Concepts to Reality: Driving the Next Century of Flight Innovation Final Program

2O16 13–17 JUNE 2016 WASHINGTON, D.C. CONCEPTS TO REALITY: DRIVING THE NEXT CENTURY OF FLIGHT INNOVATION

FINAL PROGRAM Organized by www.aiaa-aviation.org #aiaaAviation

14-315 B:9” T:8.5” S:7.5”

FROM THE PRESENT TO THE FUTURE A BETTER WAY TO FLY. B:11.5” S:10” T:11”

There’s a promise built into every Boeing plane that transcends route maps and data points. It’s a promise to innovate beyond the needs of today. To exceed efﬁ ciency standards. To craft superior experiences for passengers. To ensure that our planes will continue to be the most advanced and reliable in the world. To always deliver a better way to ﬂ y.

boeing.com/commercial Executive Steering Committee AIAA AVIATION 2016 2O16 Welcome Welcome to Washington, DC, and AIAA AVIATION 2016! This year’s theme is “Concepts to Reality: Driving the Next Century of Flight Innovation,” and we believe you will find our program full of opportunities to consider how today’s ideas become tomorrow’s realities, and how those realities transform our community and our world. Michael Delaney will get our plenary program started with a keynote address reflecting on the history of flight and how that storied past will inform our future. Michael Lombardi will treat attendees to a visually rich presentation on the distinguished 100-year history of The Boeing Company. Congressman Steve Knight (R-CA), a member of the House Committee on Science, Space, and Technology, will announce the introduction of his “Aeronautics Innovation Act,” while Michimasa Fujino will tell us about the HondaJet and how it reflects Michael B. Bragg Thomas Edwards the intersection of innovation and inspiration. Richard Clarke will talk to us about the University of Washington NASA Ames Research cybersecurity threats posed to the connected commercial aviation environment, and John Center Langford will help us see a future dominated by UAS and how the arrival of those systems is changing our world. Wrapping things up, Charlie Bolden will discuss NASA’s journey to transform aeronautics and aviation. Taking the plenary sessions one step further, our dynamic Forum 360 program will tackle some of the most pressing issues our community faces. With the number of people flying each year increasing, airport and airline management must consider issues that cause disruptions and how the industry can minimizing their effect on the air transport network. We will examine how aerospace education programs are preparing the future workforce and what might be done to enhance aerospace programs so that our workforce is the best prepared in the world to tackle tomorrow’s challenges. Commercial airplane companies from Robert D. Gregg, III Todd Zarfos around the world will discuss what it takes to develop a new aircraft design in today’s global Boeing Commercial Boeing Commercial landscape. NASA will take us through their aeronautics programs, giving us a good look at Airplanes Airplanes how they are tackling the hard challenges posed by the need for safe and environmentally responsible air systems. There will be an in-depth look at the future of military aviation as well, considering how that enterprise will evolve. We will grapple with cybersecurity through interactive exercises designed to pose real-time problems and solutions to common vulnerabilities encountered in the aviation enterprise. The future of regulations will be on the table as we examine which regulations help our community innovate and evolve, and which hamper us and how we can change them. We will also examine the future of flight testing and consider the legacy of the X-15 and Space Shuttle on hypersonic flight. In short, we have a lot to talk about. With over 1,300 presentations scheduled, our technical program is second to none. You will not find the quality, depth, and breadth of this week’s presentations at any other gathering, and we thank the Technical Program Committee for developing this outstanding program. AIAA AVIATION 2016 will excite, motivate, and solidify our community’s efforts to constantly dream of the future of aviation and then make that future a reality. We thank you for choosing to be here this week and we are confident you will be pleased with your choice.

AIAA AVIATION 2O16 is proud to feature the following conferences: 32nd AIAA Aerodynamic Measurement Technology and 8th AIAA Flow Control Conference Ground Testing Conference 46th AIAA Fluid Dynamics Conference 34th AIAA Applied Aerodynamics Conference AIAA Modeling and Simulation Technologies Conference AIAA Atmospheric Flight Mechanics Conference 17th AIAA/ISSMO Multidisciplinary Analysis and 8th AIAA Atmospheric and Space Environments Optimization Conference Conference 47th AIAA Plasmadynamics and Lasers Conference 16th AIAA Aviation Technology, Integration, and 46th AIAA Thermophysics Conference Operations Conference DEMAND for UNMANNED: Catalyst for the Machine AIAA Flight Testing Conference Intelligence Revolution

www.aiaa-aviation.org 3 #aiaaAviation IntroOrganizing Committee

General Chair Virginia Stouffer, LMI Modeling and Simulation Technologies Robert D. Gregg, III, Boeing Commercial Peter Zaal, San Jose State University Airplanes Andrew Gibson, Empirical Systems Aerospace, Inc. Alaa Elmiligui, NASA Langley Research Forum 360 Chair Center Samantha Magill, Honda Aircraft Company Isaac Choutapalli, The University of Texas - Pan American Multidisciplinary Analysis and Optimization Forum Technical Co-Chair Vijay Kalivarapu, Iowa State University Latunia Melton (Aerospace Sciences Group), Applied Aerodynamics NASA Langley Research Center Kursat Kara, Khalifa University Scott Ferguson, North Carolina State University Forum Technical Co-Chair John Farnsworth, University of Colorado Cees Bil (Aircraft and Atmospheric Systems Boulder Plasmadynamics and Lasers Group), RMIT University Joseph W. Zimmerman, CU Aerospace, LLC Jeremy Pinier, NASA Langley Research Technical Program Committee Center Thermophysics Forum Deputy Technical Co-Chairs Andy Williams, Air Force Research Atmospheric and Space Environments James Guglielmo (Aerospace Sciences Laboratory Justin Likar, UTC Aerospace Systems Group), The Boeing Company Michael Winter, University of Kentucky Nashat Ahmad, NASA Langley Research Richard Mange (Aircraft and Atmospheric Center Systems Group), Lockheed Martin Aeronautics David Thompson, Mississippi State ITAR Co-Chairs University Katya M. Casper, Sandia National Atmospheric Flight Mechanics Laboratories Mark Phillips, NASA Marshall Space Flight Center Peggy Hayes, NASA Armstrong Flight Research Center Ellen Gillespie, United Space Alliance

Technical Discipline Chairs Flight Testing Aerodynamic Measurement Technology Karl Garman, Federal Aviation Administration Todd Lowe, Virginia Polytechnic Institute and State University Reagan Woolf, Edwards Air Force Base

Brett Bathel, NASA Langley Research Center Flight Testing/Ground Testing Air Transportation Integration & Operations Starr Ginn, NASA Armstrong Flight Research Center Richard Mange, Lockheed Martin Aeronautics Calain Schuman, Department of Defense

Hernando Jimenez, Georgia Institute of Ben Mills, Arnold Engineering Development Technology Center/Aerospace Testing Alliance

Nicholas K. Borer, NASA Langley Research Flow Control Center Kenneth Granlund, Air Force Research Laboratory Sidney Rowe, NASA Marshall Space Flight Center Fluid Dynamics Haoxiang Luo, Vanderbilt University Ron Hochstetler, Science Applications International Corporation Ground Testing Timothy Wadhams, CUBRC Karen Marais, Purdue University Christine Pastor-Barsi, NASA Glenn Scot Campbell, MIT Lincoln Laboratory Research Center Vincent Schultz, NASA Langley Research Center

www.aiaa-aviation.org 4 #aiaaAviation IntroContents

Welcome 3

Organizing Committee 4

Forum Overview 8

Sponsors 10

Keynote Speakers and Plenary Sessions 11 www.twitter.com/aiaa Forum 360 12

www.facebook.com/AIAAfan DEMAND FOR UNMANNED 15

www.youtube.com/AIAATV Special Sessions and Events 18

www.linkedin.com/companies/aiaa Networking Events 20

www.flickr.com/aiaaevents Recognition Events 21 http://livestream.com/AIAAvideo/ ITAR Information 24 AVIATION2016

www.instagram.com/aiaaerospace Exposition Hall 27

Exhibitors 29

Join the conversation! General Information 33 #aiaaAviation

Author and Session Chair Information 35 On-Site Wi-Fi Information Network Name: HHonors-Meeting Committee Meetings 36 Password: AIAA2016

Sessions at a Glance 39

Session Detail Matrix 48 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 Author and Session Chair Index 134 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 Venue Map Inside Back Cover Twitter @AIAA. www.aiaa-aviation.org 5 #aiaaAviation Get Your Conference Info on the Go!

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Participate in Session Polls 1. If Polls are available they will appear at the top of the page. Simply click/tap on a Poll to respond. 2. Choose your response(s) and hit “submit”. 3. After responding you will be able to see the results on your own device!* * Some Poll results may be hidden IntroForum Overview

SATURDAY/ MONDAY TUESDAY SUNDAY 11–12 June 13 June 14 June 0730 hrs Speakers’ Briefing in Session Rooms Speakers’ Briefing in Session Rooms

0800 hrs Plenary Plenary 0830 hrs

0900 hrs Networking Break Networking Break in Exposition Hall

0930 hrs 0845 hrs 1000 hrs Forum 360 Exposition 1030 hrs Hall Open Technical Technical Forum 360 Sessions Sessions 1100 hrs

1130 hrs Rising Leaders in Aerospace 1200 hrs Continuing Education 1230 hrs Courses Recognition Luncheon: 1300 hrs Lunch on Own Celebrating Achievements in Lunch on Own Fluid Dynamics Aerospace Sciences Award Lecture 1330 hrs

1400 hrs

1430 hrs Forum 360 Forum 360 Exposition 1500 hrs Hall Open Rising Technical Technical 1530 hrs Leaders in Sessions Sessions Aerospace Networking Networking Coffee Break 1600 hrs Speed Coffee Break in Exposition Hall Networking 1630 hrs and Plasmadynamics Aerodynamics Reception and Lasers Award Lecture 1700 hrs Award Lecture

1730 hrs

1800 hrs Student Reception Plenary Reception in Exposition Hall 1830 hrs (Sunday) 1900 hrs 1930 hrs

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WEDNESDAY THURSDAY FRIDAY 15 June 16 June 17 June

0730 hrs Speakers’ Briefing in Session Rooms Speakers’ Briefing in Session Rooms Speakers’ Briefing in Session Rooms

0800 hrs Plenary Plenary Plenary 0830 hrs

0900 hrs Networking Break in Exposition Hall Networking Break Networking Break

0930 hrs 0845 hrs 1000 hrs Forum 360 Forum 360 Exposition Forum 360 1030 hrs Hall Open Technical Technical Technical 1100 hrs Sessions Sessions Sessions 1130 hrs Rising Leaders in Aerospace 1200 hrs

1230 hrs Recognition Drag Luncheon: Prediction 1300 hrs Celebrating Workshop Drag Networking Luncheon Achievements Lunch on Own DEMAND for Prediction in Aircraft and DEMAND for UNMANNED Workshop 1330 hrs Atmospheric UNMANNED Systems

1400 hrs

1430 hrs Forum 360 Forum 360 1500 hrs Exposition Hall Open 1530 hrs Technical Technical Sessions Sessions Networking Networking 1600 hrs Coffee Break in Coffee Break Exposition Hall

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1700 hrs

1730 hrs Multidisciplinary DEMAND for Design Thermophysics Aerodynamic Measurement UNMANNED: Optimization Award Lecture Technology Award Lecture 1800 hrs Award Lecture Student Competition 1830 hrs Alpha Test

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2130 hrs

2200 hrs

www.aiaa-aviation.org 9 #aiaaAviation IntroSponsors

Exclusive Premier and Rising Leaders Speed Networking Sponsor

Platinum Sponsor

Executive Sponsor Livestream Sponsor

Lanyard Sponsor Student Reception Sponsor Sustaining Small Business and Tuesday Afternoon Coffee Break Sponsor

Gold Small Business Sponsors

Silver Small Business Sponsor Media Sponsors

www.aiaa-aviation.org 10 #aiaaAviation IntroKeynote Speakers and Plenary Sessions

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

Monday, 13 June Wednesday, 15 June 0800–0900 hrs International Ballroom (Center) 0800–0900 hrs International Ballroom (Center) The Second Century of Flight — Looking Back to Cybersecurity Look Forward Richard A. Clarke, Chairman & CEO, Good Harbor Security Michael Delaney, Vice President and General Manager, Airplane Risk Management, LLC Development, Boeing Commercial Airplanes

1730–1830 hrs International Ballroom (Center) Thursday, 16 June Making Dreams into Reality — The Epochal 0800–0900 hrs International Ballroom (Center) Stories That Deﬁne The Boeing Company The Ascent of (Un)manned Michael Lombardi, Director of Boeing Archives, The Boeing John S. Langford, Chairman and Chief Executive Officer, Company Aurora Flight Sciences Corporation

Tuesday, 14 June Friday, 17 June 0745 hrs International Ballroom (Center) 0800–0900 hrs International Ballroom (Center) Renewing Innovation in U.S. Aeronautics Concept to Reality — Our Journey to Congressman Steve Knight (R-CA), House Committee on Transforming Aviation Science, Space, and Technology Charles F. Bolden Jr., Administrator, NASA 0810–0900 hrs Balancing Innovation and Inspiration — The HondaJet Michimasa Fujino, President & CEO, Honda Aircraft Company

www.aiaa-aviation.org 11 #aiaaAviation Forum 360

1400–1600 hrs Cabinet Concepts to Reality — Airplane Development in a Global Environment Moderator: Ken Sanger, Vice President / General Manager, 787 Airplane Development, The Boeing Company Panelists: Luis Carlos Affonso, Chief Operating Officer, Commercial Aviation, Embraer S.A. These conversations will cover a spectrum of Simon Carlisle, Director, Strategy, Civil Aerospace, Rolls-Royce timely topics including programs, systems, policy, Tom Pelland, President, Engine & Environmental Control operations, applications, platforms and more! Systems, UTC Aerospace Systems Monday, 13 June Tuesday, 14 June 0930–1130 hrs International Ballroom (East) 0930–1230 hrs International Ballroom (East) Commercial Aviation — Solving the Disruption NASA Roadmaps — Guiding Direction for Challenge Aeronautics Research Investments Moderator: Ben Iannotta, Editor-in-Chief, Aerospace America Moderator: Richard A. Wahls, Strategic Technical Advisor – Advanced Air Vehicles Program, NASA Aeronautics Research Panelists: Mission Directorate, NASA Langley Research Center Jim Eck, Assistant Administrator for NextGen, FAA Panelists: Robert Pearce, Deputy Associate Administrator for Strategy, Office of the Associate Administrator for Aeronautics, NASA Mark Ballin, Technical Integration Manager, Airspace Operations and Safety Program, NASA Langley Research Bryan Quigley, Managing Director, United Airlines Flight Center Operations John Cavolowsky, Director, Airspace Operations and Safety Lance Sherry, Director, Center for Air Transportation Systems Program, NASA Aeronautics Research Mission Directorate, Research and Associate Professor, Systems Engineering and NASA Operations Research Department, George Mason University Fayette Collier, Manager, Environmentally Responsible Aviation Project, NASA Langley Research Center 1400–1600 hrs International Ballroom (East) Peter Coen, Manager, Commercial Supersonic Technology The Future of Education Project, NASA Langley Research Center Moderator: Todd W. Zarfos, Vice President, Engineering Jay Dryer, Director, Advanced Air Vehicles Program, NASA Functions, Boeing Commercial Airplanes Aeronautics Research Mission Directorate, NASA Barbara Esker, Deputy Director, Advanced Air Vehicles Panelists: Program, NASA Glenn Research Center Tara Chklovski, Founder and CEO, Iridescent Susan Gorton, Manager, Revolutionary Vertical Lift Technology Norman L. Fortenberry, Executive Director, American Society Project, NASA Langley Research Center for Engineering Education Jessica Nowinski, Detailee, Airspace Operations and Safety Alton D. Romig Jr., Executive Officer, National Academy of Program, NASA Engineering Jaiwon Shin, Associate Administrator, NASA Aeronautics Melissa Musgrave, Head of Employment, Airbus and Airbus Research Mission Directorate, NASA Group North America Barry Sullivan, Technical Integration Manager for LaRC Darryll J. Pines, Nariman Farvardin Professor of Aerospace Airspace Operations and Safety Program, NASA Ames Engineering and Dean, A. James Clark School of Engineering, Research Center University of Maryland Tom Davis, Technology Advisor, Airspace Systems Technology Program, Aviation Systems Division, NASA Ames Research Center

www.aiaa-aviation.org 12 #aiaaAviation IntroForum 360

1400–1600 hrs International Ballroom (East) 1400–1600 hrs International Ballroom (East) The Future of Military Aviation TTX Hot Wash and Cybersecurity Interactive Moderator: Tom Bell, Vice President, Global Sales & Marketing, Training Session Boeing Defense, Space & Security Following the TTX, teams will participate in a “hot wash” Panelists: session that will review the TTX’s learning objectives and results. Participants will gain further instruction and insights when Shawn Brimley, Executive Vice President and Director of a panel of thought leaders in cybersecurity, risk management, Studies, Center for New American Security threat assessment, and role-based training for cyber awareness Rear Admiral Donald Gaddis, U.S. Navy (Ret.) engage in discussion and answer questions. The day promises to Michael O’Hanlon, Senior Fellow, Foreign Policy, Brookings be both instructive and entertaining. Institution Moderator: David Shaw, Founder & CEO, Global Business Analysis Wednesday, 15 June Panelists: 0930–1130 hrs International Ballroom (East) Briguette Carstensen, Vice President & Director of Research, Global Business Analysis Cybersecurity Table Top War Gaming Exercise Barbara Endicott-Popovsky, PhD, Professor, University of Take part in a Table Top Exercise (TTX) focusing on the risks Washington Institute of Technology & Executive Director, and complexities cyber events/cyber incidents can have on Center for Information Assurance and Cybersecurity supply chain and supply chain management within the aviation Faye Francy, Executive Director, The Aviation ISAC domain. Participants will experience a facilitated Brown Paper Ilanko Subramaniam, GBA CISO, President, Global Business War Game that will allow them to participate as responders Analysis (Blue Team) or threat actors (Red Team) in order to better Russ Syphert, Senior Threat Analyst, Global Business Analysis understand the TTX process and provide them with the ability to discuss aviation-centric approaches to cybersecurity and risk management. During play, participants will be divided into sub teams representative of key functions within the supply chain domain and can expect to discuss topics such as threat actors, threat surfaces, and other cybersecurity issues. Participants are encouraged to return at 1400 hrs for an extended Hot Wash forum session with industry thought leaders in cybersecurity and the aviation domain. Those interested in becoming an active participant are expected to be present for the full two-hour morning session and will need to preregister. Those who wish to observe will also need to preregister. Preregister no later than 1600 hrs on Tuesday, 14 June, at www.surveymonkey.com/r/G22M7FF.

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Thursday, 16 June Friday, 17 June 0930–1130 hrs International Ballroom (East) 0930–1130 hrs International Ballroom (East) Restoring the Foundation of Aviation Hypersonic and Re-Entry Flight Testing — X-15 to Moderator: Gregory J. Bowles, Director, European Regulatory Space Shuttle and Beyond Affairs & Engineering, General Aviation Manufacturers Moderator: Sandra H. Magnus, Executive Director, AIAA Association Panelists: Panelists: Doug Cooke, Aerospace Consultant, Cooke Concepts Nicholas K. Borer, Principal Investigator, Aeronautics Systems and Solutions Analysis Branch, NASA Langley Research Center Colonel Lee Archambault, Chief Systems Engineer and Test Lowell Foster, Flight Test Engineer, FAA Small Airplane Pilot, Sierra Nevada Corporation; United States Air Force Certification (Ret.); and NASA Astronaut (Ret.) Rick Peri, Vice President, Government and Industry Affairs, Major General Joe H. Engle, United States Air Force, Air Aircraft Electronics Association National Guard (Ret.) and NASA Astronaut (Ret.) Andy Supinie, Director, Aerosciences, Textron Aviation John Olson, Vice President, Space Exploration Systems, Sierra Nevada Corporation 1400–1600 hrs International Ballroom (East) The session is being held in support of the AIAA Foundation. Participants are asked to consider a donation to the AIAA Aircraft Design and Testing—Today and Tomorrow Foundation for their educational programs that foster innovation Moderator: Irene M. Gregory, Senior Technologist for Advanced in science, technology, engineering, and mathematics. Control Theory and Applications, NASA Langley Research Center Panelists: Jay Brandon, Senior Research Engineer, Flight Dynamics Branch, NASA Langley Research Center Clay Harden, Principal Engineer, AAP Flight Sciences Integration, Gulfstream Alan Lawless, Chief Flight Test Engineer, Honda Aircraft Company Anthony Washburn, Langley Senior Technologist for Aerosciences, NASA Langley Research Center

www.aiaa-aviation.org 14 #aiaaAviation IntroDEMAND FOR UNMANNED

Steering Committee Richard Wlezien, Iowa State University Paramal H. Kopardekar, NASA Ames Research Center John S. Langford, Aurora Flight Sciences Corporation Michael S. Francis, United Technologies Research Center

This symposium brings together stakeholders from academia, government, and industry to identify research challenges Wednesday, 15 June that will lead to operational opportunities for the Unmanned 0930–1030 hrs International Ballroom (West) Aerial Systems (UAS) community. You will discover how UAS are catalysts for autonomy, robotics, and machine intelligence, The Changing Face of Aerospace: The Impact of UAS and how they have the potential to change the nature of civil on Aviation and military aviation. Applications for autonomous systems are untold as technology Visionaries see a future where UAS are used for myriad continues to improve. What advancements need to occur in purposes—ranging from enhancing public safety and welfare, order for unmanned systems and technologies to transform to expanding business opportunities that are limited only by flight and air transportation? Radio-controlled aircraft have our imaginations, to widened use in entertainment, sports, not received the same level of attention or caused anxiety like leisure, and recreation. UAS. What’s different about UAS? How much of the public If an era of unheralded UAS utilization is to happen, reaction is due to media hype? What steps need to be taken to significant advances in vehicle autonomy, autonomy of change public perception? operations, and the requisite machine intelligence need to Moderator: I. J. Hudson, Former Technology Reporter, NBC4 occur. The R&D community from traditional aerospace and Washington (WRC-TV) from other industry sectors such as information technologies, communication technology, robotics, and energy will need Panelists to step up to this challenge. Similarly, both the regulatory Michael S. Francis, Chief, Advanced Programs & Senior Fellow, and nonregulatory parts of the government have a significant United Technologies Research Center role to play. Furthermore, society must accept both the Parimal H. Kopardekar, Manager, Safe Autonomous System technologies and the legal and regulatory considerations Operations Project, and Principal Investigator, Unmanned and concerns. If and when these technical, legal, and Aerial Systems Traffic Management, NASA Ames Research societal changes occur, then the near ubiquitous presence Center of Unmanned Systems with all that they can offer will be realized. John S. Langford, Chairman and Chief Executive Officer, Aurora Flight Sciences Corporation Just as UAS are catalysts for advances in autonomy, machine Richard Wlezien, Professor and Vance and Arlene Coffman intelligence, and robotic solutions in aerospace, so too can Endowed Department Chair in Aerospace Engineering and AIAA be a catalyst for bringing together the R&D community Director, Iowa Space Grant Consortium, Iowa State University for purposes of networking, vetting of ideas, and presenting research plans and results to peers. DEMAND for UNMANNED Host: 1030–1130 hrs International Ballroom (West) Jay Gundlach, Founder and President, Flighthouse Engineering LLC Invention, Entrepreneurship, and Unmanned Systems How were, and are, early-stage technologies and systems developed and what lessons can be adopted to move from Announcing A New Competition! remotely piloted vehicles to fully autonomous systems The AIAA Unmanned Systems Program Committee is operations? pleased to be collaborating with Drone World Expo on a new Moderator: John Langford, Chairman and Chief Executive competition. The competition will help inform the end - user Officer, Aurora Flight Sciences Corporation community about emerging technologies or concepts related to autonomous aerial systems that are most likely to have an effect on their future businesses or operations. Winners will have the Break for Lunch opportunity to present their ideas to the end-user community during Drone World Expo, 15–16 November, San Jose, CA. 1130–1400 hrs More information about this competition will be available soon at www.aiaa-aviation.org/DEMANDforUNMANNED/. www.aiaa-aviation.org 15 #aiaaAviation IntroDEMAND FOR UNMANNED

1400–1500 hrs International Ballroom (West) 1600–1730 hrs International Ballroom (West) Perspectives on the Future of Autonomous Technology Roadmaps for Intelligent Systems and Technology Autonomous Systems How is society impacted by autonomous systems? Robots and Autonomy roadmaps for future technologies and operations autonomous systems are being increasingly integrated into will be presented and discussed. Research trends in futuristic modern society, on the battlefield, the road, and factory floor… robotic systems will be similarly be presented and discussed. in business, education, and health. Do they help or hinder? Who A roundtable discussion will ensue which ties these roadmaps is responsible when something goes wrong? and research trends back to recommendations made in the Mary Louise “Missy” Cummings, Associate Professor, NRC Autonomy Study report. Department of Mechanical Engineering and Materials Science, Moderator: Jay Gundlach, Founder and President, Flighthouse and Director, Humans and Autonomy Laboratory, Duke Engineering LLC, and author of several books on UAS University Presenters Mark G. Ballin, Technology Integration Manager, NASA 1500–1530 hrs International Ballroom (West) Airspace Operations and Safety Program The Autonomy “Dream” Sebastian Scherer, Systems Scientist, The Robotics Institute, Carnegie Mellon University As is pointed out in National Research Council’s “Autonomy Roundtable Panelists Research for Civil Aviation: Toward a New Era of Flight,” civil aviation is on the brink of potentially revolutionary Jay Gundlach, Founder and President, Flighthouse Engineering improvements in aviation capabilities and operations. Hurdles LLC and substantial barriers do exist and need to be overcome if the Mark G. Ballin, Technology Integration Manager, NASA autonomy revolution is to occur in aeronautics and in aviation. Airspace Operations and Safety Program One area that is of particular interest to this symposium and that John-Paul Clarke, Professor, Daniel Guggenheim School of requires substantial autonomous capabilities is UAS integration Aerospace Engineering, and Director, Air Transportation into the Next Generation National Airspace System. Laboratory, Georgia Institute of Technology John-Paul Clarke, Professor, Daniel Guggenheim School of Sebastian Scherer, Systems Scientist, The Robotics Institute, Aerospace Engineering, and Director, Air Transportation Carnegie Mellon University Laboratory, Georgia Institute of Technology

1530–1600 hrs International Ballroom (West) Thursday, 16 June 2016 DEMAND for UNMANNED Networking Coffee Break 0800–0900 hrs International Ballroom (Center) UAS Developments John S. Langford, Chairman and Chief Executive Officer, Aurora Flight Sciences Corporation

0900–0930 hrs Meeting Room Foyers AVIATION Forum Networking Coffee Break

Thursday, 16 June 1730–1900 hrs International Ballroom (Center) DEMAND for UNMANNED Student Competition Alpha Test Sponsored by: Teams from the University of Michigan, University of Maryland, and McKinley Technology High School in Washington, D.C., will use a UAV quadrotor to participate in a two-part competition that includes autonomy and manual flight skills.

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Thursday, 16 June 2016 1400–1545 hrs International Ballroom (West) 0930–1045 hrs International Ballroom (West) UAS Trafﬁc Management System Transformation in the National Airspace System NASA, working closely with the FAA, is using collaborative The National Airspace System (NAS) stands on the verge innovation to develop a UAS Traffic Management concept to of transformation. The convergence of robotics, intelligent safely enable UAS operations in low-altitude airspace. Bringing machines, autonomy, hybrid-electric propulsion methods, together interested parties from industry, government agencies advanced aeronautic design, and work-anywhere, be-anywhere and academia to discuss UAS challenges is an important culture is driving our society into a new era. This panel will step to accelerating the integration of UAS into the national discuss the transformations being driven by UAS, and potential airspace. End users will engage with the research, development, outcomes from the convergence of these driving technologies, and test community to discuss the challenges and needs of issues and events in our increasingly connected society. small UAS users and missions in this session. Moderator: Dallas Brooks, Director, Raspet Flight Research Session Chair: Parimal H. Kopardekar, Manager, Safe Laboratory, Mississippi State University and Co-Chair, FAA/ Autonomous System Operations Project, and Principal DoD/NASA/DHS Unmanned Aircraft System (UAS) Science Investigator, Unmanned Aerial Systems Traffic Management, and Research Panel NASA Ames Research Center Panelists Moderator: Gretchen West, Senior Advisor of Innovation John Cavolowsky, Director, Airspace Operations and Safety and Technology, Hogan Lovells and Advisory Board Member, Program, NASA Aeronautics Research Mission Directorate DroneWorld Expo Pete Dumont, Executive Director, ATCA Panelists Jonathan Evans, CEO, Skyward Gregory Agvent, Senior Director, News Operations, CNN Steven Pennington, Executive Director, DoD Policy Board on Sean Cassidy, Director, Strategic Partnerships, Amazon Prime Air Federal Aviation R. John Hansman, T. Wilson Professor of Aeronautics & Michael Singer, CEO, DroneView Technologies Astronautics and Director of the International Center for Air Transportation, MIT 1100–1215 hrs International Ballroom (West) Jesse Kallman, Director of Business Development & Regulatory ASSURE: FAA Center of Excellence for UAS Research Affairs, Airware Craig Marcinkowski, Director, Strategy and Business Panelists from the Alliance for System Safety of UAS through Development, Gryphon Sensors Research Excellence (ASSURE), the FAA’s Center for Ashok N. Srivastava, Chief Data Scientist, Verizon Excellence for UAS Research, will provide their perspectives about the technologies and operation procedures required to Peng Wei, Assistant Professor, Aerospace Engineering, Iowa make UAS operations safe in the NAS and the NextGen. State University Moderator: Sabrina Saunders-Hodge, NextGen R&D UAS Traffic Management System Integration Division Manager, Federal Aviation Administration session is presented by DRONE world e po Panelists 1545–1600 hrs International Ballroom (West) David Arterburn, Director, Rotorcraft Systems Engineering and Simulation Center, The University of Alabama in Huntsville DEMAND for UNMANNED Networking Coffee Break Mark Anthony Askelson, Associate Professor, University of North Dakota 1600–1700 hrs International Ballroom (West) Dallas Brooks, Director, Raspet Flight Research & Associate Director for Research, ASSURE FAA UAS Center of Visions of the Future Excellence (COE) Speakers will address their visions for Cognitive Assistance Major General James Poss (ret.), Executive Director, Alliance in Government and Public Sector Applications, Collaborative for System Safety of UAS through Research Excellence Operations in Denied Environments, and Human Factors/ (ASSURE) Human-Machine Interfaces as they pertain to UAS missions, Richard Stansbury, Associate Professor, Embry-Riddle UAS design, and the NextGen air traffic management systems. Aeronautical University Chuck Howell, Chief Engineer, Portfolio Programs and Integration, MITRE 1230–1400 hrs Jean-Charles Ledé, Program Manager, Tactical Technology Office, Defense Advanced Research Projects Agency (DARPA) Break for Lunch Dale Richards, Senior Research Fellow in Human Factors, Coventry University www.aiaa-aviation.org 17 #aiaaAviation IntroSpecial Sessions and Events

The multidimensional program features a leadership exchange/speed mentoring, panel session, Q&A with top industry leaders, and multiple RISING opportunities for networking. These exciting and energetic activities will LEADERS provide access to top aerospace leaders and their perspectives with subject inAEROSPACE matter relevant to your career.

Program Agenda

Monday 13 June Tuesday, 14 June 1500–1715 hrs International Ballroom (West) 1130–1230 hrs Georgetown East Speed Networking and Reception Why Work in Aerospace Instead of Silicon Valley Senior members of corporations and AIAA will be taking time Silicon Valley has been considered a leader in high tech to meet with the Rising Leaders participants and share their industries, innovation, and startups since the early 1900s. Many experiences. This event is a great way to get insight from top- young, eager, and ambitious persons have gone to Silicon Valley level officials and make some great new contacts. And, maybe, to be a “force” in their preferred field. But is Silicon Valley the they will end up being a mentor for more than just the 15 be all and end all of high tech innovation? Does the traditional minutes at this event. Don’t miss a terrific opportunity. aerospace industry have anything to offer? Immediately following the roundtable interchange with Come listen to what these panelists have to say. While senior members of the industry there will be a follow-on Silicon Valley will always be a force in high tech innovation, reception. This will allow for conversations to continue, or if learn what some are doing in partnership or in parallel. Learn a conversation was cut short, an opportunity to have a follow- how traditional aerospace is also making great advances in up discussion. It will also allow for a casual opportunity to cutting-edge research. meet the other young professionals who are attending the Moderator: Craig McGrath, Product Development, Boeing conference. Having just participated in the speed networking, Commercial Airplanes you’ll definitely have at least one thing in common. Panelist: Don’t miss a terrific opportunity. Tony Springer, Director, Integration and Management Office, Senior Mentors NASA Mark Ballin, NASA Langley Research Center Brad Belcher, Rolls-Royce Wednesday, 15 June John Cavolowsky, NASA Peter Coen, NASA Langley Research Center 1130–1230 hrs Columbia 9 Fayette Collier, NASA Innovations, Technology, and Skills for the Next Peggy Cornell, NASA Glenn Research Center 100 Years in Aerospace Michael Corcoran, The Boeing Company Greg Hyslop, Senior Vice President, Engineering, Test & Barbara Esker, NASA Technology, The Boeing Company Matthew Hutchison, Aurora Flight Sciences Sally Johnson, Adaptive Aerospace group, Inc. Dean Jorgensen, Space Electronics Art Mallett, Dunmore Corporation Jayant Ramakrishnan, Bastion Technologies David Riley, Boeing Engineering Operations and Technology Lisa Teague, Rolls-Royce Gregor Veble Mikic, Joby Aviation Richard Wahls, NASA Langley Research Center

Speed Networking Sponsor:

www.aiaa-aviation.org 18 #aiaaAviation IntroSpecial Sessions and Events

Thursday and Friday, 16–17 June Thursday, 0930–1715 hrs Lincoln West Reception: Thursday, 1745–2000 hrs International Terrace Friday, 0930–1630 hrs Conference: Friday, 0700–1630 hrs International Ballroom (West) 6th AIAA CFD Drag Prediction Workshop Regional Leadership Conference Sponsored by the Applied Aerodynamics Technical Committee The 2016 Regional Leadership Conference (RLC) is a great The focus of this workshop will be the NASA Common Research opportunity to introduce new section officers and deputy Model (CRM) with wind-tunnel measured wing twist; both directors to the Institute’s resources and programs. In addition, wing-body and wing-body-pylon-nacelle configurations will meet fellow officers from many different sections within AIAA be considered. CFD predictions of absolute and incremental and learn about the types of activities they hold. AIAA Regions force and moment values will be examined and compared. The and Sections vary in size from a few dozen to many hundreds of workshop will include grid convergence and code verification people. You may hear about activities that you want to try in your studies. Additionally, an angle-of-attack sweep with static section, or you may be able to provide assistance to a section that aero-elastic deformations will be considered. Grids will be made is having difficulty in a particular area. You will also learn how available for all required cases. your officer role fits into the overall AIAA hierarchy. Many of Optionally, participants are invited to perform solution- the presentations are made by members of the AIAA Board and adaptation calculations and/or a coupled aero-structural the conference is presided over by the Vice President, Member simulation of the CRM wing-body configuration. A finite Services. element model will be made available to participants to calculate The conference kicks off with an evening reception where twist/deflection due to aerodynamic load. attendees can mingle and discuss activities with other officers The objectives of this workshop will be to: and AIAA Board members. So if you are a new AIAA officer or a veteran who would like to get a refresher, meet new people, or • To assess the state-of-the-art computational methods as see what the latest innovations at AIAA are, plan to attend the practical aerodynamic tools for aircraft force and moment Regional Leadership Conference. prediction of industry relevant geometries. • To provide an impartial forum for evaluating the effectiveness of existing computer codes and modeling techniques using Navier-Stokes solvers. • To identify areas needing additional research and development. You must be registered for AIAA AVIATION 2016 to participate in the 6th AIAA CFD Drag Prediction Workshop. There is no additional workshop registration fee.

www.aiaa-aviation.org 19 #aiaaAviation IntroNetworking Events

Understanding the importance of networking with colleagues new and old, a series of activities have been planned that will help you connect with current colleagues and new acquaintances. Student Welcome Reception Welcome Reception Sunday, 12 June International Ballroom (West) Tuesday, 14 June Exposition Hall, Columbia 1800–1930 hrs 1730–1900 hrs Mingle with your peers and hear from AIAA Executive Take this opportunity to engage new contacts and refresh old Director Sandy Magnus. This reception provides you with the ones. A ticket for the reception is required and included in the opportunity to meet your fellow students and learn more about registration fee where indicated. Additional tickets for guests the opportunities available to you as an AIAA student member. may be purchased upon registration or on site. Sponsored by Networking Luncheon Networking Coffee Breaks Wednesday, 15 June International Ballroom (Center) 1230–1400 hrs Networking coffee breaks allow even more time for making A ticket for the luncheon is required and included in the new contacts, continuing discussions from sessions, visiting registration fee where indicated. Additional tickets for guests the Exposition Hall, or checking emails and voicemails to keep may be purchased upon registration or on site. in touch with the office while you are at the forum. Networking coffee breaks will be held at the following locations and times: Monday, 13 June 0900–0930 hrs and 1600–1630 hrs; Meeting Room Foyers Tuesday, 14 June 0845–0930 hrs and 1600–1630 hrs; Exposition Hall

Afternoon Coffee Break Sponsor:

Wednesday, 15 June 0845–0930 hrs and 1600–1630 hrs; Exposition Hall Thursday, 16 June 0900–0930 hrs and 1600–1630 hrs; Meeting Room Foyers Friday, 17 June 0900–0930 hrs; Meeting Room Foyers

www.aiaa-aviation.org 20 #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, 13 June Fluid Dynamics Award 1300–1400 hrs Cabinet Moshe Matalon Fluid Dynamics Award Lecture Caterpillar Distinguished Professor Department of Mechanical Science and Engineering e Hydrodynamic eory of Premixed Flames: University of Illinois at Urbana-Champaign Laminar to Turbulent Propagation “For contributions to the development of combustion theory, for revolutionizing understanding of chemically reacting flows, and for Moshe Matalon, Caterpillar Distinguished Professor, work on the hydrodynamic theory of premixed flames.” Department of Mechanical Science and Engineering, University of Illinois at Urbana-Champaign Ground Testing Award Zonglin Jiang 1630–1730 hrs Cabinet Professor, Institute of Mechanics Chinese Academy of Sciences Aerodynamics Award Lecture “For skillful leadership in conceiving, developing and successfully commissioning the world’s largest shock tunnel capable of true Some Applications of Computational Fluid hypersonic flight simulation.” Dynamics to Entry and Landing of the Mars Science Laboratory Losey Atmospheric Sciences Award Pieter Buning, Aerospace Technologist, NASA Langley Research William L. Smith Center Professor Emeritus, Department of Atmospheric and Oceanic Sciences, University of Wisconsin-Madison Distinguished Professor, Department of Atmospheric and Tuesday, 14 June Planetary Sciences, Hampton University 1230–1400 hrs International Ballroom (Center) “For visionary and pioneering ultraspectral resolution sounding techniques used for current and future polar satellite advanced Recognition Luncheon: Celebrating Achievements infrared sounding systems for improved weather forecasting.” in Aerospace Sciences Plasmadynamics and Lasers Award A ticket for the luncheon is required and included in the Eric J. Jumper registration fee where indicated. Additional tickets for guests Roth-Gibson Professor of Aerospace and Mechanical may be purchased upon registration or on site. Engineering The following awards will be presented: University of Notre Dame Aerodynamics Award “For major contributions in the fields of aero-optics, chemical lasers, and laser-supported detonation, and for the mentoring of Pieter Buning young engineers and scientists.” Aerospace Technologist NASA Langley Research Center Thermophysics Award “In recognition of exceptional leadership, innovation and expertise George Cunnington in the field of overset grid CFD methods and applications that CEO are used internationally for widespread advancements in the Cunnington and Associates aerodynamic design and development of air and space vehicles.” “For lifelong contributions to the development of thermal Aerodynamic Measurement Technology Award protection systems, multilayer cryogenic insulation systems, and radiative heat transfer analysis techniques.” Alan C. Eckbreth Management/Engineering Consultant Certiﬁcates of Merit: “For seminal contributions to the emerging field of laser Aerodynamic Measurement Technology Best Paper diagnostics for combustion, especially for his work in coherent anti-Stokes Raman scattering (CARS) spectroscopy.” AIAA Paper 2016-0791, “Time-Resolved PIV in a Shock Tube,” Justin Wagner, Steven Beresh, Edward Demauro, Katya Casper, Daniel Guildenbecher, Brian Pruett, and Paul Farias, Sandia National Laboratories. (continued) www.aiaa-aviation.org 21 #aiaaAviation Recognition Events

Tuesday, 14 June (continued) Wednesday, 15 June Applied Aerodynamics Best Paper 1730–1830 hrs International Ballroom (East) AIAA Paper 2015-2718, “Origins and Further Development Mutidisciplinary Design Optimization Award Lecture of the Jameson-Schmidt-Turkel Scheme,” Antony Jameson, Stanford University. A 30-Year Retrospective of Structural and David Weaver Best Student Paper Multidisciplinary Optimization Robert (Bob) A. Canfield, Professor & Assistant Department AIAA Paper 2016-0509, “Heat Transport in Aqueous Head for Academic Affairs, Virginia Polytechnic Institute and Suspensions of Alumina Nanoparticles,” Murali Gopal State University Muraleedharan, Dilip Srinivas Sundaram, and Vigor Yang, Georgia Institute of Technology. Fluid Dynamics Best Paper 1730–1830 hrs Lincoln West AIAA Paper 2016-1062, “An Overview of Combined Uncertainty and A-Posteriori Error Bound Estimates for CFD Calculations,” Thermophysics Award Lecture Timothy Barth, NASA Ames Research Center. Measurement of ermophysical Properties Ground Testing Best Paper from 4 to 4,000K AIAA Paper 2015-2861, “Unsteady Low-Speed Wind Tunnel George Cunnington, CEO, Cunnington and Associates Design,” David Greenblatt, Technion—Israel Institute of Technology. Modeling and Simulation Best Paper AIAA Paper 2015-2653, “A Bifurcation Study of a Dynamic Model of a Nose Landing Gear Mechanism Subjected to External Disturbances,” James Knowles, Loughborough University. Plasmadynamics and Lasers Best Student Paper AIAA Paper 2016-1698, “Development of a Cavity Enhanced Thomson and Raman Scattering Diagnostic,” Adam Friss, Christopher Limbach, and Azer P. Yalin, Colorado State University. Thermophysics Best Paper AIAA Paper 2016-1981, “Spectral, Directional Emittance at Elevated Temperatures for Various Materials,” Michael Winter, Robert Bickel, Dusan Sekulic, Helmut Koch, Bradley Butler, and Hai Fu, University of Kentucky.

1630–1730 hrs International Ballroom (East) Plasmadynamics and Lasers Award Lecture Aero-Optics: A Photon Odyssey Eric J. Jumper, Roth-Gibson Professor of Aerospace and Mechanical Engineering, University of Notre Dame

(continued) www.aiaa-aviation.org 22 #aiaaAviation IntroRecognition Events

Thursday, 16 June Multidisciplinary Design Optimization Award Rakesh K. Kapania 1230–1400 hrs International Ballroom (Center) Mitchell Professor of Aerospace Engineering, Department of Aerospace and Ocean Engineering Recognition Luncheon: Celebrating Achievements Virginia Polytechnic Institute and State University in Aircraft and Atmospheric Systems “For significant contributions in the MDO of truss-braced A ticket for the luncheon is required and included in the aircraft, efficient supersonic air vehicles, and pioneering the registration fee where indicated. Additional tickets for guests MDO of wings with curvilinear Spars and Ribs.” may be purchased upon registration or on site. Piper General Aviation Award The following awards will be presented: Gregor Veble Mikic Aircraft Design Award Chief Aerodynamicist Joby Aviation Navy X-47B Unmanned Combat Air System Carrier Tine Tomazic Demonstration Program (UCAS-D) Team Director of R&D Department of the Navy Pipistrel Award accepted by RADM Mathias Winter, Program Executive “For leadership in the research, design and development, and Officer for Unmanned Aviation and Strike Weapons testing of practical marketable electric general aviation aircraft “In recognition and sincere appreciation of the significant advances concepts.” to the state of the art in autonomous aircraft operations on a carrier and in the aerial refueling environment that have been 1730–1830 hrs International Ballroom (East) demonstrated by the Navy X-47B UCAS-D and enabled by this very successful aircraft design.” Aerodynamic Measurement Technology Award Gardner-Lasser Aerospace History Literature Award Lecture Monique Laney Assistant Professor of History CARS – e First Twenty Years Auburn University Alan C. Eckbreth, Management/Engineering Consultant German Rocketeers in the Heart of Dixie: Making Sense of the Nazi Past During the Civil Rights Era

Hap Arnold Award For Excellence in Aeronautical Program Management Paul R. Adams President (Ret.) Pratt & Whitney, United Technologies Corporation “For exceptional program management and leadership in the engineering, development, and production of game-changing technological products, including Pratt & Whitney’s PurePower Geared Turbofan™ engine.”

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

A limited number of papers will be presented in “U.S. Only” technical sessions during the conference. In addition to your forum registration, a separate registration process is required ITAR to attend these restricted sessions. All individuals must bring the required documentation with them to the ITAR registration desk, most importantly is proof of U.S. Citizenship or Resident Alien Status. (Please note that a CAC card IS NOT official proof of U.S. Citizenship.) Please Information see the detailed information on the ITAR Registration Grid below to determine your individual requirements.

Access to ITAR Sessions: Presenting a Paper, Chairing a Availability of Manuscripts from ITAR-Restricted Sessions Session, or Attending an ITAR-Restricted Presentation For those who are registered to attend the ITAR sessions, a Admittance to the restricted technical program is controlled by DVD containing the papers from the ITAR sessions will be the U.S. International Traffic in Arms Regulations (ITAR). All available for purchase on site at the forum for $25. Those attendees, presenters, and session chairs will need to register for the purchasing the DVD must be available to pick it up on Friday, conference, and then visit the ITAR registration desk to complete 17 June 2016, between 0900-1230 hrs at the ITAR Registration the additional processes. Anyone wishing to enter the restricted Desk. All DVDs must be picked up in person. There will be no session room MUST abide by the procedures and submission of sale or distribution of these papers after the event. verified documents mandated by the DoD. No Exceptions! ITAR Badges must be worn during the sessions. Security will be checking ITAR Electronics Policy photo IDs upon entrance to the ITAR session rooms. No phones, computers (other than the presenter), iPads, cameras, Fitbits, or other electronic devices with cameras, recording or two-way transmission 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. Large briefcases and bags will also need to be checked at the desk. 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 Trac in Arms Regulations). If you plan to aend any presentations restricted by ITAR, you must bring proof of citizenship PLUS the other verication documents as shown below. Please note that only U.S. Citizens and U.S. Resident Aliens can be considered for aendance at these restricted presentations. Admiance to restricted sessions and access to restricted technical papers is implemented and controlled by ITAR . All restricted session aendees (including speakers and session chairs for these sessions) MUST abide by the procedures and submial of verication documents as noted below – NO EXCEPTIONS: ATTENDEE CLASSIFICATION IDENTIFICATION & PROOF OF EMPLOYMENT REQUIREMENTS U.S. Government Employees 1. Proof of U.S. Citizenship (for example, passport, birth certicate, voters registration card, naturalization papers), AND 2. Personal photographic identication: U.S. Government/Military Photo ID badge, such as CAC card U.S. Citizens 1. Proof of U.S. Citizenship (for example, passport, birth certicate, voters registration card, naturalization papers), AND 2. Personal photographic identication (passport, driver’s license, etc.), AND 3. Certication credentials based on DD Form 2345 (see below for details) Resident Aliens (U.S.) 1. Resident Alien Card, AND 2. Personal photographic identication (passport, driver’s license, etc.), AND 3. Certication credentials based on DD Form 2345 (see below for details)

DD Form 2345 individual certication 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 Qualied 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 Qualied 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 Qualied U.S. Contractor List.

How to get your ITAR Clearance: Bring all of the above listed identication, proof of employment and certication credentials to the AIAA ITAR Registration Desk in the AIAA Registration area. Your documents will be veried and you will be provided with a stamp indicating your ITAR clearance. Photo ID will be checked against your ITAR badge before admiance 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 24 #aiaaAviation BUILDING THE FOUNDATION FOR INNOVATION. AT LOCKHEED MARTIN, WE’RE ENGINEERING A BETTER TOMORROW. At Lockheed Martin, we know that innovation and creativity are critical to solving the world’s most complex challenges, whether in the air, on land, at sea, or in space. We are proud to be a platinum sponsor of AIAA Aviation 2016, and salute its important mission to bring industry together to address these challenges. We look forward to continuing our longstanding relationship with the AIAA – a commitment that began with Lockheed Martin and our heritage companies more than 50 years ago.

Learn more at lockheedmartin.com

Leave everything else behind. The HondaJet won’t just get you there faster; it will do it with a level of comfort that makes getting there as exciting as the destination. Escape the gridlock. hondajet.com IntroExposition Hall

T1 1 2 3 4

LaVision Triumph Inc. Inc.

Exhibitor 101 103 105 107 109 111 113 115 117 11 & Sales Offﬁce Lounge EXIT EXIT

Wineman Ennova Technology, Inc.

ION NASA 112 114 120 L EXIT I Comsol V , . Inc. PA ENTRANCE 201 207 213 215 219 A A I A EXIT EXIT

AeroSoft MathWorks Cambridge University Inc. University of Kansas Press 202 204 206 208 210 212 214 216 218

AIAA

T Concord 9101112 T Lift T T

Exhibitors by Booth Number (êindicates AIAA Corporate Members)

113 ESTECO 105 Aerion Technologiesê 103 Exa Corporation 216 AeroSoft 214 Kamatics RWG T-3 AIAA Career Solutions 115 LaVision, Inc. 202 Altair ê 218 MathWorks 111 ANSYS, Inc. 207 NASA Aeronautics 109 Applied Dynamics, International (ADI) 119 PCB Piezotronics 121 Aurora Flight Sciences ê 210 Photron 212 BETA CAE Systems USA, Inc. 101 Pointwise, Inc. ê 201 The Boeing Company ê 213 SmartUQ 220 Cambridge Universtiy Press 107 Tecplot, Inc. ê 215 Comsol, Inc. 117 Triumph Aerospace Systems T-6 Concord Lift 222 University of Kansas Short Course Program 219 Cradle North America, Inc. 120 Vision Research 204 DARcorporation ê 114 Wineman Technology, Inc. 208 dSPACE ê 206 XFlow CFD 112 Ennova Technologies

www.aiaa-aviation.org 27 #aiaaAviation IntroExposition Hall

The Exposition Hall is the hub of activity during this event—from seeing exhibitor displays to enjoying networking breaks and other functions. All the major networking events are held in the Exposition Hall to give attendees and exhibitors an opportunity to connect with partners, industry thought leaders, and collaborators who can help move your business forward. The Exposition Hall is located in the Columbia room. Exposition Hall Hours Charging Stations

Tuesday, 14 June 0845–1200 hrs; 1330–1630 hrs; Recharge your mobile device while networking with exhibitors. Reception*, 1730–1900 hrs Quadcopter Rafﬂe Wednesday, 15 June 0845–1200 hrs; 1400–1630 hrs Enter to win one of two quadcopters! Complete the raffle ticket *A ticket is required and included in the registration fee where (behind your registration badge) and drop it in the boxes in indicated the Exposition Hall, or drop in a business card. Winner will be notified by email and does not need to be present to win.

AIAA Pavilion Stop by the AIAA Pavilion, located in the Exposition Hall, AIAA Foundation to browse publications and merchandise, learn about your Come visit us in the AIAA Pavilion. Did you know that the membership benefits, and meet AIAA staff. AIAA Foundation is celebrating its 20th anniversary? As we celebrate this milestone anniversary, we are asking all our 30% Off All Books at AIAA AVIATION 2016 members to join with us as we set out to accomplish an amazing AIAA Publications is offering a special show discount on all feat: to inspire all members to donate at least $20 each, with a titles featured at AIAA AVIATION 2016. Attendees can take goal of raising $200,000. In addition, we are hosting a Silent advantage of a 30% discount off the list price of all books for sale Auction with some cool aerospace items for bid. Come to the at the AIAA Bookstore located in the AIAA Pavilion. This show AIAA Pavilion and check it out! And to show support for the special will only be available during the forum! Take advantage AIAA Foundation, the Institute will match donations, up to $1 of these super savings and visit the AIAA Bookstore. million in unrestricted funds…doubling the impact of every donation. With your help and donation, we can reach our goal Meet the Author Sessions and continue to inspire and support the next generation of aerospace professionals. Jay Gundlach Civil And Commercial Unmanned Aircraft Systems Tuesday, 14 June AIAA Exposition Hall Pavilion Welcome Reception; 1730–1900 hrs

Leland Nicolai Lessons Learned: A Guide to Improved Aircraft Design AIAA Exposition Hall Pavilion Tuesday, 14 June Networking Coffee Breaks 0845–0930 hrs and 1600–1630 hrs Wednesday, 15 June Networking Coffee Break 0845–0930 hrs

www.aiaa-aviation.org 28 #aiaaAviation Exhibitors

Aerion Technologies (formerly Desktop Aeronautics) 105 ANSYS, Inc. 111 1900 Embarcadero Road 2600 ANSYS Drive Suite 101 Cannonsburg, PA 15317 Palo Alto, CA 94303 www.ansys.com www.aerion-tech.com [email protected] [email protected] ANSYS, Inc. develops and globally markets engineering Aerion Technologies (formerly Desktop Aeronautics) creates simulation software used by designers and engineers tools for aerodynamic design and analysis of aerospace across the aerospace and defense industry. Our open and vehicles. Our flagship product, GoCart, is an intuitive aerial flexible simulation solutions enable users to simulate design vehicle design tool built around NASA’s renowned Cartesian performance using an open platform for fast, efficient and Euler CFD solver, Cart3D. Our customer list includes the cost-effective product development. major players from the aerospace and defense industry.

AeroSoft Inc. 216 Applied Dynamics International 109 3800 Stone School Road 2000 Kraft Drive Ann Arbor, MI 48108-2499 Suite 1400 www.adi.com Blacksburg, VA 24060 [email protected] www.aerosoftinc.com [email protected] Applied Dynamics helps companies make better use of AeroSoft specializes in high-fidelity numerical algorithms for simulation assets through all stages of product development, aerodynamic simulation and design. Services include licensing, verification testing, demonstration, training, and maintenance. training and support of GASP, our premier structured and Our user base includes more than 50% of the Fortune 500 unstructured flow solver, as well as detailed analysis of aerospace and defense companies and extends into marine, customer applications and customized solutions. Come by and power systems, oil & gas, and the automotive industry. see what’s new with GASP Version 5.2. Aurora Flight Sciences 121 AIAA Career Center T-3 9950 Wakeman Drive 1430 Spring Hill Rd Manassas, VA 20110 Floor 6 www.aurora.aero McLean, VA 22102 Aurora Flight Sciences has over 25 years developing careercenter.aiaa.org [email protected] innovative, highly capable unmanned aircraft for national security requirements. From our Optionally Piloted Centaur, Our members are leaders in the field, making meaningful to our 5-day endurance Orion RPA, and our new DARPA contributions in all areas of aerospace… Aeronautics, VTOL X-Plane Technology Demonstrator, Aurora delivers! Education & Workforce, Energy & Environment, National Contact us for an in-depth discussion of our solutions. Aurora Security, Space, Grassroots Programs, State Affairs, is currently hiring – “Come Build The Future With Us” Constituent Action Center, Policy Papers. Start connecting with members today to fill your talent acquisition needs. BETA CAE Systems USA, Inc. 212 29800 Middlebelt Road Altair 202 Suite #100 1820 E Big Beaver Road Farmington Hills, MI 48334 Troy, MI 48083 www.ansa-usa.com www.altair.com [email protected] [email protected] BETA CAE Systems is an engineering services company that Altair is a leader in developing simulation-driven designs for distributes & supports the industry leading ANSA & META leading aerospace customers. Our world-class optimization software. ANSA is CAE pre-processing tool for FE & CFD methods provide designs that are lower weight, higher quality, Analysis, for full-model build, from CAD to solver input file, and have better performance vs. traditional designs. 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 29 #aiaaAviation Exhibitors Boeing 201 Cradle North America, Inc. 219 7755 E. Marginal Way S 50 Chestnut Street Mail Code 1W-02 Suite A-214 Seattle, WA 98108 Beavercreek, OH 45440 www.boeing.com/bts www.cradle-cfd.com [email protected] Boeing is the world’s leading aerospace company, and employs more than 169,000 people around the world. Cradle is a leading provider of Computational Fluid Dynamics Boeing Technology Services (BTS) is the point of access to (CFD) software including SC/Tetra (general purpose more than 500 testing facilities across the US. BTS contracts unstructured mesh), scSTREAM (general purpose Cartesian with companies, educational institutions, and government mesh), and HeatDesigner (Cartesian mesh for electronics). organizations for use of Boeing laboratories. Since 1984, Cradle has established itself as a major innovator for advancing the role of simulation in engineering design. Cambridge University Press 220 32 Avenue of the Americas DARcorporation 204 New York, NY 10013 1440 Wakarusa Drive www.cambridge.org/us/academic Lawrence, KS 66049 [email protected] www.darcorp.com [email protected] Cambridge’s publishing in books and journals combines state- of-the-art content with the highest standards of scholarship, DARcorporation (Design, Analysis and Research Corporation) writing and production. Visit our stand to browse new titles, is an aeronautical engineering firm, located in Lawrence, available at a 20% discount, and to pick up sample issues of Kansas, that has been offering aeronautical engineering our journals. Visit our website to see everything we do: www. consulting services, software and books since 1991. cambridge.org/us/academic. dSPACE 208 Comsol Inc. 215 50131 Pontiac Trail 100 District Avenue Wixom, MI 48393-2020 Burlington, MA 01803 www.dspaceinc.com www.comsol.com [email protected] [email protected] COMSOL Multiphysics® is an integrated software environment dSPACE is the world’s leading provider of hardware and for creating physics-based models and simulation apps. software tools for developing and testing sophisticated A particular strength is its ability to account for coupled electronic control systems. dSPACE systems play a vital role in or multiphysics phenomena. Interfacing tools enable the product innovation industries. Learn more at: www.dspaceinc. integration of COMSOL Multiphysics® simulations with all com. major technical computing and CAD tools on the CAE market. Ennova Technologies 112 Concord Lift T-6 2150 Allston Way Suite 250 Ennova PO Box 28205 Scalable Simulation Delivered Baltimore, MD 21234 Berkeley, CA 94704 www.concordlift.com www.ennova-cfd.com [email protected] [email protected] This is a “thought experiment” for a low cost per ton mile Leading edge grid generation software for computational competitor for truck, train, ship cargo with fast direct airborne fluid dynamics (CFD). Automated mesh generation for service. ConcordLift develops theoretical studies on practical unstructured, structured and hybrid grids for internal and problems and develops workable cost effective solutions. external flows.

www.aiaa-aviation.org 30 #aiaaAviation IntroExhibitors ESTECO 113 MathWorks 218 39555 Orchard Hill Place #457 3 Apple Hill Drive Novi, MI 48375 Natick, MA 01760 www.esteco.com www.mathworks.com [email protected] The MATLAB and Simulink product families are ESTECO is a pioneer in numerical optimization fundamental applied math and computational tools at the solutions, specializing in the research and development world’s educational institutions. Adopted by more than 5000 of engineering software for all stages of the simulation- universities and colleges, MathWorks products accelerate the driven design process. ESTECO’s top-class products, pace of learning, teaching, and research in engineering and modeFRONTIER and SOMO, are used worldwide, helping science. MathWorks products also help prepare students for companies increase efficiency in design simulation and careers in industry worldwide, where the tools are widely accelerate product innovation. used for data analysis, mathematical modeling, and algorithm development in collaborative research and new product development. Exa Corporation 103 55 Network Drive Burlington, MA 01803 NASA Aeronautics 207 www.exa.com NASA Headquarters [email protected] 300 E Street, SW Washington, D.C. 20546 Exa Corporation offers a full suite of CFD/CAE simulation www.nasa.gov/aeronautics design optimization software applications with aerodynamic, thermal and aeroacoustic simulation capabilities in addition to NASA Aeronautics is poised to transform aviation. Hear the engineering consulting services. Exa’s products and services difference in noise of current aircraft vs. future hybrid wing enable engineers to integrate simulation early in the design body, and today’s sonic boom vs. tomorrow’s quiet “thump.” process, therefore creating competitive designs, shortening Try your hand at making a UAV detect and avoid other product design cycles and speeding time-to-market. aircraft. Experience 3D view of future aircraft concepts/X- planes. Learn about our next flight test campaign for an aircraft spacing tool. Kamatics/RWG 214 1330 Blue Hills Ave Bloomﬁeld, CT 06002 PCB Piezotronics 119 www.kaman.com/engineered 3425 Walden Ave [email protected] Depew, NY 14043 www.pcb.com For decades, Kamatics (USA) and RWG have been designing, PCB Piezotronics, the pioneer of ICP® technology, designs testing, and manufacturing the highest performing bearings and manufactures microphones, vibration, force, torque, and flight critical parts in the industry, excelling under the load, strain, and pressure sensors to withstand the demanding most demanding conditions. requirements of the Aerospace & Defense industry. PCB provides sensors for applications such as ground vibration LaVision, Inc. 115 testing, flight testing, wind tunnel testing, and modal analysis. PCB® proudly stands behind their products with a Total 211 W. Michigan Avenue, Suite 100 Customer Satisfaction guarantee, which includes the Platinum Ypsilanti, MI 48197 Stock Sensors program. Platinum Stock Sensors ship the same www.lavisioninc.com [email protected] day and are backed by 24/7 customer support and a lifetime warranty. LaVision Inc. provides integrated laser imaging systems to scientific, industrial, government and educational markets. LaVision has extensive professional experience in optical Photron 210 techniques such as digital image correlation (DIC) for 9520 Padgett Street, Suite 110 deformation and strain measurement, 2-D, Stereo, and San Diego, CA 92126 Tomographic Particle Image Velocimetry (PIV), gaseous and www.photron.com liquid laser induced fluorescence (LIF), shadowgraphy for [email protected] multi-phase flows, high-speed and ultra-high-speed imaging and intensified camera systems. Photron’s wide range of light sensitive high-speed cameras including systems ideally suited to PIV and DIC, mega pixel to 21,000 frames per second (fps) and 4M pixels producing HD to 2,000 fps. Photron has a slow motion camera for every application. www.aiaa-aviation.org 31 #aiaaAviation IntroExhibitors Pointwise, Inc. 101 University of Kansas Short Course Program 222 213 S. Jennings Avenue 12600 Quivira Road Fort Worth, TX 76104 Overland Park, KS 66213 www.pointwise.com www.aeroshortcourses.ku.edu [email protected] [email protected]

Pointwise, Inc. is solving the top problem facing engineering A global leader in aerospace professional development and analysts today: mesh generation for computational fluid training. Offering 50+ short courses and Certificates of dynamics. Manufacturing firms and research organizations Specialization in Aerospace Compliance, Aircraft Design, use Pointwise’s mesh generation software to seamlessly bridge Aircraft Maintenance and Safety, Aircraft Structures, Avionics the gap between CAD and computational fluid dynamics and Avionic Components, Electromagnetic Effects, Flight analysis. Find more information at pointwise.com. Tests and Aircraft Performance, and Unmanned Aircraft. Reach your goals faster with the KU Aerospace Short Course Program. SmartUQ 213 1245 E. Washington Ave Vision Research 120 Suite 210 Madison, WI 53703 Quantify Every Uncertainty. 100 Dey Road www.smartuq.com Wayne, NJ 07470 [email protected] www.phantomhighspeed.com [email protected] SmartUQ software provides breakthrough analytics and uncertainty quantification solutions for simulation and testing. Vision Research designs and manufactures the award-winning Using advanced statistics and stochastic methods, SmartUQ Phantom® brand of digital high-speed cameras. The Phantom allows engineers to quickly analyze Big Data, understand the v2512 is capable of acquiring over 25,000 one-megapixel probabilities of all what-if scenarios, accelerate simulation frames each second. Learn how this camera can help you cycles, easily calibrate models, and create innovative designs advance your understanding of the physical world you work in with greater confidence. and the physics of the universe. Visit booth #120.

Tecplot, Inc 107 Wineman Technology, Inc. 114 3535 Factoria Blvd SE, Suite 550 1668 Champagne Drive North Bellevue, WA 98006 Saginaw, MI 48604 www.tecplot.com www.winemantech.com [email protected] [email protected] With 35 years of experience and more than 47,000 users At Wineman Technology, we bring clarity to complex worldwide, Tecplot offers the fastest and most versatile test challenges with more than 25 years of expertise in desktop visual data analysis tools on the market. Whether dynamometer and hydraulic test systems, real-time control performing simulations, analyses or experiments, you can and data acquisition, hardware-in-the-loop simulation, and quickly explore your data and present high-quality images and custom test machines. Our engineers become an extension animations exactly the way you want – and it’s easy. to your team, meeting your specific challenges and goals and ultimately delivering a test system that mitigates your risk, propels your business forward, and supports your company as Triumph Aerospace Systems 117 it grows. 703 City Center Boulevard Newport News, VA 23606 www.triumphgroup.com XFlow CFD 206 [email protected] 40 Chellis Street White River Junction, VT 05001 Triumph Aerospace Systems is an industry leader in the www.xﬂowusa.com development, engineering and manufacture of complex info@xﬂowusa.com. aerospace hardware, and prototype systems for force measurement devices, ground test and flight applications. We XFlow™ CFD is the next-generation, meshless CFD provide new balances, turn-key model positions systems, and package for modeling external aerodynamics of fixed-wing calibrations to the wind tunnel industry. 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.

www.aiaa-aviation.org 32 #aiaaAviation IntroGeneral Information

AIAA Registration and Information Center Hours Conference Proceedings The AIAA Registration and Information Center will be Proceedings for the forum will be available online. The cost located on the Ballroom Level at the Washington Hilton. is included in the registration fee where indicated. Online Hours are as follows: proceedings will be available on 13 June 2016. Attendees who register in advance for the online proceedings will be provided Sunday, 12 June 1500–1900 hrs with instructions on how to access them. Those registering on site Monday, 13 June – Thursday, 16 June 0700–1730 hrs will be provided with instructions at that time. Friday, 17 June 0700–1230 hrs Proceedings: 1. To view proceedings visit www.aiaa.org >ARC>Meeting Papers. Wi-Fi Internet Access On Site a. Log in with the link at the top right of the page. AIAA is providing limited Wi-Fi service for attendees to use b. Select the appropriate conference from the list. while on site. To keep this service available and optimized for c. Search for individual papers with the Quick Search all attendees, please do not download files larger than 2MB, toolbar in the upper-right corner of the page: create multiple sessions across multiple devices, or download multiple files in one session. If you receive an error message i. By paper number: Click the “Paper Number” link, that an AIAA server is blocking your current IP address, please select the conference year, and enter the paper number. inform the AIAA registration desk. ii. Use the Search textbox to find papers by author, title, Network Name: HHonors-Meeting or keyword. The Advanced Search link provides additional search information and options. Password: AIAA2016 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 AIAA Livestream Channel not be available until the final proceedings update, which Visit livestream.com/aiaavideo/ to view selected keynotes, may take up to 15 business days after the last day of the plenaries, and Forum 360 sessions. Share the link with conference. colleagues who couldn’t attend the forum, so they can watch 3. Direct any questions concerning access to proceedings and/ live or view later. or ARC to [email protected]. Sponsored by: Manuscript Revisions: 1. Manuscript revision is open for all presenting authors from Social Media Kiosks 0900 hrs Eastern Time, Monday, 13 June, through 2000 hrs Eastern Time, Wednesday, 28 June. Throughout the forum, social media kiosks will display content shared by forum attendees! Look for your tweets or Instagram 2. Revisions submitted for manuscripts already online photos to be displayed on the screens if you’ve used our hashtag will not refresh until after the proceedings have been #aiaaAviation. Follow @AIAA on Twitter for updates about the updated, which may take up to 15 business days after the #aiaaAviation Social Media contest and Tweet Up. last day of the conference.

www.aiaa-aviation.org 33 #aiaaAviation IntroGeneral Information

Certiﬁcate of Attendance Young Professional Guide for Gaining Certificates of Attendance are available for attendees who Management Support request documentation at the forum itself. The Certificates of Young professionals have the unique opportunity to meet and Attendance will be available for attendees to print at a self- learn from some of the most important people in the business service station at the registration desk starting Wednesday, by attending conferences and participating in AIAA activities. 15 June. AIAA offers this service to better serve the needs of A detailed online guide, published by the AIAA Young the professional community. Claims of hours or applicability Professional Committee, is available to help you gain support toward professional education requirements are the and financial backing from your company. The guide explains responsibility of the participant. the benefits of participation, offers recommendations, and provides an example letter for seeking management support and funding, and shows you how to get the most out of your Employment Opportunities participation. The online guide can be found on the AIAA website at www.aiaa.org/YPGuide. AIAA members can post and browse resumes, browse job listings, and access other online employment resources by visiting the AIAA Career Center at http://careercenter. aiaa.org. Additionally, a message board will be available for Nondiscriminatory Practices postings in the Exposition Hall. AIAA accepts registrations irrespective of race, creed, gender, color, sexual orientation, physical handicap, and national or ethnic origin. Membership AIAA is your vital lifelong link to the collective creativity and brainpower of the aerospace profession and a champion for its Restrictions achievements – and nonmembers who pay the full conference Photos, video, or audio recording of sessions or exhibits, as registration fee will receive their first year’s AIAA membership well as the unauthorized sale of AIAA-copyrighted material, is at no additional cost! Students who are not yet members may prohibited. apply their registration fee toward their first year’s student member dues. (Free membership is not included in discounted group-rate registration.) International Trafﬁc in Arms Regulations (ITAR) AIAA speakers and attendees are reminded that some AIAA Foundation topics discussed in the conference could be controlled by the International Traffic in Arms Regulations (ITAR). In celebration of the AIAA Foundation’s 20th anniversary, we U.S. nationals (U.S. citizens and permanent residents) are have challenged AIAA members to donate at least $20 to the responsible for ensuring that technical data they present foundation. To date, we have raised more than $85,000 on our in open sessions to non-U.S. nationals in attendance or in way to the goal of $200,000! With your gift, we can continue conference proceedings are not export restricted by the ITAR. to enhance and create K–12 STEM programs, including U.S. nationals are likewise responsible for ensuring that they do classroom grants and hands-on activities, university design not discuss ITAR export-restricted information with non-U.S. competitions, student conferences and recognition awards. nationals in attendance. To show support of our programming and goal, the Institute will match individual and corporate donations up to one million dollars of unrestricted funds. Your gift will be matched, doubling the impact of your donation, so please consider donating today. For more information and to make a tax- deductible donation, please visit www.aiaafoundation.org.

www.aiaa-aviation.org 34 #aiaaAviation IntroGeneral Information

Author and Session Chair Information

Speakers’ Brieﬁngs in Session Rooms Audiovisual Authors who are presenting papers will meet with session chairs Each session room will be preset with the following: one LCD and co-chairs in their session rooms for a short 30-minute projector, one screen, one microphone and sound system briefing on the day of their sessions to exchange bios and review (if necessitated by room size), and one laser pointer. Laptop final details prior to the session. Please attend on the day of computers will also be provided. You may also use your own your session(s). Laptops preloaded with the Speaker Briefing computer. Any additional audiovisual equipment requested preparation slides will be provided in each session room. onsite will be at cost to the presenter. Please note that AIAA does Speaker’s Briefing schedule is as follows: not provide security in the session rooms and recommends that Monday, 13 June – Friday, 17 June: 0730 hrs items of value not be left unattended. Speakers’ Practice Room “No Paper, No Podium” and “No Podium, No Paper” Policy Speakers who wish to practice their presentations may do so in the Convention Office #4 room located on the Terrace Level of If a written paper is not submitted by the final manuscript the Washington Hilton. A sign-up sheet will be posted on the deadline, authors will not be permitted to present the paper at door. In consideration of others, please limit practice time to the forum. Also, if the paper is not presented at the forum, it 30-minute increments. will be withdrawn from the proceedings. It is the responsibility of those authors whose papers or presentations are accepted to Session Chair Reports ensure that a representative attends the conference to present the paper. These policies are intended to improve the quality of All session chairs are asked to complete a session chair report to the program for attendees. evaluate their session for future planning. AIAA has partnered with Canvas Solutions to provide an electronic Session Chair Journal Publication Report form. You can download the FREE mobile app in your App Store, AppWorld, or Marketplace by searching for Authors of appropriate papers are encouraged to submit them “Canvas Solutions, Inc.” The mobile app is free, so please be for possible publication in one of the Institute’s archival journals: sure to download it. Detailed instructions will be provided in AIAA Journal; Journal of Aerospace Information Systems; Journal the session rooms. If you do not have a tablet or a smartphone, of Air Transportation; Journal of Aircraft; Journal of Guidance, simply use the report form as a guide and enter your session Control, and Dynamics; Journal of Propulsion and Power; Journal chair report information at the session chair reporting computer of Spacecraft and Rockets; or Journal of Thermophysics and Heat station located on site near the AIAA registration area. Report Transfer. You may now submit your paper online at data will be collected and used for future planning purposes, http://mc.manuscriptcentral.com/aiaa. including session topics and room allocations. Please submit your session chair report electronically by Friday, 17 June 2016.

