final program - american institute of aeronautics and astronautics
TRANSCRIPT
FINAL PROGRAM www.aiaa.org/sandiego2013
#aiaaFluids
24–27 June 2013San Diego, CaliforniaSheraton San Diego
Hotel & Marina
43rd AIAA Fluid Dynamics Conference and Exhibit44th AIAA Plasmadynamics and Lasers Conference
44th AIAA Thermophysics Conference31st AIAA Applied Aerodynamics Conference
21st AIAA Computational Fluid Dynamics Conference5th AIAA Atmospheric and Space Environments Conference
AIAA Ground Testing Conference
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The conference chairs and planning committee thank you for participating in the co–located 43rd AIAA Fluid Dynamics Conference and Exhibit, 44th AIAA Plasmadynamics and Lasers
Conference, 44th AIAA Thermophysics Conference, 31st AIAA Applied Aerodynamics Conference, 21st AIAA Computational Fluid Dynamics Conference, 5th AIAA Atmospheric and Space Environments Conference, and AIAA Ground Testing Conference, being held 24–27 June 2013 at the Sheraton San Diego Hotel in San Diego, CA.
This event is held to provide a forum for technical exchange and interaction among scientists, engineers, and other professionals from the industrial, governmental, and academic technical communities who participate in scientific research and development in the aerospace engineering and fluid dynamics disciplines. The co–location of these related AIAA events provides attendees with a unique opportunity to expand their knowledge of technological advances in these interrelated disciplines and explore areas of common technical expertise.
This week you will:• Present recent advances before a
knowledgeable international audience• Educate customers and providers
on the latest research and product developments
• Learn about the latest technology and research in the field from industry experts
• Network to engage new contacts and refresh old ones
• Recognize significant achievements from within the community
Here’s what to expect at this year’s event:• Program
▷ Keynote and prestigious award lecture speakers on aeronautics in the virtual age, revolutionary aerospace technologies, numerical methods for computational heat transfer, all–speed flows, behavior of liquids and gases in motion, and vortex dominated flows
▷ More than 100 technical sessions covering all aspects of fluid dynamics, plasmadynamics and lasers, thermophysics, applied aerodynamics, computational fluid dynamics, atmospheric and space environments, and ground testing
▷ Access to more than 1,000 technical papers and presentations
• Networking Events ▷ Off–Site Event: Padres Baseball
Game ▷ AIAA Awards Luncheon ▷ Lunch Reception in the Exhibit Hall ▷ Technical Tours ▷ Networking Coffee Breaks
WELCOME!
43rd AIAA Fluid Dynamics Conference and ExhibitFluid Dynamics Technical ChairLaTunia Pack MeltonNASA Langley Research Center
44th AIAA Plasmadynamics and Lasers Conference Plasmadynamics and Lasers Technical ChairNick BisekWright–Patterson Air Force Base
44th AIAA Thermophysics ConferenceThermophysics Technical ChairPatrick YeeThe Aerospace Corporation
31st AIAA Applied Aerodynamics ConferenceApplied Aerodynamics Technical ChairsKenrick WaitheGulfstream
Chunhua ShengSimCenter
Li WangSimCenter
21st AIAA Computational Fluid Dynamics ConferenceComputational Fluid Dynamics Technical ChairH.T. HuynhNASA Glenn Research Center
5th AIAA Atmospheric and Space Environments ConferenceAtmospheric and Space Environments Technical ChairsNelson W. GreenJet Propulsion Laboratory
Marcia PolitovichNational Center for Atmospheric Research
AIAA Ground Testing ConferenceGround Testing Technical ChairVictor CanacciJacobs Technology, Inc.NASA Glenn Research Center
CONFERENCE ORGANIZERSConference General Chair
Sergey MacheretLockheed Martin Aeronautics
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Monday, 24 June 2013
0800–0900 hrs Harbor Island Ballroom I/II
Opening Plenary Session
Dennis M. Bushnell, Chief Scientist, NASA Langley Research Center
“Aeronautics in the Virtual Age”
1730–1830 hrs Harbor Island Ballroom I/II
Fluid Dynamics Award Lecture
Lecturer: Donald O. Rockwell
Tuesday, 25 June 2013
1200–1400 hrs Harbor Island Ballroom I/II
Awards Luncheon and Keynote Speaker
Charles Chase, Lockheed Martin Skunk Works
“Revolutionary Aerospace Technologies”
Wednesday, 26 June 2013
0800–0900 hrs Harbor Island Ballroom I/II
Thermophysics Award Lecture
Lecturer: Gerald E. “Gerry” Schneider
Thursday, 27 June 2013
0800–0900 hrs Harbor Island Ballroom I/II
Aerodynamics Award Lecture
Lecturer: Neal T. Frink
KEYNOTE and AWARD LECTURE SPEAKERS
New! Continental BreakfastA great way to start the day and interact with other attendees, a continental breakfast open to all attendees will be offered Monday–Thursday, 0700–0800 hrs in the Harbor Island and Nautilus Foyers. No tickets required.
Monday, 24 June 2013
1830 hrs
“Take Me Out to the Ballgame” EventSan Diego Padres vs. Philadelphia Phillies
Join us for a night at Petco Park, home of the San Diego Padres, enjoying America’s favorite pastime. Bus transportation will be provided to Petco Park for the game between the Padres and the Phillies, which begins at 1910 hrs. Tickets include all you can eat burgers, hot dogs, ballpark snacks, beer, water, and soda. AIAA will have the use of several private areas, with great views of the park. Each attendee will also have a stadium seat from which to view the game.
Cost of the event is $85 and includes transportation. Transportation will start boarding at 1830 hrs, and the first pitch is at 1910 hrs (in order to attend, you must use the bus transportation provided).Admission is included in the registration fee where indicated and tickets will be handed out as you board the buses. Additional tickets may be purchased at the AIAA information and registration desk based on availability.
Tuesday, 25 June 2013
0800–1100 hrs Harbor Island Ballroom I/II
Protecting Intellectual Property Workshop
Investing in innovation is one of the keys to maintaining a competitive edge and expanding business opportunities. Protecting this investment through intellectual property rights such as patents,
copyrights, and trademarks is essential in today’s global economy, particularly when contracting with government entities. The United States recently implemented extensive changes to the patent system with far–reaching effects for companies that wish to obtain and enforce their intellectual property rights. This workshop will explore various methods of protecting intellectual property, contracting with government agencies, and how the new patent laws will impact your vital business IP assets. There is no additional charge to attend this workshop; all attendees are welcome.
1200–1400 hrs Harbor Island Ballroom I/II
Awards Luncheon and Keynote SpeakerCharles Chase, Lockheed Martin Skunk Works“Revolutionary Aerospace Technologies”
Admission is included in the registration fee where indicated. Additional tickets may be purchased for $60 at the AIAA on–site registration desk. Please be sure to arrive promptly. Doors will be closed once the awards ceremony begins. The following awards will be presented at the luncheon:
Aerodynamics AwardNeal T. Frink, NASA Langley Research Center
For meritorious achievement in the field of applied aerodynamics through notable contributions in the development, application, and evaluation of aerodynamic concepts and methods.
Fluid Dynamics AwardDonald O. Rockwell, Lehigh University
For contributions to a fundamental understanding of vortex dominated flows and their characterization with quantitative imaging.
NETWORKING ACTIVITIES and SPECIAL EVENTS
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NETWORKING ACTIVITIES and SPECIAL EVENTSGround Testing Award
Jack (Jagdish) S. Sokhey, Rolls–Royce North American Technologies, Inc. (LibertyWorks)
For exceptional service, leadership, and technical
contribution in the advancement of jet engine technology, performed through testing of small–scale and full–scale research models and jet engines.
Plasmadynamics and Lasers AwardJoseph Verdeyen, University of Illinois at Urbana–Champaign
For major contributions in the fields of gas and semiconductor lasers, plasma discharge technologies,
and the mentoring of young engineers and scientists. (Note: Award has already been presented by the University of Illinois–Urbana Student Branch.)
Thermophysics AwardGerald E. “Gerry” Schneider, University of Waterloo
For outstanding, pioneering, and sustained contributions in developing simple and advanced numerical methods
for computational heat transfer, algebraic equation solvers, phase change energy transport, all–speed flows, and conduction heat transfer.
Certificate of Merit – Best Papers:Aerodynamic Measurement TechnologyAIAA Paper 2013–0033, “NO PLIF Visualization of the Orion Capsule in LENS–I,” by Chris Combs and Noel Clemens, The University of Texas at Austin; Paul M. Danehy and Brett Bathel, NASA Langley Research Center; Ronald Parker, Tim Wadhams, Michael Holden, CUBRC; and Benjamin Kirk, NASA Johnson Space Center.
Applied AerodynamicsAIAA Paper 2012–2668, “A Transonic Laminar–Flow Wing Glove Flight Experiment: Computational Evaluation and Linear Stability,” by Matthew W Roberts, Helen Reed, and William Saric, Texas A&M University.
Fluid Dynamics AIAA Paper 2012–0086, “Investigation of Aspect Ratio and Dynamic Effects due to Rotation for a Revolving Wing Using High–Fidelity Simulation” by Daniel Garmann and Miguel Visbal, Air Force Research Laboratory; and Paul Orkwis, University of Cincinnati.
Ground TestingAIAA Paper 2012–3318, “High Reynolds Number Active Blowing Semi–Span Force Measurement System Development,” by Keith Lynn, Ray Rhew, Michael Acheson, Gregory Jones, William Milholen, and Scott Goodliff, NASA Langley Research Center.
Plasmadynamics and LasersAIAA Paper 2013–0922, “Flame Propagation Enhancement of Ethylene by Addition of Ozone,” by Matthew Pinchak and Ephraim Gutmark, University of Cincinnati; Timothy Ombrello and Campbell Carter, Air Force Research Laboratory; and Viswanath Katta, Innovative Scientific Solutions, Inc.
ThermophysicsAIAA Paper 2013–0304, “An Equilibrium Ablation Boundary Condition for the Data–Parallel Line–Relaxation Code,” by Matthew MacLean, CUBRC.
Certificate of Merit – Best Student Papers: Plasmadynamics and LasersAIAA Paper 2012–0822, “Fundamental Processes of DBD Plasma Actuators Operating at High Altitude,” by Alexander Duchmann, Bernhard Simon, Philip Magin, Cameron Tropea, and Sven Grundmann, Technical University of Darmstadt.
David Weaver ThermophysicsAIAA Paper 2012–3311, ”Large Eddy Simulations of the Hydrodynamic and Thermal Fields from a Cylindrical Film Cooling Hole,” by Lucky Tran, Perry Johnson, and Jayanta Kapat, University of Central Florida.
Wednesday, 26 June 2013
1200–1300 hrs Harbor III
Exhibitor Lunch Reception Come and have lunch with the exhibitors and network with your peers. Admission is included in the registration fee where indicated. Additional tickets may be purchased for $60 at the AIAA on–site registration and information desk.
San Diego Low Speed Wind Tunnel ToursThe facility is located one mile from the Sheraton San Diego Hotel. Two tours will be offered Wednesday afternoon (25 –person maximum per tour). The first bus will depart from the Grand Foyer parking lot at 1330 hrs, for a tour from 1345 to 1430 hrs. The second bus will depart from the Grand Foyer parking lot at 1500 hrs, for a tour from 1515 to 1600 hrs.
For over 60 years, the San Diego Low Speed Wind Tunnel (LSWT) has served the testing needs of the aerospace community. The facility is fully staffed and equipped to provide all testing and data processing services. The tunnel circuit provides low turbulence, clean airflow, and uniform velocity distribution in the test section, with controllable flow as low as 10 mph. A new variable frequency fan drive system is one of several recent tunnel upgrades. Tickets for the tour may be purchased upon registration. Visit www.lswt.com for more information.
Triumph’s Aerospace Force Measurement Systems Group Tour1700–1930 hrs
View a state–of–the–art facility for the production of Wind Tunnel Balances. Tour the Design area, Instrumentation, Calibration and System Development Labs. View balance projects currently in work, the Automatic Balance Calibration System (ABCS), and the Large Load Rig (LLR) with a 30,000–pound Semi–Span balance installed, as well as other manual dead weight load stands with a variety of balances in the calibration process.
A Model Positioning System (MPS) will be demonstrated. Other systems may be on site for demonstration depending on delivery schedules. Transportation and light snacks will be provided (buses will depart from the Grand Foyer parking lot). Space is limited to the first 50 people to sign up; the cost is $20.
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Networking Coffee BreaksCoffee breaks are included in the program to allow even more time for making new contacts, continuing discussions from technical sessions, or checking emails and voicemails to keep in touch with the office while you are at the conference. Networking coffee breaks will be located in the Harbor Island Foyer and Exhibit Hall (Harbor Island III), where indicated, at the following times:
Monday, 24 June1000–1100 hrs and
1500–1600 hrs
Tuesday, 25 June 1000–1100 hrs and 1500–1600 hrs (Exhibit Hall)
Wednesday, 26 June 1000–1100 hrs (Exhibit Hall) and 1500–1600 hrs (Harbor Island Foyer)
Thursday, 27 June 1000–1100 hrs
Cyber Café (Internet Access)There will be computers with complimentary Internet access in the Nautilus Foyer for conference attendees during the following hours:
Monday, 24 June 0700–1700 hrs
Tuesday, 25 June 0700–1730 hrs
Wednesday, 26 June 0700–1730 hrs
Thursday, 27 June 0700–1200 hrs
Complimentary Internet access is provided in the hotel rooms at the Sheraton Hotel San Diego for conference attendees booking within the AIAA room block. AIAA cannot guarantee complimentary Internet access for those attendees who book rooms outside the AIAA room block. The hotel should remove the wireless charges upon checkout.
Registration and Information CenterLocated in the Harbor Island Foyer on the lobby level of the Sheraton San Diego, the Registration and Information Center is open during the following hours:
Saturday, 22 June(Course and Workshop Registration only
0700–0815 hrs
Sunday, 23 June 1500–1900 hrs
Monday, 24 June 0700–1700 hrs
Tuesday, 25 June 0700–1730 hrs
Wednesday, 26 June 0700–1730 hrs
Thursday, 27 June 0700–1300 hrs
AIAA Livestream ChannelVisit www.livestream.com/aiaa to view two sessions scheduled for Monday, 24 June: the “Celebrating 60 Years of AFOSR” session (1300–1700 hrs PDT) and the Fluid Dynamics Award Lecture (1730–1830 hrs PDT). Share the link with colleagues who cannot make it to the conference to watch live or view afterwards.
NETWORKING ACTIVITIES and SPECIAL EVENTS
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EVENT AT A GLANCESaturday–Sunday 22–23 June 2013
Monday 24 June 2013
Tuesday 25 June 2013
Wednesday 26 June 2013
Thursday 27 June 2013
0700 hrsNetworking Breakfast
(until 0800 hrs)Networking Breakfast
(until 0800 hrs)Networking Breakfast
(until 0800 hrs)Networking Breakfast
(until 0800 hrs)
0730 hrs Speakers’ Briefing Speakers’ Briefing Speakers’ Briefing Speakers’ Briefing
0800 hrs
Continuing Education Course and
2nd AIAA CFD High Lift Prediction Workshop
Opening Plenary Session
Technical Sessions
Protecting Intellectual Property Workshop
Thermophysics Award Lecture
Aerodynamics Award Lecture0830 hrs
0900 hrs
Technical Sessions Technical Sessions
Technical Sessions
0930 hrs
1000 hrsExhibit Hall Open
Exhibit Hall Open
1030 hrs
1100 hrs
1130 hrs
1200 hrsLunch Break
(until 1300 hrs) Awards Luncheon and
Keynote Speaker
Exhibitor Lunch Reception1230 hrs Speakers’ Briefing
1300 hrs
Technical Sessions
Speakers’ Briefing
1330 hrs
Technical Sessions
San Diego Low Speed
Wind Tunnel Tours
1400 hrs Speakers’ Briefing
1430 hrs
Technical Sessions
1500 hrs
1530 hrs
1600 hrs
1630 hrs
1700 hrs Triumph’s Aerospace
Force Measurement
Systems Group Tour
1730 hrs Fluid Dynamics Award Lecture1800 hrs
1830 hrs
Offsite Event: Padres Baseball Game
Transportation leaves from hotel at 1830 hrs
1900 hrs
1930 hrs
2000 hrs
2030 hrs
2100 hrs
2130 hrs
2200 hrs
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Ciespace Corporation Booth 62905 Stender Way #38Santa Clara, CA [email protected]
Ciespace Corporation is an early stage software technology company delivering an innovative Software–as–a–Service based computer–aided engineering platform for mechanical engineering design and analysis. Ciespace is the first commercially–available end–to–end CAE solution built entirely on an open, web services platform – to deliver an entirely new paradigm of engineering design and analysis solutions.
Don’t miss this exciting exhibition, located in Harbor Island III, featuring displays on internal and external aerodynamics, airfoil and vehicle design, hypersonics, instrumentation, and other industry–related fields. Companies from all over the world will have products available for hands–on demonstrations.
Exhibit HoursTuesday, 25 June 1000–1600 hrsWednesday, 26 June 1000–1400 hrs Lunch Reception 1200–1300 hrs
EXHIBIT GUIDE
Ciespace
BETA CAE Systems Booth 329800 Middlebelt RoadSuite #100Farmington Hills, MI 48334www.ansa–usa.comDeepak@ansa–usa.com
BETA CAE Systems is an engineering services company that distributes and supports the industry leading ANSA & META software. ANSA is CAE pre–processing tool for FE & CFD Analysis, for full–model build, from CAD to solver input file, in one integrated environment. META is a post–processor for analyzing results from ANSYS, NASTRAN, ABAQUS, LS–DYNA, PAMCRASH, RADIOSS, MADYMO, FLUENT, STAR CCM, CFD++ and other solvers.
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Rev. 5/29/13
MARINA ROOMS MARINA ROOMS
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Fluid Dynamics 2013June 24-27, 2013
Sheraton San Diego Hotel & MarinaSan Diego, California
arata expositions, inc.15928 tournament drivegaithersburg, md 20877(phone) 301-921- 0800
(fax) 301-990- 1717www.arataexpo.com
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ADVANCE REGISTRATION ON-SITE REGISTRATION
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SoftwareCradle
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Rescale Booth 4589 Howard Street, 2nd FloorSan Francisco, CA [email protected]
Rescale enables aerospace engineers to set up and complete their engineering analyses and simulations orders of magnitude faster than they do today. This saves companies a lot of time and money, giving them the ability to make the next big breakthrough much faster and cheaper.
Software Cradle Booth 270 Birch Alley, Suite 240Beavercreek, OH 45440www.cradle–cfd.comando@cradle–cfd.com
Software Cradle is a leading provider of Computational Fluid Dynamics (CFD) software including SC/Tetra (general purpose unstructured mesh), scSTREAM (general purpose Cartesian mesh), and HEAT Designer (Cartesian mesh for electronics). Since inception in 1984, Cradle has established itself as a major innovator for advancing the role of simulation in engineering design.
Tecplot, Inc Booth 13535 Factoria Blvd SE, Suite 550Bellevue, WA [email protected]
Tecplot, Inc. delivers visualization software that empowers engineers and scientists to analyze, discover, and communicate the results of complex data. Our goal is to provide high–quality engineering and scientific visualization tools and services to help you be more creative, efficient, and productive.
Triumph Aerospace Systems Booth 7 Newport News 7340 Trade St., Suite DSan Diego, CA 92121www.triumph.com/companies/triumph–aerospace–systems–newport–[email protected]
Triumph Aerospace Systems–Newport News is an industry leader in the development, engineering, and manufacture of complex aerospace hardware, and prototype systems for force measurement devices, ground test, and flight applications. We have been employed in the development of nearly every domestic fixed–wing aircraft, missile, and helicopter system.
Computation Engineering International Booth 8 2166 N. Salem StreetApex, NC [email protected]
CEI are the developers of a visualization software package called EnSight, widely used in the engineering field to visualize, analyze, and communicate simulation results. EnSight’s ability to extract out quantitative and qualitative information from any CAE simulation in a single, easy to use package allows the users to fully understand, visualize, and communicate the simulation results.
Desktop Aeronautics Booth 111900 Embarcadero Way Palo Alto, CA [email protected] in 1994, Desktop Aeronautics has grown into a well–established consulting firm dedicated to advancing the state of the art in aerodynamics and aircraft design.We have significant experience and recognized expertise in aerodynamics, aircraft design, computational fluid dynamics, and multidisciplinary optimization. We have worked with leading aerospace organizations on some of the most difficult challenges in aerospace industry.
EXA Corporation Booth 955 Network DriveBurlington, MA [email protected]
Exa Corporation offers a full suite of CFD/CAE simulation design optimization software applications with aerodynamic, thermal and aeroacoustic simulation capabilities in addition to engineering consulting services. Exa’s products and services enable engineers to integrate simulation early in the design process, therefore creating competitive designs, shortening product design cycles and speeding time–to–market.
Photron Booth 109520 Padgett Street, Suite 110San Diego, CA [email protected]
Photron’s wide range of light sensitive high–speed cameras includes short inter–frame (222ns) times ideally suited for Particle Image Velocimetry (PIV), miniature cameras for microscopy, a full resolution at one million fps camera, to 4M pixels production HD to 2,000 fps. Photron has the slow motion camera for your fluidics application.
Pointwise, Inc. Booth 5213 S. Jennings AvenueFort Worth, TX [email protected]
Pointwise, Inc. is solving the top problems facing engineering analysts today: mesh generation for computational fluid dynamics. Manufacturing firms and research organizations use Pointwise’s mesh generation software to seamlessly bridge the gap between CAD and computational fluid dynamics analysis.
EXHIBIT GUIDE
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New! Speakers’ Briefing FormatAuthors who are presenting papers, session chairs, and co–chairs will meet for a short briefing in their session room. Morning sessions will meet from 0730 to 0800 hrs, and Monday–Wednesday afternoon sessions will meet in their session rooms 30 minutes prior to their start time.
Session Chair ReportsAll session chairs are asked to complete a session chair report to evaluate their session for future planning. AIAA has partnered with Canvas Solutions to provide an electronic Session Chair Report form. You can download the FREE mobile app in your App Store, AppWorld, or Marketplace by searching for “Canvas Solutions, Inc.” The mobile app is free, so please make sure to download it. Detailed instructions will be provided in the session rooms. If you do not have a tablet or a smartphone, simply enter your session chair report information at the session chair reporting computer station located on site near the AIAA registration area. Report data is collected and used for future planning purposes, including session topics and room allocations. Please submit your session chair report electronically by 28 June 2013.
“No Paper, No Podium” and “No Podium, No Paper” PolicyIf a written paper is not submitted by the final manuscript deadline, authors will not be permitted to present the paper at the conference. Also, if the paper is not presented at the conference, the written paper will be withdrawn from the conference proceedings. These policies are intended to eliminate no–shows and to improve the quality of the conference for attendees.
Speakers’ PracticeA speakers’ practice room will be available in the Executive Center Boardroom on the first floor for speakers wishing to practice their presentations. A sign–up sheet will be posted on the door for half–hour increments.
Timing of PresentationsEach paper will be allotted 30 minutes (including introduction and question–and–answer period) except where noted.
AudiovisualEach session room will be preset with the following: one laptop computer, one LCD projector, one screen, and one microphone and sound system (if necessitated by room size). Please note that AIAA does not provide security in the session rooms and recommends that items of value, including computers, not be left unattended. For additional audiovisual requirements please come to the registration and information desk.
Journal PublicationAuthors of appropriate papers are encouraged to submit them for possible publication in one of the Institute’s archival journals: AIAA Journal; Journal of Aircraft; Journal of Guidance, Control, and Dynamics; Journal of Propulsion and Power; Journal of Spacecraft and Rockets; Journal of Thermophysics and Heat Transfer; or Journal of Aerospace Information Systems (formerly Journal of Aerospace Computing, Information, and Communication). You may now submit your paper online at http://mc.manuscriptcentral.com/aiaa.
SPEAKER and SESSION CHAIR INFORMATION
For those who registered in advance, Conference Proceedings will be available 24 June 2013. Follow the steps to access them:
1. To view proceedings go to www.aiaa.org > ARC > Meeting Papers.
a. Select the appropriate conference from the list.
b. Search for individual papers with the Quick Search toolbar in the upper–right corner of the page:
i. By paper number: Click the “Paper Number” link, select the conference year and enter the paper number.
ii. Use the Search textbox to find papers by author, title, or keyword. The Advanced Search link provides additional search information and options.
2. All manuscript files submitted at least four days prior to the conference are currently in the proceedings. Files submitted after that date, both original and revised manuscripts, will not be available until the final proceedings update, which may take up to 15 business days after the last day of the conference.
3. During this event, AIAA may provide limited Wi–Fi service for attendee use. In an effort to keep this service available and optimized for all attendees, please limit downloading large files (no files larger than 2MB), creating multiple sessions across multiple devices, or downloading multiple files in one session. Should you encounter an error message that indicates that that an AIAA server is blocking your current IP address, please inform the AIAA registration desk.
4. Direct any questions concerning access to proceedings and/or ARC to [email protected].
CONFERENCE PROCEEDINGS
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HotelSheraton San Diego Hotel & Marina1380 Harbor Island DriveSan Diego, California 92101
Complimentary Shuttle TransportationThe Sheraton San Diego Hotel provides complimentary shuttle service to and from San Diego International Airport. The courtesy shuttle arrives approximately every 20 minutes, 0445–2400 hrs, seven days a week. For specific instructions on how to access the shuttle at your terminal, please consult the hotel website or the front desk.
Conference Certificate of Attendance Available Certificates of Attendance are available for attendees who request documentation at the conference itself. AIAA offers this service to better serve the needs of the professional community. Claims of hours or applicability toward professional education requirements are the responsibility of the participant. Please request your copy at the on–site registration desk starting on Tuesday afternoon.
Employment OpportunitiesAIAA assists members who are searching for employment by providing a bulletin board at technical meetings. This bulletin board is solely for “open position” and “available for employment” postings. Employers are encouraged to have personnel who are attending an AIAA technical conference bring “open position” job postings. Individual AIAA members may post “available for employment” notices. AIAA reserves the right to remove inappropriate notices, and cannot assume responsibility for notices forwarded to AIAA Headquarters. AIAA members can post and browse resumes and job listings, and access other online employment resources, by visiting the AIAA Career Center at careercenter.aiaa.org.
Nondiscriminatory PracticesThe AIAA accepts registrations irrespective of race, creed, sex, color, physical handicap, sexual orientation, and national or ethnic origin.
GENERAL INFORMATIONRestrictionsPhotography or video or audio recording of sessions, presentation slides, or technical exhibits, as well as the unauthorized sale of AIAA–copyrighted material, is prohibited.
International Traffic in Arms Regulations (ITAR)AIAA speakers and attendees are reminded that some topics discussed in the conference could be controlled by the International Traffic in Arms Regulations (ITAR). U.S. nationals (U.S. citizens and permanent residents) are responsible for ensuring that technical data they present in open sessions to non–U.S. nationals in attendance or in conference proceedings are not export restricted by the ITAR. U.S. nationals are likewise responsible for ensuring that they do not discuss ITAR export–restricted information with non–U.S. nationals in attendance.
Photo ID Needed at RegistrationAll registrants must provide a valid photo ID (driver’s license or passport) when they check in. For student registration, valid student ID is also required.
Young Professional Guide for Gaining Management SupportYoung professionals have the unique opportunity to meet and learn from some of the most important people in the business by attending conferences and participating in AIAA activities. A detailed online guide, published by the AIAA Young Professional Committee, is available to help you gain support and financial backing from your company. The guide explains the benefits of participation, offers recommendations, provides an example letter for seeking management support and funding, and shows you how to get the most out of your participation.The online guide can be found on the AIAA website, www.aiaa.org/YPGuide.
Your AIAA Membership Card Is Now Available Online –And Also Includes a QR Code for Speedy Conference Check–In!
AIAA now lets you print your membership identification card online! It’s quick, easy, and convenient. Even better, your membership card now includes a QR code to improve your conference check–in experience.
Printing your new membership card is as easy as 1–2–3:
1. Log in to www.aiaa.org using the email address associated with your member account and your self–created password.
2. Select “My AIAA” at the top right of the screen, or select the “Membership and Communities” tab and scroll down to “My AIAA.”
3. Under the “My Account Information” section, select “Member Card” and “Print.”
Printing your conference badge and tickets:
1. Upon arrival at the conference, visit the registration area.
2. Scan your QR code through an ExpressPass kiosk at Advance Registration.
3. Your conference badge and event tickets will print out in a flash!
12–14 AUGUST 2013 LOS ANGELES, CALIFORNIA
CHARTING THE FUTURE
OF FLIGHT
Premier Sponsor
REGISTER TODAY!www.aiaa.org/aviation2013#aiaaAviation
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INCLUDING
AIAA Aviation Technology, Integration, and Operations (ATIO) Conference International Powered Lift Conference (IPLC)
AIAA Complex Aerospace Systems Exchange (CASE)
AIAA AVIATION 2013 is a premier, forward-looking forum designed to showcase recent innovations and achievements in aviation, highlight new initiatives and plans, and address key issues that need to be resolved in order to defi ne clear roadmaps for future progress.
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COMMITTEE MEETINGSTime Committee/Event Room
Sunday, 23 June 2013
1400–1500 hrs GTTC Steering Subcommittee Nautilus 1
1400–1500 hrs APATC New Member Orientation Executive Conference Room 3A
1430–1500 hrs APATC Liaisons Subcommittee Executive Conference Room 2A
1500–1600 hrs GTTC Introduction/Overview Nautilus 1
1500–1600 hrs APATC Publicity & Publications Subcommittee Executive Conference Room 4
1500–1600 hrs APATC Planning Subcommittee Executive Conference Room 3B
1500–1600 hrs APATC Membership & Nominations Subcommittee Executive Conference Room 2B
1500–1600 hrs APATC Honors & Awards Subcommittee Executive Conference Room 3A
1500–1600 hrs APATC Education Subcommittee Executive Conference Room 2A
1600–1700 hrs APATC Technical Activities Meeting Executive Conference Room 2A
1600–1700 hrs GTTC Aero and Propulsion Subcommittee Nautilus 1
1630–1800 hrs FDTC Transition DG Marina 3
1630–1730 hrs FDTC LES WG Executive Conference Room 4
1630–1800 hrs FDTC New Frontiers Subcommittee Executive Conference Room 3B
1700–1800 hrs APATC Steering Committee Executive Conference Room 3A
1700–1800 hrs GTTC Awards Subcommittee Nautilus 1
1730–1830 hrs FDTC Recommended Practices for Reporting Flow Control Results WG Executive Conference Room 2A
1730–1830 hrs FDTC New Member Orientation Executive Conference Room 2B
1800–1900 hrs GTTC Publications Subcommittee Nautilus 1
1800–2100 hrs Applied Aerodynamics TC Harbor Island I
1830–2000 hrs FDTC CFD Methods Subcommittee Nautilus 2
12
Time Committee/Event Room
Sunday, 23 June 2013 (continued)
1830–2000 hrs FDTC Fundamentals of Flow Phenomena Subcommittee Nautilus 3
1830–2000 hrs FDTC Flow Control Subcommittee Nautilus 4
2000–2200 hrs FDTC Steering Subcommittee Executive Conference Room 2A
Monday, 24 June 2013
0800–1600 hrs GTTC Internal Balance WG 411
1700–1800 hrs PDLTC Steering Committee 415
1700–1800 hrs GTTC Committee on Standards 411
1830–2000 hrs FDTC Low Re DG 411
1830–2000 hrs FDTC Fluids Prize Nominating Committee 415
1900–2030 hrs FDTC Turbulence Modeling Benchmarks WG 518
Tuesday, 25 June 2013
0800–1500 hrs GTTC WT Model Attitude and Deformation Measurement WG 411
0800–1500 hrs GTTC DFRN WG 415
1500–1600 hrs TPTC Best Paper Subcommittee 411
1500–1600 hrs TPTC Awards Subcommittee 415
1600–1700 hrs TPTC Publications Subcommittee 415
1600–1700 hrs CFD General Notation System Committee on Standards 411
1700–1800 hrs TPTC Conferences Subcommittee 415
1700–1900 hrs Computational Fluids Dynamics Committee on Standards 411
1800–1900 hrs TPTC Education Subcommittee Nautilus 5
1800–1900 hrs TPTC Nominations Subcommittee Executive Conference Room 4
COMMITTEE MEETINGS
13
Time Committee/Event Room
Tuesday, 25 June 2013 (continued)
1800–2000 hrs APATC Rotorcraft Simulations & Performance Predictions DG Executive Conference Room 2B
1800–2000 hrs GTTC DOE Focus Group Executive Conference Room 3A
1800–2200 hrs Atmospheric & Space Environments TC Nautilus 1
1800–1900 hrs TPTC Publicity Subcommittee Executive Conference Room 3B
1800–2000 hrs GTTC Conference Subcommittee Executive Conference Room 2A
1800–1900 hrs APATC Low Boom (and Drag Prediction) DG Executive Conference Room 1
1830–2000 hrs FDTC Solver Technology for Turbulent Flows DG 415
1830–2000 hrs FDTC Nonequilibrium Flows WG 511
1830–2000 hrs FDTC Free Shear Layer Mixing Layer Control WG 515
1900–2200 hrs Aerodynamic Measurement Technology TC Nautilus 2
1900–2200 hrs Plasmadynamics and Lasers TC Nautilus 3
1900–2200 hrs Thermophysics TC Nautilus 4
1900–2000 hrs APATC Validation of Numerical Models DG 411
1900–2000 hrs APATC Missile and Projectile Aeroprediction DG 518
1900–2000 hrs APATC Low Reynolds Number Aerodynamic Applications & Testing DG 514
1900–2000 hrs APATC Aerodynamic Design Optimization DG Executive Conference Room 1
Wednesday, 26 June 2013
0900–1700 hrs GTTC DFRN WG 411
1200–1600 hrs GTTC Wind Tunnel Flow Quality WG 415
1700–1800 hrs GTTC Education and Student Activities Subcommittee 411
1800–1900 hrs FDTC Student Outreach Subcommittee 415
1900–2200 hrs Fluid Dynamics TC Nautilus 1
COMMITTEE MEETINGS
14
Time Committee/Event Room
Wednesday, 26 June 2013 (continued)
1800–1900 hrs FDTC Microfluids DG 511
Thursday, 27 June 2013
1300–1600 hrs Ground Testing TC Harbor Island II
COMMITTEE MEETINGS
THANK YOU! “For Lasting Contributions to the Enduring Success and
Worldwide Influence of the Drag Prediction Workshop Series”
Organizing Committee, AIAA CFD Drag Prediction Workshops (DPW):
Shreekant Agrawal, The Boeing CompanyChairman DPW–1
Olaf Brodersen, DLR Institute of Aerodynamics and Flow TechnologyMember DPW–2, DPW–3, DPW–4, DPW–5
Simone Crippa, DLR Institute of Aerodynamics and Flow TechnologyMember DPW–5
Bernhard Eisfeld, DLR Institute of Aerodynamics and Flow TechnologyMember DPW–3, DPW–4
Jean–Luc Godard, ONERAMember DPW–2
Mike Hemsch, NASA Langley Research CenterMember DPW–1
Steve Klausmeyer, Cessna Aircraft CompanyMember DPW–2
Kelly Laflin, Cessna Aircraft CompanyMember DPW–2, DPW–3, DPW–5
David Levy, Cessna Aircraft CompanyMember DPW–1, DPW–4, DPW–5
Mori Mani, The Boeing CompanyMember DPW–3, DPW–4, DPW–5
Rick Matus, Pointwise, Inc.Member DPW–1
Dimitri Mavriplis, University of WyomingMember DPW–3, DPW–4, DPW–5
Joe Morrison, NASA Langley Research CenterMember DPW–2, DPW–3, DPW–4, DPW–5
Mitsuhiro Murayama, JAXAMember DPW–4, DPW–5
Bastiaan Oskam, National Aerospace LaboratoryMember DPW–1
Shahyar Pirzadeh, NASA Langley Research CenterMember DPW–1
Juergen Quest, European Transonic Windtunnel, GmbHMember DPW–1
Mark Rakowitz, DLR Institute of Aerodynamics and Flow TechnologyMember DPW–2
Ben Rider, The Boeing CompanyMember DPW–5
Edward N. (Ed) Tinoco, The Boeing Company (Retired)Member DPW–2, DPW–3, DPW–4, DPW–5
John Vassberg, The Boeing CompanyChairman DPW–2, DPW–3, DPW–4, DPW–5, Member DPW–1
Rich Wahls, NASA Langley Research CenterMember DPW–1, DPW–2, DPW–3, DPW–4, DPW–5
Tom Zickuhr, Cessna Aircraft CompanyMember DPW–1, DPW–2, DPW–3, DPW–4
15
Session Number Session Title Time Topic Room
Monday, 24 June 2013
3–PLNRY–1 Opening Plenary Session – “Aeronautics in the Virtual Age”
0800 hrs Opening Plenary Session Harbor Ballroom I and II
10–CFD–1 Reynolds Averaged Navier–Stokes (RANS) Models of Turbulence
0900 hrs 21st AIAA Computational Fluid Dynamics Conference
Nautilus 4
11–CFD–2 High–Order Methods I 0900 hrs 21st AIAA Computational Fluid Dynamics Conference
Nautilus 5
12–CFD–3 Chemically Reacting Flows 0900 hrs 21st AIAA Computational Fluid Dynamics Conference
Seabreeze I
13–CFD–4 Numerical Algorithms for Inviscid and Viscous Flows I 0900 hrs 21st AIAA Computational Fluid Dynamics Conference
Spinaker I
14–CFD–5 Solution Adaptive Grid Techniques I 0900 hrs 21st AIAA Computational Fluid Dynamics Conference
Marina 5
15–CFD–6 Other Topics in CFD I 0900 hrs 21st AIAA Computational Fluid Dynamics Conference
Seabreeze II
16–CFD–7 Interdisciplinary Methods I 0900 hrs 21st AIAA Computational Fluid Dynamics Conference
Room 514
4–APA–1 Aerodynamics Education (Invited) 0900 hrs 31st AIAA Applied Aerodynamics Conference
Marina 2
5–APA–2 Innovative Aerodynamic Concepts and Designs 0900 hrs 31st AIAA Applied Aerodynamics Conference
Marina 3
6–APA–3 Aerodynamic–Structural Dynamics Interaction I 0900 hrs 31st AIAA Applied Aerodynamics Conference
Marina 4
7–APA–4 Environmentally Friendly and Efficient Aerodynamics 0900 hrs 31st AIAA Applied Aerodynamics Conference
Executive Conference Room 2A
8–APA–5 Propeller/Rotorcraft/Wind Turbine Aerodynamics I 0900 hrs 31st AIAA Applied Aerodynamics Conference
Executive Conference Room 4
17–FD–1 Future of Fluids – Celebrating 60 Years of AFOSR 0900 hrs 43rd AIAA Fluid Dynamics Conference
Nautilus 2
SESSIONS AT A GLANCE
16
Session Number Session Title Time Topic Room
Monday, 24 June 2013 (continued)
18–FD–2 Turbomachinery, Combustion, and Internal Flows 0900 hrs 43rd AIAA Fluid Dynamics Conference
Room 511
19–FD–3 Boundary–Layer Stability and Transition: General I 0900 hrs 43rd AIAA Fluid Dynamics Conference
Spinaker II
20–FD–4 Flapping–Wing Aerodynamics 0900 hrs 43rd AIAA Fluid Dynamics Conference
Nautilus 3
21–FD–5 Actuator Characterization and Development 0900 hrs 43rd AIAA Fluid Dynamics Conference
Executive Conference Room1
22–FD–6 Turbulent Flows I 0900 hrs 43rd AIAA Fluid Dynamics Conference
Executive Conference Room 2B
23–FD–7 Cross–Disciplinary Fluid Dynamics: Multi–Material and Multiphase Flows
0900 hrs 43rd AIAA Fluid Dynamics Conference
Room 518
25–PDL–1 Dielectric Barrier Discharges 0900 hrs 44th AIAA Plasmadynamics and Lasers Conference
Marina 6
9–ASE–1 Atmospheric Environment of the Earth and Beyond 0900 hrs 5th AIAA Atmospheric and Space Environments Conference
Room 515
24–GT–1 Ground Test Measurement Techniques I 0900 hrs AIAA Ground Testing Conference
Nautilus 1
26–TP–1 Multiphase Flows and Heat Pipes 0900 hrs 44th AIAA Thermophysics Conference
Executive Conference Room 3B
27–TP–2 Nonequilibrium Radiation 0900 hrs 44th AIAA Thermophysics Conference
Executive Conference Room 3A
38–CFD–8 Numerical Simulations of Hypersonic Flows (Invited) 1300 hrs 21st AIAA Computational Fluid Dynamics Conference
Nautilus 4
39–CFD–9 40 Years of CFD (Invited) 1300 hrs 21st AIAA Computational Fluid Dynamics Conference
Nautilus 5
40–CFD–10 High–Order Methods II 1300 hrs 21st AIAA Computational Fluid Dynamics Conference
Seabreeze I
41–CFD–11 Numerical Algorithms for Inviscid and Viscous Flows II 1300 hrs 21st AIAA Computational Fluid Dynamics Conference
Spinaker I
SESSIONS AT A GLANCE
17
Session Number Session Title Time Topic Room
Monday, 24 June 2013 (continued)
42–CFD–12 Design Optimization Techniques I 1300 hrs 21st AIAA Computational Fluid Dynamics Conference
Marina 5
43–CFD–13 Interdisciplinary Methods II 1300 hrs 21st AIAA Computational Fluid Dynamics Conference
Seabreeze II
44–CFD–14 Multi–Phase Flows 1300 hrs 21st AIAA Computational Fluid Dynamics Conference
Room 514
30–APA–6 Drag Prediction Workshop/NASA Common Research Model
1300 hrs 31st AIAA Applied Aerodynamics Conference
Nautilus 3
32–APA–8 Aerodynamic and Multidisciplinary Design and Optimization Methods I
1300 hrs 31st AIAA Applied Aerodynamics Conference
Marina 3
34–APA–10 Unsteady Aerodynamics I 1300 hrs 31st AIAA Applied Aerodynamics Conference
Executive Conference Room 2A
35–APA–11 Applied CFD I 1300 hrs 31st AIAA Applied Aerodynamics Conference
Executive Conference Room 4
45–FD–10 Mixing and Combustion 1300 hrs 43rd AIAA Fluid Dynamics Conference
Executive Conference Room 1
46–FD–11 Celebrating 60 Years of AFOSR: Hypersonics into the 21st Century – Research Progress Since 2001 and Future Directions in Aerothermodynamics
1300 hrs 43rd AIAA Fluid Dynamics Conference
Harbor Ballroom I and II
47–FD–12 Boundary–Layer Stability and Transition: General II 1300 hrs 43rd AIAA Fluid Dynamics Conference
Spinaker II
48–FD–47 Fluid Structure Interaction 1300 hrs 43rd AIAA Fluid Dynamics Conference
Nautilus 2
31–APA–7/FD–8 Active and Passive Flow Control I 1300 hrs 31st AIAA Applied Aerodynamics Conference
Marina 2
33–APA–9/FD–9 Low Speed, Low Reynolds Number Aerodynamics I 1300 hrs 31st AIAA Applied Aerodynamics Conference
Marina 4
50–PDL–2 Electric Propulsion 1300 hrs 44th AIAA Plasmadynamics and Lasers Conference
Marina 6
SESSIONS AT A GLANCE
18
Session Number Session Title Time Topic Room
Monday, 24 June 2013 (continued)
36–ASE–2 Aircraft Icing CFD and Ice Adhesion 1300 hrs 5th AIAA Atmospheric and Space Environments Conference
Room 515
37–ASE–3 Vortices and Contrails in the Atmospheric Environment 1300 hrs 5th AIAA Atmospheric and Space Environments Conference
Room 518
49–GT–2 Ground Test Facilities Improvements and Capabilities 1300 hrs AIAA Ground Testing Conference
Nautilus 1
51–TP–3 Ablation I 1300 hrs 44th AIAA Thermophysics Conference
Executive Conference Room 3B
52–TP–4 Heat Transfer I – Conduction, Convection, Radiation, and Phase Change
1300 hrs 44th AIAA Thermophysics Conference
Executive Conference Room 3A
53–TP–5 Aerothermodynamics I 1300 hrs 44th AIAA Thermophysics Conference
Executive Conference Room 2B
54–LEC–1 Fluid Dynamics Award Lecture 1730 hrs Award Lecture Harbor Ballroom I and II
Tuesday, 25 June 2013
81–WS–1 Protecting Intellectual Property Workshop 0800 hrs Workshop Harbor Ballroom I and II
64–CFD–15 High–Order Methods III 0800 hrs 21st AIAA Computational Fluid Dynamics Conference
Nautilus 5
66–CFD–17 Numerical Algorithms for Inviscid and Viscous Flows III 0800 hrs 21st AIAA Computational Fluid Dynamics Conference
Seabreeze I
67–CFD–18 Design Optimization Techniques II 0800 hrs 21st AIAA Computational Fluid Dynamics Conference
Spinaker I
68–CFD–19 Grid Generation and Effects of Grid Quality I 0800 hrs 21st AIAA Computational Fluid Dynamics Conference
Marina 5
69–CFD–20 Numerical Treatment of Boundary Conditions I 0800 hrs 21st AIAA Computational Fluid Dynamics Conference
Room 514
65–CFD–16/GT–3 High–Speed and Chemically Reacting Flows I 0800 hrs 21st AIAA Computational Fluid Dynamics Conference
Nautilus 4
SESSIONS AT A GLANCE
19
Session Number Session Title Time Topic Room
Tuesday, 25 June 2013 (continued)
70–CFD–21/FD–15
Revolutionary Computational Aerosciences (RCA) – I (Invited)
0800 hrs 21st AIAA Computational Fluid Dynamics Conference
Nautilus 2
57–APA–12 Aerodynamic and Multidisciplinary Design and Optimization Methods II
0800 hrs 31st AIAA Applied Aerodynamics Conference
Marina 2
58–APA–13 Airfoil/Wing/Configuration Aerodynamics I 0800 hrs 31st AIAA Applied Aerodynamics Conference
Marina 3
59–APA–14 Sonic Boom Mitigation and Recent Advances in Hypersonics Vehicle Aero
0800 hrs 31st AIAA Applied Aerodynamics Conference
Marina 4
61–APA–16 Icing or Roughness Effects on Vehicle Aerodynamics 0800 hrs 31st AIAA Applied Aerodynamics Conference
Executive Conference Room 4
71–FD–16 Turbomachinery 0800 hrs 43rd AIAA Fluid Dynamics Conference
Room 511
72–FD–17 Shock/Boundary Layer Interactions 0800 hrs 43rd AIAA Fluid Dynamics Conference
Nautilus 3
73–FD–18 High–Speed Transition I 0800 hrs 43rd AIAA Fluid Dynamics Conference
Nautilus 1
75–FD–20 Boundary Layer and Airfoil Separation Control 0800 hrs 43rd AIAA Fluid Dynamics Conference
Seabreeze II
60–APA–15/FD–14
Bio–Inspired Aerodynamics I 0800 hrs 31st AIAA Applied Aerodynamics Conference
Executive Conference Room 2A
76–PDL–4 Magnetohydrodynamics 0800 hrs 44th AIAA Plasmadynamics and Lasers Conference
Executive Conference Room 1
77–PDL–5 Plasma–Assisted Combustion/Plasma Diagnostics 0800 hrs 44th AIAA Plasmadynamics and Lasers Conference
Marina 6
74–FD–19/PDL–3 Plasma Actuators 0800 hrs 43rd AIAA Fluid Dynamics Conference
Spinaker II
62–ASE–4 Ice Crystal Icing 0800 hrs 5th AIAA Atmospheric and Space Environments Conference
Room 515
63–ASE–5 Modeling Spacecraft Envrionmental Interactions with Space Plasma
0800 hrs 5th AIAA Atmospheric and Space Environments Conference
Room 518
SESSIONS AT A GLANCE
20
SESSIONS AT A GLANCESession Number Session Title Time Topic Room
Tuesday, 25 June 2013 (continued)
78–TP–6 Ablation II 0800 hrs 44th AIAA Thermophysics Conference
Executive Conference Room3B
79–TP–7 Aerothermodynamics II 0800 hrs 44th AIAA Thermophysics Conference
Executive Conference Room 3A
80–TP–8 Direct Simulation Monte Carlo Methods 0800 hrs 44th AIAA Thermophysics Conference
Executive Conference Room 2B
82–LNCH–2 Tuesday Awards Luncheon 1200 hrs Awards Luncheon Harbor Ballroom I and II
93–CFD–22 High–Order Methods IV 1430 hrs 21st AIAA Computational Fluid Dynamics Conference
Nautilus 5
94–CFD–23 High–Speed and Chemically Reacting Flows II 1430 hrs 21st AIAA Computational Fluid Dynamics Conference
Nautilus 4
95–CFD–24 Large–Eddy Simulation (LES), Direct Numerical Simulation (DNS), and Hybrid RANS/LES Methods I
1430 hrs 21st AIAA Computational Fluid Dynamics Conference
Seabreeze I
96–CFD–25 Design Optimization Techniques III 1430 hrs 21st AIAA Computational Fluid Dynamics Conference
Spinaker I
97–CFD–26 Parallel Computing 1430 hrs 21st AIAA Computational Fluid Dynamics Conference
Marina 5
98–CFD–27 Unsteady Flows I 1430 hrs 21st AIAA Computational Fluid Dynamics Conference
Seabreeze II
99–CFD–28 Solution Adaptive Grid Techniques II/GPU Computing 1430 hrs 21st AIAA Computational Fluid Dynamics Conference
Room 514
100–CFD–29/FD–23
Revolutionary Computational Aerosciences (RCA) – II (Invited)
1430 hrs 21st AIAA Computational Fluid Dynamics Conference
Nautilus 2
84–APA–17 Aerodynamic–Structural Dynamics Interaction II 1430 hrs 31st AIAA Applied Aerodynamics Conference
Nautilus 3
86–APA–19 Propeller/Rotorcraft/Wind Turbine Aerodynamics II 1430 hrs 31st AIAA Applied Aerodynamics Conference
Marina 2
87–APA–20 Wind Tunnel and Flight Testing Aero I 1430 hrs 31st AIAA Applied Aerodynamics Conference
Marina 3
21
SESSIONS AT A GLANCESession Number Session Title Time Topic Room
Tuesday, 25 June 2013 (continued)
88–APA–21 Other Topics in Applied Aero 1430 hrs 31st AIAA Applied Aerodynamics Conference
Marina 4
90–APA–23 Weapons Aerodynamics and Store Separation 1430 hrs 31st AIAA Applied Aerodynamics Conference
Executive Conference Room 4
101–FD–24 Vortex Flow and Vortical Structures 1430 hrs 43rd AIAA Fluid Dynamics Conference
Room 511
102–FD–25 High–Speed Transition: Modeling 1430 hrs 43rd AIAA Fluid Dynamics Conference
Nautilus 1
89–APA–22/FD–22
Low Speed, Low Reynolds Number Aerodynamics II 1430 hrs 31st AIAA Applied Aerodynamics Conference
Executive Conference Room 1
85–APA–18/FD–21
Active and Passive Flow Control II 1430 hrs 31st AIAA Applied Aerodynamics Conference
Spinaker II
103–PDL–6 Plasma–Based Flow Control 1430 hrs 44th AIAA Plasmadynamics and Lasers Conference
Marina 6
104–PDL–7 MHD for Power Generation/Radio Blackout Mitigation 1430 hrs 44th AIAA Plasmadynamics and Lasers Conference
Executive Conference Room 2A
91–ASE–6 Swept–Wing Icing 1430 hrs 5th AIAA Atmospheric and Space Environments Conference
Room 515
92–ASE–7 Spacecraft Charging in the Earth and Lunar Systems 1430 hrs 5th AIAA Atmospheric and Space Environments Conference
Room 518
105–TP–9 Computational Heat Transfer and Simulations 1430 hrs 44th AIAA Thermophysics Conference
Executive Conference Room 3B
106–TP–10 High–Speed and Rarefied Flows 1430 hrs 44th AIAA Thermophysics Conference
Executive Conference Room 3A
107–TP–11 Thermal Management and Protection 1430 hrs 44th AIAA Thermophysics Conference
Executive Conference Room 2B
108–PANEL–1 AIRA – Aircraft Icing Research Alliance Panel 1600 hrs Panel Room 515
22
Session Number Session Title Time Topic Room
Wednesday, 26 June 2013
111–LEC–3 Thermophysics Award Lecture 0800 hrs Award Lecture Harbor Ballroom I and II
118–CFD–30 High–Order Methods V 0900 hrs 21st AIAA Computational Fluid Dynamics Conference
Nautilus 5
119–CFD–31 Numerical Algorithms for Inviscid and Viscous Flows IV 0900 hrs 21st AIAA Computational Fluid Dynamics Conference
Nautilus 4
120–CFD–32 Large–Eddy Simulation (LES), Direct Numerical Simulation (DNS), and Hybrid RANS/LES Methods II
0900 hrs 21st AIAA Computational Fluid Dynamics Conference
Seabreeze I
121–CFD–33 Unsteady Flows II 0900 hrs 21st AIAA Computational Fluid Dynamics Conference
Spinaker I
122–CFD–34 Numerical Treatment of Boundary Conditions II 0900 hrs 21st AIAA Computational Fluid Dynamics Conference
Marina 5
123–CFD–35 Other Topics in CFD II 0900 hrs 21st AIAA Computational Fluid Dynamics Conference
Room 514
112–APA–24 Aerodynamic and Multidisciplinary Design and Optimization Methods III
0900 hrs 31st AIAA Applied Aerodynamics Conference
Marina 2
113–APA–25 Applied CFD II 0900 hrs 31st AIAA Applied Aerodynamics Conference
Marina 3
114–APA–26 Airfoil/Wing/Configuration Aerodynamics II 0900 hrs 31st AIAA Applied Aerodynamics Conference
Marina 4
116–APA–28 Wind Tunnel and Flight Testing Aero II 0900 hrs 31st AIAA Applied Aerodynamics Conference
Executive Conference Room 2A
124–FD–27 Reduced–Order Modeling 0900 hrs 43rd AIAA Fluid Dynamics Conference
Room 511
125–FD–28 Micro/Nano Scale Fluid Dynamics and Spray Cooling 0900 hrs 43rd AIAA Fluid Dynamics Conference
Room 518
126–FD–29 Hypersonic and Chemically–Reacting Flows I 0900 hrs 43rd AIAA Fluid Dynamics Conference
Nautilus 1
127–FD–30 High–Speed Transition II 0900 hrs 43rd AIAA Fluid Dynamics Conference
Nautilus 2
SESSIONS AT A GLANCE
23
Session Number Session Title Time Topic Room
Wednesday, 26 June 2013 (continued)
128–FD–31 Bluff Body and Shear Layer Control 0900 hrs 43rd AIAA Fluid Dynamics Conference
Nautilus 3
129–FD–32 Pitch and Plunge Wing Aerodynamics 0900 hrs 43rd AIAA Fluid Dynamics Conference
Spinaker II
115–APA–27/FD–26
Closed–Loop Flow Control 0900 hrs 31st AIAA Applied Aerodynamics Conference
Executive Conference Room 1
117–ASE–8 On–Ground and In–Flight Ice Protection 0900 hrs 5th AIAA Atmospheric and Space Environments Conference
Room 515
131–PDL–8 MHD for Re–Entry 0900 hrs 44th AIAA Plasmadynamics and Lasers Conference
Marina 6
132–PDL–9 Plasma and Laser Physics 0900 hrs 44th AIAA Plasmadynamics and Lasers Conference
Executive Conference Room 4
130–GT–4 Ground Testing Measurement Analysis 0900 hrs AIAA Ground Testing Conference
Seabreeze II
133–TP–12 Plumes, Propulsion, and Turbomachinery 0900 hrs 44th AIAA Thermophysics Conference
Executive Conference Room 3B
134–TP–13 Testing and Diagnostics 0900 hrs 44th AIAA Thermophysics Conference
Executive Conference Room 3A
135–TP–14 Heat Transfer II 0900 hrs 44th AIAA Thermophysics Conference
Executive Conference Room 2B
136–LNCH–3 Exhibitor Lunch Reception 1200 hrs Lunch Reception Harbor Ballroom III
144–CFD–36 High–Order Methods VI 1330 hrs 21st AIAA Computational Fluid Dynamics Conference
Nautilus 5
145–CFD–37 Recent Development of CE/SE Methods (Invited) 1330 hrs 21st AIAA Computational Fluid Dynamics Conference
Nautilus 4
146–CFD–38 Grid Generation and Effects of Grid Quality II 1330 hrs 21st AIAA Computational Fluid Dynamics Conference
Seabreeze I
147–CFD–39 Large–Eddy Simulation (LES), Direct Numerical Simulation (DNS), and Hybrid RANS/LES Methods III
1330 hrs 21st AIAA Computational Fluid Dynamics Conference
Spinaker I
SESSIONS AT A GLANCE
24
Session Number Session Title Time Topic Room
Wednesday, 26 June 2013 (continued)
148–CFD–40 Other Methods for CFD/Unsteady Flows III 1330 hrs 21st AIAA Computational Fluid Dynamics Conference
Marina 5
149–CFD–41 Numerical Error Estimation and Uncertainty Quantification in CFD
1330 hrs 21st AIAA Computational Fluid Dynamics Conference
Room 518
150–CFD–42 Other Topics in CFD III 1330 hrs 21st AIAA Computational Fluid Dynamics Conference
Room 514
138–APA–29 Transonic and Supersonic Aerodynamics 1330 hrs 31st AIAA Applied Aerodynamics Conference
Marina 2
139–APA–30 High Angle–of–Attack and High lLft Aerodynamics 1330 hrs 31st AIAA Applied Aerodynamics Conference
Marina 3
140–APA–31 Unsteady Aerodynamics II 1330 hrs 31st AIAA Applied Aerodynamics Conference
Marina 4
141–APA–32 Unmanned and VSTOL Vehicle Designs/tests 1330 hrs 31st AIAA Applied Aerodynamics Conference
Executive Conference Room 2A
151–FD–34 Turbulent Flows: Jets and Wakes 1330 hrs 43rd AIAA Fluid Dynamics Conference
Room 511
152–FD–35 Hypersonic and Chemically–Reacting Flows II 1330 hrs 43rd AIAA Fluid Dynamics Conference
Nautilus 1
153–FD–36 Roughness Induced Transition 1330 hrs 43rd AIAA Fluid Dynamics Conference
Nautilus 2
154–FD–37 High–Speed Flow Control 1330 hrs 43rd AIAA Fluid Dynamics Conference
Nautilus 3
155–FD–38 Turbulence 1330 hrs 43rd AIAA Fluid Dynamics Conference
Spinaker II
142–APA–33/FD–33
Bio–Inspired Aerodynamics II 1330 hrs 31st AIAA Applied Aerodynamics Conference
Executive Conference Room 1
157–PDL–10 Weakly Ionized Plasma Physics 1330 hrs 44th AIAA Plasmadynamics and Lasers Conference
Marina 6
158–PDL–11/FD–39
Aero–Optics 1330 hrs 44th AIAA Plasmadynamics and Lasers Conference
Executive Conference Room 4
SESSIONS AT A GLANCE
25
Session Number Session Title Time Topic Room
Wednesday, 26 June 2013 (continued)
143–ASE–9 Supercooled Large Drop and Icing Physics 1330 hrs 5th AIAA Atmospheric and Space Environments Conference
Room 515
156–GT–5 Ground Test Measurement Techniques II 1330 hrs AIAA Ground Testing Conference
Seabreeze II
159–TP–16 Thermophysical Properties and Surface Catalysis 1330 hrs 44th AIAA Thermophysics Conference
Executive Conference Room 3A
160–TP–17 Nonequlibrium Flows 1330 hrs 44th AIAA Thermophysics Conference
Executive Conference Room 2B
Thursday, 27 June 2013
163–LEC–4 Aerodynamics Award Lecture 0800 hrs Award Lecture Harbor Ballroom I and II
164–APA–34 Unsteady Aerodynamics III 0900 hrs 31st AIAA Applied Aerodynamics Conference
Marina 3
165–APA–35 Applied CFD III 0900 hrs 31st AIAA Applied Aerodynamics Conference
Seabreeze II
166–APA–36 Propeller/Rotorcraft/Wind Turbine Aerodynamics III 0900 hrs 31st AIAA Applied Aerodynamics Conference
Seabreeze I
168–APA–38 Vortical/Vortex Flow 0900 hrs 31st AIAA Applied Aerodynamics Conference
Marina 6
171–FD–42 Cavity Flows: Physics and Control 0900 hrs 43rd AIAA Fluid Dynamics Conference
Spinaker I
172–FD–43 Wing Aerodynamics 0900 hrs 43rd AIAA Fluid Dynamics Conference
Spinaker II
173–FD–44 Transition Open Forum 0900 hrs 43rd AIAA Fluid Dynamics Conference
Nautilus 1
174–FD–45 Turbulent Flows II 0900 hrs 43rd AIAA Fluid Dynamics Conference
Nautilus 2
175–FD–48 Shocks 0900 hrs 43rd AIAA Fluid Dynamics Conference
Nautilus 4
176–FD–49 Modeling and Simulation of Fluids 0900 hrs 43rd AIAA Fluid Dynamics Conference
Marina 2
SESSIONS AT A GLANCE
26
Session Number Session Title Time Topic Room
Thursday, 27 June 2013 (continued)
167–APA–37/FD–40
Active and Passive Flow Control III 0900 hrs 31st AIAA Applied Aerodynamics Conference
Marina 4
169–APA–39/FD–46
Low Speed, Low Reynolds Number Aerodynamics III 0900 hrs 31st AIAA Applied Aerodynamics Conference
Executive Conference Room 4
170–FD–41/GT–6 Experimental Methods 0900 hrs 43rd AIAA Fluid Dynamics Conference
Nautilus 3
SESSIONS AT A GLANCE
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NAS
A Lan
gley R
esea
rch Ce
nter
Mond
ay, 2
4 Ju
ne 2
013
4-AP
A-1
Aero
dyna
mics
Educ
ation
(Inv
ited)
Marin
a 2Ch
aired
by: M
. HAF
EZ, U
nivers
ity of
Califo
rnia,
Davis
and B
. CYB
YK, J
HU/A
pplie
d Phy
sics L
abora
tory
0900
hrs
AIAA-2
013-2
401
Aero
dyna
mics
Educ
ation
: Wh
ere W
e’ve B
een
and W
here
We
’re G
oing
R. Cu
mming
s, U.
S. Ai
r Forc
e Ac
adem
y, Co
lorad
o Spri
ngs,
CO
0930
hrs
Oral
Prese
ntatio
n (Inv
ited)
Teac
hing L
ow-S
peed
Ae
rody
nami
csA.
Plotki
n, Sa
n Dieg
o Stat
e Un
iversi
ty, S
an D
iego,
CA
1000
hrs
Oral
Prese
ntatio
n (Inv
ited)
Integ
ratio
n of
an
Unde
rgra
duat
e Aer
odyn
amics
Cu
rricu
lumM.
Drel
a, D.
Darm
ofal,
Massa
chus
etts I
nstitu
te of
Tech
nolog
y, Ca
mbrid
ge, M
A
1030
hrs
AIAA-2
013-2
402
Hydr
odyn
amics
to O
utbo
ard
to R
otor
s To W
ake T
urbu
lence
to
Expe
rt Wi
tnes
s: Th
e Ex
perie
nces
of an
Aer
onau
tical
Engin
eer o
ver 6
0 Ye
ars
B. M
cCorm
ick, P
enns
ylvan
ia St
ate
Unive
rsity,
Univ
ersity
Park,
PA
1100
hrs
Oral
Prese
ntatio
n (Inv
ited)
Aero
dyna
mics
for E
very
one
M. H
afez,
Unive
rsity
of Ca
liforni
a, Da
vis, D
avis,
CA
1130
hrs
Pane
l Disc
ussio
n
Mond
ay, 2
4 Ju
ne 2
013
5-AP
A-2
Inno
vativ
e Aer
odyn
amic
Conc
epts
and D
esign
sMa
rina 3
Chair
ed by
: J. G
UGLIE
LMO,
Boe
ing D
efens
e, Sp
ace &
Sec
urity
and J
. PIN
IER, N
ASA-L
angle
y Res
earch
Cente
r09
00 hr
sAIA
A-201
3-240
3Ae
rody
nami
c Ana
lysis o
f Var
iable
Geom
etry R
aked
Wing
tips f
or
Mid-R
ange
Tran
sonic
Tran
spor
t Air
craft
Aero
dyna
mic A
nalys
is of
Varia
ble G
eome
try Ra
ked
Wing
tips f
or M
id-Ra
nge T
rans
onic
Trans
port
Aircra
ftD.
Jinge
leski,
J. Sc
hetz,
R. Ka
pania
, Vir
ginia
Polyt
echnic
Instit
ute an
d Stat
e Un
iversit
y, Bla
cksbu
rg, VA
0930
hrs
AIAA-2
013-2
404
Unste
ady M
otion
s of a
Ram
Wi
ng Fl
ying a
bove
Wav
es an
d Lo
w-He
ight O
bsta
cles
K. Ma
tveev
, Was
hingto
n Stat
e Un
iversi
ty, Pu
llman
, WA
1000
hrs
AIAA-2
013-2
405
Defo
rmat
ion of
the U
pper
and
Lowe
r Sur
face
s of a
n Ai
rfoil
by M
acro
Fibe
r Com
posit
e Ac
tuat
ors
M. D
ebias
i, Y. B
ourem
el, Z.
Lu,
Natio
nal U
nivers
ity of
Sing
apore
, Sin
gapo
re, S
ingap
ore; V
. Ra
vicha
ndran
, Nan
yang
Tech
nolog
ical
Unive
rsity,
Sing
apore
, Sing
apore
1030
hrs
AIAA-2
013-2
406
Nume
rical
and E
xper
imen
tal
Aero
dyna
mic I
nves
tigat
ions
of B
ound
ary L
ayer
Inge
stion
fo
r Imp
rovin
g Pro
pulsi
on
Effic
iency
of Fu
ture
Air
Trans
port
G. Ca
rrier, O
. Atin
ault,
R. Gr
enon
, C.
Verbe
cke,
ONER
A, Me
udon
, Fran
ce
1100
hrs
AIAA-2
013-2
407
Theo
retic
al an
d Exp
erim
enta
l Re
sults
for t
he S4
14, S
lotted
, Na
tura
l-Lam
inar-F
low A
irfoil
J. Co
der, M
. Mau
ghme
r, Pe
nnsy
lvania
Stat
e Univ
ersity
, Un
iversi
ty Pa
rk, PA
; D. S
omers
, Air
foils,
Inc.,
Port
Matild
a, PA
27
Mond
ay, 2
4 Ju
ne 2
013
6-AP
A-3
Aero
dyna
mic-S
tructu
ral D
ynam
ics In
terac
tion
IMa
rina 4
Chair
ed by
: J. A
ZEVE
DO an
d Z. Y
ANG,
Wrig
ht St
ate U
nivers
ity09
00 hr
sAIA
A-201
3-240
8CF
D Ba
sed R
educ
ed O
rder
Mo
del f
or Tr
anso
nic G
ust
Resp
onse
Pre
dictio
n an
d Al
leviat
ionW.
Zhan
g, W.
Zhan
g, Z.
Ye,
North
weste
rn Po
lytec
hnica
l Un
iversi
ty, X
i’an,
China
0930
hrs
AIAA-2
013-2
409
Force
d Res
pons
e Ana
lysis
of
Comp
resso
r Blad
es u
nder
Un
stead
y Inle
t Dist
ortio
nZ.
Zhan
g, A.
Hou,
Beiha
ng U
nivers
ity,
Beijin
g, Ch
ina; W
. Tuo
, A. X
ia, B
eijing
Ae
ronau
tical
Tech
nolog
y Res
earch
Ce
nter, B
eijing
, Chin
a; S.
Zhou
, Be
ihang
Univ
ersity
, Beij
ing, C
hina
1000
hrs
AIAA-2
013-2
410
Aero
elasti
c Ana
lysis
of a
Flexib
le De
lta W
ing at
High
An
gle of
Atta
ckJ.
Quan
, Z. Y
e, W.
Zhan
g, No
rthwe
stern
Polyt
echn
ical
Unive
rsity,
Xi’a
n, Ch
ina
Mond
ay, 2
4 Ju
ne 2
013
7-AP
A-4
Envir
onme
ntall
y Frie
ndly
and E
fficie
nt A
erod
ynam
icsEx
ecut
ive Co
nfer
ence
2A
Chair
ed by
: R. W
AHLS
, NAS
A-Lan
gley R
esea
rch Ce
nter a
nd P.
MOR
GAN,
Ohio
Aeros
pace
Insti
tute
0900
hrs
AIAA-2
013-2
411
Desig
n of
an In
finite
Swep
t Wi
ng G
love f
or an
In-Fl
ight
DRE E
xper
imen
tM.
Tufts
, H. R
eed,
W. S
aric,
Texa
s A&
M Un
iversi
ty, Co
llege
Stat
ion, T
X
0930
hrs
AIAA-2
013-2
412
Effe
cts of
Step
Excre
scenc
es on
Sw
ept-W
ing Tr
ansit
ionG.
Dun
can,
B. Cr
awfor
d, M.
Tufts
, W.
Sari
c, H.
Reed
, Tex
as A&
M Un
iversi
ty, Co
llege
Stat
ion, T
X
1000
hrs
AIAA-2
013-2
413
Optim
al Sh
ape D
esign
of M
ail-
Slot N
acell
e on
N3-X
Hyb
rid
Wing
Bod
y Con
figur
ation
H. Ki
m, S
AIC, C
levela
nd, O
H; M
. Lio
u, NA
SA G
lenn R
esea
rch Ce
nter,
Cleve
land,
OH
1030
hrs
AIAA-2
013-2
414
Aero
dyna
mic S
hape
Op
timiza
tion
of a
Blen
ded-
Wing
-Bod
y Reg
ional
Trans
port
for a
Shor
t Ran
ge M
ission
T. Re
ist, D
. Zing
g, Un
iversi
ty of
Toron
to, To
ronto,
Cana
da
1100
hrs
AIAA-2
013-2
415
Comp
utatio
nal In
vesti
gatio
n of
the Ef
fects
of Su
rface
Im
perfe
ction
s and
Excre
scenc
es
on th
e Cro
ssflow
Insta
bility
M. Tu
fts, G
. Dun
can, B
. Craw
ford,
H.
Reed
, W. S
aric,
Texas
A&M
Unive
rsity,
Colleg
e Stat
ion, T
X
Mond
ay, 2
4 Ju
ne 2
013
8-AP
A-5
Prop
eller
/Rot
orcra
ft/Wi
nd Tu
rbine
Aer
odyn
amics
IEx
ecut
ive Co
nfer
ence
4Ch
aired
by: C
. SHE
NG, U
nivers
ity of
Toled
o and
Z. YA
NG, W
right
State
Univ
ersity
0900
hrs
AIAA-2
013-2
416
High
-Fide
lity Co
mput
ation
al Sim
ulatio
n of
the W
ake
Char
acter
istics
of a
Mode
l Wi
nd Tu
rbine
K. Sr
eeniv
as, C
. Hilb
ert, A
. Mitta
l, L.
Heret
h, L.
Taylo
r, Univ
ersity
of
Tenn
esse
e, Ch
attan
ooga
, Ch
attan
ooga
, TN
0930
hrs
AIAA-2
013-2
417
Comp
ariso
n of
CFD
with
BEM
Te
chniq
ue fo
r Wind
Turb
ine
Simula
tion
of Th
in an
d Thic
k Ro
tor B
lades
I. Elq
atary,
Cairo
Univ
ersity
, Giza
, Eg
ypt;
B. El
hadid
i, Ain
Sham
s Un
iversi
ty, Ca
iro, E
gypt
1000
hrs
AIAA-2
013-2
418
Prop
eller
- Wi
ng In
terac
tion
using
Rap
id Co
mput
ation
al Me
thod
sC.
Agos
tinell
i, C. A
llen,
C. Liu
, Un
iversi
ty of
Brist
ol, B
ristol
, Unit
ed
Kingd
om; G
. Ferr
aro, C
ranfie
ld Un
iversi
ty, Cr
anfie
ld, U
nited
Kin
gdom
; A. R
ampu
rawala
, Airb
us,
Brist
ol, U
nited
King
dom
1030
hrs
AIAA-2
013-2
419
Near-
Wake
Flow
Simu
lation
s for
a M
id-Siz
ed Ri
m Dr
iven W
ind
Turb
ineB.
Kaise
r, S. P
orosev
a, Un
iversit
y of
New
Mexic
o, Alb
uque
rque,
Albuq
uerqu
e, NM
; E. J
ohnso
n, Sa
ndia
Natio
nal
Labo
ratori
es, Al
buqu
erque
, NM;
R.
