Distinguished lecturers to speak at 48TH AIAA Ae 14/10/2011

Public release date: 29-Oct-2009 [ | E-mail | Share ] Contact: Duane Hyland [email protected] 703-264-7558 American Institute of Aeronautics and Astronautics

Distinguished lecturers to speak at 48TH AIAA Aerospace Sciences Meeting and Exposition

October 28, 2009 – Reston, Va. – The American Institute of Aeronautics and Astronautics (AIAA) is pleased to announce that a series of distinguished lectures will be presented at the 48th AIAA Aerospace Sciences Meeting and Exposition, January 4��, 2010, at the Orlando World Center Marriott, Orlando, Fla.

Dr. Ian Poll, professor of aerospace engineering at Cranfield University, Bedfordshire, United Kingdom, will present the AIAA Dryden Lectureship in Research on Monday, January 4, at 5:30 p.m. The title of Dr. Poll's lecture is: "Potential for the Minimization of Aviation's Impact on the Environment." The Dryden Lectureship in Research honors Dr. Hugh L. Dryden, former director of the National Advisory Committee for Aeronautics, and a renowned proponent of the value of research programs to aerospace. Given annually, the lecture emphasizes the importance of basic research to the advancement of aeronautics and astronautics.

Dr. N. Albert Moussa, president of BlazeTech Corporation, Cambridge, Mass., will present the SAE/AIAA William Littlewood Memorial Lecture on Tuesday, January 5, at 5:30 p.m. The title of Dr. Moussa's lecture is: "Aircraft Fire and Explosion Protection." The William Littlewood Memorial Lecture honors William Littlewood, the only person to be president of both AIAA and SAE, and a renowned contributor to the design of, and operational requirements for, civil transport aircraft. This biennial lecture is presented to advance air transport engineering and to recognize those who make contributions to that field.

Col. Eileen M. Collins, United States Air Force, retired, a former NASA astronaut, will present the AIAA von Kármán Lectureship in Astronautics, on Wednesday, January 6, at 5:30 p.m. The title of Col. Collins' lecture is: "Human Spaceflight Success in Space Science and Human Exploration." The von Kármán Lectureship in Astronautics honors Theodore von Kármán, a world famous authority on aerospace sciences. The lectureship is given each year by an individual who has performed notably and distinguished himself or herself technically in the field of astronautics.

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For more information on the distinguished lectures, or on the AIAA Honors and Awards program, please contact Carol Stewart at [email protected] or 703.264.7623.

For more information on the 48th Aerospace Sciences Meeting, please contact Duane Hyland at [email protected] or 703.264.7558. Registration information can be found at www.aiaa.org/events/asm. Registration is free for credentialed members of the press.

AIAA is the world's largest technical society dedicated to the global aerospace profession. With more than 35,000 individual members worldwide, and 90 corporate members, AIAA brings together industry, academia, and government to advance engineering and science in aviation, space, and defense. For more information, visit http://www.aiaa.org/.

American Institute of Aeronautics and Astronautics 1801 Alexander Bell Drive, Suite 500, Reston, VA 20191-4344 Phone: 703.264.7558 Fax: 703.264.7551 http://www.aiaa.org/

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48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition 4 - 7 Jan 2010 Orlando World Center Marriott Orlando, Florida

Monday Morning / 04 January 2010 0800 - 1200 NASA Aeronautics Research: Then and Now Crystal Ballroom J2

Monday Morning / 04 January 2010 Session 1-AA-1 Airfoil & Airframe Noise Denver

Session Co-Chairs:Dr. Jaiwon Shin, Associate Administrator, Aeronautics Research Mission Directorate (ARMD), NASA Ms. Jean Wolfe, Deputy Director, Integrated Systems Research Program (ISRP), ARMD, NASA

0800-0900X-15: To the Edge of SpaceJoe Engle, Retired U.S. Air Force Major General, Former Space Shuttle Astronaut and X-15 Test Pilot

0900-0930NASA Aeronautics UpdateDr. Jaiwon Shin, Associate Administrator, Aeronautics Research Mission Directorate NASA

0930-1000 Overview of NASA’s Integrated Systems Research Program (ISRP)Ms. Jean Wolfe, Deputy Director, Integrated Systems Research Program (ISRP), ARMD, NASA

1000-1030 Overview of NASA’s Environmentally Responsible Aviation (ERA) ProjectDr. Fayette Collier, Project Manager, Environmentally Responsible Aviation (ERA) Project, NASA

1030-1100 NASA’s Current Plans for ERA Airframe TechnologyAnthony Washburn, Project Engineer (Acting), Airframe Technology Sub-Project for ERA, NASA

1100-1130 NASA’s Current Plans for ERA Propulsion TechnologyDr. Jim Heidmann, Project Engineer (Acting), Propulsion Technology Sub-Project for ERA, NASA

1130-1200NASA’s Current Plans for ERA Vehicle Systems IntegrationSteve Smith, Project Engineer (Acting), Vehicle Systems Integration Sub-Project for ERA, NASA

Chaired by: M. WANG, University of Notre Dame, Notre Dame, IN0800AIAA-2010-0006 Aeroacoustics ofTurbulent Boundary-Layer Flow over SmallSteps

M. Ji, University of NotreDame, Notre Dame, IN

0830AIAA-2010-0007 Characteristics ofSeparated Flow SurfacePressure Fluctuations onan Axisymmetric Bump

G. Byun, VirginiaPolytechnic Institute andState University,Blacksburg, VA

0900AIAA-2010-0008 The near field pressureof a small- scale rotorduring hover.

J. Stephenson,University of Texas,Austin, Austin, TX

0930AIAA-2010-0010 Investigation of Near-Field Flow UnsteadinessAround a NACA0012Wingtip Using Large-Eddy- SimulationApproach

T. Imamura, JapanAerospace ExplorationAgency (JAXA), Chofu,Japan

1000AIAA-2010-0011 Flyover NoiseMeasurements of aSpiraling NoiseAbatement ApproachProcedure

L. Bertsch, GermanAerospace Center(DLR), Braunschweig,Germany

1030AIAA-2010-0012 Vortex- SheddingInduced Trailing- EdgeAcoustics

U. Svennberg, SwedishDefence ResearchAgency, Stockholm,Sweden

Monday Morning / 04 January 2010 Session 2-AA-2 Jet Noise Suppression I Tampa

Monday Morning / 04 January 2010 Session 3-AA-3 Turbomachinery, Core, and Combustion Noise Washington

Monday Morning / 04 January 2010 Session 4-ABP-1 NPARC Alliance/Wind-US Code Crystal Ballroom D

Due to formatting reasons, this version of the program lists only the first contributing author of each meeting paper. For a complete and up-to-date listing, please visit: http://www.aiaa.org/agenda.cfm?lumeetingid=1812&dateget=all#session12805.

Chaired by: M. SAMIMY, Ohio State University, Columbus, OH0800AIAA-2010-0013 Noise Control of HighReynolds Number Mach1.3 Heated Jet UsingPlasma Actuators

M. Kearney-Fischer,Ohio State University,Columbus, OH

0830AIAA-2010-0014 Assessment of NoiseReduction Concepts forFighter AircraftApplication in SimulatedForward Flight

K. Viswanathan, TheBoeing Company,Seattle, WA

0900AIAA-2010-0015 Development ofReduced- Order Modelsfor Feedback Control ofAxisymmetric Jets

A. Sinha, Ohio StateUniversity, Columbus,OH

0930AIAA-2010-0016 Large- ScaleSimulations of AcousticSynthetic Jets

M. Mankbadi,Embry-RiddleAeronautical University,Daytona Beach, FL

1000AIAA-2010-0017 Jet Noise SuppressionUsing UltrasonicPowered ResonanceTubes

K. Chaudhari, IllinoisInstitute of Technology,Chicago, IL

1030AIAA-2010-0018 Unsteady NumericalSimulation of a RoundJet with ImpingingMicrojets for NoiseSuppresion

P. Lew, McGillUniversity, Montréal,Canada

Chaired by: J. MILES, NASA Glenn Research Center, Cleveland, OH0800AIAA-2010-0019 Separating Direct andIndirect Turbofan EngineCombustion NoiseUsing the CorrelationFunction

J. Miles, NASA GlennResearch Center,Cleveland, OH

0830AIAA-2010-0021 Gas Turbine SingleAnnular CombustorSector: CombustionDynamics

J. Cai, University ofCincinnati, Cincinnati,OH

0900AIAA-2010-0022 Proper OrthogonalDecomposition andFourier Analysis on theEnergy Release RateDynamics

F. Ichihashi, Universityof Cincinnati, Cincinnati,OH

0930AIAA-2010-0024 Numerical Analysis ofStability of Thermo-Acoustic Oscillation in a2- D Closed Tube

M. Ishigaki, NagoyaUniversity, Nagoya,Japan

1000AIAA-2010-0026 Formulation ofCombustion AcousticCoupling using MultipleTime and Length Scales

C. Balaji, Indian Instituteof Technology, Madras,Chennai, India

1030AIAA-2010-0025 Modeling NonlinearThermoacousticInstability in anElectrically Heated RijkeTube

S. Mariappan, IndianInstitute of Technology,Madras, Chennai, India

Chaired by: A. CARY, The Boeing Company, St Louis, MO, and C. NELSON, Innovative Technology Applications Company, Lynnwood, WA0800AIAA-2010-0027 An Overview of theNPARC Alliance's Wind-US Flow Solver

C. Nelson, InnovativeTechnology ApplicationsCompany, Lynnwood,WA

0830AIAA-2010-0028 Unstructured GridSolution Accuracy andMesh Dependency

A. Cary, The BoeingCompany, St. Louis, MO

0900AIAA-2010-0030 Finite Rate ChemistryImplementation andValidation forUnstructured Grids

A. Dorgan, The BoeingCompany, St. Louis, MO

0930AIAA-2010-0031 A Modular ConjugateHeat Transfer Capabilityfor the Wind- US CFDCode

E. Perrell, Embry-RiddleAeronautical University,Daytona Beach, FL

1000AIAA-2010-0032 Modeling VortexGenerators in the Wind-US Code

J. Dudek, NASA GlennResearch Center,Cleveland, OH

1030AIAA-2010-0033 CFD Models of aSerpentine Inlet, Fan,and Nozzle

R. Chima, NASA GlennResearch Center,Cleveland, OH

Chaired by: P. WILLIAMS-HAYES, NASA Dryden Flight Research Center, Barstow, CA, and A. CRASSIDIS, Rochester Institute of Technology, Rochester, NY0800 0830 0900 0930 1000 1030 1100

http://www.aiaa.org/agenda.cfm?lumeetingid=1812&dateget=all#session12805

Monday Morning / 04 January 2010 Session 5-AFM-1 Aerodynamic Prediction Methods Chicago

Monday Morning / 04 January 2010 Session 6-AMT-1 Shear Stress Measurement Technology I Crystal Ballroom J1

Monday Morning / 04 January 2010 Session 7-APA-1 Aerodynamic-Structural Dynamics Interaction Grand Ballroom 9


Chaired by: P. WILLIAMS-HAYES, NASA Dryden Flight Research Center, Barstow, CA, and A. CRASSIDIS, Rochester Institute of Technology, Rochester, NY0800AIAA-2010-0034 Introducing a CombinedEquation/Output ErrorApproach in ParameterEstimation

E. Ozger, EADS MilitaryAir Systems, Manching,Germany

0830AIAA-2010-0035 An Aeroelastic FlexibleWing Model for AircraftSimulation

S. Andrews, CranfieldUniversity, Cranfield,Great Britain

0900AIAA-2010-0036 Modeling of HelicopterSelf- Defense System

J. Blaszczyk, Air ForceMaterial Command,Warsaw, Poland

0930AIAA-2010-0037 Near Space BalloonPerformance Predictions

J. Conner, OklahomaState University,Stillwater, OK

1000AIAA-2010-0039 A Newton EulerApproach to Modeling ofa Quad- RotorAutonomous Airship –Preliminary Results.

Y. Bestaoui, LaboratoireIBISC CNRS Fre 3190University of Evry, Evry,France

1030AIAA-2010-0040 A Lagrangian Approachto Modeling of anAirship with Wind andVarying Mass Effects

Y. Bestaoui, Universityof Evry, Evry, France

1100AIAA-2010-0041 Model StructureDetermination of anOrnithopterAerodynamics Modelfrom Flight Data

J. Grauer, University ofMaryland, College Park,MD

Chaired by: T. LIU, Western Michigan University, Kalamazoo, MI, and M. BENNE, The Boeing Company, St Louis, MO0800AIAA-2010-0042 Skin FrictionMeasurements UsingElastic Films (Invited)

J. Crafton, InnovativeScientific Solutions, Inc.,Dayton, OH

0830AIAA-2010-0043 Oil Film Interferometry inthe Development ofLong- EnduranceAircraft (Invited)

A. Drake, NorthropGrumman Corporation,San Diego, CA

0900AIAA-2010-0044 Direct Measurement ofSkin Friction in ComplexFlows

J. Schetz, VirginiaPolytechnic Institute andState University,Blacksburg, VA

0930AIAA-2010-0045 ExperimentalExamination of SkinFriction Topology inSeparated Flows(Invited)

T. Liu, Western MichiganUNiversity, Kalamazoo,MI

1000AIAA-2010-0047 Effect of DynamicPressure on DirectShear Stress SensorDesign

V. Chandrasekharan,University of Florida,Gainesville, FL

Chaired by: J. DESPIRITO, U.S. Army Research Laboratory, Aberdeen Proving Ground, MD, and K. STEWART, U.S. Air Force Research Laboratory, Eglin AFB, FL0800AIAA-2010-0049 Aero- elastic Analysis ofSensor CraftConfigurations usingAVUS and Nastran

E. Alyanak, U.S. AirForce ResearchLaboratory,Wright-Patterson AFB,OH

0830AIAA-2010-0050 Development of aAerothermoelastic-Acoustics SimulationCapability of FlightVehicles

K. Gupta, NASA DrydenFlight Research Center,Edwards, CA

0900AIAA-2010-0052 ALE- Based FSISimulation of SolidPropellant Rocket Interior

S. Han, Seoul NationalUniversity, Seoul, SouthKorea

0930AIAA-2010-0053 Detached EddySimulation of 3- D WingFlutter with FullyCoupled Fluid- StructuralInteraction

X. Chen, University ofMiami, Coral Gables, FL

1000AIAA-2010-0054 In- Flight DeploymentDynamics of InflatableWings

L. Ben, Oklahoma StateUniversity, Stillwater, OK

1030AIAA-2010-0055 Flutter Analysis ofBalloon- BasedOperation Vehicle forPrecooled TurbojetEngine Demonstration

K. Miyaji, YokohamaNational University,Yokohama, Japan

1100AIAA-2010-0056 New Aeroelastic Studiesfor a Morphing Wing

S. Courchesne, ETS -LARCASE, Montréal,Canada

Chaired by: J. GUGLIELMO, The Boeing Company, Saint Peters, MO, and K. WAITHE, Gulffstream Aerospace Corporation, Savannah, GA


Monday Morning / 04 January 2010 Session 8-APA-2 Airfoil/Wing/Configuration Aerodynamics Grand Ballroom 10

Monday Morning / 04 January 2010 Session 9-APA-3 Low Speed, Low Reynolds Number Aerodynamics Grand Ballroom 11

Monday Morning / 04 January 2010 Session 10-ASE-1 Space Environment Ground Simulations and Testing Atlanta


Chaired by: J. GUGLIELMO, The Boeing Company, Saint Peters, MO, and K. WAITHE, Gulffstream Aerospace Corporation, Savannah, GA0800AIAA-2010-0057 AerodynamicOptimization andEvaluation of KC- 135RWinglets, RakedWingtips, and aWingspan Extension

J. Halpert, U.S. AirForce Academy,Colorado Springs, CO

0830AIAA-2010-0058 Aerodynamics ofCambered MembraneFlapping Wings

S. Shkarayev, Universityof Arizona, Tucson, AZ

0900AIAA-2010-0059 Detached- EddySimulation of a Double-Element Wing in GroundEffect

J. Heyder-Bruckner,University ofSouthampton,Southampton, GreatBritain

0930AIAA-2010-0060 Effect of Leading EdgeBreak Position onPerformance of DoubleDelta Movable TipStrakes

V. Nikolic, MinnesotaState University,Mankato, Mankato, MN

1000AIAA-2010-0061 Surface LaunchSimulations of anUnmanned AerialVehicle Loaded with Jet-Assisted Takeoff Motors

D. Gonzalez, NavalSurface Warfare Center,Indian Head, MD

1030AIAA-2010-0062 Passively Varying PitchPropeller for Small UAS

S. Heinzen, NorthCarolina StateUniversity, Raleigh, NC

1100AIAA-2010-0063 Preliminary Design DragCalculation UsingAdvanced PanelingSchemes

V. Ahuja, AuburnUniversity, Auburn, AL

Chaired by: F. COTON, University of Glasgow, Glasgow, Great Britain, and C. BRUNER, Sandia National Laboratories, Albuquerque, NM0800AIAA-2010-0065 How Motion TrajectoryAffects the EnergyExtraction Performanceof an Oscillating Foil

Q. Xiao, University ofStrathclyde, Glasgow,Great Britain

0830AIAA-2010-0066 Flow Visualization andForce Measurement ofan Insect- BasedFlapping Wing

J. Han, KoreaAerospace University,Goyang, South Korea

0900AIAA-2010-0067 Simulation of Insect-Sized Flapping- WingAerodynamics

W. Yuan, NationalResearch CouncilCanada, Ottawa, Canada

0930AIAA-2010-0068 Numerical Analysis ofthe Flow Around the SD7003 Airfoil

P. Catalano, ItalianAerospace ResearchCenter (CIRA), Capua,Italy

1000AIAA-2010-0069 Gust Encounters in Rigidand Flexible Wing MAVs

J. Jacob, OklahomaState University,Stillwater, OK

1030AIAA-2010-0070 A Study of Trailing-Edge Scalloping on Flat-Plate Membrane WingPerformance

T. Hicks, University ofAlabama, Tuscaloosa,AL

1100AIAA-2010-0071 Effects of IpsilateralWing- Wing Interactionson AerodynamicPerformance of FlappingWings

H. Dong, Wright StateUniversity, Dayton, OH

Chaired by: J. PREBOLA, Aerospace Testing Alliance, Arnold AFB, TN, and M. CHO, Kyushu Institute of Technology, Kitakyushu, Japan0800AIAA-2010-0073 Explosion DamagePrediction of AdvancedSpace StructuresSubject to HypervelocityImpact

M. Dal Santo, RoyalMelbourne Institute ofTechnology, Melbourne,Australia

0830AIAA-2010-0074 Preliminary Experimentsfor Establishing An ESDGround Testing Methodof Solar Array

K. Toyoda, KyushuInstitute of Technology,Kitakyushu, Japan

0900AIAA-2010-0075 Arcing on Solar Arraysat Extremely LowTemperatures

B. Vayner, OhioAerospace Institute,Cleveland, OH

0930AIAA-2010-0076 Development ofElectron- emitting Filmfor Spacecraft ChargingMitigation: EnvironmentExposure Tests

A. Khan, KyushuInstitute of Technology,Kitakyushu, Japan

1000AIAA-2010-0077 New Space WeatherMitigation Capabilities

W. Tobiska, SpaceEnvironmentTechnologies, LosAngeles, CA

Chaired by: M. MAUGHMER, Pennsylvania State University, University Park, PA


Monday Morning / 04 January 2010 Session 11-EDU-1 New Directions in Course Instruction Crystal Ballroom Q

Monday Morning / 04 January 2010 Session 12-FD-1 Active Flow Control I Grand Ballroom 3

Monday Morning / 04 January 2010 Session 13-FD-2 Droplet and Multi-Phase Flows Grand Ballroom 12


Chaired by: M. MAUGHMER, Pennsylvania State University, University Park, PA0800AIAA-2010-0079 Instruction inExperimental Methods:What Should We BeTeaching in LaboratoryCourses?

D. Bridges, MississippiState University,Mississippi State, MS

0830AIAA-2010-0080 The Beginner's Guide toWind Tunnels withTunnelSim andTunnelSys

T. Benson, NASA GlennResearch Center,Cleveland, OH

0900AIAA-2010-0081 Proven Cost Savings byUsing Modern Design ofExperiments (MDOE)

W. Line, DOES Institute,Winston-Salem, NC

0930AIAA-2010-0082 An AerodynamicsCourse Project toIllustrate Parasite DragCoefficient Prediction

E. Niemi, University ofMassachusetts, Lowell,Lowell, MA

1000AIAA-2010-0083 IncorporatingAirworthiness into theAcademic Curriculum

S. Cook, North CarolinaState University,Raleigh, NC

1030AIAA-2010-0085 A Primer for University-Level Solid RocketMotor Research andDevelopment

J. Dennis, Arizona StateUniversity, Tempe, AZ

Chaired by: S. SIEGEL, U.S. Air Force Academy, Colorado Springs, CO, and H. FASEL, University of Arizona, Tucson, AZ0800AIAA-2010-0086 Hybrid Control of aTurret Wake, Part I:Aerodynamic Effects

B. Vukasinovic, GeorgiaInstitute of Technology,Atlanta, GA

0830AIAA-2010-0087 Flow Control Effects onthe Length Scales Overa Turret

M. Andino, SyracuseUniversity, Syracuse, NY

0900AIAA-2010-0088 Experimental Study ofan Inclined Jet- in-Cross- Flow Interactingwith a Vortex Generator

K. Zaman, NASA GlennResearch Center,Cleveland, OH

0930AIAA-2010-0089 Effect of SinusoidalForcing on the Wake ofa Circular Cylinder

S. Bhattacharya,Auburn University,Auburn, AL

1000AIAA-2010-0090 Numerical Simulationsof Vortex GeneratingJets on Low PressureTurbine Blades

C. Memory, The OhioState University,Columbus, OH

1030AIAA-2010-0091 Frequency Effect onFlow Field Behind anOscillating FenceSubmerged in TurbulentBoundary Layer

M. Saini, University ofWyoming, Laramie, WY

1100AIAA-2010-0092 ProportionalAerodynamic Control ofa Swept DivergentTrailing Edge WingUsing Synthetic Jets

J. Sefcovic, University ofWyoming, Laramie, WY

1130AIAA-2010-0093 Analysis of Low SpeedFlow over an AdaptiveAirfoil with OscillatingCamber

R. LeBeau, University ofKentucky, Lexington, KY

Chaired by: R. SCHMIT, U.S. Air Force Research Laboratory, Wright-Patterson AFB, OH0800AIAA-2010-0095 Modeling of the InternalTwo- Phase Flow in aGas- Centered SwirlCoaxial Fuel Injector

N. Trask, University ofMassachusetts,Amherst, MA

0830AIAA-2010-0096 Simulation of MultiphaseBlast- StructureInteraction via CoupledCFD and CSD Codes

R. Lohner, GeorgeMason University,Fairfax, VA

0900AIAA-2010-0097 Simulation ofSupercritical EthyleneCondensation UsingHomogeneousNucleation Theory

J. Edwards, NorthCarolina StateUniversity, Raleigh, NC

0930AIAA-2010-0098 Numerical Simulation ofTwo- Phase Flow Withinan Aerated LiquidInjector

D. Cassidy, NorthCarolina StateUniversity, Raleigh, NC

1000AIAA-2010-0099 Turbulent ParticulatePressure for Two-Phase Flow Modeling

C. Hug, EADS Astrium,Les Mureaux, France

1030AIAA-2010-0100 Effects of Liquid andSurface Properties onDroplet- Film Collision

K. Pan, National TaiwanUniversity, Taipei,Taiwan (roc)

Chaired by: Z. MAHMUD, North Dakota State University, Fargo, ND, and L. UKEILEY, University of Florida, Shalimar, FL0800 0830 0900 0930 1000 1030


Monday Morning / 04 January 2010 Session 14-FD-3 Innovative Measurement Technologies and Experimental Observations Grand Ballroom 4

Monday Morning / 04 January 2010 Session 15-FD-4 Shock-Wave/Turbulence Interactions Grand Ballroom 5

Monday Morning / 04 January 2010 Session 16-FD-5 Time Integration and Solution Methods Boston


Chaired by: Z. MAHMUD, North Dakota State University, Fargo, ND, and L. UKEILEY, University of Florida, Shalimar, FL0800AIAA-2010-0102 Density FieldMeasurements of aSupersonic ImpingingJet with Microjet Control

L. Venkatakrishnan,National AerospaceLaboratories, Bangalore,India

0830AIAA-2010-0103 Virtual Shock ShapingUsing Microjet Arrays

A. Botu, Florida A&MUniversity-Florida StateUniversity, Tallahassee,FL

0900AIAA-2010-0104 Planar ImagingMeasurements of ThreeScalars in a TurbulentJet

C. Brownell, U.S. NavalAcademy, Annapolis, MD

0930AIAA-2010-0105 Reynolds Stress andTurbulence KineticEnergy Balances inSwirling Jets

S. Toutiaei, University ofWyoming, Laramie, WY

1000AIAA-2010-0106 Modeling andExperimentalInvestigation ofSynthetic Jets in Cross-flow

X. Xia, University ofColorado, Boulder,Boulder, CO

1030AIAA-2010-0107 Surface PressureFluctuations Due to anImpinging SupersonicUnderexpanded Jet

B. Pundir, FloridaAtlantic University, BocaRaton, FL

Chaired by: P. MARTIN, Princeton University, Princeton, NJ, and R. BALASUBRAMANIAN, ITT Industries, Seneca Falls, NY0800AIAA-2010-0108 Low- FrequencyUnsteadiness in theDNS of a CompressionRamp Shockwave andTurbulent BoundaryLayer Interaction

S. Priebe, PrincetonUniversity, Princeton, NJ

0830AIAA-2010-0109 Delayed- Detached-Eddy Simulation ofShock Wave/TurbulentBoundary LayerInteraction

P. Coronado, Universityof Miami, Coral Gables,FL

0900AIAA-2010-0110 Large- Eddy Simulationof Turbulent BoundaryLayer Interaction with anOblique Shock Wave

A. Jammalamadaka,Michigan StateUniversity, EastLansing, MI

0930AIAA-2010-0111 Simulation of Shock /Boundary LayerInteractions UsingImproved LES/RANSModels

D. Gieseking, NorthCarolina StateUniversity, Raleigh, NC

1000AIAA-2010-0112 Numerical Investigationsof Shock- TurbulenceInteraction in a PlanarMixing Layer

Z. Li, Michigan StateUniversity, EastLansing, MI

1030AIAA-2010-0113 WITHDRAWN Large- Eddy Simulationof Shockwave/IsotropicTurbulence Interaction

N. Grube, PrincetonUniversity, Princeton, NJ

1100AIAA-2010-0114 Numerical Simulation ofShock- TurbulenceInteractions Using High-Order Shock- FittingAlgorithms

P. Rawat, University ofCalifornia, Los Angeles,Los Angeles, CA

1130AIAA-2010-0115 Validation of a Wall-Layer Model for aShock- Wave/Boundary-Layer Interaction

R. Bond, SandiaNational Laboratories,Albuquerque, NM

Chaired by: D. KNIGHT, Rutgers University, Piscataway, NJ, and L. FUCHS, Lund Universiy, Lund, Sweden0800AIAA-2010-0116 A Parallel Newton-Krylov- Schur FlowSolver for the Navier-Stokes Equations Usingthe SBP- SAT Approach

M. Osusky, University ofToronto, Toronto,Canada

0830AIAA-2010-0117 Implementation of aRobust MultigridAlgorithm in aProduction- LevelOverset CFD Solver

S. Slimon, Electric BoatCorporation, Groton, CT

0900AIAA-2010-0118 Deflated PreconditionedConjugate GradientSolvers: Extensions andImprovements

F. Mut, George MasonUniversity, Fairfax, VA

0930AIAA-2010-0119 Computational ZoneAdaptation Strategy forUnstructured Grid Users

N. Fouladi, SharifUniversity ofTechnology, Tehran,Iran

1000AIAA-2010-0120 Time- Tensor for RapidConvergence of CFDSolutions

N. Domel, LockheedMartin Corporation, FortWorth, TX

1030AIAA-2010-0121 Spatially Non- UniformTime- Step Adaptationfor Functional Outputs inUnsteady Flow Problems

K. Mani, University ofWyoming, Laramie, WY

1100AIAA-2010-0122 Re- evaluation of anOptimized SecondOrder BackwardDifference (BDF2OPT)Scheme for UnsteadyFlow Applications

V. Vatsa, NASA LangleyResearch Center,Hampton, VA

1130AIAA-2010-0123 A Method To AccelerateLES Explicit SolversUsing Local Time-Stepping

O. Esnault, FrenchNational Center forScientific Research(CNRS),Châtenay-Malabry,France

Chaired by: C. ROY, Virginia Polytechnic Institute and State University, Blacksburg, VA, and W. OBERKAMPF, W L Oberkampf Consulting, Albuquerque, NM


Monday Morning / 04 January 2010 Session 17-FD-6 Verification, Validation, and Uncertainty Quantification in CFD Grand Ballroom 6

Monday Morning / 04 January 2010 Session 18-GPSE-1 Space Agency Programs in Gravity-Dependent Research Grand Ballroom 13

Monday Morning / 04 January 2010 Session 19-GT-1 Future of Ground Testing Crystal Ballroom G1


Chaired by: C. ROY, Virginia Polytechnic Institute and State University, Blacksburg, VA, and W. OBERKAMPF, W L Oberkampf Consulting, Albuquerque, NM0800AIAA-2010-0124 A Complete Framework for Verification,Validation, and Uncertainty Quantification inScientific Computing (Invited)

C. Roy, Virginia Polytechnic Institute and StateUniversity, Blacksburg, VA

0900AIAA-2010-0125 The AIAA CodeVerification Project -Test cases for CFDCode Verification

U. Ghia, University ofCincinnati, Cincinnati,OH

0930AIAA-2010-0126 Review of Discretization Error Estimators inScientific Computing

C. Roy, Virginia Polytechnic Institute and StateUniversity, Blacksburg, VA

1030AIAA-2010-0127 Comprehensive CodeVerification for anUnstructured FiniteVolume CFD Code

S. Veluri, VirginiaPolytechnic Institute andState University,Blacksburg, VA

1100AIAA-2010-0128 Error Estimation for HighSpeed Flows UsingContinuous and DiscreteAdjoints

K. Duraisamy, StanfordUniversity, Stanford, CA

1130AIAA-2010-0129 Non- IntrusivePolynomial ChaosMethods for UncertaintyQuantification in FluidDynamics

S. Hosder, MissouriUniversity of Scienceand Technology, Rolla,MO

Chaired by: F. KOHL and K. SACKSTEDER, NASA Glenn Research Center, Cleveland, OH0800Oral Presentation Advanced CapabilitiesDivision Program Statusand Outlook

B. Neumann, NASAHeadquarters,Washington, DC

0830Oral Presentation NASA InnovativePartnership Program

D. Comstock, NASAHeadquarters,Washington, DC

0900Oral Presentation The ISS NationalLaboratory: TheIntersection of Researchand Exploration

B. Carpenter, NASAHeadquarters,Washington, DC

0930Oral Presentation CSA ResearchPrograms

M. Dejmek, CanadianSpace Agency, St.Hubert, Canada

1000AIAA-2010-0134 Update of the GermanMicrogravity Program inPhysical Sciences

R. Kuhl, GermanAerospace Center(DLR), Bonn, Germany

1030Oral Presentation CNES ResearchProgram

B. Zappoli, FrenchSpace Agency (CNES),Toulouse, France

1100Oral Presentation ESA Research Program

O. Minster, ESA,Noordwijk, TheNetherlands

Chaired by: F. STEINLE, and J. KEGELMAN, NASA Langley Research Center, Hampton, VA0800AIAA-2010-0138 A Historical Perspectiveof Design Requirementsfor AEDC's PropulsionWind Tunnel and vonKármán Facilities.