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 12700 Sunrise Valley Drive, Suite 200 Reston, VA 20191-5807 703.264.7500 or 800.639.AIAA (2422) Fax: 703.264.7657 [email protected] www.aiaa.org

www.aiaa-aviation.org 35 #aiaaAviation IntroCommittee Meetings

Start Time End Time Title Location Sunday, 12 June 2016 0800 hrs 1700 hrs Optimal Design in Multidisciplinary Systems Embassy 0800 hrs 1700 hrs Concepts in the Modern Design of Experiments Fairchild East 0800 hrs 1700 hrs Aircraft and Rotorcraft System Identification: Engineering Methods and Hands- Gunston West On Training Using CIFER 1400 hrs 1500 hrs GTTC Steering Subcommittee Jefferson 1400 hrs 1500 hrs APATC New Member Orientation Albright 1430 hrs 1500 hrs APATC Liaisons Subcommittee Boundary 1500 hrs 1600 hrs GTTC New Member and Mentors Meeting Jefferson 1500 hrs 1600 hrs APATC Education Subcommittee Albright 1500 hrs 1600 hrs APATC Honors and Awards Subcommittee Cardozo 1500 hrs 1600 hrs APATC Membership and Nominations Subcommittee Boundary 1500 hrs 1600 hrs APATC Planning Subcommittee Fairchild West 1500 hrs 1600 hrs APATC Publicity and Publications Subcommittee Gunston East 1500 hrs 1700 hrs Information Systems Strategy Meeting - By Invite Only DuPont 1600 hrs 1630 hrs GTTC Introduction/Overview Jefferson 1600 hrs 1700 hrs APATC Technical Activities Meeting Cardozo 1630 hrs 1700 hrs GTTC Program Subcommittee Jefferson 1700 hrs 1800 hrs GTTC Conferences Subcommittee Jefferson 1700 hrs 1800 hrs APATC Steering Committee Boundary 1800 hrs 1900 hrs GTTC Awards Subcommittee Jefferson 1800 hrs 2100 hrs Applied Aerodynamics TC Lincoln 1900 hrs 2100 hrs TAC Aircraft and Atmospheric Systems Group Georgetown West 1900 hrs 2000 hrs GTTC Publications Subcommittee Jefferson 1900 hrs 2200 hrs FDTC Transition DG Cardozo 2000 hrs 2200 hrs AMTTC Conferences Subcommittee Boundary 2000 hrs 2100 hrs GTTC Education and Student Activities Subcommittee Jefferson Monday, 13 June 2016 0800 hrs 1600 hrs GTTC Internal Balance WG DuPont Parlor 1101 0930 hrs 1700 hrs Corporate Member Committee Kalorama Room (Churchill Hotel) 0930 hrs 1230 hrs Governance Retreat Part I - By Invite Only Kalorama 1200 hrs 1400 hrs Aviation MDO SPC DuPont Parlor 2101 1200 hrs 1500 hrs General Aviation TC Boundary 1400 hrs 1600 hrs GTTC Future of Ground Testing WG Lincoln West 1430 hrs 1830 hrs Governance Retreat Part II - By Invite Only Kalorama 1700 hrs 1900 hrs Computational Fluid Dynamics (CFD) CoS DuPont Parlor 1101 1730 hrs 1900 hrs AMTTC Awards Subcommittee Boundary 1730 hrs 1900 hrs APATC Flow Control Applications & Impacts DG Holmead East 1730 hrs 1830 hrs APATC Missile & Projectile Aeroprediction DG Piscataway 1845 hrs 1945 hrs GTTC Standards Subcommittee Columbia 12 1830 hrs 1930 hrs FDTC New Member Orientation Holmead West 1830 hrs 2000 hrs APATC Aeropropulsive Interactions DG DuPont 1900 hrs 2000 hrs APATC Collaborative Experiments & Computations DG Columbia 9 1900 hrs 2000 hrs FDTC Flow Control on Unmanned Aircraft Fairchild West 1900 hrs 2100 hrs Aircraft Design TC Jefferson West 1900 hrs 2100 hrs TAC Aerospace Sciences Group Lincoln West 1900 hrs 2200 hrs Product Support TC Piscataway www.aiaa-aviation.org 36 #aiaaAviation IntroCommittee Meetings

Start Time End Time Title Location Monday, 13 June 2016 (continued) 1915 hrs 2115 hrs MVCETC Meshing Subcommittee Holmead East 1900 hrs 2200 hrs Air Transportation Systems TC Cardozo 2000 hrs 2100 hrs FDTC Modal Decomposition Methods for Aerodynamic Flows DG Columbia 12 2000 hrs 2100 hrs FDTC High Speed Flow Control Fairchild West 2030 hrs 2200 hrs Flight Testing TC Boundary 2030 hrs 2200 hrs Flight Testing TC Boundary Tuesday, 14 June 2016 0730 hrs 0930 hrs International Activities Committee International Ballroom West 0800 hrs 1200 hrs GTTC Wind Tunnel Flow Quality WG DuPont Parlor 1101 0900 hrs 1700 hrs GTTC Dual Flow Reference Nozzle WG DuPont Parlor 3101 930 hrs 1100 hrs Finance Committee International Ballroom West 0930 hrs 1200 hrs TAC New Initiatives Subcommittee Piscataway 1000 hrs 1200 hrs AIAA Standards Executive Council (SEC) Meeting Boundary 1000 hrs 1400 hrs Public Policy Committee Meeting DuPont Parlor 4101 1030 hrs 1200 hrs RAC I DuPont Parlor 2101 1100 hrs 1200 hrs Compensation Committee International Ballroom West 1300 hrs 1700 hrs DETC Subcommittee Boundary 1300 hrs 1700 hrs GTTC Uncertainty Analysis WG DuPont Parlor 1101 1330 hrs 1630 hrs TAC Executive Board DuPont Parlor 2101 1400 hrs 2200 hrs Region & Section Activities Committee DuPont Parlor 6101 1430 hrs 1800 hrs Guggenheim Board of Award - By Invite Only DuPont Parlor 7101 1500 hrs 1600 hrs TPTC Best Paper Subcommittee DuPont Parlor 4101 1600 hrs 1700 hrs TPTC Awards Subcommittee DuPont Parlor 4101 1600 hrs 1700 hrs TPTC Education Subcommittee DuPont Parlor 5101 1700 hrs 1800 hrs TPTC Publicity Subcommittee DuPont Parlor 3101 1700 hrs 1800 hrs TPTC Conference Subcommittee DuPont Parlor 1101 1730 hrs 1830 hrs FDTC LES DG DuPont Parlor 4101 1730 hrs 1900 hrs FDTC Fundamentals Subcommittee DuPont Parlor 5101 1800 hrs 1900 hrs TPTC Nominations Subcommittee DuPont Parlor 1101 1800 hrs 1900 hrs TPTC Publications Subcommittee DuPont Parlor 3101 1800 hrs 2100 hrs Design Engineering TC Boundary 1800 hrs 2100 hrs Atmospheric and Space Environments TC DuPont Parlor 2101 1830 hrs 2000 hrs Aurora Recuitment Fair Columbia 2 1830 hrs 2130 hrs Atmospheric Flight Mechanics TC Lincoln West 1900 hrs 2200 hrs Plasmadynamics and Lasers TC Jefferson East 1900 hrs 2200 hrs V/STOL Aircraft Systems TC Lincoln East 1900 hrs 2200 hrs Aircraft Operations TC DuPont Parlor 4101 1915 hrs 2215 hrs Unmanned Systems PC DuPont Parlor 5101 1900 hrs 2200 hrs Thermophysics TC Monroe 1900 hrs 2000 hrs FDTC Fluid-Structure Interaction DG Fairchild West 1900 hrs 2100 hrs FDTC Free Shear and Mixing Layer Control DG Georgetown West 1900 hrs 2000 hrs FDTC Low Re DG Gunston East 1930 hrs 2200 hrs Aerodynamic Measurement Technology TC Georgetown East

www.aiaa-aviation.org 37 #aiaaAviation IntroCommittee Meetings

Start Time End Time Title Location Wednesday, 15 June 2016 0800 hrs 1200 hrs GTTC Dual Flow Reference Nozzle WG DuPont 0800 hrs 1200 hrs GTTC Future of Ground Testing WG Columbia 2 1000 hrs 1600 hrs Technical Activities Committee Kalorama Room (Churchill Hotel) 1030 hrs 1330 hrs 2017 Fellows Committee Meeting - By Invite Only DuPont Parlor 2101 1230 hrs 1400 hrs FDTC Steering Committee Boundary 1300 hrs 1530 hrs Foundation Board of Trustees (BOT) Dupont Parlor 1101 1400 hrs 1700 hrs Emerging Technologies Committee DuPont Parlor 2101 1500 hrs 1630 hrs AVIATION 2017 Technical Program Committee Kalorama 1600 hrs 1730 hrs BOD Freshman Orientation Dupont Parlor 1101 1630 hrs 1730 hrs FDTC Turbulence Model Benchmarking DG Jay 1730 hrs 1900 hrs AMTTC Nominations Subcommittee Boundary 1730 hrs 1830 hrs FDTC Solver Technology for Turbulent Flows DG Embassy 1800 hrs 2000 hrs APATC Rotorcraft Simulations & Performance Predictions DG Monroe 1830 hrs 2130 hrs Multidisciplinary Design Optimization TC Lincoln East 1830 hrs 1930 hrs FDTC Non-Equilibrium DG Jefferson West 1900 hrs 2100 hrs FDTC CFD Subcommittee Embassy 1900 hrs 2100 hrs FDTC Flow Control and Applications Subcommittee Kalorama 1900 hrs 2100 hrs NASA Aviation Autonomy Roadmap: Community Forum Georgetown East/West 1900 hrs 2200 hrs Aerospace Traffic Management PC DuPont Parlor 2101 Thursday, 16 June 2016 0800 hrs 1600 hrs GTTC WT Model Attitude and Deformation Measurement WG DuPont Parlor 1101 1000 hrs 1200 hrs GTTC Statistically Defensible Test Methods Focus Group Columbia 9 1020 hrs 1035 hrs Annual Business Meeting Monroe 1500 hrs 1600 hrs RAC II Meeting Boundary 1730 hrs 1900 hrs APATC Low Boom DG Fairchild West 1730 hrs 2030 hrs Ground Testing TC Monroe 1745 hrs 1845 hrs FDTC Future of Fluids Subcommittee Boundary 1830 hrs 2130 hrs Transformational Flight PC Jefferson West 1830 hrs 2130 hrs Modeling and Simulation TC Cardozo 1915hrs 2215 hrs Lighter-than-Air Systems TC Fairchild West 1900 hrs 2200 hrs Fluid Dynamics TC Jefferson East Friday, 17 June 2016 0700 hrs 1630 hrs Regional Leadership Conference International Ballroom West 0800 hrs 1200 hrs National Partnership for Aeronautical Testing, NPAT Oak Lawn 0800 hrs 1600 hrs GTTC Industry WG Boundary

www.aiaa-aviation.org 38 #aiaaAviation IntroSessions at a Glance

Abbreviation Title Date Start Time Location Atmospheric Flight Mechanics 4-AFM-1 Aeroservoelastic (ASE) Methods 13-Jun 0930 hrs Holmead East 5-AFM-2 Aircraft Flight Dynamics I 13-Jun 0930 hrs Holmead West 34-AFM-3 Launch Vehicle, Missile, and Projectile Flight Dynamics 13-Jun 1400 hrs Holmead East 35-AFM-4 Planetary Entry 13-Jun 1400 hrs Georgetown East 72-AFM-5 Aircraft Flight Dynamics II 14-Jun 0930 hrs Holmead West 73-AFM-6 Unmanned Aerial Systems I 14-Jun 0930 hrs Holmead East 105-AFM-7 Aircraft Flight Dynamics III 14-Jun 1400 hrs Holmead West 106-AFM-8 Unmanned Aerial Systems II 14-Jun 1400 hrs Holmead East 143-AFM-9 Flight Test, System Identification and Parameter Estimation I 15-Jun 0930 hrs Holmead West 144-AFM-10 Unmanned Aerial Systems III 15-Jun 0930 hrs Holmead East 175-AFM-11 Aerodynamic Prediction Methods 15-Jun 1400 hrs Holmead East 176-AFM-12 Flight Test, System Identification and Parameter Estimation II 15-Jun 1400 hrs Holmead West Aerodynamic Measurement Technology 6-AMT-1 Gas Scalar Measurements 13-Jun 0930 hrs Columbia 2 36-AMT-2 Velocimetry I 13-Jun 1400 hrs Columbia 2 74-AMT-3 Velocimetry II 14-Jun 0930 hrs Columbia 2 75-AMT-4 Global Surface Measurements 14-Jun 0930 hrs Oak Lawn 107-AMT-5 Gas Thermometry 14-Jun 1400 hrs Columbia 2 145-AMT-6 Highlighting the Contributions of Prof. Ron Hanson to Aerodynamic Measurement 15-Jun 0930 hrs Georgetown East Technology (Invited) 177-AMT-7 Recent Advancements in Gas Temperature Measurements in Gas Turbines (Invited) 15-Jun 1400 hrs Columbia 2 215-AMT-8 Volumetric Measurement Techniques 16-Jun 0930 hrs Columbia 2 216-AMT-9 MEMS and Novel Surface Sensors 16-Jun 0930 hrs Oak Lawn 245-AMT-10/GT-8 Ground Test Applications of Aerodynamic Measurement Technology 16-Jun 1400 hrs Columbia 2 276-LEC-6 Aerodynamic Measurement Technology Award Lecture 16-Jun 1730 hrs International Ballroom (East) 280-AMT-11 Flow Visualization and Data Acquisition Methods 17-Jun 0930 hrs Columbia 2 Applied Aerodynamics 7-APA-1 Flow Control Applications and Demonstrations I 13-Jun 0930 hrs Columbia 9 8-APA-2 Results from the 2nd AIAA Aeroelastic Prediction Workshop I 13-Jun 0930 hrs Jefferson West 9-APA-3 Propeller/Rotorcraft/Wind Turbine Aerodynamics I 13-Jun 0930 hrs Northwest 10-APA-4 Applied CFD & Numerical Correlations with Experimental Data I 13-Jun 0930 hrs Columbia 4 21-FC-2/FD-1/APA-5 Cavity Flows I 13-Jun 0930 hrs Columbia 10 37-APA-6/FD-8 Bio-Inspired Flows 13-Jun 1400 hrs Northwest 39-APA-7 Flow Control Applications and Demonstrations II 13-Jun 1400 hrs Columbia 9 40-APA-8 Results from the 2nd AIAA Aeroelastic Prediction Workshop II 13-Jun 1400 hrs Jefferson West 41-APA-9 Applied CFD & Numerical Correlations with Experimental Data II 13-Jun 1400 hrs Columbia 4 67-LEC-2 Aerodynamics Award Lecture 13-Jun 1630 hrs Cabinet 76-APA-10 VSTOL/STOL Applications 14-Jun 0930 hrs Columbia 9 77-APA-11 Aerodynamic - Structural Modeling, Optimization, and Test Techniques for Flexible Wing 14-Jun 0930 hrs Albright Technology I 78-APA-12 Propeller/Rotorcraft/Wind Turbine Aerodynamics II 14-Jun 0930 hrs Northwest 79-APA-13 Hypersonic Aerodynamics 14-Jun 0930 hrs Jefferson West 80-APA-14 Transonic & Supersonic Aerodynamics 14-Jun 0930 hrs Columbia 4

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Abbreviation Title Date Start Time Location Applied Aerodynamics (continued) 82-ASE-6/APA-15 Surface Coatings, Ice Protection and Shedding 14-Jun 0930 hrs Georgetown West 108-APA-16/FD-21 Flapping Flight Aerodynamics 14-Jun 1400 hrs Oak Lawn 109-APA-17 Inlet/Intake Aerodynamics 14-Jun 1400 hrs Columbia 9 110-APA-18 Historically Significant/Influential Papers in Applied Aerodynamics 14-Jun 1400 hrs Jefferson West 111-APA-19 Aerodynamic - Structural Modeling, Optimization, and Test Techniques for Flexible Wing Technology II 14-Jun 1400 hrs Albright 112-APA-20 Applied CFD & Numerical Correlations with Experimental Data III 14-Jun 1400 hrs Columbia 4 146-APA-21 High Angle of Attack and High Lift Aerodynamics 15-Jun 0930 hrs Columbia 9 147-APA-22 Ground Vehicle Aerodynamics 15-Jun 0930 hrs Albright 148-APA-23/FD-28 Propeller/Rotorcraft/Wind Turbine Aerodynamics III 15-Jun 0930 hrs Northwest 161-FD-30/APA-24 Modal Decomposition Methods and Analyses 15-Jun 0930 hrs Columbia 4 178-APA-25/FD-38 Aerodynamic Design Methodologies I 15-Jun 1400 hrs Albright 179-APA-26 Aerodynamic - Structural Dynamics Interactions I 15-Jun 1400 hrs Northwest 180-APA-27 Innovative Aerodynamic Concepts & Designs 15-Jun 1400 hrs Columbia 9 181-APA-28 Aerodynamic Testing: Flight, Wind-Tunnel and Flight Testing 15-Jun 1400 hrs Columbia 4 217-APA-29 Aerodynamic Design Methodologies II 16-Jun 0930 hrs Albright 218-APA-30 Aerodynamic - Structural Dynamics Interactions II 16-Jun 0930 hrs Northwest 219-APA-32 Low Boom Activities I 16-Jun 0930 hrs Jefferson West 246-APA-33/FD-54 Unsteady Wing Aerodynamics 16-Jun 1400 hrs Kalorama 247-APA-34/FD-55 Vortex/Vortical Flows I 16-Jun 1400 hrs Northwest 248-APA-35 Airfoil/Wing/Configuration Aerodynamics 16-Jun 1400 hrs Columbia 9 249-APA-36 Aerodynamic Design Methodologies III 16-Jun 1400 hrs Albright 250-APA-37 Low Boom Activities II (Invited) 16-Jun 1400 hrs Jefferson West 263-FD-59/FC-19/APA-38 Gust Response 16-Jun 1400 hrs Columbia 10 281-APA-39 Aerodynamic Design Methodologies IV 17-Jun 0930 hrs Albright 282-APA-40 Weapons Aerodynamics: Missile/Projectile/Guided-Munitions, Carriage and Store Separation 17-Jun 0930 hrs Columbia 9 283-APA-41/FD-63 Low Speed, Low Reynolds Number Aerodynamics 17-Jun 0930 hrs Jefferson East 284-APA-42/FD-64 Vortex/Vortical Flows II 17-Jun 0930 hrs Northwest Atmospheric and Space Environments 11-ASE-1 Aircraft Wake Turbulence I (Invited) 13-Jun 0930 hrs Columbia 12 12-ASE-2 Runback Water Film Dynamics 13-Jun 0930 hrs Georgetown West 42-ASE-3 Aircraft Wake Turbulence II (Invited) 13-Jun 1400 hrs Columbia 12 43-ASE-4 Supercooled-Large Droplet (SLD) Icing 13-Jun 1400 hrs Georgetown West 81-ASE-5 Aircraft Wake Turbulence III (Invited) 14-Jun 0930 hrs Columbia 12 82-ASE-6/APA-15 Surface Coatings, Ice Protection and Shedding 14-Jun 0930 hrs Georgetown West 113-ASE-7/ATIO. Characterization of the Atmospheric Environment using UAS (Invited) 14-Jun 1400 hrs Georgetown East ATM-9 114-ASE-8 Ice Roughness Characterization and Heat Transfer 14-Jun 1400 hrs Georgetown West 149-ASE-9 NASA/FAA/ONERA Swept Wing Icing Research--SUNSET2 15-Jun 0930 hrs Columbia 12 150-ASE-10 Ice-Crystal (Engine) Icing Physics 15-Jun 0930 hrs Georgetown West 182-ASE-11 Numerical Weather Prediction (Invited) 15-Jun 1400 hrs Columbia 12 183-ASE-12 NASA PSL LF11 Engine Icing Test Campaign 15-Jun 1400 hrs Georgetown West 220-ASE-13 Icing Instrumentation and Test Facilities 16-Jun 0930 hrs Columbia 12 221-ASE-14 HAIC/HIWC 2014 Darwin and 2015 Cayenne Flight Campaigns Update I 16-Jun 0930 hrs Georgetown West 251-ASE-15 Atmospheric Environments 16-Jun 1400 hrs Columbia 12 252-ASE-16 HAIC/HIWC 2014 Darwin and 2015 Cayenne Flight Campaigns Update II and AIRA Forum 16-Jun 1400 hrs Georgetown West 285-ASE-17 Icing CFD 17-Jun 0930 hrs Georgetown West www.aiaa-aviation.org 40 #aiaaAviation IntroSessions at a Glance

Abbreviation Title Date Start Time Location Aviation Technology, Integration, and Operations 13-ATIO.ACD-1 Aircraft Design Methods and Tools I: Systems Architecting and Integration 13-Jun 0930 hrs Gunston East 14-ATIO.ATM-1 UAS Operations I 13-Jun 0930 hrs Embassy 15-ATIO.ATM-2 Air Transportation Systems Modeling I 13-Jun 0930 hrs Fairchild West 16-ATIO.ATM-3 Terminal ATM 13-Jun 0930 hrs Fairchild East 17-ATIO.TFPC-1 Transformational Flight - Automation, Airspace and Flight Path Management of ODM 13-Jun 0930 hrs Columbia 1 Operations: Panel Discussion 18-ATIO.TFPC-2 Transformational Flight - Automation Coupling to Advanced Control 13-Jun 0930 hrs Gunston West 44-ATIO.ACD-2 Aircraft Design Methods and Tools II: Geometry, Aerodynamic, and Structural Design 13-Jun 1400 hrs Gunston East 45-ATIO.ATM-4 UAS in the NAS 13-Jun 1400 hrs Embassy 46-ATIO.ATM-5 Human Factors in ATM 13-Jun 1400 hrs Fairchild East 47-ATIO.TFPC-3 Transformational Flight - On-Demand Mobility (ODM) Barriers & Opportunities 13-Jun 1400 hrs Columbia 1 83-ATIO.ACD-3 Unmanned Aircraft 14-Jun 0930 hrs Gunston East 84-ATIO.ATM-7 UAS Operations II 14-Jun 0930 hrs Embassy 85-ATIO.ATM-8 Delay Management 14-Jun 0930 hrs Fairchild East 86-ATIO.DE-1 Design Engineering 14-Jun 0930 hrs Gunston West 87-ATIO.TFPC-4/ Transformational Flight - On Demand Mobility Markets/Missions 14-Jun 0930 hrs Columbia 1 ATIO.GA-1 113-ASE-7/ATIO. Characterization of the Atmospheric Environment using UAS (Invited) 14-Jun 1400 hrs Georgetown East ATM-9 115-ATIO.ACD-4 Conceptual Aircraft Design Working Group 14-Jun 1400 hrs Gunston East 116-ATIO.ATM-10 UAS Risk and Perception 14-Jun 1400 hrs Embassy 117-ATIO.ATM-11 Weather Impacts 14-Jun 1400 hrs Fairchild East 118-ATIO.TFPC-5 Transformational Flight - On-Demand Mobility (ODM) Enabling Technologies Session 14-Jun 1400 hrs Columbia 1 119-ATIO.TFPC-6/ Transformational Flight - Unconventional V/STOL Concepts 14-Jun 1400 hrs Columbia 12 ATIO.VSTOL-1 151-ATIO.ACD-5 Aircraft Technologies and Concepts - Performance Studies and Design Methods 15-Jun 0930 hrs Gunston East 152-ATIO.ATM-12 Surface Operations Modeling and Analysis I 15-Jun 0930 hrs Embassy 153-ATIO.ATM-13 Environmental Impact Mitigation I 15-Jun 0930 hrs Fairchild East 154-ATIO.ATM-14 Data Mining in ATS I 15-Jun 0930 hrs Fairchild West 155-ATIO.TFPC-7/ Transformational Flight - Electric Thin-Haul/Commuters 15-Jun 0930 hrs Columbia 1 ATIO.ACD-6/GEPC-1 184-ATIO.ATM-15 Surface Operations Modeling and Analysis II 15-Jun 1400 hrs Embassy 185-ATIO.ATM-16 Environmental Impact Mitigation II 15-Jun 1400 hrs Fairchild East 186-ATIO.ATM-17 Data Mining in ATS II 15-Jun 1400 hrs Fairchild West 187-ATIO.GA-2 General Aviation Safety 15-Jun 1400 hrs Gunston East 188-ATIO.TFPC-8/ Transformational Flight - SCEPTOR Distributed Electric Propulsion X-Plane 15-Jun 1400 hrs Columbia 1 ATIO.FT-1/GEPC-2 222-ATIO.ACD-7/ Unconventional, Innovative, and Transformative Concepts 16-Jun 0930 hrs Gunston East ATIO.TFPC-9 223-ATIO.ATM-18 En-Route ATM I 16-Jun 0930 hrs Fairchild East 224-ATIO.ATM-19 Runway Management 16-Jun 0930 hrs Embassy 225-ATIO.ATM-20 Data Mining in ATS III 16-Jun 0930 hrs Fairchild West 226-ATIO.TFPC-10/ Transformational Flight - DARPA VTOL X-Plane Concepts 16-Jun 0930 hrs Columbia 1 ATIO.VSTOL-2 253-ATIO.ATM-21 En-Route ATM II 16-Jun 1400 hrs Fairchild East 254-ATIO.ATM-22 Reliability and Safety 16-Jun 1400 hrs Embassy 255-ATIO.ATM-23 Arrival Management 16-Jun 1400 hrs Fairchild West www.aiaa-aviation.org 41 #aiaaAviation IntroSessions at a Glance

Abbreviation Title Date Start Time Location Aviation Technology, Integration, and Operations (continued) 256-ATIO.LTA-1 Lighter-than-Air Systems 16-Jun 1400 hrs Gunston East 257-ATIO.TFPC-11/ Transformational Flight - NASA Langley Autonomy Incubator 16-Jun 1400 hrs Columbia 1 ATIO.IS-1 286-ATIO.ATM-24 NextGen and Future Concepts 17-Jun 0930 hrs Embassy 287-ATIO.ATM-25 Optimal Flight Routes 17-Jun 0930 hrs Fairchild West 288-ATIO.ATM-26 Safe Landings 17-Jun 0930 hrs Fairchild East 289-ATIO.GA-3 Environmentally-Conscious Concepts and Technologies for General Aviation 17-Jun 0930 hrs Gunston East 290-ATIO.TFPC-12 Transformational Flight - UAS Emerging Markets and Technologies 17-Jun 0930 hrs Columbia 1 291-ATIO.TFPC-13/ Transformational Flight - Clean Slate Design for Autonomy in Vehicles and Airspace 17-Jun 0930 hrs Gunston West ATIO.ATM-27 DEMAND for UNMANNED 156-D4U-1 DEMAND for UNMANNED: Catalyst for the Machine Intelligence Revolution 15-Jun 0930 hrs International Ballroom (West) 227-D4U-2 DEMAND for UNMANNED: Catalyst for the Machine Intelligence Revolution 16-Jun 0930 hrs International Ballroom (West) 275-D4U-3 DEMAND for UNMANNED Student Competition Alpha Test 16-Jun 1730 hrs International Ballroom (West) Drag Prediction Workshop 214-WKSP-1 Drag Prediction Workshop 16-Jun 0930 hrs Lincoln West 304-WKSP-2 Drag Prediction Workshop 17-Jun 0930 hrs Lincoln West Flight Testing 58-FT-1 Flight Testing of Manned Aircraft 13-Jun 1400 hrs Gunston West 127-FT-2 Flight Testing of Unmanned Aerial Systems 14-Jun 1400 hrs Gunston West 198-FT-3/GT-5 Correlation of Ground and Flight Test Data 15-Jun 1400 hrs DuPont Flow Control 20-FC-1 Flow Control Integration for Flight Control 13-Jun 0930 hrs Columbia 11 21-FC-2/FD-1/APA-5 Cavity Flows I 13-Jun 0930 hrs Columbia 10 38-FC-20 Feedback Flow Control 13-Jun 1400 hrs Northwest 50-FC-3 Flow Control for High-Lift Airfoils 13-Jun 1400 hrs Columbia 11 89-FC-4 Drag Reduction 14-Jun 0930 hrs Columbia 11 121-FC-5 Modal Decomposition Methods for Aerodynamic Flows (Invited) 14-Jun 1400 hrs Jefferson East 122-FC-6/FD-22 Separation Detection and Control 14-Jun 1400 hrs Columbia 11 158-FC-7 Internal Flow Control 15-Jun 0930 hrs Columbia 11 159-FC-8 Circulation Control 15-Jun 0930 hrs Columbia 11 160-FC-9/PDL-4/FD-29 Physics of Plasma Actuators 15-Jun 0930 hrs Gunston West 162-FD-32/FC-10 In Honor of John Lumley's Lasting Legacy to Fluid Dynamics (Invited) 15-Jun 0930 hrs Holmead West 190-FC-11 Crossflow Transition and Separation 15-Jun 1400 hrs Columbia 11 193-FD-41/FC-12 Wing Aerodynamics: Separation and Control 15-Jun 1400 hrs Morgan 205-PDL-5/FC-13 DBD Actuators 15-Jun 1400 hrs Gunston West 229-FC-14 Bluff Body Flow Control 16-Jun 0930 hrs Morgan 230-FC-15 Vortex Generators 16-Jun 0930 hrs Columbia 11 259-FC-16 Physics of Sweeping and Synthetic Jet Actuators 16-Jun 1400 hrs Morgan 260-FC-17/FD-56 Dynamic Stall with Flow Control 16-Jun 1400 hrs Columbia 11 261-FC-18/FD-57 Hypersonic Boundary Layer and Control 16-Jun 1400 hrs Lincoln East 263-FD-59/FC-19/APA-38 Gust Response 16-Jun 1400 hrs Columbia 10 www.aiaa-aviation.org 42 #aiaaAviation IntroSessions at a Glance

Abbreviation Title Date Start Time Location Fluid Dynamics 21-FC-2/FD-1/APA-5 Cavity Flows I 13-Jun 0930 hrs Columbia 10 22-FD-2 Geometry and Meshing 13-Jun 0930 hrs Georgetown East 23-FD-3 Turbulence Modeling I: LES, DNS, Hybrid LES/RANS 13-Jun 0930 hrs Jay 24-FD-4 Boundary-Layer Transition: Noise and Receptivity 13-Jun 0930 hrs Lincoln East 25-FD-7 Novel CFD Applications 13-Jun 0930 hrs Jefferson East 33-LEC-1 Fluid Dynamics Award Lecture 13-Jun 1300 hrs Cabinet 37-APA-6/FD-8 Bio-Inspired Flows 13-Jun 1400 hrs Northwest 51-FD-9 Cavity Flows II 13-Jun 1400 hrs Albright 52-FD-10 Trends in Simulation Based Engineering (Invited) 13-Jun 1400 hrs Jefferson East 53-FD-11 Solver Techniques I 13-Jun 1400 hrs Holmead West 54-FD-12 Discontinuous Galerkin Methods - Applications 13-Jun 1400 hrs Jay 55-FD-13 Shock-Boundary Layer Interaction I 13-Jun 1400 hrs Oak Lawn 56-FD-14 High-Speed Boundary-Layer Transition I 13-Jun 1400 hrs Lincoln East 57-FD-15 High-Order Methods I 13-Jun 1400 hrs Columbia 10 90-FD-16 Turbulence Modeling II: RANS, Hybrid RANS/LES 14-Jun 0930 hrs Jay 91-FD-17 Combustion Simulation I 14-Jun 0930 hrs Monroe 92-FD-18 Open Issues in Meshing 2030 (Special Issue) 14-Jun 0930 hrs Jefferson East 93-FD-19 CFD Transition Models 14-Jun 0930 hrs Lincoln East 94-FD-20 High-Order Methods II 14-Jun 0930 hrs Columbia 10 108-APA-16/FD-21 Flapping Flight Aerodynamics 14-Jun 1400 hrs Oak Lawn 122-FC-6/FD-22 Separation Detection and Control 14-Jun 1400 hrs Columbia 11 123-FD-23 Aeroacoustics and Noise 14-Jun 1400 hrs Lincoln East 124-FD-24 Fluid-Structure Interaction 14-Jun 1400 hrs Monroe 125-FD-25 Turbulence Modeling III: LES, DNS, Hybrid LES/RANS 14-Jun 1400 hrs Jay 126-FD-26 Shock-Boundary Layer Interaction II 14-Jun 1400 hrs Columbia 10 129-ITAR-2 High-Speed Flows 14-Jun 1400 hrs Cabinet 148-APA-23/FD-28 Propeller/Rotorcraft/Wind Turbine Aerodynamics III 15-Jun 0930 hrs Northwest 160-FC-9/PDL-4/ Physics of Plasma Actuators 15-Jun 0930 hrs Gunston West FD-29 161-FD-30/APA-24 Modal Decomposition Methods and Analyses 15-Jun 0930 hrs Columbia 4 162-FD-32/FC-10 In Honor of John Lumley's Lasting Legacy to Fluid Dynamics (Invited) 15-Jun 0930 hrs Jefferson East 163-FD-33 Boundary-Layer Transition: Crossflow 15-Jun 0930 hrs Lincoln East 164-FD-34 RANS and LES Methods 15-Jun 0930 hrs Columbia 10 165-FD-35 Facilities and Measurement Techniques 15-Jun 0930 hrs Monroe 166-FD-36 Adjoints and Error Estimation 15-Jun 0930 hrs Oak Lawn 167-FD-37 CFD for Engineering Applications 15-Jun 0930 hrs Morgan 178-APA-25/FD-38 Aerodynamic Design Methodologies I 15-Jun 1400 hrs Albright 191-FD-39 Shock-Dominated Flows I 15-Jun 1400 hrs Oak Lawn 192-FD-40 Turbulence Modeling - Validation and Applications 15-Jun 1400 hrs Jay 193-FD-41/FC-12 Wing Aerodynamics: Separation and Control 15-Jun 1400 hrs Morgan 194-FD-42 High-Speed Boundary-Layer Transition II 15-Jun 1400 hrs Lincoln East 195-FD-43 Combustion Simulation II 15-Jun 1400 hrs Monroe 196-FD-44 Solver Techniques II 15-Jun 1400 hrs Columbia 10 197-FD-45 Novel CFD Algorithms 15-Jun 1400 hrs Jefferson East 210-FD-46 Transition Open Forum 15-Jun 1830 hrs Cardozo www.aiaa-aviation.org 43 #aiaaAviation IntroSessions at a Glance

Abbreviation Title Date Start Time Location Fluid Dynamics (continued) 231-FD-48 Jet Flows I 16-Jun 0930 hrs Holmead West 232-FD-49 Opportunities in Future Fluid Dynamics Research (Invited) 16-Jun 0930 hrs Jefferson East 233-FD-50 High-Speed Facilities and Test Methods 16-Jun 0930 hrs Lincoln East 234-FD-53 Multiphase Flows I 16-Jun 0930 hrs Columbia 10 246-APA-33/FD-54 Unsteady Wing Aerodynamics 16-Jun 1400 hrs Holmead West 247-APA-34/FD-55 Vortex/Vortical Flows I 16-Jun 1400 hrs Northwest 260-FC-17/FD-56 Dynamic Stall with Flow Control 16-Jun 1400 hrs Columbia 11 261-FC-18/FD-57 Hypersonic Boundary Layer and Control 16-Jun 1400 hrs Lincoln East 262-FD-58 Jet Flows II 16-Jun 1400 hrs Holmead West 263-FD-59/FC-19/ Gust Response 16-Jun 1400 hrs Columbia 10 APA-38 264-FD-60 Identifying the Impact of Non-Equilibrium Mechanisms on Engineering Flows (Invited) 16-Jun 1400 hrs Jefferson East 265-FD-61 Multiphase Flows II 16-Jun 1400 hrs Holmead East 266-FD-62 Shock-Dominated Flows II 16-Jun 1400 hrs Oak Lawn 283-APA-41/FD-63 Low Speed, Low Reynolds Number Aerodynamics 17-Jun 0930 hrs Jefferson East 284-APA-42/FD-64 Vortex/Vortical Flows II 17-Jun 0930 hrs Northwest 293-FD-65 Roughness-Induced Transition 17-Jun 0930 hrs Lincoln East 294-FD-66 Flow Stability 17-Jun 0930 hrs Kalorama 295-FD-67 Computational Modeling for Propulsion Applications 17-Jun 0930 hrs Columbia 10 296-FD-68 Theoretical/Fundamental Fluid Dynamics 17-Jun 0930 hrs Columbia 12 297-FD-69 Uncertainty Quantification and Sensitivity Analysis 17-Jun 0930 hrs Morgan Ground Testing 26-GT-1 High Enthalpy Ground Test Facilities 13-Jun 0930 hrs Lincoln West 95-GT-2 Assessment and Analysis of Ground Test Facilities 14-Jun 0930 hrs Lincoln West 128-GT-3 Development and Performance of Ground Test Facilities 14-Jun 1400 hrs Lincoln West 168-GT-4 Ground Testing for High Speed Flight and Reentry 15-Jun 0930 hrs Lincoln West 198-FT-3/GT-5 Correlation of Ground and Flight Test Data 15-Jun 1400 hrs DuPont 199-GT-6 Employing CFD in Parallel with Ground Testing 15-Jun 1400 hrs Lincoln West 235-GT-7 Experimental Investigations of High Speed Air Breathing Propulsion 16-Jun 0930 hrs Cardozo 245-AMT-10/GT-8 Ground Test Applications of Aerodynamic Measurement Technology 16-Jun 1400 hrs Columbia 2 ITAR Sessions 96-ITAR-1 Advancements in Oscillating Heat Pipes 14-Jun 0930 hrs Cabinet 129-ITAR-2 High-Speed Flows 14-Jun 1400 hrs Cabinet 169-ITAR-3 CITMAV 15-Jun 0930 hrs Cabinet 200-ITAR-4 NASA Orion EFT-1 Aeroscience Results - Aerothermal I 15-Jun 1400 hrs Cabinet 236-ITAR-5 NASA Orion EFT-1 Aeroscience Results - Aerothermal II 16-Jun 0930 hrs Cabinet 267-ITAR-6 NASA Orion EFT-1 Aeroscience Results - Aerodynamics 16-Jun 1400 hrs Cabinet 298-ITAR-7 NASA Orion EFT-1 Thermal Protection System 17-Jun 0930 hrs Cabinet

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Abbreviation Title Date Start Time Location Multidisciplinary Analysis and Optimization 27-MAO-1 Design Optimization of Aircrafts and Other Complex Systems I 13-Jun 0930 hrs Cardozo 28-MAO-2 Shape and Topology Optimization I 13-Jun 0930 hrs Columbia 3 59-MAO-3 Design Optimization of Aircrafts and Other Complex Systems II 13-Jun 1400 hrs Cardozo 60-MAO-4 Shape and Topology Optimization II 13-Jun 1400 hrs Columbia 3 97-MAO-5 Design Optimization of Aircrafts and Other Complex Systems III 14-Jun 0930 hrs Cardozo 98-MAO-6 Shape and Topology Optimization III 14-Jun 0930 hrs Columbia 3 130-MAO-7 Design Optimization of Aircrafts and Other Complex Systems IV 14-Jun 1400 hrs Cardozo 131-MAO-8 Shape and Topology Optimization IV 14-Jun 1400 hrs Columbia 3 170-MAO-10 Shape and Topology Optimization V 15-Jun 0930 hrs Columbia 3 201-MAO-11 Structural Optimization I 15-Jun 1400 hrs Columbia 3 202-MAO-12 Surrogate Modeling and Non-Deterministic Design - Methods and Applications I 15-Jun 1400 hrs Cardozo 209-LEC-5 Multidisciplinary Analysis and Optimization Award Lecture 15-Jun 1730 hrs International Ballroom (East) 237-MAO-13 Structural Optimization II 16-Jun 0930 hrs Columbia 3 238-MAO-14 Emerging Methods, Algorithms, and Dynamic Data Driven Systems 16-Jun 0930 hrs Columbia 4 268-MAO-16 Surrogate Modeling and Non-Deterministic Design - Methods and Applications II 16-Jun 1400 hrs Cardozo 269-MAO-17 Emerging Methods, Algorithms, and Large Scale Applications in MAO I 16-Jun 1400 hrs Columbia 4 299-MAO-18 Surrogate Modeling and Non-Deterministic Design - Methods and Applications III 17-Jun 0930 hrs Cardozo Modeling and Simulation Technologies 29-MST-1 Modeling and Simulation of Uninhabited Aerial Vehicles I 13-Jun 0930 hrs Monroe 30-MST-2 Computational Methods for Fluid Dynamics 13-Jun 0930 hrs Morgan 61-MST-3 Human Factors, Perception, and Cueing 13-Jun 1400 hrs Morgan 62-MST-4 Modeling and Simulation of Uninhabited Aerial Vehicles II 13-Jun 1400 hrs Monroe 99-MST-5 Modeling and Simulation of Air Traffic Management I 14-Jun 0930 hrs Fairchild West 100-MST-6 Modeling and Simulation of Vehicle Dynamics, Systems, and Environments 14-Jun 0930 hrs Morgan 132-MST-7 UAV Path Planning and Collision Avoidance 14-Jun 1400 hrs Morgan 133-MST-8 Modeling and Simulation of Air Traffic Management II 14-Jun 1400 hrs Fairchild West 171-MST-9 Modeling and Simulation of Aeroelasticity I 15-Jun 0930 hrs Piscataway 203-MST-10 Model and Simulation Integration 15-Jun 1400 hrs Georgetown East 204-MST-11 Modeling and Simulation of Aeroelasticity II 15-Jun 1400 hrs Piscataway 239-MST-12 Model and Simulation Design, Development, Testing, and Validation 16-Jun 0930 hrs Piscataway 240-MST-13 Fault Detection and Health Monitoring 16-Jun 0930 hrs Georgetown East 270-MST-15 Special Modeling and Simulation Topics 16-Jun 1400 hrs Georgetown East 300-MST-16 Modeling and Simulation of Propulsion Systems 17-Jun 0930 hrs Georgetown East 301-MST-17 Modeling and Simulation of Structures and Structural Dynamics 17-Jun 0930 hrs Piscataway National Institute of Aerospace 134-NIA-1 National Institute of Aerospace Graduate Student Researchers 14-Jun 1400 hrs Piscataway

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Abbreviation Title Date Start Time Location Plasmadynamics and Lasers 31-PDL-1 Computational Methods 13-Jun 0930 hrs Piscataway 63-PDL-2 Plasma and Laser Diagnostics 13-Jun 1400 hrs Piscataway 101-PDL-3 Aero-Optics 14-Jun 0930 hrs Georgetown East 138-LEC-3 Plasmadynamics and Lasers Award Lecture 14-Jun 1630 hrs International Ballroom (East) 160-FC-9/PDL-4/ Physics of Plasma Actuators 15-Jun 0930 hrs Gunston West FD-29 205-PDL-5/FC-13 DBD Actuators 15-Jun 1400 hrs Gunston West 241-PDL-6 Plasma and Laser Technologies 16-Jun 0930 hrs Gunston West 271-PDL-7 Plasma Aerodynamics 16-Jun 1400 hrs Gunston West Rising Leaders in Aerospace 250-LTA-1 Lighter-than-Air Systems & Technologies I 25-Jun 0900 hrs Steuben 65-RLA-1 Rising Leaders in Aerospace: Speed Networking and Reception 13-Jun 1500 hrs International Ballroom (West) 103-RLA-2 Rising Leaders in Aerospace Panel Discussion: Why Work in Aerospace Instead of Silicon 14-Jun 1130 hrs Georgetown East Valley? 173-RLA-3 Rising Leaders in Aerospace Keynote 15-Jun 1130 hrs Columbia 9 Thermophysics 32-TP-1 Ablation I 13-Jun 0930 hrs DuPont 64-TP-2 Ablation II - Modeling 13-Jun 1400 hrs DuPont 96-ITAR-1 Advancements in Oscillating Heat Pipes 14-Jun 0930 hrs Cabinet 102-TP-3 Reentry Systems and Instrumentation 14-Jun 0930 hrs Kalorama 135-TP-5 Radiation 14-Jun 1400 hrs Kalorama 136-TP-6 Special Session: Spacecraft Thermal Management 14-Jun 1400 hrs DuPont 169-ITAR-3 CITMAV 15-Jun 0930 hrs Cabinet 172-TP-7 Advanced Modeling I - DSMC 15-Jun 0930 hrs Jefferson West 200-ITAR-4 NASA Orion EFT-1 Aeroscience Results - Aerothermal I 15-Jun 1400 hrs Cabinet 206-TP-8 Advanced Modeling II - Hypersonic Flows 15-Jun 1400 hrs Jefferson West 208-LEC-4 Thermophysics Award Lecture 15-Jun 1730 hrs Lincoln West 236-ITAR-5 NASA Orion EFT-1 Aeroscience Results - Aerothermal II 16-Jun 0930 hrs Cabinet 242-TP-9 Special Session: Thermal Management Systems 16-Jun 0930 hrs DuPont 243-TP-10 High Enthalpy Ground Testing 16-Jun 0930 hrs Jay 267-ITAR-6 NASA Orion EFT-1 Aeroscience Results - Aerodynamics 16-Jun 1400 hrs Cabinet 272-TP-11 Thermophysics 16-Jun 1400 hrs DuPont 273-TP-12 Advanced Modeling III - DNS and State to State 16-Jun 1400 hrs Jay 298-ITAR-7 NASA Orion EFT-1 Thermal Protection System 17-Jun 0930 hrs Cabinet 302-TP-13 Heat Transfer in Aerospace Applications 17-Jun 0930 hrs DuPont 303-TP-14 Advanced Modeling IV 17-Jun 0930 hrs Jay

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In 2016, the Aviation Week Network celebrates Aviation Week & Space Technology’s centennial milestone. Join us as we look at how the past century has shaped the future of aerospace. Attend events, read archived issues, and relive milestones in aviation and aerospace from the past 100 years. Explore the Digital Archive: Every issue. Every article. Every ad. archive.aviationweek.com Follow our Centennial Coverage: aviationweek.com/100 Advertising and Custom Sponsorships: Iain Blackhall • Managing Director, Global Media +44 207 152 4495 • [email protected] Monday Monday, 13 June 2016 1-SB-1 Speakers’ Briefing Session Rooms 0730 - 0800 hrs 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 session to exchange bios and review final details prior to the session. Please attend on the day of your session. Monday, 13 June 2016 2-PLNRY-1 Plenary International Ballroom 0800 - 0900 hrs (Center) The Second Century of Flight—Looking Back to Look Forward Michael Delaney Vice President and General Manager, Airplane Development The Boeing Company Monday, 13 June 2016 3-NW-1 Networking Coffee Break Meeting Room Foyers 0900 - 0930 hrs 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. Monday, 13 June 2016 4-AFM-1 Aeroservoelastic (ASE) Methods Holmead East Chaired by: A. DA RONCH, University of Southampton and B. LEONHARDT, Northrop Grumman Corporation 0930 hrs 1000 hrs 1030 hrs AIAA-2016-2700 AIAA-2016-2701 AIAA-2016-2702 Flight Testing an Adaptive A Load-Based Feedback Approach Studies on Unsteady 48 Feedforward Controller for Gust for Distributed Aeroservoelastic Aerodynamic Modeling and Loads Alleviation on a Flexible Control Flight Simulation at High Aircraft V. Suryakumar, Texas A&M University, Angles of Attack F. Li, Y. Wang, China Academy of College Station, TX; A. Mangalam, Tao L. Shen, D. Huang, G. Wu, Nanjing Aerospace Aerodynamics, Beijing, China; of Systems Integration, Inc., Hampton, University of Aeronautics and A. Da Ronch, University of Southampton, VA; Y. Babbar, T. Strganac, Texas A&M Astronautics, Nanjing, China Southampton, United Kingdom University, College Station, TX Monday, 13 June 2016 5-AFM-2 Aircraft Flight Dynamics I Holmead West Chaired by: D. MURRI, NASA Engineering and Safety Center and N. HALL 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2016-2703 AIAA-2016-2704 AIAA-2016-2705 AIAA-2016-2706 AIAA-2016-2707 AIAA-2016-2708 Airborne Landing Distance: A Dynamic Ground Effect on the Rotary Balance Wind Tunnel Wind Tunnel Tests for Validation of Model Based Online Monitoring Investigation and Flight Neural Network Approach Aerodynamic Coefficients of a Testing for the FASER Flight Control Algorithms at High Angles of Uncertain Plants Subject to Dynamic Analysis of General B. Carvalho, Technological Institute Wing using a Panel Method Research Aircraft of Attack Using Autonomous Stochastic Disturbances Aviation Safety of Aeronautics (ITA), São José dos P. Boschetti, G. Quijada, E. Cárdenas, C. Denham, Virginia Polytechnic Institute Aircraft Model Mounted in 3DOF D. Löbl, N. Mumm, F. Holzapfel, E. Harrison, H. Jimenez, D. Mavris, Campos, Brazil Simón Bolívar University, Naiguata, and State University, Blacksburg, VA; D. Gimbals Technical University of Munich, Georgia Institute of Technology, Venezuela Owens, NASA Langley Research Center, D. Ignatyev, K. Zaripov, M. Sidoryuk, K. Garching, Germany Atlanta, GA Hampton, VA Kolinko, A. Khrabrov, TsAGI, Zhukovsky, Russia Monday, 13 June 2016 6-AMT-1 Gas Scalar Measurements Columbia 2 Chaired by: C. COMBS, The University of Tennessee Space Institute and B. BATHEL, NASA Langley Research Center 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2016-2709 AIAA-2016-2710 AIAA-2016-2711 AIAA-2016-2712 AIAA-2016-2713 AIAA-2016-2714 Two-Point Dynamic Rayleigh Simultaneous Multi-Property WIDECARS Measurements Disturbance and Phase Speed An Optical Ray Tracing Method Measurement of Dissociation Scattering Measurements in a Laser Diagnostics using Filtered of a Turbulent, Premixed, Measurements for Shock Tubes for Analyzing Beam-Steering Fraction and Temperature Free Jet Rayleigh Scattering Ethylene-Air Flame Flame in a and Hypersonic Boundary- Effects During Laser Diagnostics using Laser Rayleigh Scattering A. Fagan, K. Zaman, NASA Glenn J. George, T. Jenkins, MetroLaser, Dual-Mode Scramjet Layer Instability in Turbulent Media Methods Research Center, Cleveland, OH; K. Inc., Laguna Hills, CA; J. Sutton, Ohio A. Cutler, E. Gallo, L. Cantu, George J. Jewell, Air Force Research W. Kulatilaka, Y. Wang, Texas A&M J. George, MetroLaser, Inc., Laguna Elam, Jacobs, Cleveland, OH State University, Columbus, OH Washington University, Washington, Laboratory, Wright-Patterson AFB, University, College Station, TX Hills, CA; C. Limbach, Colorado D.C.; R. Rockwell, C. Goyne, OH; N. Parziale, Stevens Institute of State University, Fort Collins, CO; T. University of Virginia, Charlottesville, Technology, Hoboken, NJ; K. Lam, B. Jenkins, MetroLaser, Inc., Laguna Charlottesville, VA Hagen, R. Kimmel, Air Force Research Hills, CA; R. Miles, Princeton Laboratory, Wright-Patterson AFB, OH University, Princeton, NJ Monday, 13 June 2016 7-APA-1 Flow Control Applications and Demonstrations I Columbia 9 Chaired by: J. MURRAY, Sandia National Laboratories and J. FARNSWORTH, University of Colorado Boulder 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2016-2715 AIAA-2016-2716 AIAA-2016-2717 AIAA-2016-2718 AIAA-2016-2719 AIAA-2016-2720 A Method of Reducing the Drag CROR-Powerplant pylon wake Investigation of the Discrete Wingtip Vortex Modifications Aerodynamics of Wing with The Role of Spanwise Flow of Transport Wings mitigation for noise reduction Effects of Suction in Large Using Alternating Jets Oscillating Wingtip Flapper for Swept Wing Separation J. Alderman, S. Rolston, Airbus, through innovative blowing/ Scale Arrays for Laminar Flow R. Kranepuhl, University of the S. Shkarayev, University of Control with Varied Spanwise Bristol, United Kingdom; M. Gaster, C. suction-based active flow control Control German Federal Armed Forces, Arizona, Tucson, Tucson, AZ; E. Su, Jet Spacing Atkin, City University London, London, system B. Crowley, C. Atkin, City University Neubiberg, Germany; S. Shkarayev, Northwestern Polytechnical University, M. Walker, K. Hipp, J. Bons, Ohio United Kingdom Y. Bury, University of Toulouse, Toulouse, London, London, United Kingdom P. Planchenault, University of Arizona, Xi’an, China; L. Zhao, Beihang State University, Columbus, OH 49 France; A. Bordron, Aéroconseil, Blagnac, Tucson, Tucson, AZ University, Beijing, China France; H. Belloc, University of Toulouse, Toulouse, France; D. Prat, Airbus, Toulouse, France Monday, 13 June 2016 8-APA-2 Results from the 2nd AIAA Aeroelastic Prediction Workshop I Jefferson West Chaired by: J. HEEG, NASA-Langley Research Center and D. SCHUSTER, NASA-Langley Research Center 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2016-2721 AIAA-2016-2722 AIAA-2016-2723 AIAA-2016-2724 Overview and Data Comparisons FUN3D Analyses in Support A Comparison of CFD and AIC- Flow Simulations for the from the 2nd Aeroelastic Prediction of the Second Aeroelastic Based Methods for Unsteady Second Aeroelastic Prediction Workshop Prediction Workshop Aerodynamics and Flutter Workshop Using the EZNSS J. Heeg, P. Chwalowski, NASA Langley P. Chwalowski, J. Heeg, NASA Computations of the AEPW-2 Code Research Center, Hampton, VA; D. Langley Research Center, Hampton, Wing Model D. Raveh, Technion--Israel Institute of Raveh, Technion--Israel Institute of VA G. Begnini, C. Spode, A. Pantaleao, Technology, Haifa, Israel Technology, Haifa, Israel; A. Jirasek, M. B. Guaraldo, G. Marcório, M. Pedras, Dalenbring, Swedish Defense Research Embraer, São José dos Campos, Agency (FOI), Stockholm, Sweden Brazil; et al. Monday, 13 June 2016 9-APA-3 Propeller/Rotorcraft/Wind Turbine Aerodynamics I Northwest Chaired by: J. RAULEDER, Technical University of Munich and M. CALVERT, U.S. Army AMRDEC 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2016-2725 AIAA-2016-2726 AIAA-2016-2727 AIAA-2016-2728 AIAA-2016-2729 Design of advanced airfoil for Transient CFD analysis of three DDES and URANS comparison An Experimental Study on the A Comparative Assessment of stall-regulated wind turbines dimensional dynamic stall of the NREL phase-VI wind Wake Characteristics of Dual- Correlation-based Transition F. Grasso, Aerodynamix, Naples, Italy; on 5 MW NREL wind turbine turbine at deep stall Rotor Wind Turbines by Using a Models for Wind Power D. Coiro, N. Bizzarrini, G. Calise, baseline rotor H. Rahimi, B. Dose, I. Herraez, J. Stereoscopic PIV Technique Applications University of Naples “Federico II”, N. Fatima, D. Gopal, Indian Institute Peinke, University of Oldenburg, H. Hu, T. Wei, Z. Wang, Iowa State D. Corson, Altair Engineering, Inc., Naples, Italy of Technology Madras, Chennai, India Oldenburg, Germany; B. Stoevesandt, University, Ames, IA Malta, NY; A. Zamora, Siemens, Fraunhofer, Oldenburg, Germany Boulder, CO; S. Medida, Altair Engineering, Inc., Sunnyvale, CA Monday, 13 June 2016 10-APA-4 Applied CFD & Numerical Correlations with Experimental Data I Columbia 4 Chaired by: K. KONTIS, University of Glasgow and K. MASSEY, DARPA/TTO 0930 hrs 1000 hrs 1030 hrs AIAA-2016-2730 AIAA-2016-2731 AIAA-2016-2732 Application of Multi-Strand Solver Assessment of CREATE-AV(TM) Computational Study of a to Complex Rotorcraft Simulations Helios Near-Body Solvers for the Lifting Surface in Propeller V. Lakshminarayan, Science and Wake Prediction of HART-II Rotor Slipstreams Technology Corporation, Moffett Field, B. Jayaraman, Science and Technology S. Chadha, B. Pomeroy, M. Selig, CA; J. Sitaraman, Parallel Geometric Corporation, Moffett Field, CA; J. Lim, R. University of Illinois, Urbana- Algorithms, LLC, Sunnyvale, CA; A. Jain, Army Aviation and Missile Research Champaign, Urbana, IL Wissink, Army Aviation and Missile Development and Engineering Center, Research Development and Engineering Moffett Field, CA 50 Center, Moffett Field, CA Monday, 13 June 2016 11-ASE-1 Aircraft Wake Turbulence I (Invited) Columbia 12 Chaired by: J. CROUCH, Boeing Commercial Airplanes and D. SCHAUERHAMER, Jacobs Technology 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2016-2733 AIAA-2016-2734 AIAA-2016-2735 AIAA-2016-2736 AIAA-2016-2737 Assessing Wake-Turbulence Effect of Ground Obstacle of Numerical Optimization Reduced Order Modeling of Sensitivity Study of Aircraft Characteristics for Commercial Different Aspect Ratio on Wake of Plate Lines Design for Contrails: Jet Induction and Wake Vortices Using Aircraft (Invited) Vortex Dissipation (Invited) Enhanced Wake Vortex Decay Vortex Phases OVERFLOW (Invited) J. Crouch, M. Czech, The Boeing C. Wang, D. Zhao, Nanyang (Invited) A. Inamdar, S. Lele, M. Jacobson, D. Schauerhamer, S. Robinson, Company, Seattle, WA Technological University, Singapore, A. Stephan, F. Holzäpfel, Stanford University, Stanford, CA University of California, Davis, Singapore; J. Schluter, Deakin University, German Aerospace Center (DLR), Davis, CA Melbourne, Australia; F. Holzäpfel, A. Oberpfaffenhofen, Germany Stephan, German Aerospace Center (DLR), Oberpfaffenhofen, Germany Monday, 13 June 2016 12-ASE-2 Runback Water Film Dynamics Georgetown West Chaired by: W. WRIGHT, ASRC Aerospace Corporation and A. WORK 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2016-2738 AIAA-2016-2739 AIAA-2016-2740 AIAA-2016-2741 AIAA-2016-2742 An Experimental Invesitgation An Experimental Investigation An Experimental Investigation Gravitational Effects in Low- Droplet reemission from rotating on the Dynamic Water Runback on the Effects of Surface on the Water Runback Process Speed Air-Driven Films surfaces: experimental study on Process Over an Airfoil Surface Wettability on Water Runback over an Airfoil Surface with A. Rothmayer, K. Zhang, H. Hu, Iowa disks and a scale model fan, and Pertinent to Aircraft Icing and Ice Accretion over an Realistic Ice Roughness State University, Ames, IA model derivation. Phenomena Airfoil Surface Y. Liu, K. Zhang, H. Hu, Iowa State B. Déjean, E. Radenac, P. Berthoumieu, K. Zhang, A. Rothmayer, H. Hu, Iowa R. Waldman, H. Li, H. Hu, Iowa State University, Ames, IA ONERA, Toulouse, France State University, Ames, IA University, Ames, IA Monday, 13 June 2016 13-ATIO.ACD-1 Aircraft Design Methods and Tools I: Systems Architecting and Integration Gunston East Chaired by: M. DRAKE, Boeing Commercial Airplanes and S. KOMADINA, Northrop Grumman Aerospace Systems 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2016-2743 AIAA-2016-2744 AIAA-2016-2745 AIAA-2016-2746 AIAA-2016-2747 Aircraft Systems Architecting Heuristic Definition, Evaluation, Assessing Impact of Epistemic Impact of Subsystem Extraction of Conceptual – a Functional-Logical Domain and Impact Decomposition and Technological Uncertainty Secondary Power Requirements Design Information Concerning Perspective of Aircraft Subsystem on Aircraft Subsystem on Gas Turbine Sizing and Aircraft Systems by Genetic M. Guenov, A. Molina-Cristobal, V. Architectures Architectures Performance Programming Voloshin, A. Riaz, A. van Heerden, I. Chakraborty, D. Mavris, Georgia I. Chakraborty, D. Mavris, Georgia M. Ozcan, I. Chakraborty, D. Mavris, T. Maedomari, K. Rinoie, University of Cranfield University, Cranfield, United Institute of Technology, Atlanta, GA Institute of Technology, Atlanta, GA Georgia Institute of Technology, Tokyo, Tokyo, Japan Kingdom; S. Sharma, Airbus, Bristol, Atlanta, GA United Kingdom; et al. Monday, 13 June 2016 14-ATIO.ATM-1 UAS Operations I Embassy Chaired by: K. MARAIS, Purdue University 0930 hrs 1000 hrs 1030 hrs AIAA-2016-2748 AIAA-2016-2749 AIAA-2016-2750 Towards Autonomous Aviation Rapid Trajectory Feasibility Multi-Mode Guidance for Operations: What can we learn Verification for UAS Traffic an Independent Multicopter from other areas of automation? Management Geofencing System B. Sridhar, P. Kopardekar, NASA Ames A. Ishihara, J. Jung, J. Rios, NASA Ames M. Stevens, E. Atkins, University of Research Center, Moffett Field, CA Research Center, Moffett Field, CA Michigan, Ann Arbor, Ann Arbor, MI Monday, 13 June 2016 15-ATIO.ATM-2 Air Transportation Systems Modeling I Fairchild West 51 Chaired by: K. SHETH, NASA Ames Research Center and J. KOELLING, NASA-Langley Research Center 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2016-2751 AIAA-2016-2752 AIAA-2016-2753 AIAA-2016-2754 AIAA-2016-2755 AIAA-2016-2756 Analysis of Prediction The U.S. National Airspace Initial Feasibility Test of Exploring Hierarchical Decision- Initial Results from the Coordination Logic for Uncertainty in Interval System: a Model for the Air Traffic management Modeling Framework for Air Metrosim Project Repulsive Resolution Management Verification and Validation of Design Tradespace through Transportation System F. Wieland, A. Tyagi, R. Sharma, M. Maneuvers S. Torres, G. Nagle, Lockheed Martin Complex, Distributed Systems- Surrogate Modeling K. Moolchandani, Z. Sha, A. Santos, Intelligent Automation, Inc., A. Narkawicz, C. Munoz, A. Dutle, Corporation, Rockville, MD of-systems K. Schwartz, H. Pfaender, M. Kirby, D. Maheshwari, J. Thekinen, N. Rockville, MD NASA Langley Research Center, W. Felder, Stevens Institute of Mavris, Georgia Institute of Technology, Davendralingam, J. Panchal, Purdue Hampton, VA Technology, Hoboken, NJ Atlanta, GA; V. Stouffer, V. Kumar, LMI, University, West Lafayette, IN; et al. Tysons, VA; et al. Monday, 13 June 2016 16-ATIO.ATM-3 Terminal ATM Fairchild East Chaired by: B. BAXLEY, NASA Langley Research Center 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2016-2757 AIAA-2016-2758 AIAA-2016-2759 AIAA-2016-2760 AIAA-2016-2761 AIAA-2016-2762 Study on Continuous Descent Impact of Runway Closures Performance of an Automated Miles-in-Trail Requirements Operational Characteristics Identifying significant traffic Operation for Efficient Air on Arrival Flows at a Major System for Control of Traffic in Relaxation: A Key Benefit Identification and Simulation flow patterns in Multi-Airport Transport System Metropolitan Airport Terminal Airspace Mechanism of Integrated Model Verification for Incheon Systems Terminal Manoeuvring A. Errico, V. Di Vito, L. Federico, J. DeArmon, J. Conroy, T. Masek, A. Nikoleris, H. Erzberger, R. Paielli, Arrival Departure Surface International Airport Areas under uncertainty. Italian Aerospace Research Center MITRE Corporation, McLean, VA NASA Ames Research Center, Moffett Traffic Management Y. Eun, D. Jeon, Korea Aerospace S. Sidiropoulos, A. Majumdar, K. Han, (CIRA), Capua, Italy Field, CA; Y. Chu, University of A. Saraf, J. Bertino, N. Luch, ATAC Research Institute, Daejeon, South Korea; W. Ochieng, Imperial College London, California, Santa Cruz, Santa Cruz, CA Corporation, Santa Clara, CA; H. H. Lee, University of California, Santa London, United Kingdom Idris, N. Shen, Engility Corporation, Cruz, Moffett Field, CA; Z. Zhu, Stinger Billerica, MA Ghaffarian Technologies, Inc., Moffett Field, CA; Y. Jung, NASA Ames Research Center, Moffett Field, CA; M. Jeong, Korea Aerospace Research Institute, Daejeon, South Korea; et al. Monday, 13 June 2016 17-ATIO.TFPC-1 Transformational Flight - Automation, Airspace and Flight Path Management of ODM Operations: Panel Discussion Columbia 1 0930 - 1230 hrs Moderator: Bruce J. Holmes, CEO, AirMarkets Corporation Panelists: Natalia Alexandrov Joe Burns Parimal Kopardekar John Langford Neil Planzer Brien Seeley Ryan Stone Senior Research Scientist CEO UTM Project Director Chairman and CEO Vice President, Air Traffic Management Founder President

52 NASA Langley Research Center Sensurion Corporation NASA Ames Research Center Aurora Flight Sciences Boeing Commercial Airplanes Sustainable Aviation Foundation - CAFÉ SmartSky Networks Foundation

Monday, 13 June 2016 18-ATIO.TFPC-2 Transformational Flight - Automation Coupling to Advanced Control Gunston West Chaired by: A. GIBSON, Empirical Systems Aerospace and K. GOODRICH, NASA Langley Research Center 0930 hrs 1000 hrs 1030 hrs 1100 hrs Oral Presentation Oral Presentation AIAA-2016-2763 Oral Presentation Automation and Pilot Aids to Remote Rescue Mission Self-Aware Vehicles: Mission Control Systems for Distributed Improve Single-Pilot Safety Autonomy: Robust Outer Loop and Performance Adaptation to Aerial Robotics and Performance in Part 135 Control Needs System Health Degradation P. Rothhaar, J. Cooper, J. Neilan, L. Operations B. Allen, P. Rothhaar, J. Neilan, L. Tran, I. Gregory, NASA Langley Research Tran, A. Trujillo, A. Hagiopol, NASA K. Goodrich, M. Moore, NASA Langley A. Trujillo, K. Goodrich, NASA Langley Center, Hampton, VA Langley Research Center, Hampton, Research Center, Hampton, VA Research Center, Hampton, VA; et al. VA; et al. Monday, 13 June 2016 19-F360-1 Commercial Aviation—Solving the Disruption Challenge International Ballroom 0930 - 1130 hrs (East) Moderator: Ben Iannotta, Editor-in-Chief, Aerospace America Panelists: Jim Eck Robert Pearce Bryan Quigley Lance Sherry Assistant Administrator for NextGen Deputy Associate Administrator for Strategy Managing Director Director, Center for Air Transportation Systems Research and Associate FAA Office of the Associate Administrator for Aeronautics NASA United Airlines Flight Operations Professor, System Engineering and Operations Research Department George Mason University Monday, 13 June 2016 20-FC-1 Flow Control Integration for Flight Control Columbia 11 Chaired by: K. HUBER, and G. DALE, Air Force Research Laboratory 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2016-2764 AIAA-2016-2765 AIAA-2016-2766 AIAA-2016-2767 AIAA-2016-2768 Crossed-Actuation AFC for Active Flow Control on Application of Active Flow Discrete vortices on delta wings Actuations of Synthetic Jets Lateral-Directional Control of the Stability and Control Control to a Generic Low with unsteady leading-edge on a UCAV Planform at High an ICE-101/Saccon UCAV Configuration (SACCON) Aspect-Ratio Trapezoidal Wing blowing Angles of Attack D. Williams, Illinois Institute of M. Jentzsch, L. Taubert, I. for High Lift Generation J. Bartasevicius, University of Glasgow, J. Lee, S. Lee, C. Kim, Seoul National Technology, Chicago, IL; J. Seidel, Wygnanski, University of Arizona, B. Röntsch, L. Taubert, P. Tewes, J. Glasgow, United Kingdom; A. Buzica, University, Seoul, South Korea U.S. Air Force Academy, Colorado Tucson, Tucson, AZ Little, I. Wygnanski, University of C. Breitsamter, Technical University of Springs, CO Arizona, Tucson, Tucson, AZ Munich, Munich, Germany Monday, 13 June 2016 21-FC-2/FD-1/APA-5 Cavity Flows I Columbia 10 Chaired by: K. CASPER, Sandia National Laboratories and L. UKEILEY, University of Florida 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2016-2769 AIAA-2016-2770 AIAA-2016-2771 AIAA-2016-2772 AIAA-2016-2773 AIAA-2016-2774 Control of Low-Speed Cavity Supersonic Cavity Flow Control Computational Analysis of Effect of Rear Face Geometry on Generic Cavity Test within the Wavelet Analysis of Complex Flow Using Steady Jets for Scramjet Applications Partially-Covered Cavity With the Open Cavity Oscillatory Flow NRC 1.5 m Trisonic Wind Tunnel Geometry Transonic Cavity N. Al Haddabi, K. Kontis, H. Zare- N. Webb, M. Samimy, Ohio State and Without Side Walls at M=0.9 M. MacMaster, National Research Flows Behtash, University of Glasgow, University, Columbus, OH S. Premachandran, Z. Hu, X. S. Das, Birla Institute of Technology, Council Canada, Ottawa, Canada D. Bacci, A. Saddington, D. Bray, Glasgow, United Kingdom Zhang, University of Southampton, Ranchi, India; J. Cohen, Technion--Israel Cranfield University, Shrivenham, Southampton, United Kingdom Institute of Technology, Haifa, Israel United Kingdom Monday, 13 June 2016 22-FD-2 Geometry and Meshing Georgetown East 53 Chaired by: N. CHRISOCHOIDES, Old Dominion University and H. LUO, North Carolina State University 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2016-2775 AIAA-2016-2776 AIAA-2016-2777 AIAA-2016-2778 AIAA-2016-2779 AIAA-2016-2780 High-Order Mesh Curving Using Curved mesh generation using An adaptive remeshing strategy Telescopic Approach for Singular mesh generation from Comparison of linear and WCN Mesh Optimization radial basis functions for unsteady aerodynamics Extreme-Scale Parallel multiple overset meshes: a tool non-linear elasticity large S. Karman, Pointwise, Inc., Fort A. Kashi, H. Luo, North Carolina State applications Mesh Generation for CFD for industrial applications displacement mesh deformation Worth, TX; J. Erwin, R. Glasby, D. University, Raleigh, NC A. Limare, University of Technology, Applications G. Abbruzzese, M. Cordero Gracia, M. in Computational Fluid Dynamics Stefanski, University of Tennessee, Troyes, France; P. Brenner, Airbus, N. Chrisochoides, Old Dominion Gómez López, Technical University of B. Shamsaei, J. Newman, University of Knoxville, TN Les Mureaux, France; H. Borouchaki, University, Norfolk, VA Madrid, Madrid, Spain Tennessee, Chattanooga, Chattanooga, University of Technology, Troyes, France TN Monday, 13 June 2016 23-FD-3 Turbulence Modeling I: LES, DNS, Hybrid LES/RANS Jay Chaired by: G. CANDLER, University of Minnesota 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2016-2781 AIAA-2016-2782 AIAA-2016-2783 AIAA-2016-2784 AIAA-2016-2785 AIAA-2016-2786 Filtered velocity based LES Simulation of Airfoil Stall Flows Wall--modeled Large Eddy Budget of Turbulent Kinetic Shedding Light into the Quasi- Wall-Modeled Large Eddy of mixing in high speed Using IDDES with High Order Simulation of Flow Over a Wall-- Energy in a Shock Wave/ Laminarization Process Simulation of Laminar recirculating shear flow Schemes mounted Hump Boundary-layer Interaction G. Araya, University of Puerto Rico, Separation Bubble Flows S. Gs, A. Kartha, G. Candler, Y. Yang, G. Zha, University of Miami, P. Iyer, National Institute of Aerospace, M. Vyas, NASA Glenn Research Mayaguez, Mayaguez, F. Cadieux, J. Sadique, X. Yang, C. University of Minnesota, Minneapolis, Coral Gables, FL Hampton, VA; M. Malik, NASA Langley Center, Cleveland, OH; M. Waindim, Meneveau, R. Mittal, Johns Hopkins Minneapolis, MN Research Center, Hampton, VA D. Gaitonde, Ohio State University, University, Baltimore, MD Columbus, OH Monday, 13 June 2016 24-FD-4 Boundary-Layer Transition: Noise and Receptivity Lincoln East Chaired by: A. CHOU, NASA Langley Research Center and J. SMITH, Sandia National Laboratories 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2016-2787 AIAA-2016-2788 AIAA-2016-2789 AIAA-2016-2790 AIAA-2016-2791 AIAA-2016-2792 Multivariate Statistics Analysis Receptivity of High-Speed High Frequency Free-Stream Receptivity and Forced Local scattering theory and the Direct numerical simulation of of the Pressure Field Induced Boundary Layers to Kinetic Disturbance Measurements in Response to Acoustic role of an abrupt change on a wavepacket in a boundary by High-Speed Turbulent Fluctuations Hypersonic Wind Tunnels by Disturbances in High-Speed boundary-layer instability and layer at Mach 0.9 Boundary Layers A. Fedorov, Moscow Institute of Means of a Slender Wedge Probe Boundary Layers acoustic radiation A. Martinez, M. Medeiros, University C. Zhang, L. Duan, Missouri University Physics and Technology, Zhukovsky, A. Wagner, E. Schuelein, K. Hannemann, P. Balakumar, R. King, A. Chou, L. M. Dong, Tianjin University, Tianjin, of São Paulo, São Carlos, Brazil of Science and Technology, Rolla, MO Russia; A. Tumin, University of German Aerospace Center (DLR), Owens, M. Kegerise, NASA Langley China; X. Wu, Imperial College Arizona, Tucson, Tucson, AZ Göttingen, Germany Research Center, Hampton, VA London, London, United Kingdom Monday, 13 June 2016 25-FD-7 Novel CFD Applications Jefferson East Chaired by: J. SEIDEL, USAF Academy and C. SCHROCK, Air Force Research Laboratory 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2016-2793 AIAA-2016-2794 AIAA-2016-2795 AIAA-2016-2796 AIAA-2016-2797 Neutralization of Airborne Evaporative Cooling of CFD Investigation of Supersonic Indicial Methods For the Dynamic Stability Analysis of Contaminants Idealized Torso Geometries Bleed with Discretely Modeled Numerical Calculation of Dynamic the Orion Crew Module through J. Boris, G. Patnaik, Naval Research Including Protective Armor Holes in Cambridge Wind Derivatives of a Finned Projectile Computational Fluid Dynamics Laboratory, Washington, D.C. D. Mott, A. Kercher, A. Corrigan, Tunnel at Various Conditions M. Ghoreyshi, P. French, U.S. Air Force A. Potturi, O. Peroomian, Metacomp Naval Research Laboratory, S. Duncan, P. Orkwis, M. Ugolotti, Academy, Colorado Springs, CO; D. Technologies, Agoura Hills, CA Washington, D.C. University of Cincinnati, Cincinnati, OH Findlay, J. Lee, Naval Air Warfare Center, Patuxent River, MD; A. Jirasek, A. Lofthouse, U.S. Air Force Academy, Colorado Springs, CO 54 Monday, 13 June 2016 26-GT-1 High Enthalpy Ground Test Facilities Lincoln West Chaired by: M. RHODE, NASA Langley Research Center and B. MILLS, AEDC/ ATA 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2016-2798 AIAA-2016-2799 AIAA-2016-2800 AIAA-2016-2801 AIAA-2016-2802 AIAA-2016-2803 The Plasma Wind Tunnels at Plasma Wind Tunnel Flow Tomographic Optical Emission Analysis of Air Plasma Flows in Review of Heat Flux Characterizing FLEET for the Institute of Space Systems: Analysis with High Speed Spectroscopy for Plasma Wind Magnetoplasmadynamic Arcjet Measurements for High Aerodynamic Measurements Current Status and Challenges Imaging Tunnel Testing Testing Enthalpy Flows in Various Gas Mixtures and S. Loehle, S. Fasoulas, G. Herdrich, F. Zander, T. Hermann, S. Loehle, T. Hermann, S. Loehle, University of F. Zander, S. Loehle, University of S. Loehle, University of Stuttgart, non-Air Environments T. Hermann, B. Massuti-Ballester, University of Stuttgart, Stuttgart, Stuttgart, Stuttgart, Germany Stuttgart, Stuttgart, Germany Stuttgart, Germany N. Calvert, Y. Zhang, R. Miles, A. Meindl, University of Stuttgart, Germany Princeton University, Princeton, NJ Stuttgart, Germany; et al. Monday, 13 June 2016 27-MAO-1 Design Optimization of Aircrafts and Other Complex Systems I Cardozo Chaired by: R. KOLONAY, Air Force Research Laboratory/RQVC/WPAFB and C. HEATH, NASA Glenn Research Center 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2016-2804 AIAA-2016-2805 AIAA-2016-2806 AIAA-2016-2807 AIAA-2016-2808 Parallel Aircraft Trajectory Multi-Disciplinary, Multi-Fidelity Aerostructural design optimization A Methodology for Probabilistic Evaluation of the impacts of the Optimization with Analytic Discrete Data Transfer Using of a continuous morphing trailing Analysis of Distributed Objective Function definition in Derivatives Degenerate Geometry Forms edge aircraft for improved Multidisciplinary Architecture Aircraft Conceptual Design R. Falck, J. Gray, NASA Glenn E. Olson, NASA Langley Research mission performance (PADMA) D. Bianchi, T. Orra, Embraer, São Research Center, Cleveland, OH; Center, Hampton, VA D. Burdette, G. Kenway, J. Martins, S. Ghosh, D. Mavris, Georgia Institute José dos Campos, Brazil; F. Silvestre, B. Naylor, DB Consulting, Inc., University of Michigan, Ann Arbor, Ann of Technology, Atlanta, GA Technological Institute of Aeronautics Cleveland, OH Arbor, MI (ITA), São José dos Campos, Brazil Monday, 13 June 2016 28-MAO-2 Shape and Topology Optimization I Columbia 3 Chaired by: S. FERGUSON, North Carolina State University and G. KENWAY, Univeristy of Michigan Department of Aerospace Engineering 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2016-2809 AIAA-2016-2810 AIAA-2016-2811 AIAA-2016-2812 AIAA-2016-2813 Topology Optimization of Topology Optimization for Topology Optimization of 3D Efficient Modal Design Broadband Shape and Nonlinear Cellular Materials Additive Manufacturing: Woven Micro-lattices using Variables Applied to Topology Optimization of J. Carstensen, J. Guest, Johns New Projection-based Design a Projection-based Ground Aerodynamic Optimization of a Acoustic Metamaterials and Hopkins University, Baltimore, MD Algorithms Structure Approach Modern Transport Wing Phononic Crystals M. Osanov, J. Carstensen, E. Tromme, S. Ha, Korea Maritime and Ocean C. Allen, D. Poole, T. Rendall, W. Lin, J. Newman, W. Anderson, J. Guest, Johns Hopkins University, University, Busan, South Korea; J. University of Bristol, Bristol, United University of Tennessee, Chattanooga, Baltimore, MD; C. Williams, Virginia Guest, Johns Hopkins University, Kingdom Chattanooga, TN Polytechnic Institute and State Baltimore, MD University, Blacksburg, VA Monday, 13 June 2016 29-MST-1 Modeling and Simulation of Uninhabited Aerial Vehicles I Monroe Chaired by: N. MACCHIARELLA, Embry-Riddle Aeronautical University and S. BEARD, NASA-Ames Research Center 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2016-2814 AIAA-2016-2815 AIAA-2016-2816 AIAA-2016-2817 AIAA-2016-2818 AIAA-2016-2819 Analysis of the quality control Design, Development, and Testing Development of a Microgravity A family of universal miniature Developing Automated First-Principles Modeling of UAVs for the case of the of a UAV Hardware-in-the-Loop Generating UAV Using COTS autopilots – design solutions, Contingency Procedures for the of A Miniature Tilt-Rotor analytical redundancy of testbed for Aviation and Airspace Autopilots characteristics, hardware/ ATOL System of a Fixed-Wing Convertiplane in Low-Speed measurements Prognostics Research J. Hathaway, J. Jacob, Oklahoma software-in-the-loop UAV through Online FDD Operation D. Nowak, A. Tomczyk, G. Kopecki, C. Teubert, G. Gorospe, C. Kulkarni, State University, Stillwater, OK simulations M. Kügler, F. Holzapfel, Technical G. Cai, A. Saeed, A. Younes, T. Rzeszow University of Technology, Stinger Ghaffarian Technologies, Inc., G. Kopecki, P. Rzucidlo, P. University of Munich, Munich, Taha, J. Dias, L. Seneviratne, Khalifa Rzeszow, Poland Moffett Field, CA; C. Quach, NASA Grzybowski, D. Kordos, Rzeszow Germany University, Abu Dhabi, United Arab 55 Langley Research Center, Hampton, University of Technology, Rzeszow, Emirates VA; E. Hogge, Northrop Grumman Poland Corporation, Hampton, VA; D. Burgett, Christopher Newport University, Newport News, VA Monday, 13 June 2016 30-MST-2 Computational Methods for Fluid Dynamics Morgan Chaired by: A. ELMILIGUI, NASA Langley Research Center and D. KEATING 0930 hrs 1000 hrs 1030 hrs AIAA-2016-2820 AIAA-2016-2821 AIAA-2016-2822 Non-Intrusive Uncertainty Improved Kriging Model for A High-Order Overset Method Quantification of CFD Based on MDOE wind tunnel tests on Moving and Deforming Adaptive Stochastic Kriging H. Ma, J. Zhang, Y. Qin, China Grids B. Wang, Y. Zhang, J. Gong, W. Zhang, Academy of Aerospace Aerodynamics, J. Crabill, A. Jameson, Stanford K. Zhang, China Academy of Aerospace Beijing, China University, Stanford, CA Aerodynamics, Beijing, China Monday, 13 June 2016 31-PDL-1 Computational Methods Piscataway Chaired by: T. MOELLER, University of Tennessee Space Institute and J. POGGIE, Purdue University- Sch of Aero and Astro 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2016-2823 AIAA-2016-2824 AIAA-2016-2825 AIAA-2016-2826 Finite Volume Method for Numerical Simulation of Computational Multi-Fluid Numerical Simulation and Divergence-free Solutions to Mars Entry Flight using Model for Partially Ionized and Analysis of Hypersonic Vehicle Maxwell’s Equations Magnetohydrodynamic Magnetized Plasma Plasma Sheath R. Thompson, The Boeing Company, Parachute Effect A. Alvarez Laguna, A. Lani, von Kármán T. Deyang, Q. Kun, Zhejiang Huntsville, AL; T. Moeller, University of T. Fujino, T. Takahashi, University of Institute for Fluid Dynamics, Rhode-Saint- University, Hangzhou, China Tennessee, Tullahoma, Tullahoma, TN Tsukuba, Tsukuba, Japan Genèse, Belgium; Y. Maneva, Catholic University of Leuven, Leuven, Belgium; H. Deconinck, von Kármán Institute for Fluid Dynamics, Rhode-Saint-Genèse, Belgium; S. Poedts, Catholic University of Leuven, Leuven, Belgium Monday, 13 June 2016 32-TP-1 Ablation I DuPont Chaired by: A. MARTIN, University of Kentucky and E. STERN, NASA Ames Research Center 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2016-2827 AIAA-2016-2828 AIAA-2016-2829 AIAA-2016-2830 AIAA-2016-2831 AIAA-2016-2832 Gas-surface interactions of Expansion Tunnel Ablation Electromagnetic Wave Characterization of Ablation The ESA ARC Project: Ablation Investigation of Pyrolysis Gas high-temperature materials Testing in Venus Entry Transmission through Product Radiation Signatures of Radiation Coupling for Chemistry in an Inductively under high-enthlapy flows Conditions Lightweight Carbon Phenolic PICA and FiberForm hypervelocity re-entry with low Coupled Plasma Facility using plasma wind tunnels N. Banerji, P. Leyland, Swiss Federal Ablator: Microwave to Infrared M. Winter, B. Butler, University of density type ablators C. Tillson, J. Uhl, J. Meyers, D. B. Massuti-Ballester, G. Herdrich, Institute of Technology, Lausanne, Frequencies Kentucky, Lexington, Lexington, P. Leyland, U. Sheikh, B. Duval, Fletcher, University of Vermont, 56 University of Stuttgart, Stuttgart, Switzerland; R. Morgan, University of M. Eberhart, S. Loehle, F. Zander, KY; P. Danehy, S. Splinter, NASA Swiss Federal Institute of Technology, Burlington, Burlington, VT Germany Queensland, Brisbane, Australia University of Stuttgart, Stuttgart, Langley Research Center, Hampton, Lausanne, Switzerland; T. Hermann, Germany; H. Merbold, ABB Group, VA; Z. Diao, F. Pnaerai, University S. Loehle, University of Stuttgart, Zurich, Switzerland; A. Murk, of Kentucky, Lexington, Lexington, Stuttgart, Germany; T. McIntyre, University of Bern, Bern, Switzerland; KY; et al. University of Queensland, Brisbane, S. Merli, University of Stuttgart, Australia; et al. Stuttgart, Germany Monday, 13 June 2016 33-LEC-1 Fluid Dynamics Award Lecture Cabinet 1300 - 1400 hrs The Hydrodynamic theory of Premixed Flames: Laminar to Turbulent Propagation Moshe Matalon Caterpillar Distinguished Professor, Mechanical Science and Engineering University of Illinois at Urbana-Champaign Monday, 13 June 2016 34-AFM-3 Launch Vehicle, Missile, and Projectile Flight Dynamics Holmead East Chaired by: F. FRESCONI, US Army Research Lab and T. LAVIN, Sandia National Laboratories 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs AIAA-2016-2833 AIAA-2016-2834 AIAA-2016-2835 AIAA-2016-2836 AIAA-2016-2837 Optimal Gliding Guidance for SHEFEX II - An Aerodynamic Epsilon-Trig Regularization Airship Control using Expert Distributed Cooperative Guidance Long Range Hypersonic vehicles and Structural Post-Flight Method for Bang-Bang Optimal Demonstrations Law for Multiple Flight Vehicles of with Impact angle Constraints Analysis Control Problems O. Daskiran, A. Dogan, University of Saturation Attack using Pseudospectral Method M. Franze, German Aerospace Center K. Mall, M. Grant, Purdue University, Texas, Arlington, Arlington, TX Z. Enjiao, T. Chao, S. Wang, M. Yang, K. Kalirajan, A. Joshi, Indian Institute of (DLR), Brunswick, Germany West Lafayette, IN Harbin Institute of Technology, Harbin, Technology Bombay, Mumbai, India China Monday, 13 June 2016 35-AFM-4 Planetary Entry Georgetown East Chaired by: M. GRANT, Purdue University and C. KARLGAARD, Analytical Mechanics Associates Inc 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs AIAA-2016-2838 AIAA-2016-2839 AIAA-2016-2840 AIAA-2016-2841 AIAA-2016-2842 Constrained Trajectory Reconstructed Parachute Dynamic CFD Simulations of Trigonomerization of Optimal Incorporation of Effects Optimization for Planetary System Performance During the MEADS II Ballistic Range Control Problems with Bounded of Control Surfaces into Entry via Sequential Convex the Second LDSD Supersonic Test Model Controls Hypersonic Trajectory Programming Flight Dynamics Test E. Stern, NASA Ames Research K. Mall, M. Grant, Purdue University, Optimization Framework Z. Wang, M. Grant, Purdue University, C. O’Farrell, E. Brandeau, C. Tanner, Center, Moffett Field, CA; A. Schwing, West Lafayette, IN H. Saranathan, M. Grant, Purdue West Lafayette, IN J. Gallon, Jet Propulsion Laboratory, NASA Johnson Space Center, University, West Lafayette, IN California Institute of Technology, Houston, TX; J. Brock, Analytical Pasadena, CA; S. Muppidi, ERC, Mechanics Associates, Inc., Moffett Inc., Moffett Field, CA; I. Clark, Jet Field, CA; M. Schoenenberger, Propulsion Laboratory, California NASA Langley Research Center, Institute of Technology, Pasadena, CA Hampton, VA Monday, 13 June 2016 36-AMT-2 Velocimetry I Columbia 2 Chaired by: L. MA, Virginia Tech and A. FAGAN, NASA Glenn Research Center 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2016-2843 AIAA-2016-2844 AIAA-2016-2845 AIAA-2016-2846 AIAA-2016-2847 AIAA-2016-2848 Femtosecond-Laser-Based Development of Hydroxyl Femtosecond Laser Tagging Enhancement of FLEET in Argon Selective Two-Photon Absorptive An Experimental Investigation Measurements of Velocity and Tagging Velocimetry for Low Characterization of a Sweeping Gas Mixtures Resonance Femtosecond-Laser with Molecular Tagging Density in the NASA Langley Velocity Flows Jet Actuator Operating in the Y. Zhang, N. Calvert, M. Shneider, Electronic-Excitation Tagging Technique on the Spray Flow 0.3-m Transonic Cryogenic M. Andre, P. Bardet, George Compressible Regime R. Miles, Princeton University, (STARFLEET) Velocimetry in Flow Ejected from an Air-Blast Washington University, Washington, C. Peters, R. Miles, Princeton Princeton, NJ

57 Tunnel and Combustion Diagnostics Nozzle R. Burns, C. Peters, P. Danehy, D.C.; R. Burns, P. Danehy, NASA University, Princeton, NJ; R. Burns, N. Jiang, Spectral Energies, LLC, F. Chen, H. Liu, Shanghai Jiao Tong NASA Langley Research Center, Langley Research Center, Hampton, P. Danehy, B. Bathel, G. Jones, Dayton, OH; B. Halls, Air Force Research University, Shanghai, China; H. Li, H. Hampton, VA VA NASA Langley Research Center, Laboratory, Wright-Patterson AFB, OH; H. Hu, Iowa State University, Ames, IA Hampton, VA Stauffer, Spectral Energies, LLC, Dayton, OH; P. Danehy, NASA Langley Research Center, Hampton, VA; J. Gord, Air Force Research Laboratory, Wright-Patterson AFB, OH; S. Roy, Spectral Energies, LLC, Dayton, OH Monday, 13 June 2016 37-APA-6/FD-8 Bio-Inspired Flows Northwest Chaired by: R. RAMAMURTI and J. MURRAY, Sandia National Laboratories 1400 hrs 1430 hrs 1500 hrs 1530 hrs AIAA-2016-2849 AIAA-2016-2850 AIAA-2016-2851 AIAA-2016-2852 Instantaneous Lift and Motion Three-Dimensional Numerical Influence of Vortical Bio-Inspired Sinusoidal Characteristics of Butterflies in Simulation of Hummingbird Interactions on Thunniform Fish Leading-Edged Wings Free Flight Forward Flight Motions M. Post, A. Sapell, J. Hart, U.S. Air M. Sridhar, C. Kang, D. Landrum, J. Song, H. Luo, Vanderbilt University, K. Srivastava, K. Duraisamy, Force Academy, Colorado Springs, CO University of Alabama, Huntsville, Nashville, TN; B. Tobalske, University University of Michigan, Ann Arbor, Huntsville, AL of Montana, Missoula, Missoula, Ann Arbor, MI MT; T. Hedrick, University of North Carolina, Chapel Hill, Chapel Hill, NC Monday, 13 June 2016 38-FC-20 Feedback Flow Control Northwest Chaired by: D. WILLIAMS, Illinois Institute of Technology and U. KAUL, NASA ARC 1400 hrs 1600 hrs 1630 hrs 1700 hrs No Presentations AIAA-2016-2853 AIAA-2016-2854 AIAA-2016-2855 Discrete Time Open-Loop and Analysis of the filtering effect Global Mode Based Control of Closed-Loop Flow Control Based of the stochastic estimation and Supersonic Jet Noise on Van der Pol Modeling accuracy improvement by sensor M. Natarajan, J. Freund, D. Bodony, V. Motta, P. Mouyon, C. Döll, ONERA, location optimization University of Illinois, Urbana- Toulouse, France A. Arnault, J. Dandois, J. Monnier, J. Champaign, Urbana, IL Delva, ONERA, Meudon, France; J. Foucaut, Lille University of Science and Technology, Villeneuve d’Ascq, France Monday, 13 June 2016 39-APA-7 Flow Control Applications and Demonstrations II Columbia 9 Chaired by: B. CYBYK, The Johns Hopkins University Applied Physics Laboratory and K. KARA, Khalifa University of Science, Technology & Research 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs AIAA-2016-2856 AIAA-2016-2857 AIAA-2016-2858 AIAA-2016-2859 AIAA-2016-2860 Numerical Study of a Double Reynolds Number Effect of Numerical Simulation of a Flow Control and Analysis on Effects of Geometric Stream Jet: ZDES Simulation, Leading Edge Tubercles on Sweeping Jet Actuator Simplified Ship Helideck Parameters on Performance of Stability Analysis and Noise Airfoil Aerodynamics K. Kara, Khalifa University, Abu Dhabi, Q. Gallas, M. Lamoureux, J. Monnier, Sweeping Jet Actuator Reduction L. Peristy, R. Perez, A. Asghar, W. United Arab Emirates A. Gilliot, C. Verbeke, J. Delva, B. Slupski, K. Kara, Khalifa University, F. Sartor, F. Gand, M. Huet, S. Allan, Royal Military College of ONERA, Lille, France Abu Dhabi, United Arab Emirates Beneddine, D. Sipp, ONERA, Meudon, Canada, Kingston, Canada France