Hovsa
pian,
Idaho
Nati
onal
Labo
ratory
, Ida
ho Fa
lls, ID
1100
hrs
AIAA-2
013-2
420
Vorti
city C
onfin
emen
t tec
hniqu
e for
pres
erva
tion
of
tip vo
rtex
of ro
tatin
g blad
eK.
Pierso
n, A.
Povit
sky,
Unive
rsity
of Ak
ron, A
kron,
OH
28
Mond
ay, 2
4 Ju
ne 2
013
9-AS
E-1At
mosp
heric
Envir
onme
nt of
the E
arth
and B
eyon
dRo
om 5
15Ch
aired
by: M
. POL
ITOVIC
H, N
ation
al Ce
nter f
or Atm
osph
eric R
esea
rch an
d N. A
HMAD
, NAS
A Lan
gley R
esea
rch Ce
nter
0900
hrs
AIAA-2
013-2
421
Fillin
g the
Gap
s: Th
e Sy
nerg
istic
Appli
catio
n of
Sa
tellite
Dat
a for
the V
olcan
ic As
h Th
reat
to A
viatio
nJ.
Murra
y, J.
Verni
er, T.
Fairli
e, NA
SA
Lang
ley Re
searc
h Cen
ter, H
ampto
n, VA
; A. T
uppe
r, Aus
tralia
n Bure
au of
Me
teorol
ogy,
Casu
arina
, Aus
tralia
; M.
Pavo
lonis,
Nati
onal
Ocea
nic
and A
tmos
pheri
c Adm
inistr
ation
, Ma
dison
, WI;
N. Kr
otkov
, Univ
ersity
of
Maryl
and,
Baltim
ore, B
altim
ore,
MD; F
. Lind
say,
J. Ha
ynes
, NAS
A He
adqu
arters
, Was
hingto
n, DC
0930
hrs
AIAA-2
013-2
422
Wind
Tunn
el An
alysis
of th
e Wi
nd In
ciden
ce A
ngle
in th
e Flo
w Pa
ttern
in th
e Cen
tro de
La
nçam
ento
de A
lcânt
ara
A. Av
elar, F
. Carn
eiro B
rasile
iro, A
. Fa
ria, G
. Fisc
h, Ae
ronau
tics a
nd
Spac
e Ins
titute
(IAE)
, São
José
dos
Camp
os, B
razil
Mond
ay, 2
4 Ju
ne 2
013
10-C
FD-1
Reyn
olds A
vera
ged N
avier
-Sto
kes (
RANS
) Mod
els of
Turb
ulenc
eNa
utilu
s 4Ch
aired
by: C
. RUM
SEY,
NASA
-Lang
ley Re
searc
h Cen
ter an
d H. A
TKIN
S, N
ASA-L
angle
y Res
earch
Cente
r09
00 hr
sAIA
A-201
3-242
3Co
upled
/Unc
ouple
d solu
tions
of
RAN
S equ
ation
s usin
g a
Jaco
bian-
free N
ewto
n-Kr
ylov
meth
odC.
Conte
nt, P.
Outt
ier, P
. Cinn
ella,
Paris
Insti
tute o
f Tec
hnolo
gy, P
aris,
Franc
e
0930
hrs
AIAA-2
013-2
424
Adva
nced
Num
erica
l Sim
ulatio
n of
Mixin
g Hot
Core
and
Cold
Bypa
ss Flo
w in
Mode
rn
Prop
ulsion
Syste
ms w
ith In
terna
l Lo
bed F
orced
Mixe
rS.
Saeg
eler, C
. Mun
dt, Un
iversit
y of th
e Ge
rman
Fede
ral Ar
med F
orces,
Mun
ich,
Germ
any
1000
hrs
AIAA-2
013-2
425
Bypa
ss Tra
nsitio
n an
d Trip
ping
in Re
ynold
s-stre
ss Mo
del
Comp
utat
ions
G. G
erolym
os, I
. Vall
et, Pi
erre a
nd
Marie
Curie
Univ
ersity
, Pari
s, Fra
nce
1030
hrs
AIAA-2
013-2
426
Adve
rse P
ressu
re G
radie
nt
Modifi
catio
n to
Turb
ulenc
e Mo
dels
for W
all-b
ound
ed
Flows
S. M
edida
, J. B
aede
r, Univ
ersity
of
Maryl
and,
Colle
ge Pa
rk, Co
llege
Pa
rk, M
D
1100
hrs
AIAA-2
013-2
427
An In
vesti
gatio
n into
the
Failu
re of
a Non
-Line
ar Ed
dy-
Visco
sity M
odel
in Ca
pturin
g the
La
mina
risati
on Ph
enom
enon
A. Ke
shmiri,
Man
cheste
r Metr
opolit
an
Unive
rsity,
Manch
ester,
Unite
d King
dom;
R.
Erfan
i, H. G
ohari
Darab
khan
i, Un
iversit
y of M
anche
ster, M
anche
ster,
Unite
d King
dom
Mond
ay, 2
4 Ju
ne 2
013
11-C
FD-2
High
-Ord
er M
ethod
s INa
utilu
s 5Ch
aired
by: P
. ORK
WIS,
Univ
ersity
of Ci
ncinn
ati an
d C. L
IANG,
Geo
rge W
ashin
gton U
nivers
ity09
00 hr
sAIA
A-201
3-242
8Ho
le Cu
tting
of Cu
rved
Di
scont
inuou
s Gale
rkin
Chim
era O
verse
t Mes
hes u
sing
a Dire
ct Cu
t Meth
odM.
Galb
raith,
P. O
rkwis,
Univ
ersity
of
Cincin
nati,
Cincin
nati,
OH; J
. Ben
ek,
Air Fo
rce Re
searc
h Lab
orator
y, W
right-
Patte
rson A
FB, O
H
0930
hrs
AIAA-2
013-2
429
Aero
dyna
mic a
nd ac
ousti
c an
alysis
of an
extru
ded a
irfoil
wi
th a t
railin
g edg
e dev
ice us
ing
Detac
hed E
ddy S
imula
tion w
ith a
Disco
ntinu
ous G
alerk
in me
thod
M. W
urst, M
. Kess
ler, E.
Krae
mer,
Unive
rsity o
f Stut
tgart,
Stuttg
art,
Germ
any
1000
hrs
AIAA-2
013-2
430
High
orde
r sch
emes
for
cylin
drica
l/sph
erica
l co
ordin
ates
with
radia
l sy
mmetr
yS.
Wan
g, E.
John
sen,
Unive
rsity
of Mi
chiga
n, An
n Arbo
r, Ann
Arbo
r, MI
1030
hrs
AIAA-2
013-2
431
Fully
comp
ressib
le flo
w mo
del
and h
igh-or
der s
imula
tion o
f co
nvect
ion an
d diff
erenti
al ro
tation
of so
lar co
nvect
ion zo
neJ.
Wang
, C. L
iang,
Georg
e Wash
ington
Un
iversit
y, Wa
shing
ton, D
C; M.
Mies
ch,
Natio
nal C
enter
for A
tmosp
heric
Resea
rch, B
oulde
r, CO
1100
hrs
AIAA-2
013-2
432
High
-Ord
er Sp
ace-
Time
Meth
ods f
or Co
nser
vatio
n Law
sH.
Huy
nh, N
ASA G
lenn R
esea
rch
Cente
r, Clev
eland
, OH
29
Mond
ay, 2
4 Ju
ne 2
013
12-C
FD-3
Chem
ically
Rea
cting
Flow
sSe
abre
eze I
Chair
ed by
: C. G
ROTH
, Univ
ersity
of To
ronto
0900
hrs
AIAA-2
013-2
433
Para
llel I
mplic
it Ad
aptiv
e Mes
h Re
finem
ent f
or U
nstea
dy
Fully
-Com
pres
sible
Reac
tive
Flows
S. N
orthru
p, C.
Groth
, Univ
ersity
of
Toron
to, To
ronto,
Cana
da
0930
hrs
AIAA-2
013-2
434
Nume
rical
Simula
tion
of th
e No
n-Re
activ
e and
Rea
ctive
Flo
w in
a Swi
rled M
odel
Gas
Turb
ine Co
mbus
tor
G. Re
ichlin
g, B.
Noll
, M. A
igner,
Ge
rman
Aeros
pace
Cente
r (DL
R),
Stutt
gart,
Germ
any
1000
hrs
AIAA-2
013-2
435
1D an
d 2D
Simula
ation
s Rela
ted
to the
NAS
A Elec
tric A
rc Sh
ock
Tube
Expe
rimen
tsD.
Kotov
, Stan
ford U
nivers
ity, St
anfor
d, CA
; H. Y
ee, N
ASA A
mes R
esearc
h Ce
nter, M
offett
Field
, CA;
M. Pa
nesi,
Unive
rsity o
f Illino
is, Urb
ana-C
hamp
aign,
Urban
a, IL;
D. Pr
abhu
, A. W
ray, N
ASA
Ames
Resea
rch Ce
nter, M
offett
Field
, CA
1030
hrs
AIAA-2
013-2
436
Carb
uncle
s in
highe
r-ord
er
reso
lution
Euler
ian-La
gran
gian
comp
utat
ion of
high
-spee
d, pa
rticle
-lade
n flo
wS.
Dav
is, G
. Jac
obs,
W. D
on,
San D
iego S
tate U
nivers
ity, S
an
Diego
, CA
Mond
ay, 2
4 Ju
ne 2
013
13-C
FD-4
Nume
rical
Algo
rithm
s for
Invis
cid an
d Visc
ous F
lows I
Spina
ker I
Chair
ed by
: N. B
URGE
SS, U
nivers
ity of
Wyo
ming
and B
. DISK
IN, N
ation
al Ins
titute
of Ae
rospa
ce09
00 hr
sAIA
A-201
3-243
7Th
ree-
Dime
nsion
al In
tegra
l Bo
unda
ry La
yer F
ormu
lation
fo
r Gen
eral
Confi
gura
tions
M. D
rela,
Massa
chus
etts I
nstitu
te of
Tech
nolog
y, Ca
mbrid
ge, M
A
0930
hrs
AIAA-2
013-2
438
Effe
cts of
Turb
ulenc
e Mod
eling
fo
r a D
ual M
esh
CFD
Solve
rN.
Burg
ess,
Scien
ce an
d Tec
hnolo
gy
Corpo
ration
, Moff
ett Fi
eld, C
A; A.
Wiss
ink, A
rmy A
viatio
n and
Mi
ssile
Rese
arch D
evelo
pmen
t and
En
ginee
ring C
enter
, Moff
ett Fi
eld, C
A
1000
hrs
AIAA-2
013-2
439
The h
igh-o
rder
dyna
mic
comp
utat
ional
labor
ator
y for
CF
D re
sear
ch an
d app
licat
ions
P. Ou
ttier, C
. Con
tent,
P. Cin
nella
, Pa
ris In
stitut
e of T
echn
ology
, Pari
s, Fra
nce;
B. M
ichel,
ONE
RA, C
hâtill
on,
Franc
e
1030
hrs
AIAA-2
013-2
440
Deve
lopme
nt of
Num
erica
l Sc
heme
s for
Hyb
rid Tu
rbule
nce
Mode
lling i
n an
Indu
strial
CFD
Solve
rG.
Pont,
J. Ro
binet,
P. Ci
nnell
a, La
borat
ory D
ynFlu
id, Pa
ris, F
rance
; P.
Bren
ner, E
ADS,
Les M
ureau
x, Fra
nce
1100
hrs
AIAA-2
013-2
441
An A
LE-Eu
lerian
Form
ulatio
n of
Embe
dded
Bou
ndar
y Me
thod
s for
Turb
ulent
Fluid
-Str
uctu
re In
terac
tion
Prob
lems
V. La
kshm
inaray
an, C
. Farh
at,
Stan
ford U
nivers
ity, S
tanfor
d, CA
Mond
ay, 2
4 Ju
ne 2
013
14-C
FD-5
Solut
ion A
dapt
ive G
rid Te
chniq
ues I
Marin
a 5Ch
aired
by: C
. ROY
, Virg
inia T
ech a
nd S
. ARU
NAJAT
ESAN
, San
dia N
ation
al La
bs09
00 hr
sAIA
A-201
3-244
2Pa
ralle
l Anis
otro
pic B
lock-
Base
d Ada
ptive
Mes
h Re
finem
ent A
lgorit
hm Fo
r Th
ree-
Dime
nsion
al Flo
wsM.
Willi
amsch
en, C
. Grot
h, Un
iversi
ty of
Toron
to, To
ronto,
Cana
da
0930
hrs
AIAA-2
013-2
443
An ad
aptiv
e sim
plex c
ut-cel
l meth
od fo
r high
-orde
r dis
conti
nuou
s Gale
rkin
discre
tizati
ons o
f mult
i-mate
rial
and m
ulti-p
hysic
s pro
blems
H. Su
n, D.
Darm
ofal, M
assach
usetts
Ins
titute
of Tec
hnolo
gy, Ca
mbrid
ge, M
A
1000
hrs
AIAA-2
013-2
444
Struc
ture
d Mes
h r-R
efine
ment
us
ing Tr
unca
tion
Erro
r Eq
uidist
ribut
ion fo
r 1D
and 2
D Eu
ler P
roble
msA.
Chou
dhary
, C. R
oy, V
irgini
a Po
lytec
hnic
Institu
te an
d Stat
e Un
iversi
ty, B
lacks
burg,
VA
1030
hrs
AIAA-2
013-2
445
Boun
dary
Laye
r Ada
ptivit
y for
Tra
nson
ic Tur
bulen
t Flow
sK.
Chita
le, Un
iversit
y of C
olorad
o, Bo
ulder,
Bould
er, CO
; O. S
ahni,
Re
nssela
er Po
lytech
nic In
stitute
, Tro
y, NY
; S. T
endu
lkar, R
. Nast
asia,
Simme
trix, In
c., Cl
ifton P
ark, N
Y; M.
Sh
epha
rd, Re
nssela
er Po
lytech
nic
Institu
te, Tro
y, NY
; K. J
ansen
, Univ
ersity
of
Color
ado,
Bould
er, Bo
ulder,
CO
1100
hrs
AIAA-2
013-2
446
Imple
ment
ation
of A
dapt
ive
Mesh
Refi
neme
nt in
an
Impli
cit U
nstru
cture
d Fini
te-Vo
lume F
low So
lver
A. Sc
hwing
, I. N
ompe
lis, G
. Ca
ndler
, Univ
ersity
of M
innes
ota,
Minn
eapo
lis, M
innea
polis,
MN
30
Mond
ay, 2
4 Ju
ne 2
013
15-C
FD-6
Othe
r Top
ics in
CFD
ISe
abre
eze I
ICh
aired
by: M
. ZAH
R and
D. A
MSAL
LEM,
Stan
ford U
nivers
ity09
00 hr
sAIA
A-201
3-244
7On
the A
ccura
cy an
d Co
nver
genc
e of M
inimu
m-Re
sidua
l-Bas
ed N
onlin
ear
Redu
ced-
Orde
r Mod
els in
CFD
D. Am
salle
m, M
. Zah
r, C. F
arhat,
St
anfor
d Univ
ersity
, Stan
ford,
CA
0930
hrs
AIAA-2
013-2
448
Verifi
catio
n and
Valid
ation
Stu
dies f
or th
e LAV
A CFD
Solve
rS.
Moini-
Yekta
, Univ
ersity
of Ca
liforni
a, Da
vis, D
avis,
CA; M
. Bara
d, J.
Housm
an,
C. Kir
is, NA
SA Am
es Re
search
Cente
r, Mo
ffett F
ield, C
A; E.
Soze
r, C. B
rehm,
Sc
ience
and T
echno
logy C
orpora
tion,
Moffe
tt Field
, CA
1000
hrs
AIAA-2
013-2
449
Nume
rical
solut
ion of
ion
ized g
as co
mpre
ssible
flo
ws u
nder
the i
nflue
nce o
f ele
ctrom
agne
tic fi
elds
K. Pa
nourg
ias, J
. Eka
terina
ris,
Unive
rsity
of Pa
tras,
Patra
s, Gr
eece
1030
hrs
AIAA-2
013-2
450
SENS
EI Co
mput
ation
al Flu
id Dy
nami
cs Co
de: A
Case
Stud
y in
Mode
rn Fo
rtran
Softw
are
Deve
lopme
ntJ.
Derla
ga, T
. Phil
lips,
C. Ro
y, Vir
ginia
Polyt
echn
ic Ins
titute
and S
tate
Unive
rsity,
Blac
ksbu
rg, VA
1100
hrs
AIAA-2
013-2
451
Imme
rsed B
ound
ary M
ethod
fo
r Com
pres
sible
Turb
ulent
Flo
w Co
mput
ation
s in
Build
ing-
Cube
Meth
odT.
Ishida
, K. N
akah
ashi,
Japa
n Ae
rospa
ce Ex
plorat
ion Ag
ency
(JA
XA),
Chofu
, Jap
an
1130
hrs
AIAA-2
013-2
452
A hy
brid
adjoi
nt ap
proa
ch
appli
ed to
turb
ulent
flow
sim
ulatio
nsT.
Taylo
r, F. P
alacio
s, K.
Durai
samy
, J.
Alons
o, St
anfor
d Univ
ersity
, St
anfor
d, CA
Mond
ay, 2
4 Ju
ne 2
013
16-C
FD-7
Inter
discip
linar
y Meth
ods I
Room
514
Chair
ed by
: R. D
AVIS,
Univ
ersity
of Ca
liforni
a Dav
is09
00 hr
sAIA
A-201
3-245
3Pa
rame
tric A
nalys
is of
Icing
Co
ntro
l Usin
g Syn
theti
c Jet
Actu
ator
sN.
Nag
appa
n, V.
Golub
ev, E
mbry-
Riddle
Aeron
autic
al Un
iversi
ty,
Dayto
na B
each
, FL;
W. H
abas
hi,
McGil
l Univ
ersity
, Mon
tréal,
Cana
da
0930
hrs
AIAA-2
013-2
454
CFD
Base
d Opt
imiza
tion
of A
Fle
xible
Flapp
ing W
ingC.
Carso
n, H.
Luo,
B. Y
in, Va
nderb
ilt Un
iversi
ty, N
ashv
ille, T
N
1000
hrs
AIAA-2
013-2
455
Massi
vely
Para
llel 3
D Sp
ectra
l Diff
eren
ce So
lver f
or
Simula
ting V
ortex
-Indu
ced
Vibra
tions
of Ci
rcular
Cylin
ders
A. De
Jong
, C. L
iang,
Georg
e Wa
shing
ton U
nivers
ity, W
ashin
gton,
DC
1030
hrs
AIAA-2
013-2
456
Lift a
nd dr
ag co
ntro
l usin
g die
lectri
c bar
rier d
ischa
rge
plasm
a actu
ator
s ins
talle
d on
the w
ingtip
sT.
Mizo
kami
, D. N
oguc
hi, K.
Fu
kaga
ta, Ke
io Un
iversi
ty,
Yoko
hama
, Jap
an
1100
hrs
AIAA-2
013-2
457
Disco
ntinu
ous G
alerk
in dis
cretiz
ation
coup
led w
ith sh
arp
interf
ace m
ethod
for a
blativ
e ma
terial
sP. S
chroo
yen,
Catho
lic Un
iversit
y of
Leuve
n, Leu
ven,
Belgiu
m; K.
Hillew
aert,
Cena
ero, G
osselie
s, Be
lgium;
T. M
agin,
vo
n Kárm
án In
stitute
for F
luid Dy
nami
cs,
Rhod
e-Sain
t-Gen
èse, B
elgium
; P.
Chate
lain, C
atholic
Unive
rsity o
f Leu
ven,
Leuve
n, Be
lgium
1130
hrs
AIAA-2
013-2
458
Fluid-
Solid
Inter
actio
n Mo
delin
g of C
ompr
essib
le Dr
oplet
Impa
ct on
to El
astic
Su
bstra
tesS.
Naja
fi Marz
bali,
A. Do
latab
adi,
Conc
ordia
Unive
rsity,
Mon
tréal,
Ca
nada
; P. J
edrze
jowsk
i, Roll
s-Roy
ce
Grou
p plc,
Mon
tréal,
Cana
da
Mond
ay, 2
4 Ju
ne 2
013
17-FD
-1Fu
ture
of Fl
uids -
Celeb
ratin
g 60
Year
s of A
FOSR
Naut
ilus 2
Chair
ed by
: D. H
ITT, U
nivers
ity of
Verm
ont
0900
hrs
Oral
Prese
ntatio
n (Inv
ited)
Low
Orde
r Mod
eling
for
Agile
Fligh
t: Pr
ogre
ss an
d Ch
allen
ges
J. Eld
redge
, Univ
ersity
of Ca
liforni
a, Lo
s Ang
eles,
Los A
ngele
s, CA
0930
hrs
Oral
Prese
ntatio
n (Inv
ited)
Dyna
mics
and C
ontro
l of W
all-
Boun
ded S
hear
Flow
sM.
Jova
novic
, Univ
ersity
of
Minn
esota
, Minn
eapo
lis,
Minn
eapo
lis, M
N
1000
hrs
Oral
Prese
ntatio
n (Inv
ited)
Comp
utat
ional
Chall
enge
s and
Op
portu
nities
in Cl
osed
-Loop
Flo
w Co
ntro
lT.
Colon
ius, C
alifor
nia In
stitut
e of
Tech
nolog
y, Pa
sade
na, C
A
1030
hrs
Oral
Presen
tation
(Inv
ited)
Simpli
fying
Comp
lex
Meas
urem
ents:
Plen
optic
Ca
mera
s and
the F
uture
of
Expe
rimen
tal Fl
ow D
iagno
stics
B. Th
urow,
Aubu
rn Un
iversit
y, Au
burn,
AL 11
00 hr
sOr
al Pre
senta
tion (
Invite
d)Pe
rspec
tives
on W
all-B
ound
ed
Turb
ulent
Flow
sB.
McK
eon,
Califo
rnia I
nstitu
te of
Tech
nolog
y, Pa
sade
na, C
A
31
Mond
ay, 2
4 Ju
ne 2
013
18-FD
-2Tu
rbom
achin
ery,
Comb
ustio
n, an
d Int
erna
l Flow
sRo
om 5
11Ch
aired
by: A
. GRO
SS, T
he U
nivers
ity of
Arizo
na09
00 hr
sAIA
A-201
3-245
9Flo
w Inv
estiga
tion a
nd Ac
ousti
c Me
asur
emen
ts of
an U
ncon
fined
Tu
rbule
nt Pr
emixe
d Jet
Flame
H. Na
wroth
, C. P
asche
reit, T
echnic
al Un
iversit
y of B
erlin,
Berlin
, Germ
any;
F. Zha
ng, P.
Habis
reuthe
r, H. B
ockho
rn,
Karlsr
uhe I
nstitu
te of
Techn
ology,
Ka
rlsruh
e, Ge
rman
y
0930
hrs
AIAA-2
013-2
460
Comp
utat
ional
Fluid
Dyna
mics
Inve
stiga
tion
of So
lar Ch
imne
y Po
wer P
lant
F. Me
ng, A
. Gros
s, H.
Fase
l, Un
iversi
ty of
Arizo
na, T
ucso
n, Tu
cson,
AZ
1000
hrs
AIAA-2
013-2
461
Inve
stiga
tion
of Su
bgrid
Clo
sure
Mod
els fo
r Fini
te-Ra
te Sc
ramj
et Co
mbus
tion
A. Po
tturi,
J. Ed
wards
, Nort
h Caro
lina
State
Univ
ersity
, Rale
igh, N
C
1030
hrs
AIAA-2
013-2
462
High
Fide
lity D
esign
Op
timiza
tion
of a
Thre
e Di
mens
ion Su
perso
nic In
take
M. Az
iz, In
stitut
e of A
viatio
n En
ginee
ring a
nd Te
chno
logy,
Giza,
Egyp
t; H.
Elba
nna,
M.
Abdu
lraha
man,
Cairo
Univ
ersity
, Giz
a, Eg
ypt
Mond
ay, 2
4 Ju
ne 2
013
19-FD
-3Bo
unda
ry-La
yer S
tabil
ity an
d Tra
nsitio
n: G
ener
al I
Spina
ker I
ICh
aired
by: K
. CAS
SEL,
Illino
is Ins
titute
of Te
chno
logy a
nd E.
WHI
TE, T
exas
A&M
Unive
rsity
0900
hrs
AIAA-2
013-2
463
A unifi
ed fr
amew
ork f
or gl
obal
instab
ility m
echan
isms in
the
plane
chan
nel, d
iverg
ing ch
anne
l an
d bac
kwar
d-fac
ing st
ep fl
owM.
Jotka
r, Tata
Instit
ute of
Fund
amen
tal
Resea
rch, H
ydera
bad,
India;
J. Pe
rez,
Techn
ical U
nivers
ity of
Mad
rid, M
adrid
, Sp
ain; R
. Gov
indarj
an, T
ata In
stitute
of
Fund
amen
tal Re
search
, Hyd
eraba
d, Ind
ia; V.
Theo
filis,
Techn
ical U
nivers
ity of
Ma
drid,
Madri
d, Sp
ain
0930
hrs
AIAA-2
013-2
464
An ap
proa
ch fo
r find
ing
quan
tum
leap o
f dra
g re
ducti
on: b
ased
on th
e we
akly-
stoch
astic
Nav
ier-
Stoke
s equ
ation
K. Na
itoh,
T. No
gami
, T. T
obe,
Wase
da U
nivers
ity, S
hinjuk
u, Ja
pan
1000
hrs
AIAA-2
013-2
465
On Co
ntinu
ous S
pectr
a of
the O
rr-So
mmer
feld/
Squir
e Eq
uatio
ns an
d Ent
rainm
ent
of Fr
ee-st
ream
Vorti
cal
Distu
rban
ces i
n th
e Blas
ius
Boun
dary
Laye
rX.
Wu,
Impe
rial C
olleg
e Lon
don,
Lond
on, U
nited
King
dom;
M. D
ong,
Tianji
n Univ
ersity
, Tian
jin, C
hina
1030
hrs
AIAA-2
013-2
466
Trans
ition
on a
Wing
with
Sp
anwi
se Va
rying
Cros
sflow
Ev
aluat
ed w
ith Li
near
Stab
ility
Theo
ryR.
Petzo
ld, R.
Rade
spiel
, Tec
hnica
l Un
iversi
ty of
Brau
nsch
weig,
Br
auns
chwe
ig, G
erman
y
1100
hrs
AIAA-2
013-2
467
Nonli
near
Dev
elopm
ent o
f th
e Mult
iple G
ortle
r Mod
es in
Hy
perso
nic B
ound
ary L
ayer
Flo
wsJ.
Ren,
S. Fu
, Tsin
ghua
Univ
ersity
, Be
ijing,
China
Mond
ay, 2
4 Ju
ne 2
013
20-FD
-4Fla
pping
-Wing
Aer
odyn
amics
Naut
ilus 3
Chair
ed by
: M. O
L, Air
Force
Rese
ach L
abora
tory a
nd M
. GRE
EN, S
yracu
se U
nivers
ity09
00 hr
sAIA
A-201
3-246
8Ex
perim
enta
l Stu
dy of
Two-
Dime
nsion
al Fla
pping
Wing
s in
Tand
em Co
nfigu
ratio
nX.
Zhan
g, K.
Lua,
T. Lim
, K. Y
eo,
Natio
nal U
nivers
ity of
Sing
apore
, Sin
gapo
re, S
ingap
ore
0930
hrs
AIAA-2
013-2
469
Mode
ling o
f Ins
tant
aneo
us
Passi
ve P
itch
of Fl
exibl
e Fla
pping
Wing
sC.
Kang
, Univ
ersity
of M
ichiga
n, An
n Arbo
r, Ann
Arbo
r, MI;
W. S
hyy,
Hong
Kong
Univ
ersity
of S
cienc
e an
d Tec
hnolo
gy, C
lear W
ater B
ay,
Hong
Kong
1000
hrs
AIAA-2
013-2
470
High
Rey
nolds
num
ber fl
ow
past
a flap
ping m
ulti-e
lemen
t air
foil
S. Ka
rampe
las, B
rno U
nivers
ity of
Te
chno
logy,
Brno
, Cze
ch Re
publi
c
1030
hrs
AIAA-2
013-2
471
Nume
rical
and e
xperi
menta
l an
alysis
of ta
ndem
flap
ping
flight
W. Ta
y, M.
Percin
, B. v
an O
udhe
usden
, H.
Bijl, D
elft U
nivers
ity of
Techn
ology,
De
lft, Th
e Neth
erlan
ds; O
. Ceti
ner, M
. Un
al, Is
tanbu
l Techn
ical U
nivers
ity,
Istan
bul, T
urkey
1100
hrs
AIAA-2
013-2
472
Adjoi
nt-b
ased
shap
e and
kin
emat
ics op
timiza
tion
of
flapp
ing w
ing pr
opuls
ive
effic
iency
M. Jo
nes,
N. Ya
malee
v, No
rth
Carol
ina A&
T Stat
e Univ
ersity
, Gr
eens
boro,
NC
1130
hrs
AIAA-2
013-2
473
PIV D
ata A
nalys
is ar
ound
a Fla
pping
Wing
via P
rope
r Or
thog
onal
Deco
mpos
ition
W. Ya
maza
ki, H
. Yam
ada,
Naga
oka
Unive
rsity
of Te
chno
logy,
Naga
oka,
Japa
n
32
Mond
ay, 2
4 Ju
ne 2
013
21-FD
-5Ac
tuat
or Ch
arac
teriza
tion
and D
evelo
pmen
tEx
ecut
ive Co
nfer
ence
1Ch
aired
by: J
. GRE
GORY
, The
Ohio
Stat
e Univ
ersity
and K
. CAS
PER,
Sand
ia Na
tiona
l Lab
orator
ies09
00 hr
sAIA
A-201
3-247
4A
Revie
w of
Fluid
ic Os
cillat
or
Deve
lopme
ntJ.
Greg
ory, M
. Tom
ac, O
hio S
tate
Unive
rsity,
Colum
bus,
OH
0930
hrs
AIAA-2
013-2
475
Expe
rimen
tal An
alysis
of th
e Eff
ect of
Inter
actio
n Par
amete
rs on
Synth
etic J
et Ac
tuator
Arra
ysZ.
Hasna
in, A.
Flata
u, J.
Hubb
ard,
A. Sa
ssoon
, Univ
ersity
of M
arylan
d, Co
llege P
ark, C
ollege
Park,
MD
1000
hrs
AIAA-2
013-2
476
Deve
lopme
nt an
d Ch
arac
teriza
tion o
f Ultr
a-High
Fre
quen
cy Re
sona
nce-E
nhan
ced
Micro
jet Ac
tuator
P. Upa
dhya
y, J.
Gusta
vsson
, F. Al
vi,
Florid
a Stat
e Univ
ersity,
Tallah
assee
, FL
1030
hrs
AIAA-2
013-2
477
Swee
ping J
et Ac
tuat
or in
a Qu
iesce
nt En
viron
ment
M. Ko
klu, L
. Pac
k Melt
on, N
ASA
Lang
ley Re
searc
h Cen
ter, H
ampto
n, VA
1100
hrs
AIAA-2
013-2
478
Jet I
nter
actio
ns in
a Fe
edba
ck-
Free
Fluid
ic Os
cillat
or at
Low
Flow
Rate
M. To
mac,
J. Gr
egory
, Ohio
Stat
e Un
iversi
ty, Co
lumbu
s, OH
Mond
ay, 2
4 Ju
ne 2
013
22-FD
-6Tu
rbule
nt Fl
ows I
Exec
utive
Conf
eren
ce 2
BCh
aired
by: S
. RAG
AB, V
irgini
a Tec
h and
D. D
ONZIS
, Tex
as A&
M Un
iversi
ty09
00 hr
sAIA
A-201
3-247
9Ax
isymm
etric
Simula
tion
of
Turb
ulent
Hyp
erso
nic fl
ows i
n co
ntou
red n
ozzle
K. Be
nsas
si, G
. Gros
sir, P
. Ram
baud
, vo
n Kárm
án In
stitut
e for
Fluid
Dyna
mics,
Rhod
e-Sain
t-Gen
èse,
Belgi
um
0930
hrs
AIAA-2
013-2
480
On ef
fectiv
eness
of a
rank
-1
mode
l of t
urbu
lent c
hann
els fo
r rep
resen
ting t
he ve
locity
spect
raR.
Moarr
ef, Ca
liforni
a Inst
itute
of Tec
hnolo
gy, Pa
saden
a, CA
; A. S
harm
a, Un
iversit
y of S
heffie
ld, Sh
effield
, Unit
ed
Kingd
om; J
. Trop
p, B.
McKe
on, C
aliforn
ia Ins
titute
of Tec
hnolo
gy, Pa
saden
a, CA
1000
hrs
AIAA-2
013-2
481
A Sys
tems A
ppro
ach t
o Mod
eling
Op
posit
ion Co
ntrol
in Tu
rbule
nt Pip
e Flow
M. Lu
har, C
aliforn
ia Ins
titute
of Tec
hnolo
gy, Pa
saden
a, CA
; A. S
harm
a, Un
iversit
y of S
heffie
ld, Sh
effield
, Unit
ed
Kingd
om; B
. McK
eon,
Califo
rnia I
nstitu
te of
Techn
ology,
Pasad
ena,
CA
1030
hrs
AIAA-2
013-2
482
Nume
rical
Expe
rimen
ts wi
th
Obse
rvab
le Eu
ler an
d Nav
ier-
Stoke
s Equ
ation
s in
Shoc
ks
and T
urbu
lent F
lows
K. Mo
hsen
i, H. N
ataraj
an, U
nivers
ity
of Flo
rida,
Gaine
sville
, Gain
esvil
le, FL
1100
hrs
AIAA-2
013-2
483
Hybr
id Re
ynold
s-Ave
rage
d and
La
rge-
Eddy
Simu
lation
s of a
Su
perso
nic Ca
vity F
lameh
older
D. Pe
terso
n, M.
Hag
enma
ier, C
. Ca
rter, A
ir Forc
e Res
earch
Labo
ratory
, W
right-
Patte
rson A
FB, O
H; S
. Tu
ttle, N
aval
Rese
arch L
abora
tory,
Wash
ington
, DC
Mond
ay, 2
4 Ju
ne 2
013
23-FD
-7Cr
oss-D
iscipl
inary
Fluid
Dyn
amics
: Mult
i-Mat
erial
and M
ultiph
ase F
lows
Room
518
Chair
ed by
: A. R
OTHM
AYER
, Iow
a Stat
e Univ
ersity
and S
. OTTA
, GE G
lobal
Rese
arch C
enter
0900
hrs
AIAA-2
013-2
484
A Su
rvey
of A
irbor
ne P
artic
le Im
pact
Char
acter
istics
Usin
g Hi
gh Sp
eed P
artic
le Sh
adow
Ve
locim
etry
S. W
hitak
er, D
. Reil
ly, J.
Bon
s, Oh
io St
ate U
nivers
ity, C
olumb
us, O
H
0930
hrs
AIAA-2
013-2
485
Appli
catio
n of
a No
vel
Appr
oach
for T
urbu
lence
Mod
el In
itializ
ation
: Pre
limina
ry
Resu
ltsB.
Rollin
, N. D
eniss
en, J
. Reis
ner,
M. An
drews
, Los
Alam
os N
ation
al La
borat
ory, L
os Al
amos
, NM
1000
hrs
AIAA-2
013-2
486
Drop
let Im
pact
and
Solid
ificati
on on
Hyd
roph
ilic an
d Su
perh
ydro
phob
ic Sub
strate
s in
Icing
Cond
itions
M. M
oham
madi,
Conco
rdia U
nivers
ity,
Montr
éal, C
anad
a; D.
De Pa
uw, D
elft
Unive
rsity o
f Tech
nolog
y, De
lft, Th
e Ne
therla
nds;
M. Te
mbely
, A. D
olatab
adi,
Conco
rdia U
nivers
ity, M
ontré
al, Ca
nada
1030
hrs
AIAA-2
013-2
487
Mode
ling T
urbu
lent R
aylei
gh-
Taylo
r Mixi
ng w
ith D
ynam
ic In
terfa
ces
N. D
eniss
en, B
. Roll
in, J.
Reisn
er,
M. An
drews
, Los
Alam
os N
ation
al La
borat
ory, L
os Al
amos
, NM
33
Mond
ay, 2
4 Ju
ne 2
013
24-G
T-1Gr
ound
Test
Meas
urem
ent T
echn
iques
INa
utilu
s 1Ch
aired
by: R
. DAN
FORT
H, AE
RO S
ystem
s Eng
ineeri
ng, I
nc. a
nd J.
EVER
HART
, NAS
A-Lan
gley R
esea
rch Ce
nter
0900
hrs
AIAA-2
013-2
488
Expe
rimen
tal d
emon
strat
ion of
An
alyzin
g an
Engin
e’s Ex
haus
t Je
t with
the B
ackg
roun
d-Or
iented
Schli
eren
Meth
odR.
Adam
czuk
, U. H
artma
nn, J
. Se
ume,
Leibn
iz Un
iversi
ty of
Hann
over,
Han
nove
r, Germ
any
0930
hrs
AIAA-2
013-2
489
Desig
n, A
nalys
is, an
d Tes
ting
of N
anop
artic
le-In
fuse
d Thin
Fil
m Se
nsor
s for
Low
Skin
Frict
ion A
pplic
ation
sB.
Leslie
, J. S
chetz
, Virg
inia
Polyt
echn
ic Ins
titute
and S
tate
Unive
rsity,
Blac
ksbu
rg, VA
; K. H
ill,
Nano
sonic
, Inc
., Pe
mbrok
e, VA
1000
hrs
AIAA-2
013-2
490
Comp
ariso
n of
Force
, Mom
ent,
and P
ressu
re Co
effic
ients
for t
he Sa
me Te
st Ar
ticle
in Mu
ltiple
Wind
Tunn
elsR.
DeLo
ach,
NASA
Lang
ley Re
searc
h Ce
nter, H
ampto
n, VA
1030
hrs
AIAA-2
013-2
491
Contr
ol of
Wind
Tunn
el Tes
t Tem
pera
ture U
sing a
Ma
thema
tical
Mode
lP. S
utcliff
e, A.
Vorob
iev, M
. Ren
nie,
Unive
rsity o
f Notr
e Dam
e, No
tre Da
me,
IN; A.
Cain,
Inno
vativ
e Tech
nolog
y Ap
plicati
ons C
ompa
ny, Ch
esterfi
eld, M
O
Mond
ay, 2
4 Ju
ne 2
013
25-P
DL-1
Diele
ctric
Barri
er D
ischa
rges
Marin
a 6Ch
aired
by: A
. LIKH
ANSK
II, Te
ch-X
Corpo
ration
and J
. ZITO
, Univ
ersity
of Fl
orida
0900
hrs
AIAA-2
013-2
492
Diele
ctric
Barri
er D
ischa
rge
Devic
e Thr
ust P
erfo
rman
ce at
Lo
w Pr
essu
res
S. G
ordon
, A. S
tariko
vskiy
, R. M
iles,
Princ
eton U
nivers
ity, P
rince
ton, N
J
0930
hrs
AIAA-2
013-2
493
The e
ffect
of ex
terna
l flow
ve
locity
on th
e mom
entu
m tra
nsfe
r of D
BD pl
asma
ac
tuat
ors
M. Ko
tsonis
, Delf
t Univ
ersity
of
Tech
nolog
y, De
lft, Th
e Neth
erlan
ds
1000
hrs
AIAA-2
013-2
494
On th
e vali
datio
n of
fluid
pla
sma m
odel
for p
ulsed
DBD
pla
sma a
ctuat
or si
mulat
ions
again
st fu
ll kine
tic ap
proa
chA.
Likha
nskii
, Tec
h-X Co
rporat
ion,
Bould
er, CO
; J. P
oggie
, Air F
orce
Rese
arch L
abora
tory,
Wrig
ht-Pa
tterso
n AFB
, OH
1030
hrs
AIAA-2
013-2
495
Explo
ratio
n of
Cera
mic
Diele
ctrics
for M
icros
cale
Diele
ctric
Barri
er D
ischa
rge
Plasm
a Actu
ator
sJ.
Zito,
D. Ar
nold,
R. D
ursch
er,
S. Ro
y, Un
iversi
ty of
Florid
a, Ga
inesv
ille, G
aines
ville,
FL
1100
hrs
AIAA-2
013-2
496
Time R
esolv
ed Sp
ectra
of
Pulse
d Nan
osec
ond D
ischa
rges
in
Argo
nT.
Kase
man,
S. O
’Byrn
e, W.
Yan,
J. Fle
tcher,
Univ
ersity
of N
ew S
outh
Wales
at th
e Aus
tralia
n Defe
nce
Force
Acad
emy,
Canb
erra,
Austr
alia
Mond
ay, 2
4 Ju
ne 2
013
26-TP
-1Mu
ltipha
se Fl
ows a
nd H
eat P
ipes
Exec
utive
Conf
eren
ce 3
BCh
aired
by: M
. MAN
TELLI
, Fun
daçã
o de E
nsino
e En
genh
aria d
e San
ta Ca
tarina
and B
. DRO
LEN,
Boe
ing D
efens
e, Sp
ace &
Sec
urity
0900
hrs
AIAA-2
013-2
497
Pred
icting
Por
osity
and
Effe
ctive
Ther
mal C
ondu
ctivit
y of
Sint
ered
Por
ous M
edia
Base
d on
Powd
er G
eome
tryG.
Verdi
eri N
uernb
erg, J
. Flor
ez
Mera
M. M
antel
li, F.
Milan
ese,
Fede
ral U
nivers
ity of
San
ta Ca
tarina
, Flo
rianó
polis,
Braz
il
0930
hrs
AIAA-2
013-2
498
Ther
mal P
erfo
rman
ce of
ATLA
S La
ser T
herm
al Co
ntro
l Sys
tem
Demo
nstra
tion
Unit
J. Ku
, F. R
obins
on, D
. Pate
l, L.
Otten
stein,
NAS
A God
dard
Spac
e Fli
ght C
enter
, Gree
nbelt
, Mary
land,
MD
1000
hrs
AIAA-2
013-2
499
Veloc
ity m
easu
reme
nt of
th
ermo
capil
ary fl
ows a
roun
d a
single
vapo
r bub
ble of
FC-7
2V.
Carva
lho, F
EMTO
Scie
nces
&
Tech
nolog
ies, B
elfort
, Fran
ce
1030
hrs
AIAA-2
013-2
500
Mode
ling o
f Spo
ntan
eous
Co
nden
satio
n in
High
-Spe
ed
Expa
nsion
of G
aseo
us M
ixtur
eI.
Kim, O
. Pero
omian
, X. Y
ang,
Metac
omp T
echn
ologie
s, Ag
oura
Hills,
CA
1100
hrs
AIAA-2
013-2
501
Nume
rical
Simula
tion
of
the T
herm
al Ef
fect
in th
e Ca
vitat
ing Ve
ntur
i Flow
D. Ca
o, G.
He,
H. Pa
n, F.
Qin,
North
weste
rn Po
lytec
hnica
l Un
iversi
ty, X
i’an,
China
34
Mond
ay, 2
4 Ju
ne 2
013
27-TP
-2No
nequ
ilibriu
m Ra
diatio
nEx
ecut
ive Co
nfer
ence
3A
Chair
ed by
: Y. S
UZEN
, Nort
h Dak
ota S
tate U
nivers
ity an
d A. A
LEXE
ENKO
, Purd
ue U
nivers
ity09
00 hr
sAIA
A-201
3-250
2Co
mpos
itiona
l Dep
ende
nce
of R
adian
ce in
CO2/
N2/A
r Sy
stems
B. Cr
uden
, A. B
randis
, D. P
rabhu
, ER
C, Inc
., Mo
ffett
Field,
CA
0930
hrs
AIAA-2
013-2
504
Infra
red R
adiat
ion
Meas
urem
ent b
ehind
Shoc
k Wa
ve in
Mar
s Sim
ulant
Gas
for
Aero
capt
ure M
ission
sH.
Taka
yana
gi, K.
Fujita
, Jap
an
Aeros
pace
Explo
ration
Agen
cy
(JAXA
), To
kyo,
Japa
n
1000
hrs
AIAA-2
013-2
505
None
quilib
rium
Spec
tral
Radia
tion
Behin
d the
Shoc
k Wa
ves i
n Ma
rtian
and E
arth
At
mosp
here
sA.
Dikaly
uk, R
ussia
n Aca
demy
of
Scien
ces,
Mosco
w, Ru
ssia;
P. Ko
zlov,
Y. Ro
mane
nko,
O. S
hatal
ov, M
osco
w St
ate U
nivers
ity, M
osco
w, Ru
ssia;
S. S
urzhik
ov, R
ussia
n Aca
demy
of
Scien
ces,
Mosco
w, Ru
ssia
1030
hrs
AIAA-2
013-2
506
Theo
retic
al Va
lidat
ion of
a Te
st Ga
s Sub
stitu
tion
for E
xpan
sion
Tube
Simu
lation
of G
as G
iant
Entry
C. Ja
mes,
D. G
ildfin
d, R.
Morga
n, T.
Mcint
yre, U
nivers
ity of
Que
ensla
nd,
Brisb
ane,
Austr
alia
1100
hrs
Mond
ay, 2
4 Ju
ne 2
013
28-LN
CH-1
12
00 -
1300
hrs
Lunc
h Br
eak
Lunc
h on
Own
Mond
ay, 2
4 Ju
ne 2
013
29-S
B-2
1230
- 13
00 h
rsMo
nday
Afte
rnoo
n Sp
eake
rs’ B
riefin
gSe
ssion
Roo
ms
Mond
ay, 2
4 Ju
ne 2
013
30-A
PA-6
Drag
Pre
dictio
n Wo
rksh
op/N
ASA
Comm
on R
esea
rch M
odel
Naut
ilus 3
Chair
ed by
: K. L
AFLIN
, Ces
sna A
ircraf
t Com
pany
and M
. MUR
AYAM
A, Ja
pan A
erosp
ace E
xplor
ation
Agen
cy13
00 hr
sAIA
A-201
3-250
7Fa
r-Fiel
d Dra
g Dec
ompo
sition
Me
thod
App
lied t
o the
DPW
-5
Test
Case
Res
ults
M. G
ariep
y, B.
Malo
uin, J
. Trep
anier
, E.
Laure
ndea
u, Éc
ole Po
lytec
hniqu
e de
Mon
tréal,
Mon
tréal,
Cana
da
1330
hrs
AIAA-2
013-2
508
CFD
Inve
stiga
tions
on th
e DP
W-5
Confi
gura
tion
with
Me
asur
ed Ex
perim
enta
l Wing
Tw
ist u
sing t
he el
sA So
lver a
nd
the F
ar-Fi
eld A
ppro
ach
D. H
ue, O
NERA
, Meu
don,
Franc
e
1400
hrs
AIAA-2
013-2
509
Invest
igatio
ns of
Fluid
-Stru
cture
Co
uplin
g and
Turb
ulenc
e Mod
el Eff
ects o
n the
DLR
Resu
lts of
the
Fifth
AIAA C
FD D
rag P
redict
ion
Work
shop
S. Ke
ye, O
. Brod
ersen
, Germ
an
Aeros
pace
Cente
r (DL
R), B
raunsc
hweig
, Ge
rman
y
1430
hrs
AIAA-2
013-2
510
Trans
onic
Tail B
uffe
t Sim
ulatio
ns fo
r the
Comm
on
Rese
arch
Mod
elS.
Illi, C
. Fing
skes
, T. L
utz, E
. Kra
emer,
Univ
ersity
of S
tuttga
rt,
Stutt
gart,
Germ
any
1500
hrs
AIAA-2
013-2
511
Resu
lts fr
om th
e Fifth
AIAA
Dra
g Pr
edict
ion W
orks
hop o
btaine
d wi
th a p
arall
el Ne
wton
-Kry
lov-
Schur
flow
solve
r disc
retize
d us
ing su
mmati
on-by
-parts
op
erator
sM.
Osus
ky, P.
Boom
, D. Z
ingg,
Unive
rsity o
f Toro
nto, T
oronto
, Can
ada
1530
hrs
Pane
lSta
tus a
nd D
irecti
ons o
f the
DPW
Serie
sDr
ag Pr
edict
ion W
orksh
op Co
mmitte
e: J
ohn V
assb
erg, B
oeing
Stev
e Allm
aras,
MIT
Chri
s Rum
sey,
NASA
Chri
s Roy
, Virg
inia T
ech
Rich
Wah
ls, N
ASA
Joe
Mori
son,
NASA
Mond
ay, 2
4 Ju
ne 2
013
31-A
PA-7
/FD-
8Ac
tive a
nd P
assiv
e Flow
Cont
rol I
Marin
a 2Ch
aired
by: D
. LAC
Y, Bo
eing C
omme
rcial
Airpla
nes a
nd H
. FAS
EL13
00 hr
sAIA
A-201
3-251
2Im
prov
emen
t of F
low Co
ntrol
Perfo
rman
ce of
Plasm
a Actu
ator
Using
Wind
-Tunn
el Tes
t Bas
ed
Efficie
nt Glo
bal O
ptimi
zatio
nT.
Matsu
no, K
. Mae
da, G
. Yam
ada,
H. Ka
wazo
e, Tot
tori U
nivers
ity, To
ttori,
Japan
; M. K
anaz
aki, T
okyo
Metr
opolit
an
Unive
rsity,
Hino,
Japan
1330
hrs
AIAA-2
013-2
513
Asse
ssmen
t of A
erod
ynam
ic Ef
fecti
vene
ss fo
r Aer
ospik
e Ap
plica
tion
on H
ypot
hesiz
ed
Liftin
g Bod
y Con
figur
ation
in
Hype
rsonic
Flow
S. Kh
urana
, K. S
uzuk
i, Univ
ersity
of
Toky
o, Ka
shiw
a, Ja
pan
1400
hrs
AIAA-2
013-2
514
Activ
e Sep
arat
ion Co
ntro
l on
a 2D
High
-Lift
Wing
Secti
on
Towa
rds H
igh R
eyno
lds
Numb
er A
pplic
ation
F. Ha
ucke
, W. N
itsch
e, Te
chnic
al Un
iversi
ty of
Berlin
, Berl
in, G
erman
y
1430
hrs
AIAA-2
013-2
515
Vecto
ring o
f a W
all bo
unde
d Pla
nar J
et us
ing Sy
nthe
tic Je
t Ac
tuat
orC.
Wu,
N. Ah
med,
Unive
rsity
of Ne
w So
uth W
ales,
Sydn
ey, A
ustra
lia
1500
hrs
AIAA-2
013-2
517
Nume
rical
Simula
tion
of
Pitch
ing A
irfoil
Per
form
ance
En
hanc
emen
t Usin
g Co-
Flow
Jet F
low Co
ntro
lA.
Lefeb
vre, G
. Zha
, Univ
ersity
of
Miam
i, Cora
l Gab
les, F
L
1530
hrs
AIAA-2
013-2
518
Desig
n of A
ctive
Flow
Contr
ol at
a Dr
oope
d Spo
iler C
onfig
urati
onP. S
cholz,
S. M
ahmo
od, M
. Casp
er,
Techn
ical U
nivers
ity of
Brau
nschw
eig,
Braun
schwe
ig, Ge
rman
y; S.
Wallin
, D.
Skoo
gh, S
wedis
h Defe
nse Re
search
Ag
ency
(FOI)
, Stoc
kholm
, Swe
den;
S. Ad
den,
IBK In
nova
tion,
Nurem
berg,
Ge
rman
y
1600
hrs
AIAA-2
013-2
519
Aero
-Effe
cted C
ontro
l of a
Pit
ching
Airf
oil by
Blee
d Ac
tuat
ionJ.
Kearn
ey, A
. Glez
er, G
eorgi
a Ins
titute
of Te
chno
logy,
Atlan
ta, G
A
1630
hrs
AIAA-2
013-2
516
Wind
Tunn
el an
d Fre
e-Fli
ght
Testi
ng of
Acti
ve Fl
ow Co
ntro
l fo
r Mod
ified
NAC
A 61
3-61
8 Ai
rfoil
J. Dia
nics,
M. B
altha
zar, A
. Gros
s, H.
Fa
sel, U
nivers
ity of
Arizo
na, T
ucso
n, Tu
cson,
AZ
35
Mond
ay, 2
4 Ju
ne 2
013
32-A
PA-8
Aero
dyna
mic a
nd M
ultidi
scipli
nary
Des
ign an
d Opt
imiza
tion
Meth
ods I
Marin
a 3Ch
aired
by: G
. ZHA
and N
. HAR
IHAR
AN, C
REAT
E-AV
1300
hrs
AIAA-2
013-2
520
Syste
matic
Opt
imiza
tion
of th
e Co
oling
Duc
t Sys
tem of
Elec
tric
Vehic
lesA.
Heft,
T. In
dinge
r, N. A
dams
, Te
chnic
al Un
iversi
ty of
Munic
h, Mu
nich,
Germ
any
1330
hrs
AIAA-2
013-2
521
Influ
ence
of P
rope
ller
Aero
dyna
mics
on St
ructu
ral
Wing
Box
Opt
imiza
tion
in In
tegra
ted P
relim
inary
Airc
raft
Desig
nT.
Weiss
, W. H
einze
, P. H
orst,
Tech
nical
Unive
rsity
of Br
auns
chwe
ig,
Brau
nsch
weig,
Germ
any
1400
hrs
AIAA-2
013-2
522
A Hy
brid
Appr
oach
to
Appr
oxim
ate t
he Tr
ade-
off
Surfa
ce in
Engin
eerin
g De
sign
via Sc
alariz
ation
and
Evolu
tiona
ry Co
mput
ation
T. Erf
ani, U
nivers
ity Co
llege
Lond
on,
Lond
on, U
nited
King
dom;
H.
Sama
mi, U
nivers
ity of
Leice
ster,
Leice
ster, U
nited
King
dom;
R. Er
fani,
Manc
heste
r Metr
opoli
tan U
nivers
ity,
Manc
heste
r, Unit
ed Ki
ngdo
m
1430
hrs
AIAA-2
013-2
523
Aero
dyna
mic D
esign
of EA
V Pr
opell
er u
sing a
Mult
i-Lev
el Op
timiza
tion
Meth
odH.
Kwon
, S. C
hoi, S
. Yi, K
orea
Adva
nced
Insti
tute o
f Scie
nce a
nd
Tech
nolog
y, Da
ejeon
, Sou
th Ko
rea;
K. Kim
, Kore
a Aero
spac
e Res
earch
Ins
titute,
Dae
jeon,
South
Korea
1500
hrs
AIAA-2
013-2
524
Aero
dyna
mic D
esign
Op
timiza
tion
of W
ing-sa
ilsY.
Jo, H
. Lee
, S. C
hoi, K
orea
Adva
nced
Insti
tute o
f Scie
nce a
nd
Tech
nolog
y, Da
ejeon
, Sou
th Ko
rea;
J. Kw
on, S
. Ahn
, Sam
sung
, Dae
jeon,
South
Korea
1530
hrs
AIAA-2
013-2
525
Planf
orm
Desig
n fo
r a Fi
ve
Blad
ed Is
olated
Heli
copt
er
Roto
r Usin
g Flui
d-Str
uctu
re
Coup
led CF
D Sim
ulatio
nsM.
Holl
ands
, M. K
essle
r, E. K
raeme
r, Un
iversi
ty of
Stutt
gart,
Stut
tgart,
Ge
rman
y
1600
hrs
AIAA-2
013-2
526
Drag
coef
ficien
t sto
chas
tic
unce
rtaint
y in
aero
dyna
mics
desig
n of
atmo
sphe
ric re
entry
ve
hicle
O. Fr
ayssi
net,
D. B
ardy,
P. Ma
ire,
J. Cla
ude,
Atomi
c Ene
rgy an
d Alt
ernati
ve En
ergies
Comm
ission
, Le
Barp,
Fran
ce
Mond
ay, 2
4 Ju
ne 2
013
33-A
PA-9
/FD-
9Lo
w Sp
eed,
Low
Reyn
olds N
umbe
r Aer
odyn
amics
IMa
rina 4
Chair
ed by
: P. M
ORGA
N, O
hio Ae
rospa
ce In
stitut
e and
L. U
KEILE
Y, Un
iversi
ty of
Florid
a13
00 hr
sAIA
A-201
3-252
7Un
stead
y Effe
cts on
Stat
ionar
y Ai
rfoils
due t
o Uns
teady
Flow
Se
para
tions
at Lo
w Re
ynold
s Nu
mber
sD.
Mate
escu
, A. P
anah
i, C. W
ang,
McGil
l Univ
ersity
, Mon
tréal,
Cana
da
1330
hrs
AIAA-2
013-2
528
A Nu
meric
al Me
thod
to D
etect
Lami
nar S
epar
ation
Bub
bles
over
Airf
oils
P. Ca
talan
o, Ita
lian A
erosp
ace
Rese
arch C
enter
(CIRA
), Ca
pua,
Italy;
R. To
gnac
cini, B
. Mele
, Un
iversi
ty of
Naple
s “Fe
deric
o II”,
Na
ples,
Italy
1400
hrs
AIAA-2
013-2
529
A lat
tice B
oltzm
ann f
rame
work
fo
r ana
lysis
of ‘c
lap an
d fling
’ mo
tion
of fi
nite t
hickn
ess
memb
rane
sN.
Arora
, A. G
upta,
S. S
angh
i, Ind
ian In
stitut
e of T
echn
ology
New
De
lhi, N
ew D
elhi, I
ndia;
H. A
ono,
Japa
n Aero
spac
e Exp
lorati
on Ag
ency
(JA
XA),
Kana
gawa
, Jap
an; W
. Shy
y, Ho
ng Ko
ng U
nivers
ity of
Scie
nce a
nd
Tech
nolog
y, Ho
ng Ko
ng, H
ong K
ong
1430
hrs
AIAA-2
013-2
530
Desig
n of
a 2-
D Fa
iring
for a
Wi
nd Tu
rbine
Towe
rK.
O’Co
nnor,
E. Lo
th, U
nivers
ity
of Vir
ginia,
Charl
ottes
ville,
Ch
arlott
esvil
le, VA
; M. S
elig,
Unive
rsity
of Illi
nois,
Urba
na-
Cham
paign
, Urba
na, I
L
1500
hrs
AIAA-2
013-2
531
A No
vel I
nter
mitte
ncy
Distr
ibutio
n Ba
sed T
rans
ition
Mode
l For
Low-
Re N
umbe
r Ai
rfoils
O. B
as, R
OKET
SAN
Missi
le Ind
ustrie
s, Inc
., An
kara,
Turke
y; S.
Cakm
akcio
glu, U
. Kay
nak,
TOBB
Univ
ersity
of Ec
onom
ics an
d Te
chno
logy,
Anka
ra, Tu
rkey
1530
hrs
AIAA-2
013-2
532
Time-
reso
lved P
IV an
d for
ce
meas
urem
ents
of w
ing
mode
ls wi
th ar
tificia
l sur
face
str
uctu
res
A. W
inzen
, M. K
laas,
W. S
chröe
der,
RWTH
Aach
en U
nivers
ity, A
ache
n, Ge
rman
y
1600
hrs
AIAA-2
013-2
533
Visua
lizat
ion of
Coun
ter-
rota
ting S
tream
wise
Vorti
ces
in a R
ecta
ngula
r Cha
nnel
with
On
e-sid
ed W
avy S
urfa
ceA.
Budim
an, H
. Mits
udha
rmad
i, H.
Low,
S. W
inoto,
Nati
onal
Unive
rsity
of Sin
gapo
re, S
ingap
ore, S
ingap
ore
1630
hrs
AIAA-2
013-2
534
Evalu
ating
the F
low Fi
elds
Arou
nd Lo
w As
pect
Ratio
Fla
t Plat
es in
Wind
Tunn
el Tu
rbule
nce
M. S
ytsma
, Air F
orce R
esea
rch
Labo
ratory
, Egli
n AFB
, FL;
L. Uk
eiley
, Un
iversi
ty of
Florid
a, Ga
inesv
ille,
Gaine
sville
, FL
Mond
ay, 2
4 Ju
ne 2
013
34-A
PA-1
0Un
stead
y Aer
odyn
amics
IEx
ecut
ive Co
nfer
ence
2A
Chair
ed by
: K. V
ANDE
N, U
SAF a
nd K.
ABDO
L-HAM
ID, N
ASA L
angle
y Res
earch
Cente
r13
00 hr
sAIA
A-201
3-253
5Un
stead
y Aer
odyn
amic
Mode
ling o
f Airc
raft
Cont
rol
Surfa
ces b
y Ind
icial
Resp
onse
Me
thod
sM.
Gho
reysh
i, A. J
irase
k, R.
Cumm
ings,
U.S.
Air F
orce A
cade
my,
Color
ado S
pring
s, CO
1330
hrs
AIAA-2
013-2
536
Cohe
rent
Wak
e Stru
cture
s fo
r Tra
nspo
rt Ai
rcraf
t at
Carg
o Aird
rop C
onfig
urat
ions
Inclu
ding P
arac
hutes
E. Ro
osen
boom
, A. S
chröd
er, J.
Ag
ocs,
R. Ge
isler, G
erman
Aeros
pace
Ce
nter (
DLR)
, Gött
ingen
, Germ
any
1400
hrs
AIAA-2
013-2
537
Aero
dyna
mic a
nd A
eroa
cous
tic
Meas
urem
ents
of a
Land
ing
Gear
Torq
ue Li
nkS.
Wind
iate,
X. Zh
ang,
D. An
gland
, Un
iversi
ty of
South
ampto
n, So
utham
pton,
Unite
d King
dom
1430
hrs
AIAA-2
013-2
538
Comp
utatio
nal P
redict
ion
of Pr
essur
e and
Therm
al En
viron
ments
in th
e Flam
e Tre
nch w
ith La
unch
Vehic
lesC.
Brehm
, E. S
ozer,
Scien
ce an
d Tec
hnolo
gy Co
rporat
ion, M
offett
Field
, CA
; S. M
oini-Ye
kta, U
nivers
ity of
Ca
liforni
a, Da
vis, D
avis,
CA; J
. Hou
sman
, C.
Kiris,
M. Ba
rad, N
ASA A
mes R
esearc
h Ce
nter, M
offett
Field
, CA;
B. Vu
, P.
Christ
ophe
r, NAS
A Ken
nedy
Space
Ce
nter, C
ape C
anav
eral, F
L
36
Mond
ay, 2
4 Ju
ne 2
013
35-A
PA-1
1Ap
plied
CFD
IEx
ecut
ive Co
nfer
ence
4Ch
aired
by: J
. DEB
ONIS,
NAS
A Glen
n Res
earch
Cente
r and
A. M
AJAM
AKI,
The A
erosp
ace C
orpora
tion
1300
hrs
AIAA-2
013-2
539
Nume
rical
Simula
tion
of th
e UA
V Nav
igato
r X-2
A. Gir
aldo,
W. B
uitrag
o J. E
scoba
r, Un
iversi
ty of
San B
uena
ventu
ra,
Bogo
ta, Co
lombia
1330
hrs
AIAA-2
013-2
540
URAN
S-Sim
ulatio
ns of
Comb
at
Aircr
aft F
light
Man
oeuv
res
S. H
itzel,
EADS
, Man
ching
, Germ
any
1400
hrs
AIAA-2
013-2
541
Towa
rd Ve
rifica
tion
of U
SM3D
Ex
tensio
ns fo
r Mixe
d Elem
ent
Grids
M. Pa
ndya
, N. F
rink,
NASA
Lang
ley
Rese
arch C
enter
, Ham
pton,
VA;
E. Din
g, An
alytic
al Se
rvice
s and
Ma
terial
s, Inc
., Ha
mpton
, VA;
E. Pa
rlette
, ViGY
AN, I
nc.,
Hamp
ton, V
A
1430
hrs
AIAA-2
013-2
542
Effe
ct of
Tip G
eome
try on
a Ho
verin
g Rot
or in
Gro
und
Effe
ct: A
Comp
utat
ional
Study
T. Ka
lra, V
. Lak
shmi
naray
an, J
. Ba
eder,
Univ
ersity
of M
arylan
d, Co
llege
Park,
Colle
ge Pa
rk, M
D
1500
hrs
AIAA-2
013-2
543
Pres
sure
-bas
ed Co
upled
Nu
meric
al Ap
proa
ch to
the
Prob
lem of
Comp
ressi
ble Fl
ow
thro
ugh
Conv
erge
nt Co
nical
Nozz
lesK.
Kurba
tskii,
A. Le
stari,
ANSY
S, In
c.,
Leba
non,
NH
Mond
ay, 2
4 Ju
ne 2
013
36-A
SE-2
Aircr
aft I
cing C
FD an
d Ice
Adh
esion
Room
515
Chair
ed by
: Z. S
WET
KY, A
ero-In
sturm
ents
Co. a
nd T.
BEN
CIC, N
ASA G
lenn R
esea
rch Ce
nter
1300
hrs
AIAA-2
013-2
544
Discr
ete Su
rface
Evolu
tion
and
Mesh
Def
orma
tion
for A
ircra
ft Ici
ng A
pplic
ation
sD.
Thom
pson
, X. T
ong,
Q. Ar
noldu
s, E.
Collin
s, E.
Luke
, Miss
issipp
i Stat
e Un
iversi
ty, M
ississ
ippi S
tate,
MS;
C. Bid
well,
NASA
Glen
n Res
earch
Ce
nter, C
levela
nd, O
H
1330
hrs
AIAA-2
013-2
545
Impa
ct Ef
ficien
cy P
redit
ions
On Ic
ing Su
rface
s Usin
g the
La
gran
gian
Parce
l Volu
me
Meth
odC.
Triph
ahn,
Unive
rsity
of Illi
nois,
Ur
bana
-Cham
paign
, Urba
na, I
L; E.
Loth,
Univ
ersity
of V
irgini
a, Ch
arlott
esvil
le, Ch
arlott
esvil
le, VA
1400
hrs
AIAA-2
013-2
546
Asse
ssmen
t of I
ce Sh
ape
Roug
hnes
s Usin
g a Se
lf-Or
ganiz
ing M
ap A
ppro
ach
S. M
cClai
n, Ba
ylor U
nivers
ity, W
aco,
TX; R
. Kree
ger, N
ASA G
lenn R
esea
rch
Cente
r, Clev
eland
, OH
1430
hrs
AIAA-2
013-2
547
Evalu
ation
of R
ough
ness
Effe
cts on
Ice A
dhes
ionT.
Strob
l, D. R
aps,
Europ
ean
Aeron
autic
Defe
nce a
nd S
pace
Co
mpan
y, Mu
nich,
Germ
any;
M.
Hornu
ng, B
auha
us Lu
ftfah
rt e.V
., Mu
nich,
Germ
any
1500
hrs
AIAA-2
013-2
548
Deve
lopme
nt an
d App
licatio
n of
Dual-
Lumi
nesce
nce I
magin
g for
Ca
pturin
g Sup
ercoo
led-W
ater
Drop
let un
der I
cing C
ondit
ions
M. Ta
naka
, Kan
agaw
a Inst
itute
of Tec
hnolo
gy, At
sugi, J
apan
; K. M
orita,
Jap
an Ae
rospa
ce Ex
plorat
ion Ag
ency
(JAXA
), Ch
ofu, J
apan
; S. K
imura
, Ka
naga
wa In
stitute
of Te
chnolo
gy,
Atsug
i, Jap
an; H
. Sak
aue,
Japan
Ae
rospa
ce Ex
plorat
ion Ag
ency
(JAXA
), Ch
ofu, J
apan
1530
hrs
AIAA-2
013-2
549
Statio
nary
- and
Dyn
amic-
Icing
Pr
oces
ses o
f Sup
erco
oled-
Water
Dro
plet o
n Ice
phob
ic Co
ating
K. Mo
rita, J
apan
Aeros
pace
Ex
plorat
ion Ag
ency
(JAX
A), C
hofu,
Ja
pan;
M. Ta
naka
, S. K
imura
, Ka
naga
wa In
stitut
e of T
echn
ology
, Ats
ugi, J
apan
; H. S
akau
e, Ja
pan
Aeros
pace
Explo
ration
Agen
cy
(JAXA
), Ch
ofu, J
apan
Mond
ay, 2
4 Ju
ne 2
013
37-A
SE-3
Vorti
ces a
nd Co
ntra
ils in
the A
tmos
pher
ic En
viron
ment
Room
518
Chair
ed by
: J. M
URRA
Y, NA
SA-La
ngley
Rese
arch C
enter
and Z
. ZHE
NG, T
he U
nivers
ity of
Kans
as13
00 hr
sAIA
A-201
3-255
0In
fluen
ce of
Atm
osph
eric
Turb
ulenc
e on
Crow
-Type
In
stabil
ity of
a Vo
rtex
in Gr
ound
Effe
ctZ.
Zhen
g, Un
iversi
ty of
Kans
as,
Lawr
ence
, Law
rence
, KS
1330
hrs
AIAA-2
013-2
551
Nonli
near
Wak
e Vor
tices
of an
Os
cillat
ing A
irfoil
in Su
bson
ic Flo
wsM.
Tsai,
Nati
onal
Form
osa U
nivers
ity,
Yunli
n, Ta
iwan
1400
hrs
AIAA-2
013-2
552
Nume
rical
Simula
tion
of th
e Ai
rcraf
t Wak
e Vor
tex Fl
owfie
ldN.
Ahma
d, NA
SA La
ngley
Rese
arch
Cente
r, Ham
pton,
VA
1430
hrs
AIAA-2
013-2
553
A Pr
obab
ilistic
Ice H
abit
Mode
l fo
r LES
of Co
ntra
ilsA.
Inamd
ar, S
. Lele
, M. J
acob
son,
Stan
ford U
nivers
ity, S
tanfor
d, CA
1500
hrs
AIAA-2
013-2
554
Rese
arch
es of
inter
actio
n of
air
craft
wake
vorti
ces a
nd
cond
ensa
tion
trails
V. De
desh
, A. Z
amya
tin, M
. Grig
orev,
Intern
ation
al Sc
ience
& Te
chno
logy
Cente
r, Zhu
kovs
ky, R
ussia
; S. Z
uev,
Grom
ov Fl
ight R
esea
rch In
stitut
e, Zh
ukov
sky,
Russi
a; A.
Zhela
nniko
v, TsA
GI, Z
huko
vsky
, Rus
sia
1530
hrs
AIAA-2
013-2
555
Metho
dolog
y of e
valua
tion a
nd
pred
iction
of fo
rmati
on an
d ex
isten
ce of
cond
ensa
tion t
rails
and c
onde
nsati
on cir
rus c
louds
du
ring fl
ights
of pa
rticu
lar civ
il jet
aircr
aft an
d it a
ppro
batio
n on
conc
rete fl
ight r
outes
V. De
desh,
Mosc
ow In
stitute
of Ph
ysics
and T
echno
logy,
Zhuk
ovsky
, Russ
ia; A.
Za
myati
n, M.
Grigo
rev, A
. Zhe
lannik
ov,
Intern
ation
al Sc
ience
& Tec
hnolo
gy
Cente
r, Zhu
kovsk
y, Ru
ssia;
A. La
nshin,
A.
Evstig
neev,
Centr
al Ins
titute
of Av
iation
Moto
rs, M
oscow
, Russ
ia
37
Mond
ay, 2
4 Ju
ne 2
013
38-C
FD-8
Nume
rical
Simula
tions
of H
yper
sonic
Flow
s (In
vited
)Na
utilu
s 4Ch
aired
by: R
. CUM
MING
S, U
S Air
Force
Acad
emy
1300
hrs
AIAA-2
013-2
556
Hype
rsonic
Stab
ility a
nd
Trans
ition
Pred
iction
H. Re
ed, T
exas
A&M
Unive
rsity,
Co
llege
Stat
ion, T
X
1330
hrs
Oral
Prese
ntatio
n (Inv
ited)
Simula
tion
of Tr
ansit
ion to
Tu
rbule
nce o
n an
Ellip
tic Co
neG.
Cand
ler, U
nivers
ity of
Minn
esota
, Mi
nnea
polis,
Minn
eapo
lis, M
N
1400
hrs
AIAA-2
013-2
557
Comp
utat
ion of
Hyp
erso
nic
Flows
Usin
g the
Dire
ct Sim
ulatio
n Mo
nte C
arlo
Meth
odI.
Boyd
, Univ
ersity
of M
ichiga
n, An
n Arb
or, An
n Arbo
r, MI
1430
hrs
AIAA-2
013-2
558
Func
tiona
l Equ
ivalen
ce
Acce
ptan
ce Te
sting
of FU
N3D
for E
ntry
, Des
cent
, and
La
nding
App
licat
ions
P. Gn
offo,
W. W
ood,
B. Kl
eb, S
. Alte
r, J.
Padil
la, J.
Whit
e, NA
SA La
ngley
Re
searc
h Cen
ter, H
ampto
n, VA
1500
hrs
AIAA-2
013-2
559
Rece
nt A
dvan
ceme
nts i
n Fu
lly
Impli
cit N
umer
ical M
ethod
s for
Hy
perso
nic R
eacti
ng Fl
ows
B. Ki
rk, N
ASA J
ohns
on S
pace
Cente
r, Ho
uston
, TX;
R. S
togne
r, T. O
liver,
P.