D. Hiebert, ArnoldEngineeringDevelopment Center,Arnold AFB, TN

0830AIAA-2010-0139 IntegratingComputational Scienceand Engineering To Re-Engineer theAeronauticalDevelopment Process

E. Kraft, ArnoldEngineeringDevelopment Center,Arnold AFB, TN

0900AIAA-2010-0140 Technical WorkforceNeeds for a NewNational TrisonicGround Test Capability

J. Best, ArnoldEngineeringDevelopment Center,Arnold AFB, TN

0930AIAA-2010-0141 WITHDRAWN A New Wind TunnelOperations Concept forExpected 2020Technology

F. Jackson, ArnoldEngineeringDevelopment Center,Arnold AFB, TN

1000AIAA-2010-0142 Wind Tunnel Testing’sFuture: A Vision of theNext Generation of WindTunnel TestRequirements andFacilities

M. Melanson, LockheedMartin Aeronautics, FortWorth, TX

1030AIAA-2010-0143 Langley GroundFacilities and Testing inthe 21st Century

D. Ambur, NASALangley ResearchCenter, Hampton, VA

1100AIAA-2010-0145 Industry Expectationsfor Aerodynamic TestFacility Capabilities toSupport FutureDevelopment Programs– A User Perspective

L. McGill, RaytheonMissile Systems,Tuscon, AZ


Monday Morning / 04 January 2010 Session 20-GTE-10800 - 1200 Alternative Fuels - Government Funded Programs (Invited) Grand Ballroom 14

Monday Morning / 04 January 2010 Session 21-HAPB-1 Pulse Detonation Engines Crystal Ballroom E

Monday Morning / 04 January 2010 Session 22-HIS-1 History of Aviation Crystal Ballroom P

Chaired by: B. SEKAR and J. DATKO, U.S. Air Force Research Laboratory, Wright-Patterson AFB, OHConventional aviation fuels are derived from petroleum-based crude oils. Increasing energy demand, cost and environmental concerns increase the need to seek alternate transportation fuels from natural gas,coal and biomass to achieve the goal of energy independence from petroleum-based energy sources. There has been considerable interest in recent years for alterative aviation fuels produced fromnon-petroleum sources. New technologies are being developed and supported by the Government and private enterprise to replace petroleum-based aviation fuels in a cost effective way. For example, naturalgas or coal-liquid can be converted into paraffinic synthetic fuels using the Fischer-Tropsch (FT) process. Similarly, selective cracking and isomerization processes are used to produce paraffinic aviation gradesynthetic jet fuels from biodiesel. As the new form of alternative fuels enter the aviation industry, a series of new engine technologies are also under development to use these fuels with the aim of achievingimproved combustion stability and efficiency, and reduced emissions. As a result, there is a greater need for a coordinated strategic effort between the Government and private institutions to developaffordable and cost effective technologies for practical aviation applications. Therefore, this special topic will address the Government programs for the alternate fuel development and the technical efforts thatare being currently pursued.

Speakers:

William Harrison, U.S. Air Force: Air Force Alternative Fuels/Energy "Big Picture"

John Datko, U.S. Air Force Research Laboratory: Air Force Alternative Fuels Science & Technology Program

David Shifler, Office of Naval Research: US Navy Alternative Fuels/F-18 Flight Demonstration

Dan Bulzan, NASA Glenn Research Center: NASA Fundamental Aeronautics Research on Alternative Fuels

Donald Ferguson, U.S. Department of Energy/NETLFuel: Flexibility for Next Generation Combustion Applications

Jim Skaleky, Federal Aviation Administration: Federal Aviation Administration Continuous Lower Energy, Emissions and Noise (CLEEN) Technologies Development

Pat Muzzell, U.S. Army: Alternative Aviation Fuels and the Army

Chaired by: D. PAXSON, NASA Glenn Research Center, Cleveland, OH, and V. TANGIRALA, General Electric Company, Niskayuna, NY0800AIAA-2010-0146 Testing of a ContinuousDetonation WaveEngine with SwirledInjection

E. Braun, University ofTexas, Arlington,Arlington, TX

0830AIAA-2010-0147 Effects of a CatalystCoating on a PDEEndothermic FuelHeating System

C. Stevens, U.S. AirForce Institute ofTechnology,Wright-Patterson AFB,OH

0900AIAA-2010-0148 Net ImpulseMeasurements of PulseDetonation Tube byUsing Fuel- Air Mixture

S. Takeuchi, Universityof Tsukuba, Tsukuba,Japan

0930AIAA-2010-0149 Unsteady Ejectors: TheEffect of Driver JetMark- Space Ratio

C. Ward, CambridgeUniversity, Cambridge ,Great Britain

1000AIAA-2010-0150 Numerical Investigationof Pre- Detonators forPulse DetonationEngines

R. Fievisohn, U.S. AirForce Institue ofTechnology,Wright-Patterson AFB,OH

1030AIAA-2010-0151 Unsteady Flame SpeedControl and DDTEnhancement UsingFluidic Obstacles

B. Knox, StateUniversity of New York,Buffalo, Buffalo, NY

1100AIAA-2010-0152 Effect of Nozzle Shapeson the Performance ofContinuously- RotatingDetonation Engine

T. Yi, Institute of HighPerformanceComputing, Singapore,Singapore

1130AIAA-2010-0153 Numerical Analysis ofThreshold of LimitDetonation in RotatingDetonation Engine

T. Yamada, AoyamaGakuin University,Sagamihara, Japan

Chaired by: S. EBERHARDT, The Boeing Company, Seattle, WA, and K. BURNS, Wyle Laboratories, San Diego, CA0800AIAA-2010-0154 PaleoaerodynamicExplorations Part I:Evolution of Biologicaland Technical Flight

0830AIAA-2010-0155 PaleoaerodynamicExplorations Part II:Options for FutureTechnology Innovations

0900AIAA-2010-0156 Gago Coutinho and theAircraft Navigation

F. Neves, University ofBeira Interior , Covilhã,

0930AIAA-2010-0157 The Centennial Eventsfor 100 Years of NavalAviation

K. Burns, Wyle

1000AIAA-2010-0158 To Boldly Go Where NoUnmanned Aircraft HasGone Before: A Half-Century of DARPA’sContributions to

1030AIAA-2010-0159 Tracing the Growth ofU.S. Navy Aviation

M. Spearman, NASALangley Research


B. Kulfan, The BoeingCompany, Seattle, WA

B. Kulfan, The BoeingCompany, Seattle, WA

Portugal Laboratories, San Diego,CA

Unmanned Aircraft

M. Hirschberg, CentraTechnology, Inc.,Arlington, VA

Center, Hampton, VA

Chaired by: A. SHIH, University of Alabama, Birmingham, Birmingham, AL, and A. IANNETTI, NASA Glenn Research Center, Cleveland, OK0800 0830 0900 0930 1000 1030 1100

Chaired by: R. GREENWOOD, U.S. Air Force Academy, Colorado Springs, CO0800 0830 0900 0930 1000 1030 1100

Chaired by: C. TWOMEY-LAMB, MIT Lincoln Lab, Lexington, MA0800 0830 0900 0930 1000


Monday Morning / 04 January 2010 Session 23-MVC-1 CFD Meshing Crystal Ballroom L

Monday Morning / 04 January 2010 Session 25-NSC-1 AIAA Foundation Masters Crystal Ballroom A

Monday Morning / 04 January 2010 Session 26-NSC-2 AIAA Foundation Team Crystal Ballroom B


Chaired by: A. SHIH, University of Alabama, Birmingham, Birmingham, AL, and A. IANNETTI, NASA Glenn Research Center, Cleveland, OK0800AIAA-2010-0161 A Surface RemeshingApproach

R. Aubry, BarcelonaSupercomputing Center,Barcelona, Spain

0830AIAA-2010-0162 Generation ofConjugate Meshes forComplex Geometriesfor Coupled Multi-Physics Simulations

W. Dawes, CambridgeUniversity, Cambridge,Great Britain

0900AIAA-2010-0163 Automatic MeshGeneration of HybridMesh on Valves inMultiple Positions inFeedline Systems

D. Ross, University ofAlabama, Birmingham,Birmingham, AL

0930AIAA-2010-0164 A Classical Elasticity-Based Mesh UpdateMethod for Moving andDeforming Meshes

R. Smith, Naval SurfaceWarfare Center,Panama City, FL

1000AIAA-2010-0165 Explicit and RobustInverse DistanceWeighting MeshDeformation for CFD

J. Witteveen, Center forTurbulence ResearchStanford University,Stanford, CA

1030AIAA-2010-0166 Image- BasedComputational Modelingof Complex Organismsand Biological Structures

S. Dillard, University ofIowa, Iowa City, IA

1100AIAA-2010-0167 An Improvement toPatched Grid with theHigh- OrderConservativeRemapping Method

Y. Zhang, TsinghuaUniversity, Beijing,China (prc)

Chaired by: R. GREENWOOD, U.S. Air Force Academy, Colorado Springs, CO0800AIAA-2010-0173 Experimental Methodsfor Impact of CompositeMaterials

B. Gulker, MichiganState University,Lansing, MI

0830AIAA-2010-0174 The Implicit FunctionTheorem withApplications inDynamics and Control

M. Harris, Texas A&MUniversity, CollegeStation, TX

0900AIAA-2010-0175 Flight Testing of aPrototypeLOX/Propylene UpperStage Engine

D. Verma, CaliforniaState University, , LongBeach, CA

0930AIAA-2010-0176 A "Free" Approach toComputationalAeroelasticity

G. Romanelli,Department ofAerospace Engineering ,Milan, Italy

1000AIAA-2010-0177 Behavior ofMagnetorheologicalFluid CompositesEmploying Carrier FluidsCertified for LandingGear Use

L. Ahure, SmartStructures Laboratory,Alfred Gessow RotorcraftCenter, University ofMaryland, College Park,MD

1030AIAA-2010-0178 Characteristics of MetalCombustion Obtainedfrom Constant VolumeExplosion Experiments

P. Santhanam, NewJersey Institute ofTechnology, Newark, NJ

1100AIAA-2010-0179 Unscented Kalman Filterfor Thermal ParameterIdentification

M. Hazard, NorthCarolina StateUniversity, Charlotte, NC

Chaired by: C. TWOMEY-LAMB, MIT Lincoln Lab, Lexington, MA0800AIAA-2010-0180 Design, Fabrication, andTesting of aSurveillance/Attack UAV

K. Albarado, AuburnUniversity, Auburn, AL

0830AIAA-2010-0181 High PerformanceComputingImplementation on aRisk Assessment Code

J. Ocampo, University ofTexas, San Antonio, SanAntonio, TX

0900AIAA-2010-0182 FalconSAT- 3 and theSpace Environment

S. Gay, U.S. Air ForceAcademy, ColoradoSprings, CO

0930AIAA-2010-0183 Design of a N20/HTPBHybrid Rocket MotorUtilizing a ToroidalAerospike Nozzle

J. Dennis, Arizona StateUniversity, Tempe, AZ

1000AIAA-2010-0184 Design and Constructionof All- Composite UAVsUtilizing a ModifiedVARTM Process

R. Vocke, University ofMaryland, College Park,MD


Monday Morning / 04 January 2010 Session 27-NSC-3 AIAA Foundation Undergraduate Crystal Ballroom C

Monday Morning / 04 January 2010 Session 28-PC-1 Diagnostics and Measurements in Combustion Systems Crystal Ballroom F

Monday Morning / 04 January 2010 Session 29-PC-2 Large Eddy Simulation for Combustion Applications New Orleans


Chaired by: A. MITCHELL, U.S. Air Force, Arlington, VA0800AIAA-2010-0186 Fatigue Testing ofPneumatic ArtificialMuscle Actuators

M. Gentry, University ofMaryland, College Park,MD

0830AIAA-2010-0187 Application ofProportional- Integral-Derivative Control to aSupersonic Wind Tunnel

K. Busa, SyracuseUniversity, Syracuse, NY

0900AIAA-2010-0188 A Factorial DesignExperiment to Analyzethe Optical StrainResponse of aLuminescentPhotoelastic Coating

D. Gerber, University ofAlabama, Tuscaloosa,AL

0930AIAA-2010-0190 Fatigue Study of aNanocomposite Laminate

J. Wilkerson, TexasA&M University,Department ofAerospace Engineering,College Station, TX

1000AIAA-2010-0191 AerodynamicInvestigation of NASACrew ExplorationVehicle Forward BayCover SeparationCharacteristics

B. Henicke, U.S. AirForce Academy,Colorado Springs, CO

1030AIAA-2010-0192 Bubble Behavior inNucleate BoilingExperiment Aboard theSpace Shuttle

J. Koeln, Utah StateUniversity, Logan, UT

1100AIAA-2010-1599 Water Vapor AbsorptionSpectroscopy in aSimulated HelicopterExhaust Using Vertical-Cavity Surface- EmittingLasers

L. Huynh, University ofNew South Wales,Canberra, Australia

Chaired by: R. PITZ, Vanderbilt University, Nashville, TN, and Y. IKEDA, Imagineering, Inc., Kobe, Japan0800AIAA-2010-0193 Static Stability MarginSensing in a Lean DirectInjection (LDI) TurbineEngine Combustor

R. Bompelly,Guggenheim School ofAerospace Engineering,Georgia Institute ofTechnology, Atlanta, GA

0830AIAA-2010-0194 Spray Structure ofAerated Liquid JetsUsing Double- ViewDigital Holography

K. Sallam, OklahomaState University,Stillwater, OK

0900AIAA-2010-0196 A Second- GenerationAerosol Shock Tube forCombustion Research

D. Haylett, MechanicalEngineeringDepartmennt, StanfordUniversity, Stanford, CA

0930AIAA-2010-0197 Measurement ofExtinction Limits and OHRadicals forTrimethybenzene and n-Propylbenzene DiffusionFlames

S. Won, PrincetonUniversity, Princeton, NJ

1000AIAA-2010-0198 Mulit- SpeciesMeasurements BehindReflected Shock Wavesin Hydrocarbons UsingLaser Absorption

D. Davidson, StanfordUniversity, Stanford, CA

1030AIAA-2010-0200 Numerical andExperimental Evaluationof the OpticalConnectivity Techniquefor Measurement ofLiquid Breakup Lengthin Atomizers

G. Charalampous,Imperial CollegeLondon, London, GreatBritain

Chaired by: J. OEFELEIN, Sandia National Laboratories, Livermore, CA, and E. MASTORAKOS, University of Cambridge, Cambridge, Great Britain0800AIAA-2010-0201 Unsteady FlameEmbedding (UFE)Subgrid Model forTurbulent PremixedCombustion Simulations

H. El-Asrag,Massachusetts Instituteof Technology,Cambridge, MA

0830AIAA-2010-0202 Large Eddy Simulationsof Supersonic TurbulentReacting Flows

A. Banaeizadeh,Michigan StateUniversity, EastLansing, MI

0900AIAA-2010-0203 Large Eddy Simulationof SupersonicCombustion UsingDirect QuadratureMethod of Moments

P. Donde, University ofTexas, Austin, Austin,TX

0930AIAA-2010-0204 On Experimental Datafor Validation of Large-Eddy Simulation ofEvaporating Droplets ina Mxing Layer

S. Radhakrishnan, JetPropulsion Laboratory,Pasadena, CA

1000AIAA-2010-0205 A Filtered TabulatedChemistry Model forLarge Eddy Simulationof Reactive Flows

P. Auzillon, ÉcoleCentrale Paris,Chatenay Malabry,France

1030AIAA-2010-0206 Large Eddy Simulationsof Temporal MixingLayers UnderSupercriticalThermodynamicConditions: O2/H2

E. Taskinoglu, JetPropulsion Laboratory,Pasadena, CA

1100AIAA-2010-0207 The LES- ODT Modelfor Turbulent PremixedFlames

T. Echekki, Departmentof Mechanical andAerospace Engineering,North Carolina StateUniversity, Raleigh, NC

1130AIAA-2010-0208 Large Eddy Simulationof LOX/GH2 Shear-Coaxial Jet Flame atSupercritical Pressure

S. Matsuyama, JapanAerospace ExplorationAgency (JAXA), Chofu,Japan


Monday Morning / 04 January 2010 Session 30-PC-3 Liquid Injection and Atomization Los Angeles

Monday Morning / 04 January 2010 Session 31-PC-4 Turbulent Flames I Miami

Monday Morning / 04 January 2010 Session 32-PDL-1 Magnetohydrodynamic Numerical Simulations New York


Chaired by: E. GUTMARK, University of Cincinnati, Cincinnati, OH, and A. AGRAWAL, University of Alabama, Tuscaloosa, AL0800AIAA-2010-0209 Operation and Controlof a Pulsejet with HighPressure Liquid FuelInjection

A. Naples, InnovativeScientific Solutions, Inc.,Dayton, OH

0830AIAA-2010-0210 Towards an Efficient,High- FidelityMethodology for LiquidJet AtomizationComputations

X. Li, UnitedTechnologies ResearchCenter, East Hartford,CT

0900AIAA-2010-0212 Parametric Study ofPrimary Breakup ofTurbulent Liquid Jets inCrossflow: Role ofWeber number

M. Pai, StanfordUniversity, Stanford, CA

0930AIAA-2010-0213 Fully- coupledMultiphysics Model toSimulate an ElectrostaticMicropump

B. Spatafore, Universityof Colorado, Boulder,Boulder, CO

1000AIAA-2010-0214 Liquid Fuel Jet inCrossflow –TrajectoryCorrelations based onthe Column BreakupPoint

Y. Gopala, GeorgiaInstitute of Technology,Atlanta, GA

1030AIAA-2010-0215 On the Modeling of aSpray Impinging on aSurface

A. Silva, University ofBeira Interior, Covilhã,Portugal

1100AIAA-2010-0216 Effect of Fuel InjectionLocation on CombustionInstability in a DumpCombustor

R. Desai, Indian Instituteof Technology, Madras,Ahmedabad, India

Chaired by: M. SMOOKE, Yale University, New Haven, CT, and C. BROPHY, Naval Postgraduate School, Monterey, CA0800AIAA-2010-0217 Numerical Simulation ofAutoignition of a DilutedHydrogen Plume in Co-Flowing Turbulent Hot Air

S. Kerkemeier, SwissFederal Institute ofTechnology, Zurich,Switzerland

0830AIAA-2010-0218 Direct NumericalSimulation of Non-Premixed FlameExtinction by WaterSpray

P. Arias, Department ofMechanical Engineering,University of Michigan,Ann Arbor, MI

0900AIAA-2010-0220 Transitional BlowoffBehavior of Wake-Stabilized Flames inVitiated Flow

S. Tuttle, University ofConnecticut, Storrs, CT

0930AIAA-2010-0222 Characterization andSensitivity Analysis of aTurbulent DiffusionFlame in Diluted HotCoflow

Y. See, University ofMichigan, Ann Arbor, MI

1000AIAA-2010-0223 Numerical simulation ofa gas jet diffusion flamein a venturicascadeburner and experimentalvalidation

A. Qubbaj, University ofTexas, Pan-American,Edinburg, TX

Chaired by: J. SHANG and H. YAN, Wright State University, Dayton, OH0800AIAA-2010-0225 Non- Equilibrium IonizedFlow Simulations WithinStrong Electro-Magnetic Fields

R. MacCormack,Stanford University,Stanford, CA

0830AIAA-2010-0227 Numerical Study ofMagnetoaerodynamicFlow Around aHemisphere

N. Bisek, University ofMichigan, Ann Arbor, MI

0900AIAA-2010-0229 Low Rem 3- D MHDHypersonic EquilibriumFlow Using High- OrderWENO Schemes

J. Lee, University ofMiami, Coral Gables, FL

0930AIAA-2010-0230 Numerical ParameterStudy of Low ElectricPower Segmented ArcHeaters

J. Lee, University ofStuttgart, Stuttgart,Germany

1000AIAA-2010-0231 Simulation Studies ofAlternating- CurrentMicrodischarges forMicrothrusterApplications

H. Sitaraman, Universityof Texas, Austin, Austin,TX

1030AIAA-2010-0232 The Effect of MHDEnergy Bypass onSpecific Thrust forSupersonic TurbojetEngine

T. Benyo, NASA GlennResearch Center,Cleveland, OH

Chaired by: B. DROLEN, and C. WANG, University of Florida, Gainesville, FL


Monday Morning / 04 January 2010 Session 33-TP-1 Non-Equilibrium Radiation Crystal Ballroom M

Monday Morning / 04 January 2010 Session 34-TP-2 Orbiter Entry Aerothermo Flight Experiments: Recent Flight Testing Crystal Ballroom N

Monday Morning / 04 January 2010 Session 35-WE-1 Wind Turbine Control Algorithms Crystal Ballroom G2


Chaired by: B. DROLEN, and C. WANG, University of Florida, Gainesville, FL0800AIAA-2010-0234 k- Distributions for GasMixtures in HypersonicNonequilibrium Flows

A. Bansal, PennsylvaniaState University , StateCollege, PA

0830AIAA-2010-0235 Comparative Analysis ofTwo- Temperature vs.Multi- Species, Multi-Temperature Modelingin NonequilibriumRadiating Shock Layers

C. Martin, U.S. Air ForceInstitute of Technology,Wright-Patterson AFB,OH

0900AIAA-2010-0236 Role of Viscous Effectson NEQAIR Predictionof EAST Measurements

E. McCorkle, NorthCarolina StateUniversity, Raleigh, NC

0930AIAA-2010-0237 Analysis of Shock LayerRadiation in Vacuum-Ultraviolet Region forHAYABUSA ReturnConditions

G. Yamada, Univeristyof Tokyo, Kashiwa,Japan

1000AIAA-2010-0238 The Influence ofTurbulent Fluctuationson the RadiationIntensity Emitted fromthe Core Region ofExhaust Plumes

D. Blunck, PurdueUniversity, WestLafayette, IN

1030AIAA-2010-0239 UncertaintyQuantification ofRadiative Heat FluxModeling for TitanAtmospheric Entry

S. Ghaffari, StanfordUniversity, Stanford, CA

Chaired by: T. HORVATH, NASA Langley Research Center, Hampton, VA, and C. CAMPBELL, NASA Johnson Space Center, Houston, TX0800AIAA-2010-0240 Boundary LayerTransition FlightExperiment Overviewand In SituMeasurements

B. Anderson, NASAJohnson Space Center,Houston, TX

0830AIAA-2010-0241 The Hythirm Project:Flight Thermography ofthe Space ShuttleDuring Hypersonic Re-Entry

T. Horvath, NASALangley ResearchCenter, Hampton, VA

0900AIAA-2010-0242 Design andImplementation of theBoundary LayerTransition FlightExperiment on SpaceShuttle Discovery

T. Spanos, UnitedSpace Alliance, CapeCanaveral, FL

0930AIAA-2010-0243 Cast Glance NearInfrared ImagingObservations of theSpace Shuttle DuringHypersonic Re- entry

S. Tack, Naval AirSystems Command, Pt.Mugu, CA

1000AIAA-2010-0244 HYTHIRM RadianceModeling and ImageAnalyses in Support ofSTS- 119 and STS- 125and STS- 128 SpaceShuttle Hypersonic Re-Entries

D. Gibson, JohnsHopkins UniversityApplied PhysicsLaboratory, Laurel, MD

1030AIAA-2010-0245 Application of a NearInfrared ImagingSystem forThermographic Imagingof the Space Shuttleduring Hypersonic Re-Entry

J. Zalameda, NASALangley ResearchCenter, Hampton, VA

1100AIAA-2010-0246 Orbiter Boundary LayerTransition PredictionTool Enhancements

S. Berry, NASA LangleyResearch Center,Hampton, VA

1130AIAA-2010-0247 Roles of EngineeringCorrelations inHypersonic EntryBoundary LayerTransition Prediction

C. Campbell, NASAJohnson Space Center,Houston, TX

Chaired by: M. LACKNER, University of Massachusetts, Amherst, Amherst, MA, and A. WRIGHT, National Renewable Energy Laboratory, Golden, CO0800AIAA-2010-0248 Adaptive DisturbanceTracking Control forLarge Horizontal AxisWind Turbines inVariable Speed RegionII Operation

M. Balas, Univeristy ofWyoming, Laramie, WY

0830AIAA-2010-0249 Modified AdaptiveControl for Region 3Operation in thePresence of WindTurbine StructuralModes

S. Frost, NASA AmesResearch Center,Moffett Field, CA

0900AIAA-2010-0250 Combining StandardFeedback Controllerswith Feedforward BladePitch Control for LoadMitigation in WindTurbines

F. Dunne, University ofColorado, Boulder,Boulder, CO

0930AIAA-2010-0251 Blade Pitch Control withPreview WindMeasurements

J. Laks, University ofColorado, Boulder,Boulder, CO

1000AIAA-2010-0252 Testing Further Controlsto Mitigate Loads in theControls AdvancedResearch Turbine

A. Wright, NationalRenewable EnergyLaboratory, Golden, CO

1030AIAA-2010-0253 Impact of Higher FidelityModels on ActiveAerodynamic LoadControl For FatigueDamage Reduction

B. Resor, SandiaNational Laboratories,Albuquerque, NM

1100AIAA-2010-0254 Active AerodynamicBlade Distributed FlapControl DesignProceedure for LoadReduction on theUPWIND 5MW WindTurbine

D. Wilson, SandiaNational Laboratories,Albuquerque, NM

1130AIAA-2010-1600 A Study of DynamicCoupling and CompositeLoad Control for WindTurbines

J. Lazaro, University ofAuckland, Auckland,New Zealand


Monday Morning / 04 January 2010 Session 36-WIG-1 / PDL-2 Joint PDL/WIG/FD/TP Plasma Actuator Session I Grand Ballroom 1

Monday Morning / 04 January 2010 Session 37-WIG-2 / PDL-3 Plasma-Assisted Combustion I Grand Ballroom 2

Monday Morning / 04 January 2010 Session 246-TES-4 Combustion I Crystal Ballroom K


Chaired by: O. AZAROVA, Russian Academy of Sciences, Moscow, Russia, and G. ELLIOTT, University of Illinois, Urbana-Champaign, Urbana, IL0800AIAA-2010-0256 Electrode PolarityEffects in SurfacePlasma Discharges forSupersonic Flow ControlApplications: aComputational Study

S. Mahadevan,University of Texas,Austin, Austin, TX

0830AIAA-2010-0257 Electrodynamic Controlof Shock Interactions ina 25/55 Biconic Model inHypersonic Flow

K. Wasai, TokaiUniversity, Hiratsuka,Japan

0900AIAA-2010-0259 High- Power FilamentaryPulse Discharge inSupersonic Flow

S. Leonov, RussianAcademy of Sciences,Moscow, Russia

0930AIAA-2010-0260 Active Steering of ShockWaves in CompressionRamp by NonuniformPlasma

S. Leonov, RussianAcademy of Sciences,Moscow, Russia

Chaired by: C. CARTER, U.S. Air Force Research Laboratory, Wright-Patterson AFB, OH, and V. SHIBKOV, Moscow State University, Moscow, Russia0800AIAA-2010-0263 Plasma- Assisted Flame Holding in Subsonicand Supersonic Flows

W. Kim, Stanford University, Stanford, CA

0900AIAA-2010-0264 Gradient Mechanism ofDetonation Initiation forPDE Applications

A. Rakitin, NEQLabResearch BV, Delft, TheNetherlands

0930AIAA-2010-0265 Internal and ExternalIgnition Under Conditionof Combined Discharge

V. Shibkov, MoscowState University,Moscow, Russia

1000AIAA-2010-0266 Cavity Ignition andFlameholding ofEthylene- Air andHydrogen- Air Flows bya Repetitively PulsedNanosecond Discharge1

A. Dutta, Ohio StateUniversity, Columbus,OH

1030AIAA-2010-0267 Stable plasma formationin non uniform flow ofPropane - air mixture:Propagation andtransition to explosion

S. Kamenschikov,Moscow StateUniversity, Moscow,Russia

1100AIAA-2010-0268 Millisecond PulseCurrent- VoltageInduced Perturbations ofa Premixed Propane/AirFlame

J. Schmidt, SpectralEnergies, LLC, Dayton,OH

1130AIAA-2010-0269 Non- SelfmaintainedGas Discharge forPlasma Impact on GasFlammable Mixtures

V. Bychkov, RussianAcademy of Sciences,Moscow, Russia

Chaired by: H. MONGIA, Purdue University, West Lafayette, IN, and N. SYRED, Cardiff University, Cardiff, Great Britain0900AIAA-2010-1353 Investigation of Non-Premixed and PremixedDistributed Combustionfor GT Application

V. Arghode, Universityof Maryland, CollegePark, MD

0930AIAA-2010-1354 Combustion Propertiesof Turbulent CanolaMethyl Ester and DieselFlames

N. Dhamale, Universityof Oklahoma, Norman,OK

1000AIAA-2010-1355 Implementation of NovelError Propagation BasedReduction Approach inH2S/O2 ReactionMechanism

H. Selim, University ofMaryland , College Park,MD

1030AIAA-2010-1356 Numerical Simulationsof the Thermal Stage inClaus Process:Equilibrium and KineticInvestigation

N. Al Amoodi, Universityof Maryland, CollegePark,, MD

1100AIAA-2010-1357 Ignition of Methane-Hydrogen Mixtures atHigh Pressure

B. Adhikary, Universityof Illinois, Chicago,Chicago, IL


Monday Afternoon / 04 January 2010 1300 - 1400 New Horizons Forum Keynote Address Crystal Ballroom H

Monday Afternoon / 04 January 2010

1400 - 1630 New Horizons Forum Panel Discussion - Future of the Airspace: Issues andSolutions for NextGen and Beyond … Crystal Ballroom J2

Monday Afternoon / 04 January 2010 Session 38-AA-4 Jet Noise I Washington


Distinguished Speaker: Henry P. "Hank" Krakowski, Chief Operating Officer, Federal Aviation Administration, Air Traffic Organization

21st Century Air Transportation Management – Where Are We Headed?