58 Monday, 13 June 2016 40-APA-8 Results from the 2nd AIAA Aeroelastic Prediction Workshop II Jefferson West Chaired by: J. HEEG, NASA-Langley Research Center and D. RAVEH 1400 hrs 1430 hrs AIAA-2016-2861 AIAA-2016-2862 RANS-LES Hybrid Turbulence An Immersed Boundary Method Modelling for Aeroelastic for Solving the Compressible Problems: Test Case 3 in Navier-Stokes Equations with the Second AIAA Aeroelastic Fluid-Structure Interaction Prediction Workshop C. Brehm, University of Arizona, Tucson, M. Righi, Zurich University of Applied Tucson, AZ; M. Barad, C. Kiris, NASA Sciences, Zurich, Switzerland Ames Research Center, Moffett Field, CA Monday, 13 June 2016 41-APA-9 Applied CFD & Numerical Correlations with Experimental Data II Columbia 4 Chaired by: K. VANDEN, USAF and L. UKEILEY, University of Florida 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs AIAA-2016-2863 AIAA-2016-2864 AIAA-2016-2865 AIAA-2016-2866 AIAA-2016-2867 Assessment of an Inviscid Euler- A Low Subsonic Study of the Aerodynamic Interactions DDES Simulation of a Complex Numerical Assessment for PIV Adjoint Solver for Prediction of NASA N2A Hybrid Wing-Body between Landing-Gear Main Landing Gear with Six- Measurement in Airplane Wakes Aerodynamic Characteristics of Using an Inviscid Euler-Adjoint Components Wheel Bogie K. Matsushima, Toyama University, the NASA HL-20 Lifting Body Solver S. Spagnolo, X. Zhang, Z. Hu, D. U. Oza, Z. Hu, X. Zhang, University of Toyama, Japan; H. Kato, Japan D. Almosnino, Self, Redmond, WA D. Almosnino, Self, Redmond, WA Angland, University of Southampton, Southampton, Southampton, United Aerospace Exploration Agency (JAXA), Southampton, United Kingdom Kingdom Chofu, Japan Monday, 13 June 2016 42-ASE-3 Aircraft Wake Turbulence II (Invited) Columbia 12 Chaired by: M. PRUIS, Northwest Research Associates Inc and S. KOERNER, DLR 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs AIAA-2016-2868 AIAA-2016-2869 AIAA-2016-2870 AIAA-2016-2871 AIAA-2016-3715 Uncertainly Quantification of Development and assessment of Deployment of a next Summary of NASA Wake and Weather Aware Route Planning Lidar-Derived Wake Vortex a Wake Vortex characterization generation and operational Weather Data Collection at (WARP) Parameters with/without Data algorithm based on a hybrid LIDAR solution for monitoring Memphis International Airport: J. Eanes, W. Monach, Daniel H. Assimilation (Invited) LIDAR signal processing wake vortices for supporting 2013-2015 (Invited) Wagner Associates, Inc., Hampton, VA T. Misaka, S. Obayashi, Tohoku A. Hallermeyer, A. Dolfi-Bouteyre, M. new wake turbulence M. Pruis, D. Delisi, NorthWest University, Sendai, Japan; S. Jeong, Valla, ONERA, Palaiseau, France; L. Le regulations (Invited) Research Associates, Redmond, WA; KyungHee University, Seoul, South Brusquet, G. Fleury, Laboratory of Signals L. Thobois, R. Krishnamurthy, J. D. Jacob, Coherent Research Group, Korea and Systems (L2S), Gif-sur-Yvette, Cariou, J. Nicolaon, LEOSPHERE, LLC, Key West, FL; D. Lai, NorthWest France; L. Thobois, LEOSPHERE, Orsay, Orsay, France Research Associates, Redmond, WA France; et al. Monday, 13 June 2016 43-ASE-4 Supercooled-Large Droplet (SLD) Icing Georgetown West Chaired by: M. POTAPCZUK, NASA Glenn Research Center and P. VILLEDIEU 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2016-2872 AIAA-2016-2873 AIAA-2016-2874 AIAA-2016-2875 AIAA-2016-2876 AIAA-2016-2877 Numerical Investigation of A revisited model for SLD Additional Results of Glaze Super-cooled Large Droplet Ice Numerical Modeling of First A combined post-processing High-Speed Droplet Impact on impact onto a solid surface. Icing Scaling in SLD Conditions Accretion Reproduction and and Second Order SLD Effects method for SLD modeling Solid and Wet Surfaces P. Trontin, P. Villedieu, ONERA, J. Tsao, Ohio Aerospace Institute, Scaling Law Validation on 3D Geometries J. Cliquet, Airbus, Toulouse, France Y. Guo, Y. Lian, University of Toulouse, France Cleveland, OH E. Rocco, Y. Han, J. Palacios, D. Bilodeau, W. Habashi, McGill Louisville, Louisville, KY Pennsylvania State University, University, Montréal, Canada; G. University Park, PA; R. Kreeger, NASA Baruzzi, ANSYS, Inc., Montréal, 59 Glenn Research Center, Cleveland, OH Canada; M. Fossati, McGill University, Montréal, Canada Monday, 13 June 2016 44-ATIO.ACD-2 Aircraft Design Methods and Tools II: Geometry, Aerodynamic, and Structural Design Gunston East Chaired by: W. ANEMAAT, DARcorporation and R. VOS 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs AIAA-2016-2878 AIAA-2016-2879 AIAA-2016-2880 AIAA-2016-2881 AIAA-2016-2882 AIAA-2016-2883 AIAA-2016-2884 Advanced Modeling in OpenVSP Framework for Assessing Robust Optimization of Conceptual Design of Swept- A Ground Structure Approach Automated Generation of Rapid Design and Optimization R. McDonald, California Polytechnic Impact of Active Flow Control Transonic Airfoil for Generic Wing Root Airfoils for the Evolutionary Finite-Element Meshes for of Waverider from 3D Flow State University, San Luis Obispo, CA Technologies for Commercial Fighter Aircraft using Global M. Sol, R. Vos, Delft University of Optimization of Aircraft Wing Aircraft Conceptual Design C. Liu, B. Peng, B. Chen, C. Ji, China Aircraft Variable Fidelity Modeling Technology, Delft, The Netherlands Structures W. Li, J. Robinson, NASA Langley Academy of Aerospace Aerodynamics, B. Hiller, Y. Cai, E. Karagoz, Georgia M. Tyan, N. Nguyen, J. Lee, Konkuk T. Ikonen, A. Sobester, University of Research Center, Hampton, VA Beijing, China Institute of Technology, Atlanta, GA; C. University, Seoul, South Korea Southampton, Southampton, United Wilhelms, RWTH Aachen University, Kingdom Aachen, Germany; I. Chakraborty, S. Briceno, Georgia Institute of Technology, Atlanta, GA; et al. Monday, 13 June 2016 45-ATIO.ATM-4 UAS in the NAS Embassy Chaired by: L. REDDY, Purdue University 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2016-2885 AIAA-2016-2886 AIAA-2016-2887 AIAA-2016-2888 AIAA-2016-2889 AIAA-2016-2890 Investigating Traffic Avoidance Emergent Detect and Avoid From Rural to Urban UAS Traffic Management Demonstration of an Adaptable A Hierarchical Hybrid State Maneuver Preferences in the Absence of Intent Environments: Human/ (UTM) Concept of Operations NextGen Interface for the UAS System Based Controller Design of Unmanned Aircraft Information of Intruder Aircraft Systems Simulation Research to Safely Enable Low Altitude Ground Control Station Approach for an Autonomous Operators_20151027 V. Kuo, Human Solutions, Inc., for Low Altitude UAS Traffic Flight Operations J. Murphy, N. Otto, S. Jovic, NASA UAS Mission M. Kuffner, Lincoln Laboratory, Washington, D.C. Management (UTM) T. Prevot, J. Rios, P. Kopardekar, J. Ames Research Center, Moffett M. Hejase, Ohio State University, Massachusetts Institute of Technology, T. Prevot, J. Homola, J. Mercer, Robinson III, M. Johnson, J. Jung, Field, CA; T. Carniol, RGI Commercial Columbus, OH; A. Oguz, Turkish Air Lexington, MA; R. Guendel, Odyssey NASA Ames Research Center, Moffett NASA Ames Research Center, Moffett Solutions, Fairfax, VA Force Academy, Istanbul, Turkey; A. Systems Consulting Group, Wakefield, Field, CA Field, CA Kurt, Center for Automotive Research, MA; S. Darrah, Booz Allen Hamilton, Columbus, OH; U. Ozguner, K. Redmill, Dayton, OH Ohio State University, Columbus, OH Monday, 13 June 2016 46-ATIO.ATM-5 Human Factors in ATM Fairchild East Chaired by: N. SMITH, NASA-Ames 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2016-2891 AIAA-2016-2892 AIAA-2016-2893 AIAA-2016-2894 AIAA-2016-2895 AIAA-2016-2896 Pilot Evaluation of a Decision Insights in Mining the NTSB Impacts of Guidance function The Effect of Cockpit- Flight Crew Responses from Human-in-the-Loop Investigation Support Tool for Weather Accident and Incident Database on Air Traffic Controller Based Convective Weather the Interval Management of Interoperability Between and Terrain Avoidance during J. Cistone, Sullivan Aviation Services, situation awareness Notifications on Pilot Decision Alternative Clearances Terminal Sequencing and Spacing, Departure LLC, Hanover, PA M. Ellejmi, S. Dubuisson, M. Bonnier, Making (IMAC) Human-In-The-Loop Automated Terminal Proximity J. Gauci, K. Theuma, D. Zammit R. Lane, EUROCONTROL, Bretigny, S. Campbell, A. Alexander, Lincoln Experiment Alert, and Wake-Separation Mangion, University of Malta, Msida, France Laboratory, Massachusetts Institute of B. Baxley, S. Wilson, R. Roper, K. 60 Recategorization Malta Technology, Lexington, MA Swieringa, NASA Langley Research T. Callantine, San Jose State University, Center, Hampton, VA Moffett Field, CA; T. Prevot, NASA Ames Research Center, Moffett Field, CA; N. Bienert, A. Borade, C. Gabriel, V. Gujral, San Jose State University, Moffett Field, CA; et al. Monday, 13 June 2016 47-ATIO.TFPC-3 Transformational Flight - On-Demand Mobility (ODM) Barriers & Opportunities Columbia 1 Chaired by: V. STOUFFER, LMI and V. KUMAR, Intelligent Automation Inc. 1400 hrs 1430 hrs 1500 hrs 1530 hrs AIAA-2016-2897 AIAA-2016-2898 AIAA-2016-2899 AIAA-2016-2900 On-Demand Aviation Net Present Value, Trade-space, Impact of Reduced Crew Economical assessment of air Regulatory Obstacles and and Feasibility of On-Demand Operations on Airlines - mobility on demand concepts Resulting Research Roadmaps Aircraft Operational Challenges and with focus on Germany R. Hemm, D. Duncan, V. Stouffer, M. Narkus-Kramer, LMI, Tysons, Cost Benefits M. Kreimeier, E. Stumpf, D. LMI, Tysons, VA VA; J. Tejeda, Booz Allen Hamilton, A. Malik, V. Gollnick, Institute of Air Gottschalk, RWTH Aachen University, Washington, D.C.; V. Stouffer, R. Transportation Systems, Hamburg, Aachen, Germany Hemm, S. Trajkov, LMI, Tysons, VA; Germany J. Creedon, Old Dominion University, Norfolk, VA; et al. Monday, 13 June 2016 48-F360-2 The Future of Education International Ballroom 1400 - 1600 hrs (East) Moderator: Todd W. Zarfos, Vice President, Engineering Functions, Boeing Commercial Airplanes Panelists: Tara Chklovski Norman L. Fortenberry Alton D. Romig, Jr. Melissa Musgrave Darryll J. Pines Founder, CEO Executive Director Executive Officer Head of Employment Nariman Farvardin Professor of Aerospace Engineering Iridescent American Society for Engineering Education National Academy of Engineering Airbus and Airbus Group North America Dean, A. James Clark School of Engineering University of Maryland

Monday, 13 June 2016 49-F360-3 Concepts to Reality—Airplane Development In A Global Environment Cabinet 1400 - 1600 hrs Moderator: Ken Sanger, Vice President / General Manager 787 Airplane Development, The Boeing Company

Panelists: Luis Carlos Affonso Tom Pelland Simon Carlisle Chief Operating Ofﬁcer, Commercial Aviation President, Engine & Environmental Control Systems Director, Strategy, Civil Aerospace Embraer S.A. UTC Aerospace Systems Rolls Royce

Monday, 13 June 2016 50-FC-3 Flow Control for High-Lift Airfoils Columbia 11 Chaired by: R. KUMAR, Florida State University and J. LIN, NASA-Langley Research Center 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs AIAA-2016-2901 AIAA-2016-2902 AIAA-2016-2903 AIAA-2016-2904 AIAA-2016-2905 AIAA-2016-2906 AIAA-2016-2907

61 Performance Enhancement of High-Lift Performance Unsteady Active Flow Control Implementation and Testing of Traverse Actuation Method Unsteady Active Flow Control Using Computational Fluid an Airfoil Model with a Control Enhancement of a Simple Flap on the Morphed Leading Edge a Modular Rapid Prototyped A. Shmilovich, Y. Yadlin, The Boeing on the Leading Edge of a Dynamics and Experiments Surface using Synthetic Jets using Aerodynamic Flow Control of a High-lift Configuration Laminar Airfoil with Steady Company, Huntington Beach, CA High-lift Configuration Laminar to Design Sweeping Jets for M. Monastero, M. Amitay, Rensselaer M. DeSalvo, Georgia Institute of Laminar Airfoil Blown Active Flow Control Slots Airfoil High Reynolds Number Cruise Polytechnic Institute, Troy, NY Technology, Atlanta, GA; A. Gissen, A. Jairam, L. Clemons, R. Wlezien, L. Clemons, P. Clayton, A. Jairam, L. Clemons, R. Wlezien, Iowa State Configurations E. Whalen, The Boeing Company, St. Iowa State University, Ames, IA R. Wlezien, Iowa State University, University, Ames, IA G. Jones, W. Milholen, J. Fell, S. Louis, MO; A. Glezer, Georgia Institute of Ames, IA Webb, C. Cagle, NASA Langley Technology, Atlanta, GA Research Center, Hampton, VA Monday, 13 June 2016 51-FD-9 Cavity Flows II Albright Chaired by: R. SCHMIT, USAF AFRL and S. DAS, Birla Institute of Technology, Mesra, Ranchi 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2016-2908 AIAA-2016-2909 AIAA-2016-2910 AIAA-2016-2911 AIAA-2016-2912 AIAA-2016-2913 Time-dependent airloads on a Compressibility Effects in the Three-Dimensional Unsteady Pressure Sensitive A numerical study of the Control of flow instabilities in an cylinder in a supersonic cavity Shear Layer over a Rectangular Measurement of Edge Effects in Paint Measurements of saturation process in an open open aircraft bay model cavity D. Chin, K. Granlund, North Carolina Cavity Open Cavities of Finite-Span Resonance Properties in cavity flow Q. Liu, Technical University of Madrid, State University, Raleigh, NC S. Beresh, J. Wagner, K. Casper, E. Demauro, S. Beresh, J. Wagner, J. Complex Cavities N. Vinha, F. Meseguer-Garrido, J. Madrid, Spain; F. Gómez, Monash Sandia National Laboratories, Henfling, R. Spillers, Sandia National K. Casper, J. Wagner, S. Beresh, R. de Vicente, E. Valero, Technical University, Melbourne, Australia; V. Albuquerque, NM Laboratories, Albuquerque, NM Spillers, J. Henfling, Sandia National University of Madrid, Madrid, Spain Theofilis, Technical University of Madrid, Laboratories, Albuquerque, NM Madrid, Spain Monday, 13 June 2016 52-FD-10 Trends in Simulation Based Engineering (Invited) Jefferson East Chaired by: M. MALIK, NASA-Langley Research Center and M. ROGERS, NASA-Ames Research Center 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2016-2914 Oral Presentation Oral Presentation AIAA-2016-2916 AIAA-2016-2917 AIAA-2016-2918 The Need for Advanced Requirements for Certification DLR’s efforts for Digital Flight: Outcomes from the DOE Future Directions of High Unstructured Grid Adaptation: Simulations for Advanced Air by Analysis and Implications A Virtual Aircraft Technology Workshop on Turbulent Flow Fidelity CFD for Aerothermal Status, Potential Impacts, and Vehicle Concepts for CFD Integration Platform Simulation at the Exascale Turbomachinery Analysis and Recommended Investments J. Dryer, NASA Headquarters, R. Gregg-III, The Boeing Company, C. Rossow, N. Kroll, S. Goertz, M. Sprague, National Renewable Energy Design Towards CFD 2030 Washington, D.C.; M. Rogers, NASA Seattle, WA; J. Alonso, Stanford German Aerospace Center (DLR), Laboratory, Golden, CO; S. Boldyrev, G. Laskowski, J. Kopriva, V. M. Park, NASA Langley Research Ames Research Center, MOFFETT University, Stanford, CA Braunschweig, Germany University of Wisconsin, Madison, Michelassi, S. Shankaran, GE Center, Hampton, VA; A. Loseille, FIELD, CA Madison, WI; C. Chang, Princeton Aviation, Lynn, MA; U. Paliath, R. French National Institute for Research University, Princeton, NJ; P. Fischer, Bhaskaran, GE Global Research, in Computer Science and Control University of Illinois, Urbana-Champaign, Niskayuna, NY; et al. (INRIA), Le Chesnay, France; J. Urbana, IL; R. Grout, National Renewable Krakos, T. Michal, The Boeing Energy Laboratory, Golden, CO; W. Company, St. Louis, MO; J. Alonso, Gustafson, Pacific Northwest National Stanford University, Stanford, CA Laboratory, Richland, WA; et al. Monday, 13 June 2016 53-FD-11 Solver Techniques I Holmead West Chaired by: P. BUNING, NASA-Langley Research Center and D. FRENCH, University of Cincinnati 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2016-2919 AIAA-2016-2920 AIAA-2016-2921 AIAA-2016-2922 AIAA-2016-2923 AIAA-2016-2924 Comparative Analysis of the Cartesian Grid Method for Near-Body Grid Adaption for Theoretical Error Analysis of Hybrid Parallel CPU-GPU Multilevel Parallelism for Arbitrary Mesh Interface(AMI) Complex Compressible Flows Overset Grids Direct Overset Finite Element Incompressible Flow Solver with CFD Codes on Heterogeneous and Overset Methods for Dynamic and Its Applications P. Buning, NASA Langley Research Methods Ghost-cell Immersed Boundary Platforms 62 Body Motions in OpenFOAM N. Zhao, Z. Shen, Nanjing University Center, Hampton, VA; T. Pulliam, D. French, University of Cincinnati, Method and Adaptive Mesh B. Baghapour, A. McCall, C. Roy, D. Chandar, H. Gopalan, Institute of High of Aeronautics and Astronautics, NASA Ames Research Center, Moffett Cincinnati, OH; J. Benek, C. Schrock, Refinement Virginia Polytechnic Institute and Performance Computing, Singapore, Nanjing, China; O. Hu, Aviation Field, CA Air Force Research Laboratory, Wright- A. Jost, J. Zhang, Florida Institute of State University, Blacksburg, VA Singapore Industry Corporation of China (AVIC), Patterson AFB, OH Technology, Melbourne, FL Jingdezhen, China Monday, 13 June 2016 54-FD-12 Discontinuous Galerkin Methods - Applications Jay Chaired by: K. SHAHBAZI, South Dakota School of Mines and Technology and D. KESSLER, Naval Research Laboratory 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs AIAA-2016-2925 AIAA-2016-2926 AIAA-2016-2927 AIAA-2016-2928 AIAA-2016-2929 AIAA-2016-2930 AIAA-2016-2931 Simulations of Compressible Progress Towards the A Reconstructed Direct A Direct Discontinuous Galerkin Validation of Overset A fully-implicit, Giles-type Supersonic Film Cooling Taylor-Green Flow by a Application of the Recovery- Discontinuous Galerkin Method Method for Computation of Discontinuous Galerkin and nonreflecting boundary Simulation with a DG Method Discontinuous Galerkin Method Based Disontinuous Galerkin for Compressible Turbulent Flows Turbulent Flows on Hybrid Hybrid RANS/LES Method for condition in a DG-Chimera X. Shi, N. Hu, G. Zhang, C. Yue, X. H. Atkins, NASA Langley Research Method to Practical Flow on Hybrid Grids Grids Jet Noise Prediction turbomachinery solver Yuan, China Academy of Aerospace Center, Hampton, VA Physics Problems X. Yang, Commercial Aircraft Corporation J. Cheng, Beihang University, Beijing, R. Harris, R. Arslanbekov, CFD N. Wukie, P. Orkwis, M. Turner, Aerodynamics, Beijing, China; C. Shu, P. Johnson, E. Johnsen, University of of China, Ltd. (COMAC), Shanghai, China; X. Liu, North Carolina State Research Corporation, Huntsville, University of Cincinnati, Cincinnati, Brown University, Providence, RI Michigan, Ann Arbor, Ann Arbor, MI China; J. Cheng, Beihang University, University, Raleigh, NC; X. Yang, AL; A. Sescu, E. Collins, E. Luke, OH Beijing, China; X. Liu, C. Wang, North Commercial Aircraft Corporation of Mississippi State University, Carolina State University, Raleigh, NC; China, Ltd. (COMAC), Shanghai, Mississippi State, AL J. Si, Commercial Aircraft Corporation of China; T. Liu, Beihang University, China, Ltd. (COMAC), Shanghai, China; Beijing, China; H. Luo, North Carolina H. Luo, North Carolina State University, State University, Raleigh, NC Raleigh, NC Monday, 13 June 2016 55-FD-13 Shock-Boundary Layer Interaction I Oak Lawn Chaired by: J. BENEK, Air Force Research Lab AFRL/RQ and P. MORGAN, Ohio Aerospace Institute 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2016-2932 AIAA-2016-2933 AIAA-2016-2934 AIAA-2016-2935 AIAA-2016-2936 AIAA-2016-2937 Reynolds-Averaged Navier- Investigation of Unsteadiness Effect of Reynolds Number on Sharp-Fin Induced Shock Low-frequency unsteadiness in Pulse Energy Effect on Stokes Simulations of Swept in a Mach 2 Swept-Ramp 3-D Shock Wave Boundary Wave/Turbulent Boundary a wide-span hypersonic shock/ Shock Wave Boundary Layer Shock Wave Boundary Layer Shock/Boundary-Layer Layer Interactions Layer Interactions in an turbulent boundary layer Interaction Control using Interactions at Mach 2 and 5 Interaction Using 50 kHz PIV A. Baldwin, N. Arora, R. Kumar, Axisymmetric Configuration interaction Repetitive Energy Depositions K. Holst, J. Schmisseur, University of L. Vanstone, N. Clemens, M. Saleem, F. Alvi, Florida State University, J. Pickles, P. Subbareddy, V. C. Helm, M. Martin, University of A. Iwakawa, T. Tamba, S. Pham, T. Tennessee, Tullahoma, Tullahoma, TN S. Seckin, University of Texas, Austin, Tallahassee, FL Narayanaswamy, North Carolina Maryland, College Park, College Shoda, A. Sasoh, Nagoya University, Austin, TX State University, Raleigh, NC Park, MD Nagoya, Japan Monday, 13 June 2016 56-FD-14 High-Speed Boundary-Layer Transition I Lincoln East Chaired by: R. KIMMEL, USAF AFRL/RQHF and B. WHEATON, JHU Applied Physics Laboratory 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2016-2938 AIAA-2016-2939 AIAA-2016-2940 AIAA-2016-2941 AIAA-2016-2942 AIAA-2016-2943 Instability Measurements in the Laminar-Turbulent Transition Modal Analysis of Receptivity PSE and Spatial Biglobal DNS and PSE study on the Optical Measurements of Boeing/AFOSR Mach-6 Quiet on a Flared Cone at Mach 6 Mechanisms for a Freestream Instability Analysis of HIFiRE-5 stabilization effect of hypersonic Transitional Events in a Mach-6 Tunnel C. Hader, H. Fasel, University of Hot-Spot Perturbation on Geometry boundary layer waves using 2-D Laminar Boundary Layer J. Edelman, B. Chynoweth, G. Arizona, Tucson, Tucson, AZ a Blunt Compression-Cone T. Kocian, A. Moyes, C. Mullen, H. surface roughness S. Gordeyev, T. Juliano, University of McKiernan, C. Sweeney, S. Boundary Layer Reed, Texas A&M University, College K. Fong, X. Zhong, University of Notre Dame, Notre Dame, IN Schneider, Purdue University, West M. Miselis, Y. Huang, X. Zhong, Station, TX California, Los Angeles, Los Angeles, CA Lafayette, IN University of California, Los Angeles, Los Angeles, CA

63 Monday, 13 June 2016 57-FD-15 High-Order Methods I Columbia 10 Chaired by: D. WILLIS, University of Massachusetts Lowell and C. LIANG, George Washington University 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2016-2944 AIAA-2016-2945 AIAA-2016-2946 AIAA-2016-2947 AIAA-2016-2948 AIAA-2016-2949 A High-Order Conservative High-Order Eulerian Methods High-Order Strand Grid Implicit Spectral Difference High-Order Hybrid Fourier A high order spectral difference Eulerian Simulation Method for for Elastic-Plastic Flow in Solids Methods for Multi-species Method Solutions of Continuation-WENO Scheme for method for fluid-structure Vortex Dominated Flows and Coupling with Fluid Flows Reacting Flow Compressible Flows Considering 3D Compressible Navier-Stokes interaction using an implicit- J. Bevan, D. Willis, University of N. Ghaisas, A. Subramaniam, S. Lele, C. Blakely, A. Katz, O. Tong, Utah High-Order Meshes Equations explicit RK coupling scheme Massachusetts, Lowell, Lowell, MA Stanford University, Stanford, CA State University, Logan, UT F. Moreira, E. Jourdan, C. Breviglieri, K. Shahbazi, South Dakota School of X. Zhang, C. Liang, L. Li, Z. Zhang, J. Technological Institute of Aeronautics Mines and Technology, Rapid City, SD Lee, George Washington University, (ITA), São José dos Campos, Brazil; Washington, D.C. A. Aguiar, Federal University of ABC, Santo André, Brazil; J. Azevedo, Aeronautics and Space Institute (IAE), São José dos Campos, Brazil Monday, 13 June 2016 58-FT-1 Flight Testing of Manned Aircraft Gunston West Chaired by: S. GINN, NASA AFRC and R. ROEDTS, Columbia Helicopters, Inc 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2016-2950 AIAA-2016-2951 AIAA-2016-2952 AIAA-2016-2953 AIAA-2016-2954 Oral Presentation Wing Deformation Background Oriented Schlieren Entry Flight Testing the Space Flight Test Experiments on Variable Stability Learjets – Instrumentation and Baseline Measurement As Bases for (BOS) of a Supersonic Aircraft Shuttle, 1977 to 1984 Cavity Flow in a SUU-41 Pod First Flights of an Old Airplane Characterization of a Tecnam In-flight Aerodynamics in Flight D. Cooke, Cooke Concepts and Z. Probst, M. Reeder, Air Force with a New VSS P2006T for the SCEPTOR R. Tagai, K. Nakakita, M. Kurita, J. Heineck, NASA Ames Research Solutions, Gettysburg, PA; J. Engle, Institute of Technology, Wright- Z. McCarley, J. Lindak, Calspan Distributed Electric Propulsion T. Nakajima, Japan Aerospace Center, Moffett Field, CA; D. Banks, Engle Technologies, Houston, TX Patterson AFB, OH; R. Johnson, J. Corporation, Niagara Falls, NY test vehicle. Exploration Agency (JAXA), Chofu, NASA Armstrong Flight Research Center, Grove, Air Force Research Laboratory, T. Foster, D. Howe, P. Osterkamp, Japan Edwards, CA; E. Schairer, NASA Ames Wright-Patterson AFB, OH Empirical Systems Aerospace, Inc., Research Center, Moffett Field, CA; E. Pismo Beach, CA Haering, P. Bean, NASA Armstrong Flight Research Center, Edwards, CA Monday, 13 June 2016 59-MAO-3 Design Optimization of Aircrafts and Other Complex Systems II Cardozo Chaired by: A. NAJAFI, ANSYS, Inc. and S. CHOI, Virginia Polytechnic Institute and State University 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2016-2955 AIAA-2016-2956 AIAA-2016-2957 AIAA-2016-2958 AIAA-2016-2959 AIAA-2016-2960 Control Power Optimization Comparing Different Off-the- Development of a Topology Optimization of a Efficient Framework for Missile Multidisciplinary Design Using Artificial Intelligence Shelf Optimizers’ Performance Multidisciplinary Design Blended-Wing-Body Aircraft Design and 6DoF Simulation Optimization Research of For Forward Swept Wing And in Conceptual Aircraft Design Analysis and Optimization Structure using Multi-fidelity Analysis overall Aero-engine based on Hybrid Wing Body Aircraft A. Wendorff, E. Botero, J. Alonso, Toolset for Integrated G. Singh, V. Toropov, Queen Mary and Data Fusion Flow Path M. Adegbindin, N. Love, R. Kapania, Stanford University, Stanford, CA Spacecraft Subsystem Models University of London, London, United N. Nguyen, M. Tyan, J. Lee, Konkuk X. Shen, W. Hu, Beihang University, J. Schetz, Virginia Polytechnic T. Winter, M4 Engineering, Inc., Long Kingdom; J. Eves, Altair Engineering, University, Seoul, South Korea Beijing, China 64 Institute and State University, Beach, CA; B. Coleman, H. Pernicka, Inc., Bristol, United Kingdom Blacksburg, VA Missouri University of Science and Technology, Rolla, MO Monday, 13 June 2016 60-MAO-4 Shape and Topology Optimization II Columbia 3 Chaired by: S. CHOWDHURY, University at Buffalo and T. HEARN, NASA Glenn Research Center 1400 hrs 1430 hrs 1500 hrs AIAA-2016-2961 AIAA-2016-2962 AIAA-2016-2963 A Multifidelity Multiobjective Comparison and combination An Efficient Unsteady Optimization Framework for of experience-based Aerodynamic and Aeroacoustic High-Lift Airfoils parameterization with vertex Design Framework Using J. Demange, A. Savill, T. Kipouros, morphing in aerodynamic shape Discrete Adjoint Cranfield University, Cranfield, United optimization of a forward-swept B. Zhou, T. Albring, N. Gauger, Kingdom wing aircraft Technical University of Kaiserslautern, D. Baumgärtner, Technical University of Kaiserslautern, Germany; T. Munich, Munich, Germany; A. Viti, A. Economon, J. Alonso, Stanford Dumont, G. Carrier, ONERA, Meudon, University, Stanford, CA France; K. Bletzinger, Technical University of Munich, Munich, Germany Monday, 13 June 2016 61-MST-3 Human Factors, Perception, and Cueing Morgan Chaired by: D. CARTMELL, Boeing Engineering Operations & Technology and C. TAYLOR, The MITRE Corporation 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs AIAA-2016-2964 AIAA-2016-2965 AIAA-2016-2966 AIAA-2016-2967 AIAA-2016-2968 Interactions of Outside Visual Effects of Different Heave Measurement of Perceived Flight Crew Response to Functional Symbology – Cues and Motion Cueing Motion Components on Pilot Motion In a Fixed Base Unexpected Events: A Simulator Evaluation of task-specific Settings in Yaw Tracking Pitch Control Behavior Simulator Experiment Head-Up Display information H. Peterse, D. Pool, M. van Paassen, P. Zaal, San Jose State University, S. Chivukula, F. Cardullo, K. Zaychik, J. Field, National Aerospace Laboratory for use on a commercial flight M. Mulder, Delft University of Moffett Field, CA A. Momani, State University of New (NLR), Amsterdam, The Netherlands; deck Technology, Delft, The Netherlands York, Binghamton, NY L. Fucke, B. Correia Grácio, The Boeing D. Richards, Coventry University, Company, Madrid, Spain; F. Mohrmann, Coventry, United Kingdom; P. Lamb, National Aerospace Laboratory (NLR), BAE Systems, Rochester, United Amsterdam, The Netherlands Kingdom Monday, 13 June 2016 62-MST-4 Modeling and Simulation of Uninhabited Aerial Vehicles II Monroe Chaired by: S. BEARD, NASA-Ames Research Center and T. BURRESS, Lockheed Martin 1400 hrs 1430 hrs 1500 hrs 1530 hrs AIAA-2016-2969 AIAA-2016-2970 AIAA-2016-2971 AIAA-2016-2972 Modeling SJA-based UAV Flight Analysis of Onboard Takeoff Small-scale coaxial armed Attitude and Altitude Control in Extraterrestrial and Landing Characteristics for unmanned helicopter flight Stabilization of Fixed Wing Conditions Unmanned Aerial Vehicles dynamics investigation VTOL Unmanned Air Vehicle P. Pagadala, M. Reed, E. Besson, V. D. Liu, G. Liu, G. Hong, Beihang M. Wu, M. Chen, F. Wang, Q. Wang, A. Guclu, ROKETSAN Missile Golubev, N. Uddanti, Embry-Riddle University, Beijing, China Beihang University, Beijing, China Industries, Inc., Ankara, Turkey; Aeronautical University, Daytona D. Kurtulus, Middle East Technical Beach, FL University, Ankara, Turkey; K. Arikan, 65 Atilim University, Ankara, Turkey Monday, 13 June 2016 63-PDL-2 Plasma and Laser Diagnostics Piscataway Chaired by: J. DRAKES, Aerojet Rocketdyne and C. SUCHOMEL, USAF 1400 hrs 1430 hrs 1500 hrs 1530 hrs AIAA-2016-2973 AIAA-2016-2974 AIAA-2016-2975 AIAA-2016-2976 Assessment of Coherent Laser Characterization of NO Laser Light Scattering from A Microscopic Study of Laser Diagnostic Techniques for Production Over Metallic Equilibrium, High Temperature Interactions with Single Probing Atomic Oxygen in Surfaces in Air Plasmas Using Gases: Limitations on Rayleigh Levitated Liquid Droplets in an High-Enthalpy Flows Laser Induced Fluorescence Scattering Thermometry Electrodynamic Balance A. Meindl, T. Hermann, S. Loehle, L. Allen, J. Meyers, D. Fletcher, C. Limbach, C. Dumitrache, A. Yalin, C. Limbach, R. Robinson, D. Adams, S. Fasoulas, University of Stuttgart, University of Vermont, Burlington, Colorado State University, Fort M. Wilbanks, A. Yalin, Colorado State Stuttgart, Germany Burlington, VT Collins, CO University, Fort Collins, CO Monday, 13 June 2016 64-TP-2 Ablation II - Modeling DuPont Chaired by: B. HOLLIS, NASA-Langley Research Center and T. GOKCEN, Analytical Mechanics Associates, Inc. 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2016-2977 AIAA-2016-2978 AIAA-2016-2979 AIAA-2016-2980 AIAA-2016-2981 AIAA-2016-2982 Two-Dimensional Modeling of Inverse Heat Conduction Overview of the CHarring Tangle-free Finite Element Advanced Parallelization Development and Verification Ablation and Pyrolysis with Methods in the CHAR Code Ablator Response (CHAR) Code Mesh Motion for Ablation Strategies for Modelling Flow of Enclosure Radiation Application to Rocket Nozzles for Aerothermal Flight Data A. Amar, B. Oliver, B. Kirk, G. Problems Through Ablative Thermal Capabilities in the CHarring P. Cross, Naval Air Warfare Center, Reconstruction Salazar, NASA Johnson Space J. Droba, NASA Johnson Space Protection Systems Ablator Response (CHAR) code. China Lake, CA; I. Boyd, University of B. Oliver, A. Amar, NASA Johnson Center, Houston, TX; J. Droba, HX5, Center, Houston, TX R. Jambunathan, D. Levin, University of G. Salazar, J. Droba, B. Oliver, A. Michigan, Ann Arbor, Ann Arbor, MI Space Center, Houston, TX Houston, TX Illinois, Urbana-Champaign, Urbana, IL Amar, NASA Johnson Space Center, Houston, TX Monday, 13 June 2016 65-RLA-1 Rising Leaders in Aerospace: Speed Networking and Reception International Ballroom 1500 - 1715 hrs (West) Get your questions answered! Senior Mentors will include:

Mark Ballin Brad Belcher John Cavolowsky Peter Coen Fayette Collier Michael Corcoran NASA Langley Research Center Rolls Royce NASA NASA Langley Research Center NASA The Boeing Company Peggy Cornelle Barbara Esker Matthew Hutchison Sally Johnson Dean Jorgensen Art Mallett NASA Glenn Research Center NASA Aurora Flight Sciences Adaptive Aerospace group, Inc. Space Electronics Dunmore Corporation Jayant Ramakrishnan David Riley Lisa Teague Richard Wahls Matthew Hutchison Gregor Verble Mikic Bastion Technologies Boeing Engineering Operations and Technology Rolls Royce NASA Langley Research Center Aurora Flight Sciences Joby Aviation

Monday, 13 June 2016 66-NW-2 Networking Coffee Break Meeting Room Foyers 1600 - 1630 hrs 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. Monday, 13 June 2016 67-LEC-2 Aerodynamics Award Lecture Cabinet 1630 - 1730 hrs Some Applications of Computational Fluid Dynamics to Entry and Landing of the Mars Science Laboratory Pieter Buning Aerospace Technologist NASA Langley Research Center 66 Monday, 13 June 2016 68-PLNRY-2 Plenary International Ballroom 1730 - 1830 hrs (Center) Making Dreams into Reality—The Epochal Stories That Define the Boeing Company Michael Lombardi Director of Boeing Archives The Boeing Company Tuesday Tuesday, 14 June 2016 69-SB-2 Speakers’ Briefing Session Rooms 0730 - 0800 hrs 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 session to exchange bios and review final details prior to the session. Please attend on the day of your session. Tuesday, 14 June 2016 70-PLNRY-3 Plenary International Ballroom 0745 - 0900 hrs (Center)

0745 hrs Renewing Innovation in U.S. Aeronautics Congressman Steve Knight (R-CA) House Committee on Science, Space, and Technology

0810 hrs Innovation and Inspiration — The HondaJet Michimasa Fujino President & CEO Honda Aircraft Company Tuesday, 14 June 2016 71-NW-3 Networking Coffee Break Columbia 0845 - 0930 hrs 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. Tuesday, 14 June 2016 72-AFM-5 Aircraft Flight Dynamics II Holmead West Chaired by: F. FRESCONI, US Army Research Lab 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2016-2983 AIAA-2016-2984 AIAA-2016-2985 AIAA-2016-2986 AIAA-2016-2987 Propeller Torque Effect on A wind tunnel tested control Aerobatic Maneuvers of a Development and Evaluation of Formation Flight for Steady-State Turn Trim of system for a morphing wing Compound Rotorcraft at High a Unified Control Architecture Fuel Saving in Coronet Standard and Mass-Actuated actuation mechanism Advance Ratios - Flight Path for a Compound Rotorcraft in Mission - Part A: Sweet Spot Airplane M. Tchatchueng Kammegne, R. Botez, L. Generation and Dynamic Maneuvering Flight Determination S. Erturk, A. Dogan, University of Grigorie, University of Québec, Montréal, Simulation A. Thorsen, J. Horn, Pennsylvania C. Kniffin, A. Dogan, University of Texas, Arlington, Arlington, TX Canada; M. Mamou, Y. Mebarki, A. Thorsen, J. Horn, Pennsylvania State University, University Park, PA Texas, Arlington, Arlington, TX; W. National Research Council Canada, State University, University Park, PA Blake, Air Force Research Laboratory, Ottawa, Canada Wright-Patterson AFB, OH Tuesday, 14 June 2016 73-AFM-6 Unmanned Aerial Systems I Holmead East Chaired by: T. FIELDS, University of Missouri-Kansas City and K. CUNNINGHAM, NASA Langley Research Center 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2016-2988 AIAA-2016-2989 AIAA-2016-2990 AIAA-2016-2991 AIAA-2016-2992 AIAA-2016-2993 Development of Robust Flight Meta Aircraft Controllability Overcoming the Challenges of An Autonomous, Visually- Linear Control of Highly Assessment of Asymmetric Control Laws for a Highly Flexible B. Troub, C. Montalvo, University of Using Unmanned Aircraft for Guided, Counter-sUAS Flexible Aircraft based on Loop Flight on Solar UAS

67 Aircraft in the Frequency Domain South Alabama, Mobile, AL Bridge Inspections Aerial Vehicle with Net Separation E. Belfield, A. Drake, California A. Köthe, R. Luckner, Technical University I. Hernandez, T. Fields, J. Kevern, Countermeasure P. Gonzalez, F. Silvestre, P. Paglione, Polytechnic State University, San Luis of Berlin, Berlin, Germany; P. González University of Missouri, Kansas City, T. Horiuchi, M. Paras, T. Cervi, B. Technological Institute of Aeronautics Obispo, CA Ramirez, F. Silvestre, Technological Kansas City, MO Oursler, S. Sanz, J. Gaus, University (ITA), São José dos Campos, Brazil; Institute of Aeronautics (ITA), São José of Maryland, College Park, College A. Köthe, Technical University of dos Campos, Brazil; Z. Pang, C. Cesnik, Park, MD; et al. Berlin, Berlin, Germany; Z. Pang, C. University of Michigan, Ann Arbor, Ann Cesnik, University of Michigan, Ann Arbor, MI Arbor, Ann Arbor, MI Tuesday, 14 June 2016 74-AMT-3 Velocimetry II Columbia 2 Chaired by: J. JEWELL, Air Force Research Laboratory and R. BURNS, NASA Langley Research Center 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2016-2994 AIAA-2016-2995 AIAA-2016-2996 AIAA-2016-2997 AIAA-2016-2998 Applications of Temporal PIV Measurements of a Investigation on the Response Investigation of the influence In-Flight PIV for CROR Flight Supersampling in Pulse-Burst PIV plunging Airfoil at High Angles Mechanisms of Tracer Particles of subgrid-scale stress on the Test Demonstration S. Beresh, J. Wagner, E. Demauro, J. of Attack for PIV measurements in accuracy of non-intrusive spatial V. Pommier-Budinger, Y. Bury, Henfling, R. Spillers, P. Farias, Sandia M. Zakaria, F. Jafari, M. Hajj, Virginia Supersonic Flows pressure measurement using a University of Toulouse, Toulouse, National Laboratories, Albuquerque, NM Polytechnic Institute and State F. Chen, Y. Mi, X. Chen, H. Liu, DNS channel flow database France; G. Michon, Clément Ader University, Blacksburg, VA Shanghai Jiao Tong University, X. Liu, S. Siddle-Mitchel, San Diego State Institute, Toulouse, France; G. Napias, Shanghai, China University, San Diego, CA; J. Katz, Johns University of Toulouse, Toulouse, Hopkins University, Baltimore, MD France Tuesday, 14 June 2016 75-AMT-4 Global Surface Measurements Oak Lawn Chaired by: T. IOPPOLO, Southern Methodist University and B. THUROW, Auburn University 0930 hrs 1000 hrs 1030 hrs AIAA-2016-2999 AIAA-2016-3000 AIAA-2016-3001 Development of a Grid PSP/ Skin Friction Measurements An Experimental Study of TSP System for Unsteady to Evaluate Viscous Drag Barchan-Dune-Shaped Injection Measurements on Rotating Reduction Approaches Compounds for Improved Film Surfaces J. Naughton, E. DeMillard, P. Cooling Effectiveness D. Peng, L. Jiao, Y. Liu, Shanghai Jiao Davidson, University of Wyoming, W. Zhou, H. Hu, Iowa State Tong University, Shanghai, China Laramie, Laramie, WY University, Ames, IA Tuesday, 14 June 2016 76-APA-10 VSTOL/STOL Applications Columbia 9 Chaired by: N. HALL and J. GEORGE, Metrolaser Inc. 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2016-3002 AIAA-2016-3003 AIAA-2016-3004 AIAA-2016-3005 AIAA-2016-3006 Aerodynamic Analysis for Numerical Investigations of Experimental Verification of a Unsteady Velocity UC2AV:Unmanned Circulation Conceptual Design of a Lift-Fan Fan-In-Wing Aerodynamic Semi-Empirical V/STOL Aircraft Measurements of Supersonic Control Aerial Vehicle for Short type Aircraft Performance with Active Flow Performance Analysis Method Military-Style Exhaust Jets in Takeoff and Enhanced Payload H. Lee, R. Prasad, S. Choi, Virginia Control M. Bronz, A. Drouin, French Civil Practical Configurations K. Kanistras, P. Saka, K. Valavanis, Polytechnic Institute and State C. Sheng, Q. Zhao, University of Aviation University, Toulouse, France S. Hromisin, Pennsylvania State M. Rutherford, University of Denver, University, Blacksburg, VA Toledo, Toledo, OH University, University Park, PA; R. Denver, CO Powers, L. Myers, Naval Air Systems Command, Patuxent River, MD; D. McLaughlin, Pennsylvania State University, University Park, PA 68 Tuesday, 14 June 2016 77-APA-11 Aerodynamic - Structural Modeling, Optimization, and Test Techniques for Flexible Wing Technology I Albright Chaired by: N. NGUYEN, NASA-Ames Research Center and A. JONES, University of Maryland 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2016-3007 AIAA-2016-3008 AIAA-2016-3009 AIAA-2016-3010 AIAA-2016-3011 AIAA-2016-3012 Wing Shaping Concept for A Study on VGTM Actuation Comparison of Curvilinear Aerodynamic Characteristics A Status Review of the Aerodynamic Modeling of Distributed Propulsion Aircraft System for Multi Axis Morphing Stiffeners and Tow Steered and Shape Optimization of a Commercial Supersonic Transonic Aircraft Using Vortex to Improve Aerodynamic Wing of UAV Composites for Aeroelastic Variable Camber Compliant Technology (CST) Lattice Coupled with Transonic Efficiency P. Shanmugam, S. Raja, National Tailoring of Transports Wing Aeroservoelasticity (ASE) Small Disturbance for Conceptual N. Nguyen, K. Reynolds, NASA Ames Aerospace Laboratories, Bengaluru, B. Stanford, NASA Langley Research Y. Jo, Korea Advanced Institute of Project Design Research Center, Moffett Field, CA; E. India; K. Parammasivam, F. Zohra, Center, Hampton, VA; C. Jutte, Craig Science and Technology, Daejeon, W. Silva, M. Sanetrik, P. Chwalowski, D. Chaparro, MORI Associates, Inc., Ting, Stinger Ghaffarian Technologies, Anna University, Chennai, India Technologies, Inc., Cape Canaveral, FL South Korea; S. Choi, Virginia C. Funk, NASA Langley Research Moffett Field, CA; G. Fujiwara, University Inc., Moffett Field, CA Polytechnic Institute and State Center, Hampton, VA of Washington, Seattle, Seattle, WA; E. University, Blacksburg, VA; L. Ting, Stinger Ghaffarian Technologies, Zientarski, J. Joo, Air Force Research Inc., Moffett Field, CA; N. Nguyen, NASA Laboratory, Wright-Patterson AFB, OH Ames Research Center, Moffett Field, CA Tuesday, 14 June 2016 78-APA-12 Propeller/Rotorcraft/Wind Turbine Aerodynamics II Northwest Chaired by: J. RAULEDER, Technical University of Munich and J. CODER, Applied Research Laboratory - Penn State 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2016-3013 AIAA-2016-3014 AIAA-2016-3015 AIAA-2016-3016 AIAA-2016-3017 AIAA-2016-3018 Aeromechanics Analysis of Investigation of Centrifugal Pusher-Propeller Blade Loading A More Comprehensive Effect of Reynolds Numbers of Turbulent Boundary Layer a Coaxial Rotor System in Pumping Rotor Blades in Hover With and Without Pylon Database for Low Reynolds 10,000 to 100,000 on Rotor Response to Multiple Step Hover and High-Advance-Ratio Using CFD Trailing-Edge Blowing Number Propeller Performance Blades of Small Unmanned Changes in Surface Roughness Forward Flight S. Platzer, J. Rauleder, M. Hajek, T. Sinnige, D. Ragni, G. Eitelberg, Validations Aerial Vehicles J. George, MetroLaser, Inc., Laguna R. Feil, J. Rauleder, M. Hajek, Technical University of Munich, L. Veldhuis, Delft University of A. Ghoddoussi, L. Miller, Wichita H. Otsuka, K. Nagatani, Tohoku Hills, CA; G. Byun, R. Simpson, Technical University of Munich, Munich, Germany Technology, Delft, The Netherlands State University, Wichita, KS University, Sendai, Japan Applied University Research, Inc., Munich, Germany Blacksburg, VA Tuesday, 14 June 2016 79-APA-13 Hypersonic Aerodynamics Jefferson West Chaired by: A. VANDERWYST, Leidos and B. OSBORNE, The Boeing Company 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2016-3019 AIAA-2016-3021 AIAA-2016-3022 AIAA-2016-3023 AIAA-2016-3024 Numerical analysis of a Coefficient Revision for Euler model of mass loss in Aerodynamic Force Numerical Simulation of Time- separated flow on a supersonic Supersonic Turbulent Density the process of hypersonic solid Measurements during 100 Varying Plasma Sheath for cone flare model Fluctuation Model particle impact Milliseconds Test Duration Reentry Vehicle O. Frayssinet, French Atomic Energy H. Pan, P. Su, X. Cheng, H. Ma, China H. Dai, C. Zhu, H. Zhao, Z. Wang, Y. Wang, Y. Liu, C. Luo, Z. Jiang, C. Shao, T. Deyang, W. Chen, and Alternative Energies Commission, Academy of Aerospace Aerodynamics, Nanjing University of Aeronautics and Chinese Academy of Sciences, Zhejiang University, Hangzhou, China Le Barp, France Beijing, China Astronautics, Nanjing, China Beijing, China Tuesday, 14 June 2016 80-APA-14 Transonic & Supersonic Aerodynamics Columbia 4 69 Chaired by: M. POST, USAF Academy and V. BHAGWANDIN, US Army Research Laboratory 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2016-3025 AIAA-2016-3026 AIAA-2016-3027 AIAA-2016-3028 AIAA-2016-3029 A novel mid-field breakdown An Investigation of C-130 Development of Deformed CAD Shape Optimization of CFD Performance of Turbulence of the aerodynamic force in Aircraft Base Drag Reduction Geometries of NASA’s Common Supersonic Bodies to Reduce Models for Flow from compressible flows with Aftbody Modifications Research Model for the Sixth AIAA Sonic Boom Signature Supersonic Nozzle Exhausts M. Ostieri, R. Tognaccini, B. Mele, H. Telli, Turkish Air Force Academy, CFD Drag Prediction Workshop J. Li, T. Wray, R. Agarwal, H. Lee, T. Wray, R. Agarwal, University of Naples “Federico II”, Istanbul, Turkey; E. Ayan, Middle S. Keye, German Aerospace Center Washington University in St. Louis, Washington University in St. Louis, Naples, Italy East Technical University, Ankara, (DLR), Braunschweig, Germany; M. St. Louis, MO St. Louis, MO Turkey; S. Soyer, Istanbul Technical Gammon, International TechneGroup, University, Istanbul, Turkey; E. Inc. (ITI), Cambridge, United Kingdom Gülsever, S. Özcan, Turkish Air Force Academy, Istanbul, Turkey Tuesday, 14 June 2016 81-ASE-5 Aircraft Wake Turbulence III (Invited) Columbia 12 Chaired by: A. BROWN, National Research Council Canada and D. DELISI, Northwest Research Associates Inc 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2016-3030 AIAA-2016-3031 AIAA-2016-3032 AIAA-2016-3033 AIAA-2016-3034 AIAA-2016-3035 The Development of Wake Flight data of axial flows Wake Vortex Collection APA3.8 Fast-Time, Numerical Multi-Model Ensemble Wake A Study on Wake Turbulence Turbulence Re-Categorization in wake vortex instability and Analysis at the Dubai Wake Model Description and Vortex Prediction - Further Encounter during UAV in the United States (Invited) (Invited) International Airport (Invited) Validation (Invited) Development and Probabilistic Formation Flight Using Coupled J. Cheng, A. Hoff, Engility A. Brown, National Research Council M. Fantauzzi, Dubai Air Navigation D. Delisi, NorthWest Research Assessment (Invited) Aerodynamics/Flight Dynamics Corporation, Washington, D.C.; J. Canada, Ottawa, Canada Services, Dubai, United Arab Associates, Redmond, WA; R. Robins, S. Koerner, F. Holzäpfel, German Simulation (Invited) Tittsworth, W. Gallo, Federal Aviation Emirates; D. Delisi, M. Pruis, D. Lai, Scientific Computing Associates, Aerospace Center (DLR), A. He, Z. Zheng, H. Chao, P. Tian, Administration, Washington, D.C. NorthWest Research Associates, Seattle, WA; M. Pruis, NorthWest Oberpfaffenhofen, Germany University of Kansas, Lawrence, Redmond, WA; D. Jacob, Coherent Research Associates, Redmond, WA Lawrence, KS; Y. Gu, West Virginia Research Group, LLC, Key West, FL University, Morgantown, WV Tuesday, 14 June 2016 82-ASE-6/APA-15 Surface Coatings, Ice Protection and Shedding Georgetown West Chaired by: J. PALACIOS, The Pennsylvania State University 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2016-3036 AIAA-2016-3037 AIAA-2016-3038 AIAA-2016-3039 AIAA-2016-3040 AIAA-2016-3041 Multi Time Scale Ice Growth Studies on Electro Impulse Analysis of Piezoelectric Ice Analysis and Prediction of Ice Surface Chemical Functionality Characterization of Insect in Films Flowing Over an De-Icing of a Leading Edge Protection Systems Combined Shedding for a Full-Scale Heated Effect Upon Ice Adhesion Shear Residue on an Aerodynamic Anisotropic Solid Structure in an Icing Wind with Ice-Phobic Coatings Tail Rotor Strength Leading Edge A. Rothmayer, Iowa State University, Tunnel V. Pommier-Budinger, University R. Kreeger, NASA Glenn Research Center, J. Smith, C. Wohl, NASA Langley K. Krishnan, R. Robison, F. Tetteh, Ames, IA H. Sommerwerk, P. Horst, S. of Toulouse, Toulouse, France; M. Cleveland, OH; R. Douglass, Ohio Research Center, Hampton, VA; E. Loth, University of Virginia, Bansmer, Technical University of Budinger, Clément Ader Institute, Northern University, Ada, OH; M. Gazella, R. Kreeger, NASA Glenn Research Charlottesville, Charlottesville, VA; Braunschweig, Braunschweig, Toulouse, France; N. Tepylo, X. Kent State University, Kent, OH; Z. Center, Cleveland, OH; J. Palacios, T. T. Farrell, J. Crouch, The Boeing Germany Huang, Carleton University, Ottawa, Koster, Virginia Polytechnic Institute and Knuth, Pennsylvania State University, Company, Seattle, WA; et al. Canada State University, Blacksburg, VA; J. Turk, University Park, PA Cleveland State University, Cleveland, OH; A. Work, Ohio Aerospace Institute, Cleveland, OH Tuesday, 14 June 2016 83-ATIO.ACD-3 Unmanned Aircraft Gunston East Chaired by: M. LOGAN, NASA Langley Research Center and P. RAJ, Virginia Polytechnic Institute and State University 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2016-3042 AIAA-2016-3043 AIAA-2016-3044 AIAA-2016-3045 AIAA-2016-3046 Design, Flight Mechanics and A Framework for Integrated Unlimited Endurance Low Conceptual design study of an Flight dynamics study of a Flight Demonstration of a Analysis, Design, and Rapid Altitude Wind Powered Anti-Drone Drone small tilt rotor UAV with tail Tiltable Propeller VTOL UAV Prototyping of Small Unmanned Unmanned Aerial Vehicle T. Lefebvre, T. Dubot, ONERA, propeller Z. Öznalbant, M. Kavsaoğlu, M. Airplanes M. Sadraey, Daniel Webster College, Toulouse, France D. Wu, H. Li, Commercial Aircraft 70 Cavcar, Anadolu University, Eskisehir, D. Locascio, C. Ramee, E. Schaus, K. Nashua, NH Corporation of China, Ltd. (COMAC), Turkey Cooksey, Georgia Institute of Technology, Shanghai, China; S. Li, Beihang Atlanta, GA; E. Spero, Army Research University, Beijing, China Laboratory, Aberdeen Proving Ground, MD; D. Mavris, Georgia Institute of Technology, Atlanta, GA Tuesday, 14 June 2016 84-ATIO.ATM-7 UAS Operations II Embassy Chaired by: M. WILCOXEN 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2016-3047 AIAA-2016-3048 AIAA-2016-3049 AIAA-2016-3050 A Value Driven Design A Variable-Fidelity Approach Low-Altitude UAS Traffic Artificial Potantial Field Based Approach to Municipal Electric to Wake Safety Analysis in the Coordination with Dynamic Autonomus UAV Fligh in Utility Unmanned Aerial Context of UAS Integration in Geofencing Dynamic Environment Systems Deployment the NAS G. Zhu, P. Wei, Iowa State University, A. Oguz, E. Duymaz, Turkish Air Force D. Long, S. Ferguson, North Carolina P. Kazarin, V. Golubev, Embry-Riddle Ames, IA Academy, Istanbul, Turkey State University, Raleigh, NC Aeronautical University, Daytona Beach, FL; A. Provalov, ISA Software, Bethesda, MD; S. Borener, D. Hufty, Federal Aviation Administration, Washington, D.C. Tuesday, 14 June 2016 85-ATIO.ATM-8 Delay Management Fairchild East Chaired by: N. NEOGI, NASA Langley Research Center 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2016-3051 AIAA-2016-3052 AIAA-2016-3053 AIAA-2016-3054 Estimating Over-Conservatism Analyzing Double Delays at A Human-in-the-loop Evaluation Analysis of Additional Delays in Airspace Constraint Newark Liberty International of a Coordinated Arrival/ Experienced by Flights Subject Management Airport Departure Scheduling Operations to Ground Holding S. Heitin, J. DeArmon, B. Bateman, A. Evans, University of California, for Managing Departure Delays K. Bilimoria, NASA Ames Research J. Conroy, MITRE Corporation, Santa Cruz, Moffett Field, CA; P. Lee, at LaGuardia Airport Center, Moffett Field, CA McLean, VA NASA Ames Research Center, Moffett P. Lee, N. Smith, NASA Ames Research Field, CA Center, Moffett Field, CA; N. Bienert, C. Brasil, N. Buckley, E. Chevalley, San Jose State University, Moffett Field, CA; et al. Tuesday, 14 June 2016 86-ATIO.DE-1 Design Engineering Gunston West Chaired by: S. ROWE, NASA Marshall Space Flight Center and C. DAVIES, Lockheed Martin Aeronautics 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2016-3055 AIAA-2016-3056 AIAA-2016-3057 AIAA-2016-3058 AIAA-2016-3059 AIAA-2016-3060 Uncertainty Quantification Optimization of an Advanced A Lean Product Development Aerospace Partners for the The Effects of Supersonic Inlet Sizing Study for Assessing via Elicitation of Expert Hybrid Wing Body Concept (LPD) approach on education Advancement of Collaborative Topology on the Installed First-Order Feasibility of the Judgements using HCDstruct Version 1.2 and knowledge management Engineering, a Review Performance of Tubofan Bell X-1A Supersonic Rocket- B. Profir, M. Eres, J. Scanlan, J. Quinlan, F. Gern, NASA Langley in aircraft design M. Wald, S. Gorrell, Brigham Young Engines Powered Aircraft University of Southampton, Research Center, Hampton, VA C. Feltrin, A. de Paula, M. de Queiroz University, Provo, UT; M. Richey, R. Palma, T. Takahashi, Arizona State S. Hussein, B. Chudoba, University of Southampton, United Kingdom; M. Cordova Santos, Technological K. Chang, F. Zender, The Boeing University, Tempe, AZ Texas, Arlington, Arlington, TX Moss, R. Bates, Rolls-Royce Group Institute of Aeronautics (ITA), São Company, Everett, WA 71 plc, Derby, United Kingdom José dos Campos, Brazil Tuesday, 14 June 2016 87-ATIO.TFPC-4/ATIO.GA-1 Transformational Flight - On Demand Mobility Markets/Missions Columbia 1 Chaired by: N. BORER, NASA Langley Research Center and M. MOORE, NASA Langley Research Center 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2016-3061 AIAA-2016-3062 Oral Presentation Oral Presentation AIAA-2016-3063 A Vision and Opportunity for Silicon Valley as an Early Adopter Impact of Operational Inter-Urban Civil VTOL Air-Taxi Regional Sky Transit II Transformation of On-Demand for On-Demand Civil VTOL Requirements on Intra-Urban Feasibility B. Seeley, Sustainable Aviation Air Mobility Operations VTOL Conceptual Design M. Moore, K. Goodrich, K. Antcliff, W. Foundation, Inc., Santa Rosa, CA B. Holmes, Holmes Consulting, LLC, K. Antcliff, M. Moore, K. Goodrich, NASA W. Fredericks, NASA Langley Fredericks, NASA Langley Research Williamsburg, VA Langley Research Center, Hampton, VA Research Center, Hampton, VA Center, Hampton, VA Tuesday, 14 June 2016 88-F360-4 NASA Roadmaps—Guiding Direction for Aeronautics Research Investments International Ballroom 0930 - 1230 hrs (East) Moderator: Richard A. Wahls, Strategic Technical Advisor – Advanced Air Vehicles Program, NASA Aeronautics Research Mission Directorate, NASA Langley Research Center Panelists: Mark Ballin John Cavolowsky Fayette Collier Jay Dryer Barbara Esker Technical Integration Manager for NASA Langley Director, Airspace Operations and Safety Program Manager, Environmentally Responsible Aviation Project Director, Advanced Air Vehicles Program Deputy Manager, Advanced Air Vehicles Program Research Center NASA Aeronautics Research Mission Directorate NASA Langley Research Center Peter Coen, Manager, NASA Aeronautics Research Mission Directorate NASA Airspace Operations and Safety Program NASA Commercial Supersonic Technology Project NASA NASA NASA Susan Gorton Jessica Nowinski Jaiwon Shin Barry Sullivan Tom Davis Manager, Revolutionary Vertical Lift Technology Project Research Psychologist, Human Systems Integration Associate Administrator Integration Manager, Next Generation Air Transportation Technology Advisor, Airspace Systems Technology NASA Langley Research Center Division NASA Aeronautics Research Mission Directorate System (NextGen), Program, Aviation Systems Division NASA NASA NASA Airspace Systems Program Office NASA Ames Research Center NASA NASA

Tuesday, 14 June 2016 89-FC-4 Drag Reduction Columbia 11 Chaired by: R. KIMMEL, USAF AFRL/RQHF 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2016-3064 AIAA-2016-3065 AIAA-2016-3066 AIAA-2016-3067 AIAA-2016-3068 On the effect of discrete The effect of local steady Transonic Airfoil Performance Hairy Chemical Coating for Predetermined control of roughness on crossflow suction on the stability and Enhancement Using Co-Flow Jet Drag Reduction turbulent boundary layer by instability in very low transition of boundary layer on Active Flow Control M. Hasegawa, H. Sakaue, University means of a piezoelectric oscillator of Notre Dame, Notre Dame, IN 72 turbulence environment a flat plate Z. Liu, G. Zha, University of Miami, X. Zheng, H. Zhang, Tianjin University, M. Placidi, E. van Bokhorst, C. Atkin, Z. Huang, Tianjin University, Tianjin, Miami, FL Tianjin, China; S. Yang, Nanyang City University London, London, China; X. Wu, Imperial College Technological University, Singapore, United Kingdom London, London, United Kingdom Singapore; N. Jiang, Tianjin University, Tianjin, China; Y. Wu, Nanyang Technological University, Singapore, Singapore Tuesday, 14 June 2016 90-FD-16 Turbulence Modeling II: RANS, Hybrid RANS/LES Jay Chaired by: L. DUAN, Missouri University of Science and Technology and Y. LV, Stanford University 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2016-3069 AIAA-2016-3070 AIAA-2016-3071 AIAA-2016-3072 AIAA-2016-3073 AIAA-2016-3074 Application of a New Simple Application of the Quadratic Validation of the Wray- Implementation and Validation Simulating Sources of Verification of RANS and Rotation and Curvature Constitutive Relation to Agarwal Turbulence Model for of Correlation-based Transition Unsteadiness in a High-Speed Hybrid RANS-LES Modelling in Correction to the Wray-Agarwal Various Turbulence Models in Shock-Wave Boundary Layer Models in AcuSolve Wall-Bounded Jet Computations of a Delta-Wing Turbulence Model OpenFOAM Interaction Flows S. Medida, D. Corson, M. Barton, K. Low, R. Bush, Pratt & Whitney, Flow X. Zhang, T. Wray, R. Agarwal, H. Nagapetyan, T. Wray, R. Agarwal, F. Acquaye, J. Li, T. Wray, R. Agarwal, Altair Engineering, Inc., Sunnyvale, East Hartford, CT; J. Winkler, United S. Peng, Swedish Defense Research Washington University in St. Louis, Washington University in St. Louis, Washington University in St. Louis, CA Technologies Corporation, East Agency (FOI), Stockholm, Sweden St. Louis, MO St. Louis, MO St. Louis, MO Hartford, CT Tuesday, 14 June 2016 91-FD-17 Combustion Simulation I Monroe Chaired by: B. MAICKE, Pennsylvania State University and K. DURAISAMY, University of Michigan, Ann Arbor 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2016-3075 AIAA-2016-3076 AIAA-2016-3077 AIAA-2016-3078 Application of the Evolution- Simulation of a Lean-Direct Numerical Investigations of Properties of a New Ensemble Variable Manifold Approach Injection Combustor Using a High Frequency Pulsed Fuel Kalman Filter Algorithm for to Cavity-Stabilized Ethylene Body-Fitted Voxel Mesh Injection into Supersonic Combustion Application Combustion C. Wey, NASA Glenn Research Center, Crossflows X. Gao, Y. Wang, N. Overton, N. Cymbalist, California Institute of Cleveland, OH N. Williams, T. Moeller, University of Colorado State University, Fort Technology, Pasadena, CA; G. Candler, Tennessee, Tullahoma, Tullahoma, TN Collins, CO; X. Tu, University of University of Minnesota, Minneapolis, Kansas, Lawrence, Lawrence, KS; M. Minneapolis, MN; P. Dimotakis, California Zupanski, Colorado State University, Institute of Technology, Pasadena, CA Fort Collins, CO Tuesday, 14 June 2016 92-FD-18 Open Issues in Meshing 2030 (Special Issue) Jefferson East Chaired by: J. MASTERS, AEDC and H. THORNBURG, DRC PETTT 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2016-3079 AIAA-2016-3080 AIAA-2016-3081 Open Discusion Geometry, Mesh Generation, The NASA Common Research A Survey of Solver-Related and the CFD 2030 Vision Model: A Geometry-Handling Geometry and Meshing Issues J. Chawner, Pointwise, Inc., Fort Perspective J. Masters, Arnold Engineering Worth, TX; J. Dannenhoffer, Syracuse M. Gammon, International TechneGroup, Development Center, Arnold AFB, TN University, Syracuse, NY; N. Taylor, Inc. (ITI), Cambridge, United Kingdom; MBDA, Filton, United Kingdom N. Taylor, MBDA, Filton, United Kingdom

73 Tuesday, 14 June 2016 93-FD-19 CFD Transition Models Lincoln East Chaired by: H. JOHNSON, University of Minnesota and M. TUFTS, Texas A&M University 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2016-3082 AIAA-2016-3083 AIAA-2016-3084 AIAA-2016-3085 AIAA-2016-3086 Database Approach for 2D Understanding Transition with A Linear Stability Theory-Based Implementation of Three Numerical Aspects of Including Flow Transition Prediction in a Reynolds Stresses and Rapidly Transition Model Using Local Different Transition Methods Crossflow Effects in the RANS Code Distorting Shear Flow Variables for RANS Simulations and Comparative Analysis Recently Proposed Transition G. Bégou, H. Deniau, O. Vermeersch, J. Moore, Self, Blacksburg, VA of Transitional Flow of the Results Computed by Models G. Casalis, ONERA, Toulouse, France J. Xu, J. Bai, L. Qiao, Y. Zhang, Z. Fu, OVERSET Software L. Wang, Z. Liu, S. Fu, Tsinghua Northwestern Polytechnical University, H. Li, Y. Ren, H. Tang, Z. Qian, University, Beijing, China Xi’an, China Aviation Industry Corporation of China (AVIC), Shenyang, China Tuesday, 14 June 2016 94-FD-20 High-Order Methods II Columbia 10 Chaired by: M. PLESNIAK and B. HELENBROOK, Clarkson University 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2016-3087 AIAA-2016-3088 AIAA-2016-3089 AIAA-2016-3090 Adjoint-Consistency of Analysis of Implicit Time- Accuracy Enhancement of a High-Order Entropy Stable Spacetime Discontinuous Advancing p-Multigrid Schemes Riemann-Solver-Free Spacetime Discontinuous Galerkin Galerkin Discretizations for for Discontinuous Galerkin Discontinuous Galerkin Method Schemes in a Space-Time Incompressible Flows Discretizations of the Euler via Constrained Least Square Computational Framework A. Kercher, A. Corrigan, D. Kessler, Equations Reconstruction M. Zakerzadeh, G. May, RWTH R. Johnson, D. Mott, Naval Research B. Mascarenhas, Pratt & Whitney, S. Tu, Jackson State University, Aachen University, Aachen, Germany Laboratory, Washington, D.C. East Hartford, CT; B. Helenbrook, Jackson, MS Clarkson University, Potsdam, NY Tuesday, 14 June 2016 95-GT-2 Assessment and Analysis of Ground Test Facilities Lincoln West Chaired by: W. HUMPHREYS, NASA Langley Research Center and M. RIVERS, NASA Langley Research Center 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2016-3091 AIAA-2016-3092 AIAA-2016-3093 AIAA-2016-3094 AIAA-2016-3095 AIAA-2016-3096 Towards the Use of CFD to Uncertainty Analysis of Test The Impact of Truth Surrogate Uncertainty Propagation via Analysis and calculation of Calculation of Missile Testing Improve and Validate the Wall Data at the NRC 1.5-Meter Variance on Quality Monte Carlo Simulation in the droplet-air mixed phase flow Capability with All Up Round Correction Methodology at the Trisonic Wind Tunnel Assessment/Assurance in Wind PWT and VKF Wind Tunnels model in icing wind tunnel Test Equipment NRC 1.5 m Trisonic Wind Tunnel S. Fakhraei, J. Weiss, University of Tunnel Testing at AEDC D. Qian, Z. Wang, C. Zhu, Nanjing F. Akalin, ROKETSAN Missile A. Toledano, J. Weiss, F. Morency, Québec, Montréal, Canada R. DeLoach, NASA Langley Research C. Morris, Aerospace Testing Alliance, University of Aeronautics and Industries, Inc., Ankara, Turkey University of Québec, Montréal, Center, Hampton, VA Tullahoma, TN; D. Crowley, Arnold Astronautics, Nanjing, China Canada; C. Broughton, A. Engineering Development Complex, Benmeddour, National Research Tullahoma, TN Council Canada, Ottawa, Canada Tuesday, 14 June 2016 96-ITAR-1 Advancements in Oscillating Heat Pipes Cabinet Chaired by: E. SILK, NASA-Goddard Space Flight Center and D. PYTEL, Lockheed Martin Space Systems 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2016-3097 AIAA-2016-3098 AIAA-2016-3099 AIAA-2016-3100 AIAA-2016-3101 The Performance Limits of The effect of hybrid An Empirical Study of the Experimental Investigation of Thermal Performance Oscillating Heat Pipes: Theory hydrophobic and hydrophilic Two-Phase Thermal Resistance Flow Induced Vibrations of an Characterization of Flexible, and Validation surfaces on heat transfer in an Oscillating Heat Pipe Heat Oscillating Heat Pipe Multi-material Oscillating Heat B. Drolen, The Boeing Company, El performance of an oscillating Spreader S. Smith, Air Force Research Laboratory, Pipes Segundo, CA; C. Smoot, ThermAvant heat pipe D. Pounds, J. Boswell, L. Ellebracht, Kirtland AFB, NM; M. Rhodes, Mississippi D. Hengeveld, M. Wilson, LoadPath, Technologies, Columbia, MO F. Zhang, R. Winholtz, H. Ma, ThermAvant Technologies, Columbia, State University, Mississippi State, Albuquerque, NM; B. Taft, Air Force University of Missouri, Columbia, MO MS; E. Ardelean, Acme Solutions, LLC, Research Laboratory, Kirtland AFB, 74 Columbia, MO Albuquerque, NM; B. Taft, Air Force NM Research Laboratory, Kirtland AFB, NM Tuesday, 14 June 2016 97-MAO-5 Design Optimization of Aircrafts and Other Complex Systems III Cardozo Chaired by: A. NAJAFI, ANSYS, Inc. and J. MARTINS, University of Michigan 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2016-3102 AIAA-2016-3103 AIAA-2016-3104 AIAA-2016-3105 AIAA-2016-3106 AIAA-2016-3107 High fidelity aerodynamic Multi-disciplinary Optimization Combined Aerostructural Aeroservoelastic Optimisation Aero-structural approach A Probabilistic Parameter optimization in distributed of Stiffened, Fiber-steered Wing and High-Lift System of an Aerofoil with coupled with direct operative Sensitivity Analysis Approach overall aircraft design Composite Fuselage for Optimization Active Compliant Flap via cost optimization for new aircraft For An Aircraft X. Gu, P. Ciampa, B. Nagel, German Mechanical and Vibro-acoustic K. van den Kieboom, A. Elham, Delft Reparametrisation and design in preliminary design S. Selvi, ROKETSAN Missile Industries, Aerospace Center (DLR), Hamburg, Requirements University of Technology, Delft, The Variable Selection A. Viti, ONERA, Meudon, France; T. Inc., Ankara, Turkey Germany G. Serhat, I. Basdogan, Koç Netherlands J. Broughton-Venner, A. Wynn, R. Druot, Airbus, Toulouse, France; A. University, Istanbul, Turkey Palacios, Imperial College London, Dumont, G. Carrier, ONERA, Meudon, London, United Kingdom France Tuesday, 14 June 2016 98-MAO-6 Shape and Topology Optimization III Columbia 3 Chaired by: J. GRAY, NASA Glenn Research Center and G. KENNEDY, Georgia Institute of Technology 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2016-3108 AIAA-2016-3109 AIAA-2016-3110 AIAA-2016-3111 AIAA-2016-3112 RANS-based Shape Efficient Multi-Objective Topology Optimization of a A CMA-ES enhanced MOEA/D Efficient Aerodynamic Design Optimization of Dual-Rotor Aerodynamic Optimization Bi-Stable Cardiovascular Stent applied to multiobjective using the Discrete Adjoint Wind Turbines using Variable- by Design Space Dimension with Snap-Through Response aerodynamic optimization Method in SU2 fidelity Models Reduction and Co-Kriging K. James, University of Illinois, design T. Albring, M. Sagebaum, N. Gauger, A. Thelen, L. Leifsson, A. Sharma, A. Amrit, L. Leifsson, Iowa State Urbana-Champaign, Urbana, IL; H. X. Zhu, Z. Gao, Northwestern Technical University of Kaiserslautern, Iowa State University, Ames, IA; University, Ames, IA; S. Koziel, Y. Waisman, Columbia University, New Polytechnical University, Xi’an, China Kaiserslautern, Germany S. Koziel, Reykjavik University, Tesfahunegn, Reykjavik University, York, NY Reykjavik, Iceland Reykjavik, Iceland Tuesday, 14 June 2016 99-MST-5 Modeling and Simulation of Air Traffic Management I Fairchild West Chaired by: C. TAYLOR, The MITRE Corporation and B. APONSO, NASA-Ames Research Center 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2016-3113 AIAA-2016-3114 AIAA-2016-3115 AIAA-2016-3116 Design and Evaluation of Using Visualization to Formal Scenario Definition Aircraft Performance for Open Air User Interfaces for an Airport Understand Simulations of ATM Language for Aviation: Aircraft Traffic Simulations Management Simulation scenarios Landing Case Study I. Metz, German Aerospace Center S. Schier, T. Pett, O. Mohr, S. Yeo, A. Wallace, E. Mercer, Brigham Young S. Jafer, B. Chhaya, Embry-Riddle (DLR), Braunschweig, Germany; J. German Aerospace Center (DLR), University, Provo, UT; N. Rungta, Aeronautical University, Daytona Hoekstra, J. Ellerbroek, Delft University Braunschweig, Germany NASA Ames Research Center, Moffett Beach, FL; U. Durak, T. Gerlach, of Technology, Delft, The Netherlands; D. Field, CA German Aerospace Center (DLR), Kügler, German Aerospace Center (DLR), Braunschweig, Germany Braunschweig, Germany 75 Tuesday, 14 June 2016 100-MST-6 Modeling and Simulation of Vehicle Dynamics, Systems, and Environments Morgan Chaired by: D. GINGRAS, Bihrle Applied Research Inc. and N. MACCHIARELLA, Embry-Riddle Aeronautical University 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2016-3117 AIAA-2016-3118 AIAA-2016-3119 AIAA-2016-3120 AIAA-2016-3121 AIAA-2016-3122 A Model for Real-Time NISAR Spacecraft Conceptual Flight Dynamic Real-Time Planning in the Net- Design and Simulation of F/A- Lateral-Directional Simulation Detection of Aircraft Damage Environmental Torque Model for Bombardier Global Centric Warfare Environment 18A Automatic Carrier Landing of F/A-18 Aircraft Landing B. Blair, H. Lee, University of Modeling During Operations 5000 Aircraft Based on the Aircraft Guidance Controller on a Carrier in Complex California, Santa Cruz, Santa Cruz, F. Rizvi, Jet Propulsion Laboratory, M. Moallemi, S. Jafer, M. Susceptibility L. Yue, G. Liu, G. Hong, Beihang Environment CA; M. Davies, NASA Ames Research California Institute of Technology, Towhidnejad, Embry-Riddle S. Shi, B. Song, Y. Pei, R. Zhang, University, Beijing, China K. Wang, G. Liu, G. Hong, Beihang Center, Moffett Field, CA Pasadena, CA Aeronautical University, Daytona Northwestern Polytechnical University, University, Beijing, China Beach, FL Xi’an, China Tuesday, 14 June 2016 101-PDL-3 Aero-Optics Georgetown East Chaired by: M. RENNIE, University of Notre Dame and C. NOREN, Directed Energy Directorate, Air Force Research Laboratory 0930 hrs 1000 hrs 1030 hrs AIAA-2016-3123 AIAA-2016-3124 AIAA-2016-3125 A Robust Modification of a Multiple Aperture Approach LES/RANS Modeling of Aero- Predictive Adaptive-Optic for the Study of Large-Scale Optical Effects in a Supersonic Control Method for Aero-Optics Boundary-Layer Structures Cavity Flow W. Burns, E. Jumper, S. Gordeyev, M. Kemnetz, W. Burns, S. Gordeyev, I. Zilberter, J. Edwards, North Carolina University of Notre Dame, Notre University of Notre Dame, Notre State University, Raleigh, NC Dame, IN Dame, IN Tuesday, 14 June 2016 102-TP-3 Reentry Systems and Instrumentation Kalorama Chaired by: D. HASH, NASA - ARC 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2016-3126 AIAA-2016-3127 AIAA-2016-3128 AIAA-2016-3129 AIAA-2016-3130 Experimental and Flight Experiment Verification Assessment of Fencing on the Uncertainty Analysis of Mars 2020 Entry, Descent, Computational Fluid Dynamics of Shuttle Boundary Layer Orion Heatshield Thermal Protection System and Landing Instrumentation Studies of Superorbital Earth Transition Prediction Tool A. Alunni, T. Gokcen, Analytical Response of a Hypersonic (MEDLI2) Re-entry. S. Berry, K. Berger, T. Horvath, Mechanics Associates, Inc., Moffett Inflatable Aerodynamic H. Hwang, D. Bose, NASA Ames E. Fahy, University of Queensland, NASA Langley Research Center, Field, CA Decelerator Research Center, Moffett Field, CA; H. Brisbane, Australia; D. Buttsworth, Hampton, VA A. Brune, S. Hosder, Missouri Wright, NASA Langley Research Center, University of Southern Queensland, University of Science and Technology, Hampton, VA; T. White, Analytical Toowoomba, Australia; R. Gollan, Rolla, MO; K. Edquist, S. Tobin, Mechanics Associates, Inc., Moffett Field, P. Jacobs, R. Morgan, University of NASA Langley Research Center, CA; M. Schoenenberger, NASA Langley Queensland, Brisbane, Australia Hampton, VA Research Center, Hampton, VA; J. Santos, Jacobs, Moffett Field, CA; et al. Tuesday, 14 June 2016 103-RLA-2 Rising Leaders in Aerospace Panel Discussion: Why Work in Aerospace Instead of Silicon Valley? Georgetown East 1130 - 1230 hrs Come listen to what these panelists have to say. While Silicon Valley will always be a force in high tech innovation, learn what some are doing in partnership or in parallel. Learn how traditional aerospace is also making great advances in cutting edge research.

Moderator: Craig McGrath, Product Development, Boeing Commercial Airplanes

Panelist: Tony Springer Director – Integration & Management Ofﬁce, NASA 76 Tuesday, 14 June 2016 104-LNCH-1 Awards Luncheon: Celebrating the Achievements in Aerospace Sciences International Ballroom 1230 - 1400 hrs (Center) A ticket for the luncheon is required and included in the registration fee where indicated. Additional tickets for guests may be purchased upon registration or on site, as space is available.