Baum
an, U
nivers
ity of
Texa
s, Au
stin,
Austi
n, TX
1530
hrs
AIAA-2
013-2
560
Nume
rical
rebuil
ding o
f uns
teady
loa
ds on
ARIAN
E5 by
URA
NS an
d LE
S/DE
S/XL
ES ca
lculat
ions a
nd
valid
ation
again
st tim
e accu
rate
PIV m
easu
remen
tsR.
Schw
ane,
ESA,
Noord
wijk,
The
Nethe
rland
s
1600
hrs
AIAA-2
013-2
561
CFD
analy
sis of
radia
tive
heat
load
ing on
hyp
erve
locity
re
-ent
ry ve
hicles
S. Ka
rl, D.
Potte
r, M. L
ambe
rt, K.
Ha
nnem
ann,
Germ
an Ae
rospa
ce
Cente
r (DL
R), G
ötting
en, G
erman
y
Mond
ay, 2
4 Ju
ne 2
013
39-C
FD-9
40 Ye
ars o
f CFD
(Inv
ited)
Naut
ilus 5
Chair
ed by
: M. H
AFEZ
, Univ
ersity
of Ca
liforni
a, Da
vis an
d M. L
IOU,
NAS
A Glen
n Res
earch
Cente
r13
00 hr
sOr
al Pre
senta
tion (
Invite
d)Bo
unda
ry co
nditio
ns an
d mu
ltilev
el me
thod
s for
fluid
me
chan
icsA.
Bous
quet,
India
na U
nivers
ity,
Bloom
ington
, IN;
M. M
arion
, Éc
ole Ce
ntrale
de Ly
on, E
cully,
Fra
nce;
M. Pe
tcu, U
nivers
ity of
Po
itiers,
Futur
osco
pe Ch
asse
neuil
Ce
dex,
Franc
e; R.
Tema
m, In
diana
Un
iversi
ty, B
loomi
ngton
, IN
1330
hrs
AIAA-2
013-2
562
High
orde
r pre
serv
ing re
sidua
l dis
tribu
tion
schem
es fo
r the
lam
inar a
nd tu
rbule
nt N
avier
Sto
kes o
n ar
bitra
ry gr
idsR.
Abgra
ll, Fre
nch N
ation
al Ins
titute
for Re
searc
h in C
ompu
ter S
cienc
e an
d Con
trol (
INRIA
), Bo
rdeau
x, Fra
nce
1400
hrs
AIAA-2
013-2
563
A re
view
of 4
4 ye
ars o
f vo
n Ka
rman
Insti
tute
Comp
utat
ional
Fluid
Dyna
mics
Lectu
re Se
ries
H. D
econ
inck,
von K
ármán
Insti
tute
for Fl
uid D
ynam
ics, R
hode
-Saint
-Ge
nèse
, Belg
ium
1430
hrs
Oral
Prese
ntatio
n (Inv
ited)
Hybr
idize
d Disc
ontin
uous
Ga
lerkin
Meth
ods f
or Fl
uid
Mech
anics
J. Pe
raire,
Mas
sach
usett
s Ins
titute
of Te
chno
logy,
Camb
ridge
, MA
1500
hrs
Oral
Prese
ntatio
n (Inv
ited)
An A
erod
ynam
ic An
alysis
and
Optim
izatio
n Me
thod
ology
Ba
sed o
n a N
ewto
n-Kr
ylov-
Schu
r Algo
rithm
Comb
ined
with
Summ
ation
-by-
Parts
Op
erat
ors
D. Zi
ngg,
Unive
rsity
of To
ronto,
To
ronto,
Cana
da
1530
hrs
AIAA-2
013-2
564
High
-Ord
er Me
thods
for
Comp
utatio
nal F
luid D
ynam
ics:
A Brie
f Rev
iew of
Comp
act
Diffe
rentia
l For
mulat
ion on
Un
struc
tured
Grid
sH.
Huyn
h, NA
SA Gl
enn R
esearc
h Cen
ter,
Cleve
land,
OH; Z
. Wan
g, Un
iversit
y of
Kansa
s, La
wren
ce, La
wren
ce, KS
; P. V
incen
t, Imp
erial
Colleg
e Lon
don,
Lond
on, U
nited
King
dom
1600
hrs
Open
Disc
ussio
n
Mond
ay, 2
4 Ju
ne 2
013
40-C
FD-1
0Hi
gh-O
rder
Meth
ods I
ISe
abre
eze I
Chair
ed by
: A. K
ATZ a
nd H
. NISH
IKAWA
, Nati
onal
Institu
te of
Aeros
pace
1300
hrs
AIAA-2
013-2
565
High
er-O
rder
Finit
e Volu
me
Solut
ion R
econ
struc
tion
on
High
ly An
isotro
pic M
eshe
sA.
Jalal
i, C. O
llivier
Goo
ch, U
nivers
ity
of Br
itish C
olumb
ia, Va
ncou
ver,
Cana
da
1330
hrs
AIAA-2
013-2
566
High
-Ord
er Fl
ux Co
rrecti
on
for V
iscou
s Flow
s on
Arbit
rary
Un
struc
ture
d Grid
sB.
Pinc
ock,
A. Ka
tz, U
tah S
tate
Unive
rsity,
Loga
n, UT
1400
hrs
AIAA-2
013-2
567
A Hi
gh-O
rder
Cent
ral E
NO
Finite
-Volu
me Sc
heme
for
Thre
e-Di
mens
ional
Turb
ulent
Re
activ
e Flow
s on U
nstru
cture
d Me
shM.
Chare
st, C.
Grot
h, Un
iversi
ty of
Toron
to, To
ronto,
Cana
da
1430
hrs
AIAA-2
013-2
568
First,
Seco
nd, a
nd Th
ird O
rder
Fin
ite-V
olume
Sche
mes f
or
Adve
ction
-Diff
usion
H. N
ishika
wa, N
ation
al Ins
titute
of Ae
rospa
ce, H
ampto
n, VA
1500
hrs
AIAA-2
013-2
569
A Ne
w Te
chniq
ue fo
r Fini
te Di
ffere
nce W
ENO
with
Ge
ometr
ic Co
nser
vatio
n La
wT.
Nono
mura,
Insti
tute o
f Spa
ce an
d As
trona
utica
l Scie
nce,
Saga
miha
ra,
Japa
n; Y.
Abe,
Unive
rsity
of To
kyo,
Saga
miha
ra, Ja
pan;
K. Fu
jii, In
stitut
e of
Spac
e and
Astro
nauti
cal S
cienc
e, Sa
gami
hara,
Japa
n
1530
hrs
AIAA-2
013-2
570
High
-Ord
er Co
mpac
t-Sten
cil
Summ
ation
-By-
Parts
Ope
rato
rs fo
r the
Comp
ressi
ble N
avier
-Sto
kes E
quat
ions
D. D
el Re
y Fern
ánde
z, D.
Zing
g, Un
iversi
ty of
Toron
to, To
ronto,
Ca
nada
1600
hrs
AIAA-2
013-2
571
High
-Ord
er Fi
nite-
Eleme
nt
Meth
od fo
r Thr
ee-D
imen
siona
l Tu
rbule
nt N
avier
-Sto
kes
J. Erw
in, L.
Wan
g, W.
Ande
rson,
S.
Kapa
dia, U
nivers
ity of
Tenn
esse
e, Ch
attan
ooga
, Cha
ttano
oga,
TN
38
Mond
ay, 2
4 Ju
ne 2
013
41-C
FD-1
1Nu
meric
al Al
gorit
hms f
or In
viscid
and V
iscou
s Flow
s II
Spina
ker I
Chair
ed by
: A. P
OVITS
KY, T
he U
nivers
ity of
Akron
and X
. ZEN
G, D
uke U
niveri
sity
1300
hrs
AIAA-2
013-2
572
A Hy
brid
Finite
Diff
eren
ce-
Finite
Volum
e App
roac
h an
d Its
App
licat
ions t
o Inv
iscid
Comp
ressi
ble Fl
ows
X. Ze
ng, D
uke U
nivers
ity, D
urham
, NC
1330
hrs
AIAA-2
013-2
573
An ex
tensio
n of
the L
attic
e Bo
ltzma
nn M
ethod
for
simula
ting t
urbu
lent fl
ows
arou
nd ro
tatin
g geo
metri
es of
ar
bitra
ry sh
ape
P. Na
then,
D. G
audli
tz, Te
chnic
al Un
iversi
ty of
Munic
h, Mu
nich,
Germ
any;
M. Kr
ause
, J. K
ratzk
e, Ka
rlsruh
e Ins
titute
of Te
chno
logy,
Karls
ruhe,
Germ
any
1400
hrs
AIAA-2
013-2
574
Vorti
city C
onfin
emen
t App
lied
to Tu
rbule
nt W
ing Ti
p Vor
tices
fo
r Wak
e-int
egra
l Dra
g Pr
edict
ionK.
Pierso
n, A.
Povit
sky,
Unive
rsity
of Ak
ron, A
kron,
OH
1430
hrs
AIAA-2
013-2
575
Selec
tion
of Im
plicit
CFD
Tech
nique
s for
Uns
tructu
red
Grids
and T
urbo
mach
inery
Ap
plica
tions
J. Pu
eblas
, R. C
orral,
Tech
nical
Unive
rsity
of Ma
drid,
Madri
d, Sp
ain;
F. Gis
bert,
ITP,
Madri
d, Sp
ain
1500
hrs
AIAA-2
013-2
576
A Thr
ee-D
imen
siona
l Un
struc
tured
Finit
e Volu
me
Metho
d for
Dro
plet Im
pinge
ment
in Air
craft
Icing
K. Jun
g, Gy
eong
sang N
ation
al Un
iversit
y, Jin
ju, So
uth Ko
rea; S
. Jun
g, Ko
rea Ae
rospa
ce Ind
ustrie
s, Sa
cheon
, So
uth Ko
rea; R
. Myo
ng, G
yeon
gsang
Na
tiona
l Univ
ersity,
Jinju,
South
Korea
; J.
Kim, K
orea A
erospa
ce Ind
ustrie
s, Sa
cheon
, Sou
th Ko
rea
1530
hrs
AIAA-2
013-2
577
Visco
us Fl
ow A
nalys
is an
d De
sign
Optim
izatio
n in
Rock
et Mo
tors
M. Yu
musa
k, RO
KETS
AN M
issile
Ind
ustrie
s, Inc
., An
kara,
Turke
y
1600
hrs
AIAA-2
013-2
578
Multig
rid te
chniq
ue an
d Op
timize
d Sch
warz
meth
od
on bl
ock-
struc
ture
d grid
s with
dis
cont
inuou
s int
erfa
ces
D. Ko
lmog
orov,
Tech
nical
Unive
rsity
of De
nmark
, Lyn
gby,
Denm
ark;
N. S
ørens
en, T
echn
ical U
nivers
ity
of De
nmark
, Ros
kilde
, Den
mark;
W.
She
n, J.
Søren
sen,
Tech
nical
Unive
rsity
of De
nmark
, Lyn
gby,
Denm
ark
1630
hrs
AIAA-2
013-2
579
Ener
gy St
able
High
Ord
er
Finite
Dier
ence
Meth
ods
for H
yper
bolic
Equa
tions
in
Movin
g Coo
rdina
te Sy
stems
S. N
ikkar,
J. N
ordstr
om, L
inköp
ing
Unive
rsity,
Link
öping
, Swe
den
Mond
ay, 2
4 Ju
ne 2
013
42-C
FD-1
2De
sign
Optim
izatio
n Te
chniq
ues I
Marin
a 5Ch
aired
by: D
. ZIN
GG, U
nivers
ity of
Toron
to an
d N. G
AUGE
R, RW
TH Aa
chen
Univ
ersity
1300
hrs
AIAA-2
013-2
580
A Vis
cous
Cont
inuou
s Adjo
int
Appr
oach
for t
he D
esign
of
Rot
ating
Engin
eerin
g Ap
plica
tions
T. Ec
onom
on, F
. Pala
cios,
J. Alo
nso,
Stan
ford U
nivers
ity, S
tanfor
d, CA
1330
hrs
AIAA-2
013-2
581
Autom
atic D
iffere
ntiati
on Ad
joint
of the
Reyn
olds-A
vera
ged
Navie
r-Stok
es Eq
uatio
ns w
ith a
Turb
ulenc
e Mod
elZ.
Lyu, G
. Ken
way,
Unive
rsity o
f Mi
chiga
n, An
n Arbo
r, Ann
Arbo
r, MI; C
. Pa
ige, U
nivers
ity of
Toron
to, To
ronto,
Ca
nada
; J. M
artins
, Univ
ersity
of
Michi
gan,
Ann A
rbor, A
nn Ar
bor, M
I
1400
hrs
AIAA-2
013-2
582
Aero
dyna
mic a
ircra
ft de
sign
for m
ission
perfo
rman
ce by
mu
ltipoin
t opt
imiza
tion
F. Ga
llard,
Airbu
s, To
ulous
e, Fra
nce;
M. M
eaux
, EAD
S, To
ulous
e, Fra
nce;
M. M
ontag
nac,
B. M
oham
madi,
CE
RFAC
S, To
ulous
e, Fra
nce
1430
hrs
AIAA-2
013-2
583
Towa
rd H
igh-Fi
delity
Ae
rody
nami
c Sha
pe
Optim
izatio
n fo
r Nat
ural
Lami
nar F
lowR.
Rash
ad, D
. Zing
g, Un
iversi
ty of
Toron
to, To
ronto,
Cana
da
1500
hrs
AIAA-2
013-2
584
Appli
catio
n of
an ef
ficien
t Ne
wton
-Kry
lov al
gorit
hm
for a
erod
ynam
ic sh
ape
optim
izatio
n ba
sed o
n th
e Re
ynold
s-Ave
rage
d Nav
ier-
Stoke
s equ
ation
sL.
Osus
ky, D
. Zing
g, Un
iversi
ty of
Toron
to, To
ronto,
Cana
da
1530
hrs
AIAA-2
013-2
585
Discr
ete Ad
joint
based
Sens
itivity
An
alysis
for O
ptima
l Flow
Contr
ol of
a 3D
High
-Lift
Confi
gura
tion
A. Ne
mili,
. Emr
e, N.
Gaug
er, RW
TH
Aache
n Univ
ersity,
Aache
n, Ge
rman
y; F. K
ramer,
A. Ca
rnariu
s, Tec
hnica
l Un
iversit
y of B
erlin,
Berlin
, Germ
any;
F. Thie
le, CF
D Soft
ware
GmbH
, Berl
in,
Germ
any
1600
hrs
AIAA-2
013-2
586
RANS
-bas
ed A
erod
ynam
ic Sh
ape O
ptim
izatio
n of
a Bl
ende
d-Wi
ng-B
ody A
ircra
ftZ.
Lyu,
J. Ma
rtins,
Unive
rsity
of Mi
chiga
n, An
n Arbo
r, Ann
Arbo
r, MI
Mond
ay, 2
4 Ju
ne 2
013
43-C
FD-1
3In
terdis
ciplin
ary M
ethod
s II
Seab
reez
e II
Chair
ed by
: J. S
HANG
, Wrig
ht St
ate U
nivers
ity13
00 hr
sAIA
A-201
3-258
7An
effic
ient c
ompu
tatio
nal
appr
oach
to h
yper
sonic
no
nequ
ilibriu
m ra
diatio
n ut
ilizing
Gau
ssian
Qua
drat
ure
and S
pace
Par
tition
J. Sh
ang,
D. An
drien
ko, W
right
State
Un
iversi
ty, D
ayton
, OH;
S. S
urzhik
ov,
Russi
an Ac
adem
y of S
cienc
es,
Mosco
w, Ru
ssia;
G. H
uang
, Wrig
ht St
ate U
nivers
ity, D
ayton
, OH
1330
hrs
AIAA-2
013-2
588
Mode
l Pre
dictiv
e Con
trol
unde
r Cou
pled F
luid-
Struc
ture
Co
nstra
ints U
sing a
Dat
abas
e of
Red
uced
-Ord
er M
odels
on
a Tab
letD.
Amsa
llem,
S. D
eolal
ikar, S
tanfor
d Un
iversi
ty, S
tanfor
d, CA
; F. G
urrola
, Ne
w Me
xico S
tate U
nivers
ity, L
as
Cruce
s, NM
; C. F
arhat,
Stan
ford
Unive
rsity,
Stan
ford,
CA
1400
hrs
AIAA-2
013-2
589
COOL
FluiD
: an o
pen
comp
utatio
nal p
latfor
m for
mult
i-ph
ysics
simula
tion a
nd re
search
A. La
ni, N
. Ville
die, K
. Ben
sassi,
L. Ko
losza
r, M. V
ymaz
al, vo
n Kárm
án
Institu
te for
Fluid
Dyna
mics,
Rhod
e-Sain
t-Ge
nèse,
Belgiu
m; S.
Yalim
, Cath
olic
Unive
rsity o
f Leu
ven,
Leuve
n, Be
lgium;
M.
Pane
si, Un
iversit
y of Il
linois,
Urban
a-Ch
ampa
ign, U
rbana
, IL
1430
hrs
AIAA-2
013-2
590
Flow
arou
nd an
Elas
ticall
y Mo
unted
Slen
der B
ody a
t High
In
ciden
ceS.
Gen
del, O
. Gott
lieb,
D. D
egan
i, Te
chnio
n--Isr
ael In
stitut
e of
Tech
nolog
y, Ha
ifa, I
srael
1500
hrs
AIAA-2
013-2
591
Towa
rd a
CFD/
6 DO
F Cou
pled
Mode
l Enh
ancin
g Pro
jectile
Tra
jecto
ry P
redic
tion
V. Lu
u, Éc
ole N
ation
ale S
upéri
eure
de M
écan
ique e
t d’Aé
rotec
hniqu
e, Fu
turos
cope
, Fran
ce; C
. Grig
non,
DGA,
Bourg
es, F
rance
; F. P
lourde
, Éc
ole N
ation
ale S
upéri
eure
de
Méca
nique
et d’
Aérot
echn
ique,
Futur
osco
pe, F
rance
39
Mond
ay, 2
4 Ju
ne 2
013
44-C
FD-1
4Mu
lti-Ph
ase F
lows
Room
514
Chair
ed by
: E. J
OHNS
EN, U
nivers
ity of
Mich
igan a
nd G
. JAC
OBS,
San
Dieg
o Stat
e Univ
1300
hrs
AIAA-2
013-2
592
Multip
hase
Mod
eling
of W
ater
In
jectio
n on
Flam
e Defl
ecto
rB.
Vu, N
ASA K
enne
dy S
pace
Cente
r, Ca
pe Ca
nave
ral, F
L; N.
Bac
hcha
n, O.
Peroo
mian
, V. A
kdag
, Meta
comp
Te
chno
logies
, Tho
usan
d Oak
s, CA
1330
hrs
AIAA-2
013-2
593
Comp
utatio
n of G
as an
d Mu
ltipha
se Su
perso
nic Je
ts wi
th No
n-Equ
ilibriu
m Pr
ocess
esF. Z
avele
vich,
Keldy
sh Re
search
Cente
r, Mo
scow,
Russi
a; A.
Molch
anov,
Mosc
ow
Aviat
ion In
stitute
, Mosc
ow, R
ussia;
N.
Usha
kov,
Keldy
sh Re
search
Cente
r, Mo
scow,
Russi
a
1400
hrs
AIAA-2
013-2
594
Effic
ient a
nd A
ccura
te Co
mput
ation
s of C
ryog
enic
Cavit
ating
Flow
s aro
und
Turb
opum
p Ind
ucer
H. Ki
m, D
. Min,
C. Ki
m, S
eoul
Natio
nal U
nivers
ity, S
eoul,
Sou
th Ko
rea
1430
hrs
AIAA-2
013-2
595
Disco
ntinu
ous G
alerk
in me
thod
for m
ultifl
uid Eu
ler
equa
tions
M. H
enry
de Fr
ahan
, E. J
ohns
en,
Unive
rsity
of Mi
chiga
n, An
n Arbo
r, An
n Arbo
r, MI
1500
hrs
AIAA-2
013-2
596
Multis
cale
Euler
ian-La
gran
gian
meth
od fo
r par
allel
simula
tion
of at
omiza
tion
induc
ed by
air
-blas
t plan
ar in
jecto
rsA.
Sarth
ou, D
. Zuz
io, J.
Estiv
aleze
s, ON
ERA,
Toulo
use,
Franc
e
1530
hrs
AIAA-2
013-2
597
On th
e mod
elling
of sp
ray/
wall i
mping
emen
t und
er
crossfl
ow co
nditio
nsC.
Rodri
gues
, J. B
arata,
A. S
ilva,
Unive
rsity
of Be
ira In
terior
, Cov
ilha,
Portu
gal
1600
hrs
AIAA-2
013-2
598
Towa
rds a
n ef
ficien
t sim
ulatio
n of
two-
phas
e flow
s with
real
gas e
ffects
and c
avita
tion
P. Co
nged
o, M.
Rodio
, R. A
bgral
l, Fre
nch N
ation
al Ins
titute
for Re
searc
h in
Comp
uter S
cienc
e and
Contr
ol (IN
RIA),
Borde
aux,
Franc
e
Mond
ay, 2
4 Ju
ne 2
013
45-FD
-10
Mixin
g and
Comb
ustio
nEx
ecut
ive Co
nfer
ence
1Ch
aired
by: V
. NAR
AYAN
ASWA
MY, U
nivers
ity of
Texa
s, Au
stin
1300
hrs
AIAA-2
013-2
599
Larg
e Edd
y Sim
ulatio
n of
Sp
ray M
ixing
and C
ombu
stion
wi
th Tw
o-Ph
ase M
ass D
ensit
y Fu
nctio
nA.
Irann
ejad,
F. Ja
beri,
Mich
igan
State
Univ
ersity
, Eas
t Lan
sing,
MI
1330
hrs
AIAA-2
013-2
600
A Nu
meric
al Stu
dy of
Ax
isymm
etric
Comp
ressi
ble
Non-
Isoth
erma
l and
Rea
ctive
Sw
irling
Flow
W. Ta
verne
tti, M
. Hafe
z, Un
iversi
ty of
Califo
rnia,
Davis
, Dav
is, CA
1400
hrs
AIAA-2
013-2
601
Expe
rimen
tal I
nves
tigat
ion of
an
Unc
onfin
ed Sw
irl-S
tabil
ized
Turb
ulent
Pre
mixe
d Flam
eH.
Naw
roth,
K. Mo
riarty
, J. B
euth,
C.
Pasch
ereit,
Tech
nical
Unive
rsity
of Be
rlin, B
erlin,
Germ
any
1430
hrs
AIAA-2
013-2
602
Vorte
x Br
eakd
own
and G
lobal
Mode
s in
Swirl
ing Co
mbus
tor
Flows
with
Axia
l Air
Injec
tion
S. Te
rhaar,
T. Re
ichel,
C. S
chrod
inger,
L.
Ruke
s, K.
Oberl
eithn
er, C.
Pa
schere
it, Te
chnic
al Un
iversi
ty of
Berlin
, Berl
in, G
erman
y
1500
hrs
AIAA-2
013-2
603
Flow
Field
Manip
ulatio
n by
Ax
ial A
ir In
jectio
n to
Ach
ieve
Flash
back
Res
istan
ce an
d its
Impa
ct on
Mixi
ng Q
uality
T. Re
ichel,
S. T
erhaa
r, C. P
asch
ereit,
Tech
nical
Unive
rsity
of Be
rlin, B
erlin,
Ge
rman
y
1530
hrs
AIAA-2
013-2
604
Expe
rimen
tal in
vesti
gatio
n of
fla
shba
ck in
prem
ixed C
H4/
H2-a
ir sw
irl fl
ames
D. Eb
i, N. C
lemen
s, Un
iversi
ty of
Texa
s, Au
stin,
Austi
n, TX
1600
hrs
AIAA-2
013-2
605
Study
of th
e Flam
e Stru
cture
an
d Dyn
amics
Usin
g Non
-int
rusiv
e Com
busti
on D
iagno
stic
Techn
iques
H. Go
hari D
arabk
hani,
J. O
akey,
Cra
nfield
Unive
rsity,
Cranfi
eld, U
nited
Kin
gdom
; Y. Z
hang
, She
ffield
Unive
rsity,
Sheffi
eld, U
nited
King
dom;
A. Ke
shmiri,
Ma
nchest
er Me
tropo
litan U
nivers
ity,
Manch
ester,
Unite
d King
dom
Mond
ay, 2
4 Ju
ne 2
013
46-FD
-11
Celeb
ratin
g 60
Year
s of A
FOSR
: Hyp
erso
nics i
nto t
he 2
1st C
entu
ry -
Rese
arch
Pro
gres
s Sinc
e 200
1 an
d Fut
ure D
irecti
ons i
n Ae
roth
ermo
dyna
mics
Harb
or B
allro
om I
and I
ICh
aired
by: M
. LEW
IS, S
cienc
e & Te
chno
logy P
olicy
Inst/
Inst f
or De
f Ana
lyses
1300
hrs
AIAA-2
013-2
606
The A
FOSR
Hyp
erso
nic
Strat
egy
J. Sc
hmiss
eur, A
ir Forc
e Offic
e of
Scien
tific R
esea
rch, A
rlingto
n, VA
1330
hrs
AIAA-2
013-2
607
Prog
ress
in Sh
ock
Wave
/Bo
unda
ry La
yer I
nter
actio
nsD.
Gait
onde
, Ohio
Stat
e Univ
ersity
, Co
lumbu
s, OH
1400
hrs
AIAA-2
013-2
608
Deve
loping
Mec
hanis
m-Ba
sed
Meth
ods f
or Es
timat
ing
Hype
rsonic
Bou
ndar
y-La
yer
Trans
ition
in Fli
ght:
The R
ole of
Qu
iet Tu
nnels
S. S
chne
ider, P
urdue
Univ
ersity
, Wes
t La
fayett
e, IN
1430
hrs
AIAA-2
013-2
609
Hype
rsonic
Bou
ndar
y-La
yer
Lami
nar-T
urbu
lent T
rans
ition
W. S
aric,
H. Re
ed, R
. Bow
ersox
, Te
xas A
&M U
nivers
ity, C
olleg
e St
ation
, TX
1500
hrs
AIAA-2
013-2
610
Optic
al Di
agno
stics
for H
igh-
Spee
d Flow
sR.
Miles
, Prin
ceton
Univ
ersity
, Pri
nceto
n, NJ
1530
hrs
Oral
Prese
ntatio
n (Inv
ited)
Ener
gy co
nver
sion m
echa
nisms
in
none
quilib
rium
plasm
as an
d hig
h-en
thalp
y flow
sI.
Adam
ovich
, J. R
ich, W
. Lem
pert,
Oh
io St
ate U
nivers
ity, C
olumb
us, O
H
1600
hrs
AIAA-2
013-2
612
Rate-
Depe
nden
t Ene
rgeti
c Pr
oces
ses i
n Hy
perso
nic Fl
ows
G. Ca
ndler
, Univ
ersity
of M
innes
ota,
Minn
eapo
lis, M
innea
polis,
MN
1630
hrs
AIAA-2
013-2
613
Prog
ress a
nd Fu
ture P
rosp
ects
for Pa
rticle
-Bas
ed Si
mulat
ion of
Hy
perso
nic Fl
owT.
Schw
artze
ntrub
er, Un
iversit
y of
Minn
esota,
Minn
eapo
lis, M
innea
polis,
MN
; I. Bo
yd, U
nivers
ity of
Mich
igan,
Ann A
rbor, A
nn Ar
bor, M
I
40
Mond
ay, 2
4 Ju
ne 2
013
47-FD
-12
Boun
dary
-Laye
r Sta
bility
and T
rans
ition:
Gen
eral
IISp
inake
r II
Chair
ed by
: M. K
EGER
ISE, N
ASA-L
angle
y Res
earch
Cente
r and
S. W
OODR
UFF
1300
hrs
AIAA-2
013-2
615
The E
ffect
of W
avep
acke
t Fr
eque
ncy B
andw
idth
on th
e La
mina
r-Tur
bulen
t Tra
nsitio
n Pr
oces
s in
a Blas
ius B
ound
ary
Laye
rK.
Kang
, K. Y
eo, N
ation
al Un
iversi
ty of
Singa
pore,
Sing
apore
, Sing
apore
1330
hrs
AIAA-2
013-2
616
VEST
A to
olkit:
a So
ftwar
e to
Comp
ute T
rans
ition
and
Stabil
ity of
Bou
ndar
y Lay
ers
F. Pin
na, v
on Ká
rmán
Insti
tute f
or Flu
id Dy
nami
cs, Rh
ode-S
aint-G
enès
e, Be
lgium
1400
hrs
AIAA-2
013-2
617
Dire
ct Nu
meric
al Sim
ulatio
n of
Tran
sition
in a
Swep
t Wing
Bo
unda
ry La
yer
L. Du
an, N
ation
al Ins
titute
of Ae
rospa
ce, H
ampto
n, VA
; M.
Chou
dhari
, F. L
i, NAS
A Lan
gley
Rese
arch C
enter
, Ham
pton,
VA; M
. W
u, Na
tiona
l Insti
tute o
f Aero
spac
e, Ha
mpton
, VA
1430
hrs
AIAA-2
013-2
619
On Se
lf-Su
staine
d Flow
-Aco
ustic
Re
sona
nt Int
eracti
ons in
Airfo
il Tra
nsitio
nal B
ound
ary L
ayers
V. Go
lubev,
L. N
guye
n, R.
Mank
badi,
Em
bry-Ri
ddle
Aeron
autica
l Univ
ersity,
Da
ytona
Beach
, FL;
J. Du
dley,
Air Fo
rce
Resea
rch La
borat
ory, E
glin AF
B, FL;
M.
Visba
l, Air F
orce R
esearc
h Lab
orator
y, Wr
ight-P
atters
on AF
B, OH
1500
hrs
AIAA-2
013-2
620
Glob
al sta
bility
Ana
lysis
with
Co
mpre
ssible
CFD
Solve
rF.
Guiho
, Pari
s Ins
titute
of Te
chno
logy,
Paris
, Fran
ce; F
. Aliz
ard,
Natio
nal C
onse
rvator
y of A
rts an
d Cra
fts, P
aris,
Franc
e; J.
Robin
et, Pa
ris
Institu
te of
Tech
nolog
y, Pa
ris, F
rance
1530
hrs
AIAA-2
013-2
621
On th
e two
clas
ses o
f glob
al pr
imar
y mod
al ins
tabil
ity in
lam
inar s
epar
ation
bubb
lesD.
Rodri
guez
, E. G
enna
ro, U
nivers
ity
of Sã
o Pau
lo, S
ão Ca
rlos,
Braz
il; M.
Ju
niper,
Univ
ersity
of Ca
mbrid
ge,
Camb
ridge
, Unit
ed Ki
ngdo
m
1600
hrs
AIAA-2
013-2
614
Dire
ct Nu
meric
al Sim
ulatio
ns
of Co
ntro
l of L
amina
r Se
para
tion
Bubb
les by
Puls
ed
Vorte
x Ge
nera
tor J
ets in
Low
and E
levat
ed Fr
ee-S
tream
Tu
rbule
nce
S. H
osse
inverd
i, H. F
asel,
Univ
ersity
of
Arizo
na, T
ucso
n, Tu
cson,
AZ
1630
hrs
AIAA-2
013-2
618
Influ
ence
of A
dver
se P
ressu
re
Grad
ient o
n th
e Spa
tial
Deve
lopme
nt of
a Wa
vepa
cket
in a F
lat P
late B
ound
ary L
ayer
A. Ha
as, H
. Fas
el, U
nivers
ity of
Ari
zona
, Tuc
son,
Tucso
n, AZ
Mond
ay, 2
4 Ju
ne 2
013
48-FD
-47
Fluid
Struc
ture
Inter
actio
nNa
utilu
s 2Ch
aired
by: S
. GOR
DEYE
V, Un
iversi
ty of
Notre
Dam
e and
D. B
ODON
Y, Un
iversi
ty of
Illino
is at
Urba
na-Ch
ampa
ign13
00 hr
sAIA
A-201
3-319
6Plu
nging
and h
eavin
g airf
oils:
impo
sed f
orwa
rd m
otion
or
self-
prop
ulsion
?S.
Etien
ne, F
. Plan
te, A.
Hay
, D.
Pelle
tier, É
cole
Polyt
echn
ique d
e Mo
ntréa
l, Mon
tréal,
Cana
da; J
. Cori
, Sa
fran G
roup,
Brux
elles
, Belg
ium;
A. Ga
ron, É
cole
Polyt
echn
ique d
e Mo
ntréa
l, Mon
tréal,
Cana
da
1330
hrs
AIAA-2
013-3
197
A Stu
dy on
the A
eroe
lastic
and
Aero
acou
stic E
ffects
of a
Sonic
Un
der-e
xpan
ded J
etS.
Pallu
coni,
J. Cr
afton
, Inn
ovati
ve
Scien
tific S
olutio
ns, I
nc.,
Dayto
n, OH
; H. D
ong,
Wrig
ht St
ate
Unive
rsity,
Day
ton, O
H
1400
hrs
AIAA-2
013-3
198
Expe
rimen
tal in
vesti
gatio
n of
flu
id-str
uctu
re in
terac
tion
in ela
stic v
esse
lsK.
Pielho
p, M.
Klaa
s, W.
Sch
röede
r, RW
TH Aa
chen
Univ
ersity
, Aac
hen,
Germ
any
1430
hrs
AIAA-2
013-3
199
A Mo
nolith
ic Ap
proa
ch fo
r the
Nu
meric
al Sim
ulatio
n of
Fluid
Str
uctu
re In
terac
tion
Prob
lems
M. S
ahin,
A. Ek
en, I
stanb
ul Te
chnic
al Un
iversi
ty, Is
tanbu
l, Turk
ey
1500
hrs
AIAA-2
013-3
200
Dire
ct nu
meric
al sim
ulatio
n of
the a
eroe
lastic
resp
onse
of
a pa
nel u
nder
high
spee
d tu
rbule
nt bo
unda
ry la
yers
C. Os
toich
, D. B
odon
y, P.
Geub
elle,
Unive
rsity
of Illi
nois,
Urba
na-
Cham
paign
, Urba
na, I
L
Mond
ay, 2
4 Ju
ne 2
013
49-G
T-2Gr
ound
Test
Facil
ities I
mpro
veme
nts a
nd Ca
pabil
ities
Naut
ilus 1
Chair
ed by
: D. B
ELTE
R, Th
e Boe
ing Co
mpan
y and
M. W
RENN
, Aero
spac
e Tes
ting A
llianc
e (AT
A)13
00 hr
sAIA
A-201
3-262
2Me
thod
ology
for F
light
Re
levan
t Arc-
Jet T
estin
g of
Flexib
le Th
erma
l Pro
tectio
n Sy
stems
A. Ma
zahe
ri, W.
Bruc
e, N.
Mes
ick,
NASA
Lang
ley Re
searc
h Cen
ter,
Hamp
ton, V
A
1330
hrs
AIAA-2
013-2
623
Hybr
id Wi
ng B
ody A
ircra
ft Ac
ousti
c Tes
t Pre
para
tions
and
Facil
ity U
pgra
des
S. H
eath,
H. H
askin
, M. D
oty, F
. Hu
tches
on, T
. Broo
ks, T
. Spa
lt, S.
Bart
ram, W
. Hum
phrey
s, C.
Luns
ford,
NASA
Lang
ley Re
searc
h Ce
nter, H
ampto
n, VA
; D. H
oad,
L. Be
cker,
D. S
tead,
North
rop G
rumma
n Co
rporat
ion, H
ampto
n, VA
1400
hrs
AIAA-2
013-2
624
Esta
blish
ment
of
Aero
prop
ulsion
Mac
h 3.
6 Te
st fa
cility
for H
igh Sp
eed
Comb
usto
r Res
earch
M. Pu
lumath
i, S. K
umara
samy
, V.
Gana
puram
, V. I
yeng
ar, J.
Ch
enna
kesh
ava,
S. G
agula
, P.
Kuma
r, Nati
onal
Aeros
pace
La
borat
ories
, Ban
galor
e, Ind
ia
1430
hrs
AIAA-2
013-2
625
Uniqu
e Tes
ting C
apab
ilities
of
the N
ASA
Lang
ley Tr
anso
nic
Dyna
mics
Tunn
el, an
Exer
cise
in Ae
roela
stic S
calin
gT.
Ivanc
o, NA
SA La
ngley
Rese
arch
Cente
r, Ham
pton,
VA
41
Mond
ay, 2
4 Ju
ne 2
013
50-P
DL-2
Electr
ic Pr
opuls
ionMa
rina 6
Chair
ed by
: T. M
OELLE
R, Un
iversi
ty of
Tenn
esse
e Spa
ce In
stitut
e and
G. W
ILLIAM
S, O
hio Ae
rospa
ce In
stitut
e13
00 hr
sAIA
A-201
3-262
6Sim
ulatio
ns of
Elec
tron
Heat
ing in
a Ca
pacit
ively
Coup
led R
adio
Freq
uenc
y Mi
cro-Th
ruste
r usin
g Co
mput
ation
al Flu
id Dy
nami
csA.
Greig
, C. C
harle
s, R.
Bosw
ell,
Austr
alian
Nati
onal
Unive
rsity,
Ca
nberr
a, Au
strali
a
1330
hrs
AIAA-2
013-2
627
Mode
ling o
f hyp
erso
nic fl
ow
on a
MPD
thru
ster g
eome
try
using
a PI
SO ba
sed m
ethod
C. Xis
to, J.
Pásco
a, P.
Olive
ira,
Unive
rsity
of Be
ira In
terior
, Cov
ilha,
Portu
gal
1400
hrs
AIAA-2
013-2
628
Char
acter
izatio
n of
a co
axial
EC
R pla
sma t
hrus
terJ.
Jarrig
e, P.
Elias
, D. P
acka
n, F.
Cann
at, O
NERA
, Pala
iseau
, Fran
ce
1430
hrs
AIAA-2
013-2
629
Simula
tions
of El
ectro
spra
y in
a Coll
oid Th
ruste
r with
a Hi
gh
Reso
lution
Thre
e-dim
ensio
nal
Parti
cle-in
-Cell
Mod
elP.
Wang
, A. B
orner,
Z. Li
, D. L
evin,
Pe
nnsy
lvania
Stat
e Univ
ersity
, Un
iversi
ty Pa
rk, PA
1500
hrs
AIAA-2
013-2
630
Impa
ct of
Excit
ation
and R
eacti
on
Proc
esses
on th
e Fiel
d Rev
ersed
Co
nfigu
ratio
n Thr
uster
Effic
iency
R. Bo
swort
h, Un
iversit
y of C
olorad
o, Co
lorad
o Spri
ngs,
Color
ado S
pring
s, CO
; J. B
rackb
ill, ER
C, Inc
., Edw
ards
AFB,
CA; J
. Cam
bier, A
ir Forc
e Rese
arch
Labo
ratory
, Edw
ards A
FB, C
A; S.
Gimels
hein,
N. G
imels
hein,
ERC,
Inc.,
Edwa
rds AF
B, CA
; A. K
etsde
ver,
Unive
rsity o
f Colo
rado,
Color
ado S
pring
s, Co
lorad
o Spri
ngs,
CO
1530
hrs
AIAA-2
013-2
632
Lase
r Plas
ma Fo
rmat
ion in
Ai
r Usin
g Dua
l Puls
e Pre
-Io
nizat
ionC.
Dumi
trach
e, Co
lorad
o Stat
e Un
iversi
ty, Fo
rt Co
llins,
CO; M
. Sh
neide
r, Prin
ceton
Univ
ersity
, Pri
nceto
n, NJ
; A. Y
alin,
Color
ado
State
Univ
ersity
, Fort
Collin
s, CO
Mond
ay, 2
4 Ju
ne 2
013
51-TP
-3Ab
lation
IEx
ecut
ive Co
nfer
ence
3B
Chair
ed by
: N. D
OUGH
ERTY
, ERC
Inco
rporat
ed an
d D. P
YTEL
, Loc
khee
d Mart
in Sp
ace S
ystem
s13
00 hr
sAIA
A-201
3-263
3Im
plicit
Coup
ling f
or
Simula
tion
of Ch
arrin
g Car
bon
Ablat
ors
Y. Ch
en, N
ASA A
mes R
esea
rch
Cente
r, Moff
ett Fi
eld, C
A; T.
Gokc
en,
ERC,
Inc.,
Moffe
tt Fie
ld, CA
1330
hrs
AIAA-2
013-2
634
Coup
led Fl
ow Fi
eld Si
mulat
ions
of Ch
arrin
g Abla
tors
with
No
nequ
ilibriu
m Su
rface
Ch
emist
ryH.
Alka
ndry,
I. B
oyd,
Unive
rsity
of Mi
chiga
n, An
n Arbo
r, Ann
Arbo
r, MI;
A. Ma
rtin, U
nivers
ity of
Kentu
cky,
Lexin
gton,
KY
1400
hrs
AIAA-2
013-2
635
Multi-
dimen
siona
l mod
eling
of
char
ring a
blato
rsH.
Wen
g, A.
Martin
, Univ
ersity
of
Kentu
cky,
Lexin
gton,
Lexin
gton,
KY
1430
hrs
AIAA-2
013-2
636
Volum
e ave
rage
d mod
eling
of
the o
xidat
ion of
poro
us ca
rbon
fib
er m
ater
ialA.
Martin
, Univ
ersity
of Ke
ntuck
y, Le
xingto
n, Le
xingto
n, KY
Mond
ay, 2
4 Ju
ne 2
013
52-TP
-4He
at Tr
ansfe
r I -
Cond
uctio
n, Co
nvec
tion,
Rad
iation
, and
Pha
se Ch
ange
Exec
utive
Conf
eren
ce 3
ACh
aired
by: D
. KUN
TZ, S
andia
Nati
onal
Labo
ratori
es an
d G. S
CHNE
IDER
, Univ
ersity
of W
aterlo
o13
00 hr
sAIA
A-201
3-263
7Ap
plica
tion
of So
lution
Str
uctu
re Th
eore
ms fo
r As
ymme
tric H
eatin
g in
Thin
Films
T. La
m, E.
Fong
, The
Aeros
pace
Co
rporat
ion, E
l Seg
undo
, CA
1330
hrs
AIAA-2
013-2
638
Chao
tic N
atur
al Co
nvec
tion
in a T
oroid
al Th
ermo
syph
on w
ith
Heat
Flux
Bou
ndar
iesW.
Louis
os, D
. Hitt,
C. D
anfor
th,
Unive
rsity
of Ve
rmon
t, Bu
rlingto
n, Bu
rlingto
n, VT
1400
hrs
AIAA-2
013-2
639
TALIF
-Inve
stiga
tion
of a
CO2
Indu
ctive
ly Co
upled
Plas
ma
Relev
ant f
or M
ars E
ntry
T. Ma
rynow
ski, S
. Loh
le, S
. Fa
soula
s, Un
iversi
ty of
Stutt
gart,
St
uttga
rt, G
erman
y
1430
hrs
AIAA-2
013-2
640
Theo
retic
al sta
bility
analy
sis
for i
nver
se h
eat c
ondu
ction
pr
oblem
s usin
g the
cond
ition
numb
erU.
Fuch
s, S.
Loeh
le, S
. Fas
oulas
, Un
iversi
ty of
Stutt
gart,
Stut
tgart,
Ge
rman
y
1500
hrs
AIAA-2
013-2
641
Ther
mal S
prea
ding R
esist
ance
in
Comp
ound
Orth
otro
pic
Circu
lar D
isks a
nd R
ecta
ngula
r Ch
anne
ls wi
th In
terfa
cial
Resis
tanc
eY.
Muzy
chka
, Mem
orial
Unive
rsity
of Ne
wfou
ndlan
d, St
. Joh
n’s, C
anad
a
1530
hrs
AIAA-2
013-2
642
Nume
rical
pred
iction
of
conv
ective
and r
adiat
ive he
ating
of
Scram
jet co
mbus
tion c
hamb
er
with
hydr
ocar
bon f
uels
S. Su
rzhiko
v, Ru
ssian
Acad
emy o
f Sc
iences
, Mosc
ow, R
ussia;
J. Sh
ang,
Wrigh
t Stat
e Univ
ersity,
Dayto
n, OH
; R.
Rivir,
Air Fo
rce Re
search
Labo
ratory
, Wr
ight-P
atters
on AF
B, OH
42
Mond
ay, 2
4 Ju
ne 2
013
53-TP
-5Ae
roth
ermo
dyna
mics
IEx
ecut
ive Co
nfer
ence
2B
Chair
ed by
: J. L
EE, T
he Ae
rospa
ce Co
rporat
ion13
00 hr
sAIA
A-201
3-264
3Ne
ar-S
urfa
ce N
itric
Oxide
Co
ncen
tratio
n Me
asur
emen
t in
the L
ENS-
XX Ex
pans
ion Tu
nnel
Facil
ityJ.
Weisb
erger,
M. M
acLe
an, R
. Pa
rker, P
. Des
Jardi
n, Un
iversi
ty at
Buffa
lo, B
uffalo
, NY
1330
hrs
AIAA-2
013-2
644
Thro
ugh
Surfa
ce an
d Acro
ss Su
rface
Vacu
um U
ltrav
iolet
Spec
tral M
easu
reme
nts i
n an
Ex
pans
ion Tu
beU.
She
ikh, U
nivers
ity of
Que
ensla
nd,
Brisb
ane,
Austr
alia;
C. La
ux, É
cole
Centr
ale de
Paris
, Pari
s, Fra
nce;
R. Mo
rgan,
T. Mc
intyre
, Univ
ersity
of
Quee
nslan
d, Br
isban
e, Au
strali
a
1400
hrs
AIAA-2
013-2
645
Pred
iction
s of C
onve
ctive
He
at Tr
ansfe
r Rat
es u
sing
a Car
tesian
Grid
Solve
r for
Hy
perso
nic Fl
ows
S. S
ekha
r, NAS
A Ame
s Res
earch
Ce
nter, M
offett
Field
, CA;
S. Ru
ffin,
Georg
ia Ins
titute
of Te
chno
logy,
Atlan
ta, G
A
1430
hrs
AIAA-2
013-2
646
Manu
factu
red S
olutio
ns fo
r Ve
rifica
tion
of a
Coup
led Fl
ow
and M
ater
ial R
espo
nse C
ode
J. W
ieben
ga, I
. Boy
d, Un
iversi
ty of
Mich
igan,
Ann A
rbor, A
nn Ar
bor, M
I
1500
hrs
AIAA-2
013-2
647
Vacu
um U
ltrav
iolet
and
Ultra
violet
Emiss
ion
Spec
trosco
py M
easu
reme
nts
for T
itan
and M
ars
Atmo
sphe
ric En
try Co
nditio
nsH.
Porat
, U. S
heikh
, R. M
organ
, T.
Mcint
yre, U
nivers
ity of
Que
ensla
nd,
Brisb
ane,
Austr
alia
Mond
ay, 2
4 Ju
ne 2
013
54-LE
C-1
1730
- 18
30 h
rsFlu
id Dy
nami
cs Aw
ard L
ectu
reHa
rbor
Ball
room
I an
d II
Dona
ld O.
Roc
kwell
Lehig
h Univ
ersity
Tues
day
Tues
day,
25 Ju
ne 2
013
55-N
B-2
0700
- 08
00 h
rsTu
esda
y Mor
ning N
etwor
king B
reak
fast
Naut
ilus a
nd H
arbo
r Isl
and F
oyer
s
Tues
day,
25 Ju
ne 2
013
56-S
B-3
0730
- 08
00 h
rsTu
esda
y Mor
ning S
peak
ers’
Briefi
ngSe
ssion
Roo
ms
Tues
day,
25 Ju
ne 2
013
57-A
PA-1
2Ae
rody
nami
c and
Mult
idisci
plina
ry D
esign
and O
ptim
izatio
n Me
thod
s II
Marin
a 2Ch
aired
by: A
. ARS
LAN
and J
. GUG
LIELM
O, B
oeing
Defe
nse,
Spac
e & S
ecuri
ty08
00 hr
sAIA
A-201
3-264
8Co
opera
tion a
nd Co
mpeti
tion
Strate
gies in
Mult
i-obje
ctive
Sh
ape O
ptimi
zatio
n - Ap
plica
tion
to Lo
w-bo
om/L
ow-dr
ag
Supe
rsonic
Busin
ess Je
tA.
Mine
lli, I. S
alah e
l Din,
G. Ca
rrier,
ONER
A, Me
udon
, Fran
ce; A.
Zerbi
nati,
J. De
sideri
, Fren
ch Na
tiona
l Instit
ute
for Re
search
in Co
mpute
r Scie
nce an
d Co
ntrol
(INRIA
), So
phia
Antip
olis, F
rance
0830
hrs
AIAA-2
013-2
649
An A
djoint
-Bas
ed A
erod
ynam
ic Sh
ape O
ptim
izatio
n Me
thod
ology
for F
airing
Sy
stems
M. Co
lonno
, F. P
alacio
s, T.
Econ
omon
, A. L
onka
r, J. A
lonso
, St
anfor
d Univ
ersity
, Stan
ford,
CA
0900
hrs
AIAA-2
013-2
650
Imple
ment
ing A
utom
atic-
Wake
Bod
y Int
erse
ction
s for
Fu
ll Airc
raft
Cong
urat
ions i
n Di
richle
t Pan
el Me
thod
sD.
Willi
s, Un
iversi
ty of
Massa
chus
etts,
Lowe
ll, Lo
well,
MA
0930
hrs
AIAA-2
013-2
651
Optim
ized p
relim
inary
desig
n of
comp
act a
xial co
mpres
sors:
A
comp
ariso
n of t
wo de
sign t
ools
S. Tei
chel, L
eibniz
Unive
rsity o
f Ha
nnov
er, Ha
nnov
er, Ge
rman
y; T.
Verst
raete,
von K
ármán
Instit
ute fo
r Flu
id Dy
nami
cs, Rh
ode-S
aint-G
enèse
, Be
lgium;
J. Se
ume,
Leibn
iz Un
iversit
y of
Hann
over,
Hann
over,
Germ
any
1000
hrs
AIAA-2
013-2
652
Sens
itivity
-Bas
ed Se
quen
tial
Samp
ling o
f Cok
riging
Re
spon
se Su
rface
s for
Ae
rody
nami
c Dat
aA.
Paul-
Dubo
is-Tain
e, S.
Nad
arajah
, Mc
Gill U
nivers
ity, M
ontré
al, Ca
nada
1030
hrs
AIAA-2
013-2
653
Mitig
ation
of A
dver
se Ef
fects
Ca
used
by Sh
ock
Wave
Bo
unda
ry La
yer I
nter
actio
ns
thro
ugh
Optim
al Wa
ll Sha
ping
M. Li
ou, N
ASA G
lenn R
esea
rch
Cente
r, Clev
eland
, OH;
B. L
ee,
Unive
rsity
of Ca
liforni
a, Sa
nta
Barba
ra, S
anta
Barba
ra, CA
43
Tues
day,
25 Ju
ne 2
013
58-A
PA-1
3Ai
rfoil/
Wing
/Con
figur
ation
Aer
odyn
amics
IMa
rina 3
Chair
ed by
: A. M
CCOM
AS, A
nalyt
ical M
ethod
s Inc
and M
. POS
T, US
AF Ac
adem
y08
00 hr
sAIA
A-201
3-265
4En
velop
e Pro
tectio
n for
Co
ntami
nant-
Induc
ed Ad
verse
Ae
rody
nami
cs on
a Wi
ng
Using
Flap
Hing
e Mom
ent
Meas
urem
ents
P. Anse
ll, Un
iversit
y of Il
linois,
Urban
a-Ch
ampa
ign, U
rbana
, IL; M
. Kerh
o, Ro
lling H
ills Re
search
Corpo
ration
, El
Segu
ndo,
CA; M
. Brag
g, Un
iversit
y of
Illinois
, Urba
na-Ch
ampa
ign, U
rbana
, IL
0830
hrs
AIAA-2
013-2
655
Aero
dyna
mic C
hara
cteris
tics
of a
Micro
Air
Vehic
le an
d the
In
fluen
ce of
Pro
pelle
r Loc
ation
J. Ah
n, D.
Lee,
Sejon
g Univ
ersity
, Se
oul, S
outh
Korea
0900
hrs
AIAA-2
013-2
656
Trailin
g Vor
tex St
reng
th
Atten
uatio
n via
Chipp
ed
Wing
tip Sh
apes
J. Jin
, K. Y
ee, S
. Oh,
Pusa
n Nati
onal
Unive
rsity,
Bus
an, S
outh
Korea
0930
hrs
AIAA-2
013-2
657
Resp
onse
Surfa
ce A
nalys
is of
Tra
pped
-Vor
tex A
ugme
nted
Ai
rfoils
J. Ja
nus,
A. Zo
pe, M
ississ
ippi S
tate
Unive
rsity,
Star
kville
, MS
1000
hrs
AIAA-2
013-2
658
Comp
utat
ional
Study
of th
e Sta
bility
Der
ivativ
es fo
r the
Sta
ndar
d Dyn
amic
Mode
lH.
Lee,
B. Ki
m, S
. Lee
, Inh
a Un
iversi
ty, In
cheo
n, So
uth Ko
rea
1030
hrs
AIAA-2
013-2
659
Lift a
nd D
rag M
easu
reme
nts
of Ta
ndem
, Sym
metri
c Airf
oils
J. Ka
tz, S
an D
iego S
tate U
nivers
ity,
San D
iego,
CA
Tues
day,
25 Ju
ne 2
013
59-A
PA-1
4So
nic B
oom
Mitig
ation
and R
ecen
t Adv
ance
s in
Hype
rsonic
s Veh
icle A
ero
Marin
a 4Ch
aired
by: G
. ZHA
and A
. JON
ES, U
nivers
ity of
Mary
land
0800
hrs
AIAA-2
013-2
660
Using
CFD
Surfa
ce So
lution
s to
Shap
e Son
ic Bo
om Si
gnat
ures
Pr
opag
ated
from
Off-
Body
Pr
essu
reI.
Orda
z, W.
Li, N
ASA L
angle
y Re
searc
h Cen
ter, H
ampto
n, VA
0830
hrs
AIAA-2
013-2
661
Near
Field
Pre
ssure
Me
asur
emen
t aro
und T
hree
Di
mens
ional
Free
Fligh
t Mo
dels
A. To
yoda
, T. I
maizu
mi, A
. Sas
oh,
Nago
ya U
nivers
ity, N
agoy
a, Ja
pan
0900
hrs
AIAA-2
013-2
662
Long
Pen
etrat
ion M
ode
Coun
terflo
wing
Jets
for S
uper
sonic
Slen
der
Confi
gura
tions
— A
Nu
meric
al Stu
dyB.
Venk
atach
ari, G
. Che
ng,
Unive
rsity
of Ala
bama
, Birm
ingha
m,
Birmi
ngha
m, AL
; C. C
hang
, NAS
A La
ngley
Rese
arch C
enter
, Ham
pton,
VA; B
. Zich
ettell
o, Co
oper
Union
for
the Ad
vanc
emen
t of S
cienc
e and
Art,
New
York,
NY;
D. B
ilyeu
, Ohio
Stat
e Un
iversi
ty, Co
lumbu
s, OH
0930
hrs
AIAA-2
013-2
663
Appli
catio
n of
Adjo
int
Meth
odolo
gy to
Supe
rsonic
Ai
rcraf
t Des
ign U
sing R
ever
sed
Equiv
alent
Are
asS.
Ralla
bhan
di, N
ation
al Ins
titute
of Ae
rospa
ce, H
ampto
n, VA
1000
hrs
AIAA-2
013-2
664
Evolu
tion
of A
erod
ynam
ic Sh
ape f
or a
Conc
ept o
f Au
tono
mus R
e-En
try Ve
hicle
F. Pe
trosin
o, M.
De S
tefan
o Fum
o, G.
Pe
zzell
a, Ita
lian A
erosp
ace R
esea
rch
Cente
r (CIR
A), C
apua
, Ital
y
1030
hrs
AIAA-2
013-2
665
Strea
mline
Trac
ing Te
chniq
ue
Base
d Des
ign of
Ellip
tical-
to-R
ecta
ngula
r Tra
nsitio
ning
Hype
rsonic
Inlet
M. Ro
sli, M
. Tak
ahas
hi, T.
Sato
, Wa
seda
Univ
ersity
, Shin
juku,
Japa
n; T.
Kojim
a, H.
Tagu
chi, J
apan
Ae
rospa
ce Ex
plorat
ion Ag
ency
(JA
XA),
Chofu
, Jap
an; Y
. Maru
, Ja
pan A
erosp
ace E
xplor
ation
Agen
cy
(JAXA
), Sa
gami
hara,
Japa
n
Tues
day,
25 Ju
ne 2
013
60-A
PA-1
5/FD
-14
Bio-
Insp
ired A
erod
ynam
ics I
Exec
utive
Conf
eren
ce 2
ACh
aired
by: H
. HU,
Iowa
Stat
e Univ
ersity
and M
. PLE
SNIAK
, Geo
rge W
ashin
gton U
nivers
ity08
00 hr
sAIA
A-201
3-266
6Ge
nera
ting L
EVs o
n Ene
rgeti
cally
Op
timal,
Flap
ping W
ing D
esign
s by
Mod
ulatin
g Lea
ding E
dge
Angle
D. Wi
llis, U
nivers
ity of
Mass
achuse
tts,
Lowe
ll, Lo
well,
MA; P.
Perss
on,
Unive
rsity o
f Calif
ornia,
Berke
ley,
Berke
ley, C
A
0830
hrs
AIAA-2
013-2
667
The E
ffect
of R
otat
ion on
the
Span
wise
Tran
spor
t of V
ortic
ity
in th
e Abs
ence
of Ti
p Effe
ctsJ.
Wong
, D. R
ival, U
nivers
ity of
Ca
lgary,
Calga
ry, Ca
nada
0900
hrs
AIAA-2
013-2
668
Thre
e-dim
ensio
nal U
nstea
dy
Aero
dyna
mic C
hara
cteris
tics o
f Wi
ng-b
ody-
vorte
x In
terac
tions
in
Inse
cts’ F
lappin
g Flig
htK.
Lee,
C. Kim
, Seo
ul Na
tiona
l Un
iversi
ty, S
eoul,
Sou
th Ko
rea
0930
hrs
AIAA-2
013-2
669
Low
Reyn
olds’
Numb
er
Appli
catio
n of
Feat
her I
nspir
ed
Passi
ve H
igh Li
ft De
vice o
n Fin
ite W
ingC.
Wang
, J. S
chlut
er, N
anya
ng
Tech
nolog
ical U
nivers
ity, S
ingap
ore,
Singa
pore
1000
hrs
AIAA-2
013-2
670
Nume
rical
simula
tion
of
oscil
lating
-wing
base
d ene
rgy
harv
est m
echa
nism
using
the
high-
orde
r spe
ctral
diffe
renc
e me
thod
M. Yu
, Z. W
ang,
Unive
rsity
of Ka
nsas
, Law
rence
, Law
rence
, KS
44
Tues
day,
25 Ju
ne 2
013
61-A
PA-1
6Ici
ng or
Rou
ghne
ss Ef
fects
on Ve
hicle
Aero
dyna
mics
Exec
utive
Conf
eren
ce 4
Chair
ed by
: G. J
ONES
, NAS
A-Lan
gley R
esea
rch Ce
nter a
nd C.
SHE
NG, U
nivers
ity of
Toled
o08
00 hr
sAIA
A-201
3-267
1Va
lidat
ion an
d Ver
ifica
tion
of
Multi-
Steps
Icing
Calcu
lation
Us
ing CA
NICE
2D-N
S Cod
eK.
Hasa
nzad
eh La
shka
jani, E
. La
urend
eau,
I. Pa
rasch
ivoiu,
Éc
ole Po
lytec
hniqu
e de M
ontré
al,
Montr
éal, C
anad
a
0830
hrs
AIAA-2
013-2
672
Impr
oved
Finit
e Volu
me
Drop
let Tr
ajecto
ries f
or Ic
ing
Simula
tion
T. Re
ndall
, C. A
llen,
Unive
rsity
of Br
istol,
Bris
tol, U
nited
King
dom
0900
hrs
AIAA-2
013-2
673
Char
acter
izatio
n of I
ce-In
duce
d Lo
w-Fr
eque
ncy F
lowfie
ld Os
cillat
ions a
nd th
eir Ef
fect
on
Airfo
il Per
form
ance
P. An
sell,
M. B
ragg,
Unive
rsity
of Illi
nois,
Urba
na-Ch
ampa
ign,
Urba
na, I
L
Tues
day,
25 Ju
ne 2
013
62-A
SE-4
Ice Cr
ysta
l Icin
gRo
om 5
15Ch
aired
by: K
. VEN
KATA
RAMA
NI an
d M. O
LIVER
, NAS
A Glen
n Res
earch
Cente
r08
00 hr
sAIA
A-201
3-267
4HA
IC - H
igh A
ltitud
e Ice
Cr
ysta
lsF.
Dezit
ter, A
. Gran
din, A
irbus
, To
ulous
e, Fra
nce;
J. Br
engu
ier,
Meteo
Fran
ce, T
oulou
se, F
rance
; F.
Hervy
, DGA
, Sac
lay, F
rance
; H.
Schla
ger, G
erman
Aeros
pace
Cente
r (D
LR),
Wessl
ing, G
erman
y; P.
Villed
ieu, O
NERA
, Tou
louse
, Fran
ce;
G. Za
laman
sky,
Dassa
ult G
roup,
Paris
, Fran
ce
0830
hrs
AIAA-2
013-2
675
Prep
arat
ion fo
r Sca
ling S
tudie
s of
Ice-
Crys
tal I
cing a
t the
NRC
Re
sear
ch A
ltitud
e Tes
t Fac
ility
P. St
ruk, T
. Ben
cic, N
ASA G
lenn
Rese
arch C
enter
, Clev
eland
, OH;
J.
Tsao,
Ohio
Aeros
pace
Insti
tute,
Cleve
land,
OH; D
. Fule
ki, D
. Kn
ezev
ici, N
ation
al Re
searc
h Cou
ncil
Cana
da, O
ttawa
, Can
ada
0900
hrs
AIAA-2
013-2
676
Parti
cle Si
ze Ef
fects
on Ic
e Cr
ysta
l Accr
etion
- Pa
rt II
D. Kn
ezev
ici, D
. Fule
ki, T.
Currie
, J.
MaCle
od, N
ation
al Re
searc
h Cou
ncil
Cana
da, O
ttawa
, Can
ada
0930
hrs
AIAA-2
013-2
677
Altit
ude S
calin
g of I
ce Cr
ysta
l Ac
cretio
nT.
Currie
, D. F
uleki,
D. K
neze
vici, J
. Ma
Cleod
, Nati
onal
Rese
arch C
ounc
il Ca
nada
, Otta
wa, C
anad
a
1000
hrs
AIAA-2
013-2
678
Adva
nced
Opti
cal D
iagno
stics
for
Ice Cr
ystal
Clou
d Mea
surem
ents
in the
NAS
A Glen
n Pro
pulsio
n Sy
stems
Labo
rator
yT.
Benci
c, A.
Faga
n, J.
Van Z
ante,
NAS
A Gle
nn Re
search
Cente
r, Clev
eland
, OH
; J. K
irkeg
aard,
Jacob
s, Cle
velan
d, OH
; D. R
ohler,
A. M
aniye
dath,
Plex
ar As
sociat
es, In
c., Sh
aker
Heigh
ts, O
H; S.
Izen,
Case
Weste
rn Re
serve
Unive
rsity,
Cleve
land,
OH
1030
hrs
AIAA-2
013-2
679
Mode
ling C
omme
rcial
Turb
ofan
En
gine I
cing R
isk w
ith Ic
e Cr
ysta
l Ing
estio
nJ.
Veres
, P. J
orgen
son,
NASA
Glen
n Re
searc
h Cen
ter, C
levela
nd, O
H
Tues
day,
25 Ju
ne 2
013
63-A
SE-5
Mode
ling S
pace
craft
Envr
ionme
ntal
Inter
actio
ns w
ith Sp
ace P
lasma
Room
518
Chair
ed by
: N. G
REEN
, Jet
Propu
lsion L
abora
tory
0800
hrs
AIAA-2
013-2
680
Deta
iled M
odeli
ng an
d An
alysis
of Sp
acec
raft
Plume
/Io
nosp
here
Inter
actio
ns in
Low
Earth
Orb
itK.
Step
hani,
I. B
oyd,
Unive
rsity
of Mi
chiga
n, An
n Arbo
r, Ann
Arbo
r, MI
0830
hrs
AIAA-2
013-2
681
Char
acter
izatio
n of
an A
tomi
c Ox
ygen
Plas
ma So
urce
for
Grou
nd-B
ased
Simu
lation
of
the L
EO N
eutra
l Env
ironm
ent
C. Ma
ldona
do, A
. Kets
deve
r, Un
iversi
ty of
Color
ado,
Color
ado
Sprin
gs, C
olorad
o Spri
ngs,
CO; L
. Ra
nd, K
. Xie,
C. Fa
rnell,
J. W
illiam
s, Co
lorad
o Stat
e Univ
ersity
, Fort
Co
llins,
CO
0900
hrs
AIAA-2
013-2
682
Prop
agat
ion of
Surfa
ce-to
-LEO
Vorte
x Ri
ngs F
or O
rbita
l Deb
ris
Mana
geme
ntM.
Noy
es, U
nivers
ity of
Roch
ester
, Ro
ches
ter, N
Y
0930
hrs
AIAA-2
013-2
683
Unce
rtaint
ies in
Satel
lite D
rag
Asso
ciated
with
Varia
tions
in
Atmo
sphe
ric Co
nditio
nsE.
Titov
, Dyn
amics
Rese
arch
Corpo
ration
, Wrig
ht-Pa
tterso
n AFB
, OH
; J. B
urt, U
nivers
al Te
chno
logy
Corpo
ration
, Wrig
ht-Pa
tterso
n AFB
, OH
; E. J
osyu
la, Ai
r Forc
e Res
earch
La
borat
ory, W
right-
Patte
rson A
FB,
OH; E
. Sutt
on, C
. Lin,
Air F
orce
Rese
arch L
abora
tory,
Kirtla
nd
AFB,
NM
1000
hrs
AIAA-2
013-2
684
Deve
lopme
nt of
Samp
le Ca
pture
Sy
stem
for M
ars A
ero-fl
yby
Samp
le Co
llecti
on M
ission
T. Oz
awa,
T. Su
zuki,
Japa
n Aero
space
Ex
plorat
ion Ag
ency
(JAXA
), Ch
ofu,
Japan
; K. K
urosaw
a, Ch
iba In
stitute
of
Techn
ology,
Nara
shio,
Japan
; Y.
Hatak
eyam
a, Nih
on Un
iversit
y, Tok
yo,
Japan
; K. O
kuda
ira, U
nivers
ity of
Aizu
, Aiz
u-Wak
amats
u, Jap
an; T
. Miko
uchi,
Unive
rsity o
f Tok
yo, T
okyo
, Jap
an; H
. Tak
ayan
agi, K
. Fujit
a, Jap
an Ae
rospa
ce
Explo
ration
Agen
cy (JA
XA),
Chofu
, Jap
an
45
Tues
day,
25 Ju
ne 2
013
64-C
FD-1
5Hi
gh-O
rder
Meth
ods I
IINa
utilu
s 5Ch
aired
by: K
. FID
KOW
SKI,
Unive
rsity
of Mi
chiga
n and
Z. W
ANG,
Univ
ersity
of Ka
nsas
0800
hrs
AIAA-2
013-2
685
Perfo
rman
ce tu
ning o
f Ne
wton
-GMR
ES m
ethod
s fo
r disc
ontin
uous
Gale
rkin
discre
tizat
ions o
f the
Nav
ier-
Stoke
s equ
ation
sM.
Zahr,
Stan
ford U
nivers
ity,
Stan
ford,
CA; P
. Pers
son,
Unive
rsity
of Ca
liforni
a, Be
rkeley
, Berk
eley,
CA
0830
hrs
AIAA-2
013-2
686
Pseu
do-tr
ansie
nt Co
ntinu
ation
, So
lution
Upd
ate M
ethod
s, an
d CFL
Stra
tegies
for D
G Di
screti
zatio
ns of
the R
ANS-
SA
Equa
tions
M. Ce
ze, K
. Fidk
owsk
i, Univ
ersity
of
Mich
igan,
Ann A
rbor, A
nn Ar
bor, M
I
0900
hrs
AIAA-2
013-2
687
Adap
tive I
MEX
Time-
Stepp
ing
for t
he Co
rrecti
on P
roce
dure
via
Rec
onstr
uctio
n Sc
heme
B. Ve
rmeir
e, S.
Nad
arajah
, McG
ill Un
iversi
ty, M
ontré
al, Ca
nada
0930
hrs
AIAA-2
013-2
688
An Ev
aluat
ion of
Impli
cit
Time I
nteg
ratio
n Sc
heme
s fo
r Disc
ontin
uous
High
Ord
er
Meth
ods
C. Zh
ou, Z
. Wan
g, Un
iversi
ty of
Kans
as, L
awren
ce, L
awren
ce, K
S
1000
hrs
AIAA-2
013-2
689
Evalu
ation
of O
ptim
ized C
PR
Sche
mes f
or Co
mput
ation
al Ae
roac
ousti
cs Be
nchm
ark
Prob
lems
Y. Li,
Z. W
ang,
Unive
rsity
of Ka
nsas
, La
wren
ce, L
awren
ce, K
S
1030
hrs
AIAA-2
013-2
690
A Hi
gh-O
rder
Impli
cit-Ex
plicit
Flu
id-Str
uctu
re In
terac
tion
Meth
od fo
r Flap
ping F
light
B. Fr
oehle
, P. P
ersso
n, Un
iversi
ty of
Califo
rnia,
Berke
ley, B
erkele
y, CA
1100
hrs
AIAA-2
013-2
691
Optim
al Ac
cura
cy of
Di
scont
inuou
s Gale
rkin
for
Diffu
sion
L. Kh
ieu, B
. Van
Leer,
Univ
ersity
of
Mich
igan,
Ann A
rbor, A
nn Ar
bor, M
I; M.
Lo, S
elf, H
ong K
ong,
Hong
Kong
1130
hrs
AIAA-2
013-2
692
The E
fficie
nt Im
pleme
ntat
ion
of Co
rrecti
on P
roce
dure
Via
Reco
nstru
ction
with
GPU
Co
mput
ingB.
Zimm
erman
, Iow
a Stat
e Un
iversi
ty, Am
es, I
A; Z.
Wang
, Un
iversi
ty of
Kans
as, L
awren
ce,
Lawr
ence
, KS
Tues
day,
25 Ju
ne 2
013
65-C
FD-1
6/GT
-3Hi
gh-S
peed
and C
hemi
cally
Rea
cting
Flow
s INa
utilu
s 4Ch
aired
by: R
. CAS
TNER
, NAS
A Glen
n Res
earch
Cente
r08
00 hr
sAIA
A-201
3-269
3Ae
roth
ermo
dyna
mic S
hape
Op
timiza
tion
of H
yper
sonic
Bl
unt B
odies
M. Yu
musa
k, RO
KETS
AN M
issile
Ind
ustrie
s, Inc
., An
kara,
Turke
y; S.
Ey
i, Midd
le Ea
st Te
chnic
al Un
iversi
ty,
Anka
ra, Tu
rkey
0830
hrs
AIAA-2
013-2
694
Nume
rical
explo
ratio
n of
tra
nsien
t flow
phen
omen
a in
hype
rsonic
gun
tunn
elK.
Bens
assi,
A. La
ni, H
. Dec
oninc
k, O.
Chaz
ot, P.
Ramb
aud,
von K
ármán
Ins
titute
for Fl
uid D
ynam
ics, R
hode
-Sa
int-Ge
nèse
, Belg
ium
0900
hrs
AIAA-2
013-2
695
Multip
hase
and C
hemi
cally
Re
activ
e Flow
s in
LS-D
YNA
G. Co
ok, K
. Im,
Z. Zh
ang,
Liverm
ore
Softw
are Te
chno
logy C
orpora
tion,
Liverm
ore, C
A
Tues
day,
25 Ju
ne 2
013
66-C
FD-1
7Nu
meric
al Al
gorit
hms f
or In
viscid
and V
iscou
s Flow
s III
Seab
reez
e ICh
aired
by: M
. LIO
U, N
ASA G
lenn R
esea
rch Ce
nter a
nd E.
SHI
MA, J
apan
Aeros
pace
Explo
ration
Agen
cy08
00 hr
sAIA
A-201
3-269
6On
the i
mpro
veme
nt of
the
all-sp
eed fl
ux sc
heme
for v
ery
low M
ach
numb
er fl
ows
E. Sh
ima,
Japa
n Aero
spac
e Ex
plorat
ion Ag
ency
(JAX
A),
Saga
miha
ra, Ja
pan
0830
hrs
AIAA-2
013-2
697
Why i
s the
over
heat
ing
prob
lem di
fficu
lt: Th
e role
of
entro
pyM.