The panel will discuss a variety of topics that are shaping access to the civil airspace, including the expectations for NextGen as an enabler, the new found urgency for change in airspace management, theevolving role of automation and its impact on the human controller; unmanned air systems and airspace access, expectations for flight safety in the 21st century, and more.

Moderator:Victoria Cox,Senior Vice President for NextGen and Operations Planning, Air Traffic Organization, Federal Aviation Administration, Washington D.C

Panelists:

David W. Vos, Senior Director, Rockwell Collins Control Technologies, Warrenton, VA

Gerald F. "Fred" Pease Jr., SES, Director of Air Operations and Executive Director of the Department of Defense Policy Board on Federal Aviation, Deputy Chief of Staff for Operations, Plans andRequirements, Headquarters U.S. Air Force, Washington, D.C

Steve J. Vail, Senior Advisor, Global Air Traffic Operations, FedEx, Memphis TN

Bruce Landsberg, President, Aircraft Owners and Pilots Association (AOPA) Air Safety Foundation, Frederick, MD

Chaired by: D. MCLAUGHLIN, Pennsylvania State University, University Park, PA1400AIAA-2010-0270 Supersonic Jet NoisePrediction Using Non-Eddy Viscosity- TypeLES Models

N. Dittakavi, AdvancedDynamics, Inc.,Lexington, KY

1430AIAA-2010-0271 Large- Eddy Simulationsof Perfectly- ExpandedSupersonic Jets: QualityAssessment andValidation

S. Mendez, StanfordUniversity, Stanford, CA

1500AIAA-2010-0272 Numerical Simulation ofAxisymmetric JetScreech Tones Using aGeneral Purpose Finite-Volume CFD Code

K. Kurbatskii, ANSYS,Inc., Lebanon, NH

1530AIAA-2010-0273 Noise and FlowfieldCharacteristics of aSupersonic JetImpinging on a PorousSurface

A. Wiley, Florida A&MUniversity-Florida StateUniversity, Tallahassee,FL

1600AIAA-2010-0275 Numerical Simulation ofBroadband Shock-Associated Noise from ACircular Supersonic Jet

J. Gao, BeihangUniversity, Beijing,China (prc)

Chaired by: H. REEVE, United Technologies Research Center, East Hartford, CT, and C. CHUCK, The Boeing Company, Mercer Island, WA1400 1430 1500 1530


Monday Afternoon / 04 January 2010 Session 39-ABP-2 Engine Systems and Optimization Crystal Ballroom D

Monday Afternoon / 04 January 2010 Session 40-AD-1 Subsonic Aircraft Design Crystal Ballroom K

Monday Afternoon / 04 January 2010 Session 41-AD-2 U.S. Air Force INVENT Program Crystal Ballroom L


Chaired by: H. REEVE, United Technologies Research Center, East Hartford, CT, and C. CHUCK, The Boeing Company, Mercer Island, WA1400AIAA-2010-0276 The Potential andChallenge ofTurboElectric Propulsionfor Subsonic TransportAircraft

A. Gibson, EmpiricalSystems Aerospace,Pismo Beach, CA

1430AIAA-2010-0277 Near Stall Flow Analysisin the Transonic Fan ofthe RTA PropulsionSystem

C. Hah, NASA GlennResearch Center,Cleveland, OH

1500AIAA-2010-0278 Statistical, ModularSystems IntegrationUsing Combined Energy& Exergy Concepts

J. Doty, University ofDayton, Dayton, OH

1530AIAA-2010-0279 Mission PerformanceComparisons ofSubsonic Airliners withCurrent and FuturePropulsion Technologies

B. Schiltgen, EmpiricalSystems Aerospace,Pismo Beach, CA

Chaired by: D. LEVY, Cessna Aircraft Company, Wichita, KS, and E. CRAMER, The Boeing Company, Seattle, WA1400AIAA-2010-0281 A Tradeoff Analysis ofFuture Small AircraftCapacity from a Point-to- Point OperationPerspective

J. Lewe, GeorgiaInstitute of Technology,Atlanta, GA

1430AIAA-2010-0282 Assessing New Aircraftand Technology Impactson Fleet- WideEnvironmental Metricsincluding FutureScenarios

J. Zhao, PurdueUniversity, WestLafayette, IN

1500AIAA-2010-0283 A Design Methodologyfor Lifelong AircraftEvolution

D. Lim, Georgia Instituteof Technology, Atlanta,GA

1530AIAA-2010-0284 Non- SymmetricalGeneral Aviation Aircraftand its Flight ControlLaw Design UsingCEASIOM Software

A. Khrabrov, TsAGI,Moscow, Russia

1600AIAA-2010-0285 Parameter Estimation ofFundamental TechnicalAircraft InformationApplied to AircraftPerformance

M. Vallone, CaliforniaPolytechnic StateUniversity, San LuisObispo, CA

Chaired by: W. MASON, Virginia Polytechnic Institute and State University, Blacksburg, VA, and T. TAKAHASHI, Northrop Grumman Corporation, El Segundo, CA1400AIAA-2010-0287 INVENT Modeling,Simulation, Analysis andOptimization

E. Walters, PCKA, WestLafayette, IN

1430AIAA-2010-0288 Thermal Analysis of anIntegrated Aircraft Model

M. Bodie, PCKA,Wright-Patterson AFB,OH

1500AIAA-2010-0289 Non- EquilibriumThermodynamic IssuesRelated to On- DemandSystems

M. von Spakovsky,Virginia PolytechnicInstitute and StateUniversity, Blacksburg,VA

1530AIAA-2010-0290 Dynamic HeatGeneration Modeling ofHigh PerformanceElectromechanicalActuator

D. Woodburn, Unviersityof Central Florida,Orlando, FL

1600AIAA-2010-0291 Simulation of EmergingHeat ExchangerTechnologies forProgressive AerospacePlatforms

A. Heltzel, PCKA,Austin, TX

1630AIAA-2010-0292 StochasticalMathematics forEngineering Applications

J. Doty, EngineeringManagement &Systems, University ofDayton, Dayton, OH

Chaired by: K. SHWEYK, The Boeing Company, Huntington Beach, CA, and A. CRASSIDIS, Rochester Institute of Technology, Rochester, NY


Monday Afternoon / 04 January 2010 Session 42-AFM-2 Flight Dynamics and Flying Qualities Chicago

Monday Afternoon / 04 January 2010 Session 43-AMT-2 Spectroscopic and Scattering Techniques Miami

Monday Afternoon / 04 January 2010 Session 44-AMT-3 Surface Measurement Techniques I Crystal Ballroom J1


Chaired by: K. SHWEYK, The Boeing Company, Huntington Beach, CA, and A. CRASSIDIS, Rochester Institute of Technology, Rochester, NY1400AIAA-2010-0293 Stability andPerformance of a LightUnmanned Airplane inGround Effect

P. Boschetti, SimónBolívar University,Naiguatá, Venezuela

1430AIAA-2010-0295 Developmental FlightTesting of the SPAAROUAV

M. Cotting, VirginiaPolytechnic Institute andState University,Blacksburg, VA

1500AIAA-2010-0297 Review of Pilot ModellingTechniques

M. Lone, CranfieldUniversity, Cranfield,Great Britain

1530AIAA-2010-0298 Evaluation of the FlyingQualities of a Half- ScaleUnmanned Airplane viaFlight Simulation

P. González, NationalPolytechnic ResearchUniversity of the ArmedForces , Caracas,Venezuela

Chaired by: T. ROSSMANN, and S. ZAIDI, Princeton University, Princeton, NJ1400AIAA-2010-0299 Tunable Diode LaserAbsorption TechniqueDevelopment forDetermination ofSpatially ResolvedWater Concentrationand Temperature

E. Bryner, University ofVirginia, Charlottesville,VA

1430AIAA-2010-0300 Quantitative Laser-Induced IncandescenceMeasurements of Sootin Turbulent Pool Fires

S. Kearney, SandiaNational Laboratories,Albuquerque, NM

1500AIAA-2010-0301 Fiber- BasedMeasurement of Bow-Shock Spectra forReentry Flight Testing

T. Schott, NASA LangleyResearch Center,Hampton, VA, VA

1530AIAA-2010-0302 Accuracy, Precision, andScatter in TDLASMeasurements

M. Brown, InnovativeScientific Solutions, Inc.,Dayton, OH

1600AIAA-2010-0303 Mass Flux Sensing viaTunable Diode LaserAbsorption of WaterVapor

L. Chang, StanfordUniversity, Stanford, CA

1630AIAA-2010-0304 Hypersonic FlowsProbing with a CompactAbsorption SpectrometerMonitoring CO2 at2.7µm

R. Vallon, ONERA,Palaiseau, France

Chaired by: V. CHANDRASEKHARAN, University of Florida, Gainesville, FL, and S. OLCMEN, University of Alabama, Tuscaloosa, AL1400AIAA-2010-0305 Measurement ofFluctuating WallPressures Beneath aSupersonic TurbulentBoundary Layer

S. Beresh, SandiaNational Laboratories,Albuquerque, NM

1430AIAA-2010-0306 MEMS Pressure SensorArray for AeroacousticAnalysis of the TurbulentBoundary Layer

J. Krause, TuftsUniversity, Medford, MA

1500AIAA-2010-0307 Unsteady PSPTechnique forMeasuring Naturally-Disturbed PeriodicPhenomena

D. Yorita, TohokuUniversity, Sendai,Japan

1530AIAA-2010-0309 Determination ofTransfer Function ofPressure- Sensitive Paint

C. Klein, GermanAerospace Center(DLR), Göttingen,Germany

1600AIAA-2010-0310 Measurement ofhypersonic high-enthalpy boundary layertransition on a 7º conemodel

H. Tanno, JapanAerospace ExplorationAgency (JAXA),Kakuda, Japan


Monday Afternoon / 04 January 2010 Session 45-APA-4 Applied CFD in Engineering Grand Ballroom 9

Monday Afternoon / 04 January 2010 Session 46-APA-5 Unsteady Aerodynamics I Grand Ballroom 10

Monday Afternoon / 04 January 2010 Session 47-APA-6 Vortical/Vortex Flows Grand Ballroom 11


Chaired by: J. MARTEL, Jacobs Engineering, Eglin AFB, FL, and S. LEDOUX, The Boeing Company, Everett, WA1400AIAA-2010-0311 Process ImprovementThrough Tool IntegrationIn Aero- MechanicalDesign

C. Briggs, ATAEngineering, San Diego,CA

1430AIAA-2010-0312 Rotor Wake Modelingwith a Coupled Eulerianand Vortex ParticleMethod

C. Stone, IntelligentLight, East Rutherford,NJ

1500AIAA-2010-0313 Computational Study ofAircraft Forebody Impacton Aerodynamic ForcesExperienced DuringPilot Ejection

C. Tyler, U.S. Air ForceResearch Laboratory,Wright-Patterson AFB,OH

1530AIAA-2010-0315 Loss CoefficientEstimation in aControlled DiffusionCascade Using LargeEddy Simulation

A. McMullan,LoughboroughUniversity,Loughborough, GreatBritain

1600AIAA-2010-0316 Development of aQuadtree BasedAgglomeration Methodfor a Multigrid ViscousFlow Solver onUnstructured Grids

E. Mahmutyazicioglu,TUBITAK-SAGE,Ankara, Turkey

Chaired by: J. GEORGE, Innovative Aerospace Solutions, Downey, CA, and W. TOLEDO, Army Research Development Engineering Center, Picatinny, NJ1400AIAA-2010-0317 Measurements of theSteady Skin Friction andCross- Flow SeparationLocation on anEllipsoidal Model in Yawor Pitch over a Range ofRoll Angles

J. DeMoss, VirginiaPolytechnic Institute andState University,Blacksburg, VA

1430AIAA-2010-0318 Aerodynamics of anOscillating Wing inGround Effect

J. Molina, University ofSouthampton,Southampton, GreatBritain

1500AIAA-2010-0319 Unsteady Force andMoment Measurementson a Non- Body ofRevolution VehicleUndergoing OscillatoryRoll

S. Tanious, VirginiaPolytechnic Institute andState University,Blacksburg, VA

1530AIAA-2010-0320 Experimental Study onDynamic Instability ofRe- Entry Capsule-Shaped Body usingPressure- Sensitive Paint

D. Sugimoto, TohokuUniversity, Sendai,Japan

1600AIAA-2010-0321 Vortex Structure AroundHeaving Elastic Airfoilsand Characteristics ofDynamic Thrust

T. Kurinami, KyushuInstitute of Technology,Iizuka, Japan

1630AIAA-2010-0322 Unsteady Aerodynamicsof Deformable ThinAirfoils

W. Walker, VirginiaPolytechnic Institute andState University,Blacksburg, VA

Chaired by: C. SHENG, University of Toledo, Toledo, OH, and R. TRAMEL, Kratos/Digital Fusion Solutions, Inc., Huntsville, AL1400AIAA-2010-0323 Effects of Leading- EdgeRadius on AerodynamicCharacteristics of 50ºDelta Wings

N. Verhaagen, DelftUniversity ofTechnology, Delft, TheNetherlands

1430AIAA-2010-0324 A Method andApplications for TrackingAirplane Trailing Wakes

Y. Yadlin, The BoeingCompany, HuntingtonBeach, CA

1500AIAA-2010-0325 Wind Tunnel Effects onWingtip Vortices

P. Durbin, Iowa StateUniversity, Ames, IA

1530AIAA-2010-0326 Experimental Studies onCo- Axial Vortex Loops

R. Mariani, University ofManchester,Manchester, GreatBritain

1600AIAA-2010-0327 Unsteady Computationsof a Ground Vortex

R. Nunes, University ofBeira Interior, Covilhã,Portugal

1630AIAA-2010-0328 Comparison ofPredictive Capabilities ofDES and RANSSimulations of theSeparated Flow Arounda Circular Cylinder

M. Xia, NorthwesternPolytechnical University,Xi'an, China (prc)


Monday Afternoon / 04 January 2010 Session 48-ASE-2 Space Flight Results and Lessons Learned Atlanta

Monday Afternoon / 04 January 2010 Session 49-ECS-1 Modeling the Performance of Energetic Materials Crystal Ballroom C

Monday Afternoon / 04 January 2010 Session 50-FD-7 Best Practice for the Industrial Application of Large Eddy Simulation (Invited) New Orleans


Chaired by: S. LAI, U.S. Air Force Research Laboratory, Hanscom AFB, MA, and D. FERGUSON, NASA Marshall Space Flight Center, Huntsville, AL1400AIAA-2010-0329 In- Situ O/N2 Ratiosfrom the AFRL MassSpectrometer on theTacSat- 2 Satellite

J. Wise, U.S. Air ForceResearch Laboratory,Hanscom AFB, MA

1430AIAA-2010-0332 The Effects of Eclipse-Exit Weather andMagnetic Latitude onISS Rapid- ChargingEvents

D. Ferguson, Air ForceResearchLaboratory/SpaceVehicles Directorate,Kirtland Air Force Base,NM

1500AIAA-2010-0333 Natural Environmentand AerospaceVehicles: Some LessonsLearned

W. Vaughan, Universityof Alabama, Huntsville,Huntsville, AL

1530AIAA-2010-1602 Flashover PlasmaCharacteristics on 5m2Solar Array Panels in aSimulated PlasmaEnvironment ofGeostationary Orbit andLow Earth Orbit

T. Okumura, JapanAerospace ExplorationAgency (JAXA),Tsukuba, Japan

Chaired by: J. BAGLINI, Exodynamics Technology, Inc., Phoenix, AZ1400AIAA-2010-0334 Modeling thePyrotechnically- InducedDissociation of NitrousOxide in Closed Vessels

K. Rink, University ofIdaho, Moscow, ID

1430AIAA-2010-0335 Preliminary Investigationof SPLA/RD- 1333 LeadAzide ThermalDecomposition Kinetics

H. Lee, ScotIncorporated, DownersGrove, IL

1500AIAA-2010-0336 Atomistic Simulation ofthe AluminumNanoparticle OxidationMechanism

B. Henz, U.S. ArmyResearch Laboratory,Aberdeen ProvingGround, MD

1530AIAA-2010-0337 Instrumented Burn Tube:ExperimentalObservations andAnalysis of Data

C. Yarrington, LosAlamos NationalLaboratory, Los Alamos,NM

Chaired by: P. TUCKER, Whittle Laboratory, Cambridge, Great Britain, and J. DEBONIS, NASA Glenn Research Center, Cleveland, OH1400Oral Presentation Status of Application ofLES for Gas TurbineAnalyses and FutureNeeds

J. Coupland,Rolls-Royce, Derby,Great Britain

1430Oral Presentation Best Practice forIndustrial LES- Lessonsfrom the Past andFuture Possibilities

A. Hutton, ERCOFTAC,Brussels, Belgium

1500Oral Presentation On Application of LargeEddy Simulations forGas TurbineCombustion System

S. Hsieh, GeneralElectric Company,Cincinnati, OH

1530Oral Presentation What Lessons Can BeLearned from LES Error-Landscapes?

J. Meyers, CatholicUniversity Leuven,Leuven, Belgium

1600Oral Presentation Towards ImprovedUnderstanding ofAirframe Noise SourcesUsing Detached EddySimulation

R. Langtry, The BoeingCompany , Seattle, WA

1630AIAA-2010-0343 Application of LESMethods to MilitaryAircraft Flow Problems

B. Smith, LockheedMartin Corporation, FortWorth, TX

Chaired by: M. ROGERS, NASA Ames Research Center, Moffett Field, CA, and R. WAHLS, NASA Langley Research Center, Hampton, VA


Monday Afternoon / 04 January 2010 Session 51-FD-8 Circulation Control Research and Applications Boston

Monday Afternoon / 04 January 2010 Session 52-FD-9 Compressible Turbulence Grand Ballroom 3

Monday Afternoon / 04 January 2010 Session 53-FD-10 Feedback Flow Control Grand Ballroom 4


Chaired by: M. ROGERS, NASA Ames Research Center, Moffett Field, CA, and R. WAHLS, NASA Langley Research Center, Hampton, VA1400AIAA-2010-0344 NASA High- ReynoldsNumber CirculationControl Research -Overview of CFD andPlanned Experiments(Invited)

W. Milholen, NASALangley ResearchCenter, Hampton, VA

1430AIAA-2010-0345 Recent ExperimentalDevelopment ofCirculation ControlAirfoils and PneumaticPowered- Lift Systems

R. Englar, GeorgiaInstitute of Technology,Atlanta, GA

1500AIAA-2010-0346 An ExperimentalInvestigation ofUnsteady and SteadyCirculation Control foran Elliptical Airfoil

A. Jones, University ofFlorida, Gainesville, FL

1530AIAA-2010-0347 Calculation of theTurbulenceCharacteristics of FlowAround a CirculationControl Airfoil Using LES(Invited Paper)

T. Nishino, NASA AmesResearch Center,Moffett Field, CA

1600AIAA-2010-0348 Overview of RecentCirculation ControlModeling Activities atCal Poly

D. Marshall, CaliforniaPolytechnic StateUniversity, San LuisObispo, CA

1630AIAA-2010-0349 Enabling Speed Agilityfor the Air Force

C. Zeune, U.S. Air ForceResearch Laboratory,Wright-Patterson AFB,OH

Chaired by: G. BLAISDELL, Purdue University, West Lafayette, IN, and W. KIM, Pratt & Whitney, A United Technologies Company, East Hartford, CT1400AIAA-2010-0350 Decay of CompressibleHomogeneousTurbulence with Multi-Temperature Non-Equilibrium

W. Liao, Old DominionUniversity, Norfolk, VA

1430AIAA-2010-0351 Detonation TurbulenceInteraction

L. Massa, University ofTexas, Arlington,Arlington, TX

1500AIAA-2010-0352 Numerical Simulation ofMulticomponent ShockAccelerated Flows andMixing using LocalizedArtificial DiffusivityMethod

S. Shankar, StanfordUniversity, Stanford, CA

1530AIAA-2010-0353 Direct numericalsimulation of hypersonicturbulent boundarylayers with varyingfreestream Mach number

L. Duan, PrincetonUniversity, Princeton, NJ

1600AIAA-2010-0354 Study of EmissionTurbulence- RadiationInteraction in HypersonicBoundary layers

L. Duan, PrincetonUniversity, Princeton, NJ

1630AIAA-2010-0355 DNS of a SpatiallyEvolvingTransitional/TurbulentBoundary Layer at M=2.0

Y. Tokura, HiroshimaUniversity, Hiroshima,Japan

Chaired by: J. SEIDEL, U.S. Air Force Academy, Colorado Springs, CO, and F. CANNELLE, Northrop Grumman Corporation, El Segundo, CA1400AIAA-2010-0356 Feedback Flow Controlof a Shear Layer forAero- Optic Applications

J. Seidel, U.S. Air ForceAcademy, ColoradoSprings, CO

1430AIAA-2010-0357 Feedback Control ofHigh- Lift State for ALow- Aspect- Ratio Wing

K. Taira, PrincetonUniversity, Princeton, NJ

1500AIAA-2010-0358 Closed- Loop Control ofa Wing in an UnsteadyFlow

D. Williams, IllinoisInstitute of Technology,Chicago, IL

1530AIAA-2010-0359 A Temporal ProperOrthogonalDecomposition (TPOD)Method for Closed-Loop Flow Control

S. Gordeyev, Universityof Notre Dame, NotreDame, IN

1600AIAA-2010-0360 Feedback Flow Controlfor a Pitching Turret(Part I)

T. Vaithianathan, ClearScience Corporation,Harford, NY

1630AIAA-2010-0361 Feedback Flow Controlfor a Pitching Turret(Part II)

R. Wallace, SyracuseUniversity, Syracuse, NY

Chaired by: C. RUMSEY, NASA Langley Research Center, Hampton, VA, and N. DOMEL, Lockheed Martin Corporation, Aledo, TX


Monday Afternoon / 04 January 2010 Session 54-FD-11 High Order Methods I Grand Ballroom 5

Monday Afternoon / 04 January 2010 Session 55-FD-12 Injection/Mixing Flows for Combustion Crystal Ballroom F

Monday Afternoon / 04 January 2010 Session 56-FD-13 Instability and Transition: Effects of Roughness Tampa


Chaired by: C. RUMSEY, NASA Langley Research Center, Hampton, VA, and N. DOMEL, Lockheed Martin Corporation, Aledo, TX1400AIAA-2010-0362 A HybridizableDiscontinuous GalerkinMethod for theIncompressible Navier-Stokes Equations

N. Nguyen,Massachusetts Instituteof Technology,Cambridge, MA

1430AIAA-2010-0363 A HybridizableDiscontinuous GalerkinMethod for theCompressible Euler andNavier- Stokes Equations

J. Peraire,Massachusetts Instituteof Technology,Cambridge, MA

1500AIAA-2010-0364 A ReconstructedDiscontinuous GalerkinMethod for theCompressible Navier-Stokes Equations onArbitrary Grids

H. Luo, North CarolinaState University,Raleigh, NC

1530AIAA-2010-0365 Automated Quadrature-Free DiscontinuousGalerkin Method with aTailored RecoveryFormulation

M. Galbraith, Universityof Cincinnati, Cincinnati,OH

1600AIAA-2010-0366 A ParallelReconstructedDiscontinuous GalerkinMethod forCompressible Flows onArbitrary Grids

H. Luo, North CarolinaState University,Raleigh, NC

1630AIAA-2010-0367 Unsteady DiscreteAdjoint Formulation forHigh- orderDiscontinuous GalerkinDiscretizations in Time-dependent FlowProblems

L. Wang, University ofTennessee,Chattanooga ,Chattanooga, TN

Chaired by: D. CULLEY and N. GEORGIADIS, NASA Glenn Research Center, Cleveland, OH1400AIAA-2010-0368 Effect of Cup Length onFilm Profiles in Gas-Centered Swirl- CoaxialInjectors

S. Schumaker, U.S. AirForce ResearchLaboratory, EdwardsAFB, CA

1430AIAA-2010-0370 LES/RANS Simulationof a SupersonicReacting Wall Jet

J. Edwards, NorthCarolina StateUniversity, Raleigh, NC

1500AIAA-2010-0371 Contrast BetweenSteady and Time-Averaged UnsteadyCombustion Simulations

C. Lian, PurdueUniversity, WestLafayette , IN

1530AIAA-2010-0372 A Ghost Fluid, Level SetApproach for ModelingElectrohydrodynamicAtomization

B. Van Poppel, Universityof Colorado, Boulder,Boulder, CO

Chaired by: G. DALE, U.S. Air Force Research Laboratory, Wright-Patterson AFB, OH, and A. DRAKE, Northrop Grumman Corporation, El Segundo, CA1400AIAA-2010-0373 An Approach toMeasuring StepExcrescence Effects inthe Presence of aPressure Gradient

A. Bender, NorthropGrumman Corporation,El Segundo, CA

1430AIAA-2010-0374 Hot- WireMeasurements of theInfluence of SurfaceSteps on Transition inFavorable PressureGradient BoundaryLayers

S. Gerashchenko,California Institute ofTechnology, Pasadena,CA

1500AIAA-2010-0375 Step ExcrescenceEffects forManufacturingTolerances on LaminarFlow Wings

A. Drake, NorthropGrumman Corporation,El Segundo, CA

1530AIAA-2010-0376 Effect of Three-Dimensional SurfacePerturbations onBoundary LayerTransitionalCharacteristics

J. Early, Queen'sUniversity Belfast,Belfast, Northern Ireland

1600AIAA-2010-0377 Direct NumericalSimulation of DistributedRoughness on a SweptWing Leading Edge

D. Rizzetta, U.S. AirForce ResearchLaboratory,Wright-Patterson AFB,OH

1630AIAA-2010-0378 Excitation of CrossflowInstabilities in a SweptWing Boundary Layer

M. Carpenter, NASALangley ResearchCenter, Hampton, VA


Monday Afternoon / 04 January 2010 Session 57-FD-14 Joseph A. Schetz Invited Session: Celebrating 45 Years of Graduate Education Grand Ballroom 2

Monday Afternoon / 04 January 2010 Session 58-FD-15 Pitching and Plunging Wing Aerodynamics Crystal Ballroom B

Monday Afternoon / 04 January 2010 Session 59-GPSE-2 NASA ISS Research Program Overviews Grand Ballroom 6


Chaired by: W. PULLIAM, Defense Advanced Research Projects Agency, Arlington, VA, and S. MAGILL, Talon Aircraft Holding GmbH, Myrtle Beach, SC1400AIAA-2010-0379 Studies of Diamond-Shaped Injectors in aSupersonic Flow (InvitedPresentation)

R. Srinivasan, RamgenPower Systems,Bellevue, WA

1430AIAA-2010-0380 Injectant MolecularWeight Effects inInjectors for CircularScramjet Combustors

C. Rock, VirginiaPolytechnic Institute andState University,Blacksburg, VA

1500AIAA-2010-0382 Study of Bow- ShockWave Unsteadiness inHypervelocity Flow fromReservoir Fluctuations

E. Marineau, CUBRC,Buffalo, NY

1530AIAA-2010-0383 Adaptivity andUncertainty: TowardsRigorous Veri cation andValidation of FlowSimulations

D. Pelletier, ÉcolePolytechnique deMontréal , Montréal,Canada

1600AIAA-2010-0384 Fabri Choking in a Two-Dimensional ReactingFlow Mixer- Ejector

D. DeTurris, CaliforniaPolytechnic StateUniversity, San LuisObispo, CA

Chaired by: M. OL, U.S. Air Force Research Laboratory, Wright-Patterson AFB, OH, and H. DONG, Wright State University, Dayton, OH1400AIAA-2010-0385 Computation andExperiments on a LowAspect Ratio PitchingFlat Plate

Y. Lian, University ofLouisville, Louisville, KY

1430AIAA-2010-0386 Lift Enhancement of aRectangular WingUndergoing a SmallAmplitude PlungingMotion

D. Calderon, Universityof Bath, Bath, GreatBritain

1500AIAA-2010-0387 Low Reynolds NumberUnsteady Aerodynamicover a Pitching-Plunging Flat Plate