The following awards will be presented: Aerodynamics Award Aerodynamic Measurement Technology Award Fluid Dynamics Award Ground Testing Award Losey Atmospheric Sciences Award Plasmadynamics and Lasers Award Thermophysics Award

Tuesday, 14 June 2016 105-AFM-7 Aircraft Flight Dynamics III Holmead West Chaired by: C. SUCHOMEL, USAF and N. HALL 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2016-3131 AIAA-2016-3132 AIAA-2016-3133 AIAA-2016-3134 AIAA-2016-3135 AIAA-2016-3136 Formation Flight for Fuel Influence of Piston Propeller- Influence of aircraft flexibility Effect of body configuration Steady-State Stall/Post-Stall Flying Qualities Evaluation of Saving in Coronet Mission - driven engine Model into the on Frequency Domain Handling and deformation on the Modeling for a Low-Wing an Unmanned Aircraft Using Part B: Full Mission Analysis Design of Cruise Autopilot Qualities Criteria dynamic stability of flapping General Aviation Aircraft JSBSim C. Kniffin, A. Dogan, University of P. Gonzalez, Technological Institute D. Drewiacki, F. Silvestre, A. flight G. Ananda , M. Selig, University J. Kim, D. Kunz, Air Force Institute of Texas, Arlington, Arlington, TX; W. of Aeronautics (ITA), São José Guimaraes Neto, Technological S. Zeyghami, A. Bode-Oke, H. Dong, of Illinois, Urbana-Champaign, Technology, Wright-Patterson AFB, OH Blake, Air Force Research Laboratory, dos Campos, Brazil; P. Boschetti, Institute of Aeronautics (ITA), São University of Virginia, Charlottesville, Urbana, IL Wright-Patterson AFB, OH Simón Bolívar University, Naiguata, José dos Campos, Brazil Charlottesville, VA Venezuela; F. Silvestre, Technological Institute of Aeronautics (ITA), São José dos Campos, Brazil Tuesday, 14 June 2016 106-AFM-8 Unmanned Aerial Systems II Holmead East Chaired by: A. DA RONCH, University of Southampton 1400 hrs 1430 hrs 1500 hrs 1530 hrs AIAA-2016-3137 AIAA-2016-3138 AIAA-2016-3139 AIAA-2016-3140 Experimental and Numerical Longitudinal and Directional Small Unmanned Aerial Vehicle Investigation On Dynamic Investigation of Entomopter Control Modeling for a Small Passive Range Estimation from Characteristic Of a Mini Angle Flapping Wings Aerodynamic Powered Parafoil Aerial Vehicle a Single Microphone Of Attack Sensor For Small UAV Performance V. Devalla, P. Om, University of J. King, I. Faruque, University of D. Wu, Z. Tan, Y. Zhong, S. Yang, A. Zyluk, K. Sibilski, Air Force Institute Petroleum and Energy Studies, Maryland, College Park, College Commercial Aircraft Corporation of of Technology, Warsaw, Poland; P. Dehradun, India Park, MD China, Ltd. (COMAC), Shanghai, Czekalowski, Institute of Aviation, China; L. Song, Beihang University, Warsaw, Poland Beijing, China Tuesday, 14 June 2016 107-AMT-5 Gas Thermometry Columbia 2 Chaired by: P. BARDET, George Washington University and A. SYDNEY, Naval Research Laboratory 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs AIAA-2016-3141 AIAA-2016-3142 AIAA-2016-3143 AIAA-2016-3144 AIAA-2016-3145 Simultaneous Minor-Species Tunable diode laser absorption 100-KHz-Rate Gas-Phase Spontaneous Raman Scattering Comparison of Chirped-Probe

Detection and Single-Shot spectroscopy of CO2 and H2O at Temperature Measurements Temperature Measurements in and Hybrid fs/ps Femtosecond Thermometry via Femtosecond, 2.7 µm in a scramjet combustor using Picosecond, Burst-Mode, High-Speed H2 Jet Flames CARS for Gas Phase Fully Resonant, Electronically and in exhaust gases of a Laser-Based CARS Spectroscopy H. Reising, T. Haller, N. Clemens, P. Thermometry Enhanced CARS (FREE-CARS) hybrid rocket motor P. Hsu, S. Roy, N. Jiang, M. Varghese, University of Texas, Austin, D. Richardson, H. Stauffer, S. Roy, H. Stauffer, D. Richardson, J. Schmidt, S. A. Mohamed, J. Messineo, J. Splichenko, Spectral Energies, LLC, Austin, TX Spectral Energies, LLC, Dayton, OH; J. Roy, Spectral Energies, LLC, Dayton, OH; Lestrade, S. Defoort, J. Soutade, P. Dayton, OH; J. Gord, Air Force Gord, Air Force Research Laboratory, P. Wrzesinski, J. Gord, Air Force Research Viguier, ONERA, Palaiseau, France Research Laboratory, Wright-Patterson Wright-Patterson AFB, OH 77 Laboratory, Wright-Patterson AFB, OH AFB, OH Tuesday, 14 June 2016 108-APA-16/FD-21 Flapping Flight Aerodynamics Oak Lawn Chaired by: K. MOORED, Lehigh University and A. JONES, University of Maryland 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs AIAA-2016-3146 AIAA-2016-3147 AIAA-2016-3148 AIAA-2016-3149 AIAA-2016-3150 AIAA-2016-3151 AIAA-2016-3152 Numerical simulation of a Computational Study of Three- Force Measurements of Low order modeling of forces Thrust generation in heaving CFD-Coupled Trim Analysis of a Varying Reynolds Number of flapping wing MAV based on wing Dimensional Rigid Flapping Flapping Membrane Wings and flow features in flapping and flapping wings in forward Millimeter-Scale Flapping Wing Biomimetic Flapping Wing By deformation capture analysis Wings with Unequal Pitch/ with Spanwise Chord Variation wings flight MAV in Steady Turning Flight Changing Air Density and Wing W. Tay, National University of Singapore, Plunge Frequency Operating at High Angles of M. Raiola, P. Moral, S. Discetti, G. Arranz, O. Flores, Universidad C. Badrya, A. Sridharan, J. Baeder, Length Singapore, Singapore; J. de Baar, N. Lee, M. Kim, S. Lee, Inha Attack A. Ianiro, Charles III University of Carlos III de Madrid, Leganes, Spain University of Maryland, College Park, D. Hope, A. Deluca, R. O’Hara, Air Australian National University, Canberra, University, Incheon, South Korea; M. Zakaria, D. Allen, C. Woolsey, M. Madrid, Leganes, Spain College Park, MD Force Institute of Technology, Wright- Australia; M. Percin, S. Deng, B. H. Cho, S. Shin, Seoul National Hajj, Virginia Polytechnic Institute and Patterson AFB, OH van Oudheusden, Delft University of University, Seoul, South Korea State University, Blacksburg, VA Technology, Delft, The Netherlands Tuesday, 14 June 2016 109-APA-17 Inlet/Intake Aerodynamics Columbia 9 Chaired by: N. HARIHARAN, CREATE-AV and D. O’BRIEN, US Army RDECOM 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2016-3153 AIAA-2016-3154 AIAA-2016-3155 AIAA-2016-3156 AIAA-2016-3157 AIAA-2016-3158 Influence of near-leading edge Convoluted Intake Distortion Pressure flow field and inlet flow Dynamic Flow Distortion Passive flow control study in a Numerical Investigation of curvature on the performance Measurements Using Stereo distortion metrics reconstruction Investigation in an S-duct using convoluted intake using Stereo Bleed Effects on Supersonic of aero-engine intake lips at Particle Image Velocimetry from velocity data DDES and SPIV data Particle Image Velocimetry Inlet under Various Bleed and high-incidence D. Gil-Prieto, P. Zachos, D. MacManus, M. Frascella, P. Zachos, D. Gil-Prieto, D. Gil-Prieto, P. Zachos, D. MacManus, G. Tanguy, P. Zachos, D. MacManus, Inlet Conditions A. Coschignano, H. Babinsky, G. Tanguy, Cranfield University, D. MacManus, Cranfield University, G. Tanguy, Cranfield University, D. Gil-Prieto, Cranfield University, Y. Choe, C. Kim, Seoul National University of Cambridge, Cambridge, Cranfield, United Kingdom Cranfield, United Kingdom Cranfield, United Kingdom Cranfield, United Kingdom; E. Garnier, University, Seoul, South Korea United Kingdom ONERA, Meudon, France Tuesday, 14 June 2016 110-APA-18 Historically Significant/Influential Papers in Applied Aerodynamics Jefferson West Chaired by: J. PINIER, NASA Langley Research Center and B. MCGRATH, JHU/Applied Physics Laboratory and R. WAHLS, NASA Aeronautics Research Mission Directorate 1400 hrs 1500 hrs AIAA-2016-3939 Oral Presentation Selected Scientific and Technical Contributions of Edward C. Polhamus On the Design of Subsonic Airfoils for High Lift J. Luckring, NASA Langley Research Center, Hampton, VA R. Liebeck, The Boeing Company, Huntington Beach, CA Tuesday, 14 June 2016 111-APA-19 Aerodynamic - Structural Modeling, Optimization, and Test Techniques for Flexible Wing Technology II Albright Chaired by: N. NGUYEN, NASA-Ames Research Center and A. VANDERWYST, Leidos 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs AIAA-2016-3159 AIAA-2016-3160 AIAA-2016-3161 AIAA-2016-3162 AIAA-2016-3163 Real-Time Adaptive Least- An Integral Boundary Layer Lift Optimization Study of a Roll Control Evaluation of the Static Aeroelastic Model Squares Drag Minimization Direct Method Applied to 2D Multi-Element Three-Segment X-56A Flying Wing Aircraft Using Assessment in the Transonic for Performance Adaptive Transonic Small-Disturbance Variable Camber Airfoil Active Camber Control compared Regime Aeroelastic Wing Equations U. Kaul, N. Nguyen, NASA Ames to Conventional Ailerons using M. Denison, Science and Technology Y. Ferrier, Stinger Ghaffarian G. Fujiwara, University of Research Center, Moffett Field, CA Vortex Lattice Theory Corporation, Mountain View, CA; E. Technologies, Inc., Moffett Field, CA; Washington, Seattle, Seattle, WA; E. Yerly, A. Deluca, Air Force Institute of Ting, Stinger Ghaffarian Technologies, N. Nguyen, NASA Ames Research D. Chaparro, MORI Associates, Inc., Technology, Wright-Patterson AFB, OH; Inc., Moffett Field, CA; J. Housman, Center, Moffett Field, CA; E. Ting, Moffett Field, CA; N. Nguyen, NASA J. Joo, Air Force Research Laboratory, N. Nguyen, NASA Ames Research Stinger Ghaffarian Technologies, Inc., Ames Research Center, Moffett Wright-Patterson AFB, OH Center, Moffett Field, CA Moffett Field, CA Field, CA Tuesday, 14 June 2016 112-APA-20 Applied CFD & Numerical Correlations with Experimental Data III Columbia 4 Chaired by: M. CONWAY, The Aerospace Corporation and K. KONTIS, University of Glasgow 78 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs AIAA-2016-3164 AIAA-2016-3165 AIAA-2016-3166 AIAA-2016-3167 AIAA-2016-3168 AIAA-2016-3169 AIAA-2016-3170 Transition Transport Modeling Evaluation of Six Turbulence Comparison of Uncoupled and A numerical Method for Numerical Simulation of Hypersonic Experimental Numerical Prediction of for the Prediction of Crossflow Models for Accurate Numerical Coupled CFD-based Simulation Transonic Wind Tunnel Wall Supersonic Jets in Transonic Aero-thermal Capability Study Longitudinal Dynamic Stability Transition Simulation of 2D Slot Nozzle Techniques for the Prediction of Interference Correction in and Supersonic Crossflows through Multilevel Fidelity for a Lifting Body in Transonic C. Grabe, N. Shengyang, A. Ejector the Aerodynamic Behavior of a Airfoil Testing Using Kestrel Computational Fluid Dynamics Flow Krumbein, German Aerospace Center I. Witte, Washington University in Complex Projectile B. Ma, G. Wang, Z. Ye, Northwestern L. Johnsen, Air Force Institute of D. Sagerman, University of Dayton, B. Reimann, German Aerospace (DLR), Braunschweig, Germany St. Louis, St. Louis, MO; C. Graham, S. Silton, J. Sahu, F. Fresconi, Army Polytechnical University, Xi’an, China; Technology, Wright-Patterson AFB, Dayton, OH; J. Tancred, Air Force Center (DLR), Braunschweig, The Boeing Company, St. Louis, MO; Research Laboratory, Aberdeen L. Xu, University of New South OH; C. Martin, Air Force Research Research Laboratory, Wright-Patterson Germany R. Agarwal, T. Wray, Washington Proving Ground, MD Wales, Canberra, Australia Laboratory, Eglin AFB, FL; M. Reeder, AFB, OH; M. Rumpfkeil, University of University in St. Louis, St. Louis, MO D. Crowe, Air Force Institute of Dayton, Dayton, OH; B. Hellman, Air Technology, Wright-Patterson AFB, OH Force Research Laboratory, Wright- Patterson AFB, OH Tuesday, 14 June 2016 113-ASE-7/ATIO.ATM-9 Characterization of the Atmospheric Environment using UAS (Invited) Georgetown East Chaired by: D. THOMPSON, Mississippi State University and V. SCHULTZ, NASA Langley Research Center 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs Oral Presentation AIAA-2016-3171 AIAA-2016-3172 Oral Presentation AIAA-2016-3173 AIAA-2016-3174 Oral Presentation CLOUD-MAP: Advancing Toward an Autonomous Integration of Infrasonic The Application of Unmanned Boundary Layer Measurements Fundamental Turbulence NOAA Atmospheric, Marine and Meteorology and Atmospheric Airborne Scientist for Studying Sensing with UAS (Invited) Aircraft Systems towards Over Land Use/Cover Measurement with Unmanned Polar Monitoring Using UASs Physics Through Unmanned Severe Local Storms (Invited) B. Elbing, R. Gaeta, Oklahoma State Supercell Research and Discontinuities Using a Small Aerial Vehicles (Invited) (including Rapid Response) Aerial Systems (Invited) E. Frew, B. Argrow, University of University, Stillwater, OK Forecasting (Invited) UAS (Invited) B. Witte, J. Mullen, M. Thamann, J. Coffey, Cherokee Nation Technologies, P. Chilson, University of Oklahoma, Colorado, Boulder, Boulder, CO A. Houston, University of Nebraska, J. Dyer, L. Wasson, R. Moorhead, S. Bailey, University of Kentucky, Washington, D.C.; R. Hood, T. Jacobs, G. Norman, Norman, OK; J. Jacob, Lincoln, Lincoln, NE Mississippi State University, Lexington, Lexington, KY Wick, National Oceanic and Atmospheric Oklahoma State University, Stillwater, Mississippi State, MS Administration, Silver Spring, MD; R. OK; S. Smith, University of Kentucky, Moorhead, Mississippi State University, Lexington, Lexington, KY; A. Houston, Starkville, MS; J. Walker, Cherokee University of Nebraska, Lincoln, Nation Technologies, Washington, D.C. Lincoln, NE Tuesday, 14 June 2016 114-ASE-8 Ice Roughness Characterization and Heat Transfer Georgetown West Chaired by: D. RIGBY, Vantage Partners Limited and S. OTTA, GE Global Research Center 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs AIAA-2016-3175 AIAA-2016-3176 AIAA-2016-3177 AIAA-2016-3178 AIAA-2016-3179 AIAA-2016-3180 AIAA-2016-3181 Convection from Hemispherical Heat Transfer Evaluation on Convection from a Simulated Surface Roughness and Manual Point Cloud Ice Roughness and its Impact Characterization of Ice and Conical Model Ice Ice Roughened Cylinders in NACA 0012 with Icing Heat Transfer Prediction for Registration for Combined Ice on the Ice Accretion Process Roughness Variations in Scaled Roughness Elements in Transition Regime Roughness of Different Shape Development of an Improved Roughness and Ice Thickness J. Steiner, German Aerospace Center Glaze Icing Conditions Stagnation Region Flows Y. Han, J. Palacios, Pennsylvania and Thermal Conductivity Aircraft Ice Accretion Modeling Measurements (DLR), Braunschweig, Germany; S. McClain, Baylor University, Waco, M. Hughes, S. McClain, T. Shannon, State University, University Park, PA T. Shannon, S. McClain, Baylor Tool S. McClain, Baylor University, S. Bansmer, Technical University TX; M. Vargas, NASA Glenn Research Baylor University, Waco, TX; M. University, Waco, TX Y. Han, J. Palacios, Pennsylvania Waco, TX of Braunschweig, Braunschweig, Center, Cleveland, OH; J. Tsao, Ohio Vargas, A. Broeren, NASA Glenn State University, University Park, PA Germany Aerospace Institute, Cleveland, OH Research Center, Cleveland, OH Tuesday, 14 June 2016 115-ATIO.ACD-4 Conceptual Aircraft Design Working Group Gunston East 1400 - 1700 hrs CADWG - The Conceptual Aircraft Design Working Group will host a panel discussion focusing on unmanned aircraft design.

Panelists: Michael Logan M. Christopher Cotting Darold Cummings Clif Davies Jay Gundlach Robert Love NASA Langley Research Center USAF/TPS Consultant Lockheed Martin Corporation UAV Design Book Author & Entrepreneur General Atomics

Tuesday, 14 June 2016 116-ATIO.ATM-10 UAS Risk and Perception Embassy Chaired by: B. SRIDHAR, NASA Ames Research Center

79 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs AIAA-2016-3182 AIAA-2016-3183 AIAA-2016-3184 AIAA-2016-3185 AIAA-2016-3186 Identifying and Mitigating Capturing Safety Requirements Assessing System Safety for an Multivariate Probit Models and Strategies to Model System Human Factors Errors in to Enable Effective Task Urban, Tethered UAS Qualitative Analysis of Survey Risk Using UAS Safety Analysis Unmanned Aircraft Systems Allocation between Humans L. Hale, C. Denham, Virginia on Public and Stakeholder Model (USAM) P. Neff, K. Garman, Federal Aviation and Automaton in Increasingly Polytechnic Institute and State Perception of Unmanned A. Tyagi, Y. Zhang, Intelligent Administration, Lakewood, CA Autonomous Systems University, Blacksburg, VA; J. Luxhoj, Aircraft Automation, Inc., Rockville, MD; N. Neogi, NASA Langley Research Rutgers University, Piscataway, NJ; L. Reddy, D. DeLaurentis, Purdue S. Toussaint, Coherent Technical Center, Hampton, VA C. Mancini, Northrop Grumman University, West Lafayette, IN Services, Inc., Lexington Park, MD; J. Corporation, Brooklyn, NY; C. Luxhoj, LCR, LLC, Somerset, NJ Woolsey, R. Mooney, Virginia Polytechnic Institute and State University, Blacksburg, VA Tuesday, 14 June 2016 117-ATIO.ATM-11 Weather Impacts Fairchild East Chaired by: A. EVANS, University of California Santa Cruz 1400 hrs 1430 hrs 1500 hrs 1530 hrs AIAA-2016-3187 AIAA-2016-3188 AIAA-2016-3189 AIAA-2016-3190 Algorithms for Collision Using Ensemble Weather Improving Operational Risk-Hedged Approach for Detection Between a Point Forecasts for Predicting Airport Acceptability of Dynamic Weather Re-routing Air Trafﬁc Under and a Moving Polygon, with Runway Conﬁguration and Routes Through Analysis of Weather Uncertainty Applications to Aircraft Weather Capacity Commonly Use Routings A. Sadovsky, K. Bilimoria, NASA Ames Avoidance S. Tien, C. Taylor, C. Wanke, MITRE A. Evans, University of California, Santa Research Center, Moffett Field, CA A. Narkawicz, G. Hagen, NASA Corporation, McLean, VA Cruz, Moffett Field, CA; B. Sridhar, D. Langley Research Center, McNally, NASA Ames Research Center, Hampton, VA Moffett Field, CA Tuesday, 14 June 2016 118-ATIO.TFPC-5 Transformational Flight - On-Demand Mobility (ODM) Enabling Technologies Session Columbia 1 Chaired by: M. PATTERSON and M. MOORE, NASA Langley Research Center 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs Oral Presentation Oral Presentation AIAA-2016-3191 Oral Presentation AIAA-2016-3192 Oral Presentation FAA-NASA On-Demand Mobility Electric Propulsion Market Transformational Autonomy Robotic Legged Landing Gear Tactile Active Gear (TAG) For Wind Tunnel Validation of and Emerging Aviation Pathway Emergence as a and Personal Transportation: for Rotorcraft V/ESTOL Electrically Powered High-Lift Propellers Technology Roadmap Disruptive Technology Synergies and Differences M. Ward, M. Costello, Georgia Aircraft X. Fei, B. German, Georgia Institute K. Goodrich, NASA Langley Research M. Moore, N. Borer, NASA Langley between Cars and Planes Institute of Technology, Atlanta, GA B. Seeley, Sustainable Aviation of Technology, Atlanta, GA Center, Hampton, VA; W. Ryan, Research Center, Hampton, VA K. Goodrich, NASA Langley Research Foundation, Inc., Santa Rosa, CA Federal Aviation Administration, Center, Hampton, VA; J. Nickolaou, Kansas City, MO General Motors, Warren, MI; M. Moore, NASA Langley Research Center, Hampton, VA Tuesday, 14 June 2016 119-ATIO.TFPC-6/ATIO. Transformational Flight - Unconventional V/STOL Concepts Columbia 12 VSTOL-1 Chaired by: W. FREDERICKS, NASA-Langley Research Center and G. GATLIN, NASA Langley Research Center 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs Oral Presentation Oral Presentation AIAA-2016-3193 Oral Presentation Oral Presentation AIAA-2016-3194 Sikorsky X2 Technology, S-97 Joby S4 Electric VTOL Concept Tri-Fan VTOL Conceptual Design Hexplane Technology: Three The $2 Million Dollar GoFly Prize FlyKart - Mini Personal Air RAIDER and Future Applications A. Stoll, J. Bevirt, G. Veble Mikic, D. Olcott, Answer Engineering, LLP, Wing, Six Tilt-Propulsion Units, G. Lighter, Go Fly Prize, Greenwich, CT Vehicle M. Alber, Sikorsky Aircraft Joby Aviation, Santa Cruz, CA Parker, CO VTOL Aircraft R. Bulaga, Trek Aerospace, Inc., Corporation, Stratford, CT R. Oliver, J. Rutherford, Oliver VTOL, Folsom, CA; J. Portlock, Electro.Aero Bluffton, SC; W. Anemaat, Design, Pty Ltd, Perth, Australia Analysis and Research Corporation, 80 Lawrence, KS Tuesday, 14 June 2016 120-F360-5 The Future of Military Aviation International Ballroom 1400 - 1600 hrs (East) Moderator: Tom Bell, Vice President, Global Sales & Marketing, Boeing Defense, Space & Security

Panelists: Shawn Brimley Rear Admiral Donald Gaddis Michael O’Hanlon Executive Vice President and Director of Studies U.S. Navy (Ret.) Senior Fellow, Foreign Policy Center for New American Security Brookings Institution

Tuesday, 14 June 2016 121-FC-5 Modal Decomposition Methods for Aerodynamic Flows (Invited) Jefferson East Chaired by: K. TAIRA, Florida State University and D. SMITH, Office of Naval Research 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs Oral Presentation Oral Presentation Oral Presentation Oral Presentation Oral Presentation Oral Presentation Oral Presentation An Overview of Modal Applications of the Proper Balanced POD and the Decomposing Fluid Flows Global linear stability analysis Resolvent Analysis Compressed sensing and Decomposition Methods for Orthogonal Decomposition Eigensystem Realization According to their Dynamics: past the solution of multi- M. Luhar, University of Southern coherent structures in fluids Aerodynamic Flows L. Ukeiley, University of Florida, Algorithm A~Tutorial on Dynamic Mode dimensional EVP and SVD California, Los Angeles, CA; B. S. Brunton, University of Washington, T. Colonius, California Institute of Gainesville, Gainesville, FL D. Luchtenburg, Cooper Union, Decomposition of Fluids Data problems McKeon, California Institute of Seattle, Seattle, WA Technology, Pasadena, CA New York, NY; C. Rowley, Princeton M. Hemati, University of Minnesota, J. Perez, V. Theofilis, Technical Technology, Pasadena, CA University, Princeton, NJ Twin Cities, Minneapolis, MN; M. University of Madrid, Madrid, Spain Williams, United Technologies Corporation, East Hartford, CT Tuesday, 14 June 2016 122-FC-6/FD-22 Separation Detection and Control Columbia 11 Chaired by: D. GARMANN, Air Force Research Laboratory 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs AIAA-2016-3195 AIAA-2016-3196 AIAA-2016-3197 AIAA-2016-3198 AIAA-2016-3199 Induced Stall Cells on a Separation Control Using Low-Cost Detection of Control of Airfoil Flow at Cruise Separation Control on a NACA0015 Airfoil using Passive Plasma Actuator on an Elliptic Boundary Layer Separation Condition by DBD Plasma NACA 0015 Airfoil with and Active Trips Airfoil at Low Reynolds with Dynamic Pressure Actuator - Sophisticated Airfoil vs. Plasma-Actuator-Generated H. Dell’Orso, W. Chan, M. Amitay, Numbers Measurements Simple Airfoil with Flow Control - Disturbance Rensselaer Polytechnic Institute, X. Yan, X. Meng, Northwestern L. Edelman, A. Pensado, S. Robinson, K. Asano, University of Tokyo, Z. Lu, C. Wong, L. Wang, M. Alam, Y. Troy, NY Polytechnical University, Xi’an, China; C. Van Dam, University of California, Sagamihara, Japan; M. Sato, T. Zhou, Harbin Institute of Technology, S. Luo, F. Liu, University of California, Davis, Davis, CA Nonomura, A. Oyama, Japan Aerospace Shenzhen, China Irvine, Irvine, CA Exploration Agency (JAXA), Sagamihara, Japan; K. Fujii, Tokyo University of Science, Shinjuku, Japan Tuesday, 14 June 2016 123-FD-23 Aeroacoustics and Noise Lincoln East Chaired by: R. WLEZIEN, Iowa State University and F. SARTOR, ONERA 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2016-3200 AIAA-2016-3201 AIAA-2016-3202 AIAA-2016-3203 AIAA-2016-3204 AIAA-2016-3205 Direct numerical investigation Modification of Flow Structures The Influence of Velocity Field Experiments on Slat Noise from Direct numerical simulations of Effect of Geometry Variations of sound-orifice interaction Associated with Broadband Estimation on the Prediction of -6° to 18° Angles of Attack tonal noise generation for a two on Tandem Airfoil Interaction grazed by a Mach 0.5 turbulent Trailing Edge Noise Far-Field Acoustics F. Amaral, M. Medeiros, C. Pagani, dimensional airfoil at low and Noise boundary layer H. Clemons, R. Wlezien, Iowa State A. Nickels, L. Ukeiley, University of University of São Paulo, São Carlos, moderate Reynolds numbers C. Zhang, Shanghai Jiao Tong Q. Zhang, D. Bodony, University of University, Ames, IA Florida, Gainesville, Gainesville, FL; Brazil Y. Zhang, X. Wu, W. Li, Shanghai Jiao University, Shanghai, China Illinois, Urbana-Champaign, Urbana, IL R. Reger, L. Cattafesta, Florida State Tong University, Shanghai, China 81 University, Tallahassee, FL Tuesday, 14 June 2016 124-FD-24 Fluid-Structure Interaction Monroe Chaired by: J. JAWORSKI, Lehigh University and X. LIU, San Diego State University 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2016-3206 AIAA-2016-3207 AIAA-2016-3208 AIAA-2016-3209 AIAA-2016-3210 AIAA-2016-3211 Flow Field Analysis of Fully The Response of a Single Aeroelastic Response of an On the Effective Length of Non-linear Fluid-Structure Modeling Unsteady Lift on a Coupled Computations of a Degree-of-Freedom Wing at Airfoil at Transitional Reynolds Fluttering Finite-Length Pipes Interaction using a Partitioned Hydrofoil due to the Ingestion Flexible Wing undergoing Stall Low Reynolds Number Numbers K. Lupo, J. Sargeant, J. Jaworski, Lattice Boltzmann - FEA approach. of Turbulence and Hydro-elastic Flutter F. Manar, M. Cassell, A. Jones, C. Barnes, M. Visbal, Air Force Lehigh University, Bethlehem, PA G. Trapani, R. Brionnaud, D. Holman, Motion C. Fagley, J. Seidel, T. McLaughlin, U.S. University of Maryland, College Park, Research Laboratory, Wright-Patterson Next Limit Technologies, Madrid, Spain M. Catlett, J. Anderson, Naval Surface Air Force Academy, Colorado Springs, CO College Park, MD AFB, OH Warfare Center, West Bethesda, MD Tuesday, 14 June 2016 125-FD-25 Turbulence Modeling III: LES, DNS, Hybrid LES/RANS Jay Chaired by: J. EDWARDS and M. VYAS, NASA Glenn Research Center 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs AIAA-2016-3212 AIAA-2016-3213 AIAA-2016-3214 AIAA-2016-3215 AIAA-2016-3216 AIAA-2016-3217 AIAA-2016-3218 Development of a new LES/ Turbulent Inflow Generation Reduced Order Modeling Application of the Wray- Numerical Investigation of Development of a One- High Temperature Effects on RANS formulation for Direct Simulations of of Turbulent Flows Using Agarwal Model to Compressible Pressure Gradient Effects Equation Turbulence Model DNS of Shock/Turbulence J. Edwards, North Carolina State Hypersonic Turbulent Boundary Statistical Coarse-graining Flows on Coherent Structures and based on Epsilon-Equation Interaction University, Raleigh, NC Layers and their Freestream E. Parish, K. Duraisamy, University of T. Wray, R. Agarwal, Washington Turbulence Anisotropy M. Rahman, Aalto University, J. Samuel, S. Ghosh, Indian Institute Acoustic Radiation Michigan, Ann Arbor, Ann Arbor, MI University in St. Louis, St. Louis, MO L. Schiavo, W. Wolf, University of Helsinki, Finland; R. Agarwal, of Technology Madras, Chennai, India J. Huang, L. Duan, Missouri University Campinas, Campinas, Brazil; J. Azevedo, Washington University in St. Louis, of Science and Technology, Rolla, MO Aeronautics and Space Institute (IAE), St. Louis, MO; T. Siikonen, Aalto São José dos Campos, Brazil University, Helsinki, Finland Tuesday, 14 June 2016 126-FD-26 Shock-Boundary Layer Interaction II Columbia 10 Chaired by: J. SIVASUBRAMANIAN, The University of Arizona and A. GROSS, New Mexico State University 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2016-3219 AIAA-2016-3220 AIAA-2016-3221 AIAA-2016-3222 AIAA-2016-3223 AIAA-2016-3224 Experimental Investigation of Numerical Investigation of Interaction of an oblique shock Experiments on Unsteadiness Flowfield of a 3-D Swept Shock Numerical Exploration of Corner Shock Boundary Layer Oblique-Shock/Boundary-Layer with a transitional Mach 5.92 Associated with Cylinder- Boundary Layer Interaction in Supersonic Flow Over a Wall- Interactions Interactions in Supersonic Flows boundary layer induced Shock-Laminar a Mach 2 Flow Mounted Hemisphere M. Funderburk, V. Narayanaswamy, J. Sivasubramanian, H. Fasel, University P. Shrestha, N. Hildebrand, A. Boundary Layer Interaction in N. Arora, M. Ali, F. Alvi, Florida State P. Morgan, Ohio Aerospace Institute, North Carolina State University, of Arizona, Tucson, Tucson, AZ Dwivedi, J. Nichols, M. Jovanovic, Hypersonic Flow University, Tallahassee, FL Wright-Patterson AFB, OH; S. Raleigh, NC G. Candler, University of Minnesota, H. Itoh, M. Mizoguchi, National Sherer, M. Visbal, Air Force Research Twin Cities, Minneapolis, MN Defense Academy, Yokosuka, Japan Laboratory, Wright-Patterson AFB, OH Tuesday, 14 June 2016 127-FT-2 Flight Testing of Unmanned Aerial Systems Gunston West Chaired by: D. OWENS, NASA-Langley Research Center and W. SCHUMAN 1400 hrs 1430 hrs 1500 hrs AIAA-2016-3225 AIAA-2016-3226 AIAA-2016-3227 Application of an ADS-B Sense Integration and Evaluation of Aircraft Instrumentation and and Avoid Algorithm COTS Pressure Sensors for Flush Computer Vision-Aided Flight R. Arteaga, M. Cavalin, M. Air Data Sensing on Small-Scale Analysis of Local Air Flow Dandachy, NASA Armstrong Flight UAVs J. Strader, S. Harper, Y. Gu, West Research Center, Edwards, CA; R. A. Alkurdi, King Abdulaziz City for Science Virginia University, Morgantown, WV Kotcher, Carnegie Mellon University, and Technology, Riyadh, Saudi Arabia; R. Pittsburgh, PA Bunge, Stanford University, Stanford, CA; E. Alfaris, King Abdulaziz City for Science and Technology, Riyadh, Saudi Arabia 82 Tuesday, 14 June 2016 128-GT-3 Development and Performance of Ground Test Facilities Lincoln West Chaired by: J. MICOL, NASA and S. HELLAND, NASA 1400 hrs 1430 hrs 1500 hrs 1530 hrs AIAA-2016-3228 AIAA-2016-3229 AIAA-2016-3230 AIAA-2016-3231 Pressure Tap Effects on the Wind Tunnel Support System The Overall Scheme Design Mechanical Simulation and Lift Measurement of an Airfoil Influence on NASA Common and Debugging of the Liquid Experiment of Electric Impulse Section Research Model at Low Speed Nitrogen Injection Cooling De-icing System M. Kuester, A. Borgoltz, W. Conditions System in NF-6 Wind Tunnel Y. Wang, C. Zhu, Nanjing University of Devenport, Virginia Polytechnic A. Waldmann, T. Lutz, E. Kraemer, C. Gao, T. Zhou, Z. Zhang, Aeronautics and Astronautics, Nanjing, Institute and State University, University of Stuttgart, Stuttgart, Northwestern Polytechnical University, China; B. Fu, Science and Technology Blacksburg, VA Germany Xi’an, China on Space Physics Laboratory, Beijing, China; K. Li, Z. Wang, Nanjing University of Aeronautics and Astronautics, Nanjing, China Tuesday, 14 June 2016 129-ITAR-2 High-Speed Flows Cabinet Chaired by: K. CASPER, Sandia National Laboratories and D. LEWIS, Aerospace Testing Alliance (ATA) 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs Oral Presentation Oral Presentation AIAA-2016-3233 AIAA-2016-3234 AIAA-2016-3235 AIAA-2016-3236 Effect of bluntness and angle Amplitude Method for Estimating Numerically Assessing Optimization of a Mach 6 Quiet Investigations of Supersonic Wind Tunnel Demonstration of attack on circular cone the Boundary Layer Transition Boundary Layer Stabilization Wind Tunnel Nozzle Flow over a Hemispherical of a Gust Rejecting Wing transition at Mach 10 Onset on Inclined Blunt Circular due to Axisymmetric M. Lakebrink, The Boeing Company, Turret Using Numerical Using Distributed Bio-Inspired I. Leyva, Air Force Research Cones at Mach 10 Roughness Strips in Hypersonic Saint Louis, MO; K. Bowcutt, The Simulations Pressure Sensing Laboratory, Edwards AFB, CA; E. E. Marineau, Arnold Engineering Flow Boeing Company, Huntington Beach, C. Tam, T. Madden, D. Wittich, C. R. Griffin, M. Lieu, A. Dropkin, Marineau, C. Moraru, M. Marana, Development Center, Silver Spring, B. Grier, Z. Riley, J. McNamara, Ohio CA; T. Winfree, The Boeing Company, Noren, Air Force Research Laboratory, Aurora Flight Sciences, Cambridge, Arnold Engineering Development MD; I. Leyva, Air Force Research State University, Columbus, OH Tukwila, WA; T. Juliano, University of Kirtland AFB, NM; D. Carnrike, R. MA; M. Sytsma, Air Force Research Complex, Silver Spring, MD; A. Laboratory, Edwards AFB, CA; C. Notre Dame, Notre Dame, IN Kumar, Florida State University, Laboratory, Eglin AFB, FL Lingfu, University of Maryland, Moraru, M. Marana, Arnold Engineering Tallahassee, FL; et al. College Park, College Park, MD Development Center, Silver Spring, MD; A. Lingfu, University of Maryland, College Park, College Park, MD Tuesday, 14 June 2016 130-MAO-7 Design Optimization of Aircrafts and Other Complex Systems IV Cardozo Chaired by: S. CHOI, Virginia Polytechnic Institute and State University and P. LYU, COMSOL Inc. 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs AIAA-2016-3237 AIAA-2016-3238 AIAA-2016-3239 AIAA-2016-3240 AIAA-2016-3241 A Risk-Aversion-Based Project A Methodology to Evaluate Optimal Spacecraft Hardware Assessment of airframe- Adjoint Approach based on Valuation Method to Determine Tradeoffs between Individual Placement to Minimize subsystems synergy on overall Reduced-order Model for Optimal Technology Infusion Architecture Development and Required Power Input for aircraft performance in a Steady PDE Systems and Architecture in Aircraft Numerality to Achieve Group Hibernation Survival Collaborative Design J. Li, K. Qu, J. Cai, C. Cao, 83 Design Performance in Robotics Swarms R. Pitre, I. Kim, Queen’s University, P. Prakasha, P. Ciampa, German Northwestern Polytechnical University, F. Burgaud, J. Durand, D. Mavris, J. Durand, F. Burgaud, K. Cooksey, D. Kingston, Canada Aerospace Center (DLR), Hamburg, Xi’an, China Georgia Institute of Technology, Mavris, Georgia Institute of Technology, Germany; L. Boggero, M. Fioriti, Atlanta, GA Atlanta, GA Technical University of Turin, Turin, Italy Tuesday, 14 June 2016 131-MAO-8 Shape and Topology Optimization IV Columbia 3 Chaired by: M. STELMACK, Lockheed Martin Aeronautics and B. STANFORD, NASA Langley Research Center 1400 hrs 1430 hrs 1500 hrs 1530 hrs AIAA-2016-3242 AIAA-2016-3243 AIAA-2016-3244 AIAA-2016-3245 Topology Optimization Wing airfoil geometric A Hybrid Aerodynamic Multilevel Collaborative Formulations for Circuit Board parametrization method for Optimization Algorithm Based Aerodynamic Design Heat Spreader Design efficient aerodynamic design on Differential Evolution and Optimization Based on Sobol’ D. Lohan, University of Illinois, Urbana- optimization RBF Response Surface Global Sensitivity Analysis Champaign, Urbana, IL; E. Dede, Toyota R. de Souza, A. Cuco, T. Orra, K. Deng, H. Chen, Tsinghua C. Wang, Z. Gao, Northwestern Motor Corporation, Ann Arbor, MI; J. Embraer, São José dos Campos, University, Beijing, China Polytechnical University, Xi’an, China Allison, University of Illinois, Urbana- Brazil Champaign, Urbana, IL Tuesday, 14 June 2016 132-MST-7 UAV Path Planning and Collision Avoidance Morgan Chaired by: P. ZAAL, NASA Ames Research Center and F. CARDULLO, State University of NY 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2016-3246 AIAA-2016-3247 AIAA-2016-3248 AIAA-2016-3249 AIAA-2016-3250 AIAA-2016-3251 Multi-Rotor Aircraft Collision Simulation Comparison of UAV Path-Planning using Bio-Inspired Opportunistic Multi-UAVs Target Assignment Swarming Coordination of Avoidance using Partially Collision Avoidance Algorithms Bezier Curves and a Receding Approaches in Energy- Using Opposition-based Multiple Unmanned Aerial Observable Markov Decision for Small Multi-Rotor Aircraft Horizon Approach Conserving/Harnessing Flight- Genetic Algorithm with Multiple Vehicles in Three-Dimensional Processes E. Mueller, NASA Ames Research B. Ingersoll, J. Ingersoll, P. DeFranco, Path Modeling for UAS Mutation Operators Space E. Mueller, NASA Ames Research Center, Center, Moffett Field, CA; M. A. Ning, Brigham Young University, S. Gudmundsson, V. Golubev, S. Y. Wen, L. Liu, Z. Wang, J. Kou, T. Y. Jia, China Aerospace Science Moffett Field, CA; M. Kochenderfer, Kochenderfer, Stanford University, Provo, UT Drakunov, C. Reinholtz, Embry-Riddle Long, Beijing Institute of Technology, and Industry Corporation (CASIC), Stanford University, Stanford, CA Stanford, CA Aeronautical University, Daytona Beijing, China Beijing, China Beach, FL Tuesday, 14 June 2016 133-MST-8 Modeling and Simulation of Air Traffic Management II Fairchild West Chaired by: B. APONSO, NASA-Ames Research Center and D. CARTMELL, Boeing Engineering Operations & Technology 1400 hrs 1430 hrs 1500 hrs 1530 hrs AIAA-2016-3252 AIAA-2016-3253 AIAA-2016-3254 AIAA-2016-3255 A Method to Extract Aircraft Exploring the Air-Ground Modeling Functional Specifications Flight planning in case of Information from Noisy VFR Workload Tradespace of Ground Systems in the NAS volcanic eruption Flight Track Data K. Nelson, H. Lee, University of C. Krantz, Royal Institute of Technology A. Schmitt, A. Kuenz, German S. Ayyalasomayajula, Y. Zhang, California, Santa Cruz, Santa Cruz, (KTH), Stockholm, Sweden; N. Rungta, Aerospace Center (DLR), N. Nigam, F. Wieland, Intelligent CA; M. Davies, NASA Ames Research NASA Ames Research Center, Moffett Braunschweig, Germany Automation, Inc., Rockville, MD Center, Moffett Field, CA Field, CA; E. Mercer, Brigham Young University, Provo, UT

84 Tuesday, 14 June 2016 134-NIA-1 National Institute of Aerospace Graduate Student Researchers Piscataway Chaired by: C. BRITCHER, Old Dominon University 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs Oral Presentation Oral Presentation Oral Presentation Oral Presentation Oral Presentation Oral Presentation Oral Presentation Titan Aerial Explorer Impact of Turboprop Propulsion Optimization of a Quiet Performance and Noise Modeling and Control of Linked Adaptive Robust Noise Control Development of a Method E. Petro, University of Maeryland, on Fuel Efficiency and Propeller for the Gl-10 All- Study of Propellers for Small Aircraft Systems in an Active Headrest for Analysis & Incorporation College Park, MD Economic Feasibility Electric Aircraft Distributed Electric Propulsion J. Cooper, University of Connecticut, J. Bean, Virginia Polytechnic Institute of Rotor-craft Fluctuation in K. Antcliff, NASA Langley Research X. Fei, Georgia Institute of Applications Mansfield, CT and State University, Blacksburg, VA Synthesized Flyover Noise Center, Hampton, VA Technology, Atlanta, GA B. Duvall, Old Dominion University, N. Pera, Virginia Polytechnic Institute Norfolk, VA and State University, Blacksburg, VA Tuesday, 14 June 2016 135-TP-5 Radiation Kalorama Chaired by: B. CRUDEN, ERC Inc at NASA Ames Research Center and D. ANDRIENKO, University of Michigan 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2016-3256 AIAA-2016-3257 AIAA-2016-3258 AIAA-2016-3259 AIAA-2016-3260 AIAA-2016-3261 Non-equilibrium Radiation for Echelle Spectroscopy for High Characterization of High- Refinements to Afterbody A Tunable Laser Absorption Reduced Order Modeling of Earth Entry Enthalpy Flow Diagnostics Enthalpy and non-Equilibrium Radiative Heating Simulations for Diagnostic for Measurements Non-equilibrium Radiation A. Brandis, Analytical Mechanics S. Loehle, T. Hermann, F. Zander, Flows using Laser Absorption Earth Entry of CO in Shock-Heated Gases for CO2. Associates, Inc., Moffett Field, CA; University of Stuttgart, Stuttgart, Spectroscopy C. Johnston, NASA Langley Research M. MacDonald, Jacobs, Moffett Field, A. Sahai, M. Panesi, University C. Johnston, NASA Langley Research Germany; T. Marynowski, Airbus, T. Mayer, B. Massuti-Ballester, G. Center, Hampton, VA; A. Brandis, NASA CA; B. Cruden, Analytical Mechanics of Illinois, Urbana-Champaign, Center, Hampton, VA; B. Cruden, Oberkochen, Germany Herdrich, S. Fasoulas, University of Ames Research Center, Moffett Field, CA; Associates, Inc., Moffett Field, CA Urbana, IL Analytical Mechanics Associates, Inc., Stuttgart, Stuttgart, Germany M. Panesi, University of Illinois, Urbana- Moffett Field, CA Champaign, Urbana, IL Tuesday, 14 June 2016 136-TP-6 Special Session: Spacecraft Thermal Management DuPont Chaired by: S. SMITH and W. TSAI, California State University, Maritime Academy 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs AIAA-2016-3262 AIAA-2016-3263 AIAA-2016-3264 AIAA-2016-3265 AIAA-2016-3266 AIAA-2016-3267 AIAA-2016-3268 Thermal Enhancements for An Advanced Card Lock Reduced-Order Modeling for Single-Sided Guarded Hot Enabling Future Spacecraft Development of the Two Phase Thermal Control of a Gravitational Separable Thermal Mechanical for Space and Terrestrial Rapid Thermal Analysis and Plate Method for Comparative Missions through Isothermal Flow Separator Experiment Reference Sensor Interfaces Applications Evaluation of Spacecraft Testing of Thermal Radiation Bus Thermal Management E. Golliher, D. Gotti, K. Gilkey, J. A. Alfauwaz, Stanford University, M. Flannery, J. Schmidt, J. Weyant, N. Kattamis, J. Rozzi, Creare, Inc., D. Hengeveld, LoadPath, Barriers in Vacuum D. Hengeveld, LoadPath, Owens, N. Pham, P. Stehno, NASA Stanford, CA; F. Alamri, King Abdulaziz Advanced Cooling Technologies, Inc., Hanover, NH Albuquerque, NM K. Irick, Applied Technology Albuquerque, NM Glenn Research Center, Cleveland, OH City for Science and Technology, Riyadh, Lancaster, PA; K. Thorson, Lockheed Associates, Albuquerque, NM; D. Saudi Arabia; A. Zoellner, Stanford Martin Corporation, Eagan, MN Hengeveld, LoadPath, Albuquerque, University, Stanford, CA; A. Alhussain, NM King Abdulaziz City for Science and Technology, Riyadh, Saudi Arabia; S. Wang, S. Saraf, Stanford University, Stanford, CA; et al. Tuesday, 14 June 2016 137-NW-4 Networking Coffee Break Columbia 1600 - 1630 hrs 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. Tuesday, 14 June 2016 138-LEC-3 Plasmadynamics and Lasers Award Lecture International Ballroom 1630 - 1730 hrs (East) Aero-Optics: A Photon Odyssey

85 Eric J. Jumper Roth-Gibson Professor of Aerospace and Mechanical Engineering, Department of Aerospace and Mechanical Engineering University of Notre Dame Tuesday, 14 June 2016 139-NW-5 Reception in the Exposition Hall Columbia 1730 - 1900 hrs 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 upon registration or on site. Wednesday Wednesday, 15 June 2016 140-SB-3 Speakers’ Briefing Session Rooms 0730 - 0800 hrs 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 session to exchange bios and review final details prior to the session. Please attend on the day of your session. Wednesday, 15 June 2016 141-PLNRY-4 Plenary International Ballroom 0800 - 0900 hrs (Center) Cybersecurity Richard A. Clarke Chairman & CEO Good Harbor Security Risk Management, LLC Wednesday, 15 June 2016 142-NW-5 Networking Coffee Break Columbia 0845 - 0930 hrs 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. Wednesday, 15 June 2016 143-AFM-9 Flight Test, System Identification and Parameter Estimation I Holmead West Chaired by: C. KARLGAARD, Analytical Mechanics Associates Inc and J. GRAUER, NASA Langley Research Center 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2016-3269 AIAA-2016-3270 AIAA-2016-3271 AIAA-2016-3272 AIAA-2016-3273 AIAA-2016-3274 Longitudinal Aerodynamic Simultaneous Multi-step Reconstruction of Aircraft Time-Domain System Comparison of Static Pressure Stable and Unstable Aircraft Modeling of the Adaptive Excitations for Aircraft System Trajectories during Landing Identification of Rigid-Body from Aircraft Trailing Cone Parameter Estimation in Compliant Trailing Edge Flaps on Identification using a Rauch-Tung-Striebel Multipoint Loads Model Measurements and Numerical Presence of Noise Using a GIII Aircraft and Comparisons to P. Lichota, Warsaw University of Smoother, Instrument Landing M. Preisighe Viana, German Weather Prediction Analysis Intelligent Estimation Technique Flight Data Technology, Warsaw, Poland; P. System Deviation Information, Aerospace Center (DLR), A. Giez, C. Mallaun, M. Zöger, A. Ghosh Roy , N. Peyada, Indian M. Smith, T. Bui, NASA Armstrong Flight Ohme, German Aerospace Center and Taxiway Locations Braunschweig, Germany A. Dörnbrack, U. Schumann, Institute of Technology Kharagpur, Research Center, Edwards, CA; C. Garcia, (DLR), Braunschweig, Germany; L. Höhndorf, J. Siegel, J. Sembiring, German Aerospace Center (DLR), Kharagpur, India Jacobs Technology, Inc., Edwards, CA; K. Sibilski, Warsaw University of P. Koppitz, F. Holzapfel, Technical Oberpfaffenhofen, Germany S. Cumming, NASA Armstrong Flight Technology, Warsaw, Poland University of Munich, Munich, Research Center, Edwards, CA Germany Wednesday, 15 June 2016 144-AFM-10 Unmanned Aerial Systems III Holmead East Chaired by: T. FIELDS, University of Missouri-Kansas City and D. MURRI, NASA Engineering and Safety Center and K. CUNNINGHAM, NASA Langley Research Center 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2016-3275 AIAA-2016-3276 AIAA-2016-3277 AIAA-2016-3278 AIAA-2016-3279 AIAA-2016-3280 Optical Target Tracking with Robust Control of Wind Design of a Rocketsonde Gramian-Inspired Unmanned Development and Flight Test Propulsion System Design for User Input for Automated RPA Powered Autonomous Launched UAS for Weather Aerial Flight Control for of Moving-mass Actuated Micro Aerial Vehicles Recovery Unmanned Aerial Vehicle Prediction and Modeling Atmospheric Energy Capture Unmanned Aerial Vehicle J. Vasconez, J. Grewal, E. Leonardo, C. Wilson, M. Anderson, M. Hyde, M. Sadraey, Daniel Webster College, S. Fehrenbach, J. Jacob, Oklahoma U. Saxena, I. Faruque, University S. Vengate, S. Erturk, A. Dogan, M. Marwa, C. Guzman, R. Mankbadi, K. Jensen, U.S. Air Force Academy, Nashua, NH State University, Stillwater, OK of Maryland, College Park, College University of Texas, Arlington, Embry-Riddle Aeronautical University, Colorado Springs, CO Park, MD Arlington, TX Daytona Beach, FL 86 Wednesday, 15 June 2016 145-AMT-6 Highlighting the Contributions of Prof. Ron Hanson to Aerodynamic Measurement Technology (Invited) Georgetown East Chaired by: P. DANEHY, NASA Langley Research Center and J. SEITZMAN, Georgia Institute of Technology 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs Oral Presentation Oral Presentation Oral Presentation Oral Presentation Oral Presentation Ron Hanson’s Integrated Laser absorption sensing Toward High-Speed Four- Impact of the Hanson Group’s Ron Hanson: Four Decades of Approach for Developing from the laboratory to field Dimensional Laser-Based 1980’s Fluorescence Experiments Research Accomplishments Effective Laser Diagnostics applications (Invited) Imaging on Aerospace Measurement J. Tishkoff, Air Force Office of J. Seitzman, Georgia Institute of J. Jeffries, R. Hanson, D. Davidson, J. Gord, Air Force Research Technology (Invited) Scientific Research, Arlington, VA Technology, Atlanta, GA Stanford University, Stanford, CA Laboratory, Wright-Patterson AFB, OH P. Danehy, NASA Langley Research Center, Hampton, VA Wednesday, 15 June 2016 146-APA-21 High Angle of Attack and High Lift Aerodynamics Columbia 9 Chaired by: C. PASILIAO, AFRL/RWWV and J. LATZ, Northrop Grumman Aerospace Systems 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2016-3281 AIAA-2016-3282 AIAA-2016-3283 AIAA-2016-3284 Analysis of Low-Speed Stall Lattice-Boltzmann Simulations Numerical Study of Aerodynamics Optimization of Chine-Shaped Aerodynamics of a Swept Wing of the JAXA JSM High-Lift and Flow Physics of the 30P30N Forebody of an Aircraft in with Seamless Flaps Configuration Three-Element Airfoil in Dynamic Terms of Providing Directional T. Bui, NASA Armstrong Flight B. Konig, E. Fares, Exa GmbH, Ground Effect Stability Research Center, Edwards, CA; S. Stuttgart, Germany; M. Murayama, Q. Qu, L. Huang, P. Liu, W. Wang, K. Makarov, A. Pavlenko, TsAGI, Moini-Yekta, Science and Technology Y. Ito, Y. Yokokawa, K. Yamamoto, Beihang University, Beijing, China; R. Zhukovsky, Russia Corporation, Moffett Field, CA Japan Aerospace Exploration Agency Agarwal, Washington University in St. (JAXA), Tokyo, Japan; et al. Louis, St. Louis, MO Wednesday, 15 June 2016 147-APA-22 Ground Vehicle Aerodynamics Albright Chaired by: A. SCLAFANI, Boeing Commercial Airplanes and X. WANG, Air Force Research Laboratory 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2016-3285 AIAA-2016-3286 AIAA-2016-3287 AIAA-2016-3288 Forcing Boundary-Layer Wake Deceleration of a Aerodynamics Simulation of Dynamic Mode Decomposition Transition on an Inverted Racecar Multielement Airfoil in a Sedan-type Road Vehicle in of Flow around a Full-Scale Road Airfoil in Ground Effect at Ground Effect Cornering Motion with Roll Angle Vehicle using Unsteady CFD Varying Incidence S. Bansal, M. Selig, University R. Kono, T. Nakashima, Hiroshima J. Ikeda, D. Matsumoto, Hokkaido L. Roberts, M. Finnis, K. Knowles, of Illinois, Urbana-Champaign, University, Higashi, Japan; M. Tsubokura, University, Sapporo, Japan; M. Cranfield University, Shrivenham, Urbana, IL Kobe University, Kobe, Japan; Y. Okada, Tsubokura, Kobe University, Kobe, Japan; United Kingdom T. Nouzawa, Mazda Motor Corporation, M. Uchida, T. Hasegawa, R. Kobayashi, Aki, Japan Fuji Heavy Industries, Ota, Japan Wednesday, 15 June 2016 148-APA-23/FD-28 Propeller/Rotorcraft/Wind Turbine Aerodynamics III Northwest Chaired by: K. MULLENERS, EPFL and J. MURRAY, Sandia National Laboratories 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2016-3289 AIAA-2016-3290 AIAA-2016-3291 AIAA-2016-3292 AIAA-2016-3293 Towards the optimization of wind Ducted Wind Turbine Vestas V136 rotor: Design and Numerical Investigation of Effects of Leading-Edge turbine rotor blades by means of Optimization testing of the tip airfoil Self-Starting Capability of Structures on Stall Behaviors of computational fluid dynamics and R. Venters, B. Helenbrook, K. Visser, F. Grasso, Vestas, Newport, United Vertical-Axis Wind Turbines at a NACA0015 Airfoil: A Multi- the adjoint approach Clarkson University, Potsdam, NY Kingdom Low Reynolds Numbers plane PIV Study L. Vorspel, University of Oldenburg, H. Tsai, T. Colonius, California Y. Zhang, J. Estevadeordal, S. Oldenburg, Germany; B. Stoevesandt, Institute of Technology, Pasadena, CA Bhusal, J. Krech, North Dakota State Fraunhofer, Oldenburg, Germany; University, Fargo, ND J. Peinke, I. Herraez, University of 87 Oldenburg, Oldenburg, Germany Wednesday, 15 June 2016 149-ASE-9 NASA/FAA/ONERA Swept Wing Icing Research--SUNSET2 Columbia 12 Chaired by: S. LEE, ASRC Aerospace Corporation and B. WOODARD, University of Illinois 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2016-3294 AIAA-2016-3295 AIAA-2016-3296 AIAA-2016-3297 AIAA-2016-3298 Ice-Accretion Test Results for Three Computational and Validation of a 3D ice accretion Improved Delayed Detached- Generation of Full-Span Large-Scale Swept-Wing Models in Experimental Ice Accretions of tool on swept wings of the Eddy Simulation on a Swept Leading-Edge 3D Ice Shapes the NASA Icing Research Tunnel Large Swept Wings in the Icing SUNSET2 program Hybrid Model in IRT for Swept-Wing Aerodynamic A. Broeren, M. Potapczuk, NASA Glenn Research Tunnel E. Radenac, ONERA, Toulouse, France C. Butler, University of Maryland, Testing Research Center, Cleveland, OH; S. Lee, G. Fujiwara, M. Bragg, S. Camello, College Park, College Park, MD; C. S. Camello, University of Washington, Vantage Partners, LLC, Cleveland, OH; A. C. Lum, University of Washington, Qin, E. Loth, University of Virginia, Seattle, Seattle, WA; S. Lee, Vantage Malone, B. Paul, The Boeing Company, Seattle, Seattle, WA Charlottesville, Charlottesville, VA Partners, LLC, Cleveland, OH; C. Lum, Seattle, WA; B. Woodard, University of M. Bragg, University of Washington, Illinois, Urbana-Champaign, Urbana, IL Seattle, Seattle, WA Wednesday, 15 June 2016 150-ASE-10 Ice-Crystal (Engine) Icing Physics Georgetown West Chaired by: D. FULEKI, National Research Council Canada and D. KNEZEVICI, GE Aviation 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2016-3299 AIAA-2016-3300 AIAA-2016-3301 AIAA-2016-3302 AIAA-2016-3303 AIAA-2016-3304 Plans and Preliminary Results Numerical Analysis of Mixed- Experimental Results for Ice Experimental Measurement A comprehensive numerical Mixed Phase Ice Accretion of Fundamental Studies of Phase Icing Cloud Simulations Crystal Icing on Hemispherical of the Percentage of Partial model for mixed-phase and Prediction with TAICE Ice Crystal Icing Physics in in the NASA Propulsion Systems and Double Wedge Geometries Melting in A Single Ice Crystal glaciated icing conditions E. Ayan, S. Özgen, M. Canibek, the NASA Propulsion Systems Laboratory at Varying Mach Numbers and S. Yan, J. Palacios, Pennsylvania P. Trontin, G. Blanchard, P. Villedieu, Turkish Aerospace Industries, Inc., Laboratory T. Bartkus, Ohio Aerospace Institute, Wet Bulb Temperatures State University, University Park, PA ONERA, Toulouse, France Ankara, Turkey P. Struk, NASA Glenn Research Cleveland, OH; P. Struk, NASA Glenn T. Currie, D. Fuleki, National Research Center, Cleveland, OH; J. Tsao, T. Research Center, Cleveland, OH; Council Canada, Ottawa, Canada Bartkus, Ohio Aerospace Institute, J. Tsao, Ohio Aerospace Institute, Cleveland, OH Cleveland, OH; J. Van Zante, NASA Glenn Research Center, Cleveland, OH Wednesday, 15 June 2016 151-ATIO.ACD-5 Aircraft Technologies and Concepts - Performance Studies and Design Methods Gunston East Chaired by: T. TAKAHASHI, Arizona State University and M. ORR, Boeing Commercial Airplanes 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2016-3305 AIAA-2016-3306 AIAA-2016-3307 AIAA-2016-3308 AIAA-2016-3309 Conceptualizing Active- The Clean Sky Technology Active Flow Control (AFC) and Risk-Based Approach to Integrated Design and Load-Alleviation: Impacts on Evaluator: review and results Insect Accretion and Mitigation Assessment of Advanced Optimization of Aircraft Transport Category Aircraft of the environmental impact (IAM) System Design and Technologies for Conceptual Families and Air Transport Wing Structural Design assessment at mission level Integration on the Boeing 757 Design Network M. Allyn, T. Takahashi, Arizona State R. Lafage, S. Aubry, ONERA, ecoDemonstrator A. Asmady, A. Drake, California P. Jansen, R. Perez, Royal Military University, Tempe, AZ Toulouse, France M. Alexander, F. Harris, NASA Langley Polytechnic State University, San Luis College of Canada, Kingston, Canada 88 Research Center, Hampton, VA; M. Obispo, CA Spoor, S. Boyland, T. Farrell, D. Raines, The Boeing Company, Seattle, WA Wednesday, 15 June 2016 152-ATIO.ATM-12 Surface Operations Modeling and Analysis I Embassy Chaired by: K. SWIERINGA, NASA Langley Research Center 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2016-3310 AIAA-2016-3311 AIAA-2016-3312 AIAA-2016-3313 AIAA-2016-3314 Using ASDE-X Surveillance for Methods for Determining A Mixed Integer Linear A Mixed Integer Linear A Concept of Operations for Taxi-Out Time Benchmarking Aircraft Surface State at Lesser- Program for Real-Time Programming Approach for Trajectory-based Taxi Operations and Delay Estimation Equipped Airports Computing the Optimal Push Computing the Optimal Chance- J. Okuniek, I. Gerdes, J. Jakobi, T. S. Hotle, GRA, Inc., Washington, K. Roach, J. Null, NASA Ames Back Time Windows Constrained Push Back Time Ludwig, German Aerospace Center D.C.; B. Baszczewski, J. Gulding, Research Center, Moffett Field, CA J. Coupe, D. Milutinovic, W. Malik, Windows (DLR), Braunschweig, Germany; B. Federal Aviation Administration, University of California, Santa Cruz, J. Coupe, D. Milutinovic, W. Malik, Hooey, San Jose State University, Moffett Washington, D.C. Santa Cruz, CA; Y. Jung, NASA Ames University of California, Santa Cruz, Field, CA; D. Foyle, NASA Ames Research Research Center, Moffett Field, CA Santa Cruz, CA; Y. Jung, NASA Ames Center, Moffett Field, CA; et al. Research Center, Moffett Field, CA Wednesday, 15 June 2016 153-ATIO.ATM-13 Environmental Impact Mitigation I Fairchild East Chaired by: K. MARAIS, Purdue University 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2016-3315 AIAA-2016-3316 AIAA-2016-3317 AIAA-2016-3318 AIAA-2016-3319 AIAA-2016-3320 Aviation and Electrical Road Are Climate Restricted Areas a Green Airlines 2025: Formation Generation in Huge Cost-Benefit Assessment of 2D Airline Competition in Duopoly Vehicles Viable Interim Climate Mitigation Environment and Sustainability Traffic Scenarios and 3D Climate And Weather Market and its Impact on J. Fregnani, B. Mattos, Technological Option over the North Atlantic? in Commercial Aviation - A F. Morscheck, German Aerospace Optimized Trajectories Environmental Emissions: A Institute of Aeronautics (ITA), São M. Niklass, German Aerospace Center Scenario Study Center (DLR), Braunschweig, B. Lührs, Hamburg University of Game Theory Approach José dos Campos, Brazil (DLR), Hamburg, Germany; B. Lührs, F. Will, G. Tay, Technical University Germany Technology, Hamburg, Germany; H. Chao, K. Ogunsina, K. Hamburg University of Technology, of Munich, Munich, Germany; A. M. Niklass, German Aerospace Moolchandani, D. DeLaurentis, W. Hamburg, Germany; K. Dahlmann, Becker, Airbus, Hamburg, Germany; Center (DLR), Hamburg, Germany; Crossley, Purdue University, West V. Grewe, German Aerospace Center D. Carnelly, F. Eychenne, Airbus, C. Froemming, V. Grewe, Lafayette, IN (DLR), Hamburg, Germany; V. Gollnick, Toulouse, France; M. Hornung, German Aerospace Center (DLR), Hamburg University of Technology, Technical University of Munich, Oberpfaffenhofen, Germany; V. Hamburg, Germany Munich, Germany Gollnick, Hamburg University of Technology, Hamburg, Germany Wednesday, 15 June 2016 154-ATIO.ATM-14 Data Mining in ATS I Fairchild West Chaired by: A. RAO, Purdue University 0930 hrs 1000 hrs 1030 hrs AIAA-2016-3321 AIAA-2016-3322 AIAA-2016-3323 Trajectory Clustering and Multi-Scale Data Mining for Identification of Convective Classification for Characterization Air Transportation System Hazards in New York Oceanic of Air Traffic Flows Diagnostics Airspace M. Conde Rocha Murca, Massachusetts R. DeLaura, R. Jordan, T. Reynolds, M. Veillette, R. DeLaura, MIT Lincoln 89 Institute of Technology, Cambridge, Lincoln Laboratory, Massachusetts Laboratory, Lexington, MA MA; R. DeLaura, Lincoln Laboratory, Institute of Technology, Lexington, Massachusetts Institute of Technology, MA; J. Avery, H. Balakrishnan, M. Cambridge, MA; R. Hansman, Conde Rocha Murca, Massachusetts Massachusetts Institute of Technology, Institute of Technology, Cambridge, Cambridge, MA; R. Jordan, T. Reynolds, MA; et al. Lincoln Laboratory, Massachusetts Institute of Technology, Cambridge, MA; H. Balakrishnan, Massachusetts Institute of Technology, Cambridge, MA Wednesday, 15 June 2016 155-ATIO.TFPC-7/ATIO. Transformational Flight - Electric Thin-Haul/Commuters Columbia 1 ACD-6/GEPC-1 Chaired by: R. MCDONALD, California Polytechnic State University-San Luis Obispo and M. PATTERSON 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs Oral Presentation AIAA-2016-3324 AIAA-2016-3325 AIAA-2016-3326 AIAA-2016-3327 Oral Presentation Thin-Haul Commuter Market Fuselage Boundary Layer Application of Distributed Sizing Power Components of Economics of Advanced Thin- Leading in the new era of Requirements and CONOPs Ingestion Propulsion Applied to Electric Propulsion to Thin-Haul an Electrically Driven Tail Cone Haul Concepts and Operations electric propulsion M. Patterson, M. Moore, K. Goodrich, a Thin Haul Commuter Aircraft Commuters Thruster and a Range Extender A. Harish, C. Perron, D. Bavaro, J. B. Knapp, Tzunum Aircraft, LLC, NASA Langley Research Center, for Optimal Efficiency A. Stoll, G. Veble Mikic, J. Bevirt, R. Jansen, C. Bowman, A. Jankovsky, Ahuja, M. Ozcan, C. Justin, Georgia Kirkland, WA Hampton, VA G. Veble Mikic, A. Stoll, J. Bevirt, Joby Aviation, Santa Cruz, CA NASA Glenn Research Center, Institute of Technology, Atlanta, Joby Aviation, Santa Cruz, CA; Cleveland, OH GA; et al. R. Grah, Institute of Science and Technology Austria, Klosterneuburg, Austria; M. Moore, NASA Langley Research Center, Hampton, VA Wednesday, 15 June 2016 156-D4U-1 DEMAND for UNMANNED: Catalyst for the Machine Intelligence Revolution International Ballroom 0930 - 1730 hrs (West)

0930-1030 hrs The Changing Face of Aerospace: The Impact of UAS on Aviation Moderator: I. J. Hudson, Former Technology Reporter, NBC4 Washington (WRC-TV) Panelists: Michael S. Francis Parimal H. Kopardekar John S. Langford Richard Wlezien Chief Advanced Programs & Senior Fellow Manager, Safe Autonomous System Operations Project, Chairman and Chief Executive Ofﬁcer Professor and Vance and Arlene Coffman Endowed United Technologies Research Center and Principal Investigator, Unmanned Aerial Systems Trafﬁc Aurora Flight Sciences Corporation Department Chair in Aerospace Engineering Management and Director, Iowa Space Grant Consortium NASA Ames Research Center Iowa State University

1030-1130 hrs Invention, Entrepreneurship, and Unmanned Systems Moderator: John Langford, Chairman and Chief Executive Ofﬁcer, Aurora Flight Sciences Corporation

1130-1400 hrs Break for Lunch

1400-1500 hrs Perspectives on the Future of Autonomous Systems and Technology Mary Louise “Missy” Cummings Associate Professor, Department of Mechanical Engineering and Materials Science, and Director, Humans and Autonomy Laboratory Duke University

90 1500-1530 hrs The Autonomy “Dream” John-Paul Clarke Professor, Daniel Guggenheim School of Aerospace Engineering, and Director, Air Transportation Laboratory Georgia Institute of Technology

1530-1600 hrs DEMAND for UNMANNED Networking Coffee Break

1600-1730 hrs Technology Roadmaps for Intelligent Autonomous Systems

Moderator: Jay Gundlach, Founder and President, Flighthouse Engineering LLC

Presenters: Mark G. Ballin Sebastian Scherer Technology Integration Manager Systems Scientist, The Robotics Institute NASA Airspace Operations and Safety Program Carnegie Mellon University Roundtable Panelists: Jay Gundlach Mark G. Ballin John-Paul Clarke Sebastian Scherer Founder and President Technology Integration Manager Professor, Daniel Guggenheim School of Aerospace Engineering, Systems ScientistThe Robotics Institute Flighthouse Engineering LLC NASA Airspace Operations and Safety Program and Director, Air Transportation Laboratory Carnegie Mellon University Georgia Institute of Technology Wednesday, 15 June 2016 157-F360-6 Cybersecurity Table Top War Gaming Exercise International Ballroom 0930 - 1130 hrs (East) Take part in a Table Top Exercise (TTX) focusing on the risks and complexities cyber events/cyber incidents can have on supply chain and supply chain management within the aviation domain. Participants will experience a facilitated Brown Paper War Game that will allow them to participate as responders (Blue Team) or threat actors (Red Team) in order to better understand the TTX process and provide them with the ability to discuss aviation-centric approaches to cyber security and risk management. During play, participants will be divided into sub teams representative of key functions within the supply chain domain and can expect to discuss topics such as threat actors, threat surfaces, and other cyber security issues.

Participants are encouraged to return at 1400 hrs for an extended Hot Wash forum session with industry thought leaders in cyber security and the aviation domain.

Those interested in becoming an active participant are expected to be present for the full two hour morning session and will need to pre-register. Those who wish to observe will also need to pre-register. Pre-register no later than 4PM on Tuesday, 14 June 2016, at https://www.surveymonkey.com/r/G22M7FF. Wednesday, 15 June 2016 158-FC-7 Internal Flow Control Columbia 11 Chaired by: C. BOURASSA, GE Aviation and O. SAHNI, Rensselaer Polytech Inst 0930 hrs 1000 hrs 1030 hrs AIAA-2016-3328 AIAA-2016-3329 AIAA-2016-3330 Comparison of vortex Vortex generators effectiveness Active Flow Control of Separation generators effect on shock compared to active ﬂow control in a Branched Duct wave induced separation techniques in a transonic C. Peterson, B. Vukasinovic, A. Glezer, P. Flaszynski, Polish Academy of diffuser Georgia Institute of Technology, Atlanta, Sciences, Gdansk, Poland J. Gartner, M. Amitay, Rensselaer GA; K. Saripalli, The Boeing Company, Polytechnic Institute, Troy, NY St. Louis, MO; N. Packard, The Boeing Company, Seattle, WA Wednesday, 15 June 2016

91 159-FC-8 Circulation Control Columbia 11 Chaired by: R. JOSLIN, Office of Naval Research and H. DONG, University of Virginia 0930 hrs 1130 hrs 1200 hrs No Presentations AIAA-2016-3331 AIAA-2016-3332 NACA0015 Circulation Control Multipoint Optimisation of Coanda Airfoil Using Synthetic Jets at Surfaces for Transonic Circulation Low Angles of Attack and Low Control using the Adjoint Method Reynolds Number M. Forster, University of Liverpool, P. Itsariyapinyo, R. Sharma, University Liverpool, United Kingdom; M. Biava, R. of Auckland, Auckland, New Zealand Steijl, University of Glasgow, Glasgow, United Kingdom Wednesday, 15 June 2016 160-FC-9/PDL-4/FD-29 Physics of Plasma Actuators Gunston West Chaired by: M. KOKLU, NASA Langley Research Center 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2016-3333 AIAA-2016-3334 AIAA-2016-3335 AIAA-2016-3336 Modelling of Dielectric Barrier Active Multiple Jets System Oblique Shock Control by Dynamic Characteristics of the Discharge Plasma Actuators for Using Surface Plasma Actuator Surface Arc Discharge Plasma Density Field near Wall Region Direct Numerical Simulations N. Benard, University of Poitiers, H. Yan, F. Liu, J. Xu, Northwestern Actuated by Plasma T. Brauner, S. Laizet, Imperial College Futuroscope, France; A. Mizuno, Polytechnical University, Xi’an, China L. Feng, C. Gao, Z. Lv, B. Wu, London, London, United Kingdom; University of Toyoashi, Toyoashi, Northwestern Polytechnical University, N. Benard, E. Moreau, University of Japan; E. Moreau, University of Xi’an, China Poitiers, Poitiers, France Poitiers, Futuroscope, France Wednesday, 15 June 2016 161-FD-30/APA-24 Modal Decomposition Methods and Analyses Columbia 4 Chaired by: B. MCGRATH, JHU/Applied Physics Laboratory and H. HU, Iowa State University 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2016-3337 AIAA-2016-3338 AIAA-2016-3339 AIAA-2016-3340 AIAA-2016-3341 Modal and non-modal global Analysis of Wake Structures Analysis of Turbine Wake Learning Wake Regimes from Extraction and analysis of instability analyses of low-Re Behind an Oscillating Square Characteristics using Proper Snapshot Data the second mode instability massively separated flow around Cylinder Using Dynamic Mode Orthogonal Decomposition M. Hemati, University of Minnesota, wave based on singular-value a NACA 0015 airfoil Decomposition (POD) and Triple Twin Cities, Minneapolis, MN decomposition and empirical R. Gioria, University of São Paulo, São B. Wang, University of Kansas, Decomposition Methods mode decomposition Paulo, Brazil; W. He, J. Perez, Technical Lawrence, Lawrence, KS; M. Yu, P. Premaratne, T. Wei, H. Hu, Iowa S. Xie, F. Ji, China Academy of University of Madrid, Madrid, Spain; University of Maryland, Baltimore State University, Ames, IA Aerospace Aerodynamics, Beijing, V. Theofilis, Universidade Federal County, Baltimore, MD China Fluminense, Niteroi, Brazil Wednesday, 15 June 2016 162-FD-32/FC-10 In Honor of John Lumley’s Lasting Legacy to Fluid Dynamics (Invited) Jefferson East Chaired by: D. SMITH, Office of Naval Research 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs Oral Presentation Oral Presentation Oral Presentation Oral Presentation Oral Presentation Remembering John L. Lumley John Lumley’s Turbulence The fusion of POD with Understanding Atmospheric Rational Control of Turbulent A. Smits, Princeton University, Closure Modeling Legacy stochastic estimation and Turbulence Structure through Boundary Layers – John Princeton, NJ S. Girimaji, Texas A&M University, compressive sensing to extract Simulation and Field Data, a Lumley’s Legacy College Station, TX low-dimensional physics for Lumley Legacy D. Rempfer, Illinois Institute of understanding and control of J. Brasseur, University of Colorado, Technology, Chicago, IL turbulent flows Boulder, Boulder, CO

92 M. Glauser, Syracuse University, Syracuse, NY Wednesday, 15 June 2016 163-FD-33 Boundary-Layer Transition: Crossflow Lincoln East Chaired by: B. WHEATON, JHU Applied Physics Laboratory and H. REED, Texas A&M University 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2016-3342 AIAA-2016-3343 AIAA-2016-3344 AIAA-2016-3345 AIAA-2016-3346 AIAA-2016-3347 Influence of Stationary Stationary Crossflow Breakdown Instability analysis and Tomographic PIV investigation Spatio-temporal characteristics Investigations of the Effect of Crossflow Modulation on due to Mixed Mode Spectra of transition prediction on a swept of crossflow instability of swept of secondary instabilities in Unsteady Pressure Gradient Secondary Instability Secondary Instabilities RAE2822 airfoil with constant wing boundary layers swept wing boundary layers and Cross-Flow on the Structure M. Choudhari, F. Li, P. Paredes, F. Li, M. Choudhari, NASA Langley lift coefficient J. Serpieri, M. Kotsonis, Delft J. Serpieri, M. Kotsonis, Delft and Dynamics of Laminar NASA Langley Research Center, Research Center, Hampton, VA; L. Duan, Z. Jing, Z. Huang, Tianjin University, University of Technology, Delft, The University of Technology, Delft, The Separation Bubbles Hampton, VA Missouri University of Science and Tianjin, China Netherlands Netherlands S. Hosseinverdi, University of Arizona, Technology, Rolla, MO Tucson, Tucson, AZ Wednesday, 15 June 2016 164-FD-34 RANS and LES Methods Columbia 10 Chaired by: G. ARAYA, University of Puerto Rico Mayaguez and C. SCHROCK, Air Force Research Laboratory 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2016-3348 AIAA-2016-3349 AIAA-2016-3350 AIAA-2016-3351 AIAA-2016-3352 AIAA-2016-3353 Discrete Filtering Formulations for Passive separation control on a An Assessment of Various Near-wall modification of A Study of LES Methods for LES modeling of scalar Large-Eddy Simulations backward facing ramp Turbulence Models for Spalart-Allmaras Turbulence Simulation of Ship Airwakes transport based on high-order A. Edoh, University of California, Los S. Shinde, S. Tandon, K. Maki, E. Preconditioned High-Order Model for Immersed Boundary D. Linton, B. Thornber, University of discontinuous finite-element Angeles, Los Angeles, CA; N. Mundis, Johnsen, University of Michigan, Ann Solutions of Flow Around Method Sydney, Sydney, Australia; R. Widjaja, method: Assessment of implicit Air Force Research Laboratory, Edwards Arbor, Ann Arbor, MI Submersibles Y. Tamaki, M. Harada, T. Imamura, Defence Science and Technology LES and scalar variance AFB, CA; A. Karagozian, University of O. Tong, Y. Yanagita, A. Katz, Utah University of Tokyo, Tokyo, Japan Group, Melbourne, Australia modeling California, Los Angeles, Los Angeles, State University, Logan, UT Y. Lv, M. Ihme, Stanford University, CA; V. Sankaran, Air Force Research Stanford, CA Laboratory, Edwards AFB, CA Wednesday, 15 June 2016 165-FD-35 Facilities and Measurement Techniques Monroe Chaired by: R. DELOACH, NASA-Langley Research Center and T. ROSSMANN, Lafayette College 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2016-3354 AIAA-2016-3355 AIAA-2016-3356 AIAA-2016-3357 AIAA-2016-3358 Characterization and Validation An Investigation of the Role of A Numerical Comparison of Volumetric PIV Measurements Studies of the Large-Scale of an Anechoic Facility for an Upstream Burst Diaphragm Symmetric and Asymmetric in the Wake of a Wavy Cylinder Structure in Turbulent Boundary High-Temperature Jet Noise on Flow Quality within a Supersonic Wind Tunnels A. Ahmed, Auburn University, Auburn, Layers Using Simultaneous Studies Ludwieg Tube using RANS K. Clark, P. Orkwis, University of AL; M. Khan, Tuskegee University, Velocity-Wavefront Measurements J. Craft, P. Upadhyay, T. Worden, S. Lindörfer, P. Anusonti-Inthra, J. Cincinnati, Cincinnati, OH Tuskegee, AL S. Gordeyev, University of Notre F. Alvi, Florida State University, Schmisseur, C. Combs, University of Dame, Notre Dame, IN; A. Smith, MZA Tallahassee, FL Tennessee, Tullahoma, Tullahoma, TN Associates Corporation, Dayton, OH Wednesday, 15 June 2016 166-FD-36 Adjoints and Error Estimation Oak Lawn Chaired by: K. FIDKOWSKI, University of Michigan and D. MOTT, Naval Research Laboratory 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2016-3359 AIAA-2016-3360 AIAA-2016-3361 AIAA-2016-3362 AIAA-2016-3363 AIAA-2016-3364 A Comprehensive Study of Output Error Estimation for An Extension of Adjoint Method Optimal Mesh Adaptation for Improved Functional-Based Multiresolution Wavelet Adjoint-Based Optimization Chaotic Flows Capabilities 1D Euler Equations with Multi- Error Estimation and Approach for Feature Detection of Non-Linear Systems with Y. Shimizu, K. Fidkowski, University M. Hayashi, E. Volpe, University of Mesh Applications Adaptation without Adjoints in Adaptive Mesh Refinement Application to Burgers’ Equation of Michigan, Ann Arbor, Ann Arbor, MI São Paulo, São Paulo, Brazil C. Jackson, H. Wang, C. Roy, W. Tyson, K. Swirydowicz, J. Derlaga, with High-Order Shock- and A. Fikl, V. Le Chenadec, T. Sayadi, Virginia Polytechnic Institute and C. Roy, E. de Sturler, Virginia Interface-Capturing Scheme University of Illinois, Urbana-Champaign, State University, Blacksburg, VA; Polytechnic Institute and State M. Wong, S. Lele, Stanford Urbana, IL; P. Schmid, Imperial College C. Schrock, Air Force Research University, Blacksburg, VA University, Stanford, CA London, London, United Kingdom Laboratory, Dayton, OH

93 Wednesday, 15 June 2016 167-FD-37 CFD for Engineering Applications Morgan Chaired by: M. GHOREYSHI, United States Air Force Academy and B. JOLLY, US Air Force 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2016-3365 AIAA-2016-3366 AIAA-2016-3367 AIAA-2016-3368 AIAA-2016-3369 AIAA-2016-3370 Development and Use of Computational Investigation Parametric optimization of an Back-Pressure Stall Prediction Investigation of Helicopter Large Eddy Simulation of a 3D Engineering Standards for of a Boundary Layer Ingestion existing supersonic-subsonic in Eductor-Jet Pumps Ditching Angle on Fuselage Transonic Fan Computational Fluid Dynamics for Propulsion System for the ejector design by means of W. Liu, K. Pochiraju, Stevens Institute Pressure Load using a SPH R. Bhaskaran, T. Wood, U. Paliath, A. Complex Aerospace Systems Common Research Model computational fluid dynamics of Technology, Hoboken, NJ Method Breeze-Stringfellow, General Electric H. Lee, Bettis Laboratory, West Mifflin, B. Blumenthal, A. Elmiligui, K. M. Diaz Brito, Pall, Portsmouth, Z. Lu, T. Xiao, Nanjing University Company, Niskayuna, NY PA; U. Ghia, University of Cincinnati, Geiselhart, R. Campbell, NASA United Kingdom of Aeronautics and Astronautics, Cincinnati, OH; S. Bayyuk, ESI Group, Langley Research Center, Hampton, Nanjing, China Huntsville, AL; W. Oberkampf, WLO VA; M. Maughmer, S. Schmitz, Consulting, Austin, TX; C. Roy, Virginia Pennsylvania State University, State Polytechnic Institute and State University, College, PA Blacksburg, VA; J. Benek, Air Force Research Laboratory, Wright-Patterson AFB, OH; et al. Wednesday, 15 June 2016 168-GT-4 Ground Testing for High Speed Flight and Reentry Lincoln West Chaired by: B. WILLIAMS, Aerospace Coporation and P. MACALUSO, US Air Force 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2016-3371 AIAA-2016-3372 AIAA-2016-3373 AIAA-2016-3374 AIAA-2016-3375 AIAA-2016-3376 Basic characteristics of the free- Theoretical Considerations to Baseline characterization of the Development of a Hypersonic Investigation on Aerodynamic Development of a Thermal piston driven expansion tube Extend the Operational Map of 30kW miniature arc jet facility Flutter Test Capability Measurement of Hypersonic Simulator to Thermally Test the JAXA HEK-X the VKI Longshot Hypersonic mARC at NASA Ames C. Ji, Z. Liu, N. Chen, L. Feng, China Wind Tunnel with Cable Driven Solar Probe Plus Spacecraft H. Tanno, T. Komuro, K. Sato, K. Itoh, Wind Tunnel A. Nawaz, T. Ho, Jacobs, Moffett Field, Academy of Aerospace Aerodynamics, Parallel Suspension System E. Congdon, E. Abel, E. Heisler, T. Japan Aerospace Exploration Agency G. Grossir, Z. Ilich, S. Paris, O. CA; D. Philippidis, Qualis Corporation, Beijing, China X. Wang, Q. Lin, Xiamen University, Hartka, Johns Hopkins University (JAXA), Kakuda, Japan; K. Arai, Chazot, von Kármán Institute for Moffett Field, CA; M. MacDonald, Jacobs, Xiamen, China Applied Physics Laboratory, Laurel, Tokai University, Hiratsuka, Japan; K. Fluid Dynamics, Rhode-Saint-Genèse, Moffett Field, CA; M. McGlaughlin, D. MD Yamada, Japan Aerospace Exploration Belgium Driver, NASA Ames Research Center, Agency (JAXA), Sagamihara, Japan Moffett Field, CA Wednesday, 15 June 2016 169-ITAR-3 CITMAV Cabinet Chaired by: T. FISHER and K. YERKES, Air Force Reseach Laboratory 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs Oral Presentation Oral Presentation AIAA-2016-3377 Oral Presentation Oral Presentation AIAA-2016-3378 Effects of Thermal Hardware-In-The-Loop Validation An Exact Solution for Cooling of Transient, High- A Cryogenic Based Aviation CTE Matched High Heat Flux Management on the Beam of Advanced Fuel Thermal Temperature Excursions in Flat Heat-Flux Loads Generated by Thermal Management System Spreader for Space Systems Quality of High Power Laser Management Control Plates with Step Changes in Thermally Sensitive Devices A. Donovan, S. Nuzum, M. Wolff, Applications Diode Bars H. Pangborn, University of Illinois, Surrounding Temperatures J. Engerer, T. Fisher, Purdue R. Roberts, Wright State University, B. Richard, D. Pellicone, C. Chen, T. Fisher, P. Bermel, D. Konopa, Urbana-Champaign, Urbana, IL; J. Hey, L. Byrd, Air Force Research University, West Lafayette, IN Dayton, OH Advanced Cooling Technologies, Inc., Purdue University, West Lafayette, IN Purdue University, West Lafayette, IN; Laboratory, Wright-Patterson AFB, OH Lancaster, PA T. Deppen, PC Krause and Associates, 94 West Lafayette, IN; A. Alleyne, University of Illinois, Urbana-Champaign, Urbana, IL; T. Fisher, Purdue University, West Lafayette, IN Wednesday, 15 June 2016 170-MAO-10 Shape and Topology Optimization V Columbia 3 Chaired by: T. HEARN, NASA Glenn Research Center and S. FERGUSON, North Carolina State University 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2016-3379 AIAA-2016-3380 AIAA-2016-3381 AIAA-2016-3382 AIAA-2016-3383 Thermal Topology Optimization Shape Optimization of Acoustic CAD-based Aerodynamic Shape Multidisciplinary, Multiobjective Transonic Nacelle Aerodynamic in OptiStruct Software Metamaterials and Phononic Optimization Using Geometry Analysis and Optimization for Optimization Based on Hybrid X. Qu, N. Pagaldipti, R. Fleury, Crystals with a Time-Dependent Surrogate Model And Adjoint the Design of Missile Jet Vane Genetic Algorithm J. Saiki, Altair Engineering, Inc., Adjoint Formulation: Three- Methods C. Citak, M. Akdemir, M. Yumusak, X. Fang, Y. Zhang, S. Li, H. Chen, Irvine, CA Dimensional Applications K. Bobrowski, Technical University of ROKETSAN Missile Industries, Inc., Tsinghua University, Beijing, China W. Lin, J. Newman, W. Anderson, Madrid, Madrid, Spain; H. Barnewitz, Ankara, Turkey X. Zhang, University of Tennessee, Airbus, Bremen, Germany; E. Ferrer, Chattanooga, Chattanooga, TN E. Valero, Technical University of Madrid, Madrid, Spain Wednesday, 15 June 2016 171-MST-9 Modeling and Simulation of Aeroelasticity I Piscataway Chaired by: A. ELMILIGUI, NASA Langley Research Center and D. KEATING 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2016-3384 AIAA-2016-3385 AIAA-2016-3386 AIAA-2016-3387 AIAA-2016-3388 Nonlinear and Linear Aeroelastic Flutter Suppression for a Effects of Turbulence Model on Transonic Aeroelastic Moving Maneuver Loads Calculation Modeling and Experimental Prototype Wing – Numerical Flutter Prediction of a Transonic Gust Responses and Alleviation with Enhanced Aerodynamics Analysis of Flexibles Wings for Modeling, Control Law Design, Fan based on CFD for a UCAV Configuration Wind Tunnel Flutter Test and Experimental Results X. Zhang, Y. Wang, N. Wang, A. Tian, Z. Qiang, G. Chen, Y. Li, Xi’an A. Voss, T. Klimmek, German M. Westin, R. da Silva, J. Balthazar, K. Lai, Z. Lu, Y. Cui, National University Beijing University of Aeronautics and Jiaotong University, Xi’an, China; Aerospace Center (DLR), Göttingen, A. Nabarrete, M. Pereira, Technological of Singapore, Singapore, Singapore; K. Astronautics, Beijing, China A. Da Ronch, University of Germany Institute of Aeronautics (ITA), São José Lum, National Chi Nan University, Puli Southampton, Southampton, United dos Campos, Brazil Township Nantou County, Taiwan Kingdom Wednesday, 15 June 2016 172-TP-7 Advanced Modeling I - DSMC Jefferson West Chaired by: T. SCHWARTZENTRUBER, University of Minnesota and K. STEPHANI, University of Illinois at Urbana-Champaign 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2016-3389 AIAA-2016-3390 AIAA-2016-3391 AIAA-2016-3392 AIAA-2016-3393 AIAA-2016-3394 State-to-State Vibrational DSMC Shock Simulation of Heat Flux and Drag Finite-rate oxidation model for Reducing Statistical Scatter in Adapting vibrational relaxation Energy Modeling in DSMC Saturn Entry Probe Conditions Correlations for High Speed carbon surfaces from molecular DSMC Solutions of Hypersonic models in DSMC and CFD to using Quasiclassical Trajectory K. Higdon, University of Texas, Austin, Flight at any Knudsen Number beam experiments Ionizing Flows ab-initio calculations Calculations for O + O2 Austin, TX; B. Cruden, A. Brandis, N. Singh, T. Schwartzentruber, S. Poovathingal, T. Schwartzentruber, C. Kaplan, E. Oran, U. Aggarwal, M. Kulakhmetov, I. Sebastiao, A. T. Wilson, K. Stephani, University NASA Ames Research Center, Moffett University of Minnesota, Minneapolis, University of Minnesota, Minneapolis, University of Maryland, College Park, Alexeenko, Purdue University, West of Illinois, Urbana-Champaign, Field, CA; D. Liechty, NASA Langley Minneapolis, MN Minneapolis, MN; V. Murray, T. Minton, College Park, MD Lafayette, IN Urbana, IL Research Center, Hampton, VA; D. Montana State University, Bozeman, Goldstein, P. Varghese, University of MT; G. Candler, University of Minnesota, 95 Texas, Austin, Austin, TX Minneapolis, Minneapolis, MN Wednesday, 15 June 2016 173-RLA-3 Rising Leaders in Aerospace Keynote Columbia 9 1130 - 1230 hrs Innovations, Technology, and Skills for the Next 100 Years in Aerospace Greg Hyslop Senior Vice President, Engineering, Test & Technology The Boeing Company Wednesday, 15 June 2016 174-LNCH-2 Networking Luncheon International Ballroom 1230 - 1400 hrs (Center) A ticket for the luncheon is required and included in the registration fee where indicated. Additional tickets for guests may be purchased upon registration or on site, as space is available. Wednesday, 15 June 2016 175-AFM-11 Aerodynamic Prediction Methods Holmead East Chaired by: C. SUCHOMEL, USAF and T. LAVIN, Sandia National Laboratories and B. JOLLY, US Air Force 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs Oral Presentation AIAA-2016-3395 AIAA-2016-3396 AIAA-2016-3397 AIAA-2016-3398 AIAA-2016-3399 AIAA-2016-3400 Computing Aerodynamic Application of an Angle of Attack Upset Detection Towards Three-Dimensional Experimental Study of a Flight Dynamics Mode Accurate Prediction for Non- Derivatives Based on Harmonic Autoregressive Moving Average for Passenger Airliners using Global Stability Analysis of Morphing Wing Configuration Identification and Model Gravitational Aerodynamic Balance Method by Using Approach in Flight Trajectory Classification of Anemometric Transonic Shock Buffet with Multi-Slotted Variable- Reduction using Computational Forces acting on the GOCE Open-Source SU2 Simulation and Inertial Sensor Data S. Timme, R. Thormann, University of Camber Mechanism Fluid Dynamics Satellite Using the Test Particle A. Shi, J. Wang, Northwestern Y. Xing, G. Wang, Y. Zhu, P. Malan, J. Engelbrecht, H. Liverpool, Liverpool, United Kingdom M. Maki, Japan Aerospace G. Pagliuca, S. Timme, University of Monte Carlo Method Polytechnical University, Xi’an, China Northwestern Polytechnical University, Engelbrecht, Stellenbosch University, Exploration Agency (JAXA), Tokyo, Liverpool, Liverpool, United Kingdom X. Jin, F. Huang, X. Cheng, J. Xi’an, China Stellenbosch, South Africa Japan Yu, China Academy of Aerospace Aerodynamics, Beijing, China Wednesday, 15 June 2016 176-AFM-12 Flight Test, System Identification and Parameter Estimation II Holmead West Chaired by: A. VANDERWYST, Leidos and J. GRAUER, NASA Langley Research Center 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs AIAA-2016-3401 AIAA-2016-3402 AIAA-2016-3403 AIAA-2016-3404 AIAA-2016-3405 AIAA-2016-3406 AIAA-2016-3407 Aerodynamic Modeling, System An Easy to Use Engineering Virtual Flight Testing of High Aerodynamic Flight Test Results Aerodynamic Parameter Design and Control of a Micro A flutter boundary Identification and Analysis of Method for Identification of Performance Fighter Aircraft for the Adaptive Compliant Estimation of a Supersonic Air UAV prediction technique based Iced Aircraft Configurations Complex Flight Dynamics From Using High-Resolution CFD Trailing Edge to Air Missile with Rapid Speed D. Kaya, A. Büyükkoçak, A. Kutay, on atmospheric turbulence C. Deiler, German Aerospace Center Flight Test Data C. Ratcliff, D. Bodkin, J. Clifton, M. S. Cumming, M. Smith, A. Ali, T. Bui, Variation O. Tekinalp, Middle East Technical excitation responses (DLR), Braunschweig, Germany R. Larsson, Saab, Linköping, Sweden; Willis, Air Force SEEK EAGLE Office, J. Ellsworth, NASA Armstrong Flight T. Bayoğlu, O. Nalci, A. Kutay, University, Ankara, Turkey Y. Li, L. Zhou, Nanjing University M. Enqvist, Linköping University, Eglin AFB, FL Research Center, Edwards, CA; C. ROKETSAN Missile Industries, Inc., of Aeronautics and Astronautics, Linköping, Sweden Garcia, Jacobs, Edwards, CA Ankara, Turkey Nanjing, China Wednesday, 15 June 2016 177-AMT-7 Recent Advancements in Gas Temperature Measurements in Gas Turbines (Invited) Columbia 2 Chaired by: D. RICHARDSON, Air Force Research Laboratory 1400 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs Oral Presentation Oral Presentation Oral Presentation Oral Presentation Oral Presentation The Evolution of Temperature Sensing in Combustion/Propulsion Optical Measurements of Diagnostic to Measure Turbine Recent Advances in Cooling Effectiveness Flows using Laser-Induced Absorption and Fluorescence (Invited) Temperature and Species Blade Temperatures During Temperature Measurements Measurements for Air Film R. Hanson, J. Jeffries, D. Davidson, Stanford University, Stanford, CA Concentrations in Gas Turbine Engine Operation (Invited) Using Coherent Anti-Stoles Cooling of Thermal Barrier Components and Full-Scale T. Jenkins, MetroLaser, Inc., Laguna Raman Scattering (CARS) Coated Surfaces in a Burner Engines (Invited) Hills, CA; S. Allison, Emerging (Invited) Rig Test Environment Using J. Gord, Air Force Research Measurements, Inc., Knoxville, TN; R. Lucht, A. Satija, L. Thomas, Purdue Phosphor Thermometry Laboratory, Wright-Patterson AFB, OH J. Eldridge, NASA Glenn Research University, West Lafayette, IN J. Eldridge, V. Shyam, A. Wroblewski, Center, Cleveland, OH D. Zhu, NASA Glenn Research Center,