Liou
, NAS
A Glen
n Res
earch
Ce
nter, C
levela
nd, O
H
0900
hrs
AIAA-2
013-2
698
A Fu
rther
Surv
ey of
Shoc
k Ca
ptur
ing M
ethod
s on
Hype
rsonic
Hea
ting I
ssues
K. Kit
amura
, Nag
oya U
nivers
ity,
Nago
ya, J
apan
0930
hrs
AIAA-2
013-2
699
A Seco
nd-O
rder
Finite
Volum
e Me
thod t
hat R
educ
es Nu
meric
al Sh
ockw
ave A
noma
lies in
One
Di
mens
ionD.
Zaide
, Univ
ersity
of Br
itish C
olumb
ia,
Vanco
uver,
Cana
da; P.
Roe,
Unive
rsity o
f Mi
chiga
n, An
n Arbo
r, Ann
Arbo
r, MI
1000
hrs
AIAA-2
013-2
700
Nume
rical
Simula
tion
of
Comp
ressi
ble Vi
scous
Flow
Us
ing a
Veloc
ity-P
ressu
re-
Vorti
city V
ariat
ional
Form
ulatio
n an
d Dire
ct So
lver
B. Ch
acon
, M. H
afez,
Unive
rsity
of Ca
liforni
a, Da
vis, D
avis,
CA
1030
hrs
AIAA-2
013-2
701
Conv
erge
nce A
cceler
ation
Ba
sed o
n Co
nver
genc
e Erro
r Es
timat
ionS.
Eyi, M
iddle
East
Tech
nical
Unive
rsity,
Anka
ra, Tu
rkey;
M.
Yumu
sak,
ROKE
TSAN
Miss
ile
Indus
tries,
Inc.,
Anka
ra, Tu
rkey
46
Tues
day,
25 Ju
ne 2
013
67-C
FD-1
8De
sign
Optim
izatio
n Te
chniq
ues I
ISp
inake
r ICh
aired
by: F
. PAL
ACIO
S, S
tanfor
d Univ
ersity
and S
. KIM
, Kon
kuk U
nivers
ity08
00 hr
sAIA
A-201
3-270
2Dy
nami
cal o
ptim
izatio
n of
the
trailin
g-ed
ge sh
ape o
f a bl
uff
body
by m
eans
of Ex
tremu
m-se
eking
K. Na
kaya
ma, H
. Nait
o, K.
Fuka
gata,
Ke
io Un
iversi
ty, Yo
koha
ma, J
apan
0830
hrs
AIAA-2
013-2
703
Stall P
redic
tion
of Ve
ry Li
ght
Aircr
aft u
sing H
igh fi
delity
An
alysis
D. le
e, S.
Kim,
J. Le
e, Ko
nkuk
Un
iversi
ty, S
eoul,
Sou
th Ko
rea
0900
hrs
AIAA-2
013-2
704
Desig
n Op
timiza
tion
of
Subs
onic
Airfo
il and
Slot
ted
Flap S
hape
Usin
g Mult
i-Fide
lity
Aero
dyna
mic A
nalys
isM.
Tyan
, J. P
ark, S
. Kim
, J. L
ee,
Konk
uk U
nivers
ity, S
eoul,
Sou
th Ko
rea
0930
hrs
AIAA-2
013-2
705
Aero
foil D
esign
Varia
ble
Extra
ction
for A
erod
ynam
ic Op
timiza
tion
D. Po
ole, C
. Alle
n, T.
Rend
all,
Unive
rsity
of Br
istol,
Bris
tol, U
nited
Kin
gdom
1000
hrs
AIAA-2
013-2
706
Flap D
esign
Opt
imiza
tion
for V
ery L
ight A
ircra
ft in
comp
lianc
e with
Airw
orth
iness
Certi
ficat
ionJ.
Park,
S. K
im, N
. Ngu
yen,
M. Ty
an,
J. Le
e, Ko
nkuk
Univ
ersity
, Seo
ul,
South
Korea
1030
hrs
AIAA-2
013-2
707
Delau
nay-
base
d Der
ivativ
e-fre
e Opt
imiza
tion
via G
lobal
Surro
gate,
Par
t 1: T
heor
yP.
Beyh
aghi,
D. C
avag
lieri,
T. Be
wley
, Un
iversi
ty of
Califo
rnia,
San D
iego,
La Jo
lla, C
A
1100
hrs
AIAA-2
013-2
708
Intro
ducin
g New
Comp
act
Para
meter
izatio
n Meth
od fo
r an
Autom
ated B
lade S
hape
Op
timiza
tion
S. Go
hari,
Unive
rsity o
f Calif
ornia,
San
Diego
, San
Dieg
o, CA
; A. G
hasem
i K.,
Unive
rsity o
f Teh
ran, T
ehran
, Iran
1130
hrs
AIAA-2
013-2
709
Nume
rical
Invest
igatio
ns on
Ge
ometr
ic Par
amete
rs Af
fectin
g the
Osci
llatio
n Pro
perti
es of
a Flu
idic O
scilla
torB.
Bobu
sch, R
. Wosz
idlo, O
. Krüg
er, C.
Pa
schere
it, Tec
hnica
l Univ
ersity
of Be
rlin,
Berlin
, Germ
any
Tues
day,
25 Ju
ne 2
013
68-C
FD-1
9Gr
id Ge
nera
tion
and E
ffects
of G
rid Q
uality
IMa
rina 5
Chair
ed by
: C. O
LLIVIE
R GOO
CH, U
nivers
ity of
Briti
sh Co
lumbia
and H
. JAS
AK, W
ikki L
td08
00 hr
sAIA
A-201
3-271
0Un
struc
ture
d Mes
h Ge
nera
tion
Using
Adv
ancin
g Lay
ers a
nd
Metri
c-Bas
ed Tr
ansit
ion fo
r Vis
cous
Flow
fields
D. M
arcum
, Miss
issipp
i Stat
e Un
iversi
ty, M
ississ
ippi S
tate,
MS; F
. Ala
uzet,
Fren
ch N
ation
al Ins
titute
for
Rese
arch i
n Com
puter
Scie
nce a
nd
Contr
ol (IN
RIA),
Le Ch
esna
y, Fra
nce
0830
hrs
AIAA-2
013-2
711
Effic
ient a
nd A
ccura
te Ev
aluat
ion of
Airc
raft
in Di
ffere
nt Co
nfigu
ratio
ns w
ith
Auto
matic
Loca
l Rem
eshin
gY.
Ito, M
. Mura
yama
, K. Y
amam
oto,
Japa
n Aero
spac
e Exp
lorati
on Ag
ency
(JA
XA),
Mitak
a, Ja
pan
0900
hrs
AIAA-2
013-2
712
Effe
cts of
Mes
h De
form
ation
on
the Q
uality
of La
rge E
ddy
Simula
tions
J. Ke
skine
n, V.
Vuori
nen,
O. Ka
ario,
M. La
rmi, A
alto U
nivers
ity, E
spoo
, Fin
land
Tues
day,
25 Ju
ne 2
013
69-C
FD-2
0Nu
meric
al Tre
atme
nt of
Bou
ndar
y Con
dition
s IRo
om 5
14Ch
aired
by: F
. CAP
IZZAN
O, It
alian
Aeros
pace
Rese
arch C
enter
(CIRA
) and
M. M
EINKE
0800
hrs
AIAA-2
013-2
713
Use o
f the
Imme
rsed B
ound
ary
Metho
d with
in the
Build
ing Cu
be
Metho
d and
its Ap
plica
tion t
o Re
al Ve
hicle
CAD
Data
K. On
ishi, S
. Oba
yshi, T
ohok
u Univ
ersity
Ins
titute
of Flu
id Sc
ience,
Send
ai,
Japan
; K. N
akah
ashi, J
apan
Aeros
pace
Ex
plorat
ion Ag
ency
(JAXA
), Ch
ofu,
Japan
; M. T
subok
ura, H
okka
ido
Unive
rsity,
Sapp
oro, J
apan
0830
hrs
AIAA-2
013-2
714
Appli
catio
n of
imme
rsed
boun
dary
tech
nique
in SR
M sim
ulatio
ns: t
owar
d new
ins
ights
T. Ph
u, F.
Plourd
e, Éc
ole N
ation
ale
Supé
rieure
de M
écan
ique e
t d’A
érotec
hniqu
e, Fu
turos
cope
, Fra
nce
0900
hrs
AIAA-2
013-2
715
Coup
ling a
Wall
Diff
usion
-Mo
del w
ith an
Imme
rsed
Boun
dary
Tech
nique
F. Ca
pizza
no, I
talian
Aeros
pace
Re
searc
h Cen
ter (C
IRA),
Capu
a, Ita
ly
0930
hrs
AIAA-2
013-2
716
A ro
bust
cut-c
ell m
ethod
for
fluid-
struc
ture
inter
actio
n on
ad
aptiv
e mes
hes
L. Sc
hneid
ers, M
. Mein
ke, W
. Sc
hröed
er, RW
TH Aa
chen
Univ
ersity
, Aa
chen
, Germ
any
1000
hrs
AIAA-2
013-2
717
A Hy
bridi
zed L
east-
Squa
res
Ghos
t Flui
d Meth
od w
ith
Redu
ced N
umer
ical O
scilla
tions
in
Movin
g Bou
ndar
y Pro
blems
J. Mo
usel,
U. K
umar,
Univ
ersity
of
Iowa,
Iowa C
ity, I
owa C
ity, I
A
47
Tues
day,
25 Ju
ne 2
013
70-C
FD-2
1/FD
-15
Revo
lution
ary C
ompu
tatio
nal A
eros
cienc
es (R
CA) -
I (In
vited
)Na
utilu
s 2Ch
aired
by: M
. MAL
IK, N
ASA-L
angle
y Res
earch
Cente
r and
M. R
OGER
S, N
ASA A
mes R
esea
rch Ce
nter
0800
hrs
AIAA-2
013-2
718
Towa
rds B
ridgin
g the
Gap
s in
Holis
tic Tr
ansit
ion P
redic
tion
via N
umer
ical S
imula
tions
M. Ch
oudh
ari, F
. Li, C
. Cha
ng, M
. Ca
rpente
r, C. S
treett
, M. M
alik,
NASA
Lang
ley Re
searc
h Cen
ter,
Hamp
ton, V
A; L.
Duan
, Nati
onal
Institu
te of
Aeros
pace
, Ham
pton,
VA
0830
hrs
AIAA-2
013-2
719
Towa
rds a
Two-
Equa
tion
Alge
braic
Stru
cture
-Bas
ed
Mode
l with
App
licat
ions t
o Tu
rbule
nt Se
para
ted Fl
ows
A. Ca
mpos
, K. D
uraisa
my, G
. Iac
carin
o, St
anfor
d Univ
ersity
, St
anfor
d, CA
0900
hrs
AIAA-2
013-2
720
Sepa
ratio
n Pred
iction
of La
rge
Sepa
ratio
n with
Reyn
olds S
tress
Mode
lsM.
Olse
n, NA
SA Am
es Re
search
Cente
r, Mo
ffett F
ield, C
A; R.
Lillard
, NAS
A Joh
nson S
pace
Cente
r, Hou
ston,
TX; S
. Mu
rman
, NAS
A Ame
s Rese
arch C
enter
, Mo
ffett F
ield, C
A; M.
Rive
rs, N
ASA
Lang
ley Re
search
Cente
r, Ham
pton,
VA;
K. Lo
ng, J
. Ross
, NAS
A Ame
s Rese
arch
Cente
r, Moff
ett Fi
eld, C
A
0930
hrs
AIAA-2
013-2
721
Mode
ling o
f Tur
bulen
t Fre
e Sh
ear F
lows
D. Yo
der, N
. Geo
rgiad
is, J.
DeB
onis,
NA
SA G
lenn R
esea
rch Ce
nter,
Cleve
land,
OH
1000
hrs
AIAA-2
013-2
722
A Ne
w Fo
rmula
tion
for H
ybrid
LE
S-RA
NS Co
mput
ation
sS.
Woo
druff,
NAS
A Lan
gley R
esea
rch
Cente
r, Ham
pton,
VA
1030
hrs
AIAA-2
013-2
723
DNS,
Enstr
ophy
Bala
nce,
and
the D
issipa
tion
Rate
Equa
tion
in a S
epar
ated
Turb
ulent
Ch
anne
l Flow
P. Ba
lakum
ar, R.
Rubin
stein,
C.
Rums
ey, N
ASA L
angle
y Res
earch
Ce
nter, H
ampto
n, VA
1100
hrs
AIAA-2
013-2
724
Larg
e edd
y sim
ulatio
n of
hig
h-lif
t dev
ices
J. Bo
dart,
Stan
ford U
nivers
ity,
Stan
ford,
CA; J
. Lars
son,
Unive
rsity
of Ma
rylan
d, Co
llege
Park,
Colle
ge
Park,
MD;
P. M
oin, S
tanfor
d Un
iversi
ty, S
tanfor
d, CA
1130
hrs
AIAA-2
013-2
725
Adva
nced
and h
igh-o
rder
nu
meric
al dis
cretiz
ation
me
thod
s for
larg
e-ed
dy
simula
tion
that
max
imize
su
bgrid
-scale
mod
el re
solut
ionJ.
Byun
, C. P
antan
o, Un
iversi
ty of
Illino
is, U
rbana
-Cham
paign
, Ur
bana
, IL
Tues
day,
25 Ju
ne 2
013
71-FD
-16
Turb
omac
hiner
yRo
om 5
11Ch
aired
by: G
. WOO
, Geo
rgia I
nstitu
te of
Tech
nolog
y and
C. B
IDW
ELL,
NASA
Glen
n Res
earch
Cente
r08
00 hr
sAIA
A-201
3-272
6Ac
tive C
ontro
l of T
ip Le
akag
e Flo
w fo
r Low
-Pre
ssure
Turb
ine
by R
ing-Ty
pe P
lasma
Actu
ator
sT.
Matsu
numa
, T. S
egaw
a, Na
tiona
l Ins
titute
of Ad
vanc
ed In
dustr
ial
Scien
ce an
d Tec
hnolo
gy, T
suku
ba,
Japa
n
0830
hrs
AIAA-2
013-2
727
Geom
etry/
Grid
Gene
ratio
n fo
r 3D
Multi-
Disci
plina
ry
Simula
tions
in M
ulti-S
tage
Tu
rbom
achin
ery
R. Da
vis, U
nivers
ity of
Califo
rnia,
Davis
, Dav
is, CA
; J. C
lark,
Air
Force
Rese
arch L
abora
tory,
Wrig
ht-Pa
tterso
n AFB
, OH
0900
hrs
AIAA-2
013-2
728
Aero
dyna
mic C
hara
cteriz
ation
of
Thre
e-dim
ensio
nal T
urbo
fan
Bypa
ss-flo
w He
at Ex
chan
ger
Effe
cts in
an In
termi
ttent
Tra
nson
ic Fa
cility
L. Vil
lafañ
e, G.
Pania
gua,
von
Kárm
án In
stitut
e for
Fluid
Dyna
mics,
Rh
ode-S
aint-G
enès
e, Be
lgium
0930
hrs
AIAA-2
013-2
729
Effe
ct of
num
ber o
f slot
s and
ov
erlap
on th
e per
form
ance
of
Non
-circu
lar Ej
ecto
r Air
Diffu
ser
S. S
ingh,
Indian
Insti
tute o
f Te
chno
logy D
elhi, N
ew D
elhi, I
ndia
1000
hrs
AIAA-2
013-2
730
Nume
rical
flow
analy
sis in
ce
ntrif
ugal
comp
resso
r nea
r su
rge c
ondit
ionV.
Jyoth
ishku
mar, M
. Miha
escu
, B.
Seml
itsch
, L. F
uchs
, Roy
al Ins
titute
of Te
chno
logy (
KTH)
, Stoc
kholm
, Sw
eden
1030
hrs
AIAA-2
013-2
731
Thre
e-Di
mens
ional
Nume
rical
Mode
ling o
f Tip
Leak
age F
low
over
a Cy
linde
rO.
Khan
, J. K
han,
Tusk
egee
Un
iversi
ty, Tu
skeg
ee, A
L
1100
hrs
AIAA-2
013-2
732
Multi-
Objec
tive D
esign
Op
timiza
tion
of a
Trans
onic
Comp
resso
r Rot
or U
sing a
n Ad
joint
Equa
tion
Meth
odJ.
Luo,
Pekin
g Univ
ersity
, Beij
ing,
China
; F. L
iu, U
nivers
ity of
Califo
rnia,
Irvine
, Irvi
ne, C
A
Tues
day,
25 Ju
ne 2
013
72-FD
-17
Shoc
k/Bo
unda
ry La
yer I
nter
actio
nsNa
utilu
s 3Ch
aired
by: D
. GAIT
ONDE
, The
Ohio
Stat
e Univ
ersity
and D
. MILL
ER, L
ockh
eed M
artin
Corpo
ration
0800
hrs
AIAA-2
013-2
733
Impin
ging S
hock
Wav
e -
Boun
dary
Laye
r Int
erac
tions
on
a Th
ree-
Dime
nsion
al Bo
dyE.
Step
hen,
J. Fa
rnswo
rth, C
. Port
er,
R. De
cker,
T. M
cLaug
hlin,
J. Du
dley,
U.S.
Air F
orce A
cade
my, C
olorad
o Sp
rings
, CO
0830
hrs
AIAA-2
013-2
734
Analy
sis of
the L
arge
Eddy
Sim
ulatio
n of
a Sh
ock
Wave
an
d Tur
bulen
t Bou
ndar
y Lay
er
Inter
actio
nJ.
Li, N
. Grub
e, S.
Prieb
e, P.
Martin
, Un
iversi
ty of
Maryl
and,
Colle
ge Pa
rk,
Colle
ge Pa
rk, M
D
0900
hrs
AIAA-2
013-2
735
Dyna
mics
of a
shoc
k-ind
uced
se
para
tion
in a t
rans
onic
flow:
a l
inear
ized a
ppro
ach
F. Sa
rtor, M
. Clem
ent,
D. S
ipp, R
. Bu
r, ONE
RA, M
eudo
n, Fra
nce
0930
hrs
AIAA-2
013-2
736
Shoc
k In
duce
d Sep
arat
ion
in Tra
nsitio
nal H
yper
sonic
Bo
unda
ry La
yers
L. Va
nston
e, D.
Estru
ch-Sa
mper,
R.
Hillie
r, Imp
erial
Colle
ge Lo
ndon
, Lo
ndon
, Unit
ed Ki
ngdo
m; B
. Ga
napa
thisu
brama
ni, U
nivers
ity of
So
utham
pton,
South
ampto
n, Un
ited
Kingd
om
48
Tues
day,
25 Ju
ne 2
013
73-FD
-18
High
-Spe
ed Tr
ansit
ion I
Naut
ilus 1
Chair
ed by
: S. M
ATSU
MURA
and X
. ZHO
NG, U
nivers
ity of
Califo
rnia L
os An
geles
0800
hrs
AIAA-2
013-2
737
Trave
ling C
rossfl
ow In
stabil
ity
for H
IFiRE
-5 in
a Qu
iet
Hype
rsonic
Wind
Tunn
elM.
Borg
, Boo
z Alle
n Ham
ilton,
Dayto
n, OH
; R. K
imme
l, Air F
orce
Rese
arch L
abora
tory,
Wrig
ht-Pa
tterso
n AFB
, OH;
S. S
tanfie
ld,
Spec
tral E
nergi
es, D
ayton
, OH
0830
hrs
AIAA-2
013-2
738
Boun
dary
-Laye
r Tra
nsitio
n Ex
perim
ents
in a H
yper
sonic
Qu
iet W
ind Tu
nnel
C. Wa
rd, D
. Berr
idge,
R. Gr
eenw
ood,
A. Ab
ney,
S. S
chne
ider, P
urdue
Un
iversi
ty, W
est L
afaye
tte, I
N
0900
hrs
AIAA-2
013-2
739
Simult
aneo
us Pr
essur
e Me
asur
emen
ts an
d High
-Sp
eed S
chlie
ren Im
aging
of
Distu
rban
ces in
a Tra
nsitio
nal
Hype
rsonic
Boun
dary
Laye
rK.
Caspe
r, S. B
eresh,
R. W
agnild
, J.
Henfl
ing, R
. Spill
ers, B
. Prue
tt, Sa
ndia
Natio
nal La
borat
ories,
Albu
querq
ue, N
M
0930
hrs
AIAA-2
013-2
740
Nume
rical
Inve
stiga
tion
of
trans
ition
delay
usin
g por
ous
walls
C. Ha
der, C
. Breh
m, H
. Fas
el,
Unive
rsity
of Ari
zona
, Tuc
son,
Tucso
n, AZ
1000
hrs
AIAA-2
013-2
741
Nume
rical
Simula
tion
of
Free
strea
m Wa
ves R
ecep
tivity
an
d Bre
akdo
wn ov
er M
ach
6 Fla
red C
one
J. Le
i, X. Z
hong
, Univ
ersity
of
Califo
rnia,
Los A
ngele
s, Lo
s Ang
eles,
CA
1030
hrs
AIAA-2
013-2
742
Study
on St
abiliz
ation
and
Desta
biliza
tion
Effe
ct of
a Sm
ooth
Hum
p in
Hype
rsonic
Bo
unda
ry La
yers
by P
SED.
Park,
S. P
ark, K
orea A
dvan
ced
Institu
te of
Scien
ce an
d Tec
hnolo
gy,
Daeje
on, S
outh
Korea
Tues
day,
25 Ju
ne 2
013
74-FD
-19/
PDL-3
Plasm
a Actu
ator
sSp
inake
r II
Chair
ed by
: J. L
ITTLE
, The
Univ
ersity
of Ar
izona
and D
. ASH
PIS, N
ASA G
lenn R
esea
rch Ce
nter
0800
hrs
AIAA-2
013-2
743
An Em
pirica
l Mod
el of
Na
nosec
ond P
ulsed
SDBD
Ac
tuator
s for
Sepa
ratio
n Con
trol
Z. Ch
en, L
. Hao
, B. Z
hang
, Nort
hwest
ern
Polyt
echnic
al Un
iversit
y, Xi’
an, C
hina;
H. Lia
ng, Y
. Li, A
ir Forc
e Eng
ineeri
ng
Unive
rsity,
Xi’an
, Chin
a
0830
hrs
AIAA-2
013-2
744
Nume
rical
Simula
tions
Ex
plorin
g Diel
ectri
c Bar
rier
Disch
arge
-Indu
ced S
teady
and
Pulse
d Suc
tion
P. Mo
rgan,
Ohio
Aeros
pace
Insti
tute,
Wrig
ht-Pa
tterso
n AFB
, OH;
M. V
isbal,
Air
Force
Rese
arch L
abora
tory,
Wrig
ht-Pa
tterso
n AFB
, OH
0900
hrs
AIAA-2
013-2
745
Effe
cts of
Puls
e Pola
rity o
n Na
nose
cond
Puls
e Driv
en
Diele
ctric
Barri
er D
ischa
rge
Plasm
a Actu
ator
sR.
Daws
on, J
. Littl
e, Un
iversi
ty of
Arizo
na, T
ucso
n, Tu
cson,
AZ
0930
hrs
AIAA-2
013-2
746
Aero
dyna
mic F
low A
cceler
ation
wi
th O
ne A
tmos
pher
e Unif
orm
Indu
ced b
y Sing
le an
d Mult
iple
DBD
Plasm
a Actu
ation
Bas
ed
on P
IVL.
Feng
, C. G
ao, B
. Zhe
ng, Y
. Wa
ng, X
. Hu,
Z. Lv,
Nort
hwes
tern
Polyt
echn
ical U
nivers
ity, X
i’an,
China
Tues
day,
25 Ju
ne 2
013
75-FD
-20
Boun
dary
Laye
r and
Airf
oil Se
para
tion
Cont
rol
Seab
reez
e II
Chair
ed by
: M. B
RIGHT
, Nort
hrop G
rumma
n Aero
spac
e Sys
tems a
nd E.
WHA
LEN,
Boe
ing En
ginee
ring O
perat
ions &
Tech
nolog
y08
00 hr
sAIA
A-201
3-274
7Lo
cal A
cous
tic Fo
rcing
of
a Wing
at Lo
w Re
ynold
s Nu
mber
sS.
Yang
, G. S
pedd
ing, U
nivers
ity of
So
uthern
Califo
rnia,
Los A
ngele
s, CA
0830
hrs
AIAA-2
013-2
748
Signifi
canc
e of T
hree
-dim
ensio
nal U
nstea
dy
Flows
insid
e the
Cavit
y on
Sepa
rated
-flow
Cont
rol
arou
nd an
NAC
A001
5 us
ing a
Synt
hetic
Jet
Y. Ab
e, Un
iversi
ty of
Toky
o, Sa
gami
hara,
Japa
n; K.
Okad
a, Ry
oyu
Syste
ms Co
mpan
y, Ltd
., Na
goya
, Ja
pan;
M. S
ato, T
. Non
omura
, K.
Fujii,
Japa
n Aero
spac
e Exp
lorati
on
Agen
cy (J
AXA)
, Sag
amiha
ra, Ja
pan
0900
hrs
AIAA-2
013-2
749
On th
e Per
form
ance
of
Boun
dary
Laye
r Suc
tion
for
Seco
ndar
y Flow
Cont
rol in
a H
igh Sp
eed C
ompr
esso
r Ca
scade
K. Lie
sner,
R. M
eyer,
Germ
an
Aeros
pace
Cente
r (DL
R), B
erlin,
Ge
rman
y; C.
Gmeli
n, F.
Thiel
e, Te
chnic
al Un
iversi
ty of
Berlin
, Berl
in,
Germ
any
0930
hrs
AIAA-2
013-2
750
Massi
ve Pa
rame
tric S
tudy b
y LE
S on S
epar
ated-fl
ow Co
ntrol
arou
nd Ai
rfoil u
sing D
BD Pl
asma
Ac
tuator
at Re
ynold
s Num
ber
63,00
0M.
Sato,
Japa
n Aero
space
Explo
ration
Ag
ency
(JAXA
), Sa
gami
hara,
Japa
n; K.
Okad
a, Ry
oyu S
ystem
s Com
pany,
Ltd.,
Na
goya
, Jap
an; T
. Non
omura
, H. A
ono,
A. Ya
keno
, Jap
an Ae
rospa
ce Ex
plorat
ion
Agen
cy (JA
XA),
Saga
miha
ra, Ja
pan;
K. As
ada,
Y. Ab
e, Un
iversit
y of T
okyo
, Sa
gami
hara,
Japa
n; K.
Fujii,
Japan
Ae
rospa
ce Ex
plorat
ion Ag
ency
(JAXA
), Sa
gami
hara,
Japa
n
1000
hrs
AIAA-2
013-2
751
Nume
rical
Inve
stiga
tion
of
Sepa
ratio
n Co
ntro
l for
Wing
Se
ction
at R
e=30
0,00
0A.
Gros
s, H.
Fase
l, Univ
ersity
of
Arizo
na, T
ucso
n, Tu
cson,
AZ
1030
hrs
AIAA-2
013-2
752
Effe
cts of
High
Volta
ge P
ulsed
DB
D on
the A
erod
ynam
ic Pe
rform
ance
s in
Subs
onic
and
Trans
onic
Cond
itions
A. Ma
rino,
P. Ca
talan
o, C.
Maron
giu,
Italia
n Aero
spac
e Res
earch
Cente
r (C
IRA),
Capu
a, Ita
ly; P.
Pesch
ke,
C. Ho
llens
tein,
Swiss
Fede
ral
Institu
te of
Tech
nolog
y, La
usan
ne,
Switz
erlan
d; R.
Done
lli, It
alian
Ae
rospa
ce Re
searc
h Cen
ter (C
IRA),
Capu
a, Ita
ly
1100
hrs
AIAA-2
013-2
753
The M
ixing
Laye
r Per
turb
ed by
a D
ielec
tric B
arrie
r Disc
harg
eR.
Ely, J
. Littl
e, Un
iversi
ty of
Arizo
na,
Tucso
n, Tu
cson,
AZ
49
Tues
day,
25 Ju
ne 2
013
76-P
DL-4
Magn
etohy
drod
ynam
icsEx
ecut
ive Co
nfer
ence
1Ch
aired
by: S
. WU,
The U
nivers
ity of
Alab
ama i
n Hun
tsville
0800
hrs
AIAA-2
013-2
754
Simula
tion
of R
eacti
ng Fl
ows
in Ma
gneti
c Fiel
ds w
ith
Prec
ondit
ioning
A. Lo
nkar,
F. Pa
lacios
, J. A
lonso
, St
anfor
d Univ
ersity
, Stan
ford,
CA
0830
hrs
AIAA-2
013-2
755
Riem
ann-
solve
r Fre
e Sp
ace-
time D
iscon
tinuo
us
Galer
kin M
ethod
for
Magn
etohy
drod
ynam
icsS.
Tu, J
acks
on S
tate U
nivers
ity,
Jack
son,
MS
0900
hrs
AIAA-2
013-2
756
High
-ord
er di
verg
ence
-free
me
thod
for c
ompr
essib
le MH
D wi
th sh
ock
wave
sS.
Kawa
i, Jap
an Ae
rospa
ce
Explo
ration
Agen
cy (J
AXA)
, Sa
gami
hara,
Japa
n
0930
hrs
AIAA-2
013-2
757
Study
of In
comp
ressib
le MH
D Flo
w in
a Circ
ular P
ipe w
ith
Trans
verse
Mag
netic
Field
using
a Sp
ectra
l/Fini
te Ele
ment
Solve
rX.
Decha
mps,
Unive
rsité L
ibre d
e Bru
xelles
, Brus
sels,
Belgiu
m; M
. Ra
squin,
Argo
nne N
ation
al La
borat
ory,
Argon
ne, IL
; G. D
egrez
, Univ
ersité
Libre
de Br
uxelle
s, Bru
ssels,
Belgiu
m; K.
Jan
sen, U
nivers
ity of
Color
ado,
Bould
er,
Bould
er, CO
1000
hrs
AIAA-2
013-2
758
Magn
eto-h
ydro
dyna
mics
simula
tion
study
of h
igh sp
eed
flow
cont
rol u
sing t
he R
ail
Plasm
a Actu
ator
(Rail
PAc)
H. S
itaram
an, L
. Raja
, Univ
ersity
of
Texa
s, Au
stin,
Austi
n, TX
1030
hrs
AIAA-2
013-2
759
Resis
tive
Magn
etohy
drod
ynam
ic Stu
dy
of M
agne
tic Fi
eld Ef
fects
on
Plasm
a Plum
esF.
Ebers
ohn,
L. Ra
ja, U
nivers
ity
of Te
xas,
Austi
n, Au
stin,
TX; J
. Sh
ebali
n, NA
SA Jo
hnso
n Spa
ce
Cente
r, Hou
ston,
TX
Tues
day,
25 Ju
ne 2
013
77-P
DL-5
Plasm
a-As
sisted
Comb
ustio
n/Pla
sma D
iagno
stics
Marin
a 6Ch
aired
by: R
. MILE
S, Pr
inceto
n Univ
ersity
0800
hrs
AIAA-2
013-2
760
Nano
seco
nd ti
me-re
solve
d 2 +
2
Rada
r REM
PI m
easu
reme
nts
perfo
rmed
in m
olecu
lar
nitro
gen
S. M
cGuir
e, T.
Chng
, R. M
iles,
Princ
eton U
nivers
ity, P
rince
ton, N
J
0830
hrs
AIAA-2
013-2
761
Monit
oring
temp
eratur
e in h
igh
entha
lpy ar
c-hea
ted pl
asma
flo
ws us
ing tu
nable
diod
e las
er
abso
rptio
n spe
ctros
copy
M. N
ation
s Mart
in, L.
Chan
g, J.
Jeffrie
s, R.
Hanso
n, Sta
nford
Unive
rsity,
Stanfo
rd, CA
; A. N
awaz
, J. T
aunk
, D.
Drive
r, G. R
aiche
, NAS
A Ame
s Rese
arch
Cente
r, Moff
ett Fi
eld, C
A
0900
hrs
AIAA-2
013-2
762
FLEE
T Bou
ndar
y Lay
er Ve
locity
Pr
ofile
Meas
urem
ents
N. Ca
lvert,
A. D
ogari
u, R.
Miles
, Pri
nceto
n Univ
ersity
, Prin
ceton
, NJ
0930
hrs
AIAA-2
013-2
763
Cavit
y Enh
ance
d Tho
mson
Sc
atter
ing fo
r Diag
nosti
cs of
We
akly
Ioniz
ed D
ischa
rges
A. Fri
ss, I.
Fran
ka, B
. Lee
, A. Y
alin,
Color
ado S
tate U
nivers
ity, F
ort
Collin
s, CO
1000
hrs
AIAA-2
013-2
764
Mode
ling o
f Non
-Ther
mal
Plasm
a Ign
ition
of Co
mbus
tion
Mixt
ures
D. B
reden
, L. R
aja, U
nivers
ity of
Te
xas,
Austi
n, Au
stin,
TX
1030
hrs
AIAA-2
013-2
765
Mixin
g Effi
cienc
y Esti
matio
n by
Pro
be D
ischa
rge
Spec
trosco
pyS.
Leon
ov, D
. Yara
ntsev
, S. M
ichail
, A.
Firso
v, Ru
ssian
Acad
emy o
f Sc
ience
s, Mo
scow,
Russi
a
1100
hrs
AIAA-2
013-2
766
Ignit
ion an
d sta
biliza
tion
of
burn
ing h
ydro
carb
onic
fuels
in
a stre
am pu
lse-p
eriod
ic las
er
radia
tion
V. Zu
dov,
P. Tre
tyako
v, A.
Tupik
in,
Russi
an Ac
adem
y of S
cienc
es,
Novo
sibirs
k, Ru
ssia
Tues
day,
25 Ju
ne 2
013
78-TP
-6Ab
lation
IIEx
ecut
ive Co
nfer
ence
3B
Chair
ed by
: J. Z
ITO, U
nivers
ity of
Flori
da an
d C. P
ARK,
Korea
Adva
nced
Insti
tute o
f Scie
nce &
Tech
nolog
y08
00 hr
sAIA
A-201
3-276
7Po
rous
-mat
erial
Ana
lysis
Toolb
ox ba
sed o
n Op
enFO
AM-
exten
d and
App
licat
ions
J. La
chau
d, Un
iversi
ty of
Califo
rnia,
Santa
Cruz
, San
ta Cru
z, CA
; N.
Mans
our, N
ASA A
mes R
esea
rch
Cente
r, Moff
ett Fi
eld, C
A
0830
hrs
AIAA-2
013-2
768
A New
Appr
oach
To Li
ght-W
eight
Ablat
ors A
nalys
is: Fro
m Mi
cro-
Tomo
grap
hy M
easu
remen
ts to
Statis
tical
Analy
sis an
d Mod
eling
N. M
ansou
r, NAS
A Ame
s Rese
arch
Cente
r, Moff
ett Fi
eld, C
A; F. P
anera
i, A.
Martin
, Univ
ersity
of Ke
ntucky
, Lex
ington
, Lex
ington
, KY;
D. Pa
rkinso
n, A.
MacD
owell,
Lawr
ence
Berke
ley
Natio
nal La
borat
ory, B
erkele
y, CA
; T.
Fast,
Unive
rsity o
f Calif
ornia,
Santa
Ba
rbara,
Santa
Barba
ra, CA
; G. V
ignole
s, Un
iversit
y of B
ordea
ux, P
essac,
Fran
ce;
J. La
chaud
, Univ
ersity
of Ca
liforni
a, Sa
nta Cr
uz, M
offett
Field
, CA
0900
hrs
AIAA-2
013-2
769
Flow-
tube
Oxid
ation
Ex
perim
ents
on th
e Car
bon
Pref
orm
of P
ICAF.
Pane
rai, A
. Mart
in, U
nivers
ity of
Ke
ntuck
y, Le
xingto
n, Le
xingto
n, KY
; N.
Man
sour,
NAS
A Ame
s Res
earch
Ce
nter, M
offett
Field
, CA;
S. S
epka
, ER
C, Inc
., Hu
ntsvil
le, AL
; J. L
acha
ud,
Unive
rsity
of Ca
liforni
a, Sa
nta Cr
uz,
Moffe
tt Fie
ld, CA
0930
hrs
AIAA-2
013-2
770
Spac
e and
Time
-Res
olved
Em
ission
Spec
trosco
py of
Ca
rbon
Phe
nolic
Abla
tion
in Ai
r an
d Nitr
ogen
Plas
mas
B. H
elber,
O. C
hazo
t, T.
Magin
, von
Ká
rmán
Insti
tute f
or Flu
id Dy
nami
cs,
Rhod
e-Sain
t-Gen
èse,
Belgi
um; A
. Hu
bin, V
rije U
nivers
iteit B
russe
ls,
Brus
sels,
Belg
ium
1000
hrs
AIAA-2
013-2
771
Stagn
ation
regio
n ra
diativ
e ab
lation
of as
teroid
al me
teoro
ids in
the R
osse
land
appr
oxim
ation
C. Pa
rk, Ko
rea Ad
vanc
ed In
stitut
e of
Scien
ce an
d Tec
hnolo
gy, D
aejeo
n, So
uth Ko
rea
1030
hrs
AIAA-2
013-2
772
Meas
urem
ents
of A
ir Pla
sma/
Ablat
or In
terac
tions
in a
50 k
W In
ducti
vely
Coup
led
Plasm
a Tor
chM.
Mac
Dona
ld, C.
Jaco
bs, U
. She
ikh,
C. La
ux, É
cole
Centr
ale de
Paris
, Pa
ris, F
rance
1100
hrs
AIAA-2
013-2
773
Study
on Ch
emica
l Fac
tory
in
Hype
rsonic
Wind
Tunn
el Flo
w Us
ing A
blatio
n an
d Elec
tric
Disch
arge
K. Su
zuki,
Y. W
atana
be, U
nivers
ity
of To
kyo,
Kash
iwa,
Japa
n
50
Tues
day,
25 Ju
ne 2
013
79-TP
-7Ae
roth
ermo
dyna
mics
IIEx
ecut
ive Co
nfer
ence
3A
Chair
ed by
: D. B
OSE,
NASA
-Ames
0800
hrs
AIAA-2
013-2
774
Influ
ence
of Tu
rbule
nce
Mode
ling O
n Af
tbod
y Sur
face
He
ating
Pre
dictio
n Fo
r A
Hype
rsonic
Entry
Caps
uleK.
Neitz
el, I.
Boy
d, Un
iversi
ty of
Mich
igan,
Ann A
rbor, A
nn Ar
bor, M
I
0830
hrs
AIAA-2
013-2
775
Analy
sis of
Flow
field
Past
a Sa
mple
Retu
rn Ca
psule
with
He
atsh
ield A
blatio
nA.
Vivian
i, Sec
ond U
nivers
ity of
Na
ples,
Avers
a, Ita
ly; G
. Pez
zella
, Ita
lian A
erosp
ace R
esea
rch Ce
nter
(CIRA
), Ca
pua,
Italy
0900
hrs
AIAA-2
013-2
776
Unce
rtaint
y Ana
lysis
of
Surfa
ce H
eatin
g Rat
es fo
r Ou
ter P
lanet
Entri
esG.
Palm
er, B
. Crud
en, A
. Bran
dis, D
. Pra
bhu,
ERC,
Inc.,
Hunts
ville,
AL
0930
hrs
AIAA-2
013-2
777
Valid
ation
of H
yper
Rad f
or
Earth
Entri
esA.
Bran
dis, E
RC, I
nc.,
Moun
tain
View,
CA; A
. Wray
, Y. L
iu, D
. Sc
hwen
ke, N
ASA A
mes R
esea
rch
Cente
r, Moff
ett Fi
eld, C
A; W.
Huo
, ER
C, Inc
., Mo
untai
n View
, CA;
C. Jo
hnsto
n, NA
SA La
ngley
Rese
arch
Cente
r, Ham
pton,
VA
1000
hrs
AIAA-2
013-2
778
Mars
Scien
ce La
bora
tory
Hea
t Sh
ield I
nstru
ment
ation
and A
rc Je
t Cha
racte
rizat
ionD.
Bos
e, NA
SA Am
es Re
searc
h Ce
nter, M
offett
Field
, CA;
J. Sa
ntos,
Sierra
Lobo
, Inc
., Mo
ffett
Field,
CA
; E. R
odrig
uez,
T. W
hite,
ERC,
Inc.,
Moffe
tt Fie
ld, CA
; M. M
ahza
ri, Ge
orgia
Institu
te of
Tech
nolog
y, Atl
anta,
GA
1030
hrs
AIAA-2
013-2
779
Post-
fligh
t Ana
lysis
of M
ars
Scien
ce La
bora
tory
’s En
try
Aero
ther
mal E
nviro
nmen
t and
Th
erma
l Pro
tectio
n Sy
stem
Resp
onse
T. W
hite,
ERC,
Inc.,
Moffe
tt Fie
ld,
CA; M
. Mah
zari,
Georg
ia Ins
titute
of Te
chno
logy,
Atlan
ta, G
A; D.
Bos
e, NA
SA Am
es Re
searc
h Cen
ter, M
offett
Fie
ld, CA
; J. S
antos
, Sier
ra Lo
bo,
Inc.,
Moffe
tt Fie
ld, CA
1100
hrs
AIAA-2
013-2
780
Invers
e Esti
matio
n of t
he
Mars
Scien
ce La
bora
tory E
ntry
Aero
therm
al En
viron
ment
and
Therm
al Pr
otecti
on Sy
stem
Resp
onse
M. M
ahza
ri, Ge
orgia
Institu
te of
Techn
ology,
Atlan
ta, GA
; T. W
hite,
ERC,
Inc., M
offett
Field
, CA;
R. Bra
un, G
eorgi
a Ins
titute
of Tec
hnolo
gy, At
lanta,
GA;
D. Bo
se, N
ASA A
mes R
esearc
h Cen
ter,
Moffe
tt Field
, CA
1130
hrs
AIAA-2
013-2
781
Mars
Scien
ce
Labo
rato
ry H
eatsh
ield
Aero
ther
mody
nami
cs: D
esign
an
d Rec
onstr
uctio
nK.
Edqu
ist, B
. Holl
is, N
ASA L
angle
y Re
searc
h Cen
ter, H
ampto
n, VA
Tues
day,
25 Ju
ne 2
013
80-TP
-8Di
rect
Simula
tion
Mont
e Car
lo Me
thod
sEx
ecut
ive Co
nfer
ence
2B
Chair
ed by
: D. L
EVIN
, Pen
nsylv
ania
State
Univ
ersity
0800
hrs
AIAA-2
013-2
782
Conti
nuum
Brea
kdow
n Effe
cts on
Su
rface
Prop
erties
for H
ypers
onic
Shoc
k Wav
e-Bou
ndar
y Lay
er
Intera
ction
J. Bu
rt, E.
Josyu
la, Ai
r Forc
e Rese
arch
Labo
ratory
, Wrig
ht-Pa
tterso
n AFB
, OH
0830
hrs
AIAA-2
013-2
783
Imple
menta
tion C
halle
nges
and
Perfo
rman
ce of
Force
d Har
monic
Os
cillato
r Mod
el in
Direc
t Sim
ulatio
n Mon
te Ca
rloA.
Weav
er, V.
Ayya
swam
y, A.
Alexe
enko
, Purd
ue Un
iversit
y, We
st La
fayett
e, IN
0900
hrs
AIAA-2
013-2
784
Comp
ariso
n of
DSM
C and
ex
perim
enta
l res
ults o
f H2O
Su
perso
nic Co
nden
sed J
etsA.
Borne
r, Z. L
i, D. L
evin,
Pe
nnsy
lvania
Stat
e Univ
ersity
, Un
iversi
ty Pa
rk, PA
0930
hrs
AIAA-2
013-2
785
DSMC
imple
ment
ation
of
MD/Q
CT ge
nera
ted en
ergy
dis
tribu
tions
for S
O 2 + O
co
llision
sN.
Parso
ns, D
. Lev
in, Pe
nnsy
lvania
St
ate U
nivers
ity, U
nivers
ity Pa
rk, PA
1000
hrs
AIAA-2
013-2
786
Mode
ling o
f NO
Radia
tion
from
Unste
ady a
nd St
eady
Sh
ocks
Usin
g DSM
CT.
Zhu,
Z. Li,
D. L
evin,
Penn
sylva
nia
State
Univ
ersity
, Univ
ersity
Park,
PA
1030
hrs
AIAA-2
013-2
787
DSMC
Simu
lation
of N
ear-fi
eld
Ence
ladus
Plum
es fr
om Ti
ger
Stripe
Frac
ture
sZ.
Li, D
. Lev
in, Pe
nnsy
lvania
Stat
e Un
iversi
ty, U
nivers
ity Pa
rk, PA
1100
hrs
AIAA-2
013-2
788
Comp
utat
ional
Analy
sis of
Lo
w-De
nsity
Hyp
erso
nic Fl
ow
over
Bac
kwar
d-Fa
cing S
teps
P. Le
ite, W
. San
tos, N
ation
al Ins
titute
for S
pace
Rese
arch (
INPE
), Ca
choe
ira Pa
ulista
, Braz
il
1130
hrs
AIAA-2
013-2
789
Leng
th-to
-Dep
th R
atio
Effe
cts
on A
erod
ynam
ic Su
rface
Qu
antit
ies of
a Ra
refie
d Hy
perso
nic G
ap Fl
owL.
Paoli
cchi, W
. San
tos, N
ation
al Ins
titute
for S
pace
Rese
arch (
INPE
), Ca
choe
ira Pa
ulista
, Braz
il
Tues
day,
25 Ju
ne 2
013
81-W
S-1
0800
- 11
00 h
rsPr
otec
ting I
ntell
ectu
al Pr
oper
ty W
orks
hop
Harb
or B
allro
om I
and I
I
Tues
day,
25 Ju
ne 2
013
82-LN
CH-2
12
00 -
1400
hrs
Tues
day A
ward
s Lun
cheo
nHa
rbor
Ball
room
I an
d II
Revo
lution
ary Ae
rospa
ce Tec
hnolo
gies
Char
les Ch
ase
Lock
heed
Mart
in Sk
unk W
orks
Tues
day,
25 Ju
ne 2
013
83-S
B-4
1400
- 14
30 h
rsTu
esda
y Afte
rnoo
n Sp
eake
rs’ B
riefin
gSe
ssion
Roo
ms
51
Tues
day,
25 Ju
ne 2
013
84-A
PA-1
7Ae
rody
nami
c-Stru
ctura
l Dyn
amics
Inter
actio
n II
Naut
ilus 3
Chair
ed by
: J. A
ZEVE
DO an
d J. F
ARNS
WOR
TH, U
S Air
Force
Acad
emy
1430
hrs
AIAA-2
013-2
790
Perfo
rman
ce R
eliab
ility
Asse
ssmen
t of a
Flex
ible
Wing
Micr
o Air
Vehic
le us
ing
an Ef
ficien
t Flui
d-Str
uctu
re
Inter
actio
n Me
thod
T. Co
mbes
, F. Z
hang
, M. H
acke
tt, A.
Ma
lik, G
. Bram
esfel
d, Sa
int Lo
uis
Unive
rsity,
St.
Louis
, MO
1500
hrs
AIAA-2
013-2
791
Aero
elasti
c Per
form
ance
As
sessm
ent o
f a W
ing w
ith
Coan
da Ef
fect
Circu
lation
Co
ntro
l via
Fluid-
Struc
ture
In
terac
tion
K. So
mmerw
erk, M
. Hau
pt, P.
Hors
t, Te
chnic
al Un
iversi
ty of
Brau
nsch
weig,
Br
auns
chwe
ig, G
erman
y
1530
hrs
AIAA-2
013-2
792
CFD/
CSD
Coup
led Si
mulat
ions
for H
elico
pter
Rot
ors i
n Fo
rwar
d and
Man
euve
r Flig
hts
C. Sh
eng,
J. Ick
es, J
. Wan
g, Q.
Zh
ao, U
nivers
ity of
Toled
o, To
ledo,
OH
1600
hrs
AIAA-2
013-2
793
A Tw
o-Di
mens
ional
Comp
utat
ional
Mode
l of F
uel
Slosh
ing Ef
fects
on A
eroe
lastic
Be
havio
urJ.
Hall,
T. Re
ndall
, C. A
llen,
Unive
rsity
of Br
istol,
Bris
tol, U
nited
Kin
gdom
Tues
day,
25 Ju
ne 2
013
85-A
PA-1
8/FD
-21
Activ
e and
Pas
sive F
low Co
ntro
l II
Spina
ker I
ICh
aired
by: M
. AMI
TAY, R
ensse
laer P
olytec
hnic
Institu
te an
d G. G
ATLIN
1430
hrs
AIAA-2
013-2
794
Enha
ncem
ents
to th
e FAS
T-MA
C Circ
ulatio
n Co
ntro
l Mod
el an
d Rec
ent H
igh-R
eyno
lds
Numb
er Te
sting
in th
e Nat
ional
Trans
onic
Facil
ityW.
Milh
olen,
G. Jo
nes,
D. Ch
an, S
. Go
odliff
, S. A
nders
, L. P
ack M
elton
, M.
Carte
r, B. A
llan,
NASA
Lang
ley
Rese
arch C
enter
, Ham
pton,
VA;
F. Ca
pone
, Ana
lytica
l Mec
hanic
s As
socia
tes, I
nc.,
Hamp
ton, V
A
1500
hrs
AIAA-2
013-2
795
Activ
e Flow
Contr
ol on
a Hi
gh-Li
ft Air
foil: U
RANS
Simu
lation
s and
Co
mpar
ison w
ith Ti
me-A
ccura
te Me
asur
emen
tsV.
Cioba
ca, Ge
rman
Aeros
pace
Cente
r (D
LR),
Braun
schwe
ig, Ge
rman
y; F.
Hauck
e, Tec
hnica
l Univ
ersity
of Be
rlin,
Berlin
, Germ
any;
R. Ru
dnik,
Germ
an
Aeros
pace
Cente
r (DL
R), B
raunsc
hweig
, Ge
rman
y; W.
Nitsc
he, T
echnic
al Un
iversit
y of B
erlin,
Berlin
, Germ
any
1530
hrs
AIAA-2
013-2
796
Lift E
nhan
ceme
nt fo
r Upp
er
Surfa
ce B
lowing
Airp
lanes
Y. Ya
dlin,
A. Sh
milov
ich, T
he B
oeing
Co
mpan
y, Hu
nting
ton B
each
, CA
1600
hrs
AIAA-2
013-2
797
Para
metri
c Stu
dy of
Synt
hetic
-Je
t-Bas
ed Fl
ow Co
ntro
l for
Pe
rform
ance
Enha
ncem
ent o
f a V
ertic
al Sta
bilize
rN.
Ratha
y, M.
Bou
cher,
M. A
mitay
, Re
nsse
laer P
olytec
hnic
Institu
te,
Troy,
NY; E
. Wha
len, T
he B
oeing
Co
mpan
y, Ha
zelw
ood,
MO
1630
hrs
AIAA-2
013-2
798
Activ
e flow
cont
rol a
t a
swep
t wing
: A co
mpar
ison
of
nume
rical
and e
xper
imen
tal
resu
ltsC.
Hueh
ne, S
. Mah
mood
, P. S
cholz
, Te
chnic
al Un
iversi
ty of
Brau
nsch
weig,
Br
auns
chwe
ig, G
erman
y
Tues
day,
25 Ju
ne 2
013
86-A
PA-1
9Pr
opell
er/R
otor
craft/
Wind
Turb
ine A
erod
ynam
ics II
Marin
a 2Ch
aired
by: A
. JON
ES, U
nivers
ity of
Mary
land a
nd K.
KARA
, Kha
lifa U
nivers
ity of
Scie
nce,
Tech
nolog
y & Re
searc
h14
30 hr
sAIA
A-201
3-279
9Ex
perim
enta
l Ver
ifica
tion
of P
itch
Angle
s for
Pow
er
Regu
lation
of Va
riable
Pitc
h Ho
rizon
tal A
xis W
ind Tu
rbine
I. Elq
atary,
B. E
lhadid
i, Cair
o Un
iversi
ty, G
iza, E
gypt
1500
hrs
AIAA-2
013-2
800
Reali
stic L
eadin
g-Edg
e Rou
ghne
ss Eff
ects o
n Airf
oil Pe
rform
ance
R. Eh
rman
n, E.
White
, Tex
as A&
M Un
iversit
y, Co
llege S
tation
, TX;
M.
Rums
ey, Sa
ndia
Natio
nal La
borat
ories,
Alb
uque
rque,
NM; R
. Cho
w, C.
Lang
el,
C. Va
n Dam
, Univ
ersity
of Ca
liforni
a, Da
vis, D
avis,
CA
1530
hrs
AIAA-2
013-2
801
Non-
Unifo
rm In
flow
Effe
cts on
Pr
opell
er P
erfo
rman
ceL.
Veldh
uis, M
. Kots
onis,
E.
van B
erkel,
Delf
t Univ
ersity
of
Tech
nolog
y, De
lft, Th
e Neth
erlan
ds
1600
hrs
AIAA-2
013-2
802
Doub
le Mu
ltiple
Strea
mtub
e Mo
del f
or Va
riable
Pitc
h Ve
rtica
l Axis
Wind
Turb
ines
C. So
ragha
n, W.
Leith
ead,
J. Fe
uchtw
ang,
H. Yu
e, Un
iversi
ty of
Strat
hclyd
e, Gla
sgow
, Unit
ed
Kingd
om
1630
hrs
AIAA-2
013-2
803
Thru
st an
d Tor
que F
ar-fi
eld
Analy
sis of
Pro
pelle
r and
Co
unter
Rot
ating
Ope
n Ro
tor
Confi
gura
tions
M. M
eheu
t, ON
ERA,
Meud
on, F
rance
1700
hrs
AIAA-2
013-2
804
An Ex
perim
enta
l Inv
estig
ation
on
the P
erfo
manc
es of
Wind
Tu
rbine
s Site
d ove
r a H
illy
Terra
inW.
Tian
, A. O
zbay
, W. Y
uan,
H. H
u, Iow
a Stat
e Univ
ersity
, Ame
s, IA
52
Tues
day,
25 Ju
ne 2
013
87-A
PA-2
0Wi
nd Tu
nnel
and F
light
Testi
ng A
ero I
Marin
a 3Ch
aired
by: J
. PIN
IER, N
ASA-L
angle
y Res
earch
Cente
r and
E. RO
OSEN
BOOM
, DLR
- Germ
an Ae
rospa
ce Ce
nter
1430
hrs
AIAA-2
013-2
805
Multi
Degr
ee-o
f-Fre
edom
Te
chniq
ue fo
r Dyn
amic
Char
acter
istics
of A
tmos
pher
ic En
try Ca
psule
K. Hir
aki, K
. Yas
uoka
, Kyu
shu
Institu
te of
Tech
nolog
y, Kit
akyu
shu,
Japa
n; H.
Klein
e, Un
iversi
ty of
New
South
Wale
s, Ca
nberr
a, Au
strali
a
1500
hrs
AIAA-2
013-2
806
Stall/
Spin
Mitig
ation
Fligh
t Te
sting
with
a Su
bsca
le Ae
roba
tic A
ircra
ftA.
Ragh
eb, O
. Dan
tsker,
M. S
elig,
Unive
rsity
of Illi
nois,
Urba
na-
Cham
paign
, Urba
na, I
L
1530
hrs
AIAA-2
013-2
807
Deve
lopme
nt an
d Init
ial
Testi
ng of
the A
ero T
estb
ed:
A La
rge-
Scale
Unm
anne
d Ele
ctric
Aero
batic
Airc
raft
for
Aero
dyna
mics
Rese
arch
O. D
antsk
er, M
. Joh
nson
, M. S
elig,
T. Br
etl, U
nivers
ity of
Illino
is, U
rbana
-Ch
ampa
ign, U
rbana
, IL
1600
hrs
AIAA-2
013-2
808
Testi
ng of
the T
rim Ta
b Pa
rame
tric M
odel
in NA
SA
Lang
ley’s
Unita
ry P
lan W
ind
Tunn
elK.
Murph
y, A.
Korzu
n, N.
Watk
ins,
K. Ed
quist
, NAS
A Lan
gley R
esea
rch
Cente
r, Ham
pton,
VA
1630
hrs
AIAA-2
013-2
809
Supe
rsonic
Aer
odyn
amic
Char
acter
istics
of B
lunt B
ody
Trim
Tab C
onfig
urat
ions
A. Ko
rzun,
K. Mu
rphy,
K. Ed
quist
, NA
SA La
ngley
Rese
arch C
enter
, Ha
mpton
, VA
1700
hrs
AIAA-2
013-2
810
Plana
r Las
er-In
duce
d Flu
ores
cenc
e Velo
city
Meas
urem
ents
of
Retro
prop
ulsion
Jets
in a M
ach
12 Fr
eestr
eam
J. Co
doni,
E. Re
ed, J
. McD
aniel
, Un
iversi
ty of
Virgin
ia, Ch
arlott
esvil
le,
Charl
ottes
ville,
VA; H
. Alka
ndry,
I.
Boyd
, Univ
ersity
of M
ichiga
n, An
n Arb
or, An
n Arbo
r, MI
Tues
day,
25 Ju
ne 2
013
88-A
PA-2
1Ot
her T
opics
in A
pplie
d Aer
oMa
rina 4
Chair
ed by
: B. M
CGRA
TH, J
HU/A
pplie
d Phy
sics L
abora
tory a
nd S
. FER
GUSO
N, B
oeing
Defe
nse,
Spac
e & S
ecuri
ty14
30 hr
sAIA
A-201
3-281
1An
Expe
rimen
tal S
tudy
of th
e Un
stead
y Vor
tex an
d Flow
Str
uctu
res a
roun
d Twi
n-Bo
x-Gi
rder
Brid
ge D
eck
Mode
lsW.
Chen
, Iow
a Stat
e Univ
ersity
, Am
es, I
A; S.
Lima
, H. L
i, Harb
in Ins
titute
of Te
chno
logy,
Harbi
n, Ch
ina; H
. Hu,
Iowa S
tate U
nivers
ity,
Ames
, IA
1500
hrs
AIAA-2
013-2
812
Innov
ative
Vibr
ation
and A
cous
tic
Metho
dolog
ies fo
r the
Desi
gn of
En
hanc
ed Co
mpos
ite Pa
nel fo
r Air
craft
A. Ma
rino,
V. Pa
squale
, Italia
n Aero
space
Re
search
Cente
r (CIR
A), C
apua
, Italy
; P. T
iziano
, Univ
ersity
of Ro
me, R
ome,
Italy;
V. Q
uaran
ta, B.
Impe
ratore
, Italia
n Ae
rospa
ce Re
search
Cente
r (CIR
A),
Capu
a, Ita
ly; C.
Robe
rto, U
nivers
ity of
Ro
me, R
ome,
Italy
1530
hrs
AIAA-2
013-2
813
An Ex
perim
enta
l Setu
p to
Study
the I
mpac
t of S
urfa
ce
Distu
rban
ces o
n Bo
unda
ry
Laye
r Tra
nsitio
n ov
er a
Trans
onic
Lami
nar W
ing
Secti
onR.
Sema
an, P
. Sch
olz, Y
. El-S
ayed
, Te
chnic
al Un
iversi
ty of
Brau
nsch
weig,
Br
auns
chwe
ig, G
erman
y
1600
hrs
AIAA-2
013-2
814
Spat
ial op
timal
grow
th of
Gö
rtler
vorti
ces i
n tw
o-dim
ensio
nal c
ompr
essib
le bo
unda
ry la
yers
J. Lu
cas,
O. Ve
rmee
rsch,
D. Ar
nal,
ONER
A, To
ulous
e, Fra
nce
1630
hrs
AIAA-2
013-2
815
Comp
rehe
nsive
Stud
y of t
he
Flow
Arou
nd a
Simpli
fied
Orion
Caps
ule M
odel
J. Ro
ss, J.
Hein
eck,
N. B
urnsid
e, NA
SA Am
es Re
searc
h Cen
ter, M
offett
Fie
ld, CA
; M. S
ellers
, Aero
spac
e Te
sting
Allia
nce,
Arnold
AFB,
TN; N
. Ha
lcomb
, T. G
arbeff
, G. Y
amau
chi,
L. Ku
shne
r, NAS
A Ame
s Res
earch
Ce
nter, M
offett
Field
, CA
Tues
day,
25 Ju
ne 2
013
89-A
PA-2
2/FD
-22
Low
Spee
d, Lo
w Re
ynold
s Num
ber A
erod
ynam
ics II
Exec
utive
Conf
eren
ce 1
Chair
ed by
: A. A
HMED
, Aub
urn U
nivers
ity an
d J. M
URRA
Y, Sa
ndia
Natio
nal L
abora
tories
1430
hrs
AIAA-2
013-2
816
An Ex
perim
enta
l Stu
dy
of D
ynam
ic Tra
iling E
dge
Defle
ction
s on
a Two
Di
mens
ional
Trans
lating
Wing
Y. Liu
, B. C
heng
, X. D
eng,
Purdu
e Un
iversi
ty, W
est L
afaye
tte, I
N
1500
hrs
AIAA-2
013-2
817
Expe
rimen
tal S
tudy
of
Flow
over
Two O
scilla
tory
Pit
ching
Airf
oils i
n Ta
ndem
Co
nfigu
ratio
nA.
Bin Az
ry Se
et, H
. Tan
g, S.
Yu
Ching
Man
, Nan
yang
Tech
nolog
ical
Unive
rsity,
Sing
apore
, Sing
apore
1530
hrs
AIAA-2
013-2
818
Meas
urem
ents
of th
e Thr
ee-
Dime
nsion
al To
polog
ical
Evolu
tion
of a
Dyna
mic S
tall
Even
t Usin
g Wav
elet M
ethod
sA.
Buch
ner, J
. Sori
a, Mo
nash
Un
iversi
ty, M
elbou
rne, A
ustra
lia
1600
hrs
AIAA-2
013-2
819
Mode
ling o
f 2D
Unste
ady
Motio
n of
a Fla
t Plat
e usin
g Po
tentia
l Flow
X. X
ia, K.
Moh
seni,
Univ
ersity
of
Florid
a, Ga
inesv
ille, G
aines
ville,
FL
1630
hrs
AIAA-2
013-2
820
BiGl
obal
and P
oint V
ortex
Me
thod
s for
the I
nsta
bility
An
alysis
of W
akes
J. Te
ndero
Venta
nas,
P. Pa
redes
, Te
chnic
al Un
iversi
ty of
Madri
d, Ma
drid,
Spain
; M. R
oura
Sués
, Ga
mesa
Corpo
ration
, Mad
rid, S
pain;
R.
Govin
daraj
an, T
ata In
stitut
e of
Fund
amen
tal Re
searc
h, Hy
derab
ad,
India;
V. Th
eofili
s, Te
chnic
al Un
iversi
ty of
Madri
d, Ma
drid,
Spain
1700
hrs
AIAA-2
013-2
821
Later
Stag
es of
Tran
sition
over
a N
ACA
0018
Airf
oil at
Low
Reyn
olds N
umbe
rsT.
Kirk,
S. Ya
rusev
ych,
Unive
rsity
of Wa
terloo
, Wate
rloo,
Cana
da
53
Tues
day,
25 Ju
ne 2
013
90-A
PA-2
3We
apon
s Aer
odyn
amics
and S
tore
Sepa
ratio
nEx
ecut
ive Co
nfer
ence
4Ch
aired
by: J
. DES
PIRITO
, US
Army R
esea
rch La
borat
ory an
d K. B
REKK
E, Sa
ndia
Natio
nal L
abs
1430
hrs
AIAA-2
013-2
822
Towa
rds a
Redu
ced-O
rder
Mo
del fo
r Ung
uided
Proje
ctile
Trajec
tories
in M
ultipl
e-Bod
y Hi
gh-Sp
eed A
ir-Deli
vered
Sy
stems
R. Ha
rris, P.
Lieve
r, CFD
Resea
rch
Corpo
ration
, Hun
tsville
, AL;
E. Lu
ke,
Missi
ssipp
i Stat
e Univ
ersity,
Miss
issipp
i Sta
te, M
S; J.
Dudle
y, Air
Force
Resea
rch
Labo
ratory
, Eglin
AFB,
FL
1500
hrs
AIAA-2
013-2
823
An En
ginee
ring M
ethod
for V
ery
Low
Aspe
ct Ra
tio Cr
ucifo
rm W
ing-
Body
Confi
gura
tions
S. Tul
ing, C
ounci
l for S
cienti
fic an
d Ind
ustria
l Rese
arch,
Pretor
ia, So
uth
Africa
; L. D
ala, U
nivers
ity of
the
Witw
atersr
and,
Johan
nesbu
rg, So
uth
Africa
; C. T
oome
r, Univ
ersity
of th
e West
of
Engla
nd, B
ristol,
Unite
d King
dom
Tues
day,
25 Ju
ne 2
013
91-A
SE-6
Swep
t-Wing
Icing
Room
515
Chair
ed by
: D. M
ARCO
TTE a
nd J.
TSAO
, Ohio
Aeros
pace
Insti
tute
1430
hrs
AIAA-2
013-2
824
Swep
t-Wing
Ice A
ccreti
on
Char
acter
izatio
n and
Ae
rody
nami
csA.
Broere
n, M.
Potap
czuk,
NASA
Glen
n Re
search
Cente
r, Clev
eland
, OH;
J. Ril
ey,
Fede
ral Av
iation
Admi
nistra
tion,
Atlan
tic
City A
irport
, NJ;
P. Ville
dieu,
ONER
A, Tou
louse,
Fran
ce; F.
Moen
s, ON
ERA,
Meud
on, F
rance;
M. B
ragg,
Unive
rsity o
f Illin
ois, U
rbana
-Cham
paign
, Urba
na, IL
1500
hrs
AIAA-2
013-2
825
Aero
dyna
mic C
lassifi
catio
n of
Sw
ept-W
ing Ic
e Accr
etion
J. Die
bold,
Univ
ersity
of Ill
inois,
Ur
bana
-Cham
paign
, Urba
na, I
L; A.
Broe
ren, N
ASA G
lenn R
esea
rch
Cente
r, Clev
eland
, OH;
M. B
ragg,
Unive
rsity
of Illi
nois,
Urba
na-
Cham
paign
, Urba
na, I
L
1530
hrs
AIAA-2
013-2
826
A Hy
brid
Airfo
il Des
ign M
ethod
fo
r Icin
g Wind
Tunn
el Te
stsG.
Fujiw
ara, B
. Woo
dard,
B. W
iberg,
A.
Morto
nson
, M. B
ragg,
Unive
rsity
of Illi
nois,
Urba
na-Ch
ampa
ign,
Urba
na, I
L
Tues
day,
25 Ju
ne 2
013
92-A
SE-7
Spac
ecra
ft Ch
argin
g in
the E
arth
and L
unar
Syste
msRo
om 5
18Ch
aired
by: D
. FER
GUSO
N, Ai
r Forc
e Res
each
Labo
ratory
1430
hrs
AIAA-2
013-2
827
Comp
rehe
nsive
Theo
retic
al Fr
amew
ork
for M
odeli
ng
Dive
rse El
ectro
n Tra
nspo
rt Ex
perim
ents
in Pa
ralle
l Plat
e Ge
ometr
iesA.
Sim, I
rvine
Valle
y Coll
ege,
Irvine
, CA;
J. De
nniso
n, Ut
ah S
tate
Unive
rsity,
Loga
n, UT
1500
hrs
AIAA-2
013-2
828
On th
e Fea
sibilit
y of D
etecti
ng
Spac
ecra
ft Ch
argin
g and
Arci
ng
by R
emot
e Sen
sing
D. Fe
rguso
n, Air
Force
Rese
arch
Labo
ratory
, Kirtl
and A
FB, N
M; J.
De
nniso
n, Ut
ah S
tate U
nivers
ity,
Loga
n, UT
; J. M
urray
-Krez
an, A
ir Fo
rce Re
searc
h Lab
orator
y, Kir
tland
AF
B, N
M; S
. Greg
ory, T
he B
oeing
Co
mpan
y, Alb
uque
rque,
NM
1530
hrs
AIAA-2
013-2
829
Labo
rato
ry In
vesti
gatio
ns
of Lu
nar S
imula
nt Su
rface
Ch
argin
gJ.
Polan
sky,
J. Wa
ng, U
nivers
ity of
So
uthern
Califo
rnia,
Los A
ngele
s, CA
54
Tues
day,
25 Ju
ne 2
013
93-C
FD-2
2Hi
gh-O
rder
Meth
ods I
VNa
utilu
s 5Ch
aired
by: D
. ZIN
GG, U
nivers
ity of
Toron
to an
d P. P
ERSS
ON14
30 hr
sAIA
A-201
3-283
0No
dal P
oints
and t
he N
onlin
ear
Stabil
ity of
High
-Ord
er
Meth
ods f
or U
nstea
dy Fl
ow
Prob
lems o
n Te
trahe
dral
Mesh
esD.
Willi
ams,
A. Ja
meso
n, St
anfor
d Un
iversi
ty, S
tanfor
d, CA
1500
hrs
AIAA-2
013-2
831
High
-Ord
er Im
plicit
Temp
oral
Integ
ratio
n fo
r Uns
teady
Co
mpre
ssible
Fluid
Flow
Sim
ulatio
nP.
Boom
, D. Z
ingg,
Unive
rsity
of To
ronto,
Toron
to, Ca
nada
1530
hrs
AIAA-2
013-2
832
High
-Ord
er So
lution
of
Visco
elasti
c Flui
d Flow
s Usin
g Un
struc
ture
d Disc
ontin
uous
Ga
lerkin
Meth
odA.
Nejat
, Univ
ersity
of Te
hran,
Tehra
n, Ira
n
1600
hrs
AIAA-2
013-2
833
A Di
scont
inuou
s Gale
rkin
Meth
od fo
r the
Nav
ier-S
toke
s Eq
uatio
ns on
Def
ormi
ng
Doma
ins u
sing U
nstru
cture
d Mo
ving S
pace
-Time
Mes
hes
L. Wa
ng, P
. Pers
son,
Unive
rsity
of Ca
liforni
a, Be
rkeley
, Berk
eley,
CA
1630
hrs
AIAA-2
013-2
834
The S
BP-S
AT Te
chniq
ue fo
r Tim
e-Di
screti
zatio
nT.
Lund
quist
, J. N
ordstr
om, L
inköp
ing
Unive
rsity,
Link
öping
, Swe
den
Tues
day,
25 Ju
ne 2
013
94-C
FD-2
3Hi
gh-S
peed
and C
hemi
cally
Rea
cting
Flow
s II
Naut
ilus 4
Chair
ed by
: M. M
ACLE
AN, C
UBRC
1430
hrs
AIAA-2
013-2
835
Para
llel C
ompr
essib
le So
lver
for U
nstea
dy Tu
rbule
nt
Comb
ustio
n in
Rock
et In
jecto
rs Us
ing Fl
amele
t Mod
elsS.
Thak
ur, J.
Wrig
ht, S
tream
line
Nume
rics,
Inc.,
Gaine
sville
, FL;
M.
Ihme,
Stan
ford U
nivers
ity, S
tanfor
d, CA
1500
hrs
AIAA-2
013-2
836
Meas
urem
ents
in Re
gions
of
Shoc
k Wa
ve/T
urbu
lent
Boun
dary
Laye
r Int
erac
tion
from
Mach
4 to
10
for O
pen
and “
Blind
” Cod
e Eva
luatio
n/Va
lidat
ionM.
Hold
en, T
. Wad
hams
, M.
MacLe
an, C
UBRC
, Buff
alo, N
Y
1530
hrs
AIAA-2
013-2
837
Meas
urem
ents
of Re
al Ga
s Eff
ects o
n Reg
ions o
f Lam
inar
Shoc
k Wav
e/Bo
unda
ry La
yer
Intera
ction
in H
yper
veloc
ity
Flows
for “
Blind
’ Cod
e Vali
datio
n Stu
dies
M. Ho
lden,
T. Wa
dham
s, M.
MacL
ean,
A. Du
frene
, CUB
RC, B
uffalo
, NY
1600
hrs
AIAA-2
013-2
838
Flow
Disto
rtion
: Com
puta
tiona
l In
vesti
gatio
n of
a Sh
ocke
d Ca
vity F
lameh
older
R. Mi
lligan
, J. B
oles,
Taite
ch, I
nc.,
Beav
ercree
k, OH
; M. H
agen
maier
, J.
Donb
ar, C.
Carte
r, Air F
orce R
esea
rch
Labo
ratory
, Wrig
ht-Pa
tterso
n AFB
, OH
; K. H
su, I
nnov
ative
Scie
ntific
So
lution
s, Inc
., Da
yton,
OH
Tues
day,
25 Ju
ne 2
013
95-C
FD-2
4La
rge-
Eddy
Simu
lation
(LES
), Di
rect
Nume
rical
Simula
tion
(DNS
), an
d Hyb
rid R
ANS/
LES M
ethod
s ISe
abre
eze I
Chair
ed by
: M. C
HOUD
HARI,
NAS
A-Lan
gley R
esea
rch Ce
nter a
nd L.
