whalen, The Boeing Company, Huntington Beach, CA D. Manosalvas, T. Economon, F. Palacios, A. Jameson, Stanford University, Stanford, CA M. Pruis, D. Delisi, NorthWest Research Associates, Redmond, WA; D. Jacob, Coherent Research Group, Ormond Beach, FL T. Nakashima, Y. Morikawa, Hiroshima University, Higashi-Hiroshima, Japan; M. Tsubokura, Hokkaido University, Sapporo, Japan; Y. Okada, T. Nouzawa, Mazda Motor Corporation, Aki Gun, Japan 1600 hrs AIAA-2015-3307 Unsteady Aerodynamics Simulations of a Sedan-Type Road Vehicle during Sinusoidal Steering Input 1530 hrs AIAA-2015-3318 Evaluation of Fast-Time Wake Models using Denver 2006 Field Experiment Data 1600 hrs AIAA-2015-3319 Aerodynamic Simulation of Wake Encounter for Aircraft Close Formation Operations (Invited) Aircraft Wake Turbulence II (Invited) 1600 hrs AIAA-2015-3314 Plenum design for compact fluidic effectors J. Chard, A. Llopis-Pascual, W. Crowther, U. Cordes, K. Hufnagel, C. Tropea, Technical University of Manchester, Manchester, University of Darmstadt, Darmstadt, Germany; United Kingdom G. Kampers, M. Hölling, J. Peinke, University of Oldenburg, Oldenburg, Germany 1530 hrs AIAA-2015-3313 Experimental investigation of Passive Load Reduction under dynamic inflow conditions N. Ahmad, NASA Langley Research A. He, Z. Zheng, University of Kansas, Center, Hampton, VA; M. Pruis, NorthWest Lawrence, Lawrence, KS M. Pruis, D. Delisi, NorthWest Research L. Thobois, R. Krishnamurthy, S. Loaec, J. Research Associates, Seattle, WA Associates, Redmond, WA; D. Jacob, Coherent Cariou, Leosphere, Orsay, France; A. DolfiResearch Group, Ormond Beach, FL; D. Lai, Bouteyre, M. Valla, ONERA, Palaiseau, France NorthWest Research Associates, Redmond, WA Chaired by: Z. ZHENG, The University of Kansas and M. PRUIS, Northwest Research Associates Inc 1430 hrs 1500 hrs 1400 hrs AIAA-2015-3316 AIAA-2015-3317 AIAA-2015-3315 Effect of Atmospheric Sheets Fast-time Wake Vortex Model Wind and EDR Measurements and Layers Near the Ground on Predictions Compared with with Scanning Doppler LIDARs for Wake Vortex Transport and Decay Observations Behind Landing Aircraft Preparing Future Weather Dependent (Invited) Near the Ground (Invited) Separation Concepts (Invited) Thursday, 25 June 2015 272-ASE-4 J. Wang, H. Li, X. Meng, D. Zhang, Northwestern Polytechnical University, Xi’an, China; F. Liu, S. Luo, University of California, Irvine, Irvine, CA C. Junqueira-Junior, S. Yamouni, Technological Institute of Aeronautics (ITA), São José dos Campos, Brazil; J. Azevedo, Aeronautics and Space Institute (IAE), São José dos Campos, Brazil; W. Wolf, University of Campinas, Campinas, Brazil 1530 hrs AIAA-2015-3306 Large Eddy Simulations of Supersonic Jet Flows for Aeroacoustic Applications Unsteady Aerodynamics II Flow Control Applications & Demonstrations (Active & Passive) III P. Zachos, D. MacManus, N. Chiereghin, Cranfield University, Cranfield, United Kingdom 1500 hrs AIAA-2015-3305 Flow distortion measurements in convoluted aero engine intakes Chaired by: C. TILMANN, Air Force Reseach Laboratory and S. SILTON, US Army Research Laboratory 1400 hrs 1430 hrs 1500 hrs AIAA-2015-3310 AIAA-2015-3311 AIAA-2015-3312 Nanosecond-SDBD Actuation over a Computational Evaluation of Flow Techniques for the Design of Active Conical Forebody at Wind Speed 72 Control for Enhanced Control Flow Control Systems in Heavy m/s and Angle of Attack 45 degree Authority af a Vertical Tail Vehicles Thursday, 25 June 2015 271-APA-33 C. Barnes, M. Visbal, Air Force Research Laboratory, Wright-Patterson AFB, OH; G. Huang, Wright State University, Dayton, OH Chaired by: E. FELTROP, The Cessna Aircraft Company and K. VANDEN, USAF 1400 hrs 1430 hrs AIAA-2015-3303 AIAA-2015-3304 Complex aero-engine intake ducts Effect of Bending-Oscillations on and dynamic distortion a Streamwise-Oriented Vortex D. MacManus, N. Chiereghin, D. Gil Prieto, Interaction Thursday, 25 June 2015 270-APA-32 H. Ishioka, Hokkaido University, Sapporo, Japan; K. Onishi, RIKEN Advanced Institute for Computational Science, Kobe, Japan; K. Nakasato, Nissan Motor Corporation, Yokohama, Japan; T. Nakashima, Hiroshima University, Higashi-Hiroshima, Japan; M. Tsubokura, Hokkaido University, Sapporo, Japan 1630 hrs AIAA-2015-3308 Coupled 6DoF motion and Aerodynamics Simulation of Road Vehicles in Crosswind gusts Plum Blossom B Stemmons C V. Suryakumar, Y. Babbar, T. Strganac, Texas A&M University, College Station, TX; A. Mangalam, Tao of Systems Integration, Inc., Hampton, VA 1700 hrs AIAA-2015-3309 An Unsteady Aerodynamic Model based on the Leading-Edge Stagnation Point Stemmons A 112 of California, Irvine, Irvine, CA 1600 hrs AIAA-2015-3324 Energy-Aware Path Optimization for Persistent Sampling of Severe Storms UAS Integration & Operations I of Technology, Delft, The Netherlands; S. S. Roy, Washington State University, Mahlich, EUROCONTROL, Bretigny, France Pullman, WA; Y. Wan, University of North Texas, Denton, TX E. Vargo, C. Taylor, C. Wanke, MITRE Corporation, McLean, VA 1530 hrs AIAA-2015-3333 Probabilistic Time-Series Models for Ground Delay Program Decision Support D. Long, S. Hasan, V. Stouffer, LMI, McLean, VA; K. Ramamoorthy, Saab Sensis Corporation, East Syracuse, NY; H. Idris, Engility Corporation, Billerica, MA; B. Ballard, GRA, Inc., Jenkintown, PA; et al. 1600 hrs AIAA-2015-3334 Analytical Identification and Ranking of Choke Points in the National Airspace System ATM VI - Management of NAS Resources M. Stevens, B. Coloe, E. Atkins, University of Michigan, Ann Arbor, Ann Arbor, MI 1500 hrs AIAA-2015-3329 Platform-Independent Geofencing for Low Altitude UAS Operations 1500 hrs AIAA-2015-3332 Proactive and Reactive Management of Non-Weather Capacity Disruption Events in the National Airspace System: A Flow R. Curran, E. Konnemann, Delft University Modeling and Design Approach Chaired by: K. MARAIS, Purdue University 1430 hrs 1400 hrs AIAA-2015-3331 AIAA-2015-3330 Strategic Air Traffic Planning with Performance Impact of Improved Frechet Distance Aggregation and Departure Time Prediction Relative Rerouting to Sector Demand & Arrival Time A. Bombelli, L. Soler, K. Mease, University Predictability Thursday, 25 June 2015 275-ATIO-25 L. Fern, R. Rorie, San Jose State University, Moffett Field, CA; J. Pack, Infoscitex Corporation, Dayton, OH; J. Shively, NASA Ames Research Center, Moffett Field, CA; M. Draper, Air Force Research Laboratory, WrightPatterson AFB, OH Chaired by: V. SCHULTZ, NASA Langley Research Center 1400 hrs 1430 hrs AIAA-2015-3327 AIAA-2015-3328 An Evaluation of Detect and Avoid System Development for the NASA (DAA) Displays for Unmanned Aircraft UAS Airspace Operations Challenge S. Fehrenbach, Z. Barbeau, J. Jacob, G. Systems: The Effect of Information Chowdhary, Oklahoma State University, Level and Display Location on Pilot Stillwater, OK Performance Thursday, 25 June 2015 274-ATIO-24 1530 hrs AIAA-2015-3323 Elastomer Seal Performance after Terrestrial Ultraviolet Radiation Exposure Atmospheric and Space Environments C. Daniels, J. Mather, H. Oravec, University W. Silva, E. Frew, University of Colorado, of Akron, Akron, OH; S. Taylor, University Boulder, Boulder, CO S. Taylor, University of Toledo, Toledo, OH; of Toledo, Toledo, OH; P. Dunlap, NASA J. Mather, C. Daniels, University of Akron, Glenn Research Center, Cleveland, OH Akron, OH Chaired by: W. VAUGHAN, William W Vaughan Consultant and R. SCULLY, NASA 1400 hrs 1430 hrs 1500 hrs AIAA-2015-3320 AIAA-2015-3321 AIAA-2015-3322 Investigation of the Impact of Lightning Protection for the Orion Advanced Spacecraft Systems Emulation for Space Environment Surface Blending and Ultraviolet Space Vehicle R. Scully, NASA Johnson Space Center, Qualification Testing Radiation Exposure on Elastomer Houston, TX H. Rumann, Bastion Technologies, Inc., Seal Leak Rate Performance for Houston, TX Space Seal Applications Thursday, 25 June 2015 273-ASE-5 M. Alcabin, The Boeing Company, Seattle, WA; R. Golaszewski, GRA, Inc., Jenkintown, PA; W. Cotton, Cotton Aviation Enterprises, Lakeway, TX; V. Stouffer, LMI, McLean, VA; J. Musiak, The Boeing Company, Seattle, WA Morocco Ming Y. Şöhret, T. Karakoc, Anadolu University, Eskisehir, Turkey; N. Karakoç, Osmangazi University, Eskisehir, Turkey 1700 hrs AIAA-2015-3326 Mathematical Modelling for Carbon Dioxide Equivalent Prediction of Greenhouse Gases Emitted from a Small Scale Turbojet Engine 1630 hrs AIAA-2015-3335 Stakeholder Feedback-Based Identification, Ranking, and Causes of Choke Points in the National Airspace System W. Okolo, A. Dogan, University of Texas, Arlington, Arlington, TX; W. Blake, Air Force Research Laboratory, WrightPatterson AFB, OH 1630 hrs AIAA-2015-3325 Ride Quality Within Trail Aircraft In Formation Flight Plum Blossom A 113 Cruz, CA; A. Stoll, B. Goldsmith, Joby Aviation, Santa Cruz, CA W. Tavernetti, M. Hafez, University of California, Davis, Davis, CA M. Moore, NASA Langley Research Center, Hampton, VA 1600 hrs Oral Presentation The Centrifugally Stiffened Rotor (CSR) VTOL Long Endurance Concept Hypersonic and Chemically-Reacting Flows Mark Seager Intel Fellow CTO, High Performance Computing Ecosystem, Intel Corporation Tucson, AZ; U. Kaul, NASA Ames Research D. Akins, A. Singh, J. Little, University of Center, Moffett Field, CA Arizona, Tucson, Tucson, AZ MN; N. Cymbalist, P. Dimotakis, California Institute of Technology, Pasadena, CA E. Baydar, F. Lu, University of Texas, Arlington, Arlington, TX; J. Slater, NASA Glenn Research Center, Cleveland, OH Chaired by: M. YU, University of Maryland, Baltimore County and L. PACK MELTON, NASA-Langley Research Center 1430 hrs 1500 hrs 1400 hrs AIAA-2015-3343 AIAA-2015-3344 AIAA-2015-3342 Mixing Layer: Numerical and Effects of Pulse Energy on Shear Observations on the Mean and Layer Control using Surface Plasma Turbulent Wake of a Micro-Ramp Experimental Control Strategies J. Little, University of Arizona, Tucson, Discharges Array Thursday, 25 June 2015 279-FD-31 Cummings, U.S. Air Force Academy, Colorado Springs, CO D. Baldacchino, C. Simao Ferreira, G. van Bussel, Delft University of Technology, Delft, The Netherlands 1530 hrs AIAA-2015-3345 Towards integral boundary layer modelling of vane-type vortex generators Flow Control - Vortical Flows 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 G. Candler, P. Subbareddy, University of M. Righi, Zurich University of Applied Tube to Thermal Ignition and Flame Minnesota, Minneapolis, Minneapolis, Sciences, Winterthur, Switzerland R. Decker, M. Semper, J. Anthony, R. Fronts Thursday, 25 June 2015 278-FD-30 E. Demers Bouchard, D. Rancourt, D. Mavris, Georgia Institute of Technology, Atlanta, GA 1530 hrs AIAA-2015-3337 Integration of Electric Propulsion in Efficient Heavy-Lift VTOL Concept Supercomputing: Roadmap and its Future Role in Aerospace Engineering A. Stoll, P. Pei, A. Clark, J. Bevirt, Joby Aviation, Santa Cruz, CA 1500 hrs Oral Presentation Design and Testing of the Joby S2 Electric VTOL PAV Propellers Transformational Flight - Unconventional VTOL Configurations Moderator: Doug Cline, Technical Lead, High Performance Computing, Lockheed Martin Aeronautics Panelists: Brian Mitchell William Gropp Senior Principal Engineer Thomas M. Siebel Chair, Department of Computer Science and Director, Parallel Computing Institute GE Global Research University of Illinois at Urbana-Champaign Thursday, 25 June 2015 277-F360-9 1400 - 1630 hrs M. Page, DZYNE Technologies, Irvine, CA Chaired by: I. CHOUTAPALLI, The University of Texas - Pan American 1400 hrs 1430 hrs Oral Presentation AIAA-2015-3336 Design and Testing of the Joby Lotus Flight Test Results for the DZYNE Multifunctional Rotor VTOL UAV ROTORwing - A High Endurance P. Sinha, Transition Robotics, Inc., Santa VTOL Concept Thursday, 25 June 2015 276-ATIO-26 Sapphire Grand Ballroom E Senators Lecture Hall Jef Dawson Applications Manager Cray, Inc. Monet Ballroom 114 R. Del Rosario, NASA Glenn Research Center, Cleveland, OH; S. Anders, NASA Langley Research Center, Hampton, VA; N. Madavan, NASA Ames Research Center, Moffett Field, CA J. Krausman, D. Miller, TCOM, L.P., Columbia, MD J. Hall, D. Poole, T. Rendall, C. Allen, University of Bristol, Bristol, United Kingdom M. Kasprzyk, P. Bibik, M. Malinowski, J. Polaczek, K. Wronowski, Warsaw University of Technology, Warsaw, Poland 1530 hrs AIAA-2015-3349 Application of a small UAV fleet for demonstration of optimized mission J. Santos, D. Garcia, M. Cunha, L. Góes, Technological Institute of Aeronautics (ITA), São José dos Campos, Brazil; R. Pant, Indian Institute of Technology Mumbai, Mumbai, India 1500 hrs AIAA-2015-3352 Design and Flight Testing of an Autonomous Airship S. Gorton, NASA Langley Research Center, Hampton, VA; I. López, NASA Glenn Research Center, Cleveland, OH; C. Theodore, NASA Ames Research Center, Moffett Field, CA 1530 hrs Oral Presentation Revolutionary Vertical Lift Technology Project R. Young, S. Smeltzer, NASA Langley Research Center, Hampton, VA 1600 hrs Oral Presentation Advanced Composites Project Overview R. Munjulury, P. Berry, T. Melin, K. University of Kaiserslautern, Kaiserslautern, R. Najian Asl, D. Baumgärtner, K. Amadori, P. Krus, Linköping University, Germany; T. Economon, F. Palacios, J. Bletzinger, Technical University of Munich, Linköping, Sweden Alonso, Stanford University, Stanford, CA Munich, Germany 1530 hrs AIAA-2015-3357 Knowledge-based Integrated Wing Automation and Optimization for Conceptual Design Shape and Topology II K. Cromer, S. Petersen, TCOM, L.P., Columbia, MD 1530 hrs AIAA-2015-3353 Diaphragm Testing of Fabric Components & Correlation to Analysis P. Magalhaes, B. Mattos, Technological Institute of Aeronautics (ITA), São José dos Campos, Brazil 1600 hrs AIAA-2015-3358 Conceptual optimal design of environmentally friendly airliners: a review of available methodologies and their integration into a consistent framework for everyday use Lighter-than-Air Systems & Technologies II P. Coen, NASA Langley Research Center, Hampton, VA; K. Civinskas, L. Povinelli, NASA Glenn Research Center, Cleveland, OH 1500 hrs Oral Presentation Commercial Supersonic Technology Project Overview Overview of NASA Advanced Air Vehicles Program Chaired by: B. MESMER, University of Alabama and V. KALIVARAPU, Iowa State University 1430 hrs 1500 hrs 1400 hrs AIAA-2015-3355 AIAA-2015-3356 AIAA-2015-3354 Towards shape optimization Volumetric Shape Parameterisation A Discrete Adjoint Framework for Unsteady Aerodynamic and of steady-state fluid-structure for Combined Aerodynamic Aeroacoustic Optimization interaction problems using vertex Geometry and Topology B. Zhou, T. Albring, N. Gauger, Technical morphing Optimisation Thursday, 25 June 2015 283-MAO-10 J. Deese, T. Muyimbwa, N. Deodhar, C. Vermillion, P. Tkacik, University of North Carolina, Charlotte, Charlotte, NC