96 Cleveland, OH; M. Cuy, Vantage Partners, LLC, Cleveland, OH; D. Wolfe, Pennsylvania State University, College Township, PA Wednesday, 15 June 2016 178-APA-25/FD-38 Aerodynamic Design Methodologies I Albright Chaired by: B. DETERT, Boeing Commercial Airplanes and M. POST, USAF Academy 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs AIAA-2016-3408 AIAA-2016-3409 AIAA-2016-3410 AIAA-2016-3411 AIAA-2016-3412 AIAA-2016-3413 AIAA-2016-3414 Data-Driven Probabilistic Aerodynamic Shape A Locally Adaptive Subdivision Development of An Efficient Three Dimensional Design A New Formulation of Optimization of Flap position Boundary Layer Modeling for Optimization by Variable- Parameterisation Scheme Three-Dimensional Tightly Optimization Using Adjoint Gradient-Enhanced Surrogate using a Modified Discrete Airfoil Performance Prediction fidelity Models and Gradient- for Aerodynamic Shape Coupled Euler/Panel Solver for Method Model and Application to Vortex method A. Marques, Q. Wang, Y. Marzouk, Enhanced Manifold Mapping Optimisation Transonic Flow Analysis A. Yildirim, S. Eyi, Middle East Aerodynamic Design B. Narayanarao, P. Mondal, A. Massachusetts Institute of L. Leifsson, Iowa State University, D. Masters, University of Bristol, Y. Jo, D. Lee, Korea Advanced Technical University, Ankara, Turkey C. Song, Z. Han, Y. Zhang, Kanale, Indian Institute of Science, Technology, Cambridge, MA Ames, IA; Y. Tesfahunegn, S. Koziel, Bristol, United Kingdom; N. Taylor, Institute of Science and Technology, Northwestern Polytechnical University, Bengaluru, India; N. Shende, Reykjavik University, Reykjavik, MBDA, Filton, United Kingdom; T. Daejeon, South Korea; S. Choi, Xi’an, China R. Wadnerkar, S&I Engineering Iceland Rendall, C. Allen, University of Bristol, Virginia Polytechnic Institute and Solutions Pvt., Ltd., Bengaluru, India Bristol, United Kingdom State University, Blacksburg, VA Wednesday, 15 June 2016 179-APA-26 Aerodynamic - Structural Dynamics Interactions I Northwest Chaired by: J. AZEVEDO and L. WANG, NASA Langley Research Center 1400 hrs 1430 hrs 1500 hrs AIAA-2016-3415 AIAA-2016-3416 AIAA-2016-3417 Development of a Fluid- Understanding Energy Transfer A Reduced Order Model for Structure Interaction in Aeroelastic Flutter Aeroelastic Response Prediction to Framework Using Unstructured P. Deshpande, A. Kelkar, Iowa State Continuous Turbulence Encounter Cartesian CFD Methods University, Ames, IA including CFD Aerodynamics M. Bopp, S. Ruffin, Georgia Institute D. Quero-Martin, W. Krüger, German of Technology, Atlanta, GA Aerospace Center (DLR), Göttingen, Germany; G. Jenaro, Airbus, Hamburg, Germany Wednesday, 15 June 2016 180-APA-27 Innovative Aerodynamic Concepts & Designs Columbia 9 Chaired by: N. HALL and G. GATLIN, NASA Langley Research Center 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2016-3418 AIAA-2016-3419 AIAA-2016-3420 AIAA-2016-3421 AIAA-2016-3422 AIAA-2016-3423 Aerodynamic Design of Aerodynamic Design of the Design and Analyses of High Virtual Flight Demonstration of Efficient Design Optimization Wing-In-Ground-Effect Craft as Blended Wing-Body and Hybrid Wing Body with Nacelle: Aspect Ratio Nozzles for the Stratospheric Dual-Aircraft of Flexible CROR Blade for a Potential Domestic Transport Lifting-Fuselage Aircraft N3-X Propulsion-Airframe Distributed Propulsion Acoustic Platform Low-level Noise Vehicle T. Reist, D. Zingg, University of Configuration Measurements W. Engblom, Embry-Riddle S. Yi, D. Lee, Korea Advanced S. Wiriadidjaja, Z. Mohamad, A. Toronto, Toronto, Canada M. Liou, NASA Glenn Research Center, V. Dippold, NASA Glenn Research Aeronautical University, Daytona Institute of Science and Technology, Mohd Rafie, Universiti Putra Malaysia Cleveland, OH; D. Gronstal, University Center, Cleveland, OH Beach, FL; R. Decker, NASA Marshall Daejeon, South Korea; S. Choi, D. (UPM), Serdang, Malaysia; M. Elhadi, of Alabama, Tuscaloosa, Tuscaloosa, Space Flight Center, Huntsville, AL Im, Virginia Polytechnic Institute and Karary University, Khartoum, Sudan; AL; H. Kim, SAIC, Cleveland, OH; M. State University, Blacksburg, VA A. Fariduzzaman, F. Hasim, Agency for 97 Liou, NASA Glenn Research Center, Assessment & Application of Technology, Cleveland, OH Jakarta-Pusat, Indonesia Wednesday, 15 June 2016 181-APA-28 Aerodynamic Testing: Flight, Wind-Tunnel and Flight Testing Columbia 4 Chaired by: C. ROSEMA, US Army AMRDEC and D. O’BRIEN, US Army RDECOM 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs AIAA-2016-3424 AIAA-2016-3425 AIAA-2016-3426 AIAA-2016-3427 AIAA-2016-3428 Experimental Visualization of Investigation of the Wind Tunnel Test of Subscale Aerodynamic Models for Robust SJA-Based Nonlinear Junction Separation Bubbles Aerodynamic Characteristics Ringsail and Disk-Gap-Band the Low Density Supersonic Trajectory Tracking Control at Low- to Moderate-Reynolds of a Lifting Body in Ground Parachutes Declerator (LDSD) Test Vehicles Using Unmanned Aircraft LPV Numbers Proximity C. Zumwalt, J. Cruz, NASA Langley J. Van Norman, Analytical Mechanics Model M. Kuester, A. Borgoltz, W. J. Holt, K. Garry, T. Smith, Cranfield Research Center, Hampton, VA; C. Associates, Inc., Hampton, VA; A. P. Kazarin, V. Golubev, W. MacKunis, Devenport, Virginia Polytechnic University, Bedford, United Kingdom O’Farrell, Jet Propulsion Laboratory, Dyakonov, M. Schoenenberger, J. Embry-Riddle Aeronautical Institute and State University, California Institute of Technology, Davis, NASA Langley Research Center, University, Daytona Beach, FL; S. Blacksburg, VA Pasadena, CA; D. Keller, NASA Langley Hampton, VA; S. Muppidi, Analytical Borener, D. Hufty, Federal Aviation Research Center, Hampton, VA Mechanics Associates, Inc., Hampton, Administration, Washington, D.C. VA; C. Tang, NASA Ames Research Center, Moffett Field, CA; et al. Wednesday, 15 June 2016 182-ASE-11 Numerical Weather Prediction (Invited) Columbia 12 Chaired by: V. TALLAPRAGADA and N. AHMAD, NASA Langley Research Center 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs Oral Presentation Oral Presentation Oral Presentation AIAA-2016-3429 Oral Presentation AIAA-2016-3430 AIAA-2016-3431 Next Generation Unified Global Forecasting Airship Operations Numerical Weather Prediction A High-Order Multiscale Global Implementation of new Global Design of Representing Multi- Comparison of Fully- Modeling System Development at in Remote Areas (Invited) at Deutscher Wetterdienst Atmospheric Model (Invited) Forecast Icing products at NCEP’s scale Interactions in the HWRF Compressible Equation Sets NCEP for Seamless Weather and D. Bacon, A. Sarma, Leidos, Reston, (DWD, Germany) (Invited) R. Nair , National Center for Operations based on NCAR’s Modeling System (Invited) for Atmospheric Dynamics Climate Predictions (Invited) VA D. Majewski, Deutscher Wetterdienst Atmospheric Research, Boulder, CO Aviation Algorithms (Invited) X. Zhang, S. Gopalakrishnan, (Invited) V. Tallapragada, National Oceanic and (DWD), Offenbach, Germany V. Tallapragada, H. Chuang, Y. Mao, National Oceanic and Atmospheric N. Ahmad, NASA Langley Research Atmospheric Administration, College National Oceanic and Atmospheric Administration, Miami, FL Center, Hampton, VA Park, MD Administration, College Park, MD Wednesday, 15 June 2016 183-ASE-12 NASA PSL LF11 Engine Icing Test Campaign Georgetown West Chaired by: M. BRAVIN, Boeing Commercial Airplanes and E. LOTH, University of Virginia 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs AIAA-2016-3432 AIAA-2016-3433 AIAA-2016-3434 AIAA-2016-3435 Oral Presentation AIAA-2016-3436 Oral Presentation Turbofan Ice Crystal Rollback Determination of engine recovery Preliminary Results from a Modeling of Highly Test Point Selection for Engine NASA Glenn Propulsion Aircraft engine icing Investigation and Preparations after an ice accretion rollback, Heavily Instrumented Engine Instrumented Honeywell Crystal Icing Test at NASA Systems Lab Ice Crystal Cloud instrumentation used in Leading to the Second, Heavily engine performance deterioration Ice Crystal Icing Test in a Turbofan Engine Tested with Ice PSL-3 for focused sensitivity, Characterization Update 2015 the NASA Glenn Propulsion Instrumented, Ice Crystal and health monitoring using Ground Based Altitude Test Crystal Ingestion in the NASA peak intensity, and anti-ice J. Van Zante, T. Bencic, T. Ratvasky, Systems Laboratory Engine Test at NASA PSL-3 test minimal instrumentation during Facility Propulsion System Laboratory evaluations NASA Glenn Research Center, T. Bencic, NASA Glenn Research Facility icing testing at NASA Glenn PSL3 A. Flegel, M. Oliver, NASA Glenn J. Veres, P. Jorgenson, S. Jones, D. Dischinger, W. Sandel, Honeywell Cleveland, OH Center, Cleveland, OH R. Goodwin, Honeywell International, D. Walker, Honeywell International, Inc., Research Center, Cleveland, OH NASA Glenn Research Center, International, Inc., Phoenix, AZ Inc., Phoenix, AZ Phoenix, AZ Cleveland, OH 98 Wednesday, 15 June 2016 184-ATIO.ATM-15 Surface Operations Modeling and Analysis II Embassy Chaired by: Y. JUNG, NASA Ames Research Center 1400 hrs 1430 hrs 1500 hrs AIAA-2016-3437 AIAA-2016-3438 AIAA-2016-3439 A Data Driven Approach for System Performance of an Queue Buffer Sizing for Characterization of Ramp Area Integrated Airborne Spacing Efficient and Robust Integrated Push Back and Ramp-Taxi Algorithm with Ground Departure Scheduling Processes Automation H. Idris, N. Shen, Engility Corporation, J. Coupe, D. Milutinovic, W. Malik, K. Swieringa, S. Wilson, B. Baxley, Billerica, MA; A. Saraf, J. Bertino, University of California, Santa Cruz, NASA Langley Research Center, N. Luch, ATAC Corporation, Santa Santa Cruz, CA; Y. Jung, NASA Ames Hampton, VA Clara, CA Research Center, Moffett Field, CA Wednesday, 15 June 2016 185-ATIO.ATM-16 Environmental Impact Mitigation II Fairchild East Chaired by: J. CISTONE, Sullivan Aviation Services, LLC 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs AIAA-2016-3440 AIAA-2016-3441 AIAA-2016-3442 AIAA-2016-3443 AIAA-2016-3444 AIAA-2016-3445 AIAA-2016-3446 Development of a New Aircraft Logistics for Air to Air How Slow is Too Slow? AIRNOISE: a Tool for Operational Shortfalls and Delayed Deceleration Approach Contrail Mitigation Through 3D Noise Prediction Program Refuelling in Civil Aviation, Economics of Aircraft Concepts Preliminary Noise-Abatement Potential Benefits of Path- Noise Assessment Aircraft Trajectory Optimization A. Filippone, University of Step Jump in Fuel/Weight / with Reduced Cruise Speeds Terminal Approach Route Based Wind Shear Prediction T. Reynolds, M. Sandberg, Lincoln S. Hartjes, T. Hendriks, D. Visser, Manchester, Manchester, United Cost Efficiency & Smaller A. Evans, University of California, Design C. Reiche, M. Robinson, C. Craun, Laboratory, Massachusetts Institute of Delft University of Technology, Delft, Kingdom Tankers Needed Santa Cruz, Moffett Field, CA J. Li, B. Sridhar, M. Xue, H. Ng, AvMet Applications, Inc., Reston, Technology, Lexington, MA; J. Thomas, The Netherlands R. Nangia, Nangia Aero Research NASA Ames Research Center, Moffett VA; R. Bass, Federal Aviation R. Hansman, Massachusetts Institute of Associates, Bristol, United Kingdom Field, CA Administration, Washington, D.C. Technology, Cambridge, MA Wednesday, 15 June 2016 186-ATIO.ATM-17 Data Mining in ATS II Fairchild West Chaired by: B. HOLGUIN, Federal Aviation Administration 1400 hrs 1430 hrs 1500 hrs 1530 hrs AIAA-2016-3447 AIAA-2016-3448 AIAA-2016-3449 AIAA-2016-3450 An Integrated Gate Turnaround Taxi-Out Time Prediction for Association Rules for Traffic Airport Gate Operation Management Concept Departures at Charlotte Airport Flow Management Decision Monitoring Using Computer Leveraging Big Data/ Using Machine Learning Support Vision Techniques Analytics for NAS Performance Techniques E. Vargo, C. Taylor, C. Wanke, MITRE H. Lu, S. Vaddi, V. Cheng, Optimal Improvements H. Lee, W. Malik, University of Corporation, McLean, VA Synthesis, Inc., Los Altos, CA W. Chung, SAIC, Moffett Field, CA California, Santa Cruz, Moffett Field, CA; Y. Jung, NASA Ames Research Center, Moffett Field, CA Wednesday, 15 June 2016 187-ATIO.GA-2 General Aviation Safety Gunston East Chaired by: T. DOWNEN, Gulfstream and A. PRZEKOP, NASA 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs AIAA-2016-3451 AIAA-2016-3452 AIAA-2016-3453 AIAA-2016-3454 AIAA-2016-3455 AIAA-2016-3456 AIAA-2016-3457 General Aviation Approach and Detecting Safety Events during Energy-Based Metrics for Comparing Hazardous States Integration of Affordable Designing an Automatic Beacon Aircraft Loss-Of-Control Recovery Landing Analysis using Flight Approach in General Aviation General Aviation Flight Data and Trigger Events in Fatal and Information Technology Ejection System for Aircraft Strategy Using High Order Sliding Data Records Operations Record Analysis Non-Fatal Helicopter Accidents Products into General Aviation L. Peters, RMIT University, Melbourne, Mode Control Based on Optimal T. Puranik, E. Harrison, S. Min, H. N. Fala, K. Marais, Purdue University, T. Puranik, E. Harrison, S. Min, H. A. Rao, K. Marais, Purdue University, Training and Research Australia Trim Condition Jimenez, D. Mavris, Georgia Institute West Lafayette, IN Jimenez, D. Mavris, Georgia Institute West Lafayette, IN V. Risukhin, Western Michigan W. Zhang, H. Chen, Beihang University, of Technology, Atlanta, GA of Technology, Atlanta, GA University, Battle Creek, MI Beijing, China Wednesday, 15 June 2016 99 188-ATIO.TFPC-8/ATIO. Transformational Flight - SCEPTOR Distributed Electric Propulsion X-Plane Columbia 1 FT-1/GEPC-2 Chaired by: A. GIBSON, Empirical Systems Aerospace and S. GINN, NASA AFRC 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs AIAA-2016-3458 Oral Presentation AIAA-2016-3459 Oral Presentation Oral Presentation AIAA-2016-3460 Oral Presentation Design and Performance of Comparison of Mixed- High-Lift Propeller System Analysis of Propeller Designs Cooling of electric motors used Design of an Electric Propulsion SCEPTOR Power System Design the NASA SCEPTOR Distributed Order Aero-Propulsive Configuration Selection for and Integration Strategies for propulsion on SCEPTOR System for SCEPTOR’s Outboard S. Clarke, NASA Armstrong Flight Electric Propulsion Flight Performance Predictions for NASA’s SCEPTOR Distributed During Conceptual Design via R. Christie, NASA Glenn Research Nacelle Research Center, Edwards, CA Demonstrator Distributed Electric Propulsion Electric Propulsion Flight Computational Fluid Dynamics Center, Cleveland, OH; A. Dubois, A. Dubois, M. van der Geest, J. Bevirt, N. Borer, M. Patterson, J. Viken, Configurations Demonstrator with Overset Grids Joby Aviation, Santa Cruz, CA; J. Joby Aviation, Santa Cruz, CA; R. Christie, M. Moore, NASA Langley Research N. Borer, M. Patterson, J. Derlaga, B. M. Patterson, J. Derlaga, N. Borer, J. Derlaga, N. Borer, M. Patterson, Derlaga, NASA Langley Research NASA Glenn Research Center, Cleveland, Center, Hampton, VA; J. Bevirt, A. Litherland, K. Deere, NASA Langley NASA Langley Research Center, M. Moore, NASA Langley Research Center, Hampton, VA OH; N. Borer, NASA Langley Research Stoll, Joby Aviation, Santa Cruz, Research Center, Hampton, VA; A. Hampton, VA Center, Hampton, VA Center, Hampton, VA; S. Clarke, NASA CA; et al. Stoll, Joby Aviation, Santa Cruz, CA Armstrong Flight Research Center, Edwards, CA Wednesday, 15 June 2016 189-F360-7 TTX Hot Wash and Cybersecurity Interactive Training Session International Ballroom 1400 - 1600 hrs (East) Following the TTX, teams will participate in a “hot wash” session that will review the TTX’s learning objectives and results. Participants will gain further instruction and insights when a panel of thought leaders in cybersecurity, risk management, threat assessment, and role-based training for cyber awareness engage in discussion and answer questions. The day promises to be both instructive and entertaining.

Moderator: David Shaw, Founder & CEO, Global Business Analysis (Moderator)

Panelists: Briguette Carstensen Barbara Endicott-Popovsky Faye Francy Ilanko Subramaniam Russell Syphert Vice President & Director of Research Professor, University of Washington Institute of Executive Director GBA CISO, President Senior Threat Analyst Global Business Analysis Technology & Executive Director The Aviation ISAC Global Business Analysis Global Business Analysis Center for Information Assurance and Cybersecurity Wednesday, 15 June 2016 190-FC-11 Crossflow Transition and Separation Columbia 11 Chaired by: L. PACK MELTON, NASA-Langley Research Center and D. BRZOZOWSKI, The Boeing Company 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs AIAA-2016-3461 AIAA-2016-3462 AIAA-2016-3463 AIAA-2016-3464 AIAA-2016-3465 AIAA-2016-3466 AIAA-2016-3467 Full-scale Flight Demonstration A Comparative Study of Hybrid Numerical Simulations of an Plasma-Based Control of The influence of the spatial Numerical Simulation of Sensitivity analysis of crossflow of an Active Flow Control Flow Control System Architectures Airplane with an Active Flow Excrescence-Generated frequency content of discrete a High-Lift Configuration boundary layer and transition Enhanced Vertical Tail for an A320 Aircraft Control System Transition on a Swept Wing roughness distributions on the Embedded with High delay using plasma actuator E. Whalen, The Boeing Company, M. Jabbal, S. Everett, Brunel University A. Shmilovich, Y. Yadlin, E. Whalen, D. Rizzetta, M. Visbal, Air Force development of the crossflow Momentum Fluidic Actuators Z. Wang, L. Wang, S. Fu, Tsinghua Hazelwood, MO; M. Spoor, P. Vijgen, London, Uxbridge, United Kingdom; G. The Boeing Company, Huntington Research Laboratory, Wright-Patterson instability V. Vatsa, NASA Langley Research University, Beijing, China J. Tran, The Boeing Company, Kalarikovilagam Srinivasan, German Beach, CA AFB, OH E. van Bokhorst, M. Placidi, C. Atkin, Center, Hampton, VA; B. Duda, E. Mukilteo, WA; A. Shmilovich, The Aerospace Center (DLR), Braunschweig, City University London, London, Fares, Exa GmbH, Munich, Germany; Boeing Company, Huntington Beach, Germany; S. Raghu, Advanced Fluidics, United Kingdom J. Lin, NASA Langley Research Center, CA; J. Lin, NASA Langley Research LLC, Columbia, MD Hampton, VA Center, Hampton, VA; et al. Wednesday, 15 June 2016 191-FD-39 Shock-Dominated Flows I Oak Lawn Chaired by: P. GNOFFO, NASA-Langley Research Center and V. NARAYANASWAMY, North Carolina State Univ 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2016-3468 AIAA-2016-3469 AIAA-2016-3470 AIAA-2016-3471 AIAA-2016-3472 AIAA-2016-3473 A highly temperature Experimental study of shock Oscillation Characteristics of Experimental Investigation of Large-Eddy Simulation of Experimental Research on sensitive and ultra-fast wave patterns over an airfoil the Shock Waves around a Interactions Between a Normal Shock Train in a Supersonic Flow Characteristics around response TSP (Temperature- A. Avelar, J. Falcao Filho, Aeronautics Supersonic Deceleration-Device Shock Wave and Various Turbulent Pipe Flow Combination of Forward jet Sensitive-Paints) for unsteady and Space Institute (IAE), São José Model with Aerospike Counter Flows Using Counter- S. Ghosh, S. Mahapatra, Indian and Spike aerothermodynamics on shock- dos Campos, Brazil; H. Leite, R. T. Mizukaki, Tokai University, Driver Shock Tube Institute of Technology Kharagpur, J. Zhang, H. Ma, Y. Qin, China Annes da Silva, Technological Institute Kharagpur, India 100 tube wall Hiratsuka, Japan; K. Yamada, Japan T. Tamba, M. Kayumi, H. Kawasaki, Academy of Aerospace Aerodynamics, H. Ozawa, Tokyo Metropolitan of Aeronautics (ITA), São José dos Aerospace Exploration Agency (JAXA), A. Iwakawa, A. Sasoh, Nagoya Beijing, China University, Hino, Japan Campos, Brazil; J. Hsu, Aeronautics Sagamihara, Japan University, Nagoya, Japan and Space Institute (IAE), São José dos Campos, Brazil Wednesday, 15 June 2016 192-FD-40 Turbulence Modeling - Validation and Applications Jay Chaired by: B. SMITH, Lockheed Martin Aeronautics 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs AIAA-2016-3474 AIAA-2016-3475 AIAA-2016-3476 AIAA-2016-3477 AIAA-2016-3478 The Effect of the DNS Data Verification and Validation of Reynolds-stress and triple- Computation of Turbulent Application of a Full Reynolds Averaging Time on the Accuracy the k-kL Turbulence Model in product models applied Flow in a Rotating Pipe using Stress Model to High Lift Flows of RANS-DNS Simulations FUN3D and CFL3D Codes to flows with rotation and the Elliptic Blending Reynolds E. Lee-Rausch, C. Rumsey, S. Poroseva, University of New Mexico, K. Abdol-Hamid, J. Carlson, C. curvature Stress Model NASA Langley Research Center, Albuquerque, Albuquerque, NM; E. Rumsey, NASA Langley Research M. Olsen, NASA Ames Research N. Ashton, University of Manchester, Hampton, VA; V. Togiti, B. Eisfeld, Jeyapaul, Missouri University of Science Center, Hampton, VA Center, Moffett Field, CA Manchester, United Kingdom; M. German Aerospace Center (DLR), and Technology, Rolla, MO; S. Murman, Stoellinger, University of Wyoming, Braunschweig, Germany NASA Ames Research Center, Moffett Laramie, Laramie, WY Field, CA; J. Colmenares, University of New Mexico, Albuquerque, Albuquerque, NM Wednesday, 15 June 2016 193-FD-41/FC-12 Wing Aerodynamics: Separation and Control Morgan Chaired by: D. WILLIAMS, Illinois Institute of Technology and K. TAIRA, Florida State University 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2016-3479 AIAA-2016-3480 AIAA-2016-3481 AIAA-2016-3482 AIAA-2016-3483 AIAA-2016-3484 Revisiting Conventional Flaps The effect of free-stream Numerical Simulation of Wing The effect of acoustic excitation Numerical Investigation on Control of Gortler vortices by at High Deflection-Rate: turbulence on the structure of Section Near Stall on the later stages of transition Flow Separation Control of Low means of staggered surface Separation Control laminar separation bubbles A. Gross, New Mexico State in a laminar separation bubble Reynolds Number Sinusoidal streaks M. Ol, A. Medina, Air Force Research M. Istvan, J. Kurelek, S. Yarusevych, University, Las Cruces, NM; J. Little, J. Kurelek, S. Yarusevych, University Aerofoils A. Sescu, L. Taoudi, Mississippi State Laboratory, Wright-Patterson AFB, University of Waterloo, Waterloo, H. Fasel, University of Arizona, of Waterloo, Waterloo, Canada J. Joy, Nanyang Technological University, University, Starkville, MS; M. Afsar, OH; P. Mancini, A. Jones, University Canada Tucson, Tucson, AZ Singapore, Singapore; I. Ibrahim, Imperial College London, London, of Maryland, College Park, College University of Glasgow, Glasgow, United United Kingdom; D. Thompson, Park, MD Kingdom; T. New, Nanyang Technological Mississippi State University, University, Singapore, Singapore Starkville, MS Wednesday, 15 June 2016 194-FD-42 High-Speed Boundary-Layer Transition II Lincoln East Chaired by: T. JULIANO, University of Notre Dame and J. JEWELL, Air Force Research Laboratory 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2016-3485 AIAA-2016-3486 AIAA-2016-3487 AIAA-2016-3488 AIAA-2016-3489 AIAA-2016-3490 Characterizing the Transient Direct Numerical Simulations Transition Route of Klebanoff Secondary instabilities of Effects of Vibrational Nonlinear Transient Growth Growth Mechanism on a of Transitional Boundary Layer Type in Hypersonic Boundary Görtler vortices in high-speed Relaxation and Dissociation on and Boundary Layer Transition Hypersonic Blunt Body at a over a Flat Plate in Hypersonic Layers boundary layer flows Hypersonic Boundary-Layer P. Paredes, M. Choudhari, F. Li, High Angle of Attack Free-Stream X. Wu, Imperial College London, J. Ren, S. Fu, Tsinghua University, Stability NASA Langley Research Center, E. Reshotko, Case Western Reserve A. Novikov, Moscow Institute of London, United Kingdom; J. Luo, Beijing, China X. Wang, E. Josyula, Air Force Hampton, VA University, Cleveland, OH; A. Leidy, Physics and Technology (MIPT), Tianjin University, Tianjin, China Research Laboratory, Wright-Patterson

101 F. Siddiqui, R. Bowersox, Texas A&M Zhukovsky, Russia; I. Egorov, Central AFB, OH University, College Station, TX Aerohydrodynamic Institute (TsAGI), Zhukovsky, Russia Wednesday, 15 June 2016 195-FD-43 Combustion Simulation II Monroe Chaired by: J. EDWARDS and O. SAMIMI ABIANEH, Georgia Southern University 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs AIAA-2016-3492 AIAA-2016-3493 AIAA-2016-3494 AIAA-2016-3495 AIAA-2016-3496 Improved 4D Data Assimilation RANS Modeling and Numerical Simulation of Liquid CFD simulations of acoustic and A comparison study of for Large-Eddy Simulation Uncertainty Quantification of Kerosene Combustion in a thermoacoustic phenomena in predicted pressure-based of High-Speed Turbulent Supersonic Reacting Flows in a Dual-Mode Scramjet Combustor internal flows ignition delay time of Combustion Scramjet Combustor Using Flamelet/Progress E. Gonzalez, Combustion Science & n-dodecane fuel using various J. Edwards, C. Patton, T. Wignall, N. Arnold-Medabalimi, K. Duraisamy, Variable Approach Engineering, Inc., Columbia, MD skeletal kinetic mechanisms T. Echekki, North Carolina State University of Michigan, Ann Arbor, J. Niu, Y. Piao, Tsinghua University, O. Samimi Abianeh, Georgia Southern University, Raleigh, NC Ann Arbor, MI Beijing, China University, Statesboro, GA Wednesday, 15 June 2016 196-FD-44 Solver Techniques II Columbia 10 Chaired by: T. ECONOMON, Stanford University 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs AIAA-2016-3497 AIAA-2016-3498 AIAA-2016-3499 AIAA-2016-3500 AIAA-2016-3501 AIAA-2016-3502 AIAA-2016-3503 A Fast Differential Deficit Stability Analysis of Dual-time Application of Nonlinear Krylov Multi-GPU, Implicit Time Robust uniform time sampling Preconditioned pseudo- Parallelization of the flow and Control Volume Approach for Stepping Acceleration to a Reconstructed Stepping for High-order approach for the harmonic compressibility methods transport code ADVED_NS Modeling Turbine-Turbine J. Chiew, Stanford University, Discontinuous Galerkin Method Methods on Unstructured Grids balance method for Three-dimensional using the MPI porting library, Interactions Stanford, CA; T. Pulliam, NASA Ames for Compressible Flows J. Watkins, J. Romero, A. Jameson, S. Nimmagadda, T. Economon, J. incompressible Navier-Stokes UGLIB M. DiPaola, D. Willis, University of Research Center, Moffett Field, CA C. Wang, North Carolina State University, Stanford University, Stanford, CA Alonso, C. Ilario da Silva, Stanford equations Y. Khine, Engility Corporation, Massachusetts, Lowell, Lowell, MA Raleigh, NC; J. Cheng, Beihang University, Stanford, CA Z. Qian, Aviation Industry Corporation Chantilly, VA; R. Rosenberg, University, Beijing, China; M. Berndt, N. of China (AVIC), Beijing, China W. Szymczak, Naval Research Carlson, Los Alamos National Laboratory, Laboratory, Washington, D.C. Los Alamos, NM; H. Luo, North Carolina State University, Raleigh, NC Wednesday, 15 June 2016 197-FD-45 Novel CFD Algorithms Jefferson East Chaired by: A. MAZAHERI, NASA-Langley Research Center and S. KARMAN, Pointwise, Inc. 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs AIAA-2016-3504 AIAA-2016-3505 AIAA-2016-3506 AIAA-2016-3507 AIAA-2016-3508 AIAA-2016-3509 AIAA-2016-3510 Third-Order Inviscid and Hyperbolic Method for Simultaneous Approximation hp-Spectral Hull: A Minimum Development of A Multiscale A Rotating Reference Frame, Convergence Acceleration Second-Order Hyperbolic Dispersive PDEs: Same High- Terms for Multidimensional Degree of Freedom Enforcing Flow Solver Using Wavelet Integral Boundary Layer Based on Eigenvalue Analysis Navier-Stokes Schemes for Order of Accuracy for Solution, Summation-by-parts Operators Spectral Element Method Decomposition for Error Method S. Eyi, Middle East Technical Three-Dimensional Inviscid and Gradient, and Hessian J. Hicken, Rensselaer Polytechnic For Nonlinear Conservation Control, Grid Adaptation, and M. DiPaola, D. Willis, University of University, Ankara, Turkey Viscous Flows A. Mazaheri, NASA Langley Research Institute, Troy, NY; D. Del Rey Laws with Application to Flow Data Compression Massachusetts, Lowell, Lowell, MA

102 Y. Liu, H. Nishikawa, National Center, Hampton, VA; M. Ricchiuto, Fernández, D. Zingg, University of Compressible Fluid Flow P. Anusonti-Inthra, University of Institute of Aerospace, Hampton, VA French National Institute for Research Toronto, Toronto, Canada A. Ghasemi, L. Taylor, J. Newman, Tennessee, Tullahoma, Tullahoma, TN in Computer Science and Control University of Tennessee, Chattanooga, (INRIA), Bordeaux, France; H. Chattanooga, TN Nishikawa, National Institute of Aerospace, Hampton, VA Wednesday, 15 June 2016 198-FT-3/GT-5 Correlation of Ground and Flight Test Data DuPont Chaired by: B. MILLS, AEDC/ ATA and W. SCHUMAN 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs AIAA-2016-3511 AIAA-2016-3512 AIAA-2016-3513 AIAA-2016-3514 AIAA-2016-3515 Flight Simulation Training Device Hardware in the Loop Design of Experiments Aerodynamic Characterization of Investigation on correlation Qualification for Suborbital Simulation for Micro Air Enhanced Statistical Process an Off-the-Shelf Aircraft via Flight between wind tunnel and flight Spaceflight Simulator Vehicles Control for Wind Tunnel Check Test and Numerical Simulation test data for boundary layer E. Seedhouse, Embry-Riddle Aeronautical E. Ozger, T. Drouven, Ingolstadt Standard Testing M. Bronz, G. Hattenberger, French Civil transition University, Daytona Beach, FL University of Applied Sciences, B. Phillips, D. Landman, Old Aviation University, Toulouse, France Z. Liu, W. Yang, Q. Shen, China Ingolstadt, Germany Dominion University, Norfolk, VA Academy of Aerospace Aerodynamics, Beijing, China Wednesday, 15 June 2016 199-GT-6 Employing CFD in Parallel with Ground Testing Lincoln West Chaired by: R. KUMAR, Florida State University and R. RHEW, NASA-Langley Research Center 1400 hrs 1430 hrs 1500 hrs AIAA-2016-3516 AIAA-2016-3517 AIAA-2016-3518 An Application of CFD to Guide A Compressible Mixing Layer CFD Simulations for Arc-Jet Forced Boundary-Layer Transition Facility for CFD Validation Panel Testing Capability for Low-Speed Tests of a Hybrid Measurements Development Using Semi- Wing-Body Configuration G. Lee, K. Kim, B. Johnson, G. Elliott, Elliptical Nozzles J. Luckring, K. Deere, NASA Langley J. Dutton, University of Illinois, T. Gokcen, Analytical Mechanics Research Center, Hampton, VA; R. Childs, Urbana-Champaign, Urbana, IL Associates, Inc., Moffett Field, CA; J. P. Stremel, Science and Technology Balboni, NASA Ames Research Center, Corporation, Moffett Field, CA; K. Long, Moffett Field, CA; G. Hartman, NASA Ames Research Center, Moffett Jacobs, Moffett Field, CA Field, CA Wednesday, 15 June 2016 200-ITAR-4 NASA Orion EFT-1 Aeroscience Results - Aerothermal I Cabinet Chaired by: J. OLEJNICZAK, NASA Ames Research Center and A. BRANDIS, AMA Inc at NASA Ames 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs 1730 hrs AIAA-2016-3519 AIAA-2016-3520 AIAA-2016-3521 AIAA-2016-3522 AIAA-2016-3523 AIAA-2016-3524 AIAA-2016-3525 AIAA-2016-3526 Overview of the NASA Orion Orion-MPCV EFT-1 Heatshield Aerothermal Exploration Flight Test 1 Orion Crew Module and Orion EFT-1 FADS-Based Reconstruction of the Orion Quiet Hubless Ducted Fan Exploration Flight Test-1 Aerothermodynamic Database Environment Reconstruction Afterbody Aerothermal Parachute System Aerodynamic Trajectory Reconstruction Crew Module Aerodynamics for Hybrid Propulsion Reentry from an Aerosciences Design Methodology B. Oliver, A. Amar, NASA Johnson Environment Reconstruction Modeling K. Bibb, NASA Langley Research the EFT-1 Flight Test S. Wilson III, Self, Bethesda, MD; Perspective A. Cassady, NASA Johnson Space Space Center, Houston, TX; J. Droba, A. Hyatt, B. Oliver, A. Amar, NASA D. Owens, NASA Langley Research Center, Hampton, VA; L. Cassady, K. Bibb, NASA Langley Research B. Bialczak, Self, Vertrees, KY; T. J. Olejniczak, NASA Ames Research Center, Houston, TX HX5, Houston, TX; V. Lessarad, NASA Johnson Space Center, Houston, TX; Center, Hampton, VA; L. Cassady, A. Schwing, NASA Johnson Space Center, Hampton, VA; P. Robinson, L. Streett, Self, Louisville, KY Langley Research Center, Hampton, Center, Houston, TX 103 Center, Moffett Field, CA V. Lessarad, NASA Langley Research J. Powell, P. Stuart, NASA Johnson Cassady, NASA Johnson Space Center, VA; M. Mahzari, Analytical Mechanics Center, Hampton, VA Space Center, Houston, TX Houston, TX Associates, Inc., Moffett Field, CA Wednesday, 15 June 2016 201-MAO-11 Structural Optimization I Columbia 3 Chaired by: J. HICKEN, Rensselaer Polytechnic Institute and B. STANFORD, NASA Langley Research Center 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs AIAA-2016-3527 AIAA-2016-3528 AIAA-2016-3529 AIAA-2016-3530 AIAA-2016-3531 A Robust Analytical Sensitivity Analysis and Sensitivity Aeroservoelastic Optimization Active Aeroelastic Alteration Wing Aerostructural Analysis for Weakly Coupled Calculation using High Fidelity of Wing Structure Using to Reduce Off-Design Induced Optimization Using the Aero-Structural Systems Spectral Formulation-Based FSI Curvilinear Spars and Ribs Drag Individual Discipline Feasible K. Gobal, R. Grandhi, Wright State and Coupled Adjoint Method (SpaRibs) J. Lin, Control Research Corporation, Strategy University, Dayton, OH R. Prasad, H. Kim, D. Im, S. Choi, J. Robinson, S. Doyle, G. Ogawa, M. Lexington, MA J. Hoogervorst, A. Elham, Delft Virginia Polytechnic Institute and State Baker, M4 Engineering, Inc., Long University of Technology, Delft, The University, Blacksburg, VA; S. Yi, Korea Beach, CA; S. De, M. Jrad, Virginia Netherlands Advanced Institute of Science and Polytechnic Institute and State Technology, Daejeon, South Korea University, Blacksburg, VA; et al. Wednesday, 15 June 2016 202-MAO-12 Surrogate Modeling and Non-Deterministic Design - Methods and Applications I Cardozo Chaired by: V. TOROPOV, Queen Mary, University of London and S. CHOWDHURY, University at Buffalo 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2016-3532 AIAA-2016-3533 AIAA-2016-3534 AIAA-2016-3535 AIAA-2016-3536 AIAA-2016-3537 Reducing Large Viking I Based Uncertainty Quantification of Integrating Aerodynamic Adding Flight Mechanics to Flight Improvement of efficient global A sequential sampling strategy Martian Entry, Descent and Material Mechanical Properties Uncertainty into Aircraft Loads Surrogate Model using optimization with application to for Kriging metamodel based Landing Response Surface Using Surrogate Models Maneuvers During Conceptual Multi-Output Gaussian Processes aircraft wing design on Delaunay triangulation and Methodology Produced Quadratic C. Smith, B. Lapp, M. Glavicic, Rolls- Design A. Chiplunkar, Airbus, Toulouse, France; N. Bartoli, ONERA, Toulouse, France; M. TOPSIS Models Royce Group plc, Indianapolis, IN A. Wendorff, J. Alonso, Stanford E. Rachelson, University of Toulouse, Bouhlel, Safran Group, Paris, France; I. P. Jiang, Y. Zhang, Q. Zhou, L. Shu, N. Norman, Embry-Riddle Aeronautical University, Stanford, CA; S. Toulouse, France; M. Colombo, Airbus, Kurek, R. Lafage, T. Lefebvre, ONERA, State Key Laboratory of Digital University, Daytona Beach, FL; S. Smith, Bieniawski, B. Whitehead, The Toulouse, France; J. Morlier, Higher Toulouse, France; J. Morlier, University of Manufacturing Equipment and Howard University, Washington, D.C. Boeing Company, Seattle, WA Institute of Aeronautics and Space, Toulouse, Toulouse, France Technology, Wuhan, China Toulouse, France Wednesday, 15 June 2016 203-MST-10 Model and Simulation Integration Georgetown East Chaired by: R. RUFF and D. GINGRAS, Bihrle Applied Research Inc. 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2016-3538 AIAA-2016-3539 AIAA-2016-3540 AIAA-2016-3541 AIAA-2016-3542 AIAA-2016-3543 A simulating method of Automated Model Integration Ontology-Driven Metamodel Development of a Physics- Multi-fidelity Geometry-centric Establishment of a C4ISR dynamic inter-connection Workflow for Supporting Pilot- Validation in Cyber-Physical Based Weight (PBWeight) Multi-disciplinary Analysis for Interoperability Prototyping between models in-the-Loop Testing in Model- Systems Prediction Tool for Conceptual Design and LVC Environment R. Hong, Z. Xiong, Q. Zhou, Aviation Based Rotorcraft Design D. Larkin, K. Lynch, G. Ball, Raytheon Design R. Haimes, Massachusetts Institute A. Coyle, The Boeing Company, Industry Corporation of China (AVIC), U. Durak, T. Gerlach, German Company, Tucson, AZ; K. Collins, T. Winter, J. Marquez, B. Scheneman, of Technology, Cambridge, MA; J. Washington, D.C. Shanghai, China Aerospace Center (DLR), M. Schmit, Georgia Institute of M4 Engineering, Inc., Long Beach, CA Dannenhoffer, Syracuse University, Technology, Atlanta, GA; T. Bapty, Syracuse, NY; N. Bhagat, Wright

104 Braunschweig, Germany; A. Ozturk, V. Kargin, H. Aydemir, U. Zengin, MetaMorph, Nashville, TN; et al. State Research Institute, Beavercreek, Turkish Aerospace Industries, Inc., OH; D. Allison, Optimal Flight Ankara, Turkey Sciences, LLC, Dayton, OH Wednesday, 15 June 2016 204-MST-11 Modeling and Simulation of Aeroelasticity II Piscataway Chaired by: T. BURRESS, Lockheed Martin and A. ELMILIGUI, NASA Langley Research Center 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs AIAA-2016-3544 AIAA-2016-3545 AIAA-2016-3546 AIAA-2016-3547 AIAA-2016-3548 Aeroelastic Analysis and Balancing the Efﬁciency Frequency Domain Approach Improved Servoelastic Tracking Control System Design Ground Vibration Testing of and Stability of the Coupled for Transonic Unsteady Response Prediction Models For for Roll Maneuver via Active Ultra-WideBand Ice Radar Dynamics and Aerodynamics of Aerodynamic Modelling applied Aircraft Using MultiObjective Wings Using Macro Fiber Installations on the Basler a Flapping Flyer to a 3D Wing Optimization Techniques Composites BT-67 J. Bluman, C. Kang, University of A. Poncet-Montanges, J. Cooper, D. P. Srinivasan, Aeronautical X. Wang, Dalian University of W. Liu, Design, Analysis and Research Alabama, Huntsville, Huntsville, AL Jones, A. Gaitonde, University of Development Agency, Bengaluru, Technology, Dalian, China; W. Zhou, Z. Corporation, Lawrence, KS; M. Bristol, Bristol, United Kingdom; Y. India; A. Joshi, Indian Institute of Wu, State Key Laboratory of Structural Ewing, R. Hale, University of Kansas, Lemmens, Siemens, Leuven, Belgium Technology Bombay, Mumbai, India Analysis for Industrial Equipment, Dalian, Lawrence, Lawrence, KS China; J. Xing, Dalian University of Technology, Dalian, China Wednesday, 15 June 2016 205-PDL-5/FC-13 DBD Actuators Gunston West Chaired by: D. ASHPIS, NASA Glenn Research Center and S. ROY, University of Florida 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs AIAA-2016-3549 AIAA-2016-3550 AIAA-2016-3551 AIAA-2016-3552 AIAA-2016-3553 AIAA-2016-3554 AIAA-2016-3555 Characterization of DBD Basic Study on the Voltage Simulation of Body Force New Frequency Dependent Experimental Investigation of Optimization of Dielectric Experimental Study of Anti- Plasma Actuators Performance Characteristic of Dual- Effect on Steady and Unsteady Capacitance Based SDBD Plasma Dynamic Stall in a Wide Range Barrier Discharge Plasma icing and Deicing on a Cylinder without External Flow – Part Grounded Tri–Electrode Plasma Flow Induced by DBD Plasma Model for Direct Simulation of 2D of Mach Numbers by Plasma Actuators for Conical-Forebody by DBD plasma actuation I: Thrust-Voltage Quadratic Actuator by Plasma Simulation Actuator Navier-Stokes Equation Actuators with Combined Flow Control X. Meng, J. Cai, Y. Tian, X. Han, D. Relationship in Logarithmic A. Nakano, H. Nishida, Tokyo B. Wu, University of California, Irvine, T. Sengupta, Indian Institute of Energy/Momentum Action H. Hu, H. Li, X. Meng, X. Yan, Zhang, Northwestern Polytechnical Space for Sinusoidal Excitation University of Agriculture and Irvine, CA; C. Gao, Northwestern Technology Kanpur, Kanpur, India; A. Starikovskiy, Princeton University, Northwestern Polytechnical University, University, Xi’an, China D. Ashpis, NASA Glenn Research Technology, Koganei, Japan Polytechnical University, Xi’an, S. Sengupta, Ohio State University, Princeton, NJ Xi’an, China; F. Liu, S. Luo, University Center, Cleveland, OH; M. Laun, HX5 China; F. Liu, J. Xiong, University of Columbus, OH; P. Bagade, Indian of California, Irvine, Irvine, CA Sierra LLC, Glenn Research Center, California, Irvine, Irvine, CA Institute of Technology Kanpur, Kanpur, Cleveland, OH India Wednesday, 15 June 2016 206-TP-8 Advanced Modeling II - Hypersonic Flows Jefferson West Chaired by: M. PANESI, University of Illinois at Urbana Champaign 1400 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs Oral Presentation AIAA-2016-3556 AIAA-2016-3557 AIAA-2016-3558 AIAA-2016-3559 AIAA-2016-3560 Hypersonics Then and Now (Invited) Vibrational relaxation and Radiative Gas Dynamics of Thermochemical Nonequilibrium Numerical Model Development SPARK: A Software Package for J. Anderson, Smithsonian Institution, National Air and Space Museum, dissociation in O2-O mixtures Apollo Command Modules at Modeling for Hypersonic Flows for Thermochemical Aerodynamics, Radiation and Washington, D.C. D. Andrienko, I. Boyd, University of Angles of Attack Containing Oxygen Nonequilibrium in Hypersonic Kinetics Michigan, Ann Arbor, Ann Arbor, MI S. Surzhikov, Russian Academy of K. Neitzel, D. Andrienko, I. Boyd, Flows B. Lopez, M. Lino Da Silva, Technical Sciences, Moscow, Russia University of Michigan, Ann Arbor, Ann J. Burt, E. Josyula, Air Force Research University of Lisbon, Lisbon, Portugal

105 Arbor, MI Laboratory, Wright-Patterson AFB, OH Wednesday, 15 June 2016 207-NW-6 Networking Coffee Break Columbia 1600 - 1630 hrs 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. Wednesday, 15 June 2016 208-LEC-4 Thermophysics Award Lecture Lincoln West 1730 - 1830 hrs Measurement of Thermophysical Properties from 4 to 4,000K George Cunnington CEO Cunnington and Associates Wednesday, 15 June 2016 209-LEC-5 Multidisciplinary Analysis and Optimization Award Lecture International Ballroom 1730 - 1830 hrs (East) A 30-Year Retrospective of Structural and Multidisciplinary Optimization Robert (Bob) A. Canfield Professor & Assistant Department Head for Academic Affairs Virginia Polytechnic Institute and State University Wednesday, 15 June 2016 210-FD-46 Transition Open Forum Cardozo 1830 - 2200 hrs Thursday Thursday, 16 June 2016 211-SB-4 Speakers’ Briefing Session Rooms 0730 - 0800 hrs 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 session to exchange bios and review final details prior to the session. Please attend on the day of your session. Thursday, 16 June 2016 212-PLNRY-5 Plenary International Ballroom 0800 - 0900 hrs (Center) The Ascent of (Un)manned John S. Langford Chairman and Chief Executive Officer Aurora Flight Sciences Corporation Thursday, 16 June 2016 213-NW-7 Networking Coffee Break Meeting Room Foyers 0900 - 0930 hrs 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. Thursday, 16 June 2016 214-WKSP-1 Drag Prediction Workshop Lincoln West 0930 - 1715 hrs Agenda: 0930 – 1130 hrs Sessions 1, 2 The focus of this workshop will be the NASA Common Research Model (CRM) with wind-tunnel measured wing twist; both wing-body and wing-body-pylon-nacelle configurations will be considered. CFD 106 predictions of absolute and incremental force and moment values will be examined and compared. The workshop will include grid convergence and code verification studies. Additionally, an angle-of-attack 1130 – 1300 hrs Break for Lunch sweep with static aero-elastic deformations will be considered. Grids will be made available for all required cases. 1300 – 1715 hrs Session 3, 4, 5 Optionally, participants are invited to perform solution-adaptation calculations and/or a coupled aero-structural simulation of the CRM wing-body configuration. A finite element model will be made available to participants to calculate twist/deflection due to aerodynamic load.

Thursday, 16 June 2016 215-AMT-8 Volumetric Measurement Techniques Columbia 2 Chaired by: P. DANEHY, NASA Langley Research Center and W. KULATILAKA, Texas A & M University 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2016-3561 AIAA-2016-3562 AIAA-2016-3563 AIAA-2016-3564 AIAA-2016-3565 20 kHz 3D measurements in High-speed three-dimensional Single-Shot 3D Flame Imaging Volumetric Measurement of a 5 kHz VLIF (Volumetric a Mach 2 combustor based on tomographic measurements for Using CH-Based VLIF (Volumetric Shock Wave-Turbulent Boundary Laser Induced Fluoresence) tomographic chemiluminescence combustion systems Laser Induced Fluorescence) Layer Interaction Using Plenoptic Measurements in Turbulent Q. Lei, Y. Wu, L. Ma, Virginia Polytechnic B. Halls, J. Gord, Air Force Research L. Ma, W. Xu, Q. Lei, J. Ikeda, Virginia Particle Image Velocimetry Flows Seeded with Iodine Institute and State University, Blacksburg, Laboratory, Wright-Patterson AFB, OH; Polytechnic Institute and State University, J. Bolton, B. Thurow, Auburn University, Y. Wu, Q. Lei, W. Xu, L. Ma, Virginia VA; T. Ombrello, C. Carter, Air Force N. Jiang, M. Splichenko, S. Roy, Spectral Blacksburg, VA; C. Carter, Air Force Auburn, AL; F. Alvi, N. Arora, Florida State Polytechnic Institute and State Research Laboratory, Wright-Patterson Energies, LLC, Dayton, OH; T. Meyer, Research Laboratory, Wright-Patterson University, Tallahassee, FL University, Blacksburg, VA AFB, OH Purdue University, West Lafayette, IN AFB, OH Thursday, 16 June 2016 216-AMT-9 MEMS and Novel Surface Sensors Oak Lawn Chaired by: C. GOYNE, University of Virginia and H. HU, Iowa State University 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2016-3566 AIAA-2016-3567 AIAA-2016-3568 AIAA-2016-3569 AIAA-2016-3570 A New Skin Friction Gauge Study on Effect of Thickness Testing of a New Type of MEMS Study on delta wing skin Development of a High- B. Kinkade, A. Sullivan, Northrop Simpliﬁcation on High Thermal Shear-Stress Sensor friction measurement based Resolution, Fast Pressure and Grumman Corporation, Redondo Frequency Measurement of J. Weiss, Q. Schwaab, University of on liquid crystal coatings in Strain Measurement System for Beach, CA; R. Westphal, J. Gerhardt, Thin-Film Heat Flux Gauge Québec, Montréal, Canada; A. Giani, hypersonic wind tunnel Unsteady Supersonic Testing California Polytechnic State University, X. Xu, Q. Zhao, W. Luo, F. Tang, J. C. Guigue, P. Combette, B. Charlot, X. Chen, S. Wen, J. Pan, D. Yao, A. Wrist, J. Hubner, University of San Luis Obispo, CA Li, Chinese Academy of Sciences, University of Montpellier, Montpellier, China Academy of Aerospace Alabama, Tuscaloosa, Tuscaloosa, Beijing, China France Aerodynamics, Beijing, China AL; J. Crafton, Innovative Scientiﬁc Solutions, Inc., Dayton, OH Thursday, 16 June 2016 217-APA-29 Aerodynamic Design Methodologies II Albright Chaired by: J. GUGLIELMO, Boeing Defense, Space & Security and C. PASILIAO, AFRL/RWWV 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2016-3571 AIAA-2016-3572 AIAA-2016-3573 AIAA-2016-3574 AIAA-2016-3575 AIAA-2016-3576 Analysis of the Aerodynamic A Genetic Algorithm Variable-Fidelity Multidisciplinary Transonic Aerodynamics Research on the Parameters Trajectory and Aerodynamic Performance of a Morphing Optimization Method Design Optimization for Innovative Analysis for Multidisciplinary Optimization of Combination of Control Optimization of Civil Wing-Tip Demonstrator Using a for a Morphing Wing Tip Control Surface of Tailless Aircraft Design Optimization Spike and Forward-facing Jet Aircraft Descent Under Hazard Novel Nonlinear Vortex Lattice Demonstrator Validated Using J. Park, Virginia Polytechnic Institute and Applications J. Zhang, H. Ma, Y. Qin, China Situations Based on High- Method Infra Red Experimental Data State University, Blacksburg, VA; Y. Jo, S. Yi, M. Segee, J. Schetz, R. Kapania, Academy of Aerospace Aerodynamics, Fidelity Aerodynamic Database. S. Oliviu, A. Koreanschi, R. Botez, A. Koreanschi, S. Oliviu, J. Acotto, Korea Institute of Science and Technology, Virginia Polytechnic Institute and Beijing, China N. Othman, M. Kanazaki, Tokyo University of Québec, Montréal, R. Botez, University of Québec, Daejeon, South Korea; J. Choi, P. Raj, S. State University, Blacksburg, VA Metropolitan University, Hino, Japan

107 Canada; M. Mamou, Y. Mebarki, Montréal, Canada; M. Mamou, Y. Choi, Virginia Polytechnic Institute and State National Research Council Canada, Mebarki, National Research Council University, Blacksburg, VA Ottawa, Canada Canada, Ottawa, Canada Thursday, 16 June 2016 218-APA-30 Aerodynamic - Structural Dynamics Interactions II Northwest Chaired by: D. O’BRIEN, US Army RDECOM and P. ANSELL, University of Illinois at Urbana-Champaign 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2016-3577 AIAA-2016-3578 AIAA-2016-3579 AIAA-2016-3580 AIAA-2016-3581 AIAA-2016-3582 Aerodynamic Study of a Aerodynamic Excitation on Unsteady Pressure Measurement Steady Reynolds Averaged Delayed Detached Eddy Validation of a Turbulent Pusher-Propeller effects on a MLG Door Exposed to Vortices of Transonic Buffet on NASA Navier Stokes Equation-Based Simulation of Supersonic Panel Boundary Layer Pressure simple flap Emanating from NLG of an Common Research Model Buffet Loads Estimation Aeroelasticity Using Fully Coupled Fluctuation Model for S. Algozino, J. Marañon, J. Delnero, Aircraft Model S. Koike, M. Ueno, K. Nakakita, A. T. Chyczewski, Northrop Grumman Fluid Structure Interaction with Hypersonic Flow over a Cone I. Echapresto Garay, National S. Peng, A. Jirasek, M. Dalenbring, P. Hashimoto, Japan Aerospace Exploration Corporation, Melbourne, FL High Order Schemes J. Smith, M. Mesh, L. DeChant, K. University of La Plata, La Plata, Eliasson, Swedish Defense Research Agency (JAXA), Chofu, Japan J. Gan, G. Zha, University of Miami, Casper, R. Field, Sandia National Argentina Agency (FOI), Stockholm, Sweden Miami, FL Laboratories, Albuquerque, NM Thursday, 16 June 2016 219-APA-32 Low Boom Activities I Jefferson West Chaired by: L. BANGERT, NASA Langley Research Center and D. FINLEY, Lockheed Martin Aeronautics 0930 hrs 1000 hrs 1030 hrs AIAA-2016-3583 AIAA-2016-3584 AIAA-2016-3585 Near-Field Measurement of The Research of Supersonic Inlet Trade Study for a Low Post-Shock Pressure Modulation Aircraft Low Sonic Boom Boom Aircraft Demonstrator Induced by Supersonic Flight Configuration Design and C. Heath, J. Slater, NASA Glenn Model past a Grid Turbulence Optimizations Research Center, Cleveland, OH; S. A. Sasoh, A. Iwakawa, D. Furukawa, Y. X. Hao, C. Su, J. Zhou, China Rallabhandi, National Institute of Aoki, Nagoya University, Nagoya, Japan Academy of Aerospace Aerodynamics, Aerospace, Hampton, VA Beijing, China Thursday, 16 June 2016 220-ASE-13 Icing Instrumentation and Test Facilities Columbia 12 Chaired by: K. AL-KHALIL, Cox & Company, Inc. and D. ORCHARD, National Research Council Canada 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2016-3586 AIAA-2016-3587 AIAA-2016-3588 AIAA-2016-3589 AIAA-2016-3590 An Assessment of the Icing Development and Validation of Simulating natural ice crystal Simulating the Behavior of Vibrating-Wire, Supercooled Blade and the SEA Multi- Compact Isokinetic Total Water cloud conditions for icing wind Droplets entrained into the Liquid Water Content Element Sensor for Liquid Content Probe for Wind Tunnel tunnel experiments - A review Wake Flow of Spray Bar Sensor Calibration and Water Content Calibration of Characterization on the design, commissioning H. Tang, S. Chang, Beihang Characterization Progress the NASA GRC Icing Research C. Davison, M. Benner, C. Landreville, and calibration of the TU University, Beijing, China; Z. Cheng, M. King, NASA Glenn Research Tunnel D. Fuleki, National Research Council Braunschweig ice crystal Aircraft Strength Research Institute of Center, Cleveland, OH; J. Bognar, D. L. Steen, R. Ide, HX5, Cleveland, OH; Canada, Ottawa, Canada generation system China, Xi’an, China Guest, Anasphere, Inc., Belgrade, MT J. Van Zante, NASA Glenn Research A. Baumert, S. Bansmer, S. Sattler, Center, Cleveland, OH Technical University of Braunschweig, Braunschweig, Germany; H. Pervier, Cranfield University, Cranfield, United Kingdom; B. Esposito, Italian Aerospace Research Center (CIRA), Capua, Italy Thursday, 16 June 2016 221-ASE-14 HAIC/HIWC 2014 Darwin and 2015 Cayenne Flight Campaigns Update I Georgetown West Chaired by: M. WADEL, NASA Glenn Research Center and F. DEZITTER, Airbus Operations S.A.S 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2016-3591 Oral Presentation AIAA-2016-3592 AIAA-2016-3593 AIAA-2016-3594 HAIC/HIWC field campaigns - An Update on the Assessment Description and Results Isokinetic TWC Evaporator Isokinetic TWC Evaporator Specific findings on ice crystals of Appendix D/P Total for a Simple Ice Crystal Probe: Development of the Probe: Calculations and

108 characteristics in high ice water Water Content from In-Situ Detection System for Airborne IKP2 and Performance Testing Systemic Error Analysis content cloud regions Measurements of Deep Applications for the HAIC-HIWC Darwin C. Davison, National Research D. Leroy, P. Coutris, F. Emmanuel, A. Convective Clouds: Measurements L. Lilie, C. Sivo, D. Bouley, Science 2014 and Cayenne Field Council Canada, Ottawa, Canada; J. Schwarzenboeck, National Center for from Two HAIC-HIWC Flight Engineering Associates, Tolland, CT Campaigns Strapp, Met Analytics, Inc., Toronto, Scientific Research (CNRS), Clermont Campaigns J. Strapp, Met Analytics, Inc., Aurora, Canada; L. Lilie, Science Engineering Ferrand, France; J. Strapp, Met J. Strapp, Met Analytics, Inc., Aurora, Canada; L. Lilie, Science Engineering Associates, Mansfield Hollow, CT; Analytics, Inc., Toronto, Canada; L. Canada; A. Schwarzenboeck, National Associates, Mansfield Center, CT; T. Ratvasky, NASA Glenn Research Lilie, Science Engineering Associates, Center for Scientific Research (CNRS), T. Ratvasky, NASA Glenn Research Center, Cleveland, OH; C. Dumont, Mansfield Center, CT; et al. Clermont Ferrand, France; J. Delanoe, Center, Cleveland, OH; C. Davison, Federal Aviation Administration, National Center for Scientific Research National Research Council Canada, Atlantic City, NJ (CNRS), Paris, France; F. Dezitter, Ottawa, Canada; C. Dumont, Federal Airbus, Toulouse, France; C. Dumont, Aviation Administration, Atlantic Federal Aviation Administration, Atlantic City, NJ City, NJ; A. Grandin, Airbus, Toulouse, France; et al. Thursday, 16 June 2016 222-ATIO.ACD-7/ATIO. Unconventional, Innovative, and Transformative Concepts Gunston East TFPC-9 Chaired by: E. DIGIROLAMO, Lockheed Martin Aeronautics and D. HALL, DHC Engineering 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2016-3595 AIAA-2016-3596 AIAA-2016-3597 AIAA-2016-3598 AIAA-2016-3599 Suborbital Air-Launch of Very Design, Build and Fly: Basler Research on Design Domain of Aeropropulsive Interaction and Synthesized analysis to the Light Payloads from a Fixed BT-67 with External Antenna Propeller-Driven Hybrid-Mode Thermal System Integration aircraft configuration with Wing Platform Fairings Aerial Vehicle within the ECO-150: A open rotor engines A. Sobester, A. Lock, University of W. Anemaat, W. Liu, M. Yang, W. Wenkai, Z. Hou, Z. Guo, Q. Chen, Turboelectric Distributed C. Ma, Z. Tan, D. Wu, Commercial Southampton, Southampton, United Design, Analysis and Research B. Wang, B. Zhu, National University Propulsion Airliner with Aircraft Corporation of China, Ltd. Kingdom Corporation, Lawrence, KS; R. Hale, of Defense Technology, Changsha, Conventional Electric Machines (COMAC), Shanghai, China University of Kansas, Lawrence, China B. Schiltgen, J. Freeman, Empirical Lawrence, KS Systems Aerospace, Inc., Pismo Beach, CA Thursday, 16 June 2016 223-ATIO.ATM-18 En-Route ATM I Fairchild East Chaired by: J. BRONSVOORT, Airservices Australia 0930 hrs 1000 hrs 1030 hrs 1100 hrs Oral Presentation AIAA-2016-3600 AIAA-2016-3601 AIAA-2016-3602 Using Sector Capacity Traffic Aware Planner for Design and Development of a Methods of Selecting Forecast Indicators for Tracking and Cockpit-based Trajectory Flight Route Modification Logging Winds for Flight Management Improving ATC Performance Optimization and Communication Network Systems to Support Four Y. Zhang, Y. Wang, University S. Woods, R. Vivona, Engility D. Merlino, University of North Texas, Dimensional Trajectory-Based of South Florida, Tampa, FL; J. Corporation, Billerica, MA; D. Wing, Denton, TX; C. Wilson, University of Operations 109 Gulding, K. Hanson, Federal Aviation K. Burke, NASA Langley Research Maryland, College Park, College Park, J. Jones, M. McPartland, T. Reynolds, Administration, Washington, D.C. Center, Hampton, VA MD; L. Carboneau, Florida Gulf Coast Y. Glina, C. Edwards, S. Troxel, Lincoln University, Fort Meyers, FL; A. Wilder, Laboratory, Massachusetts Institute of University of Kentucky, Lexington, Technology, Lexington, MA Lexington, KY; M. Underwood, NASA Langley Research Center, Hampton, VA Thursday, 16 June 2016 224-ATIO.ATM-19 Runway Management Embassy Chaired by: H. IDRIS, Engility Corporation (HQ) 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2016-3603 AIAA-2016-3604 AIAA-2016-3605 AIAA-2016-3606 Analysis of the Capacity Potential Evaluation of a standardized Exact and Heuristic Algorithms Runway Scheduling for of Current Day and Novel single runway airport model for Runway Scheduling Charlotte Douglas International Runway Configurations for New with respect to runway capacity W. Malik, University of California, Airport York’s John F. Kennedy Airport S. Kern, M. Schultz, German Santa Cruz, Moffett Field, CA; Y. W. Malik, H. Lee, University of P. Glaab, NASA Langley Research Aerospace Center (DLR), Jung, NASA Ames Research Center, California, Santa Cruz, Moffett Field, Center, Hampton, VA; R. Tamburro, Port Braunschweig, Germany Moffett Field, CA CA; Y. Jung, NASA Ames Research Authority of New York and New Jersey, Center, Moffett Field, CA New York, NY; P. Lee, NASA Ames Research Center, Moffett Field, CA Thursday, 16 June 2016 225-ATIO.ATM-20 Data Mining in ATS III Fairchild West Chaired by: A. EVANS, University of California Santa Cruz 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2016-3607 AIAA-2016-3608 AIAA-2016-3609 AIAA-2016-3610 AIAA-2016-3611 Cluster Analysis of Fuel Flow in Classification of Conflict Application of data mining to Clustering Algorithm for Large- Extraction of Helicopter Flight Operational Flight Data Resolution Methods using Data- forecast air traffic: a 3-stage Scale Flight Data Analysis Information from Cockpit Video P. Koppitz, D. Sauterleute, F. Mining Techniques model using discrete choice of Cockpit Human Machine Data using DBSCAN Clustering Holzapfel, Technical University of K. Kim, I. Hwang, Purdue University, modeling Interaction Issues S. Shin, I. Hwang, Purdue University, Munich, Munich, Germany West Lafayette, IN; B. Yang, Optimal J. Busquets, City University London, A. Vaidya, S. Lee, I. Hwang, Purdue West Lafayette, IN Synthesis, Inc., Los Altos, CA London, United Kingdom; A. Evans, University, West Lafayette, IN University of California, Santa Cruz, Santa Cruz, CA; E. Alonso, City University London, London, United Kingdom Thursday, 16 June 2016 226-ATIO.TFPC-10/ATIO. Transformational Flight - DARPA VTOL X-Plane Concepts Columbia 1 VSTOL-2 Chaired by: M. MOORE, NASA Langley Research Center and A. GIBSON, Empirical Systems Aerospace 0930 hrs 1000 hrs Oral Presentation Oral Presentation PhantomSwift Quad-Ducted Sikorsky / LM RBW Tail Sitter Fan Aircraft Configuration and Future Applications Development M. Alber, Sikorsky Aircraft R. Lacy, P. Ziegenbein, E. Gianopulos, Corporation, Stratford, CT R. Preator, The Boeing Company,

110 Ridley Park, PA Thursday, 16 June 2016 227-D4U-2 DEMAND for UNMANNED: Catalyst for the Machine Intelligence Revolution International Ballroom 0930 - 1700 hrs (West)

0930-1045 hrs Transformation in the National Airspace System Moderator: Dallas Brooks, Director, Raspet Flight Research Laboratory, Mississippi State University and Co-Chair, FAA/DoD/NASA/DHS Unmanned Aircraft System (UAS) Science and Research Panel Panelists: John Cavolowsky Pete Dumont Jonathan Evans Steven Pennington Michael Singer Director, Airspace Operations and Safety Program Executive Director CEO Executive Director CEO NASA Aeronautics Research Mission Directorate ATCA Skyward DoD Policy Board on Federal Aviation DroneView Technologies

1100-1215 hrs ASSURE: FAA Center of Excellence for UAS Research Moderator: Sabrina Saunders-Hodge, NextGen R&D Integration Division Manager, Federal Aviation Administration Panelists: David Arterburn Mark Anthony Askelson Dallas Brooks Major General James Poss (Ret.) Richard Stansbury Director, Rotorcraft Systems Engineering and Associate Professor Director, Raspet Flight Research & Associate Executive Director, Alliance for System Safety Associate Professor Simulation Center University of North Dakota Director for Research, ASSURE FAA UAS Center of UAS through Research Excellence Embry-Riddle Aeronautical University The University of Alabama in Huntsville of Excellence

1230-1400 hrs Break for Lunch

1400-1545 hrs UAS Trafﬁc Management System Session Chair: Parimal H. Kopardekar, Manager, Safe Autonomous System Operations Project, and Principal Investigator, Unmanned Aerial Systems Trafﬁc Management, NASA Ames Research Center 111 Moderator: Gretchen West, Senior Advisor of Innovation and Technology, Hogan Lovells and Advisory Board Member, DroneWorld Expo Panelists: Gregory Agvent Sean Cassidy R. John Hansman Jesse Kallman Senior Director, News Operations Director, Strategic Partnerships T. Wilson Professor of Aeronautics & Astronautics and Director of Business Development & Regulatory Affairs CNN Amazon Prime Air Director of the International Center for Air Transportation Airware Massachusetts Institute of Technology

Craig Marcinkowski Ashok N. Srivastava Peng Wei Director, Strategy and Business Development Chief Data Scientist Assistant Professor, Aerospace Engineering Gryphon Sensors Verizon Iowa State University

1545-1600 hrs DEMAND for UNMANNED Networking Coffee Break

1600-1700 hrs Visions of the Future Chuck Howell Jean-Charles Ledé Dale Richards Chief Engineer, Portfolio Programs and Integration Program Manager, Tactical Technology Ofﬁce Senior Research Fellow in Human Factors MITRE Defense Advanced Research Projects Agency Coventry University Thursday, 16 June 2016 228-F360-8 Restoring the Foundation of Aviation International Ballroom 0930 - 1130 hrs (East) Moderator: Gregory J. Bowles, Director, European Regulatory Affairs & Engineering Panelists: Nicholas K. Borer Lowell Foster Andy Supinie Rick Peri Principal Investigator, Aeronautics Systems Analysis Branch ACE 111, FAA Regulations and Policy, FAA Small Airplane Flight Director, Aerosciences Vice President, Government and Industry Affairs NASA Langley Research Center Test Engineer Textron Aviation Aircraft Electronics Association FAA Small Plane Certiﬁcation

Thursday, 16 June 2016 229-FC-14 Bluff Body Flow Control Morgan Chaired by: A. AHMED, Auburn University 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2016-3612 AIAA-2016-3613 AIAA-2016-3614 AIAA-2016-3615 Aerodynamic Flow Control of Computational Design of Drag Closed-Loop Flow Control of Validation of a Plasma Actuator Wake Dynamics Coupled to a Diminishing Active Flow Control the Oscillations of a Free- Model by Simulation of the Moving Bluff Body Systems for Heavy Vehicles Suspended Cylinder at Low Detached Flow Over a Half- T. Lambert, B. Vukasinovic, A. Glezer, D. Manosalvas, T. Economon, Reynolds Numbers Cylinder Georgia Institute of Technology, Stanford University, Stanford, CA; C. A. Hillier, O. Friedland, A. Seifert, Tel R. Futrzynski, G. Efraimsson, Royal Atlanta, GA Othmer, Volkswagen of America, Inc., Aviv University, Tel Aviv, Israel Institute of Technology (KTH), Belmont, CA; A. Jameson, Stanford Stockholm, Sweden University, Stanford, CA Thursday, 16 June 2016

112 230-FC-15 Vortex Generators Columbia 11 Chaired by: S. YARUSEVYCH, University of Waterloo 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2016-3616 AIAA-2016-3617 AIAA-2016-3618 AIAA-2016-3619 AIAA-2016-3620 AIAA-2016-3621 An Aerodynamic Model for Evaluation of Some Wedge- Experimental and Numerical Separation Control over a The Effects of Freestream Tomographic PIV Vane-Type Vortex Generators shaped Vortex Generators Investigation of Static and Flapped NACA 0012 Model Turbulence on Steady VGJ Flow measurements of turbulent D. Poole, R. Bevan, C. Allen, T. Using Swirl Center Tracking Dynamic Vortex Generators on an using an Array of Low Aspect Control on a Highly Loaded boundary layer perturbed by Rendall, University of Bristol, Bristol, J. Sandhu, S. Subramanian, S. Airfoil with a Deflected Flap Ratio Cylindrical Pins Transonic LPT Cascade a dynamic cylinder roughness United Kingdom Ghosh, Indian Institute of Technology T. Rice, R. Cummings, Rensselaer S. Gildersleeve, Rensselaer C. Sacco, M. Hossain, J. Bons, Ohio element Madras, Chennai, India; P. Sharma, Polytechnic Institute, Troy, NY; D. Polytechnic Institute, Troy, NY; D. State University, Columbus, OH Z. Tang, Hebei University of Indian Institute of Technology Kanpur, Clingman, The Boeing Company, Seattle, Clingman, The Boeing Company, Technology, Tianjin, China; Y. Wu, Kanpur, India WA; O. Sahni, M. Amitay, Rensselaer Seattle, WA; M. Amitay, Rensselaer Nanyang Technological University, Polytechnic Institute, Troy, NY Polytechnic Institute, Troy, NY Singapore, Singapore Thursday, 16 June 2016 231-FD-48 Jet Flows I Holmead West Chaired by: D. MCLAUGHLIN and M. TACHIE 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2016-3622 AIAA-2016-3623 AIAA-2016-3624 AIAA-2016-3625 AIAA-2016-3626 Uncertainty Quantification and Application of Navier-Stokes Influence of Different Subgrid Lagrangian Characterization of Effect of Asymmetric Nozzle Sensitivity Analysis applied to based Mean-Flow Perturbation Scale Models in LES of Supersonic Jet Near-Fields Configuration on Jet Flow an under-expanded single jet Method to Supersonic Jet Noise Supersonic Jet Flows D. Gonzalez, Naval Surface Warfare Characteristics F. Granados-Ortiz, University of S. Bhaumik, D. Gaitonde, K. C. Junqueira-Junior, S. Yamouni, Center, Indian Head, MD; D. S. Sengupta, L. Agostini, D. Gaitonde, Greenwich, London, United Kingdom; Goparaju, S. Unnikrishnan, M. Technological Institute of Aeronautics Gaitonde, Ohio State University, Ohio State University, Columbus, OH C. Perez Arroyo, CERFACS, Toulouse, Waindim, Ohio State University, (ITA), São José dos Campos, Brazil; Columbus, OH; M. Lewis, Science France; C. Lai, University of Columbus, OH J. Azevedo, Aeronautics and Space and Technology Policy Institute, Greenwich, London, United Kingdom; Institute (IAE), São José dos Campos, Washington, D.C. G. Puigt, CERFACS, Toulouse, France; Brazil; W. Wolf, University of C. Airiau, Fluid Mechanics Institute of Campinas, Campinas, Brazil Toulouse (IMFT), Toulouse, France Thursday, 16 June 2016 232-FD-49 Opportunities in Future Fluid Dynamics Research (Invited) Jefferson East Chaired by: H. LUO, Vanderbilt University and D. BODONY, University of Illinois at Urbana-Champaign 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs Oral Presentation Oral Presentation Oral Presentation Oral Presentation Oral Presentation Oral Presentation Environmentally Responsible Opportunities in Turbulence Future Paradigm Shifts in Data-Driven Models and Their Bringing the Future of Fluids Problems Looking for Solutions: Aviation and the Role of Fluid and Unsteady Flows Computing Fluid Dynamics Role in Understanding and into the Present Fluid Dynamics Research in Dynamics A. Smits, Princeton University, J. Boris, Naval Research Laboratory, Controlling Fluids E. Whalen, The Boeing Company, St. Propulsion and Energy Systems F. Collier, NASA Headquarters, Princeton, NJ Washington, D.C. C. Rowley, Princeton University, Louis, MO A. Karagozian, University of California, Washington, D.C. Princeton, NJ Los Angeles, Los Angeles, CA Thursday, 16 June 2016 233-FD-50 High-Speed Facilities and Test Methods Lincoln East Chaired by: T. WADHAMS, CUBRC and T. ROSSMANN, Lafayette College 0930 hrs 1000 hrs 1030 hrs AIAA-2016-3627 AIAA-2016-3628 AIAA-2016-3629 Design and Characterization Analysis of Hypersonic Flow Porous Injection Effect on Surface of the Lafayette College Effects on Sensor Performance Heat Flux in High-enthalpy High- Expansion Tube for High-Speed L. Mackey, I. Boyd, University of Reynolds number flow Turbulent Combustion Michigan, Ann Arbor, Ann Arbor, MI H. Tanno, T. Komuro, K. Sato, K. Itoh, R. Sanzi, D. Jones, T. Rossmann, Japan Aerospace Exploration Agency Lafayette College, Easton, PA (JAXA), Kakuda, Japan; M. Kuhn, I. Petkov, German Aerospace Center (DLR), Stuttgart, Germany Thursday, 16 June 2016

