final program - american institute of aeronautics and astronautics

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FINAL PROGRAM www.aiaa.org/sandiego2013 #aiaaFluids 24–27 June 2013 San Diego, California Sheraton San Diego Hotel & Marina 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 AIAA Ground Testing Conference

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Page 1: FINAL PROGRAM - American Institute of Aeronautics and Astronautics

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

Page 2: FINAL PROGRAM - American Institute of Aeronautics and Astronautics

Compatible with iPhone/iPad, Android, and

BlackBerry!

GET YOUR CONFERENCE INFO ON THE GO!

Download the FREE AIAA 2013 Conference Mobile App

FEATURES• Browse Program – View the program at your fi ngertips• My Itinerary – Create your own conference schedule• Conference Info – Including special events• Take Notes – Take notes during sessions• City Map – See the surrounding area and Sheraton San Diego Hotel• Connect to Twitter – Tweet about what you’re doing and who you’re meeting with

#aiaaFluids

HOW TO DOWNLOADAny version can be run without an active Internet connection! You can also sync an itinerary you created online with the app by entering your unique itinerary name.

MyItinerary Web App

• For optimal use, we recommend: s iPhone 3GS, iPod Touch (3rd

generation), iPad iOS 4.0, or later s Most mobile devices using Android

2.2 or later with the default browser s BlackBerry Torch or later device

using BlackBerry OS 7.0 with the default browser

• Download the MyItinerary app by scanning the QR code or accessing http://download.abstractcentral.com/aiaa-mfd13/index.htm

• Once downloaded, you can bookmark the site to access it later or add a link to your home screen.

13-0345

MyItinerary Mobile App

• For optimal use, we recommendiPhone 3GS, iPod Touch (3rd generation), iPad iOS 4.0, or later

• Download the MyItinerary app by searching for “ScholarOne” in the App Store directly from your mobile device. Or, access the link below or scan the QR code to access the iTunes page for the app. http://itunes.apple.com/us/app/scholarone-my-itinerary/id497884329?mt=8

• Select the meeting “AIAA Summer Fluids Conferences”

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www.facebook.com/AIAAfan

www.linkedin.com/company/AIAA

@aiaa#aiaaFluids

www.flickr.com/aiaaevents

www.youtube.com/wwwaiaaorg

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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Harbor Island Ballroom III & Foyer

9-10x10 booths, 12-6x2 tablesCeiling height 18' max.Aisle widths as noted

Rev. 5/29/13

MARINA ROOMS MARINA ROOMS

MARINA TOWER - FIRST FLOOR

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GRANDEBALLROOM

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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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!

Page 12: FINAL PROGRAM - American Institute of Aeronautics and Astronautics

12–14 AUGUST 2013 LOS ANGELES, CALIFORNIA

CHARTING THE FUTURE

OF FLIGHT

Premier Sponsor

REGISTER TODAY!www.aiaa.org/aviation2013#aiaaAviation

13-0316

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.

Page 13: FINAL PROGRAM - American Institute of Aeronautics and Astronautics

11

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

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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

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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

Page 16: FINAL PROGRAM - American Institute of Aeronautics and Astronautics

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

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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

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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

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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

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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

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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

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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

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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

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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

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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

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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

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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

Page 28: FINAL PROGRAM - American Institute of Aeronautics and Astronautics

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

Page 29: FINAL PROGRAM - American Institute of Aeronautics and Astronautics

Mond

ay

Mond

ay, 2

4 Ju

ne 2

013

1-NB

-1

0700

- 08

00 h

rsMo

nday

Mor

ning N

etwor

king B

reak

fast

Naut

ilus a

nd H

arbo

r Isl

and F

oyer

s

Mond

ay, 2

4 Ju

ne 2

013

2-SB

-1

0730

- 08

00 h

rsMo

nday

Mor

ning S

peak

ers’

Briefi

ngSe

ssion

Roo

ms

Mond

ay, 2

4 Ju

ne 2

013

3-PL

NRY-1

08

00 -

0900

hrs

Open

ing P

lenar

y Ses

sion

Harb

or B

allro

om I

and I

I

Aeron

autic

s in t

he Vi

rtual

Age

Denn

is M.