A. Hart, University ofFlorida, Shalimar, FL

1530AIAA-2010-0388 Experimental Study ofGoverning Parametersin Pitching and PlungingAirfoil at Low ReynoldsNumber

Y. Baik, University ofMichigan, Ann Arbor, MI

1600AIAA-2010-0389 Effect of Aspect Ratioon Rigid Lifting FlatPlates in Pitch- PlungeMotion at Low ReynoldsNumbers

J. Rausch, University ofMichigan, Ann Arbor, MI

1630AIAA-2010-0390 Vortex Mode Bifurcationand Lift Force of aPlunging Airfoil at LowReynolds Numbers

D. Cleaver, University ofBath, Bath, Great Britain

Chaired by: S. TSE, Rutgers University, Piscataway, NJ, and F. KOHL, NASA Glenn Research Center, Cleveland, OH1400Oral Presentation Science on theInternational SpaceStation in the Final Yearof Assembly

J. Robinson, NASAJohnson Space Center,Houston, TX

1430Oral Presentation ISS Research in FluidPhysics and Transport:Status, Recent Resultsand Future Plans

B. Motil, NASA GlennResearch Center,Cleveland, OH

1500Oral Presentation Microgravity Combustionand Reacting Systems:Status, Recent Results,Plans, and Applicationsto Exploration Systems

D. Urban, NASA GlennResearch Center,Cleveland, OH

1530Oral Presentation US Materials Science onISS: Status and Plans

F. Szofran, NASAMarshall Space FlightCenter, Huntsville, AL

1600Oral Presentation Fundamental SpaceBiology: Past, Present,and Future

S. Sun, NASA AmesResearch Center, MoffetField, CA

1630Oral Presentation Status on CurrentSpaceflight and Ground-Based NASA PlantStudies

H. Levine, NASAKennedy Space Center,Cape Canaveral, FL

Chaired by: R. WHITE, ViGYAN Inc, Hampton, VA, and T. WAYMAN, Gulfstream Aerospace Corporation, Richmond Hill, GA


Monday Afternoon / 04 January 2010 Session 60-GT-2 Aerodynamic Ground Testing Crystal Ballroom G1

Monday Afternoon / 04 January 2010 Session 61-GTE-2 Gas Turbine Engines - Turbines I Grand Ballroom 13

Monday Afternoon / 04 January 2010 Session 62-GTE-31400 - 1700 Pressure-Gain Combustion for the Gas Turbine (Invited) Grand Ballroom 14

Chaired by: R. WHITE, ViGYAN Inc, Hampton, VA, and T. WAYMAN, Gulfstream Aerospace Corporation, Richmond Hill, GA1400AIAA-2010-0397 Aerodynamics ofVertical- Axis WindTurbines: Assessmentof Accepted WindTunnel Blockage Practice

I. Ross, University ofDayton, Dayton, OH

1430AIAA-2010-0398 Influence of WingElasticity on DynamicDerivatives of TransportAircraft

T. Loeser, DNW,Braunschweig, Germany

1500AIAA-2010-0399 Boundary Layer Trips forLow Reynolds NumberWind Tunnel Tests

A. Rona, University ofLeicester, Leicester,Great Britain

1530AIAA-2010-0400 Unstable at All Speeds:Flight Testing the 1903Wright FlyerReproduction in 2003

N. Crabill, ViGYAN, Inc.,Hampton, VA

1600Oral Presentation Transonic TunnelComparison Test

S. Helland, NASAGlenn Research Center,Cleveland, OH

1630AIAA-2010-0401 WITHDRAWN Exploring the Effects ofFreestream Turbulenceon Sphere DragTransition

C. Lamb, MassachusettsInstitute of Technology,Arlington, MA

Chaired by: I. HALLIWELL, Avetec, Springfield, OH, and R. GAETA, Georgia Institute of Technology, Smyrna, GA1400AIAA-2010-0403 Prediction of HeatTransfer Characteristicsof Turbine RotorPedestal Arrays

T. Barber, University ofConnecticut, Storrs, CT

1430AIAA-2010-0404 Prediction of AdiabaticEffectiveness of VariousCratered Film HoleConfigurations:Sensitivity Analysis forthe Rectangle ShapedMask

N. Tran, University ofCentral Florida, Orlando,FL

1500AIAA-2010-0405 Numerical andExperimental Study ofTrenched Film HoleCooling for a RealisticCascade in an AnnularEndwall, Phase1: TestRig Construction andPreliminary Data

C. Nguyen, University ofCentral Florida, Orlando,FL

1530AIAA-2010-0406 Effect of Hole Shape onBlade CoolingEffectiveness

J. Yao, KingstonUniversity, London,Great Britain

1600AIAA-2010-0408 Effects of IncidenceAngle on thePerformance of LightlyLoaded Turbine GuideVanes

F. Ames, University ofNorth Dakota, GrandForks, ND

There has been significant recent progress in developing non-steady pressure-gain combustors to enable engines to reduce fuel consumption and boost performance significantly. The theoretical potential ofconstant-volume combustion has led to investigation of various devices that approach this ideal, such as pulse detonation engines, wave rotors, and pulse combustors. This session aims to provide anoverview of the advantages and challenges of these combustors, and the needed research to make them successful in gas turbine and aircraft engine core applications.

Panelists:

Dr. Razi Nalim, Purdue University, Indianapolis, IN - co-chair

Dr. Daniel Paxson, NASA Glenn Research Center, Cleveland, OH: "Background, Motivation, History, Performance Metrics, Scope" - co-chair

Dr. Peter Strakey, DoE National Energy Technology Laboratory, Morgantown, WV: "Pressure-Gain Combustion for Power Generation Gas Turbines, Activities at NETL"

Dr. Robert Miller, University of Cambridge, United Kingdom: "Pressure-Gain Combustion for Aircraft Gas Turbines, Activities in the UK and Europe"

Dr. Philip Snyder, Rolls Royce Liberty Works, Indianapolis, IN: "Wave Rotor Combustion, Activities at Rolls Royce/IUPUI/Purdue and ABB"

Dr. K. Kailasanath, Naval Research Laboratory, Washington, DC: "Detonation Engine Progress Review, and Application to Gas Turbines and Propulsion"

Monday Afternoon / 04 January 2010 Session 63-HAPB-2 Ramjet/Scramjet Simulation with URANS/LES/DES I Grand Ballroom 12

Monday Afternoon / 04 January 2010 Session 64-IS-1 Intelligent Flight Planning and Guidance Crystal Ballroom Q

Monday Afternoon / 04 January 2010 Session 65-PC-5 Drops and Sprays I Los Angeles


Chaired by: B. SEKAR, U.S. Air Force Research Laboratory, Wright-Patterson AFB, OH, and D. KIRK, Florida Institute of Technology, Melbourne, FL1400AIAA-2010-0409 Ignition Transient in anEthylene FueledScramjet Engine with AirThrottling Part I: Non-Reacting flowDevelopment and Mixing

V. Yang, PennsylvaniaState University, StateCollege, PA

1430AIAA-2010-0410 Ignition Transient in anEthylene FueledScramjet Engine with AirThrottling Part II: Ignitionand Flame Development

V. Yang, PennsylvaniaState University, StateCollege, PA

1500AIAA-2010-0411 Supersonic CombustorFuel InjectionSimulations Using aHybrid RANS/LESApproach

D. Peterson, Universityof Minnesota,Minneapolis, MN

1530AIAA-2010-0412 Three DimensionalAnalysis of a FullyCoupled Hypersonic Air-breathing Inlet-Combustor Flowpath

F. Malo-Molina, U.S. AirForce ResearchLaboratory,Wright-Patterson AFB,OH

1600AIAA-2010-0414 Large- Eddy Simulationof Cavity Flame- Holdingin a Mach 2.5 CrossFlow

J. Choi, Georgia Instituteof Technology, Atlanta,GA

Chaired by: L. LONG, Pennsylvania State University, University Park, PA, and E. ATKINS, University of Michigan, Ann Arbor, MI1400AIAA-2010-0415 3- D Flight Plan for anAutonomous Aircraft

Y. Bestaoui, Universityof Evry, Evry, France

1430AIAA-2010-0416 Trim State Discovery foran Adaptive FlightPlanner

G. Yi, Harbin Institute ofTechnology, Harbin,China (prc)

1500AIAA-2010-0417 Effectiveness of 2D PathPlanning in Real Timeusing Fuzzy Logic

C. Sabo, University ofCincinnati, Cincinnati,OH

1530AIAA-2010-0418 Dynamic Flight PlanDesign for UAS RemoteSensing Applications

M. Sole, TechnicalUniversity of Catalonia,Barcelona, Spain

1600AIAA-2010-0420 Synergistic Computing:Combining CFD andNeural Networks forManeuvering Simulation

W. Faller, AppliedSimulationTechnologies, CocoaBeach, FL

Chaired by: J. GREENBERG, Technion--Israel Institute of Technology, Haifa, Israel, and P. LE CLERCQ, German Aerospace Center (DLR), Stuttgart, Germany1400AIAA-2010-0421 Droplet Burning of JP-8/Silica Gels

R. Arnold, PurdueUniversity, WestLafayette, IN

1430AIAA-2010-0422 Comparison ofMonomethylhydrazine/Hydroxypropylcelluloseand Hydrocarbon/SilicaGels


1500AIAA-2010-1595 Design and testing of aporous injector head fortranspiration cooledcombustion chambers

J. Deeken, GermanAerospace Center(DLR),Lampoldshausen,Germany

1530AIAA-2010-0425 Edge Flames with a FuelSpray and ReactantsHaving DifferentDiffusivities

J. Greenberg,Technion--Israel Instituteof Technology, Haifa,Israel

1600AIAA-2010-0426 Decomposition andIgnition Characteristicsof Liquid GAP

R. Kaya, NihonUniversity, Funabashi,Japan


Monday Afternoon / 04 January 2010 Session 66-PC-6 Turbulent Flames II New York

Monday Afternoon / 04 January 2010 Session 67-PDL-4 Aero-Optics Crystal Ballroom E

Monday Afternoon / 04 January 2010 Session 68-SAT-1 Society and Aerospace Sciences Denver

Due to formatting reasons, this version of the program lists only the first contributing author of each meeting paper. For a complete and up-to-date listing, please visit:

http://www.aiaa.org/agenda.cfm?lumeetingid=1812&dateget=all#session12890.

Chaired by: H. IM, University of Michigan, Ann Arbor, MI, and C. CADOU, University of Maryland, College Park, MD1400AIAA-2010-0428 The Effects of VariedOctane Rating on aSmall Spark IgnitionInternal CombustionEngine

C. Wilson, U.S. AirForce Institute ofTechnology,Wright-Patterson AFB,OH

1430AIAA-2010-0429 Simulations of theChemicalTransformations In a JetEngine Exhaust Plume

A. Garmory, Universityof Cambridge,Cambridge, Great Britain

1500AIAA-2010-0430 WITHDRAWN A Study of Lean Direct-Injection Flames UnderPressurized Conditions

R. Villalva Gomez,University of Cincinnati,Cincinnati, OH

1530AIAA-2010-0431 Swirling Flame Dynamicsand Describing Function

P. Palies, École CentraleParis,Chatenay-Malabry,France

Chaired by: D. CARROLL, CU Aerospace, Champaign, IL, and J. HORKOVICH, Raytheon Company, Tucson, AZ1400AIAA-2010-0433 High Fidelity Aero-Optical Analysis

M. White, U.S. Air ForceResearch Laboratory,Wright-Patterson AFB,OH

1430AIAA-2010-0434 Aero- OpticalMeasurements in aHeated, Subsonic,Turbulent BoundaryLayer

J. Cress, University ofNotre Dame, NotreDame, IN

1500AIAA-2010-0435 Aero- Optic Effects of aWing Tip Vortex

C. Porter, University ofNotre Dame, NotreDame, IN

1530AIAA-2010-0436 Use of Plasma Actuatorsto Force Shear LayerInstabilities

K. Schjodt, U.S. AirForce Academy,Colorado Springs, CO

1600AIAA-2010-0437 Aerodynamic Design ofan Aircraft- Mounted Podfor Improved Aero-Optic Performance

M. Rennie, University ofNotre Dame, NotreDame, IN

1630AIAA-2010-0438 Hybrid Flow Control of aTurret Wake, Part II:Aero- Optical Effects

S. Gordeyev, Universityof Notre Dame, NotreDame, IN

Chaired by: S. O'BRIEN, Embry-Riddle Aeronautical University, Daytona Beach, FL, and J. CHRISTIAN, University of Texas, Austin, Austin, TX

Chaired by: C. MOEN, Sandia National Laboratories, Livermore, CA, and F. JABERI, Michigan State University, East Lansing, MI1400 1430 1500


Monday Afternoon / 04 January 2010 Session 279-TES-6 Numerical Simulation I Crystal Ballroom A

Monday Afternoon / 04 January 2010 Session 69-TP-3 Aerothermodynamics I Crystal Ballroom M

Monday Afternoon / 04 January 2010 Session 70-TP-4 Direct Simulation Monte Carlo Methods I Crystal Ballroom N


Chaired by: C. MOEN, Sandia National Laboratories, Livermore, CA, and F. JABERI, Michigan State University, East Lansing, MI1400AIAA-2010-1553 A WENO- Z BasedEulerian- LagrangianCode for Simulation ofShocked Flows Ladenwith EvaporatingDroplets.

J. Meijerink, San DiegoState University, SanDiego, CA

1430AIAA-2010-1554 Modeling of FlowRegimes and ThermalPatterns Interactions inComplex Applications

E. Khalil, CairoUniversity, Cairo, Egypt

1500AIAA-2010-1555 AFTC: A Computer Codefor General Fuel- AirCombustion of Waste forEnergy Production withMinimal Pollution

D. Lilley, Lilley &Associates, Stillwater, OK

Chaired by: N. DOUGHERTY, Jacobs Engineering, Huntsville, AL, and J. KAPAT, University of Central Florida, Oviedo, FL1400AIAA-2010-0443 A Review ofAerothermal Modelingfor Mars Entry Missions

M. Wright, NASA AmesResearch Center,Moffett Field, CA

1430AIAA-2010-0444 A Computational Studyof High Enthalpy FlowOver a Rearward FacingStep

D. Narayan Ramanath,University of New SouthWales at the AustralianDefence ForceAcademy, Canberra,Australia

1500AIAA-2010-0445 Results & Analysis ofLarge Scale ArticleTesting in the Ames 60MW Interaction HeatingArc Jet Facility

M. Loomis, NASA AmesResearch Center,Moffett Field, CA

1530AIAA-2010-0446 Apollo- Shaped CapsuleBoundary LayerTransition at High-Enthalpy in T5

E. Marineau, CUBRC,Buffalo, NY

1600AIAA-2010-0447 Parameter SensitivityAnalysis for HypersonicViscous Flow Using aDiscrete AdjointApproach

B. Lockwood, Universityof Wyoming, Laramie,WY

Chaired by: D. GOLDSTEIN, University of Texas, Austin, Austin, TX, and E. TITOV, Pennsylvania State University, University Park, PA1400AIAA-2010-0449 Treatment of ElectronicEnergy Level Transitionand Ionization Followingthe Particle- BasedChemistry Model

D. Liechty, NASALangley ResearchCenter, Hampton, VA

1430AIAA-2010-0450 A Three- LevelCartesian Geometry-Based Implementationof the DSMC Method

D. Gao, University ofMinnesota, Minneapolis,MN

1500AIAA-2010-0451 Parallel Implementationof the Direct SimulationMonte Carlo Method ForShared MemoryArchitectures

D. Gao, University ofMinnesota, Minneapolis,MN

1530AIAA-2010-0989 State- to- StateTransition and Non-Equilibrium ChemicalReaction in DirectSimulation Monte CarloMethod

J. Kim, KAIST, Daejeon,South Korea


Monday Afternoon / 04 January 2010 Session 71-TP-5 Orbiter Entry Aerothermo Flight Experiments: Orbiter Computational Analyses Crystal Ballroom P

Monday Afternoon / 04 January 2010 Session 72-WE-2 Wind Turbine Aerodynamics Modeling and Analysis Crystal Ballroom G2

Monday Afternoon / 04 January 2010 Session 73-WIG-3 / PDL-5 Joint PDL/WIG/FD/TP Plasma Actuator Session II Grand Ballroom 1


Chaired by: M. CHOUDHARI, NASA Langley Research Center, Hampton, VA, and J. PAYNE, Sandia National Laboratories, Albuquerque, NM1400AIAA-2010-0453 Numerical Simulationsof the Boundary LayerTransition FlightExperiment

C. Tang, NASA AmesResearch Center,Moffett Field, CA

1430AIAA-2010-0454 Comparison of CFDPredictions with ShuttleGlobal Flight ThermalImagery and DiscreteSurface Measurements

W. Wood, NASALangley ResearchCenter, Hampton, VA

1500AIAA-2010-0455 Hypersonic NavierStokes Comparisons toOrbiter Flight Data

G. Candler, University ofMinnesota, Minneapolis,MN

1530AIAA-2010-0456 Effects of Rarefaction onHypersonic BoundaryLayer Flow OverDiscrete SurfaceRoughness

K. Stephani, Universityof Texas, Austin, Austin,TX

1600AIAA-2010-0457 Orbiter Boundary LayerStability Analysis atFlight Entry Conditions

H. Johnson, Universityof Minnesota,Minneapolis, MN

1630AIAA-2010-0458 Boundary LayerProtuberanceSimulations in ChannelNozzle Arc Jet

J. Marichalar, JacobsTechnology, Houston, TX

Chaired by: J. LAURSEN, Siemens, Brande, Denmark, and C. VAN DAM, University of California, Davis, Davis, CA1400AIAA-2010-0459 Hybrid RANS/LESSimulations of aHorizontal Axis WindTurbine

C. Stone, ComputationalScience & Engineering,Athens, GA

1430AIAA-2010-0460 ComputationalPredictions of AirfoilRoughness Sensitivity

K. Standish, Siemens,Boulder, CO

1500AIAA-2010-0461 Using the ActuatorSurface Method toModel the Three- BladedMexico Wind Turbine

S. Breton, École deTechnologie Supérieure,Montréal, Canada

1530AIAA-2010-0462 Validating BEM, Directand Inverse Free WakeModels with theMEXICO Experiment.

D. Micallef, University ofMalta, Msida, Malta

1600AIAA-2010-0463 Comparison of PotentialFlow Wake Models forHorizontal- Axis WindTurbine Rotors

S. Cline, University ofVictoria, Victoria, Canada

Chaired by: D. VAN WIE, Johns Hopkins University Applied Physics Laboratory, Laurel, MD, and N. YURCHENKO, National Academy of Sciences of Ukraine, Kiev, Ukraine1400AIAA-2010-0465 Rate of PlasmaThermalization ofPulsed NanosecondSurface DielectricBarrier Discharge

A. Starikovskii, DrexelUniversity, Philadelphia,PA

1430AIAA-2010-0467 Dielectric BarrierDischarge InitiationUnder the SupersonicAirflow

A. Saveliev, MoscowInstitute of Physics andTechnology,Dolgoprudny, Russia

1500AIAA-2010-0468 Separation ControlUsing Vectoring PlasmaActuators

S. Fleming, OklahomaState University,Stillwater, OK

1530AIAA-2010-0470 Limitations of the DBDeffects on the externalflow

A. Likhanskii, Tech-X,Boulder, CO

1600AIAA-2010-0469 Surface plasma inducedwall jets

D. Opaits, PrincetonUniversity, Princeton, NJ

D. Ian Poll


Monday Afternoon / 04 January 2010 1730 - 1830 2010 Dryden Lectureship In Research Crystal Ballroom H

Tuesday Morning / 05 January 2010 0800 - 0900 New Horizons Forum Keynote Address Crystal Ballroom H

Tuesday Morning / 05 January 2010

0900 - 1130 A New Horizons Forum Panel Discussion - Environment & Energy Issues forAerospace... Issues & Perspectives Crystal Ballroom J2


D. Ian PollProfessor of Aerospace EngineeringCranfield UniversityBedfordshire, United Kingdom

Distinguished Speaker: Dr. Steven E. Koonin, Under Secretary for Science, U.S. Department of Energy

Global Energy Challenges

The panel will discuss key issues affecting the aerospace community in the years ahead, including topics such as aerospace community impact on energy and environment – good and bad; the role ofaerospace systems in environmental assessment & change … climate & weather, natural disasters; power & propulsion – the changes ahead, among others.

Moderator: George K. Muellner, AIAA President 2008-2009, The Boeing Company, (Retired), USAF Lt. Gen. (Retired)

Panelists:

Rear Admiral David W. Titley, Oceanographer and Navigator of the Navy, Washington D.C.

David E. Parekh, Vice President, Research, and Director, United Technologies Research Center, Hartford CN

Ray O. Johnson, Senior Vice President and Chief Technology Officer, Lockheed Martin Corporation, Bethesda, MD

Chris J. Smith, Director of Operations, IDS Energy Solutions, The Boeing Company, Saint Louis, MO

The morning sessions are focused on personal development topics and activities focused on enhancing your career.

Chaired by: S. LELE, Stanford University, Stanford, CA0900 0930 1000 1030 1100 1130


Tuesday Morning / 05 January 2010

0900 - 1200 Career and Workforce Development Workshop - Laying the Foundation for the Futureof Aerospace I Crystal Ballroom G1

Tuesday Morning / 05 January 2010 Session 74-AA-5 Jet Noise II Washington

Tuesday Morning / 05 January 2010 Session 75-ABP-3 Inlets I Crystal Ballroom D


The morning sessions are focused on personal development topics and activities focused on enhancing your career.

Chaired by: S. LELE, Stanford University, Stanford, CA0900AIAA-2010-0471 Experimental andNumerical Investigationof Flow Properties ofSupersonic Helium- AirJets

S. Miller, NASA LangleyResearch Center,Hampton, VA

0930AIAA-2010-0472 Flight Effects onSupersonic Jet: Noise,Thrust, SourceDistribution and ShockPatterns

D. Long, Aero SystemsEngineering, St. Paul,MN

1000AIAA-2010-0473 Forward Flight Effectson the Shock StructureFrom a Chevron C- DNozzle

D. Munday, University ofCincinnati, Cincinnati,OH

1030AIAA-2010-0474 Effects of Jet NoiseSource Distribution onAcoustic Far- FieldMeasurements

C. Kuo, PennsylvaniaState University, StateCollege, PA

1100AIAA-2010-0475 Stability of the InnerNozzle Wake withRelevance to theCoannular JetAeroacoustics

S. Sarpotdar, IllinoisInstitute of Technology,Chicago, IL

1130AIAA-2010-0476 Acoustic Waves from aSupersonic JetImpinging on an InclinedFlat Plate

T. Nonomura, Universityof Tokyo, Sagamihara,Japan

Chaired by: D. MAYER, The Boeing Company, Kent, WA, and I. HALLIWELL, Avetec, Springfield, OH0900AIAA-2010-0477 Analysis of a ChanneledCenterbody SupersonicInlet for F- 15B FlightResearch

N. Ratnayake, NASADryden Flight ResearchCenter, Edwards AFB,CA

0930AIAA-2010-0479 Coupled Analysis of anInlet and Fan for a QuietSupersonic Jet

R. Chima, NASA GlennResearch Center,Cleveland, OH

1000AIAA-2010-0480 Flow Simulation ofSupersonic Inlet withBypass Annular Duct

H. Kim, NASA GlennResearch Center,Cleveland, OH

1030AIAA-2010-0481 Flow Field andPerformance Analysis ofan IntegratedDiverterless SupersonicInlet

J. Masud, IAA, AirUniversity, Islamabad,Pakistan

Chaired by: R. MCDONALD, California Polytechnic State University, San Luis Obispo, CA0900 0930 1000 1030


Tuesday Morning / 05 January 2010 Session 76-AD-3 Unmanned Aircraft Design Crystal Ballroom K

Tuesday Morning / 05 January 2010 Session 77-AFM-3 Flight Dynamics and Control Chicago

Tuesday Morning / 05 January 2010 Session 78-AMT-4 Shear Stress Measurement Technology II Crystal Ballroom J1


Chaired by: R. MCDONALD, California Polytechnic State University, San Luis Obispo, CA0900AIAA-2010-0482 MultidisciplinaryUnmanned Combat AirVehicle (UCAV) SystemDesign Using Multi-Fidelity Models

S. Choi, KonkukUniversity, Seoul, SouthKorea

0930AIAA-2010-0483 Validation of Models forSmall Scale ElectricPropulsion Systems

D. Lundström, LinköpingUniversity, Linköping,Sweden

1000AIAA-2010-0484 Experimental Validationof a FEA- Based ModelUsed for BucklingAnalysis of LoadStiffening Bendable UAVWings

A. Patil, University ofFlorida, Gainesville, FL

1030AIAA-2010-0485 Bioinspired UAV Wing

A. Bright, TuftsUniversity, Medford, MA

Chaired by: C. COX and M. BOLENDER, U.S. Air Force Research Laboratory, Wright-Patterson AFB, OH0900AIAA-2010-0488 The Influence of Free-Play and Friction inElevator Control Systemon Aircraft Dynamics

K. Sibilski, WroclawUniversity ofTechnology, Wroclaw,Poland

0930AIAA-2010-0489 Challenges and LessonsLearned FromResurrecting a LegacyResearch FlightController

C. Moua, NASA DrydenFlight Research Center,Edwards, CA

1000AIAA-2010-0490 Simulation and Controlof Fixed Wing AircraftAfter a MajorComponent Loss

U. Ozdemir, IstanbulTechnical University,Istanbul, Turkey

1030AIAA-2010-0491 Investigation ofAttainable EquilibriumSets for Clearance ofFlight Control Laws

N. Abramov, De MontfortUniversity, Leicester,Great Britain

1100AIAA-2010-0492 Using DescribingFunctions for Limit-Cycle- OscillationAnalysis Applied toAeroservoelastic Modelswith Free- Play

B. Danowsky, SystemsTechnology, Inc.,Hawthorne, CA

1130AIAA-2010-0493 3- D Formulation ofFormation Flight Basedon Model PredictiveControl with CollisionAvoidance Scheme

W. Zhao, NanyangTechnologicalUniversity, Singapore,Singapore

Chaired by: T. LIU, Western Michigan University, Kalamazoo, MI, and M. BENNE, The Boeing Company, St Louis, MO0900AIAA-2010-0494 Time- Resolved Wall-Shear Imaging onSurfaces Coated withArrays of Flexible Micro-Pillars (Invited)

C. Bruecker, TechnicalUniversity of Freiberg,Freiberg, Germany

0930AIAA-2010-0495 Measuring the Two-Dimensional, Two-Directional TemporalWall- Shear StressDistribution with theMicro- Pillar Shear-Stress Sensor MPS³(Invited)

S. Grosse, RWTHAachen University,Aachen, Germany

1000AIAA-2010-0497 Naval ManeuveringResearch and the Needfor Shear StressMeasurements (Invited)

D. Hess, Naval SurfaceWarfare Center,Bethesda, MD

1030AIAA-2010-0498 Optical Miniaturization ofa MEMS- BasedFloating Element ShearStress Sensor with MoiréAmplification

T. Chen, University ofFlorida, Gainesville, FL


Tuesday Morning / 05 January 2010 Session 79-APA-7 Applied CFD to Configurations and Experimental Validation Grand Ballroom 9

Tuesday Morning / 05 January 2010 Session 80-APA-8 Moving Body CFD Simulation I Grand Ballroom 10

Tuesday Morning / 05 January 2010 Session 81-APA-9 Unsteady Aerodynamics II Grand Ballroom 11


Chaired by: T. CHYCZEWSKI, Northrop Grumman Corporation, Bethpage, NY, and W. SICKLES, Arnold Engineering Development Center, Arnold AFB, TN0900AIAA-2010-0500 CFD Assessment ofAerodynamicDegradation of aSubsonic Transport Dueto Airframe Damage

N. Frink, NASA LangleyResearch Center,Hampton, VA

0930AIAA-2010-0501 Creation of AerodynamicDatabase for the X- 31

M. Tomac, KTH RoyalInstitute of Technology,Stockholm, Sweden

1000AIAA-2010-0502 Computational andExperimentalComparison of aPowered Lift, UpperSurface BlowingConfiguration

J. Marcos, CaliforniaPolytechnic StateUniversity, San LuisObispo, CA

1030AIAA-2010-0503 A MUSCL and WENO –PNS Approach forVortex DominatedFlowfields

D. de Feo, University ofSheffield, Sheffield,Great Britain

Chaired by: D. FINDLAY, Naval Air Systems Command, Patuxent River, MD, and J. MARTEL, Jacobs Engineering, Eglin AFB, FL0900AIAA-2010-0506 Flow Simulation ofTension Cone InflatableAeroshell with FluidStructure Interactions

V. Gidzak, University ofMinnesota, Minneapolis,MN

0930AIAA-2010-0507 WITHDRAWN Efficient AutomatedOverset AdaptiveCartesian/UnstructuredGrid Generation forObjects in CloseGeometrical Proximity

R. Kannan, CFDResearch Corporation,Huntsville, AL

1000AIAA-2010-0508 Hybrid CartesianGrid/Gridless Algorithmfor Store SeparationPrediction

L. Tang, D&P LLC,Phoenix, AZ

1030AIAA-2010-0509 Conservative UnsteadySimulation of ArbitraryBoundary DeformationUsing SpacetimeMeshes

T. Rendall, University ofBristol, Bristol, GreatBritain

1100AIAA-2010-0510 Store Separations in JetFlow Environments

J. Lee, Naval AirSystems Command,Patuxent River, MD

1130AIAA-2010-0511 Kestrel v2 - 6DoF andControl SurfaceAdditions to a CREATESimulation Tool

S. Morton, U.S. AirForce SEEK EAGLEOffice, Eglin AFB, FL

Chaired by: B. MCGRATH, Johns Hopkins University Applied Physics Laboratory, Laurel, MD0900AIAA-2010-0513 Simulation of theDynamic Stall at LowReynolds Number

C. Marongiu, ItalianAerospace ResearchCenter (CIRA), Capua,Italy

0930AIAA-2010-0514 Unsteady ConfinedViscous Flows withOscillating Walls andVariable Inflow Velocity