DUA
N, N
ation
al Ins
titute
of Ae
rospa
ce14
30 hr
sAIA
A-201
3-283
9Ch
arac
teriza
tion o
f the
Cavit
y Sh
ear L
ayer
of the
Stra
tosph
eric
Obser
vator
y For
Infra
red
Astro
nomy
by M
eans
of Pr
essur
e Se
nsor
Data
and a
Hyb
rid RA
NS-
LES S
tudy
C. En
gfer, T
. Lutz
, E. K
raeme
r, Univ
ersity
of
Stuttg
art, S
tuttga
rt, Ge
rman
y
1500
hrs
AIAA-2
013-2
840
A Sim
ple A
ltern
ative
to
Unste
ady S
tress-
Flux
RANS
/LE
S Mod
elsC.
Wink
ler, A
. Dorg
an, M
. Man
i, The
Bo
eing C
ompa
ny, S
t. Lo
uis, M
O
1530
hrs
AIAA-2
013-2
841
Lesso
ns Le
arne
d fro
m Hy
brid
RANS
-LES C
ompu
tatio
ns of
a Th
ree-
Eleme
nt A
irfoil
Flow
S. Pe
ng, S
wedis
h Defe
nse R
esea
rch
Agen
cy (F
OI),
Stoc
kholm
, Swe
den;
B. N
eben
fuhr, L
. Dav
idson
, Cha
lmers
Un
iversi
ty of
Tech
nolog
y, Gö
teborg
, Sw
eden
1600
hrs
AIAA-2
013-2
842
Simula
tion
of Sw
ept-W
ing
Rece
ptivi
ty to
Dist
ribut
ed
Roug
hnes
sV.
Mistr
y, G.
Page
, J. M
cGuir
k, Lo
ughb
oroug
h Univ
ersity
, Lo
ughb
oroug
h, Un
ited K
ingdo
m
1630
hrs
AIAA-2
013-2
843
LES o
f High
Spee
d Jet
Flow
From
Conv
erge
nt-D
iverg
ent
Recta
ngula
r S-b
end D
ucts
Using
Synt
hetic
Inlet
Cond
itions
T. Co
ates,
G. Pa
ge, L
ough
borou
gh
Unive
rsity,
Loug
hboro
ugh,
Unite
d Kin
gdom
1700
hrs
AIAA-2
013-2
844
Char
acter
izatio
n of
Shar
p-Ed
ged A
irfoil
s Usin
g Lar
ge
Eddy
Simu
lation
s (LE
S)K.
Shale
r, D. G
aiton
de, O
hio S
tate
Unive
rsity,
Colum
bus,
OH
55
Tues
day,
25 Ju
ne 2
013
96-C
FD-2
5De
sign
Optim
izatio
n Te
chniq
ues I
IISp
inake
r ICh
aired
by: K
. FID
KOW
SKI,
Unive
rsity
of Mi
chiga
n and
Q. W
ANG,
MIT
1430
hrs
AIAA-2
013-2
845
Cons
tructi
on of
Par
ametr
ically
-Ro
bust
CFD-
Base
d Red
uced
-Or
der M
odels
for P
DE-
Cons
traine
d Opt
imiza
tion
M. Za
hr, D
. Ams
allem
, C. F
arhat,
St
anfor
d Univ
ersity
, Stan
ford,
CA
1500
hrs
AIAA-2
013-2
846
Impa
ct of
Turb
ulenc
e Clos
ures
an
d Num
erica
l Erro
rs for
the
Optim
izatio
n of F
low Co
ntrol
Devic
esJ.
Labro
quère
, R. D
uvign
eau,
French
Na
tiona
l Instit
ute fo
r Rese
arch i
n Co
mpute
r Scie
nce an
d Con
trol (I
NRIA)
, So
phia
Antip
olis, F
rance;
E. Gu
ilmine
au,
Natio
nal C
enter
for S
cienti
fic Re
search
(C
NRS)
, Nan
tes, F
rance
1530
hrs
AIAA-2
013-2
847
Effic
ient C
AD-b
ased
Ae
rody
nami
c Des
ign
Optim
izatio
n wi
th A
djoint
CFD
Data
P. Th
omps
on, T
. Rob
inson
, C.
Armstr
ong,
Quee
n’s U
nivers
ity
Belfa
st, B
elfas
t, Un
ited K
ingdo
m
1600
hrs
AIAA-2
013-2
848
Adjoi
nt-B
ased
Opt
imiza
tion
of
Flapp
ing K
inema
tics i
n Vis
cous
Flo
wsM.
van S
chroj
enste
in La
ntman
, Un
iversi
ty of
Twen
te, En
sched
e, Th
e Ne
therla
nds;
K. Fid
kows
ki, U
nivers
ity
of Mi
chiga
n, An
n Arbo
r, Ann
Arbo
r, MI
1630
hrs
AIAA-2
013-2
849
Unste
ady A
ero-
Struc
ture
Co
upled
Adjo
int M
ethod
for
Flutte
r Sup
pres
sion
Z. Zh
ang,
P. Ch
en, S
. Yan
g, Z.
Wang
, ZO
NA Te
chno
logy,
Inc.,
Scott
sdale
, AZ
; Q. W
ang,
Massa
chus
etts I
nstitu
te of
Tech
nolog
y, Ca
mbrid
ge, M
A
1700
hrs
AIAA-2
013-2
850
Geom
etry G
ener
ation
of
Comp
lex U
ncon
vent
ional
Aircr
aft w
ith A
pplic
ation
to
High
-Fide
lity A
erod
ynam
ic Sh
ape O
ptim
izatio
nH.
Gag
non,
D. Zi
ngg,
Unive
rsity
of To
ronto,
Toron
to, Ca
nada
1730
hrs
AIAA-2
013-2
851
Aero
dyna
mic D
esign
Op
timiza
tion
of Th
ree
Dime
nsion
al Ro
cket
Nozz
les
Using
Adjo
int M
ethod
S. Ey
i, Midd
le Ea
st Te
chnic
al Un
iversi
ty, An
kara,
Turke
y; M.
Yu
musa
k, RO
KETS
AN M
issile
Ind
ustrie
s, Inc
., An
kara,
Turke
y
Tues
day,
25 Ju
ne 2
013
97-C
FD-2
6Pa
ralle
l Com
putin
gMa
rina 5
Chair
ed by
: J. B
AEDE
R, Un
iversi
ty of
Maryl
and
1430
hrs
AIAA-2
013-2
852
On th
e Ach
ievab
le Sp
eeds
of
Finite
Diff
erenc
e Solv
ers on
CPUs
an
d GPU
sR.
Lohn
er, Ge
orge M
ason U
nivers
ity,
Fairfa
x, VA
; A. C
orriga
n, Na
val R
esearc
h La
borat
ory, W
ashing
ton, D
C; K.
Wichm
ann,
W. W
all, Te
chnica
l Univ
ersity
of
Munic
h, Mu
nich,
Germ
any
1500
hrs
AIAA-2
013-2
853
Mode
ling t
he Tw
o-ph
ase
flowfi
eld be
neat
h a H
over
ing
Roto
r on
Grap
hics P
roce
ssing
Un
its us
ing a
FVM-
RANS
Hyb
rid
Meth
odolo
gyS.
Thom
as, J
. Bae
der, U
nivers
ity
of Ma
rylan
d, Co
llege
Park,
Colle
ge
Park,
MD
1530
hrs
AIAA-2
013-2
854
Para
llel S
emi-M
eshle
ss Ste
ncil
Selec
tion
for M
oving
Geo
metry
Sim
ulatio
nsJ.
Angu
lo, D
. Ken
nett,
S. T
imme
, K.
Badc
ock,
Unive
rsity
of Liv
erpoo
l, Liv
erpoo
l, Unit
ed Ki
ngdo
m
1600
hrs
AIAA-2
013-2
855
A Hy
brid
Multi-
GPU/
CPU
Comp
utat
ional
Fram
ewor
k fo
r Rot
orcra
ft Flo
ws on
Un
struc
ture
d Ove
rset G
rids
D. Ch
anda
r, J. S
itaram
an, D
. Ma
vripli
s, Un
iversi
ty of
Wyo
ming
, La
ramie,
Laram
ie, W
Y
1630
hrs
AIAA-2
013-2
856
Load
Bala
ncing
for
Multip
hysic
sR.
Lohn
er, G
eorge
Mas
on U
nivers
ity,
Fairfa
x, VA
; J. B
aum,
SAIC
, McLe
an,
VA
Tues
day,
25 Ju
ne 2
013
98-C
FD-2
7Un
stead
y Flow
s ISe
abre
eze I
ICh
aired
by: X
. WAN
G, N
ASA G
lenn R
esea
rch Ce
nter a
nd F.
FERG
USON
1430
hrs
AIAA-2
013-2
857
Unste
ady F
low Si
mulat
ion
arou
nd Cy
linde
r und
er A
irfoil
us
ing Ca
rtesia
n-ba
sed F
low
Solve
rT.
Imam
ura, Y
. Tak
ahas
hi, U
nivers
ity
of To
kyo,
Toky
o, Ja
pan
1500
hrs
AIAA-2
013-2
859
A Fin
ite Vo
lume M
odel
For
Simula
ting t
he U
nstea
dy
Navie
r-Sto
kes E
quat
ions U
nder
Sp
ace T
ime C
onse
rvat
ions
F. Fe
rguso
n, N.
Das
que,
M. D
hana
sar,
North
Carol
ina A&
T Stat
e Univ
ersity
, Gr
eens
boro,
NC
1530
hrs
AIAA-2
013-2
860
The S
hock
Tube
Pro
blem
from
a Com
bined
Expe
rimen
tal a
nd
Comp
utat
ional
Persp
ectiv
eD.
Huy
nh, O
hio S
tate U
nivers
ity,
Colum
bus,
OH
1600
hrs
AIAA-2
013-2
861
A Tim
e-Sp
ectra
l Hyb
ridiza
ble
Disco
ntinu
ous G
alerk
in Me
thod
fo
r Per
iodic
Flow
Prob
lems
H. Ch
auras
ia, C.
Ngu
yen,
J. Pe
raire,
Mas
sach
usett
s Ins
titute
of Te
chno
logy,
Camb
ridge
, MA
1630
hrs
AIAA-2
013-2
862
Prac
tical
Larg
e-Edd
y Sim
ulatio
n for
Comp
lex Tu
rbule
nt Flo
wfield
wi
th Ad
aptiv
e Car
tesian
Mesh
and
Data
Comp
ressio
n Tech
nique
R. Sa
kai, S
. Oba
yashi
, Toh
oku
Unive
rsity,
Send
ai, Ja
pan;
Y. Ma
tsuo,
K. Na
kaha
shi, J
apan
Aeros
pace
Explo
ration
Ag
ency
(JAXA
), Ch
ofu, J
apan
56
Tues
day,
25 Ju
ne 2
013
99-C
FD-2
8So
lution
Ada
ptive
Grid
Tech
nique
s II/
GPU
Comp
uting
Room
514
Chair
ed by
: R. H
ARRIS
and B
. WILL
IAMS,
CFD
Rese
arch C
orpora
tion
1430
hrs
AIAA-2
013-2
863
GPU
Acce
lerat
ed K
inetic
So
lvers
for R
arefi
ed G
as
Dyna
mics
V. Ko
lobov
, CFD
Rese
arch
Corpo
ration
, Hun
tsville
, AL
1500
hrs
AIAA-2
013-2
864
Comp
utat
ion of
Tu
rbom
achin
ery F
lows w
ith
a Par
allel
Unstr
uctu
red M
esh
Navie
r-Sto
kes e
quat
ions S
olver
on
GPU
sF.
Gisbe
rt, R.
Corra
l, ITP,
Mad
rid,
Spain
; J. P
uebla
s, Te
chnic
al Un
iversi
ty of
Madri
d, Ma
drid,
Spain
1530
hrs
AIAA-2
013-2
865
Adjoi
nt an
d Tru
ncat
ion Er
ror
Base
d Ada
ptat
ion fo
r 1D
Finite
Vo
lume S
chem
esJ.
Derla
ga, C
. Roy
, Virg
inia
Polyt
echn
ic Ins
titute
and S
tate
Unive
rsity,
Blac
ksbu
rg, VA
1600
hrs
AIAA-2
013-2
866
Vent
us: A
n Ov
erse
t Ada
ptive
Ca
rtesia
n Sim
ulatio
n Fr
amew
ork
for M
oving
Bo
unda
ry P
roble
msR.
Harris
, B. W
illiam
s, Se
lf, Hu
ntsvil
le, AL
1630
hrs
AIAA-2
013-2
867
Adap
tive S
hape
Para
meter
(A
SP) T
echniq
ue fo
r Loc
al Ra
dial
Basis
Func
tions
(RBF
s) an
d The
ir Ap
plica
tion f
or So
lution
of N
avier
-Sto
kes E
quati
ons
A. Jav
ed, K
. Djidj
eli, Un
iversit
y of
South
ampto
n, So
utham
pton,
Unite
d Kin
gdom
Tues
day,
25 Ju
ne 2
013
100-
CFD-
29/F
D-23
Revo
lution
ary C
ompu
tatio
nal A
eros
cienc
es (R
CA) -
II (I
nvite
d)Na
utilu
s 2Ch
aired
by: M
. MAL
IK, N
ASA-L
angle
y Res
earch
Cente
r and
M. R
OGER
S, N
ASA A
mes R
esea
rch Ce
nter
1430
hrs
Oral
Presen
tation
(Inv
ited)
Vision
2030
CFD
Code
Stu
dy: D
efinin
g the
Path
for
Revo
lution
ary C
ompu
tation
al Ae
rosci
ences
J. Slo
tnick,
A. Kh
odad
oust,
The B
oeing
Co
mpan
y, Hu
nting
ton Be
ach, C
A; J.
Alonso
, Stan
ford U
nivers
ity, St
anfor
d, CA
; D.
Darm
ofal, M
assach
usetts
Instit
ute of
Tec
hnolo
gy, Ca
mbrid
ge, M
A; W.
Grop
p, Un
iversit
y of Il
linois,
Urban
a-Cha
mpaig
n, Urb
ana,
IL; E.
Lurie
, Prat
t & W
hitne
y, Ea
st Ha
rtford,
CT; D
. Mav
riplis,
Unive
rsity
of Wy
oming
, Lara
mie,
Laram
ie, W
Y
1500
hrs
AIAA-2
013-2
868
High
-Ord
er En
tropy
Sta
ble Fo
rmula
tions
for
Comp
utat
ional
Fluid
Dyna
mics
M. Ca
rpente
r, NAS
A Lan
gley
Rese
arch C
enter
, Ham
pton,
VA; T
. Fis
her, S
andia
Nati
onal
Labo
ratori
es,
Albuq
uerqu
e, NM
1530
hrs
AIAA-2
013-2
869
Adjoi
nt B
ased
Anis
otro
pic M
esh
Adap
tatio
n fo
r the
CPR
Meth
odL.
Shi, Z
. Wan
g, Un
iversi
ty of
Kans
as,
Lawr
ence
, Law
rence
, KS
1600
hrs
AIAA-2
013-2
870
Desig
n of
a Va
riatio
nal
Multis
cale
Meth
od fo
r Hi
gh R
eyno
lds N
umbe
r Co
mpre
ssible
Flow
sL.
Diosa
dy, S
. Murm
an, N
ASA A
mes
Rese
arch C
enter
, Moff
ett Fi
eld, C
A
1630
hrs
AIAA-2
013-2
871
Prog
ress
Towa
rds a
High
er-
orde
r Ada
ptive
Solve
r for
Ae
rody
nami
csD.
Darm
ofal, S
. Allm
aras,
M.
Yano
, Mas
sach
usett
s Ins
titute
of Te
chno
logy,
Camb
ridge
, MA
1700
hrs
AIAA-2
013-2
872
High
-ord
er pr
ovab
ly sta
ble
over
set g
rid m
ethod
s for
blo
ck-st
ructu
red a
dapt
ive m
esh
refin
emen
tN.
Sha
ran, D
. Bod
ony,
Unive
rsity
of Illi
nois,
Urba
na-Ch
ampa
ign,
Urba
na, I
L
Tues
day,
25 Ju
ne 2
013
101-
FD-2
4Vo
rtex
Flow
and V
ortic
al Str
uctu
res
Room
511
Chair
ed by
: W. L
OUISO
S, U
nivers
ity of
Verm
ont
1430
hrs
AIAA-2
013-2
873
Expe
rimen
tal M
easu
reme
nts
of Co
nvec
tive M
ass T
rans
fer
from
a Sur
face
Due
to a
Boun
d Vo
rtex
Flow
N. Va
chon
, D. H
itt, U
nivers
ity of
Ve
rmon
t, Bu
rlingto
n, Bu
rlingto
n, VT
1500
hrs
AIAA-2
013-2
874
The I
nter
actio
n of
Hyp
erbo
lic
and S
hear
Stre
tching
in
Geop
hysic
al Vo
rtex
Flows
D. Li
pinsk
i, K. M
ohse
ni, U
nivers
ity of
Flo
rida,
Gaine
sville
, Gain
esvil
le, FL
1530
hrs
AIAA-2
013-2
875
Vorte
x inte
racti
ons w
ith a
high-l
ift
airfoi
l in a
low sp
eed w
ind tu
nnel
D. Ha
hn, S
. Klein
, P. Sc
holz,
R.
Rade
spiel,
Techn
ical U
nivers
ity of
Bra
unsch
weig,
Brau
nschw
eig, G
erman
y
1600
hrs
AIAA-2
013-2
876
Casca
ding o
f Vor
tical
Struc
ture
s an
d Tra
nsitio
n to
Turb
ulenc
eV.
Katta
, Inn
ovati
ve S
cienti
fic
Solut
ions,
Inc.,
Dayto
n, OH
; W.
Roqu
emore
, Air F
orce R
esea
rch
Labo
ratory
, Wrig
ht-Pa
tterso
n AFB
, OH
1630
hrs
AIAA-2
013-2
877
Statio
nary
and T
rave
ling
Vorti
cal S
tructu
res o
n Sw
ept
Cylin
ders
and T
urbin
e Blad
esJ.
Goste
low, A
. Ron
a, S.
Garr
ett, W
. Mc
Mulla
n, Un
iversi
ty of
Leice
ster,
Leice
ster, U
nited
King
dom
57
Tues
day,
25 Ju
ne 2
013
102-
FD-2
5Hi
gh-S
peed
Tran
sition
: Mod
eling
Naut
ilus 1
Chair
ed by
: V. T
HEOF
ILIS,
Univ
ersida
d Poli
técnic
a de M
adrid
and A
. FED
EROV
1430
hrs
AIAA-2
013-2
879
Insta
bilitie
s on
a Hyp
erso
nic
Yawe
d Stra
ight C
one
E. Pe
rez, T
. Koc
ian, N
. Oliv
iero,
J. Ku
ehl, H
. Ree
d, Te
xas A
&M
Unive
rsity,
Colle
ge S
tation
, TX
1500
hrs
AIAA-2
013-2
880
Spat
ial lin
ear g
lobal
insta
bility
an
alysis
of th
e HIFi
RE-5
ellip
tic
cone
mod
el flo
wP.
Pared
es, V
. The
ofilis,
Tech
nical
Unive
rsity
of Ma
drid,
Madri
d, Sp
ain
1530
hrs
AIAA-2
013-2
881
Effect
of lo
cal v
olume
energ
y su
pply
on hi
gh-sp
eed b
ound
ary
layer
stabil
ityV.
Soud
akov,
TsAG
I, Zhu
kovsk
y, Ru
ssia;
A. Fe
dorov
, Mosc
ow In
stitute
of Ph
ysics
and T
echno
logy,
Zhuk
ovsky
, Russ
ia; A.
Ry
zhov,
TsAG
I, Zhu
kovsk
y, Ru
ssia
1600
hrs
AIAA-2
013-2
882
Stabil
ity an
d rec
eptiv
ity of
hig
h sp
eed b
ound
ary l
ayer
s in
oxyg
enJ.
Klentz
man,
A. Tu
min,
Unive
rsity
of Ari
zona
, Tuc
son,
Tucso
n, AZ
1630
hrs
AIAA-2
013-2
883
Statis
tical
inver
se an
alysis
an
d sto
chas
tic m
odeli
ng of
tra
nsitio
nG.
Seri
no, T
. Mag
in, P.
Ramb
aud,
F. Pin
na, v
on Ká
rmán
Insti
tute f
or Flu
id Dy
nami
cs, Rh
ode-S
aint-G
enès
e, Be
lgium
Tues
day,
25 Ju
ne 2
013
103-
PDL-6
Plasm
a-Ba
sed F
low Co
ntro
lMa
rina 6
Chair
ed by
: J. D
RAKE
S, Ae
rojet
and K
. KRE
MEYE
R, PM
& AM
Rese
arch
1430
hrs
AIAA-2
013-2
884
Multip
le En
caps
ulated
Elect
rode
Pla
sma A
ctuato
r Effe
ct on
Ae
rofoi
l-Wak
e Inte
racti
onR.
Erfan
i, Man
cheste
r Metr
opolit
an
Unive
rsity,
Manch
ester,
Unite
d King
dom;
T.
Erfan
i, Univ
ersity
Colleg
e Lon
don,
Lond
on, U
nited
King
dom;
K. Ko
ntis,
H.
Zare-
behta
sh, M
anche
ster U
nivers
ity,
Manch
ester,
Unite
d King
dom
1500
hrs
AIAA-2
013-2
885
Expe
rimen
tal I
nves
tigat
ion
of P
ulsed
Diel
ectri
c Bar
rier
Disch
arge
Actu
ator
s in
Sub-
an
d Tra
nson
ic Flo
wP.
Pesch
ke, S
. Goe
kce,
P. Le
yland
, P.
Ott,
C. Ho
llens
tein,
Swiss
Fede
ral
Institu
te of
Tech
nolog
y, La
usan
ne,
Switz
erlan
d
1530
hrs
AIAA-2
013-2
886
Expe
rimen
tal C
hara
cteriz
ation
of
the R
ailPA
c Plas
ma Fl
ow
Actu
ator
J. Sir
ohi, B
. Paff
ord, L
. Raja
, Un
iversi
ty of
Texa
s, Au
stin,
Austi
n, TX
1600
hrs
AIAA-2
013-2
887
Effe
ct of
Plas
ma Fl
ow Co
ntro
l on
Low
Reyn
olds N
umbe
r Ai
rfoil a
nd Fl
ying W
ing
Perfo
rman
ceB.
Goe
ksel,
I. Re
chen
berg,
F.
Behre
ndt,
C. Pa
schere
it, Te
chnic
al Un
iversi
ty of
Berlin
, Berl
in, G
erman
y
1630
hrs
AIAA-2
013-2
888
Effect
s of e
xtern
al cir
cuit o
n DBD
pla
sma a
ctuato
r ope
ratio
nA.
Likha
nskii,
S. Zh
ou, T
ech-X
Corpo
ration
, Bou
lder, C
O; M
. Shn
eider,
Pri
nceton
Unive
rsity,
Prince
ton, N
J; D.
As
hpis,
NASA
Glen
n Rese
arch C
enter
, Cle
velan
d, OH
; M. L
aun,
Sierra
Lobo
, Inc
., Clev
eland
, OH
Tues
day,
25 Ju
ne 2
013
104-
PDL-7
MHD
for P
ower
Gen
erat
ion/R
adio
Blac
kout
Mitig
ation
Exec
utive
Conf
eren
ce 2
ACh
aired
by: M
. KIM
, nive
rsity
of Ad
elaide
and M
. WHI
TE14
30 hr
sAIA
A-201
3-288
9Ex
perim
ents
of H
igh
Temp
erat
ure I
nert
Gas P
lasma
MH
D Po
wer G
ener
ation
with
a Fa
rada
y Typ
e Gen
erat
orM.
Tana
ka, Y
. Zhu
ang,
F. Ko
matsu
, T.
Murak
ami, Y
. Oku
no, T
okyo
Insti
tute
of Te
chno
logy,
Yoko
hama
, Jap
an
1500
hrs
AIAA-2
013-2
890
Study
of In
fluen
ce of
Electr
odes
Ar
rang
emen
t for
Fara
day T
ype
MHD
Gene
rator
and C
oal P
ower
Cy
cle An
alysis
with
CO2 R
ecove
ryH.
Watan
abe,
T. Fu
jino, M
. Ishik
awa,
Unive
rsity o
f Tsuk
uba,
Tsuku
ba, J
apan
1530
hrs
AIAA-2
013-2
891
Influe
nce o
f Cro
ss-sec
tiona
l Sha
pe
on G
enera
tor Pe
rform
ance
and
Electr
omag
netic
Fluid
Phen
omen
a of
DCW-
MHD
Gene
rator
s for
Hy
perso
nic Ai
rplan
esY.
Tamad
a, N.
Niw
a, T.
Takah
ashi,
T. Fu
jino, M
. Ishik
awa,
Unive
rsity o
f Tsu
kuba
, Tsuk
uba,
Japan
1600
hrs
AIAA-2
013-2
892
Inve
stiga
ting t
he Fe
asibi
lity of
Ele
ctron
Man
ipulat
ion Sc
heme
us
ing a
Cold
Atmo
sphe
ric
Plasm
a Jet
M. Ki
m, U
nivers
ity of
Adela
ide,
Adela
ide, A
ustra
lia
58
Tues
day,
25 Ju
ne 2
013
105-
TP-9
Comp
utat
ional
Heat
Tran
sfer a
nd Si
mulat
ions
Exec
utive
Conf
eren
ce 3
BCh
aired
by: A
. SUR
ESH,
GE a
nd N
. MAN
SOUR
, NAS
A-Ame
s14
30 hr
sAIA
A-201
3-289
3An
effic
ient M
onte
Carlo
meth
od
for ra
diatio
n tra
nspo
rt in
aero
therm
odyn
amic s
imula
tions
A. La
ni, vo
n Kárm
án In
stitute
for F
luid
Dyna
mics,
Rhod
e-Sain
t-Gen
èse, B
elgium
; P. D
uarte
Santo
s, Tec
hnica
l Univ
ersity
of
Lisbo
n, Lis
bon,
Portu
gal; A
. San
na,
Unive
rsity o
f Cag
liari, C
agliar
i, Ital
y
1500
hrs
AIAA-2
013-2
894
An A
rtific
ial Co
mpre
ssibil
ity
Algo
rithm
for C
onve
ctive
Hea
t Tra
nsfe
rL.
Taylo
r, K. S
reeniv
as, R
. Web
ster,
J. Kre
ss, U
nivers
ity of
Tenn
esse
e, Ch
attan
ooga
, Cha
ttano
oga,
TN
1530
hrs
AIAA-2
013-2
895
Comp
utat
ion of
radia
tive a
nd
conv
ectiv
e con
tribu
tions
to
Viking
after
body
hea
ting
D. Po
tter, S
. Karl
, M. L
ambe
rt, K.
Ha
nnem
ann,
Germ
an Ae
rospa
ce
Cente
r (DL
R), G
ötting
en, G
erman
y
1600
hrs
AIAA-2
013-2
896
CFD
Invest
igatio
n For
Obta
ining
Ar
cjet F
reestr
eam
With
High
er
Dyna
mic P
ressu
res U
sing A
n Ar
cjet F
acilit
yT.
Saka
i, Nag
oya U
nivers
ity, N
agoy
a, Jap
an; K
. Fujit
a, K.
Fujii,
H. Tak
ayan
agi,
T. Su
zuki,
Japa
n Aero
space
Explo
ration
Ag
ency
(JAXA
), Tok
yo, J
apan
Tues
day,
25 Ju
ne 2
013
106-
TP-1
0Hi
gh-S
peed
and R
arefi
ed Fl
ows
Exec
utive
Conf
eren
ce 3
ACh
aired
by: M
. MAR
TIN, L
ouisia
na S
tate U
nivers
ity an
d S. C
HIGU
LLAPA
LLI, P
urdue
Univ
ersity
1430
hrs
AIAA-2
013-2
897
Influ
ence
of B
ound
ary-
Laye
r Tu
rbule
nce o
n Ef
fusio
n Co
oling
at
Mac
h 2.
67M.
Kelle
r, M. K
loker,
Univ
ersity
of
Stutt
gart,
Stut
tgart,
Germ
any
1500
hrs
AIAA-2
013-2
898
Towa
rds H
eat T
rans
fer C
ontro
l by
Aer
ospik
es fo
r Lift
ing-B
ody
Confi
gura
tion
in Hy
perso
nic
Flow
at M
ach
7S.
Khura
na, K
. Suz
uki, U
nivers
ity of
To
kyo,
Kash
iwa,
Japa
n
1530
hrs
AIAA-2
013-2
899
Glob
al Pr
essu
re M
easu
reme
nt
of a
Movin
g Bull
etY.
Yama
da, U
nivers
ity of
Elec
tro-
Comm
unica
tions
, Cho
fu, Ja
pan;
M.
Ishii,
Natio
nal R
esea
rch In
stitut
e of
Police
Scie
nce,
Kash
iwa,
Japa
n; T.
Miya
zaki,
Univ
ersity
of El
ectro
-Co
mmun
icatio
ns, C
hofu,
Japa
n; H.
Sa
kaue
, Jap
an Ae
rospa
ce Ex
plorat
ion
Agen
cy (J
AXA)
, Cho
fu, Ja
pan
1600
hrs
AIAA-2
013-2
900
Imme
rsed B
ound
ary M
ethod
fo
r Ana
lysis
of U
nstea
dy
Rare
fied G
as D
ampin
gC.
Peka
rdan,
V. Ay
yasw
amy,
A. Ale
xeen
ko, P
urdue
Univ
ersity
, Wes
t La
fayett
e, IN
1630
hrs
AIAA-2
013-2
901
State-
to-S
tate
Inter
nal E
nerg
y Re
laxat
ion Fo
llowi
ng th
e Qu
antu
m-Ki
netic
Mod
el in
DSMC
D. Li
echty
, NAS
A Lan
gley R
esea
rch
Cente
r, Ham
pton,
VA
Tues
day,
25 Ju
ne 2
013
107-
TP-1
1Th
erma
l Man
agem
ent a
nd P
rotec
tion
Exec
utive
Conf
eren
ce 2
BCh
aired
by: T
. LAM
, The
Aeros
pace
Corpo
ration
1430
hrs
AIAA-2
013-2
902
Equa
tion
of P
hono
n Hy
drod
ynam
ics fo
r Non
-Fo
urier
Hea
t Con
ducti
onY.
Ma, U
nivers
ity of
Califo
rnia,
Merce
d, Me
rced,
CA
1500
hrs
AIAA-2
013-2
903
Arcje
t Test
ing of
Micr
o-Mete
oroid
Im
pacte
d The
rmal
Prote
ction
Ma
terial
sP. A
grawa
l, ERC
, Inc.,
Moff
ett Fi
eld,
CA; M
. Mun
k, L.
Glaab
, NAS
A Lan
gley
Resea
rch Ce
nter, H
ampto
n, VA
1530
hrs
AIAA-2
013-2
904
Arc J
et Te
sting
of CM
C Sam
ples
with
Tran
spira
tion
Cooli
ngT.
Reim
er, G
erman
Aeros
pace
Cente
r (D
LR),
Stutt
gart,
Germ
any;
B. Es
ser,
A. Gu
elhan
, Germ
an Ae
rospa
ce
Cente
r (DL
R), C
ologn
e, Ge
rman
y
59
Tues
day,
25 Ju
ne 2
013
108-
PANE
L-1
1600
- 17
30 h
rsAI
RA -
Aircr
aft I
cing R
esea
rch A
llianc
e Pan
elRo
om 5
15
Inaug
ural Ic
e Crys
tal Ic
ing En
gine T
est in
the N
ASA G
lenn R
esea
rch Ce
nter, P
ropuls
ion S
ystem
s Lab
orator
yMi
chae
l Oliv
erNA
SA G
lenn R
esea
rch Ce
nter
Icing
Forec
ast R
esea
rch Ac
tivitie
s at N
CAR
Marci
a Poli
tovic
hNa
ction
al Ce
nter f
or Atm
osph
eric R
esea
rch
Pane
l Disc
ussio
nMo
derat
ed by
Jame
s Mac
Cleod
Na
tiona
l Res
earch
Cente
r, Can
ada
Wedn
esda
y
Wedn
esda
y, 26
June
201
310
9-NB
-3
0700
- 08
00 h
rsWe
dnes
day M
ornin
g Netw
orkin
g Bre
akfa
stNa
utilu
s and
Har
bor
Islan
d Foy
ers
Wedn
esda
y, 26
June
201
311
0-SB
-5
0730
- 08
00 h
rsWe
dnes
day M
ornin
g Spe
aker
s’ Br
iefing
Sessi
on R
ooms
Wedn
esda
y, 26
June
201
311
1-LE
C-3
0800
- 09
00 h
rsTh
ermo
phys
ics A
ward
Lectu
reHa
rbor
Ball
room
I an
d II
Gera
ld E.
Schn
eider
Unive
rsity
of Wa
terloo
Wedn
esda
y, 26
June
201
311
2-AP
A-24
Aero
dyna
mic a
nd M
ultidi
scipli
nary
Des
ign an
d Opt
imiza
tion
Meth
ods I
IIMa
rina 2
Chair
ed by
: A. A
RSLA
N an
d S. F
ERGU
SON,
Boe
ing D
efens
e, Sp
ace &
Sec
urity
0900
hrs
AIAA-2
013-2
905
Gene
tic Al
gorit
hm an
d Adjo
int
Optim
izatio
n of P
eriod
ic Wing
Pr
otube
rences
for S
tall M
itigati
onM.
Lohry
, L. M
artine
lli, Pri
nceton
Un
iversit
y, Pri
nceton
, NJ;
J. Ko
llasch,
Un
iversit
y of W
iscon
sin, M
adiso
n, Ma
dison
, WI
0930
hrs
AIAA-2
013-2
906
Helic
opter
Rot
or D
esign
usin
g Ad
joint
-bas
ed O
ptim
izatio
n in
a Cou
pled C
FD-C
SD Fr
amew
ork
A. Mi
shra,
K. M
ani, D
. Mav
riplis,
J.
Sitara
man,
Unive
rsity
of W
yomi
ng,
Laram
ie, La
ramie,
WY
1000
hrs
AIAA-2
013-2
907
Shap
e Opt
imiza
tion
of A
irfoil
s in
Trans
onic
Flow
Using
a M
ulti-O
bjecti
ve G
eneti
c Al
gorit
hmX.
Chen
, R. A
garw
al, W
ashin
gton
Unive
rsity
in St
. Lou
is, S
t. Lo
uis, M
O
1030
hrs
AIAA-2
013-2
908
Blen
ded W
ing B
ody A
ircra
ft -
Reco
mmen
datio
ns fr
om H
igh
Lift a
nd Co
ntro
l Sur
face
Des
ign
and O
ptim
izatio
nD.
Paulu
s, C.
Wirth
, M. H
ornun
g, Te
chnic
al Un
iversi
ty of
Munic
h, Mu
nich,
Germ
any
1100
hrs
AIAA-2
013-2
909
Adjoi
nt-B
ased
Aer
odyn
amic
Desig
n Op
timiza
tion
Using
the
Drag
Dec
ompo
sition
Meth
odF.
Bisso
n, S.
Nad
arajah
, McG
ill Un
iversi
ty, M
ontré
al, Ca
nada
60
Wedn
esda
y, 26
June
201
311
3-AP
A-25
Appli
ed CF
D II
Marin
a 3Ch
aired
by: A
. MAJ
AMAK
I, Th
e Aero
spac
e Corp
oratio
n and
K. VA
NDEN
, USA
F09
00 hr
sAIA
A-201
3-291
0C-
295
AEW
aero
dyna
mic
desig
n pr
oces
s: CF
D, w
ind
tunn
el tes
ts an
d fligh
t tes
tsA.
Casta
no S
anch
ez, E
. Rod
rigue
z Cis
neros
, E. A
ngel
Blasco
, Airb
us,
Getaf
e, Sp
ain
0930
hrs
AIAA-2
013-2
911
RANS
CFD
pred
iction
s of a
su
perso
nic je
t in
a tra
nson
ic cro
ssflow
R. Ch
aplin
, Defe
nce S
cienc
e and
Te
chno
logy L
abora
tory,
Fareh
am,
Unite
d King
dom
1000
hrs
AIAA-2
013-2
912
Inve
stiga
tion
of th
e Flow
with
in Pa
rtiall
y Sub
merg
ed Sc
oop
Type
Air
Inta
kes
M. Ru
etten
, S. K
och,
Germ
an
Aeros
pace
Cente
r (DL
R), G
ötting
en,
Germ
any;
S. Ku
cken
burg,
Univ
ersity
of
Kasse
l, Kas
sel, G
erman
y; M.
Rein,
Ge
rman
Aeros
pace
Cente
r (DL
R),
Göttin
gen,
Germ
any
1030
hrs
AIAA-2
013-2
913
Hybr
id RA
NS-LE
S Com
puta
tions
of
Turb
ulent
Flow
over
Ru
dimen
tary
Land
ing G
ear
S. Pe
ng, S
wedis
h Defe
nse R
esea
rch
Agen
cy (F
OI),
Stoc
kholm
, Swe
den
1100
hrs
AIAA-2
013-2
914
Comp
ariso
n of C
FD so
lvers
for
low sp
eed v
ortex
domi
nated
flo
wsM.
Gaffu
ri, J.
Brezill
on, G
erman
Ae
rospa
ce Ce
nter (
DLR)
, Brau
nschw
eig,
Germ
any;
D. Kw
ak, J
apan
Aeros
pace
Ex
plorat
ion Ag
ency
(JAXA
), Tok
yo,
Japan
; K. O
hira,
Ryoy
u Syst
ems
Comp
any,
Ltd., N
agoy
a, Jap
an; G
. Ca
rrier, O
NERA
, Meu
don,
France
1130
hrs
AIAA-2
013-2
915
Asses
smen
t of W
ENO
and S
FV
High
-Ord
er Re
cons
tructi
on
Schem
es for
Aero
dyna
mic F
lows
C. Bre
viglier
i, L. P
aula,
Techn
ologic
al Ins
titute
of Ae
ronau
tics (I
TA), S
ão
José d
os Ca
mpos,
Braz
il; W.
Wolf
, J.
Azev
edo,
Aeron
autics
and S
pace
Institu
te (IA
E), Sã
o José
dos C
ampo
s, Bra
zil
Wedn
esda
y, 26
June
201
311
4-AP
A-26
Airfo
il/Wi
ng/C
onfig
urat
ion A
erod
ynam
ics II
Marin
a 4Ch
aired
by: A
. MCC
OMAS
, Ana
lytica
l Meth
ods I
nc an
d J. H
OOKE
R, Lo
ckhe
ed M
artin
Aeron
autic
s09
00 hr
sAIA
A-201
3-291
6A
CFD
Data
base
for A
irfoil
s an
d Wing
s at P
ost-S
tall A
ngles
of
Atta
ckJ.
Petril
li, R.
Paul,
A. G
opala
rathn
am,
N. Fr
ink, N
orth C
arolin
a Stat
e Un
iversi
ty, Ra
leigh
, NC
0930
hrs
AIAA-2
013-2
917
Liftin
g-Lin
e Pre
dictio
ns fo
r In
duce
d Dra
g and
Lift
in Gr
ound
Effe
ctW.
Philli
ps, U
tah S
tate U
nivers
ity,
Loga
n, UT
; D. H
unsa
ker, S
caled
Co
mpos
ites,
Mojav
e, CA
1000
hrs
AIAA-2
013-2
918
Analy
tical
Deco
mpos
ition
of
Wing
Roll
and F
lappin
g Usin
g Lif
ting-
Line T
heor
yW.
Philli
ps, U
tah S
tate U
nivers
ity,
Loga
n, UT
1030
hrs
AIAA-2
013-2
919
A Stu
dy of
Bur
st Wa
kes i
n a
Multie
lemen
t Airf
oil Fl
owfie
ldB.
Pome
roy, P
. Ans
ell, J
. Dieb
old, M
. Se
lig, U
nivers
ity of
Illino
is, U
rbana
-Ch
ampa
ign, U
rbana
, IL
1100
hrs
AIAA-2
013-2
920
Over
Wing
Nac
elle I
nstal
lation
s for
Impr
oved
Energ
y Effi
cienc
yJ.
Hook
er, A.
Wick
, Lock
heed
Mart
in Co
rporat
ion, M
ariett
a, GA
; C. Z
eune
, Air
Force
Resea
rch La
borat
ory, W
right-
Patte
rson A
FB, O
H; A.
Agela
stos,
Sand
ia Na
tiona
l Labo
ratori
es, Al
buqu
erque
, NM
1130
hrs
AIAA-2
013-2
921
Deco
mpos
ed Li
fting
-Line
Pr
edict
ions a
nd O
ptim
izatio
n fo
r Pro
pulsi
ve Ef
ficien
cy of
Fla
pping
Wing
sW.
Philli
ps, R
. Mille
r, D. H
unsa
ker,
Utah
Stat
e Univ
ersity
, Log
an, U
T
Wedn
esda
y, 26
June
201
311
5-AP
A-27
/FD-
26Clo
sed-
Loop
Flow
Cont
rol
Exec
utive
Conf
eren
ce 1
Chair
ed by
: K. K
ARA,
Khali
fa Un
iversi
ty of
Scien
ce, T
echn
ology
& Re
searc
h and
T. CO
LONI
US, C
alifor
nia In
stitut
e of T
echn
ology
0900
hrs
AIAA-2
013-2
922
Expe
rimen
tal C
losed
-Loop
Co
ntro
l of F
low Se
para
tion
on
a Sim
ple H
inged
Flap
usin
g Ex
tremu
m-Se
eking
C. Tim
othee
, J. D
ando
is, E.
Garn
ier,
L. Ja
cquin
, ONE
RA, M
eudo
n, Fra
nce
0930
hrs
AIAA-2
013-2
923
Nume
rical
Simula
tions
of
Close
d-Lo
op Fl
ow Co
ntro
l of a
Ta
ngen
t Ogiv
e at a
High
Ang
le of
Atta
ckC.
Porte
r, C. F
agley
, J. F
arnsw
orth,
J. Se
idel, T
. McLa
ughli
n, U.
S. Ai
r Forc
e Ac
adem
y, Co
lorad
o Spri
ngs,
CO
1000
hrs
AIAA-2
013-2
924
Expe
rimen
tal C
losed
-Loop
Flow
Co
ntro
l of a
von
Karm
an O
give
at a
High
Ang
le of
Atta
ckJ.
Farns
worth
, C. P
orter,
J. S
eidel,
T.
McLa
ughli
n, C.
Fagle
y, U.
S. Ai
r Forc
e Ac
adem
y, Co
lorad
o Spri
ngs,
CO
1030
hrs
AIAA-2
013-2
925
Close
d-loo
p Acti
ve Fl
ow Co
ntro
l of
Stall
Sepa
ratio
n us
ing
Synt
hetic
Jets
B. Le
e, M.
Kim,
B. C
hoi, C
. Kim
, H.
Kim,
Seo
ul Na
tiona
l Univ
ersity
, Se
oul, S
outh
Korea
; K. J
ung,
Agen
cy
for D
efens
e Dev
elopm
ent,
Daeje
on,
South
Korea
1100
hrs
AIAA-2
013-2
926
Robu
st Hi
nf Co
ntro
l of
Theo
dorse
n’s Li
ft Mo
del f
or a
Pitch
ing an
d Plun
ging A
irfoil
Us
ing LM
I App
roac
hZ.
Li, R.
Agarw
al, W
ashin
gton
Unive
rsity
in St
. Lou
is, S
t. Lo
uis,
MO; H
. Gao
, Harb
in Ins
titute
of Te
chno
logy,
Harbi
n, Ch
ina
61
Wedn
esda
y, 26
June
201
311
6-AP
A-28
Wind
Tunn
el an
d Flig
ht Te
sting
Aer
o II
Exec
utive
Conf
eren
ce 2
ACh
aired
by: B
. MCG
RATH
, JHU
/App
lied P
hysic
s Lab
orator
y and
G. G
ATLIN
0900
hrs
AIAA-2
013-2
927
Flexib
le Fli
ght R
esea
rch
Platfo
rm at
Texa
s A&M
Un
iversi
ty Fl
ight R
esea
rch
Labo
rato
ryA.
Tuck
er, D
. Wes
t, B.
Craw
ford,
W.
Saric
, Tex
as A&
M Un
iversi
ty, Co
llege
St
ation
, TX
0930
hrs
AIAA-2
013-2
928
Study
on th
e Hyp
erso
nic W
ind
Tunn
el Flo
wfield
Affe
cted b
y th
e Tra
nsve
rse Je
tX.
Zhao
, Chin
a Aca
demy
of
Aeros
pace
Aerod
ynam
ics, B
eijing
, Ch
ina
1000
hrs
AIAA-2
013-2
929
A He
at Fl
ux Se
nsor
to th
e De
tectio
n of
Tran
sition
on
Airfo
ilsT.
Waitz
, W. N
itsch
e, Te
chnic
al Un
iversi
ty of
Berlin
, Berl
in, G
erman
y
1030
hrs
AIAA-2
013-2
930
Desig
n of a
Wind
Tunn
el Mo
del
for M
axim
um Li
ft Pr
edict
ions
Based
on Fl
ight T
est D
ataN.
Bier,
S. Ke
ye, D
. Roh
lman
n, Ge
rman
Ae
rospa
ce Ce
nter (
DLR)
, Brau
nschw
eig,
Germ
any;
S. vo
n Dee
tzen,
Deha
rde
Masch
inenb
au He
lmut
Hoffm
ann G
mbH,
Va
rel, G
erman
y
1100
hrs
AIAA-2
013-2
931
Expe
rimen
tal In
vesti
gatio
n Of
An Ae
rody
nami
c Flow
Of
Geom
etrica
l Mod
els In
Hyp
erson
ic Ae
rody
nami
c Sho
ck Tu
beI. K
ryuko
v, M.
Kotov
, L. R
uleva
, S.
Solod
ovnik
ov, S.
Surzh
ikov,
Russi
an
Acad
emy o
f Scie
nces,
Mosco
w, Ru
ssia
Wedn
esda
y, 26
June
201
311
7-AS
E-8On
-Gro
und a
nd In
-Fligh
t Ice
Pro
tectio
nRo
om 5
15Ch
aired
by: D
. FUL
EKI a
nd J.
MAC
LEOD
, Nati
onal
Rese
arch C
ounc
il Can
ada
0900
hrs
AIAA-2
013-2
932
Anti-
icing
Fluid
Flow
Off
Proc
ess o
n a W
ing Se
ction
du
ring S
imula
ted Ta
xi an
d Ta
ke-o
ffP.
Koivi
sto, A
alto U
nivers
ity, E
spoo
, Fin
land
0930
hrs
AIAA-2
013-2
933
Aero
dyna
mic C
hara
cteriz
ation
of
a Th
in, H
igh-P
erfo
rman
ce
Airfo
il for
Use
in G
roun
d Flui
ds
Testi
ngA.
Broe
ren, N
ASA G
lenn R
esea
rch
Cente
r, Clev
eland
, OH;
S. L
ee,
Vanta
ge Pa
rtners
, LLC
, Clev
eland
, OH
; C. C
lark,
Natio
nal R
esea
rch
Coun
cil Ca
nada
, Otta
wa, C
anad
a
1000
hrs
AIAA-2
013-2
934
A Stu
dy of
the E
ffects
of
Altit
ude o
n Th
erma
l Ice
Pr
otec
tion
Syste
m Pe
rform
ance
H. Ad
dy, N
ASA G
lenn R
esea
rch
Cente
r, Clev
eland
, OH;
M. O
leskiw
, Na
tiona
l Res
earch
Coun
cil Ca
nada
, Ot
tawa,
Cana
da; A
. Broe
ren, N
ASA
Glenn
Rese
arch C
enter
, Clev
eland
, OH
; D. O
rchard
, Nati
onal
Rese
arch
Coun
cil Ca
nada
, Otta
wa, C
anad
a
1030
hrs
AIAA-2
013-2
935
CFD
Analy
sis of
a Wi
ng w
ith a
Blee
d Air
Ice P
rotec
tion
Syste
mJ.
Wong
, M. P
apad
akis,
J. W
ong,
Wich
ita S
tate U
nivers
ity, W
ichita
, KS
1100
hrs
AIAA-2
013-2
936
Two d
imen
siona
l mod
el of
an
electr
o-th
erma
l ice p
rotec
tion
syste
mL.
Benn
ani, A
irbus
, Tou
louse
, Fran
ce;
P. Vil
ledieu
, ONE
RA, T
oulou
se, F
rance
; M.
Sala
un, U
nivers
ity of
Toulo
use,
Toulo
use,
Franc
e
1130
hrs
AIAA-2
013-2
937
On O
ptim
al De
sign
of El
ectro
-Th
erma
l In-
Fligh
t Ice
Pro
tectio
n Sy
stems
M. Po
urbag
ian, W
. Hab
ashi,
McG
ill Un
iversi
ty, M
ontré
al, Ca
nada
Wedn
esda
y, 26
June
201
311
8-CF
D-30
High
-Ord
er M
ethod
s VNa
utilu
s 5Ch
aired
by: G
. MAY
, AICE
S Gr
adua
te Sc
hool
and T
. EYM
ANN,
CREA
TE-AV
/Kes
trel
0900
hrs
AIAA-2
013-2
938
Adjoi
nt-B
ased
Hp-
Adap
tatio
n fo
r a Cl
ass o
f High
-Ord
er
Hybr
idize
d Fini
te Ele
ment
Sc
heme
s for
Comp
ressi
ble
Flows
A. Ba
lan, M
. Woo
pen,
G. M
ay, R
WTH
Aa
chen
Univ
ersity
, Aac
hen,
Germ
any
0930
hrs
AIAA-2
013-2
939
Scala
ble pa
ralle
lizat
ion of
th
e hyb
ridize
d disc
ontin
uous
Ga
lerkin
meth
od fo
r co
mpre
ssible
flow
X. Ro
ca, C
. Ngu
yen,
J. Pe
raire,
Ma
ssach
usett
s Ins
titute
of Te
chno
logy,
Camb
ridge
, MA
1000
hrs
AIAA-2
013-2
940
Multid
imen
siona
l Acti
ve Fl
ux
Sche
mes
T. Ey
mann
, CRE
ATE K
estre
l Tea
m,
Eglin
AFB,
FL; P
. Roe
, Univ
ersity
of
Mich
igan,
Ann A
rbor, A
nn Ar
bor, M
I
1030
hrs
AIAA-2
013-2
941
High
-Ord
er Sp
ectra
l Diff
erenc
e: Ve
rifica
tion a
nd Ac
celera
tion
using
GPU
Comp
uting
B. Zim
merm
an, Io
wa St
ate Un
iversit
y, Am
es, IA
; Z. W
ang,
Unive
rsity o
f Kan
sas,
Lawr
ence,
Lawr
ence,
KS; M
. Visb
al,
Air Fo
rce Re
search
Labo
ratory
, Wrig
ht-Pa
tterso
n AFB
, OH
1100
hrs
AIAA-2
013-2
942
Adjoi
nt-B
ased
Erro
r Esti
matio
n an
d Mes
h Ad
apta
tion
for t
he
Activ
e Flux
Meth
odK.
Ding,
K. Fid
kows
ki, P.
Roe,
Unive
rsity
of Mi
chiga
n, An
n Arbo
r, An
n Arbo
r, MI
62
Wedn
esda
y, 26
June
201
311
9-CF
D-31
Nume
rical
Algo
rithm
s for
Invis
cid an
d Visc
ous F
lows I
VNa
utilu
s 4Ch
aired
by: M
. DRE
LA, M
assa
chus
ettes
Insti
tute o
f Tec
hnolo
gy an
d D. M
ORO
0900
hrs
AIAA-2
013-2
943
Adva
nces
in th
e dev
elopm
ent
of a
High
Ord
er, Vi
scous
-In
viscid
Inter
actio
n So
lver
D. M
oro, C
. Ngu
yen,
J. Pe
raire,
M.
Drela
, Mas
sach
usett
s Ins
titute
of Te
chno
logy,
Camb
ridge
, MA
0930
hrs
AIAA-2
013-2
944
Adva
nces
in H
omot
opy
Cont
inuat
ion M
ethod
s in
Comp
utat
ional
Fluid
Dyna
mics
D. B
rown,
D. Zi
ngg,
Unive
rsity
of To
ronto,
Toron
to, Ca
nada
1000
hrs
AIAA-2
013-2
945
Deve
lopme
nt of
a Low
-Di
ssipa
tion A
lgorit
hm in
a Ru
le-Ba
sed Fr
amew
ork f
or U
nstea
dy
Flows
in Co
mplex
Geo
metri
esM.
Parm
ar, Un
iversit
y of F
lorida
, Ga
inesvi
lle, Ga
inesvi
lle, FL
; S. T
haku
r, Str
eaml
ine N
umeri
cs, In
c., Ga
inesvi
lle, FL
1030
hrs
AIAA-2
013-2
946
Prog
ress
Towa
rds a
n Ar
bitra
rily
High
-Ord
er, U
nstru
cture
d, Fr
ee-W
ake P
anel
Solve
rJ.
Moore
, J. P
eraire
, M. D
rela,
Massa
chus
etts I
nstitu
te of
Tech
nolog
y, Ca
mbrid
ge, M
A
1100
hrs
AIAA-2
013-2
947
Loca
l Fini
te Vo
lume M
ethod
fo
r Calc
ulatio
n of
Comp
ressi
ble
Flow
on A
rbitr
ary S
catte
red
Node
sT.
Taka
tani, K
. Suz
uki, U
nivers
ity of
To
kyo,
Kash
iwa,
Japa
n
Wedn
esda
y, 26
June
201
312
0-CF
D-32
Larg
e-Ed
dy Si
mulat
ion (L
ES),
Dire
ct Nu
meric
al Sim
ulatio
n (D
NS),
and H
ybrid
RAN
S/LE
S Meth
ods I
ISe
abre
eze I
Chair
ed by
: T. S
HIH,
Ohio
Aeros
pace
Insti
tute
0900
hrs
AIAA-2
013-2
948
Very
larg
e edd
y sim
ulatio
ns
of a
spra
y rea
cting
flow
in a
single
elem
ent L
DI in
jecto
r wi
th an
d with
out i
nvok
ing th
e Eu
lerian
scala
r DWF
DF m
ethod
T. Sh
ih, O
hio Ae
rospa
ce In
stitut
e, Cle
velan
d, OH
; N. L
iu, N
ASA G
lenn
Rese
arch C
enter
, Clev
eland
, OH
0930
hrs
AIAA-2
013-2
949
Simula
tion
of A
ttach
ed
and S
epar
ated
Flow
s usin
g Re
aliza
ble Li
near
and N
on-
Linea
r Hyb
rid R
ANS-
LES
Mode
lsH.
Gop
alan,
J. Sit
arama
n, S.
Hein
z, Un
iversi
ty of
Wyo
ming
, Lara
mie,
Laram
ie, W
Y
1000
hrs
AIAA-2
013-2
950
Larg
e-Ed
dy Si
mulat
ion
of Tu
rbule
nt Tr
ans-
and
Supe
rcritic
al Mi
C. Nie
derm
eier, T
echn
ical U
nivers
ity
of Mu
nich,
Garch
ing, G
erman
y; M.
Jarcz
yk, ;
S. H
ickel,
N. A
dams
, Te
chnic
al Un
iversi
ty of
Munic
h, Ga
rching
, Germ
any;
M. Pfi
tzner,
Wedn
esda
y, 26
June
201
312
1-CF
D-33
Unste
ady F
lows I
ISp
inake
r ICh
aired
by: M
. BIES
TER,
Lebn
iz Un
iversi
tät H
anno
ver
0900
hrs
AIAA-2
013-2
951
Wind
Turb
ine D
ynam
ic Sta
ll An
alysis
Usin
g Har
monic
Ba
lance
and C
orre
lation
-bas
ed
Trans
ition
Mode
lsJ.
Howi
son,
K. Ek
ici, U
nivers
ity of
Te
nnes
see,
Knox
ville,
Knox
ville,
TN
0930
hrs
AIAA-2
013-2
952
Nume
rical
Inve
stiga
tion
of
Shoc
k Os
cillat
ion ov
er A
irfoil
s at
Tran
sonic
Spee
ds In
fluen
ced
by Tr
ailing
Edge
Jet
Z. Zh
ang,
North
weste
rn Po
lytec
hnica
l Un
iversi
ty, X
i’an,
China
1000
hrs
AIAA-2
013-2
953
Nume
rical
Inve
stiga
tions
and
Moda
l Ana
lysis
of th
e Coh
eren
t Str
uctu
res i
n a G
ener
ic Sw
irl
Burn
erO.
Krüg
er, Te
chnic
al Un
iversi
ty of
Berlin
, Berl
in, G
erman
y; C.
Duwi
g, Lu
nd U
nivers
ity, L
und,
Swed
en; S
. Te
rhaar,
C. Pa
schere
it, Te
chnic
al Un
iversi
ty of
Berlin
, Berl
in, G
erman
y
1030
hrs
AIAA-2
013-2
954
Para
metri
c Stu
dy of
Low
Reyn
olds N
umbe
r Flap
ping
Wing
Aer
odyn
amics
S. Le
guiza
mon,
Swiss
Fede
ral
Institu
te of
Tech
nolog
y, La
usan
ne,
Switz
erlan
d; O.
Lope
z, Un
iversi
ty of
the An
des,
Bogo
ta, Co
lombia
1100
hrs
AIAA-2
013-2
955
Clock
ing Ef
fects
on Su
rface
-Pr
essu
re Fl
uctu
ation
s for
Va
riable
Axia
l-Gap
sM.
Bies
ter, L
eibniz
Univ
ersity
of
Hann
over,
Han
nove
r, Germ
any;
Y. Gu
endo
gdu,
MTU
Aero
Engin
es
GmbH
, Mun
ich, G
erman
y; J.
Seum
e, Le
ibniz
Unive
rsity
of Ha
nnov
er,
Hann
over,
Germ
any
63
Wedn
esda
y, 26
June
201
312
2-CF
D-34
Nume
rical
Treat
ment
of B
ound
ary C
ondit
ions I
IMa
rina 5
Chair
ed by
: J. N
ORDS
TROM
, Link
öping
Univ
ersity
0900
hrs
AIAA-2
013-2
956
The I
nflue
nce o
f Visc
ous
Oper
ator
and W
all B
ound
ary
Cond
itions
on th
e Accu
racy
of
the N
avier
-Sto
kes E
quat
ions
P. Eli
asso
n, Sw
edish
Defe
nse
Rese
arch A
genc
y (FO
I), S
tockh
olm,
Swed
en; J
. Nord
strom
, Link
öping
Un
iversi
ty, Li
nköp
ing, S
wede
n
0930
hrs
AIAA-2
013-2
957
Incre
asing
the c
onve
rgen
ce
rate
to st
eady
-stat
e by u
sing
multip
le pe
nalty
term
s app
lied
in a d
omain
H. Fr
enan
der, J
. Nord
strom
, Lin
köpin
g Univ
ersity
, Link
öping
, Sw
eden
1000
hrs
AIAA-2
013-2
958
Effe
ct of
Inter
face
Thick
ness
on
Smoo
thed
Pro
file M
odeli
ng of
Flo
w Ov
er a
Statio
nary
Sphe
re
in 1<
Re<3
00F.
Moha
gheg
h, J.
Mous
el, U
. Kum
ar,
Unive
rsity
of Iow
a, Iow
a City
, Iow
a Cit
y, IA
1030
hrs
AIAA-2
013-2
959
Duali
ty ba
sed b
ound
ary
treat
ment
for t
he Eu
ler an
d Na
vier-S
toke
s equ
ation
sJ.
Berg,
Upp
sala
Unive
rsity,
Upp
sala,
Sw
eden
; J. N
ordstr
om, L
inköp
ing
Unive
rsity,
Link
öping
, Swe
den
1100
hrs
AIAA-2
013-2
960
Well-
pose
dnes
s and
Stab
ility o
f Ex
act N
on-re
flecti
ng B
ound
ary
Cond
itions
S. Er
iksso
n, Up
psala
Univ
ersity
, Up
psala
, Swe
den;
J. No
rdstro
m,
Linkö
ping U
nivers
ity, L
inköp
ing,
Swed
en
1130
hrs
AIAA-2
013-2
961
Frict
ionles
s con
tact
algor
ithm
for E
uleria
n hig
h sp
eed
multim
ater
ial dy
nami
c sim
ulatio
nsN.
Rai, A
. Kap
ahi, U
. Kum
ar,
Unive
rsity
of Iow
a, Iow
a City
, Iow
a Cit
y, IA
Wedn
esda
y, 26
June
201
312
3-CF
D-35
Othe
r Top
ics in
CFD
IIRo
om 5
14Ch
aired
by: D
. CAR
AENI
, CD-A
dapc
o and
J. W
EISS
0900
hrs
AIAA-2
013-2
962
Cont
inuity
Conv
erge
nce
Acce
lerat
ion of
a De
nsity
-Ba
sed C
ouple
d Algo
rithm
D. Ca
raeni,
J. W
eiss,
W. S
mith,
D.
Snyd
er, N
. Hall
iday,
J. Cle
ment,
CD
-adap
co, L
eban
on, N
H
0930
hrs
AIAA-2
013-2
963
Nume
rical
Simula
tions
of
Turb
ulent
Flow
over
Por
ous
Media
M. M
oessn
er, R.
Rade
spiel
, Tec
hnica
l Un
iversi
ty of
Brau
nsch
weig,
Br
auns
chwe
ig, G
erman
y
1000
hrs
AIAA-2
013-2
964
A Mu
ltivar
iate I
nter
polat
ion
and R
egre
ssion
Enha
nced
Kr
iging
Surro
gate
Mode
lK.
Boop
athy,
M. Ru
mpfke
il, Un
iversi
ty of
Dayto
n, Da
yton,
OH
1030
hrs
AIAA-2
013-2
965
Non-u
nique
Num
erica
l Solu
tions
an
d The
ir Stab
ility o
f the
Euler
Eq
uatio
ns fo
r Tra
nson
ic Flow
over
Air
foils
Y. Liu
, J. X
iong,
F. Liu,
S. Lu
o, Un
iversit
y of
Califo
rnia,
Irvine
, Irvin
e, CA
1100
hrs
AIAA-2
013-2
966
Comp
utat
ional
Analy
sis of
a D
iffus
er U
sing U
SM3D
for
Diffu
ser A
ugme
nted
Wind
Tu
rbine
sD.
Jeda
mski,
K. V
isser,
Clark
son
Unive
rsity,
Potsd
am, N
Y
Wedn
esda
y, 26
June
201
312
4-FD
-27
Redu
ced-
Orde
r Mod
eling
Room
511
Chair
ed by
: L. C
ATTA
FEST
A, FA
MU-FS
U Co
llege
of En
ginee
ring
0900
hrs
AIAA-2
013-2
967
Nonli
near
Dim
ensio
nality
Re
ducti
on fo
r Par
amete
rized
Pa
rtial
Diffe
rent
ial Eq
uatio
nL.
Peng
, K. M
ohse
ni, U
nivers
ity of
Flo
rida,
Gaine
sville
, Gain
esvil
le, FL
0930
hrs
AIAA-2
013-2
968
Cont
rol o
f a ca
nonic
al se
para
ted fl
owJ.
Griffi
n, M.
Oya
rzun,
Unive
rsity
of Flo
rida,
Gaine
sville
, Gain
esvil
le, FL
; L.
Catta
festa,
Flori
da S
tate U
nivers
ity,
Talla
hasse
e, FL
; J. T
u, C.
Rowl
ey,
Princ
eton U
nivers
ity, P
rince
ton, N
J
1000
hrs
AIAA-2
013-2
969
Laun
ch Ve
hicle
Cavit
y Ven
ting:
Mode
ling C
once
pts &
Valid
atio
D. Pa
tel, O
rbital
Scie
nces
Co
rporat
ion, D
ulles
, VA
1030
hrs
AIAA-2
013-2
970
Film-
Cooli
ng Je
ts An
alyze
d wi
th P
rope
r Orth
ogon
al De
comp
ositio
n an
d Dyn
amic
Mode
Dec
ompo
sition
G. B
idan,
D. N
ikitop
oulos
, Lou
isiana
St
ate U
nivers
ity, B
aton R
ouge
, LA
1100
hrs
AIAA-2
013-2
971
Nonli
near
Mod
el Re
ducti
on vi
a Pie
cewi
se B
alanc
e Tru
ncat
ionW.
yao,
M. Li
ou, N
ASA G
lenn
Rese
arch C
enter
, Clev
eland
, OH
Wedn
esda
y, 26
June
201
312
5-FD
-28
Micro
/Nan
o Sca
le Flu
id Dy
nami
cs an
d Spr
ay Co
oling
Room
518
Chair
ed by
: D. H
ITT, U
nivers
ity of
Verm
ont
0900
hrs
AIAA-2
013-2
973
Enha
nced
Lami
nar M
ixing
in
Multifl
uid D
rople
ts via
Mult
iphas
e Flow
in a
Micro
chan
nel
M. M
cDev
itt, D
. Hitt,
Univ
ersity
of
Verm
ont,
Burlin
gton,
Burlin
gton,
VT
0930
hrs
AIAA-2
013-2
974
Slip a
t the
tripl
e con
tact
point
in tw
o pha
se fl
ow in
mi
croch
anne
lsJ.
Thala
kkott
or, K.
Moh
seni,
Un
iversi
ty of
Florid
a, Ga
inesv
ille,
Gaine
sville
, FL
1000
hrs
AIAA-2
013-2
975
Spra
y Sim
ulatio
ns to
Supp
ort
the D
evelo
pmen
t of a
Mon
te Ca
rlo-B
ased
Spra
y Coo
ling
Mode
lM.
Dinc
, D. G
ray, N
. Hille
n, J.
Taylo
r, J.
Kuhlm
an, W
est V
irgini
a Univ
ersity
, Mo
rganto
wn, W
V
1030
hrs
AIAA-2
013-2
976
Drop
let im
pact
time h
istor
ies
for a
rang
e of W
eber
num
bers
and l
iquid
film
thick
nesse
s for
sp
ray c
oolin
g app
licat
ionN.
Hille
n, J.
Taylo
r, C. M
ench
ini,
G. M
orris,
M. D
inc, D
. Gray
, J.
Kuhlm
an, W
est V
irgini
a Univ
ersity
, Mo
rganto
wn, W
V
64
Wedn
esda
y, 26
June
201
312
6-FD
-29
Hype
rsonic
and C
hemi
cally
-Rea
cting
Flow
s INa
utilu
s 1Ch
aired
by: A
. DOR
D, G
E Avia
tion a
nd R.
BOW
ERSO
X, Te
xas A
&M U
nivers
ity09
00 hr
sAIA
A-201
3-297
7Nu
meric
al In
vesti
gatio
n on
RC
S Jet
Inter
actio
ns fo
r a M
ars
Entry
Vehic
leS.
Mats
uyam
a, H.
Taka
yana
gi, K.
Fu
jita, J
apan
Aeros
pace
Explo
ration
Ag
ency
(JAX
A), C
hofu,
Japa
n
0930
hrs
AIAA-2
013-2
978
A pa
rame
tric s
tudy
of
ethyle
ne-fu
eled s
cramj
et co
mbus
tion
N. Cy
mbali
st, P.
Dim
otakis
, Cali
fornia
Ins
titute
of Te
chno
logy,
Pasa
dena
, CA
1000
hrs
AIAA-2
013-2
979
Free-fl
ight te
sts of
reen
try
caps
ule m
odels
in fr
ee-pi
ston
shoc
k tun
nel
H. Tan
no, T
. Kom
uro, K
. Sato
, K. It
oh, T
. Ya
mada
, Jap
an Ae
rospa
ce Ex
plorat
ion
Agen
cy (JA
XA),
Kaku
da, J
apan
1030
hrs
AIAA-2
013-2
980
On G
lobal
Linea
r Ins
tabil
ity
Analy
sis of
Hyp
erso
nic Fl
ow
Arou
nd a
Mode
l Re-
Entry
Ve
hicle
V. Th
eofili
s, M.
Herm
anns
, Tec
hnica
l Un
iversi
ty of
Madri
d, Ma
drid,
Spain
Wedn
esda
y, 26
June
201
312
7-FD
-30
High
-Spe
ed Tr
ansit
ion II
Naut
ilus 2
Chair
ed by
: M. B
ORG,
Boo
z Alle
n Ham
ilton a
nd M
. CHO
UDHA
RI, N
ASA-L
angle
y Res
earch
Cente
r09
00 hr
sAIA
A-201
3-298
1Re
al Ga
s and
Surfa
ce Ab
lation
Eff
ects o
n Hyp
erson
ic Bou
ndar
y La
yer I
nstab
ility o
ver a
Blun
t Co
neC.
Morte
nsen,
X. Zh
ong,
Unive
rsity o
f Ca
liforni
a, Lo
s Ang
eles,
Los A
ngele
s, CA
0930
hrs
AIAA-2
013-2
982
Stabil
ity an
d Uns
teadin
ess i
n a 2
D La
mina
r Sho
ck-In
duce
d Se
para
tion
Bubb
leA.
Sans
ica, N
. San
dham
, Z.
Hu, U
nivers
ity of
Sou
thamp
ton,
South
ampto
n, Un
ited K
ingdo
m
1000
hrs
AIAA-2
013-2
983
High
-Ord
er Si
mulat
ion of
In
duce
d Dist
urba
nce i
n a M
ach
6 Bo
unda
ry La
yer
H. At
kins,
NASA
Lang
ley Re
searc
h Ce
nter, H
ampto
n, VA
1030
hrs
AIAA-2
013-2
984
Linea
rized
Nav
ier-St
okes
Sim
ulatio
n of t
he Sp
atial
Stabil
ity
of a H
ypers
onic B
ound
ary L
ayer
in
Chem
ical E
quilib
rium
L. Sa
lemi, H
. Fase
l, Univ
ersity
of
Arizo
na, T
ucson
, Tucs
on, A
Z
1100
hrs
AIAA-2
013-2
985
Stabil
izatio
n of
hyp
erso
nic
boun
dary
laye
r wav
es u
sing
2-D
surfa
ce ro
ughn
ess
K. Fo
ng, X
. Wan
g, X.
Zhon
g, Un
iversi
ty of
Califo
rnia,
Los A
ngele
s, Lo
s Ang
eles,
CA
Wedn
esda
y, 26
June
201
312
8-FD
-31
Bluf
f Bod
y and
Shea
r Lay
er Co
ntro
lNa
utilu
s 3Ch
aired
by: D
. WILL
IAMS,
Illino
is Ins
titute
of Te
chno
logy a
nd U
. KAU
L, NA
SA-Am
es09
00 hr
sAIA
A-201
3-298
6An
Effic
ient C
FD-b
ased
PID
Co
ntro
l of F
ree S
hear
Laye
r Flo
wU.
Kaul,
NAS
A Ame
s Res
earch
Cente
r, Mo
ffett
Field,
CA
0930
hrs
AIAA-2
013-2
987
Stabil
ity an
alysis
of th
e flow
ar
ound
a cy
linde
r fitte
d with
he
lical st
rake
sF. G
omez
Carra
sco, J
. Que
sada,
G.
Raqu
el, N
ation
al Ins
titute
of Ae
rospa
ce
Techn
ology
INTA,
Mad
rid, S
pain;
V.
Theo
filis,
Scho
ol of
Aeron
autics
, Un
iversid
ad Po
litecni
ca de
Mad
rid,
Madri
d, Sp
ain; B
. Carm
o, J.
Mene
ghini,
De
partm
ent o
f Mech
anica
l Eng
ineeri
ng
NDF-P
OLI, U
nivers
ity of
Sao P
aulo,
São
Paulo
, Braz
il
1000
hrs
AIAA-2
013-2
988
On th
e Cyli
nder
Wak
e Su
bjecte
d to I
n-Ph
ase a
nd ou
t-of
-Pha
se P
eriod
ic Fo
rcing
A. Ah
med,
H. M
oore,
Aubu
rn Un
iversi
ty, Au
burn,
AL
1030
hrs
AIAA-2
013-2
989
A co
mput
ation
al an
alysis
of
the fl
ow ov
er a
side-
supp
orted
sp
here
with
loca
lised
synt
hetic
jet N.
Find
anis,
Penta
ir Env
ironm
ental
Sy
stems
, Milp
erra,
Austr
alia;
N.
Ahme
d, Un
iversi
ty of
New
South
Wa
les, S
ydne
y, Au
strali
a
1100
hrs
AIAA-2
013-2
990
Multi
objec
tive o
ptim
izatio
n of
a sy
nthe
tic je
t acti
ng on
a se
para
ted fl
ow ov
er a
hump
M. N
akam
ura, U
nivers
ity of
Toky
o, Sa
gami
hara,
Japa
n; T.
Nono
mura,
Y.