113 234-FD-53 Multiphase Flows I Columbia 10 Chaired by: D. KESSLER and Y. LIAN, University of Louisville 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2016-3630 AIAA-2016-3631 AIAA-2016-3632 AIAA-2016-3633 AIAA-2016-3634 AIAA-2016-3635 A Numerical Study of Transient A Study of the Effects of Compressible and Non- Numerical Study of the Prompt Application of the Discrete Computational Skin Friction Deformation and Drag Turning Angle on Particle Expanding Fluid Model Splashing Caused by a Droplet Element Method to Ice and Heat Transfer Modeling of Properties of Accelerating and Deposition in Turbine for Simulation of Impact Impinging on a Liquid Film Accretion Geometries Ice Roughened Airfoils Decelerating Liquid Drops Combustor Effusion Cooling Phenomena Q. Qu, Y. Zhang, P. Liu, Beihang D. Hanson, M. Kinzel, Pennsylvania D. Hanson, M. Kinzel, Y. Han, Q. Qu, P. Ma, P. Liu, Beihang Holes K. Suzuki, University of Tokyo, University, Beijing, China; F. Zhang, State University, University Park, PA J. Palacios, Pennsylvania State University, Beijing, China; R. Agarwal, S. Whitaker, J. Bons, R. Blunt, Ohio Kashiwa, Japan China Aerospace Science and Industry University, University Park, PA Washington University in St. Louis, State University, Columbus, OH Corporation (CASIC), Beijing, China; St. Louis, MO R. Agarwal, Washington University in St. Louis, St. Louis, MO Thursday, 16 June 2016 235-GT-7 Experimental Investigations of High Speed Air Breathing Propulsion Cardozo Chaired by: C. JORGENS, Boeing and K. BUTLER, Aerospace Testing Alliance/AEDC/4001 0930 hrs 1000 hrs AIAA-2016-3636 AIAA-2016-3637 Experimental Investigation Measurement of heat flux of Dynamic Separation for a distribution of supercritical Hypersonic Inlet Cover in Mach kerosene fueled supersonic 6 Flow combustor G. Zhu, L. Wang, Beijing Aerospace D. Cheng, China Academy of Aerospace Technology Institute, Beijing, China Aerodynamics, Beijing, China; J. Wang, Chinese Academy of Sciences, Beijing, China; J. Gong, China Academy of Aerospace Aerodynamics, Beijing, China; L. Yang, W. Yao, L. Li, Chinese Academy of Sciences, Beijing, China; et al. Thursday, 16 June 2016 236-ITAR-5 NASA Orion EFT-1 Aeroscience Results - Aerothermal II Cabinet Chaired by: A. AMAR, NASA Johnson Space Center and D. OWENS, NASA-Langley Research Center 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2016-3638 AIAA-2016-3639 AIAA-2016-3640 AIAA-2016-3641 AIAA-2016-3642 AIAA-2016-3643 Characterization of EFT-1 Aerothermal Analysis of Orion Exploration Flight Test Orion EFT-1 Cavity Heating and Reentry Communication Aerothermal Analyses for Orion Radiative Heating and Compression Pad Features on Reaction Control System Catalytic Tile Experiments. Ionization Blackout for Orion MPCV TPS Design Radiometer Data the Orion EFT-1 Heatshield Jet Interaction Heating G. Salazar, A. Amar, B. Oliver, A. EFT-1 Flight Test R. McDaniel, NASA Ames Research B. Cruden, Analytical Mechanics R. Thompson, V. Lessard, NASA Environment from Flight Data Hyatt, NASA Johnson Space Center, D. Gulick, Lockheed Martin Center, Moffett Field, CA Associates, Inc., Moffett Field, CA; Langley Research Center, Hampton, M. White, A. Hyatt, NASA Johnson Houston, TX; M. Rezin, NASA Ames Corporation, Denver, CO; R. C. Johnston, NASA Langley Research VA Space Center, Houston, TX Research Center, Moffett Field, CA Thompson, NASA Langley Research Center, Hampton, VA Center, Hampton, VA Thursday, 16 June 2016 237-MAO-13 Structural Optimization II Columbia 3 Chaired by: J. GRAY, NASA Glenn Research Center and S. CHOI, Virginia Polytechnic Institute and State University 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2016-3644 AIAA-2016-3645 AIAA-2016-3646 AIAA-2016-3647 AIAA-2016-3648 Design of Thermally-Stressed On the Trade-off between An Uncoupled Approach to Aeroelastic Optimization of A linear aerodynamics-based Panels Subject to Transonic Stress and Dynamic Responses Compute Aero-Structure Variable Stiffness Composite Wing preconditioner for high-fidelity Flutter Constraints in the Design of Thermal Gradients Using High-Fidelity with Blending Constraints aeroelastic analysis and M. Bhatia, Mississippi State Structures CFD-CSM M. Bordogna, ONERA, Châtillon, sensitivity analysis University, Mississippi State, MS; P. J. Deaton, Adjoint Technologies, T. Achard, C. Blondeau, ONERA, France; T. Macquart, Delft University of K. Jovanov, R. De Breuker, Beran, Air Force Research Laboratory, LLC, Dayton, OH; P. Beran, Air Force Châtillon, France; R. Ohayon, Technology, Delft, The Netherlands; D. M. Abdalla, Delft University of Wright-Patterson AFB, OH Research Laboratory, Wright-Patterson National Conservatory of Arts and Bettebghor, ONERA, Châtillon, France; Technology, Delft, The Netherlands; C. AFB, OH Crafts, Paris, France R. De Breuker, Delft University of Blondeau, ONERA, Paris, France Technology, Delft, The Netherlands 114 Thursday, 16 June 2016 238-MAO-14 Emerging Methods, Algorithms, and Dynamic Data Driven Systems Columbia 4 Chaired by: K. WILLCOX, Massachusetts Institute of Technology and D. ALLAIRE, Texas A&M University 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2016-3649 AIAA-2016-3650 AIAA-2016-3651 AIAA-2016-3652 AIAA-2016-3653 AIAA-2016-3654 Methodology for Path Planning A Dynamic Data-Driven Dynamic-Data-Driven Damage Adjoint-based Mesh Adaptation Route-Planning for Real-Time Real-Time Safety-Assured with Dynamic Data-Driven Approach to Multiple Task Prediction in Aerospace Techniques for Aggregation Safety-Assured Autonomous Autonomous Aircraft Flight Capability Estimation Capability Estimation for Self- Composite Structures Functionals in Structural Design Aircraft J. Chambers, Aurora Flight Sciences, V. Singh, K. Willcox, Massachusetts Aware Aerospace Vehicles A. Korobenko, X. Deng, M. Pigazzini, Optimization R. Cowlagi, Worcester Polytechnic Manassas, VA; N. Baltadjiev, Aurora Institute of Technology, Cambridge, B. Burrows, B. Isaac, D. Allaire, Texas Y. Bazilevs, University of California, G. Kennedy, Georgia Institute of Institute, Worcester, MA; J. Flight Sciences, Cambridge, MA; MA A&M University, College Station, TX San Diego, La Jolla, CA Technology, Atlanta, GA Chambers, N. Baltadjiev, Aurora Flight R. Cowlagi, Worcester Polytechnic Sciences, Manassas, VA Institute, Worcester, MA Thursday, 16 June 2016 239-MST-12 Model and Simulation Design, Development, Testing, and Validation Piscataway Chaired by: U. DURAK, DLR-German Aerospace Center and M. ALVAREZ, NASA Langley Research Center 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2016-3655 AIAA-2016-3656 AIAA-2016-3657 AIAA-2016-3658 Running High Level Toward Qualification Standards Matching of Aerodynamic Aerodynamic Longitudinal Architecture in Real-Time for for Future Simulation Training databank with Flight test data – Coefficient Modeling During Flight Simulator Integration Devices and Applications – Longitudinal Dynamics Aircraft Design Phases T. Gerlach, U. Durak, A. Knüppel, T. Experiences, Opportunities and A. de Paula, Technological Institute of A. de Paula, Technological Institute Rambau, German Aerospace Center Challenges Aeronautics (ITA), São José dos Campos, of Aeronautics (ITA), São José dos (DLR), Braunschweig, Germany M. Roza, A. Gerretsen, J. Field, Brazil; M. Sousa, Federal University Campos, Brazil; F. Magalhães Porto, National Aerospace Laboratory (NLR), of Itajubá, Itajubá, Brazil; F. Porto, Embraer, São José dos Campos, Amsterdam, The Netherlands EMBRAER, São José dos Campos, Brazil; Brazil; M. Sousa, Federal University S. Cunha Junior, Federal University of of Itajubá, Itajubá, Brazil Itajubá, Itajubá, Brazil Thursday, 16 June 2016 240-MST-13 Fault Detection and Health Monitoring Georgetown East Chaired by: J. KRUEP, Aerojet Rocketdyne and R. RUFF 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2016-3659 AIAA-2016-3660 AIAA-2016-3661 AIAA-2016-3662 AIAA-2016-3663 Synchronizing Design Knowledge A Fault Diagnosis Method for Reliability assessment method Component-level Modeling Multi-signal Model in and Real Time Monitoring Complex System Based on for Integrated Modular Avionics and Simulation of Cable Fault Application of Spacecraft Power Information for Aircraft Complex Hierarchical Bayesian Network System Based on Bayesian Detection System System Testability System Diagnosis W. Niu, W. Niu, Aviation Industry network J. Mao, L. Wang, Nanjing University Z. Dai, L. Wang, S. Yang, Nanjing X. Chen, H. Ren, Shanghai Engineering Corporation of China (AVIC), Xi’an, D. Ling, Beihang University, Beijing, of Aeronautics and Astronautics, University of Aeronautics and Research Center of Civil Aircraft Health China; J. Cheng, Xi’an Institute of China Nanjing, China; G. Cheng, Shanghai Astronautics, Nanjing, China; J. Zhao, Monitoring, Shanghai, China; C. Bil, Applied Optics, Xi’an, China Aircraft Design and Research Institute, Shandong Institute of Aerospace RMIT University, Melbourne, Australia; Y. Shanghai, China Electronics Technology, Yantai, China Sun, Institute of Sensor and Reliability Engineering, Harbin, China Thursday, 16 June 2016 241-PDL-6 Plasma and Laser Technologies Gunston West Chaired by: J. ZIMMERMAN, CU Aerospace and S. LEONOV, University of Notre Dame 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2016-3664 AIAA-2016-3665 AIAA-2016-3666 AIAA-2016-3667 AIAA-2016-3668 AIAA-2016-3669 Multiphysics modeling of Internal structure of LSD wave Numerical Analysis of Remote Lasing in Humid Air Measurement of Heat-Flux Comparative Study of plasma-assisted methane based on a 1-D Laser-induced Comb Shaped Plasma Front from Atomic Hydrogen for Magneto-Aerodynamic Nonequilibrium Plasma combustion with direct Discharge model: comparison Propagation in Millimeter- T. Chng, A. Dogariu, R. Miles, Interaction Studies in a Generation and Plasma- comparisons to experiments between numerical simulation Wave Discharge under Princeton University, Princeton, NJ Hypersonic Flow Assisted Ignition for Different J. Zimmerman, A. Palla, D. King, and experiment Atmospheric Pressure A. Kkn, K. Reddy, Indian Institute of C2 Hydrocarbons

115 D. Carroll, CU Aerospace, LLC, J. Ofosu, R. Kawashima, K. Matsui, Y. Nakamura, M. Fukunari, T. Science, Bengaluru, India A. Starikovskiy, Princeton University, Champaign, IL; R. Rajasegar, C. T. Shimano, K. Komurasaki, Yamaguchi, K. Komurasaki, H. Princeton, NJ Mitsingas, University of Illinois, University of Tokyo, Tokyo, Japan; K. Koizumi, University of Tokyo, Tokyo, Urbana-Champaign, Urbana, IL; et al. Shimamura, University of Tsukuba, Japan Tsukuba, Japan; et al. Thursday, 16 June 2016 242-TP-9 Special Session: Thermal Management Systems DuPont Chaired by: J. DIDION, NASA-Goddard Space Flight Center and L. BYRD 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2016-3670 Oral Presentation AIAA-2016-3671 Oral Presentation AIAA-2016-3672 AIAA-2016-3673 Performance of a Loop Heat Pipe Silicon Vapor Chamber: A Chip- Nonlinear Dynamics in Loop Single-phase and Two- Two Phase Thermal Protection High Fidelity Modeling of Energy

Subjected to a Phase-Coupled level Super Heat Spreader Heat Pipe Operation phase Flow Distribution of the Hypersonic Leading Edge Transfer in the N2 + N system for Heat Input to an Acceleration S. Cai, A. Bhunia, Teledyne T. Hoang, TTH Research, Inc., Clifton, Control in Meso-scale J. Maxwell, Naval Research Strong Shock Conditions Field Technologies, Inc., Thousand Oaks, VA; R. Baldauff, Naval Research via Electrohydrodynamic Laboratory, Washington, D.C.; T. T. Zhu, University of Illinois, Urbana- K. Yerkes, J. Scoﬁeld, Air Force Research CA Laboratory, Washington, D.C. Conduction Pumping Hoang, TTH Research, Inc., Clifton, VA Champaign, Urbana, IL; Z. Li, Laboratory, Wright-Patterson AFB, OH; D. L. Yang, M. Talmor, J. Seyed-Yagoobi, Pennsylvania State University, University Courson, University of Dayton Research Worcester Polytechnic Institute, Park, PA; D. Levin, University of Illinois, Institute, Dayton, OH Worcester, MA Urbana-Champaign, Urbana, IL Thursday, 16 June 2016 243-TP-10 High Enthalpy Ground Testing Jay Chaired by: D. KUNTZ, Sandia National Laboratories 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2016-3674 AIAA-2016-3675 AIAA-2016-3676 AIAA-2016-3677 AIAA-2016-3678 AIAA-2016-3679 Blunt-Body Heating and Operational Envelope of the Flow Characterization Studies Experimental Thermal Analysis and Rebuilding of High-Pressure H2/He/O2 Pressure Database from High- Low Power Plasma Facilities at of the 10-MW TP3 Arc-Jet Response and Demisability Experiments on a Reinforced- Combustion Experiments for

Enthalpy, CO2 Testing in an the University of Kentucky Facility Investigations on ﬁve Carbon-Carbon model in X2 the Design of the ESTHER Expansion Tunnel H. Koch, B. Butler, M. Winter, T. Gokcen, A. Alunni, Analytical Aerospace Structure Materials Expansion Tunnel Shock-Tube Driver B. Hollis, NASA Langley Research University of Kentucky, Lexington, Mechanics Associates, Inc., Moffett under Simulated Destructive J. Mora-Monteros, P. Leyland, U. Sheikh, M. Lino Da Silva, B. Carvalho, Center, Hampton, VA; D. Prabhu, ERC, Lexington, KY; C. Arnold, University of Field, CA Re-Entry Conditions E. Fahy, S. Lewis, Swiss Federal Institute Technical University of Lisbon, Lisbon, Inc., Moffett Field, CA; M. MacLean, Stuttgart, Stuttgart, Germany A. Pagan, B. Massuti-Ballester, G. of Technology, Lausanne, Switzerland; Portugal CUBRC, Buffalo, NY Herdrich, University of Stuttgart, T. McIntyre, University of Queensland, Stuttgart, Germany Brisbane, Australia; et al. Thursday, 16 June 2016 244-LNCH-3 Awards Luncheon: Celebrating the Achievements in Aircraft and Atmospheric Systems International Ballroom 1230 - 1400 hrs (Center) A ticket for the luncheon is required and included in the registration fee where indicated. Additional tickets for guests may be purchased upon registration or on site, as space is available.

The following awards will be presented: Aircraft Design Award Gardner-Lasser Aerospace Literature Award Hap Arnold Award For Excellence in Aeronautical Program Management Multidisciplinary Design Optimization Award Piper General Aviation Award

116 Thursday, 16 June 2016 245-AMT-10/GT-8 Ground Test Applications of Aerodynamic Measurement Technology Columbia 2 Chaired by: K. LOWE, Virginia Tech and T. WAYMAN, Gulfstream Aerospace Corporation 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2016-3680 AIAA-2016-3681 AIAA-2016-3682 AIAA-2016-3683 AIAA-2016-3684 AIAA-2016-3685 Assessment of the Uniqueness Investigation rear-end of flow Consolidated Laser-Induced Non-Intrusive Measurement Pressure-Sensitive Paint Feasibility of Dynamic Stability of Wind Tunnel Strain-Gage structures on a 6:1 prolate Fluorescence Diagnostic Systems of Gas Turbine Engine Exhaust Measurements on a Moving Measurements of Planetary Balance Load Predictions spheroid by using the magnetic for the NASA Ames Arc Jet Characteristics using Acoustic Store in the NRC 1.5 m Entry Capsules Using a N. Ulbrich, Jacobs, Moffett Field, CA suspension and balance system Facilities Measurements. Blowdown Wind Tunnel Magnetic Suspension and T. Ambo, Tohoku University, Sendai, J. Grinstead, M. Wilder, NASA Ames R. Otero, K. Lowe, W. Ng, L. Ma, C. Y. Mebarki, National Research Council Balance System Japan; T. Otsuki, Georgia Institute Research Center, Moffett Field, CA; Kim, Virginia Polytechnic Institute and Canada, Ottawa, Canada C. Britcher, Old Dominion University, of Technology, Atlanta, GA; S. B. Porter, Aerospace Computing, Inc., State University, Blacksburg, VA Norfolk, VA Taniguchi, D. Numata, K. Asai, Moffett Field, CA; J. Brown, Analytical Tohoku University, Sendai, Japan; Mechanics Associates, Inc., Moffett Field, T. Liu, Western Michigan University, CA; D. Yeung, Jacobs, Moffett Field, Kalamazoo, MI CA; S. Battazzo, NASA Ames Research Center, Moffett Field, CA; et al. Thursday, 16 June 2016 246-APA-33/FD-54 Unsteady Wing Aerodynamics Kalorama Chaired by: C. SHENG, The University of Toledo and J. AZEVEDO 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs AIAA-2016-3686 AIAA-2016-3687 AIAA-2016-3688 AIAA-2016-3689 AIAA-2016-3690 AIAA-2016-3691 AIAA-2016-3692 Model Reduction in Discrete Nonlinear Lifting-Line A Subsonic Indicial Aerodynamics Dynamic Stall Simulations on a Dynamic Ground Effect Low-dimensional Modeling An investigation into the Vortex Methods for 2D Algorithm for Unsteady and for the Unsteady Loads of Pitching Finite Wing Analysis using a Novel Sinking and Aerodynamics of Flexible effect of airfoil camber on Unsteady Aerodynamic Flows Post-stall Conditions Trapezoidal Wings K. Kaufmann, C. Merz, A. Gardner, Grid Methodology Wings in Flapping Flight the aerodynamics of MAV A. Suresh Babu, North Carolina State J. Dias, University of Maryland, M. Righi, Zurich University of Applied German Aerospace Center (DLR), P. Mondal, Indian Institute of Science, Y. Ren, H. Dong, University scale cycloidal propeller under University, Raleigh, NC; K. Ramesh, College Park, College Park, MD Sciences, Zurich, Switzerland; M. Berci, Göttingen, Germany Bengaluru, India; M. Nagaram, N. of Virginia, Charlottesville, hovering status University of Glasgow, Glasgow, University of Leeds, Leeds, United Shende, S&I Engineering Solutions Charlottesville, VA H. Zhang, Y. Hu, G. Wang, Z. Fan, United Kingdom; A. Gopalarathnam, Kingdom; M. Franciolini, Marche Pvt., Ltd., Bengaluru, India; B. Y. Wang, Northwestern Polytechnical North Carolina State University, Polytechnic University, Ancona, Italy; A. Narayanarao, Indian Institute of University, Xi’an, China Raleigh, NC Da Ronch, University of Southampton, Science, Bengaluru, India Southampton, United Kingdom Thursday, 16 June 2016 247-APA-34/FD-55 Vortex/Vortical Flows I Northwest Chaired by: M. YU, University of Maryland, Baltimore County and R. DOWGWILLO, The Boeing Company 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs AIAA-2016-3693 AIAA-2016-3694 AIAA-2016-3695 AIAA-2016-3696 AIAA-2016-3697 AIAA-2016-3698 AIAA-2016-3699 Vortex Induced Aerodynamic The Vortex Aerodynamics of Numerical investigations of the An Assessment of the Fast Numerical Investigation of Investigation of Unsteady Effect of Ground Obstacle Forces on a Flat Plate in Delta Wings vortical flow on swept wings Multipole Method Applied to Vortex Breakdown Characteristics of Vortex Separation Distance on Wake Ground Proximity S. Lee, CLAS Consultants, Lake Forest with round leading edges a Vortex Sheet Roll-Up Problem T. van Jindelt, University of Twente, Breakdown Vortex Dissipation J. Holt, K. Garry, Cranfield University, Park, WA A. Schuette, German Aerospace T. Rodarte Ricciardi, W. Wolf, Enschede, The Netherlands; J. van L. Chen, China Academy of Aerospace C. Wang, D. Zhao, Nanyang Cranfield, United Kingdom Center (DLR), Braunschweig, University of Campinas, Campinas, der Burg, Airbus, Bremen, Germany; Aerodynamics, Beijing, China; J. Wang, Technological University, Singapore, Germany Brazil; A. Bimbato, São Paulo State E. van der Weide, H. Hoeijmakers, L. Feng, Beihang University, Beijing, Singapore; J. Schluter, Deakin University, 117 University, Guaratingueta, Brazil University of Twente, Enschede, The China; H. Hu, China Aerodynamics Melbourne, Australia; F. Holzäpfel, A. Netherlands Research and Development Center, Stephan, German Aerospace Center Mianyang, China (DLR), Oberpfaffenhofen, Germany Thursday, 16 June 2016 248-APA-35 Airfoil/Wing/Configuration Aerodynamics Columbia 9 Chaired by: D. FINLEY, Lockheed Martin Aeronautics 1400 hrs 1430 hrs 1500 hrs 1530 hrs AIAA-2016-3700 AIAA-2016-3701 AIAA-2016-3702 AIAA-2016-3703 Research of the effects of Design, Analysis, and Canard-Wing Interference Effects Numerical Investigation of the power on aerodynamic Evaluation of a Propulsive on the Flight Characteristics of a Aerodynamics of an Inverted characteristics of a civil aircraft Wing Concept Transonic Passenger Aircraft Three-Element Airfoil in Ground G. Shao Jie, P. Zhou, W. Bin, Y. Zhong M. Kerho, Rolling Hills Research S. Harrison, R. Darragh, P. Hamlington, Effect for Race Car Application Yan, China Academy of Aerospace Corporation, El Segundo, CA; P. University of Colorado, Boulder, Boulder, Q. Qu, P. Zuo, Y. Qin, P. Liu, Beihang Aerodynamics, Beijing, China Ansell, S. D’Urso, G. Ananda, A. CO; M. Ghoreyshi, A. Lofthouse, U.S. Air University, Beijing, China; R. Agarwal, Perry, University of Illinois, Urbana- Force Academy, Colorado Springs, CO Washington University in St. Louis, St. Champaign, Urbana, IL Louis, MO Thursday, 16 June 2016 249-APA-36 Aerodynamic Design Methodologies III Albright Chaired by: N. HARIHARAN, CREATE-AV and J. DOYLE, US Army AMRDEC 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs AIAA-2016-3704 AIAA-2016-3705 AIAA-2016-3706 AIAA-2016-3707 AIAA-2016-3708 AIAA-2016-3709 AIAA-2016-3710 An Application for Air on a Numerical Simulation of Wake Research on the Effect of Detailed Study of Effects of Shock Effects on Rotating A Comparison of Computational Design of a Cooling Duct New Form of Prandtl Meyer FlowField Behind the C-130H Propeller Slipstream on Twin Crosswind and Turbulence Detonation Waves in the and Experimental Results for for the Solar Cells on a Function Cargo Ramp boom UAV Trim Characteristic Intensity on Aircraft Wake- Hydrogen-Air Mixture Three-Dimensional Flow over a Solar Powered Unmanned M. Salhi, T. Zebbiche, University of M. Ghoreyshi, U.S. Air Force Academy, L. Chen, Z. Guo, Z. Hou, National Vortex in Ground Proximity Y. Wang, Southwest University of Undulating Inflatable Wing Aerial Vehicle to Improve Blida 1, Blida, Algeria Colorado Springs, CO; K. Bergeron, Army University of Defense Technology, S. Paramasivam, D. Zhao, M. Skote, Science and Technology, Mianyang, J. Beltz, S. Kota, G. Spencer, J. Performance Research, Development and Engineering Changsha, China Nanyang Technological University, China Krofta, R. LeBeau, Saint Louis R. Murzello, M. Nazarinia, A. Hughes, Command, Natick, MA; A. Lofthouse, Singapore, Singapore; J. Schluter, University, St. Louis, MO Heriot-Watt University, Dubai, United U.S. Air Force Academy, Colorado Deakin University, Geelong, Australia Arab Emirates Springs, CO Thursday, 16 June 2016 250-APA-37 Low Boom Activities II (Invited) Jefferson West Chaired by: A. ELMILIGUI, NASA Langley Research Center and J. MORGENSTERN, Lockheed Martin Aeronautics 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs Oral Presentation Oral Presentation Oral Presentation Oral Presentation Oral Presentation Oral Presentation Overview of NASA’s Development of High Fidelity Development of Metrics Designing Supersonic Airliners Status and Plans for Concept Development of the Commercial Supersonic Tools and Robust Design and Models for Assessing to Meet Airport Noise NASA’s Low-Boom Flight Quiet Supersonic Technology Technology Project Approaches for Low Boom Aircraft Community Response to Regulations Demonstration and Quiet Aircraft P. Coen, NASA Langley Research L. Bangert, L. Ozoroski, NASA Langley Supersonic En Route Noise J. Bridges, NASA Glenn Research SuperSonic Technology Aircraft P. Iosifidis, Lockheed Martin Center, Hampton, VA Research Center, Hampton, VA A. Loubeau, NASA Langley Research Center, Cleveland, OH D. Richwine, NASA Langley Research Corporation, Palmdale, CA Center, Hampton, VA Center, Hampton, VA

118 Thursday, 16 June 2016 251-ASE-15 Atmospheric Environments Columbia 12 Chaired by: Z. ZHENG, The University of Kansas and M. PRUIS, Northwest Research Associates Inc 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2016-3711 AIAA-2016-3712 AIAA-2016-3713 AIAA-2016-3714 AIAA-2016-3716 AIAA-2016-3717 Contrail flight data from Meteorological Data Collection Rebuilding freestream Spline Trajectory Algorithm Drifting Ice Giant Dark Spots Development of Wind petroleum and bio-fuel for Three-Dimensional atmospheric conditions using Development: Bézier Curve and Their Potential Connections Sensing from Small UAS with emissions at cruise altitude Forecasting Advancements surface pressure and heat flux Control Point Generation for to Terrestrial Hurricanes Distributed Pressure Sensors A. Brown, M. Bastian, S. Alavi, N. Foster, J. Jacob, Oklahoma State data UAVs R. LeBeau, Saint Louis University, St. R. Laurence, B. Argrow, E. Frew, National Research Council Canada, University, Stillwater, OK A. Cortesi, P. Congedo, National Institute L. Howell, B. Allen, NASA Langley Louis, MO; C. Palotai, Florida Institute University of Colorado, Boulder, Ottawa, Canada; M. Wasey, Wasey for Research in Computer Science and Research Center, Hampton, VA of Technology, Melbourne, FL Boulder, CO Consultants, Toronto, Canada Control, Talence, France; T. Magin, von Kármán Institute for Fluid Dynamics, Rhode-Saint-Genèse, Belgium; B. Van Hove, O. Karatekin, Royal Observatory of Belgium, Brussels, Belgium Thursday, 16 June 2016 252-ASE-16 HAIC/HIWC 2014 Darwin and 2015 Cayenne Flight Campaigns Update II and AIRA Forum Georgetown West Chaired by: D. MARCOTTE and T. RATVASKY, NASA Glenn Research Center 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs Oral Presentation AIAA-2016-3718 AIAA-2016-3719 AIAA-2016-3720 Oral Presentation Oral Presentation Oral Presentation Instrumentation and Characterization of the Pilot In-situ Wind-fields Measured Numerical Simulation of HIWC History of AIRA and an 75 Years of Icing at the Reduction of Aviation Icing Risk preliminary results obtained X-band radar responses to the by the NRC Convair during Conditions with the Terminal Overview of AIRA Sponsored National Research Council of D. Marcotte, National Research from the NRC Convair-580 HIWC environment during the HAIC-HIWC 2015 Area Simulation System Projects Canada Council Canada, Ottawa, Canada during the High Ice Water Cayenne HAIC-HIWC 2015 A. Brown, M. Wolde, National F. Proctor, NASA Langley Research J. MaCleod, National Research J. MaCleod, National Research Content field campaign in Campaign Research Council Canada, Ottawa, Center, Hampton, VA; G. Switzer, Council Canada, Ottawa, Canada Council Canada, Ottawa, Canada Cayenne in May 2015 M. Wolde, C. Nguyen, National Research Canada; A. Korolev, Environment Analytical Mechanics Associates, Inc., A. Korolev, Environment Canada, Council Canada, Ottawa, Canada; A. Canada, Toronto, Canada Hampton, VA Toronto, Canada; M. Wolde, National Korolev, Environment Canada, Toronto, Research Council Canada, Ottawa, Canada; M. Bastian, National Research Canada Council Canada, Ottawa, Canada Thursday, 16 June 2016 253-ATIO.ATM-21 En-Route ATM II Fairchild East Chaired by: C. TAYLOR, The MITRE Corporation 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2016-3721 AIAA-2016-3722 AIAA-2016-3723 AIAA-2016-3724 AIAA-2016-3725 AIAA-2016-3726 Analysis of Multiple Flight Aircraft Vertical Reference Lateral Reference Trajectory Proof-of-Concept Demonstrations Cruise Altitude and Speed A Vision and Roadmap for Common Route for Traffic Flow Trajectory Optimization With a Algorithm Using Ant Colony of a Flight Adjustment Logging Optimization Implemented in a Increasing User Autonomy Management RTA Constraint Using the ABC Optimization and Communication Network Pilot Decision Support Tool in Flight Operations in the K. Sheth, NASA Ames Research Algorithm A. Murrieta Mendoza, A. Hamy, M. Underwood, NASA Langley Research S. Folse, H. Tran, L. Jensen, R. National Airspace Center, Moffett Field, CA; A. Clymer, A. Murrieta Mendoza, A. Bunel, R. Botez, University of Québec, Center, Hampton, VA; D. Merlino, Hansman, Massachusetts Institute of W. Cotton, R. Hilb, National Institute

119 A. Morando, University of California, R. Botez, University of Québec, Montréal, Canada University of North Texas, Denton, TX; L. Technology, Cambridge, MA of Aerospace, Hampton, VA; S. Santa Cruz, Moffett Field, CA; F. Shih, Montréal, Canada Carboneau, Florida Gulf Coast University, Koczo, Self, Cedar Rapids, IA; D. Stinger Ghaffarian Technologies, Inc., Fort Meyers, FL; C. Wilson, University of Wing, NASA Langley Research Center, Moffett Field, CA Maryland, College Park, College Park, Hampton, VA MD; A. Wilder, University of Kentucky, Lexington, Lexington, KY Thursday, 16 June 2016 254-ATIO.ATM-22 Reliability and Safety Embassy Chaired by: J. O`CALLAGHAN, NTSB 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs AIAA-2016-3727 AIAA-2016-3728 AIAA-2016-3729 AIAA-2016-3730 AIAA-2016-3731 Air Traffic Impacts Caused by Development of a Metrics Development of Real-time Initial Case Studies Demonstrating Climbing While Turning: Lightning Safety Procedures Framework for Real-time System-wide Safety Assurance the Real-Time Safety Analysis Combat Energy Management M. Steiner, W. Deierling, K. Ikeda, System-Wide Safety Assurance Definitions and Concept Framework for the National Principles Applied to Civilian National Center for Atmospheric H. Jimenez, Georgia Institute of Fundamentals Airspace System Obstacle Clearance Research, Boulder, CO; M. Technology, Atlanta, GA; M. Blake, D. Rinehart, Architecture Technology I. Roychoudhury, Stinger Ghaffarian T. Takahashi, Arizona State University, Robinson, A. Klein, J. Bewley, AvMet Crown Consulting, Inc., Arlington, VA; Corporation, Arlington, VA; H. Technologies, Inc., Moffett Field, CA; Tempe, AZ; L. Bays, DragonFly Applications, Inc., Reston, VA; et al. J. Nowinski, NASA Ames Research Jimenez, Georgia Institute of K. Goebel, M. Daigle, NASA Ames Aeronautics, LLC, Alpharetta, GA Center, Moffett Field, CA Technology, Atlanta, GA; M. Blake, Research Center, Moffett Field, CA; S. Crown Consulting, Inc., Arlington, VA; Sankararaman, C. Kulkarni, J. Ossenfort, J. Nowinski, NASA Ames Research Stinger Ghaffarian Technologies, Inc., Center, Moffett Field, CA Moffett Field, CA; et al. Thursday, 16 June 2016 255-ATIO.ATM-23 Arrival Management Fairchild West Chaired by: S. CAMPBELL, MIT Lincoln Laboratory and T. REYNOLDS, Massachusetts Institute of Technology 1400 hrs 1430 hrs 1500 hrs 1530 hrs AIAA-2016-3732 AIAA-2016-3733 AIAA-2016-3734 AIAA-2016-3735 Assessment of Delivery An Operator-Focussed Metric Measuring Terminal Arrival Integrated Demand Management: Accuracy in an Operational Like for Measuring Predictability and Efficiency Rates using Coordinating Strategic and Tactical Environment Efficiency of Descent Operations Individual Runways Flow Scheduling Operations S. Sharma, NASA Ames Research Center, J. Bronsvoort, T. Huynh, Airservices R. Galaviz-Schomisch, J. Gulding, Z. N. Smith, C. Brasil, P. Lee, N. Buckley, Moffett Field, CA; M. Wynnyk, MITRE Australia, Melbourne, Australia; G. Enea, Zou, Federal Aviation Administration, C. Gabriel, C. Mohlenbrink, NASA Ames Corporation, McLean, VA TASC, Inc., Billerica, MA Washington, D.C. Research Center, Moffett Field, CA; et al. Thursday, 16 June 2016 256-ATIO.LTA-1 Lighter-than-Air Systems Gunston East Chaired by: R. VAN TREUREN 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs AIAA-2016-3736 AIAA-2016-3737 AIAA-2016-3738 AIAA-2016-3739 Oral Presentation Modeling Transient Heat Lighter-Than-Air (LTA) Stability Augmentation System Dynamic simulation of Airship Industry Study Transfer in Stratospheric “AirStation” - Unmanned for a Tethered Airship breakaway aerostat with R. Hochstetler, G. Chachad, SAIC, Airships Aircraft System (UAS) Carrier J. Santos, S. Stevanovic, K. Kondak, emergency deflation valves Washington, D.C.; J. Melton, NASA M. Alam, R. Pant, Indian Institute of Concept German Aerospace Center (DLR), A. Kshirsagar, R. Pant, K. Bodi, Indian Ames Research Center, Moffett Technology Bombay, Mumbai, India R. Hochstetler, SAIC, Washington, Oberpfaffenhofen, Germany; F. Institute of Technology Bombay, Field, CA D.C.; J. Bosma, Bosma & Associates, Holzapfel, Technical University of Mumbai, India Baltimore, MD; G. Chachad, SAIC, Munich, Munich, Germany; L. Góes, Washington, D.C. Technological Institute of Aeronautics (ITA), São José dos Campos, Brazil; R. Pant, Indian Institute of Technology 120 Bombay, Mumbai, India Thursday, 16 June 2016 257-ATIO.TFPC-11/ATIO. Transformational Flight - NASA Langley Autonomy Incubator Columbia 1 IS-1 Chaired by: B. ALLEN, NASA Langley Research Center 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs Oral Presentation Oral Presentation AIAA-2016-3741 Oral Presentation Oral Presentation Oral Presentation Enabling Non-UAV Pilots to A Natural Interaction Interface Bézier Curves for Safe Multi Sensor Self-Localization Using Deep Neural Networks 3D Reconstruction From Control Multiple Heterogeneous for UAVs Using Intuitive Cooperative Atmospheric for Small UAVs for MAV in-flight Object Tracked Maximally Stable UAVs Gesture Recognition Missions with Multiple L. Tran, NASA Langley Research Detection and Classification Extremal Regions (MSERs) A. Trujillo, NASA Langley Research Center, M. Chandarana, Carnegie Mellon Heterogeneous UAS Center, Hampton, VA; M. J. Neilan, D. Atha, P. Rothhaar, L. A. Hagiopol, F. Dellaert, Georgia Hampton, VA; J. Lemanski, Northrop University, Pittsburgh, PA; A. Trujillo, J. Puig-Navarro, S. Mehdi, University Chandarana, Carnegie Mellon Tran, A. Trujillo, G. Qualls, NASA Institute of Technology, Atlanta, GA; J. Grumman Corporation, Hampton, VA; B. NASA Langley Research Center, of Illinois, Urbana-Champaign, University, Pittsburgh, PA; A. Langley Research Center, Hampton, Neilan, P. Rothhaar, L. Tran, A. Trujillo, Kelley, Analytical Mechanics Associates, Hampton, VA; J. Puig-Navarro, S. Urbana, IL; A. Trujillo, P. Rothhaar, Hagiopol, Georgia Institute of VA; et al. NASA Langley Research Center, Inc., Hampton, VA; J. Puig-Navarro, S. Mehdi, University of Illinois, Urbana- NASA Langley Research Center, Technology, Atlanta, GA; J. Neilan, Hampton, VA; et al. Mehdi, University of Illinois, Urbana- Champaign, Champaign, IL; L. Tran, Hampton, VA; M. Chandarana, P. Rothhaar, NASA Langley Research Champaign, Urbana, IL; M. Chandarana, J. Neilan, NASA Langley Research Carnegie Mellon University, Center, Hampton, VA; J. Puig-Navarro, Carnegie Mellon University, Pittsburgh, Center, Hampton, VA; et al. Pittsburgh, PA; L. Tran, NASA Langley University of Illinois, Urbana- PA; et al. Research Center, Hampton, VA; et al. Champaign, Urbana, IL; et al. Thursday, 16 June 2016 258-F360-9 Aircraft Design and Testing—Today and Tomorrow International Ballroom 1400 - 1600 hrs (East) Moderator: Irene M. Gregory, Senior Technologist for Advanced Control Theory and Applications, NASA Langley Research Center Panelists: Jay Brandon Clay Harden Alan Lawless Anthony Washburn Senior Research Engineer, Flight Dynamics Branch Principal Engineer, AAP Flight Sciences Integration Chief Flight Test Engineer Langley Sr. Technologist for Aerosciences NASA Langley Research Center Gulfstream Honda Aircraft Company NASA Langley Research Center

Thursday, 16 June 2016 259-FC-16 Physics of Sweeping and Synthetic Jet Actuators Morgan Chaired by: J. SEIDEL, USAF Academy 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2016-3742 AIAA-2016-3743 AIAA-2016-3744 AIAA-2016-3745 AIAA-2016-3746 AIAA-2016-3747 Sweeping Jet Optimization Experimental and Numerical Exeprimental and Numerical Optimization of Synthetic Effect of Downstream Microjet Synthetic Jet and Turbulent Studies Study of the Frequency Studies of a Plasma Fluidic Jet Actuator design for Fluidic Injection on Mixing Boundary Layer Interaction L. Pack Melton, M. Koklu, M. Andino, Response of a Fluidic Oscillator Device for Active Flow Control noise reduction and velocity Characteristics of Supersonic Quantiﬁcation J. Lin, L. Edelman, NASA Langley for Active Flow Control L. Chen, J. Turner, M. Bacic, P. enhancement Jet D. Schatzman, J. Wilson, Army Research Center, Hampton, VA S. Wang, Beihang University, Beijing, Ireland, Oxford University, Oxford, J. Jeyalingam, M. Jabbal, Brunel H. Pourhashem, I. Kalkhoran, NYU Research, Development and China; L. Baldas, S. Colin, S. Orieux, United Kingdom University London, Uxbridge, United Tandon School of Engineering, Engineering Command, Moffett University of Toulouse, Toulouse, Kingdom Brooklyn, NY Field, CA; M. Chandrasekhara, Naval France; A. Kourta, N. Mazellier, Postgraduate School, Monterey, CA University of Orléans, Orléans, France Thursday, 16 June 2016

121 260-FC-17/FD-56 Dynamic Stall with Flow Control Columbia 11 Chaired by: J. NAUGHTON, University of Wyoming and K. GRANLUND, North Carolina State University 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2016-3748 AIAA-2016-3749 AIAA-2016-3750 AIAA-2016-3751 AIAA-2016-3752 AIAA-2016-3753 Control of Dynamically Stalled Goman-Khrabrov Model on Investigation of High- Smart rotor: controlling High-Fidelity Simulations of Numerical Investigation of Flowfield around a Pitching Airfoil a Pitching Airfoil with Flow Frequency Separation Control dynamic stall by means of an Dynamic Stall over a Finite- Helicopter Blade Section by DBD Plasma Actuator Control Mechanisms for Delay of actuated flap Aspect-Ratio Wing Undergoing Time-Periodic H. Fukumoto, University of Tokyo, D. Greenblatt, H. Mueller-Vahl, Unsteady Separation M. Raiola, A. Ianiro, S. Discetti, M. Visbal, D. Garmann, Air Force Motions Sagamihara, Japan; H. Aono, Tokyo Technion--Israel Institute of S. Benton, M. Visbal, Air Force Charles III University of Madrid, Research Laboratory, Wright-Patterson A. Gross, G. Wen, New Mexico State University of Science, Katsushika, Technology, Haifa, Israel; D. Williams, Research Laboratory, Wright-Patterson Leganés, Spain; T. Gillebaart, D. AFB, OH University, Las Cruces, NM Japan; T. Nonomura, A. Oyama, Japan Illinois Institute of Technology, AFB, OH Ragni, G. van Kuik, Delft University of Aerospace Exploration Agency (JAXA), Chicago, IL; F. Reissner, Technical Technology, Delft, The Netherlands; Sagamihara, Japan; K. Fujii, Tokyo University of Berlin, Berlin, Germany et al. University of Science, Shinjuku, Japan Thursday, 16 June 2016 261-FC-18/FD-57 Hypersonic Boundary Layer and Control Lincoln East Chaired by: D. YOUNG, Raytheon Missile Systems and T. JULIANO, University of Notre Dame 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2016-3754 AIAA-2016-3755 AIAA-2016-3756 AIAA-2016-3757 AIAA-2016-3758 AIAA-2016-3759 Spontaneous radiation of The Reynolds Number Effect Boundary-layer receptivity and Reynolds Stresses in a Reflection of Acoustic Wave in Passive hypersonic boundary sound by instability of a highly on Receptivity to a Localized breakdown in hypersonic flow Hypersonic Boundary Layer Real Atmosphere for Hypersonic layer control: The Potential of cooled hypersonic boundary Disturbance in a Hypersonic over a swept blunt wedge with with Streamline Curvature- Boundary Layer Control an Ultrasonically Absorptive layer Boundary Layer three-dimensional freestream Driven Adverse Pressure P. Lv, China Academy of Aerospace Ceramic for HEXAFLY-INT P. Chuvakhov, TsAGI, Zhukovsky, J. Sivasubramanian, A. Tumin, H. acoustic disturbances Gradients Aerodynamics, Beijing, China; T. V. Wartemann, A. Wagner, T. Eggers, Russia; A. Fedorov, Moscow Fasel, University of Arizona, Tucson, A. Cerminara, N. Sandham, University I. Neel, A. Leidy, R. Bowersox, Texas Pagliaroli, Roma Tre University, Rome, German Aerospace Center (DLR), Institute of Physics and Technology, Tucson, AZ of Southampton, Southampton, A&M University, College Station, TX; Italy; J. Gong, Y. Zhang, China Academy Braunschweig, Germany Zhukovsky, Russia United Kingdom N. Tichenor, Physics, Materials, and of Aerospace Aerodynamics, Beijing, Applied Mathematics Research, LLC, China; F. Mohd-Zawawi, University of Bryan, TX Technology, Johor Bahru, Malaysia Thursday, 16 June 2016 262-FD-58 Jet Flows II Holmead West Chaired by: D. GONZALEZ, Naval Surface Warfare Center and D. GAITONDE, The Ohio State University 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2016-3760 AIAA-2016-3761 AIAA-2016-3762 AIAA-2016-3763 AIAA-2016-3764 AIAA-2016-3765 Turbulent Characteristics of Turbulent Structure of An Investigation of A Validation Effort of a Dual, Thermal Characterization of a Investigation of the Plume Submerged Twin Jets Submerged Twin Jets Compressible Gas Jets Impinging-Jet Flow Dual Impinging Jet Flow Field Dynamics and the Near-field of a E. Essel, A. Laban, S. Mali, M. Tachie, E. Essel, A. Laban, M. Rahman, Submerged Into Water J. Valenti, M. Fronzeo, M. Kinzel, L. with a Heated Jet Supersonic Twinjet University of Manitoba, Winnipeg, M. Tachie, University of Manitoba, M. Fronzeo, M. Kinzel, Pennsylvania Myers, Pennsylvania State University, N. Rudenko, S. Hromisin, D. K. Goparaju, D. Gaitonde, S. Bhaumik, Canada Winnipeg, Canada State University, University Park, PA University Park, PA McLaughlin, Pennsylvania State Ohio State University, Columbus, OH; D. University, University Park, PA Garmann, Air Force Research Laboratory, Wright-Patterson AFB, OH Thursday, 16 June 2016 263-FD-59/FC-19/APA-38 Gust Response Columbia 10 Chaired by: K. MULLENERS, EPFL and C. TILMANN, AFRL/RQV 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2016-3766 AIAA-2016-3767 AIAA-2016-3768 AIAA-2016-3769 AIAA-2016-3770 AIAA-2016-3771 Isolated Gust Generation for Experimental investigation of 2D and 3D gust response using Linear Frequency Domain Application of Reduced Towards Experimental Validation the Investigation of Airfoil-Gust a large aspect ratio flat plate a prescribed velocity method in Reduced Order Modelling of Order Models in Aircraft Gust of Robust Control of Gust-induced Interaction encountering a steam-wise gust viscous flows Aerofoil Gust Response Response Studies Airfoil Limit Cycle Oscillations E. Hufstedler, B. McKeon, California K. Mulleners, Swiss Federal S. Huntley, D. Jones, A. Gaitonde, A. Bagheri, D. Jones, A. Gaitonde, S. Williams, D. Jones, A. Gaitonde, Using Synthetic Jet Actuators Institute of Technology, Pasadena, CA Institute of Technology, Lausanne, University of Bristol, Bristol, United University of Bristol, Bristol, United C. Wales, S. Huntley, University of S. Krishnappa, N. Jogi, L. Nguyen, S. Switzerland; P. Mancini, A. Jones, Kingdom Kingdom Bristol, Bristol, United Kingdom Gudmundsson, W. MacKunis, V. Golubev, University of Maryland, College Park, Embry-Riddle Aeronautical University, College Park, MD Daytona Beach, FL

122 Thursday, 16 June 2016 264-FD-60 Identifying the Impact of Non-Equilibrium Mechanisms on Engineering Flows (Invited) Jefferson East Chaired by: J. BURT, Universal Technology Corporation and K. STEPHANI, University of Illinois at Urbana-Champaign 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs Oral Presentation Oral Presentation Oral Presentation Oral Presentation Oral Presentation Oral Presentation Non-equilibrium Mechanisms in Recent Advancement of Non- The Role of Nonequilibrium Evaluating Effects of Aerospace Engineering The Effects of Thermal Rarefied Hypersonic Flows equilibrium Radiation in Understanding Expansions Nonequilibrium in Applications of Non-equilibrium Nonequilibrium on Instability I. Boyd, University of Michigan, Ann M. Panesi, University of Illinois, from Propulsion Flows Hypervelocity Ground Testing Plasmas Growth and Turbulent Motion Arbor, Ann Arbor, MI Urbana-Champaign, Urbana, IL; C. D. Levin, University of Illinois, Urbana- J. Austin, California Institute of I. Blankson, NASA Glenn Research G. Candler, University of Minnesota, Johnston, NASA Langley Research Champaign, Urbana, IL Technology, Pasadena, CA Center, Cleveland, OH Minneapolis, Minneapolis, MN Center, Hampton, VA Thursday, 16 June 2016 265-FD-61 Multiphase Flows II Holmead East Chaired by: D. KESSLER, Naval Research Laboratory and Q. QU 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2016-3772 AIAA-2016-3773 AIAA-2016-3774 AIAA-2016-3775 AIAA-2016-3776 AIAA-2016-3777 A model and numerical method An Arbitrary Lagrangian- Droplets Evaporation Effects Analysis of LN2 Filling, Draining, Dynamics of Redirected Investigation of Multiphase for high speed flows with Eulerian Reconstructed on Scalar Dissipation Rate in Stratification and Sloshing Flashing Jets of a Fire Flow in a Packed Bed Reactor capillary, viscous and heat Discontinuous Galerkin method Supersonic Turbulent Shear Experiments Suppression Agent under Microgravity Conditions conduction effects for Compressible Multiphase Flows M. Konopka, P. Noeding, J. Klatte, P. D. Kessler, B. Taylor, A. Corrigan, D. Y. Lian, University of Louisville, K. Schmidmayer, F. Petitpas, E. flows Z. Ren, B. Wang, Tsinghua University, Behruzi, Airbus, Bremen, Germany; J. Mott, Naval Research Laboratory, Louisville, KY; B. Motil, E. Rame, Daniel, University of Provence, A. Pandare, H. Luo, North Carolina Beijing, China Gerstmann, A. Stark, German Aerospace Washington, D.C. NASA Glenn Research Center, Marseille, France State University, Raleigh, NC Center (DLR), Bremen, Germany; et al. Cleveland, OH Thursday, 16 June 2016 266-FD-62 Shock-Dominated Flows II Oak Lawn Chaired by: C. BRUNER, Sandia National Laboratories and N. BISEK, Air Force Reseach Laboratory 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs AIAA-2016-3778 AIAA-2016-3779 AIAA-2016-3780 AIAA-2016-3781 AIAA-2016-3782 Supersonic Cones at Zero High-Fidelity Simulations of the Tapping the Brake for Entry, Performance Evaluation of A Morphing Continuum Incidence HIFiRE-6 Flow Path at Angle Descent, and Landing Turbine-Based Combination Approach to Compressible R. Ferreyra, National University of of Attack P. Gnoffo, K. Thompson, A. Korzun, Cycle Propulsion Systems with Flows: Shock Wave-Turbulent Cordoba, Córdoba, Argentina N. Bisek, Air Force Research NASA Langley Research Center, Advanced Nozzle Integration Boundary Layer Interaction Laboratory, Wright-Patterson AFB, OH Hampton, VA H. Takahashi, Japan Aerospace L. Wonnell, J. Chen, Kansas State Exploration Agency (JAXA), Kakuda, University, Manhattan, KS Japan Thursday, 16 June 2016 267-ITAR-6 NASA Orion EFT-1 Aeroscience Results - Aerodynamics Cabinet Chaired by: S. BOUSLOG, NASA-Johnson Space Center and A. BRANDIS, AMA Inc at NASA Ames 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs 1700 hrs 1730 hrs AIAA-2016-3783 AIAA-2016-3784 AIAA-2016-3785 AIAA-2016-3786 AIAA-2016-3787 AIAA-2016-3788 AIAA-2016-3789 AIAA-2016-3790 Boundary Layer Transition NASA CFD Overview for Orion Crew Module CFD Computational Assessment of Numerical Simulations of Infrared Observations of the Processing Near-Infrared Imagery Comparisons Between Pretest During the Orion Exploration Orion’s Aerodynamic Database Validation from Wind Tunnel to Orion Command-Module RCS Jet Afterbody Heating on the Orion Orion Capsule During EFT-1 of the Orion Heatshield During Prediction and Flight Test Flight Test 1 (EFT-1) Development Exploration Flight Test-1 Interaction Multi-Purpose Crew Vehicle for Hypersonic Re-entry EFT-1 Hypersonic Reentry Data of Aerodynamic Loads L. Kirk, NASA Johnson Space Center, J. Garcia, S. Rogers, S. Murman, J. R. Childs, Science and Technology S. Rogers, NASA Ames Research Center, the Exploration Flight Test 1 T. Horvath, S. Rufer, D. Schuster, NASA T. Spisz, J. Taylor, D. Gibson, S. Kennerly, for EFT-1 Houston, TX Melton, NASA Ames Research Center, Corporation, Hampton, VA; J. Garcia, Moffett Field, CA; A. Schwing, D. Vicker, C. Tang, NASA Ames Research Center, Langley Research Center, Hampton, VA; K. Osei-Wusu, Johns Hopkins University A. Schwing, NASA Johnson Space Moffett Field, CA; J. Greathouse, D. S. Murman, S. Rogers, NASA Ames NASA Johnson Space Center, Houston, Moffett Field, CA G. Mendeck, B. Oliver, NASA Johnson Applied Physics Laboratory, Laurel, MD; T. Center, Houston, TX Vicker, NASA Johnson Space Center, Research Center, Moffett Field, CA; TX; K. Bibb, NASA Langley Research Space Center, Houston, TX; R. Schwartz, Horvath, NASA Langley Research Center, Houston, TX; et al. J. Greathouse, NASA Johnson Space Center, Hampton, VA NASA Langley Research Center, Hampton, VA; et al.

123 Center, Houston, TX Hampton, VA; et al. Thursday, 16 June 2016 268-MAO-16 Surrogate Modeling and Non-Deterministic Design - Methods and Applications II Cardozo Chaired by: E. BOEKELOO, Boeing and V. KALIVARAPU, Iowa State University 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs AIAA-2016-3791 AIAA-2016-3792 AIAA-2016-3793 AIAA-2016-3794 AIAA-2016-3795 Polynomial Chaos A Probabilistic Multi-Fidelity Reliability based design Reliability estimation for low Aeroelastic Optimization of Decomposition with Aero-Engine Preliminary Design optimization of structures cycle fatigue life of a gas Flap-gliding Micro Air Vehicle Differentiation Operation Optimization Framework: considering several incomplete turbine disk wings M. Thapa, S. Mulani, University of Technical and Commercial configurations H. Feng, Y. Wang, X. Jiang, Beihang D. Xue, B. Song, W. Song, W. Yang, Alabama, Tuscaloosa, Tuscaloosa, Perspectives C. Cid, A. Baldomir, S. Hernandez, University, Beijing, China Z. Han, Northwestern Polytechnical AL; R. Walters, Virginia Polytechnic J. Gramatyka, M. Eres, J. Scanlan, University of A Coruña, A Coruña, University, Xi’an, China Institute and State University, University of Southampton, Spain Blacksburg, VA Southampton, United Kingdom; M. Moss, P. Holloway, R. Bates, Rolls-Royce Group plc, Derby, United Kingdom Thursday, 16 June 2016 269-MAO-17 Emerging Methods, Algorithms, and Large Scale Applications in MAO I Columbia 4 Chaired by: D. ALLAIRE, Texas A&M University and B. STANFORD, NASA Langley Research Center 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2016-3796 AIAA-2016-3797 AIAA-2016-3798 AIAA-2016-3799 AIAA-2016-3800 AIAA-2016-3801 Multi-Fidelity Design On Active Subspaces in Car Design Space Dimensionality A Deterministic Constrained Optimization of Turbine Engine Adaptive Cell Network Design Optimization via Low-Fidelity Aerodynamics Reduction for Single- and Global Optimization Algorithm Cycle Analysis with Analytic Using S.A.N.DY For A Battery Correction Technique C. Othmer, Volkswagen of America, Multi-Disciplinary Shape Without Penalty Function Derivatives Pack-Switching Algorithm aNd C. Fischer, R. Grandhi, Wright State Inc., Belmont, CA; T. Lukaczyk, Optimization J. Kou, T. Long, Z. Wang, Y. Wen, L. T. Hearn, E. Hendricks, J. Chin, J. cell DYnamics (S.A.N.DY), A University, Dayton, OH Stanford University, Stanford, CA; M. Diez, A. Serani, E. Campana, Liu, Beijing Institute of Technology, Gray, NASA Glenn Research Center, Novel Approach For Optimum P. Constantine, Colorado School Italian Institute for Naval Beijing, China Cleveland, OH Discharging/Charging Of A of Mines, Golden, CO; J. Alonso, Hydrodynamic Research and Ship Stanford University, Stanford, CA Lithium-Polymer Battery Pack Model Basin, Rome, Italy; F. Stern, For Hybrid/Electric UAVs. - University of Iowa, Iowa City, Iowa J. Mishra, Siddaganga Institute of City, IA Technology, Tumkur, India Thursday, 16 June 2016 270-MST-15 Special Modeling and Simulation Topics Georgetown East Chaired by: F. CARDULLO, State University of NY and P. ZAAL, NASA Ames Research Center 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs AIAA-2016-3802 AIAA-2016-3803 AIAA-2016-3804 AIAA-2016-3805 AIAA-2016-3806 Objective ARX Model Order Key Performance Indicator Analytical Determination of Modeling Carbon Tax Policy Modeling and Simulation of Selection for Multi-Channel for Security Measurement at Trim Values for Nonlinear Fixed Impacts on U.S. Commercial Rectangular Cable in Application Human Operator Identification Airports Wing Aircraft Models Airlines using Agent-Based of Optimization of the Main N. Roggenkämper, D. Pool, Delft O. Milbredt, A. Deutschmann, M. Rhudy, Pennsylvania State Modeling and Crowdsourced Feeder Wiring Strategy University of Technology, Delft, The German Aerospace Center (DLR), University, Reading, PA Data Y. Zhang, L. Wang, L. Ruan, Nanjing 124 Netherlands; F. Drop, Max Planck Braunschweig, Germany B. Horio, V. Kumar, D. Levin, P. Sung, University of Aeronautics and Institute for Biological Cybernetics, LMI, Tysons, VA Astronautics, Nanjing, China; Y. Hui, Tübingen, Germany; M. van Paassen, Commercial Aircraft Corporation of China, M. Mulder, Delft University of Ltd. (COMAC), Beijing, China; J. Zhao, Technology, Delft, The Netherlands Shanghai Aircraft Design and Research Institute, Shanghai, China Thursday, 16 June 2016 271-PDL-7 Plasma Aerodynamics Gunston West Chaired by: A. STARIKOVSKIY, Princeton University and S. LEONOV, University of Notre Dame 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs 1630 hrs AIAA-2016-3807 AIAA-2016-3808 AIAA-2016-3809 AIAA-2016-3810 AIAA-2016-3811 AIAA-2016-3812 Transient Plasma Impact on Numerical Rebuilding of Shock Controllable Shock Wave Ionization Processes in Combined Trajectory Control of Small Aerodynamic Effects of Spectra of Flow Disturbances Layer Ionization for Two Flight Generation by Near-Surface High-Voltage Nanosecond – Laser Rotating Projectiles by Laser Microwave-Excited Plasmas in a Corner Separation Zone at Tests Electrical Discharge Discharges in Inert Gas Discharges N. Hu, X. Shi, H. Ma, China Academy Mach 4.5 S. Surzhikov, Russian Academy of S. Leonov, A. Houpt, B. Hedlund, I. Semenov, University of Maryland, A. Starikovskiy, Princeton University, of Aerospace Aerodynamics, Beijing, A. Houpt, B. Hedlund, S. Gordeyev, Sciences, Moscow, Russia University of Notre Dame, Notre Dame, College Park, College Park, MD; A. Princeton, NJ China T. Juliano, S. Leonov, University of IN; T. Ombrello, Air Force Research Starikovskiy, M. Shneider, Princeton Notre Dame, Notre Dame, IN Laboratory, Wright-Patterson AFB, OH University, Princeton, NJ Thursday, 16 June 2016 272-TP-11 Thermophysics DuPont Chaired by: D. HENGEVELD and K. IRICK 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs AIAA-2016-3813 AIAA-2016-3814 AIAA-2016-3815 AIAA-2016-3816 AIAA-2016-3817 Fluid Flow Through Tree-Like PLIF Experiments on Analysis of opportunities for Numerical study on heat transfer Influences of Multi- Networks of Varying Scale Evaporating Isolated Droplet comparing models of effective in aeronautical systems using Temperature Models on the D. Calamas, L. Zamora, Georgia and Droplets Array thermal conductivity different conductivity laws and Shock Structures of Weakly Southern University, Statesboro, H. Rehman, A. Mohammed-Taifour, J. R. Wyczolkowski, H. Radomiak, T. different materials Ionized Hypersonic Flows GA; D. Dannelley, Embry-Riddle Weiss, P. Seers, École de Technologie Wylecial, D. Urbaniak, Czestochowa A. Carozza, Italian Aerospace Research P. Raghunandan, S. Ruffin, Georgia Aeronautical University, Prescott, AZ Supérieure, Montréal, Canada University of Technology, Center (CIRA), San Marco Evangelista, Institute of Technology, Atlanta, GA Czestochowa, Poland Italy Thursday, 16 June 2016 273-TP-12 Advanced Modeling III - DNS and State to State Jay Chaired by: S. MUPPIDI and C. JOHNSTON, NASA-Langley Research Center 1400 hrs 1430 hrs 1500 hrs 1530 hrs 1600 hrs AIAA-2016-3818 AIAA-2016-3819 AIAA-2016-3820 AIAA-2016-3821 AIAA-2016-3822 Rovibrational grouping for State-to-State Kinetic Modeling Numerical Modeling of A Coupled Vibration- Analysis of Dissociation and 1 + 1 + N2( Σ g)-N2( Σ g) energy of Oxygen in Hypersonic Reacting Turbulence Using Dissociation Model for Internal Energy Transfer in High- transfer using state-to-state Nonequilibrium Flows State-to-State Kinetic Approach Nitrogen from Direct Molecular Energy N2+O2 Collisions using the model E. Josyula, J. Burt, Air Force Research for High Speed ISR Missions Simulation Quasiclassical Trajectory Method R. Macdonald, A. Munafò, M. Laboratory, Wright-Patterson AFB, K. Vogiatzis, Engility Corporation, N. Singh, P. Valentini, T. R. Chaudhry, J. Bender, P. Valentini, T. Panesi, University of Illinois, Urbana- OH; V. Laporta, National Research Dayton, OH; P. Vedula, University Schwartzentruber, University of Schwartzentruber, G. Candler, University Champaign, Urbana, IL Council (CNR), Bari, Italy; P. Vedula, of Oklahoma, Norman, Norman, Minnesota, Minneapolis, Minneapolis, of Minnesota, Minneapolis, Minneapolis, University of Oklahoma, Norman, OK; E. Josyula, Air Force Research MN MN

125 Norman, OK Laboratory, Wright-Patterson AFB, OH Thursday, 16 June 2016 274-NW-8 Networking Coffee Break Meeting Room Foyers 1600 - 1630 hrs 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. Thursday, 16 June 2016 275-D4U-3 DEMAND for UNMANNED Student Competition Alpha Test International Ballroom 1730 - 1900 hrs (Center) Teams from the University of Michigan, University of Maryland, and McKinley Technology High School in Washington, D.C., will use a UAV quadrotor to participate in a two-part competition that includes autonomy and manual flight skills. Thursday, 16 June 2016 276-LEC-6 Aerodynamic Measurement Technology Award Lecture International Ballroom 1730 - 1830 hrs (East) CARS – The First Twenty Years Alan C. Eckbreth Management/Engineering Consultant Friday Friday, 17 June 2016 277-SB-5 Speakers’ Briefing Session Rooms 0730 - 0800 hrs 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 session to exchange bios and review final details prior to the session. Please attend on the day of your session. Friday, 17 June 2016 278-PLNRY-6 Plenary International Ballroom 0800 - 0900 hrs (Center) Concept to Reality—Our Journey to Transforming Aviation Charles F. Bolden Jr. Administrator NASA Friday, 17 June 2016 279-NW-9 Networking Coffee Break Meeting Room Foyers 0900 - 0930 hrs 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. Friday, 17 June 2016 280-AMT-11 Flow Visualization and Data Acquisition Methods Columbia 2 Chaired by: T. MIZUKAKI, Tokai University and G. JONES, NASA-Langley Research Center 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2016-3823 AIAA-2016-3824 AIAA-2016-3825 AIAA-2016-3826 AIAA-2016-3827

126 Developing an Image-Based Investigation of a Cylinder- Features of the Upgraded Low-Cost Arduino-Based Studies of a Hot Wire Analysis of the Dynamics of Induced Transitional Shock Wave- Imaging for Hypersonic Data Acquisition System with Anemometer with Digital Transitional Shock Wave- Boundary Layer Interaction using Experimental Aeroheating Android Mobile Interface for Feedback Boundary Layer Interactions Laser Diagnostics Testing (IHEAT) Software Undergraduate Aerodynamics C. Britcher, Old Dominion University, E. Lash, C. Combs, J. Schmisseur, E. C. Combs, E. Lash, J. Schmisseur, M. Mason, S. Rufer, NASA Langley Laboratories Norfolk, VA; R. White, J. Bledsoe, A. Beckman, University of Tennessee, University of Tennessee, Tullahoma, Research Center, Hampton, VA Q. Schwaab, J. Weiss, C. Belleau, Favaregh, ViGYAN, Inc., Hampton, VA Tullahoma, Tullahoma, TN Tullahoma, TN F. Morency, University of Québec, Montréal, Canada Friday, 17 June 2016 281-APA-39 Aerodynamic Design Methodologies IV Albright Chaired by: M. SCHOENENBERGER, NASA-Langley Research Center 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2016-3828 AIAA-2016-3829 AIAA-2016-3830 AIAA-2016-3831 AIAA-2016-3832 AIAA-2016-3833 Evaluation of Reduced-Order Natural Laminar Flow Design Expanding the Natural Laminar Towards an Effective Nonplanar Revisiting the Transonic Aerodynamic Design Guidelines Models for Predictions of for Wings with Moderate Sweep Flow Boundary for Supersonic Wing Design Strategy Similarity Rule: Critical Mach of Aircraft Dorsal Fin Separated and Vortical Flows R. Campbell, M. Lynde, NASA Langley Transports M. Lee, K. Visser, Clarkson University, Number Prediction Using F. Nicolosi, D. Ciliberti, P. Della R. Darragh, P. Hamlington, University Research Center, Hampton, VA M. Lynde, R. Campbell, NASA Langley Potsdam, NY Potential Flow Solutions Vecchia, University of Naples of Colorado, Boulder, Boulder, CO; Research Center, Hampton, VA J. Kirkman, T. Takahashi, Arizona “Federico II”, Naples, Italy M. Ghoreyshi, A. Lofthouse, U.S. Air State University, Tempe, AZ Force Academy, Colorado Springs, CO Friday, 17 June 2016 282-APA-40 Weapons Aerodynamics: Missile/Projectile/Guided-Munitions, Carriage and Store Separation Columbia 9 Chaired by: C. PASILIAO, AFRL/RWWV and J. DOYLE, US Army AMRDEC 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2016-3834 AIAA-2016-3835 AIAA-2016-3836 AIAA-2016-3837 AIAA-2016-3838 AIAA-2016-3839 Numerical Study on Bending Flight Behaviors of a Complex A Computationally Efficient, Nonlinear Rolling Motion of Store Separation Analyses by CFD Based Response Surface Body Projectile Aerodynamics Projectile using a Coupled CFD- Multi-fidelity Assessment of Triform Finned Missiles Means of Response Surface Modeling with an Application in E. Youn, U.S. Military Academy, West based Simulation Technique: Jet Interactions for Highly J. Morote, G. Liaño, J. Jiménez, Modeling Missile Aerodynamics Point, NY; S. Silton, Army Research Closed-loop Control Maneuverable Missiles National Institute of Aerospace O. Özgür, A. Çetiner, B. Yagiz, G. A. Çetiner, B. Yagiz, G. Guzel, O. Laboratory, Aberdeen Proving J. Sahu, F. Fresconi, Army Research A. Vanderwyst, A. Shelton, C. Martin, Technology (INTA), Madrid, Spain Guzel, ASELSAN, Inc., Ankara, Turkey Özgür, I. Koc, ASELSAN, Inc., Ankara, Ground, MD Laboratory, Aberdeen Proving Leidos, Fort Walton Beach, FL Turkey Ground, MD Friday, 17 June 2016 283-APA-41/FD-63 Low Speed, Low Reynolds Number Aerodynamics Jefferson East Chaired by: M. GREEN, Syracuse University and M. YU, University of Maryland, Baltimore County 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2016-3840 AIAA-2016-3841 AIAA-2016-3842 AIAA-2016-3843 AIAA-2016-3844 AIAA-2016-3845 Evolution of the Non-linear Toward Simulating a Pitch- Quantification and Analysis of Modeling of Pitching and Experimental Investigation An experimental and numerical and Unsteady Low Reynolds Up Maneuver for a Small Propulsive Wake Topologies in Plunging Airfoils in Proximity of Aspect-Ratio-One Wing study of laminar separation on Number Laminar Separation Unmanned Aerial Vehicle Finite Aspect-Ratio Pitching- for Thrust Generation Characteristics at Low Reynolds elliptic airfoil at low Reynolds Bubble around the Airfoil with J. Blake, D. Thompson, Mississippi Rolling Plates A. Povitsky, University of Akron, Numbers numbers Small angle of attack State University, Mississippi State, C. Li, H. Dong, University of Virginia, Akron, OH M. Mizoguchi, H. Itoh, National L. Yang, X. Meng, X. Yan, B. Peng, F. Li, Q. Liu, H. Zhan, China MS Charlottesville, Charlottesville, VA Defense Academy, Yokosuka, Japan Northwestern Polytechnical University, Academy of Aerospace Aerodynamics, Xi’an, China; F. Liu, S. Luo, University Beijing, China of California, Irvine, Irvine, CA 127 Friday, 17 June 2016 284-APA-42/FD-64 Vortex/Vortical Flows II Northwest Chaired by: M. OL, US Air Force Reseach Laboratory and G. GATLIN, NASA Langley Research Center 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2016-3846 AIAA-2016-3847 AIAA-2016-3848 AIAA-2016-3849 AIAA-2016-3850 AIAA-2016-3851 Further Investigations of the Effect of Upsweep Angle on Vortical Flow Structure Genesis Co-rotating equal strength Dynamical System Analysis on Flow Past Rotating Low Axis Tip Vortex on an Oscillating Afterbody Vortices of Lobed Nozzle Flows vortex pair merging in the Onset of Recirculating Flow Ratio Elliptic Cylinder NACA0012 Wing D. Bulathsinghala, Z. Wang, I. Gursul, M. Ruetten, German Aerospace pressure gradient environment Region Associated with Vorex S. Naik, S. Vengadesan, K. Arul, D. Garmann, M. Visbal, Air Force University of Bath, Bath, United Center (DLR), Göttingen, Germany; Y. Yi, P. Liu, T. Hu, Beihang University, Breakdown Indian Institute of Technology Research Laboratory, Wright-Patterson Kingdom F. Woldegiorgis, University of Kassel, Beijing, China K. Yamada, University of Tokyo, Madras, Chennai, India AFB, OH Kassel, Germany Bunkyo, Japan; K. Suzuki, University of Tokyo, Kashiwa, Japan Friday, 17 June 2016 285-ASE-17 Icing CFD Georgetown West Chaired by: M. POTAPCZUK, NASA Glenn Research Center and D. THOMPSON, Mississippi State University 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2016-3852 AIAA-2016-3853 AIAA-2016-3854 AIAA-2016-3855 AIAA-2016-3856 Validation Process for LEWICE Simulations of ice accretion, Sensitivity analysis of ice piece Atmospheric Considerations of Multi-physics Simulation of by Use of a Naviér-Stokes runback and droplet re- trajectory calculation the Cercigani, Lampis, and Lord Aircraft Ice Protection System Solver emission in a multi-stage L. Védie, University of Bordeaux, Model for Gas-Surface Interaction and Ice Impact with Turbofan W. Wright, Vantage Partners, LLC, model of aeronautical engine Boredeaux, France; F. Morency, École in DSMC Simulations Blades Cleveland, OH G. Gomez de Segura Solay, E. de Technologie Supérieure, Montréal, P. Braden, Joint Information Operations G. Baruzzi, M. Oswald, A. Pett, B. Radenac, R. Chauvin, C. Laurent, Canada; N. Kubler, University of Warfare Center, Lackland AFB, TX Gerber, P. Rajarao, B. Sasanapuri, ONERA, Toulouse, France Toulouse, Chasseneuil-du-Poitou, France ANSYS, Inc., Pune, India; et al. Friday, 17 June 2016 286-ATIO.ATM-24 NextGen and Future Concepts Embassy Chaired by: D. DELAURENTIS, Purdue University 0930 hrs 1000 hrs 1030 hrs AIAA-2016-3857 AIAA-2016-3858 AIAA-2016-3859 Cyber- Threat Assessment for NextGen Far-Term Concept Role of Extended Projected Profile the Air Traffic Management Exploration for Integrated Down-Link to Achieve Trajectory System: A Network Controls Gate-to-Gate Trajectory-Based Synchronisation in support of Approach Operations Trajectory Based Operations S. Roy, Washington State University, S. Johnson, Adaptive Aerospace J. Bronsvoort, Airservices Australia, Pullman, WA; B. Sridhar, NASA Ames Group, Inc., Hampton, VA; B. Melbourne, Australia; G. McDonald, Research Center, Moffett Field, CA Barmore, NASA Langley Research Self, Melbourne, Australia; S. Torres, Center, Hampton, VA Lockheed Martin Corporation, Arlington, VA; M. Paglione, C. Young, Federal Aviation Administration, Atlantic City, NJ; J. Hochwarth, General Electric Company, Grand Rapids, MI; et al. Friday, 17 June 2016 287-ATIO.ATM-25 Optimal Flight Routes Fairchild West Chaired by: M. UNDERWOOD, NASA Langley Research Center 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2016-3860 AIAA-2016-3861 AIAA-2016-3862 AIAA-2016-3863 AIAA-2016-3864 Optimized Route Capability Oceanic Flights and Airspace: Measuring Flight Efficiency in Wind-optimal ATS Route Computing Wind-Optimal (ORC) Intelligent Offloading of Improving Efficiency by the National Airspace System Redesign: A Methodology and Routes for Flight Performance Congested Arrival Routes Trajectory-Based Operations J. DeArmon, W. Cooper, T. Masek, A. its Application to Route A461 Benchmarking Tien, MITRE Corporation, McLean, VA 128 S. Zelinski, NASA Ames Research A. Fernandes, J. Rebollo, Mosaic in China F. Cheng, J. Gulding, Federal Aviation Center, Moffett Field, CA; M. Xue, ATM, Inc., Leesburg, VA; M. Koch, M. Swaid, German Aerospace Center Administration, Washington, D.C. University of California, Santa Cruz, NASA Langley Research Center, (DLR), Hamburg, Germany; K. Cai, Moffett Field, CA; P. Bassett, Federal Hampton, VA National Key Laboratory of CNS/ATM, Aviation Administration, Washington, Beihang University, Beijing, China; D.C. F. Linke, German Aerospace Center (DLR), Hamburg, Germany; B. Lührs, V. Gollnick, Institute of Air Transportation Systems,Hamburg University of Technology, Hamburg, Germany Friday, 17 June 2016 288-ATIO.ATM-26 Safe Landings Fairchild East Chaired by: S. CAMPBELL, MIT Lincoln Laboratory 0930 hrs 1000 hrs 1030 hrs AIAA-2016-3865 AIAA-2016-3866 AIAA-2016-3867 Development of Airport Low-level Uncertainty Analysis for Slippery When Wet: The Case Wind Information (ALWIN) Calculating Reverse Thrust for More Conservative Wet N. Matayoshi, T. Iijima, Japan Aerospace using In Situ Data Runway Braking Coefficient Exploration Agency (JAXA), Mitaka, A. Campbell, A. Cheng, Federal Models Japan; K. Yamamoto, E. Fujita, Japan Aviation Administration, Atlantic J. O`Callaghan, National Meteorological Agency, Choyoda, Japan City, NJ Transportation Safety Board, Washington, D.C. Friday, 17 June 2016 289-ATIO.GA-3 Environmentally-Conscious Concepts and Technologies for General Aviation Gunston East Chaired by: K. HOFFLER, Adaptive Aerospace Group, Inc. 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2016-3868 AIAA-2016-3869 AIAA-2016-3870 AIAA-2016-3871 Prediction of Community Noise Fuel Flow Rate and Duration of Sustainability assessment of Open loop morphing wing Impacts from Commercialization General Aviation Landing and hydro-processed renewable architecture based ANFIS of Vertical Takeoff and Landing Takeoff Cycle jet fuel from algae from controller Personal Air Vehicles C. Huang, M. Johnson, Purdue market-entry year 2020: Use D. Nguyen, M. Tchatchueng J. Kim, D. Lim, S. Min, D. Mavris, University, West Lafayette, IN in passenger aircrafts Kammegne, R. Botez, L. Grigorie, Georgia Institute of Technology, S. Jagtap, Georgia Institute of University of Québec, Montréal, Atlanta, GA Technology, Atlanta, GA Canada Friday, 17 June 2016 290-ATIO.TFPC-12 Transformational Flight - UAS Emerging Markets and Technologies Columbia 1 Chaired by: S. BRICENO, Georgia Institute of Technology and A. GIBSON, Empirical Systems Aerospace 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2016-3872 AIAA-2016-3873 AIAA-2016-3874 AIAA-2016-3875 AIAA-2016-3876 An Unmanned VTOL and Fixed An Airborne Package Retrieval & Evaluation of Concepts of Mission Analysis of Solar, High- Assessing the Impact of Wing Vehicle Equipped for Delivery System with Mechanized Operations for sUAS Package Altitude, Long-Endurance UAVs Operational Constraints on the Package Retrieval and Delivery CG Relocation Delivery for Weather Operations Near-Term Unmanned Aircraft Z. Bassett, University of Texas, Austin, Z. Bassett, University of Texas, Austin, D. Locascio, M. Levy, K. Ravikumar, C. Chamchalaem, A. Drake, California System Traffic Management Austin, TX; M. Holdren, Case Western Austin, TX; M. Holdren, Case Western H. Maniar, B. German, S. Briceno, Polytechnic State University, San Luis Supported Market Reserve University, Cleveland, OH; Reserve University, Cleveland, OH; D. Georgia Institute of Technology, Obispo, CA P. Vascik, Massachusetts Institute of D. Vutetakis, University of North Vutetakis, University of North Carolina, Atlanta, GA; et al. Technology, Cambridge, MA; J. Jung, Carolina, Charlotte, Charlotte, NC; A. Charlotte, Charlotte, NC; A. Bass, NASA Ames Research Center, Moffett

129 Bass, Illinois Institute of Technology, Illinois Institute of Technology, Chicago, Field, CA Chicago, IL; P. Finch , New York IL; H. Kwan, State University of New University, New York , NY; A. Flock , York, Buffalo, NY; P. Finch , New York Kent State University, Kent, OH; et al. University, New York, NY; et al. Friday, 17 June 2016 291-ATIO.TFPC-13/ATIO. Transformational Flight - Clean Slate Design for Autonomy in Vehicles and Airspace Gunston West ATM-27 Chaired by: N. ALEXANDROV, NASA Langley Research Center and T. LEWIS, NASA Langley Research Center 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2016-3877 AIAA-2016-3878 AIAA-2016-3879 AIAA-2016-3880 AIAA-2016-3881 Design for Survivability: An Flight Simulation of Clean-Slate Probabilistic Modeling of Entropy-based Design of Air Toward n-Ship Computation of Approach to Assured Autonomy (Ab Initio) National Airspace Aircraft Trajectories for Trafﬁc Management Trajectories for Shared Airspace N. Alexandrov, NASA Langley System (NAS) Designs Dynamic Separation Volumes M. Lowry, NASA Ames Research D. Moerder, R. Butler, P. Rothhaar, Research Center, Hampton, VA; B. Allen, J. Neilan, P. Rothhaar, L. Tran, T. Lewis, NASA Langley Research Center, Moffett Field, CA NASA Langley Research Center, T. Ozoroski, Analytical Mechanics A. Trujillo, N. Alexandrov, NASA Langley Center, Hampton, VA Hampton, VA Associates, Inc., Hampton, VA Research Center, Hampton, VA Friday, 17 June 2016 292-F360-10 Hypersonic and Re-Entry Flight Testing—X-15 to Space Shuttle and Beyond International Ballroom 0930 - 1130 hrs (East) Moderator: Sandra H. Magnus, Executive Director, AIAA

Panelists: Doug Cooke Colonel Lee Archambault Major General Joe H. Engle John Olson Principal Chief Systems Engineer and Test Pilot United States Air Force, Air National Guard (Ret.) and Vice PresidentSpace Exploration Systems Cooke Concepts and Solutions Sierra Nevada Corporation NASA Astronaut (Ret.) Sierra Nevada Corporation United States Air Force (Ret.) and NASA Astronaut (Ret.) Friday, 17 June 2016 293-FD-65 Roughness-Induced Transition Lincoln East Chaired by: E. WHITE, Texas A&M University and P. SUBBAREDDY 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2016-3882 AIAA-2016-3883 AIAA-2016-3884 AIAA-2016-3885 AIAA-2016-3886 AIAA-2016-3887 Numerical Simulation of Trip-induced transition of Compressible Boundary Layer Wake flow instability studies BiGlobal Stability Analysis of a Understanding the Effects of Interactions Between Görtler a Mach 5.65 low Reynolds Receptivity to Freestream behind discrete roughness Micro-Ramp Wake using PIV Surface Roughness on the Vortex and Roughness-Induced number boundary layer Disturbances and Step elements on a generic re-entry Base Flows Growth of Disturbances Disturbances in Hypersonic P. Shrestha, G. Candler, University of Excrescences: Numerical Study capsule K. Groot, Q. Ye, Delft University of M. Gaster, City University London, Boundary Layers Minnesota, Twin Cities, Minneapolis, A. Sescu, S. Yassir, Mississippi State A. Theiss, S. Hein, German Aerospace Technology, Delft, The Netherlands; Y. London, United Kingdom M. Yu, Z. Zhu, X. Yuan, China MN University, Starkville, MS; M. Visbal, Center (DLR), Göttingen, Germany; S. Zhang, Nanjing University of Aeronautics Academy of Aerospace Aerodynamics, Air Force Research Laboratory, Wright- Ali, R. Radespiel, Technical University and Astronautics, Nanjing, China; F. Beijing, China Patterson AFB, OH of Braunschweig, Braunschweig, Pinna, von Kármán Institute for Fluid Germany Dynamics, Rhode-Saint-Genèse, Belgium; B. van Oudheusden, Delft University of Technology, Delft, The Netherlands Friday, 17 June 2016 294-FD-66 Flow Stability Kalorama Chaired by: Z. RUSAK, Rensselaer Polytechnic Institute and D. ZHAO, Nanyang Technological University 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2016-3888 AIAA-2016-3889 AIAA-2016-3890 AIAA-2016-3891 A classical linear stability Numerical study of transonic The Dynamics of Three- Flow Simulations of The Dynamics analysis of normal mode shock buffet instability Dimensional Perturbations a of a Perturbed Solid-Body instability of the compressible mechanism Solid-Body Rotation Flow in a Rotation Flow planar mixing-layer flow of a Y. Liu, G. Wang, S. Zhu, Z. Ye, Circular Pipe C. Feng, Northwestern Polytechnical Northwestern Polytechnical University, University, Xi’an, China; Y. Liu, Peking 130 supercritical fluid R. Gong, S. Wang, University of L. Alves, Fluminese Federal University Xi’an, China Auckland, Auckland, New Zealand; University, Beijing, China; F. Liu, (UFF), Niterói, Brazil Z. Rusak, Rensselaer Polytechnic University of California, Irvine, Irvine, Institute, Troy, NY CA; Z. Rusak, Rensselaer Polytechnic Institute, Troy, NY; S. Wang, University of Auckland, Auckland, New Zealand Friday, 17 June 2016 295-FD-67 Computational Modeling for Propulsion Applications Columbia 10 Chaired by: L. VILLASMIL, Rochester Institute of Technology and X. GAO, Colorado State Univ 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs AIAA-2016-3892 AIAA-2016-3893 AIAA-2016-3894 AIAA-2016-3895 AIAA-2016-3896 Advanced Modelling of Numerical Investigation of Scramjet Combustor Flow Numerical Simulations of Gas- Evaluation of CFD Codes for Turbulent Heat-Flux in Asymmetric Lobe Structure on Analysis Using Coupled Centered Swirl-Coaxial Injectors Swirl-Driven Combustors Turbofan Engines with Lobed Aerodynamic Performance of a Navier-Stokes and Finite Rate for Rocket Engine Applications. G. Talamantes, B. Maicke, Mixers Lobed S-Shaped Nozzle Chemical Equations Evaluating the ability of Pennsylvania State University, J. Trümner, C. Mundt, University of L. Du, Y. Liu, Y. Ding, H. Ren, R. Rouzbar, S. Eyi, Middle East “standard” turbulence models in Middletown, PA the German Federal Armed Forces, Beihang University, Beijing, China Technical University, Ankara, Turkey capturing the complex nature of Neubiberg, Germany spray atomization. L. Villasmil, Rochester Institute of Technology, Rochester, NY; S. Danczyk, M. Lightfoot, S. Shumaker, A. Himansu, Air Force Research Laboratory, Edwards AFB, CA Friday, 17 June 2016 296-FD-68 Theoretical/Fundamental Fluid Dynamics Columbia 12 Chaired by: A. GOPALARATHNAM, North Carolina State University and G. ARAYA, University of Puerto Rico Mayaguez 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2016-3897 AIAA-2016-3898 AIAA-2016-3899 AIAA-2016-3900 Advanced Kinetic Theory Spatio-Temporal Response of Phase relationships between velocity, Spatial Evolution of Large Scale for Polyatomic Gases at a Laminar Separation Bubble wall pressure, and wall shear stress in Structures in Supersonic Shear Equilibrium Under Impulsive Forcing a forced turbulent boundary layer Layers J. Chen, Kansas State University, T. Michelis, M. Kotsonis, Delft K. Rosenberg, S. Duvvuri, M. Luhar, B. X. Shi, G. Zhang, W. Wang, T. Manhattan, KS University of Technology, Delft, The McKeon, California Institute of Technology, Wang, China Academy of Aerospace Netherlands Pasadena, CA; C. Barnard, B. Freidkes, Aerodynamics, Beijing, China; C. Shu, University of Florida, Gainesville, Gainesville, Brown University, Providence, RI FL; et al. Friday, 17 June 2016 297-FD-69 Uncertainty Quantification and Sensitivity Analysis Morgan Chaired by: Q. WANG, MIT and K. DURAISAMY, University of Michigan, Ann Arbor 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2016-3901 AIAA-2016-3902 AIAA-2016-3903 AIAA-2016-3904 A Multi Level Monte Carlo Sensitivity analysis on The Effect of Grid Topology and Uncertainty Quantification of Algorithm for the Treatment of chaotic dynamical system by Flow Solver on Turbulence Model Turbulence Model Coefficients Geometrical and Operational Non-Intrusive Least Square Closure Coefficient Uncertainties in OpenFOAM and Fluent for Uncertainties in Internal and Shadowing (NI-LSS) for a Transonic Airfoil Mildly Separated Flows External Aerodynamics A. Ni, P. Blonigan, M. Chater, Q. J. Schaefer, The Boeing Company, Saint K. Stephanopoulos, I. Witte, T. Wray, M. Pisaroni, P. Leyland, F. Nobile, Wang, Massachusetts Institute of Louis, MO; S. Hosder, Missouri University R. Agarwal, Washington University in Swiss Federal Institute of Technology, Technology, Cambridge, MA of Science and Technology, Rolla, MO; St. Louis, St. Louis, MO