D. Mateescu, McGillUniversity, Montréal,Canada

1000AIAA-2010-0515 Improved Methodologiesfor Maneuver Design ofAircraft Stability andControl Simulations

A. Jirasek, U.S. AirForce Academy,Colorado Springs, CO

1030AIAA-2010-0516 WITHDRAWN Computational Analysisof Winglet Modificationson the KC- 135

M. Arndt, U.S. Air ForceAcademy, ColoradoSprings, CO


Tuesday Morning / 05 January 2010 Session 82-ASE-3 Quantifying and Modeling Atmospheric Phenomena Atlanta

Tuesday Morning / 05 January 2010 Session 83-CS-1 HPC I: GPU Applications and Benchmarking Tampa

Tuesday Morning / 05 January 2010 Session 84-ECS-2 Green Initiatives in the Development and Manufacture of Energetic Materials New York


Chaired by: W. VAUGHAN, University of Alabama, Huntsville, Huntsville, AL, and J. MURRAY, NASA Langley Research Center, Hampton, VA0900AIAA-2010-0518 Gust Load- Line AnalysisResearch of WakeVortex Encounter FlightData

A. Brown, NationalResearch CouncilCanada, Ottawa, Canada

0930AIAA-2010-0519 Analytical Approach toWake Vortex and JetWake Flow Interaction inCruising Flight

A. Brown, NationalResearch CouncilCanada, Ottawa, Canada

1000AIAA-2010-0520 The detection,characterization andtracking of recentAleutian Island volcanicash plumes and theassessment of theirimpact on aviation

J. Murray, NASA LangleyResearch Center,Hampton, VA

Chaired by: C. LI, Aerojet, Folsom, CA0900AIAA-2010-0522 An MPI- CUDAImplementation forMassively ParallelIncompressible FlowComputations on Multi-GPU Clusters

D. Jacobsen, BoiseState University, Boise,ID

0930AIAA-2010-0523 Porting of an Edge-Based CFD Solver toGPUs

A. Corrigan, GeorgeMason University,Fairfax, VA

1000AIAA-2010-0524 Using GPU on HPCApplications to SatisfyLow- PowerComputationalRequirement

G. Patnaik, NavalResearch Laboratory,Washington, DC

1030AIAA-2010-0525 Acceleration of a Finite-Difference WENOScheme for Large- ScaleSimulations on Many-Core Architectures

A. Antoniou, Universityof Patras, Patra, Greece

Chaired by: K. RINK, University of Idaho, Moscow, ID, and H. LEE, Scot Incorporated, Downers Grove, IL0900AIAA-2010-0528 PerformanceCharacterization ofNanoscale EnergeticMaterials onSemiconductor Bridges(SCBs)

G. Strohm, PurdueUniversity, WestLafayette, IN


Tuesday Morning / 05 January 2010 Session 85-EDU-2 Panels: The CDIO Approach and Industry Engagement in Engineering Education Crystal Ballroom Q

Tuesday Morning / 05 January 2010 Session 86-FD-16 Boundary Layer Transition I Grand Ballroom 2

Tuesday Morning / 05 January 2010 Session 87-FD-17 High Order Methods II Grand Ballroom 3


Chaired by: D. KRAUSCHE, Florida Center for Engineering Education, Gainesville, FL, and R. NIEWOEHNER, U.S. Naval Academy, Annapolis, MD0900AIAA-2010-0531 The Education of Future Aeronautical Engineers:Conceiving, Designing, Implementing andOperating

E. Crawley, Massachusetts Institute ofTechnology, Cambridge, MA

0945AIAA-2010-0532 North American Aerospace Project: CDIO inAerospace Engineering Education

E. Crawley, Massachusetts Institute ofTechnology, Cambridge, MA

1030Oral Presentation Panel Discussion: Industry Engagement inAerospace Education

R. Niewoehner, U.S. Naval Academy, Annapolis,MD

Chaired by: V. THEOFILIS, Technical University of Madrid, Madrid, Spain, and X. ZHONG, University of California, Los Angeles, Los Angeles, CA0900AIAA-2010-0534 Numerical Simulationand Theoretical Analysison HypersonicBoundary- LayerReceptivity to WallBlowing- Suction

A. Tumin, University ofArizona, Tucson, AZ

0930AIAA-2010-0535 Transient Growth of AMach 5.92 Flat- PlateBoundary Layer

X. Wang, University ofCalifornia, Los Angeles,Los Angeles, CA

1000AIAA-2010-0536 Investigation of theresponse of ahypersonic 2D boundarylayer to controlledacoustic disturbances

D. Heitmann, TechnicalUniversity ofBraunschweig,Braunschweig, Germany

1030AIAA-2010-0538 On the ComplexSpectrum BoundariesCalculation

S. Chernyshev, TsAGI,Zhukovsky, Russia

1100AIAA-2010-1367 Transition Experimentson Blunt Bodies withIsolated RoughnessElements in HypersonicFree Flight

D. Reda, NASA AmesResearch Center,Moffett Field, CA

Chaired by: M. MALIK, NASA Langley Research Center, Hampton, VA, and R. DAVIS, University of California, Davis, Davis, CA0900AIAA-2010-0539 A High- ResolutionMethod Using AdaptivePolynomial for LocalRefinement

J. Shang, Wright StateUniversity, Dayton, OH

0930AIAA-2010-0540 A High- Order UnifyingDiscontinuousFormulation for 3- DMixed Grids

T. Haga, Iowa StateUniversity, Ames, IA

1000AIAA-2010-0541 High- Order SpectralDifference Method forthe Navier- StokesEquation onUnstructured MovingDeformable Grid

K. Ou, StanfordUniversity, Stanford, CA

1030AIAA-2010-0542 On the Impact ofTriangle Shapes forBoundary LayerProblems Using High-Order Finite ElementDiscretization

H. Sun, MassachusettsInstitute of Technology,Cambridge, MA

1100AIAA-2010-0543 A New Approach forConstructing HighlyStable High OrderCESE Schemes

S. Chang, NASA GlennResearch Center,Cleveland, OH

1130AIAA-2010-0544 PreliminaryImplementation of a HighOrder Space- timeMethod on OversetCartesian/QuadrilateralGrids

S. Tu, Jackson StateUniversity, Jackson, MS

Chaired by: T. CORKE, University of Notre Dame, Notre Dame, IN, and E. STEPHEN, U.S. Air Force Academy, Colorado Springs, CO0900 0930 1000 1030


Tuesday Morning / 05 January 2010 Session 88-FD-18 Joint PDL/WIG/FD/TP Plasma Actuator Session III Grand Ballroom 4

Tuesday Morning / 05 January 2010 Session 89-FD-19 Low Reynolds Number and Bio-Inspired Aerodynamics I Grand Ballroom 5

Tuesday Morning / 05 January 2010 Session 90-FD-20 Unsteady Flows Crystal Ballroom B


Chaired by: T. CORKE, University of Notre Dame, Notre Dame, IN, and E. STEPHEN, U.S. Air Force Academy, Colorado Springs, CO0900AIAA-2010-0545 Effects of OxygenContent on the Behaviorof the Dielectric BarrierDischarge AerodynamicPlasma Actuator

G. Font, U.S. Air ForceAcademy, ColoradoSprings, CO

0930AIAA-2010-0547 Closed- Loop StallControl on a MorphingAirfoil Using Hot- FilmSensors and DBDActuators

J. Poggie, U.S. Air ForceResearch Laboratory,Wright-Patterson AFB,OH

1000AIAA-2010-0549 Flow Behavior Behind aCircular Cylinder byDBD Plasma Actuatorsin Low Reynolds Number

S. Yamada, TokyoUniversity of Science,Tokyo, Japan

1030AIAA-2010-0550 Low- Pressure Effectson a Single DBD PlasmaActuator

K. Bottelberghe, NorthDakota State University,Fargo, ND

Chaired by: A. ALTMAN, University of Dayton, Dayton, OH, and J. ELDREDGE, University of California, Los Angeles, Los Angeles, CA0900AIAA-2010-0551 Three- DimensionalEffects on a WavingWing

A. Jones, University ofCambridge, Cambridge,Great Britain

0930AIAA-2010-0552 Unsteady AerodynamicModels for Agile Flightat Low Reynolds Number

S. Brunton, PrincetonUniversity, Princeton, NJ

1000AIAA-2010-0553 Numerical Study ofFlexible Flapping WingPropulsion

T. Yang, New MexicoState University, LasCruces, NM

1030AIAA-2010-0554 A Computational andExperimental Studies ofFlexible WingAerodynamics

H. Aono, University ofMichigan, Ann Arbor, MI

1100AIAA-2010-0555 Computational Analysisof HoveringHummingbird Flight

Z. Liang, Wright StateUniversity, Dayton, OH

1130AIAA-2010-0556 A 3D ComputationalStudy of the Flow-Structure Interaction inFlapping Flight

H. Luo, VanderbiltUniversity, Nashville, TN

Chaired by: M. HONG, The Boeing Company, Seattle, WA, and J. LIN, NASA Langley Research Center, Hampton, VA0900AIAA-2010-0557 Development of AnIntegrated Aero- OpticsModeling Capability:OVERFLOW- AeroOptics

W. Coirier, Kratos/DigitalFusion Solutions, Inc.,Huntsville, AL

0930AIAA-2010-0558 Transverse Injection intoSubsonic Crossflow withVarious Injector OrificeGeometries

L. Foster, NASA GlennResearch Center,Cleveland, OH

1000AIAA-2010-0559 Vortex- SheddingMechanisms in InternalFlows

M. Boghosian, IllinoisInstitute of Technology,Chicago, IL

1030AIAA-2010-0560 LES of an OscillatingCylinder in a SteadyFlow

A. Feymark, ChalmersUniversity ofTechnology, Göteborg,Sweden

1100AIAA-2010-0561 Large Eddy Simulationof Pulsed Jet inCross?ow

A. Coussement,Université Libre deBruxelles, Brussels ,Belgium

1130AIAA-2010-0562 Visualization of aGround Vortex Flow

J. Barata, University ofBeira Interior, Covilhã,Portugal

Chaired by: W. KIM, Pratt & Whitney, A United Technologies Company, East Hartford, CT, and D. HITT, University of Vermont, Burlington, VT0900 0930 1000 1030


Tuesday Morning / 05 January 2010 Session 91-FD-21 Micro/Nano Fluidics I New Orleans

Tuesday Morning / 05 January 2010 Session 92-GPSE-3 Emerging Opportunities in Research Flights I Grand Ballroom 6

Tuesday Morning / 05 January 2010 Session 93-GT-3 / HIS-2 History of Wind Tunnels I Miami


Chaired by: W. KIM, Pratt & Whitney, A United Technologies Company, East Hartford, CT, and D. HITT, University of Vermont, Burlington, VT0900AIAA-2010-0563 A ComputationallyEfficient Framework forModeling Microscaleand Rarefied Gas FlowsBased on NewConstitutive Relations

R. Myong, GyeongsangNational University,Jinju, South Korea

0930AIAA-2010-0564 OscillatoryMagnetogasdynamicsSlip Flow in aMicrochannel

R. Agarwal, WashingtonUniversity in St. Louis,St. Louis, MO

1000AIAA-2010-0565 An Experimental Studyof Pulsed Micro- FlowsDriven by an InsulinPump

B. Wang, Iowa StateUniversity, Ames, IA

1030AIAA-2010-0567 WITHDRAWN Numerical FlowSolutions of a ValvelessMicropump

M. Galbraith, Universityof Cincinnati, Cincinnati,OH

Chaired by: S. COLLICOTT, Purdue University, West Lafayette, IN, and J. COHEN, NASA Headquarters, Washington, DC0900Oral Presentation Microgravity and OtherResearch ApplicationsUsing the EmergingHuman SuborbitalVehicles

A. Stern, SouthwestResearch Institute,Boulder, CO

0930Oral Presentation Space- X EmergingResearch Opportunities

E. Spengler, Space-X,Hawthorne, CA

1000Oral Presentation Armadillo AerospaceUpdate

N. Milburn, ArmadilloAerospace, Rockwall, TX

Chaired by: V. CANACCI, and S. EBERHARDT, The Boeing Company, Seattle, WA, and S. SMITH-BRITO, The Boeing Company, Bellevue, WA0900Oral Presentation History of UWAL

S. Eberhardt, TheBoeing Company,Seattle, WA

0930Oral Presentation History of Wind Tunnelsas They HaveInfluenced Specific AirVehicle Development

S. Smith-Brito, TheBoeing Company,Bellevue, WA

1000Oral Presentation National Full- ScaleAerodynamics Complex,NFAC

J. Van Aken, JacobsTechnology, MoffettField, CA

1030AIAA-2010-0575 DNW- HST (High SpeedTunnel) 50- YearAnniversary

I. Philipsen,German-Dutch WindTunnels (DNW),Emmeloord, TheNetherlands

1100Oral Presentation History of ArnoldEngineeringDevelopment CenterWind Tunnels

M. Mills , ArnoldEngineeringDevelopment Center,Arnold AFB, TN

1130Oral Presentation A Brief History ofSandia's Wind Tunnels,and a Look to the Future

S. Beresh, SandiaNational Laboratories,Albuquerque, NM

Chaired by: J. COHEN, United Technologies Research Center, East Hartford, CT, and M. IHME, University of Michigan, Ann Arbor, MI


Tuesday Morning / 05 January 2010 Session 94-GTE-4 Gas Turbine Combustion Grand Ballroom 13

Tuesday Morning / 05 January 2010 Session 95-GTE-5 Gas Turbine Materials Crystal Ballroom E

Tuesday Morning / 05 January 2010 Session 96-GTE-6 Large CFD Simulations of Engine Components (Invited) Grand Ballroom 14


Chaired by: J. COHEN, United Technologies Research Center, East Hartford, CT, and M. IHME, University of Michigan, Ann Arbor, MI0900AIAA-2010-0578 Comparing SprayCharacteristics fromRANS NCC CalculationsAgainst ExperimentalData for a TurbulentReacting Flow

A. Iannetti, NASA GlennResearch Center,Cleveland, OH

0930AIAA-2010-0579 Gas Turbine SingleAnnular CombustorSector Aerodynamics

B. Mohammad,University of Cincinnati,Cincinnati, OH

1000AIAA-2010-0580 A Transonic Vane foruse Downstream of aPressure GainCombustor

J. Heffer, WhittleLaboratory, Cambridge,Great Britain

1030AIAA-2010-0581 Effect of Vane Notchand Ramp Design onthe Performance of aRectangular Inter-Turbine Burner

A. Briones, University ofDayton ResearchInstitute, Dayton, OH

1100AIAA-2010-0583 A Numerical Study ofFlow Dynamics in anAnnular Combustor withMultiple Swirl Injectors

H. Sung, KoreaAerospace University,Goyang, South Korea

1130AIAA-2010-0584 Proper OrthogonalDecomposition forExperimentalInvestigation of SwirlingFlame Instabilities

P. Iudiciani, LundTechnical University,Lund, Sweden

Chaired by: J. KAPAT, University of Central Florida, Oviedo, FL0900AIAA-2010-0587 Crack- DetectionExperiments onSimulated TurbineEngine Disks in NASAGlenn ResearchCenter's RotordynamicsLaboratory

M. Woike, NASA GlennResearch Center,Cleveland, OH

Chaired by: G. WELCH, U.S. Army Research Laboratory, Cleveland, OH, and M. HATHAWAY, NASA Glenn Research Center, Cleveland, OH0900AIAA-2010-1603 Aspects of NumericalAnalysis for UnsteadyFlows in Aircraft Engines

J. Yao, General ElectricCompany, Niskayuna,NY

0930AIAA-2010-1604 Flow Characteristics ofTip- Injection onCompressor RotatingInstability via Time-Accurate Simulation

J. Chen, Ohio StateUniversity, Columbus,OH

1000AIAA-2010-1605 Unstructured GridTechnology Applied toAxial- flow Compressors

R. Webster, University ofTennessee,Chattanooga,Chattanooga, TN

1030AIAA-2010-1606 Lessons Learned fromthe GE90 3- D FullEngine Simulations

M. Turner, University ofCincinnati, Cincinati, OH


Tuesday Morning / 05 January 2010 Session 97-HAPB-3 Supersonic Inlets Grand Ballroom 12

Tuesday Morning / 05 January 2010 Session 98-HS-1 Homeland Security Crystal Ballroom P

Tuesday Morning / 05 January 2010 Session 99-NSC-4 AIAA Foundation Graduate Student Awards Presentations Crystal Ballroom A


Chaired by: F. MALO-MOLINA, U.S. Air Force Research Laboratory, Wright-Patterson AFB, OH, and W. ENGBLOM, Embry-Riddle Aeronautical University, Daytona Beach, FL0900AIAA-2010-0588 Development of aLudwieg Tube with FreePiston CompressionHeating for ScramjetInlet StartingExperiments

D. Buttsworth, Universityof SouthernQueensland,Toowoomba, Australia

0930AIAA-2010-0589 Experimental andComputationalInvestigation of aDynamic Starting MethodforSupersonic/HypersonicInlets

R. Throckmorton,Virginia PolytechnicInstitute and StateUniversity, Blacksburg,VA

1000AIAA-2010-0590 Micro- VortexGenerators Applied to aFlow- Field Containing aNormal Shock- Waveand Diffuser

N. Titchener, CambridgeUniversity, Cambridge,Great Britain

1030AIAA-2010-0591 Effect of Reynoldsnumber on supersonicflow bleed

A. Hamed, University ofCincinnati, Cincinnati,OH

1100AIAA-2010-0592 LES for SupersonicRamp Control FlowUsing MVG at M=2.5and Re?=1440

Q. Li, University ofTexas, Arlington,Arlington, TX

Chaired by: J. BRADER, The Aerospace Corporation, Los Angeles, CA0900Oral Presentation Full- ScaleDemonstrations ofEnhanced Low- SpeedManeuverability Airshipsfor ISR Missions

B. Buerge, GuardianFlight Systems, LLC,Elizabeth City, NC

0930AIAA-2010-0594 Protection of CriticalInfrastructures: AMethodology forFacilitating Modelingand Simulation ofNotional Scenarios

A. Payan, GeorgiaInstitute of Technology,Atlanta, GA

1000AIAA-2010-0595 Fuzzy Counter AntAlgorithm for MazeProblem

M. Ahuja, University ofCincinnati, Cincinnati, OH

1030AIAA-2010-0597 The MonotonicLagrangian Grid for FastAir- Traffic Evaluation

C. Kaplan, NavalResearch Laboratory,Washington, DC

Chaired by: S. BROCK, American Institute of Aeronautics and Astronautics, Reston, VA0900Oral Presentation Advanced CombinedCycle PropulsionGraduate Award

D. Wood, University ofColorado, Boulder,Boulder, CO

0930Oral Presentation High Resolution OpticalMeasurements inAerodynamic andPropulsion SystemsGraduate Award

A. Bhuiyan, PurdueUniversity, WestLafayette, IN

1000Oral Presentation Hypervelocity ImpactGraduate Award

J. Mihaly, CaliforniaInstitute of Technology,Pasadena, CA

1030Oral Presentation John Leland AtwoodGraduate Award Winner- Optimal Control Theoryand ComputationalTechniques

X. Bai, Texas A&MUniversity, CollegeStation, TX

1100Oral Presentation High Energy Ions inElectric ThrustersGraduate Award

J. Przybylowski ,California Institute ofTechnology, Pasadena,CA


Tuesday Morning / 05 January 2010 Session 100-PC-7 Chemical Kinetics and Combustion Boston

Tuesday Morning / 05 January 2010 Session 101-PC-8 Drops and Sprays II Los Angeles

Tuesday Morning / 05 January 2010 Session 102-PC-9 Solid Propellants Denver


Chaired by: W. TSANG, National Institute of Standards and Technology, Gaithersburg, MD, and Y. JU, Princeton University, Princeton, NJ0900AIAA-2010-0605 To Kerosene ReactionModel Development:Propylcyclohexane,C9H18, Dodecane,C12H26, andHexadecane C16H34Combustion

N. Slavinskaya, GermanAerospace Center(DLR), Stuttgart,Germany

0930AIAA-2010-0606 Direct Modeling of Auto-Ignition and FlamePropagation of N-heptane- Air Mixtures atHCCI Conditions byUsing Dynamic Multi-Timescale Method

Y. Ju, PrincetonUniversity, Princeton, NJ

1000AIAA-2010-0607 Kinetic InteractionEffects of Methyl-Butanoate/ n- HeptaneMixture on ExtinctionLimits of CounterflowDiffusion Flames.

M. Uddi, PrincetonUniversity, Princeton, NJ

1030AIAA-2010-0608 A Novel ProgressVariable Approach forPredicting NO in LaminarHydrogen Flames

A. Fiolitakis, GermanAerospace Center(DLR), Stuttgart,Germany

Chaired by: J. BELLAN, Jet Propulsion Laboratory, Pasadena, CA, and C. BRUNO, University of Rome "La Sapienza", Rome, Italy0900AIAA-2010-0609 Spray Flames in an Air-Heptane SwirlingCombustor

K. Luo, StanfordUniversity, Stanford, CA

0930AIAA-2010-0611 A Concept forSimultaneous High-Frequency Actuation ofLiquid SprayCharacteristics

C. Martin, VirginiaPolytechnic Institute andState University,Blacksburg, VA

1000AIAA-2010-0613 Impact of Fischer-Tropsch Fuels on Aero-Engine CombustionPerformance

P. Le Clercq, GermanAerospace Center(DLR), Stuttgart,Germany

1030AIAA-2010-0614 Simulations of SparkIgnition of a Swirling n-Heptane Spray Flamewith Conditional MomentClosure

P. Schroll, University ofCambridge, Cambridge,Great Britain

Chaired by: T. JACKSON, University of Illinois, Urbana-Champaign, Urbana, IL, and R. ERICKSON, United Technologies Research Center, East Hartford, CT0900AIAA-2010-0615 Mechanical Erosion ofNozzle Material in Solid-Propellant Rocket Motors

P. Thakre, CD-adapco,New Rochelle, NY

0930AIAA-2010-0616 Erosive Burning of SolidPropellants

T. Jackson, University ofIllinois,Urbana-Champaign,Urbana, IL

1000AIAA-2010-0617 Simulations ofComposite SolidPropellant CombustionWith and WithoutInternal Burning

J. Choi, Georgia Instituteof Technology, Atlanta,GA

1030AIAA-2010-0618 Mechanically Alloyed Al-I Composite Materials

S. Zhang, New JerseyInstitute of Technology,Newark, NJ

1100AIAA-2010-0619 Characterization of FineAluminum PowderCoated with Nickel as aPotential Fuel Additive

S. Vummidi, New JerseyInstitute of Technology,Newark, NJ

1130AIAA-2010-0620 Burning Characteristicsof Fuel DropletsContaining DiluteEnergetic Nanopartilces

Y. Gan, PurdueUniversity, WestLafayette, IN


Tuesday Morning / 05 January 2010 Session 103-PDL-6 Plasma Space Propulsion Crystal Ballroom F

Tuesday Morning / 05 January 2010 Session 104-SEC-1 Space Exploration Strategies and Mission Logistics Crystal Ballroom L

Tuesday Morning / 05 January 2010 Session 105-TP-6 Aerothermodynamics II Crystal Ballroom M


Chaired by: G. WILLIAMS, NASA Glenn Research Center, Cleveland, OH, and S. MAHALINGAM, Tech-X Corporation, Boulder, CO0900AIAA-2010-0621 SuperconductingHelicon Thruster

R. Sedwick, University ofMaryland, College Park,MD

0930AIAA-2010-0622 Exhaust Plume SpatialStructure of theVASIMR® VX- 200

E. Bering, University ofHouston, Houston, TX

1000AIAA-2010-0623 Hall Thruster PlumeDiagnostics UtilizingMicrowave Interferometry

J. Thurman, U.S. AirForce, Wright-PattersonAFB, OH

1030AIAA-2010-0624 Towards Hall ThrusterErosion Prediction Usinga Kinetic Plasma Modeland a MolecularDynamics Simulation

Y. Choi, Tech-XCorporation, Boulder, CO

1100AIAA-2010-0625 Performance andContamination Potentialof Micro- Pulsed PlasmaThrusters (uPPT)

J. Selstrom, U.S. AirForce Institute ofTechnology,Wright-Patterson AFB,OH

1130AIAA-2010-0626 Pulse DischargeNetwork Developmentfor a Heavy Gas FieldReversed ConfigurationPlasma Device

S. Miller, MissouriUniversity of Scienceand Technology , Rolla,MO

Chaired by: A. GALE, Space Settlement Design Competitions, Nassau Bay, TX, and D. DAVIS, The Boeing Company, El Segundo, CA0900AIAA-2010-0627 Feasibility Assessmentof Nonstop Mars SampleReturn System

H. Takayanagi, JapanAerospace ExplorationAgency (JAXA), Tokyo,Japan

0930AIAA-2010-0628 Low- Altitude Explorationof the VenusAtmosphere by Balloon

G. Landis, NASA GlennResearch Center,Cleveland, OH

1000AIAA-2010-0629 HERRO: A Science-Oriented Strategy forCrewed MissionsBeyond LEO

G. Schmidt, NASAGlenn Research Center,Cleveland, OH

Chaired by: M. WRIGHT, NASA Ames Research Center, Moffett Field, CA, and D. REDDY, NASA Glenn Research Center, Cleveland, OH0900AIAA-2010-0635 Modeling of the ElectricField in a HypersonicRarefied Flow

E. Farbar, University ofMichigan, Ann Arbor, MI

0930AIAA-2010-0630 Effect of ChemicalReaction Rates on Aero-Heating Predictions ofRe- Entry Flows

D. Reddy, IndianInstitute of Technology,Bombay, Mumbai, India

1000AIAA-2010-0634 Expansion TunnelRadiation Experimentsto Support HayabusaRe- Entry Observations

D. Buttsworth, Universityof SouthernQueensland,Toowoomba, Australia

Chaired by: T. LAM, The Aerospace Corporation, El Segundo, CA, and J. KAPAT, University of Central Florida, Oviedo, FL0900 0930 1000 1030 1100


Tuesday Morning / 05 January 2010 Session 106-TP-7 Heat Transfer I Crystal Ballroom N

Tuesday Morning / 05 January 2010 Session 107-WE-3 Wind Turbine Aerodynamics Experiments Crystal Ballroom G2

Tuesday Morning / 05 January 2010 Session 108-WIG-4 / PDL-7 Plasma-Assisted Combustion II Grand Ballroom 1


Chaired by: T. LAM, The Aerospace Corporation, El Segundo, CA, and J. KAPAT, University of Central Florida, Oviedo, FL0900AIAA-2010-0636 Air Flow Regimes forComfort in AirConditioned Spaces


0930AIAA-2010-0637 Effect of First VibrationMode on Sub- CriticalThermocapillaryConvection in FloatingZone Liquid Bridge

A. Ahmed, AirUniversity, Islamabad,Pakistan

1000AIAA-2010-0638 DNS and LES of Wall-Bounded CompressibleTurbulent Flows inNarrow Cooling Channel

D. Taieb, CORIA, SaintEtienne Du Rouvray,France

1030AIAA-2010-0639 Modeling InfraredSensing Mechanism ofMelanophila Beetles

J. Zhang, University ofOklahoma, Norman, OK

1100AIAA-2010-1474 Numerical Simulation ofContinuous and PulsedFilm Cooling on aTurbine- BladeLeading–Edge Model,including SurfaceConductance

D. Stenger, University ofCincinnati, Cincinnati,OH

Chaired by: J. NAUGHTON, University of Wyoming, Laramie, WY, and D. BERG, Sandia National Laboratories, Albuquerque, NM0900AIAA-2010-0640 Low FrequencyShedding Prompted byThree- DimensionalityUnder RotationalAugmentation

S. Schreck, NationalRenewable EnergyLaboratory, Golden, CO

0930AIAA-2010-0641 ExperimentalInvestigation of the WindTurbine Blade Root Flow

B. Akay, Delft Universityof Technology, Delft,The Netherlands

1000AIAA-2010-0642 Aeroacoustic NoiseMeasurements of aWind Turbine with BSDSBlades Using anAcoustic Array

E. Simley, University ofColorado, Boulder,Boulder, CO

1030AIAA-2010-0643 3- D Wake Dynamics ofthe VAWT: Experimentaland NumericalInvestigation

C. Simao Ferreira, DelftUniversity ofTechnology, Delft, TheNetherlands

1100AIAA-2010-0644 Active AerodynamicControl of Wind TurbineBlades with HighDeflection Flexible Flaps

G. Pechlivanoglou,Technical University ofBerlin, Berlin, Germany

1130AIAA-2010-0645 The DAN- AERO MWExperiments

H. Madsen, Risø DTU,Roskilde, Denmark

Chaired by: T. OMBRELLO, U.S. Air Force Research Laboratory, Wright-Patterson AFB, OH, and D. YARANTSEV, Russion Academy of Sciences, Moscow, Russia0900AIAA-2010-0646 Resonant Laser InducedBreakdown for Fuel- AirIgnition

S. Adams, U.S. AirForce ResearchLaboratory,Wright-Patterson AFB,OH

0930AIAA-2010-0648 Pure Rotational CARSMeasurements ofThermal EnergyRelease and Ignition inNanosecond Pulse BurstAir and Hydrogen- AirPlasmas

Y. Zuzeek, Ohio StateUniversity, Columbus,OH

1000AIAA-2010-0650 Laser- Initiated,Microwave DrivenIgnition in Methane/AirMixtures

J. Michael, PrincetonUniversity, Princeton, NJ

1030AIAA-2010-0651 Plasma EnhancedCombustion usingMicrowave EnergyCoupling in a Re- entrantCavity Applicator

X. Rao, Michigan StateUniversity, East Lansing,MI


Tuesday Morning / 05 January 2010 1000 - 1200 Remembering Dr. Shahyar Pirzadeh (Invited) Crystal Ballroom C

Tuesday Afternoon / 05 January 2010 1200 - 1400 Awards Luncheon Grand Ballroom 7/8

Tuesday Afternoon / 05 January 2010 1400 - Astrosociology Student Forum Crystal Ballroom F


Chaired by: W. JONES, NASA Langley Research Center, Hampton, VAMarch 18, 2009 marked the passing of a valued contributor to the field of unstructured numerical mesh generation, Dr. Shahyar Pirzadeh. Dr. Pirzadeh was most notably known for his work with the VGRIDunstructured mesh generator. His career was marked with many innovations including the Advancing Layers Method (ALM) and early adoption of the Cartesian Background Grid to control mesh spacing. Amethodical approach to his work resulted in numerous advances in the field. This session provides an opportunity for those who knew and worked closely with Shahyar to share memories and thoughts with thecommunity.