Bus

hnell

Chief

Scie

ntist,

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

 

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

Page 30: FINAL PROGRAM - American Institute of Aeronautics and Astronautics

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

Page 31: FINAL PROGRAM - American Institute of Aeronautics and Astronautics

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

Page 32: FINAL PROGRAM - American Institute of Aeronautics and Astronautics

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

Page 33: FINAL PROGRAM - American Institute of Aeronautics and Astronautics

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

Page 34: FINAL PROGRAM - American Institute of Aeronautics and Astronautics

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

Page 35: FINAL PROGRAM - American Institute of Aeronautics and Astronautics

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

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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

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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

Page 38: FINAL PROGRAM - American Institute of Aeronautics and Astronautics

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

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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

Page 40: FINAL PROGRAM - American Institute of Aeronautics and Astronautics

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

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

Page 41: FINAL PROGRAM - American Institute of Aeronautics and Astronautics

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

Page 42: FINAL PROGRAM - American Institute of Aeronautics and Astronautics

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

Page 43: FINAL PROGRAM - American Institute of Aeronautics and Astronautics

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

Page 44: FINAL PROGRAM - American Institute of Aeronautics and Astronautics

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

Page 45: FINAL PROGRAM - American Institute of Aeronautics and Astronautics

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

Page 46: FINAL PROGRAM - American Institute of Aeronautics and Astronautics

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

Page 47: FINAL PROGRAM - American Institute of Aeronautics and Astronautics

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

Page 48: FINAL PROGRAM - American Institute of Aeronautics and Astronautics

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

Page 49: FINAL PROGRAM - American Institute of Aeronautics and Astronautics

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

Page 50: FINAL PROGRAM - American Institute of Aeronautics and Astronautics

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

Page 51: FINAL PROGRAM - American Institute of Aeronautics and Astronautics

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

Page 52: FINAL PROGRAM - American Institute of Aeronautics and Astronautics

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

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

Page 53: FINAL PROGRAM - American Institute of Aeronautics and Astronautics

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

Page 54: FINAL PROGRAM - American Institute of Aeronautics and Astronautics

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

Page 55: FINAL PROGRAM - American Institute of Aeronautics and Astronautics

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

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

Page 56: FINAL PROGRAM - American Institute of Aeronautics and Astronautics

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

Page 57: FINAL PROGRAM - American Institute of Aeronautics and Astronautics

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

Page 58: FINAL PROGRAM - American Institute of Aeronautics and Astronautics

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

Page 59: FINAL PROGRAM - American Institute of Aeronautics and Astronautics

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

Page 60: FINAL PROGRAM - American Institute of Aeronautics and Astronautics

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

Page 61: FINAL PROGRAM - American Institute of Aeronautics and Astronautics

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

Page 62: FINAL PROGRAM - American Institute of Aeronautics and Astronautics

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

Page 63: FINAL PROGRAM - American Institute of Aeronautics and Astronautics

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

Page 64: FINAL PROGRAM - American Institute of Aeronautics and Astronautics

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

Page 65: FINAL PROGRAM - American Institute of Aeronautics and Astronautics

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

xing

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

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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

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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

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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

Page 69: FINAL PROGRAM - American Institute of Aeronautics and Astronautics

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

Page 70: FINAL PROGRAM - American Institute of Aeronautics and Astronautics

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

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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

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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

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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

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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

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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

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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

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Wedn

esda

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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

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sday

Thur

sday

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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

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201

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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

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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

Page 81: FINAL PROGRAM - American Institute of Aeronautics and Astronautics

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

Page 82: FINAL PROGRAM - American Institute of Aeronautics and Astronautics

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

Page 83: FINAL PROGRAM - American Institute of Aeronautics and Astronautics

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

Page 84: FINAL PROGRAM - American Institute of Aeronautics and Astronautics

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

Page 85: FINAL PROGRAM - American Institute of Aeronautics and Astronautics

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

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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

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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,

R., 2

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

hamm

adi, B

., 42

-CFD-1

2Mo

hamm

adi, M

., 23

-FD-7

Mohs

eni, K

., 22

-FD-6,

89-A

PA-22

/FD-2

2, 1

01-FD

-24,

124

-FD-27

, 125

-FD-28

, 169

-APA-3

9/FD

-46Mo

in, P.

, 70-C

FD-21

/FD-1

5Mo

ini-Ye

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

, J.,

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

y, J.,

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

chka

, Y.,

52-TP

-4My

ong,

R., 4

1-CFD

-11Na

daraj

ah, S

., 57

-APA-1

2, 6

4-CFD

-15, 1

12-AP

A-24

Naga

ppan

, N.,

16-CF

D-7Na

gata,

Y., 1

31-PD

L-8Na

idu, V

., 14

2-APA

-33/F

D-33

Nair,

A., 1

44-CF

D-36

Naito

, H.,

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

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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

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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

, J.,

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

ken,

J., 1

30-GT

-4va

n Berk

el, E.