131 Lausanne, Switzerland M. Mani, A. Cary, J. Krakos, The Boeing Company, Saint Louis, MO Friday, 17 June 2016 298-ITAR-7 NASA Orion EFT-1 Thermal Protection System Cabinet Chaired by: B. CRUDEN, ERC Inc at NASA Ames Research Center and R. THOMPSON, NASA-Langley Research Center 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2016-3905 AIAA-2016-3906 AIAA-2016-3907 AIAA-2016-3908 AIAA-2016-3909 AIAA-2016-3910 Development, Manufacturing Flight Performance of the Development of the Avcoat Estimating Orion Heat Shield Orion EFT-1 Purge and Venting Post-Flight Assessment of the and Qualiﬁcation of the MPCV Thermal Protection System during Ablation Model for the MPCV Failure Due To Ablator Cracking Performance Avcoat Thermal Protection Heat Shield for the Exploration the Orion Exploration Flight Test-1 Exploration Flight Test – 1 During The EFT-1 Mission R. Smith, Lockheed Martin System for the Orion Flight Test-1 Mission B. Remark, NASA Johnson Space J. Vander Kam, NASA Ames Research Corporation, Houston, TX; J. Hall, J. Exploration Flight Test-1 S. Bouslog, M. Fowler, J. Kowal, J. Kowal, NASA Johnson Space Center, Center, Houston, TX Center, Moffett Field, CA; P. Gage, Chuhta, Lockheed Martin Corporation, J. Vander Kam, D. Bose, NASA Ames NASA Johnson Space Center, Houston, TX; J. Vander Kam, NASA Ames Neerim Corporation, Mountain Denver, CO Research Center, Moffett Field, CA; E. Houston, TX Research Center, Moffett Field, CA; S. View, CA Rodriguez, J. Santos, Jacobs, Moffett Bouslog, NASA Johnson Space Center, Field, CA; J. Feldman, M. Mahzari, Houston, TX; M. Rezin, NASA Ames Analytical Mechanics Associates, Inc., Research Center, Moffett Field, CA Moffett Field, CA; et al. Friday, 17 June 2016 299-MAO-18 Surrogate Modeling and Non-Deterministic Design - Methods and Applications III Cardozo Chaired by: V. TOROPOV, Queen Mary, University of London and M. STELMACK, Lockheed Martin Aeronautics 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs AIAA-2016-3911 AIAA-2016-3912 AIAA-2016-3913 AIAA-2016-3914 AIAA-2016-3915 AIAA-2016-3916 Sequential Robust Design of a Sensitivity Analysis of Chaotic Efﬁcient Aircraft Routing A Kriging-PDD surrogate model Reliability Estimation Using Composite Structure Ram Air Turbine Problems using a Fourier Algorithm Based on Ant Colony for low-cost sensitivity analysis MCMC Based Tail Modeling Optimization for Satellite Using M. Walter, D. Mavris, Georgia Approximation of the Least- Optimization A. Cortesi, P. Congedo, French E. Acar, G. Bayrak, TOBB University of Discrete Dynamic Radial Basis Institute of Technology, Atlanta, GA Squares Adjoint R. Entz, Airbus, Munich, Germany; H. National Institute for Research Economics and Technology, Ankara, Function Metamodel A. Ashley, J. Hicken, Rensselaer Andrade Porto, University of São Paulo, in Computer Science and Control Turkey L. Jian, T. Long, R. Shi, B. Yuan, L. Polytechnic Institute, Troy, NY São Carlos, Brazil; R. Fernandes de (INRIA), Talence, France Liu, Beijing Institute of Technology, Oliveira, Airbus, Munich, Germany; R. Beijing, China Alves de Lima, University of São Paulo, São Carlos, Brazil Friday, 17 June 2016 300-MST-16 Modeling and Simulation of Propulsion Systems Georgetown East Chaired by: D. KEATING and U. DURAK, DLR-German Aerospace Center 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2016-3917 AIAA-2016-3918 AIAA-2016-3919 AIAA-2016-3920 Antares Liquid Rocket Engine Antares Liquid Rocket Engine A 3-D Computational Model for Simulation of Fuel Spray and IOP and Transient Flow Convective Base Heating: AJ-26 Optimum Design and Analysis Combustion of Compression Entertainment: AJ-26 to to RD-181 of Vertical Take-off in Aircraft Ignition Heavy-oil Engine RD-181 D. Patel, Orbital ATK, Chandler, AZ U. Jain, Purdue University, West J. Qiu, M. Zhou, Tsinghua University, D. Patel, Orbital ATK, Chandler, AZ Lafayette, IN; Y. Mukkamala, Vellore Beijing, China Institute of Technology, Vellore, India

132 Friday, 17 June 2016 301-MST-17 Modeling and Simulation of Structures and Structural Dynamics Piscataway Chaired by: M. ALVAREZ, NASA Langley Research Center and R. RUFF 0930 hrs 1000 hrs 1030 hrs 1100 hrs AIAA-2016-3921 AIAA-2016-3922 AIAA-2016-3923 AIAA-2016-3924 Linear Elasticity Finite Volume Structural Configuration Nonlinear State Estimation for Simulation and Control Based Structural Dynamics Systems Analysis for Advanced Aeroelastic Multi-Body Models of a Space Web Deployed Solver Aircraft Fuselage Concepts T. Benoit, Y. Lemmens, Siemens, by Centrifugal Forces in a M. Selim, R. Koomullil, D. McDaniel, V. Mukhopadhyay, J. Welstead, J. Leuven, Belgium; W. Desmet, Sounding Rocket Experiment University of Alabama, Birmingham, Quinlan, M. Guynn, NASA Langley Catholic University of Leuven, Leuven, H. Mao, Royal Institute of Technology Birmingham, AL Research Center, Hampton, VA Belgium (KTH), Stockholm, Sweden; T. Sinn, M. Vasile, University of Strathclyde, Glasgow, United Kingdom; G. Tibert, Royal Institute of Technology (KTH), Stockholm, Sweden Friday, 17 June 2016 302-TP-13 Heat Transfer in Aerospace Applications DuPont Chaired by: E. SHORT, Raytheon Company and A. WILLIAMS, Air Force Reseach Laboratory 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs 1230 hrs AIAA-2016-3925 AIAA-2016-3926 AIAA-2016-3927 AIAA-2016-3928 AIAA-2016-3929 AIAA-2016-3930 AIAA-2016-3931 Comparison of Heat Flux Gages Blockage-Ratio Effect of a Bluff- A Mini-Scale Primary-Air Experimental and Numerical Investigation of Nose Cone Exploring Mechanisms of Aerodynamic Heating for High Enthalpy Flows - NASA Body Stabilized Flame on Aerosol Injector Mass-Flow-Rate Study on the Flame Base of Electrothermal Anti-icing Particle Size Effects of Iron Prediction Tool for a Supersonic Ames and IRS Behavior of Carbonaceous (Soot) Effect on Soot Nano-Aerosol Premixed Flame after a Small Control Law Oxide on Thermal Behaviors Vehicle for Conceptual Design S. Loehle, University of Stuttgart, Nano-PM in a Combustor Burning Formation in a JP-Fueled Gas- Size V-Gutter L. Ding, S. Chang, S. Yang, M. Leng, and Combustion Characteristics Phase Stuttgart, Germany; A. Nawaz, Jet Propulsion Fuel Turbine Combustor F. Gong, Y. Huang, Beihang Beihang University, Beijing, China for 5AT/Sr(NO3)2 Propellant B. Simsek, B. Kuran, M. Ak, Jacobs, Moffett Field, CA; G. Herdrich, M. Darbandi, M. Ghafourizadeh, Sharif M. Darbandi, M. Ghafourizadeh, University, Beijing, China D. Zhang , S. Lu, H. Zhang, University ROKETSAN Missile Industries, S. Fasoulas, University of Stuttgart, University of Technology, Tehran, Iran; Sharif University of Technology, of Science and Technology of China, Inc., Ankara, Turkey; S. Uslu, Stuttgart, Germany; E. Martinez, G. G. Schneider, University of Waterloo, Tehran, Iran; G. Schneider, University Hefei, China TOBB University of Economics and Raiche, NASA Ames Research Center, Waterloo, Canada of Waterloo, Waterloo, Canada Technology, Ankara, Turkey Moffett Field, CA Friday, 17 June 2016 303-TP-14 Advanced Modeling IV Jay Chaired by: S. MUPPIDI and E. JOSYULA, Air Force Reseach Laboratory 0930 hrs 1000 hrs 1030 hrs 1100 hrs 1130 hrs 1200 hrs 1230 hrs AIAA-2016-3932 AIAA-2016-3933 AIAA-2016-3934 AIAA-2016-3935 AIAA-2016-3936 AIAA-2016-3937 AIAA-2016-3938 Rarefaction effects for the Inviscid-flow Approximation of Inelastic Electron Scattering by Application of A New Thermal- Modeling of Electron Assessment of continuum Extension of Kestrel to General transonic airfoils in low Radiative Ablation of Cometary Nitrogen Atoms Mechanical Coupling Solver for Transpiration Cooling for breakdown for high-speed Thermochemical Models, Part I Reynolds number regime Meteoroids M. Panesi, University of Illinois, Ablation Hypersonic Vehicles chemically reacting wake flows R. Bond, Arnold Engineering C. Pekardan, A. Alexeenko, Purdue C. Park, Korea Advanced Institute of Urbana-Champaign, Urbana, IL; C. R. Fu, H. Weng, J. Wenk, A. Martin, K. Hanquist, University of Michigan, S. Subramaniam, K. Swaminathan Development Complex, Arnold AFB, University, West Lafayette, IN Science and Technology, Daejeon, Johnston, NASA Langley Research University of Kentucky, Lexington, Ann Arbor, Ann Arbor, MI; K. Hara, Gopalan, K. Stephani, University TN; R. Nichols, University of Alabama, South Korea Center, Hampton, VA; R. Macdonald, Lexington, KY Princeton Plasma Physics Laboratory, of Illinois, Urbana-Champaign, Birmingham, Arnold AFB, TN; G. Power, 133 University of Illinois, Urbana- Princeton, NJ; I. Boyd, University of Urbana, IL Arnold Engineering Development Champaign, Urbana, IL Michigan, Ann Arbor, Ann Arbor, MI Complex, Arnold AFB, TN Friday, 17 June 2016 304-WKSP-2 Drag Prediction Workshop Lincoln West 0930 - 1630 hrs Agenda: 0930 -1125 hrs Sessions 6, 7 The focus of this workshop will be the NASA Common Research Model (CRM) with wind-tunnel measured wing twist; both wing-body and wing-body-pylon-nacelle configurations will be considered. CFD predictions of absolute and incremental force and moment values will be examined and compared. The workshop will include grid convergence and code verification studies. Additionally, an angle-of-attack sweep with static aero-elastic 1130 – 1245 hrs Break for Lunch deformations will be considered. Grids will be made available for all required cases. 1245 – 1430 hrs Session 8, 9, 10 Optionally, participants are invited to perform solution-adaptation calculations and/or a coupled aero-structural simulation of the CRM wing-body configuration. A finite element model will be made available to participants to calculate twist/deflection due to aerodynamic load.

The objectives of this workshop will be to: • To assess the state-of-the-art computational methods as practical aerodynamic tools for aircraft force and moment prediction of industry relevant geometries. • To provide an impartial forum for evaluating the effectiveness of existing computer codes and modeling techniques using Navier-Stokes solvers. • To identify areas needing additional research and development. Author/Session Chair Index Abbruzzese, G., 22-FD-2 Allen, L., 63-PDL-2 Arteaga, R., 127-FT-2 Bardet, P., 36-AMT-2, 107-AMT-5 Beran, P., 237-MAO-13 Abdalla, M., 237-MAO-13 Alleyne, A., 169-ITAR-3 Arul, K., 284-APA-42/FD-64 Barmore, B., 286-ATIO.ATM-24 Berci, M., 246-APA-33/FD-54 Abdol-Hamid, K., 192-FD-40 Allison, D., 203-MST-10 Asai, K., 245-AMT-10/GT-8 Barnard, C., 296-FD-68 Beresh, S., 51-FD-9, 74-AMT-3 Abel, E., 168-GT-4 Allison, J., 131-MAO-8 Asano, K., 122-FC-6/FD-22 Barnes, C., 124-FD-24 Berger, K., 102-TP-3 Acar, E., 299-MAO-18 Allison, S., 177-AMT-7 Asghar, A., 39-APA-7 Barnewitz, H., 170-MAO-10 Bergeron, K., 249-APA-36 Achard, T., 237-MAO-13 Allyn, M., 151-ATIO.ACD-5 Ashley, A., 299-MAO-18 Bartasevicius, J., 20-FC-1 Bermel, P., 169-ITAR-3 Acotto, J., 217-APA-29 Almosnino, D., 41-APA-9 Ashpis, D., 205-PDL-5/FC-13 Bartkus, T., 150-ASE-10 Berndt, M., 196-FD-44 Acquaye, F., 90-FD-16 Alonso, E., 225-ATIO.ATM-20 Ashton, N., 192-FD-40 Bartoli, N., 202-MAO-12 Berry, S., 102-TP-3 Adams, D., 63-PDL-2 Alonso, J., 52-FD-10, 59-MAO-3, 60-MAO-4, 196-FD- Asmady, A., 151-ATIO.ACD-5 Barton, M., 90-FD-16 Berthoumieu, P., 12-ASE-2 Adegbindin, M., 59-MAO-3 44, 202-MAO-12, 269-MAO-17 Atha, D., 257-ATIO.TFPC-11/ATIO.IS-1 Baruzzi, G., 43-ASE-4, 285-ASE-17 Bertino, J., 16-ATIO.ATM-3, 184-ATIO.ATM-15 Afsar, M., 193-FD-41/FC-12 Alunni, A., 102-TP-3, 243-TP-10 Atkin, C., 7-APA-1, 89-FC-4, 190-FC-11 Basdogan, I., 97-MAO-5 Besson, E., 62-MST-4 Agarwal, R., 80-APA-14, 90-FD-16, 112-APA-20, Alvarez, M., 239-MST-12, 301-MST-17 Atkins, E., 14-ATIO.ATM-1 Bass, A., 290-ATIO.TFPC-12 Bettebghor, D., 237-MAO-13 125-FD-25, 146-APA-21, 234-FD-53, 248-APA-35, Alvarez Laguna, A., 31-PDL-1 Atkins, H., 54-FD-12 Bass, R., 185-ATIO.ATM-16 Bevan, J., 57-FD-15 297-FD-69 Alves, L., 294-FD-66 Aubry, S., 151-ATIO.ACD-5 Bassett, P., 287-ATIO.ATM-25 Bevan, R., 230-FC-15 Aggarwal, U., 172-TP-7 Alves de Lima, R., 299-MAO-18 Austin, J., 264-FD-60 Bassett, Z., 290-ATIO.TFPC-12 Bevirt, J., 119-ATIO.TFPC-6/ATIO.VSTOL-1, Agostini, L., 231-FD-48 Alvi, F., 55-FD-13, 126-FD-26, 165-FD-35, 215-AMT-8 Avelar, A., 191-FD-39 Bastian, M., 251-ASE-15, 252-ASE-16 155-ATIO.TFPC-7/ATIO.ACD-6/GEPC-1, Aguiar, A., 57-FD-15 Amar, A., 64-TP-2, 200-ITAR-4, 236-ITAR-5 Avery, J., 154-ATIO.ATM-14 Baszczewski, B., 152-ATIO.ATM-12 188-ATIO.TFPC-8/ATIO.FT-1/GEPC-2 Ahmad, N., 182-ASE-11 Amaral, F., 123-FD-23 Ayan, E., 80-APA-14, 150-ASE-10 Bateman, B., 85-ATIO.ATM-8 Bewley, J., 254-ATIO.ATM-22 Ahmed, A., 165-FD-35, 229-FC-14 Ambo, T., 245-AMT-10/GT-8 Aydemir, H., 203-MST-10 Bates, R., 86-ATIO.DE-1, 268-MAO-16 Bhagat, N., 203-MST-10 Ahuja, J., 155-ATIO.TFPC-7/ATIO.ACD-6/GEPC-1 Amitay, M., 50-FC-3, 122-FC-6/FD-22, 158-FC-7, Ayyalasomayajula, S., 133-MST-8 Bathel, B., 6-AMT-1, 36-AMT-2 Bhagwandin, V., 80-APA-14 Airiau, C., 231-FD-48 230-FC-15 Azevedo, J., 57-FD-15, 125-FD-25, 179-APA-26, Battazzo, S., 245-AMT-10/GT-8 Bhaskaran, R., 52-FD-10, 167-FD-37 Ak, M., 302-TP-13 Amrit, A., 98-MAO-6 231-FD-48, 246-APA-33/FD-54 Baumert, A., 220-ASE-13 Bhatia, M., 237-MAO-13 Akalin, F., 95-GT-2 Ananda, G., 105-AFM-7, 248-APA-35 Babbar, Y., 4-AFM-1 Baumgärtner, D., 60-MAO-4 Bhaumik, S., 231-FD-48, 262-FD-58 Akdemir, M., 170-MAO-10 Anderson, J., 124-FD-24, 206-TP-8 Babinsky, H., 109-APA-17 Bavaro, D., 155-ATIO.TFPC-7/ATIO.ACD-6/GEPC-1 Bhunia, A., 242-TP-9

134 Alam, M., 122-FC-6/FD-22, 256-ATIO.LTA-1 Anderson, M., 144-AFM-10 Bacci, D., 21-FC-2/FD-1/APA-5 Baxley, B., 16-ATIO.ATM-3, 46-ATIO.ATM-5, Bhusal, S., 148-APA-23/FD-28 Alamri, F., 136-TP-6 Anderson, W., 28-MAO-2, 170-MAO-10 Bacic, M., 259-FC-16 184-ATIO.ATM-15 Bialczak, B., 200-ITAR-4 Alavi, S., 251-ASE-15 Andino, M., 259-FC-16 Bacon, D., 182-ASE-11 Bayoğlu, T., 176-AFM-12 Bianchi, D., 27-MAO-1 Alber, M., 119-ATIO.TFPC-6/ATIO.VSTOL-1, Andrade Porto, H., 299-MAO-18 Badrya, C., 108-APA-16/FD-21 Bayrak, G., 299-MAO-18 Biava, M., 159-FC-8 226-ATIO.TFPC-10/ATIO.VSTOL-2 Andre, M., 36-AMT-2 Baeder, J., 108-APA-16/FD-21 Bays, L., 254-ATIO.ATM-22 Bibb, K., 200-ITAR-4, 267-ITAR-6 Albring, T., 60-MAO-4, 98-MAO-6 Andrienko, D., 135-TP-5, 206-TP-8 Bagade, P., 205-PDL-5/FC-13 Bayyuk, S., 167-FD-37 Bienert, N., 46-ATIO.ATM-5, 85-ATIO.ATM-8 Alderman, J., 7-APA-1 Anemaat, W., 44-ATIO.ACD-2, Baghapour, B., 53-FD-11 Bazilevs, Y., 238-MAO-14 Bieniawski, S., 202-MAO-12 Alexander, A., 46-ATIO.ATM-5 119-ATIO.TFPC-6/ATIO.VSTOL-1, Bagheri, A., 263-FD-59/FC-19/APA-38 Bean, J., 134-NIA-1 Bil, C., 240-MST-13 Alexander, M., 151-ATIO.ACD-5 222-ATIO.ACD-7/ATIO.TFPC-9 Bai, J., 93-FD-19 Bean, P., 58-FT-1 Bilimoria, K., 85-ATIO.ATM-8, 117-ATIO.ATM-11 Alexandrov, N., 291-ATIO.TFPC-13/ATIO.ATM-27 Angland, D., 41-APA-9 Bailey, S., 113-ASE-7/ATIO.ATM-9 Beard, S., 29-MST-1, 62-MST-4 Bilodeau, D., 43-ASE-4 Alexeenko, A., 172-TP-7, 303-TP-14 Annes da Silva, R., 191-FD-39 Baker, M., 201-MAO-11 Becker, A., 153-ATIO.ATM-13 Bimbato, A., 247-APA-34/FD-55 Alfaris, E., 127-FT-2 Ansell, P., 218-APA-30, 248-APA-35 Balakrishnan, H., 154-ATIO.ATM-14 Beckman, E., 280-AMT-11 Bin, W., 248-APA-35 Alfauwaz, A., 136-TP-6 Antcliff, K., 87-ATIO.TFPC-4/ATIO.GA-1, 134-NIA-1 Balakumar, P., 24-FD-4 Begnini, G., 8-APA-2 Bisek, N., 266-FD-62 Algozino, S., 218-APA-30 Anusonti-Inthra, P., 165-FD-35, 197-FD-45 Balboni, J., 199-GT-6 Bégou, G., 93-FD-19 Bizzarrini, N., 9-APA-3 Al Haddabi, N., 21-FC-2/FD-1/APA-5 Aoki, Y., 219-APA-32 Baldas, L., 259-FC-16 Behruzi, P., 265-FD-61 Blair, B., 100-MST-6 Alhussain, A., 136-TP-6 Aono, H., 260-FC-17/FD-56 Baldauff, R., 242-TP-9 Belﬁeld, E., 73-AFM-6 Blake, J., 283-APA-41/FD-63 Ali, A., 176-AFM-12 Aponso, B., 99-MST-5, 133-MST-8 Baldomir, A., 268-MAO-16 Belleau, C., 280-AMT-11 Blake, M., 254-ATIO.ATM-22 Ali, M., 126-FD-26 Arai, K., 168-GT-4 Baldwin, A., 55-FD-13 Belloc, H., 7-APA-1 Blake, W., 72-AFM-5, 105-AFM-7 Ali, S., 293-FD-65 Araya, G., 23-FD-3, 164-FD-34, 296-FD-68 Ball, G., 203-MST-10 Beltz, J., 249-APA-36 Blakely, C., 57-FD-15 Al-Khalil, K., 220-ASE-13 Ardelean, E., 96-ITAR-1 Baltadjiev, N., 238-MAO-14 Benard, N., 160-FC-9/PDL-4/FD-29 Blanchard, G., 150-ASE-10 Alkurdi, A., 127-FT-2 Argrow, B., 113-ASE-7/ATIO.ATM-9, 251-ASE-15 Balthazar, J., 171-MST-9 Bencic, T., 183-ASE-12 Blankson, I., 264-FD-60 Allaire, D., 238-MAO-14, 269-MAO-17 Arikan, K., 62-MST-4 Banerji, N., 32-TP-1 Bender, J., 273-TP-12 Bledsoe, J., 280-AMT-11 Allan, W., 39-APA-7 Arnault, A., 38-FC-20 Bangert, L., 219-APA-32, 250-APA-37 Beneddine, S., 39-APA-7 Bletzinger, K., 60-MAO-4 Allen, B., 18-ATIO.TFPC-2, 251-ASE-15, Arnold, C., 243-TP-10 Banks, D., 58-FT-1 Benek, J., 53-FD-11, 55-FD-13, 167-FD-37 Blondeau, C., 237-MAO-13 257-ATIO.TFPC-11/ATIO.IS-1, Arnold-Medabalimi, N., 195-FD-43 Bansal, S., 147-APA-22 Benmeddour, A., 95-GT-2 Blonigan, P., 297-FD-69 291-ATIO.TFPC-13/ATIO.ATM-27 Arora, N., 55-FD-13, 126-FD-26, 215-AMT-8 Bansmer, S., 82-ASE-6/APA-15, 114-ASE-8, 220-ASE-13 Benner, M., 220-ASE-13 Bluman, J., 204-MST-11 Allen, C., 28-MAO-2, 178-APA-25/FD-38, 230-FC-15 Arranz, G., 108-APA-16/FD-21 Bapty, T., 203-MST-10 Benoit, T., 301-MST-17 Blumenthal, B., 167-FD-37 Allen, D., 108-APA-16/FD-21 Arslanbekov, R., 54-FD-12 Barad, M., 40-APA-8 Benton, S., 260-FC-17/FD-56 Blunt, R., 234-FD-53 Author/Session Chair Index Bobrowski, K., 170-MAO-10 Brenner, P., 22-FD-2 Cai, K., 287-ATIO.ATM-25 Chakraborty, I., 13-ATIO.ACD-1, 44-ATIO.ACD-2 Choi, S., 59-MAO-3, 76-APA-10, 77-APA-11, 130-MAO-7, Bode-Oke, A., 105-AFM-7 Breviglieri, C., 57-FD-15 Cai, S., 242-TP-9 Chambers, J., 238-MAO-14 178-APA-25/FD-38, 180-APA-27, 201-MAO-11, Bodi, K., 256-ATIO.LTA-1 Briceno, S., 44-ATIO.ACD-2, 290-ATIO.TFPC-12 Cai, Y., 44-ATIO.ACD-2 Chamchalaem, C., 290-ATIO.TFPC-12 217-APA-29, 237-MAO-13 Bodkin, D., 176-AFM-12 Bridges, J., 250-APA-37 Calamas, D., 272-TP-11 Chan, W., 122-FC-6/FD-22 Chou, A., 24-FD-4 Bodony, D., 38-FC-20, 123-FD-23, 232-FD-49 Brionnaud, R., 124-FD-24 Calise, G., 9-APA-3 Chandar, D., 53-FD-11 Choudhari, M., 163-FD-33, 194-FD-42 Boekeloo, E., 268-MAO-16 Britcher, C., 134-NIA-1, 245-AMT-10/GT-8, 280-AMT-11 Callantine, T., 46-ATIO.ATM-5 Chandarana, M., 257-ATIO.TFPC-11/ATIO.IS-1 Chowdhury, S., 60-MAO-4, 202-MAO-12 Boggero, L., 130-MAO-7 Brock, J., 35-AFM-4 Calvert, M., 9-APA-3 Chandrasekhara, M., 259-FC-16 Chrisochoides, N., 22-FD-2 Bognar, J., 220-ASE-13 Broeren, A., 114-ASE-8, 149-ASE-9 Calvert, N., 26-GT-1, 36-AMT-2 Chang, C., 52-FD-10 Christie, R., 188-ATIO.TFPC-8/ATIO.FT-1/GEPC-2 Boldyrev, S., 52-FD-10 Bronsvoort, J., 223-ATIO.ATM-18, 255-ATIO.ATM-23, Camello, S., 149-ASE-9 Chang, K., 86-ATIO.DE-1 Chu, Y., 16-ATIO.ATM-3 Bolton, J., 215-AMT-8 286-ATIO.ATM-24 Campana, E., 269-MAO-17 Chang, S., 220-ASE-13, 302-TP-13 Chuang, H., 182-ASE-11 Bond, R., 303-TP-14 Bronz, M., 76-APA-10, 198-FT-3/GT-5 Campbell, A., 288-ATIO.ATM-26 Chao, H., 81-ASE-5, 153-ATIO.ATM-13 Chudoba, B., 86-ATIO.DE-1 Bonnier, M., 46-ATIO.ATM-5 Broughton, C., 95-GT-2 Campbell, R., 167-FD-37, 281-APA-39 Chao, T., 34-AFM-3 Chuhta, J., 298-ITAR-7 Bons, J., 7-APA-1, 230-FC-15, 234-FD-53 Broughton-Venner, J., 97-MAO-5 Campbell, S., 46-ATIO.ATM-5, 255-ATIO.ATM-23, Chaparro, D., 77-APA-11, 111-APA-19 Chung, W., 186-ATIO.ATM-17 Bopp, M., 179-APA-26 Brown, A., 81-ASE-5, 251-ASE-15, 252-ASE-16 288-ATIO.ATM-26 Charlot, B., 216-AMT-9 Chuvakhov, P., 261-FC-18/FD-57 Borade, A., 46-ATIO.ATM-5 Brown, J., 245-AMT-10/GT-8 Candler, G., 23-FD-3, 91-FD-17, 126-FD-26, 172-TP-7, Chater, M., 297-FD-69 Chwalowski, P., 8-APA-2, 77-APA-11 Bordogna, M., 237-MAO-13 Brune, A., 102-TP-3 264-FD-60, 273-TP-12, 293-FD-65 Chaudhry, R., 273-TP-12 Chyczewski, T., 218-APA-30 Bordron, A., 7-APA-1 Bruner, C., 266-FD-62 Canibek, M., 150-ASE-10 Chauvin, R., 285-ASE-17 Chynoweth, B., 56-FD-14 Borener, S., 84-ATIO.ATM-7, 181-APA-28 Brunton, S., 121-FC-5 Cantu, L., 6-AMT-1 Chawner, J., 92-FD-18 Ciampa, P., 97-MAO-5, 130-MAO-7 Borer, N., 87-ATIO.TFPC-4/ATIO.GA-1, 118-ATIO.TFPC-5, Brzozowski, D., 190-FC-11 Cao, C., 130-MAO-7 Chazot, O., 168-GT-4 Cid, C., 268-MAO-16 188-ATIO.TFPC-8/ATIO.FT-1/GEPC-2 Buckley, N., 85-ATIO.ATM-8, 255-ATIO.ATM-23 Carboneau, L., 223-ATIO.ATM-18, 253-ATIO.ATM-21 Chen, B., 44-ATIO.ACD-2 Ciliberti, D., 281-APA-39 Borgoltz, A., 128-GT-3, 181-APA-28 Budinger, M., 82-ASE-6/APA-15 Cárdenas, E., 5-AFM-2 Chen, C., 169-ITAR-3 Cistone, J., 46-ATIO.ATM-5, 185-ATIO.ATM-16 Boris, J., 25-FD-7, 232-FD-49 Bui, T., 143-AFM-9, 146-APA-21, 176-AFM-12 Cardullo, F., 61-MST-3, 132-MST-7, 270-MST-15 Chen, F., 36-AMT-2, 74-AMT-3 Citak, C., 170-MAO-10 Borouchaki, H., 22-FD-2 Bulaga, R., 119-ATIO.TFPC-6/ATIO.VSTOL-1 Cariou, J., 42-ASE-3 Chen, G., 171-MST-9 Clark, I., 35-AFM-4 Boschetti, P., 5-AFM-2, 105-AFM-7 Bulathsinghala, D., 284-APA-42/FD-64 Carlson, J., 192-FD-40 Chen, H., 131-MAO-8, 170-MAO-10, 187-ATIO.GA-2 Clark, K., 165-FD-35

135 Bose, D., 102-TP-3, 298-ITAR-7 Bunel, A., 253-ATIO.ATM-21 Carlson, N., 196-FD-44 Chen, J., 266-FD-62, 296-FD-68 Clarke, S., 188-ATIO.TFPC-8/ATIO.FT-1/GEPC-2 Bosma, J., 256-ATIO.LTA-1 Bunge, R., 127-FT-2 Carnelly, D., 153-ATIO.ATM-13 Chen, L., 247-APA-34/FD-55, 249-APA-36, 259-FC-16 Clayton, P., 50-FC-3 Boswell, J., 96-ITAR-1 Buning, P., 53-FD-11 Carniol, T., 45-ATIO.ATM-4 Chen, M., 62-MST-4 Clemens, N., 55-FD-13, 107-AMT-5 Botero, E., 59-MAO-3 Burdette, D., 27-MAO-1 Carnrike, D., 129-ITAR-2 Chen, N., 168-GT-4 Clemons, H., 123-FD-23 Botez, R., 72-AFM-5, 217-APA-29, 253-ATIO.ATM-21, Burgaud, F., 130-MAO-7 Carozza, A., 272-TP-11 Chen, Q., 222-ATIO.ACD-7/ATIO.TFPC-9 Clemons, L., 50-FC-3 289-ATIO.GA-3 Burgett, D., 29-MST-1 Carrier, G., 60-MAO-4, 97-MAO-5 Chen, W., 79-APA-13 Clifton, J., 176-AFM-12 Bouhlel, M., 202-MAO-12 Burke, K., 223-ATIO.ATM-18 Carroll, D., 241-PDL-6 Chen, X., 74-AMT-3, 216-AMT-9, 240-MST-13 Clingman, D., 230-FC-15 Bouley, D., 221-ASE-14 Burns, R., 36-AMT-2, 74-AMT-3 Carstensen, J., 28-MAO-2 Cheng, A., 288-ATIO.ATM-26 Cliquet, J., 43-ASE-4 Bourassa, C., 158-FC-7 Burns, W., 101-PDL-3 Carter, C., 215-AMT-8 Cheng, D., 235-GT-7 Clymer, A., 253-ATIO.ATM-21 Bouslog, S., 267-ITAR-6, 298-ITAR-7 Burress, T., 62-MST-4, 204-MST-11 Cartmell, D., 61-MST-3, 133-MST-8 Cheng, F., 287-ATIO.ATM-25 Coder, J., 78-APA-12 Bowcutt, K., 129-ITAR-2 Burrows, B., 238-MAO-14 Carvalho, B., 5-AFM-2, 243-TP-10 Cheng, G., 240-MST-13 Coen, P., 250-APA-37 Bowersox, R., 194-FD-42, 261-FC-18/FD-57 Burt, J., 206-TP-8, 264-FD-60, 273-TP-12 Cary, A., 297-FD-69 Cheng, J., 54-FD-12, 81-ASE-5, 196-FD-44, 240-MST-13 Coffey, J., 113-ASE-7/ATIO.ATM-9 Bowman, C., 155-ATIO.TFPC-7/ATIO.ACD-6/GEPC-1 Bury, Y., 7-APA-1, 74-AMT-3 Casalis, G., 93-FD-19 Cheng, V., 186-ATIO.ATM-17 Cohen, J., 21-FC-2/FD-1/APA-5 Boyd, I., 64-TP-2, 206-TP-8, 233-FD-50, 264-FD-60, Bush, R., 90-FD-16 Casper, K., 21-FC-2/FD-1/APA-5, 51-FD-9, 129-ITAR-2, Cheng, X., 79-APA-13, 175-AFM-11 Coiro, D., 9-APA-3 303-TP-14 Busquets, J., 225-ATIO.ATM-20 218-APA-30 Cheng, Z., 220-ASE-13 Coleman, B., 59-MAO-3 Boyland, S., 151-ATIO.ACD-5 Butler, B., 32-TP-1, 243-TP-10 Cassady, A., 200-ITAR-4 Chevalley, E., 85-ATIO.ATM-8 Colin, S., 259-FC-16 Braden, P., 285-ASE-17 Butler, C., 149-ASE-9 Cassady, L., 200-ITAR-4 Chhaya, B., 99-MST-5 Collier, F., 232-FD-49 Bragg, M., 149-ASE-9 Butler, K., 235-GT-7 Cassell, M., 124-FD-24 Chiew, J., 196-FD-44 Collins, E., 54-FD-12 Brandeau, E., 35-AFM-4 Butler, R., 291-ATIO.TFPC-13/ATIO.ATM-27 Catlett, M., 124-FD-24 Childs, R., 199-GT-6, 267-ITAR-6 Collins, K., 203-MST-10 Brandis, A., 135-TP-5, 172-TP-7, 200-ITAR-4, 267-ITAR-6 Buttsworth, D., 102-TP-3 Cattafesta, L., 123-FD-23 Chilson, P., 113-ASE-7/ATIO.ATM-9 Colmenares, J., 192-FD-40 Brasil, C., 85-ATIO.ATM-8, 255-ATIO.ATM-23 Büyükkoçak, A., 176-AFM-12 Cavalin, M., 127-FT-2 Chin, D., 51-FD-9 Colombo, M., 202-MAO-12 Brasseur, J., 162-FD-32/FC-10 Buzica, A., 20-FC-1 Cavcar, M., 83-ATIO.ACD-3 Chin, J., 269-MAO-17 Colonius, T., 121-FC-5, 148-APA-23/FD-28 Brauner, T., 160-FC-9/PDL-4/FD-29 Byrd, L., 169-ITAR-3, 242-TP-9 Cerminara, A., 261-FC-18/FD-57 Chiplunkar, A., 202-MAO-12 Combette, P., 216-AMT-9 Bravin, M., 183-ASE-12 Byun, G., 78-APA-12 Cervi, T., 73-AFM-6 Chivukula, S., 61-MST-3 Combs, C., 6-AMT-1, 165-FD-35, 280-AMT-11 Bray, D., 21-FC-2/FD-1/APA-5 Cadieux, F., 23-FD-3 Cesnik, C., 73-AFM-6 Chng, T., 241-PDL-6 Conde Rocha Murca, M., 154-ATIO.ATM-14 Breeze-Stringfellow, A., 167-FD-37 Cagle, C., 50-FC-3 Çetiner, A., 282-APA-40 Cho, H., 108-APA-16/FD-21 Congdon, E., 168-GT-4 Brehm, C., 40-APA-8 Cai, G., 29-MST-1 Chachad, G., 256-ATIO.LTA-1 Choe, Y., 109-APA-17 Congedo, P., 251-ASE-15, 299-MAO-18 Breitsamter, C., 20-FC-1 Cai, J., 130-MAO-7, 205-PDL-5/FC-13 Chadha, S., 10-APA-4 Choi, J., 217-APA-29 Conroy, J., 16-ATIO.ATM-3, 85-ATIO.ATM-8 Author/Session Chair Index Constantine, P., 269-MAO-17 Danczyk, S., 295-FD-67 Demauro, E., 51-FD-9, 74-AMT-3 Downen, T., 187-ATIO.GA-2 Edwards, J., 101-PDL-3, 125-FD-25, 195-FD-43 Conway, M., 112-APA-20 Dandachy, M., 127-FT-2 DeMillard, E., 75-AMT-4 Doyle, J., 249-APA-36, 282-APA-40 Efraimsson, G., 229-FC-14 Cooke, D., 58-FT-1 Dandois, J., 38-FC-20 Deng, K., 131-MAO-8 Doyle, S., 201-MAO-11 Eggers, T., 261-FC-18/FD-57 Cooksey, K., 83-ATIO.ACD-3, 130-MAO-7 Danehy, P., 32-TP-1, 36-AMT-2, 145-AMT-6, 215-AMT-8 Deng, S., 108-APA-16/FD-21 Drake, A., 73-AFM-6, 151-ATIO.ACD-5, 290-ATIO.TFPC-12 Egorov, I., 194-FD-42 Cooper, J., 18-ATIO.TFPC-2, 134-NIA-1, 204-MST-11 Daniel, E., 265-FD-61 Deng, X., 238-MAO-14 Drake, M., 13-ATIO.ACD-1 Eisfeld, B., 192-FD-40 Cooper, W., 287-ATIO.ATM-25 Dannelley, D., 272-TP-11 Denham, C., 5-AFM-2, 116-ATIO.ATM-10 Drakes, J., 63-PDL-2 Eitelberg, G., 78-APA-12 Cordero Gracia, M., 22-FD-2 Dannenhoffer, J., 92-FD-18, 203-MST-10 Deniau, H., 93-FD-19 Drakunov, S., 132-MST-7 Elam, K., 6-AMT-1 Correia Grácio, B., 61-MST-3 Darbandi, M., 302-TP-13 Denison, M., 111-APA-19 Drewiacki, D., 105-AFM-7 Elbing, B., 113-ASE-7/ATIO.ATM-9 Corrigan, A., 25-FD-7, 94-FD-20, 265-FD-61 Da Ronch, A., 4-AFM-1, 106-AFM-8, 171-MST-9, de Paula, A., 86-ATIO.DE-1, 239-MST-12 Driver, D., 168-GT-4 Eldridge, J., 177-AMT-7 Corson, D., 9-APA-3, 90-FD-16 246-APA-33/FD-54 Deppen, T., 169-ITAR-3 Droba, J., 64-TP-2, 200-ITAR-4 Elhadi, M., 180-APA-27 Cortesi, A., 251-ASE-15, 299-MAO-18 Darragh, R., 248-APA-35, 281-APA-39 de Queiroz Cordova Santos, M., 86-ATIO.DE-1 Drolen, B., 96-ITAR-1 Elham, A., 97-MAO-5, 201-MAO-11 Coschignano, A., 109-APA-17 Darrah, S., 45-ATIO.ATM-4 Derlaga, J., 166-FD-36, Drop, F., 270-MST-15 Eliasson, P., 218-APA-30 Costello, M., 118-ATIO.TFPC-5 Das, S., 21-FC-2/FD-1/APA-5, 51-FD-9 188-ATIO.TFPC-8/ATIO.FT-1/GEPC-2 Dropkin, A., 129-ITAR-2 Ellebracht, L., 96-ITAR-1 Cotton, W., 253-ATIO.ATM-21 da Silva, R., 171-MST-9 DeSalvo, M., 50-FC-3 Drouin, A., 76-APA-10 Ellejmi, M., 46-ATIO.ATM-5 Coupe, J., 152-ATIO.ATM-12, 184-ATIO.ATM-15 Daskiran, O., 34-AFM-3 Deshpande, P., 179-APA-26 Drouven, T., 198-FT-3/GT-5 Ellerbroek, J., 99-MST-5 Courson, D., 242-TP-9 Davendralingam, N., 15-ATIO.ATM-2 Desmet, W., 301-MST-17 Druot, T., 97-MAO-5 Elliott, G., 199-GT-6 Coutris, P., 221-ASE-14 Davidson, D., 145-AMT-6, 177-AMT-7 de Souza, R., 131-MAO-8 Dryer, J., 52-FD-10 Ellsworth, J., 176-AFM-12 Cowlagi, R., 238-MAO-14 Davidson, P., 75-AMT-4 de Sturler, E., 166-FD-36 Du, L., 295-FD-67 Elmiligui, A., 30-MST-2, 167-FD-37, 171-MST-9, Coyle, A., 203-MST-10 Davies, C., 86-ATIO.DE-1 Detert, B., 178-APA-25/FD-38 Duan, L., 24-FD-4, 90-FD-16, 125-FD-25, 163-FD-33 204-MST-11, 250-APA-37 Crabill, J., 30-MST-2 Davies, M., 100-MST-6, 133-MST-8 Deutschmann, A., 270-MST-15 Dubois, A., 188-ATIO.TFPC-8/ATIO.FT-1/GEPC-2 Emmanuel, F., 221-ASE-14 Craft, J., 165-FD-35 Davis, J., 181-APA-28 Devalla, V., 106-AFM-8 Dubot, T., 83-ATIO.ACD-3 Enea, G., 255-ATIO.ATM-23 Crafton, J., 216-AMT-9 Davison, C., 220-ASE-13, 221-ASE-14 Devenport, W., 128-GT-3, 181-APA-28 Dubuisson, S., 46-ATIO.ATM-5 Engblom, W., 180-APA-27 Craun, C., 185-ATIO.ATM-16 De, S., 201-MAO-11 de Vicente, J., 51-FD-9 Duda, B., 190-FC-11 Engelbrecht, H., 175-AFM-11 Creedon, J., 47-ATIO.TFPC-3 DeArmon, J., 16-ATIO.ATM-3, 85-ATIO.ATM-8, Deyang, T., 31-PDL-1, 79-APA-13 Dumitrache, C., 63-PDL-2 Engelbrecht, J., 175-AFM-11

136 Cross, P., 64-TP-2 287-ATIO.ATM-25 Dezitter, F., 221-ASE-14 Dumont, A., 60-MAO-4, 97-MAO-5 Engerer, J., 169-ITAR-3 Crossley, W., 153-ATIO.ATM-13 Deaton, J., 237-MAO-13 Diao, Z., 32-TP-1 Dumont, C., 221-ASE-14 Engle, J., 58-FT-1 Crouch, J., 11-ASE-1, 82-ASE-6/APA-15 de Baar, J., 108-APA-16/FD-21 Dias, J., 29-MST-1, 246-APA-33/FD-54 Duncan, D., 47-ATIO.TFPC-3 Enjiao, Z., 34-AFM-3 Crowe, D., 112-APA-20 De Breuker, R., 237-MAO-13 Diaz Brito, M., 167-FD-37 Duncan, S., 25-FD-7 Enqvist, M., 176-AFM-12 Crowley, B., 7-APA-1 DeChant, L., 218-APA-30 Didion, J., 242-TP-9 Duraisamy, K., 37-APA-6/FD-8, 91-FD-17, 125-FD-25, Entz, R., 299-MAO-18 Crowley, D., 95-GT-2 Decker, R., 180-APA-27 Diez, M., 269-MAO-17 195-FD-43, 297-FD-69 Eres, M., 86-ATIO.DE-1, 268-MAO-16 Cruden, B., 135-TP-5, 172-TP-7, 236-ITAR-5, 298-ITAR-7 Deconinck, H., 31-PDL-1 DiGirolamo, E., 222-ATIO.ACD-7/ATIO.TFPC-9 Durak, U., 99-MST-5, 203-MST-10, 239-MST-12, Errico, A., 16-ATIO.ATM-3 Cruz, J., 181-APA-28 Dede, E., 131-MAO-8 Dimotakis, P., 91-FD-17 300-MST-16 Erturk, S., 72-AFM-5, 144-AFM-10 Cuco, A., 131-MAO-8 Deere, K., 188-ATIO.TFPC-8/ATIO.FT-1/GEPC-2, 199-GT-6 Ding, L., 302-TP-13 Durand, J., 130-MAO-7 Erwin, J., 22-FD-2 Cui, Y., 171-MST-9 Defoort, S., 107-AMT-5 Ding, Y., 295-FD-67 Dutle, A., 15-ATIO.ATM-2 Erzberger, H., 16-ATIO.ATM-3 Cumming, S., 143-AFM-9, 176-AFM-12 DeFranco, P., 132-MST-7 DiPaola, M., 196-FD-44, 197-FD-45 Dutton, J., 199-GT-6 Esposito, B., 220-ASE-13 Cummings, R., 230-FC-15 Deierling, W., 254-ATIO.ATM-22 Dippold, V., 180-APA-27 Duval, B., 32-TP-1 Essel, E., 262-FD-58 Cunha Junior, S., 239-MST-12 Deiler, C., 176-AFM-12 Discetti, S., 108-APA-16/FD-21, 260-FC-17/FD-56 Duvall, B., 134-NIA-1 Estevadeordal, J., 148-APA-23/FD-28 Cunningham, K., 73-AFM-6, 144-AFM-10 Déjean, B., 12-ASE-2 Dischinger, D., 183-ASE-12 Duvvuri, S., 296-FD-68 Eun, Y., 16-ATIO.ATM-3 Currie, T., 150-ASE-10 Delanoe, J., 221-ASE-14 Di Vito, V., 16-ATIO.ATM-3 Duymaz, E., 84-ATIO.ATM-7 Evans, A., 85-ATIO.ATM-8, 117-ATIO.ATM-11, Cutler, A., 6-AMT-1 DeLaura, R., 154-ATIO.ATM-14 Dogan, A., 34-AFM-3, 72-AFM-5, 105-AFM-7, Dwivedi, A., 126-FD-26 185-ATIO.ATM-16, 225-ATIO.ATM-20 Cuy, M., 177-AMT-7 DeLaurentis, D., 116-ATIO.ATM-10, 153-ATIO.ATM-13, 144-AFM-10 Dyakonov, A., 181-APA-28 Everett, S., 190-FC-11 Cybyk, B., 39-APA-7 286-ATIO.ATM-24 Dogariu, A., 241-PDL-6 Dyer, J., 113-ASE-7/ATIO.ATM-9 Eves, J., 59-MAO-3 Cymbalist, N., 91-FD-17 Delisi, D., 42-ASE-3, 81-ASE-5 Dolﬁ-Bouteyre, A., 42-ASE-3 Eanes, J., 42-ASE-3 Ewing, M., 204-MST-11 Czech, M., 11-ASE-1 Dell’Orso, H., 122-FC-6/FD-22 Döll, C., 38-FC-20 Eberhart, M., 32-TP-1 Eychenne, F., 153-ATIO.ATM-13 Czekalowski, P., 106-AFM-8 Dellaert, F., 257-ATIO.TFPC-11/ATIO.IS-1 Dong, H., 105-AFM-7, 159-FC-8, 246-APA-33/FD-54, Echapresto Garay, I., 218-APA-30 Eyi, S., 178-APA-25/FD-38, 197-FD-45, 295-FD-67 D’Urso, S., 248-APA-35 Della Vecchia, P., 281-APA-39 283-APA-41/FD-63 Echekki, T., 195-FD-43 Fagan, A., 6-AMT-1, 36-AMT-2 Dahlmann, K., 153-ATIO.ATM-13 Delnero, J., 218-APA-30 Dong, M., 24-FD-4 Economon, T., 60-MAO-4, 196-FD-44, 229-FC-14 Fagley, C., 124-FD-24 Dai, H., 79-APA-13 DeLoach, R., 95-GT-2, 165-FD-35 Donovan, A., 169-ITAR-3 Edelman, J., 56-FD-14 Fahy, E., 102-TP-3, 243-TP-10 Dai, Z., 240-MST-13 Del Rey Fernández, D., 197-FD-45 Dörnbrack, A., 143-AFM-9 Edelman, L., 122-FC-6/FD-22, 259-FC-16 Fakhraei, S., 95-GT-2 Daigle, M., 254-ATIO.ATM-22 Deluca, A., 108-APA-16/FD-21, 111-APA-19 Dose, B., 9-APA-3 Edoh, A., 164-FD-34 Fala, N., 187-ATIO.GA-2 Dale, G., 20-FC-1 Delva, J., 38-FC-20, 39-APA-7 Douglass, R., 82-ASE-6/APA-15 Edquist, K., 102-TP-3 Falcao Filho, J., 191-FD-39 Dalenbring, M., 8-APA-2, 218-APA-30 Demange, J., 60-MAO-4 Dowgwillo, R., 247-APA-34/FD-55 Edwards, C., 223-ATIO.ATM-18 Falck, R., 27-MAO-1 Author/Session Chair Index Fan, Z., 246-APA-33/FD-54 Fleury, R., 170-MAO-10 Gallas, Q., 39-APA-7 Gibson, D., 267-ITAR-6 Gordeyev, S., 56-FD-14, 101-PDL-3, 165-FD-35, Fang, X., 170-MAO-10 Flock, A., 290-ATIO.TFPC-12 Gallo, E., 6-AMT-1 Giez, A., 143-AFM-9 271-PDL-7 Fantauzzi, M., 81-ASE-5 Flores, O., 108-APA-16/FD-21 Gallo, W., 81-ASE-5 Gildersleeve, S., 230-FC-15 Gorospe, G., 29-MST-1 Fares, E., 146-APA-21, 190-FC-11 Folse, S., 253-ATIO.ATM-21 Gallon, J., 35-AFM-4 Gilkey, K., 136-TP-6 Gorrell, S., 86-ATIO.DE-1 Farias, P., 74-AMT-3 Fong, K., 56-FD-14 Gammon, M., 80-APA-14, 92-FD-18 Gillebaart, T., 260-FC-17/FD-56 Gotti, D., 136-TP-6 Fariduzzaman, A., 180-APA-27 Forster, M., 159-FC-8 Gan, J., 218-APA-30 Gilliot, A., 39-APA-7 Gottschalk, D., 47-ATIO.TFPC-3 Farnsworth, J., 7-APA-1 Fossati, M., 43-ASE-4 Gand, F., 39-APA-7 Gil-Prieto, D., 109-APA-17 Goyne, C., 6-AMT-1, 216-AMT-9 Farrell, T., 82-ASE-6/APA-15, 151-ATIO.ACD-5 Foster, N., 251-ASE-15 Gao, C., 128-GT-3, 160-FC-9/PDL-4/FD-29, Gingras, D., 100-MST-6, 203-MST-10 Grabe, C., 112-APA-20 Faruque, I., 106-AFM-8, 144-AFM-10 Foster, T., 58-FT-1 205-PDL-5/FC-13 Ginn, S., 58-FT-1, 188-ATIO.TFPC-8/ATIO.FT-1/GEPC-2 Grah, R., 155-ATIO.TFPC-7/ATIO.ACD-6/GEPC-1 Fasel, H., 56-FD-14, 126-FD-26, 193-FD-41/FC-12, Foucaut, J., 38-FC-20 Gao, X., 91-FD-17, 295-FD-67 Gioria, R., 161-FD-30/APA-24 Graham, C., 112-APA-20 261-FC-18/FD-57 Fowler, M., 298-ITAR-7 Gao, Z., 98-MAO-6, 131-MAO-8 Girimaji, S., 162-FD-32/FC-10 Gramatyka, J., 268-MAO-16 Fasoulas, S., 26-GT-1, 63-PDL-2, 135-TP-5, 302-TP-13 Foyle, D., 152-ATIO.ATM-12 Garcia, C., 143-AFM-9, 176-AFM-12 Gissen, A., 50-FC-3 Granados-Ortiz, F., 231-FD-48 Fatima, N., 9-APA-3 Franciolini, M., 246-APA-33/FD-54 Garcia, J., 267-ITAR-6 Glaab, P., 224-ATIO.ATM-19 Grandhi, R., 201-MAO-11, 269-MAO-17 Favaregh, A., 280-AMT-11 Franze, M., 34-AFM-3 Gardner, A., 246-APA-33/FD-54 Glasby, R., 22-FD-2 Grandin, A., 221-ASE-14 Federico, L., 16-ATIO.ATM-3 Frascella, M., 109-APA-17 Garman, K., 116-ATIO.ATM-10 Glauser, M., 162-FD-32/FC-10 Granlund, K., 51-FD-9, 260-FC-17/FD-56 Fedorov, A., 24-FD-4, 261-FC-18/FD-57 Frayssinet, O., 79-APA-13 Garmann, D., 122-FC-6/FD-22, 260-FC-17/FD-56, Glavicic, M., 202-MAO-12 Grant, M., 34-AFM-3, 35-AFM-4 Fehrenbach, S., 144-AFM-10 Fredericks, W., 87-ATIO.TFPC-4/ATIO.GA-1, 262-FD-58, 284-APA-42/FD-64 Glezer, A., 50-FC-3, 158-FC-7, 229-FC-14 Grasso, F., 9-APA-3, 148-APA-23/FD-28 Fei, X., 118-ATIO.TFPC-5, 134-NIA-1 119-ATIO.TFPC-6/ATIO.VSTOL-1 Garnier, E., 109-APA-17 Glina, Y., 223-ATIO.ATM-18 Grauer, J., 143-AFM-9, 176-AFM-12 Feil, R., 78-APA-12 Freeman, J., 222-ATIO.ACD-7/ATIO.TFPC-9 Garry, K., 181-APA-28, 247-APA-34/FD-55 Gnoffo, P., 191-FD-39, 266-FD-62 Gray, J., 27-MAO-1, 98-MAO-6, 237-MAO-13, Felder, W., 15-ATIO.ATM-2 Fregnani, J., 153-ATIO.ATM-13 Gartner, J., 158-FC-7 Gobal, K., 201-MAO-11 269-MAO-17 Feldman, J., 298-ITAR-7 Freidkes, B., 296-FD-68 Gaster, M., 7-APA-1, 293-FD-65 Goebel, K., 254-ATIO.ATM-22 Greathouse, J., 267-ITAR-6 Fell, J., 50-FC-3 French, D., 53-FD-11 Gatlin, G., 119-ATIO.TFPC-6/ATIO.VSTOL-1, 180-APA-27, Goertz, S., 52-FD-10 Green, M., 283-APA-41/FD-63 Feltrin, C., 86-ATIO.DE-1 French, P., 25-FD-7 284-APA-42/FD-64 Góes, L., 256-ATIO.LTA-1 Greenblatt, D., 260-FC-17/FD-56 Feng, C., 294-FD-66 Fresconi, F., 34-AFM-3, 72-AFM-5, 112-APA-20, Gauci, J., 46-ATIO.ATM-5 Gokcen, T., 64-TP-2, 102-TP-3, 199-GT-6, 243-TP-10 Gregg-III, R., 52-FD-10

137 Feng, H., 268-MAO-16 282-APA-40 Gauger, N., 60-MAO-4, 98-MAO-6 Goldstein, D., 172-TP-7 Gregory, I., 18-ATIO.TFPC-2 Feng, L., 160-FC-9/PDL-4/FD-29, 168-GT-4, Freund, J., 38-FC-20 Gaus, J., 73-AFM-6 Gollan, R., 102-TP-3 Grewal, J., 144-AFM-10 247-APA-34/FD-55 Frew, E., 113-ASE-7/ATIO.ATM-9, 251-ASE-15 Gazella, M., 82-ASE-6/APA-15 Golliher, E., 136-TP-6 Grewe, V., 153-ATIO.ATM-13 Ferguson, S., 28-MAO-2, 84-ATIO.ATM-7, 170-MAO-10 Friedland, O., 229-FC-14 Geiselhart, K., 167-FD-37 Gollnick, V., 47-ATIO.TFPC-3, 153-ATIO.ATM-13, Grier, B., 129-ITAR-2 Fernandes, A., 287-ATIO.ATM-25 Froemming, C., 153-ATIO.ATM-13 George, J., 6-AMT-1, 76-APA-10, 78-APA-12 287-ATIO.ATM-25 Grifﬁn, R., 129-ITAR-2 Fernandes de Oliveira, R., 299-MAO-18 Fronzeo, M., 262-FD-58 Gerber, B., 285-ASE-17 Golubev, V., 62-MST-4, 84-ATIO.ATM-7, 132-MST-7, Grigorie, L., 72-AFM-5, 289-ATIO.GA-3 Ferrer, E., 170-MAO-10 Fu, B., 128-GT-3 Gerdes, I., 152-ATIO.ATM-12 181-APA-28, 263-FD-59/FC-19/APA-38 Grinstead, J., 245-AMT-10/GT-8 Ferreyra, R., 266-FD-62 Fu, R., 303-TP-14 Gerhardt, J., 216-AMT-9 Gómez, F., 51-FD-9 Gronstal, D., 180-APA-27 Ferrier, Y., 111-APA-19 Fu, S., 93-FD-19, 190-FC-11, 194-FD-42 Gerlach, T., 99-MST-5, 203-MST-10, 239-MST-12 Gomez de Segura Solay, G., 285-ASE-17 Groot, K., 293-FD-65 Fidkowski, K., 166-FD-36 Fu, Z., 93-FD-19 German, B., 118-ATIO.TFPC-5, 290-ATIO.TFPC-12 Gómez López, M., 22-FD-2 Gross, A., 126-FD-26, 193-FD-41/FC-12, Field, J., 61-MST-3, 239-MST-12 Fucke, L., 61-MST-3 Gern, F., 86-ATIO.DE-1 Gong, F., 302-TP-13 260-FC-17/FD-56 Field, R., 218-APA-30 Fujii, K., 122-FC-6/FD-22, 260-FC-17/FD-56 Gerretsen, A., 239-MST-12 Gong, J., 30-MST-2, 235-GT-7, 261-FC-18/FD-57 Grossir, G., 168-GT-4 Fields, T., 73-AFM-6, 144-AFM-10 Fujino, T., 31-PDL-1 Gerstmann, J., 265-FD-61 Gong, R., 294-FD-66 Grout, R., 52-FD-10 Fikl, A., 166-FD-36 Fujita, E., 288-ATIO.ATM-26 Ghafourizadeh, M., 302-TP-13 Gonzalez, D., 231-FD-48, 262-FD-58 Grove, J., 58-FT-1 Filippone, A., 185-ATIO.ATM-16 Fujiwara, G., 77-APA-11, 111-APA-19, 149-ASE-9 Ghaisas, N., 57-FD-15 Gonzalez, E., 195-FD-43 Grzybowski, P., 29-MST-1 Finch, P., 290-ATIO.TFPC-12 Fukumoto, H., 260-FC-17/FD-56 Ghasemi, A., 197-FD-45 Gonzalez, P., 73-AFM-6, 105-AFM-7 Gs, S., 23-FD-3 Findlay, D., 25-FD-7 Fukunari, M., 241-PDL-6 Ghia, U., 167-FD-37 González Ramirez, P., 73-AFM-6 Gu, X., 97-MAO-5 Finley, D., 219-APA-32, 248-APA-35 Fuleki, D., 150-ASE-10, 220-ASE-13 Ghoddoussi, A., 78-APA-12 Goodrich, K., 18-ATIO.TFPC-2, Gu, Y., 81-ASE-5, 127-FT-2 Finnis, M., 147-APA-22 Funderburk, M., 126-FD-26 Ghoreyshi, M., 25-FD-7, 167-FD-37, 248-APA-35, 87-ATIO.TFPC-4/ATIO.GA-1, 118-ATIO.TFPC-5, Guaraldo, B., 8-APA-2 Fioriti, M., 130-MAO-7 Funk, C., 77-APA-11 249-APA-36, 281-APA-39 155-ATIO.TFPC-7/ATIO.ACD-6/GEPC-1 Guclu, A., 62-MST-4 Fischer, C., 269-MAO-17 Furukawa, D., 219-APA-32 Ghosh, S., 27-MAO-1, 125-FD-25, 191-FD-39, Goodwin, R., 183-ASE-12 Gudmundsson, S., 132-MST-7, Fischer, P., 52-FD-10 Futrzynski, R., 229-FC-14 230-FC-15 Gopal, D., 9-APA-3 263-FD-59/FC-19/APA-38 Fisher, T., 169-ITAR-3 Gabriel, C., 46-ATIO.ATM-5, 255-ATIO.ATM-23 Ghosh Roy, A., 143-AFM-9 Gopalakrishnan, S., 182-ASE-11 Guendel, R., 45-ATIO.ATM-4 Flannery, M., 136-TP-6 Gaeta, R., 113-ASE-7/ATIO.ATM-9 Giani, A., 216-AMT-9 Gopalan, H., 53-FD-11 Guenov, M., 13-ATIO.ACD-1 Flaszynski, P., 158-FC-7 Gage, P., 298-ITAR-7 Gianopulos, E., 226-ATIO.TFPC-10/ATIO.VSTOL-2 Gopalarathnam, A., 246-APA-33/FD-54, 296-FD-68 Guest, D., 220-ASE-13 Flegel, A., 183-ASE-12 Gaitonde, A., 204-MST-11, 263-FD-59/FC-19/APA-38 Gibson, A., 18-ATIO.TFPC-2, 1 Goparaju, K., 231-FD-48, 262-FD-58 Guest, J., 28-MAO-2 Fletcher, D., 32-TP-1, 63-PDL-2 Gaitonde, D., 23-FD-3, 231-FD-48, 262-FD-58 88-ATIO.TFPC-8/ATIO.FT-1/GEPC-2, Gord, J., 36-AMT-2, 107-AMT-5, 145-AMT-6, 177-AMT-7, Guglielmo, J., 217-APA-29 Fleury, G., 42-ASE-3 Galaviz-Schomisch, R., 255-ATIO.ATM-23 226-ATIO.TFPC-10/ATIO.VSTOL-2, 290-ATIO.TFPC-12 215-AMT-8 Guigue, C., 216-AMT-9 Author/Session Chair Index Guimaraes Neto, A., 105-AFM-7 Harris, R., 54-FD-12 Ho, T., 168-GT-4 Hu, T., 284-APA-42/FD-64 Istvan, M., 193-FD-41/FC-12 Gujral, V., 46-ATIO.ATM-5 Harrison, E., 5-AFM-2, 187-ATIO.GA-2 Hoang, T., 242-TP-9 Hu, W., 59-MAO-3 Ito, Y., 146-APA-21 Gulding, J., 152-ATIO.ATM-12, 223-ATIO.ATM-18, Harrison, S., 248-APA-35 Hochstetler, R., 256-ATIO.LTA-1 Hu, Y., 246-APA-33/FD-54 Itoh, H., 126-FD-26, 283-APA-41/FD-63 255-ATIO.ATM-23, 287-ATIO.ATM-25 Hart, J., 37-APA-6/FD-8 Hochwarth, J., 286-ATIO.ATM-24 Hu, Z., 21-FC-2/FD-1/APA-5, 41-APA-9 Itoh, K., 168-GT-4, 233-FD-50 Gulick, D., 236-ITAR-5 Hartjes, S., 185-ATIO.ATM-16 Hoeijmakers, H., 247-APA-34/FD-55 Huang, C., 289-ATIO.GA-3 Itsariyapinyo, P., 159-FC-8 Gülsever, E., 80-APA-14 Hartka, T., 168-GT-4 Hoekstra, J., 99-MST-5 Huang, D., 4-AFM-1 Iwakawa, A., 55-FD-13, 191-FD-39, 219-APA-32 Guo, Y., 43-ASE-4 Hartman, G., 199-GT-6 Hoff, A., 81-ASE-5 Huang, F., 175-AFM-11 Iyer, P., 23-FD-3 Guo, Z., 222-ATIO.ACD-7/ATIO.TFPC-9, 249-APA-36 Hasegawa, M., 89-FC-4 Hofﬂer, K., 289-ATIO.GA-3 Huang, J., 125-FD-25 Jabbal, M., 190-FC-11, 259-FC-16 Gursul, I., 284-APA-42/FD-64 Hasegawa, T., 147-APA-22 Hogge, E., 29-MST-1 Huang, L., 146-APA-21 Jackson, C., 166-FD-36 Gustafson, W., 52-FD-10 Hash, D., 102-TP-3 Höhndorf, L., 143-AFM-9 Huang, X., 82-ASE-6/APA-15 Jacob, D., 42-ASE-3, 81-ASE-5 Guynn, M., 301-MST-17 Hashimoto, A., 218-APA-30 Holdren, M., 290-ATIO.TFPC-12 Huang, Y., 56-FD-14, 302-TP-13 Jacob, J., 29-MST-1, 113-ASE-7/ATIO.ATM-9, Guzel, G., 282-APA-40 Hasim, F., 180-APA-27 Holguin, B., 186-ATIO.ATM-17 Huang, Z., 89-FC-4, 163-FD-33 144-AFM-10, 251-ASE-15 Guzman, C., 144-AFM-10 Hathaway, J., 29-MST-1 Hollis, B., 64-TP-2, 243-TP-10 Huber, K., 20-FC-1 Jacobs, P., 102-TP-3 Ha, S., 28-MAO-2 Hattenberger, G., 198-FT-3/GT-5 Holloway, P., 268-MAO-16 Hubner, J., 216-AMT-9 Jacobs, T., 113-ASE-7/ATIO.ATM-9 Habashi, W., 43-ASE-4 Hayashi, M., 166-FD-36 Holman, D., 124-FD-24 Huet, M., 39-APA-7 Jacobson, M., 11-ASE-1 Hader, C., 56-FD-14 He, A., 81-ASE-5 Holmes, B., 87-ATIO.TFPC-4/ATIO.GA-1 Hufstedler, E., 263-FD-59/FC-19/APA-38 Jafari, F., 74-AMT-3 Haering, E., 58-FT-1 He, W., 161-FD-30/APA-24 Holst, K., 55-FD-13 Hufty, D., 84-ATIO.ATM-7, 181-APA-28 Jafer, S., 99-MST-5, 100-MST-6 Hagen, B., 6-AMT-1 Hearn, T., 60-MAO-4, 170-MAO-10, 269-MAO-17 Holt, J., 181-APA-28, 247-APA-34/FD-55 Hughes, A., 249-APA-36 Jagtap, S., 289-ATIO.GA-3 Hagen, G., 117-ATIO.ATM-11 Heath, C., 27-MAO-1, 219-APA-32 Holzapfel, F., 5-AFM-2, 29-MST-1, 143-AFM-9, Hughes, M., 114-ASE-8 Jain, R., 10-APA-4 Hagiopol, A., 18-ATIO.TFPC-2, Hedlund, B., 271-PDL-7 225-ATIO.ATM-20, 256-ATIO.LTA-1 Hui, Y., 270-MST-15 Jain, U., 300-MST-16 257-ATIO.TFPC-11/ATIO.IS-1 Hedrick, T., 37-APA-6/FD-8 Holzäpfel, F., 11-ASE-1, 81-ASE-5, 247-APA-34/FD-55 Humphreys, W., 95-GT-2 Jairam, A., 50-FC-3 Haimes, R., 203-MST-10 Heeg, J., 8-APA-2, 40-APA-8 Homola, J., 45-ATIO.ATM-4 Huntley, S., 263-FD-59/FC-19/APA-38 Jakobi, J., 152-ATIO.ATM-12 Hajek, M., 78-APA-12 Hein, S., 293-FD-65 Hong, G., 62-MST-4, 100-MST-6 Hussein, S., 86-ATIO.DE-1 Jambunathan, R., 64-TP-2 Hajj, M., 74-AMT-3, 108-APA-16/FD-21 Heineck, J., 58-FT-1 Hong, R., 203-MST-10 Huynh, T., 255-ATIO.ATM-23 James, K., 98-MAO-6

138 Hale, L., 116-ATIO.ATM-10 Heisler, E., 168-GT-4 Hood, R., 113-ASE-7/ATIO.ATM-9 Hwang, H., 102-TP-3 Jameson, A., 30-MST-2, 196-FD-44, 229-FC-14 Hale, R., 204-MST-11, 222-ATIO.ACD-7/ATIO.TFPC-9 Heitin, S., 85-ATIO.ATM-8 Hooey, B., 152-ATIO.ATM-12 Hwang, I., 225-ATIO.ATM-20 Jankovsky, A., 155-ATIO.TFPC-7/ATIO.ACD-6/GEPC-1 Hall, D., 222-ATIO.ACD-7/ATIO.TFPC-9 Hejase, M., 45-ATIO.ATM-4 Hoogervorst, J., 201-MAO-11 Hyatt, A., 200-ITAR-4, 236-ITAR-5 Jansen, P., 151-ATIO.ACD-5 Hall, J., 298-ITAR-7 Helenbrook, B., 94-FD-20, 148-APA-23/FD-28 Hope, D., 108-APA-16/FD-21 Hyde, M., 144-AFM-10 Jansen, R., 155-ATIO.TFPC-7/ATIO.ACD-6/GEPC-1 Hall, N., 5-AFM-2, 76-APA-10, 105-AFM-7, 180-APA-27 Helland, S., 128-GT-3 Horio, B., 270-MST-15 Ianiro, A., 108-APA-16/FD-21, 260-FC-17/FD-56 Jaworski, J., 124-FD-24 Haller, T., 107-AMT-5 Hellman, B., 112-APA-20 Horiuchi, T., 73-AFM-6 Ibrahim, I., 193-FD-41/FC-12 Jayaraman, B., 10-APA-4 Hallermeyer, A., 42-ASE-3 Helm, C., 55-FD-13 Horn, J., 72-AFM-5 Ide, R., 220-ASE-13 Jeffries, J., 145-AMT-6, 177-AMT-7 Halls, B., 36-AMT-2, 215-AMT-8 Hemati, M., 121-FC-5, 161-FD-30/APA-24 Hornung, M., 153-ATIO.ATM-13 Idris, H., 16-ATIO.ATM-3, 184-ATIO.ATM-15, Jenaro, G., 179-APA-26 Hamlington, P., 248-APA-35, 281-APA-39 Hemm, R., 47-ATIO.TFPC-3 Horst, P., 82-ASE-6/APA-15 224-ATIO.ATM-19 Jenkins, T., 6-AMT-1, 177-AMT-7 Hamy, A., 253-ATIO.ATM-21 Hendricks, E., 269-MAO-17 Horvath, T., 102-TP-3, 267-ITAR-6 Ignatyev, D., 5-AFM-2 Jensen, K., 144-AFM-10 Han, K., 16-ATIO.ATM-3 Hendriks, T., 185-ATIO.ATM-16 Hosder, S., 102-TP-3, 297-FD-69 Ihme, M., 164-FD-34 Jensen, L., 253-ATIO.ATM-21 Han, X., 205-PDL-5/FC-13 Henfling, J., 51-FD-9, 74-AMT-3 Hossain, M., 230-FC-15 Iijima, T., 288-ATIO.ATM-26 Jentzsch, M., 20-FC-1 Han, Y., 43-ASE-4, 114-ASE-8, 234-FD-53 Hengeveld, D., 96-ITAR-1, 136-TP-6, 272-TP-11 Hosseinverdi, S., 163-FD-33 Ikeda, J., 147-APA-22, 215-AMT-8 Jeon, D., 16-ATIO.ATM-3 Han, Z., 178-APA-25/FD-38, 268-MAO-16 Herdrich, G., 26-GT-1, 32-TP-1, 135-TP-5, 243-TP-10, Hotle, S., 152-ATIO.ATM-12 Ikeda, K., 254-ATIO.ATM-22 Jeong, M., 16-ATIO.ATM-3 Hannemann, K., 24-FD-4 302-TP-13 Hou, Z., 222-ATIO.ACD-7/ATIO.TFPC-9, 249-APA-36 Ikonen, T., 44-ATIO.ACD-2 Jeong, S., 42-ASE-3 Hanquist, K., 303-TP-14 Hermann, T., 26-GT-1, 32-TP-1, 63-PDL-2, 135-TP-5 Houpt, A., 271-PDL-7 Ilario da Silva, C., 196-FD-44 Jewell, J., 6-AMT-1, 74-AMT-3, 194-FD-42 Hansman, R., 154-ATIO.ATM-14, 185-ATIO.ATM-16, Hernandez, I., 73-AFM-6 Housman, J., 111-APA-19 Ilich, Z., 168-GT-4 Jeyalingam, J., 259-FC-16 253-ATIO.ATM-21 Hernandez, S., 268-MAO-16 Houston, A., 113-ASE-7/ATIO.ATM-9 Im, D., 180-APA-27, 201-MAO-11 Jeyapaul, E., 192-FD-40 Hanson, D., 234-FD-53 Herraez, I., 9-APA-3, 148-APA-23/FD-28 Howe, D., 58-FT-1 Imamura, T., 164-FD-34 Ji, C., 44-ATIO.ACD-2, 168-GT-4 Hanson, K., 223-ATIO.ATM-18 Hey, J., 169-ITAR-3 Howell, L., 251-ASE-15 Inamdar, A., 11-ASE-1 Ji, F., 161-FD-30/APA-24 Hanson, R., 145-AMT-6, 177-AMT-7 Hicken, J., 197-FD-45, 201-MAO-11, 299-MAO-18 Hromisin, S., 76-APA-10, 262-FD-58 Ingersoll, B., 132-MST-7 Jia, Y., 132-MST-7 Hao, X., 219-APA-32 Higdon, K., 172-TP-7 Hsu, J., 191-FD-39 Ingersoll, J., 132-MST-7 Jian, L., 299-MAO-18 Hara, K., 303-TP-14 Hilb, R., 253-ATIO.ATM-21 Hsu, P., 107-AMT-5 Ioppolo, T., 75-AMT-4 Jiang, N., 36-AMT-2, 89-FC-4, 107-AMT-5, 215-AMT-8 Harada, M., 164-FD-34 Hildebrand, N., 126-FD-26 Hu, H., 9-APA-3, 12-ASE-2, 36-AMT-2, 75-AMT-4, Iosifidis, P., 250-APA-37 Jiang, P., 202-MAO-12 Hariharan, N., 109-APA-17, 249-APA-36 Hiller, B., 44-ATIO.ACD-2 161-FD-30/APA-24, 205-PDL-5/FC-13, 216-AMT-9, Ireland, P., 259-FC-16 Jiang, X., 268-MAO-16 Harish, A., 155-ATIO.TFPC-7/ATIO.ACD-6/GEPC-1 Hillier, A., 229-FC-14 247-APA-34/FD-55 Irick, K., 136-TP-6, 272-TP-11 Jiang, Z., 79-APA-13 Harper, S., 127-FT-2 Himansu, A., 295-FD-67 Hu, N., 54-FD-12, 271-PDL-7 Isaac, B., 238-MAO-14 Jiao, L., 75-AMT-4 Harris, F., 151-ATIO.ACD-5 Hipp, K., 7-APA-1 Hu, O., 53-FD-11 Ishihara, A., 14-ATIO.ATM-1 Jimenez, H., 5-AFM-2, 187-ATIO.GA-2, 254-ATIO.ATM-22 Author/Session Chair Index Jiménez, J., 282-APA-40 Kanale, A., 178-APA-25/FD-38 King, D., 241-PDL-6 Korobenko, A., 238-MAO-14 Laban, A., 262-FD-58 Jin, X., 175-AFM-11 Kanazaki, M., 217-APA-29 King, J., 106-AFM-8 Korolev, A., 252-ASE-16 Lacy, R., 226-ATIO.TFPC-10/ATIO.VSTOL-2 Jing, Z., 163-FD-33 Kang, C., 37-APA-6/FD-8, 204-MST-11 King, M., 220-ASE-13 Korzun, A., 266-FD-62 Lafage, R., 151-ATIO.ACD-5, 202-MAO-12 Jirasek, A., 8-APA-2, 25-FD-7, 218-APA-30 Kanistras, K., 76-APA-10 King, R., 24-FD-4 Koster, Z., 82-ASE-6/APA-15 Lai, C., 231-FD-48 Jo, Y., 77-APA-11, 178-APA-25/FD-38, 217-APA-29 Kapania, R., 59-MAO-3, 217-APA-29 Kinkade, B., 216-AMT-9 Kota, S., 249-APA-36 Lai, D., 42-ASE-3, 81-ASE-5 Jogi, N., 263-FD-59/FC-19/APA-38 Kaplan, C., 172-TP-7 Kinzel, M., 234-FD-53, 262-FD-58 Kotcher, R., 127-FT-2 Lai, K., 171-MST-9 Johnsen, E., 54-FD-12, 164-FD-34 Kara, K., 39-APA-7 Kipouros, T., 60-MAO-4 Köthe, A., 73-AFM-6 Laizet, S., 160-FC-9/PDL-4/FD-29 Johnsen, L., 112-APA-20 Karagoz, E., 44-ATIO.ACD-2 Kirby, M., 15-ATIO.ATM-2 Kotsonis, M., 163-FD-33, 296-FD-68 Lakebrink, M., 129-ITAR-2 Johnson, B., 199-GT-6 Karagozian, A., 164-FD-34, 232-FD-49 Kiris, C., 40-APA-8 Kou, J., 132-MST-7, 269-MAO-17 Lakshminarayan, V., 10-APA-4 Johnson, H., 93-FD-19 Karatekin, O., 251-ASE-15 Kirk, B., 64-TP-2 Kourta, A., 259-FC-16 Lam, K., 6-AMT-1 Johnson, M., 45-ATIO.ATM-4, 289-ATIO.GA-3 Kargin, V., 203-MST-10 Kirk, L., 267-ITAR-6 Kowal, J., 298-ITAR-7 Lamb, P., 61-MST-3 Johnson, P., 54-FD-12 Karlgaard, C., 35-AFM-4, 143-AFM-9 Kirkman, J., 281-APA-39 Koziel, S., 98-MAO-6, 178-APA-25/FD-38 Lambert, T., 229-FC-14 Johnson, R., 58-FT-1, 94-FD-20 Karman, S., 22-FD-2, 197-FD-45 Kkn, A., 241-PDL-6 Kraemer, E., 128-GT-3 Lamoureux, M., 39-APA-7 Johnson, S., 286-ATIO.ATM-24 Kartha, A., 23-FD-3 Klatte, J., 265-FD-61 Krakos, J., 52-FD-10, 297-FD-69 Landman, D., 198-FT-3/GT-5 Johnston, C., 135-TP-5, 236-ITAR-5, 264-FD-60, Kashi, A., 22-FD-2 Klein, A., 254-ATIO.ATM-22 Kranepuhl, R., 7-APA-1 Landreville, C., 220-ASE-13 273-TP-12, 303-TP-14 Kato, H., 41-APA-9 Klimmek, T., 171-MST-9 Krantz, C., 133-MST-8 Landrum, D., 37-APA-6/FD-8 Jolly, B., 167-FD-37, 175-AFM-11 Kattamis, N., 136-TP-6 Knapp, B., 155-ATIO.TFPC-7/ATIO.ACD-6/GEPC-1 Krech, J., 148-APA-23/FD-28 Lane, R., 46-ATIO.ATM-5 Jones, A., 77-APA-11, 108-APA-16/FD-21, 124-FD-24, Katz, A., 57-FD-15, 164-FD-34 Knezevici, D., 150-ASE-10 Kreeger, R., 43-ASE-4, 82-ASE-6/APA-15 Lani, A., 31-PDL-1 193-FD-41/FC-12, 263-FD-59/FC-19/APA-38 Katz, J., 74-AMT-3 Kniffin, C., 72-AFM-5, 105-AFM-7 Kreimeier, M., 47-ATIO.TFPC-3 Laporta, V., 273-TP-12 Jones, D., 204-MST-11, 233-FD-50, Kaufmann, K., 246-APA-33/FD-54 Knowles, K., 147-APA-22 Krishnamurthy, R., 42-ASE-3 Lapp, B., 202-MAO-12 263-FD-59/FC-19/APA-38 Kaul, U., 38-FC-20, 111-APA-19 Knüppel, A., 239-MST-12 Krishnan, K., 82-ASE-6/APA-15 Larkin, D., 203-MST-10 Jones, G., 36-AMT-2, 50-FC-3, 280-AMT-11 Kavsaoğlu, M., 83-ATIO.ACD-3 Knuth, T., 82-ASE-6/APA-15 Krishnappa, S., 263-FD-59/FC-19/APA-38 Larsson, R., 176-AFM-12 Jones, J., 223-ATIO.ATM-18 Kawasaki, H., 191-FD-39 Kobayashi, R., 147-APA-22 Krofta, J., 249-APA-36 Lash, E., 280-AMT-11 Jones, S., 183-ASE-12 Kawashima, R., 241-PDL-6 Koc, I., 282-APA-40 Kroll, N., 52-FD-10 Laskowski, G., 52-FD-10