Chaired by: J. PASS, Astrosociology Research Institute, Huntington Beach, CA, and J. PALAIA, 4Frontiers Corporation, New Port Richey, FLThis session focuses on the issues common to both traditional aerospace engineering/scientific inquiry and the social sciences. Astrosociology represents the social sciences as the only developingmultidisciplinary field intended to highlight issues pertinent to the relationship between (1) space and (2) society (or the human dimension). Many questions arise when confronting this relationship. Forexample, a well-engineered space habitat may meet the life support needs of a human group, but is this adequate for their long-term survival?

Panelists: Simone Caroti, Michael Grant, Michael Serrano, Jason Dunn

The afternoon sessions shift to workforce development topics and activities to develop and grow the aerospace workforce for the near and long term.

Chaired by: K. VISWANATHAN, The Boeing Company, Seattle, WA1400 1430 1500 1530 1600

Chaired by: M. MOORE, NASA Langley Research Center, Hampton, VA, and G. CROUSE, Auburn University, Auburn, AL1400 1430 1500 1530 1600


Tuesday Afternoon / 05 January 2010

1400 - 1700 Career and Workforce Development Workshop - Laying the Foundation for the Futureof Aerospace II Crystal Ballroom G1

Tuesday Afternoon / 05 January 2010 Session 109-AA-6 Jet Noise Suppression II Washington

Tuesday Afternoon / 05 January 2010 Session 110-AD-4 Conceptual Aircraft Design Geometry Modeling Crystal Ballroom K


The afternoon sessions shift to workforce development topics and activities to develop and grow the aerospace workforce for the near and long term.

Chaired by: K. VISWANATHAN, The Boeing Company, Seattle, WA1400AIAA-2010-0652 Effects of SourceRedistribution on JetNoise Shielding

S. Mayoral, University ofCalifornia, Irvine, Irvine,CA

1430AIAA-2010-0653 Prediction of Jet NoiseShielding

D. Papamoschou,University of California,Irvine, Irvine, CA

1500AIAA-2010-0654 Adaptation of theBeveled Nozzle for HighSpeed Jet NoiseReduction

K. Viswanathan, TheBoeing Company,Seattle, WA

1530AIAA-2010-0655 Towards Developmentof an Active Single-Layer Acoustic Liner forJet Engine NoiseReduction

M. Perrino, University ofCincinnati, Cincinnati,OH

1600AIAA-2010-0656 An Application ofCommercial NoiseReduction Techniquesto Military AircraftNozzles

N. Heeb, University ofCincinnati, Cincinnati,OH

Chaired by: M. MOORE, NASA Langley Research Center, Hampton, VA, and G. CROUSE, Auburn University, Auburn, AL1400AIAA-2010-0657 Vehicle Sketch Pad: AParametric GeometryModeler for ConceptualAircraft Design

A. Hahn, NASA LangleyResearch Center,Hampton, VA

1430AIAA-2010-0658 Aircraft ConceptualDesign Using VehicleSketch Pad

W. Fredericks, NASALangley ResearchCenter, Hampton, VA

1500AIAA-2010-0659 Improved GeometryModeling for HighFidelity ParametricDesign

J. Gloudemans, , SanMateo, CA

1530Oral Presentation Vehicle Sketch PadSoftware Demonstration

W. Fredericks, NASALangley ResearchCenter, Hampton, VA

1600Oral Presentation Geometry Needs ofConceptual AircraftDesign - PanelDiscussion


Chaired by: G. COOPER, U.S. Army Research Laboratory, Aberdeen Proving Ground, MD, and M. KNISKERN, Sandia National Laboratories, Albuquerque, NM1400 1430 1500


Tuesday Afternoon / 05 January 2010 Session 111-AFM-4 Launch Vehicles Chicago

Tuesday Afternoon / 05 January 2010 Session 112-AMT-5 Surface Measurement Techniques II Crystal Ballroom J1

Tuesday Afternoon / 05 January 2010 Session 113-APA-10 Propellor/Rotorcraft Aerodynamics Grand Ballroom 9


Chaired by: G. COOPER, U.S. Army Research Laboratory, Aberdeen Proving Ground, MD, and M. KNISKERN, Sandia National Laboratories, Albuquerque, NM1400AIAA-2010-0664 Improvements to Power-On Base PressurePrediction for theAeroprediction Code

F. Moore,Aeroprediction, Inc., KingGeorge, VA

1430AIAA-2010-0665 Analytical ModelDevelopment andImpulse ThrustersPairing Guidelines forTrajectory Corrections ofSpin- StabilizedProjectiles

D. Corriveau, DefenceR&D Canada, Québec,Canada

1500AIAA-2010-0668 The Range SafetyDebris Catalog Analysisin Preparation for thePad Abort One FlightTestt

P. Kutty, AnalyticalMechanics Associates,Inc., Edwards, CA

Chaired by: S. BERESH, Sandia National Laboratories, Albuquerque, NM, and A. DRAKE, Northrop Grumman Corporation, San Diego, CA1400AIAA-2010-0669 WITHDRAWN TemperatureMeasurements ofRotating ComponentsUsing PhosphorThermometry

A. Khalid, University ofManchester,Manchester, GreatBritain

1430AIAA-2010-0670 Window TemperatureImpact on IRThermography for HeatTransfer Measurements

J. Gustavsson,Siemens, Finspong,Sweden

1500AIAA-2010-0671 Comparative SurfaceHeat TransferMeasurements inHypervelocity Flow

W. Flaherty, Universityof Illinois, Urbana, IL

1530AIAA-2010-0672 Europium- DopedPyrochlores for Use asThermographicPhosphors in ThermalBarrier Coatings

S. Desai, VanderbiltUniversity, Nashville, TN

1600AIAA-2010-0673 Temperature- CancelledAnodized- AluminumPressure Sensitive Paintfor HypersonicCompression CornerFlows

T. Kuriki, JapanAerospace ExplorationAgency (JAXA), Chofu,Japan

1630AIAA-2010-0674 Experiment Researcheson the Location ofTransition Onset in theHypersonic Wind Tunnel

X. Zhao, ChinaAcademy of AerospaceAerodynamics, Beijing,China (prc)

Chaired by: R. KREEGER, NASA Glenn Research Center, Cleveland, OH, and M. CALVERT, U.S. Army Research, Development and Engineering Command, Redstone Arsenal, AL1400AIAA-2010-0675 Evaluation of a PotentialFlow Model for Propellerand Wind TurbineDesign

J. Katz, San Diego StateUniversity, San Diego,CA

1430AIAA-2010-0676 CFD- Based TwistOptimization of HoveringRotors

C. Allen, University ofBristol, Bristol, GreatBritain

1500AIAA-2010-0677 Critical Aspects in theAerodynamics ofHelicopter Blade- VortexInteraction: A NumericalStudy Using LES

M. Ilie, University ofCentral Florida, Orlando,FL

1530AIAA-2010-0679 A Three- DimensionalVortex Particle- PanelMethod for ModelingPropulsion- AirframeInteraction

J. Calabretta, CaliforniaPolytechnic StateUniversity, San LuisObispo, CA

1600AIAA-2010-0680 LES Studies ofHelicopter Blade- VortexMechanism ofInteraction: The IcingEffect



Tuesday Afternoon / 05 January 2010 Session 114-APA-11 Weapons Carriage and Store Separation Grand Ballroom 10

Tuesday Afternoon / 05 January 2010 Session 115-APA-12 Wind Tunnel and Flight Testing Aerodynamics Grand Ballroom 11

Tuesday Afternoon / 05 January 2010 Session 116-ASE-4 Numerical Modeling of Atmospheric Phenomena Atlanta


Chaired by: S. FERGUSON, The Boeing Company, Renton, WA1400AIAA-2010-0681 Scaled- Drop- Tests:WYSIWYG or Not?

R. Deslandes,EADS-Military AirSystems, Manching,Germany

1430AIAA-2010-0682 WITHDRAWN Dynamic Simulation onWeapon Dispensing inHigh Speed Flows

T. Lin, NorthropGrumman Corporation,San Bernardino, CA

Chaired by: M. CHANG, Lockheed Martin, Santa Clarita, CA, and R. VERMELAND, Lockheed Martin, Lancaster, CA1400AIAA-2010-0684 Aerodynamic Influenceof a Half- Span ModelInstallation for High- LiftConfiguration Experiment

Y. Yokokawa, JapanAerospace ExplorationAgency (JAXA),Chofu,Tokyo, Japan

1430AIAA-2010-0686 Preliminary Study onFlat- Plate Wing withSweptback UtilizingWake Measurements

M. Kashitani, NationalDefense Academy,Yokosuka, Japan

1500AIAA-2010-0687 An Approach TowardsUsing Dynamic WindTunnel Testing toCharacterize MicroAerial Vehicle Stability

M. Shields, University ofColorado, Boulder,Boulder, CO

Chaired by: M. POLITOVICH, National Center for Atmospheric Research, Boulder, CO, and E. WHALEN, The Boeing Company, St Louis, MO1400AIAA-2010-0688 Simulation of Flows withLarge Gradients usingAdaptive MeshRefinement

N. Ahmad, ScienceApplications InternationalCorporation, McLean, VA

1430AIAA-2010-0690 Application of a GalerkinFinite Element Schemeto Atmospheric Buoyantand Gravity Driven Flows

S. Marras, BarcelonaSupercomputing Center,Barcelona, Spain

1500AIAA-2010-0691 An Unstructured CFDApproach for NumericalWeather Prediction

R. Aubry, BarcelonaSupercomputing Center,Barcelona, Spain

Chaired by: K. RINK, University of Idaho, Moscow, ID, and H. LEE, Scot Incorporated, Downers Grove, IL1400 1430 1500


Tuesday Afternoon / 05 January 2010 Session 117-ECS-3 Energetic Materials: Applications Crystal Ballroom A

Tuesday Afternoon / 05 January 2010 Session 118-FD-22 Fundamental Wall-Bounded Turbulence Grand Ballroom 3

Tuesday Afternoon / 05 January 2010 Session 119-FD-23 Boundary Layer Transition II Grand Ballroom 4


Chaired by: K. RINK, University of Idaho, Moscow, ID, and H. LEE, Scot Incorporated, Downers Grove, IL1400AIAA-2010-0694 An Overview ofNanoscale SiliconReactive CompositesApplied toMicroengergetics

S. Son, PurdueUniversity, WestLafayette, IN

1430AIAA-2010-0695 Optical Spectroscopy ofFireballs from MetallizedReactive Materials

N. Glumac, University ofIllinois,Urbana-Champaign,Urbana, IL

1500AIAA-2010-1598 Analysis of the Influenceof Nanometric AluminumParticle Vaporization onFlame Propagation inBulk Powder Media

B. Dikici, Texas TechUniversity, Lubbock, TX

Chaired by: K. CHRISTENSEN, University of Illinois, Urbana-Champaign, Urbana, IL, and B. MCKEON, California Institute of Technology, Pasadena, CA1400AIAA-2010-0697 Energetic Modes inTurbulent Pipe FlowFrom Resolvent Analysis

B. McKeon, CaliforniaInstitute of Technology,Pasadena, CA

1430AIAA-2010-0698 A Basic Three-Dimensional TurbulentBoundary LayerExperiment to TestSecond- MomentClosure Models

S. Sadek, VirginiaPolytechnic Institute andState University,Blacksburg, VA

1500AIAA-2010-0699 Extracting GloballyDominant Parameters ofA Realistic RoughSurface UsingContinuous Wavelets

H. Ren, Wright StateUniversity, Dayton, OH

1530AIAA-2010-0700 Structure of TurbulentBoundary Layers andSurface PressureFluctuations with SparseRoughness

N. Varano, VirginiaPolytechnic Institute andState University,Blacksburg, VA

1600AIAA-2010-0701 Structure of TurbulentBoundary Layers withDense Roughness

A. Hopkins, VirginiaPolytechnic Institute andState University,Blacksburg, VA

Chaired by: A. TUMIN, University of Arizona, Tucson, AZ, and J. BONS, Ohio State University, Columbus, OH1400AIAA-2010-0703 High- Speed PLIFImaging of HypersonicTransition over DiscreteCylindrical Roughness

P. Danehy, NASALangley ResearchCenter, Hampton, VA

1430AIAA-2010-0705 Development andBreakdown of GortlerVortices in High SpeedBoundary Layers

F. Li, NASA LangleyResearch Center,Hampton, VA

1500AIAA-2010-0706 Numerical Simulations ofHypersonic Boundary-Layer Instability withWall Blowing

S. Ghaffari, StanfordUniversity, Stanford, CA

1530AIAA-2010-0707 Hypersonic Boundary-Layer Instability withChemical Reactions

O. Marxen, StanfordUniversity, Stanford, CA

Chaired by: G. HE, Chinese Academy of Sciences, Beijing, China (prc), and T. RAMSAY, Honda R&D Americas Inc, Raymond, OH


Tuesday Afternoon / 05 January 2010 Session 120-FD-24 Cartesian Grid and Immersed Boundary Methods Crystal Ballroom B

Tuesday Afternoon / 05 January 2010 Session 121-FD-25 Flow Control Simulations Grand Ballroom 5

Tuesday Afternoon / 05 January 2010 Session 122-FD-26 High Order Methods III New York


Chaired by: G. HE, Chinese Academy of Sciences, Beijing, China (prc), and T. RAMSAY, Honda R&D Americas Inc, Raymond, OH1400AIAA-2010-0708 Towards Large- eddySimulation of TurbulentFlows with ComplexGeometric BoundariesUsing ImmersedBoundary Method

G. He, ChineseAcademy of Sciences,Beijing, China (prc)

1430AIAA-2010-0709 Towards a Ghost- CellMethod for Analysis ofViscous Flows onCartesian- Grids

A. Dadone, TechnicalUniversity of Bari, Bari,Italy

1500AIAA-2010-0710 RANS SimulationAround Airfoils UsingBuilding- Cube Method

S. Nishimoto, TohokuUniversity, Sendai, Japan

1530AIAA-2010-0711 A Second- OrderImmersed BoundaryProjection Method forElliptic and ParabolicProblems

P. Young, University ofColorado, Boulder,Boulder, CO

1600AIAA-2010-0712 A Turbulent Wall Modelfor Immersed BoundaryMethods

F. Capizzano, ItalianAerospace ResearchCenter (CIRA), Capua,Italy

Chaired by: K. GHIA, University of Cincinnati, Cincinnati, OH1400AIAA-2010-0713 Two- DimensionalSimulation of Horseshoeand Parallel ActuatorsInside a Micro Geometry

C. Wang, University ofFlorida, Gainesville, FL

1430AIAA-2010-0714 Numerical Investigationson the Effects of theDeclining Back- Edge ofMVG

Q. Li, University ofTexas, Arlington,Arlington, TX

1500AIAA-2010-0715 Boundary ConditionImplementation for aCoupled LatticeBoltzmann and Navier-Stokes Methodology

N. Yeshala, GeorgiaInstitute of Technology,Atlanta, GA

1530AIAA-2010-0716 Investigation ofTurbulent SpotSpreading Mechanism

J. Chu, University ofTexas, Austin, Austin,TX

1600AIAA-2010-0717 Fluidic Injection FlowControl for HighPressure Turbine AreaModulation – AComputational FluidDynamics Investigation

D. Baruzzini, LockheedMartin Corporation, FortWorth, TX

Chaired by: R. HARRIS, CFD Research Corporation, Huntsville, AL, and S. TU, Jackson State University, Jackson, MS1400AIAA-2010-0718 WITHDRAWN Development of AnAdaptive Space- TimeMethod for High- OrderResolution ofDiscontinuities, Part II

Z. Yang, University ofWyoming, Laramie, WY

1430AIAA-2010-0719 AUSM- Based High-Order Solution for EulerEquations

A. Scandaliato, OhioAerospace Institute,Cleveland, OH

1500AIAA-2010-0720 Partition Design andOptimization for High-Order Spectral VolumeSchemes on TetrahedralGrids

R. Harris, CFDResearch Corporation,Huntsville, AL

1530AIAA-2010-0721 Toward a Robust,Higher- Order Cut- CellMethod for ViscousFlows

J. Modisette,Massachusetts Instituteof Technology,Cambridge, MA

1600AIAA-2010-0722 A High- Order Gas-Kinetic Navier- StokesFlow Solver

Q. Li, TsinghuaUniversity, Beijing,China (prc)

1630AIAA-2010-0723 Modified UpwindingCompact Scheme for 1-D and 2- D Shock /Wave Interaction

C. Liu, University ofTexas, Arlington,Arlington, TX

Chaired by: H. LUO, Vanderbilt University, Nashville, TN, and D. WILLIS, University of Massachusetts, Revere, MA


Tuesday Afternoon / 05 January 2010 Session 123-FD-27 Low Reynolds Number and Bio-Inspired Aerodynamics II Grand Ballroom 6

Tuesday Afternoon / 05 January 2010 Session 124-FD-28 / SST-2 Micro-Scale Flow Sensing and Control (Invited) Crystal Ballroom C

Tuesday Afternoon / 05 January 2010 Session 125-GPSE-4 Emerging Opportunities in Research Flights II Crystal Ballroom D


Chaired by: H. LUO, Vanderbilt University, Nashville, TN, and D. WILLIS, University of Massachusetts, Revere, MA1400AIAA-2010-0724 The NumericalSimulation of FlappingWings at Low ReynoldsNumbers

P. Persson, University ofCalifornia, Berkeley,Berkeley, CA

1430AIAA-2010-0725 WITHDRAWN Sinusoidal High-Frequency Oscillation ofan AR=2 Flat Plate:Computation andExperiment

Y. Suzen, North DakotaState University, Fargo,ND

1500AIAA-2010-0726 A Numerical Study ofVortex- Dominated Flowaround an OscillatingAirfoil with High- OrderSpectral DifferenceMethod

M. Yu, Iowa StateUniversity, Ames, IA

1530AIAA-2010-0727 Optimization of a PIVBased Study UsingMaximum WorkPotential and Design ofExperiments Techniques

D. Stanley, The BoeingCompany, Kent, WA

1600AIAA-2010-0728 Direct NumericalSimulations of PlungingAirfoils

Y. Allaneau, StanfordUniversity, Stanford, CA

1630AIAA-2010-0729 Unsteady Aerodynamicsof Low Aspect RatioMembrane Wings

P. Rojratsirikul,University of Bath, Bath,Great Britain

Chaired by: D. HITT, University of Vermont, Burlington, VT, and M. MARTIN, Louisiana State University, Baton Rouge, LA1400Oral Presentation Interfacial Control ofHigh- Viscosity Fluids inMicrosystems

T. Cubaud, StateUniversity of New York,Stony Brook, StonyBrook, NY

1430Oral Presentation Micro- Optical Sensorsfor Wall Pressure andShear Stress

V. Otugen, SouthernMethodist University,Dallas, TX

1500Oral Presentation Control of Micro- UAVs

M. Amitay, RensselaerPolytechnic Institute,Troy, NY

1530Oral Presentation CFD Design for Lab-On- A- ChipMicrosystems

D. Mott, Naval ResearchLaboratory, Washington,DC

1600Oral Presentation Smart Chemical SensorSystems for AerospaceApplications

G. Hunter, NASA GlennResearch Center,Cleveland, OH

1630Oral Presentation Open Discussion: Micro-Scale Flow Control &Sensing

D. Hitt, University ofVermont, Burlington, VT

Chaired by: J. COHEN, NASA Headquarters, Washington, DC, and S. COLLICOTT, Purdue University, West Lafayette, IN1400Oral Presentation PharmaSat: ANanosatellite Platformfor BiologicalExperimentation

D. Niesel, University ofTexas Medical Branch,Galveston, TX

1430Oral Presentation Free FlyingNanoSatellites andPayload Technologiesfor Fundamental SpaceBiology Applications

J. Hines, NASA AmesResearch Center, MoffetField, CA

1500Oral Presentation Decoupling TransportPhenomena inMicrogravity to DevelopPersonalized Medicineon Earth

A. Ziemys, University ofTexas Health ScienceCenter, Houston, TX

1530Oral Presentation Perspective on FOTONand BION Experiences

M. Skidmore, NASAAmes Research Center,Moffett Field, CA

Chaired by: S. POWELL, Aerospace Testing Alliance, Arnold AFB, TN, and N. ULBRICH, Jacobs Technology, Moffett Field, CA1400 1500 1530 1600 1630


Tuesday Afternoon / 05 January 2010 Session 126-GT-4 Data Analysis Miami

Tuesday Afternoon / 05 January 2010 Session 127-GTE-7 Gas Turbine Fans and Compressors Grand Ballroom 14

Tuesday Afternoon / 05 January 2010 Session 128-HAPB-4 Ramjet/Scramjet Injectors Grand Ballroom 12


Chaired by: S. POWELL, Aerospace Testing Alliance, Arnold AFB, TN, and N. ULBRICH, Jacobs Technology, Moffett Field, CA1400

Break

,

1500AIAA-2010-0741 Assessment ofResponse SurfaceModels UsingIndependentConfirmation PointAnalysis

R. DeLoach, NASALangley ResearchCenter, Hampton, VA

1530AIAA-2010-0742 Correlation of WindTunnel and Flight TestResults for a P- 51BAirplane

N. Ulbrich, JacobsTechnology, MoffettField, CA

1600AIAA-2010-0743 Uncertainty Identificationof Supersonic WindTunnel Testing

S. Nagai, JapanAerospace ExplorationAgency (JAXA), Chofu,Japan

1630AIAA-2010-0744 Preliminary Study onDiaphragmless ShockTube for Transonic AirfoilTesting with PDI

M. Kashitani, NationalDefense Academy,Yokosuka, Japan

Chaired by: M. LIST, U.S. Air Force Research Laboratory, Wright-Patterson AFB, OH, and N. KEY, Purdue University, West Lafayette, IN1400AIAA-2010-0745 Effects of RadialDistortion onPerformance of a Fan

D. Voytovych, PurdueUniversity, WestLafayette, IN

1430AIAA-2010-0746 A ComputationalInvestigation of VaneClocking Effects onCompressor ForcedResponse

J. Salontay, PurdueUniversity, WestLafayette, IN

1500AIAA-2010-0747 The Effect of LipskinDamage on InletDistortion

S. Kennedy, Queen'sUniversity Belfast,Belfast, Northern Ireland

Chaired by: J. DONOHUE, United Technologies Research Center, East Hartford, CT, and J. LEE, NASA Glenn Research Center, Cleveland, OH1400AIAA-2010-0750 Investigation of DropletNucleation InsideSupercritical EthyleneJets Using Small AngleX- Ray Scattering(SAXS) Technique

K. Lin, Taitech, Inc.,Beavercreek , OH

1430AIAA-2010-0751 Dual Mode ScramjetCombustor: Analysis ofTwo Configurations

R. Milligan, Taitech, inc.,Beavercreek, OH

1500AIAA-2010-0752 Injection and Disruptionof Supersonic Droplets

Y. Kim, University ofWashington, Seattle, WA

1530AIAA-2010-0753 Supersonic TurbulentMixing Structure inStaged InjectionFlowfields

H. Takahashi, TohokuUniversity, Sendai,Japan

1600AIAA-2010-0755 On the Effects ofTransverse- Jet Injectioninto a Supersonic ShearLayer

L. Maddalena, CaliforniaInstitute of Technology,Pasadena, CA

Chaired by: W. ENGBLOM, Embry-Riddle Aeronautical University, Daytona Beach, FL, and H. HASSAN, North Carolina State University, Raleigh, NC


Tuesday Afternoon / 05 January 2010 Session 129-HAPB-5 Ramjet/Scramjet Simulation with URANS/LES/DES II Grand Ballroom 13

Tuesday Afternoon / 05 January 2010 Session 130-HIS-3 / GT-5 History of Wind Tunnels II--Historical Research: A "How To" Primer New Orleans

Tuesday Afternoon / 05 January 2010 Session 131-IS-2 Multi-Agent Supervision and Coordination Crystal Ballroom L


Chaired by: W. ENGBLOM, Embry-Riddle Aeronautical University, Daytona Beach, FL, and H. HASSAN, North Carolina State University, Raleigh, NC1400AIAA-2010-0756 Inlet Buzz andCombustion Oscillationin an AxisymmetricRamjet Engine

H. Sung, KoreaAerospace University,Goyang, South Korea

1430AIAA-2010-0757 Three- DimensionalSimulation of IgnitionTransient in HyshotScramjet Configuration

S. Won, Seoul NationalUniversity, Seoul, SouthKorea

1500AIAA-2010-0758 LES of the HyshotScramjet Combustor

A. Ingenito, University ofRome "La Sapienza",Rome, Italy

1530AIAA-2010-1129 Thrust Prediction inThermally Choked RamAccelerator

T. Bengherbia, FrenchNational Center forScientific Research(CNRS), Poitiers, France

Chaired by: S. EBERHARDT, The Boeing Company, Seattle, WA, and K. BURNS, Wyle Laboratories, San Diego, CA1400Oral Presentation History of Wind Tunnelsat Cal Tech

F. Khorrami, CaliforniaInstitute of Technology,Pasadena, CA

1430AIAA-2010-0760 A 50 Year Chronology ofthe Boeing PolySonicWind Tunnel: An Era ofAerodynamic Inventionand Innovation

M. Benne, The BoeingCompany, St. Louis, MO

1500Oral Presentation Panel Discussion:Historical Research- - A"How To" Primer

T. Crouch, SeniorCurator, Divison ofAeronautics, NationalAir and Space Museum,Washington, DC

Chaired by: E. ATKINS, University of Michigan, Ann Arbor, MI, and L. LONG, Pennsylvania State University, University Park, PA1400AIAA-2010-0762 Multi- Agent MazeExploration

E. Kivelevitch, Universityof Cincinnati, Cincinnati,OH

1430AIAA-2010-0763 Assessing OperatorWorkload andPerformance inExpeditionary MultipleUnmanned VehicleControl

A. Clare, MassachusettsInstitute of Technology,Cambridge, MA

1500AIAA-2010-0764 Human- AutonomousSystem InteractionFramework to SupportSafety in Astronaut-Robot Team Interactions

M. Lyell, IntelligentAutomation, Inc.,Rockville, MD

1530AIAA-2010-0767 Satellite DesignAutomation Using AITools in Step_SATdband QuickSAT, a Web-Based and Open-Source Satellite DesignAutomation Environment

A. Santangelo,sci_Zone, Holland, MI

Chaired by: J. SINIBALDI, Naval Postgraduate School, Monterey, CA, and S. MENON, Georgia Institute of Technology, Atlanta, GA1400 1430 1500 1530 1600


Tuesday Afternoon / 05 January 2010 Session 132-PC-10 Detonations Denver

Tuesday Afternoon / 05 January 2010 Session 133-PC-11 Laminar Flames I Los Angeles

Tuesday Afternoon / 05 January 2010 Session 134-PDL-8 Joint PDL/WIG/FD/TP Plasma Actuator Session IV: RF/HF Discharges Grand Ballroom 1


Chaired by: J. SINIBALDI, Naval Postgraduate School, Monterey, CA, and S. MENON, Georgia Institute of Technology, Atlanta, GA1400AIAA-2010-0768 Numerical Investigationof Particle Dispersal inMultiphase Explosions

Y. Ling, University ofFlorida, Gainesville, FL

1430AIAA-2010-0770 Study of Interaction ofDilute or Dense Cloud ofInert and ReactiveParticles with CellularDetonation Structures

K. Gottiparthi, GeorgiaInstitute of Technology,Atlanta, GA

1500AIAA-2010-0771 Effect of Loading WaveProfile on HydrodynamicVoid Collapse inDetonation Initiation

A. Swantek, University ofIllinois,Urbana-Champaign,Urbana, IL

1530AIAA-2010-0772 Numerical Simulation ofNon- Equilibrium Effectsand Ionization in H2 AirDetonations

J. Schulz, GeorgiaInstitute of Technology,Atlanta, GA

1600AIAA-2010-0773 Predicting Mixing andCombustion in theAfterburn Stage of AirBlasts

E. Fedina, SwedishDefence ResearchAgency, Tumba, Sweden

Chaired by: E. TASKINOGLU, California Institute of Technology, South Pasadena, CA, and L. BAUWENS, University of Calgary, Calgary, Canada1400AIAA-2010-0774 Laminar Flame Speedsof C5 to C8 n- Alkanesat Elevated Pressuresand Temperatures

A. Kelley, PrincetonUniversity, Princeton, NJ

1430AIAA-2010-0775 Structure of LaminarMethane- OxygenDiffusion Flames at HighPressures

H. Joo, University ofToronto, Toronto,Canada

1500AIAA-2010-0776 Negative PressureDependence of HighPressure Burning Ratesof H2/O2 Flames atLean Conditions

M. Burke, PrincetonUniversity, Princeton, NJ

1530AIAA-2010-0777 Flame- Flow Interactionsand Flow Reversal

G. Bansal, StanfordUniversity, Stanford, CA

1600AIAA-2010-0778 Laminar Flame Speed ofHydrocarbon Fuels withPreheat and LowOxygen Content

Y. Kochar, GeorgiaInstitute of Technology,Atlanta, GA

1630AIAA-2010-0779 Pressure Effects onStructure andTemperature Field ofLaminar Diffusion Flames