Inatan
i, Jap
an Ae
rospa
ce Ex
plorat
ion
Agen
cy (J
AXA)
, Sag
amiha
ra, Ja
pan
65
Wedn
esda
y, 26
June
201
312
9-FD
-32
Pitch
and P
lunge
Wing
Aer
odyn
amics
Spina
ker I
ICh
aired
by: J
. ELD
REDG
E, UC
LA an
d K. G
RANL
UND,
Air F
orce R
esea
ch La
borat
ory09
00 hr
sAIA
A-201
3-299
1Pe
rform
ance
of h
eavin
g and
pa
ssive
ly pit
ching
hyd
rofo
ilsJ.
Matth
eijsse
ns, J
. Marc
el, W
. Bo
sscha
erts,
Roya
l Milit
ary Ac
adem
y, Br
usse
ls, B
elgium
; D. L
efebe
r, Vri
je Un
iversi
teit B
russe
l, Brus
sels,
Be
lgium
0930
hrs
AIAA-2
013-2
992
Effect
s of P
lanfor
m Ge
ometr
y an
d Pivo
t Axis
Loca
tion o
n the
Ae
rody
nami
cs of
Pitch
ing Lo
w As
pect
Ratio
Wing
sH.
Yu, L
. Bern
al, Un
iversit
y of M
ichiga
n, An
n Arbo
r, Ann
Arbo
r, MI; M
. Ol, A
ir Fo
rce Re
search
Labo
ratory
, Wrig
ht-Pa
tterso
n AFB
, OH
1000
hrs
AIAA-2
013-2
993
Wake
Stru
cture
of P
lungin
g Fin
ite W
ings
D. Ca
lderon
, D. C
leave
r, Z. W
ang,
I. Gu
rsul, U
nivers
ity of
Bath
, Bath
, Un
ited K
ingdo
m
1030
hrs
AIAA-2
013-2
994
Comp
lianc
e Effe
cts in
Dy
nami
cally
Pitc
hing W
ind
Turb
ine A
irfoil
sA.
Mags
tadt,
J. St
rike,
P. Nik
ouee
yan,
M. H
ind, J
. Nau
ghton
, Un
iversi
ty of
Wyo
ming
, Lara
mie,
Laram
ie, W
Y
Wedn
esda
y, 26
June
201
313
0-GT
-4Gr
ound
Testi
ng M
easu
reme
nt A
nalys
isSe
abre
eze I
ICh
aired
by: J
. VAN
AKEN
, Jac
obs T
echn
ology
and B
. MILL
S09
00 hr
sAIA
A-201
3-299
5A
Statis
tical
Theo
ry of
Bi
direc
tiona
lityR.
DeLo
ach,
NASA
Lang
ley Re
searc
h Ce
nter, H
ampto
n, VA
; N. U
lbrich
, Ja
cobs
, Moff
ett Fi
eld, C
A
0930
hrs
AIAA-2
013-2
996
Analy
sis of
Mult
ivaria
te Ex
perim
enta
l Dat
a Usin
g A
Simpli
fied R
egre
ssion
Mod
el Se
arch
Algo
rithm
N. U
lbrich
, Jac
obs,
Moffe
tt Fie
ld, CA
1000
hrs
AIAA-2
013-2
997
Baye
sian
Revis
ion of
Res
idual
Detec
tion
Powe
rR.
DeLo
ach,
NASA
Lang
ley Re
searc
h Ce
nter, H
ampto
n, VA
1030
hrs
AIAA-2
013-2
998
Calib
ratio
n Va
riable
Se
lectio
n an
d Nat
ural
Zero
De
termi
natio
n fo
r Sem
ispan
an
d Can
ard B
alanc
esN.
Ulbr
ich, J
acob
s, Mo
ffett
Field,
CA
Wedn
esda
y, 26
June
201
313
1-PD
L-8MH
D fo
r Re-
Entry
Marin
a 6Ch
aired
by: N
. HAR
ADA,
Naga
oka U
nivers
ity of
Tech
nolog
y and
D. K
ONIG
ORSK
I09
00 hr
sAIA
A-201
3-299
9Ex
perim
ental
Stud
y on t
he
Magn
eto-ae
rody
nami
c For
ce
Defle
cted b
y Mag
netic
Field
Int
eracti
on in
a We
akly-
ionize
d Pla
sma F
lowY.
Naga
ta, Ja
pan A
erospa
ce Ex
plorat
ion
Agen
cy (JA
XA),
Saga
miha
ra, Ja
pan;
Y. Sa
tofuk
a, Y.
Watan
abe,
A. Tez
uka,
Wased
a Univ
ersity,
Shinju
ku, J
apan
; K.
Yama
da, T
. Abe
, Jap
an Ae
rospa
ce
Explo
ration
Agen
cy (JA
XA),
Saga
miha
ra,
Japan
0930
hrs
AIAA-2
013-3
000
Nume
rical
Simula
tion
of M
HD
Flow
Cont
rol a
long S
uper
Or
bital
Reen
try Tr
ajecto
ryT.
Fujin
o, M.
Ishik
awa,
Unive
rsity
of Tsu
kuba
, Tsu
kuba
, Jap
an
1000
hrs
AIAA-2
013-3
001
Expa
nsion
Tube
Expe
rimen
t on
Aero
dyna
mic F
orce
Enha
ncem
ent
due t
o the
Elect
rody
nami
c Int
eracti
on of
a Ma
gneti
zed B
ody
in a W
eakly
-ioniz
ed Fl
owM.
Hatto
ri, A.
Tezuk
a, Wa
seda
Unive
rsity,
Tokyo
, Jap
an; Y
. Tak
ahash
i, Ho
kkaid
o Univ
ersity,
Sapp
oro, J
apan
; Y.
Naga
ta, K.
Yama
da, T
. Abe
, Jap
an
Aeros
pace
Explo
ration
Agen
cy (JA
XA),
Tokyo
, Jap
an
1030
hrs
AIAA-2
013-3
002
Effe
ct of
the S
hape
Varia
tion
on th
e Elec
trody
nami
c Hea
t Sh
ield S
ystem
und
er th
e Stro
ng
Magn
etic F
ield
H. O
tsu, R
yuko
ku U
nivers
ity, O
tsu,
Japa
n; D.
Konig
orski,
EADS
, Brem
en,
Germ
any;
T. Ab
e, Ja
pan A
erosp
ace
Explo
ration
Agen
cy (J
AXA)
, Sa
gami
hara,
Japa
n
1100
hrs
AIAA-2
013-3
003
Nume
rical
Inve
stiga
tion
of a
Critic
al Al
titud
e on
Electr
odyn
amic
Aero
brak
ing
in a H
yper
sonic
Cont
inuum
-Ra
refie
d Tra
nsitio
nal R
egim
eH.
Katsu
rayam
a, Ya
magu
chi
Unive
rsity,
Ube
, Jap
an; T
. Abe
, Ja
pan A
erosp
ace E
xplor
ation
Agen
cy
(JAXA
), Sa
gami
hara,
Japa
n
66
Wedn
esda
y, 26
June
201
313
2-PD
L-9Pla
sma a
nd La
ser P
hysic
sEx
ecut
ive Co
nfer
ence
4Ch
aired
by: T
. MAD
DEN,
Air F
orce R
esea
ch La
borat
ory an
d A. Y
ALIN
, Colo
rado S
tate U
nivers
ity09
00 hr
sAIA
A-201
3-300
4An
unstr
uctur
ed so
lver f
or ar
gon
plasm
a flow
s with
redu
ced st
ate-
to-sta
te kin
etics
R. Pe
pe, A
. Bon
figliol
i, A. D
’Ango
la,
Unive
rsity o
f Basi
licata,
Poten
za, It
aly;
G. Co
lonna
, Nati
onal
Resea
rch Co
uncil
(CNR
), Ba
ri, Ita
ly; R.
Pacio
rri, Un
iversit
y of
Rome
“La S
apien
za”,
Rome
, Italy
0930
hrs
AIAA-2
013-3
005
An A
USM-
base
d Algo
rithm
for
Solvi
ng th
e Cou
pled N
avier
-Sto
kes a
nd M
axwe
ll Equ
ation
sR.
Thom
pson
, A. W
ilson,
T. Mo
eller,
Un
iversi
ty of
Tenn
esse
e Spa
ce
Institu
te, Tu
llaho
ma, T
N; C.
Merk
le,
Purdu
e Univ
ersity
, Wes
t LaF
ayett
e, IN
1000
hrs
AIAA-2
013-3
006
Tempe
ratur
e mea
surem
ents
inside
repe
titive
strea
mer
disch
arge
s and
comp
ariso
n with
nu
meric
al sim
ulatio
nsD.
Marku
s, T.
Lang
er, Fe
deral
Instit
ute
of Ph
ysical
and T
echnic
al Aff
airs,
Braun
schwe
ig, Ge
rman
y; U.
Maas,
Ka
rlsruh
e Inst
itute
of Tec
hnolo
gy,
Karlsr
uhe,
Germ
any
1030
hrs
AIAA-2
013-3
007
Nume
rical
Studie
s of
Filam
enta
ry P
lasma
Stru
cture
in
Micro
wave
Roc
ket
N. W
ongs
uryrat
, T. T
akeic
hi,
T. Ya
magu
chi, K
. Kom
urasa
ki,
Unive
rsity
of To
kyo,
Kash
iwa,
Japa
n; H.
Koizu
mi, U
nivers
ity of
Toky
o, Bu
nkyo
, Jap
an
1100
hrs
AIAA-2
013-3
008
Deve
lopme
nt of
a Gas
-Fed
Capil
lary S
ource
for P
ulsed
High
-De
nsity
Plas
ma Ap
plica
tions
M. Pa
chuilo,
L. Ra
ja, F.
Stefan
i, R.
Beng
tson,
Unive
rsity o
f Tex
as, Au
stin,
Austin
, TX;
C. Tas
, Univ
ersity
of Ill
inois,
Urban
a-Cha
mpaig
n, Urb
ana,
IL
Wedn
esda
y, 26
June
201
313
3-TP
-12
Plume
s, Pr
opuls
ion, a
nd Tu
rbom
achin
ery
Exec
utive
Conf
eren
ce 3
BCh
aired
by: P
. YEE
, The
Aeros
pace
Corpo
ration
0900
hrs
AIAA-2
013-3
009
Gene
raliz
ed N
ewto
n Me
thod
Fo
r Solv
ing D
iffer
entia
l Eq
uatio
ns of
Chem
ical K
inetic
sR.
Selez
nev,
S. S
urzhik
ov, R
ussia
n Ac
adem
y of S
cienc
es, M
osco
w,
Russi
a
0930
hrs
AIAA-2
013-3
010
Nume
rical
Simula
tion
of La
ser
Ignit
ion of
Roc
ket F
uels
in Ig
niter
sS.
Rebro
v, Ke
ldysh
Rese
arch C
enter
, Mo
scow,
Russi
a; A.
Molch
anov
, G.
Yakh
ina, M
osco
w Av
iation
Insti
tute,
Mosco
w, Ru
ssia
1000
hrs
AIAA-2
013-3
011
Simult
aneo
us at
tainm
ent o
f lig
ht-w
eight
, high
-effi
cienc
y, an
d low
nois
e: by
the
supe
rmult
ijet-t
wiste
r eng
ine
work
ing fr
om st
artu
p to
hype
rsonic
scra
m mo
deK.
Naito
h, M.
Maru
i, K. I
shida
, Wa
seda
Univ
ersity
, Shin
juku,
Japa
n
1030
hrs
AIAA-2
013-3
012
Char
acter
izatio
n of
Th
ermo
chro
mic L
iquid
Crys
tals
for M
ulti-C
olor T
rans
ient H
eat
Trans
fer E
xper
imen
tsL.
Tran,
A. Ph
am, Z
. Littl
e, J.
Kapa
t, CA
TER,
Orlan
do, F
L
1100
hrs
AIAA-2
013-3
013
A Mu
lti-Co
lor Th
ermo
chro
mic
Liquid
Crys
tals
Tech
nique
fo
r Tra
nsien
t Hea
t Tra
nsfe
r Ex
perim
ents
L. Tra
n, A.
Pham
, Z. L
ittle,
J. Ka
pat,
CATE
R, Or
lando
, FL
Wedn
esda
y, 26
June
201
313
4-TP
-13
Testi
ng an
d Diag
nosti
csEx
ecut
ive Co
nfer
ence
3A
Chair
ed by
: E. S
HORT
, Ray
theon
Comp
any
0900
hrs
AIAA-2
013-3
014
Unste
ady P
ressu
re D
istrib
ution
on
a Flu
tterin
g Airf
oil u
sing
Motio
n-Ca
ptur
ing P
SP Sy
stem
T. Ok
abe,
T. Mi
yaza
ki, U
nivers
ity
of Ele
ctro-c
ommu
nicati
ons,
Chofu
, Ja
pan;
K. Sa
itoh,
H. S
akau
e, Ja
pan
Aeros
pace
Explo
ration
Agen
cy
(JAXA
), Ch
ofu, J
apan
0930
hrs
AIAA-2
013-3
015
Vacu
um u
ltrav
iolet
radia
tion
studie
s in
a plas
ma to
rch
facil
ityC.
Jaco
bs, U
. She
ikh, M
. Mac
Dona
ld,
C. La
ux, É
cole
Centr
ale de
Paris
, Ch
âtena
y-Mala
bry, F
rance
1000
hrs
AIAA-2
013-3
016
Deter
mina
tion
of Te
mper
atur
e Pr
ofiles
in th
e Plen
um R
egion
of
the N
ASA
IHF A
rc Je
t Fac
ility
from
Emiss
ion Sp
ectro
scopic
Me
asur
emen
tsM.
Wint
er, U
nivers
ity of
Kentu
cky,
Lexin
gton,
Lexin
gton,
KY; D
. Prab
hu,
ERC,
Inc.,
Moun
tain V
iew, C
A; W.
W
illiam
s, Un
iversi
ty of
Kentu
cky,
Lexin
gton,
Lexin
gton,
KY
1030
hrs
AIAA-2
013-3
017
Persp
ective
on Re
Entry
Brea
kup
Reco
rder
Deriv
ed Co
ncep
ts for
Sm
all Pa
yload
Fligh
t Exp
erime
ntsI. C
ozmu
ta, Sc
ience
and T
echno
logy
Corpo
ration
, Moff
ett Fi
eld, C
A; D.
Ra
sky, N
ASA A
mes R
esearc
h Cen
ter,
Moffe
tt Field
, CA;
M. W
eave
r, W.
Ailor,
The A
erospa
ce Co
rporat
ion, E
l Se
gund
o, CA
; M. N
ewfie
ld, N
ASA A
mes
Resea
rch Ce
nter, M
offett
Field
, CA;
P. Su
brahm
anya
m, Sc
ience
and T
echno
logy
Corpo
ration
, Moff
ett Fi
eld, C
A
1100
hrs
AIAA-2
013-3
018
Comp
ariso
n of
Calor
imetr
ic Se
nsor
s - N
ASA
Ames
and I
RSA.
Nawa
z, Sie
rra Lo
bo, I
nc.,
Moffe
tt Fie
ld, CA
; S. L
oehle
, G. H
erdric
h, Un
iversi
ty of
Stutt
gart,
Stut
tgart,
Ge
rman
y; E.
Martin
ez, N
ASA A
mes
Rese
arch C
enter
, Moff
ett Fi
eld, C
A
67
Wedn
esda
y, 26
June
201
313
5-TP
-14
Heat
Tran
sfer I
IEx
ecut
ive Co
nfer
ence
2B
Chair
ed by
: E. S
ILK, N
ASA-G
odda
rd Sp
ace F
light
Cente
r09
00 hr
sAIA
A-201
3-301
9Ae
rody
nami
c Cha
racte
ristic
s Ev
aluat
ion U
nder
Hyp
erso
nic
Rare
fied F
low Co
nditio
nsT.
Suzu
ki, T.
Oza
wa, K
. Fuji
ta,
Japa
n Aero
spac
e Exp
lorati
on Ag
ency
(JA
XA),
Toky
o, Ja
pan
0930
hrs
AIAA-2
013-3
020
Two-
Dime
nsion
al Me
thyl
Radic
al Co
ncen
tratio
n Me
asur
emen
ts in
Flame
s usin
g Ra
dar R
EMPI
Y. W
u, Z.
Zhan
g, Un
iversi
ty of
Tenn
esse
e, Kn
oxvil
le, Kn
oxvil
le, TN
1000
hrs
AIAA-2
013-3
021
Inve
stiga
tion
of TD
LAS
with
VCSE
L at 9
50 n
m an
d 19
93 n
m fo
r Wat
er Va
pour
De
tectio
n in
High
Temp
erat
ure
Envir
onme
nts
H. Fu
lge, S
. Loe
hle, S
. Fas
oulas
, Un
iversi
ty of
Stutt
gart,
Stut
tgart,
Ge
rman
y
1030
hrs
AIAA-2
013-3
022
Effect
of G
eome
try on
Dro
plet
Form
ation
in a
Micro
fluidi
c Flow
-Fo
cusin
g Dev
iceH.
Matha
roo, D
. Mak
kar, A
. Gup
ta,
Indian
Instit
ute of
Techn
ology
New
Delhi,
Ne
w De
lhi, In
dia; S
. Hari
, M. R
amad
oss,
CD-ad
apco,
Bang
alore,
India
; R. K
umar,
Un
iversit
y of C
entra
l Flor
ida, O
rland
o, FL
Wedn
esda
y, 26
June
201
313
6-LN
CH-3
12
00 -
1300
hrs
Exhib
itor L
unch
Rec
eptio
nHa
rbor
Ball
room
III
Wedn
esda
y, 26
June
201
313
7-SB
-6
1300
- 13
30 h
rsWe
dnes
day A
ftern
oon
Spea
kers’
Brie
fing
Sessi
on R
ooms
Wedn
esda
y, 26
June
201
313
8-AP
A-29
Trans
onic
and S
uper
sonic
Aer
odyn
amics
Marin
a 2Ch
aired
by: K
. BRE
KKE,
Sand
ia Na
tiona
l Lab
s and
R. W
AHLS
, NAS
A-Lan
gley R
esea
rch Ce
nter
1330
hrs
AIAA-2
013-3
023
CFD
Simula
tion
of gr
id fin
flo
wsR.
Krish
namu
rthy,
N. S
hend
e, B.
Na
rayan
arao,
Indian
Insti
tute o
f Sc
ience
, Ban
galor
e, Ind
ia
1400
hrs
AIAA-2
013-3
024
Turb
ulenc
e Mod
el As
sessm
ent
for Si
mulat
ion of
Shoc
k Wav
e-Bo
unda
ry La
yer I
ntera
ction
Flow
sR.
Vieira
, Tech
nolog
ical In
stitute
of
Aeron
autics
(ITA)
, São
José
dos C
ampo
s, Bra
zil; J.
Azev
edo,
Aeron
autics
and
Space
Instit
ute (I
AE),
São J
osé do
s Ca
mpos,
Braz
il
1430
hrs
AIAA-2
013-3
025
Nume
rical
Study
of th
e Effe
ct of
Exit
Confi
gura
tions
on
Supe
rsonic
Inlet
Buz
zE.
Kwak
, S. L
ee, I
nha U
nivers
ity,
Inche
on, S
outh
Korea
1500
hrs
AIAA-2
013-3
026
Multip
le So
lution
s and
Buf
fet
of Tr
anso
nic Fl
ow ov
er th
e NA
CA00
12 A
irfoil
J. Xio
ng, Y
. Liu,
F. Li
u, S.
Luo,
Unive
rsity
of Ca
liforni
a, Irv
ine,
Irvine
, CA;
Z. Zh
ao, X
. Ren
, C.
Gao,
North
weste
rn Po
lytec
hnica
l Un
iversi
ty, X
i’an,
China
1530
hrs
AIAA-2
013-3
027
Dyna
mic D
eriva
tive C
ompu
tation
of
a Sub
-orbit
al Ve
hicle
C. Ma
rongiu
, Italia
n Aero
space
Resea
rch
Cente
r (CIR
A), C
apua
, Italy
; F. Ta
rfeld,
Ge
rman
Aeros
pace
Cente
r (DL
R),
Colog
ne, G
erman
y; H.
Adirim
, N. P
ilz,
Aeros
pace
Innov
ation
GmbH
, Berl
in,
Germ
any
1600
hrs
AIAA-2
013-3
028
Impa
ct of
Alte
rnat
ing Tr
ailing
-Ed
ge N
oise o
n Bu
ffet F
lows
A. Fe
ldhus
en, A
. Hart
mann
, M.
Klaas
, W. S
chröe
der, R
WTH
Aach
en
Unive
rsity,
Aach
en, G
erman
y
1630
hrs
AIAA-2
013-3
029
Multifi
delity
Aer
odyn
amics
wi
th Se
cond
Ord
er A
ugme
nted
Kr
iging
Ada
ptive
Samp
ling
H. S
chwa
rtz, C
. Lee
, D. M
avris
, Ge
orgia
Institu
te of
Tech
nolog
y, Atl
anta,
GA
Wedn
esda
y, 26
June
201
313
9-AP
A-30
High
Ang
le-of
-Atta
ck an
d High
lLft
Aero
dyna
mics
Marin
a 3Ch
aired
by: D
. LAC
Y, Bo
eing C
omme
rcial
Airpla
nes a
nd S
. MOR
RIS, E
ngine
ering
Sys
tems,
Inc.
1330
hrs
AIAA-2
013-3
030
CFD
Valid
ation
for t
he Su
perso
nic
Trans
port
Confi
gura
tion a
t Low
-Sp
eed a
nd H
igh Al
pha F
light
Cond
ition
D. Kw
ak, J
apan
Aeros
pace
Explo
ration
Ag
ency
(JAXA
), Tok
yo, J
apan
; K. O
hira,
Ryoy
u Syst
ems C
ompa
ny, Lt
d., N
agoy
a, Jap
an; M
. Gaff
uri, J
. Brez
illon,
Germ
an
Aeros
pace
Cente
r (DL
R), B
raunsc
hweig
, Ge
rman
y
1400
hrs
AIAA-2
013-3
031
Nume
rical
Inve
stiga
tion
of En
gine E
ffects
on th
e Sta
bility
and C
ontro
llabil
ity
of a
Trans
port
Aircr
aft w
ith
Circu
lation
Cont
rol
D. Ke
ller, G
erman
Aeros
pace
Cente
r (D
LR),
Brun
swick
, Germ
any
1430
hrs
AIAA-2
013-3
032
Analy
sis of
Low-
Spee
d Sta
ll Ae
rody
nami
cs of
a Sw
ept W
ing
with
Lami
nar-F
low G
love
T. Bu
i, NAS
A Dryd
en Fl
ight R
esea
rch
Cente
r, Edw
ards,
CA
1500
hrs
AIAA-2
013-3
033
Expe
rimen
tal I
nves
tigat
ions o
n th
e Pha
ntom
Yaw
Effe
ct on
a ma
neuv
ering
slen
der b
ody
O. W
ysoc
ki, E.
Sch
uelei
n, Ge
rman
Ae
rospa
ce Ce
nter (
DLR)
, Gött
ingen
, Ge
rman
y
1530
hrs
AIAA-2
013-3
034
Nume
rical
inves
tigat
ion on
the
Phan
tom
Yaw
Effe
ct du
e to
small
nos
e defl
ectio
nsC.
Schn
epf,
O. W
ysoc
ki, E.
Sch
uelei
n, Ge
rman
Aeros
pace
Cente
r (DL
R),
Göttin
gen,
Germ
any
1600
hrs
AIAA-2
013-3
035
Expe
rimen
tal A
nalys
is of
Se
para
tion
and T
rans
ition
Phen
omen
a for
the D
LR-F1
1 Hi
gh Li
ft Co
nfigu
ratio
nR.
Rudn
ik, G
erman
Aeros
pace
Cente
r (D
LR),
Brau
nsch
weig,
Germ
any
1630
hrs
AIAA-2
013-3
036
Expe
rimen
tal I
nves
tigat
ion of
Re
verse
Flow
over
Shar
p and
Bl
unt T
railin
g Edg
e Airf
oils
A. Lin
d, J.
Lefeb
vre’s,
A. Jo
nes,
Unive
rsity
of Ma
rylan
d, Co
llege
Park,
Co
llege
Park,
MD
1700
hrs
AIAA-2
013-3
037
Wall-
Mode
lled I
mplic
it La
rge-
Eddy
Simu
lation
of
the R
A16S
C1 H
ighlif
t Co
nfigu
ratio
nM.
Mey
er, EA
DS, M
unich
, Ge
rman
y; S.
Hick
el, C.
Br
eitsa
mter,
N. A
dams
, Tec
hnica
l Un
iversi
ty of
Munic
h, Mu
nich,
Germ
any
68
Wedn
esda
y, 26
June
201
314
0-AP
A-31
Unste
ady A
erod
ynam
ics II
Marin
a 4Ch
aired
by: J
. DEB
ONIS,
NAS
A Glen
n Res
earch
Cente
r and
J. D
ESPIR
ITO, U
S Arm
y Res
earch
Labo
ratory
1330
hrs
AIAA-2
013-3
039
Aero
dyna
mic P
erfo
rman
ce of
Fla
pping
Wing
s und
er A
cous
tic
Distu
rban
ces
Z. Ya
ng, G
. Hua
ng, S
. Hua
ng, W
right
State
Univ
ersity
, Day
ton, O
H
1400
hrs
AIAA-2
013-3
040
Analy
sis of
Dyn
amic
Stall u
sing
Dyna
mic M
ode D
ecom
posit
ion
Tech
nique
S. M
ariap
pan,
A. Ga
rdner,
K. Ri
chter
, M.
Raffe
l, Germ
an Ae
rospa
ce Ce
nter
(DLR
), Gö
ttinge
n, Ge
rman
y
1430
hrs
AIAA-2
013-3
041
Unste
ady A
erody
nami
cs Sim
ulatio
n of A
Road
Vehic
le Ru
nning
with
Cyclic
Yaw
and
Side-s
lip M
otion
sT.
Naka
shima
, Hiro
shima
Unive
rsity,
Higash
i-Hiro
shima
, Jap
an; Y
. Oka
da, T
. No
uzaw
a, Ma
zda M
otor C
orpora
tion,
Aki G
un, J
apan
; M. T
subok
ura, H
okka
ido
Unive
rsity,
Sapp
oro, J
apan
1500
hrs
AIAA-2
013-3
042
The M
easu
reme
nt an
d Co
mpar
ison
of th
e Uns
teady
Ae
rody
nami
c Cha
racte
ristic
s of
a De
lta W
ing in
the L
ater
al Mo
tions
X. G
eng,
Z. Sh
i, K. C
heng
, Nan
jing
Unive
rsity
of Ae
ronau
tics a
nd
Astro
nauti
cs, N
anjin
g, Ch
ina
1530
hrs
AIAA-2
013-3
043
Thre
e-dim
ensio
nal A
nalys
is of
th
e Fluc
tuat
ing P
ressu
re Fi
eld
of a
Spac
e Lau
nche
r Afte
rbod
y wi
th B
ooste
rs us
ing Z
DES
R. Pa
in, W
. Pier
re-Eli
e, S.
Dec
k, ON
ERA,
Meud
on, F
rance
1600
hrs
AIAA-2
013-3
044
Deve
loping
an A
ccura
te CF
D Ba
sed G
ust M
odel
for t
he Tr
uss
Brac
ed W
ing A
ircra
ftR.
Barte
ls, N
ASA L
angle
y Res
earch
Ce
nter, H
ampto
n, VA
Wedn
esda
y, 26
June
201
314
1-AP
A-32
Unma
nned
and V
STOL
Vehic
le De
signs
/tes
tsEx
ecut
ive Co
nfer
ence
2A
Chair
ed by
: L. A
UMAN
, US
Army A
RMDE
C and
W. F
RITZ,
Cassi
dian
1330
hrs
AIAA-2
013-3
045
Deve
lopme
nt of
the G
enii-
UAS
Demo
nstra
tor:
a Sma
ll-Cla
ss Ve
hicle
with
Low
Wing
Load
ing
and F
uel C
ell P
ropu
lsion
C. Ch
aney
, P. A
dam,
J. Le
achm
an,
K. Ma
tveev
, Was
hingto
n Stat
e Un
iversi
ty, Pu
llman
, WA
1400
hrs
AIAA-2
013-3
046
Flow
Field
Inve
stiga
tions
on a
UCAV
with
a Du
cted E
ngine
Air
Inta
ke at
Tran
sonic
Cond
itions
E. Ro
osen
boom
, R. K
onrat
h, J.
Agoc
s, D.
Otte
r, Germ
an Ae
rospa
ce Ce
nter
(DLR
), Gö
ttinge
n, Ge
rman
y
1430
hrs
AIAA-2
013-3
047
Imple
ment
ation
and V
alida
tion
of an
Actu
ator
Disk
Mod
el fo
r Aer
odyn
amic
Analy
sis of
Pr
opell
ed U
AVs
M. At
esog
lu, G
. Guz
el, As
elsan
, Inc
., An
kara,
Turke
y
1500
hrs
AIAA-2
013-3
048
Deve
lopme
nt of
the Ci
rculat
ion
Contr
ol Flo
w Sch
eme u
sed in
the
NTF S
emi-S
pan F
AST-M
AC M
odel
G. Jon
es, W
. Milho
len, D
. Cha
n, B.
Allan
, S.
Good
liff, L
. Pack
Melt
on, S
. And
ers,
M. Ca
rter, F
. Cap
one,
NASA
Lang
ley
Resea
rch Ce
nter, H
ampto
n, VA
Wedn
esda
y, 26
June
201
314
2-AP
A-33
/FD-
33Bi
o-In
spire
d Aer
odyn
amics
IIEx
ecut
ive Co
nfer
ence
1Ch
aired
by: H
. HU,
Iowa
Stat
e Univ
ersity
and M
. PLE
SNIAK
, Geo
rge W
ashin
gton U
nivers
ity13
30 hr
sAIA
A-201
3-304
9A
Nume
rical
Analy
sis of
Bu
mbleb
ee P
ropu
lsion
S. To
bing,
J. Yo
ung,
J. La
i, Univ
ersity
of
New
South
Wale
s at t
he Au
strali
an
Defen
ce Fo
rce Ac
adem
y, Ca
nberr
a, Au
strali
a
1400
hrs
AIAA-2
013-3
050
Lift c
hara
cteris
tics o
f a
hove
ring r
ufou
s hum
ming
bird
J. So
ng, H
. Luo
, Van
derbi
lt Univ
ersity
, Na
shvil
le, TN
; T. H
edric
k, Un
iversi
ty of
North
Carol
ina, C
hape
l Hill,
Chap
el Hil
l, NC
1430
hrs
AIAA-2
013-3
052
Inve
stiga
tion
of vo
rtex
form
ation
on a
hovin
g wing
us
ing h
igh-fi
delity
simu
lation
D. G
arman
n, M.
Visb
al, Ai
r Forc
e Re
searc
h Lab
orator
y, W
right-
Patte
rson A
FB, O
H
1500
hrs
AIAA-2
013-3
053
Analy
sis of
a Va
riable
Camb
er
Wing
durin
g High
ly Un
stead
y Ma
neuv
ers
Z. Le
go, A
. Altm
an, U
nivers
ity of
Da
yton,
Dayto
n, OH
1530
hrs
AIAA-2
013-3
051
Effe
ct of
wing
flex
ibility
on
phas
ing of
tand
em w
ings
durin
g hov
er fl
ight
V. Na
idu, J
. You
ng, J
. Lai,
Univ
ersity
of
New
South
Wale
s at t
he Au
strali
an
Defen
ce Fo
rce Ac
adem
y, Ca
nberr
a, Au
strali
a
69
Wedn
esda
y, 26
June
201
314
3-AS
E-9Su
perco
oled L
arge
Dro
p and
Icing
Phy
sics
Room
515
Chair
ed by
: M. P
OTAP
CZUK
, NAS
A Glen
n Res
earch
Cente
r and
C. TA
N, G
E13
30 hr
sAIA
A-201
3-305
4Dr
ag Co
effic
ient o
f Wat
er
Drop
lets a
ppro
achin
g the
Le
ading
Edge
of an
Airf
oilM.
Varga
s, NA
SA G
lenn R
esea
rch
Cente
r, Clev
eland
, OH;
S. S
or, A.
Ga
rcía M
agari
ño, N
ation
al Ins
titute
of Ae
rospa
ce Te
chno
logy (
INTA
), Ma
drid,
Spain
1400
hrs
AIAA-2
013-3
055
Linea
rized
Solut
ions o
f Thr
ee-
Dime
nsion
al Co
nden
sed L
ayer
Fil
msA.
Rothm
ayer,
H. H
u, Iow
a Stat
e Un
iversi
ty, Am
es, I
A
1430
hrs
AIAA-2
013-3
056
The E
ffect
of Te
mper
atur
e and
Wa
ter Fi
lm Th
ickne
ss on
the
Linea
r Ins
tabil
ity of
an Ic
e Su
rface
A. Ro
thmay
er, H
. Hu,
Iowa S
tate
Unive
rsity,
Ames
, IA
1500
hrs
AIAA-2
013-3
057
Quas
i-mole
cular
Mod
eling
of
Supe
rcoole
d Lar
ge D
rople
ts Dy
nami
cs fo
r In-
fligh
t Icin
g Sim
ulatio
nsV.
Abdo
llahi,
W. H
abas
hi, M
. Fos
sati,
McGil
l Univ
ersity
, Mon
tréal,
Cana
da;
G. B
aruzz
i, New
meric
al Te
chno
logies
Int
ernati
onal,
Mon
tréal,
Cana
da
1530
hrs
AIAA-2
013-3
058
An Eu
lerian
Re-im
pinge
ment
Mode
l of S
plash
ing an
d Bou
ncing
Su
perco
oled L
arge
Dro
plets
D. Bil
odea
u, W.
Haba
shi, M
cGill
Unive
rsity,
Montr
éal, C
anad
a; G.
Baruz
zi,
Newm
erical
Techn
ologie
s Inte
rnatio
nal,
Montr
éal, C
anad
a; M.
Fossa
ti, Mc
Gill
Unive
rsity,
Montr
éal, C
anad
a
1600
hrs
AIAA-2
013-3
059
Mode
ling o
f Rea
listic
Ice
Rou
ghne
ss Ele
ment
Di
stribu
tions
to Ch
arac
terize
Co
nvec
tive H
eat T
rans
fer
L. Te
cson,
S. M
cClai
n, Ba
ylor
Unive
rsity,
Wac
o, TX
1630
hrs
AIAA-2
013-3
060
Conv
ectiv
e Enh
ance
ment
of
Surfa
ces w
ith R
ealis
tic Ic
e Ro
ughn
ess D
istrib
ution
sL.
Tecso
n, S.
McC
lain,
Baylo
r Un
iversi
ty, W
aco,
TX
Wedn
esda
y, 26
June
201
314
4-CF
D-36
High
-Ord
er M
ethod
s VI
Naut
ilus 5
Chair
ed by
: H. L
UO, N
orth C
arolin
a Stat
e Univ
ersity
and E
. JOH
NSEN
, Univ
ersity
of M
ichiga
n13
30 hr
sAIA
A-201
3-306
1Sh
ock
Capt
uring
for H
igh-
Orde
r Disc
ontin
uous
Gale
rkin
Simula
tion
of Tr
ansie
nt Fl
ow
Prob
lems
P. Pe
rsson
, Univ
ersity
of Ca
liforni
a, Be
rkeley
, Berk
eley,
CA
1400
hrs
AIAA-2
013-3
062
A Par
allel,
Impli
cit Re
cons
tructe
d Di
sconti
nuou
s Gale
rkin
Metho
d for
the C
ompr
essibl
e Flow
s on 3
D Ar
bitra
ry G
rids
Y. Xia
, H. L
uo, S
. Spie
gel, M
. Frisb
ey,
North
Carol
ina St
ate Un
iversit
y, Ra
leigh,
NC; R
. Nou
rgaliev
, Idah
o Nati
onal
Labo
ratory
, Idah
o Falls
, ID
1430
hrs
AIAA-2
013-3
063
A Re
cons
tructe
d Disc
ontin
uous
Ga
lerkin
Meth
od B
ased
on
a Hi
erar
chica
l WEN
O Re
cons
tructi
on fo
r Com
putin
g Sh
ock
Wave
s on
Hybr
id Gr
idsH.
Luo,
North
Carol
ina S
tate
Unive
rsity,
Ralei
gh, N
C
1500
hrs
AIAA-2
013-3
064
3D M
ixed E
lemen
t Di
scont
inuou
s Gale
rkin
with
Sh
ock
Capt
uring
M. B
razell
, D. M
avrip
lis, U
nivers
ity of
W
yomi
ng, L
arami
e, La
ramie,
WY
1530
hrs
AIAA-2
013-3
065
Towa
rd A
ccura
te Sim
ulatio
n of
Shoc
kwav
e-Tu
rbule
nce
Inter
actio
n on
Uns
tructu
red
Mesh
es: A
Coup
ling o
f High
-Or
der F
R an
d LAD
Sche
mes
T. Ha
ga, S
. Kaw
ai, Ja
pan A
erosp
ace
Explo
ration
Agen
cy (J
AXA)
, Sa
gami
hara,
Japa
n
1600
hrs
AIAA-2
013-3
066
Reco
very
Disc
ontin
uous
Ga
lerkin
Meth
od fo
r Co
mpre
ssible
Turb
ulenc
eE.
John
sen,
A. Na
ir, S.
Varad
an,
Unive
rsity
of Mi
chiga
n, An
n Arbo
r, An
n Arbo
r, MI
1630
hrs
AIAA-2
013-3
067
Disco
ntinu
ous G
alerk
in Me
thod
fo
r Com
pres
sible
Visco
us
Reac
ting F
lowY.
Lv, M
. Ihm
e, Un
iversi
ty of
Mich
igan,
Ann A
rbor, A
nn Ar
bor, M
I
Wedn
esda
y, 26
June
201
314
5-CF
D-37
Rece
nt D
evelo
pmen
t of C
E/SE
Meth
ods (
Invit
ed)
Naut
ilus 4
Chair
ed by
: X. W
ANG,
NAS
A Glen
n Res
earch
Cente
r and
C. CH
ANG,
NAS
A-Lan
geley
Rese
arch C
enter
1330
hrs
Oral
Prese
ntatio
n (Inv
ited)
The C
ESE M
ethod
as a
Cons
isten
t Num
erica
l Fr
amew
ork
for A
ccura
te Co
mput
ation
s of C
onse
rvat
ion
Laws
-- A
Rev
iewC.
Chan
g, NA
SA La
ngley
Rese
arch
Cente
r, Ham
pton,
VA
1400
hrs
AIAA-2
013-3
068
Recen
t CES
E Dev
elopm
ents
for
the So
lution
of th
e Nav
ier-St
okes
Eq
uatio
ns U
sing U
nstru
ctured
Tri
angu
lar or
Tetra
hedr
al Me
shes
Wi
th Hi
gh As
pect
Ratio
S. Ch
ang,
NASA
Glen
n Rese
arch C
enter
, Cle
velan
d, OH
; C. C
hang
, NAS
A Lan
gley
Resea
rch Ce
nter, H
ampto
n, VA
; C. Y
en,
Jacob
s, Tul
lahom
a, TN
1430
hrs
AIAA-2
013-3
069
Time-A
ccura
te Lo
cal T
ime
Stepp
ing an
d High
-Ord
er
Spac
e Tim
e CES
E Meth
ods f
or
Multi-
Dime
nsion
al Flo
ws U
sing
Unstr
uctur
ed M
eshes
C. Ch
ang,
NASA
Lang
ley Re
search
Ce
nter, H
ampto
n, VA
; B. V
enka
tacha
ri, G.
Chen
g, Un
iversit
y of A
labam
a, Bir
ming
ham,
Birm
ingha
m, AL
1500
hrs
Oral
Prese
ntatio
n (Inv
ited)
Demo
nstra
tion
of a
Time-
Accu
rate
Loca
l-Tim
e-Ste
pping
CE
SE M
ethod
for a
n Ac
ousti
c Re
sona
nce S
tudy
with
an
Open
-Jet W
ind Tu
nnel
Geom
etry
C. Ye
n, Ja
cobs
, Tull
ahom
a, TN
1530
hrs
Oral
Prese
ntatio
n (Inv
ited)
Impa
ct of
Grid
Qua
lity on
Ac
cura
cy of
CESE
Simu
lation
sB.
Venk
atach
ari, G
. Che
ng,
Unive
rsity
of Ala
bama
, Birm
ingha
m,
Birmi
ngha
m, AL
; C. C
hang
, NAS
A La
ngley
Rese
arch C
enter
, Ham
pton,
VA; S
. Cha
ng, N
ASA G
lenn R
esea
rch
Cente
r, Clev
eland
, OH
1600
hrs
AIAA-2
013-3
070
Appli
catio
ns of
the C
ESE
meth
od in
LS-D
YNA
G. Co
ok, Z
. Zha
ng, K
. Im,
Live
rmore
So
ftware
Tech
nolog
y Corp
oratio
n, Liv
ermore
, CA
1630
hrs
AIAA-2
013-3
071
A 3D
Uns
tructu
red-
Mesh
Euler
So
lver B
ased
on th
e Fou
rth-
Orde
r CES
E Meth
odD.
Bily
eu, S
. Yu,
Ohio
State
Un
iversi
ty, Co
lumbu
s, OH
1700
hrs
AIAA-2
013-3
072
Simula
tion
of a
Statio
nary
Pla
sma T
hrus
ter u
sing t
he
Spac
e-Tim
e Con
serv
ation
Me
thod
J. Mu
rphy,
The A
erosp
ace
Corpo
ration
, El S
egun
do, C
A
70
Wedn
esda
y, 26
June
201
314
6-CF
D-38
Grid
Gene
ratio
n an
d Effe
cts of
Grid
Qua
lity II
Seab
reez
e ICh
aired
by: R
. DAV
IS, U
nivers
ity of
Califo
rnia D
avis
and D
. THO
MPSO
N, M
ississ
ippi S
tate U
nivers
ity13
30 hr
sAIA
A-201
3-307
3Th
e Eng
ineer
ing Sk
etch
Pad:
A So
lid-M
odeli
ng, F
eatu
re-B
ased
, We
b-En
abled
Syste
m fo
r Bu
ilding
Par
ametr
ic Ge
ometr
yR.
Haim
es, M
assa
chus
etts I
nstitu
te of
Tech
nolog
y, Ca
mbrid
ge, M
A; J.
Dann
enho
ffer, S
yracu
se U
nivers
ity,
Syrac
use,
NY
1400
hrs
AIAA-2
013-3
074
Effic
ient C
reat
ion of
Ove
rset
Grid
Hole
Boun
darie
s and
Ef
fects
of Th
eir Lo
catio
ns on
Ae
rody
nami
c Loa
dsW.
Chan
, S. P
andy
a, S.
Roge
rs,
NASA
Ames
Rese
arch C
enter
, Moff
ett
Field,
CA
1430
hrs
AIAA-2
013-3
075
Prog
ress
in Au
toma
tic Vi
scous
Me
shing
from
CAD
Using
Str
and/
Carte
sian
Mesh
esA.
Wiss
ink, A
rmy A
viatio
n and
Mi
ssile
Rese
arch D
evelo
pmen
t and
En
ginee
ring C
enter
, Moff
ett Fi
eld,
CA; A
. Katz
, Utah
Stat
e Univ
ersity
, Lo
gan,
UT; J
. Sita
raman
, Univ
ersity
of
Wyo
ming
, Lara
mie,
Laram
ie, W
Y; R.
Haim
es, M
assa
chus
etts I
nstitu
te of
Tech
nolog
y, Ca
mbrid
ge, M
A
1500
hrs
AIAA-2
013-3
076
An Im
prov
ed Po
int Se
lectio
n Me
thod f
or H
ybrid
-Uns
tructu
red
Mesh
Defo
rmati
on U
sing R
adial
Ba
sis Fu
nctio
nsG.
Wang
, H. H
amee
d, Z.
Ye,
North
weste
rn Po
lytech
nical
Unive
rsity,
Xi’an
, Chin
a; J.
Lee, B
eijing
Aeron
autica
l Sc
ience
and T
echno
logy R
esearc
h Ins
titute,
Beijin
g, Ch
ina
1530
hrs
AIAA-2
013-3
077
Crea
ting E
xact
Bezie
r Re
pres
enta
tions
of CS
T Sha
pes
D. M
arsha
ll, Ca
liforni
a Poly
techn
ic St
ate U
nivers
ity, S
an Lu
is Ob
ispo,
CA
Wedn
esda
y, 26
June
201
314
7-CF
D-39
Larg
e-Ed
dy Si
mulat
ion (L
ES),
Dire
ct Nu
meric
al Sim
ulatio
n (D
NS),
and H
ybrid
RAN
S/LE
S Meth
ods I
IISp
inake
r ICh
aired
by: K
. DUR
AISAM
Y, Un
iversi
ty of
Glasg
ow13
30 hr
sAIA
A-201
3-307
8Co
mput
ation
al sh
ip air
wake
de
termi
natio
n to
supp
ort
helic
opter
-ship
dyna
mic
inter
face
asse
ssmen
tJ.
Van M
uijde
n, O.
Boe
lens,
J. va
n der
Vorst
, J. G
oode
n, Na
tiona
l Ae
rospa
ce La
borat
ory (N
LR),
Amste
rdam,
The N
etherl
ands
1400
hrs
AIAA-2
013-3
079
Refin
emen
t of a
Two-
Equa
tion
Hybr
id RA
NS/L
ES M
odel
in BC
FDC.
Wink
ler, A
. Dorg
an, M
. Man
i, The
Bo
eing C
ompa
ny, S
t. Lo
uis, M
O
1430
hrs
AIAA-2
013-3
080
Larg
e Edd
y Sim
ulatio
n of
lean
blo
w of
fE.
Hodiz
c, C.
Duwi
g, R.
Szas
z, Lu
nd
Unive
rsity,
Lund
, Swe
den;
O. Kr
üger,
He
rman
n-Fött
inger-
Institu
t, TU
-Berlin
, Ge
rman
y; L.
Fuch
s, Lu
nd U
nivers
ity,
Lund
, Swe
den
1500
hrs
AIAA-2
013-3
081
A Ne
w Cr
ossfl
ow Tr
ansit
ion
Onse
t Crit
erion
for R
ANS
Turb
ulenc
e Mod
elsS.
Med
ida, J
. Bae
der, U
nivers
ity
of Ma
rylan
d, Co
llege
Park,
Colle
ge
Park,
MD
Wedn
esda
y, 26
June
201
314
8-CF
D-40
Othe
r Meth
ods f
or CF
D/Un
stead
y Flow
s III
Marin
a 5Ch
aired
by: B
. KOR
EN13
30 hr
sAIA
A-201
3-308
2A r
obus
t sim
plex c
ut-cel
l meth
od
for hi
gh-or
der d
iscon
tinuo
us
Galer
kin di
screti
zatio
ns of
thr
ee-di
mens
ional
aero
dyna
mic
prob
lems
H. Su
n, D.
Darm
ofal, R
. Haim
es,
Massa
chuset
ts Ins
titute
of Tec
hnolo
gy,
Camb
ridge
, MA
1400
hrs
AIAA-2
013-3
083
Aniso
tropic
Out
put-B
ased
Mes
h Op
timiza
tion
for U
nstea
dy
Flows
J. Kra
kos,
The B
oeing
Comp
any,
St. L
ouis,
MO;
D. D
armofa
l, Ma
ssach
usett
s Ins
titute
of Te
chno
logy,
Camb
ridge
, MA
1430
hrs
AIAA-2
013-3
084
GMRE
S app
lied t
o the
Time
Sp
ectra
l and
Qua
si-pe
riodic
Tim
e Spe
ctral
Meth
ods
N. M
undis
, D. M
avrip
lis, U
nivers
ity of
W
yomi
ng, L
arami
e, La
ramie,
WY
1500
hrs
AIAA-2
013-3
085
Rung
e-Ku
tta m
ethod
s for
the
incom
pres
sible
Navie
r-Sto
kes
equa
tions
B. S
ande
rse, E
nergy
Rese
arch C
enter
of
the N
etherl
ands
, Pett
en, T
he
Nethe
rland
s; B.
Koren
, Eind
hove
n Un
iversi
ty of
Tech
nolog
y, Ein
dhov
en,
The N
etherl
ands
1530
hrs
AIAA-2
013-3
086
Effic
ient c
ompu
tatio
n of
the
finite
-time
Lyap
unov
expo
nent
P. Mi
ron, J
. Véte
l, A. G
aron,
École
Po
lytec
hniqu
e de M
ontré
al, M
ontré
al,
Cana
da
1600
hrs
AIAA-2
013-3
087
Nume
rical
Mode
ling a
nd
Valid
ation
of th
e Flow
in a
Fluidi
c Osci
llato
rO.
Krüg
er, B
. Bob
usch
, R. W
oszid
lo,
C. Pa
schere
it, Te
chnic
al Un
iversi
ty of
Berlin
, Berl
in, G
erman
y
1630
hrs
Oral
Prese
ntatio
n (Inv
ited)
A co
mplet
ely co
nser
vativ
e dif
fere
nce s
chem
e for
mo
delin
g elas
topla
stic fl
ows i
n La
gran
gian
varia
bles
N. Es
kov,
Y. Pro
nin, R
ussia
n Fed
eral
Nucle
ar Ce
ntre,
Snez
hinsk
, Rus
sia
71
Wedn
esda
y, 26
June
201
314
9-CF
D-41
Nume
rical
Erro
r Esti
matio
n an
d Unc
erta
inty Q
uant
ifica
tion
in CF
DRo
om 5
18Ch
aired
by: C
. OLLI
VIER G
OOCH
, Univ
ersity
of B
ritish
Colum
bia an
d C. R
OY, V
irgini
a Tec
h13
30 hr
sAIA
A-201
3-308
8Co
de Ve
rifica
tion
of an
un
stead
y RAN
S finit
e-ele
ment
so
lver
A. Ha
y, S.
Etien
ne, D
. Pell
etier,
A.
Garon
, Éco
le Po
lytec
hniqu
e de
Montr
éal, M
ontré
al, Ca
nada
1400
hrs
AIAA-2
013-3
089
Eigen
analy
sis of
Trun
catio
n an
d Disc
retiz
ation
Erro
r on
Unstr
uctu
red M
eshe
sM.
Sha
rbatda
r, C. O
llivier
Goo
ch,
Unive
rsity
of Br
itish C
olumb
ia,
Vanc
ouve
r, Can
ada
1430
hrs
AIAA-2
013-3
090
Finite
Volum
e Solu
tion
Reco
nstru
ction
Meth
ods F
or
Trunc
ation
Erro
r Esti
matio
nT.
Phillip
s, J.
Derla
ga, C
. Roy,
J.
Borgg
aard,
Virgi
nia Po
lytech
nic In
stitute
an
d Stat
e Univ
ersity,
Black
sburg,
VA
1500
hrs
AIAA-2
013-3
091
Optim
al Se
nsor
Loca
tion
for
Mode
l Par
amete
r Esti
matio
n in
CFD
D. Pa
padim
itriou
, C. P
apad
imitri
ou,
Unive
rsity
of Th
essa
ly, Vo
los, G
reece
Wedn
esda
y, 26
June
201
315
0-CF
D-42
Othe
r Top
ics in
CFD
IIIRo
om 5
14Ch
aired
by: J
. DAN
NENH
OFFE
R, Sy
racus
e Univ
ersity
and C
. RUS
CHER
, Syra
cuse
Univ
ersity
1330
hrs
AIAA-2
013-3
092
Mode
ling F
low Th
roug
h a
Perfo
rated
Plate
for a
New
Co
mbus
tion R
igC.
Rusch
er, J.
Dann
enho
ffer, M
. Glau
ser,
Syrac
use Un
iversit
y, Sy
racuse
, NY;
B. Se
kar, V
. Belo
vich,
Air Fo
rce Re
search
La
borat
ory, W
right-
Patte
rson A
FB, O
H
1400
hrs
AIAA-2
013-3
093
Nume
rical
Study
of Fi
xed
Artifi
cial T
rans
ition
and t
he
Minim
um H
eight
of R
ough
ness
Strip
for I
tZ.
Zhan
g, No
rthwe
stern
Polyt
echn
ical
Unive
rsity,
Xi’a
n, Ch
ina
1430
hrs
AIAA-2
013-3
094
Low-
stora
ge IM
EX R
unge
-Kut
ta
schem
es fo
r the
simu
lation
of
Navie
r-Sto
kes s
ystem
sD.
Cava
glieri
, P. B
eyha
ghi, T
. Bew
ley,
Unive
rsity
of Ca
liforni
a, Sa
n Dieg
o, La
Jolla
, CA
Wedn
esda
y, 26
June
201
315
1-FD
-34
Turb
ulent
Flow
s: Je
ts an
d Wak
esRo
om 5
11Ch
aired
by: A
. ELM
ILIGU
I, NA
SA La
ngley
Rese
arch C
enter
and J
. KUH
LMAN
, Wes
t Virg
inia U
nivers
ity13
30 hr
sAIA
A-201
3-309
5Nu
meric
al inv
estig
ation
of th
e flo
w pr
edict
ion ar
ound
a wa
ll-mo
unted
recta
ngula
r cyli
nder
Z. Ch
en, M
. El H
assa
n, Z.
Hosse
ini,
R. Ma
rtinuz
zi, U
nivers
ity of
Calga
ry,
Calga
ry, Ca
nada
1400
hrs
AIAA-2
013-3
096
Enfo
rceme
nt of
Flow
-Indu
ced
Oscil
lation
s of a
Circu
lar
Cylin
der d
ue to
Inter
fere
nce
Effe
cts -N
umer
ical S
imula
tions
an
d Exp
erim
enta
l Stu
dies-
R. He
inze,
S. B
ecke
rs, T.
Wah
l, F.
Kame
ier, U
nivers
ity of
Appli
ed
Scien
ces,
Düsse
ldorf,
Germ
any;
C. Pa
schere
it, Te
chnic
al Un
iversi
ty of
Berlin
, Berl
in, G
erman
y
1430
hrs
AIAA-2
013-3
097
Deta
ched
Eddy
Simu
lation
s of
Supe
rsonic
Jets
Impin
ging o
n Fla
t Plat
esY.
Dewa
n, V.
Golub
ev, A
. Lyri
ntzis,
R.
Mank
badi,
Embry
-Ridd
le Ae
ronau
tical
Unive
rsity,
Day
tona B
each
, FL;
K. Ku
rbatsk
ii, AN
SYS,
Inc.,
Leba
non,
NH; E
. Osm
an, U
nited
Laun
ch
Allian
ce, C
enten
nial, C
O
1500
hrs
AIAA-2
013-3
098
Dire
ct Nu
meric
al Sim
ulatio
n of
a R
ecta
ngula
r Sup
erso
nic Je
t Im
pingin
g on
a Soli
d Wall
K. Ak
htar, S
. Rag
ab, V
irgini
a Po
lytec
hnic
Institu
te an
d Stat
e Un
iversi
ty, B
lacks
burg,
VA
1530
hrs
AIAA-2
013-3
099
Unste
ady M
odeli
ng of
Jet-i
n-Cr
ossfl
ow P
roble
msS.
Arun
ajates
an, M
. McW
herte
r-Pa
yne,
Sand
ia Na
tiona
l Lab
orator
ies,
Albuq
uerqu
e, NM
1600
hrs
AIAA-2
013-3
100
Nume
rical
inves
tigat
ion of
sca
lar m
ixing
in th
e tur
bulen
t wa
ke of
a sq
uare
cylin
der
G. Lo
dato,
INSA
Roue
n, Ro
uen,
Franc
e; R.
Rossi
, Univ
ersity
of
Bolog
na, B
ologn
a, Ita
ly
72
Wedn
esda
y, 26
June
201
315
2-FD
-35
Hype
rsonic
and C
hemi
cally
-Rea
cting
Flow
s II
Naut
ilus 1
Chair
ed by
: A. A
LEXE
ENKO
, Purd
ue U
nivers
ity an
d T. D
ROZD
A, NA
SA La
ngley
Rese
arch C
enter
1330
hrs
AIAA-2
013-3
101
Nume
rical
Simula
tion
of th
e No
zzle
and T
est S
ectio
n of
a Ma
ch 6
Ludw
ieg Tu
beB.
Agha
babia
n, B.
Reym
ond,
Milita
ry Sc
hool
of Air
and S
pace
, Salo
n Air,
Franc
e; R.
Cumm
ings,
U.S.
Air F
orce
Acad
emy,
Color
ado S
pring
s, CO
1400
hrs
AIAA-2
013-3
102
Visua
lizat
ion of
Shoc
k Tra
in-Bo
unda
ry La
yer I
nter
actio
n in
Mach
2.5
Isola
tor F
lowJ.
Geert
s, K.
Yu, U
nivers
ity of
Ma
rylan
d, Co
llege
Park,
Colle
ge
Park,
MD
1430
hrs
AIAA-2
013-3
103
Oscil
lation
of B
ow-sh
ock
Wave
s at
Hyp
erso
nic Sp
eeds
K. Fu
jii, S
. Tsu
da, T
. Koy
ama,
N.
Hirab
ayas
hi, Ja
pan A
erosp
ace
Explo
ration
Agen
cy (J
AXA)
, Cho
fu,
Japa
n
1500
hrs
AIAA-2
013-3
104
Nitri
c Oxid
e Che
mistr
y Effe
cts
in Hy
perso
nic B
ound
ary L
ayer
sC.
Arism
an, C
. Joh
anse
n, W.
Galu
ppo,
A. Mc
Phail
, Univ
ersity
of Ca
lgary,
Ca
lgary,
Cana
da
Wedn
esda
y, 26
June
201
315
3-FD
-36
Roug
hnes
s Ind
uced
Tran
sition
Naut
ilus 2
Chair
ed by
: H. J
OHNS
ON, U
nivers
ity of
Minn
esota
and R
. KIN
G, N
ASA-L
angle
y Res
earch
Cente
r13
30 hr
sAIA
A-201
3-310
5Ro
ughn
ess I
nduc
ed Tr
ansit
ion
in a S
uper
sonic
Bou
ndar
y La
yer
P. Ba
lakum
ar, M
. Keg
erise
, NAS
A La
ngley
Rese
arch C
enter
, Ham
pton,
VA
1400
hrs
AIAA-2
013-3
106
Uncer
tainty
Qua
ntific
ation
Ba
sed Re
ceptiv
ity M
odell
ing of
Cro
ssflow
Insta
bilitie
s Ind
uced
by
Distr
ibuted
Surfa
ce Ro
ughn
ess in
Sw
ept W
ing Bo
unda
ry La
yers
M. M
ugha
l, Imp
erial
Colleg
e Lon
don,
Lond
on, U
nited
King
dom;
R. As
hwort
h, EA
DS, B
ristol,
Unite
d King
dom
1430
hrs
AIAA-2
013-3
107
Distr
ibuted
-Rou
ghne
ss-In
duce
d Tra
nsien
t Gro
wth
in a F
lat P
late
Boun
dary
Laye
rM.
Kues
ter, E
. Whit
e, Te
xas A
&M
Unive
rsity,
Colle
ge S
tation
, TX
1500
hrs
AIAA-2
013-3
108
The E
ffect
of Tw
o-Di
mens
ional
Geom
etric
Distu
rban
ces o
n Bo
unda
ry-La
yer S
tabil
ityD.
Rizz
etta,
M. V
isbal,
Air F
orce
Rese
arch L
abora
tory,
Wrig
ht-Pa
tterso
n AFB
, OH
1530
hrs
AIAA-2
013-3
109
The I
nflue
nce o
f a Cy
lindr
ical
Roug
hnes
s Elem
ent o
n a
Pertu
rbed
Lami
nar B
ound
ary
Laye
rB.
Plog
mann
, W. W
uerz,
Univ
ersity
of
Stutt
gart,
Stut
tgart,
Germ
any
1600
hrs
AIAA-2
013-3
110
Effe
ct of
a Sm
all Su
rface
Wav
e on
Bou
ndar
y-La
yer T
rans
ition
A. Ga
rzon,
M. Ro
berts
, Aeri
on
Corpo
ration
, Ren
o, NV
1630
hrs
AIAA-2
013-3
111
Simula
tion
of Tr
ansit
ions
Indu
ced b
y Rou
ghne
ss Us
ing
Thre
e-Eq
uatio
n Tra
nsitio
n Mo
del
Z. Hu
a, Tsi
nghu
a Univ
ersity
, Beij
ing,
China
1700
hrs
AIAA-2
013-3
112
Trans
ition T
rigge
red by
Isola
ted
Roug
hness
Elem
ent U
sing
Impr
oved
Dela
yed D
etach
ed
Eddy
Simu
lation
Mod
elZ.
Duan
, Z. X
iao, S
. Fu,
Tsing
hua
Unive
rsity,
Beijin
g, Ch
ina
Wedn
esda
y, 26
June
201
315
4-FD
-37
High
-Spe
ed Fl
ow Co
ntro
lNa
utilu
s 3Ch
aired
by: F
. ALV
I, Flo
rida S
tate U
nivers
ity13
30 hr
sAIA
A-201
3-311
3Ap
plica
tion
of A
eros
pikes
for
Liftin
g-Bo
dy Co
nfigu
ratio
n in
Hype
rsonic
Flow
at M
ach
7S.
Khura
na, K
. Suz
uki, U
nivers
ity of
To
kyo,
Kash
iwa,
Japa
n
1400
hrs
AIAA-2
013-3
114
A no
vel m
eans
of di
ssipa
tion
of
shoc
k wa
ve in
duce
d hea
t in
a hig
h sp
eed fl
owY.
Zhen
g, N.
Ahme
d, Un
iversi
ty of
New
South
Wale
s, Sy
dney
, Aus
tralia
1430
hrs
AIAA-2
013-3
115
Plasm
a Con
trol o
f SW
Confi
gura
tion
in M=
2 In
let at
Of
f-Des
ign M
ode
S. Le
onov
, D. Y
arants
ev, A
. Firs
ov,
Russi
an Ac
adem
y of S
cienc
es,
Mosco
w, Ru
ssia;
F. Fa
lempin
, MBD
A, Le
Ples
sis Ro
binso
n, Fra
nce;
M.
Goldf
eld, P
. Geo
rge, R
ussia
n Aca
demy
of
Scien
ces,
Novo
sibirs
k, Ru
ssia
1500
hrs
AIAA-2
013-3
116
Activ
e Sho
ck Co
ntro
l in a
Trans
onic
Flow
A. Gis
sen,
B. Vu
kasin
ovic,
A. G
lezer,
Ge
orgia
Institu
te of
Tech
nolog
y, Atl
anta,
GA;
G. S
ivaram
, Spe
ctral
Energ
ies, D
ayton
, OH
1530
hrs
AIAA-2
013-3
117
Thre
e - di
mens
ional
Flowfi
eld
of M
icroje
ts in
Supe
rsonic
Cr
ossfl
owM.
Ali, N
. Aror
a, F.
Alvi, F
lorida
Stat
e Un
iversi
ty, Ta
llaha
ssee,
FL
73
Wedn
esda
y, 26
June
201
315
5-FD
-38
Turb
ulenc
eSp
inake
r II
Chair
ed by
: J. E
DWAR
DS an
d R. M
OARR
EF, Ca
liforni
a Ins
titute
of Te
chno
logy
1330
hrs
AIAA-2
013-3
118
Closin
g the
loop
: an
expli
cit
calcu
lation
of th
e non
linea
rity
in th
e res
olven
t for
mulat
ion of
wa
ll tur
bulen
ceA.
Sharm
a, Un
iversi
ty of
Sheffi
eld,
Sheffi
eld, U
nited
King
dom;
B.
McKe
on, C
alifor
nia In
stitut
e of
Tech
nolog
y, Pa
sade
na, C
A
1400
hrs
AIAA-2
013-3
119
Turb
ulenc
e Stru
cture
and
its Si
gnat
ure i
n Hy
perso
nic
Turb
ulent
Bou
ndar
y Lay
ers
Y. Ka
n, P.
Martin
, Univ
ersity
of
Maryl
and,
Colle
ge Pa
rk, Co
llege
Pa
rk, M
D
1430
hrs
AIAA-2
013-3
120
Exam
inatio
n of t
he sp
atiall
y de
velop
ing w
ind tu
rbine
bo
unda
ry la
yer:
Low
dimen
siona
l an
alysis
, larg
e sca
les of
moti
on
and e
nerg
y entr
ainme
ntL.
Castil
lo, A.
New
man,
Texas
Tech
Unive
rsity,
Lubb
ock, T
X
1500
hrs
AIAA-2
013-3
121
Turb
ulenc
e diff
usion
effe
cts
at m
ater
ial in
terfa
ces,
with
ap
plica
tion
to th
e Ray
leigh
-Ta
ylor i
nsta
bility
P. Mo
vahe
d, E.
John
sen,
Unive
rsity
of Mi
chiga
n, An
n Arbo
r, Ann
Arbo
r, MI
Wedn
esda
y, 26
June
201
315
6-GT
-5Gr
ound
Test
Meas
urem
ent T
echn
iques
IISe
abre
eze I
ICh
aired
by: S
. LUM
B, B
oeing
Defe
nse,
Spac
e & S
ecuri
ty an
d R. R
HEW,
NAS
A-Lan
gley R
esea
rch Ce
nter
1330
hrs
AIAA-2
013-3
122
Back
grou
nd P
ressu
re P
rofil
es
for S
onic
Boom
Vehic
le Te
sting
in
the N
ASA
Glen
n 8-
foot
by
6-fo
ot Su
perso
nic W
ind Tu
nnel
R. Ca
stner,
NAS
A Glen
n Res
earch
Ce
nter, C
levela
nd, O
H; S
. Sha
w, E.
Ad
amso
n, Th
e Boe
ing Co
mpan
y, Se
attle,
WA;
S. S
imerl
y, NA
SA G
lenn
Rese
arch C
enter
, Clev
eland
, OH
1400
hrs
AIAA-2
013-3
123
Dyna
mic C
alibr
ation
s for
Fast-
Resp
onse
Por
ous P
olyme
r/Ce
rami
c Pre
ssure
-Sen
sitive
Pa
intJ.
Crafto
n, S.
Pallu
coni,
R. Fo
rlines
, Inn
ovati
ve S
cienti
fic S
olutio
ns, I
nc.,
Dayto
n, OH
; J. G
regory
, Ohio
Stat
e Un
iversi
ty, Co
lumbu
s, OH
1430
hrs
AIAA-2
013-3
124
Phas
e Dela
y and
Corre
lation
Ar
ea D
etecti
on of
Uns
teady
Pr
essu
re Fi
eld U
sing U
nstea
dy
PSP
Meas
urem
ent
K. Na
kakit
a, Ja
pan A
erosp
ace
Explo
ration
Agen
cy (J
AXA)
, Cho
fu,
Japa
n
1500
hrs
AIAA-2
013-3
125
Deve
lopme
nt of
Spra
y-able
Su
perh
ydro
phob
ic Pres
sure-
Sens
itive P
aint f
or U
nstea
dy
Aero
dyna
mic A
pplica
tions
H. Ko
dama
, Tok
yo Un
iversit
y of S
cience
, Ch
iyoda
, Jap
an; K
. Mori
ta, Ja
pan
Aeros
pace
Explo
ration
Agen
cy (JA
XA),
Chofu
, Jap
an; H
. Ishik
awa,
Tokyo
Un
iversit
y of S
cience
, Chiy
oda,
Japan
; H.
Saka
ue, J
apan
Aeros
pace
Explo
ration
Ag
ency
(JAXA
), Ch
ofu, J
apan
1530
hrs
AIAA-2
013-3
126
Resp
onse
Time
Ch
arac
teriza
tion
of P
olyme
r-Ce
rami
c Pre
ssure
-Sen
sitive
Pa
int fo
r Sho
rt Du
ratio
n Te
sting
and U
nstea
dy
Aero
dyna
mic M
easu
reme
nts
T. Ta
ni, H
. Ish
ikawa
, Tok
yo U
nivers
ity
of Sc
ience
, Chiy
oda,
Japa
n; H.
Sa
kaue
, Jap
an Ae
rospa
ce Ex
plorat
ion
Agen
cy (J
AXA)
, Cho
fu, Ja
pan
Wedn
esda
y, 26
June
201
315
7-PD
L-10
Weak
ly Io
nized
Plas
ma P
hysic
sMa
rina 6
Chair
ed by
: D. L
EVIN
, Pen
nsylv
ania
State
Univ
ersity
and C
. SUC
HOME
L, US
AF13
30 hr
sAIA
A-201
3-312
7Su
perso
nic D
rag R
educ
tion
Perfo
rman
ce of
Blun
t-Bod
y wi
th Co
nical
Spike
usin
g with
En
ergy
Dep
ositio
nsA.
Iwak
awa,
N. H
aseg
awa,
T. Os
uka,
R. Ma
jima,
T. Sa
kai, A
. Sas
oh,
Nago
ya U
nivers
ity, N
agoy
a, Ja
pan
1400
hrs
AIAA-2
013-3
128
Radia
l Pro
files
of P
lasma
Ele
ctron
Char
acter
istics
in a
30
kW A
rc Je
tD.
Codro
n, Un
iversi
ties S
pace
Re
searc
h Asso
ciatio
n, Mo
ffett
Field,
CA
; A. N
awaz
, Sier
ra Lo
bo, I
nc.,
Moffe
tt Fie
ld, CA
1430
hrs
AIAA-2
013-3
129
Nume
rical
Simula
tion
of
Ioniz
ed R
ocke
t Plum
esD.
Gue
yffier,
B. F
romen
tin-De
nozie
re,
J. Sim
on, A
. Merl
en, O
NERA
, Pa
laise
au, F
rance
; V. G
iovan
gigli,
École
Polyt
echn
ique,
Palai
seau
, Fra
nce
1500
hrs
AIAA-2
013-3
130
Inve
stiga
tion
of A
rc Pla
sma
Disch
arge
in H
yper
sonic
Flo
w ov
er Co
mpre
ssion
and
Expa
nsion
Corn
erY.
Watan
abe,
K. Su
zuki,
Univ
ersity
of
Toky
o, Ka
shiw
a, Ja
pan
74
Wedn
esda
y, 26
June
201
315
8-PD
L-11/
FD-3
9Ae
ro-O
ptics
Exec
utive
Conf
eren
ce 4
Chair
ed by
: S. G
ORDE
YEV,
Unive
rsity
of No
tre D
ame a
nd M
. REN
NIE
1330
hrs
AIAA-2
013-3
131
The A
ero-
Optic
al En
viron
ment
Ar
ound
a He
licop
ter Co
mput
ed
using
the C
ompr
essib
le Vo
rticit
y Con
finem
ent M
ethod
R. Ke
lly, A.
Jemc
ov, M
. Ren
nie, E
. Ju
mper,
Univ
ersity
of N
otre D
ame,
Notre
Dam
e, IN
1400
hrs
AIAA-2
013-3
132
The I
mpro
veme
nt of
the
Aero
-Opt
ical E
nviro
nmen
t of a
He
misp
here
-on-
Cylin
der T
urre
t us
ing Vo
rtex
Gene
rato
rsN.
De L
ucca
, S. G
ordey
ev, E
. Jum
per,
Unive
rsity
of No
tre D
ame,
Notre
Da
me, I
N
1430
hrs
AIAA-2
013-3
133
The E
ffects
of W
all Co
oling
on
Aer
o-Op
tical
Aber
ratio
ns
Caus
ed by
Subs
onic
Turb
ulent
Bo
unda
ry La
yers
A. Sm
ith, S
. Gord
eyev
, Univ
ersity
of
Notre
Dam
e, No
tre D
ame,
IN
1500
hrs
AIAA-2
013-3
134
Comp
utat
ional
inves
tigat
ion
of th
e infl
uenc
e of u
nstea
dy
shoc
k mo
tion
on ab
erra
ting
struc
ture
s in
supe
rsonic
bo
unda
ry la
yers
M. W
hite,
Ohio
Aeros
pace
Insti
tute,
Dayto
n, OH
; M. V
isbal,
Air F
orce
Rese
arch L
abora
tory,
Wrig
ht-Pa
tterso
n AFB
, OH
1530
hrs
AIAA-2
013-3
135
Study
of U
nstea
dy Su
rface
Pr
essu
re on
a Tu
rret v
ia Pr
essu
re-S
ensit
ive P
aint
K. Hir
d, T.
Julia
no, J
. Greg
ory, O
hio
State
Univ
ersity
, Colu
mbus
, OH;
S.
Gorde
yev,
N. D
e Luc
ca, E
. Jum
per,
Unive
rsity
of No
tre D
ame,
Notre
Da
me, I
N; J.