Chaired by: D. HORKHEIMER, Honeywell International, Inc. 1400 hrs 1430 hrs AIAA-2015-3350 AIAA-2015-3351 Lab-Scale Characterization of a The 12M™ Tethered Aerostat Lighter-Than-Air Wind Energy System: Rapid Tactical Deployment System - Closing the Loop for Surveillance Missions Thursday, 25 June 2015 282-LTA-2 J. Dryer, B. Esker, NASA Headquarters, Washington, DC 1500 hrs AIAA-2015-3348 Evaluation of Low-Cost Autopilots for SUAS Operations Optimization Techniques in Flight Test/Ground Test C. Brown, J. Jacob, Oklahoma State University, Stillwater, OK Y. Minqiang, C. Yue, Taiyuan AeroInstruments Company, Ltd., Taiyuan, China Chaired by: B. ESKER and R. DEL ROSARIO, NASA Glenn Research Center 1400 hrs 1430 hrs Oral Presentation Oral Presentation Advanced Air Vehicles Program NASA’s Advanced Air Transport Overview Technology Project Thursday, 25 June 2015 281-GEPC-1 C. He, Aviation Industry Corporation of China (AVIC), Xi’an, China Chaired by: W. SCHUMAN, AF TSTA/AEDC and B. MILLS, AEDC/ ATA 1400 hrs 1430 hrs AIAA-2015-3346 AIAA-2015-3347 Optimized Calculation of Forces for The design and test result of pressure Fullscale Aircraft Structure Fatigue distortion compensation device in Weight and Balance System Testing Thursday, 25 June 2015 280-FT-2/GT-14 D. Papadimitriou, C. Papadimitriou, University of Thessaly, Volos, Greece 1630 hrs AIAA-2015-3359 Robust and Reliability-Based Topology Optimization of Wing Bodies C. Mouring, NASA Langley Research Center, Hampton, VA; R. Colantonio, NASA Glenn Research Center, Cleveland, OH 1630 hrs Oral Presentation NASA Aeronautics Evaluation and Test Capabilities Project Madrid Steuben Metropolitan Ballroom Obelisk B 115 University of Munich, Munich, Germany; A. Fischersworring-Bunk, MTU Aero Engines, Munich, Germany J. Qian, F. Liu, Nanjing University of Aeronautics and Astronautics, Nanjing, China; X. Qiu, Aviation Motor Control System Institute, Wuxi, China Tsukuba, Tsukuba, Japan; S. Ogawa, T. Yoshino, Toshiba Corporation, Kawasaki, Japan; T. Fujino, University of Tsukuba, Tsukuba, Japan H. Katsurayama, Yamaguchi University, Ube, Japan 1530 hrs AIAA-2015-3368 Numerical Investigation of Several Alkali Metal Addition Methods for the Forced Elevation of the Starting Altitude in the Electrodynamic Aerobraking Declearation S. Krishnamoorthy, S. Close, Stanford University, Stanford, CA 1600 hrs AIAA-2015-3369 Particle in Cell (PIC) simulations of plasma-electrode interactions for Reentry Blackout Alleviation Rising Leaders in Aerospace Panel Discussion: Transitioning to Leadership G. de Oliveira, R. Santos Pereira, D. Ragni, M. Kotsonis, Delft University of Technology, Delft, The Netherlands 1500 hrs AIAA-2015-3367 Modeling DBD Plasma Actuators in Integral Boundary Layer Formulation for Application in Panel Methods Propulsion Systems Plasma Aerodynamics & Flow Control V Y. Liu, M. Junkui, G. Dilan, Nanjing University of Aeronautics and Astronautics, Nanjing, China 1500 hrs AIAA-2015-3364 Numerical Study of Similarity and Dimensional Methods in Scaled Turbine Vane cooling performance experiment Uncertainty I 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 Chief Engineer President and Executive Director Raytheon Missile Systems National Institute of Aerospace Thursday, 25 June 2015 287-RLA-3 1400 - 1530 hrs T. Takahashi, Y. Shimosawa, K. Masuda, T. Fujino, University of Tsukuba, Tsukuba, Japan Chaired by: J. POGGIE, USAF AFRL/RBAC 1400 hrs 1430 hrs AIAA-2015-3365 AIAA-2015-3366 Numerical Study of Three-dimensional Numerical Thermal Protection Using Simulation of Magnetohydrodynamic Magnetohydrodynamic Flow Flow Control in Reentry Flight K. Masuda, Y. Shimosawa, University of Control in Mars Entry Flight Thursday, 25 June 2015 286-PDL-13 J. Lu, China Shipbuilding Industry Corporation Company, Ltd., Xi’an, China Chaired by: A. ELMILIGUI, NASA Langley Research Center 1400 hrs 1430 hrs AIAA-2015-3362 AIAA-2015-3363 One-dimensional Model of a Individual model identification for Closed-loop Underwater Propulsion turbofan engine based on particle System swarm optimization Thursday, 25 June 2015 285-MST-12 N. Nigam, S. Ayyalasomayajula, X. Qi, P. Chen, Intelligent Automation, Inc., Rockville, MD; J. Alonso, Stanford University, Stanford, CA 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 Surrogate-based Robust Shape High-Fidelity Weight Estimation Optimization for Vane Clusters for Aircraft Conceptual Design I. Arsenyev, F. Duddeck, Technical Optimization Thursday, 25 June 2015 284-MAO-11 Frederick Wieland Director, Air Traffic Management Intelligent Automation Systems, Inc. Emerald Miro Travertine Manchester 116 University, Tempe, AZ 1000 hrs AIAA-2015-3376 Revisiting Busemann: The Design Implications of Inconsistencies Found Within Simple Sweep Theory M. Swann, T. Takahashi, Arizona State University, Tempe, AZ 1030 hrs AIAA-2015-3377 A Total Flight Envelope Approach to Conceptual Design Stability & Control K. Chiba, S. Satori, R. Hiramoto, S. Kase, R. Mitsuhashi, Hokkaido University of Science, Sapporo, Japan; J. Sasaki, Hokkaido Aerospace Science and Technology Incubation Center, Sapporo, Japan; et al. 1100 hrs AIAA-2015-3378 Feasibility Studies on a High-Altitude Captive Lighter-Than-Air Platform System Aeronautic Discipline Considerations in Aircraft Design T. Takahashi, S. Kamat, Arizona State M. Guynn, NASA Langley Research Center, University, Tempe, AZ Hampton, VA Chaired by: H. JIMENEZ, Georgia Institute of Technology 0930 hrs 0900 hrs AIAA-2015-3375 AIAA-2015-3374 Prediction of Wing Structural Mass Effective L/D: A Theoretical for Transport Category Aicraft Approach to the Measurement Conceptual Design of Aero-Structural Efficiency in T. Takahashi, T. Lemonds, Arizona State Aircraft Design Friday, 26 June 2015 293-ACD-8 Plenary Keynote Friday, 26 June 2015 292-PLNRY-5 0800 - 0900 hrs The G650 Design, Development, and Test Kurt Erbacher Vice President, G650 Aircraft Program Gulfstream Aerospace Corporation Speakers’ Briefing Friday, 26 June 2015 291-SB-5 0730 - 0800 hrs Friday Development and Testing of the X-47B Pablo Gonzalez, II UCAS-D Program Manager Northrop Grumman Aerospace Systems Wright Brothers Lectureship in Aeronautics Thursday, 25 June 2015 290-LEC-6 1730 - 1830 hrs 1530 hrs AIAA-2015-3373 Calibration of DSMC parameters for transport processes in ionized air mixtures I. Borges Sebastiao, A. Alexeenko, Purdue K. Swaminathan Gopalan, K. Stephani, University, West Lafayette, IN University of Illinois, Urbana-Champaign, Urbana, IL 1500 hrs AIAA-2015-3372 DSMC Investigation of Nonequilibrium Effects in a H2-O2 Unstretched Diffusion Flame Networking Coffee Break K. Higdon, D. Goldstein, P. Varghese, University of Texas, Austin, Austin, TX 1430 hrs AIAA-2015-3371 Sensitivity Analysis of DSMC Parameters for Ionizing, Radiating Hypersonic Flows DSMC Thursday, 25 June 2015 289-NW-9 1530 - 1600 hrs A. Borner, NASA Ames Research Center, Moffett Field, CA; F. Panerai, University of Kentucky, Lexington, Lexington, KY; N. Mansour, NASA Ames Research Center, Moffett Field, CA Chaired by: D. HASH, NASA - ARC 1400 hrs AIAA-2015-3370 DSMC Study of Carbon Fiber Oxidation in Ablative Thermal Protection Systems Thursday, 25 June 2015 288-TP-13 Miro Chantilly Ballroom West Session Rooms Chantilly Ballroom West Meeting Room Foyers Rosetta 117 N. Ulbrich, Jacobs, Moffett Field, CA Devenport, Virginia Polytechnic Institute and State University, Blacksburg, VA A. Borgoltz, W. Devenport, Virginia Polytechnic Institute and State University, Blacksburg, VA; J. Luedke, General Electric Company, Greenville, SC; et al. 1000 hrs AIAA-2015-3388 Aerodynamic performance study of high pressure zone capture wing configurations S. Vey, D. Marten, G. Pechlivanoglou, C. Briley, D. Nichols, University of Tennessee, Nayeri, C. Paschereit, Technical University Chattanooga, Chattanooga, TN of Berlin, Berlin, Germany 1030 hrs AIAA-2015-3392 Experimental and Numerical Investigations of a Small Research Wind Turbine G. Fiore, M. Selig, University of Illinois, Urbana-Champaign, Urbana, IL 1100 hrs AIAA-2015-3393 Optimization of Wind Turbine Airfoils Subject to Particle Erosion Propeller/Rotorcraft/Wind Turbine Aerodynamics III K. Cui, G. Li, Y. Xiao, Chinese Academy of J. Park, C. Ocheltree, J. Choi, S. Choi, P. Raj, Sciences, Beijing, China A. Friedman, Virginia Polytechnic Institute and State University, Blacksburg, VA D. Marten, Technical University of Berlin, Berlin, Germany; H. Spiegelberg, Technical University of Darmstadt, Darmstadt, Germany; G. Pechlivanoglou, C. Nayeri, C. Paschereit, Technical University of Berlin, Berlin, Germany; C. Tropea, Technical University of Darmstadt, Darmstadt, Germany Aerodynamic Design Methodologies III C. Zhang, F. Wang, W. Kong, H. Liu, Shanghai Jiao Tong University, Shanghai, China Chaired by: K. MASSEY, DARPA/TTO and J. MURRAY, Sandia National Laboratories 0930 hrs 1000 hrs 0900 hrs AIAA-2015-3390 AIAA-2015-3391 AIAA-2015-3389 Extension of a Parabolic Method Sensitivity of Wind Turbine Airfoil Configuration and Numerical Investigation of the Adaptive Camber without Pressure Approximations Sections to Geometry Variations Airfoil as Passive Load Alleviation for Wind Turbines in ABL Flows Inherent in Modular Blades K. Brown, N. Molinaro, T. Meyers, A. Mittal, L. Taylor, K. Sreenivas, W. Mechanism for Wind Turbines Friday, 26 June 2015 297-APA-37 University of Québec, Montréal, Canada Chaired by: C. ROSEMA, US Army AMRDEC 0900 hrs 0930 hrs AIAA-2015-3386 AIAA-2015-3387 Experimental Validation of a Stability Derivative Computation of Morphed Wing Geometry Using Tailless Aircraft using Variable-Fidelity Small Wind Tunnel Testing Aerodynamic Analysis and WindA. Koreanschi, S. Oliviu, R. Botez, Tunnel Experiments Friday, 26 June 2015 296-APA-35 A. DeGennaro, C. Rowley, L. Martinelli, Princeton University, Princeton, NJ M. Kammeyer, The Boeing Company, St. Louis, MO; N. Ulbrich, Jacobs, Moffett Field, CA 1100 hrs AIAA-2015-3382 The Use of Absolute-Value Terms in Regression Modeling of Multi-Piece Force Balances (Invited) Icing or Roughness Effects on Vehicle Aerodynamics S. Karahan, A. Kutay, Middle East Technical University, Ankara, Turkey R. Callahan, D. Landman, Old Dominion University, Norfolk, VA; S. Commo, K. Lynn, NASA Langley Research Center, Hampton, VA 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 L. Joseph, J. Fenouil, A. Borgoltz, W. Quantification for Airfoil Icing high-lift configurations Friday, 26 June 2015 295-APA-34 Langley Research Center, Hampton, VA 1030 hrs AIAA-2015-3381 Analysis of Five-Hole Probe Calibration Parameters Aerodynamic Measurement Systems: Calibration and Monitoring Chaired by: R. RHEW, NASA-Langley Research Center and G. JONES, NASA-Langley Research Center 0900 hrs 0930 hrs 1000 hrs Oral Presentation AIAA-2015-3379 AIAA-2015-3380 Measurement System Calibration Improved Regression Analysis of Statistical Process Control Temperature-Dependent StrainImplemented for Long Term Study of Fundamentals R. Rhew, P. Parker, G. Jones, NASA Gage Balance Calibration Data Wind Tunnel Balance Calibrations Friday, 26 June 2015 294-AMT-14/GT-15 Stemmons B Carpenter Ballroom Stemmons C Topaz 118 M. Underwood, M. Guminsky, NASA Langley Research Center, Hampton, VA S. Ayyalasomayajula, R. Sharma, F. Wieland, Intelligent Automation, Inc., Rockville, MD; A. Trani, N. Hinze, T. Spencer, Virginia Polytechnic Institute and State University, Blacksburg, VA A. Tyagi, F. Wieland, Intelligent Automation, Inc., Rockville, MD; S. Toussaint, Coherent Technical Services, Inc., Lexington Park, MD; J. Luxhoj, LCR, LLC, Somerset, NJ Chaired by: D. DELAURENTIS, Purdue University 0900 hrs 0930 hrs AIAA-2015-3405 AIAA-2015-3406 UAS Demand Generation Using Investigation of Simulated UAS Subject Matter Expert Interviews Safety Incidents Using UAS Safety and Socio-economic Analysis Analysis Model (USAM) Friday, 26 June 2015 300-ATIO-29 Chaired by: K. MARAIS, Purdue University 0900 hrs 0930 hrs AIAA-2015-3400 AIAA-2015-3401 Achieving TASAR Operational A Preliminary Evaluation of Readiness Supersonic Transport Category D. Wing, NASA Langley Research Center, Vehicle Operations in the National Hampton, VA Airspace System Friday, 26 June 2015 299-ATIO-28 C. Gong, D. Mcnally, NASA Ames Research Moffett Field, CA Center, Moffett Field, CA Chaired by: Y. JUNG, NASA Ames Research Center 0900 hrs 0930 hrs AIAA-2015-3394 AIAA-2015-3395 Initial Analysis of and Predictive Dynamic Arrival Routes: A Model Development for Weather Trajectory-Based Weather Reroute Advisory Use Avoidance System for Merging H. Arneson, NASA Ames Research Center, Arrivals and Metering Friday, 26 June 2015 298-ATIO-27 E. Filippone, Italian Aerospace Research Center (CIRA), Capua, Italy 1000 hrs AIAA-2015-3407 RPAS - ATM Integration Demonstration - Real-Time Simulation Results UAS Integration & Operations II T. Dubot, S. Aubry, J. Bedouet, ONERA, Toulouse, France 1030 hrs AIAA-2015-3403 Dynamic Airspace Configuration in SESAR: building a smooth and A. Staley, C. Bolczak, MITRE Corporation, dynamic opening scheme through McLean, VA airspace building blocks assessment 1000 hrs AIAA-2015-3402 Improving Situation Awareness with a Traffic Management Portal Future Concepts 1030 hrs AIAA-2015-3397 Dynamic Wake Vortex Separation Combining with AMAN/DMAN Concept S. Campbell, M. McPartland, M. Ishutkina, N. Matayoshi, E. Yoshikawa, Japan Lincoln Laboratory, Massachusetts Institute Aerospace Exploration Agency (JAXA), of Technology, Lexington, MA Mitaka, Japan 1000 hrs AIAA-2015-3396 Benefits Analysis of GroundSourced Convective Weather Alerting in the Cockpit ATM VII - Weather Impact N. Dzikus, German Aerospace Center (DLR), Hamburg, Germany; S. Bartosch, RWTH Aachen University, Aachen, Germany; M. Schaefer, Federal Ministry of Transport and Digital Infrastructure, Bonn, Germany L. Thobois, Leosphere, Orsay, France 1130 hrs AIAA-2015-3399 Wind Measurements with groundbased fiber-based wind Doppler LIDAR systems for aviation weather applications 1100 hrs AIAA-2015-3404 The Impact of Mitigation Measures for System Capacity Constraints on the Future Air Transportation System N. Ahmad, B. Barmore, K. Swieringa, NASA Langley Research Center, Hampton, VA 1100 hrs AIAA-2015-3398 Wind Information Uplink to Aircraft Performing Interval Management Operations Ming Wyeth Morocco 119 J. Buehn, P. Slaboch, Saint Martin’s University, Lacey, WA X. Zhao, Alabama A&M University, Huntsville, AL; S. Zhang, ESI Group, Huntsville, AL Chaired by: P. SLABOCH and D. GONZALEZ, Naval Surface Warfare Center 0930 hrs 0900 hrs AIAA-2015-3414 AIAA-2015-3413 Computational Study of Active Flow Aeroelastic Response of Rocket Control of a Flow-Excited Helmholtz Nozzles Subected to Combined Resonator Thrust and Side Loads Friday, 26 June 2015 303-CFD-33 