, 86-A

PA-19

Van D

am, C

., 86

-APA-1

9va

n der

Vorst

, J.,

147-C

FD-39

Van L

eer, B

., 64

-CFD-1

5Va

n Muij

den,

J., 1

47-CF

D-39

van O

udhe

usde

n, B.

, 20-F

D-4va

n Sch

rojen

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

rnberg

, G.,

26-TP

-1Ve

res, J

., 62

-ASE-4

Verho

ff, A.

, 160

-TP-17

Verm

eersc

h, O.

, 88-A

PA-21

Verm

eire,

B., 6

4-CFD

-15Ve

rnier,

J., 9

-ASE-1

Verst

raete,

T., 5

7-APA

-12Vé

tel, J

., 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,

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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.,

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D-2, 8

4-APA

-17, 9

2-ASE

-7Wa

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., 40

-CFD-1

0, 9

3-CFD

-22Wa

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., 50

-PDL-2

Wang

, Q.,

96-CF

D-25

Wang

, S.,

11-CF

D-2Wa

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., 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,

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3-FD-1

8Wa

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e, H.

, 104

-PDL-7

Watan

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8-TP-6

, 131

-PDL-8

, 157

-PDL-1

0Wa

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, N.,

87-AP

A-20

Wawr

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, K.,

172-F

D-43

Weav

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, 80-T

P-8We

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134-T

P-13

Webs

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., 10

5-TP-9

Weisb

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3-TP-5

Weiss

, J.,

123-C

FD-35

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A-8We

ng, H

., 51

-TP-3

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116-A

PA-28

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., 75

-FD-20

, 85-A

PA-18

/FD-2

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., 23

-FD-7

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6-APA

-19, 1

53-FD

-36W

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8-CFD

-8W

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M., 1

04-PD

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58-PD

L-11/

FD-39

Whit

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79-T

P-7W

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91-AS

E-6W

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., 97

-CFD-2

6W

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., 11

4-APA

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., 53

-TP-5

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9-CFD

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, 93-C

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, 128

-FD-31

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0-PDL

-2W

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63-A

SE-5

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34-TP

-13W

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, M.,

14-CF

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7-APA

-12, 6

0-APA

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D-14

Wilso

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132

-PDL-9

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., 33

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., 13

-CFD-4

, 146

-CFD-3

8W

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/FD-3

9Wo

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, 170

-FD-41

/GT-6

Wolf,

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13-AP

A-25

Wong

, J.,

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FD-14

, 117

-ASE-8

Wong

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at, N

., 13

2-PDL

-9Wo

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, 71-F

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60-TP

-17Wo

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91-AS

E-6Wo

odruf

f, S.

, 47-F

D-12,

70-C

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/FD-1

5Wo

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, M.,

118-C

FD-30

Wosz

idlo,

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7-CFD

-18, 1

48-CF

D-40

Wray

, A.,

12-CF

D-3, 7

9-TP-7

, 159

-TP-16

Wray

, T.,

174-F

D-45

Wren

n, M.

, 49-G

T-2W

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J., 9

4-CFD

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PA-7/

FD-8

Wu,

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7-FD-1

2W

u, S.

, 76-P

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or/S

essio

n Ch

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dex

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, 11-C

FD-2

Wys

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PA-30

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., 6-A

PA-3

Xia, X

., 89

-APA-2

2/FD

-22Xia

, Y.,

144-C

FD-36

Xiao,

Z., 1

53-FD

-36Xia

obo,

L., 1

67-AP

A-37/

FD-40

Xie, K

., 63

-ASE-5

Xiong

, J.,

123-C

FD-35

, 138

-APA-2

9, 1

75-FD

-48Xis

to, C.

, 50-P

DL-2

Yadli

n, Y.,

85-A

PA-18

/FD-2

1Ya

keno

, A.,

75-FD

-20Ya

khina

, G.,

133-T

P-12

Yalim

, S.,

43-CF

D-13

Yalin

, A.,

50-PD

L-2, 7

7-PDL

-5, 1

32-PD

L-9Ya

mada

, G.,

31-AP

A-7/F

D-8Ya

mada

, H.,

20-FD

-4Ya

mada

, K.,

131-P

DL-8

Yama

da, T

., 12

6-FD-2

9Ya

mada

, Y.,

106-T

P-10

Yama

guch

i, T.,

132-P

DL-9

Yama

leev,

N., 2

0-FD-4

Yama

moto,

K., 6

8-CFD

-19Ya

mauc

hi, G

., 88

-APA-2

1, 1

66-AP

A-36

Yama

zaki,

W.,

20-FD

-4Ya

n, W.