Thord
ahl, D
. Witti
ch, A
ir Fo
rce Re
searc
h Lab
orator
y, Kir
tland
AF
B, N
M
1600
hrs
AIAA-2
013-3
136
The E
stima
tion
of th
e Uns
teady
Ae
rody
nami
c For
ce A
pplie
d to
a Tur
ret i
n Fli
ght
N. D
e Luc
ca, S
. Gord
eyev
, E. J
umpe
r, Un
iversi
ty of
Notre
Dam
e, No
tre
Dame
, IN;
K. H
ird, T
. Juli
ano,
J. Gr
egory
, Ohio
Stat
e Univ
ersity
, Co
lumbu
s, OH
; J. T
horda
hl,
D. W
ittich
, Air F
orce R
esea
rch
Labo
ratory
, Kirtl
and A
FB, N
M
1630
hrs
AIAA-2
013-3
137
The C
ompa
rison
of U
nstea
dy
Press
ure F
ield o
ver F
lat- a
nd
Confo
rmal-
Wind
ow Tu
rrets
using
Pr
essur
e Sen
sitive
Paint
S. Go
rdeye
v, N.
De Lu
cca, E
. Jum
per,
Unive
rsity o
f Notr
e Dam
e, No
tre Da
me,
IN; K.
Hird,
T. Ju
liano,
J. Gre
gory,
Ohio
Sta
te Un
iversit
y, Co
lumbu
s, OH
; J.
Thord
ahl, D
. Witti
ch, Ai
r Forc
e Rese
arch
Labo
ratory
, Kirtl
and A
FB, N
M
Wedn
esda
y, 26
June
201
315
9-TP
-16
Ther
moph
ysica
l Pro
perti
es an
d Sur
face
Cata
lysis
Exec
utive
Conf
eren
ce 3
ACh
aired
by: J
. BAT
SON,
Lock
heed
Mart
in Sp
ace S
ystem
s and
I. H
SU, L
ockh
eed M
artin
Spac
e Sys
tems
1330
hrs
AIAA-2
013-3
138
Surfa
ce Ca
talys
is an
d Ox
idatio
n on
Stag
natio
n Po
int
Heat
Flux
Mea
sure
ment
s in
High
Enth
alpy A
rc Je
tsA.
Nawa
z, Sie
rra Lo
bo, I
nc.,
Moffe
tt Fie
ld, CA
; D. D
river,
I. Te
rraza
s-Sa
linas
, NAS
A Ame
s Res
earch
Cente
r, Mo
ffett
Field,
CA; S
. Sep
ka, E
RC,
Inc.,
Moffe
tt Fie
ld, CA
1400
hrs
AIAA-2
013-3
139
Surfa
ce Ca
talyz
ed R
eacti
on
Effic
iencie
s in
Nitro
gen
and O
xyge
n Pla
smas
from
La
ser I
nduc
ed Fl
uore
scenc
e Me
asur
emen
tsJ.
Meye
rs, W
. Owe
ns, D
. Flet
cher,
Un
iversi
ty of
Verm
ont,
Burlin
gton,
Burlin
gton,
VT
1430
hrs
AIAA-2
013-3
140
Surfa
ce Ca
talyz
ed R
eacti
on
Effic
iencie
s in
Air P
lasma
s Us
ing La
ser I
nduc
ed
Fluor
esce
nce M
easu
reme
nts
J. Me
yers,
W. O
wens
, D. F
letch
er,
Unive
rsity
of Ve
rmon
t, Bu
rlingto
n, Bu
rlingto
n, VT
1500
hrs
AIAA-2
013-3
141
Surfa
ce Ca
talyz
ed
Reco
mbina
tion
Effic
iencie
s for
Fle
xible
Ther
mal P
rotec
tion
Mater
ials i
n Ai
r Plas
maW.
Owe
ns, J
. Mey
ers, D
. Flet
cher,
Un
iversi
ty of
Verm
ont,
Burlin
gton,
Burlin
gton,
VT
1530
hrs
AIAA-2
013-3
142
Multi-
Grou
p Red
uctio
ns of
LTE
Air P
lasma
Rad
iative
Tran
sfer
in Cy
lindr
ical G
eome
tries
J. Sc
oggin
s, T.
Magin
, von
Kárm
án
Institu
te for
Fluid
Dyn
amics
, Rho
de-
Saint
-Genè
se, B
elgium
; A. W
ray,
N. M
anso
ur, N
ASA A
mes R
esea
rch
Cente
r, Moff
ett Fi
eld, C
A
1600
hrs
AIAA-2
013-3
143
Benc
hmar
king a
nove
l tech
nique
for
estim
ating
princ
ipal th
ermal
cond
uctiv
ities o
f ana
nisotr
opic
comp
osite
med
iumB.
Chak
ravart
hy, S.
Venk
atesha
n, S.
Chan
da, In
dian I
nstitu
te of
Techn
ology
Ma
dras,
Chen
nai, I
ndia;
A. Am
biraja
n, Ind
ian Sp
ace Re
search
Orga
nisati
on,
Bang
alore,
India
Wedn
esda
y, 26
June
201
316
0-TP
-17
None
qulib
rium
Flows
Exec
utive
Conf
eren
ce 2
BCh
aired
by: W
. WOO
D, La
ngley
Rese
arch C
enter
1330
hrs
AIAA-2
013-3
144
Cont
inuum
Simu
lation
of
Hype
rsonic
Flow
s usin
g the
Qu
antu
m-Ki
netic
Chem
ical
Reac
tion
Mode
lR.
Wagn
ild, M
. Gall
is, S
andia
Na
tiona
l Lab
orator
ies, A
lbuqu
erque
, NM
1400
hrs
AIAA-2
013-3
145
Cons
isten
t Mod
eling
of
Rota
tiona
l Non
equil
ibrium
in
a Hyb
rid P
artic
le-Co
ntinu
um
Meth
odA.
Verho
ff, I.
Boy
d, Un
iversi
ty of
Mich
igan,
Ann A
rbor, A
nn Ar
bor, M
I
1430
hrs
AIAA-2
013-3
146
Micro
scopic
Simu
lation
and
Macro
scopic
Mod
eling
for
Therm
al an
d Che
mica
l Non
-Eq
uilibr
ium G
ases
Y. Liu
, NAS
A Ame
s Rese
arch C
enter
, Mo
ffett F
ield, C
A; M.
Pane
si, Un
iversit
y of
Illinois
, Urba
na-Ch
ampa
ign, U
rbana
, IL;
M. V
inoku
r, NAS
A Ame
s Rese
arch
Cente
r, Moff
ett Fi
eld, C
A; P. C
larke
, Un
iversit
y of T
exas,
Austin
, Aust
in, TX
1500
hrs
AIAA-2
013-3
147
Energ
y tra
nsfer
stud
y of N
2-N2
int
eracti
ons b
y usin
g rov
ibrati
onal
state-
to-sta
te mo
del
M. Pa
nesi,
Unive
rsity o
f Illino
is, Urb
ana-
Cham
paign
, Urba
na, IL
; R. J
affe,
D.
Schw
enke
, NAS
A Ame
s Rese
arch C
enter
, Mo
ffett F
ield, C
A; T.
Magin
, von
Kárm
án
Institu
te for
Fluid
Dyna
mics,
Rhod
e-Sain
t-Ge
nèse,
Belgiu
m
1530
hrs
AIAA-2
013-3
148
Gene
raliz
ed P
olyno
mial
Chao
s Sa
mplin
g of Q
uasi-
Classi
cal
Trajec
torie
s for
Non
equil
ibrium
Re
actin
g Flow
Simu
lation
sM.
Kulak
hmeto
v, A.
Alexe
enko
, Pu
rdue U
nivers
ity, W
est L
afaye
tte, I
N
1600
hrs
AIAA-2
013-3
149
Coup
led H
ydro
dyna
mic/
State-
Spec
ific H
igh-Te
mper
atur
e Mo
delin
g of N
itrog
en
Vibra
tiona
l Exc
itatio
n an
d Di
ssocia
tion
B. Lo
pez,
M. Li
no D
a Silv
a, V.
Guerr
a, J.
Loure
iro, T
echn
ical U
nivers
ity of
Lis
bon,
Lisbo
n, Po
rtuga
l
1630
hrs
AIAA-2
013-3
150
Mode
ling o
f Stro
ng
None
quilib
rium
in Ni
troge
n Sh
ock
Wave
sJ.
Kim, I
. Boy
d, Un
iversi
ty of
Mich
igan,
Ann A
rbor, A
nn Ar
bor, M
I
75
Thur
sday
Thur
sday
, 27
June
201
316
1-NB
-4
0700
- 08
00 h
rsTh
ursd
ay M
ornin
g Netw
orkin
g Bre
akfa
stNa
utilu
s and
Har
bor
Islan
d Foy
ers
Thur
sday
, 27
June
201
316
2-SB
-7
0730
- 08
00 h
rsTh
ursd
ay M
ornin
g Spe
aker
s’ Br
iefing
Sessi
on R
ooms
Thur
sday
, 27
June
201
316
3-LE
C-4
0800
- 09
00 h
rsAe
rody
nami
cs Aw
ard L
ectu
reHa
rbor
Ball
room
I an
d II
Neal
T. Fr
inkNA
SA La
ngley
Rese
arch C
enter
Thur
sday
, 27
June
201
316
4-AP
A-34
Unste
ady A
erod
ynam
ics II
IMa
rina 3
Chair
ed by
: J. F
ARNS
WOR
TH, U
S Air
Force
Acad
emy a
nd M
. YU,
Iowa
Stat
e Univ
ersity
0900
hrs
AIAA-2
013-3
151
Accu
rate
Comp
utat
ion of
Flow
be
low th
e Rot
or D
isk by
a Fin
ite-S
tate
Meth
odZ.
Fei, D
. Pete
rs, W
ashin
gton
Unive
rsity
in St
. Lou
is, S
t. Lo
uis, M
O
0930
hrs
AIAA-2
013-3
152
Expe
rimen
tal Ae
roela
stic A
nalys
is of
Cluste
red Tu
rbine
Blad
es
Vibra
ting i
n Mixe
d Tor
sion/
Bend
ing M
ode
A. Za
nker,
P. Ot
t, Swi
ss Fe
deral
Instit
ute
of Tec
hnolo
gy, La
usann
e, Sw
itzerl
and;
P. Ca
lza, A
vio S.
p.A., R
ivalta
di To
rino,
Italy
1000
hrs
AIAA-2
013-3
153
On th
e Con
tribu
tion
of
Indiv
idual
Land
ing G
ear
Comp
onen
ts to
Land
ing G
ear
Load
s and
Nois
eO.
Stal
nov,
D. An
gland
, X. Z
hang
, Un
iversi
ty of
South
ampto
n, So
utham
pton,
Unite
d King
dom
Thur
sday
, 27
June
201
316
5-AP
A-35
Appli
ed CF
D III
Seab
reez
e II
Chair
ed by
: N. H
ARIH
ARAN
, CRE
ATE-A
V an
d K. A
BDOL
-HAMI
D, N
ASA L
angle
y Res
earch
Cente
r09
00 hr
sAIA
A-201
3-315
4Pe
rform
ance
of R
eyno
lds
Aver
aged
Nav
ier-S
toke
s Mo
dels
in Pr
edict
ing Se
para
ted
Flows
: Stu
dy of
the H
ump F
low
Mode
l Pro
blem
D. Ca
ppell
i, Éco
le Na
tiona
le Su
périe
ure de
l’Aéro
nauti
que e
t de
l’Esp
ace,
Toulo
use,
Franc
e; N.
Ma
nsou
r, NAS
A Ame
s Res
earch
Ce
nter, M
offett
Field
, CA
0930
hrs
AIAA-2
013-3
155
Valid
ation
of th
e Flow
Topo
logy
Arou
nd Se
vera
l Aird
rop C
argo
Co
nfigu
ratio
ns at
Stati
c Con
dition
sS.
Geisb
auer,
N. B
ier, Ge
rman
Ae
rospa
ce Ce
nter (
DLR)
, Brau
nschw
eig,
Germ
any;
J. Kir
z, Tec
hnica
l Univ
ersity
of
Braun
schwe
ig, Br
aunsc
hweig
, Germ
any;
E. Ro
osenb
oom,
Germ
an Ae
rospa
ce
Cente
r (DL
R), G
ötting
en, G
erman
y
1000
hrs
AIAA-2
013-3
156
Aero
dyna
mic A
nalys
is and
Fligh
t Sim
ulatio
n of a
n Ane
mome
ter
for Ro
tation
al Sta
biliza
tion o
f a
Helico
pter S
lung L
oad
M. Po
tsdam
, U.S.
Army
, Moff
ett Fi
eld,
CA; L
. Cico
lani, S
an Jo
se Sta
te Un
iversit
y Fo
unda
tion,
Moffe
tt Field
, CA;
B. Ga
ssawa
y, U.S
. Arm
y, Re
dston
e Arse
nal,
AL; D
. Matt
le, Dy
netics
, Inc.,
Redst
one
Arsen
al, AL
76
Thur
sday
, 27
June
201
316
6-AP
A-36
Prop
eller
/Rot
orcra
ft/Wi
nd Tu
rbine
Aer
odyn
amics
III
Seab
reez
e ICh
aired
by: E
. ROO
SENB
OOM,
DLR
- Germ
an Ae
rospa
ce Ce
nter
0900
hrs
AIAA-2
013-3
157
Fuse
lage m
odeli
zatio
n fo
r mu
lti-fid
elity
coup
led CF
D/CS
D sim
ulatio
n of
roto
rcraf
ts in
BVI
cond
ition
M. Am
iraux
, S. T
homa
s, J.
Baed
er,
Unive
rsity
of Ma
rylan
d, Co
llege
Park,
Co
llege
Park,
MD
0930
hrs
AIAA-2
013-3
158
Coup
led CF
D/CS
D An
alysis
of
Roto
r Blad
e Stru
ctura
l Loa
ds
with
Expe
rimen
tal V
alida
tion
S. M
asse
y, NA
SA La
ngley
Rese
arch
Cente
r, Ham
pton,
VA; A
. Kres
hock
, Arm
y Res
earch
Labo
ratory
, Ham
pton,
VA; M
. Sek
ula, N
ASA L
angle
y Re
searc
h Cen
ter, H
ampto
n, VA
1000
hrs
AIAA-2
013-3
159
An Ex
perim
enta
l Stu
dy of
Mi
crobu
rst-W
ind In
duce
d Loa
ds
on a
Wind
Turb
ine M
odel
Y. Zh
ang,
P. Sa
rkar, H
. Hu,
Iowa
State
Univ
ersity
, Ame
s, IA
1030
hrs
AIAA-2
013-3
160
Comp
ariso
n of
Comp
uted
and
Meas
ured
Vorte
x Ev
olutio
n fo
r a U
H-60
A Ro
tor i
n Fo
rwar
d Fli
ght
J. Ah
mad,
G. Ya
mauc
hi, D
. Kao
, NA
SA Am
es Re
searc
h Cen
ter, M
offett
Fie
ld, CA
1100
hrs
AIAA-2
013-3
161
Mome
ntum
Theo
ry w
ith
Slips
tream
Rot
ation
App
lied t
o Wi
nd Tu
rbine
sD.
Hun
sake
r, W. P
hillip
s, Ut
ah S
tate
Unive
rsity,
Loga
n, UT
Thur
sday
, 27
June
201
316
7-AP
A-37
/FD-
40Ac
tive a
nd P
assiv
e Flow
Cont
rol I
IIMa
rina 4
Chair
ed by
: M. P
OST,
USAF
Acad
emy a
nd G
. JON
ES, N
ASA-L
angle
y Res
earch
Cente
r09
00 hr
sAIA
A-201
3-316
2Co
ntro
l of T
hree
-dim
ensio
nal
Flow
Insta
bilitie
s at t
he Si
de-
wall J
uncti
on of
an A
irfoil
Ca
scade
S. B
enton
, C. B
ernard
ini, J
. Bon
s, Oh
io St
ate U
nivers
ity, C
olumb
us, O
H
0930
hrs
AIAA-2
013-3
163
Expe
rimen
tal St
udy o
n Uns
teady
Ae
rody
nami
c Loa
ds of
a Sy
ntheti
c Je
t at A
irfoil
Trail
ing Ed
geC.
Gao,
W. Zh
ang,
North
weste
rn Po
lytech
nical
Unive
rsity,
Xi’an
, Chin
a; L.
Xiaob
o, Sh
angh
ai Ac
adem
y of
Space
flight
Techn
ology,
Shan
ghai,
China
; Z.
Jian,
North
weste
rn Po
lytech
nical
Unive
rsity,
Xi’an
, Chin
a
1000
hrs
AIAA-2
013-3
164
Expe
rimen
tal S
tudy
on A
irfoil
Cir
culat
ion Co
ntro
l usin
g Pla
sma A
ctuat
ors
M. Ko
tsonis
, R. P
ul, L.
Veldh
uis, D
elft
Unive
rsity
of Te
chno
logy,
Delft,
The
Nethe
rland
s
1030
hrs
AIAA-2
013-3
165
Role
of Sy
nthe
tic Je
t Fre
quen
cy
& Or
ienta
tion
in Dy
nami
c Sta
ll Vo
rticit
y Cre
ation
J. Ye
n, N.
Ahme
d, Un
iversi
ty of
New
South
Wale
s, Sy
dney
, Aus
tralia
1100
hrs
AIAA-2
013-3
166
The F
low O
ver a
Bac
kwar
d Fa
cing S
tep Su
bjecte
d to
Multip
le Sy
nthe
tic Je
t Actu
ator
sA.
Sasso
on, U
nivers
ity of
Mary
land,
Colle
ge Pa
rk, Co
llege
Park,
MD;
J.
Hubb
ard, N
ation
al Ins
titute
of Ae
rospa
ce, H
ampto
n, VA
; A. F
latau
, Z.
Hasn
ain, U
nivers
ity of
Mary
land,
Colle
ge Pa
rk, Co
llege
Park,
MD
Thur
sday
, 27
June
201
316
8-AP
A-38
Vorti
cal/V
ortex
Flow
Marin
a 6Ch
aired
by: H
. BAB
INSK
Y, Un
iversi
ty of
Camb
ridge
and W
. FRIT
Z, Ca
ssidia
n09
00 hr
sAIA
A-201
3-318
6Ch
arac
teriza
tion
of a
helic
al vo
rtex,
gene
rated
behin
d a r
otat
ing bl
ade,
using
the
Actu
ator
Line
Meth
odM.
ali, N
ation
al Ce
nter f
or Sc
ientifi
c Re
searc
h (CN
RS),
Marse
ille, F
rance
; M.
Abid,
Aix-M
arseil
le Un
iversi
ty,
Marse
ille, F
rance
0930
hrs
AIAA-2
013-3
187
Lead
ing-Ed
ge G
eome
try
Effe
cts on
the V
ortex
Syste
m Fo
rmat
ion of
a Di
amon
d Wing
Co
nfigu
ratio
nA.
Höve
lman
n, C.
Breit
samt
er,
Tech
nical
Unive
rsity
of Mu
nich,
Garch
ing, G
erman
y
1000
hrs
AIAA-2
013-3
188
A Ne
w Ap
proa
ch fo
r Mod
eling
th
e Uns
teady
Beh
avior
of
Trailin
g Line
Axia
l Vor
tices
M. Ab
uhara
z, R.
Ash,
Old D
omini
on
Unive
rsity,
Norf
olk, V
A
1030
hrs
AIAA-2
013-3
189
Vorte
x Fo
rmat
ion in
Confi
ned
Recta
ngula
r-Cav
ity Fl
ows
J. Fe
rnand
o, J.
Krieg
seis,
D. R
ival,
Unive
rsity
of Ca
lgary,
Calga
ry,
Cana
da
1100
hrs
AIAA-2
013-3
190
Comp
utat
ional
and
Expe
rimen
tal S
tudie
s in
Multip
air W
ake V
ortex
In
stabil
ities
T. Qu
acke
nbus
h, A.
Bilan
in, A.
Bo
schits
ch, C
ontin
uum
Dyna
mics,
Inc
., Ew
ing, N
J
77
Thur
sday
, 27
June
201
316
9-AP
A-39
/FD-
46Lo
w Sp
eed,
Low
Reyn
olds N
umbe
r Aer
odyn
amics
III
Exec
utive
Conf
eren
ce 4
Chair
ed by
: K. G
RANL
UND,
Air F
orce R
esea
ch La
borat
ory an
d J. M
URRA
Y, Sa
ndia
Natio
nal L
abora
tories
0900
hrs
AIAA-2
013-3
191
Aero
dyna
mic M
odeli
ng of
Sm
all U
AV fo
r Per
ching
Ex
perim
ents
C. Me
ckstr
oth, U
nivers
ity of
Day
ton
Rese
arch I
nstitu
te, D
ayton
, OH;
G.
Reich
, Air F
orce R
esea
rch La
borat
ory,
Wrig
ht-Pa
tterso
n AFB
, OH
0930
hrs
AIAA-2
013-3
192
Aero
dyna
mic d
ampin
g de
rivat
ives o
f low
aspe
ct ra
tio
wing
s at l
ow R
eyno
lds n
umbe
rsM.
Shie
lds, K
. Moh
seni,
Univ
ersity
of
Florid
a, Ga
inesv
ille, F
L
1000
hrs
AIAA-2
013-3
193
Prop
eller
Slips
tream
Effe
cts
on W
ings a
t Low
Rey
nolds
Nu
mber
sG.
Anan
da Kr
ishna
n, R.
Deter
s, M.
Se
lig, U
nivers
ity of
Illino
is, U
rbana
-Ch
ampa
ign, U
rbana
, IL
1030
hrs
AIAA-2
013-3
194
Theo
retica
l Ana
lysis o
f Perc
hing
and H
overi
ng M
aneu
vers
K. Ra
mesh,
A. Go
palar
athna
m, J.
Ed
wards
, Nort
h Caro
lina St
ate Un
iversit
y, Ra
leigh,
NC; K
. Gran
lund,
M. O
l, Air
Force
Resea
rch La
borat
ory, W
right-
Patte
rson A
FB, O
H
1100
hrs
AIAA-2
013-3
195
Expe
rimen
tal I
nves
tigat
ion of
No
n-Bo
dy of
Rev
olutio
n Mo
del
durin
g Com
bined
Roll
-Yaw
C. Ja
gade
esh,
M. B
altha
zar, A
. Gros
s, H.
Fase
l, Univ
ersity
of Ar
izona
, Tu
cson,
Tucso
n, AZ
Thur
sday
, 27
June
201
317
0-FD
-41/
GT-6
Expe
rimen
tal M
ethod
sNa
utilu
s 3Ch
aired
by: K
. LOW
E, Vir
ginia
Tech
and J
. KEG
ELMA
N, N
ASA
0900
hrs
AIAA-2
013-3
167
Expe
rimen
tal a
nd N
umer
ical
Inve
stiga
tions
on D
rag i
nduc
ed
by Fl
at P
late I
mper
fecti
ons i
n Co
mpre
ssible
Flow
Reg
imes
P. Mo
lton,
D. H
ue, R
. Bur,
ONE
RA,
Meud
on, F
rance
0930
hrs
AIAA-2
013-3
168
Char
acter
izatio
n of
fluo
resce
nt
polys
tyre
ne m
icros
pher
es fo
r ad
vanc
ed fl
ow di
agno
stics
P. Ma
isto,
K. Lo
we, V
irgini
a Po
lytec
hnic
Institu
te an
d Stat
e Un
iversi
ty, B
lacks
burg,
VA; P
. Dan
ehy,
P. Tie
msin,
C. W
ohl, N
ASA L
angle
y Re
searc
h Cen
ter, H
ampto
n, VA
; G.
Byu
n, R.
Simps
on, A
UR, I
nc.,
Black
sburg
, VA
1000
hrs
AIAA-2
013-3
169
Comp
ensa
tion
Meth
od fo
r the
Es
timat
ion of
the A
utos
pectr
al De
nsity
Func
tion
of th
e Un
even
ly Sp
aced
HIFi
RE-1
Fli
ght D
ata
S. S
tanfie
ld, S
pectr
al En
ergies
, Da
yton,
OH; R
. Kim
mel, A
ir Forc
e Re
searc
h Lab
orator
y, W
right-
Patte
rson A
FB, O
H
1030
hrs
AIAA-2
013-3
170
Therm
odyn
amic C
hara
cteriz
ation
of
Supe
rsonic
Expa
nsion
s Usin
g Sh
adow
grap
hy an
d Num
erica
l Sim
ulatio
nsJ.
Loren
zi, N
ation
al Ato
mic E
nergy
Co
mmiss
ion, B
ueno
s Aire
s, Arg
entin
a; C.
Rinald
i, Nati
onal
Auton
omou
s Univ
ersity
of
Mexic
o, Me
xico C
ity, M
exico
; C.
Toro S
alaza
r, Nati
onal
Atomi
c Ene
rgy
Comm
ission
, Bue
nos A
ires,
Argen
tina;
M.
Villag
ran M
uñiz,
Nati
onal
Scien
tific a
nd
Techn
ical R
esearc
h Cou
ncil (C
ONICE
T),
Buen
os Air
es, Ar
genti
na; S
. Ortiz
, Na
tiona
l Atom
ic Ene
rgy Co
mmiss
ion,
Buen
os Air
es, Ar
genti
na
Thur
sday
, 27
June
201
317
1-FD
-42
Cavit
y Flow
s:Phy
sics a
nd Co
ntro
lSp
inake
r ICh
aired
by: U
. KAU
L, NA
SA-Am
es09
00 hr
sAIA
A-201
3-317
1Flo
w In
terac
tion
Analy
sis N
ear
the U
pstre
am Ca
vity E
dge
unde
r Tur
bulen
t Inc
ident
Flow
M. G
arcia
Sainz
, Scie
ntific
Rese
arch
Comm
ittee o
f Bue
nos A
ires,
La Pl
ata,
Argen
tina;
J. De
lnero,
J. M
araño
n Di
Leo,
Natio
nal S
cienti
fic an
d Tec
hnica
l Re
searc
h Cou
ncil (
CONI
CET)
, Bue
nos
Aires
, Arge
ntina
; J. C
olman
, S.
Algoz
ino, N
ation
al Un
iversi
ty of
La
Plata,
La Pl
ata, A
rgenti
na
0930
hrs
AIAA-2
013-3
172
Expe
rimen
tal I
nves
tigat
ion of
Flu
id-Str
uctu
re In
terac
tions
in
Comp
ressi
ble Ca
vity F
lows
J. Wa
gner,
S. B
eresh
, K. C
aspe
r, J.
Henfl
ing, R
. Spil
lers,
P. Hu
nter, R
. Ma
yes,
Sand
ia Na
tiona
l Lab
orator
ies,
Albuq
uerqu
e, NM
1000
hrs
AIAA-2
013-3
173
An Ex
perim
enta
l Inv
estig
ation
of
Supe
rsonic
Cavit
y Flow
Co
ntro
l with
Verti
cal C
ylind
ers
G. M
ilne,
C. Th
ieman
, A. V
akili,
Un
iversi
ty of
Tenn
esse
e, Tu
llaho
ma,
Tulla
homa
, TN
1030
hrs
AIAA-2
013-3
174
Sens
itivity
analy
sis an
d pas
sive
cont
rol o
f a co
mpre
ssible
tu
rbule
nt fl
ow in
a de
ep ca
vity
M. Cl
emen
t, D.
Sipp
, ONE
RA,
Meud
on, F
rance
78
Thur
sday
, 27
June
201
317
2-FD
-43
Wing
Aer
odyn
amics
Spina
ker I
ICh
aired
by: N
. AHM
ED, T
he U
nivers
ity of
New
Sou
th Wa
les an
d S. A
NDER
S09
00 hr
sAIA
A-201
3-317
5Sim
ulatio
n of W
ing St
allR.
Rade
spiel,
D. Fr
ancoi
s, D.
Hopp
mann
, S.
Klein,
P. Sc
holz,
Techn
ical U
nivers
ity of
Bra
unsch
weig,
Brau
nschw
eig, G
erman
y; K.
Wawr
zinek
, T. L
utz, U
nivers
ity
of Stu
ttgart
, Stut
tgart,
Germ
any;
T. Au
erswa
ld, J.
Bang
e, Un
iversit
y of
Tübing
en, T
übing
en, G
erman
y; C.
Knigg
e, Lei
bniz
Unive
rsity o
f Han
nove
r, Ha
nnov
er, Ge
rman
y; P. K
ellene
rs, R.
He
inrich
, Germ
an Ae
rospa
ce Ce
nter
(DLR
), Bra
unsch
weig,
Germ
any;
S. Re
uss, A
. Prob
st, T.
Knop
p, Ge
rman
Ae
rospa
ce Ce
nter (
DLR)
, Gött
ingen
, Ge
rman
y
0930
hrs
AIAA-2
013-3
176
Non-
plana
rity t
o imp
rove
su
bson
ic pe
rform
ance
of de
lta
wing
at lo
w an
gles o
f atta
ckN.
Ahme
d, Y.
Zhen
g, Un
iversi
ty of
New
South
Wale
s, Sy
dney
, Aus
tralia
1000
hrs
AIAA-2
013-3
177
Shap
e, lif
t, an
d vibr
ation
s of
highly
comp
liant
mem
bran
e wi
ngs
R. Wa
ldman
, K. B
reuer,
Brow
n Un
iversi
ty, Pr
ovide
nce,
RI
1030
hrs
AIAA-2
013-3
178
Low
Aspe
ct Ra
tio O
scilla
ting
Flexib
le Wi
ngs a
t Low
Rey
nolds
Nu
mber
sD.
Clea
ver, D
. Cald
eron,
Z. Wa
ng,
I. Gu
rsul, U
nivers
ity of
Bath
, Bath
, Un
ited K
ingdo
m
1100
hrs
AIAA-2
013-3
179
High
-Fide
lity Si
mulat
ions o
f a
Flexib
le He
aving
Finit
e-As
pect-
Ratio
Wing
C. Ba
rnes,
M. V
isbal,
R. G
ordnie
r, Air
Force
Rese
arch L
abora
tory,
Wrig
ht-Pa
tterso
n AFB
, OH
1130
hrs
AIAA-2
013-3
180
Effe
ct of
Wing
Plan
form
on
Aero
dyna
mic C
hara
cteris
tics a
t Lo
w Re
ynold
s Num
bers
using
a Lo
w De
nsity
Wind
Tunn
elM.
Anyo
ji, T.
Liu, T
. Non
omura
, A.
Oyam
a, K.
Fujii,
Japa
n Aero
spac
e Ex
plorat
ion Ag
ency
(JAX
A),
Saga
miha
ra, Ja
pan
Thur
sday
, 27
June
201
317
3-FD
-44
0900
- 11
00 h
rsTra
nsitio
n Op
en Fo
rum
Naut
ilus 1
Thur
sday
, 27
June
201
317
4-FD
-45
Turb
ulent
Flow
s II
Naut
ilus 2
Chair
ed by
: M. L
UHAR
, Cali
fornia
Insti
tute o
f Tec
hnolo
gy an
d R. A
GARW
AL, W
ashin
gton U
nivers
ity in
St L
ouis
0900
hrs
AIAA-2
013-3
181
Thre
e-Eq
uatio
n K-ε-V
n Tu
rbule
nce M
odel
for H
igh-
Spee
d Flow
sA.
Molch
anov
, Mos
cow
Aviat
ion
Institu
te, M
osco
w, Ru
ssia
0930
hrs
AIAA-2
013-3
182
Appli
catio
n of
a Ne
w On
e-Eq
uatio
n Tu
rbule
nce M
odel
to
Comp
utat
ions o
f Sep
arat
ed
Flows
T. W
ray, R
. Aga
rwal,
Was
hingto
n Un
iversi
ty in
St. L
ouis,
St.
Louis
, MO
1000
hrs
AIAA-2
013-3
183
Larg
e-Ed
dy Si
mulat
ion of
Pa
rticle
s and
Bub
bles C
ollisi
ons
in Ho
moge
neou
s Iso
tropic
Tu
rbule
nce
H. Fa
yed,
S. Ra
gab,
Virgin
ia Po
lytec
hnic
Institu
te an
d Stat
e Un
iversi
ty, B
lacks
burg,
VA
1030
hrs
AIAA-2
013-3
184
Impli
cit La
rge-
Eddy
Simu
lation
of
Isot
ropic
Turb
ulent
Mixi
ngF.
Grins
tein,
A. Wa
chtor
, Los
Alam
os
Natio
nal L
abora
tory,
Los A
lamos
, NM
; C. D
eVore
, Nav
al Re
searc
h La
borat
ory, W
ashin
gton,
DC
1100
hrs
AIAA-2
013-3
185
LES o
f a hi
gh-R
eyno
lds nu
mber,
ch
emica
lly re
actin
g mixi
ng la
yer
P. Ferr
ero, A
. Kart
ha, P.
Subb
aredd
y, G.
Cand
ler, Un
iversit
y of M
inneso
ta,
Minn
eapo
lis, M
innea
polis,
MN;
P.
Dimota
kis, C
aliforn
ia Ins
titute
of Tec
hnolo
gy, Pa
saden
a, CA
Thur
sday
, 27
June
201
317
5-FD
-48
Shoc
ksNa
utilu
s 4Ch
aired
by: J
. BOL
ES09
00 hr
sAIA
A-201
3-320
1Un
stead
y Sho
ck M
otion
in a
Trans
onic
Flow
over
a Wa
ll-Mo
unted
Hem
isphe
reS.
Bere
sh, J
. Hen
fling,
R. Sp
illers,
B.
Pruett
, San
dia N
ation
al La
borat
ories
, Alb
uque
rque,
NM
0930
hrs
AIAA-2
013-3
202
Study
of sh
ock-
shoc
k int
erac
tions
for t
he H
ET fa
cility
do
uble
wedg
e con
figur
ation
us
ing th
e DSM
C app
roac
hV.
Patil,
D. L
evin,
Penn
sylva
nia S
tate
Unive
rsity,
Univ
ersity
Park,
PA; S
. Gim
elshe
in, U
nivers
ity of
Sou
thern
Califo
rnia,
Los A
ngele
s, CA
; J.
Austi
n, Un
iversi
ty of
Illino
is, U
rbana
-Ch
ampa
ign, U
rbana
, IL
1000
hrs
AIAA-2
013-3
203
Spec
tral C
hara
cteris
tics o
f Se
para
tion
Shoc
k Un
stead
iness
J. Po
ggie,
N. B
isek,
R. Kim
mel, A
ir Fo
rce Re
searc
h Lab
orator
y, W
right-
Patte
rson A
FB, O
H; S
. Stan
field,
Sp
ectra
l Ene
rgies
, Day
ton, O
H
1030
hrs
AIAA-2
013-3
204
Simula
tions
of a
Norm
al Sh
ock
Train
in a C
onsta
nt A
rea D
uct
Using
Wall
-Mod
eled L
ESZ.
Vane
, S. L
ele, S
tanfor
d Univ
ersity
, St
anfor
d, CA
1100
hrs
AIAA-2
013-3
205
Nume
rical
Simula
tion
of
Trans
onic
Buffe
t on
Swep
t Wi
ng of
Supe
rcritic
al Ai
rfoils
J. Xio
ng, F
. Liu,
Univ
ersity
of
Califo
rnia,
Irvine
, Irvi
ne, C
A
1130
hrs
AIAA-2
013-3
206
Fund
amen
tal S
tudy
on
Nume
rical
Meth
ods o
f Glob
al In
stabil
ity A
nalys
is fo
r Co
mpre
ssible
Flow
s with
Shoc
k wa
veY.
Ohmi
chi, K
. Suz
uki, U
nivers
ity of
To
kyo,
Kash
iwa,
Japa
n
79
Thur
sday
, 27
June
201
317
6-FD
-49
Mode
ling a
nd Si
mulat
ion of
Fluid
sMa
rina 2
Chair
ed by
: W. L
OUISO
S, U
nivers
ity of
Verm
ont a
nd S
. SPE
ER, N
orthro
p Grum
man C
orpora
tion
0900
hrs
AIAA-2
013-3
207
Nume
rical
Simula
tion
of
Hydr
odyn
amics
of an
Ann
ular
Hybr
id In
jecto
rS.
Chatt
erjee
, S. M
ahap
atra,
A. Mu
khop
adhy
ay, S
. Sen
, Jad
avpu
r Un
iversi
ty, Ko
lkata,
India
0930
hrs
AIAA-2
013-3
208
Towa
rds f
ull-sc
ale n
umer
ical
simula
tions
of a
trave
ling-
wave
ther
moac
ousti
c Stir
ling
heat
engin
eC.
Scalo
, J. L
in, S
. Lele
, L. H
esse
link,
Stan
ford U
nivers
ity, S
tanfor
d, CA
1000
hrs
AIAA-2
013-3
209
Rang
e-de
pend
ent p
ropa
gatio
n mo
delin
g of i
nfra
soun
d in
comp
lex at
mosp
here
sG.
Derg
ham,
C. M
illet,
M. B
ertin,
Ato
mic E
nergy
and A
lterna
tive
Energ
ies Co
mmiss
ion, A
rpajon
, Fra
nce
1030
hrs
AIAA-2
013-3
210
Desig
n of
free
-surfa
ce
inter
face
s usin
g RAN
S eq
uatio
nsF.
Palac
ios, J
. Alon
so, A
. Jam
eson
, St
anfor
d Univ
ersity
, Stan
ford,
CA
1100
hrs
AIAA-2
013-3
211
Effe
ct of
Mac
h nu
mber
on
linea
r sta
bility
of lid
-driv
en
cavit
y flow
sL.
Berga
mo, E
. Gen
naro,
M.
Mede
iros,
Unive
rsity
of Sã
o Pau
lo,
São C
arlos
, Braz
il
1130
hrs
AIAA-2
013-3
212
Two D
imen
siona
l Num
erica
l Stu
dy of
the F
low ov
er a
Bridg
e Dec
k wi
th th
e Ope
n So
urce
CFD
Tool
Open
FOAM
G. Ca
mpite
lli, W
est V
irgini
a Un
iversi
ty, M
organ
town,
WV;
V. Kra
stev,
Unive
rsity
of Ro
me, R
ome,
Italy;
W. H
uebs
ch, M
. Gau
tam, W
est
Virgin
ia Un
iversi
ty, M
organ
town,
WV
80
Auth
or/S
essio
n Ch
air In
dex
Abdo
l-Ham
id, K.
, 34-A
PA-10
, 165
-APA-3
5Ab
dolla
hi, V.
, 143
-ASE-9
Abdu
lraha
man,
M., 1
8-FD-2
Abe,
T., 1
31-PD
L-8Ab
e, Y.,
40-C
FD-10
, 75-F
D-20
Abgra
ll, R.,
39-C
FD-9,
44-C
FD-14
Abid,
M.,
168-A
PA-38
Abne
y, A.,
73-F
D-18
Abuh
araz,
M., 1
68-AP
A-38
Adam
, P.,
141-A
PA-32
Adam
czuk
, R.,
24-GT
-1Ad
amov
ich, I
., 46
-FD-11
Adam
s, N.
, 32-A
PA-8,
120
-CFD-3
2, 1
39-AP
A-30
Adam
son,
E., 1
56-GT
-5Ad
den,
S., 3
1-APA
-7/FD
-8Ad
dy, H
., 11
7-ASE
-8Ad
irim, H
., 13
8-APA
-29Ag
arwal,
R., 1
12-AP
A-24,
115
-APA-2
7/FD
-26,
174
-FD-45
Agela
stos,
A., 1
14-AP
A-26
Agha
babia
n, B.
, 152
-FD-35
Agoc
s, J.,
34-A
PA-10
, 141
-APA-3
2Ag
ostin
elli, C
., 8-A
PA-5
Agraw
al, P.
, 107
-TP-11
Ahma
d, J.,
166
-APA-3
6Ah
mad,
N., 9
-ASE-1
, 37-A
SE-3
Ahme
d, A.,
89-A
PA-22
/FD-2
2, 1
28-FD
-31Ah
med,
N., 3
1-APA
-7/FD
-8, 1
28-FD
-31, 1
54-FD
-37,
167
-APA-3
7/FD
-40, 1
72-FD
-43Ah
n, J.,
58-A
PA-13
Ahn,
S., 3
2-APA
-8Aig
ner, M
., 12
-CFD-3
Ailor,
W.,
134-T
P-13
Akda
g, V.,
44-C
FD-14
Akhta
r, K.,
151-F
D-34
Alauz
et, F.
, 68-C
FD-19
Alexe
enko
, A.,
27-TP
-2, 8
0-TP-8
, 106
-TP-10
, 1
52-FD
-35, 1
60-TP
-17Alg
ozino
, S.,
171-F
D-42
ali, M
., 16
8-APA
-38Ali
, M.,
154-F
D-37
Aliza
rd, F.
, 47-F
D-12
Alkan
dry, H
., 51
-TP-3,
87-A
PA-20
Allan
, B.,
85-AP
A-18/
FD-21
, 141
-APA-3
2All
en, C
., 8-A
PA-5,
61-A
PA-16
, 67-C
FD-18
, 84-A
PA-17
Allma
ras, S
., 10
0-CFD
-29/F
D-23
Alons
o, J.,
15-C
FD-6,
42-C
FD-12
, 57-A
PA-12
, 7
6-PDL
-4, 1
00-CF
D-29/
FD-23
, 176
-FD-49
Alter,
S.,
38-CF
D-8Alt
man,
A., 1
42-AP
A-33/
FD-33
Alvi, F
., 21
-FD-5,
154
-FD-37
Ambir
ajan,
A., 1
59-TP
-16
Amira
ux, M
., 16
6-APA
-36Am
itay,
M., 8
5-APA
-18/F
D-21
Amsa
llem,
D.,
15-CF
D-6, 4
3-CFD
-13, 9
6-CFD
-25An
anda
Krish
nan,
G., 1
69-AP
A-39/
FD-46
Ande
rs, S
., 85-A
PA-18
/FD-2
1, 14
1-APA
-32, 1
72-FD
-43An
derso
n, W.
, 40-C
FD-10
Andre
ws, M
., 23
-FD-7
Andri
enko
, D.,
43-CF
D-13
Ange
l Blas
co, E
., 11
3-APA
-25An
gland
, D.,
34-AP
A-10,
164
-APA-3
4An
gulo,
J., 9
7-CFD
-26An
sell,
P., 5
8-APA
-13, 6
1-APA
-16, 1
14-AP
A-26
Anyo
ji, M.
, 172
-FD-43
Aono
, H.,
33-AP
A-9/F
D-9, 7
5-FD-2
0Ari
sman
, C.,
152-F
D-35
Armstr
ong,
C., 9
6-CFD
-25Arn
al, D
., 88
-APA-2
1Arn
old, D
., 25
-PDL-1
Arnold
us, Q
., 36
-ASE-2
Arora,
N.,
33-AP
A-9/F
D-9, 1
54-FD
-37Ars
lan, A
., 57
-APA-1
2, 1
12-AP
A-24
Aruna
jates
an, S
., 14
-CFD-5
, 151
-FD-34
Asad
a, K.,
75-F
D-20
Ash,
R., 1
68-AP
A-38
Ashp
is, D
., 74
-FD-19
/PDL
-3, 1
03-PD
L-6As
hwort
h, R.,
153
-FD-36
Ateso
glu, M
., 14
1-APA
-32Ati
nault
, O.,
5-APA
-2Atk
ins, H
., 10
-CFD-1
, 127
-FD-30
Auers
wald,
T., 1
72-FD
-43Au
man,
L., 1
41-AP
A-32
Austi
n, J.,
175
-FD-48
Avela
r, A.,
9-ASE
-1Ay
yasw
amy,
V., 8
0-TP-8
, 106
-TP-10
Azev
edo,
J., 6
-APA-3
, 84-A
PA-17
, 113
-APA-2
5,
138
-APA-2
9Az
iz, M
., 18
-FD-2
Babin
sky,
H., 1
68-AP
A-38
Bach
chan
, N.,
44-CF
D-14
Badc
ock,
K., 9
7-CFD
-26Ba
eder,
J., 1
0-CFD
-1, 3
5-APA
-11, 9
7-CFD
-26,
147
-CFD-3
9, 1
66-AP
A-36
Balak
umar,
P., 7
0-CFD
-21/F
D-15,
153
-FD-36
Balan
, A.,
118-C
FD-30
Balth
azar,
M.,
31-AP
A-7/F
D-8, 1
69-AP
A-39/
FD-46
Bang
e, J.,
172
-FD-43
Barad
, M.,
15-CF
D-6, 3
4-APA
-10Ba
rata,
J., 4
4-CFD
-14Ba
rdy, D
., 32
-APA-8
Barne
s, C.,
172
-FD-43
Barte
ls, R.
, 140
-APA-3
1Ba
rtram
, S.,
49-GT
-2
Baruz
zi, G
., 14
3-ASE
-9Ba
s, O.
, 33-A
PA-9/
FD-9
Batso
n, J.,
159
-TP-16
Baum
, J.,
97-CF
D-26
Baum
an, P
., 38
-CFD-8
Beck
er, L.
, 49-G
T-2Be
ckers
, S.,
151-F
D-34
Behre
ndt,
F., 1
03-PD
L-6Be
lovich
, V.,
150-C
FD-42
Belte
r, D.,
49-GT
-2Be
ncic,
T., 3
6-ASE
-2, 6
2-ASE
-4Be
nek,
J., 1
1-CFD
-2Be
ngtso
n, R.,
132
-PDL-9
Benn
ani, L
., 11
7-ASE
-8Be
nsas
si, K.
, 22-F
D-6, 4
3-CFD
-13, 6
5-CFD
-16/G
T-3Be
nton,
S., 1
67-AP
A-37/
FD-40
Beres
h, S.
, 73-F
D-18,
171
-FD-42
, 175
-FD-48
Berg,
J., 1
22-CF
D-34
Berga
mo, L
., 17
6-FD-4
9Be
rnal, L
., 12
9-FD-3
2Be
rnardi
ni, C.
, 167
-APA-3
7/FD
-40Be
rridge
, D.,
73-FD
-18Be
rtin, M
., 17
6-FD-4
9Be
uth, J
., 45
-FD-10
Bewl
ey, T
., 67
-CFD-1
8, 1
50-CF
D-42
Beyh
aghi,
P., 6
7-CFD
-18, 1
50-CF
D-42
Bidan
, G.,
124-F
D-27
Bidwe
ll, C.,
36-A
SE-2,
71-F
D-16
Bier, N
., 11
6-APA
-28, 1
65-AP
A-35
Bieste
r, M.,
121-C
FD-33
Bijl, H
., 20
-FD-4
Bilan
in, A.
, 168
-APA-3
8Bil
odea
u, D.
, 143
-ASE-9
Bilye
u, D.
, 59-A
PA-14
, 145
-CFD-3
7Bin
Azry
Seet,
A., 8
9-APA
-22/F
D-22
Bisek
, N.,
175-F
D-48
Bisso
n, F.,
112
-APA-2
4Bo
busch
, B.,
67-CF
D-18,
148
-CFD-4
0Bo
ckho
rn, H
., 18
-FD-2
Boda
rt, J.
, 70-C
FD-21
/FD-1
5Bo
dony
, D.,
48-FD
-47, 1
00-CF
D-29/
FD-23
Boele
ns, O
., 14
7-CFD
-39Bo
les, J
., 94
-CFD-2
3, 1
75-FD
-48Bo
nfigli
oli, A
., 13
2-PDL
-9Bo
ns, J
., 23
-FD-7,
167
-APA-3
7/FD
-40Bo
om, P
., 30
-APA-6
, 93-C
FD-22
Boop
athy,
K., 1
23-CF
D-35
Borg,
M.,
73-FD
-18, 1
27-FD
-30Bo
rggaa
rd, J.
, 149
-CFD-4
1Bo
rner, A
., 50
-PDL-2
, 80-T
P-8Bo
schits
ch, A
., 16
8-APA
-38Bo
se, D
., 79
-TP-7
Bossc
haert
s, W.
, 129
-FD-32
Bosw
ell, R
., 50
-PDL-2
Bosw
orth,
R., 5
0-PDL
-2Bo
uche
r, M.,
85-AP
A-18/
FD-21
Boure
mel, Y
., 5-A
PA-2
Bous
quet,
A., 3
9-CFD
-9Bo
werso
x, R.,
46-F
D-11,
126
-FD-29
Boyd
, I.,
38-CF
D-8, 4
6-FD-1
1, 5
1-TP-3
, 53-T
P-5,
63-A
SE-5,
79-T
P-7, 8
7-APA
-20, 1
60-TP
-17Br
ackb
ill, J.
, 50-P
DL-2
Brag
g, M.
, 58-A
PA-13
, 61-A
PA-16
, 91-A
SE-6
Bram
esfel
d, G.
, 84-A
PA-17
Bran
dis, A
., 27
-TP-2,
79-T
P-7Br
aun,
R., 7
9-TP-7
Braz
ell, M
., 14
4-CFD
-36Br
eden
, D.,
77-PD
L-5Br
ehm,
C., 1
5-CFD
-6, 3
4-APA
-10, 7
3-FD-1
8Br
eitsa
mter,
C., 1
39-AP
A-30,
168
-APA-3
8Br
ekke
, K.,
90-AP
A-23,
138
-APA-2
9Br
engu
ier, J
., 62
-ASE-4
Bren
ner, P
., 13
-CFD-4
Bretl
, T.,
87-AP
A-20
Breu
er, K.
, 172
-FD-43
Brev
iglier
i, C.,
113-A
PA-25
Brez
illon,
J., 1
13-AP
A-25,
139
-APA-3
0Br
ight,
M., 7
5-FD-2
0Br
oders
en, O
., 30
-APA-6
Broe
ren, A
., 91
-ASE-6
, 117
-ASE-8
Broo
ks, T
., 49
-GT-2
Brow
n, D.
, 119
-CFD-3
1Br
uce,
W., 4
9-GT-2
Buch
ner, A
., 89
-APA-2
2/FD
-22Bu
diman
, A.,
33-AP
A-9/F
D-9Bu
i, T.,
139-A
PA-30
Buitra
go, W
., 35
-APA-1
1Bu
r, R.,
72-FD
-17, 1
70-FD
-41/G
T-6Bu
rgess,
N.,
13-CF
D-4Bu
rnside
, N.,
88-AP
A-21
Burt,
J., 6
3-ASE
-5, 8
0-TP-8
Byun
, G.,
170-F
D-41/
GT-6
Byun
, J.,
70-CF
D-21/
FD-15
Cain,
A., 2
4-GT-1
Cakm
akcio
glu, S
., 33
-APA-9
/FD-9
Calde
ron, D
., 12
9-FD-3
2, 1
72-FD
-43Ca
lvert,
N.,
77-PD
L-5Ca
lza, P
., 16
4-APA
-34Ca
mbier
, J.,
50-PD
L-2Ca
mpite
lli, G
., 17
6-FD-4
9Ca
mpos
, A.,
70-CF
D-21/
FD-15
Cand
ler, G
., 14-C
FD-5,
38-CF
D-8, 4
6-FD-1
1, 17
4-FD-4
5Ca
nnat,
F., 5
0-PDL
-2Ca
o, D.
, 26-T
P-1
Capiz
zano
, F.,
69-CF
D-20
Capo
ne, F
., 85
-APA-1
8/FD
-21, 1
41-AP
A-32
Capp
elli, D
., 16
5-APA
-35Ca
raeni,
D.,
123-C
FD-35
Carm
o, B.
, 128
-FD-31
Carna
rius,
A., 4
2-CFD
-12Ca
rneiro
Bras
ileiro
, F.,
9-ASE
-1Ca
rpente
r, M., 7
0-CFD
-21/F
D-15,
100-C
FD-29
/FD-2
3Ca
rrier, G
., 5-A
PA-2,
57-A
PA-12
, 113
-APA-2
5Ca
rson,
C., 1
6-CFD
-7Ca
rter, C
., 22
-FD-6,
94-C
FD-23
Carte
r, M.,
85-AP
A-18/
FD-21
, 141
-APA-3
2Ca
rvalho
, V.,
26-TP
-1Ca
sper,
K., 2
1-FD-5
, 73-F
D-18,
171
-FD-42
Casp
er, M
., 31
-APA-7
/FD-8
Casse
l, K.,
19-FD
-3Ca
stano
San
chez
, A.,
113-A
PA-25
Casti
llo, L
., 15
5-FD-3
8Ca
stner,
R., 6
5-CFD
-16/G
T-3, 1
56-GT
-5Ca
talan
o, P.,
33-A
PA-9/
FD-9,
75-F
D-20
Catta
festa,
L., 1
24-FD
-27Ca
vagli
eri, D
., 67
-CFD-1
8, 1
50-CF
D-42
Cetin
er, O
., 20
-FD-4
Ceze
, M.,
64-CF
D-15
Chac
on, B
., 66
-CFD-1
7Ch
akrav
arthy
, B.,
159-T
P-16
Chan
, D.,
85-AP
A-18/
FD-21
, 141
-APA-3
2Ch
an, W
., 14
6-CFD
-38Ch
anda
, S.,
159-T
P-16
Chan
dar, D
., 97
-CFD-2
6Ch
aney
, C.,
141-A
PA-32
Chan
g, C.,
59-AP
A-14,
70-CF
D-21/
FD-15
, 145
-CFD-3
7Ch
ang,
L., 7
7-PDL
-5Ch
ang,
S., 1
45-CF
D-37
Chap
lin, R
., 11
3-APA
-25Ch
arest,
M.,
40-CF
D-10
Charl
es, C
., 50
-PDL-2
Chate
lain,
P., 1
6-CFD
-7Ch
atterj
ee, S
., 17
6-FD-4
9Ch
auras
ia, H
., 98
-CFD-2
7Ch
azot,
O.,
65-CF
D-16/
GT-3,
78-T
P-6Ch
en, P
., 96
-CFD-2
5Ch
en, W
., 88
-APA-2
1Ch
en, X
., 11
2-APA
-24Ch
en, Y
., 51
-TP-3
Chen
, Z.,
74-FD
-19/P
DL-3,
151
-FD-34
Chen
g, B.
, 89-A
PA-22
/FD-2
2Ch
eng,
G., 5
9-APA
-14, 1
45-CF
D-37
Chen
g, K.,
140
-APA-3
1Ch
enna
kesh
ava,
J., 4
9-GT-2
Chigu
llapa
lli, S
., 10
6-TP-1
0Ch
itale,
K., 1
4-CFD
-5
81
Auth
or/S
essio
n Ch
air In
dex
Chng
, T.,
77-PD
L-5Ch
oi, B
., 11
5-APA
-27/F
D-26
Choi,
S.,
32-AP
A-8Ch
oudh
ari, M
., 47
-FD-12
, 70-C
FD-21
/FD-1
5,
95-C
FD-24
, 127
-FD-30
Chou
dhary
, A.,
14-CF
D-5Ch
ow, R
., 86
-APA-1
9Ch
ristop
her, P
., 34
-APA-1
0Cic
olani,
L., 1
65-AP
A-35
Cinne
lla, P
., 10
-CFD-1
, 13-C
FD-4
Cioba
ca, V
., 85
-APA-1
8/FD
-21Cla
rk, C.
, 117
-ASE-8
Clark,
J., 7
1-FD-1
6Cla
rke, P
., 16
0-TP-1
7Cla
ude,
J., 3
2-APA
-8Cle
aver,
D.,
129-F
D-32,
172
-FD-43
Cleme
ns, N
., 45
-FD-10
Cleme
nt, J.
, 123
-CFD-3
5Cle
ment,
M.,
72-FD
-17, 1
71-FD
-42Co
ates,
T., 9
5-CFD
-24Co
der, J
., 5-A
PA-2
Codo
ni, J.
, 87-A
PA-20
Codro
n, D.
, 157
-PDL-1
0Co
llins,
E., 3
6-ASE
-2Co
lman
, J.,
171-F
D-42
Colon
ius, T
., 17
-FD-1,
115
-APA-2
7/FD
-26Co
lonna
, G.,
132-P
DL-9
Colon
no, M
., 57
-APA-1
2Co
mbes
, T.,
84-AP
A-17
Cong
edo,
P., 4
4-CFD
-14Co
ntent,
C., 1
0-CFD
-1, 1
3-CFD
-4Co
ok, G
., 65
-CFD-1
6/GT
-3, 1
45-CF
D-37
Cori,
J., 4
8-FD-4
7Co
rral, R
., 41
-CFD-1
1, 9
9-CFD
-28Co
rrigan
, A.,
97-CF
D-26
Cozm
uta, I
., 13
4-TP-1
3Cra
fton,
J., 4
8-FD-4
7, 1
56-GT
-5Cra
wford
, B.,
7-APA
-4, 1
16-AP
A-28
Crude
n, B.
, 27-T
P-2, 7
9-TP-7
Cumm
ings,
R., 4
-APA-1
, 34-A
PA-10
, 38-C
FD-8,
1
52-FD
-35Cu
rrie, T
., 62
-ASE-4
Cyby
k, B.
, 4-AP
A-1Cy
mbali
st, N
., 12
6-FD-2
9D’
Ango
la, A.
, 132
-PDL-9
Dala,
L., 9
0-APA
-23Da
ndois
, J.,
115-A
PA-27
/FD-2
6Da
nehy
, P.,
170-F
D-41/
GT-6
Danfo
rth, C
., 52
-TP-4
Danfo
rth, R
., 24
-GT-1
Dann
enho
ffer, J
., 14
6-CFD
-38, 1
50-CF
D-42
Dants
ker, O
., 87
-APA-2
0
Darm
ofal, D
., 4-AP
A-1, 1
4-CFD
-5, 10
0-CFD
-29/F
D-23,
1
48-CF
D-40
Dasq
ue, N
., 98
-CFD-2
7Da
vidso
n, L.,
95-C
FD-24
Davis
, R.,
16-CF
D-7, 7
1-FD-1
6, 1
46-CF
D-38
Davis
, S.,
12-CF
D-3Da
wson
, R.,
74-FD
-19/P
DL-3
De Lu
cca, N
., 15
8-PDL
-11/F
D-39
De Pa
uw, D
., 23
-FD-7
De S
tefan
o Fum
o, M.
, 59-A
PA-14
Debia
si, M
., 5-A
PA-2
DeBo
nis, J
., 35-A
PA-11
, 70-C
FD-21
/FD-1
5, 14
0-APA
-31De
cham
ps, X
., 76
-PDL-4
Deck
, S.,
140-A
PA-31
Deck
er, R.
, 72-F
D-17
Deco
ninck
, H.,
39-CF
D-9, 6
5-CFD
-16/G
T-3De
desh
, V.,
37-AS
E-3De
gani,
D.,
43-CF
D-13
Degre
z, G.
, 76-P
DL-4
DeJo
ng, A
., 16
-CFD-7
Del R
ey Fe
rnánd
ez, D
., 40
-CFD-1
0De
lnero,
J., 1
71-FD
-42De
Loac
h, R.,
24-G
T-1, 1
30-GT
-4De
ng, X
., 89
-APA-2
2/FD
-22De
nisse
n, N.
, 23-F
D-7De
nniso
n, J.,
92-A
SE-7
Deola
likar,
S.,
43-CF
D-13
Dergh
am, G
., 17
6-FD-4
9De
rlaga
, J.,
15-CF
D-6, 9
9-CFD
-28, 1
49-CF
D-41
Desid
eri, J
., 57
-APA-1
2De
sJardi
n, P.,
53-T
P-5De
Spirit
o, J.,
90-A
PA-23
, 140
-APA-3
1De
ters,
R., 1
69-AP
A-39/
FD-46
DeVo
re, C.
, 174
-FD-45
Dewa
n, Y.,
151
-FD-34
Dezit
ter, F
., 62
-ASE-4
Dhan
asar,
M.,
98-CF
D-27
Dianic
s, J.,
31-A
PA-7/
FD-8
Diebo
ld, J.
, 91-A
SE-6,
114
-APA-2
6Dik
alyuk
, A.,
27-TP
-2Dim
otakis
, P.,
126-F
D-29,
174
-FD-45
Dinc,
M., 1
25-FD
-28Din
g, E.,
35-A
PA-11
Ding,
K., 1
18-CF
D-30
Diosa
dy, L
., 10
0-CFD
-29/F
D-23
Diskin
, B.,
13-CF
D-4Dji
djeli,
K., 9
9-CFD
-28Do
gariu
, A.,
77-PD
L-5Do
latab
adi, A
., 16
-CFD-7
, 23-F
D-7Do
n, W.
, 12-C
FD-3
Donb
ar, J.
, 94-C
FD-23
Done
lli, R.
, 75-F
D-20
Dong
, H.,
48-FD
-47Do
ng, M
., 19
-FD-3
Donz
is, D
., 22
-FD-6
Dord,
A., 1
26-FD
-29Do
rgan,
A., 9
5-CFD
-24, 1
47-CF
D-39
Doty,
M.,
49-GT
-2Do
ughe
rty, N
., 51
-TP-3
Drak
es, J
., 10
3-PDL
-6Dr
ela, M
., 4-A
PA-1,
13-C
FD-4,
119
-CFD-3
1Dr
iver, D
., 77
-PDL-5
, 159
-TP-16
Drole
n, B.
, 26-T
P-1Dr
ozda
, T.,
152-F
D-35
Duan
, L.,
47-FD
-12, 7
0-CFD
-21/F
D-15,
95-C
FD-24
Duan
, Z.,
153-F
D-36
Duart
e San
tos, P
., 10
5-TP-9
Dudle
y, J.,
47-F
D-12,
72-F
D-17,
90-A
PA-23
Dufre
ne, A
., 94
-CFD-2
3Du
mitra
che,
C., 5
0-PDL
-2Du
ncan
, G.,
7-APA
-4Du
raisa
my, K
., 15
-CFD-6
, 70-C
FD-21
/FD-1
5,
147
-CFD-3
9Du
rsche
r, R.,
25-PD
L-1Du
vigne
au, R
., 96
-CFD-2
5Du
wig,
C., 1
21-CF
D-33,
147
-CFD-3
9Eb
ersoh
n, F.,
76-P
DL-4
Ebi, D
., 45
-FD-10
Econ
omon
, T.,
42-CF
D-12,
57-A
PA-12
Edqu
ist, K
., 79
-TP-7,
87-A
PA-20
Edwa
rds, J
., 18-F
D-2, 1
55-FD
-38, 1
69-AP
A-39/
FD-46
Ehrm
ann,
R., 8
6-APA
-19Ek
aterin
aris,
J., 1
5-CFD
-6Ek
en, A
., 48
-FD-47
Ekici,
K., 1
21-CF
D-33
El Ha
ssan,
M., 1
51-FD
-34El-
Saye
d, Y.,
88-A
PA-21
Elban
na, H
., 18
-FD-2
Eldred
ge, J
., 17
-FD-1,
129
-FD-32
Elhad
idi, B
., 8-A
PA-5,
86-A
PA-19
Elias
, P.,
50-PD
L-2Eli
asso
n, P.,
122
-CFD-3
4Elm
iligui,
A., 1
51-FD
-34Elq
atary,
I., 8
-APA-5
, 86-A
PA-19
Ely, R
., 75
-FD-20
Emre,
., 4
2-CFD
-12En
gfer, C
., 95
-CFD-2
4Erf
ani, R
., 10
-CFD-1
, 32-A
PA-8,
103
-PDL-6
Erfan
i, T.,
32-AP
A-8, 1
03-PD
L-6Eri
ksso
n, S.
, 122
-CFD-3
4Erw
in, J.
, 40-C
FD-10
Esco
bar, J
., 35
-APA-1
1Es
kov,
N., 1
48-CF
D-40
Esse
r, B.,
107-T
P-11
Estiv
aleze
s, J.,
44-C
FD-14
Estru
ch-Sa
mper,
D.,
72-FD
-17Eti
enne
, S.,
48-FD
-47, 1
49-CF
D-41
Everh
art, J
., 24
-GT-1
Evsti
gnee
v, A.,
37-A
SE-3
Eyi, S
., 65
-CFD-1
6/GT
-3, 6
6-CFD
-17, 9
6-CFD
-25Ey
mann
, T.,
118-C
FD-30
Faga
n, A.,
62-A
SE-4
Fagle
y, C.,
115
-APA-2
7/FD
-26Fa
irlie,
T., 9
-ASE-1
Falem
pin, F
., 15
4-FD-3
7Fa
rhat,
C., 13
-CFD-4
, 15-C
FD-6,
43-CF
D-13,
96-CF
D-25
Faria
, A.,
9-ASE
-1Fa
rnell,
C., 6
3-ASE
-5Fa
rnswo
rth, J
., 72
-FD-17
, 84-A
PA-17
, 1
15-AP
A-27/
FD-26
, 164
-APA-3
4Fa
sel, H
., 18-F
D-2, 3
1-APA
-7/FD
-8, 47
-FD-12
, 73-F
D-18,
7
5-FD-2
0, 1
27-FD
-30, 1
69-AP
A-39/
FD-46
Faso
ulas,
S., 5
2-TP-4
, 135
-TP-14
Fast,
T., 7
8-TP-6
Faye
d, H.
, 174
-FD-45
Fede
rov, A
., 10
2-FD-2
5Fe
dorov
, A.,
102-F
D-25
Fei, Z
., 16
4-APA
-34Fe
ldhus
en, A
., 13
8-APA
-29Fe
ng, L
., 74
-FD-19
/PDL
-3Fe
rguso
n, D.
, 92-A
SE-7
Fergu
son,
F., 9
8-CFD
-27Fe
rguso
n, S.
, 88-A
PA-21
, 112
-APA-2
4Fe
rnand
o, J.,
168
-APA-3
8Fe
rraro,
G.,
8-APA
-5Fe
rrero,
P., 1
74-FD
-45Fe
uchtw
ang,
J., 8
6-APA
-19Fid
kows
ki, K.
, 64-C
FD-15
, 96-C
FD-25
, 118
-CFD-3
0Fin
danis
, N.,
128-F
D-31
Fings
kes,
C., 3
0-APA
-6Fir
sov,
A., 7
7-PDL
-5, 1
54-FD
-37Fis
ch, G
., 9-A
SE-1
Fishe
r, T.,
100-C
FD-29
/FD-2
3Fla
tau, A
., 21
-FD-5,
167
-APA-3
7/FD
-40Fle
tcher,
D.,
159-T
P-16
Fletch
er, J.
, 25-P
DL-1
Florez
Mera
, J.,
26-TP
-1Fo
ng, E
., 52
-TP-4
Fong
, K.,
127-F
D-30
Forlin
es, R
., 15
6-GT-5
Fossa
ti, M.
, 143
-ASE-9
Franc
ois, D
., 17
2-FD-4
3Fra
nka,
I., 7
7-PDL
-5Fra
yssin
et, O
., 32
-APA-8
Frena
nder,
H.,
122-C
FD-34
Frink
, N.,
35-AP
A-11,
114
-APA-2
6
Frisb
ey, M
., 14
4-CFD
-36Fri
ss, A.
, 77-P
DL-5
Fritz,
W.,
141-A
PA-32
, 168
-APA-3
8Fro
ehle,
B.,
64-CF
D-15
Frome
ntin-D
enoz
iere,
B., 1
57-PD
L-10
Fu, S
., 19
-FD-3,
153
-FD-36
Fuch
s, L.,
71-F
D-16,
147
-CFD-3
9Fu
chs,
U., 5
2-TP-4
Fujii,
K., 4
0-CFD
-10, 7
5-FD-2
0, 10
5-TP-9
, 152
-FD-35
, 1
72-FD
-43Fu
jino,
T., 1
04-PD
L-7, 1
31-PD
L-8Fu
jita, K
., 27
-TP-2,
63-A
SE-5,
105
-TP-9,
126
-FD-29
, 1
35-TP
-14Fu
jiwara
, G.,
91-AS
E-6Fu
kaga
ta, K.
, 16-C
FD-7,
67-C
FD-18
Fulek
i, D.,
62-AS
E-4, 1
17-AS
E-8Fu
lge, H
., 13
5-TP-1
4Ga
ffuri,
M., 1
13-AP
A-25,
139
-APA-3
0Ga
gnon
, H.,
96-CF
D-25
Gagu
la, S
., 49
-GT-2
Gaito
nde,
D., 4
6-FD-1
1, 7
2-FD-1
7, 9
5-CFD
-24Ga
lbrait
h, M.
, 11-C
FD-2
Galla
rd, F.
, 42-C
FD-12
Gallis
, M.,
160-T
P-17
Galup
po, W
., 15
2-FD-3
5Ga
napa
thisu
brama
ni, B
., 72
-FD-17
Gana
puram
, V.,
49-GT
-2Ga
o, C.,
74-F
D-19/
PDL-3
, 138
-APA-2
9,
167
-APA-3
7/FD
-40Ga
o, H.
, 115
-APA-2
7/FD
-26Ga
rbeff,
T., 8
8-APA
-21Ga
rcía M
agari
ño, A
., 14
3-ASE
-9Ga
rcia S
ainz,
M., 1
71-FD
-42Ga
rdner,
A., 1
40-AP
A-31
Garie
py, M
., 30
-APA-6
Garm
ann,
D., 1
42-AP
A-33/
FD-33
Garni
er, E.
, 115
-APA-2
7/FD
-26Ga
ron, A
., 48
-FD-47
, 148
-CFD-4
0, 1
49-CF
D-41
Garre
tt, S
., 10
1-FD-2
4Ga
rzon,
A., 1
53-FD
-36Ga
ssawa
y, B.
, 165
-APA-3
5Ga
tlin, G
., 85
-APA-1
8/FD
-21, 1
16-AP
A-28
Gaud
litz, D
., 41
-CFD-1
1Ga
uger,
N.,
42-CF
D-12
Gauta
m, M
., 17
6-FD-4
9Ge
erts,
J., 1
52-FD
-35Ge
isbau
er, S
., 16
5-APA
-35Ge
isler, R
., 34
-APA-1
0Ge
ndel,
S.,
43-CF
D-13
Geng
, X.,
140-A
PA-31
Genn
aro, E
., 47
-FD-12
, 176
-FD-49
Georg
e, P.,
154
-FD-37
82
Auth
or/S
essio
n Ch
air In
dex
Georg
iadis,
N.,
70-CF
D-21/
FD-15
Gerol
ymos
, G.,
10-CF
D-1Ge
ubell
e, P.,
48-F
D-47
Ghas
emi K
., A.,
67-C
FD-18
Ghore
yshi,
M.,
34-AP
A-10
Gildfi
nd, D
., 27
-TP-2
Gimels
hein,
N.,
50-PD
L-2Gim
elshe
in, S
., 50
-PDL-2
, 175
-FD-48
Giova
ngigl
i, V.,
157-P
DL-10
Girald
o, A.,
35-A
PA-11
Gisbe
rt, F.
, 41-C
FD-11
, 99-C
FD-28
Gisse
n, A.,
154
-FD-37
Glaab
, L.,
107-T
P-11
Glaus
er, M
., 15
0-CFD
-42Gle
zer, A
., 31
-APA-7
/FD-8
, 154
-FD-37
Gmeli
n, C.,
75-F
D-20
Gnoff
o, P.,
38-C
FD-8
Goek
ce, S
., 10
3-PDL
-6Go
ekse
l, B.,
103-P
DL-6
Goha
ri, S.
, 67-C
FD-18
Goha
ri Dara
bkha
ni, H
., 10
-CFD-1
, 45-F
D-10
Gokc
en, T
., 51
-TP-3
Goldf
eld, M
., 15
4-FD-3
7Go
lubev
, V.,
16-CF
D-7, 4
7-FD-1
2, 1
51-FD
-34Go
mez C
arras
co, F
., 12
8-FD-3
1Go
oden
, J.,
147-C
FD-39
Good
liff, S
., 85
-APA-1
8/FD
-21, 1
41-AP
A-32
Gopa
lan, H
., 12
0-CFD
-32Go
palar
athna
m, A.
, 114
-APA-2
6, 1
69-AP
A-39/
FD-46
Gorde
yev,
S., 4
8-FD-4
7, 1
58-PD
L-11/
FD-39
Gordn
ier, R
., 17
2-FD-4
3Go
rdon,
S., 2
5-PDL
-1Go
stelow
, J.,
101-F
D-24
Gottli
eb, O
., 43
-CFD-1
3Go
vinda
rajan
, R.,
89-AP
A-22/
FD-22
Govin
darja
n, R.,
19-F
D-3Gr
andin
, A.,
62-AS
E-4Gr
anlun
d, K.,
129
-FD-32
, 169
-APA-3
9/FD
-46Gr
ay, D
., 12
5-FD-2
8Gr
een,
M., 2
0-FD-4
Gree
n, N.
, 63-A
SE-5
Gree
nwoo
d, R.,
73-F
D-18
Greg
ory, J
., 21
-FD-5,
156
-GT-5,
158
-PDL-1
1/FD
-39Gr
egory
, S.,
92-AS
E-7Gr
eig, A
., 50
-PDL-2
Gren
on, R
., 5-A
PA-2
Griffi
n, J.,
124
-FD-27
Grign
on, C
., 43
-CFD-1
3Gr
igorev
, M.,
37-AS
E-3Gr
instei
n, F.,
174
-FD-45
Grop
p, W.
, 100
-CFD-2
9/FD
-23Gr
oss,
A., 1
8-FD-2
, 31-A
PA-7/
FD-8,
75-F
D-20,
169
-APA-3
9/FD
-46Gr
ossir
, G.,
22-FD
-6Gr
oth, C
., 12
-CFD-3
, 14-C
FD-5,
40-C
FD-10
Grub
e, N.