E. Duque, `. Hiepler, Intelligent Light, T. Horchler, K. Mani, K. Hannemann, Rutherford, NJ; R. Haimes, Massachusetts German Aerospace Center (DLR), Institute of Technology, Cambridge, MA; Göttingen, Germany C. Stone, Computational Science and Engineering, LLC, Chicago, IL; S. Gorrell, M. Jones, Brigham Young University, Provo, UT; et al. Chaired by: S. SPEER, Northrop Grumman Corporation 0900 hrs 0930 hrs AIAA-2015-3410 AIAA-2015-3411 EPIC - An Extract Plug-In Dynamic Mode Decomposition Components Toolkit for In-Situ Data of Backward Facing Step Flow Extracts Architecture Simulation Data Friday, 26 June 2015 302-CFD-32 N. Taylor, MBDA, Bristol, United Kingdom Chaired by: S. IMLAY, Tecplot, Inc 0900 hrs AIAA-2015-3408 Industrial Perspectives on Geometry Handling for Aerodynamics Friday, 26 June 2015 301-CFD-31 D. Gonzalez, Naval Surface Warfare Center, Indian Head, MD; D. Gaitonde, Ohio State University, Columbus, OH; M. Lewis, Science and Technology Policy Institute, Washington, DC 1000 hrs AIAA-2015-3415 Finite-Time Lyapunov Exponent Analysis of Intermittent Acoustic Events in a Round Jet A. Mohan, L. Agostini, D. Gaitonde, Ohio State University, Columbus, OH; D. Garmann, Air Force Research Laboratory, Wright-Patterson AFB, OH 1000 hrs AIAA-2015-3412 Statistical Analysis and Model Reduction of Surface Pressure for Interaction of a StreamwiseOriented Vortex with a Wing Z. Wei tao, China Gas Turbine Establishment, Chengdu, China Interdisciplinary CFD II 1030 hrs AIAA-2015-3416 Numerical Simulation of the Interaction between Rim Seal and Main Annulus Flow in a Four Stage Low-Pressure Axial Turbine Z. Wang, Nanjing University of Aeronautics and Astronautics, Nanjing, China 1100 hrs AIAA-2015-3417 Calculation of Airfoil Anti-icing Heat Load in SLD Conditions Post-Processing and Model Reduction 1030 hrs Panel Panel: The Path to CFD Visualization in 2030 Moderator: Scott Imlay, Tecplot, Inc 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 1000 hrs AIAA-2015-3409 The Path to and State of Geometry and Meshing in 2030: Panel Summary Visualization for CFD 2030 Plum Blossom A Grand Ballroom B Grand Ballroom A 120 H. Yang, CFD Research Corporation, Huntsville, AL Toronto, Canada; J. McDonald, University of Ottawa, Ottawa, Canada; C. Groth, University of Toronto, Toronto, Canada N. Foster, Pennsylvania State University, State College, PA Center, Moffett Field, CA University, Reykjavik, Iceland; L. Leifsson, J. Thomas, E. Dowell, Duke University, Iowa State University, Ames, IA Durham, NC Ann Arbor, MI Chaired by: B. ROTH, Walla Walla Univ and S. CHOI, Virginia Polytechnic Institute and State University 0930 hrs 1000 hrs 0900 hrs AIAA-2015-3435 AIAA-2015-3436 AIAA-2015-3434 Discrete Adjoint Design Aerodynamic Shape Optimization Adjoint-Enhanced Multi-Level Optimization Approach for of a Truss-Braced-Wing Aircraft Optimization: Investigation of Increasing Transonic Buffet Onset D. Ivaldi, N. Secco, S. Chen, J. Hwang, J. Algorithm Parameter Settings Martins, University of Michigan, Ann Arbor, Y. Tesfahunegn, S. Koziel, Reykjavik Angle-of-Attack Friday, 26 June 2015 307-MAO-12 B. Mattos, A. Paula, P. Komatsu, Technological Institute of Aeronautics (ITA), São José dos Campos, Brazil 1030 hrs AIAA-2015-3437 Considerations about Wintip Devices Design of Transport Airplane Shape and Topology III M. Fuchs, Technical University of Berlin, Berlin, Germany; C. Mockett, CFD Software GmbH, Berlin, Germany; J. Sesterhenn, F. Thiele, Technical University of Berlin, Berlin, Germany 1030 hrs AIAA-2015-3433 Assessment of novel DES approach with enhanced SGS modelling for prediction of separated flow over a delta wing B. Thornber, University of Sydney, Sydney, of North Carolina, Charlotte, Charlotte, NC Laboratory, Wright-Patterson AFB, OH Australia LES, DNS, and Hybrid RANS-LES IV Chaired by: J. POGGIE, USAF AFRL/RBAC and B. THORNBER, The University of Sydney 0900 hrs 0930 hrs 1000 hrs AIAA-2015-3430 AIAA-2015-3431 AIAA-2015-3432 Impact of Computational Direct Numerical Simulation of Supersonic Corner Flow Predictions Domain Size in Simulations of Turbulent Flow Around a Surface using the Quadratic Constitutive Homogeneous Decaying Turbulence Mounted Cube Relation A. Curley, M. Uddin, B. Peters, University T. Leger, J. Poggie, Air Force Research and Mixing Layers M. Ghoreyshi, R. Korkis-Kanaan, A. Jirasek, A. Lofthouse, R. Cummings, U.S. Air Force Academy, Colorado Springs, CO Friday, 26 June 2015 306-CFD-36 C. Liu, J. Newman, W. Anderson, University of Tennessse, Chattanooga, Chattanooga, TN B. Yagiz, G. Guzel, I. Koc, ASELSAN, Inc., Ankara, Turkey 1100 hrs AIAA-2015-3422 Simulation of the Separated flow over a Wall-Mounted Hump using Finite-Volume Based Lattice Boltzmann Method L. Schneiders, C. Guenther, J. Grimmen, M. Meinke, W. Schroeder, RWTH Aachen University, Aachen, Germany 1100 hrs AIAA-2015-3427 Sharp resolution of complex moving geometries using a multicut-cell viscous flow solver Overset and Cartesian Grid Methods A. Hay, S. Etienne, D. Pelletier, École Polytechnique de Montréal, Montréal, Canada 1030 hrs AIAA-2015-3421 An ALE/FE formulation for high precision interface tracking in separated multiphase flows Multiphase and Nonequilibrium Flows 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 AIAA-2015-3423 AIAA-2015-3424 AIAA-2015-3425 AIAA-2015-3426 Three-Dimensional Dynamic Accuracy of High-Order CFD and Advances in Distance-Based Hole Simulation Validation of Static and Overset Method for Stabilized Overset Interpolation in Finite Cuts on Overset Grids Forced Motion Flow Physics of a W. Chan, S. Pandya, NASA Ames Research Canard Configured TransCruiser Finite Elements Volume/Difference Codes Friday, 26 June 2015 305-CFD-35 Michigan, Ann Arbor, Ann Arbor, MI Chaired by: C. TSAI, Lockheed Martin Space Systems and R. AGARWAL, Washington University in St Louis 0900 hrs 0930 hrs 1000 hrs AIAA-2015-3418 AIAA-2015-3419 AIAA-2015-3420 Numerical simulation of a scramjet A Multiphase and Multiphysics CFD Application of a Maximum-EntropyTechnique for Fuel Spurt Prediction Based 14-Moment Closure for Multiisolator with thermodynamic with Cavitation and Fluid-Structure Dimensional Non-Equilibrium Flows nonequilibrium R. Fiévet, H. Koo, V. Raman, University of Interaction B. Tensuda, University of Toronto, Friday, 26 June 2015 304-CFD-34 A. Kanoria, Indian Institute of Technology Gandhinagar, Gandhinagar, India; D. Chandar, Institute of High Performance Computing, Singapore, Singapore 1130 hrs AIAA-2015-3428 Integrating the Stanford University Unstructured Code (SU2) With Overset Grids Madrid Emerald D. Hamane, O. Guerri, Renewable Energy Development Center Algeria, Bouzareah, Algeria; S. Larbi, Polytechnical School of Algiers, Elharache, Algeria Plum Blossom B 1200 hrs AIAA-2015-3429 A Comparative Study of Flow around a Circular Cylinder using Lattice Boltzmann Method Coral 121 A. Wendorff, J. Alonso, Stanford University, Stanford, CA; S. Bieniawski, The Boeing Company, Seattle, WA A. da Silva, R., 9-AFM-2 Abdelhady, M., 43-AFM-3 Abdellatif, O., 178-MST-8 Abdol-Hamid, K., 160-APA-17, 233-APA-25 Abdrashitov, R., 226-AA-31 Abdul-Latif, A., 12-APA-1 Abe, M., 23-CFD-3 Abe, T., 144-PDL-7 Abe, Y., 130-CFD-13 Acar, E., 64-MAO-2 Acar, P., 308-MAO-13 Adams, N., 87-APA-9 Adler, M., 245-CFD-30 Adusumilli, S., 159-AMT-10/GT-10 Afsar, M., 79-AA-13, 209-FD-24 Agarwal, N., 226-AA-31 Agarwal, R., 26-FD-2, 47-APA-5, 122-APA-13, 139-FD-18, 182-TP-9, 211-FD-26, 304-CFD-34 Agbolosu-Amison, S., 197-ATIO-18 Agostini, L., 80-AA-14, 302-CFD-32 Ahmad, N., 163-ASE-1, 237-ASE-3, 272-ASE-4, 298-ATIO-27 Ahmed, N., 115-AA-19 Ahsan, N., 136-FD-15 Ahuja, K., 189-AA-30, 261-AA-39 Ahuja, V., 127-ATIO-13, 161-APA-18 Aigner, M., 185-AA-26 Friday, 26 June 2015 309-NW-10 0900 - 0930 hrs 1030 hrs AIAA-2015-3441 Multidisciplinary Uncertainty Quantification in Aeroelastic Analyses of Semi-Span Supersonic Transport Wing Uncertainty II Airiau, C., 5-AA-3 Akaydin, H., 49-APA-7 Akbarzadeh, S., 131-CFD-14 Akella, M., 9-AFM-2 Akhtar, I., 133-CFD-16, 136-FD-15 Akilli, H., 25-FD-1 Akins, D., 279-FD-31 Alaoui, M., 226-AA-31 Alazard, D., 83-AFM-5 Alba, C., 34-TP-1 Albring, T., 252-MAO-9, 283-MAO-10 Albuquerque, P., 104-MAO-3 Alcabin, M., 275-ATIO-25 Alcorn, J., 250-LTA-1 Aleksentsev, A., 189-AA-30 Alessandro, T., 108-TP-5 Alexander, W., 37-AA-6, 38-AA-7, 114-AA-18, 152-AA-22, 187-AA-28, 260-AA-38, 261-AA-39 Alexeenko, A., 35-TP-2, 288-TP-13 Alexeev, T., 9-AFM-2, 105-MST-5 Alfonso, X., 234-APA-26 Algozino, S., 236-APA-28 Aliaga, C., 196-ASE-2 Alizard, F., 98-CFD-12 Allen, B., 165-ATIO-16, 199-ATIO-20 Allen, C., 64-MAO-2, 125-APA-16, 283-MAO-10 Allen, J., 104-MAO-3 Anderson, J., 231-AA-36 Anderson, W., 95-CFD-9, 170-CFD-18, 305-CFD-35 Andre, F., 65-MST-3 Andrews, S., 141-MAO-4, 267-APA-29 Andrienko, D., 69-TP-4, 256-TP-12 Anemaat, W., 117-ACD-3, 232-ACD-6 Angland, D., 205-CFD-25, 259-AA-37, 263-AA-41 Ansaldi, T., 5-AA-3 Anthony, J., 278-FD-30 Antônio dos Santos, D., 30-MST-1 Antony, T., 44-AFM-4 Anupindi, K., 171-CFD-19 Aoki, T., 68-TP-3 Aoki, Y., 89-APA-11 Aono, H., 268-APA-30 Aponso, B., 91-ATIO-9 Appel, C., 226-AA-31 Appelbaum, J., 259-AA-37 Aradag, S., 204-CFD-24 Arena, A., 157-AFM-9 Arina, R., 155-AA-25 Arnal, D., 99-FD-10 Arndt, C., 266-AMT-13/GT-13 Arneson, H., 18-ATIO-3, 298-ATIO-27 Arora, N., 97-CFD-11, 248-FD-29, 268-APA-30 Arsenyev, I., 284-MAO-11 Arunajatesan, S., 139-FD-18, 175-FD-22, 229-AA-34 Meeting Room Foyers Manchester Asada, K., 60-FD-6/PDL-2 Asano, K., 60-FD-6/PDL-2 Ashley, A., 176-MAO-5 Ashton, N., 172-CFD-20, 230-AA-35 Astley, R., 78-AA-12 Atassi, H., 77-AA-11, 151-AA-21 Atinault, O., 13-APA-2 Atkins, E., 274-ATIO-24 Atkins, S., 140-ITAR-2 Attanasio, L., 13-APA-2, 104-MAO-3 Aubert, A., 40-AA-9 Aubry, S., 42-ACD-1, 299-ATIO-28 Avery, A., 196-ASE-2 Awasthi, M., 261-AA-39 Ayton, L., 260-AA-38 Ayyad, E., 31-MST-2 Ayyalasomayajula, S., 284-MAO-11, 300-ATIO-29 Azarm, S., 29-MAO-1 Azarpeyvand, M., 3-AA-1, 38-AA-7 Azevedo, J., 12-APA-1, 98-CFD-12, 241-CFD-26, 270-APA-32 Babbar, Y., 9-AFM-2, 124-APA-15, 270-APA-32 Baccala, L., 7-AA-5 Badrinath, S., 136-FD-15 Baeder, J., 162-APA-19, 171-CFD-19 Baginski, F., 200-BAL-2 Bagwell, T., 140-ITAR-2 1130 hrs AIAA-2015-3443 A Strategy for Probabilistic Margin Allocation in Aircraft Conceptual Design T. Zang, Zang M&S Consulting, LLC, Zebulon, NC; S. Mahadevan, Vanderbilt University, Nashville, TN; J. Tai, D. J. Gramatyka, M. Eres, J. Scanlan, University of Southampton, Southampton, Mavris, Georgia Institute of Technology, United Kingdom; M. Moss, R. Bates, Rolls- Atlanta, GA Royce Group plc, Derby, United Kingdom 1100 hrs AIAA-2015-3442 An Integrated Framework for Bayesian Uncertainty Quantification and Probabilistic Multi-Criteria Decision Making in Aero-Engine Preliminary Design Allen, N., 45-AMT-3/GT-3 Allerdice, J., 197-ATIO-18 Allison, D., 104-MAO-3 Allmaras, S., 95-CFD-9, 123-APA-14, 170-CFD-18 Almeida, F., 249-FT-1 Almond, M., 88-APA-10 Alonso, E., 126-ATIO-12 Alonso, J., 202-CFD-22, 204-CFD-24, 212-MAO-6, 283-MAO-10, 284-MAO-11, 308-MAO-13 Alonso-Miralles, J., 260-AA-38 AlQadi, I., 236-APA-28 Alter, S., 233-APA-25 Altmikus, A., 88-APA-10 Alunni, A., 216-TP-10/PDL-10 Alves, L., 243-CFD-28 Aly, A., 178-MST-8 Alyanak, E., 104-MAO-3, 176-MAO-5 Alzamora Previtali, F., 102-FD-13 Amadori, K., 283-MAO-10 Amaral, F., 230-AA-35 Amili, O., 153-AA-23 Amitay, M., 63-FD-9, 101-FD-12, 248-FD-29 Amos, D., 35-TP-2 Amundson, I., 128-ATIO-14 Ananda Krishnan, G., 15-APA-4 Andalibi, M., 48-APA-6 Anders, S., 49-APA-7, 281-GEPC-1 Author/Session Chair Index Networking Coffee Break M. Nikbay, P. Acar, Istanbul Technical Consulting, LLC, Zebulon, NC; D. Mavris, J. Tai, University, Istanbul, Turkey Georgia Institute of Technology, Atlanta, GA Chaired by: S. CHOWDHURY, Mississippi State University and S. FERGUSON, North Carolina State University 0900 hrs 0930 hrs 1000 hrs AIAA-2015-3438 AIAA-2015-3439 AIAA-2015-3440 Sculpting: A Fast, Interactive Method Multi-Objective Optimization Under A Multi-Fidelity Approach to Quantification of Uncertainty in for Probabilistic Design Space Uncertainty C. Liang, S. Mahadevan, Vanderbilt Stability and Control Databases Exploration and Margin Allocation University, Nashville, TN R. Cooke, Resources for the Future, for use in Stochastic Aircraft Washington, DC; T. Zang, Zang M&S Simulations Friday, 26 June 2015 308-MAO-13 122 Bahr, C., 186-AA-27, 188-AA-29, 262-AA-40 Bai, B., 112-AA-16 Bai, J., 49-APA-7, 145-TP-7 Bailly, C., 4-AA-2, 114-AA-18, 231-AA-36 Bailly, D., 161-APA-18 Bake, F., 41-AA-10, 151-AA-21 Bakker, B., 238-ATIO-21 Balakumar, P., 61-FD-7, 139-FD-18, 248-FD-29 Balan, A., 95-CFD-9 Balaresque, N., 88-APA-10 Balas, G., 157-AFM-9 Balboni, J., 108-TP-5, 216-TP-10/PDL-10 Baldacchino, D., 279-FD-31 Ballard, B., 275-ATIO-25 Bane, S., 255-PDL-12 Bangert, L., 14-APA-3 Barbarino, M., 6-AA-4, 115-AA-19 Barbeau, Z., 274-ATIO-24 Barmore, B., 298-ATIO-27 Barnes, C., 270-APA-32 Barnes, J., 83-AFM-5 Bartels, R., 124-APA-15 Bartoli, N., 82-ACD-2 Bartosch, S., 299-ATIO-28 Bastide, M., 45-AMT-3/GT-3 Basto, K., 234-APA-26 Bates, R., 308-MAO-13 Bathel, B., 86-AMT-6/GT-6, 121-AMT-8/FD-14/TP-6/GT-8 Batista, M., 30-MST-1 Batten, P., 245-CFD-30 Bauer, M., 125-APA-16 Bauman, P., 108-TP-5 Baumgärtner, D., 283-MAO-10 Baydar, E., 279-FD-31 Bayoda, K., 33-PDL-1/FD-5 Beaverstock, C., 29-MAO-1 Beck, J., 35-TP-2 Bedouet, J., 299-ATIO-28 Bekiropoulos, D., 155-AA-25 Bellemans, A., 216-TP-10/PDL-10 Belley, C., 204-CFD-24 Belmouss, M., 255-PDL-12 Belyaev, I., 115-AA-19, 187-AA-28, 189-AA-30 Benard, N., 33-PDL-1/FD-5, 180-PDL-8/APA-20 Bender, J., 256-TP-12 Bennaceur, I., 154-AA-24 Benton, S., 50-APA-8 Berci, M., 236-APA-28 Berdanier, R., 173-FD-19 Beresh, S., 62-FD-8, 175-FD-22, 192-AMT-12/GT-12, 266-AMT-13/GT-13 Bergeron, K., 236-APA-28 Bering, E., 200-BAL-2 Bériot, H., 263-AA-41 Berkefeld, T., 186-AA-27, 260-AA-38 Bernardini, G., 162-APA-19, 263-AA-41 Bernardo, J., 52-ATIO-6, 198-ATIO-19 Berner, C., 47-APA-5 Berry, P., 283-MAO-10 Berry, S., 217-TP-11 Bersenev, Y., 189-AA-30 Berton, J., 77-AA-11 Beulze, B., 92-ATIO-10 Beuze, B., 18-ATIO-3 Bevan, R., 125-APA-16 Bevirt, J., 276-ATIO-26 Bhagat, N., 104-MAO-3 Bhagwandin, V., 267-APA-29 Bhamidipati, K., 22-CFD-2 Bhaumik, S., 205-CFD-25 Bianchi, D., 128-ATIO-14 Bibik, P., 280-FT-2/GT-14 Bidino, D., 45-AMT-3/GT-3 Bienert, N., 51-ATIO-5 Bieniawski, S., 308-MAO-13 Bieniek, D., 237-ASE-3 Bier, N., 105-MST-5 Bijl, H., 97-CFD-11 Bil, C., 42-ACD-1, 117-ACD-3, 190-ACD-5 Bilimoria, K., 177-MST-7 Bin Abdul Malik, M., 162-APA-19 Bisek, N., 98-CFD-12, 143-PDL-6, 245-CFD-30 Blackwell, B., 68-TP-3 Blair, L., 143-PDL-6 Blaisdell, G., 113-AA-17, 139-FD-18, 245-CFD-30 Blake, M., 142-MST-6 Blake, W., 8-AFM-1, 29-MAO-1, 273-ASE-5 Blandeau, V., 77-AA-11 Bleischwitz, R., 136-FD-15 Bletzinger, K., 283-MAO-10 Bloebaum, C., 212-MAO-6 Blom, H., 238-ATIO-21 