, 25-P

DL-1

Yang

, S.,

75-FD

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6-CFD

-25Ya

ng, X

., 26

-TP-1

Yang

, Z.,

6-APA

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-APA-5

, 140

-APA-3

1Ya

no, M

., 10

0-CFD

-29/F

D-23

yao,

W., 1

24-FD

-27Ya

rantse

v, D.

, 77-P

DL-5,

154

-FD-37

Yarus

evyc

h, S.

, 89-A

PA-22

/FD-2

2Ya

suok

a, K.,

87-A

PA-20

Ye, Z

., 6-A

PA-3,

146

-CFD-3

8Ye

e, H.

, 12-C

FD-3

Yee,

K., 5

8-APA

-13Ye

e, P.,

133

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Yen,

C., 1

45-CF

D-37

Yen,

J., 1

67-AP

A-37/

FD-40

Yeo,

K., 2

0-FD-4

, 47-F

D-12

Yi, S

., 32

-APA-8

Yin, B

., 16

-CFD-7

Yode

r, D.,

70-CF

D-21/

FD-15

Youn

g, J.,

142

-APA-3

3/FD

-33Yu

, H.,

129-F

D-32

Yu, K

., 15

2-FD-3

5Yu

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60-AP

A-15/

FD-14

, 164

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4Yu

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145-C

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Yu Ch

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., 89

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2/FD

-22Yu

an, W

., 86

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9Yu

e, H.

, 86-A

PA-19

Yumu

sak,

M., 4

1-CFD

-11, 6

5-CFD

-16/G

T-3,

66-C

FD-17

, 96-C

FD-25

Zahr,

M.,

15-CF

D-6, 6

4-CFD

-15, 9

6-CFD

-25Za

ide, D

., 66

-CFD-1

7Za

laman

sky,

G., 6

2-ASE

-4Za

myati

n, A.,

37-A

SE-3

Zank

er, A.

, 164

-APA-3

4Za

re-be

htash

, H.,

103-P

DL-6

Zave

levich

, F.,

44-CF

D-14

Zeng

, X.,

41-CF

D-11

Zerbi

nati,

A., 5

7-APA

-12Ze

une,

C., 1

14-AP

A-26

Zha,

G., 3

1-APA

-7/FD

-8, 3

2-APA

-8, 5

9-APA

-14Zh

ang,

B., 7

4-FD-1

9/PD

L-3Zh

ang,

F., 1

8-FD-2

, 84-A

PA-17

Zhan

g, W.

, 6-AP

A-3, 1

67-AP

A-37/

FD-40

Zhan

g, X.

, 20-F

D-4, 3

4-APA

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64-AP

A-34

Zhan

g, Y.,

45-F

D-10,

166

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6Zh

ang,

Z., 6

-APA-3

, 65-C

FD-16

/GT-3

, 96-C

FD-25

, 1

21-CF

D-33,

135

-TP-14

, 145

-CFD-3

7, 1

50-CF

D-42

Zhao

, Q.,

84-AP

A-17

Zhao

, X.,

116-A

PA-28

Zhao

, Z.,

138-A

PA-29

Zhela

nniko

v, A.,

37-A

SE-3

Zhen

g, B.

, 74-F

D-19/

PDL-3

Zhen

g, Y.,

154

-FD-37

, 172

-FD-43

Zhen

g, Z.,

37-A

SE-3

Zhon

g, X.

, 73-F

D-18,

127

-FD-30

Zhou

, C.,

64-CF

D-15

Zhou

, S.,

6-APA

-3, 1

03-PD

L-6Zh

u, T.,

80-T

P-8Zh

uang

, Y.,

104-P

DL-7

Ziche

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, B.,

59-AP

A-14

Zimme

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64-CF

D-15,

118

-CFD-3

0Zin

gg, D

., 7-A

PA-4,

30-A

PA-6,

39-C

FD-9,

40-C

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, 4

2-CFD

-12, 9

3-CFD

-22, 9

6-CFD

-25, 1

19-CF

D-31

Zito,

J., 2

5-PDL

-1, 7

8-TP-6

Zope

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58-AP

A-13

Zudo

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77-P

DL-5

Zuev

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88

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