H. Gohari Darabkhani,The University ofManchester ,Manchester, GreatBritain

Chaired by: C. LAUX, École Centrale Paris, Paris, France, and S. STANFIELD, Wright State University, Dayton, OH1400AIAA-2010-0782 Plasma ActuatorCreated by CapacityCoupled Surface HFDischarge

A. Klimov, RussianAcademy of Sciences,Moscow, Russia

1430AIAA-2010-0783 The Effect of Plasma onthe Flow Features of anAxisymmetric Jet

R. Huffman, U.S. AirForce Institute ofTechnology,Wright-Patterson AFB,OH

1500AIAA-2010-0785 Vortex Generation inCapacitive Discharge

E. Son, RussianAcademy of Sciences,Dolgoprudny, Russia

Chaired by: S. NAGANO, The Aerospace Corporation, Los Angeles, CA, and E. NICHOLS, Orbital Sciences Corporation, Chandler, AZ


Tuesday Afternoon / 05 January 2010 Session 135-SE-1 Systems Engineering I Tampa

Tuesday Afternoon / 05 January 2010 Session 136-SEC-2 Space Exploration Vehicle and Architecture Design Crystal Ballroom M

Tuesday Afternoon / 05 January 2010 Session 137-SRU-1 Space Resource Utilization and Related Technologies Boston


Chaired by: S. NAGANO, The Aerospace Corporation, Los Angeles, CA, and E. NICHOLS, Orbital Sciences Corporation, Chandler, AZ1400AIAA-2010-0786 A Process for Systemsof Systems Architecting

K. Griendling, GeorgiaInstitute of Technology,Atlanta, GA

1430AIAA-2010-0787 Complex SystemsEngineering Lessons tobe Applied to the SmartGrid

J. Dahlgren, MITRECorporation, Hampton,VA

1500AIAA-2010-0788 Use ZachmanFramework to Engineerthe Emergent Behaviorof a System- of- Systems

J. Hsu, Royal Academyof Engineering, Cypress,CA

1530AIAA-2010-0789 Adaptation of a StrategicBusiness Model toNASA Project Risk

J. Rice, DefenseAcquisition University,Huntsville, AL

1600AIAA-2010-0791 The AmmunitionReliability AnaysisApplied by Prediction ofLife Cycle

D. Kim, HanwhaCompany, Ltd.,You-Seong, South Korea

Chaired by: D. ANDREWS, The Boeing Company, Retired, Seattle, WA, and F. BECKER, QinetiQ, Cape Canaveral, FL1400AIAA-2010-0792 Architecture of SpaceVehicles for Direction-Controlled ArtificialGravity, Using AvailableAssets

B. Benjamin, Universityof Kansas, Lawrence, KS

1430AIAA-2010-0793 Deployment of InflatableSpace Habitat Models

J. Hill, Oklahoma StateUniversity, Stillwater, OK

1500AIAA-2010-0794 A High ConfidenceHeavy Lift LaunchVehicle

W. Rothschild, JohnFrassanito & Associates,Inc., Houston, TX

1530AIAA-2010-0795 Conceptual Design ofCrew Exploration Landerfor Asteroid Ceres andSaturn Moons Rhea andIapetus

M. Benton, The BoeingCompany, HuntingtonBeach, CA

Chaired by: L. GERTSCH, Missouri University of Science and Technology, Rolla, MO, and J. KLEINHENZ, National Center for Space Exploration Research, Cleveland, OH1400AIAA-2010-0797 An Extension of Analysisof Solar- HeatedThermal Wadis toSupport Extended-Duration LunarExploration

R. Balasubramanian,NASA Glenn ResearchCenter, Cleveland, OH

1430AIAA-2010-0798 Thermal Strategies forLong Duration MobileLunar Surface Missions

J. Thornton, CarnegieMellon University,Pittsburgh, PA

1500AIAA-2010-0799 In Situ ResourceUtilization on Mars -Update from DRA 5.0Study

G. Sanders, NASAJohnson Space Center,Houston, TX

1530AIAA-2010-0800 Employing ISRU Modelsto Improve HardwareDesigns

D. Linne, NASA GlennResearch Center,Cleveland, OH

1600AIAA-2010-0801 Methods forMeasurement ofThermophysicalProperties of LunarSimulant

J. Kizito, North CarolinaA&T State University,Greensboro, NC

Chaired by: E. KHALIL, Cairo University, Cairo, Egypt, and A. CHOUDHURI, University of Texas, El Paso, El Paso, TX1400 1430 1500 1530


Tuesday Afternoon / 05 January 2010 Session 138-TES-1 Energy Efficiency Crystal Ballroom E

Tuesday Afternoon / 05 January 2010 Session 139-TP-8 Integrated and Multidisciplinary Modeling and Simulation Crystal Ballroom N

Tuesday Afternoon / 05 January 2010 Session 140-TP-9 Non-Equilibrium Flows I Crystal Ballroom P


Chaired by: E. KHALIL, Cairo University, Cairo, Egypt, and A. CHOUDHURI, University of Texas, El Paso, El Paso, TX1400AIAA-2010-0802 Thermal Comfort andAir Quality inSustainable ClimateControled HealthcareApplications


1430AIAA-2010-0803 Energy EfficiencyAnalyses in SustainableGreen Buildings: Codes& Standards


1500AIAA-2010-0804 Chemical EnergyRecovery fromPolystyrene UsingPyrolysis and Gasification

I. Ahmed, University ofMaryland, College Park,MD

1530AIAA-2010-1601 Thermal Performance ofa Mesoscale LiquidFueled Combustor

V. Vijayan, University ofMaryland, College Park,MD

Chaired by: G. NATERER, University of Ontario, Oshawa, ON, and D. REDDY, NASA Glenn Research Center, Cleveland, OH1400AIAA-2010-0807 Dissipative ParticleDynamics Simulation ofElectroosmotic Flow inNanoscale Channels

M. Darbandi, SharifUniversity ofTechnology, Tehran, Iran

1430AIAA-2010-0808 Parallelization ofModular Particle-Continuum Method forHypersonic, NearEquilibrium Flows

T. Deschenes, Universityof Michigan, Ann Arbor,MI

1500AIAA-2010-0809 More Electric AircraftAnalysis Using ExergyAs A DesignComparison Tool

R. Gandolfi, EMBRAER,São José Dos Campos,Brazil

1530AIAA-2010-0810 Orion Active ThermalControl System DynamicModeling UsingSimulink/MATLAB

X. Wang, NASA GlennResearch Center,Cleveland, OH

1600AIAA-2010-0811 MultiresolutionAugmented ArtificialNeural Networks forModeling of ParticleLaden CompressibleFlows

C. Lu, University of Iowa,Iowa City, IA

1630AIAA-2010-0812 Three DimensionalAdaptive Method forCompressible Multi-Fluids Flows

H. Zheng, SheffieldUniversity, Sheffield,Great Britain

Chaired by: A. HASHEMI, Lockheed Martin Corporation, Los Altos, CA1400AIAA-2010-0813 Computation of Hypersonic Shock Wave Flows ofDiatomic Gases and Gas Mixtures Using theGeneralized Boltzmann Equation

R. Agarwal, Washington University in St. Louis,St. Louis, MO

1500AIAA-2010-0814 NonequilibriumIonization and Radiationin Hydrogen- HeliumMixtures

C. Park, KoreaAdvanced Institute ofScience andTechnology, Daejeon,South Korea

1530AIAA-2010-0817 Kinetic Solution of ShockStructure in a Non-Reactive Gas Mixture

E. Josyula, U.S. AirForce ResearchLaboratory,Wright-Patterson AFB,OH

Chaired by: R. CUNNINGTON, Raytheon Corporation, Tucson, AZ, and E. JOSYULA, U.S. Air Force Research Laboratory, Wright-Patterson AFB, OH1400 1430 1500 1530 1600 1630


Tuesday Afternoon / 05 January 2010 Session 141-TP-10 Rarefied Flow Modeling Crystal Ballroom Q

Tuesday Afternoon / 05 January 2010 Session 142-WE-4 Wind Turbine Inflow, Siting, and Wind Farm Analysis Crystal Ballroom G2

Tuesday Afternoon / 05 January 2010 Session 143-WIG-5 / PDL-9 Electrodynamic and Magneto-Hydrodynamic Interactions and Applications Grand Ballroom 2


Chaired by: R. CUNNINGTON, Raytheon Corporation, Tucson, AZ, and E. JOSYULA, U.S. Air Force Research Laboratory, Wright-Patterson AFB, OH1400AIAA-2010-0818 Modeling of CO2Condensation in theHigh Pressure FlowsUsing the StatisticalBGK Method

R. Kumar, PennsylvaniaState University,University Park, PA

1430AIAA-2010-0819 Closely- Coupled DSMCHypersonic Re- EntryFlow Simulations withPhoton Monte CarloRadiation

I. Sohn, PennsylvaniaState University,University Park, PA

1500AIAA-2010-0820 A Hybrid ParticleScheme for SimulatingMultiscale Gas Flowswith Internal EnergyNonequilibrium

J. Burt, University ofMichigan, Ann Arbor, MI

1530AIAA-2010-0821 Towards theDevelopment of a NovelDSMC/CFD CouplingScheme for theSimulation ofRarified/Continuum Flows

S. Diaz, Florida Instituteof Technology,Melbourne, FL

1600AIAA-2010-0822 All- Particle MultiscaleComputation ofHypersonic RarefiedFlow for Mars Entry

E. Jun, University ofMichigan, Ann Arbor, MI

1630AIAA-2010-0823 The Coupled MultiscaleMultiphysics Method(CM3) for Rarefied GasFlows

D. Kessler, NavalResearch Laboratory,Washington, DC

Chaired by: P. MORIARTY, National Renewable Energy Laboratory, Golden, CO, and G. PAWLAS, University of Colorado, Boulder, Boulder, CO1400AIAA-2010-0824 Interaction Between aWind Turbine Array anda Turbulent BoundaryLayer

J. Lebron, RensselaerPolytechnic Institute,Troy, NY

1430AIAA-2010-0825 Wind Farm WakeSimulations inOpenFOAM

T. Stovall, University ofColorado, Boulder,Boulder, CO

1500AIAA-2010-0826 Wind Turbine Siting byUsing Mesoscale ModelData Assimilation andComputational FluidDynamics

F. Zajaczkowski,Pennsylvania StateUniversity, StateCollege, PA

1530AIAA-2010-0827 Large Eddy Simulationsof Large Wind- TurbineArrays in theAtmospheric BoundaryLayer

J. Meyers, CatholicUniversity of Leuven,Leuven, Belgium

1600AIAA-2010-0828 Development of anEmpirical ObstacleWake Model for SmallWind Turbine Micrositing

A. Brunskill, Universityof Guelph, Guelph,Canada

1630AIAA-2010-0829 A Comparison of WindTurbine Load Statisticsfor Inflow TurbulenceFields Based onConventional SpectralMethods and LargeEddy Simulation

C. Sim, PurdueUniversity, WestLafayette, IN

Chaired by: V. BITYURIN, Russian Academy of Sciences, Moscow, Russia, and S. SCHNEIDER, NASA Glenn Research Center, Cleveland, OH1400AIAA-2010-0830 Impact of a MagneticField on Rotation of aGas Discharge Aroundan Axisymmetric Body

S. Bobashev, RussianAcademy of Sciences,Saint Petersburg, Russia

1430AIAA-2010-0831 Velocity Measurementsin Synthetic Jet UsingMagnetically DrivenSurface Discharges

C. Kalra, PrincetonUniversity, Princeton, NJ

1500AIAA-2010-0832 Local MHD Effects onSupersonic Flows in theNonuniform MagneticField

E. Sheikin,Saint-Petersburg StateUniversity, SaintPetersburg, Russia

1530AIAA-2010-0834 Physical Grounds ofExcitation of LinearElectromagneticVibrators in Proximity ofa Conducting Surface

I. Esakov, RussianAcademy of Sciences,Moscow, Russia

1600AIAA-2010-0835 WITHDRAWN Studies of Non-Equilbrium Effects inFramework of ParachuteConcept

V. Bityurin, RussianAcademy of Sciences,Moscow, Russia


Tuesday Afternoon / 05 January 2010 1500 - 1700 Patent Law Workshop Grand Ballroom 10

Tuesday Afternoon / 05 January 2010 1730 - 1830 2010 William Littlewood Memorial Lecture Crystal Ballroom H

Wednesday Morning / 06 January 2010 0800 - 0900 New Horizons Forum Keynote Address Crystal Ballroom H


Chaired by: R. JAWORSKI, Cooper Dunham, New York, NYThis workshop is designed to provide insight into the patent options that are available, as well as the process for obtaining patents. It will include recent changes to patent law to those who may have alreadynavigated, or who are currently navigating this process and will also discuss some current suggested changes and what their impacts may be.

N. Albert MoussaPresidentBlazeTech CorporationCambridge, Massachusetts

Distinguished Speaker: Gen Lester Lyles, USAF (Ret.)Member of the Review of U.S. Human Space Flight Plans Committee

Former Vice Chief of Staff of the United States Air Force, and Commander, Air Force Materiel Command (Invited)

The Future of the U.S. Space Program

The panel will discuss topics such as the new NASA – rationale roles and missions, the future of human spaceflight, Government initiatives vs. private sector investment in a resource constrained environment,


Wednesday Morning / 06 January 2010

0900 - 1130 New Horizons Forum Panel Discussion - Space in the 21st Century - ChangingPriorities Crystal Ballroom J2

Wednesday Morning / 06 January 2010 0900 - 1200 NRC Biological and Physical Sciences in Space Decadal Survey Townhall Grand Ballroom 13

Wednesday Morning / 06 January 2010 0900 - 1100 Renewable Fuels: Are Biofuels the Future Fuel for Aviation ? Grand Ballroom 14


The panel will discuss topics such as the new NASA – rationale roles and missions, the future of human spaceflight, Government initiatives vs. private sector investment in a resource constrained environment,the impact of the emerging commercial space industry, to name a few.

Moderator: Robert S. Dickman, AIAA Executive Director, Maj. Gen., USAF (Retired)

Panelists:

Maj. Gen. Ellen M. Pawlikowski, Deputy Director, National Reconnaissance Office, Chantilly, VA

Gary E. Payton, Deputy Under Secretary, Air Force Space Programs, Washington D.C.

Anthony Galasso, Director, Advanced Integration Capabilities, Phantom Works, Integrated Defense Systems, Huntington Beach, CA

Alexis Livanos, Corporate Vice President and Chief Technology Officer, Northrop Grumman Corporation, Los Angeles, CA

Damon Wells, Senior Policy Analyst, Office of Science and Technology Policy (OSTP), Washington D.C.

Janet E. Petro, Deputy Director, John F. Kennedy Space Center, Kennedy Space Center, FL

An open discussion between NRC decadal survey committee and the AIAA microgravity research community. This is a unique and valuable opportunity for participants in the January, 2010 ASM to havesignificant input to this congressionally requested study, which is intended to help NASA determine the direction of research for microgravity science and exploration for the next decade.

Chaired by: J. TRENT, NASA Ames Research Center, Moffett Field, CA, and V. LYONS, NASA Glenn Research Center, Cleveland, OHPanel session dealing with current and future issues involving renewable energy

Chaired by: D. HIXON, University of Toledo, Toledo, OH0900 0930 1000 1030


Wednesday Morning / 06 January 2010 Session 144-AA-7 Computational Aeroacoustics (CAA) Washington

Wednesday Morning / 06 January 2010 Session 145-ABP-4 Inlets II Grand Ballroom 12

Wednesday Morning / 06 January 2010 Session 146-AD-5 Transonic and Supersonic Aircraft Design Crystal Ballroom K


Chaired by: D. HIXON, University of Toledo, Toledo, OH0900AIAA-2010-0836 A Collision DetectionApproach To ChimeraGrid Assembly for HighFidelity Simulations ofTurbofan Noise

G. Zagaris, University ofIllinois,Urbana-Champaign,Champaign, IL

0930AIAA-2010-0837 Optimization of Finite-Difference BoundaryStencils for ImprovedViscous Stability

R. Hixon, University ofToledo, Toledo, OH

1000AIAA-2010-0838 Simulation of CAABenchmark ProblemsUsing High- OrderSpectral DifferenceMethod and PerfectlyMatched Layers

Y. Zhou, Iowa StateUniversity, Ames, IA

1030AIAA-2010-0839 Proposed BoundaryConditions for Gust-Airfoil Interaction Noise

A. Lau, University ofSouthampton,Southampton, GreatBritain

Chaired by: J. FLAMM, NASA Langley Research Center, Hampton, VA, and V. DIPPOLD, NASA Glenn Research Center, Cleveland, OH0900AIAA-2010-0840 Modeling of CoupledOpen Rotor EngineIntakes

S. Loiodice, University ofCambridge, Cambridge,Great Britain

0930AIAA-2010-0841 A NumericalInvestigation of S- DuctFlows with Boundary-Layer Ingestion

B. Johnson, University ofTennessee,Chattanooga,Chattanooga, TN

1000AIAA-2010-0842 Re- Design of BoundaryLayer Ingesting OffsetInlet via Passive FlowControl Manner

B. Lee, NASA GlennResearch Center,Cleveland, OH

Chaired by: W. ANEMAAT, DARcorporation, Lawrence, KS, and D. BENCHERGUI, Bombardier Aerospace, Dorval, Canada0900AIAA-2010-0843 A Multi- Shock InverseDesign Method for Low-Boom Supersonic Aircraft

A. Haas, StanfordUniversity, Stanford, CA

0930AIAA-2010-0844 Boom- ConstrainedDrag Minimization forDesign of SupersonicConcepts

S. Rallabhandi, NationalInstitute of Aerospace,Hampton, VA

1000AIAA-2010-0845 A Mixed- FidelityApproach for Design ofLow- Boom SupersonicAircraft

W. Li, NASA LangleyResearch Center,Hampton, VA

1030AIAA-2010-0847 Value OperationsMethodology for ValueDriven Design: MediumRange PassengerAirliner Validation

R. Curran, DelftUniversity ofTechnology, Delft, TheNetherlands

1100AIAA-2010-0846 Zero Lift Drag and DragDivergence Predictionfor Finite Wings inAircraft ConceptualDesign

T. Takahashi, NorthropGrumman Corporation,Torrance, CA

1130AIAA-2010-0848 Operating Efficiency ofMilitary Transports (Jetsand Turbo- Props) andComparisons with CivilAircraft

R. Nangia, Nangia AeroResearch, Bristol, GreatBritain

Chaired by: M. XIN, Mississippi State University, Starkville, MS, and S. KOMADINA, Northrop Grumman Corporation, Torrance, CA


Wednesday Morning / 06 January 2010 Session 147-AFM-5 Flight Dynamics - UAVs Chicago

Wednesday Morning / 06 January 2010 Session 148-AMT-6 Rayleigh Scattering Techniques Crystal Ballroom J1

Wednesday Morning / 06 January 2010 Session 149-APA-13 Active Flow Control II Grand Ballroom 9


Chaired by: M. XIN, Mississippi State University, Starkville, MS, and S. KOMADINA, Northrop Grumman Corporation, Torrance, CA0900AIAA-2010-0852 Micro UAV HolonomyControl System Robustfor Gust Wind

R. Kojima, YamaguchiUniversity, Ube, Japan

0930AIAA-2010-0853 Automated DynamicPropeller Testing at LowReynolds Numbers

D. Gamble, OklahomaState University,Stillwater, OK

1000AIAA-2010-0854 Flight Testing of SmallElectric Powered SmallUAS’s with FoldingPropellers

C. Hall, North CarolinaState University,Raleigh, NC

Chaired by: A. MIELKE, NASA Glenn Research Center, Cleveland, OH, and M. REEDER, U.S. Air Force Institute of Technology, Wright-Patterson AFB, OH0900AIAA-2010-0855 Study of Fabry- PerotEtalon Stability andTuning forSpectroscopic RayleighScattering

M. Clem, NASA GlennResearch Center,Cleveland, OH

0930AIAA-2010-0856 Progress on a RayleighScattering Mass FluxMeasurement Technique

A. Mielke-Fagan, NASAGlenn Research Center,Cleveland, OH

1000AIAA-2010-0857 Towards High-Repetition Rate Rayleighand Raman ScatteringImaging in TurbulentJets and Flames

J. Sutton, Ohio StateUniversity, Columbus,OH

1030AIAA-2010-0858 Microplasma ElectronNumber DensityMeasurement byResonant CoherentMicrowave RayleighScattering

Z. Zhang, University ofTennessee, Knoxville,TN

1100AIAA-2010-0859 WITHDRAWN Time- Resolved Multi-parameter RayleighScattering MeasurementSystem

D. Bivolaru, GeorgeWashington University,Hampton, VA

Chaired by: M. AMITAY, Rensselaer Polytechnic Institute, Troy, NY, and M. POST, U.S. Air Force Academy, Colorado Springs, CO0900AIAA-2010-0861 Transient Control of theSeparating Flow over aDynamic Airfoil

G. Woo, GeorgiaInstitute of Technology,Atlanta, GA

0930AIAA-2010-0862 ExperimentalInvestigation ofActuators for FlowControl in S- Duct Inlets

J. Vaccaro, RensselaerPolytechnic Institute,Troy, NY

1000AIAA-2010-0863 High- Lift EnhancementUsing Fluidic Actuation

M. DeSalvo, GeorgiaInstitute of Technology,Atlanta, GA

1030AIAA-2010-0864 Experimental andComputational Study onFlow Characteristics bySynthetic JetsConfiguration

W. Kim, Seoul NationalUniversity, Seoul, SouthKorea

Chaired by: J. LEE, Naval Air Systems Command, Patuxent River, MD, and W. SICKLES, Arnold Engineering Development Center, Arnold AFB, TN0900 0930 1000


Wednesday Morning / 06 January 2010 Session 150-APA-14 Moving Body CFD Simulation II Grand Ballroom 10

Wednesday Morning / 06 January 2010 Session 151-APA-15 Transonic, Supersonic, Hypersonic Aerodynamics I Crystal Ballroom D

Wednesday Morning / 06 January 2010 Session 152-APA-16 Unsteady Aerodynamics III Grand Ballroom 11


Chaired by: J. LEE, Naval Air Systems Command, Patuxent River, MD, and W. SICKLES, Arnold Engineering Development Center, Arnold AFB, TN0900AIAA-2010-0865 Numerical Study of TwoFlapping Airfoils inTandem Configuration

T. Broering, University ofLouisville, Louisville, KY

0930AIAA-2010-0866 Finite- Volume Methodwith TranspirationBoundary Conditions forFlow About OscillatingWings

K. Huckriede, Universityof Twente, Enschede,The Netherlands

1000AIAA-2010-0867 CFD- Modeling of RotorFlowfield Aboard Ship

Y. Lee, Naval AirSystems Command,Patuxent Rover, MD

Chaired by: J. DEBONIS, NASA Glenn Research Center, Cleveland, OH, and L. AUMAN, U.S. Army Research, Development and Engineering Command, Huntsville, AL0900AIAA-2010-0871 Experimentalinvestigation intoParameters GoverningCorner Interactions forTransonic Shock-Wave/Boundary- LayerInteractions

D. Burton, CambridgeUniversity, Cambridge,Great Britain

0930AIAA-2010-0872 A Possible Mechanismfor the Appearance ofthe CarbunclePhenomenon inAerodynamicSimulations

M. Ramalho,Universidade deBrasilia, Brasilia, Brazil

1000AIAA-2010-0873 Ballistic RangeExperiment on the LowSonic BoomCharacteristics ofSupersonic Biplane

A. Toyoda, TohokuUniversity, Sendai,Japan

1030AIAA-2010-0874 Implicit LES forShock/Blunt BodyInteraction

M. Oliveira, University ofTexas, Arlington,Arlington, TX

1100AIAA-2010-0875 A High Order CompactScheme for HypersonicAerothermodynamics

V. Fico, STFCDaresbury Laboratory,Warrington, Great Britain

Chaired by: A. ALTMAN, University of Dayton, Dayton, OH0900AIAA-2010-0876 Particle ImageVelocimetry Studies onShock Wave Diffractionwith Freestream Flow

N. Gongora-Orozco,University ofManchester,Manchester, GreatBritain

0930AIAA-2010-0877 Modeling Dynamic Stallof SC- 1095 Airfoil atHigh Mach Number

B. Clark, GeorgiaInstitute of Technology,Atlanta, GA

1000AIAA-2010-0878 Ensemble and Phase-Locked Averaged LoadsControlled by PlasmaDuty Cycles

X. Meng, NorthwesternPolytechnical University,Xi'an, China (prc)


Wednesday Morning / 06 January 2010 Session 153-ASE-5 AeroSpace Environment Modeling and Instrumentation Atlanta

Wednesday Morning / 06 January 2010 Session 154-CS-2 Engineering Computing/Modeling Environments and Tools Tampa

Wednesday Morning / 06 January 2010 Session 155-EDU-3 Curriculum Development and Best Practices Crystal Ballroom Q


Chaired by: J. WISE, U.S. Air Force Research Laboratory, Hanscom AFB, MA, and D. FERGUSON, U.S. Air Force Research Laboratory, Albuquerque, NM0900AIAA-2010-0882 An ElectromagneticInterference ReductionCheck List forUnmanned AircraftSystem

J. Tristancho, UPC,Castelldefels, Spain

0930AIAA-2010-0884 Introducing a Flight-Ready SpacecraftCharge Monitor

L. Goembel, GoembelInstruments, Baltimore,MD

1000AIAA-2010-0886 Modeling of MartianDust Collection for Non-Stop Mars SampleReturn Mission

T. Ozawa, JapanAerospace ExplorationAgency (JAXA), Chofu,Japan

1030AIAA-2010-1608 High Energy ElectronClimatology thatSupports Deep ChargingRisk Assessment inGEO

J. Bodeau, NorthropGrumman Corporation,Redondo Beach, CA

Chaired by: F. CHEN, Aerojet, Sacramento, CA0900AIAA-2010-0887 Validation of UniversalControls Analysis ToolSix Degree of FreedomKinematics

J. Faure, Florida Instituteof Technology,Melbourne, FL

0930AIAA-2010-0888 WITHDRAWN Global IntegratedDesign Environment,GLIDE, a CollaborativeEngineering Application

M. McGuire, NASAGlenn Research Center,Cleveland, OH

1000AIAA-2010-0889 Synchronize andStabilize Lifecycle Modelfor Large- ScaleSoftware Systems

R. Selby, NorthropGrumman Corporation,Redondo Beach, CA

Chaired by: A. BYERLEY, U.S. Air Force Academy, Colorado Springs, CO0900AIAA-2010-0891 Living Learning Labs: AComponent of theUniversity of Alabama’sEngineering MathAdvancement Program

K. Boykin, University ofAlabama, Tuscaloosa,AL

0930AIAA-2010-0892 ROCKS K- 12 ModelRocketry OutreachProgram at ArizonaState University

J. Villarreal, ArizonaState University, Tempe,AZ

1000AIAA-2010-0893 Capstone Design ProjectChallenges in Inter-institutional,GeographicallyDispersed Teams

P. Witte, GeorgiaInstitute of Technology,Atlanta, GA

1030AIAA-2010-0894 USAF Test Pilot SchoolCurriculum: TestManagement Projects2009

A. Freeborn, U.S. AirForce Test Pilot School,Edwards AFB, CA

1100AIAA-2010-0895 Design of a TypicalOutcome Portfolio forAssessment andContinuous Improvement

S. Karunamoorthy, SaintLouis University, St.Louis, MO

Chaired by: G. CANDLER, University of Minnesota, St Louis Park, MN, and E. WHITE, Texas A&M University, College Station, TX0900 0930 1000 1030


Wednesday Morning / 06 January 2010 Session 156-FD-29 Boundary Layer Transition III Grand Ballroom 3

Wednesday Morning / 06 January 2010 Session 157-FD-30 Internal Flows Grand Ballroom 4

Wednesday Morning / 06 January 2010 Session 158-FD-31 Micro/Nano Fluidics II Grand Ballroom 5


Chaired by: G. CANDLER, University of Minnesota, St Louis Park, MN, and E. WHITE, Texas A&M University, College Station, TX0900AIAA-2010-0896 Boundary Layer StabilityAnalysis of the Free-Piston Shock TunnelHIEST TransitionExperiments

J. Gronvall, University ofMinnesota, Minneapolis,MN

0930AIAA-2010-0897 Comparison ofExperimentallyMeasured andComputed Second-Mode Disturbances inHypersonic Boundary-Layers

C. Alba, U.S. Air ForceResearch Laboratory,Wright-Patterson AFB,OH

1000AIAA-2010-0898 Linear Stability Analysisof Nose BluntnessEffects on HypersonicBoundary LayerTransition

J. Lei, University ofCalifornia, Los Angeles,Los Angeles, CA

1030AIAA-2010-0900 Numerical Investigationof Boundary- layerTransition Initiated by aWave Packet for a Coneat Mach 6

J. Sivasubramanian,University of Arizona,Tucson, AZ

Chaired by: J. BONS, Ohio State University, Columbus, OH, and M. BRIGHT, Northrop Grumman Corporation, San Diego, CA0900AIAA-2010-0902 Consideration Of Three-DimensionalPhenomena Within Two-Dimensional MeridionalFlow Models

A. Willburger, Universityof Kassel, Kassel,Germany

0930AIAA-2010-0903 Heat Transfer Effects onthe Performance of aRadial Turbine WorkingUnder Pulsatile FlowConditions

F. Hellstrom, KTH RoyalInstitute of Technology,Stockholm, Sweden

1000AIAA-2010-0904 Organized StreamwiseVorticity on ConvexSurfaces With ParticularReference to TurbineBlades

J. Gostelow, NationalResearch CouncilCanada, Ottawa, Canada

1030AIAA-2010-0905 Numerical Simulation ofSwirling Flowfield inCombustion Chamberfor Hybrid Rocket Engine

K. Yoshimura, TohokuUniversity, Sendai, Japan

Chaired by: K. CASSEL, Illinois Institute of Technology, Wheaton, IL0900AIAA-2010-0906 Current Conduction andFluid Flow inNanochannels forElectrokinetic PowerGeneration

S. Datta, Ohio StateUniversity, Columbus, OH

0930AIAA-2010-0908 Electrochemical MHD forMicrofluidic Applications

K. Isaac, MissouriUniversity of Scienceand Technology, Rolla,MO

1000AIAA-2010-0909 Optimizing theArrangement and Shapeof Grooves in MicrofluidicComponents

D. Mott, Naval ResearchLaboratory, Washington,DC

Chaired by: A. ALEXEENKO, Purdue University, West Lafayette, IN, and A. TUMIN, University of Arizona, Tucson, AZ


Wednesday Morning / 06 January 2010 Session 159-FD-32 Non-Equilibrium Thermofluid Phenomena (Invited) Grand Ballroom 6

Wednesday Morning / 06 January 2010 Session 160-FD-33 Passive Flow Control Crystal Ballroom L

Wednesday Morning / 06 January 2010 Session 162-FD-35 Turbulent Separating Flows Crystal Ballroom M


Chaired by: A. ALEXEENKO, Purdue University, West Lafayette, IN, and A. TUMIN, University of Arizona, Tucson, AZ0900AIAA-2010-0910 Turbulence and Stochasticity in High- SpeedReactive Flows

E. Oran, Naval Research Laboratory,Washington, DC

1000AIAA-2010-0911 The Limits of Two- Temperature Kinetic Model inAir

C. Park, Korea Advanced Institute of Science andTechnology, Daejeon, South Korea

1100AIAA-2010-0912 The Potential Role ofElectronically- ExcitedStates in RecombiningFlows

G. Candler, University ofMinnesota, Minneapolis,MN

Chaired by: R. JOSLIN, Office of Naval Research, Arlington, VA, and U. GHIA, University of Cincinnati, Cincinnati, OH0900AIAA-2010-0914 Momentum Increase inWall Adjacent Flow viaHexagonal EmbeddedCavities

A. Lang, University ofAlabama, Tuscaloosa,AL

0930AIAA-2010-0915 DNS of Passive SurfaceTextures to Constrainthe Spreading ofTurbulent Spots

J. Strand, University ofTexas, Austin, Austin,TX

1000AIAA-2010-0916 Large Eddy Simulationof Flow Over a Flat-Window CylindricalTurret with Passive FlowControl

P. Morgan, OhioAerospace Institute,Wright-Patterson AFB,OH

1030AIAA-2010-0917 Control of Flow Past aCircular Cylinder via aSpanwise Surface Wire:Effect of the Scale of theWire

A. Ekmekci, University ofToronto, Toronto,Canada

Chaired by: D. RIZZETTA, U.S. Air Force Research Laboratory, Wright-Patterson AFB, OH, and A. GROSS, University of Arizona, Tucson, AZ0900AIAA-2010-0918 Three- DimensionalTurbulent FlowSeparation in Diffusers

E. Jeyapaul, Iowa StateUniversity, Ames, IA

0930AIAA-2010-0919 Hybrid RANS/LESSimulations of TurbulentChannel and DiffuserFlows

A. Gross, University ofArizona, Tucson, AZ

1000AIAA-2010-0920 A Comparison ofDetached- EddySimulation andReynolds- StressModeling Applied to theFlow over a Backward-Facing Step and anAirfoil at Stall

A. Probst, University ofBraunschweig,Braunschweig, Germany

1030AIAA-2010-0921 A DES ProcedureApplied to the Flow Overa NACA0012 Airfoil

R. Bozinoski, Universityof Califonia, Davis,Davis, CA

1100AIAA-2010-0922 Large- Eddy Simulationof Compressible Flowover Backward- FacingStep Using ChebyshevMultidomain Method

H. Kanchi, University ofIllinois, Chicago,Chicago, IL

1130AIAA-2010-0923 Implicit LES ofCompressible TurbulentFlow over a Backward-Facing Step in theNozzle of Solid RocketMotor

K. Ishiko, JapanAerospace ExplorationAgency (JAXA),Sagamihara, Japan


Wednesday Morning / 06 January 2010 Session 163-FD-36 Unsteady Compressible Flows Crystal Ballroom N

Wednesday Morning / 06 January 2010 Session 164-GT-6 Data Analysis & Instrumentation Crystal Ballroom G1

Wednesday Morning / 06 January 2010 Session 165-GTE-8 Gas Turbine Engine Modeling Crystal Ballroom A


http://www.aiaa.org/agenda.cfm?lumeetingid=1812&dateget=all#session12738.