Bo, Y., 35-TP-2, 145-TP-7 Bobenrieth Miserda, R., 77-AA-11 Bocola, F., 84-AFM-6 Boden, F., 231-AA-36 Boden, H., 7-AA-5, 261-AA-39 Bogdanoff, D., 182-TP-9 Bogey, C., 4-AA-2, 5-AA-3, 229-AA-34 Boissonneau, F., 189-AA-30 Bolczak, C., 299-ATIO-28 Bolds-Moorehead, P., 249-FT-1 Bolender, M., 44-AFM-4 Bombelli, A., 275-ATIO-25 Bonnet, J., 180-PDL-8/APA-20 Bons, J., 50-APA-8 Boo, K., 12-APA-1 Boom, P., 132-CFD-15 Bordeneuve, J., 83-AFM-5 Borer, N., 127-ATIO-13 Borg, M., 137-FD-16 Borges Sebastiao, I., 288-TP-13 Borgoltz, A., 295-APA-34, 297-APA-37 Borner, A., 288-TP-13 Bosson, C., 16-ATIO-1 Botez, R., 13-APA-2, 18-ATIO-3, 66-MST-4, 84-AFM-6, 92-ATIO-10, 238-ATIO-21, 296-APA-35 Bouhaj, M., 226-AA-31 Bouley, S., 152-AA-22 Bousfield, S., 127-ATIO-13 Boussuge, J., 188-AA-29 Bouty, E., 185-AA-26 Bouvy, Q., 259-AA-37 Bova, S., 202-CFD-22 Bowers, L., 166-ATIO-17, 239-ATIO-22 Bown, A., 167-BAL-1 Boxx, I., 266-AMT-13/GT-13 Boyd, I., 35-TP-2, 69-TP-4, 256-TP-12 Brakke, K., 200-BAL-2 Brambley, E., 7-AA-5, 81-AA-15 Brandis, A., 69-TP-4, 217-TP-11 Brandon, J., 118-AFM-7, 249-FT-1 Brandt, S., 64-MAO-2 Brauckmann, G., 233-APA-25 Braud, P., 189-AA-30 Brazier, J., 228-AA-33 Breard, C., 4-AA-2, 6-AA-4 Brehm, C., 4-AA-2 Breitsamter, C., 87-APA-9 Brès, G., 5-AA-3, 80-AA-14 Breviglieri, C., 241-CFD-26 Brichet, G., 4-AA-2 Bridges, J., 189-AA-30, 227-AA-32 Briley, W., 15-APA-4, 297-APA-37 Britchford, K., 227-AA-32 Broeren, A., 196-ASE-2 Bronz, M., 161-APA-18 Broszat, D., 151-AA-21 Brown, C., 189-AA-30, 228-AA-33, 280-FT-2/GT-14 Brown, K., 297-APA-37 Brown, L., 158-AMT-9/GT-9 Brown, M., 143-PDL-6, 214-MST-9 Brown, R., 9-AFM-2 Brunet, M., 42-ACD-1 Bryan, B., 261-AA-39 Author/Session Chair Index Buehn, J., 303-CFD-33 Bugeda, G., 180-PDL-8/APA-20 Bulte, J., 3-AA-1, 261-AA-39, 262-AA-40 Bunge, R., 8-AFM-1, 249-FT-1 Buning, P., 230-AA-35 Buono, A., 37-AA-6 Burns, R., 86-AMT-6/GT-6 Burnside, N., 186-AA-27 Burt, J., 69-TP-4, 181-PDL-9/TP-8 Burtch, T., 8-AFM-1 Busch, G., 37-AA-6 Busquets, J., 126-ATIO-12 Buttini, T., 9-AFM-2 Byerley, A., 15-APA-4 Bynum, M., 99-FD-10 Cai, J., 67-PDL-3, 178-MST-8 Cai, W., 145-TP-7 Cain, A., 88-APA-10, 143-PDL-6, 255-PDL-12 Caldas, L., 7-AA-5 Callahan, R., 294-AMT-14/GT-15 Callender, M., 62-FD-8 Callicoat, J., 231-AA-36 Calvert, M., 15-APA-4, 194-APA-22 Calvert, N., 86-AMT-6/GT-6 Campbell, S., 16-ATIO-1, 298-ATIO-27 Candler, G., 139-FD-18, 202-CFD-22, 244-CFD-29, 246-FD-27, 256-TP-12, 278-FD-30 Canfield, R., 252-MAO-9 Canpolat, C., 25-FD-1 Cantu, L., 86-AMT-6/GT-6 Capittini, G., 236-APA-28 Capizzano, F., 6-AA-4, 115-AA-19 Caprecci, M., 5-AA-3 Caraballo, E., 175-FD-22 Caraeni, M., 39-AA-8 Cardito, F., 162-APA-19 Cariou, J., 272-ASE-4 Carlson, J., 58-CFD-8, 133-CFD-16 Carmine, M., 26-FD-2 Caro, S., 6-AA-4, 113-AA-17 Carolus, T., 152-AA-22 Carranza Moyao, O., 84-AFM-6 Carroll, D., 107-PDL-4, 166-ATIO-17 Carson, H., 170-CFD-18 Carter, C., 266-AMT-13/GT-13 Cartmell, D., 31-MST-2 Caruelle, B., 155-AA-25 Casalino, D., 188-AA-29, 259-AA-37 Casalis, G., 228-AA-33 Casartelli, E., 203-CFD-23 Casper, K., 28-FD-4, 103-ITAR-1, 140-ITAR-2, 175-FD-22 Castner, R., 14-APA-3 Cathey, H., 167-BAL-1 Catlett, M., 231-AA-36 Cattafesta, L., 248-FD-29 Caudle, D., 83-AFM-5 Cavalieri, A., 5-AA-3, 41-AA-10, 80-AA-14, 189-AA-30, 260-AA-38 Cedric, C., 132-CFD-15 Cerminara, A., 209-FD-24 Cesnik, C., 9-AFM-2, 119-AFM-8 Cetin, M., 80-AA-14 Chabot, J., 175-FD-22 Chaderjian, N., 136-FD-15 Chakraborty, I., 42-ACD-1, 156-ACD-4, 265-ACD-7 Chakraborty, P., 246-FD-27 Chakravarthy, S., 245-CFD-30 Chalot, F., 99-FD-10 Chan, W., 305-CFD-35 Chandar, D., 305-CFD-35 Chaney, V., 249-FT-1 Chang, C., 193-APA-21, 211-FD-26, 228-AA-33 Chang, S., 35-TP-2, 145-TP-7 Chao, H., 43-AFM-3 Chao, T., 119-AFM-8 Chaput, A., 82-ACD-2, 128-ATIO-14 Chard, J., 271-APA-33 Charnigo, R., 181-PDL-9/TP-8 Chatterji, G., 142-MST-6, 253-MST-11 Chauvin, A., 227-AA-32 Chawner, J., 301-CFD-31 Chazot, O., 108-TP-5 Chedevergne, F., 60-FD-6/PDL-2 Cheli, R., 26-FD-2 Chelius, A., 187-AA-28 Chelliah, K., 262-AA-40 Chen, G., 301-CFD-31 Chen, L., 191-AMT-11/GT-11, 250-LTA-1 Chen, N., 92-ATIO-10, 191-AMT-11/GT-11 Chen, P., 284-MAO-11 Chen, S., 269-APA-31, 307-MAO-12 Chen, W., 107-PDL-4, 151-AA-21, 260-AA-38 Chen, X., 112-AA-16, 145-TP-7 Chen, Y., 34-TP-1 Cheng, G., 193-APA-21, 211-FD-26 Cheng, H., 229-AA-34 Cheng, J., 122-APA-13 Cheng, Y., 215-MST-10 Chernyshev, S., 228-AA-33 Chevalley, E., 51-ATIO-5 Chhabra, R., 29-MAO-1 Chiba, K., 293-ACD-8 Chiereghin, N., 270-APA-32 123 Chintagunta, A., 80-AA-14 Chng, S., 162-APA-19 Chng, T., 143-PDL-6 Cho, K., 235-APA-27 Choi, J., 27-FD-3, 55-CFD-5, 62-FD-8, 132-CFD-15, 133-CFD-16, 251-MAO-8, 296-APA-35 Choi, S., 12-APA-1, 64-MAO-2, 89-APA-11, 132-CFD-15, 251-MAO-8, 296-APA-35, 307-MAO-12 Chong, T., 3-AA-1 Chou, A., 209-FD-24 Choudhari, M., 56-CFD-6, 99-FD-10, 137-FD-16, 155-AA-25, 230-AA-35 Choudhary, A., 97-CFD-11 Choutapalli, I., 276-ATIO-26 Chowdhary, G., 274-ATIO-24 Chowdhury, S., 176-MAO-5, 213-MAO-7, 251-MAO-8, 308-MAO-13 Christophe, J., 79-AA-13, 112-AA-16 Chua, Z., 65-MST-3 Chudoba, B., 53-ATIO-7 Chue, R., 269-APA-31 Chwalowski, P., 124-APA-15 Chynoweth, B., 28-FD-4 Ciarella, A., 29-MAO-1 Ciliberti, D., 13-APA-2 Cinnella, P., 62-FD-8, 113-AA-17, 132-CFD-15 Ciobaca, V., 125-APA-16 Cisneros, E., 216-TP-10/PDL-10 Cisotto, A., 46-AMT-4/GT-4 Civinskas, K., 281-GEPC-1 Clair, V., 6-AA-4, 113-AA-17 Clark, A., 276-ATIO-26 Clark, I., 38-AA-7 Clarke, S., 240-ATIO-23 Clemens, N., 33-PDL-1/FD-5, 174-FD-20 Cléro, F., 185-AA-26 Cliff, S., 89-APA-11 Clingman, D., 63-FD-9 Close, S., 286-PDL-13 Cloutier, R., 239-ATIO-22 Cluts, J., 153-AA-23 Coakley, T., 172-CFD-20 Cobb, P., 142-MST-6 Cobb, R., 141-MAO-4, 158-AMT-9/GT-9 Coder, J., 58-CFD-8, 61-FD-7 Coen, P., 281-GEPC-1 Coetzee, E., 105-MST-5 Cofer, A., 35-TP-2 Coggon, S., 213-MAO-7 Cohen, E., 226-AA-31 Colantonio, R., 281-GEPC-1 Colburn, K., 301-CFD-31 Cole, S., 45-AMT-3/GT-3 Collery, O., 226-AA-31 Collins, E., 41-AA-10, 81-AA-15 Colmenares, J., 96-CFD-10, 205-CFD-25 Coloe, B., 274-ATIO-24 Colonius, T., 5-AA-3, 80-AA-14, 228-AA-33 Colonno, M., 212-MAO-6 Commo, S., 120-AMT-7/GT-7, 294-AMT-14/GT-15 Communier, D., 84-AFM-6 Constantinescu, E., 163-ASE-1 Cooke, R., 308-MAO-13 Coppenbarger, R., 91-ATIO-9 Cordes, U., 50-APA-8, 271-APA-33 Coreixas, C., 188-AA-29 Correale, G., 33-PDL-1/FD-5, 60-FD-6/PDL-2 Correia Grácio, B., 31-MST-2 Corrigan, A., 153-AA-23 Costes, M., 161-APA-18 Cotton, W., 275-ATIO-25 Coulouvrat, F., 114-AA-18 Coupe, J., 91-ATIO-9, 198-ATIO-19 Coupland, J., 78-AA-12, 264-AA-42 Courty, J., 99-FD-10 Cousy, M., 65-MST-3 Coyle, C., 90-APA-12, 195-APA-23 Cozzi, F., 26-FD-2 Craig, S., 137-FD-16 Cranford, J., 30-MST-1 Crawford, B., 137-FD-16 Crawley, M., 153-AA-23 Cromer, K., 282-LTA-2 Cross, C., 165-ATIO-16, 199-ATIO-20 Crossley, W., 52-ATIO-6, 82-ACD-2 Crouch, J., 61-FD-7 Crow, B., 197-ATIO-18 Crowther, W., 30-MST-1, 271-APA-33 Cruden, B., 69-TP-4, 182-TP-9, 217-TP-11 Cruz, E., 63-FD-9 Cuenca, R., 7-AA-5 Cui, D., 178-MST-8 Cui, H., 44-AFM-4 Cui, K., 296-APA-35 Culbreth, W., 31-MST-2 Cummings, R., 63-FD-9, 160-APA-17, 236-APA-28, 278-FD-30, 305-CFD-35 Cunha, G., 155-AA-25 Cunha, M., 282-LTA-2 Cuoci, A., 244-CFD-29 Curley, A., 306-CFD-36 Curran, R., 51-ATIO-5, 91-ATIO-9, 198-ATIO-19, 275-ATIO-25 Cusati, V., 13-APA-2 Cutler, A., 86-AMT-6/GT-6, 121-AMT-8/FD-14/TP-6/GT-8 Cymbalist, N., 27-FD-3, 278-FD-30 D’Souza, S., 43-AFM-3 Da Ronch, A., 9-AFM-2, 84-AFM-6 da Silva, A., 4-AA-2 da Silva, F., 4-AA-2 Dahl, D., 39-AA-8 Dahl, M., 78-AA-12 Dale, G., 26-FD-2, 210-FD-25 Dalle, D., 233-APA-25 Daly, C., 38-AA-7 Damodaran, M., 205-CFD-25, 235-APA-27, 250-LTA-1 Dancila, B., 92-ATIO-10 Dancila, R., 18-ATIO-3 Danehy, P., 86-AMT-6/GT-6, 121-AMT-8/FD-14/TP-6/GT-8 Daniels, C., 273-ASE-5 Dannenhoffer, J., 301-CFD-31 Dantsker, O., 87-APA-9 Daoud, F., 212-MAO-6 Darmofal, D., 95-CFD-9, 170-CFD-18 Daskiran, O., 128-ATIO-14 Davidson, L., 6-AA-4, 115-AA-19, 154-AA-24 Daviller, G., 229-AA-34 Davis, D., 85-AMT-5/GT-5 Davis, R., 203-CFD-23 Davy, R., 3-AA-1, 262-AA-40 Dawson, R., 174-FD-20 Dawson, S., 136-FD-15 De Breuker, R., 29-MAO-1 de Jong, A., 38-AA-7 De Kat, R., 136-FD-15 De La Puente, F., 259-AA-37 De Marco, A., 8-AFM-1, 104-MAO-3 de Monte, F., 35-TP-2 de Oliveira, G., 286-PDL-13 De Roeck, W., 113-AA-17 de Santana, L., 3-AA-1 de Souza, F., 192-AMT-12/GT-12 DeArmon, J., 197-ATIO-18 DeBonis, J., 55-CFD-5, 130-CFD-13, 175-FD-22 DeChant, L., 139-FD-18 DeCicco, A., 65-MST-3, 142-MST-6 Decker, R., 278-FD-30 Dedic, C., 181-PDL-9/TP-8 Dees, J., 173-FD-19 Deese, J., 282-LTA-2 DeGennaro, A., 295-APA-34 Degrez, G., 216-TP-10/PDL-10 Deinert, S., 212-MAO-6 Del Rey Fernández, D., 169-CFD-17, 242-CFD-27 Author/Session Chair Index Del Rosario, R., 281-GEPC-1 DeLaurentis, D., 52-ATIO-6, 239-ATIO-22, 300-ATIO-29 Deleglise, B., 46-AMT-4/GT-4 Delfs, J., 79-AA-13, 112-AA-16, 230-AA-35, 231-AA-36, 263-AA-41 Delisi, D., 237-ASE-3, 272-ASE-4 Dell’Orso, H., 101-FD-12, 248-FD-29 Della Vecchia, P., 8-AFM-1, 13-APA-2 Dellery, B., 167-BAL-1 Delnero, J., 236-APA-28 Demauro, E., 101-FD-12 Demeautis, C., 45-AMT-3/GT-3 Demers, F., 60-FD-6/PDL-2 Demers Bouchard, E., 276-ATIO-26 Deng, S., 97-CFD-11 Deniau, H., 229-AA-34 Denieul, Y., 83-AFM-5 Denison, M., 248-FD-29 Denisov, S., 115-AA-19 Denissen, K., 195-APA-23 Dennis, B., 48-APA-6 Deodhar, N., 282-LTA-2 Derlaga, J., 97-CFD-11 Deschamps, C., 4-AA-2, 80-AA-14 Desmet, W., 3-AA-1, 113-AA-17 Deters, R., 15-APA-4 Devenport, W., 37-AA-6, 38-AA-7, 114-AA-18, 152-AA-22, 187-AA-28, 260-AA-38, 261-AA-39, 295-APA-34, 297-APA-37 Dewey, R., 167-BAL-1 Dey, S., 301-CFD-31 Dhaene, T., 66-MST-4 Dhamankar, N., 245-CFD-30 Dias, B., 34-TP-1 Dias, J., 118-AFM-7 Dickey, D., 189-AA-30 Dickey, E., 49-APA-7, 87-APA-9 Dief, T., 43-AFM-3 Dierke, J., 39-AA-8, 185-AA-26, 263-AA-41 DiGirolamo, E., 265-ACD-7 Dilan, G., 285-MST-12 Dill, E., 166-ATIO-17 Dimotakis, P., 27-FD-3, 139-FD-18, 244-CFD-29, 278-FD-30 Diosady, L., 21-CFD-1, 201-CFD-21 Dirk, B., 230-AA-35 Djeddi, R., 243-CFD-28 Dogan, A., 8-AFM-1, 83-AFM-5, 128-ATIO-14, 273-ASE-5 Dogariu, A., 86-AMT-6/GT-6 Dolfi-Bouteyre, A., 272-ASE-4 Donadon, M., 260-AA-38 Dong, H., 136-FD-15, 248-FD-29 Dong, M., 99-FD-10 Dong, X., 84-AFM-6 Dongre, R., 250-LTA-1 Doolan, C., 115-AA-19, 152-AA-22, 231-AA-36 Doty, M., 158-AMT-9/GT-9 Dougherty, N., 68-TP-3, 228-AA-33 Douville, T., 180-PDL-8/APA-20, 269-APA-31 Dowell, E., 307-MAO-12 Dowling, D., 211-FD-26 Downing, J., 40-AA-9 Doyle, J., 90-APA-12 Draper, M., 274-ATIO-24 Drew, M., 126-ATIO-12 Driver, D., 108-TP-5 Drozda, T., 244-CFD-29 Dryer, J., 281-GEPC-1 Duan, D., 250-LTA-1 Duan, F., 47-APA-5 Duan, L., 137-FD-16, 205-CFD-25 Duan, Z., 23-CFD-3, 56-CFD-6 Dubot, T., 299-ATIO-28 Dubourg, V., 167-BAL-1 Dubov, Y., 31-MST-2 Ducruix, S., 185-AA-26 Duda, B., 188-AA-29 Duddeck, F., 284-MAO-11 Duffy, M., 194-APA-22 Dumitrache, C., 107-PDL-4, 143-PDL-6 Duncan, G., 137-FD-16 Duncan, M., 85-AMT-5/GT-5 Dunlap, P., 273-ASE-5 Dunn, S., 45-AMT-3/GT-3, 191-AMT-11/GT-11 Dunne, R., 162-APA-19 Duque, E., 301-CFD-31, 302-CFD-32 Duraisamy, K., 58-CFD-8 Durak, U., 177-MST-7 Durand, C., 154-AA-24 Dutta, S., 44-AFM-4 Dzikus, N., 239-ATIO-22, 299-ATIO-28 Echekki, T., 185-AA-26 Economon, T., 133-CFD-16, 204-CFD-24, 212-MAO-6, 271-APA-33, 283-MAO-10 Edgington-Mitchell, D., 153-AA-23 Edoh, A., 132-CFD-15 Edwards, D., 48-APA-6 Edwards, J., 203-CFD-23 Edwards, M., 86-AMT-6/GT-6 Efraimsson, G., 78-AA-12, 235-APA-27 Egorov, I., 99-FD-10 Ehrenfried, K., 260-AA-38 Eisfeld, B., 172-CFD-20 Eitelberg, G., 37-AA-6, 269-APA-31 124 Ekaterin, J., 56-CFD-6 Ekici, K., 243-CFD-28 Ekmekci, A., 259-AA-37 Ekoule, C., 37-AA-6 El baialy, I., 178-MST-8 Elham, A., 64-MAO-2 Eliasson, P., 160-APA-17 Eljack, E., 236-APA-28 Ellejmi, M., 91-ATIO-9 Elmiligui, A., 160-APA-17, 285-MST-12 Empl, D., 53-ATIO-7 Enghardt, L., 151-AA-21, 152-AA-22, 173-FD-19 Enjiao, Z., 119-AFM-8 Entz, R., 104-MAO-3 Envia, E., 264-AA-42 Eppink, J., 137-FD-16 Eres, M., 128-ATIO-14, 308-MAO-13 Eriksson, L., 6-AA-4, 154-AA-24 Ernst, D., 186-AA-27 Errico, A., 164-ATIO-15 Erturk, S., 83-AFM-5 Escobar, J., 234-APA-26 Esker, B., 281-GEPC-1 Etchessahar, M., 226-AA-31 Etienne, S., 304-CFD-34 Evans, A., 126-ATIO-12 Evans, M., 244-CFD-29 Eversman, W., 7-AA-5 Ewert, R., 38-AA-7, 39-AA-8, 41-AA-10, 79-AA-13, 112-AA-16, 155-AA-25, 185-AA-26, 230-AA-35 Eyi, S., 57-CFD-7, 131-CFD-14, 244-CFD-29 Eymann, T., 174-FD-20 Fagan, A., 189-AA-30 Fagley, C., 12-APA-1, 125-APA-16 Fairbrother, D., 167-BAL-1, 200-BAL-2 Fala, N., 156-ACD-4 Falcão, C., 243-CFD-28 Falissard, F., 154-AA-24 Fan, D., 56-CFD-6 Fan, H., 165-ATIO-16, 199-ATIO-20 Fan, Y., 180-PDL-8/APA-20 Faranosov, G., 115-AA-19, 189-AA-30, 228-AA-33 Fares, E., 188-AA-29 Farnsworth, J., 162-APA-19 Farr, R., 228-AA-33 Farrington, A., 202-CFD-22 Fasel, H., 28-FD-4, 100-FD-11, 102-FD-13, 208-FD-23 Fassmann, B., 79-AA-13 Fattah, R., 113-AA-17, 263-AA-41 Fedorov, A., 99-FD-10 Fehlman, W., 165-ATIO-16, 199-ATIO-20 Fehrenbach, S., 274-ATIO-24 Felder, W., 239-ATIO-22 Feldhusen, A., 41-AA-10 Felipe, V., 16-ATIO-1 Félix Patrón, R., 18-ATIO-3 Feltrop, E., 270-APA-32 Feng, F., 80-AA-14 Fenouil, J., 295-APA-34 Ferguson, S., 64-MAO-2, 104-MAO-3, 308-MAO-13 Fermen-Coker, M., 119-AFM-8 Fern, L., 274-ATIO-24 Fernandes de Oliveira, R., 104-MAO-3 Fernando, A., 229-AA-34 Fernando, R., 187-AA-28 Ferrari, D., 117-ACD-3, 213-MAO-7 Ferreira de Castro, D., 30-MST-1 Fidkowski, K., 95-CFD-9, 170-CFD-18 Field, J., 31-MST-2 Fields, T., 157-AFM-9 Fiévet, R., 304-CFD-34 Filippone, E., 164-ATIO-15, 300-ATIO-29 Filizola, A., 65-MST-3 Findanis, N., 125-APA-16 Finley, D., 47-APA-5, 161-APA-18 Fiore, G., 297-APA-37 Firsov, A., 107-PDL-4 Fischels, M., 243-CFD-28 Fischer, P., 202-CFD-22 Fischersworring-Bunk, A., 284-MAO-11 Fisher, T., 145-TP-7, 202-CFD-22 Flatau, A., 50-APA-8 Fletcher, D., 181-PDL-9/TP-8 Fleury, V., 3-AA-1, 262-AA-40 Florez Mera, J., 35-TP-2 Foster, J., 157-AFM-9 Foster, N., 305-CFD-35 Foster, T., 240-ATIO-23 Fouladi, H., 196-ASE-2 François, B., 152-AA-22 Franke, D., 13-APA-2 Frankhouser, M., 33-PDL-1/FD-5 Franko, K., 202-CFD-22 Frassoldati, A., 244-CFD-29 Frazza, L., 58-CFD-8 Fredericks, W., 19-ATIO-4, 127-ATIO-13 Freret, L., 97-CFD-11 Fresconi, F., 90-APA-12, 119-AFM-8 Freund, J., 78-AA-12 Frew, E., 157-AFM-9, 273-ASE-5 Friedman, A., 176-MAO-5, 296-APA-35 Friedman, C., 236-APA-28 Frischemeier, S., 117-ACD-3 Fuchs, M., 306-CFD-36 Fucke, L., 31-MST-2 Fujii, K., 60-FD-6/PDL-2, 114-AA-18, 130-CFD-13, 169-CFD-17 Fujino, T., 286-PDL-13 Fujita, K., 68-TP-3, 69-TP-4 Fujiwara, G., 49-APA-7 Fuller, C., 226-AA-31 Funk, C., 124-APA-15 Furukawa, D., 89-APA-11 Gabard, G., 6-AA-4, 78-AA-12, 113-AA-17, 263-AA-41 Gabbert, D., 48-APA-6 Gaddai, A., 203-CFD-23 Gaeta, R., 37-AA-6, 231-AA-36 Gaitonde, D., 80-AA-14, 174-FD-20, 205-CFD-25, 245-CFD-30, 266-AMT-13/GT-13, 302-CFD-32, 303-CFD-33 Galbraith, M., 170-CFD-18 Gallman, J., 79-AA-13 Gallo, E., 86-AMT-6/GT-6 Galyen, N., 11-AMT-2/GT-2 Gamba, M., 