, 72-F
D-17
Guelh
an, A
., 10
7-TP-1
1Gu
endo
gdu,
Y., 1
21-CF
D-33
Guerr
a, V.,
160
-TP-17
Guey
ffier, D
., 15
7-PDL
-10Gu
glielm
o, J.,
5-AP
A-2, 5
7-APA
-12Gu
iho, F
., 47
-FD-12
Guilm
ineau
, E.,
96-CF
D-25
Gupta
, A.,
33-AP
A-9/F
D-9, 1
35-TP
-14Gu
rrola,
F., 4
3-CFD
-13Gu
rsul, I
., 12
9-FD-3
2, 1
72-FD
-43Gu
stavs
son,
J., 2
1-FD-5
Guze
l, G.,
141-A
PA-32
Haas
, A.,
47-FD
-12Ha
bash
i, W.,
16-CF
D-7, 1
17-AS
E-8, 1
43-AS
E-9Ha
bisreu
ther, P
., 18
-FD-2
Hack
ett, M
., 84
-APA-1
7Ha
der, C
., 73
-FD-18
Hafez
, M.,
4-APA
-1, 3
9-CFD
-9, 4
5-FD-1
0, 6
6-CFD
-17Ha
ga, T
., 14
4-CFD
-36Ha
genm
aier, M
., 22
-FD-6,
94-C
FD-23
Hahn
, D.,
101-F
D-24
Haim
es, R
., 14
6-CFD
-38, 1
48-CF
D-40
Halco
mb, N
., 88
-APA-2
1Ha
ll, J.,
84-A
PA-17
Hallid
ay, N
., 12
3-CFD
-35Ha
meed
, H.,
146-C
FD-38
Hann
eman
n, K.,
38-C
FD-8,
105
-TP-9
Hans
on, R
., 77
-PDL-5
Hao,
L., 7
4-FD-1
9/PD
L-3Ha
rada,
N., 1
31-PD
L-8Ha
ri, S.
, 135
-TP-14
Harih
aran,
N., 3
2-APA
-8, 1
65-AP
A-35
Harris
, R.,
90-AP
A-23,
99-C
FD-28
Hartm
ann,
A., 1
38-AP
A-29
Hartm
ann,
U., 2
4-GT-1
Hasa
nzad
eh La
shka
jani, K
., 61
-APA-1
6Ha
sega
wa, N
., 15
7-PDL
-10Ha
skin,
H.,
49-GT
-2Ha
snain
, Z.,
21-FD
-5, 1
67-AP
A-37/
FD-40
Hatak
eyam
a, Y.,
63-A
SE-5
Hatto
ri, M.
, 131
-PDL-8
Hauc
ke, F
., 31
-APA-7
/FD-8
, 85-A
PA-18
/FD-2
1Ha
upt,
M., 8
4-APA
-17Ha
y, A.,
48-F
D-47,
149
-CFD-4
1Ha
ynes
, J.,
9-ASE
-1He
, G.,
26-TP
-1He
ath, S
., 49
-GT-2
Hedri
ck, T
., 14
2-APA
-33/F
D-33
Heft,
A., 3
2-APA
-8He
ineck
, J.,
88-AP
A-21
Heinr
ich, R
., 17
2-FD-4
3He
inz, S
., 12
0-CFD
-32He
inze,
R., 1
51-FD
-34He
inze,
W., 3
2-APA
-8He
lber, B
., 78
-TP-6
Henfl
ing, J
., 73
-FD-18
, 171
-FD-42
, 175
-FD-48
Henry
de Fr
ahan
, M.,
44-CF
D-14
Herdr
ich, G
., 13
4-TP-1
3He
reth,
L., 8
-APA-5
Herm
anns
, M.,
126-F
D-29
Hervy
, F.,
62-AS
E-4He
sselin
k, L.,
176
-FD-49
Hicke
l, S.,
120-C
FD-32
, 139
-APA-3
0Hil
bert,
C., 8
-APA-5
Hill, K
., 24
-GT-1
Hillen
, N.,
125-F
D-28
Hillew
aert,
K., 1
6-CFD
-7Hil
lier, R
., 72
-FD-17
Hind,
M., 1
29-FD
-32Hir
abay
ashi,
N.,
152-F
D-35
Hirak
i, K.,
87-AP
A-20
Hird,
K., 1
58-PD
L-11/
FD-39
Hitt,
D., 1
7-FD-1
, 52-T
P-4, 1
01-FD
-24, 1
25-FD
-28Hit
zel, S
., 35
-APA-1
1Ho
ad, D
., 49
-GT-2
Hodiz
c, E.,
147
-CFD-3
9Ho
lden,
M., 9
4-CFD
-23Ho
lland
s, M.
, 32-A
PA-8
Holle
nstei
n, C.,
75-F
D-20,
103
-PDL-6
Hollis
, B.,
79-TP
-7Ho
oker,
J., 1
14-AP
A-26
Hopp
mann
, D.,
172-F
D-43
Hornu
ng, M
., 36
-ASE-2
, 112
-APA-2
4Ho
rst, P
., 32
-APA-8
, 84-A
PA-17
Hosse
ini, Z
., 15
1-FD-3
4Ho
sseinv
erdi, S
., 47
-FD-12
Hou,
A., 6
-APA-3
Hous
man,
J., 1
5-CFD
-6, 3
4-APA
-10Hö
velm
ann,
A., 1
68-AP
A-38
Hovs
apian
, R.,
8-APA
-5Ho
wiso
n, J.,
121
-CFD-3
3Hs
u, I.,
159
-TP-16
Hsu,
K., 9
4-CFD
-23Hu
, H.,
60-AP
A-15/
FD-14
, 86-A
PA-19
, 88-A
PA-21
, 1
42-AP
A-33/
FD-33
, 143
-ASE-9
, 166
-APA-3
6Hu
, X.,
74-FD
-19/P
DL-3
Hu, Z
., 12
7-FD-3
0Hu
a, Z.,
153
-FD-36
Huan
g, G.
, 43-C
FD-13
, 140
-APA-3
1Hu
ang,
S., 1
40-AP
A-31
Hubb
ard, J
., 21
-FD-5,
167
-APA-3
7/FD
-40Hu
bin, A
., 78
-TP-6
Hue,
D., 3
0-APA
-6, 1
70-FD
-41/G
T-6Hu
ebsch
, W.,
176-F
D-49
Hueh
ne, C
., 85
-APA-1
8/FD
-21Hu
mphre
ys, W
., 49
-GT-2
Huns
aker,
D.,
114-A
PA-26
, 166
-APA-3
6Hu
nter, P
., 17
1-FD-4
2Hu
o, W.
, 79-T
P-7Hu
tches
on, F
., 49
-GT-2
Huyn
h, D.
, 98-C
FD-27
Huyn
h, H.
, 11-C
FD-2,
39-C
FD-9
Iacca
rino,
G., 7
0-CFD
-21/F
D-15
Ickes
, J.,
84-AP
A-17
Ihme,
M., 9
4-CFD
-23, 1
44-CF
D-36
Illi, S
., 30
-APA-6
Im, K
., 65
-CFD-1
6/GT
-3, 1
45-CF
D-37
Imaiz
umi, T
., 59
-APA-1
4Im
amura
, T.,
98-CF
D-27
Impe
ratore
, B.,
88-AP
A-21
Inamd
ar, A.
, 37-A
SE-3
Inatan
i, Y.,
128-F
D-31
Inding
er, T.
, 32-A
PA-8
Irann
ejad,
A., 4
5-FD-1
0Ish
ida, K
., 13
3-TP-1
2Ish
ida, T
., 15
-CFD-6
Ishii,
M., 1
06-TP
-10Ish
ikawa
, H.,
156-G
T-5Ish
ikawa
, M.,
104-P
DL-7,
131
-PDL-8
Ito, Y
., 68
-CFD-1
9Ito
h, K.,
126
-FD-29
Ivanc
o, T.,
49-G
T-2Iw
akaw
a, A.,
157
-PDL-1
0Iye
ngar,
V., 4
9-GT-2
Izen,
S., 6
2-ASE
-4Ja
beri,
F., 4
5-FD-1
0Ja
cobs
, C.,
78-TP
-6, 1
34-TP
-13Ja
cobs
, G.,
12-CF
D-3, 4
4-CFD
-14Ja
cobs
on, M
., 37
-ASE-3
Jacq
uin, L
., 11
5-APA
-27/F
D-26
Jaffe
, R.,
160-T
P-17
Jaga
dees
h, C.,
169
-APA-3
9/FD
-46Ja
lali, A
., 40
-CFD-1
0Ja
mes,
C., 2
7-TP-2
Jame
son,
A., 9
3-CFD
-22, 1
76-FD
-49Ja
nsen
, K.,
14-CF
D-5, 7
6-PDL
-4Ja
nus,
J., 5
8-APA
-13Ja
rczyk
, M.,
120-C
FD-32
Jarrig
e, J.,
50-P
DL-2
Jasa
k, H.
, 68-C
FD-19
Jave
d, A.,
99-C
FD-28
Jeda
mski,
D.,
123-C
FD-35
Jedrz
ejows
ki, P.
, 16-C
FD-7
Jeffr
ies, J
., 77
-PDL-5
Jemc
ov, A
., 15
8-PDL
-11/F
D-39
Jian,
Z., 1
67-AP
A-37/
FD-40
Jin, J
., 58
-APA-1
3Jin
geles
ki, D
., 5-A
PA-2
Jiras
ek, A
., 34
-APA-1
0Jo
, Y.,
32-AP
A-8Jo
hans
en, C
., 15
2-FD-3
5Jo
hnse
n, E.,
11-C
FD-2,
44-C
FD-14
, 144
-CFD-3
6,
155
-FD-38
John
son,
E., 8
-APA-5
John
son,
H., 1
53-FD
-36Jo
hnso
n, M.
, 87-A
PA-20
John
ston,
C., 7
9-TP-7
Jone
s, A.,
59-A
PA-14
, 86-A
PA-19
, 139
-APA-3
0Jo
nes,
G., 6
1-APA
-16, 8
5-APA
-18/F
D-21,
141-A
PA-32
, 1
67-AP
A-37/
FD-40
Jone
s, M.
, 20-F
D-4Jo
rgens
on, P
., 62
-ASE-4
Josy
ula, E
., 63
-ASE-5
, 80-T
P-8Jo
tkar, M
., 19
-FD-3
Jova
novic
, M.,
17-FD
-1Ju
liano
, T.,
158-P
DL-11
/FD-3
9Ju
mper,
E., 1
58-PD
L-11/
FD-39
Jung
, K.,
41-CF
D-11,
115
-APA-2
7/FD
-26Ju
ng, S
., 41
-CFD-1
1Ju
niper,
M.,
47-FD
-12Jy
othish
kuma
r, V.,
71-FD
-16Ka
ario,
O., 6
8-CFD
-19Ka
iser, B
., 8-A
PA-5
Kalra
, T.,
35-AP
A-11
Kame
ier, F
., 15
1-FD-3
4Ka
n, Y.,
155
-FD-38
Kana
zaki,
M.,
31-AP
A-7/F
D-8Ka
ng, C
., 20
-FD-4
Kang
, K.,
47-FD
-12Ka
o, D.
, 166
-APA-3
6Ka
padia
, S.,
40-CF
D-10
Kapa
hi, A.
, 122
-CFD-3
4Ka
pania
, R.,
5-APA
-2Ka
pat,
J., 1
33-TP
-12Ka
ra, K.
, 86-A
PA-19
, 115
-APA-2
7/FD
-26Ka
rampe
las, S
., 20
-FD-4
Karl,
S., 3
8-CFD
-8, 1
05-TP
-9Ka
rtha,
A., 1
74-FD
-45Ka
sema
n, T.,
25-P
DL-1
Katsu
rayam
a, H.
, 131
-PDL-8
Katta
, V.,
101-F
D-24
Katz,
A., 4
0-CFD
-10, 1
46-CF
D-38
Katz,
J., 5
8-APA
-13Ka
ul, U
., 12
8-FD-3
1, 1
71-FD
-42
83
Auth
or/S
essio
n Ch
air In
dex
Kawa
i, S.,
76-PD
L-4, 1
44-CF
D-36
Kawa
zoe,
H., 3
1-APA
-7/FD
-8Ka
ynak
, U.,
33-AP
A-9/F
D-9Ke
arney
, J.,
31-AP
A-7/F
D-8Ke
gelm
an, J
., 17
0-FD-4
1/GT
-6Ke
geris
e, M.
, 47-F
D-12,
153
-FD-36
Kelle
ners,
P., 1
72-FD
-43Ke
ller, D
., 13
9-APA
-30Ke
ller, M
., 10
6-TP-1
0Ke
lly, R.
, 158
-PDL-1
1/FD
-39Ke
nnett
, D.,
97-CF
D-26
Kenw
ay, G
., 42
-CFD-1
2Ke
rho, M
., 58
-APA-1
3Ke
shmi
ri, A.,
10-C
FD-1,
45-F
D-10
Kesk
inen,
J., 6
8-CFD
-19Ke
ssler,
M.,
11-CF
D-2, 3
2-APA
-8Ke
tsdev
er, A.
, 50-P
DL-2,
63-A
SE-5
Keye
, S.,
30-AP
A-6, 1
16-AP
A-28
Khan
, J.,
71-FD
-16Kh
an, O
., 71
-FD-16
Khieu
, L.,
64-CF
D-15
Khod
adou
st, A.
, 100
-CFD-2
9/FD
-23Kh
urana
, S.,
31-AP
A-7/F
D-8, 1
06-TP
-10, 1
54-FD
-37Kim
, B.,
58-AP
A-13
Kim, C
., 44
-CFD-1
4, 6
0-APA
-15/F
D-14,
1
15-AP
A-27/
FD-26
Kim, H
., 7-A
PA-4,
44-C
FD-14
, 115
-APA-2
7/FD
-26Kim
, I.,
26-TP
-1Kim
, J.,
41-CF
D-11,
160
-TP-17
Kim, K
., 32
-APA-8
Kim, M
., 10
4-PDL
-7, 1
15-AP
A-27/
FD-26
Kim, S
., 67
-CFD-1
8Kim
mel, R
., 73
-FD-18
, 170
-FD-41
/GT-6
, 175
-FD-48
Kimura
, S.,
36-AS
E-2Kin
g, R.,
153
-FD-36
Kiris,
C., 1
5-CFD
-6, 3
4-APA
-10Kir
k, B.
, 38-C
FD-8
Kirk,
T., 8
9-APA
-22/F
D-22
Kirke
gaard
, J.,
62-AS
E-4Kir
z, J.,
165
-APA-3
5Kit
amura
, K.,
66-CF
D-17
Klaas
, M.,
33-AP
A-9/F
D-9, 4
8-FD-4
7, 1
38-AP
A-29
Kleb,
B., 3
8-CFD
-8Kle
in, S
., 10
1-FD-2
4, 1
72-FD
-43Kle
ine, H
., 87
-APA-2
0Kle
ntzma
n, J.,
102
-FD-25
Kloke
r, M.,
106-T
P-10
Knez
evici,
D.,
62-AS
E-4Kn
igge,
C., 1
72-FD
-43Kn
opp,
T., 1
72-FD
-43Ko
ch, S
., 11
3-APA
-25Ko
cian,
T., 1
02-FD
-25
Koda
ma, H
., 15
6-GT-5
Koivi
sto, P
., 11
7-ASE
-8Ko
izumi
, H.,
132-P
DL-9
Kojim
a, T.,
59-A
PA-14
Koklu
, M.,
21-FD
-5Ko
llasch
, J.,
112-A
PA-24
Kolm
ogoro
v, D.
, 41-C
FD-11
Kolob
ov, V
., 99
-CFD-2
8Ko
losza
r, L.,
43-CF
D-13
Koma
tsu, F
., 10
4-PDL
-7Ko
muras
aki, K
., 13
2-PDL
-9Ko
muro,
T., 1
26-FD
-29Ko
nigors
ki, D
., 13
1-PDL
-8Ko
nrath,
R., 1
41-AP
A-32
Konti
s, K.,
103
-PDL-6
Koren
, B.,
148-C
FD-40
Korzu
n, A.,
87-A
PA-20
Kotov
, D.,
12-CF
D-3Ko
tov, M
., 11
6-APA
-28Ko
tsonis
, M., 2
5-PDL
-1, 86
-APA-1
9, 16
7-APA
-37/F
D-40
Koya
ma, T
., 15
2-FD-3
5Ko
zlov,
P., 2
7-TP-2
Kraem
er, E.
, 11-C
FD-2,
30-AP
A-6, 3
2-APA
-8, 95
-CFD-2
4Kra
kos,
J., 1
48-CF
D-40
Krame
r, F.,
42-CF
D-12
Kraste
v, V.,
176
-FD-49
Kratzk
e, J.,
41-C
FD-11
Kraus
e, M.
, 41-C
FD-11
Kreeg
er, R.
, 36-A
SE-2
Kreme
yer, K
., 10
3-PDL
-6Kre
shoc
k, A.,
166
-APA-3
6Kre
ss, J.
, 105
-TP-9
Krieg
seis,
J., 1
68-AP
A-38
Krish
namu
rthy,
R., 1
38-AP
A-29
Krotko
v, N.
, 9-AS
E-1Krü
ger, O
., 67
-CFD-1
8, 1
21-CF
D-33,
147
-CFD-3
9,
148
-CFD-4
0Kr
yuko
v, I.,
116
-APA-2
8Ku
, J.,
26-TP
-1Ku
cken
burg,
S.,
113-A
PA-25
Kueh
l, J.,
102-F
D-25
Kues
ter, M
., 15
3-FD-3
6Ku
hlman
, J.,
125-F
D-28,
151
-FD-34
Kulak
hmeto
v, M.
, 160
-TP-17
Kuma
r, P.,
49-GT
-2Ku
mar, R
., 13
5-TP-1
4Ku
mar, U
., 69
-CFD-2
0, 1
22-CF
D-34
Kuma
rasam
y, S.
, 49-G
T-2Ku
ntz, D
., 52
-TP-4
Kurba
tskii,
K., 3
5-APA
-11, 1
51-FD
-34Ku
rosaw
a, K.,
63-A
SE-5
Kush
ner, L
., 88
-APA-2
1
Kwak
, D.,
113-A
PA-25
, 139
-APA-3
0Kw
ak, E
., 13
8-APA
-29Kw
on, H
., 32
-APA-8
Kwon
, J.,
32-AP
A-8La
broqu
ère, J
., 96
-CFD-2
5La
chau
d, J.,
78-T
P-6La
cy, D
., 31
-APA-7
/FD-8
, 139
-APA-3
0La
flin, K
., 30
-APA-6
Lai, J
., 14
2-APA
-33/F
D-33
Laks
hmina
rayan
, V.,
13-CF
D-4, 3
5-APA
-11La
m, T.
, 52-T
P-4, 1
07-TP
-11La
mbert
, M.,
38-CF
D-8, 1
05-TP
-9La
ngel,
C., 8
6-APA
-19La
nger,
T., 1
32-PD
L-9La
ni, A.
, 43-C
FD-13
, 65-C
FD-16
/GT-3
, 105
-TP-9
Lans
hin, A
., 37
-ASE-3
Larm
i, M.,
68-CF
D-19
Larss
on, J
., 70
-CFD-2
1/FD
-15La
un, M
., 10
3-PDL
-6La
urend
eau,
E., 3
0-APA
-6, 6
1-APA
-16La
ux, C
., 53
-TP-5,
78-T
P-6, 1
34-TP
-13Le
achm
an, J
., 14
1-APA
-32lee
, D.,
67-CF
D-18
Lee,
B., 5
7-APA
-12, 7
7-PDL
-5, 1
15-AP
A-27/
FD-26
Lee,
C., 1
38-AP
A-29
Lee,
D., 5
8-APA
-13Le
e, H.
, 32-A
PA-8,
58-A
PA-13
Lee,
J., 5
3-TP-5
, 67-C
FD-18
, 146
-CFD-3
8Le
e, K.,
60-A
PA-15
/FD-1
4Le
e, S.
, 58-A
PA-13
, 117
-ASE-8
, 138
-APA-2
9Le
feber,
D.,
129-F
D-32
Lefeb
vre, A
., 31
-APA-7
/FD-8
Lefeb
vre’s,
J., 1
39-AP
A-30
Lego
, Z.,
142-A
PA-33
/FD-3
3Le
guiza
mon,
S., 1
21-CF
D-33
Lei, J
., 73
-FD-18
Leite
, P.,
80-TP
-8Le
ithea
d, W.
, 86-A
PA-19
Lele,
S.,
37-AS
E-3, 1
75-FD
-48, 1
76-FD
-49Le
mpert
, W.,
46-FD
-11Le
onov
, S.,
77-PD
L-5, 1
54-FD
-37Le
slie, B
., 24
-GT-1
Lesta
ri, A.,
35-A
PA-11
Levin
, D., 5
0-PDL
-2, 80
-TP-8,
157-P
DL-10
, 175
-FD-48
Lewi
s, M.
, 46-F
D-11
Leyla
nd, P
., 10
3-PDL
-6Li,
F., 4
7-FD-1
2, 7
0-CFD
-21/F
D-15
Li, H
., 88
-APA-2
1Li,
J., 7
2-FD-1
7Li,
W.,
59-AP
A-14
Li, Y.
, 64-C
FD-15
, 74-F
D-19/
PDL-3
Li, Z.
, 50-P
DL-2,
80-T
P-8, 1
15-AP
A-27/
FD-26
Liang
, C.,
11-CF
D-2, 1
6-CFD
-7Lia
ng, H
., 74
-FD-19
/PDL
-3Lie
chty,
D.,
106-T
P-10
Liesn
er, K.
, 75-F
D-20
Lieve
r, P.,
90-AP
A-23
Likha
nskii
, A.,
25-PD
L-1, 1
03-PD
L-6Lil
lard,
R., 7
0-CFD
-21/F
D-15
Lim, T
., 20
-FD-4
Lima,
S., 8
8-APA
-21Lin
, C.,
63-AS
E-5Lin
, J.,
176-F
D-49
Lind,
A., 1
39-AP
A-30
Linds
ay, F
., 9-A
SE-1
Lino D
a Silv
a, M.
, 160
-TP-17
Liou,
M., 7
-APA-4
, 39-C
FD-9,
57-A
PA-12
, 66-C
FD-17
, 1
24-FD
-27Lip
inski,
D.,
101-F
D-24
Little
, J.,
74-FD
-19/P
DL-3,
75-F
D-20
Little
, Z.,
133-T
P-12
Liu, C
., 8-A
PA-5
Liu, F
., 71-F
D-16,
123-C
FD-35
, 138
-APA-2
9, 17
5-FD-4
8Liu
, N.,
120-C
FD-32
Liu, T
., 17
2-FD-4
3Liu
, Y.,
79-TP
-7, 8
9-APA
-22/F
D-22,
123
-CFD-3
5,
138
-APA-2
9, 1
60-TP
-17Lo
, M.,
64-CF
D-15
Loda
to, G
., 15
1-FD-3
4Lo
ehle,
S.,
52-TP
-4, 1
34-TP
-13, 1
35-TP
-14Lo
hle, S
., 52
-TP-4
Lohn
er, R.
, 97-C
FD-26
Lohry
, M.,
112-A
PA-24
Long
, K.,
70-CF
D-21/
FD-15
Lonk
ar, A.
, 57-A
PA-12
, 76-P
DL-4
Lope
z, B.
, 160
-TP-17
Lope
z, O.
, 121
-CFD-3
3Lo
renzi,
J., 1
70-FD
-41/G
T-6Lo
th, E.
, 33-A
PA-9/
FD-9,
36-A
SE-2
Louis
os, W
., 52
-TP-4,
101
-FD-24
, 176
-FD-49
Loure
iro, J
., 16
0-TP-1
7Lo
w, H
., 33
-APA-9
/FD-9
Lowe
, K.,
170-F
D-41/
GT-6
Lu, Z
., 5-A
PA-2
Lua,
K., 2
0-FD-4
Luca
s, J.,
88-A
PA-21
Luha
r, M.,
22-FD
-6, 1
74-FD
-45Lu
ke, E
., 36
-ASE-2
, 90-A
PA-23
Lumb
, S.,
156-G
T-5Lu
ndqu
ist, T
., 93
-CFD-2
2Lu
nsfor
d, C.,
49-G
T-2Lu
o, H.
, 16-C
FD-7,
142
-APA-3
3/FD
-33, 1
44-CF
D-36
Luo,
J., 7
1-FD-1
6Lu
o, S.
, 123
-CFD-3
5, 1
38-AP
A-29
Lurie
, E.,
100-C
FD-29
/FD-2
3Lu
tz, T.
, 30-A
PA-6,
95-C
FD-24
, 172
-FD-43
Luu,
V., 4
3-CFD
-13Lv,
Y., 1
44-CF
D-36
Lv, Z.
, 74-F
D-19/
PDL-3
Lyrin
tzis,
A., 1
51-FD
-34Ly
u, Z.,
42-C
FD-12
Ma, Y
., 10
7-TP-1
1Ma
as, U
., 13
2-PDL
-9Ma
cDon
ald, M
., 78
-TP-6,
134
-TP-13
MacD
owell
, A.,
78-TP
-6Ma
cLean
, M.,
53-TP
-5, 9
4-CFD
-23Ma
Cleod
, J.,
62-AS
E-4, 1
17-AS
E-8Ma
dden
, T.,
132-P
DL-9
Maed
a, K.,
31-A
PA-7/
FD-8
Magin
, T., 1
6-CFD
-7, 78
-TP-6,
102-F
D-25,
159-T
P-16,
1
60-TP
-17Ma
gstad
t, A.,
129
-FD-32
Maha
patra
, S.,
176-F
D-49
Mahm
ood,
S., 3
1-APA
-7/FD
-8, 8
5-APA
-18/F
D-21
Mahz
ari, M
., 79
-TP-7
Maire
, P.,
32-AP
A-8Ma
isto,
P., 1
70-FD
-41/G
T-6Ma
jamak
i, A.,
35-AP
A-11,
113
-APA-2
5Ma
jima,
R., 1
57-PD
L-10
Makk
ar, D
., 13
5-TP-1
4Ma
ldona
do, C
., 63
-ASE-5
Malik
, A.,
84-AP
A-17
Malik
, M.,
70-CF
D-21/
FD-15
, 100
-CFD-2
9/FD
-23Ma
louin,
B.,
30-AP
A-6Ma
ni, K.
, 112
-APA-2
4Ma
ni, M
., 95
-CFD-2
4, 1
47-CF
D-39
Maniy
edath
, A.,
62-AS
E-4Ma
nkba
di, R.
, 47-F
D-12,
151
-FD-34
Mans
our, N
., 78-T
P-6, 1
05-TP
-9, 15
9-TP-1
6, 65
-APA-3
5Ma
ntelli,
M.,
26-TP
-1Ma
rañon
Di L
eo, J
., 17
1-FD-4
2Ma
rcel, J
., 12
9-FD-3
2Ma
rcotte
, D.,
91-AS
E-6Ma
rcum,
D.,
68-CF
D-19
Maria
ppan
, S.,
140-A
PA-31
Marin
o, A.,
75-F
D-20,
88-A
PA-21
Mario
n, M.
, 39-C
FD-9
Marku
s, D.
, 132
-PDL-9
Maron
giu, C
., 75
-FD-20
, 138
-APA-2
9Ma
rshall
, D.,
146-C
FD-38
Martin
, A.,
51-TP
-3, 7
8-TP-6
Martin
, M.,
106-T
P-10
Martin
, P.,
72-FD
-17, 1
55-FD
-38Ma
rtinell
i, L.,
112-A
PA-24
Martin
ez, E
., 13
4-TP-1
3Ma
rtins,
J., 4
2-CFD
-12
84
Auth
or/S
essio
n Ch
air In
dex
Martin
uzzi,
R., 1
51-FD
-34Ma
ru, Y.
, 59-A
PA-14
Marui
, M.,
133-T
P-12
Maryn
owsk
i, T.,
52-TP
-4Ma
ssey,
S., 1
66-AP
A-36
Matee
scu, D
., 33
-APA-9
/FD-9
Matha
roo, H
., 13
5-TP-1
4Ma
tsumu
ra, S
., 73
-FD-18
Matsu
no, T
., 31
-APA-7
/FD-8
Matsu
numa
, T.,
71-FD
-16Ma
tsuo,
Y., 9
8-CFD
-27Ma
tsuya
ma, S
., 12
6-FD-2
9Ma
ttheij
ssens
, J.,
129-F
D-32
Mattle
, D.,
165-A
PA-35
Matve
ev, K
., 5-A
PA-2,
141
-APA-3
2Ma
ughm
er, M
., 5-A
PA-2
Mavri
plis,
D., 9
7-CFD
-26, 1
00-CF
D-29/
FD-23
, 1
12-AP
A-24,
144
-CFD-3
6, 1
48-CF
D-40
Mavri
s, D.
, 138
-APA-2
9Ma
y, G.
, 118
-CFD-3
0Ma
yes,
R., 1
71-FD
-42Ma
zahe
ri, A.,
49-G
T-2Mc
Clain,
S.,
36-AS
E-2, 1
43-AS
E-9Mc
Coma
s, A.,
58-A
PA-13
, 114
-APA-2
6Mc
Corm
ick, B
., 4-A
PA-1
McDa
niel, J
., 87
-APA-2
0Mc
Devit
t, M.
, 125
-FD-28
McGr
ath, B
., 88
-APA-2
1, 1
16-AP
A-28
McGu
ire, S
., 77
-PDL-5
McGu
irk, J
., 95
-CFD-2
4Mc
intyre
, T.,
27-TP
-2, 5
3-TP-5
McKe
on, B
., 17
-FD-1,
22-F
D-6, 1
55-FD
-38Mc
Laug
hlin,
T., 7
2-FD-1
7, 1
15-AP
A-27/
FD-26
McMu
llan,
W., 1
01-FD
-24Mc
Phail
, A.,
152-F
D-35
McW
herte
r-Pay
ne, M
., 15
1-FD-3
4Me
aux,
M., 4
2-CFD
-12Me
ckstr
oth, C
., 16
9-APA
-39/F
D-46
Mede
iros,
M., 1
76-FD
-49Me
dida,
S., 1
0-CFD
-1, 1
47-CF
D-39
Mehe
ut, M
., 86
-APA-1
9Me
inke,
M., 6
9-CFD
-20Me
le, B
., 33
-APA-9
/FD-9
Menc
hini, C
., 12
5-FD-2
8Me
negh
ini, J
., 12
8-FD-3
1Me
ng, F
., 18
-FD-2
Merkl
e, C.,
132
-PDL-9
Merle
n, A.,
157
-PDL-1
0Me
sick,
N., 4
9-GT-2
Meye
r, M.,
139-A
PA-30
Meye
r, R.,
75-FD
-20Me
yers,
J., 1
59-TP
-16
Mich
ail, S
., 77
-PDL-5
Mich
el, B
., 13
-CFD-4
Mies
ch, M
., 11
-CFD-2
Miha
escu
, M.,
71-FD
-16Mi
kouc
hi, T.
, 63-A
SE-5
Milan
ese,
F., 2
6-TP-1
Miles
, R.,
25-PD
L-1, 4
6-FD-1
1, 7
7-PDL
-5Mi
lholen
, W.,
85-AP
A-18/
FD-21
, 141
-APA-3
2Mi
ller, D
., 72
-FD-17
Mille
r, R.,
114-A
PA-26
Mille
t, C.,
176
-FD-49
Millig
an, R
., 94
-CFD-2
3Mi
lls, B
., 13
0-GT-4
Milne
, G.,
171-F
D-42
Min,
D., 4
4-CFD
-14Mi
nelli,
A., 5
7-APA
-12Mi
ron, P
., 14
8-CFD
-40Mi
shra,
A., 1
12-AP
A-24
Mistr
y, V.,
95-C
FD-24
Mitsu
dharm
adi, H
., 33
-APA-9
/FD-9
Mitta
l, A.,
8-APA
-5Mi
yaza
ki, T.
, 106
-TP-10
, 134
-TP-13
Mizo
kami
, T.,
16-CF
D-7Mo
arref,
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2-FD-6
, 155
-FD-38
Moell
er, T.
, 50-P
DL-2,
132
-PDL-9
Moen
s, F.,
91-A
SE-6
Moes
sner,
M.,
123-C
FD-35
Moha
gheg
h, F.,
122
-CFD-3
4Mo
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., 42
-CFD-1
2Mo
hamm
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., 23
-FD-7
Mohs
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., 22
-FD-6,
89-A
PA-22
/FD-2
2, 1
01-FD
-24,
124
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, 125
-FD-28
, 169
-APA-3
9/FD
-46Mo
in, P.
, 70-C
FD-21
/FD-1
5Mo
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kta, S
., 15
-CFD-6
, 34-A
PA-10
Molch
anov
, A.,
44-CF
D-14,
133
-TP-12
, 174
-FD-45
Molto
n, P.,
170
-FD-41
/GT-6
Monta
gnac
, M.,
42-CF
D-12
Moore
, H.,
128-F
D-31
Moore
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119-C
FD-31
Morga
n, P.,
7-AP
A-4, 3
3-APA
-9/FD
-9, 74
-FD-19
/PDL
-3Mo
rgan,
R., 2
7-TP-2
, 53-T
P-5Mo
riarty
, K.,
45-FD
-10Mo
rita, K
., 36
-ASE-2
, 156
-GT-5
Moro,
D.,
119-C
FD-31
Morris
, G.,
125-F
D-28
Morris
, S.,
139-A
PA-30
Morte
nsen
, C.,
127-F
D-30
Morto
nson
, A.,
91-AS
E-6Mo
usel,
J., 6
9-CFD
-20, 1
22-CF
D-34
Mova
hed,
P., 1
55-FD
-38Mu
ghal,
M.,
153-F
D-36
Mukh
opad
hyay
, A.,
176-F
D-49
Mund
is, N
., 14
8-CFD
-40Mu
ndt,
C., 1
0-CFD
-1Mu
nk, M
., 10
7-TP-1
1Mu
rakam
i, T.,
104-P
DL-7
Muray
ama,
M., 3
0-APA
-6, 6
8-CFD
-19Mu
rman
, S.,
70-CF
D-21/
FD-15
, 100
-CFD-2
9/FD
-23Mu
rphy,
J., 1
45-CF
D-37
Murph
y, K.,
87-A
PA-20
Murra
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9-AS
E-1, 3
7-ASE
-3, 8
9-APA
-22/F
D-22,
1
69-AP
A-39/
FD-46
Murra
y-Krez
an, J
., 92
-ASE-7
Muzy
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52-TP
-4My
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1-CFD
-11Na
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., 57
-APA-1
2, 6
4-CFD
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12-AP
A-24
Naga
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16-CF
D-7Na
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Y., 1
31-PD
L-8Na
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., 14
2-APA
-33/F
D-33
Nair,
A., 1
44-CF
D-36
Naito
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67-CF
D-18
Naito
h, K.,
19-F
D-3, 1
33-TP
-12Na
jafi M
arzba
li, S.
, 16-C
FD-7
Naka
hash
i, K.,
15-CF
D-6, 6
9-CFD
-20, 9
8-CFD
-27Na
kakit
a, K.,
156
-GT-5
Naka
mura,
M.,
128-F
D-31
Naka
shim
a, T.,
140
-APA-3
1Na
kaya
ma, K
., 67
-CFD-1
8Na
rayan
arao,
B., 1
38-AP
A-29
Naray
anas
wamy
, V.,
45-FD
-10Na
stasia
, R.,
14-CF
D-5Na
taraja
n, H.
, 22-F
D-6Na
then,
P., 4
1-CFD
-11Na
tions
Mart
in, M
., 77
-PDL-5
Naug
hton,
J., 1
29-FD
-32Na
waz,
A., 7
7-PDL
-5, 1
34-TP
-13, 1
57-PD
L-10,
1
59-TP
-16Na
wroth
, H.,
18-FD
-2, 4
5-FD-1
0Ne
benfu
hr, B
., 95
-CFD-2
4Ne
itzel,
K., 7
9-TP-7
Nejat
, A.,
93-CF
D-22
Nemi
li, A.,
42-C
FD-12
Newfi
eld, M
., 13
4-TP-1
3Ne
wman
, A.,
155-F
D-38
Nguy
en, C
., 98
-CFD-2
7, 1
18-CF
D-30,
119
-CFD-3
1Ng
uyen
, L.,
47-FD
-12Ng
uyen
, N.,
67-CF
D-18
Niede
rmeie
r, C.,
120-C
FD-32
Nikito
poulo
s, D.
, 124
-FD-27
Nikka
r, S.,
41-CF
D-11
Nikou
eeya
n, P.,
129
-FD-32
Nishik
awa,
H., 4
0-CFD
-10Nit
sche,
W., 3
1-APA
-7/FD
-8, 8
5-APA
-18/F
D-21,
11
6-APA
-28
Niwa,
N., 1
04-PD
L-7No
gami
, T.,
19-FD
-3No
guch
i, D.,
16-CF
D-7No
ll, B.
, 12-C
FD-3
Nomp
elis,
I., 1
4-CFD
-5No
nomu
ra, T.
, 40-C
FD-10
, 75-F
D-20,
128
-FD-31
, 1
72-FD
-43No
rdstro
m, J.
, 41-C
FD-11
, 93-C
FD-22
, 122
-CFD-3
4No
rthrup
, S.,
12-CF
D-3No
urgali
ev, R
., 14
4-CFD
-36No
uzaw
a, T.,
140
-APA-3
1No
yes,
M., 6
3-ASE
-5O’
Byrne
, S.,
25-PD
L-1O’
Conn
or, K.
, 33-A
PA-9/
FD-9
Oake
y, J.,
45-F
D-10
Obay
ashi
S., 6
9-CFD
-20, 9
8-CFD
-27Ob
erleit
hner,
K., 4
5-FD-1
0Oh
, S.,
58-AP
A-13
Ohira
, K.,
113-A
PA-25
, 139
-APA-3
0Oh
mich
i, Y.,
175-F
D-48
Okab
e, T.,
134
-TP-13
Okad
a, K.,
75-F
D-20
Okad
a, Y.,
140
-APA-3
1Ok
udair
a, K.,
63-A
SE-5
Okun
o, Y.,
104
-PDL-7
Ol, M
., 20
-FD-4,
129
-FD-32
, 169
-APA-3
9/FD
-46Ol
eskiw
, M.,
117-A
SE-8
Olive
ira, P
., 50
-PDL-2
Olive
r, M.,
62-AS
E-4Ol
iver, T
., 38
-CFD-8
Olivi
ero, N
., 10
2-FD-2
5Ol
livier
Goo
ch, C
., 40-C
FD-10
, 68-C
FD-19
, 149
-CFD-4
1Ol
sen,
M., 7
0-CFD
-21/F
D-15
Onish
i, K.,
69-CF
D-20
Orch
ard, D
., 11
7-ASE
-8Or
daz,
I., 5
9-APA
-14Or
kwis,
P., 1
1-CFD
-2Or
tiz, S
., 17
0-FD-4
1/GT
-6Os
man,
E., 1
51-FD
-34Os
toich
, C.,
48-FD
-47Os
uka,
T., 1
57-PD
L-10
Osus
ky, L
., 42
-CFD-1
2Os
usky
, M.,
30-AP
A-6Ot
su, H
., 13
1-PDL
-8Ot
t, P.,
103
-PDL-6
, 164
-APA-3
4Ot
ta, S
., 23
-FD-7
Otten
stein,
L., 2
6-TP-1
Otter
, D.,
141-A
PA-32
Outtie
r, P.,
10-CF
D-1, 1
3-CFD
-4Ow
ens,
W., 1
59-TP
-16Oy
ama,
A., 1
72-FD
-43Oy
arzun
, M.,
124-F
D-27
Ozaw
a, T.,
63-A
SE-5,
135
-TP-14
Ozba
y, A.,
86-A
PA-19
Pach
uilo,
M., 1
32-PD
L-9Pa
ciorri,
R., 1
32-PD
L-9Pa
ck M
elton
, L.,
21-FD
-5, 8
5-APA
-18/F
D-21,
1
41-AP
A-32
Pack
an, D
., 50
-PDL-2
Padil
la, J.
, 38-C
FD-8
Paffo
rd, B
., 10
3-PDL
-6Pa
ge, G
., 95
-CFD-2
4Pa
ige, C
., 42
-CFD-1
2Pa
in, R.
, 140
-APA-3
1Pa
lacios
, F.,
15-CF
D-6, 4
2-CFD
-12, 5
7-APA
-12,
67-C
FD-18
, 76-P
DL-4,
176
-FD-49
Pallu
coni,
S.,
48-FD
-47, 1
56-GT
-5Pa
lmer,
G.,
79-TP
-7Pa
n, H.
, 26-T
P-1Pa
nahi,
A., 3
3-APA
-9/FD
-9Pa
ndya
, M.,
35-AP
A-11
Pand
ya, S
., 14
6-CFD
-38Pa
nerai
, F.,
78-TP
-6Pa
nesi,
M.,
12-CF
D-3, 4
3-CFD
-13, 1
60-TP
-17Pa
niagu
a, G.
, 71-F
D-16
Pano
urgias
, K.,
15-CF
D-6Pa
ntano
, C.,
70-CF
D-21/
FD-15
Paoli
cchi, L
., 80
-TP-8
Papa
dakis
, M.,
117-A
SE-8
Papa
dimitri
ou, C
., 14
9-CFD
-41Pa
padim
itriou
, D.,
149-C
FD-41
Paras
chivo
iu, I.
, 61-A
PA-16
Pared
es, P
., 89
-APA-2
2/FD
-22, 1
02-FD
-25Pa
rk, C.
, 78-T
P-6Pa
rk, D
., 73
-FD-18
Park,
J., 6
7-CFD
-18Pa
rk, S
., 73
-FD-18
Parke
r, R.,
53-TP
-5Pa
rkins
on, D
., 78
-TP-6
Parle
tte, E
., 35
-APA-1
1Pa
rmar,
M.,
119-C
FD-31
Parso
ns, N
., 80
-TP-8
Pasch
ereit,
C., 1
8-FD-2
, 45-F
D-10,
67-C
FD-18
, 1
03-PD
L-6, 1
21-CF
D-33,
148
-CFD-4
0, 1
51-FD
-34Pá
scoa,
J., 5
0-PDL
-2Pa
squa
le, V.
, 88-A
PA-21
Patel
, D.,
26-TP
-1, 1
24-FD
-27Pa
til, V.
, 175
-FD-48
Paul,
R., 1
14-AP
A-26
Paul-
Dubo
is-Tain
e, A.,
57-A
PA-12
Paula
, L.,
113-A
PA-25
Paulu
s, D.
, 112
-APA-2
4Pa
volon
is, M
., 9-A
SE-1
Peka
rdan,
C., 1
06-TP
-10
85
Auth
or/S
essio
n Ch
air In
dex
Pelle
tier, D
., 48
-FD-47
, 149
-CFD-4
1Pe
ng, L
., 12
4-FD-2
7Pe
ng, S
., 95
-CFD-2
4, 1
13-AP
A-25
Pepe
, R.,
132-P
DL-9
Perai
re, J.
, 39-C
FD-9,
98-C
FD-27
, 118
-CFD-3
0,
119
-CFD-3
1Pe
rcin,
M., 2
0-FD-4
Perez
, E.,
102-F
D-25
Perez
, J.,
19-FD
-3Pe
roomi
an, O
., 26
-TP-1,
44-C
FD-14
Perss
on, P
., 60-A
PA-15
/FD-1
4, 64
-CFD-1
5, 93
-CFD-2
2,
144
-CFD-3
6Pe
schke
, P.,
75-FD
-20, 1
03-PD
L-6Pe
tcu, M
., 39
-CFD-9
Peter
s, D.
, 164
-APA-3
4Pe
terso
n, D.
, 22-F
D-6Pe
trilli,
J., 1
14-AP
A-26
Petro
sino,
F., 5
9-APA
-14Pe
tzold,
R., 1
9-FD-3
Pezz
ella,
G., 5
9-APA
-14, 7
9-TP-7
Pfitzn
er, M
., 12
0-CFD
-32Ph
am, A
., 13
3-TP-1
2Ph
illips
, T.,
15-CF
D-6, 1
49-CF
D-41
Philli
ps, W
., 11
4-APA
-26, 1
66-AP
A-36
Phu,
T., 6
9-CFD
-20Pie
lhop,
K., 4
8-FD-4
7Pie
rre-El
ie, W
., 14
0-APA
-31Pie
rson,
K., 8
-APA-5
, 41-C
FD-11
Pilz,
N., 1
38-AP
A-29
Pinco
ck, B
., 40
-CFD-1
0Pin
ier, J
., 5-A
PA-2,
87-A
PA-20
Pinna
, F.,
47-FD
-12, 1
02-FD
-25Pla
nte, F
., 48
-FD-47
Plesn
iak, M
., 60
-APA-1
5/FD
-14, 1
42-AP
A-33/
FD-33
Plogm
ann,
B., 1
53-FD
-36Plo
tkin,
A., 4
-APA-1
Plourd
e, F.,
43-C
FD-13
, 69-C
FD-20
Pogg
ie, J.
, 25-P
DL-1,
175
-FD-48
Polan
sky,
J., 9
2-ASE
-7Po
litovic
h, M.
, 9-AS
E-1Po
meroy
, B.,
114-A
PA-26
Pont,
G.,
13-CF
D-4Po
ole, D
., 67
-CFD-1
8Po
rat, H
., 53
-TP-5
Poros
eva,
S., 8
-APA-5
Porte
r, C.,
72-FD
-17, 1
15-AP
A-27/
FD-26
Post,
M.,
58-AP
A-13,
167
-APA-3
7/FD
-40Po
tapcz
uk, M
., 91
-ASE-6
, 143
-ASE-9
Potsd
am, M
., 16
5-APA
-35Po
tter, D
., 38
-CFD-8
, 105
-TP-9
Pottu
ri, A.,
18-F
D-2Po
urbag
ian, M
., 11
7-ASE
-8
Povit
sky,
A., 8
-APA-5
, 41-C
FD-11
Prabh
u, D.
, 12-C
FD-3,
27-T
P-2, 7
9-TP-7
, 134
-TP-13
Prieb
e, S.
, 72-F
D-17
Probs
t, A.,
172
-FD-43
Pronin
, Y.,
148-C
FD-40
Pruett
, B.,
73-FD
-18, 1
75-FD
-48Pu
eblas
, J.,
41-CF
D-11,
99-C
FD-28
Pul, R
., 16
7-APA
-37/F
D-40
Pulum
athi, M
., 49
-GT-2
Pytel
, D.,
51-TP
-3Qi
n, F.,
26-T
P-1Qu
acke
nbus
h, T.,
168
-APA-3
8Qu
an, J
., 6-A
PA-3
Quara
nta, V
., 88
-APA-2
1Qu
esad
a, J.,
128
-FD-31
Rade
spiel
, R.,
19-FD
-3, 1
01-FD
-24, 1
23-CF
D-35,
1
72-FD
-43Ra
ffel, M
., 14
0-APA
-31Ra
gab,
S., 2
2-FD-6
, 151
-FD-34
, 174
-FD-45
Ragh
eb, A
., 87
-APA-2
0Ra
i, N.,
122-C
FD-34
Raich
e, G.
, 77-P
DL-5
Raja,
L., 7
6-PDL
-4, 7
7-PDL
-5, 1
03-PD
L-6, 1
32-PD
L-9Ra
llabh
andi,
S.,
59-AP
A-14
Rama
doss,
M.,
135-T
P-14
Ramb
aud,
P., 2
2-FD-6
, 65-C
FD-16
/GT-3
, 102
-FD-25
Rame
sh, K
., 16
9-APA
-39/F
D-46
Ramp
urawa
la, A.
, 8-AP
A-5Ra
nd, L
., 63
-ASE-5
Raps
, D.,
36-AS
E-2Ra
quel,
G.,
128-F
D-31
Rash
ad, R
., 42
-CFD-1
2Ra
sky,
D., 1
34-TP
-13Ra
squin
, M.,
76-PD
L-4Ra
thay,
N., 8
5-APA
-18/F
D-21
Ravic
hand
ran, V
., 5-A
PA-2
Rebro
v, S.
, 133
-TP-12
Rech
enbe
rg, I.
, 103
-PDL-6
Reed
, E.,
87-AP
A-20
Reed
, H.,
7-APA
-4, 3
8-CFD
-8, 4
6-FD-1
1, 1
02-FD
-25Re
ich, G
., 16
9-APA
-39/F
D-46
Reich
el, T.
, 45-F
D-10
Reich
ling,
G., 1
2-CFD
-3Re
illy, D
., 23
-FD-7
Reim
er, T.
, 107
-TP-11
Rein,
M.,
113-A
PA-25
Reisn
er, J.
, 23-F
D-7Re
ist, T
., 7-A
PA-4
Ren,
J., 1
9-FD-3
Ren,
X., 1
38-AP
A-29
Rend
all, T
., 61
-APA-1
6, 6
7-CFD
-18, 8
4-APA
-17Re
nnie,
M.,
24-GT
-1, 1
58-PD
L-11/
FD-39
Reus
s, S.
, 172
-FD-43
Reym
ond,
B., 1
52-FD
-35Rh
ew, R
., 15
6-GT-5
Rich,
J., 4
6-FD-1
1Ric
hter, K
., 14
0-APA
-31Ril
ey, J
., 91
-ASE-6
Rinald
i, C.,
170-F
D-41/
GT-6
Rival,
D.,
60-AP
A-15/
FD-14
, 168
-APA-3
8Riv
ers, M
., 70
-CFD-2
1/FD
-15Riv
ir, R.,
52-T
P-4Riz
zetta
, D.,
153-F
D-36
Robe
rto, C
., 88
-APA-2
1Ro
berts
, M.,
153-F
D-36
Robin
et, J.
, 13-C
FD-4,
47-F
D-12
Robin
son,
F., 2
6-TP-1
Robin
son,
T., 9
6-CFD
-25Ro
ca, X
., 11
8-CFD
-30Ro
dio, M
., 44
-CFD-1
4Ro
drigu
es, C
., 44
-CFD-1
4Ro
drigu
ez, D
., 47
-FD-12
Rodri
guez
, E.,
79-TP
-7Ro
drigu
ez Ci
snero
s, E.,
113
-APA-2
5Ro
e, P.,
66-C
FD-17
, 118
-CFD-3
0Ro
gers,
M.,
70-CF
D-21/
FD-15
, 100
-CFD-2
9/FD
-23Ro
gers,
S.,
146-C
FD-38
Rohle
r, D.,
62-AS
E-4Ro
hlman
n, D.
, 116
-APA-2
8Ro
llin, B
., 23
-FD-7
Roma
nenk
o, Y.,
27-T
P-2Ro
na, A
., 10
1-FD-2
4Ro
osen
boom
, E., 3
4-APA
-10, 8
7-APA
-20, 1
41-AP
A-32,
1
65-AP
A-35,
166
-APA-3
6Ro
quem
ore, W
., 10
1-FD-2
4Ro
sli, M
., 59
-APA-1
4Ro
ss, J.
, 70-C
FD-21
/FD-1
5, 8
8-APA
-21Ro
ssi, R
., 15
1-FD-3
4Ro
thmay
er, A.
, 23-F
D-7, 1
43-AS
E-9Ro
ura S
ués,
M., 8
9-APA
-22/F
D-22
Rowl
ey, C
., 12
4-FD-2
7Ro
y, C.,
14-CF
D-5, 1
5-CFD
-6, 99
-CFD-2
8, 14
9-CFD
-41Ro
y, S.
, 25-P
DL-1
Rubin
stein,
R., 7
0-CFD
-21/F
D-15
Rudn
ik, R.
, 85-A
PA-18
/FD-2
1, 1
39-AP
A-30
Ruett
en, M
., 11
3-APA
-25Ru
ffin, S
., 53
-TP-5
Ruke
s, L.,
45-F
D-10
Rulev
a, L.,
116
-APA-2
8Ru
mpfke
il, M.
, 123
-CFD-3
5Ru
msey
, C.,
10-CF
D-1, 7
0-CFD
-21/F
D-15
Rums
ey, M
., 86
-APA-1
9Ru
scher,
C., 1
50-CF
D-42
Ryzh
ov, A
., 10
2-FD-2
5
Saeg
eler, S
., 10
-CFD-1
Sahin
, M.,
48-FD
-47Sa
hni, O
., 14
-CFD-5
Saito
h, K.,
134
-TP-13
Saka
i, R.,
98-CF
D-27
Saka
i, T.,
105-T
P-9, 1
57-PD
L-10
Saka
ue, H
., 36
-ASE-2
, 106
-TP-10
, 134
-TP-13
, 1
56-GT
-5Sa
lah el
Din,
I., 5
7-APA
-12Sa
laun,
M., 1
17-AS
E-8Sa
lemi, L
., 12
7-FD-3
0Sa
mami
, H.,
32-AP
A-8Sa
nders
e, B.
, 148
-CFD-4
0Sa
ndha
m, N
., 12
7-FD-3
0Sa
nghi,
S.,
33-AP
A-9/F
D-9Sa
nna,
A., 1
05-TP
-9Sa
nsica
, A.,
127-F
D-30
Santo
s, J.,
79-T
P-7Sa
ntos,
W., 8
0-TP-8
Saric
, W.,
7-APA
-4, 4
6-FD-1
1, 1
16-AP
A-28
Sarka
r, P.,
166-A
PA-36
Sarth
ou, A
., 44
-CFD-1
4Sa
rtor, F
., 72
-FD-17
Saso
h, A.,
59-A
PA-14
, 157
-PDL-1
0Sa
ssoon
, A.,
21-FD
-5, 1
67-AP
A-37/
FD-40
Sato,
K., 1
26-FD
-29Sa
to, M
., 75
-FD-20
Sato,
T., 5
9-APA
-14Sa
tofuk
a, Y.,
131
-PDL-8
Scalo
, C.,
176-F
D-49
Sche
tz, J.
, 5-AP
A-2, 2
4-GT-1
Schla
ger, H
., 62
-ASE-4
Schlu
ter, J
., 60
-APA-1
5/FD
-14Sc
hmiss
eur, J
., 46
-FD-11
Schn
eider,
G.,
52-TP
-4Sc
hneid
er, S
., 46
-FD-11
, 73-F
D-18
Schn
eiders
, L.,
69-CF
D-20
Schn
epf,
C., 1
39-AP
A-30
Scho
lz, P.
, 31-A
PA-7/
FD-8,
85-A
PA-18
/FD-2
1,
88-A
PA-21
, 101
-FD-24
, 172
-FD-43
Schrö
der, A
., 34
-APA-1
0Sc
hrodin
ger, C
., 45
-FD-10
Schrö
eder,
W.,
33-AP
A-9/F
D-9, 4
8-FD-4
7,
69-C
FD-20
, 138
-APA-2
9Sc
hrooy
en, P
., 16
-CFD-7
Schu
elein,
E., 1
39-AP
A-30
Schw
ane,
R., 3
8-CFD
-8Sc
hwart
z, H.
, 138
-APA-2
9Sc
hwart
zentr
uber,
T., 4
6-FD-1
1Sc
hwen
ke, D
., 79
-TP-7,
160
-TP-17
Schw
ing, A
., 14
-CFD-5
Scog
gins,
J., 1
59-TP
-16
Sega
wa, T
., 71
-FD-16
Seide
l, J.,
115-A
PA-27
/FD-2
6Se
kar, B
., 15
0-CFD
-42Se
khar,
S.,
53-TP
-5Se
kula,
M.,
166-A
PA-36
Selez
nev,
R., 1
33-TP
-12Se
lig, M
., 33
-APA-9
/FD-9
, 87-A
PA-20
, 114
-APA-2
6,
169
-APA-3
9/FD
-46Se
llers,
M.,
88-AP
A-21
Sema
an, R
., 88
-APA-2
1Se
mlits
ch, B
., 71
-FD-16
Sen,
S., 1
76-FD
-49Se
pka,
S., 7
8-TP-6
, 159
-TP-16
Serin
o, G.
, 102
-FD-25
Seum
e, J.,
24-G
T-1, 5
7-APA
-12, 1
21-CF
D-33
Shale
r, K.,
95-CF
D-24
Shan
g, J.,
43-C
FD-13
, 52-T
P-4Sh
aran,
N., 1
00-CF
D-29/
FD-23
Sharb
atdar,
M.,
149-C
FD-41
Sharm
a, A.,
22-F
D-6, 1
55-FD
-38Sh
atalov
, O.,
27-TP
-2Sh
aw, S
., 15
6-GT-5
Sheb
alin,
J., 7
6-PDL
-4Sh
eikh,
U., 5
3-TP-5
, 78-T
P-6, 1
34-TP
-13Sh
en, W
., 41
-CFD-1
1Sh
ende
, N.,
138-A
PA-29
Shen
g, C.,
8-AP
A-5, 6
1-APA
-16, 8
4-APA
-17Sh
epha
rd, M
., 14
-CFD-5
Shi, L
., 10
0-CFD
-29/F
D-23
Shi, Z
., 14
0-APA
-31Sh
ields
, M.,
169-A
PA-39
/FD-4
6Sh
ih, T.
, 120
-CFD-3
2Sh
ima,
E., 6
6-CFD
-17Sh
milov
ich, A
., 85
-APA-1
8/FD
-21Sh
neide
r, M.,
50-PD
L-2, 1
03-PD
L-6Sh
ort, E
., 13
4-TP-1
3Sh
yy, W
., 20
-FD-4,
33-A
PA-9/
FD-9
Silk,
E., 1
35-TP
-14Sil
va, A
., 44
-CFD-1
4Sim
, A.,
92-AS
E-7Sim
erly,
S., 1
56-GT
-5Sim
on, J
., 15
7-PDL
-10Sim
pson
, R.,
170-F
D-41/
GT-6
Singh
, S.,
71-FD
-16Sip
p, D.
, 72-F
D-17,
171
-FD-42
Siroh
i, J.,
103-P
DL-6
Sitara
man,
H., 7
6-PDL
-4Sit
arama
n, J.,
97-C
FD-26
, 112
-APA-2
4, 1
20-CF
D-32,
1
46-CF
D-38
Sivara
m, G
., 15
4-FD-3
7Sk
oogh
, D.,
31-AP
A-7/F
D-8Slo
tnick
, J.,
100-C
FD-29
/FD-2
3
86
Auth
or/S
essio
n Ch
air In
dex
Smith
, A.,
158-P
DL-11
/FD-3
9Sm
ith, W
., 12
3-CFD
-35Sn
yder,
D.,
123-C
FD-35
Solod
ovnik
ov, S
., 11
6-APA
-28So
mers,
D.,
5-APA
-2So
mmerw
erk, K
., 84
-APA-1
7So
ng, J
., 14
2-APA
-33/F
D-33
Sor, S
., 14
3-ASE
-9So
ragha
n, C.,
86-A
PA-19
Soria
, J.,
89-AP
A-22/
FD-22
Soud
akov
, V.,
102-F
D-25
Soze
r, E.,
15-CF
D-6, 3
4-APA
-10Sø
rense
n, J.,
41-C
FD-11
Søren
sen,
N., 4
1-CFD
-11Sp
alt, T
., 49
-GT-2
Sped
ding,
G., 7
5-FD-2
0Sp
eer, S
., 17
6-FD-4
9Sp
iegel,
S.,
144-C
FD-36
Spille
rs, R.
, 73-F
D-18,
171
-FD-42
, 175
-FD-48
Sree
nivas
, K.,
8-APA
-5, 1
05-TP
-9St
alnov
, O.,
164-A
PA-34
Stan
field,
S.,
73-FD
-18, 1
70-FD
-41/G
T-6, 1
75-FD
-48St
ariko
vskiy
, A.,
25-PD
L-1St
ead,
D., 4
9-GT-2
Stefa
ni, F.
, 132
-PDL-9
Step
hani,
K., 6
3-ASE
-5St
ephe
n, E.,
72-F
D-17
Stog
ner, R
., 38
-CFD-8
Stree
tt, C.
, 70-C
FD-21
/FD-1
5St
rike,
J., 1
29-FD
-32St
robl, T
., 36
-ASE-2
Struk
, P.,
62-AS
E-4Su
bbare
ddy,
P., 1
74-FD
-45Su
brahm
anya
m, P.
, 134
-TP-13
Such
omel,
C., 1
57-PD
L-10
Sun,
H., 1
4-CFD
-5, 1
48-CF
D-40
Sures
h, A.,
105
-TP-9
Surzh
ikov,
S., 2
7-TP-2
, 43-C
FD-13
, 52-T
P-4,
116
-APA-2
8, 1
33-TP
-12Su
tcliffe
, P.,
24-GT
-1Su
tton,
E., 6
3-ASE
-5Su
zen,
Y., 2
7-TP-2
Suzu
ki, K.
, 31-A
PA-7/
FD-8,
78-T
P-6, 1
06-TP
-10,
119
-CFD-3
1, 1
54-FD
-37, 1
57-PD
L-10,
175
-FD-48
Suzu
ki, T.
, 63-A
SE-5,
105
-TP-9,
135
-TP-14
Swetk
y, Z.,
36-A
SE-2
Sytsm
a, M.
, 33-A
PA-9/
FD-9
Szas
z, R.,
147
-CFD-3
9Ta
guch
i, H.,
59-AP
A-14
Taka
hash
i, M.,
59-AP
A-14
Taka
hash
i, T.,
104-P
DL-7
Taka
hash
i, Y.,
98-CF
D-27,
131
-PDL-8
Taka
tani, T
., 11
9-CFD
-31Ta
kaya
nagi,
H.,
27-TP
-2, 6
3-ASE
-5, 1
05-TP
-9,
126
-FD-29
Take
ichi, T
., 13
2-PDL
-9Ta
mada
, Y.,
104-P
DL-7
Tan,
C., 1
43-AS
E-9Ta
naka
, M.,
36-AS
E-2, 1
04-PD
L-7Ta
ng, H
., 89
-APA-2
2/FD
-22Ta
ni, T.
, 156
-GT-5
Tann
o, H.
, 126
-FD-29
Tarfe
ld, F.
, 138
-APA-2
9Ta
s, C.,
132
-PDL-9
Taun
k, J.,
77-P
DL-5
Tave
rnetti,
W.,
45-FD
-10Ta
y, W.
, 20-F
D-4Ta
ylor, J
., 12
5-FD-2
8Ta
ylor, L
., 8-A
PA-5,
105
-TP-9
Taylo
r, T.,
15-CF
D-6Te
cson,
L., 1
43-AS
E-9Te
ichel,
S.,
57-AP
A-12
Tema
m, R.
, 39-C
FD-9
Temb
ely, M
., 23
-FD-7
Tend
ero Ve
ntana
s, J.,
89-A
PA-22
/FD-2
2Te
ndulk
ar, S
., 14
-CFD-5
Terha
ar, S
., 45
-FD-10
, 121
-CFD-3
3Te
rraza
s-Sali
nas,
I., 1
59-TP
-16Te
zuka
, A.,
131-P
DL-8
Thak
ur, S
., 94
-CFD-2
3, 1
19-CF
D-31
Thala
kkott
or, J.
, 125
-FD-28
Theo
filis,
V., 1
9-FD-3
, 89-A
PA-22
/FD-2
2, 1
02-FD
-25,
126
-FD-29
, 128
-FD-31
Thiel
e, F.,
42-C
FD-12
, 75-F
D-20
Thiem
an, C
., 17
1-FD-4
2Th
omas
, S.,
97-CF
D-26,
166
-APA-3
6Th
omps
on, D
., 36
-ASE-2
, 146
-CFD-3
8Th
omps
on, P
., 96
-CFD-2
5Th
omps
on, R
., 13
2-PDL
-9Th
ordah
l, J.,
158-P
DL-11
/FD-3
9Th
urow,
B.,
17-FD
-1Tia
n, W.
, 86-A
PA-19
Tiems
in, P.
, 170
-FD-41
/GT-6
Timme
, S.,
97-CF
D-26
Timoth
ee, C
., 11
5-APA
-27/F
D-26
Titov
, E.,
63-AS
E-5Tiz
iano,
P., 8
8-APA
-21To
be, T
., 19
-FD-3
Tobin
g, S.
, 142
-APA-3
3/FD
-33To
gnac
cini, R
., 33
-APA-9
/FD-9
Toma
c, M.
, 21-F
D-5To
ng, X
., 36
-ASE-2
Toom
er, C.
, 90-A
PA-23
Toro
Salaz
ar, C.
, 170
-FD-41
/GT-6
Toyo
da, A
., 59
-APA-1
4Tra
n, L.,
133
-TP-12
Trepa
nier, J
., 30
-APA-6
Tretya
kov,
P., 7
7-PDL
-5Tri
phah
n, C.,
36-A
SE-2
Tropp
, J.,
22-FD
-6Tsa
i, M.,
37-AS
E-3Tsa
o, J.,
62-A
SE-4,
91-A
SE-6
Tsubo
kura,
M.,
69-CF
D-20,
140
-APA-3
1Tsu
da, S
., 15
2-FD-3
5Tu
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124-F
D-27
Tu, S
., 76
-PDL-4
Tuck
er, A.
, 116
-APA-2
8Tu
fts, M
., 7-A
PA-4
Tulin
g, S.
, 90-A
PA-23
Tumi
n, A.,
102
-FD-25
Tuo,
W., 6
-APA-3
Tupik
in, A.
, 77-P
DL-5
Tupp
er, A.
, 9-AS
E-1Tu
ttle, S
., 22
-FD-6
Tyan
, M.,
67-CF
D-18
Ukeil
ey, L
., 33
-APA-9
/FD-9
Ulbric
h, N.
, 130
-GT-4
Unal,
M.,
20-FD
-4Up
adhy
ay, P
., 21
-FD-5
Usha
kov,
N., 4
4-CFD
-14Va
chon
, N.,
101-F
D-24
Vakil
i, A.,
171-F
D-42
Valle
t, I.,
10-C
FD-1
Van A
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J., 1
30-GT
-4va
n Berk
el, E.
, 86-A
PA-19
Van D
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., 86
-APA-1
9va
n der
Vorst
, J.,
147-C
FD-39
Van L
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., 64
-CFD-1
5Va
n Muij
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J., 1
47-CF
D-39
van O
udhe
usde
n, B.
, 20-F
D-4va
n Sch
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stein
Lantm
an, M
., 96
-CFD-2
5Va
n Zan
te, J.
, 62-A
SE-4
Vand
en, K
., 34
-APA-1
0, 1
13-AP
A-25
Vane
, Z.,
175-F
D-48
Vans
tone,
L., 7
2-FD-1
7Va
radan
, S.,
144-C
FD-36
Varga
s, M.
, 143
-ASE-9
Veldh
uis, L
., 86
-APA-1
9, 1
67-AP
A-37/
FD-40
Venk
atach
ari, B
., 59
-APA-1
4, 1
45-CF
D-37
Venk
ataram
ani, K
., 62
-ASE-4
Venk
atesh
an, S
., 15
9-TP-1
6Ve
rbeck
e, C.,
5-AP
A-2Ve
rdieri
Nue
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, G.,
26-TP
-1Ve
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., 62
-ASE-4
Verho
ff, A.
, 160
-TP-17
Verm
eersc
h, O.
, 88-A
PA-21
Verm
eire,
B., 6
4-CFD
-15Ve
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J., 9
-ASE-1
Verst
raete,
T., 5
7-APA
-12Vé
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., 14
8-CFD
-40Vie
ira, R
., 13
8-APA
-29Vig
noles
, G.,
78-TP
-6Vil
lafañ
e, L.,
71-F
D-16
Villag
ran M
uñiz,
M.,
170-F
D-41/
GT-6
Villed
ie, N
., 43
-CFD-1
3Vil
ledieu
, P.,
62-AS
E-4, 9
1-ASE
-6, 1
17-AS
E-8Vin
cent,
P., 3
9-CFD
-9Vin
okur,
M.,
160-T
P-17
Visba
l, M., 4
7-FD-1
2, 7
4-FD-1
9/PD
L-3, 1
18-CF
D-30,
4
2-APA
-33/F
D-33,
153-F
D-36,
158-P
DL-11
/FD-3
9,
172
-FD-43
Visse
r, K.,
123-C
FD-35
Vivian
i, A.,
79-TP
-7vo
n Dee
tzen,
S., 1
16-AP
A-28
Vorob
iev, A
., 24
-GT-1
Vu, B
., 34
-APA-1
0, 4
4-CFD
-14Vu
kasin
ovic,
B.,
154-F
D-37
Vuori
nen,
V., 6
8-CFD
-19Vy
maza
l, M.,
43-CF
D-13
Wach
tor, A
., 17
4-FD-4
5Wa
dham
s, T.,
94-C
FD-23
Wagn
er, J.
, 171
-FD-42
Wagn
ild, R
., 73
-FD-18
, 160
-TP-17
Wahl,
T., 1
51-FD
-34Wa
hls, R
., 7-A
PA-4,
138
-APA-2
9Wa
itz, T
., 11
6-APA
-28Wa
ldman
, R.,
172-F
D-43
Wall,
W., 9
7-CFD
-26Wa
llin, S
., 31
-APA-7
/FD-8
Wang
, C.,
33-AP
A-9/F
D-9, 6
0-APA
-15/F
D-14
Wang
, G.,
146-C
FD-38
Wang
, J.,
11-CF
D-2, 8
4-APA
-17, 9
2-ASE
-7Wa
ng, L
., 40
-CFD-1
0, 9
3-CFD
-22Wa
ng, P
., 50
-PDL-2
Wang
, Q.,
96-CF
D-25
Wang
, S.,
11-CF
D-2Wa
ng, X
., 98
-CFD-2
7, 1
27-FD
-30, 1
45-CF
D-37
Wang
, Y.,
74-FD
-19/P
DL-3
Wang
, Z.,
39-CF
D-9, 6
0-APA
-15/F
D-14,
64-C
FD-15
, 9
6-CFD
-25, 1
00-CF
D-29/
FD-23
, 118
-CFD-3
0,
129
-FD-32
, 172
-FD-43
Ward,
C., 7
3-FD-1
8Wa
tanab
e, H.
, 104
-PDL-7
Watan
abe,
Y., 7
8-TP-6
, 131
-PDL-8
, 157
-PDL-1
0Wa
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87-AP
A-20
Wawr
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, K.,
172-F
D-43
Weav
er, A.
, 80-T
P-8We
aver,
M.,
134-T
P-13
Webs
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., 10
5-TP-9
Weisb
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J., 5
3-TP-5
Weiss
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123-C
FD-35
Weiss
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32-AP
A-8We
ng, H
., 51
-TP-3
West,
D.,
116-A
PA-28
Wha
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., 75
-FD-20
, 85-A
PA-18
/FD-2
1W
hitak
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., 23
-FD-7
Whit
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19-F
D-3, 8
6-APA
-19, 1
53-FD
-36W
hite,
J., 3
8-CFD
-8W
hite,
M., 1
04-PD
L-7, 1
58-PD
L-11/
FD-39
Whit
e, T.,
79-T
P-7W
iberg,
B.,
91-AS
E-6W
ichma
nn, K
., 97
-CFD-2
6W
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., 11
4-APA
-26W
ieben
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., 53
-TP-5
Willi
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B., 9
9-CFD
-28W
illiam
s, D.
, 93-C
FD-22
, 128
-FD-31
Willi
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G., 5
0-PDL
-2W
illiam
s, J.,
63-A
SE-5
Willi
ams,
W., 1
34-TP
-13W
illiam
schen
, M.,
14-CF
D-5W
illis,
D., 5
7-APA
-12, 6
0-APA
-15/F
D-14
Wilso
n, A.,
132
-PDL-9
Wind
iate,
S., 3
4-APA
-10W
inkler
, C.,
95-CF
D-24,
147
-CFD-3
9W
inoto,
S.,
33-AP
A-9/F
D-9W
inter,
M.,
134-T
P-13
Winz
en, A
., 33
-APA-9
/FD-9
Wirth
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112-A
PA-24
Wiss
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., 13
-CFD-4
, 146
-CFD-3
8W
ittich
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158-P
DL-11
/FD-3
9Wo
hl, C.
, 170
-FD-41
/GT-6
Wolf,
W., 1
13-AP
A-25
Wong
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60-AP
A-15/
FD-14
, 117
-ASE-8
Wong
suryr
at, N
., 13
2-PDL
-9Wo
o, G.
, 71-F
D-16
Wood
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38-CF
D-8, 1
60-TP
-17Wo
odard
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91-AS
E-6Wo
odruf
f, S.
, 47-F
D-12,
70-C
FD-21
/FD-1
5Wo
open
, M.,
118-C
FD-30
Wosz
idlo,
R., 6
7-CFD
-18, 1
48-CF
D-40
Wray
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12-CF
D-3, 7
9-TP-7
, 159
-TP-16
Wray
, T.,
174-F
D-45
Wren
n, M.
, 49-G
T-2W
right,
J., 9
4-CFD
-23W
u, C.,
31-A
PA-7/
FD-8
Wu,
M., 4
7-FD-1
2W
u, S.
, 76-P
DL-4
Wu,
X., 1
9-FD-3
Wu,
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