139 Joo, J., 77-APA-11, 111-APA-19 Kaya, D., 176-AFM-12 Koch, H., 243-TP-10 Kruep, J., 240-MST-13 Latz, J., 146-APA-21 Jordan, R., 154-ATIO.ATM-14 Kayumi, M., 191-FD-39 Koch, M., 287-ATIO.ATM-25 Krüger, W., 179-APA-26 Laun, M., 205-PDL-5/FC-13 Jorgens, C., 235-GT-7 Kazarin, P., 84-ATIO.ATM-7, 181-APA-28 Kochenderfer, M., 132-MST-7 Krumbein, A., 112-APA-20 Laurence, R., 251-ASE-15 Jorgenson, P., 183-ASE-12 Keating, D., 30-MST-2, 171-MST-9, 300-MST-16 Kocian, T., 56-FD-14 Kshirsagar, A., 256-ATIO.LTA-1 Laurent, C., 285-ASE-17 Joshi, A., 34-AFM-3, 204-MST-11 Kegerise, M., 24-FD-4 Koczo, S., 253-ATIO.ATM-21 Kubler, N., 285-ASE-17 Lavin, T., 34-AFM-3, 175-AFM-11 Joslin, R., 159-FC-8 Kelkar, A., 179-APA-26 Koelling, J., 15-ATIO.ATM-2 Kuenz, A., 133-MST-8 LeBeau, R., 249-APA-36, 251-ASE-15 Jost, A., 53-FD-11 Keller, D., 181-APA-28 Koerner, S., 42-ASE-3, 81-ASE-5 Kuester, M., 128-GT-3, 181-APA-28 Le Brusquet, L., 42-ASE-3 Josyula, E., 194-FD-42, 206-TP-8, 273-TP-12, 303-TP-14 Kelley, B., 257-ATIO.TFPC-11/ATIO.IS-1 Koike, S., 218-APA-30 Kuffner, M., 45-ATIO.ATM-4 Le Chenadec, V., 166-FD-36 Jourdan, E., 57-FD-15 Kemnetz, M., 101-PDL-3 Koizumi, H., 241-PDL-6 Kügler, D., 99-MST-5 Lee, D., 178-APA-25/FD-38, 180-APA-27 Jovanov, K., 237-MAO-13 Kennedy, G., 98-MAO-6, 238-MAO-14 Koklu, M., 160-FC-9/PDL-4/FD-29, 259-FC-16 Kügler, M., 29-MST-1 Lee, G., 199-GT-6 Jovanovic, M., 126-FD-26 Kennerly, S., 267-ITAR-6 Kolinko, K., 5-AFM-2 Kuhn, M., 233-FD-50 Lee, H., 16-ATIO.ATM-3, 76-APA-10, 80-APA-14, Jovic, S., 45-ATIO.ATM-4 Kenway, G., 27-MAO-1, 28-MAO-2 Kolonay, R., 27-MAO-1 Kulakhmetov, M., 172-TP-7 100-MST-6, 133-MST-8, 167-FD-37, 186-ATIO.ATM-17, Joy, J., 193-FD-41/FC-12 Kercher, A., 25-FD-7, 94-FD-20 Komadina, S., 13-ATIO.ACD-1 Kulatilaka, W., 6-AMT-1, 215-AMT-8 224-ATIO.ATM-19 Jrad, M., 201-MAO-11 Kerho, M., 248-APA-35 Komurasaki, K., 241-PDL-6 Kulkarni, C., 29-MST-1, 254-ATIO.ATM-22 Lee, J., 20-FC-1, 25-FD-7, 44-ATIO.ACD-2, 57-FD-15, Juliano, T., 56-FD-14, 129-ITAR-2, 194-FD-42, Kern, S., 224-ATIO.ATM-19 Komuro, T., 168-GT-4, 233-FD-50 Kumar, R., 50-FC-3, 55-FD-13, 129-ITAR-2, 199-GT-6 59-MAO-3 261-FC-18/FD-57, 271-PDL-7 Kessler, D., 54-FD-12, 94-FD-20, 234-FD-53, 265-FD-61 Kondak, K., 256-ATIO.LTA-1 Kumar, V., 15-ATIO.ATM-2, 47-ATIO.TFPC-3, 270-MST-15 Lee, M., 281-APA-39 Jumper, E., 101-PDL-3 Kevern, J., 73-AFM-6 Konig, B., 146-APA-21 Kun, Q., 31-PDL-1 Lee, N., 108-APA-16/FD-21 Jung, J., 14-ATIO.ATM-1, 45-ATIO.ATM-4, Keye, S., 80-APA-14 Kono, R., 147-APA-22 Kuntz, D., 243-TP-10 Lee, P., 85-ATIO.ATM-8, 224-ATIO.ATM-19, 290-ATIO.TFPC-12 Khan, M., 165-FD-35 Konopa, D., 169-ITAR-3 Kunz, D., 105-AFM-7 255-ATIO.ATM-23 Jung, Y., 16-ATIO.ATM-3, 152-ATIO.ATM-12, Khine, Y., 196-FD-44 Konopka, M., 265-FD-61 Kuo, V., 45-ATIO.ATM-4 Lee, S., 20-FC-1, 108-APA-16/FD-21, 149-ASE-9, 184-ATIO.ATM-15, 186-ATIO.ATM-17, 224-ATIO.ATM-19 Khrabrov, A., 5-AFM-2 Kontis, K., 10-APA-4, 21-FC-2/FD-1/APA-5, 112-APA-20 Kuran, B., 302-TP-13 225-ATIO.ATM-20, 247-APA-34/FD-55 Junqueira-Junior, C., 231-FD-48 Kim, C., 20-FC-1, 109-APA-17, 245-AMT-10/GT-8 Koomullil, R., 301-MST-17 Kurek, I., 202-MAO-12 Lee-Rausch, E., 192-FD-40 Justin, C., 155-ATIO.TFPC-7/ATIO.ACD-6/GEPC-1 Kim, H., 180-APA-27, 201-MAO-11 Kopardekar, P., 14-ATIO.ATM-1, 45-ATIO.ATM-4 Kurelek, J., 193-FD-41/FC-12 Lefebvre, T., 83-ATIO.ACD-3, 202-MAO-12 Jutte, C., 77-APA-11 Kim, I., 130-MAO-7 Kopecki, G., 29-MST-1 Kurita, M., 58-FT-1 Lei, Q., 215-AMT-8 Kalarikovilagam Srinivasan, G., 190-FC-11 Kim, J., 105-AFM-7, 289-ATIO.GA-3 Koppitz, P., 143-AFM-9, 225-ATIO.ATM-20 Kurt, A., 45-ATIO.ATM-4 Leidy, A., 194-FD-42, 261-FC-18/FD-57 Kalirajan, K., 34-AFM-3 Kim, K., 199-GT-6, 225-ATIO.ATM-20 Kopriva, J., 52-FD-10 Kurtulus, D., 62-MST-4 Leifsson, L., 98-MAO-6, 178-APA-25/FD-38 Kalivarapu, V., 268-MAO-16 Kim, M., 108-APA-16/FD-21 Kordos, D., 29-MST-1 Kutay, A., 176-AFM-12 Leite, H., 191-FD-39 Kalkhoran, I., 259-FC-16 Kimmel, R., 6-AMT-1, 56-FD-14, 89-FC-4 Koreanschi, A., 217-APA-29 Kwan, H., 290-ATIO.TFPC-12 Lele, S., 11-ASE-1, 57-FD-15, 166-FD-36 Author/Session Chair Index Lemanski, J., 257-ATIO.TFPC-11/ATIO.IS-1 Linke, F., 287-ATIO.ATM-25 Luhar, M., 121-FC-5, 296-FD-68 Malan, P., 175-AFM-11 Matsushima, K., 41-APA-9 Lemmens, Y., 204-MST-11, 301-MST-17 Lino Da Silva, M., 206-TP-8, 243-TP-10 Lührs, B., 153-ATIO.ATM-13, 287-ATIO.ATM-25 Mali, S., 262-FD-58 Mattos, B., 153-ATIO.ATM-13 Leng, M., 302-TP-13 Linton, D., 164-FD-34 Lukaczyk, T., 269-MAO-17 Malik, A., 47-ATIO.TFPC-3 Maughmer, M., 167-FD-37 Leonardo, E., 144-AFM-10 Liou, M., 180-APA-27 Luke, E., 54-FD-12 Malik, M., 23-FD-3, 52-FD-10 Mavris, D., 5-AFM-2, 13-ATIO.ACD-1, 15-ATIO.ATM-2, Leonhardt, B., 4-AFM-1 Litherland, B., 188-ATIO.TFPC-8/ATIO.FT-1/GEPC-2 Lum, C., 149-ASE-9 Malik, W., 152-ATIO.ATM-12, 184-ATIO.ATM-15, 27-MAO-1, 83-ATIO.ACD-3, 130-MAO-7, 187-ATIO.GA-2, Leonov, S., 241-PDL-6, 271-PDL-7 Little, J., 20-FC-1, 193-FD-41/FC-12 Lum, K., 171-MST-9 186-ATIO.ATM-17, 224-ATIO.ATM-19 289-ATIO.GA-3, 299-MAO-18 Leroy, D., 221-ASE-14 Liu, C., 44-ATIO.ACD-2 Luo, C., 79-APA-13 Mall, K., 34-AFM-3, 35-AFM-4 Maxwell, J., 242-TP-9 Lessarad, V., 200-ITAR-4 Liu, D., 62-MST-4 Luo, H., 22-FD-2, 37-APA-6/FD-8, 54-FD-12, 196-FD-44, Mallaun, C., 143-AFM-9 May, G., 94-FD-20 Lessard, V., 236-ITAR-5 Liu, F., 122-FC-6/FD-22, 160-FC-9/PDL-4/FD-29, 232-FD-49, 265-FD-61 Malone, A., 149-ASE-9 Mayer, T., 135-TP-5 Lestrade, J., 107-AMT-5 205-PDL-5/FC-13, 283-APA-41/FD-63, 294-FD-66 Luo, J., 194-FD-42 Mamou, M., 72-AFM-5, 217-APA-29 Mazaheri, A., 197-FD-45 Levin, D., 64-TP-2, 242-TP-9, 264-FD-60, 270-MST-15 Liu, G., 62-MST-4, 100-MST-6 Luo, S., 122-FC-6/FD-22, 205-PDL-5/FC-13, Manar, F., 124-FD-24 Mazellier, N., 259-FC-16 Levy, M., 290-ATIO.TFPC-12 Liu, H., 36-AMT-2, 74-AMT-3 283-APA-41/FD-63 Mancini, C., 116-ATIO.ATM-10 McCall, A., 53-FD-11 Lewis, D., 129-ITAR-2 Liu, L., 132-MST-7, 269-MAO-17, 299-MAO-18 Luo, W., 216-AMT-9 Mancini, P., 193-FD-41/FC-12, McCarley, Z., 58-FT-1 Lewis, M., 231-FD-48 Liu, P., 146-APA-21, 234-FD-53, 248-APA-35, Lupo, K., 124-FD-24 263-FD-59/FC-19/APA-38 McClain, S., 114-ASE-8 Lewis, S., 243-TP-10 284-APA-42/FD-64 Lutz, T., 128-GT-3 Maneva, Y., 31-PDL-1 McDaniel, D., 301-MST-17 Lewis, T., 291-ATIO.TFPC-13/ATIO.ATM-27 Liu, Q., 51-FD-9, 283-APA-41/FD-63 Luxhoj, J., 116-ATIO.ATM-10 Mangalam, A., 4-AFM-1 McDaniel, R., 236-ITAR-5 Leyland, P., 32-TP-1, 243-TP-10, 297-FD-69 Liu, T., 54-FD-12, 245-AMT-10/GT-8 Lv, P., 261-FC-18/FD-57 Mani, M., 297-FD-69 McDonald, G., 286-ATIO.ATM-24 Leyva, I., 129-ITAR-2 Liu, W., 167-FD-37, 204-MST-11, Lv, Y., 90-FD-16, 164-FD-34 Maniar, H., 290-ATIO.TFPC-12 McDonald, R., 44-ATIO.ACD-2, Li, C., 283-APA-41/FD-63 222-ATIO.ACD-7/ATIO.TFPC-9 Lv, Z., 160-FC-9/PDL-4/FD-29 Mankbadi, R., 144-AFM-10 155-ATIO.TFPC-7/ATIO.ACD-6/GEPC-1 Li, F., 4-AFM-1, 163-FD-33, 194-FD-42, Liu, X., 54-FD-12, 74-AMT-3, 124-FD-24 Lynch, K., 203-MST-10 Manosalvas, D., 229-FC-14 McGlaughlin, M., 168-GT-4 283-APA-41/FD-63 Liu, Y., 12-ASE-2, 75-AMT-4, 79-APA-13, 197-FD-45, Lynde, M., 281-APA-39 Mao, H., 301-MST-17 McGrath, B., 110-APA-18, 161-FD-30/APA-24 Li, H., 12-ASE-2, 36-AMT-2, 83-ATIO.ACD-3, 294-FD-66, 295-FD-67 Lyu, P., 130-MAO-7 Mao, J., 240-MST-13 McIntyre, T., 32-TP-1, 243-TP-10 93-FD-19, 205-PDL-5/FC-13 Liu, Z., 89-FC-4, 93-FD-19, 168-GT-4, 198-FT-3/GT-5 Ma, B., 112-APA-20 Mao, Y., 182-ASE-11 McKeon, B., 121-FC-5, 263-FD-59/FC-19/APA-38, Li, J., 80-APA-14, 90-FD-16, 130-MAO-7, Löbl, D., 5-AFM-2 Ma, C., 222-ATIO.ACD-7/ATIO.TFPC-9 Marais, K., 14-ATIO.ATM-1, 153-ATIO.ATM-13, 296-FD-68

140 185-ATIO.ATM-16, 216-AMT-9 Locascio, D., 83-ATIO.ACD-3, 290-ATIO.TFPC-12 Ma, H., 30-MST-2, 79-APA-13, 96-ITAR-1, 187-ATIO.GA-2 McKiernan, G., 56-FD-14 Li, K., 128-GT-3 Lock, A., 222-ATIO.ACD-7/ATIO.TFPC-9 191-FD-39, 217-APA-29, 271-PDL-7 Marana, M., 129-ITAR-2 McLaughlin, D., 76-APA-10, 231-FD-48, 262-FD-58 Li, L., 57-FD-15, 235-GT-7 Loehle, S., 26-GT-1, 32-TP-1, 63-PDL-2, 135-TP-5, Ma, L., 36-AMT-2, 215-AMT-8, 245-AMT-10/GT-8 Marañon, J., 218-APA-30 McLaughlin, T., 124-FD-24 Li, S., 83-ATIO.ACD-3, 170-MAO-10 302-TP-13 Ma, P., 234-FD-53 Marcório, G., 8-APA-2 McNally, D., 117-ATIO.ATM-11 Li, W., 44-ATIO.ACD-2, 123-FD-23 Lofthouse, A., 25-FD-7, 248-APA-35, 249-APA-36, Macaluso, P., 168-GT-4 Marcotte, D., 252-ASE-16 McNamara, J., 129-ITAR-2 Li, Y., 171-MST-9, 176-AFM-12 281-APA-39 Macchiarella, N., 29-MST-1, 100-MST-6 Marineau, E., 129-ITAR-2 McPartland, M., 223-ATIO.ATM-18 Li, Z., 242-TP-9 Logan, M., 83-ATIO.ACD-3 MacDonald, M., 135-TP-5, 168-GT-4 Marques, A., 178-APA-25/FD-38 Mebarki, Y., 72-AFM-5, 217-APA-29, 245-AMT-10/GT-8 Lian, Y., 43-ASE-4, 234-FD-53, 265-FD-61 Lohan, D., 131-MAO-8 Macdonald, R., 273-TP-12, 303-TP-14 Marquez, J., 203-MST-10 Medeiros, M., 24-FD-4, 123-FD-23 Liang, C., 57-FD-15 Long, D., 84-ATIO.ATM-7 Mackey, L., 233-FD-50 Martin, A., 32-TP-1, 303-TP-14 Medida, S., 9-APA-3, 90-FD-16 Liaño, G., 282-APA-40 Long, K., 199-GT-6 MacKunis, W., 181-APA-28, 263-FD-59/FC-19/APA-38 Martin, C., 112-APA-20, 282-APA-40 Medina, A., 193-FD-41/FC-12 Lichota, P., 143-AFM-9 Long, T., 132-MST-7, 269-MAO-17, 299-MAO-18 MacLean, M., 243-TP-10 Martin, M., 55-FD-13 Mehdi, S., 257-ATIO.TFPC-11/ATIO.IS-1 Liebeck, R., 110-APA-18 Lopez, B., 206-TP-8 MaCleod, J., 252-ASE-16 Martinez, A., 24-FD-4 Meindl, A., 26-GT-1, 63-PDL-2 Liechty, D., 172-TP-7 Loseille, A., 52-FD-10 MacManus, D., 109-APA-17 Martinez, E., 302-TP-13 Mele, B., 80-APA-14 Lieu, M., 129-ITAR-2 Loth, E., 82-ASE-6/APA-15, 149-ASE-9, 183-ASE-12 MacMaster, M., 21-FC-2/FD-1/APA-5 Martins, J., 27-MAO-1, 97-MAO-5 Melton, J., 256-ATIO.LTA-1, 267-ITAR-6 Lighter, G., 119-ATIO.TFPC-6/ATIO.VSTOL-1 Loubeau, A., 250-APA-37 Macquart, T., 237-MAO-13 Marwa, M., 144-AFM-10 Mendeck, G., 267-ITAR-6 Lightfoot, M., 295-FD-67 Love, N., 59-MAO-3 Madden, T., 129-ITAR-2 Marynowski, T., 135-TP-5 Meneveau, C., 23-FD-3 Lilie, L., 221-ASE-14 Low, K., 90-FD-16 Maedomari, T., 13-ATIO.ACD-1 Marzouk, Y., 178-APA-25/FD-38 Meng, X., 122-FC-6/FD-22, 205-PDL-5/FC-13, Lim, D., 289-ATIO.GA-3 Lowe, K., 245-AMT-10/GT-8 Magalhães Porto, F., 239-MST-12 Mascarenhas, B., 94-FD-20 283-APA-41/FD-63 Lim, J., 10-APA-4 Lowry, M., 291-ATIO.TFPC-13/ATIO.ATM-27 Magin, T., 251-ASE-15 Masek, T., 16-ATIO.ATM-3, 287-ATIO.ATM-25 Merbold, H., 32-TP-1 Limare, A., 22-FD-2 Lu, H., 186-ATIO.ATM-17 Mahapatra, S., 191-FD-39 Mason, M., 280-AMT-11 Mercer, E., 99-MST-5, 133-MST-8 Limbach, C., 6-AMT-1, 63-PDL-2 Lu, S., 302-TP-13 Maheshwari, A., 15-ATIO.ATM-2 Massey, K., 10-APA-4 Mercer, J., 45-ATIO.ATM-4 Lin, J., 50-FC-3, 190-FC-11, 201-MAO-11, 259-FC-16 Lu, Z., 122-FC-6/FD-22, 167-FD-37, 171-MST-9 Mahzari, M., 200-ITAR-4, 298-ITAR-7 Massuti-Ballester, B., 26-GT-1, 32-TP-1, 135-TP-5, Merli, S., 32-TP-1 Lin, Q., 168-GT-4 Luch, N., 16-ATIO.ATM-3, 184-ATIO.ATM-15 Maicke, B., 91-FD-17, 295-FD-67 243-TP-10 Merlino, D., 223-ATIO.ATM-18, 253-ATIO.ATM-21 Lin, W., 28-MAO-2, 170-MAO-10 Lucht, R., 177-AMT-7 Majewski, D., 182-ASE-11 Masters, D., 178-APA-25/FD-38 Merz, C., 246-APA-33/FD-54 Lindak, J., 58-FT-1 Luchtenburg, D., 121-FC-5 Majumdar, A., 16-ATIO.ATM-3 Masters, J., 92-FD-18 Meseguer-Garrido, F., 51-FD-9 Lindörfer, S., 165-FD-35 Luckner, R., 73-AFM-6 Makarov, K., 146-APA-21 Matayoshi, N., 288-ATIO.ATM-26 Mesh, M., 218-APA-30 Ling, D., 240-MST-13 Luckring, J., 110-APA-18, 199-GT-6 Maki, K., 164-FD-34 Matsui, K., 241-PDL-6 Messineo, J., 107-AMT-5 Lingfu, A., 129-ITAR-2 Ludwig, T., 152-ATIO.ATM-12 Maki, M., 175-AFM-11 Matsumoto, D., 147-APA-22 Metz, I., 99-MST-5 Author/Session Chair Index Meyer, T., 215-AMT-8 Moorhead, R., 113-ASE-7/ATIO.ATM-9 Nagel, B., 97-MAO-5 Nishida, H., 205-PDL-5/FC-13 Osterkamp, P., 58-FT-1 Meyers, J., 32-TP-1, 63-PDL-2 Moral, P., 108-APA-16/FD-21 Nagle, G., 15-ATIO.ATM-2 Nishikawa, H., 197-FD-45 Ostieri, M., 80-APA-14 Mi, Y., 74-AMT-3 Mora-Monteros, J., 243-TP-10 Naik, S., 284-APA-42/FD-64 Niu, J., 195-FD-43 Oswald, M., 285-ASE-17 Michal, T., 52-FD-10 Morando, A., 253-ATIO.ATM-21 Nair, R., 182-ASE-11 Niu, W., 240-MST-13 Otero, R., 245-AMT-10/GT-8 Michelassi, V., 52-FD-10 Moraru, C., 129-ITAR-2 Najaﬁ, A., 59-MAO-3, 97-MAO-5 Nobile, F., 297-FD-69 Othman, N., 217-APA-29 Michelis, T., 296-FD-68 Moreau, E., 160-FC-9/PDL-4/FD-29 Nakajima, T., 58-FT-1 Noeding, P., 265-FD-61 Othmer, C., 229-FC-14, 269-MAO-17 Michon, G., 74-AMT-3 Moreira, F., 57-FD-15 Nakakita, K., 58-FT-1, 218-APA-30 Nonomura, T., 122-FC-6/FD-22, 260-FC-17/FD-56 Otsuka, H., 78-APA-12 Micol, J., 128-GT-3 Morency, F., 95-GT-2, 280-AMT-11, 285-ASE-17 Nakamura, Y., 241-PDL-6 Noren, C., 101-PDL-3, 129-ITAR-2 Otsuki, T., 245-AMT-10/GT-8 Milbredt, O., 270-MST-15 Morgan, P., 55-FD-13, 126-FD-26 Nakano, A., 205-PDL-5/FC-13 Norman, N., 202-MAO-12 Otta, S., 114-ASE-8 Miles, R., 6-AMT-1, 26-GT-1, 36-AMT-2, 241-PDL-6 Morgan, R., 32-TP-1, 102-TP-3 Nakashima, T., 147-APA-22 Nouzawa, T., 147-APA-22 Otto, N., 45-ATIO.ATM-4 Milholen, W., 50-FC-3 Morgenstern, J., 250-APA-37 Nalci, O., 176-AFM-12 Novikov, A., 194-FD-42 Oursler, B., 73-AFM-6 Miller, L., 78-APA-12 Morlier, J., 202-MAO-12 Nangia, R., 185-ATIO.ATM-16 Nowak, D., 29-MST-1 Overton, N., 91-FD-17 Mills, B., 26-GT-1, 198-FT-3/GT-5 Morote, J., 282-APA-40 Napias, G., 74-AMT-3 Nowinski, J., 254-ATIO.ATM-22 Owens, D., 5-AFM-2, 127-FT-2, 200-ITAR-4, 236-ITAR-5 Milutinovic, D., 152-ATIO.ATM-12, 184-ATIO.ATM-15 Morris, C., 95-GT-2 Narayanarao, B., 178-APA-25/FD-38, Null, J., 152-ATIO.ATM-12 Owens, J., 136-TP-6 Min, S., 187-ATIO.GA-2, 289-ATIO.GA-3 Morscheck, F., 153-ATIO.ATM-13 246-APA-33/FD-54 Numata, D., 245-AMT-10/GT-8 Owens, L., 24-FD-4 Minton, T., 172-TP-7 Moss, M., 86-ATIO.DE-1, 268-MAO-16 Narayanaswamy, V., 55-FD-13, 126-FD-26, 191-FD-39 Nuzum, S., 169-ITAR-3 Oyama, A., 122-FC-6/FD-22, 260-FC-17/FD-56 Misaka, T., 42-ASE-3 Motil, B., 265-FD-61 Narkawicz, A., 15-ATIO.ATM-2, 117-ATIO.ATM-11 O`Callaghan, J., 254-ATIO.ATM-22, 288-ATIO.ATM-26 Oza, U., 41-APA-9 Miselis, M., 56-FD-14 Mott, D., 25-FD-7, 94-FD-20, 166-FD-36, 265-FD-61 Narkus-Kramer, M., 47-ATIO.TFPC-3 O’Brien, D., 109-APA-17, 181-APA-28, 218-APA-30 Ozawa, H., 191-FD-39 Mishra, J., 269-MAO-17 Motta, V., 38-FC-20 Natarajan, M., 38-FC-20 O’Farrell, C., 35-AFM-4, 181-APA-28 Ozcan, M., 13-ATIO.ACD-1, Mitsingas, C., 241-PDL-6 Mouyon, P., 38-FC-20 Naughton, J., 75-AMT-4, 260-FC-17/FD-56 O’Hara, R., 108-APA-16/FD-21 155-ATIO.TFPC-7/ATIO.ACD-6/GEPC-1 Mittal, R., 23-FD-3 Moyes, A., 56-FD-14 Nawaz, A., 168-GT-4, 302-TP-13 Obayashi, S., 42-ASE-3 Özcan, S., 80-APA-14 Mizoguchi, M., 126-FD-26, 283-APA-41/FD-63 Mueller, E., 132-MST-7 Naylor, B., 27-MAO-1 Oberkampf, W., 167-FD-37 Özgen, S., 150-ASE-10 Mizukaki, T., 191-FD-39, 280-AMT-11 Mueller-Vahl, H., 260-FC-17/FD-56 Nazarinia, M., 249-APA-36 Ochieng, W., 16-ATIO.ATM-3 Ozger, E., 198-FT-3/GT-5 Mizuno, A., 160-FC-9/PDL-4/FD-29 Mukhopadhyay, V., 301-MST-17 Neel, I., 261-FC-18/FD-57 Ofosu, J., 241-PDL-6 Ozguner, U., 45-ATIO.ATM-4

141 Moallemi, M., 100-MST-6 Mukkamala, Y., 300-MST-16 Neff, P., 116-ATIO.ATM-10 Ogawa, G., 201-MAO-11 Özgür, O., 282-APA-40 Moeller, T., 31-PDL-1, 91-FD-17 Mulani, S., 268-MAO-16 Neilan, J., 18-ATIO.TFPC-2, 257-ATIO.TFPC-11/ATIO.IS-1, Ogunsina, K., 153-ATIO.ATM-13 Öznalbant, Z., 83-ATIO.ACD-3 Moerder, D., 291-ATIO.TFPC-13/ATIO.ATM-27 Mulder, M., 61-MST-3, 270-MST-15 291-ATIO.TFPC-13/ATIO.ATM-27 Oguz, A., 45-ATIO.ATM-4, 84-ATIO.ATM-7 Ozoroski, L., 250-APA-37 Mohamad, Z., 180-APA-27 Mullen, C., 56-FD-14 Neitzel, K., 206-TP-8 Ohayon, R., 237-MAO-13 Ozoroski, T., 291-ATIO.TFPC-13/ATIO.ATM-27 Mohamed, A., 107-AMT-5 Mullen, J., 113-ASE-7/ATIO.ATM-9 Nelson, K., 133-MST-8 Ohme, P., 143-AFM-9 Ozturk, A., 203-MST-10 Mohammed-Taifour, A., 272-TP-11 Mulleners, K., 148-APA-23/FD-28, Neogi, N., 85-ATIO.ATM-8, 116-ATIO.ATM-10 Okada, Y., 147-APA-22 Packard, N., 158-FC-7 Mohd Raﬁe, A., 180-APA-27 263-FD-59/FC-19/APA-38 New, T., 193-FD-41/FC-12 Okuniek, J., 152-ATIO.ATM-12 Pack Melton, L., 190-FC-11, 259-FC-16 Mohd-Zawawi, F., 261-FC-18/FD-57 Mumm, N., 5-AFM-2 Newman, J., 22-FD-2, 28-MAO-2, 170-MAO-10, Ol, M., 193-FD-41/FC-12, 284-APA-42/FD-64 Pagadala, P., 62-MST-4 Mohlenbrink, C., 255-ATIO.ATM-23 Munafò, A., 273-TP-12 197-FD-45 Olcott, D., 119-ATIO.TFPC-6/ATIO.VSTOL-1 Pagaldipti, N., 170-MAO-10 Mohr, O., 99-MST-5 Mundis, N., 164-FD-34 Ng, H., 185-ATIO.ATM-16 Olejniczak, J., 200-ITAR-4 Pagan, A., 243-TP-10 Mohrmann, F., 61-MST-3 Mundt, C., 295-FD-67 Ng, W., 245-AMT-10/GT-8 Oliver, B., 64-TP-2, 200-ITAR-4, 236-ITAR-5, 267-ITAR-6 Pagani, C., 123-FD-23 Moini-Yekta, S., 146-APA-21 Munoz, C., 15-ATIO.ATM-2 Nguyen, C., 252-ASE-16 Oliver, M., 183-ASE-12 Pagliaroli, T., 261-FC-18/FD-57 Molina-Cristobal, A., 13-ATIO.ACD-1 Muppidi, S., 35-AFM-4, 181-APA-28, 273-TP-12, Nguyen, D., 289-ATIO.GA-3 Oliver, R., 119-ATIO.TFPC-6/ATIO.VSTOL-1 Paglione, M., 286-ATIO.ATM-24 Momani, A., 61-MST-3 303-TP-14 Nguyen, L., 263-FD-59/FC-19/APA-38 Oliviu, S., 217-APA-29 Paglione, P., 73-AFM-6 Monach, W., 42-ASE-3 Murayama, M., 146-APA-21 Nguyen, N., 44-ATIO.ACD-2, 59-MAO-3, 77-APA-11, Olsen, M., 192-FD-40 Pagliuca, G., 175-AFM-11 Monastero, M., 50-FC-3 Murk, A., 32-TP-1 111-APA-19 Olson, E., 27-MAO-1 Paielli, R., 16-ATIO.ATM-3 Mondal, P., 178-APA-25/FD-38, 246-APA-33/FD-54 Murman, S., 192-FD-40, 267-ITAR-6 Ni, A., 297-FD-69 Om, P., 106-AFM-8 Palacios, J., 43-ASE-4, 82-ASE-6/APA-15, 114-ASE-8, Monnier, J., 38-FC-20, 39-APA-7 Murphy, J., 45-ATIO.ATM-4 Nichols, J., 126-FD-26 Ombrello, T., 215-AMT-8, 271-PDL-7 150-ASE-10, 234-FD-53 Montalvo, C., 73-AFM-6 Murray, J., 7-APA-1, 37-APA-6/FD-8, 148-APA-23/FD-28 Nichols, R., 303-TP-14 Oran, E., 172-TP-7 Palacios, R., 97-MAO-5 Moolchandani, K., 15-ATIO.ATM-2, 153-ATIO.ATM-13 Murray, V., 172-TP-7 Nickels, A., 123-FD-23 Orchard, D., 220-ASE-13 Paliath, U., 52-FD-10, 167-FD-37 Mooney, R., 116-ATIO.ATM-10 Murri, D., 5-AFM-2, 144-AFM-10 Nickolaou, J., 118-ATIO.TFPC-5 Orieux, S., 259-FC-16 Palla, A., 241-PDL-6 Moore, J., 93-FD-19 Murrieta Mendoza, A., 253-ATIO.ATM-21 Nicolaon, J., 42-ASE-3 Orkwis, P., 25-FD-7, 54-FD-12, 165-FD-35 Palma, R., 86-ATIO.DE-1 Moore, M., 18-ATIO.TFPC-2, 87-ATIO.TFPC-4/ATIO.GA-1, Murzello, R., 249-APA-36 Nicolosi, F., 281-APA-39 Orr, M., 151-ATIO.ACD-5 Palotai, C., 251-ASE-15 118-ATIO.TFPC-5, Myers, L., 76-APA-10, 262-FD-58 Nigam, N., 133-MST-8 Orra, T., 27-MAO-1, 131-MAO-8 Pan, H., 79-APA-13 155-ATIO.TFPC-7/ATIO.ACD-6/GEPC-1, Nabarrete, A., 171-MST-9 Niklass, M., 153-ATIO.ATM-13 Osanov, M., 28-MAO-2 Pan, J., 216-AMT-9 188-ATIO.TFPC-8/ATIO.FT-1/GEPC-2, Nagapetyan, H., 90-FD-16 Nikoleris, A., 16-ATIO.ATM-3 Osborne, B., 79-APA-13 Panchal, J., 15-ATIO.ATM-2 226-ATIO.TFPC-10/ATIO.VSTOL-2 Nagaram, M., 246-APA-33/FD-54 Nimmagadda, S., 196-FD-44 Osei-Wusu, K., 267-ITAR-6 Pandare, A., 265-FD-61 Moored, K., 108-APA-16/FD-21 Nagatani, K., 78-APA-12 Ning, A., 132-MST-7 Ossenfort, J., 254-ATIO.ATM-22 Author/Session Chair Index Panesi, M., 135-TP-5, 206-TP-8, 264-FD-60, Petro, E., 134-NIA-1 Prevot, T., 45-ATIO.ATM-4, 46-ATIO.ATM-5 Rauleder, J., 9-APA-3, 78-APA-12 Rizzetta, D., 190-FC-11 273-TP-12, 303-TP-14 Pett, A., 285-ASE-17 Probst, Z., 58-FT-1 Raveh, D., 8-APA-2, 40-APA-8 Roach, K., 152-ATIO.ATM-12 Pang, Z., 73-AFM-6 Pett, T., 99-MST-5 Proctor, F., 252-ASE-16 Ravikumar, K., 290-ATIO.TFPC-12 Roberts, L., 147-APA-22 Pangborn, H., 169-ITAR-3 Peyada, N., 143-AFM-9 Proﬁr, B., 86-ATIO.DE-1 Rebollo, J., 287-ATIO.ATM-25 Roberts, R., 169-ITAR-3 Pant, R., 256-ATIO.LTA-1 Pfaender, H., 15-ATIO.ATM-2 Provalov, A., 84-ATIO.ATM-7 Reddy, K., 241-PDL-6 Robins, R., 81-ASE-5 Pantaleao, A., 8-APA-2 Pham, N., 136-TP-6 Pruis, M., 42-ASE-3, 81-ASE-5, 251-ASE-15 Reddy, L., 45-ATIO.ATM-4, 116-ATIO.ATM-10 Robinson, J., 44-ATIO.ACD-2, 201-MAO-11 Paramasivam, S., 249-APA-36 Pham, S., 55-FD-13 Przekop, A., 187-ATIO.GA-2 Redmill, K., 45-ATIO.ATM-4 Robinson, M., 185-ATIO.ATM-16, 254-ATIO.ATM-22 Parammasivam, K., 77-APA-11 Philippidis, D., 168-GT-4 Puig-Navarro, J., 257-ATIO.TFPC-11/ATIO.IS-1 Reed, H., 56-FD-14, 163-FD-33, 210-FD-46 Robinson, P., 200-ITAR-4 Paras, M., 73-AFM-6 Phillips, B., 198-FT-3/GT-5 Puigt, G., 231-FD-48 Reed, M., 62-MST-4 Robinson, R., 63-PDL-2 Paredes, P., 163-FD-33, 194-FD-42 Piao, Y., 195-FD-43 Pulliam, T., 53-FD-11, 196-FD-44 Reeder, M., 58-FT-1, 112-APA-20 Robinson, S., 11-ASE-1, 122-FC-6/FD-22 Paris, S., 168-GT-4 Pickles, J., 55-FD-13 Puranik, T., 187-ATIO.GA-2 Reger, R., 123-FD-23 Robinson III, J., 45-ATIO.ATM-4 Parish, E., 125-FD-25 Pigazzini, M., 238-MAO-14 Pytel, D., 96-ITAR-1 Rehman, H., 272-TP-11 Robison, R., 82-ASE-6/APA-15 Park, C., 303-TP-14 Pinier, J., 110-APA-18 Qian, D., 95-GT-2 Reiche, C., 185-ATIO.ATM-16 Rocco, E., 43-ASE-4 Park, J., 217-APA-29 Pinna, F., 293-FD-65 Qian, Z., 93-FD-19, 196-FD-44 Reimann, B., 112-APA-20 Rockwell, R., 6-AMT-1 Park, M., 52-FD-10 Pisaroni, M., 297-FD-69 Qiang, Z., 171-MST-9 Reinholtz, C., 132-MST-7 Rodarte Ricciardi, T., 247-APA-34/FD-55 Parziale, N., 6-AMT-1 Pitre, R., 130-MAO-7 Qiao, L., 93-FD-19 Reising, H., 107-AMT-5 Rodriguez, E., 298-ITAR-7 Pasiliao, C., 146-APA-21, 217-APA-29, 282-APA-40 Placidi, M., 89-FC-4, 190-FC-11 Qin, C., 149-ASE-9 Reissner, F., 260-FC-17/FD-56 Roedts, R., 58-FT-1 Patel, D., 300-MST-16 Planchenault, P., 7-APA-1 Qin, Y., 30-MST-2, 191-FD-39, 217-APA-29, 248-APA-35 Reist, T., 180-APA-27 Rogers, M., 52-FD-10 Patnaik, G., 25-FD-7 Platzer, S., 78-APA-12 Qiu, J., 300-MST-16 Remark, B., 298-ITAR-7 Rogers, S., 267-ITAR-6 Patterson, M., 118-ATIO.TFPC-5, Plesniak, M., 94-FD-20 Qu, K., 130-MAO-7 Rempfer, D., 162-FD-32/FC-10 Roggenkämper, N., 270-MST-15 155-ATIO.TFPC-7/ATIO.ACD-6/GEPC-1, Pnaerai, F., 32-TP-1 Qu, Q., 146-APA-21, 234-FD-53, 248-APA-35, 265-FD-61 Ren, H., 240-MST-13, 295-FD-67 Rolston, S., 7-APA-1 188-ATIO.TFPC-8/ATIO.FT-1/GEPC-2 Pochiraju, K., 167-FD-37 Qu, X., 170-MAO-10 Ren, J., 194-FD-42 Romero, J., 196-FD-44 Patton, C., 195-FD-43 Poedts, S., 31-PDL-1 Quach, C., 29-MST-1 Ren, Y., 93-FD-19, 246-APA-33/FD-54 Röntsch, B., 20-FC-1 Paul, B., 149-ASE-9 Poggie, J., 31-PDL-1 Qualls, G., 257-ATIO.TFPC-11/ATIO.IS-1 Ren, Z., 265-FD-61 Roper, R., 46-ATIO.ATM-5

142 Pavlenko, A., 146-APA-21 Pomeroy, B., 10-APA-4 Quero-Martin, D., 179-APA-26 Rendall, T., 28-MAO-2, 178-APA-25/FD-38, 230-FC-15 Rosema, C., 181-APA-28 Pedras, M., 8-APA-2 Pommier-Budinger, V., 74-AMT-3, 82-ASE-6/APA-15 Quijada, G., 5-AFM-2 Rennie, M., 101-PDL-3 Rosenberg, K., 296-FD-68 Pei, Y., 100-MST-6 Poncet-Montanges, A., 204-MST-11 Quinlan, J., 86-ATIO.DE-1, 301-MST-17 Reshotko, E., 194-FD-42 Rosenberg, R., 196-FD-44 Peinke, J., 9-APA-3, 148-APA-23/FD-28 Pool, D., 61-MST-3, 270-MST-15 Rachelson, E., 202-MAO-12 Reynolds, K., 77-APA-11 Rossmann, T., 165-FD-35, 233-FD-50 Pekardan, C., 303-TP-14 Poole, D., 28-MAO-2, 230-FC-15 Radenac, E., 12-ASE-2, 149-ASE-9, 285-ASE-17 Reynolds, T., 154-ATIO.ATM-14, 185-ATIO.ATM-16, Rossow, C., 52-FD-10 Pellicone, D., 169-ITAR-3 Poovathingal, S., 172-TP-7 Radespiel, R., 293-FD-65 223-ATIO.ATM-18, 255-ATIO.ATM-23 Rothhaar, P., 18-ATIO.TFPC-2, Peng, B., 44-ATIO.ACD-2, 283-APA-41/FD-63 Poroseva, S., 192-FD-40 Radomiak, H., 272-TP-11 Rezin, M., 236-ITAR-5, 298-ITAR-7 257-ATIO.TFPC-11/ATIO.IS-1, Peng, D., 75-AMT-4 Porter, B., 245-AMT-10/GT-8 Raghu, S., 190-FC-11 Rhew, R., 199-GT-6 291-ATIO.TFPC-13/ATIO.ATM-27 Peng, S., 90-FD-16, 218-APA-30 Portlock, J., 119-ATIO.TFPC-6/ATIO.VSTOL-1 Raghunandan, P., 272-TP-11 Rhode, M., 26-GT-1 Rothmayer, A., 12-ASE-2, 82-ASE-6/APA-15 Pensado, A., 122-FC-6/FD-22 Porto, F., 239-MST-12 Ragni, D., 78-APA-12, 260-FC-17/FD-56 Rhodes, M., 96-ITAR-1 Rouzbar, R., 295-FD-67 Pera, N., 134-NIA-1 Post, M., 37-APA-6/FD-8, 80-APA-14, Rahimi, H., 9-APA-3 Rhudy, M., 270-MST-15 Rowe, S., 86-ATIO.DE-1 Percin, M., 108-APA-16/FD-21 178-APA-25/FD-38 Rahman, M., 125-FD-25, 262-FD-58 Riaz, A., 13-ATIO.ACD-1 Rowley, C., 121-FC-5, 232-FD-49 Pereira, M., 171-MST-9 Potapczuk, M., 43-ASE-4, 149-ASE-9, 285-ASE-17 Raiche, G., 302-TP-13 Ricchiuto, M., 197-FD-45 Roy, C., 53-FD-11, 166-FD-36, 167-FD-37 Perez, J., 121-FC-5, 161-FD-30/APA-24 Potturi, A., 25-FD-7 Raines, D., 151-ATIO.ACD-5 Rice, T., 230-FC-15 Roy, S., 36-AMT-2, 107-AMT-5, 205-PDL-5/FC-13, Perez, R., 39-APA-7, 115-ATIO.ACD-4, 151-ATIO.ACD-5 Pounds, D., 96-ITAR-1 Raiola, M., 108-APA-16/FD-21, 260-FC-17/FD-56 Richard, B., 169-ITAR-3 215-AMT-8, 286-ATIO.ATM-24 Perez Arroyo, C., 231-FD-48 Pourhashem, H., 259-FC-16 Raj, P., 83-ATIO.ACD-3, 217-APA-29 Richards, D., 61-MST-3 Roychoudhury, I., 254-ATIO.ATM-22 Peristy, L., 39-APA-7 Povitsky, A., 283-APA-41/FD-63 Raja, S., 77-APA-11 Richardson, D., 107-AMT-5, 177-AMT-7 Roza, M., 239-MST-12 Pernicka, H., 59-MAO-3 Powell, J., 200-ITAR-4 Rajarao, P., 285-ASE-17 Richey, M., 86-ATIO.DE-1 Rozzi, J., 136-TP-6 Peroomian, O., 25-FD-7 Power, G., 303-TP-14 Rajasegar, R., 241-PDL-6 Richwine, D., 250-APA-37 Ruan, L., 270-MST-15 Perron, C., 155-ATIO.TFPC-7/ATIO.ACD-6/GEPC-1 Powers, R., 76-APA-10 Rallabhandi, S., 219-APA-32 Rigby, D., 114-ASE-8 Rudenko, N., 262-FD-58 Perry, A., 248-APA-35 Prabhu, D., 243-TP-10 Ramamurti, R., 37-APA-6/FD-8 Righi, M., 40-APA-8, 246-APA-33/FD-54 Ruetten, M., 284-APA-42/FD-64 Pervier, H., 220-ASE-13 Prakasha, P., 130-MAO-7 Rambau, T., 239-MST-12 Riley, Z., 129-ITAR-2 Rufer, S., 267-ITAR-6, 280-AMT-11 Peters, C., 36-AMT-2 Prasad, R., 76-APA-10, 201-MAO-11 Rame, E., 265-FD-61 Rinehart, D., 254-ATIO.ATM-22 Ruff, R., 203-MST-10, 240-MST-13, 301-MST-17 Peters, L., 187-ATIO.GA-2 Prat, D., 7-APA-1 Ramee, C., 83-ATIO.ACD-3 Rinoie, K., 13-ATIO.ACD-1 Rufﬁn, S., 179-APA-26, 272-TP-11 Peterse, H., 61-MST-3 Preator, R., 226-ATIO.TFPC-10/ATIO.VSTOL-2 Ramesh, K., 246-APA-33/FD-54 Rios, J., 14-ATIO.ATM-1, 45-ATIO.ATM-4 Rumpfkeil, M., 112-APA-20 Peterson, C., 158-FC-7 Preisighe Viana, M., 143-AFM-9 Rao, A., 154-ATIO.ATM-14, 187-ATIO.GA-2 Risukhin, V., 187-ATIO.GA-2 Rumsey, C., 192-FD-40 Petitpas, F., 265-FD-61 Premachandran, S., 21-FC-2/FD-1/APA-5 Ratcliff, C., 176-AFM-12 Rivers, M., 95-GT-2 Rungta, N., 99-MST-5, 133-MST-8 Petkov, I., 233-FD-50 Premaratne, P., 161-FD-30/APA-24 Ratvasky, T., 183-ASE-12, 221-ASE-14, 252-ASE-16 Rizvi, F., 100-MST-6 Rusak, Z., 294-FD-66 Author/Session Chair Index Rutherford, J., 119-ATIO.TFPC-6/ATIO.VSTOL-1 Sayadi, T., 166-FD-36 Selvi, S., 97-MAO-5 Shu, L., 202-MAO-12 Sousa, M., 239-MST-12 Rutherford, M., 76-APA-10 Scanlan, J., 86-ATIO.DE-1, 268-MAO-16 Sembiring, J., 143-AFM-9 Shumaker, S., 295-FD-67 Soutade, J., 107-AMT-5 Ryan, W., 118-ATIO.TFPC-5 Schaefer, J., 297-FD-69 Semenov, I., 271-PDL-7 Shyam, V., 177-AMT-7 Soyer, S., 80-APA-14 Rzucidlo, P., 29-MST-1 Schairer, E., 58-FT-1 Seneviratne, L., 29-MST-1 Si, J., 54-FD-12 Spagnolo, S., 41-APA-9 Sacco, C., 230-FC-15 Schatzman, D., 259-FC-16 Sengupta, S., 205-PDL-5/FC-13, 231-FD-48 Sibilski, K., 106-AFM-8, 143-AFM-9 Spencer, G., 249-APA-36 Saddington, A., 21-FC-2/FD-1/APA-5 Schauerhamer, D., 11-ASE-1 Sengupta, T., 205-PDL-5/FC-13 Siddiqui, F., 194-FD-42 Spero, E., 83-ATIO.ACD-3 Sadique, J., 23-FD-3 Schaus, E., 83-ATIO.ACD-3 Serani, A., 269-MAO-17 Siddle-Mitchel, S., 74-AMT-3 Spillers, R., 51-FD-9, 74-AMT-3 Sadovsky, A., 117-ATIO.ATM-11 Scheneman, B., 203-MST-10 Serhat, G., 97-MAO-5 Sidiropoulos, S., 16-ATIO.ATM-3 Spisz, T., 267-ITAR-6 Sadraey, M., 83-ATIO.ACD-3, 144-AFM-10 Schetz, J., 59-MAO-3, 217-APA-29 Serpieri, J., 163-FD-33 Sidoryuk, M., 5-AFM-2 Splichenko, M., 107-AMT-5, 215-AMT-8 Saeed, A., 29-MST-1 Schiavo, L., 125-FD-25 Sescu, A., 54-FD-12, 193-FD-41/FC-12, 293-FD-65 Siegel, J., 143-AFM-9 Splinter, S., 32-TP-1 Sagebaum, M., 98-MAO-6 Schier, S., 99-MST-5 Seyed-Yagoobi, J., 242-TP-9 Siikonen, T., 125-FD-25 Spode, C., 8-APA-2 Sagerman, D., 112-APA-20 Schiltgen, B., 222-ATIO.ACD-7/ATIO.TFPC-9 Sha, Z., 15-ATIO.ATM-2 Silk, E., 96-ITAR-1 Spoor, M., 151-ATIO.ACD-5, 190-FC-11 Sahai, A., 135-TP-5 Schluter, J., 11-ASE-1, 247-APA-34/FD-55, 249-APA-36 Shahbazi, K., 54-FD-12, 57-FD-15 Silton, S., 112-APA-20, 282-APA-40 Sprague, M., 52-FD-10 Sahni, O., 158-FC-7, 230-FC-15 Schmid, P., 166-FD-36 Shamsaei, B., 22-FD-2 Silva, W., 77-APA-11 Sridhar, B., 14-ATIO.ATM-1, 116-ATIO.ATM-10, Sahu, J., 112-APA-20, 282-APA-40 Schmidmayer, K., 265-FD-61 Shankaran, S., 52-FD-10 Silvestre, F., 27-MAO-1, 73-AFM-6, 105-AFM-7 117-ATIO.ATM-11, 185-ATIO.ATM-16, 286-ATIO.ATM-24 Saiki, J., 170-MAO-10 Schmidt, J., 107-AMT-5, 136-TP-6 Shanmugam, P., 77-APA-11 Simpson, R., 78-APA-12 Sridhar, M., 37-APA-6/FD-8 Saka, P., 76-APA-10 Schmisseur, J., 55-FD-13, 165-FD-35, 280-AMT-11 Shannon, T., 114-ASE-8 Simsek, B., 302-TP-13 Sridharan, A., 108-APA-16/FD-21 Sakaue, H., 89-FC-4 Schmit, M., 203-MST-10 Shao, C., 79-APA-13 Singh, G., 59-MAO-3 Srinivasan, P., 204-MST-11 Salazar, G., 64-TP-2, 236-ITAR-5 Schmit, R., 51-FD-9 Shao Jie, G., 248-APA-35 Singh, N., 172-TP-7, 273-TP-12 Srivastava, K., 37-APA-6/FD-8 Saleem, M., 55-FD-13 Schmitt, A., 133-MST-8 Sharma, A., 98-MAO-6 Singh, V., 238-MAO-14 Stanford, B., 77-APA-11, 131-MAO-8, 201-MAO-11, Salhi, M., 249-APA-36 Schmitz, S., 167-FD-37 Sharma, P., 230-FC-15 Sinn, T., 301-MST-17 269-MAO-17 Samimi Abianeh, O., 195-FD-43 Schneider, G., 302-TP-13 Sharma, R., 15-ATIO.ATM-2, 159-FC-8 Sinnige, T., 78-APA-12 Starikovskiy, A., 205-PDL-5/FC-13, 241-PDL-6, Samimy, M., 21-FC-2/FD-1/APA-5 Schneider, S., 56-FD-14 Sharma, S., 13-ATIO.ACD-1, 255-ATIO.ATM-23 Sipp, D., 39-APA-7 271-PDL-7 Samuel, J., 125-FD-25 Schoenenberger, M., 35-AFM-4, 102-TP-3, 181-APA-28, Sheikh, U., 32-TP-1, 243-TP-10 Sitaraman, J., 10-APA-4 Stark, A., 265-FD-61

143 Sandberg, M., 185-ATIO.ATM-16 281-APA-39 Shelton, A., 282-APA-40 Sivasubramanian, J., 126-FD-26, 261-FC-18/FD-57 Stauffer, H., 36-AMT-2, 107-AMT-5 Sandel, W., 183-ASE-12 Schrock, C., 25-FD-7, 53-FD-11, 164-FD-34, 166-FD-36 Shen, L., 4-AFM-1 Sivo, C., 221-ASE-14 Steen, L., 220-ASE-13 Sandham, N., 261-FC-18/FD-57 Schuelein, E., 24-FD-4 Shen, N., 16-ATIO.ATM-3, 184-ATIO.ATM-15 Skote, M., 249-APA-36 Stefanski, D., 22-FD-2 Sandhu, J., 230-FC-15 Schuette, A., 247-APA-34/FD-55 Shen, Q., 198-FT-3/GT-5 Slater, J., 219-APA-32 Stehno, P., 136-TP-6 Sanetrik, M., 77-APA-11 Schultz, M., 224-ATIO.ATM-19 Shen, X., 59-MAO-3 Slupski, B., 39-APA-7 Steijl, R., 159-FC-8 Sankaran, V., 164-FD-34 Schultz, V., 113-ASE-7/ATIO.ATM-9 Shen, Z., 53-FD-11 Smith, A., 165-FD-35 Steiner, J., 114-ASE-8 Sankararaman, S., 254-ATIO.ATM-22 Schuman, W., 127-FT-2, 198-FT-3/GT-5 Shende, N., 178-APA-25/FD-38, 246-APA-33/FD-54 Smith, B., 192-FD-40 Steiner, M., 254-ATIO.ATM-22 Santos, J., 102-TP-3, 256-ATIO.LTA-1, 298-ITAR-7 Schumann, U., 143-AFM-9 Sheng, C., 76-APA-10, 246-APA-33/FD-54 Smith, C., 202-MAO-12 Stelmack, M., 131-MAO-8, 299-MAO-18 Santos, M., 15-ATIO.ATM-2 Schuster, D., 8-APA-2, 267-ITAR-6 Shengyang, N., 112-APA-20 Smith, D., 121-FC-5, 162-FD-32/FC-10 Stephan, A., 11-ASE-1, 247-APA-34/FD-55 Sanz, S., 73-AFM-6 Schwaab, Q., 216-AMT-9, 280-AMT-11 Sherer, S., 126-FD-26 Smith, J., 24-FD-4, 82-ASE-6/APA-15, 218-APA-30 Stephani, K., 172-TP-7, 264-FD-60, 303-TP-14 Sanzi, R., 233-FD-50 Schwartz, K., 15-ATIO.ATM-2 Sheth, K., 15-ATIO.ATM-2, 253-ATIO.ATM-21 Smith, M., 143-AFM-9, 176-AFM-12 Stephanopoulos, K., 297-FD-69 Sapell, A., 37-APA-6/FD-8 Schwartz, R., 267-ITAR-6 Shi, A., 175-AFM-11 Smith, N., 46-ATIO.ATM-5, 85-ATIO.ATM-8, Stern, E., 32-TP-1, 35-AFM-4 Saraf, A., 16-ATIO.ATM-3, 184-ATIO.ATM-15 Schwartzentruber, T., 172-TP-7, 273-TP-12 Shi, R., 299-MAO-18 255-ATIO.ATM-23 Stern, F., 269-MAO-17 Saraf, S., 136-TP-6 Schwarzenboeck, A., 221-ASE-14 Shi, S., 100-MST-6 Smith, R., 298-ITAR-7 Stevanovic, S., 256-ATIO.LTA-1 Saranathan, H., 35-AFM-4 Schwing, A., 35-AFM-4, 200-ITAR-4, 267-ITAR-6 Shi, X., 54-FD-12, 271-PDL-7, 296-FD-68 Smith, S., 96-ITAR-1, 113-ASE-7/ATIO.ATM-9, 136- Stevens, M., 14-ATIO.ATM-1 Sargeant, J., 124-FD-24 Sclafani, A., 147-APA-22 Shih, F., 253-ATIO.ATM-21 TP-6, 202-MAO-12 Stoellinger, M., 192-FD-40 Saripalli, K., 158-FC-7 Scoﬁeld, J., 242-TP-9 Shimamura, K., 241-PDL-6 Smith, T., 181-APA-28 Stoevesandt, B., 9-APA-3, 148-APA-23/FD-28 Sarma, A., 182-ASE-11 Sebastiao, I., 172-TP-7 Shimano, T., 241-PDL-6 Smits, A., 162-FD-32/FC-10, 232-FD-49 Stoll, A., 119-ATIO.TFPC-6/ATIO.VSTOL-1, Sartor, F., 39-APA-7, 123-FD-23 Seckin, S., 55-FD-13 Shimizu, Y., 166-FD-36 Smoot, C., 96-ITAR-1 155-ATIO.TFPC-7/ATIO.ACD-6/GEPC-1, Sasanapuri, B., 285-ASE-17 Seedhouse, E., 198-FT-3/GT-5 Shin, S., 108-APA-16/FD-21, 225-ATIO.ATM-20 Sobester, A., 44-ATIO.ACD-2, 188-ATIO.TFPC-8/ATIO.FT-1/GEPC-2 Sasoh, A., 55-FD-13, 191-FD-39, 219-APA-32 Seeley, B., 87-ATIO.TFPC-4/ATIO.GA-1, 118-ATIO.TFPC-5 Shinde, S., 164-FD-34 222-ATIO.ACD-7/ATIO.TFPC-9 Stouffer, V., 15-ATIO.ATM-2, 47-ATIO.TFPC-3 Satija, A., 177-AMT-7 Seers, P., 272-TP-11 Shkarayev, S., 7-APA-1 Sol, M., 44-ATIO.ACD-2 Strader, J., 127-FT-2 Sato, K., 168-GT-4, 233-FD-50 Segee, M., 217-APA-29 Shmilovich, A., 50-FC-3, 190-FC-11 Sommerwerk, H., 82-ASE-6/APA-15 Strapp, J., 221-ASE-14 Sato, M., 122-FC-6/FD-22 Seidel, J., 20-FC-1, 25-FD-7, 124-FD-24, 259-FC-16 Shneider, M., 36-AMT-2, 271-PDL-7 Song, B., 100-MST-6, 268-MAO-16 Streett, T., 200-ITAR-4 Sattler, S., 220-ASE-13 Seifert, A., 229-FC-14 Shoda, T., 55-FD-13 Song, C., 178-APA-25/FD-38 Stremel, P., 199-GT-6 Sauterleute, D., 225-ATIO.ATM-20 Seitzman, J., 145-AMT-6 Short, E., 302-TP-13 Song, J., 37-APA-6/FD-8 Strganac, T., 4-AFM-1 Savill, A., 60-MAO-4 Selig, M., 10-APA-4, 105-AFM-7, 147-APA-22 Shrestha, P., 126-FD-26, 293-FD-65 Song, L., 106-AFM-8 Struk, P., 150-ASE-10 Saxena, U., 144-AFM-10 Selim, M., 301-MST-17 Shu, C., 54-FD-12, 296-FD-68 Song, W., 268-MAO-16 Stuart, P., 200-ITAR-4 Author/Session Chair Index Stumpf, E., 47-ATIO.TFPC-3 Tanno, H., 168-GT-4, 233-FD-50 Tittsworth, J., 81-ASE-5 Uslu, S., 302-TP-13 Villedieu, P., 43-ASE-4, 150-ASE-10 Su, C., 219-APA-32 Taoudi, L., 193-FD-41/FC-12 Tobalske, B., 37-APA-6/FD-8 Vaddi, S., 186-ATIO.ATM-17 Vinha, N., 51-FD-9 Su, E., 7-APA-1 Taubert, L., 20-FC-1 Tobin, S., 102-TP-3 Vaidya, A., 225-ATIO.ATM-20 Visbal, M., 124-FD-24, 126-FD-26, 190-FC-11, Su, P., 79-APA-13 Tay, G., 153-ATIO.ATM-13 Togiti, V., 192-FD-40 Valavanis, K., 76-APA-10 260-FC-17/FD-56, 284-APA-42/FD-64, 293-FD-65 Subbareddy, P., 55-FD-13, 293-FD-65 Tay, W., 108-APA-16/FD-21 Tognaccini, R., 80-APA-14 Valenti, J., 262-FD-58 Visser, D., 185-ATIO.ATM-16 Subramaniam, A., 57-FD-15 Taylor, B., 265-FD-61 Toledano, A., 95-GT-2 Valentini, P., 273-TP-12 Visser, K., 148-APA-23/FD-28, 281-APA-39 Subramaniam, S., 303-TP-14 Taylor, C., 61-MST-3, 99-MST-5, 117-ATIO.ATM-11, Tomczyk, A., 29-MST-1 Valero, E., 51-FD-9, 170-MAO-10 Viti, A., 60-MAO-4, 97-MAO-5 Subramanian, S., 230-FC-15 186-ATIO.ATM-17, 253-ATIO.ATM-21 Tong, O., 57-FD-15, 164-FD-34 Valla, M., 42-ASE-3 Vivona, R., 223-ATIO.ATM-18 Suchomel, C., 63-PDL-2, 105-AFM-7, 175-AFM-11 Taylor, J., 267-ITAR-6 Toropov, V., 59-MAO-3, 202-MAO-12, 299-MAO-18 van Bokhorst, E., 89-FC-4, 190-FC-11 Vogiatzis, K., 273-TP-12 Sullivan, A., 216-AMT-9 Taylor, L., 197-FD-45 Torres, S., 15-ATIO.ATM-2, 286-ATIO.ATM-24 Van Dam, C., 122-FC-6/FD-22 Voloshin, V., 13-ATIO.ACD-1 Sun, Y., 240-MST-13 Taylor, N., 92-FD-18, 178-APA-25/FD-38 Toussaint, S., 116-ATIO.ATM-10 Vanden, K., 41-APA-9 Volpe, E., 166-FD-36 Sung, P., 270-MST-15 Tchatchueng Kammegne, M., 72-AFM-5, 289-ATIO.GA-3 Towhidnejad, M., 100-MST-6 van den Kieboom, K., 97-MAO-5 Vorspel, L., 148-APA-23/FD-28 Suresh Babu, A., 246-APA-33/FD-54 Tejeda, J., 47-ATIO.TFPC-3 Trajkov, S., 47-ATIO.TFPC-3 van der Burg, J., 247-APA-34/FD-55 Vos, R., 44-ATIO.ACD-2 Suryakumar, V., 4-AFM-1 Tekinalp, O., 176-AFM-12 Tran, H., 253-ATIO.ATM-21 van der Geest, M., 188-ATIO.TFPC-8/ATIO.FT-1/GEPC-2 Voss, A., 171-MST-9 Surzhikov, S., 206-TP-8, 271-PDL-7 Telli, H., 80-APA-14 Tran, J., 190-FC-11 Vander Kam, J., 298-ITAR-7 Vukasinovic, B., 158-FC-7, 229-FC-14 Sutton, J., 6-AMT-1 Tepylo, N., 82-ASE-6/APA-15 Tran, L., 18-ATIO.TFPC-2, 257-ATIO.TFPC-11/ATIO.IS-1, van der Weide, E., 247-APA-34/FD-55 Vutetakis, D., 290-ATIO.TFPC-12 Suzuki, K., 234-FD-53, 284-APA-42/FD-64 Tesfahunegn, Y., 98-MAO-6, 178-APA-25/FD-38 291-ATIO.TFPC-13/ATIO.ATM-27 Vanderwyst, A., 79-APA-13, 111-APA-19, 176-AFM-12, Vyas, M., 23-FD-3, 125-FD-25 Swaid, M., 287-ATIO.ATM-25 Tetteh, F., 82-ASE-6/APA-15 Trapani, G., 124-FD-24 282-APA-40 Wadel, M., 221-ASE-14 Swaminathan Gopalan, K., 303-TP-14 Teubert, C., 29-MST-1 Tromme, E., 28-MAO-2 van Heerden, A., 13-ATIO.ACD-1 Wadhams, T., 233-FD-50 Sweeney, C., 56-FD-14 Tewes, P., 20-FC-1 Trontin, P., 43-ASE-4, 150-ASE-10 Van Hove, B., 251-ASE-15 Wadnerkar, R., 178-APA-25/FD-38 Swieringa, K., 46-ATIO.ATM-5, 152-ATIO.ATM-12, Thamann, M., 113-ASE-7/ATIO.ATM-9 Troub, B., 73-AFM-6 van Jindelt, T., 247-APA-34/FD-55 Wagner, A., 24-FD-4, 261-FC-18/FD-57 184-ATIO.ATM-15 Thapa, M., 268-MAO-16 Troxel, S., 223-ATIO.ATM-18 van Kuik, G., 260-FC-17/FD-56 Wagner, J., 51-FD-9, 74-AMT-3 Swirydowicz, K., 166-FD-36 Theiss, A., 293-FD-65 Trujillo, A., 18-ATIO.TFPC-2, 257-ATIO.TFPC-11/ATIO.IS-1, Van Norman, J., 181-APA-28 Wahls, R., 110-APA-18 Switzer, G., 252-ASE-16 Thekinen, J., 15-ATIO.ATM-2 291-ATIO.TFPC-13/ATIO.ATM-27 van Oudheusden, B., 108-APA-16/FD-21, 293-FD-65 Waindim, M., 23-FD-3, 231-FD-48

144 Sydney, A., 107-AMT-5 Thelen, A., 98-MAO-6 Trümner, J., 295-FD-67 van Paassen, M., 61-MST-3, 270-MST-15 Waisman, H., 98-MAO-6 Sytsma, M., 129-ITAR-2 Theoﬁlis, V., 51-FD-9, 121-FC-5, 161-FD-30/APA-24 Tsai, H., 148-APA-23/FD-28 Vanstone, L., 55-FD-13 Wald, M., 86-ATIO.DE-1 Szymczak, W., 196-FD-44 Theuma, K., 46-ATIO.ATM-5 Tsai, W., 136-TP-6 Van Treuren, R., 256-ATIO.LTA-1 Waldman, R., 12-ASE-2 Tachie, M., 231-FD-48, 262-FD-58 Thobois, L., 42-ASE-3 Tsao, J., 43-ASE-4, 114-ASE-8, 150-ASE-10 Van Zante, J., 150-ASE-10, 183-ASE-12, 220-ASE-13 Waldmann, A., 128-GT-3 Taft, B., 96-ITAR-1 Thomas, J., 185-ATIO.ATM-16 Tsubokura, M., 147-APA-22 Vargas, M., 114-ASE-8 Wales, C., 263-FD-59/FC-19/APA-38 Tagai, R., 58-FT-1 Thomas, L., 177-AMT-7 Tu, S., 94-FD-20 Varghese, P., 107-AMT-5, 172-TP-7 Walker, D., 183-ASE-12 Taha, T., 29-MST-1 Thompson, D., 113-ASE-7/ATIO.ATM-9, Tu, X., 91-FD-17 Vargo, E., 186-ATIO.ATM-17 Walker, J., 113-ASE-7/ATIO.ATM-9 Taira, K., 121-FC-5, 193-FD-41/FC-12 193-FD-41/FC-12, 283-APA-41/FD-63, 285-ASE-17 Tufts, M., 93-FD-19 Vascik, P., 290-ATIO.TFPC-12 Walker, M., 7-APA-1 Takahashi, H., 266-FD-62 Thompson, K., 266-FD-62 Tumin, A., 24-FD-4, 261-FC-18/FD-57 Vasconez, J., 144-AFM-10 Wallace, A., 99-MST-5 Takahashi, T., 31-PDL-1, 86-ATIO.DE-1, 115-ATIO.ACD-4, Thompson, R., 31-PDL-1, 236-ITAR-5, 298-ITAR-7 Turk, J., 82-ASE-6/APA-15 Vasile, M., 301-MST-17 Walter, M., 299-MAO-18 151-ATIO.ACD-5, 254-ATIO.ATM-22, 281-APA-39 Thormann, R., 175-AFM-11 Turner, J., 259-FC-16 Vatsa, V., 190-FC-11 Walters, R., 268-MAO-16 Talamantes, G., 295-FD-67 Thornber, B., 164-FD-34 Turner, M., 54-FD-12 Veble Mikic, G., 119-ATIO.TFPC-6/ATIO.VSTOL-1, Wang, B., 30-MST-2, 161-FD-30/APA-24, Tallapragada, V., 182-ASE-11 Thornburg, H., 92-FD-18 Tyagi, A., 15-ATIO.ATM-2, 116-ATIO.ATM-10 155-ATIO.TFPC-7/ATIO.ACD-6/GEPC-1 222-ATIO.ACD-7/ATIO.TFPC-9, 265-FD-61 Talmor, M., 242-TP-9 Thorsen, A., 72-AFM-5 Tyan, M., 44-ATIO.ACD-2, 59-MAO-3 Védie, L., 285-ASE-17 Wang, C., 11-ASE-1, 54-FD-12, 131-MAO-8, 196-FD-44, Tam, C., 129-ITAR-2 Thorson, K., 136-TP-6 Tyson, W., 166-FD-36 Vedula, P., 273-TP-12 247-APA-34/FD-55 Tamaki, Y., 164-FD-34 Thurow, B., 75-AMT-4, 215-AMT-8 Uchida, M., 147-APA-22 Veillette, M., 154-ATIO.ATM-14 Wang, F., 62-MST-4 Tamba, T., 55-FD-13, 191-FD-39 Tian, A., 171-MST-9 Uddanti, N., 62-MST-4 Veldhuis, L., 78-APA-12 Wang, G., 112-APA-20, 175-AFM-11, Tamburro, R., 224-ATIO.ATM-19 Tian, P., 81-ASE-5 Ueno, M., 218-APA-30 Vengadesan, S., 284-APA-42/FD-64 246-APA-33/FD-54, 294-FD-66 Tan, Z., 106-AFM-8, 222-ATIO.ACD-7/ATIO.TFPC-9 Tian, Y., 205-PDL-5/FC-13 Ugolotti, M., 25-FD-7 Vengate, S., 144-AFM-10 Wang, H., 166-FD-36 Tancred, J., 112-APA-20 Tibert, G., 301-MST-17 Uhl, J., 32-TP-1 Venters, R., 148-APA-23/FD-28 Wang, J., 175-AFM-11, 235-GT-7, 247-APA-34/FD-55 Tandon, S., 164-FD-34 Tichenor, N., 261-FC-18/FD-57 Ukeiley, L., 21-FC-2/FD-1/APA-5, 41-APA-9, Verbeke, C., 39-APA-7 Wang, K., 100-MST-6 Tang, C., 181-APA-28, 267-ITAR-6 Tien, A., 287-ATIO.ATM-25 121-FC-5, 123-FD-23 Veres, J., 183-ASE-12 Wang, L., 93-FD-19, 122-FC-6/FD-22, 179-APA-26, Tang, F., 216-AMT-9 Tien, S., 117-ATIO.ATM-11 Ulbrich, N., 245-AMT-10/GT-8 Vermeersch, O., 93-FD-19 190-FC-11, 235-GT-7, 240-MST-13, 270-MST-15 Tang, H., 93-FD-19, 220-ASE-13 Tillson, C., 32-TP-1 Underwood, M., 223-ATIO.ATM-18, 253-ATIO.ATM-21, Vicker, D., 267-ITAR-6 Wang, N., 171-MST-9 Tang, Z., 230-FC-15 Tilmann, C., 263-FD-59/FC-19/APA-38 287-ATIO.ATM-25 Viguier, P., 107-AMT-5 Wang, Q., 62-MST-4, 178-APA-25/FD-38, 297-FD-69 Tanguy, G., 109-APA-17 Timme, S., 175-AFM-11 Unnikrishnan, S., 231-FD-48 Vijgen, P., 190-FC-11 Wang, S., 34-AFM-3, 136-TP-6, 259-FC-16, 294-FD-66 Taniguchi, S., 245-AMT-10/GT-8 Ting, E., 77-APA-11, 111-APA-19 Upadhyay, P., 165-FD-35 Viken, J., 188-ATIO.TFPC-8/ATIO.FT-1/GEPC-2 Wang, T., 296-FD-68 Tanner, C., 35-AFM-4 Tishkoff, J., 145-AMT-6 Urbaniak, D., 272-TP-11 Villasmil, L., 295-FD-67 Wang, W., 146-APA-21, 296-FD-68 Author/Session Chair Index Wang, X., 147-APA-22, 168-GT-4, 194-FD-42, Williams, B., 168-GT-4 Wu, D., 83-ATIO.ACD-3, 106-AFM-8, Yerly, E., 111-APA-19 Zhang, Y., 26-GT-1, 30-MST-2, 36-AMT-2, 93-FD-19, 204-MST-11 Williams, C., 28-MAO-2 222-ATIO.ACD-7/ATIO.TFPC-9 Yeung, D., 245-AMT-10/GT-8 116-ATIO.ATM-10, 123-FD-23, 133-MST-8, Wang, Y., 4-AFM-1, 6-AMT-1, 79-APA-13, 91-FD-17, Williams, D., 20-FC-1, 38-FC-20, 193-FD-41/FC-12, Wu, G., 4-AFM-1 Yi, S., 180-APA-27, 201-MAO-11, 217-APA-29 148-APA-23/FD-28, 170-MAO-10, 178-APA-25/FD-38, 128-GT-3, 171-MST-9, 223-ATIO.ATM-18, 260-FC-17/FD-56 Wu, M., 62-MST-4 Yi, Y., 284-APA-42/FD-64 202-MAO-12, 223-ATIO.ATM-18, 234-FD-53, 246-APA-33/FD-54, 249-APA-36, 268-MAO-16 Williams, M., 121-FC-5 Wu, X., 24-FD-4, 89-FC-4, 123-FD-23, 194-FD-42 Yildirim, A., 178-APA-25/FD-38 261-FC-18/FD-57, 270-MST-15, 293-FD-65 Wang, Z., 9-APA-3, 35-AFM-4, 79-APA-13, 95-GT-2, Williams, N., 91-FD-17 Wu, Y., 89-FC-4, 215-AMT-8, 230-FC-15 Yokokawa, Y., 146-APA-21 Zhang, Z., 57-FD-15, 128-GT-3 128-GT-3, 132-MST-7, 190-FC-11, 269-MAO-17, Williams, S., 263-FD-59/FC-19/APA-38 Wu, Z., 204-MST-11 Youn, E., 282-APA-40 Zhao, D., 11-ASE-1, 247-APA-34/FD-55, 284-APA-42/FD-64 Willis, D., 57-FD-15, 196-FD-44, 197-FD-45 Wukie, N., 54-FD-12 Younes, A., 29-MST-1 249-APA-36, 294-FD-66 Wanke, C., 117-ATIO.ATM-11, 186-ATIO.ATM-17 Willis, M., 176-AFM-12 Wyczolkowski, R., 272-TP-11 Young, C., 286-ATIO.ATM-24 Zhao, H., 79-APA-13 Ward, M., 118-ATIO.TFPC-5 Wilson, C., 144-AFM-10, 223-ATIO.ATM-18, Wygnanski, I., 20-FC-1 Young, D., 261-FC-18/FD-57 Zhao, J., 240-MST-13, 270-MST-15 Wartemann, V., 261-FC-18/FD-57 253-ATIO.ATM-21 Wylecial, T., 272-TP-11 Yu, J., 175-AFM-11 Zhao, L., 7-APA-1 Wasey, M., 251-ASE-15 Wilson, J., 259-FC-16 Wynn, A., 97-MAO-5 Yu, M., 161-FD-30/APA-24, 247-APA-34/FD-55, Zhao, N., 53-FD-11 Wasson, L., 113-ASE-7/ATIO.ATM-9 Wilson, M., 96-ITAR-1 Wynnyk, M., 255-ATIO.ATM-23 283-APA-41/FD-63, 293-FD-65 Zhao, Q., 76-APA-10, 216-AMT-9 Watkins, J., 196-FD-44 Wilson, S., 46-ATIO.ATM-5, 184-ATIO.ATM-15 Xiao, T., 167-FD-37 Yuan, B., 299-MAO-18 Zheng, X., 89-FC-4 Wayman, T., 245-AMT-10/GT-8 Wilson, T., 172-TP-7 Xie, S., 161-FD-30/APA-24 Yuan, X., 54-FD-12, 293-FD-65 Zheng, Z., 81-ASE-5, 251-ASE-15 Webb, N., 21-FC-2/FD-1/APA-5 Wilson III, S., 200-ITAR-4 Xing, J., 204-MST-11 Yue, C., 54-FD-12 Zhong, X., 56-FD-14 Webb, S., 50-FC-3 Winfree, T., 129-ITAR-2 Xing, Y., 175-AFM-11 Yue, L., 100-MST-6 Zhong, Y., 106-AFM-8 Wei, P., 84-ATIO.ATM-7 Wing, D., 223-ATIO.ATM-18, 253-ATIO.ATM-21 Xiong, J., 205-PDL-5/FC-13 Yumusak, M., 170-MAO-10 Zhong Yan, Y., 248-APA-35 Wei, T., 9-APA-3, 161-FD-30/APA-24 Winholtz, R., 96-ITAR-1 Xiong, Z., 203-MST-10 Zaal, P., 61-MST-3, 132-MST-7, 270-MST-15 Zhou, B., 60-MAO-4 Weiss, J., 95-GT-2, 216-AMT-9, 272-TP-11, 280-AMT-11 Winkler, J., 90-FD-16 Xu, J., 93-FD-19, 160-FC-9/PDL-4/FD-29 Zachos, P., 109-APA-17 Zhou, J., 219-APA-32 Welstead, J., 301-MST-17 Winter, M., 32-TP-1, 243-TP-10 Xu, L., 112-APA-20 Zakaria, M., 74-AMT-3, 108-APA-16/FD-21 Zhou, L., 176-AFM-12 Wen, G., 260-FC-17/FD-56 Winter, T., 59-MAO-3, 203-MST-10 Xu, W., 215-AMT-8 Zakerzadeh, M., 94-FD-20 Zhou, M., 300-MST-16 Wen, S., 216-AMT-9 Wiriadidjaja, S., 180-APA-27 Xu, X., 216-AMT-9 Zaman, K., 6-AMT-1 Zhou, P., 248-APA-35 Wen, Y., 132-MST-7, 269-MAO-17 Wissink, A., 10-APA-4 Xue, D., 268-MAO-16 Zammit Mangion, D., 46-ATIO.ATM-5 Zhou, Q., 202-MAO-12, 203-MST-10

145 Wendorff, A., 59-MAO-3, 202-MAO-12 Witte, B., 113-ASE-7/ATIO.ATM-9 Xue, M., 185-ATIO.ATM-16, 287-ATIO.ATM-25 Zamora, A., 9-APA-3 Zhou, T., 128-GT-3 Weng, H., 303-TP-14 Witte, I., 112-APA-20, 297-FD-69 Yadlin, Y., 50-FC-3, 190-FC-11 Zamora, L., 272-TP-11 Zhou, W., 75-AMT-4, 204-MST-11 Wenk, J., 303-TP-14 Wittich, D., 129-ITAR-2 Yagiz, B., 282-APA-40 Zander, F., 26-GT-1, 32-TP-1, 135-TP-5 Zhou, Y., 122-FC-6/FD-22 Wenkai, W., 222-ATIO.ACD-7/ATIO.TFPC-9 Wlezien, R., 50-FC-3, 123-FD-23 Yalin, A., 63-PDL-2 Zare-Behtash, H., 21-FC-2/FD-1/APA-5 Zhu, B., 222-ATIO.ACD-7/ATIO.TFPC-9 Westin, M., 171-MST-9 Wohl, C., 82-ASE-6/APA-15 Yamada, K., 168-GT-4, 191-FD-39, 284-APA-42/FD-64 Zaripov, K., 5-AFM-2 Zhu, C., 79-APA-13, 95-GT-2, 128-GT-3 Westphal, R., 216-AMT-9 Wolde, M., 252-ASE-16 Yamaguchi, T., 241-PDL-6 Zaychik, K., 61-MST-3 Zhu, D., 177-AMT-7 Wey, C., 91-FD-17 Woldegiorgis, F., 284-APA-42/FD-64 Yamamoto, K., 146-APA-21, 288-ATIO.ATM-26 Zebbiche, T., 249-APA-36 Zhu, G., 84-ATIO.ATM-7, 235-GT-7 Weyant, J., 136-TP-6 Wolf, W., 125-FD-25, 231-FD-48, 247-APA-34/FD-55 Yamouni, S., 231-FD-48 Zelinski, S., 287-ATIO.ATM-25 Zhu, S., 294-FD-66 Whalen, E., 50-FC-3, 190-FC-11, 232-FD-49 Wolfe, D., 177-AMT-7 Yan, H., 160-FC-9/PDL-4/FD-29 Zender, F., 86-ATIO.DE-1 Zhu, T., 242-TP-9 Wheaton, B., 56-FD-14, 163-FD-33 Wolff, M., 169-ITAR-3 Yan, S., 150-ASE-10 Zengin, U., 203-MST-10 Zhu, X., 98-MAO-6 Whitaker, S., 234-FD-53 Wong, C., 122-FC-6/FD-22 Yan, X., 122-FC-6/FD-22, 205-PDL-5/FC-13, Zeyghami, S., 105-AFM-7 Zhu, Y., 175-AFM-11 White, E., 293-FD-65 Wong, M., 166-FD-36 283-APA-41/FD-63 Zha, G., 23-FD-3, 89-FC-4, 218-APA-30 Zhu, Z., 16-ATIO.ATM-3, 293-FD-65 White, M., 236-ITAR-5 Wonnell, L., 266-FD-62 Yanagita, Y., 164-FD-34 Zhan, H., 283-APA-41/FD-63 Ziegenbein, P., 226-ATIO.TFPC-10/ATIO.VSTOL-2 White, R., 280-AMT-11 Wood, T., 167-FD-37 Yang, B., 225-ATIO.ATM-20 Zhang, C., 24-FD-4, 123-FD-23 Zientarski, L., 77-APA-11 White, T., 102-TP-3 Woodard, B., 149-ASE-9 Yang, L., 235-GT-7, 242-TP-9, 283-APA-41/FD-63 Zhang, D., 205-PDL-5/FC-13, 302-TP-13 Zilberter, I., 101-PDL-3 Whitehead, B., 202-MAO-12 Woods, S., 223-ATIO.ATM-18 Yang, M., 34-AFM-3, 222-ATIO.ACD-7/ATIO.TFPC-9 Zhang, F., 96-ITAR-1, 234-FD-53 Zimmerman, J., 241-PDL-6 Wick, G., 113-ASE-7/ATIO.ATM-9 Woolsey, C., 108-APA-16/FD-21, 116-ATIO.ATM-10 Yang, S., 89-FC-4, 106-AFM-8, 240-MST-13, 302-TP-13 Zhang, G., 54-FD-12, 296-FD-68 Zingg, D., 180-APA-27, 197-FD-45 Widjaja, R., 164-FD-34 Worden, T., 165-FD-35 Yang, W., 198-FT-3/GT-5, 268-MAO-16 Zhang, H., 89-FC-4, 246-APA-33/FD-54, 302-TP-13 Zoellner, A., 136-TP-6 Wieland, F., 15-ATIO.ATM-2, 133-MST-8 Work, A., 12-ASE-2, 82-ASE-6/APA-15 Yang, X., 23-FD-3, 54-FD-12 Zhang, J., 30-MST-2, 53-FD-11, 191-FD-39, 217-APA-29 Zöger, M., 143-AFM-9 Wignall, T., 195-FD-43 Wray, T., 80-APA-14, 90-FD-16, 112-APA-20, Yang, Y., 23-FD-3 Zhang, K., 12-ASE-2, 30-MST-2 Zohra, F., 77-APA-11 Wilbanks, M., 63-PDL-2 125-FD-25, 297-FD-69 Yao, D., 216-AMT-9 Zhang, Q., 123-FD-23 Zou, Z., 255-ATIO.ATM-23 Wilcoxen, M., 84-ATIO.ATM-7 Wright, H., 102-TP-3 Yao, W., 235-GT-7 Zhang, R., 100-MST-6 Zumwalt, C., 181-APA-28 Wilder, A., 223-ATIO.ATM-18, 253-ATIO.ATM-21 Wright, W., 12-ASE-2, 285-ASE-17 Yarusevych, S., 193-FD-41/FC-12, 230-FC-15 Zhang, W., 30-MST-2, 187-ATIO.GA-2 Zuo, P., 248-APA-35 Wilder, M., 245-AMT-10/GT-8 Wrist, A., 216-AMT-9 Yassir, S., 293-FD-65 Zhang, X., 21-FC-2/FD-1/APA-5, 41-APA-9, 57-FD-15, Zupanski, M., 91-FD-17 Wilhelms, C., 44-ATIO.ACD-2 Wroblewski, A., 177-AMT-7 Ye, Q., 293-FD-65 90-FD-16, 170-MAO-10, 171-MST-9, 182-ASE-11 Zyluk, A., 106-AFM-8 Will, F., 153-ATIO.ATM-13 Wrzesinski, P., 107-AMT-5 Ye, Z., 112-APA-20, 294-FD-66 Willcox, K., 238-MAO-14 Wu, B., 160-FC-9/PDL-4/FD-29, 205-PDL-5/FC-13 Yeo, S., 99-MST-5 Williams, A., 302-TP-13 Yerkes, K., 169-ITAR-3, 242-TP-9 IntroVenue Map

Washington Hilton

www.aiaa-aviation.org 51 #aiaaAviation 5–9 JUNE 2017 DENVER, COLORADO MARK YOUR CALENDAR! Featuring 24th AIAA Aerodynamic Decelerator Systems The AIAA Aviation and Aeronautics Forum and Technology Conference Exposition (AIAA AVIATION 2017) is the only 33rd AIAA Aerodynamic Measurement aviation event that covers the entire integrated Technology and Ground Testing Conference spectrum of aviation business and technology. 35th AIAA Applied Aerodynamics Conference Featuring 18 technical conferences in one AIAA Atmospheric Flight Mechanics Conference location, this a must-attend event in 2017! 9th AIAA Atmospheric and Space Environments Conference 17th AIAA Aviation Technology, Integration, and Operations Conference AIAA Flight Testing Conference 47th AIAA Fluid Dynamics Conference 18th AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference AIAA Modeling and Simulation Technologies The Call for Papers will be Conference 48th Plasmadynamics and Lasers Conference available in August 2016. AIAA Balloon Systems Conference 23rd AIAA Lighter-Than-Air Systems Technology Conference 23rd AIAA/CEAS Aeroacoustics Conference 8th AIAA Theoretical Fluid Mechanics Conference AIAA Complex Aerospace Systems Exchange 23rd AIAA Computational Fluid Dynamics Conference 47th Thermophysics Conference

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