102-FD-13 Gambardella, D., 104-MAO-3 Gamblin, R., 200-BAL-2 Gamboa, P., 43-AFM-3, 104-MAO-3 Gan, J., 90-APA-12 Ganapathisubramani, B., 3-AA-1, 38-AA-7, 136-FD-15 Gao, D., 107-PDL-4 Gao, Z., 161-APA-18, 213-MAO-7 Garcia, D., 282-LTA-2 Garcia, E., 239-ATIO-22 Gargiulo, F., 164-ATIO-15 Garland, M., 142-MST-6 Garman, K., 249-FT-1 Garmann, D., 208-FD-23, 302-CFD-32 Garrard, G., 120-AMT-7/GT-7 Garrett, S., 98-CFD-12, 209-FD-24 Garrick, D., 243-CFD-28 Gartner, J., 63-FD-9 Gary, J., 167-BAL-1 Gasbarri, P., 119-AFM-8 Gatian, K., 52-ATIO-6 Gatlin, G., 88-APA-10 Gauger, N., 79-AA-13, 252-MAO-9, 283-MAO-10 Gauthier, T., 47-APA-5 Gautier, M., 238-ATIO-21 Gea-Aguilera, F., 112-AA-16 Gebreegziabher, A., 42-ACD-1 Geder, J., 48-APA-6, 233-APA-25 Gee, K., 40-AA-9 Geisbauer, S., 105-MST-5, 195-APA-23 Geisler, R., 159-AMT-10/GT-10 Gemma, S., 29-MAO-1 Author/Session Chair Index Gennaretti, M., 162-APA-19, 263-AA-41 George, J., 11-AMT-2/GT-2, 50-APA-8 Georgiadis, N., 175-FD-22 Gerber, T., 167-BAL-1 Gerlach, T., 177-MST-7 German, B., 93-ATIO-11, 127-ATIO-13 Gern, F., 82-ACD-2 Gerz, T., 196-ASE-2 Getsinger, D., 173-FD-19 Geuther, S., 164-ATIO-15 Geyer, T., 231-AA-36 Gezer, R., 83-AFM-5 Gherman, G., 96-CFD-10 Ghorawat, P., 84-AFM-6 Ghorbaniasl, G., 152-AA-22 Ghoreyshi, M., 236-APA-28, 305-CFD-35 Ghosh, A., 118-AFM-7 Ghosh, D., 163-ASE-1 Ghosh, S., 125-APA-16, 213-MAO-7 Giauque, A., 185-AA-26 Giepman, R., 138-FD-17 Gil Prieto, D., 270-APA-32 Gildersleeve, S., 101-FD-12 Giles, M., 200-BAL-2 Gilge, P., 235-APA-27 Gill, J., 112-AA-16, 113-AA-17, 152-AA-22, 260-AA-38 Gillespie, E., 8-AFM-1 Gilliam, F., 64-MAO-2 Gilmore, B., 104-MAO-3 Ginn, S., 240-ATIO-23 Giret, J., 188-AA-29 Girimaji, S., 58-CFD-8 Glaab, P., 142-MST-6 Glass, C., 233-APA-25 Glegg, S., 37-AA-6, 38-AA-7, 77-AA-11, 114-AA-18, 187-AA-28, 261-AA-39 Gloerfelt, X., 56-CFD-6, 62-FD-8, 113-AA-17 , 154-AA-24, 226-AA-31 Gloudemans, J., 82-ACD-2 Gnoffo, P., 132-CFD-15 Goblet, V., 156-ACD-4 Góes, L., 30-MST-1, 282-LTA-2 Gogineni, S., 266-AMT-13/GT-13 Gojon, R., 4-AA-2 Gokcen, T., 34-TP-1, 108-TP-5, 216-TP-10/PDL-10 Golaszewski, R., 275-ATIO-25 Goldberg, U., 245-CFD-30 Goldsmith, B., 276-ATIO-26 Goldstein, D., 288-TP-13 Goli, N., 265-ACD-7 Golubev, A., 226-AA-31 Golubev, V., 79-AA-13 Gonda, J., 239-ATIO-22 Gong, C., 252-MAO-9, 298-ATIO-27 Gonzalez, D., 303-CFD-33 Gonzalez, L., 101-FD-12 Gonzalez-Linero, L., 190-ACD-5 Goodrich, K., 93-ATIO-11, 199-ATIO-20 Gopalarathnam, A., 235-APA-27, 267-APA-29 Goparaju, K., 205-CFD-25 Gordeyev, S., 88-APA-10, 143-PDL-6, 255-PDL-12 Gordnier, R., 62-FD-8, 208-FD-23 Gorham, P., 200-BAL-2 Gori, G., 133-CFD-16, 196-ASE-2 Gori, R., 162-APA-19 Gorrell, S., 302-CFD-32 Gorton, S., 281-GEPC-1 Gourinat, Y., 82-ACD-2 Govindarajan, R., 28-FD-4 Govindaraju, P., 82-ACD-2 Goyal, T., 234-APA-26 Goyne, C., 159-AMT-10/GT-10 Grabe, C., 61-FD-7 Grace, S., 264-AA-42 Graham, R., 51-ATIO-5 Gramatyka, J., 308-MAO-13 Granlund, K., 63-FD-9, 175-FD-22 Grant, J., 37-AA-6 Grant, M., 44-AFM-4, 83-AFM-5 Grasso, F., 98-CFD-12 Grasso, G., 112-AA-16 Graube, P., 108-TP-5 Grauer, J., 118-AFM-7 Green, C., 240-ATIO-23 Green, M., 26-FD-2 Greenblatt, D., 101-FD-12, 158-AMT-9/GT-9, 208-FD-23 Greendyke, R., 34-TP-1 Greene, B., 33-PDL-1/FD-5 Greene, G., 237-ASE-3 Greene, K., 43-AFM-3 Gregory, J., 33-PDL-1/FD-5, 268-APA-30 Grenon, R., 13-APA-2 Griffiths, P., 209-FD-24 Grimm, F., 185-AA-26 Grimmen, J., 305-CFD-35 Grimsley, J., 140-ITAR-2 Grinstead, J., 69-TP-4 Grivel, A., 46-AMT-4/GT-4 Gross, A., 208-FD-23 Gross, R., 99-FD-10 Groth, C., 97-CFD-11, 171-CFD-19, 304-CFD-34 Ground, C., 86-AMT-6/GT-6 Grund, T., 125-APA-16 Gu, L., 252-MAO-9 125 Gu, Q., 265-ACD-7 Gu, Y., 43-AFM-3 Guan, Y., 38-AA-7 Guardone, A., 26-FD-2, 133-CFD-16, 196-ASE-2 Guenther, C., 305-CFD-35 Guerin, S., 41-AA-10, 77-AA-11 Guerreiro, N., 17-ATIO-2 Guerri, O., 305-CFD-35 Guglielmo, J., 235-APA-27 Guminsky, M., 142-MST-6, 299-ATIO-28 Guo, C., 84-AFM-6 Guo, J., 164-ATIO-15 Guo, Y., 112-AA-16, 116-AA-20 Gupta, A., 97-CFD-11, 268-APA-30 Gupta, M., 38-AA-7 Gupte, A., 57-CFD-7 Gursul, I., 25-FD-1, 138-FD-17 Gutmark, E., 153-AA-23 Guynn, M., 293-ACD-8 Guyton, R., 85-AMT-5/GT-5 Guzel, G., 304-CFD-34 Habashi, W., 196-ASE-2 Habbit, R., 96-CFD-10 Haeri, S., 261-AA-39 Hafez, M., 105-MST-5, 278-FD-30 Haga, T., 130-CFD-13 Hagen, G., 17-ATIO-2 Hahn, M., 29-MAO-1 Haimes, R., 302-CFD-32 Hainaut, T., 6-AA-4 Haji-Sheikh, A., 35-TP-2 Hajian, R., 25-FD-1 Hajj, M., 236-APA-28 Hale, L., 30-MST-1 Hall, D., 64-MAO-2 Hall, J., 283-MAO-10 Hallock, J., 237-ASE-3 Halls, B., 86-AMT-6/GT-6 Ham, F., 202-CFD-22 Hamane, D., 305-CFD-35 Hamiche, K., 263-AA-41 Hammack, S., 107-PDL-4 Hammock, G., 158-AMT-9/GT-9, 191-AMT-11/GT-11 Han, K., 198-ATIO-19 Han, X., 144-PDL-7 Hannemann, K., 302-CFD-32 Hanquist, K., 35-TP-2 Hanses, C., 51-ATIO-5 Hansman, R., 156-ACD-4 Harada, N., 181-PDL-9/TP-8 Hariharan, N., 122-APA-13 Harik, R., 64-MAO-2 Harker, B., 40-AA-9 Harrington, A., 136-FD-15 Harris, R., 41-AA-10, 81-AA-15, 195-APA-23, 241-CFD-26 Harrison, E., 156-ACD-4 Harshe, S., 235-APA-27 Hartfield, R., 127-ATIO-13, 161-APA-18 Hartwich, P., 87-APA-9, 133-CFD-16 Hasan, S., 65-MST-3, 142-MST-6, 197-ATIO-18, 275-ATIO-25 Hash, D., 288-TP-13 Hashemi, A., 68-TP-3 Hashemi, K., 9-AFM-2 Haskin, H., 158-AMT-9/GT-9 Hasnain, Z., 12-APA-1, 50-APA-8 Hassan, M., 37-AA-6, 42-ACD-1, 53-ATIO-7, 239-ATIO-22 Hassan, W., 15-APA-4 Hathaway, J., 196-ASE-2 Hattenberger, G., 161-APA-18 Haxter, S., 260-AA-38 Hay, A., 58-CFD-8, 204-CFD-24, 304-CFD-34 Hayashibara, S., 27-FD-3 Hayden, T., 88-APA-10, 143-PDL-6, 255-PDL-12 Hays, T., 157-AFM-9 Haywood, J., 24-CFD-4 Hazir, A., 188-AA-29 He, A., 272-ASE-4 He, C., 280-FT-2/GT-14 Hebert, P., 85-AMT-5/GT-5 Hedrick, T., 100-FD-11 Heeg, J., 124-APA-15 Heffernon, T., 259-AA-37 Hegde, A., 174-FD-20 Hegen, S., 13-APA-2 Heineck, J., 192-AMT-12/GT-12 Heinrich, R., 57-CFD-7 Heiser, W., 15-APA-4 Heitmeir, F., 151-AA-21 Helber, B., 108-TP-5 Helm, S., 91-ATIO-9 Hempley, L., 165-ATIO-16, 199-ATIO-20 Henderson, B., 227-AA-32 Henderson, R., 137-FD-16 Henfling, J., 62-FD-8, 175-FD-22 Henry de Frahan, M., 201-CFD-21 Herbst, S., 88-APA-10, 253-MST-11 Hereth, L., 15-APA-4 Herold, G., 186-AA-27, 231-AA-36 Herr, M., 115-AA-19, 155-AA-25, 226-AA-31, 230-AA-35 Herrema, F., 51-ATIO-5 Herring, A., 158-AMT-9/GT-9 Herrmann, J., 29-MAO-1 Herron, A., 262-AA-40 Herzog, S., 252-MAO-9 Hess, C., 11-AMT-2/GT-2 Hickel, S., 87-APA-9 Hicken, J., 176-MAO-5, 212-MAO-6, 242-CFD-27, 251-MAO-8 Hiepler, `., 302-CFD-32 Higdon, K., 288-TP-13 High, J., 165-ATIO-16 Higuera Caubilla, D., 58-CFD-8 Hildebrand, N., 4-AA-2 Hiner, W., 79-AA-13 Hinze, N., 300-ATIO-29 Hipp, K., 50-APA-8 Hiramoto, R., 293-ACD-8 Hirayama, T., 66-MST-4 Hitzel, S., 160-APA-17 Hixon, D., 6-AA-4, 78-AA-12, 81-AA-15, 154-AA-24, 229-AA-34 Hoelling, M., 50-APA-8 Hoffler, K., 43-AFM-3 Hoffman, R., 142-MST-6 Hoffmann, K., 175-FD-22 Höger, M., 151-AA-21 Holladay, W., 85-AMT-5/GT-5 Holland, K., 186-AA-27 Holland, M., 117-ACD-3 Hölling, M., 271-APA-33 Hollingsworth, P., 30-MST-1, 53-ATIO-7 Holst, T., 136-FD-15 Holzäpfel, F., 196-ASE-2, 237-ASE-3 Hong, S., 51-ATIO-5, 166-ATIO-17 Hong, Z., 107-PDL-4 Honnery, D., 153-AA-23 Hoogreef, M., 42-ACD-1, 176-MAO-5 Hopf, J., 191-AMT-11/GT-11 Horchler, T., 302-CFD-32 Horio, B., 65-MST-3, 142-MST-6 Horkheimer, D., 282-LTA-2 Horn, J., 43-AFM-3, 83-AFM-5 Horne, W., 186-AA-27, 262-AA-40 Hornung, M., 88-APA-10, 91-ATIO-9, 253-MST-11 Hosangadi, P., 235-APA-27 Hosder, S., 58-CFD-8 Hosseinverdi, S., 100-FD-11 Housman, J., 4-AA-2, 14-APA-3, 49-APA-7 Howard, M., 68-TP-3 Howerton, B., 7-AA-5, 116-AA-20 Hu, F., 229-AA-34 Hu, H., 180-PDL-8/APA-20 Hu, J., 171-CFD-19 Hu, Y., 208-FD-23 Hu, Z., 22-CFD-2, 205-CFD-25 Author/Session Chair Index Hua, J., 35-TP-2 Huang, G., 159-AMT-10/GT-10, 162-APA-19, 267-APA-29, 270-APA-32 Huang, X., 7-AA-5, 26-FD-2, 78-AA-12, 113-AA-17 Huang, Z., 99-FD-10 Hubbard, E., 191-AMT-11/GT-11 Hubbard, J., 12-APA-1, 50-APA-8 Huber, J., 189-AA-30 Hue, D., 13-APA-2 Huehne, C., 125-APA-16 Huet, M., 185-AA-26 Huff, B., 128-ATIO-14 Hufnagel, K., 271-APA-33 Hug, S., 24-CFD-4 Hughes, M., 196-ASE-2 Hui, F., 108-TP-5 Hulshoff, S., 33-PDL-1/FD-5 Hultgren, L., 151-AA-21 Humpert, B., 37-AA-6 Humphreys, C., 141-MAO-4 Humphreys, W., 188-AA-29 Hur, J., 124-APA-15 Hussein, A., 236-APA-28 Hussein, S., 246-FD-27 Hutcheson, F., 4-AA-2, 158-AMT-9/GT-9 Huynh, H., 55-CFD-5, 130-CFD-13, 170-CFD-18, 242-CFD-27 Hwang, I., 31-MST-2, 126-ATIO-12 Hwang, J., 29-MAO-1, 307-MAO-12 Idier, A., 3-AA-1 Idris, H., 16-ATIO-1, 275-ATIO-25 Ihme, M., 151-AA-21, 242-CFD-27 Ikeda, T., 155-AA-25 Im, D., 12-APA-1, 132-CFD-15 Imamura, T., 155-AA-25, 241-CFD-26 Imlay, S., 301-CFD-31 Ims, J., 23-CFD-3 Imtiaz, H., 133-CFD-16 Ingraham, D., 6-AA-4 Ioppolo, T., 46-AMT-4/GT-4 Iorio, M., 101-FD-12 Ishida, Y., 68-TP-3 Ishioka, H., 270-APA-32 Ishutkina, M., 298-ATIO-27 Isikveren, A., 53-ATIO-7 Itasse, M., 228-AA-33 Ito, H., 23-CFD-3 Ito, K., 66-MST-4 Ito, Y., 230-AA-35 Ivaldi, D., 307-MAO-12 Ivanov, V., 243-CFD-28 Iwakawa, A., 89-APA-11, 138-FD-17 Jack, D., 43-AFM-3 Jackson, G., 145-TP-7 Jackson, R., 138-FD-17 Jackson, T., 203-CFD-23 Jacob, D., 237-ASE-3, 272-ASE-4 Jacob, J., 37-AA-6, 48-APA-6, 140-ITAR-2, 196-ASE-2, 231-AA-36, 274-ATIO-24, 280-FT-2/GT-14 Jacobi, R., 100-FD-11 Jacobs, S., 107-PDL-4 Jacques, D., 141-MAO-4 Jaffrezic, B., 178-MST-8 Jain, N., 171-CFD-19 Jalali, A., 21-CFD-1 Jambunathan, R., 203-CFD-23 James, M., 40-AA-9 Jameson, A., 55-CFD-5, 123-APA-14, 132-CFD-15, 271-APA-33 Janjic, Z., 163-ASE-1 Jann, T., 105-MST-5 Jaouani, N., 187-AA-28 Jaron, R., 77-AA-11 Jarzembski, A., 250-LTA-1 Jastrzebski, M., 17-ATIO-2 Jaunet, V., 80-AA-14, 189-AA-30 Jaworski, J., 25-FD-1, 38-AA-7 Jenkins, L., 188-AA-29, 192-AMT-12/GT-12 Jenkins, T., 11-AMT-2/GT-2, 159-AMT-10/GT-10 Jensen, L., 156-ACD-4 Jessberger, C., 52-ATIO-6 Jesus, A., 98-CFD-12 Jewell, J., 28-FD-4 Ji, C., 116-AA-20 Ji, L., 151-AA-21 Jianchun, X., 215-MST-10 Jiang, C., 180-PDL-8/APA-20 Jiang, H., 78-AA-12 Jiang, N., 86-AMT-6/GT-6 Jiang, Z., 22-CFD-2 Jiao, J., 263-AA-41 Jie, B., 253-MST-11 Jimenez, H., 52-ATIO-6, 156-ACD-4, 293-ACD-8 Jin, J., 85-AMT-5/GT-5 Jin, W., 85-AMT-5/GT-5 Jing, C., 252-MAO-9 Jinwu, X., 214-MST-9 Jirasek, A., 160-APA-17, 305-CFD-35 Jo, Y., 251-MAO-8 Johansen, C., 121-AMT-8/FD-14/TP-6/GT-8, 159-AMT-10/GT-10 Johnsen, E., 201-CFD-21, 211-FD-26 Johnson, H., 103-ITAR-1 Johnson, S., 43-AFM-3, 214-MST-9 126 Johnston, C., 69-TP-4, 217-TP-11 Jolly, B., 23-CFD-3, 136-FD-15, 241-CFD-26 Jondeau, E., 231-AA-36 Jones, A., 268-APA-30 Jones, G., 294-AMT-14/GT-15 Jones, J., 228-AA-33 Jones, M., 7-AA-5, 26-FD-2, 116-AA-20, 262-AA-40, 302-CFD-32 Jones, S., 86-AMT-6/GT-6 Jones, W., 301-CFD-31 Joo, J., 191-AMT-11/GT-11 Jordan, P., 5-AA-3, 80-AA-14, 189-AA-30 Jorris, T., 249-FT-1 Joseph, L., 295-APA-34 Joseph, P., 3-AA-1, 7-AA-5, 38-AA-7, 79-AA-13, 152-AA-22, 261-AA-39 Jost, A., 203-CFD-23 Josyula, E., 69-TP-4 Joyce, R., 31-MST-2 Juliano, T., 10-AMT-1/GT-1, 137-FD-16 Jumper, E., 88-APA-10, 143-PDL-6, 255-PDL-12 June, J., 262-AA-40 Jung, K., 235-APA-27 Jung, S., 166-ATIO-17 Jung, T., 64-MAO-2 Jung, Y., 16-ATIO-1, 91-ATIO-9, 198-ATIO-19, 298-ATIO-27 Junkui, M., 45-AMT-3/GT-3, 285-MST-12 Junqueira-Junior, C., 270-APA-32 Jurkovich, M., 193-APA-21, 269-APA-31 Justin, C., 190-ACD-5 Juve, D., 189-AA-30, 231-AA-36 Kaddouh, B., 30-MST-1 Kailasanath, K., 153-AA-23 Kalivarapu, V., 29-MAO-1, 104-MAO-3, 283-MAO-10 Kalkhoran, I., 233-APA-25 Kalyan, A., 228-AA-33 Kamali, S., 122-APA-13 Kamat, S., 293-ACD-8 Kamle, S., 234-APA-26 Kammeyer, M., 294-AMT-14/GT-15 Kampers, G., 50-APA-8, 271-APA-33 Kamruzzaman, M., 155-AA-25 Kang, H., 162-APA-19 Kanistras, K., 88-APA-10 Kannan, H., 212-MAO-6 Kanoria, A., 250-LTA-1, 305-CFD-35 Kapania, R., 29-MAO-1 Kara, K., 13-APA-2, 50-APA-8, 236-APA-28 Karabasov, S., 5-AA-3, 6-AA-4, 80-AA-14, 228-AA-33 Karahan, S., 294-AMT-14/GT-15 Karakoc, T., 273-ASE-5 Karakoç, N., 273-ASE-5 Karlgaard, C., 44-AFM-4 Karon, A., 189-AA-30 Kartha, A., 244-CFD-29 Kase, S., 293-ACD-8 Kasprzyk, M., 280-FT-2/GT-14 Kato, H., 60-FD-6/PDL-2, 192-AMT-12/GT-12 Katsurayama, H., 286-PDL-13 Katz, A., 21-CFD-1, 243-CFD-28 Katz, J., 88-APA-10 Kaul, U., 25-FD-1, 49-APA-7, 279-FD-31 Kausche, P., 152-AA-22 Kaya, D., 118-AFM-7 Ke, G., 261-AA-39 Kegerise, M., 99-FD-10 Keller, D., 87-APA-9 Keller, E., 83-AFM-5 Kelly, M., 269-APA-31 Kennedy, G., 212-MAO-6 Kenway, G., 141-MAO-4 Kerho, M., 235-APA-27 Kessler, R., 22-CFD-2, 96-CFD-10 Key, N., 158-AMT-9/GT-9, 173-FD-19 Keye, S., 87-APA-9 Khalid, M., 136-FD-15 Khalil, E., 145-TP-7, 178-MST-8 Khamis, D., 7-AA-5 Khan, S., 66-MST-4 Khire, R., 141-MAO-4 Khodadoust, A., 202-CFD-22 Khoo, B., 235-APA-27 Khorrami, M., 155-AA-25, 188-AA-29, 259-AA-37 Kidd, F., 143-PDL-6 Kim, C., 242-CFD-27 Kim, E., 51-ATIO-5 Kim, H., 88-APA-10 Kim, J., 3-AA-1, 46-AMT-4/GT-4, 151-AA-21, 261-AA-39 Kim, K., 126-ATIO-12 Kim, T., 46-AMT-4/GT-4 Kim, V., 141-MAO-4 Kim, Y., 142-MST-6 Kimmel, R., 28-FD-4, 102-FD-13, 103-ITAR-1 King, L., 161-APA-18 King, R., 99-FD-10, 137-FD-16 King, W., 250-LTA-1 Kingan, M., 5-AA-3, 37-AA-6 Kings, N., 41-AA-10, 151-AA-21 Kio, M., 35-TP-2 Kirby, A., 201-CFD-21 Kirby, M., 198-ATIO-19 Kiris, C., 4-AA-2, 14-APA-3 Kirk, C., 159-AMT-10/GT-10 Kirk, L., 69-TP-4 Kiyici, F., 204-CFD-24 Klabes, A., 226-AA-31 Kleb, W., 58-CFD-8, 233-APA-25 Kleinclaus, C., 259-AA-37 Kleine, H., 102-FD-13 Klentzman, J., 99-FD-10 Kline, H., 204-CFD-24 Kling, U., 53-ATIO-7 Klock, R., 119-AFM-8 Kloker, M., 209-FD-24 Knabe, F., 51-ATIO-5 Knobloch, K., 151-AA-21 Knowles, J., 105-MST-5 Koc, I., 304-CFD-34 Koch, J., 236-APA-28 Koch, M., 238-ATIO-21 Kocian, T., 137-FD-16 Kodama, H., 152-AA-22 Koenig, M., 4-AA-2 Koerner, S., 237-ASE-3 Koh, S., 38-AA-7, 41-AA-10, 79-AA-13, 80-AA-14 Koike, S., 192-AMT-12/GT-12 Koizumi, H., 23-CFD-3 Kok, F., 27-FD-3, 175-FD-22 Kokaly, M., 178-MST-8 Koklu, M., 63-FD-9 Kolonay, R., 29-MAO-1, 252-MAO-9, 284-MAO-11 Komatsu, P., 307-MAO-12 Kong, W., 295-APA-34 Konnemann, E., 275-ATIO-25 Kontis, K., 193-APA-21 Koo, H., 304-CFD-34 Kopiev, V., 187-AA-28, 189-AA-30, 228-AA-33 Kopyt, A., 30-MST-1 Koreanschi, A., 13-APA-2, 296-APA-35 Korkis-Kanaan, R., 305-CFD-35 Korn, B., 51-ATIO-5 Korolev, Y., 5-AA-3, 251-MAO-8 Kostiuk, P., 142-MST-6 Köthe, T., 252-MAO-9 Kotikalpudi, A., 157-AFM-9 Kotov, D., 24-CFD-4 Kotov, M., 193-APA-21 Kotsonis, M., 88-APA-10, 286-PDL-13 Koziel, S., 307-MAO-12 Kozlov, A., 77-AA-11 Krakos, J., 23-CFD-3 Krausman, J., 282-LTA-2 Kraut, J., 51-ATIO-5 Kreitzman, J., 153-AA-23 Kreuz, M., 164-ATIO-15 Author/Session Chair Index Krimmelbein, N., 61-FD-7 Krishna, Y., 11-AMT-2/GT-2 Krishnamoorthy, S., 286-PDL-13 Krishnamurthy, R., 272-ASE-4 Kroeber, S., 260-AA-38 Kronhaus, I., 144-PDL-7 Kroninger, C., 136-FD-15 Kroo, I., 8-AFM-1, 249-FT-1 Krozel, J., 142-MST-6 Krueger, P., 62-FD-8 Krueger, W., 198-ATIO-19 Krüger, W., 57-CFD-7, 105-MST-5 Krumbein, A., 61-FD-7 Krumme, A., 13-APA-2 Krus, P., 283-MAO-10 Kryukov, I., 193-APA-21 Kucukcoskun, K., 79-AA-13 Kügler, M., 128-ATIO-14 Kuhn, T., 88-APA-10 Kulkarni, M., 252-MAO-9 Kumar, D., 234-APA-26 Kumar, R., 118-AFM-7, 174-FD-20 Kumar, S., 234-APA-26 Kumar, V., 65-MST-3, 142-MST-6 Kuntz, D., 34-TP-1 Kunz, D., 43-AFM-3 Kuo, C., 153-AA-23 Kurelek, J., 100-FD-11 Kurtz, J., 46-AMT-4/GT-4 Kurz, H., 209-FD-24 Kutay, A., 66-MST-4, 83-AFM-5, 118-AFM-7, 294-AMT-14/GT-15 Kutz, D., 158-AMT-9/GT-9 Kwon, O., 133-CFD-16 La Rocca, G., 176-MAO-5 Lacaze, G., 244-CFD-29 Lachenmeier, T., 167-BAL-1 Lachowski, F., 37-AA-6 Lacor, C., 152-AA-22 Lacy, D., 87-APA-9 Lafage, R., 42-ACD-1 Laffay, P., 3-AA-1 Lafferty, J., 103-ITAR-1 Lai, D., 237-ASE-3, 272-ASE-4 Lajús, F., 5-AA-3, 80-AA-14 Lam, T., 217-TP-11 Lambert, A., 100-FD-11 Lammel, O., 266-AMT-13/GT-13 Lampinen, M., 139-FD-18 Lancaster, J., 158-AMT-9/GT-9 Landman, D., 294-AMT-14/GT-15 Landrum, B., 30-MST-1, 265-ACD-7 Landrum, D., 250-LTA-1 Landry, R., 215-MST-10 Landry, S., 164-ATIO-15, 166-ATIO-17, 197-ATIO-18 Lang, S., 200-BAL-2 Langtry, R., 61-FD-7 Larbi, S., 305-CFD-35 Larcheveque, L., 154-AA-24 Latz, J., 161-APA-18, 267-APA-29 Laurendeau, F., 60-FD-6/PDL-2 Laval, J., 98-CFD-12 Lavin, T., 119-AFM-8 Lawrence, J., 5-AA-3, 227-AA-32 Lazarus, S., 117-ACD-3 Le Bras, S., 229-AA-34 Le Garrec, T., 187-AA-28 Le Rallic, M., 80-AA-14 Lebofsky, S., 124-APA-15 Lebrun, F., 46-AMT-4/GT-4 Lee, D., 12-APA-1 Lee, H., 16-ATIO-1 Lee, K., 51-ATIO-5, 84-AFM-6, 162-APA-19, 166-ATIO-17 Lee, S., 154-AA-24 Lee, T., 107-PDL-4 Lefantzi, S., 139-FD-18 Leger, T., 306-CFD-36 Leib, S., 79-AA-13, 227-AA-32 Leifsson, L., 307-MAO-12 Lele, S., 80-AA-14 Lemonds, T., 293-ACD-8 Leng, M., 35-TP-2, 145-TP-7 Léon, O., 60-FD-6/PDL-2, 228-AA-33 Leong, C., 63-FD-9, 101-FD-12 Leonov, S., 107-PDL-4, 144-PDL-7 Leopold, F., 45-AMT-3/GT-3 Lesieutre, D., 269-APA-31 Letrenne, G., 167-BAL-1 Leung, R., 38-AA-7 Levin, D., 69-TP-4, 203-CFD-23 LeVine, M., 42-ACD-1, 52-ATIO-6, 198-ATIO-19 Lewis, D., 103-ITAR-1 Lewis, M., 10-AMT-1/GT-1, 303-CFD-33 Lewis, R., 108-TP-5 Lewis, S., 34-TP-1 Lewis, T., 17-ATIO-2 Leyva, I., 27-FD-3 Li, F., 9-AFM-2, 99-FD-10, 137-FD-16 Li, G., 296-APA-35 Li, H., 144-PDL-7, 180-PDL-8/APA-20, 271-APA-33 Li, J., 24-CFD-4, 92-ATIO-10 Li, M., 214-MST-9 Li, S., 26-FD-2, 116-AA-20 Li, V., 29-MAO-1, 176-MAO-5 127 Li, W., 89-APA-11, 241-CFD-26, 261-AA-39 Li, X., 81-AA-15, 112-AA-16, 116-AA-20 Li, Z., 69-TP-4, 178-MST-8 Liang, C., 308-MAO-13 Libsig, M., 47-APA-5 Liburdy, J., 234-APA-26 Liebeck, R., 123-APA-14 Lillard, R., 69-TP-4, 172-CFD-20 Liller, T., 15-APA-4 Lim, C., 265-ACD-7 Lim, D., 42-ACD-1, 190-ACD-5 Limbach, C., 60-FD-6/PDL-2 Lin, H., 265-ACD-7 Lin, J., 138-FD-17, 212-MAO-6 Lin, P., 202-CFD-22 Lin, Q., 241-CFD-26 Lin, Y., 46-AMT-4/GT-4, 65-MST-3, 240-ATIO-23 Lincoln, D., 159-AMT-10/GT-10 Lindsay, K., 238-ATIO-21 Linke, F., 92-ATIO-10 Liou, M., 56-CFD-6 Lippert, M., 88-APA-10 Liston, G., 10-AMT-1/GT-1 Little, J., 60-FD-6/PDL-2, 174-FD-20, 175-FD-22, 279-FD-31 Liu, A., 128-ATIO-14 Liu, C., 305-CFD-35 Liu, D., 85-AMT-5/GT-5 Liu, F., 33-PDL-1/FD-5, 45-AMT-3/GT-3, 67-PDL-3, 144-PDL-7, 180-PDL-8/APA-20, 271-APA-33, 285-MST-12 Liu, G., 248-FD-29 Liu, H., 295-APA-34 Liu, J., 30-MST-1, 84-AFM-6, 153-AA-23, 251-MAO-8 Liu, L., 25-FD-1, 31-MST-2, 213-MAO-7, 251-MAO-8 Liu, P., 26-FD-2, 47-APA-5 Liu, Q., 178-MST-8 Liu, R., 128-ATIO-14 Liu, S., 173-FD-19 Liu, T., 25-FD-1 Liu, X., 3-AA-1, 55-CFD-5, 78-AA-12, 113-AA-17 Liu, Y., 49-APA-7, 185-AA-26, 285-MST-12 Liu, Z., 57-CFD-7, 141-MAO-4 Liv, A., 18-ATIO-3 Livebardon, T., 185-AA-26 Livne, E., 49-APA-7 Llopis-Pascual, A., 271-APA-33 Lo, K., 193-APA-21 Loaec, S., 272-ASE-4 Lobel, G., 227-AA-32 Lockard, D., 3-AA-1, 155-AA-25, 188-AA-29, 230-AA-35, 259-AA-37 Lofthouse, A., 160-APA-17, 236-APA-28, 305-CFD-35 Logan, M., 190-ACD-5 Lohr, G., 91-ATIO-9 Lombardi, A., 213-MAO-7 Long, D., 275-ATIO-25 Long, T., 213-MAO-7, 251-MAO-8 Lopes, L., 112-AA-16, 155-AA-25 López, I., 281-GEPC-1 López-Morales, M., 55-CFD-5 Loseille, A., 23-CFD-3, 114-AA-18 Loth, S., 91-ATIO-9 Lou, F., 158-AMT-9/GT-9 Louman, R., 138-FD-17 Lowe, K., 46-AMT-4/GT-4, 159-AMT-10/GT-10, 192-AMT-12/GT-12, 266-AMT-13/GT-13 Lowenberg, M., 122-APA-13 Lozano, B., 156-ACD-4 Lu, F., 246-FD-27, 279-FD-31 Lu, J., 285-MST-12 Luckner, R., 237-ASE-3 Luckring, J., 160-APA-17 Ludwig, B., 159-AMT-10/GT-10 Luedke, J., 297-APA-37 Lukaczyk, T., 212-MAO-6 Luke, E., 41-AA-10, 81-AA-15, 195-APA-23 Lummer, M., 112-AA-16 Lung, T., 169-CFD-17 Luo, H., 55-CFD-5, 100-FD-11, 173-FD-19, 201-CFD-21, 203-CFD-23, 208-FD-23 Luo, L., 203-CFD-23 Luo, S., 33-PDL-1/FD-5, 67-PDL-3, 144-PDL-7, 180-PDL-8/APA-20, 271-APA-33 Luo, X., 178-MST-8 Lupoglazoff, N., 39-AA-8 Lupp, C., 9-AFM-2 Luquet, D., 114-AA-18 Lutz, A., 181-PDL-9/TP-8 Lutz, T., 249-FT-1 Luxhoj, J., 300-ATIO-29 Lv, Y., 242-CFD-27 Lynch, K., 37-AA-6, 266-AMT-13/GT-13 Lynn, K., 294-AMT-14/GT-15 Lyrintzis, A., 37-AA-6, 113-AA-17, 245-CFD-30 Lyu, B., 38-AA-7 Ma, H., 145-TP-7 Ma, P., 26-FD-2 Ma, Z., 128-ATIO-14 Macheret, S., 216-TP-10/PDL-10 MacManus, D., 270-APA-32 Madavan, N., 281-GEPC-1 Maddalena, L., 86-AMT-6/GT-6 Maddalon, J., 17-ATIO-2 Madden, T., 67-PDL-3 Maeng, J., 169-CFD-17 Magalhaes, P., 283-MAO-10 Magari, P., 33-PDL-1/FD-5 Magin, T., 34-TP-1, 216-TP-10/PDL-10, 217-TP-11 Mahadevan, S., 308-MAO-13 Mahashabde, A., 92-ATIO-10, 197-ATIO-18 Maheshwari, A., 52-ATIO-6 Mahlich, S., 275-ATIO-25 Maierl, R., 212-MAO-6 Majić, F., 78-AA-12, 235-APA-27 Majumdar, A., 198-ATIO-19 Makarov, B., 243-CFD-28 Malael, I., 96-CFD-10 Maldonado, A., 78-AA-12 Malecki, T., 30-MST-1 Malick, M., 122-APA-13 Malik, M., 61-FD-7, 202-CFD-22 Malik, W., 16-ATIO-1, 91-ATIO-9, 198-ATIO-19 Malinowski, M., 280-FT-2/GT-14 Mallet, M., 99-FD-10 Mangalam, A., 9-AFM-2, 124-APA-15, 270-APA-32 Mangani, L., 203-CFD-23 Mani, K., 302-CFD-32 Mankbadi, M., 175-FD-22 Mankbadi, R., 79-AA-13 Manoha, E., 3-AA-1, 155-AA-25, 229-AA-34, 230-AA-35, 259-AA-37 Manosalvas, D., 271-APA-33 Mansor, S., 12-APA-1 Mansour, N., 58-CFD-8, 288-TP-13 Mansouri, N., 81-AA-15 Mantelli, M., 35-TP-2 Marais, K., 156-ACD-4, 164-ATIO-15, 275-ATIO-25, 299-ATIO-28 Marañon Di Leo, J., 236-APA-28 Marchiano, R., 114-AA-18 Marie, S., 56-CFD-6 Marineau, E., 99-FD-10, 103-ITAR-1 Markesteijn, A., 6-AA-4, 80-AA-14 Marks, C., 191-AMT-11/GT-11 Marn, A., 151-AA-21 Marques, F., 236-APA-28 Marr, B., 238-ATIO-21 Marsan, A., 227-AA-32 Marsden, O., 4-AA-2, 231-AA-36 Marsh, J., 200-BAL-2 Marshall, J., 157-AFM-9 Marshall, P., 85-AMT-5/GT-5 Marten, D., 297-APA-37 Martin, A., 68-TP-3, 108-TP-5, 182-TP-9 Martin, P., 120-AMT-7/GT-7 Author/Session Chair Index Martinelli, L., 57-CFD-7, 295-APA-34 Martinez, A., 101-FD-12 Martinez, B., 45-AMT-3/GT-3, 47-APA-5 Martinez, S., 145-TP-7 Martins, J., 29-MAO-1, 141-MAO-4, 252-MAO-9, 307-MAO-12 Mary, I., 154-AA-24 Masarati, P., 84-AFM-6 Mason, M., 217-TP-11 Massa, L., 216-TP-10/PDL-10 Massey, K., 297-APA-37 Mastroddi, F., 29-MAO-1 Masuda, K., 286-PDL-13 Matayoshi, N., 298-ATIO-27 Mather, J., 273-ASE-5 Mathew, J., 24-CFD-4 Mathews, E., 255-PDL-12 Mathews, J., 3-AA-1 Matic, P., 102-FD-13 Matsuno, T., 144-PDL-7 Matsuno, Y., 51-ATIO-5 Mattos, B., 283-MAO-10, 307-MAO-12 Mattson, C., 104-MAO-3 Maughmer, M., 61-FD-7 Mavriplis, D., 201-CFD-21 Mavris, D., 37-AA-6, 42-ACD-1, 52-ATIO-6, 53-ATIO-7, 141-MAO-4, 142-MST-6, 156-ACD-4, 190-ACD-5, 198-ATIO-19, 213-MAO-7, 239-ATIO-22, 265-ACD-7, 276-ATIO-26, 308-MAO-13 May, G., 95-CFD-9 Mayer, R., 92-ATIO-10, 197-ATIO-18 Mazaheri, A., 55-CFD-5 McAlpine, A., 37-AA-6 Mccarthy, P., 145-TP-7 McCarthy, P., 259-AA-37 McClain, S., 196-ASE-2 McClure, J., 132-CFD-15 McColl, C., 83-AFM-5 McComas, A., 235-APA-27 McCrink, M., 268-APA-30 McDaniel, D., 160-APA-17 McDaniel, J., 244-CFD-29 McDonald, J., 304-CFD-34 McDonald, R., 82-ACD-2, 240-ATIO-23 McGrath, B., 123-APA-14 McGuirk, J., 24-CFD-4 McInerny, S., 40-AA-9 Mcintyre, T., 34-TP-1 McKeon, B., 162-APA-19 McKiernan, G., 28-FD-4 McKinley, R., 40-AA-9 McLaughlin, D., 39-AA-8, 40-AA-9 McLaughlin, T., 12-APA-1, 125-APA-16 McMasters, R., 35-TP-2 McMullan, W., 24-CFD-4, 98-CFD-12 Mcnally, D., 298-ATIO-27 McPartland, M., 51-ATIO-5, 298-ATIO-27 McWaters, M., 45-AMT-3/GT-3 Mead, C., 227-AA-32 Mease, K., 275-ATIO-25 Meckstroth, C., 29-MAO-1 Medeiros, F., 243-CFD-28 Medeiros, M., 230-AA-35 Medina, A., 268-APA-30 Medwell, P., 244-CFD-29 Mehmani, A., 251-MAO-8 Mehta, P., 214-MST-9 Mei, D., 180-PDL-8/APA-20 Mei, Q., 253-MST-11 Meier, W., 266-AMT-13/GT-13 Meinke, M., 26-FD-2, 38-AA-7, 41-AA-10, 79-AA-13, 80-AA-14, 229-AA-34, 305-CFD-35 Melin, T., 283-MAO-10 Mendenhall, M., 269-APA-31 Mendonca, F., 230-AA-35 Mendoza, J., 185-AA-26 Meneveau, C., 98-CFD-12, 171-CFD-19 Meng, X., 33-PDL-1/FD-5, 144-PDL-7, 180-PDL-8/APA-20, 271-APA-33 Merle, X., 113-AA-17 Merrick, J., 195-APA-23 Mery, F., 262-AA-40 Mesmer, B., 212-MAO-6, 283-MAO-10 Messac, A., 176-MAO-5, 251-MAO-8 Meyer, T., 181-PDL-9/TP-8 Meyers, J., 181-PDL-9/TP-8 Meyers, T., 152-AA-22, 297-APA-37 Michael, J., 181-PDL-9/TP-8 Michal, T., 23-CFD-3 Michel, U., 189-AA-30 Michou, Y., 46-AMT-4/GT-4, 192-AMT-12/GT-12 Micka, D., 33-PDL-1/FD-5 Mihaescu, M., 96-CFD-10, 112-AA-16 Milagre da Fonseca, I., 119-AFM-8 Milan, P., 60-FD-6/PDL-2 Milanese, F., 35-TP-2 Miles, R., 60-FD-6/PDL-2, 86-AMT-6/GT-6, 143-PDL-6, 255-PDL-12 Miller, B., 52-ATIO-6, 65-MST-3 Miller, D., 142-MST-6, 282-LTA-2 Miller, J., 28-FD-4 Miller, S., 40-AA-9, 153-AA-23 Mills, B., 85-AMT-5/GT-5, 280-FT-2/GT-14 Mills, M., 120-AMT-7/GT-7 128 Milutinovic, D., 91-ATIO-9, 198-ATIO-19 Mimani, A., 231-AA-36 Min, S., 42-ACD-1, 156-ACD-4 Mincu, D., 154-AA-24, 187-AA-28 Mineck, R., 188-AA-29 Mingione, G., 115-AA-19 Minisci, E., 214-MST-9 Minqiang, Y., 280-FT-2/GT-14 Mirochnitchenko, V., 190-ACD-5 Misaka, T., 196-ASE-2 Mitchell, K., 116-AA-20 Mitsingas, C., 107-PDL-4 Mitsuhashi, R., 293-ACD-8 Mittal, A., 15-APA-4, 234-APA-26, 297-APA-37 Mittal, R., 98-CFD-12, 171-CFD-19 Mockett, C., 306-CFD-36 Mockus, L., 239-ATIO-22 Moeller, T., 67-PDL-3, 144-PDL-7, 216-TP-10/PDL-10, 244-CFD-29 Mohan, A., 302-CFD-32 Mohite, P., 234-APA-26 Moin, P., 202-CFD-22 Moini-Yekta, S., 49-APA-7 Molinaro, N., 297-APA-37 Montalvo, C., 157-AFM-9 Montel, M., 8-AFM-1 Moolchandani, K., 52-ATIO-6 Moore, M., 54-ATIO-8, 93-ATIO-11, 127-ATIO-13, 276-ATIO-26 Moored, K., 100-FD-11 Mor-Yossef, Y., 133-CFD-16 Moraru, G., 103-ITAR-1 Moreau, A., 77-AA-11, 152-AA-22 Moreau, D., 152-AA-22, 231-AA-36 Moreau, E., 33-PDL-1/FD-5, 180-PDL-8/APA-20 Moreau, S., 3-AA-1, 79-AA-13, 81-AA-15, 115-AA-19, 152-AA-22, 185-AA-26, 187-AA-28, 227-AA-32 Moreira, F., 9-AFM-2, 241-CFD-26 Morelli, E., 118-AFM-7 Morgan, P., 102-FD-13 Morgan, R., 34-TP-1 Morikawa, Y., 270-APA-32 Morris, P., 4-AA-2, 40-AA-9, 263-AA-41 Morris, S., 38-AA-7 Morrissey, P., 108-TP-5 Morsbach, C., 133-CFD-16 Mortensen, C., 209-FD-24 Morton, S., 160-APA-17, 174-FD-20 Moses John Christy Appolo, P., 67-PDL-3 Moss, M., 308-MAO-13 Mott, D., 102-FD-13 Motter, M., 165-ATIO-16, 199-ATIO-20 Mouring, C., 281-GEPC-1 Movahed, P., 211-FD-26 Moyes, A., 137-FD-16 Muehleisen, R., 262-AA-40 Muehler-Vahl, H., 101-FD-12 Mueller, F., 203-CFD-23 Mueller, J., 131-CFD-14 Mueller-Vahl, H., 208-FD-23 Mujumdar, P., 57-CFD-7 Mukhopadhyay, V., 214-MST-9 Mulani, S., 29-MAO-1 Mullane, M., 193-APA-21 Mulleners, K., 50-APA-8, 235-APA-27 Munday, P., 101-FD-12 Mundis, N., 132-CFD-15 Munera Savino, F., 8-AFM-1, 249-FT-1 Munjulury, R., 283-MAO-10 Munson, M., 136-FD-15 Murari, K., 159-AMT-10/GT-10 Murayama, M., 229-AA-34, 230-AA-35 Muriel Gracia, M., 113-AA-17 Murman, S., 21-CFD-1, 96-CFD-10, 201-CFD-21, 205-CFD-25 Murphy, C., 52-ATIO-6, 65-MST-3 Murray, H., 114-AA-18, 187-AA-28 Murray, J., 13-APA-2, 297-APA-37 Murray, N., 80-AA-14 Murray, W., 158-AMT-9/GT-9 Murrieta Mendoza, A., 18-ATIO-3 Muscarello, V., 84-AFM-6 Musiak, J., 275-ATIO-25 Muslubas, Y., 57-CFD-7 Muyimbwa, T., 282-LTA-2 Myose, R., 27-FD-3, 175-FD-22 Nagarajan, B., 16-ATIO-1 Nahuis, R., 13-APA-2 Naitoh, K., 182-TP-9 Najafi, A., 104-MAO-3 Najian Asl, R., 283-MAO-10 Nakasato, K., 270-APA-32 Nakashima, T., 270-APA-32 Nalci, M., 66-MST-4 Nallapaneni, S., 35-TP-2 Namba, M., 152-AA-22 Namura, N., 125-APA-16 Nance, D., 262-AA-40 Napolitano, M., 43-AFM-3 Narayanaswamy, V., 27-FD-3, 143-PDL-6, 174-FD-20 Nark, D., 116-AA-20 Narkiewicz, J., 30-MST-1 Natarajan, K., 153-AA-23, 227-AA-32 Nawroth, H., 27-FD-3 Nayeri, C., 26-FD-2, 297-APA-37 Neifeld, A., 39-AA-8 Neilan, J., 165-ATIO-16, 199-ATIO-20 Neilsen, T., 40-AA-9 Neitzel, K., 69-TP-4 Nelson, C., 49-APA-7 Nelson, M., 114-AA-18, 159-AMT-10/GT-10, 187-AA-28 Neuhart, D., 188-AA-29 Neville, A., 246-FD-27 Newcamp, J., 249-FT-1 Newman, J., 95-CFD-9, 170-CFD-18, 305-CFD-35 Ng, H., 18-ATIO-3, 92-ATIO-10 Nguyen, D., 66-MST-4 Nguyen, L., 79-AA-13 Nguyen, M., 88-APA-10, 143-PDL-6 Nguyen, N., 49-APA-7, 124-APA-15 Nichols, D., 297-APA-37 Nichols, J., 4-AA-2, 39-AA-8, 153-AA-23 Nicolosi, F., 8-AFM-1, 13-APA-2, 104-MAO-3 Niedermeier, D., 31-MST-2 Nieto, B., 234-APA-26 Nigam, N., 284-MAO-11 Nikbay, M., 308-MAO-13 Nishida, H., 144-PDL-7 Nishikawa, H., 55-CFD-5, 56-CFD-6 Niu, J., 244-CFD-29 Niu, W., 215-MST-10 Nodé-Langlois, T., 112-AA-16, 187-AA-28 Noelting, S., 188-AA-29 Nojima, Y., 182-TP-9 Noll, B., 185-AA-26 Nompelis, I., 246-FD-27, 256-TP-12 Nomura, S., 69-TP-4 Nonomura, T., 60-FD-6/PDL-2, 114-AA-18, 130-CFD-13, 169-CFD-17 Nordstrom, J., 132-CFD-15, 242-CFD-27 Nott, J., 167-BAL-1, 200-BAL-2 Nouzawa, T., 270-APA-32 Novara, M., 159-AMT-10/GT-10 Novikov, A., 99-FD-10 Nowak, M., 128-ATIO-14 Ntemos, G., 202-CFD-22 O’Brien, D., 15-APA-4, 295-APA-34 O’Brien, J., 151-AA-21 O’Brien, W., 159-AMT-10/GT-10 O’Byrne, S., 11-AMT-2/GT-2, 46-AMT-4/GT-4, 121-AMT-8/FD-14/TP-6/GT-8 O’Connor, C., 91-ATIO-9 O’Neill, W., 35-TP-2 O’Reilly, C., 78-AA-12, 235-APA-27 O’Sullivan, S., 53-ATIO-7 Obayashi, S., 125-APA-16, 196-ASE-2 Author/Session Chair Index Oberleithner, K., 266-AMT-13/GT-13 Ocheltree, C., 89-APA-11, 251-MAO-8, 296-APA-35 Ochieng, W., 198-ATIO-19 Oefelein, J., 244-CFD-29 Ogasawara, T., 68-TP-3 Ogawa, S., 286-PDL-13 Ojeda, S., 95-CFD-9 Okada, Y., 270-APA-32 Okamoto, T., 182-TP-9 Okolo, W., 8-AFM-1, 273-ASE-5 Ol, M., 125-APA-16, 234-APA-26 Olejniczak, J., 69-TP-4 Oliveira, E., 119-AFM-8 Oliver, J., 104-MAO-3 Oliviero, N., 137-FD-16 Oliviu, S., 13-APA-2, 296-APA-35 Ollivier Gooch, C., 21-CFD-1, 23-CFD-3, 131-CFD-14 Olsen, M., 172-CFD-20 Olson, E., 252-MAO-9 Olson, M., 240-ATIO-23 Olson, R., 43-AFM-3 Omar, F., 51-ATIO-5 Omidy, A., 68-TP-3 Onishi, K., 270-APA-32 Oravec, H., 273-ASE-5 Ordaz, I., 14-APA-3 Orr, M., 156-ACD-4 Orra, T., 128-ATIO-14, 212-MAO-6 Osman, A., 178-MST-8 Ostrikov, N., 115-AA-19 Otsu, H., 144-PDL-7 Overmeyer, A., 120-AMT-7/GT-7 Owens, J., 196-ASE-2 Oyama, A., 114-AA-18 Oza, U., 22-CFD-2 Ozcan, M., 265-ACD-7 Özgen, S., 97-CFD-11 Oztekin, A., 164-ATIO-15 Pack, J., 274-ATIO-24 Pack Melton, L., 279-FD-31 Padois, T., 3-AA-1 Pagani, C., 230-AA-35 Page, G., 24-CFD-4 Page, M., 276-ATIO-26 Paglione, P., 128-ATIO-14 Pak, C., 9-AFM-2, 141-MAO-4 Palacios, F., 133-CFD-16, 204-CFD-24, 271-APA-33, 283-MAO-10 Palla, A., 107-PDL-4 Palmer, E., 51-ATIO-5 Palmer, G., 108-TP-5 Palmieri, F., 46-AMT-4/GT-4 Palopo, K., 142-MST-6 Paluch, B., 13-APA-2 Palumbo, R., 164-ATIO-15 Pan, J., 21-CFD-1 Pan, Q., 145-TP-7 Panchal, J., 52-ATIO-6 Panchal, K., 250-LTA-1 Panda, J., 99-FD-10 Pandare, A., 201-CFD-21 Pandya, S., 305-CFD-35 Panerai, F., 288-TP-13 Panesi, M., 69-TP-4 Pankratov, I., 187-AA-28 Pant, R., 282-LTA-2 Papadimitriou, C., 283-MAO-10 Papadimitriou, D., 283-MAO-10 Papageorgio, E., 128-ATIO-14 Papamoschou, D., 227-AA-32, 264-AA-42 Papathakis, K., 240-ATIO-23 Paranin, G., 115-AA-19 Pardowitz, B., 173-FD-19 Parent, B., 216-TP-10/PDL-10 Parente, A., 216-TP-10/PDL-10 Parish, E., 58-CFD-8 Park, G., 139-FD-18 Park, J., 202-CFD-22, 242-CFD-27, 251-MAO-8, 296-APA-35 Park, M., 14-APA-3, 23-CFD-3, 97-CFD-11, 160-APA-17 Park, S., 235-APA-27 Parke, B., 51-ATIO-5 Parker, P., 294-AMT-14/GT-15 Parry, A., 37-AA-6 Parsons, N., 69-TP-4 Paruchuri, C., 3-AA-1, 38-AA-7, 79-AA-13, 152-AA-22 Pascarella, D., 164-ATIO-15 Paschereit, C., 27-FD-3, 297-APA-37 Pasco, Y., 227-AA-32 Pasiliao, C., 12-APA-1, 22-CFD-2, 90-APA-12 Passe, B., 162-APA-19 Pastorelli, V., 77-AA-11 Patel, S., 24-CFD-4 Paterson, E., 26-FD-2 Patil, M., 9-AFM-2, 30-MST-1, 252-MAO-9 Patterson, A., 157-AFM-9 Patterson, J., 214-MST-9 Patterson, M., 127-ATIO-13 Paul, R., 235-APA-27 Paula, A., 307-MAO-12 Pauz, V., 229-AA-34 Pawletta, T., 177-MST-7 Payan, A., 53-ATIO-7, 239-ATIO-22 Peake, N., 3-AA-1, 260-AA-38 129 Pearce, R., 52-ATIO-6 Pechlivanoglou, G., 26-FD-2, 297-APA-37 Pederson, C., 174-FD-20 Pedramasl, N., 64-MAO-2 Pei, J., 119-AFM-8 Pei, P., 276-ATIO-26 Peinke, J., 50-APA-8, 271-APA-33 Pelletier, D., 58-CFD-8, 204-CFD-24, 304-CFD-34 Peltier, S., 266-AMT-13/GT-13 Peng, D., 197-ATIO-18 Peng, J., 190-ACD-5 Peng, S., 6-AA-4, 115-AA-19, 154-AA-24 Peng, W., 198-ATIO-19 Peng, X., 53-ATIO-7 Percin, M., 97-CFD-11, 208-FD-23 Pereira, D., 236-APA-28 Perez, R., 141-MAO-4, 267-APA-29 Periaux, J., 180-PDL-8/APA-20 Peroomian, O., 245-CFD-30 Persson, P., 170-CFD-18 Peter, J., 173-FD-19 Peters, B., 306-CFD-36 Peters, C., 86-AMT-6/GT-6 Petersen, S., 282-LTA-2 Petersson, Ö, 212-MAO-6 Pfaender, H., 53-ATIO-7, 239-ATIO-22 Pfifer, H., 157-AFM-9 Piantanida, S., 5-AA-3, 189-AA-30 Piao, Y., 244-CFD-29 Pierre, D., 154-AA-24 Pilon, A., 153-AA-23 Pimenta, B., 77-AA-11 Pini, M., 133-CFD-16 Pinier, J., 88-APA-10, 123-APA-14 Pinon-Fischer, O., 142-MST-6 Piot, E., 262-AA-40 Piperni, P., 104-MAO-3, 213-MAO-7, 284-MAO-11 Planck, C., 234-APA-26 Plemmons, D., 11-AMT-2/GT-2 Ploetner, K., 52-ATIO-6, 53-ATIO-7 Poggie, J., 102-FD-13, 211-FD-26, 286-PDL-13, 306-CFD-36 Poinsot, T., 185-AA-26 Polaczek, J., 280-FT-2/GT-14 Pomeroy, B., 87-APA-9 Pons-Prat, J., 180-PDL-8/APA-20 Poole, D., 64-MAO-2, 125-APA-16, 283-MAO-10 Popie, V., 262-AA-40 Popov, I., 33-PDL-1/FD-5 Pornet, C., 53-ATIO-7 Poroseva, S., 96-CFD-10, 205-CFD-25 Porteous, A., 96-CFD-10 Porumbel, I., 96-CFD-10 Post, M., 64-MAO-2, 162-APA-19 Pott-Pollenske, M., 3-AA-1, 230-AA-35 Potter, C., 141-MAO-4 Povinelli, L., 281-GEPC-1 Powers, R., 40-AA-9 Prabhu, D., 102-FD-13, 108-TP-5 Prachar, A., 233-APA-25 Pradeep, A., 57-CFD-7 Prasad, R., 12-APA-1, 205-CFD-25 Precup, N., 49-APA-7 Priolo, F., 9-AFM-2 Pröbsting, S., 38-AA-7 Pruett, B., 62-FD-8, 175-FD-22 Pruis, M., 237-ASE-3, 272-ASE-4 Przulj, V., 243-CFD-28 Pulliam, T., 136-FD-15 Pytel, D., 34-TP-1 Qi, B., 145-TP-7 Qi, X., 284-MAO-11 Qian, J., 285-MST-12 Qiao, W., 151-AA-21, 260-AA-38, 267-APA-29 Qiu, S., 204-CFD-24 Qiu, X., 285-MST-12 Qu, Q., 26-FD-2, 47-APA-5 Quaglia, M., 187-AA-28 Qualls, G., 165-ATIO-16, 199-ATIO-20 Quaranta, G., 84-AFM-6 Queiroz, R., 7-AA-5 Quinlan, J., 244-CFD-29 Quinn, M., 45-AMT-3/GT-3 Quinto, P., 158-AMT-9/GT-9 Quix, H., 85-AMT-5/GT-5 Quon, L., 91-ATIO-9 Radyisyewski, P., 30-MST-1 Raffel, M., 192-AMT-12/GT-12 Ragab, S., 236-APA-28 Ragni, D., 37-AA-6, 286-PDL-13 Rahman, M., 139-FD-18 Raj, P., 176-MAO-5, 251-MAO-8, 265-ACD-7, 296-APA-35 Rajagopalan, R., 243-CFD-28 Rajput, P., 233-APA-25 Rallabhandi, S., 14-APA-3, 89-APA-11 Ramachandran, A., 27-FD-3, 28-FD-4 Ramamoorthy, K., 275-ATIO-25 Ramamurti, R., 48-APA-6, 233-APA-25 Raman, G., 262-AA-40 Raman, V., 304-CFD-34 Ramesh, N., 67-PDL-3 Ramirez, W., 38-AA-7 Rancourt, D., 213-MAO-7, 276-ATIO-26 Rand, J., 200-BAL-2 Randt, N., 52-ATIO-6, 128-ATIO-14 Rao, A., 126-ATIO-12, 156-ACD-4 Rashad, R., 204-CFD-24 Rathakrishnan, B., 244-CFD-29 Rathakrishnan, E., 50-APA-8 Rauleder, J., 236-APA-28 Rautmann, C., 79-AA-13, 155-AA-25 Ravetta, P., 188-AA-29 Ray, J., 139-FD-18 Razi, P., 58-CFD-8 Reardon, J., 46-AMT-4/GT-4 Reardon, S., 177-MST-7 Reasor, D., 22-CFD-2 Redonnet, S., 155-AA-25, 261-AA-39 Reed, D., 262-AA-40 Reed, H., 61-FD-7, 137-FD-16, 247-FD-28 Reeder, M., 158-AMT-9/GT-9, 195-APA-23 Reeger, J., 141-MAO-4 Rege, A., 48-APA-6 Rehmanjan, U., 128-ATIO-14 Reiche, N., 39-AA-8, 112-AA-16 Reichman, B., 40-AA-9 Reimer, L., 57-CFD-7 Reissner, F., 101-FD-12 Reist, T., 267-APA-29 Remes, B., 97-CFD-11 Ren, Y., 21-CFD-1, 84-AFM-6, 214-MST-9, 241-CFD-26, 248-FD-29 Rendall, T., 64-MAO-2, 125-APA-16, 283-MAO-10 Render, P., 88-APA-10 Renner, A., 104-MAO-3 Rennie, M., 88-APA-10, 143-PDL-6, 255-PDL-12 Rey, C., 47-APA-5 Rey, M., 262-AA-40 Reyaz Ahmed, A., 50-APA-8 Reynolds, D., 31-MST-2 Reynolds, T., 51-ATIO-5, 163-ASE-1 Reza Ahrabi, B., 95-CFD-9, 122-APA-13 Rhew, R., 158-AMT-9/GT-9, 191-AMT-11/GT-11, 294-AMT-14/GT-15 Rhoads, J., 259-AA-37 Rhodes, D., 52-ATIO-6 Richardson, J., 157-AFM-9 Richardson, T., 84-AFM-6, 212-MAO-6 Ricklick, M., 145-TP-7 Righi, M., 236-APA-28, 278-FD-30 Ringuette, M., 100-FD-11 Ritter, M., 57-CFD-7 Ritz, R., 22-CFD-2, 96-CFD-10 Riviere, P., 217-TP-11 Rizzetta, D., 101-FD-12 Rizzi, A., 160-APA-17 Author/Session Chair Index Rizzi, S., 152-AA-22 Röben, T., 265-ACD-7 Robertson, G., 174-FD-20 Robinson, S., 31-MST-2, 269-APA-31 Robinson III, J., 239-ATIO-22 Rochlitz, H., 159-AMT-10/GT-10 Rodebaugh, G., 173-FD-19 Rodriguez, Y., 51-ATIO-5 Roe, P., 56-CFD-6, 169-CFD-17 Roger, M., 79-AA-13, 81-AA-15, 152-AA-22, 154-AA-24, 187-AA-28 Rogers, M., 61-FD-7 Rogers, S., 233-APA-25 Rohlmann, D., 87-APA-9 Roidl, B., 41-AA-10 Roling, P., 91-ATIO-9 Romanelli, G., 203-CFD-23 Rorie, R., 274-ATIO-24 Rose, C., 107-PDL-4 Rosema, C., 90-APA-12, 296-APA-35 Rosemann, H., 178-MST-8 Rossian, L., 231-AA-36 Rossignol, K., 231-AA-36 Roth, B., 251-MAO-8, 307-MAO-12 Rothhaar, P., 119-AFM-8, 165-ATIO-16, 199-ATIO-20 Rougier, T., 259-AA-37 Roussel, C., 98-CFD-12 Rouzbar, R., 244-CFD-29 Rowe, P., 158-AMT-9/GT-9 Rowley, C., 136-FD-15, 295-APA-34 Roy, A., 246-FD-27 Roy, C., 30-MST-1, 97-CFD-11, 131-CFD-14 Roy, R., 172-CFD-20 Roy, S., 92-ATIO-10, 275-ATIO-25 Roy Salam, I., 190-ACD-5 Royalty, C., 116-AA-20 Ru, P., 157-AFM-9 Rudnick-Cohen, E., 29-MAO-1 Rudnik, R., 87-APA-9 Ruetten, M., 22-CFD-2, 96-CFD-10, 178-MST-8 Ruleva, L., 193-APA-21 Rumann, H., 273-ASE-5 Rumsey, C., 58-CFD-8, 139-FD-18, 172-CFD-20, 208-FD-23 Rusak, Z., 62-FD-8, 173-FD-19 Russell, S., 141-MAO-4 Rutherford, M., 88-APA-10 Sa, J., 235-APA-27 Sabetta, V., 8-AFM-1 Sadique, J., 98-CFD-12, 171-CFD-19 Sadovsky, A., 17-ATIO-2 Sadraey, M., 191-AMT-11/GT-11 Sadri, V., 62-FD-8 Sagebaum, M., 252-MAO-9 Saheby, E., 267-APA-29 Sahin, B., 25-FD-1 Sahin, M., 64-MAO-2 Sahni, O., 63-FD-9 Sahu, J., 90-APA-12 Said, M., 167-BAL-1, 200-BAL-2 Saif Ullah Khalid, M., 133-CFD-16 Saikia, B., 28-FD-4 Saini, A., 46-AMT-4/GT-4, 267-APA-29 Saka, P., 88-APA-10 Sakurai, T., 66-MST-4 Salah El Din, I., 114-AA-18 Salas, P., 115-AA-19 Saleem, M., 174-FD-20 Salehian, S., 79-AA-13 Salemi, L., 28-FD-4 Salinas, M., 84-AFM-6 Salton, A., 40-AA-9 Salze, E., 231-AA-36 Samanta, A., 78-AA-12 Samareh, J., 68-TP-3 Samaritano, A., 194-APA-22 Samimy, M., 33-PDL-1/FD-5, 153-AA-23 Samuel, A., 240-ATIO-23 Sandberg, M., 51-ATIO-5 Sandberg, R., 171-CFD-19 Sanders, L., 259-AA-37 Sandham, N., 209-FD-24 Sanetrik, M., 124-APA-15 Sanjaya, D., 95-CFD-9 Sanjose, M., 227-AA-32 Sankaran, V., 132-CFD-15 Sano, A., 41-AA-10 Santos, J., 30-MST-1, 282-LTA-2 Santos, L., 117-ACD-3, 213-MAO-7 Santos, P., 43-AFM-3 Santos Pereira, R., 286-PDL-13 Saraf, A., 16-ATIO-1, 51-ATIO-5, 91-ATIO-9 Saric, W., 61-FD-7, 137-FD-16 Sarkar, S., 136-FD-15 Sarradj, E., 186-AA-27, 231-AA-36 Sartor, F., 96-CFD-10 Sasaki, J., 293-ACD-8 Sasaki, K., 5-AA-3 Sasanapuri, B., 178-MST-8 Sasidharan Nair, U., 80-AA-14 Sasoh, A., 89-APA-11, 138-FD-17 Sassanis, V., 209-FD-24 Sato, M., 60-FD-6/PDL-2 Satori, S., 293-ACD-8 130 Sattelmayer, T., 41-AA-10, 113-AA-17, 185-AA-26 Saunders, D., 182-TP-9, 217-TP-11 Saurav, S., 125-APA-16 Saw, Z., 265-ACD-7 Sawhill, B., 16-ATIO-1 Sawyer, J., 181-PDL-9/TP-8 Scanlan, J., 128-ATIO-14, 308-MAO-13 Scarano, F., 38-AA-7, 192-AMT-12/GT-12, 266-AMT-13/GT-13 Schaefer, J., 58-CFD-8 Schaefer, M., 299-ATIO-28 Schauerhamer, D., 269-APA-31 Scheel, H., 7-AA-5 Scherer Schwening, G., 104-MAO-3 Schetz, J., 29-MAO-1, 46-AMT-4/GT-4 Schiavo, L., 98-CFD-12 Schiavone, N., 136-FD-15 Schindler, M., 18-ATIO-3 Schinwald, C., 91-ATIO-9 Schlimm, K., 166-ATIO-17 Schlimpert, S., 41-AA-10 Schlottke, M., 229-AA-34 Schluter, J., 47-APA-5, 269-APA-31 Schmidt, A., 177-MST-7 Schmidt, B., 11-AMT-2/GT-2 Schmidt, H., 105-MST-5, 195-APA-23 Schmidt-Skipiol, F., 166-ATIO-17 Schmisseur, J., 10-AMT-1/GT-1 Schmitt, F., 91-ATIO-9 Schmollgruber, P., 82-ACD-2 Schneider, S., 28-FD-4, 61-FD-7, 137-FD-16, 209-FD-24 Schneiders, L., 305-CFD-35 Scholz, P., 125-APA-16, 159-AMT-10/GT-10 Schomberg, T., 22-CFD-2, 96-CFD-10 Schönleitner, F., 151-AA-21 Schram, C., 3-AA-1, 79-AA-13, 112-AA-16, 231-AA-36 Schrijer, F., 138-FD-17 Schrock, C., 201-CFD-21 Schroeder, A., 159-AMT-10/GT-10 Schroeder, W., 6-AA-4, 26-FD-2, 38-AA-7, 41-AA-10, 79-AA-13, 80-AA-14, 229-AA-34, 305-CFD-35 Schülein, E., 138-FD-17 Schultz, M., 164-ATIO-15 Schultz, V., 274-ATIO-24 Schulze, M., 113-AA-17 Schuman, W., 280-FT-2/GT-14 Schuster, D., 233-APA-25 Schuster, W., 151-AA-21, 198-ATIO-19 Schutte, J., 239-ATIO-22 Schwartzentruber, T., 256-TP-12 Schwer, D., 102-FD-13 Sciacchitano, A., 266-AMT-13/GT-13 Sclafani, A., 87-APA-9, 233-APA-25 Scoggins, J., 217-TP-11 Scolan, E., 46-AMT-4/GT-4 Scott, R., 124-APA-15 Scully, R., 273-ASE-5 Secco, N., 307-MAO-12 Seckin, S., 174-FD-20 Seeley, B., 239-ATIO-22 Seidel, J., 12-APA-1, 125-APA-16, 236-APA-28 Seitzman, J., 159-AMT-10/GT-10 Sekhar, S., 58-CFD-8 Self, R., 5-AA-3, 39-AA-8, 227-AA-32 Selfridge, J., 127-ATIO-13 Selic, T., 151-AA-21 Selig, M., 15-APA-4, 87-APA-9, 297-APA-37 Semiletov, V., 6-AA-4, 80-AA-14, 228-AA-33 Semmelmann, J., 85-AMT-5/GT-5 Semper, M., 278-FD-30 Sengissen, A., 188-AA-29 Sepka, S., 68-TP-3, 108-TP-5 Serafini, J., 162-APA-19 Serpieri, J., 38-AA-7, 88-APA-10 Serre, G., 187-AA-28 Sescu, A., 24-CFD-4, 41-AA-10, 81-AA-15, 98-CFD-12, 209-FD-24 Sesterhenn, J., 306-CFD-36 Sevil, H., 128-ATIO-14 Sezer, E., 66-MST-4 Sha, Z., 52-ATIO-6 Shah, G.,154-AFM-9 Shah, H., 203-CFD-23 Shahpar, S., 251-MAO-8 Sharbatdar, M., 131-CFD-14 Sharma, H., 235-APA-27 Sharma, R., 300-ATIO-29 Sharma, S., 239-ATIO-22 Sheehe, S., 11-AMT-2/GT-2 Shen, Q., 191-AMT-11/GT-11 Sheng, C., 122-APA-13, 194-APA-22 Shepherd, J., 11-AMT-2/GT-2 Sherry, L., 52-ATIO-6, 117-ACD-3 Sheshadri, T., 67-PDL-3 Sheta, E., 195-APA-23 Sheth, K., 126-ATIO-12 Shi, R., 190-ACD-5, 251-MAO-8 Shi, S., 107-PDL-4 Shi, Y., 25-FD-1 Shih, A., 164-ATIO-15 Shimosawa, Y., 286-PDL-13 Shimoyama, K., 125-APA-16 Shin, S., 126-ATIO-12 Shipton, L., 128-ATIO-14 Shively, J., 274-ATIO-24 Shmilovich, A., 271-APA-33 Shneider, M., 216-TP-10/PDL-10 Shoda, T., 138-FD-17 Short, E., 145-TP-7 Shukla, H., 9-AFM-2 Shyy, W., 97-CFD-11, 268-APA-30 Siala, F., 234-APA-26 Siddiqi, S., 3-AA-1 Sidharth, G., 139-FD-18 Sidiropoulos, S., 198-ATIO-19 Siebert, J., 230-AA-35 Siercke, M., 7-AA-5 Siikonen, T., 139-FD-18 Sijtsma, P., 115-AA-19 Sillekens, P., 91-ATIO-9 Silton, S., 90-APA-12, 195-APA-23, 246-FD-27, 271-APA-33 Silva, R., 117-ACD-3 Silva, S., 156-ACD-4 Silva, W., 124-APA-15, 273-ASE-5 Silvestre, F., 5-AA-3, 9-AFM-2 Silvestre, M., 104-MAO-3 Simao Ferreira, C., 279-FD-31 Simerly, S., 158-AMT-9/GT-9 Simões, L., 4-AA-2 Simon, F., 262-AA-40 Sinayoko, S., 38-AA-7, 187-AA-28 Singh, A., 279-FD-31 Singh, B., 255-PDL-12 Singh, K., 9-AFM-2 Singh, M., 235-APA-27 Singh, R., 162-APA-19, 268-APA-30 Singh, S., 84-AFM-6 Sinha, A., 228-AA-33 Sinha, K., 28-FD-4 Sinha, P., 276-ATIO-26 Sinnige, T., 37-AA-6 Siozos-Rousoulis, L., 152-AA-22 Sirohi, J., 162-APA-19 Sitaraman, J., 21-CFD-1 Sivaneri, V., 101-FD-12 Sivasubramanian, J., 102-FD-13 Sjogreen, B., 24-CFD-4 Skies, F., 132-CFD-15 Skinner, J., 117-ACD-3 Skvortsov, R., 187-AA-28 Slaboch, P., 303-CFD-33 Slagle, A., 226-AA-31 Slater, J., 279-FD-31 Slegers, N., 30-MST-1 Slotnick, J., 47-APA-5, 301-CFD-31 Author/Session Chair Index Smeltzer, S., 281-GEPC-1 Smith, A., 117-ACD-3 Smith, B., 172-CFD-20 Smith, D., 68-TP-3, 108-TP-5, 158-AMT-9/GT-9, 210-FD-25 Smith, J., 65-MST-3, 142-MST-6, 278-FD-30 Smith, K., 145-TP-7 Smith, M., 259-AA-37 Smolarkiewicz, P., 163-ASE-1 Snyder, M., 236-APA-28 Sohoni, N., 37-AA-6 Şöhret, Y., 273-ASE-5 Soler, L., 275-ATIO-25 Solodovnikov, S., 193-APA-21 Son, P., 138-FD-17 Song, J., 100-FD-11 Sontag, J., 255-PDL-12 Soria, J., 153-AA-23 Sorokach, M., 214-MST-9 Soucasse, L., 217-TP-11 Soufiani, A., 217-TP-11 Souza, D., 230-AA-35 Spagnolo, S., 205-CFD-25 Spalart, P., 123-APA-14, 211-FD-26 Spalt, T., 259-AA-37 Speck, S., 88-APA-10 Speer, S., 302-CFD-32 Spehr, C., 186-AA-27, 260-AA-38 Spencer, T., 300-ATIO-29 Spiegel, S., 55-CFD-5, 130-CFD-13 Spiegelberg, H., 297-APA-37 Spillers, R., 62-FD-8, 175-FD-22 Spinelli, A., 26-FD-2 Spravka, J., 249-FT-1 Sreenivas, K., 15-APA-4, 122-APA-13, 297-APA-37 Sridhar, B., 18-ATIO-3, 92-ATIO-10 Sridharan, A., 162-APA-19 Srigrarom, S., 162-APA-19, 234-APA-26, 265-ACD-7 Srinivasan, C., 181-PDL-9/TP-8 Srinivasan, E., 50-APA-8 Srivastava, A., 138-FD-17 Stachura, M., 157-AFM-9 Stagni, A., 244-CFD-29 Staley, A., 299-ATIO-28 Stalnov, O., 7-AA-5, 38-AA-7, 79-AA-13 Stanek, M., 33-PDL-1/FD-5 Stanford, B., 49-APA-7, 124-APA-15 Stangfeld, C., 208-FD-23 Steiger, R., 46-AMT-4/GT-4 Stein, F., 88-APA-10 Steinbrenner, J., 23-CFD-3 Stephan, A., 196-ASE-2, 237-ASE-3 Stephani, K., 216-TP-10/PDL-10, 288-TP-13 Stephen, S., 209-FD-24 Stephens, D., 114-AA-18 Stephens, J., 191-AMT-11/GT-11 Stevens, M., 274-ATIO-24 Stoellinger, M., 172-CFD-20 Stohr, M., 266-AMT-13/GT-13 Stoll, A., 240-ATIO-23, 276-ATIO-26 Stone, C., 203-CFD-23, 302-CFD-32 Storozhev, D., 216-TP-10/PDL-10 Stouffer, V., 65-MST-3, 142-MST-6, 199-ATIO-20, 275-ATIO-25 Stout, T., 40-AA-9 Strande, P., 237-ASE-3 Strangfeld, C., 101-FD-12 Straub, S., 91-ATIO-9 Streett, C., 233-APA-25 Strganac, T., 9-AFM-2, 124-APA-15, 270-APA-32 Stuchlik, D., 200-BAL-2 Stuermer, A., 162-APA-19 Su, H., 252-MAO-9 Su, L., 181-PDL-9/TP-8 Su, W., 25-FD-1, 105-MST-5 Subbarao, K., 48-APA-6, 157-AFM-9 Subbareddy, P., 244-CFD-29, 246-FD-27, 278-FD-30 Subramanian, N., 3-AA-1, 152-AA-22 Subramanyam, A., 153-AA-23 Sudani, J., 205-CFD-25 Sui, D., 65-MST-3 Sun, D., 16-ATIO-1 Sun, H., 95-CFD-9 Sun, Y., 4-AA-2, 6-AA-4, 31-MST-2, 248-FD-29 Sun, Z., 130-CFD-13 Sundström, E., 112-AA-16 Suñol, A., 250-LTA-1 Suraj Nandiganahalli, J., 31-MST-2 Surakitbanharn, C., 166-ATIO-17 Suryadi, A., 115-AA-19 Suryakumar, V., 9-AFM-2, 124-APA-15, 270-APA-32 Surzhikov, S., 69-TP-4, 193-APA-21, 216-TP-10/PDL-10 Sutliff, D., 78-AA-12, 116-AA-20 Suzuki, K., 33-PDL-1/FD-5, 89-APA-11, 102-FD-13 Suzuki, T., 68-TP-3 Swaminathan Gopalan, K., 288-TP-13 Swann, M., 293-ACD-8 Swieringa, K., 18-ATIO-3, 298-ATIO-27 Swift, S., 113-AA-17 Sytsma, M., 158-AMT-9/GT-9 Szmelter, J., 163-ASE-1 Tabanli, H., 174-FD-20 Taha, H., 236-APA-28 Tai, J., 308-MAO-13 131 Taira, K., 101-FD-12, 136-FD-15, 248-FD-29 Takahashi, T., 117-ACD-3, 190-ACD-5, 232-ACD-6, 286-PDL-13, 293-ACD-8 Takaishi, T., 230-AA-35 Takaki, R., 23-CFD-3 Takayanagi, H., 69-TP-4 Tal, E., 124-APA-15 Tam, C., 41-AA-10, 67-PDL-3, 185-AA-26 Tamaki, Y., 241-CFD-26 Tamaskar, S., 239-ATIO-22 Tamba, T., 138-FD-17 Tamura, M., 144-PDL-7 Tamura, T., 182-TP-9 Tanaka, Y., 182-TP-9 Tang, C., 162-APA-19 Tang, H., 17-ATIO-2, 145-TP-7, 173-FD-19 Tang, S., 105-MST-5 Tang, W., 267-APA-29 Tang, Y., 105-MST-5 Tanner, P., 120-AMT-7/GT-7 Tanno, H., 69-TP-4 Tao, F., 7-AA-5 Tao, G., 127-ATIO-13 Tao, L., 204-CFD-24, 245-CFD-30 Tapken, U., 173-FD-19 Taquin, G., 83-AFM-5 Tarter, J., 140-ITAR-2 Tatsukawa, T., 114-AA-18 Tavernetti, W., 278-FD-30 Tay, W., 22-CFD-2 Taylor, C., 275-ATIO-25 Taylor, L., 15-APA-4, 297-APA-37 Taylor, N., 301-CFD-31 Taylor, S., 273-ASE-5 Tchatchueng Kammegne, M., 66-MST-4 Tchipev, N., 237-ASE-3 Teare, D., 214-MST-9 Temmler, C., 113-AA-17 Tensuda, B., 304-CFD-34 Terakado, D., 169-CFD-17 Ternisien, L., 18-ATIO-3 Terracol, M., 154-AA-24, 229-AA-34 Terrazas-Salinas, I., 108-TP-5 Tesfahunegn, Y., 307-MAO-12 Testa, C., 263-AA-41 Tester, B., 186-AA-27 Thaiss, C., 83-AFM-5 Thamsen, P., 173-FD-19 Thanigaiarasu, S., 50-APA-8 Thekinen, J., 52-ATIO-6 Theodore, C., 281-GEPC-1 Theunissen, R., 3-AA-1 Thiele, F., 112-AA-16, 306-CFD-36 Thielecke, F., 8-AFM-1 Thierry, M., 108-TP-5 Thipyopas, C., 234-APA-26 Thobois, L., 272-ASE-4, 298-ATIO-27 Thomas, J., 307-MAO-12 Thompson, D., 23-CFD-3, 97-CFD-11 Thompson, F., 104-MAO-3 Thompson, R., 67-PDL-3, 244-CFD-29 Thompson, T., 42-ACD-1 Thornber, B., 306-CFD-36 Thorne, J., 243-CFD-28 Thorsen, A., 83-AFM-5 Thumiah, D., 86-AMT-6/GT-6 Thurow, B., 67-PDL-3 Tian, P., 43-AFM-3 Tian, Y., 44-AFM-4 Tian, Z., 244-CFD-29 Tibor, E., 212-MAO-6 Tilmann, C., 271-APA-33 Timme, S., 96-CFD-10 Timofeev, E., 102-FD-13 Ting, E., 124-APA-15 Tissot, G., 5-AA-3 Titarev, V., 187-AA-28 Tittsworth, J., 237-ASE-3 Tkachenko, O., 31-MST-2 Tkacik, P., 282-LTA-2 Tobalske, B., 100-FD-11 Togiti, V., 172-CFD-20 Tolomelli, L., 181-PDL-9/TP-8 Tomac, M., 160-APA-17 Tong, F., 151-AA-21, 260-AA-38 Tong, O., 21-CFD-1 Tong, W., 176-MAO-5 Tordeux, S., 262-AA-40 Toropov, V., 5-AA-3, 251-MAO-8 Torres, S., 92-ATIO-10 Toubin, H., 161-APA-18 Toussaint, C., 83-AFM-5 Toussaint, S., 300-ATIO-29 Towne, A., 5-AA-3 Tran, D., 99-FD-10 Tran, L., 165-ATIO-16 Trani, A., 300-ATIO-29 Treve, V., 51-ATIO-5 Trevino, L., 214-MST-9 Trinh, K., 124-APA-15 Tritschler, J., 43-AFM-3 Trolinger, J., 11-AMT-2/GT-2 Trollinger, L., 50-APA-8 Tropea, C., 50-APA-8, 271-APA-33, 297-APA-37 Troxel, S., 163-ASE-1 Trujillo, A., 199-ATIO-20 Truong, A., 264-AA-42 Tsai, C., 304-CFD-34 Tsao, S., 92-ATIO-10, 197-ATIO-18 Tsotskas, C., 29-MAO-1 Tsubokura, M., 270-APA-32 Tsuchiya, T., 51-ATIO-5 Tsutsumi, S., 23-CFD-3 Tufts, M., 137-FD-16 Tuinstra, M., 115-AA-19 Tule, C., 157-AFM-9 Tuna, B., 101-FD-12, 248-FD-29 Turchi, A., 34-TP-1 Turowski, M., 85-AMT-5/GT-5 Tuttle, J., 167-BAL-1 Tyagi, A., 198-ATIO-19, 300-ATIO-29 Tysell, L., 154-AA-24 Tyson, W., 97-CFD-11 Uddin, M., 306-CFD-36 Ueckermann, M., 33-PDL-1/FD-5 Uehara, A., 31-MST-2 Ukeiley, L., 48-APA-6, 195-APA-23, 248-FD-29 Ulbrich, N., 294-AMT-14/GT-15 Ullrich, W., 41-AA-10, 185-AA-26 Underbrink, J., 186-AA-27, 262-AA-40 Underwood, M., 299-ATIO-28 Upalkar, B., 145-TP-7 Ura, H., 230-AA-35 Urnes, J., 49-APA-7 Valavanis, K., 88-APA-10 Valentini, P., 256-TP-12 Valla, M., 272-ASE-4 van Bussel, G., 122-APA-13, 279-FD-31 van de Ven, T., 230-AA-35 van der Velden, W., 38-AA-7 van Kuijk, J., 37-AA-6 van Oudheusden, B., 97-CFD-11, 138-FD-17, 208-FD-23 van Tooren, M., 64-MAO-2 Van Treuren, K., 15-APA-4 Van Treuren, R., 250-LTA-1 van Zuijlen, A., 38-AA-7, 122-APA-13 Vanden, K., 270-APA-32 Vanderwel, C., 3-AA-1, 38-AA-7, 152-AA-22 Vanstone, L., 174-FD-20 VanValkenburg, R., 237-ASE-3 Varga, D., 200-BAL-2 Vargas, A., 167-BAL-1 Vargas, M., 196-ASE-2 Varghese, P., 288-TP-13 Vargo, E., 275-ATIO-25 Varma, D., 125-APA-16 Author/Session Chair Index Varney, M., 31-MST-2 Vascik, P., 52-ATIO-6 Vashishtha, A., 102-FD-13 Vasile, M., 214-MST-9 Vassaux, D., 167-BAL-1 Vatsa, V., 133-CFD-16, 259-AA-37 Vaughan, W., 196-ASE-2, 273-ASE-5 Vaux, S., 249-FT-1 Vekaria, S., 235-APA-27 Veldhuis, L., 37-AA-6, 269-APA-31 Vemuri, S., 234-APA-26 Venel, S., 167-BAL-1 Venkatachari, B., 193-APA-21, 211-FD-26 Venkatakrishnan, L., 227-AA-32 Venkatesh, B., 39-AA-8 Venkatraman, S., 50-APA-8 Venuti, J., 51-ATIO-5 Vera, J., 5-AA-3 Vergine, F., 205-CFD-25 Vermeire, B., 130-CFD-13, 202-CFD-22 Vermillion, C., 282-LTA-2 Vey, S., 26-FD-2, 297-APA-37 Viladegut, A., 216-TP-10/PDL-10 Villa, C., 65-MST-3 Vincent, P., 130-CFD-13, 202-CFD-22, 242-CFD-27 Visbal, M., 101-FD-12, 102-FD-13, 170-CFD-18, 208-FD-23, 255-PDL-12, 266-AMT-13/GT-13, 270-APA-32 Viswanath, K., 233-APA-25 Vitale, S., 133-CFD-16 Vitzilaios, N., 88-APA-10 Vo, H., 60-FD-6/PDL-2 Vos, R., 42-ACD-1 Vrchota, P., 233-APA-25 Vu, B., 56-CFD-6 Vucinic, D., 250-LTA-1 Vuillot, F., 39-AA-8, 259-AA-37 Wache, L., 52-ATIO-6 Waddington, M., 82-ACD-2 Wagle, N., 157-AFM-9 Wagner, C., 252-MAO-9 Wagner, J., 62-FD-8, 175-FD-22 Wagnild, R., 103-ITAR-1, 256-TP-12 Waindim, M., 245-CFD-30 Waithe, K., 14-APA-3, 89-APA-11 Wakayama, S., 267-APA-29 Wakefield, D., 167-BAL-1 Walker, A., 88-APA-10, 214-MST-9 Walker, M., 50-APA-8 Wall, A., 40-AA-9 Wan, Y., 65-MST-3, 275-ATIO-25 Wang, C., 161-APA-18, 213-MAO-7, 269-APA-31 Wang, F., 85-AMT-5/GT-5, 191-AMT-11/GT-11, 237-ASE-3, 295-APA-34 Wang, G., 265-ACD-7 Wang, H., 84-AFM-6, 244-CFD-29 Wang, J., 33-PDL-1/FD-5, 84-AFM-6, 180-PDL-8/ APA-20, 187-AA-28, 271-APA-33 Wang, K., 187-AA-28, 255-PDL-12 Wang, L., 151-AA-21, 260-AA-38 Wang, M., 187-AA-28, 255-PDL-12, 263-AA-41, 265-ACD-7 Wang, P., 128-ATIO-14 Wang, Q., 80-AA-14, 173-FD-19, 202-CFD-22, 241-CFD-26 Wang, S., 62-FD-8, 119-AFM-8 Wang, X., 122-APA-13, 132-CFD-15, 250-LTA-1, 260-AA-38 Wang, Y., 9-AFM-2, 22-CFD-2, 30-MST-1, 131-CFD-14, 213-MAO-7 Wang, Z., 23-CFD-3, 25-FD-1, 56-CFD-6, 99-FD-10, 130-CFD-13, 138-FD-17, 170-CFD-18, 242-CFD-27, 303-CFD-33 Wanke, C., 275-ATIO-25 Ward, C., 137-FD-16 Watanabe, Y., 33-PDL-1/FD-5, 102-FD-13 Watson, J., 104-MAO-3 Watson, W., 7-AA-5, 116-AA-20, 262-AA-40 Weaver, A., 35-TP-2 Webb, N., 33-PDL-1/FD-5 Webster, R., 122-APA-13 Wei, Q., 7-AA-5 Wei tao, Z., 303-CFD-33 Weinstein, R., 50-APA-8 Weiss, B., 91-ATIO-9 Weiss, M., 239-ATIO-22 Wells, D., 42-ACD-1 Wen, Y., 250-LTA-1 Wendorff, A., 212-MAO-6, 308-MAO-13 Weng, H., 68-TP-3 Werner, T., 151-AA-21 Wernet, M., 227-AA-32 Werter, N., 29-MAO-1 West, A., 39-AA-8, 230-AA-35 West, J., 171-CFD-19 West, T., 58-CFD-8 Wey, P., 45-AMT-3/GT-3, 47-APA-5 Whalen, E., 248-FD-29, 271-APA-33 Wheaton, B., 103-ITAR-1, 278-FD-30 White, E., 158-AMT-9/GT-9, 209-FD-24, 267-APA-29 White, J., 133-CFD-16 White, M., 67-PDL-3, 255-PDL-12 White, T., 68-TP-3, 108-TP-5, 217-TP-11 Wiart, L., 13-APA-2 132 Wieland, F., 198-ATIO-19, 300-ATIO-29 Wilcoxen, M., 17-ATIO-2 Wild, J., 125-APA-16, 230-AA-35 Wilder, M., 182-TP-9 Wilder, W., 91-ATIO-9 Wildschek, A., 64-MAO-2 Wilkinson, S., 248-FD-29 Williams, A., 35-TP-2 Williams, D., 60-FD-6/PDL-2, 101-FD-12, 136-FD-15 Williams, N., 244-CFD-29 Williamschen, M., 263-AA-41 Wilson, A., 198-ATIO-19 Winer, E., 104-MAO-3, 141-MAO-4, 176-MAO-5, 212-MAO-6 Wing, A., 239-ATIO-22 Wing, D., 299-ATIO-28 Winkel, R., 60-FD-6/PDL-2 Winter, M., 108-TP-5, 121-AMT-8/FD-14/TP-6/GT-8, 181-PDL-9/TP-8 Wintzer, M., 14-APA-3 Wisda, D., 114-AA-18, 187-AA-28 Wisniewski, C., 15-APA-4 Wisniewski, N., 15-APA-4 Wissa, A., 12-APA-1 Wissink, A., 201-CFD-21 Witherden, F., 130-CFD-13, 202-CFD-22 Wittig, S., 46-AMT-4/GT-4 Wlezien, R., 137-FD-16 Wohlbrandt, A., 41-AA-10 Wolf, W., 38-AA-7, 41-AA-10, 189-AA-30, 260-AA-38, 270-APA-32 Woo, G., 295-APA-34 Woopen, M., 95-CFD-9 Wortmann, A., 42-ACD-1 Wray, A., 24-CFD-4 Wray, T., 139-FD-18, 211-FD-26 Wright, M., 85-AMT-5/GT-5 Wrighton, C., 227-AA-32 Wronowski, K., 280-FT-2/GT-14 Wu, D., 213-MAO-7 Wu, J., 25-FD-1, 265-ACD-7 Wu, X., 99-FD-10 Wu, Y., 181-PDL-9/TP-8 Wu, Z., 250-LTA-1 Wünsch, O., 22-CFD-2, 96-CFD-10 Wyszogrodzki, A., 163-ASE-1 Xia, Y., 55-CFD-5 Xiang, J., 47-APA-5 Xiao, F., 130-CFD-13 Xiao, T., 97-CFD-11 Xiao, Y., 296-APA-35 Xiaojie, Q., 105-MST-5 Xie, J., 65-MST-3 Xie, K., 191-AMT-11/GT-11 Xu, F., 57-CFD-7 Xu, J., 116-AA-20, 241-CFD-26 Xu, K., 107-PDL-4, 143-PDL-6 Xu, Z., 105-MST-5, 241-CFD-26 Xue, M., 16-ATIO-1 Yadlin, Y., 271-APA-33 Yagiz, B., 304-CFD-34 Yakhina, G., 79-AA-13 Yakovlev, P., 228-AA-33 Yalin, A., 107-PDL-4 Yamada, K., 144-PDL-7 Yamagishi, K., 182-TP-9 Yamamoto, K., 23-CFD-3, 229-AA-34, 230-AA-35 Yamashita, R., 89-APA-11 Yamauchi, G., 192-AMT-12/GT-12 Yamouni, S., 270-APA-32 Yan, F., 128-ATIO-14 Yan, G., 131-CFD-14 Yan, K., 250-LTA-1 Yan, W., 178-MST-8 Yan, X., 180-PDL-8/APA-20 Yang, C., 145-TP-7 Yang, D., 204-CFD-24 Yang, H., 197-ATIO-18, 241-CFD-26, 304-CFD-34 Yang, M., 119-AFM-8 Yang, T., 250-LTA-1 Yang, W., 105-MST-5 Yang, X., 98-CFD-12, 171-CFD-19 Yang, Y., 4-AA-2, 6-AA-4, 97-CFD-11, 162-APA-19, 178-MST-8, 269-APA-31 Yang, Z., 159-AMT-10/GT-10, 268-APA-30 Yao, C., 57-CFD-7, 188-AA-29 Yao, H., 6-AA-4, 115-AA-19, 154-AA-24 Yao, W., 56-CFD-6 Yarusevych, S., 100-FD-11, 208-FD-23 Yauwenas, Y., 115-AA-19 Yayla, S., 25-FD-1 Yazdani, S., 229-AA-34 Ye, C., 198-ATIO-19 Yechout, T., 64-MAO-2 Yee, H., 24-CFD-4 Yee, P., 108-TP-5 Yen, C., 78-AA-12 Yeste-Ojeda, O., 215-MST-10 Yi, S., 12-APA-1 Yoder, D., 58-CFD-8, 120-AMT-7/GT-7 Yokokawa, Y., 230-AA-35 Yoon, S., 136-FD-15 Yoshida, S., 43-AFM-3 Yoshikawa, E., 298-ATIO-27 Yoshino, T., 286-PDL-13 Young, D., 25-FD-1 Young, E., 200-BAL-2 Young, L., 117-ACD-3 Young, R., 281-GEPC-1 Young, S., 166-ATIO-17 Young, T., 48-APA-6, 102-FD-13 Yu, H., 159-AMT-10/GT-10 Yu, J., 122-APA-13 Yu, L., 145-TP-7 Yu, M., 243-CFD-28, 279-FD-31 Yu, S., 269-APA-31 Yu, W., 7-AA-5 Yuan, C., 248-FD-29 Yuan-pei, S., 252-MAO-9 Yuceil, K., 174-FD-20 Yue, C., 280-FT-2/GT-14 Yue, Z., 65-MST-3 Zachos, P., 270-APA-32 Zaidi, T., 52-ATIO-6 Zajaczkowski, F., 140-ITAR-2 Zakaria, M., 236-APA-28 Zaman, K., 189-AA-30 Zambrano, J., 215-MST-10 Zanette, J., 249-FT-1 Zang, T., 308-MAO-13 Zawodny, N., 155-AA-25 Zaytsev, M., 187-AA-28, 189-AA-30 Zehner, P., 154-AA-24 Zelenak, D., 143-PDL-6 Zelinski, S., 16-ATIO-1 Zeng, D., 239-ATIO-22 Zeng, Q., 30-MST-1 Zerobin, S., 151-AA-21 Zha, G., 90-APA-12, 125-APA-16 Zhai, Q., 67-PDL-3 Zhai, Z., 215-MST-10 Zhang, B., 16-ATIO-1 Zhang, C., 253-MST-11, 295-APA-34 Zhang, D., 180-PDL-8/APA-20, 271-APA-33 Zhang, F., 47-APA-5 Zhang, G., 57-CFD-7 Zhang, H., 208-FD-23 Zhang, J., 65-MST-3, 203-CFD-23, 265-ACD-7 Zhang, L., 215-MST-10 Zhang, M., 5-AA-3 Zhang, S., 303-CFD-33 Zhang, X., 7-AA-5, 22-CFD-2, 25-FD-1, 112-AA-16, 113-AA-17, 152-AA-22, 205-CFD-25, 214-MST-9, 259-AA-37, 263-AA-41 Zhang, Y., 31-MST-2, 122-APA-13, 198-ATIO-19, 248-FD-29 Author/Session Chair Index Zhang, Z., 46-AMT-4/GT-4, 58-CFD-8, 67-PDL-3, 138-FD-17, 181-PDL-9/TP-8 Zhao, C., 128-ATIO-14 Zhao, D., 116-AA-20, 162-APA-19 Zhao, J., 33-PDL-1/FD-5 Zhao, K., 161-APA-18, 200-BAL-2 Zhao, Q., 194-APA-22, 241-CFD-26 Zhao, W., 51-ATIO-5 Zhao, X., 303-CFD-33 Zhao, Y., 35-TP-2, 145-TP-7 Zhelonkin, M., 31-MST-2 Zhelonkin, V., 31-MST-2 Zheng, J., 185-AA-26 Zheng, Y., 44-AFM-4 Zheng, Z., 43-AFM-3, 62-FD-8, 246-FD-27, 250-LTA-1, 261-AA-39, 272-ASE-4 Zhong, X., 209-FD-24 Zhou, B., 79-AA-13, 283-MAO-10 Zhou, H., 250-LTA-1 Zhou, J., 208-FD-23 Zhou, L., 7-AA-5 Zhou, P., 250-LTA-1 Zhu, J., 25-FD-1 Zhu, M., 250-LTA-1 Zhu, T., 69-TP-4 Zientarski, L., 191-AMT-11/GT-11 Zimmerman, J., 107-PDL-4 Zingg, D., 132-CFD-15, 169-CFD-17, 204-CFD-24, 242-CFD-27, 267-APA-29 Zishka, E., 182-TP-9 Zocca, M., 26-FD-2, 196-ASE-2 Zondervan, D., 197-ATIO-18 Zou, S., 25-FD-1 Zuniga Vazquez, J., 23-CFD-3 Zwerger, C., 87-APA-9 Notes Intro www.aiaa-aviation.org 133 41#aiaaAviation Intro Technical Zones 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 31st AIAA Aerodynamic Measurement Technology and Ground Testing Conference 15th AIAA Aviation Technology, Integration, and Operations Conference AIAA Balloon Systems Conference AIAA Flight Testing Conference 22nd AIAA Lighter-Than-Air Systems Technology Conference AIAA Modeling and Simulation Technologies Conference 45th AIAA Thermophysics Conference 33rd AIAA Applied Aerodynamics Conference Zone 4 31st AIAA Aerodynamic Measurement Technology and Ground Testing Conference AIAA Atmospheric Flight Mechanics Conference 7th AIAA Atmospheric and Space Environments Conference AIAA Complex Aerospace Systems Exchange 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 www.aiaa-aviation.org 134 42#aiaaAviation Intro Map Venue ZONE 3 ZONE 1 ZONE 4 ZONE 2 Hilton Anatole www.aiaa-aviation.org 135 51#aiaaAviation 2O16 13–17 JUNE 2016 WASHINGTON, D.C. See You Next Year! Technical Conferences We hope that you learned something new, achieved your goals, caught up with colleagues, and made new connections. We look forward to seeing you next year in the Nation’s capital! 34th AIAA Applied Aerodynamics Conference Why Washington, D.C.? It’s the perfect place to combine business and family fun. It is home to Congress, NASA Headquarters, NASA Goddard, NOAA, the FAA, NSSC, NRL, and the Pentagon. There are more than 100 free things to do in Washington, D.C.— including most of the Smithsonian (with TWO air and space museums, art galleries, and the National Zoo) and scores of famous landmarks— most within walking distance of one another. 32nd AIAA Aerodynamic Measurement Technology and Ground Testing Conference AIAA Atmospheric Flight Mechanics Conference 8th AIAA Atmospheric and Space Environments Conference 16th AIAA Aviation Technology, Integration, and Operations Conference AIAA Flight Testing Conference 8th AIAA Flow Control Conference 46th AIAA Fluid Dynamics Conference 17th AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference AIAA Modeling and Simulation Technologies Conference 47th AIAA Plasmadynamics and Lasers Conference 46th AIAA Thermophysics Conference Sign up for Email Alerts aiaa-aviation.org/FutureEvents Reserve your sponsorship and exhibit space today! Contact Tobey Jackson, 703.264.7570 or tobeyj@aiaa.org

Final Program - AIAA`s Aviation 2016

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