Chaired by: J. ELDREDGE, University of California, Los Angeles, Los Angeles, CA, and H. BABINSKY, University of Cambridge, Cambridge, Great Britain0900AIAA-2010-0924 A Numerical Study ofPressure/Shock WavesInteractions in TransonicAirfoil Flow UsingOptimized WENOSchemes

I. Klioutchnikov, RWTHAachen University,Aachen, Germany

0930AIAA-2010-0925 An Experimental andNumerical Study of anOscillating TransonicShock Wave in a Duct

P. Bruce, University ofCambridge, Cambridge,Great Britain

1000AIAA-2010-0926 Time- AccurateSimulation of ShockPropagation andReflection in an Axi-Symmetric Shock Tube

M. Lamnaouer,University of CentralFlorida , Orlando, FL

1030AIAA-2010-0928 Parametric ViscousAnalysis of GustInteraction with SD7003Airfoil

V. Golubev,Embry-RiddleAeronautical University,Daytona Beach, FL

1100AIAA-2010-0929 WITHDRAWN Implicit Large EddySimulation of Transitionto Turbulence in LowReynolds Number Flows

A. Uranga,Massachusetts Instituteof Technology,Cambridge, MA

Chaired by: W. BAKER, Lockheed Martin Corporation, Fort Worth, TX, and J. VAN AKEN, Jacobs Technology, Moffett Field, CA0900AIAA-2010-0930 Optimization ofRegression Models ofExperimental DataUsing ConfirmationPoints


0930AIAA-2010-0931 The Role of Hierarchy inResponse SurfaceModeling of WindTunnel Data


1000AIAA-2010-0932 Development of a UserInterface for aRegression AnalysisSoftware Tool


1030AIAA-2010-0933 Low FrequencyVibration Data Analysisvia Digital Image Data ofHigh Speed Camera

Y. Jeng, National ChengKung University, Tainan,Taiwan (roc)

1100AIAA-2010-0934 Debond Detection ofShell /Insulation in SRMby Thermal Wave NDT

Z. Yang, Xi'an Hi-TechInstitute, Xi'an, China(prc)

Chaired by: R. WEBSTER, University of Tennessee, Chattanooga, Chattanooga, TN, and A. HALE, Aerospace Testing Alliance, Arnold AFB, TN

Chaired by: D. REDDY, NASA Glenn Research Center, Cleveland, OH, and R. MOEHLENKAMP, Pratt & Whitney, A United Technologies Company, West Palm Beach, FL0900 0930 1000 1030 1100


Wednesday Morning / 06 January 2010 Session 166-HAPB-6 Supersonic Inlets and Isolators Crystal Ballroom E

Wednesday Morning / 06 January 2010 Session 167-IS-3 Fault-Tolerant Flight Control Crystal Ballroom P

Wednesday Morning / 06 January 2010 Session 238-MDO-1 Optimization Algorithms and Methodology I Crystal Ballroom C


Chaired by: D. REDDY, NASA Glenn Research Center, Cleveland, OH, and R. MOEHLENKAMP, Pratt & Whitney, A United Technologies Company, West Palm Beach, FL0900AIAA-2010-0938 ExperimentalInvestigation on theInfluence of Yaw Angleon the Inlet Performanceat Mach 7

O. Hohn, GermanAerospace Center(DLR), Cologne,Germany

0930AIAA-2010-0939 The Three WeakSolution Regimes ofSupersonic Conical Flowand Their Impact onEngine Inlets

N. Smith, University ofMaryland, College Park,MD

1000AIAA-2010-0940 Design of Modular,Shape- transitioningInlets for a ConicalHypersonic Vehicle

R. Gollan, NASALangley ResearchCenter, Hampton, VA

1030AIAA-2010-0941 A ComputationalInvestigation of FlowThrough anAxisymmetricSupersonic Inlet

M. Conway, PurdueUniversity, WestLafayette, IN

1100AIAA-2010-0942 Parametric Investigationof Racetrack- to-Circular Cross- SectionTransition of a Dual-mode Ramjet Isolator

N. Bagaveyev,Embry-RiddleAeronautical University,Daytona Beach, FL

Chaired by: S. HARVEY, U.S. Air Force Research Laboratory, Kirtland AFB, NM, and E. ATKINS, University of Michigan, Ann Arbor, MI0900AIAA-2010-0944 Fault- Tolerant FlightControl System Designby a Dual- Loop ControlStrategy

M. Mehrtash, ConcordiaUniversity, Montréal,Canada

0930AIAA-2010-0945 Adaptive Sliding ModeFault Tolerant Control ofCivil Aircraft withSeparated Uncertainties

T. Wang, ConcordiaUniversity, Montréal,Canada

1000AIAA-2010-0946 Dynamic InverseResilient Control of aDamaged AsymmetricGeneral Aviation Aircraft

M. Arruda, Wichita StateUniversity, Wichita, KS

1030AIAA-2010-0947 Fault- Tolerant Controlfor Quadrotor UAV viaBackstepping Approach

X. Zhang, ConcordiaUniversity, Montréal,Canada

1100AIAA-2010-0948 Trajectory TrackingControl of a QuadrotorUnmanned Mini-Helicopter

Z. Zuo, Beijing Universityof Aeronautics andAstronautics, Beijing,China (prc)

Chaired by: P. BERAN, U.S. Air Force Research Laboratory, Wright-Patterson AFB, OH, and A. LANDMANN, The Boeing Company, Woodinville, WA0900AIAA-2010-1310 WITHDRAWN Comparison of HeuristicOptimization Methodsfor MultidisciplinaryDesign of Air- LaunchedSpace Launch Vehicle

A. Rafique, BeihangUniversity, Beijing,China (prc)

0930AIAA-2010-1311 Aerospace Design: AComparative Study ofOptimizers

J. Badyrka, AuburnUniversity, Auburn, AL

1000AIAA-2010-1313 Simplex ElementsStochastic Collocationfor UncertaintyPropagation in RobustDesign Optimization

J. Witteveen, StanfordUniversity, Stanford, CA

1030AIAA-2010-1314 High FidelityMultidisciplinaryOptimization (HFMDO)

K. Alston, M4Engineering, LongBeach, CA

1100AIAA-2010-1315 The KNOMADMethodology forIntegration ofMultidisciplinaryEngineering KnowledgeWithin AerospaceProduction

R. Curran, DelftUniversity ofTechnology, Delft, TheNetherlands


Wednesday Morning / 06 January 2010 Session 168-PC-12 Laminar Flames II Los Angeles

Wednesday Morning / 06 January 2010 Session 169-PC-13 Solid Propellants and Detonations Denver

Wednesday Morning / 06 January 2010 Session 170-PDL-10 Joint PDL/WIG/FD/TP Plasma Actuator Session V: DBDs Grand Ballroom 1


Chaired by: J. POWERS, University of Notre Dame, Notre Dame, IN, and M. MATALON, University of Illinois, Urbana-Champaign, Urbana, IL0900AIAA-2010-0950 Performance of JP- 8Surrogate Models inPredicting LaboratoryJet Flames

V. Katta, InnovativeScientific Solutions, Inc.,Dayton, OH

0930AIAA-2010-0951 Laminar Burning Speedsand Markstein Lengthsof n- Decane/Air, n-Decane/O2/He, Jet-A/Air and S- 8/Air Flames

D. Singh, PurdueUniversity, WestLafayette, IN

1000AIAA-2010-0953 Edge Flames in ConfinedMixing Layers

J. Bieri, NorthwesternUniversity, Evanston, IL

1030AIAA-2010-0954 Analysis of the Reaction-Advection- DiffusionSpectrum OflaminarPremixed Flames

A. Al-Khateeb, Universityof Notre Dame, NotreDame, IN

Chaired by: O. HAIDN, German Aerospace Center (DLR), Lampoldshausen, Germany, and C. CARTER, U.S. Air Force Research Laboratory, Wright-Patterson AFB, OH0900AIAA-2010-0956 Study of Heat Loadsfrom Steady Deflagrationand Pulsed DetonationCombustion

A. Naples, InnovativeScientific Solutions, Inc.,Dayton, OH

0930AIAA-2010-0957 Determination ofPractical ComputationalCell Size for Simulationof H2 Air Detonations inPulse DetonationEngines

I. Ho, NavalPostgraduate School,Monterey, CA

1000AIAA-2010-0958 Parametric Investigationon the Sensitivity of theSimplified AluminumCombustion Modeling

H. Yang, YonseiUniversity, Seoul, SouthKorea

1030AIAA-2010-0960 Aluminium AgglomerateSize Measurement of theNano/Micro- AluminizedComposite Propellants

J. Kandasamy, IndianInstitute of Technology,Madras, Chennai, India

Chaired by: J. POGGIE, U.S. Air Force Research Laboratory, Wright-Patterson AFB, OH, and J. LINEBERRY, LyTec, Manchester, TN0900AIAA-2010-0961 Periodic ElectrodynamicField of Dielectric BarrierDischarge

P. Huang, Wright StateUniversity, Dayton, OH

0930AIAA-2010-0962 Spatially ResolvedOptical EmissionSpectroscopyMeasurements within aSingle Microdischarge ofa Dielectric BarrierDischarge

S. Stanfield, WrightState University,Dayton, OH

1000AIAA-2010-0963 Simulations of InitialArgon Dielectric BarrierDischarges Using thePIC Code Magic

M. Huerta, University ofMiami, Coral Gables, FL

1030AIAA-2010-0964 Investigation ofImpedanceCharacteristics andPower Delivery forDielectric BarrierDischarge PlasmaActuators

J. Zito, University ofFlorida, Gainesville, FL

1100AIAA-2010-0965 Novel Multi- BarrierPlasma Actuators forIncreased Thrust

R. Durscher, Universityof Florida, Gainesville,FL

1130AIAA-2010-0966 Three- DimensionalPlasma and Fluid FlowSimulation Inside aMicroscaleElectrohydrodynamicPump



Wednesday Morning / 06 January 2010 Session 171-SE-2 Systems Engineering II Boston

Wednesday Morning / 06 January 2010 Session 172-SEC-3 Applied Research to Enable Space Access and Exploration Crystal Ballroom F

Wednesday Morning / 06 January 2010 Session 173-TES-2 Fire Dynamics and Modeling Crystal Ballroom B


Chaired by: J. EILER, Stellar Solutions, Littleton, CO, and E. NICHOLS, Orbital Sciences Corporation, Chandler, AZ0900AIAA-2010-0967 A System LifecycleApproach toMaintenance Planning inAerospace Using DigitalManufacturing

J. Butterfield, Queen'sUniversity Belfast,Belfast, Northern Ireland

0930AIAA-2010-0968 Through- Life Supportand the Aircraft Lifecycle

L. Webb, RMITUniversity, Melbourne,Australia

1000AIAA-2010-0969 A Systems EngineeringApproach to Aero-Engine Life CycleCosting

J. Wong, University ofSouthampton,Southampton, GreatBritain

1030AIAA-2010-0970 System LevelAirworthiness Tool(SLAT)

D. Burke, North CarolinaState University,Raleigh, NC

1100AIAA-2010-0971 Systems Engineering inStep_SATdb andQuickSAT, a Web-Based and OpenSource Satellite DesignAutomation Environment

A. Santangelo,sci_Zone, Rio Ranco,NM

1130AIAA-2010-0972 An Evolution ofMorphological AnalysisApplications in SystemsEngineering

H. Jimenez, GeorgiaInstitute of Technology,Atlanta, GA

Chaired by: P. MURAD, Morningstar Applied Physics, LLC, Vienna, VA, and C. REYNERSON, The Boeing Company, Chantilly, VA0900AIAA-2010-0973 Strategic Perspectivesand TechnicalArchitecture Overview ofIndian SpaceExploration Missions

V. Sundararajan, , SanJose, CA

0930AIAA-2010-0974 Global Trends in SpaceAccess and Utilization

S. Rahman, NASAStennis Space Center,Stennis Space Center,MS

1000AIAA-2010-1609 The Challenges ofDeveloping theTechnology for ARealistic StarshipPropulsor

P. Murad, MorningstarApplied Physics, LLC,Vienna, VA

1030AIAA-2010-1610 Pure ElectromagneticPropulsion and theProblem of GEM (Gravityand Electro- Magnetism)Unification

J. Brandenburg, OrbitalTechnologiesCorporation, Madison ,WI

Chaired by: J. MODER, NASA Glenn Research Center, Cleveland, OH, and G. ROY, Office of Naval Research, Arlington, VA0900AIAA-2010-0976 BRANZFIRE:Application to StructuralFires with Sprinklers

M. Mohammed, Lilley &Associates, Stillwater,OK

0930AIAA-2010-0977 A Two- Story HouseFire: Temperatures andSmoke DetectorActivation with VariousFires Using the CFASTFire Computer Code

R. Vadlamuri, Lilley &Associates, Stillwater,OK

1000AIAA-2010-0978 Two- Room StructuralFire Calculations with theFDS Computer Code forSmoke and HeatDetector Response

S. Kotha, Lilley &Associates, Stillwater,OK

1030AIAA-2010-0979 Heat Transfer Simulationof Slug Flow inMicrochannels

A. Mehdizadeh,University of Florida,Gainesville, FL


Wednesday Morning / 06 January 2010 Session 174-TP-11 Ablation I New Orleans

Wednesday Morning / 06 January 2010 Session 175-TP-12 Direct Simulation Monte Carlo Methods II Miami

Wednesday Morning / 06 January 2010 Session 176-TP-13 Thermal Protection Systems New York


Chaired by: R. AGARWAL, Washington University in St Louis, St Louis, MO, and R. GOSSE, U.S. Air Force Research Laboratory, Wright-Patterson AFB, OH0900AIAA-2010-0981 Non- EquilibriumAblation of PhenolicImpregnated CarbonAblator

F. Milos, NASA AmesResearch Center,Moffett Field, CA

0930AIAA-2010-0983 Simulaing AblatingPhenomenon for EarthReentry

J. Shang, Wright StateUniversity, Dayton, OH

1000AIAA-2010-0984 Microscopic ScaleSimulation of theAblation of FibrousMaterials

J. Lachaud, NASA AmesResearch Center, MoffettField, CA

1030AIAA-2010-0982 Modeling the Motion ofPyrolysis Gas ThroughCharring AblatingMaterial UsingDiscontinuous GalerkinFinite Elements

A. Bhatia, University ofFlorida, Gainesville, FL

Chaired by: D. GOLDSTEIN, University of Texas, Austin, Austin, TX0900AIAA-2010-0985 Analysis of KineticApproach toHomogeneousCondensation in WaterExpansions

Z. Li, PennsylvaniaState University, StateCollege, PA

0930AIAA-2010-0986 Rarefied CompressibleTwo- Dimensional JetFlows

K. Khasawneh, NewMexico State University,Las Cruces, NM

1000AIAA-2010-0987 Modeling of ElectronicExcitation and Radiationfor Hypersonic Re- EntryFlows in DSMC

T. Ozawa, JapanAerospace ExplorationAgency, Chofu, Japan

1030AIAA-2010-0988 Modeling of CrewExploration vehicle Re-entry Ablation Flows

E. Titov, PennsylvaniaState University,University Park, PA

Chaired by: E. SHORT, and J. KAPAT, University of Central Florida, Oviedo, FL0900AIAA-2010-0991 Reducing AerodynamicHeating by the OpposingJet in Supersonic andHypersonic Flows

I. Tamada, KyushuUniversity, Fukuoka,Japan

0930AIAA-2010-0992 Assessment of InjectionInduced TurbulenceModel for theHemisphere with WallInjection

G. Jeong, SeoulNational University,Seoul, South Korea

1000AIAA-2010-0993 Development of aNumerical Code for TPSDesign and High-Temperature and High-Strength material

D. Kim, Seoul NationalUniversity, Seoul, SouthKorea

1030AIAA-2010-0994 Reliability of ClassicalMolecular DynamicsMethod toThermodynamicProperties of Hydrogen

H. Nagashima, AoyamaGakuin University,Sagamihara, Japan

Chaired by: J. JONKMAN, National Renewable Energy Laboratory, Golden, CO, and H. NAMIK, University of Auckland, Auckland, New Zealand0900 0930 1000 1030 1100


Wednesday Morning / 06 January 2010 Session 177-WE-5 Offshore Wind Turbine Simulation and Control Crystal Ballroom G2

Wednesday Morning / 06 January 2010 Session 178-WIG-6 / PDL-11 Microwave-Based Flow Control Grand Ballroom 2

Wednesday Afternoon / 06 January 2010 1200 - 1300 6th Annual Public Policy Luncheon Grand Ballroom 7/8


Chaired by: J. JONKMAN, National Renewable Energy Laboratory, Golden, CO, and H. NAMIK, University of Auckland, Auckland, New Zealand0900AIAA-2010-0996 Incorporating IrregularNonlinear Waves inCoupled Simulation ofOffshore Wind Turbines

P. Agarwal, StressEngineering Services,Houston, TX

0930AIAA-2010-0998 A Comparison of First-Order AerodynamicAnalysis Methods forFloating Wind Turbines

T. Sebastian, Universityof Massachusetts,Amherst, Amherst, MA

1000AIAA-2010-0999 Individual Blade PitchControl of a FloatingOffshore Wind Turbineon a Tension LegPlatform

H. Namik, University ofAuckland, Auckland,New Zealand

1030AIAA-2010-1000 Active Structural Controlof Offshore WindTurbines

M. Lackner, University ofMassachusetts,Amherst, Amherst, MA

1100AIAA-2010-1001 Lateral Tower LoadMitigation by GeneratorTorque Control

B. Kallesøe, Risø DTU,Roskilde, Denmark

Chaired by: E. SON, Russian Academy of Sciences, Moscow, Russia, and C. SUCHOMEL, U.S. Air Force, Wright-Patterson AFB, OH0900AIAA-2010-1002 Effective Area ofMicrowave DischargeInteraction with EMBeam Exciting It

D. Bychkov, RussianAcademy of Sciences,Moscow, Russia

0930AIAA-2010-1003 Boundary- Layer ControlBased on LocalizedPlasma Generation:Development of theMicrowave System


1000AIAA-2010-1004 Instabilities and VortexCharacteristics DuringInteraction of MicrowaveFilaments with Body inSupersonic Flow

O. Azarova, RussianAcademy of Sciences,Moscow, Russia

1030AIAA-2010-1005 Interaction ofMicrowave- GeneratedPlasma withHemisphere- Cone-Cylinder

D. Knight, RutgersUniversity, Piscataway,NJ

1100AIAA-2010-1006 ElectrodynamicProblems of Boundary-Layer Control MethodBased on Array ofMicrowave- HeatedElements


1130AIAA-2010-1007 Boundary- Layer ControlBased on LocalizedPlasma Generation:Wind- TunnelInvestigations

P. Vynogradskyy,National AviationUniversity, Kiev, Ukraine

Chaired by: C. TINNEY, University of Texas, Austin, Austin, TX1400 1430 1500


Wednesday Afternoon / 06 January 2010 Session 179-AA-8 Vibration and Active Noise Control Washington

Wednesday Afternoon / 06 January 2010 Session 180-AD-6 Aircraft Conceptual Design Studies Crystal Ballroom K

Wednesday Afternoon / 06 January 2010 Session 181-AD-7 Micro Air Vehicle Design Crystal Ballroom L


Chaired by: C. TINNEY, University of Texas, Austin, Austin, TX1400AIAA-2010-1008 Navier- StokesSimulations of AcousticStreaming for FlowControl andMicropropulsion

T. Surti, Embry-RiddleAeronautical University,Daytona Beach, FL

1430AIAA-2010-1009 Sound TransmissionCalculation ThroughStructural Models

K. Murakami, JapanAerospace ExplorationAgency (JAXA), Chofu,Japan

1500AIAA-2010-1010 WITHDRAWN Vibration Control of ARotating SmartComposite Beam

O. Ozdemir Ozgumus,Istanbul TechnicalUniversity, Istanbul,Turkey

Chaired by: M. PRICE, Queen's University Belfast, Belfast, Northern Ireland, and D. HALL, DHC Engineering, Morro Bay, CA1400AIAA-2010-1011 A Conceptual Design ofa Short Takeoff andLanding Regional JetAirliner


1430AIAA-2010-1012 Conceptual Design of aSubmersible Airplane

G. Crouse, AuburnUniversity, Auburn, AL

1500AIAA-2010-1013 Toward Zero Sonic-Boom and HighEfficiency SupersonicFlight, Part I: A NovelConcept of SupersonicBi- Directional FlyingWing

G. Zha, University ofMiami, Coral Gables, FL

1530AIAA-2010-1014 The Suitability of Hybridvs. ConventionalAirships for PersistentSurveillance Missions

B. Buerge, GuardianFlight Systems, LLC,Elizabeth City, NC

1600AIAA-2010-1015 Reducing Aviation'sEnvironmental ImpactThrough Large Aircraftfor Short Ranges

G. Kenway, University ofToronto, Toronto,Canada

1630AIAA-2010-1016 AerodynamicOptimization of an Over-the- Wing- Nacelle-Mount Configuration

R. Yoneta, TohokuUniversity, Sendai,Japan

Chaired by: G. CROUSE, Auburn University, Auburn, AL, and P. BERAN, U.S. Air Force Research Laboratory, Wright-Patterson AFB, OH1400AIAA-2010-1017 Micro Air VehicleFlapping WingEffectiveness, Efficiencyand AeroelasticityRelationships

P. Wu, University ofFlorida, Gainesville, FL

1430AIAA-2010-1018 Development ofFlapping Wing Micro AirVehicles - Design, CFD,Experiment and ActualFlight

C. Hsu, Wright StateUniversity, Dayton, OH

1500AIAA-2010-1019 Characteristics ofButterfly Wing Motionsand Their Application toMicro Flight Robot

M. Fuchiwaki, KyushuInstitute of Technology,Iizuka, Japan

1530AIAA-2010-1020 Preliminary andConceptual Design of aRemotely PilotedDucted Fan MAV

B. Stiltner, AVID LLC,Blacksburg, VA

1600AIAA-2010-1021 Detailed Design,Construction, and FlightTests of a RemotelyPiloted Ducted Fan MAV

B. Stiltner, AVID LLC,Blacksburg, VA

1630AIAA-2010-1022 Evaluation ofAutomatically DesignedMicro Air Vehicles andFlight Testing

K. Amadori, LinköpingUniversity, Linköping,Sweden

Chaired by: G. ABATE, U.S. Air Force Research Laboratory, Eglin AFB, FL, and A. AHMED, Auburn University, Auburn, AL1400 1430 1500 1530 1600 1630


Wednesday Afternoon / 06 January 2010 Session 182-AFM-6 Flight Dynamics - Flapping Flight Chicago

Wednesday Afternoon / 06 January 2010 Session 183-AMT-7 Velocimetry Crystal Ballroom J1

Wednesday Afternoon / 06 January 2010 Session 184-APA-17 Create-AV: Testing and Evaluation of High Performance Computing Software I Grand Ballroom 9


Chaired by: G. ABATE, U.S. Air Force Research Laboratory, Eglin AFB, FL, and A. AHMED, Auburn University, Auburn, AL1400AIAA-2010-1023 Dynamics and Control ofa Biomimetic VehicleUsing Biased WingbeatForcing Functions: Part I- Aerodynamic Model

M. Oppenheimer, U.S.Air Force,Wright-Patterson AFB,OH

1430AIAA-2010-1024 Dynamics and Control ofa Biomimetic VehicleUsing Biased WingbeatForcing Functions: PartII - Controller

D. Doman, U.S. AirForce, Wright-PattersonAFB, OH

1500AIAA-2010-1025 An Experimental Studyof Unsteady VortexStructures in the Wakeof a PiezoelectricFlapping Wing

L. Clemons, Iowa StateUniversity, Ames, IA

1530AIAA-2010-1026 Proper OrthogonalDecomposition ofFlexible Clap and FlingMotions via High- SpeedDeformationMeasurements

B. Stanford, U.S. AirForce ResearchLaboratory,Wright-Patterson AFB,OH

1600AIAA-2010-1027 Flexible Hovering WingMotions: ProperOrthogonalDecomposition Analysis

T. Fitzgerald, Universityof Maryland, CollegePark, MD

1630AIAA-2010-1028 Optimal Flight of RufousHummingbirds in Hover:An ExperimentalInvestigation

H. Bocanegra Evans,New Mexico StateUniversity, Las Cruces,NM

Chaired by: T. JENKINS, MetroLaser, Inc., Irvine, CA, and S. WATANABE, Japan Aerospace Exploration Agency (JAXA), Tokyo, Japan1400AIAA-2010-1029 A Stereoscopic PIVStudy of a Near- FieldWingtip Vortex

H. Igarashi, Iowa StateUniversity, Ames, IA

1430AIAA-2010-1030 Three- ComponentVelocity FieldMeasurements Near aParachute During aDrop Test

T. Jenkins, MetroLaser,Inc., Irvine, CA

1500AIAA-2010-1031 PIV Measurements ofthe CEV Hot AbortMotor Plume for CFDValidation

M. Wernet, NASA GlennResearch Center,Cleveland, OH

1530AIAA-2010-1032 PIV Investigation ofReynolds Number 200Photodriven FlappingWings in Air

A. Bani Younes,University of Dayton,Dayton, OH

1600AIAA-2010-1033 Particle Size Control forPIV Seeding Using DryIce

B. Love, U.S. Air ForceInstitute of Technology,Wright-Patterson AFB,OH

1630AIAA-2010-1034 Planar DopplerVelocimetry Applied inthe AEDC 16T Large-Scale Transonic WindTunnel

J. Wehrmeyer,Aerospace TestingAlliance, Arnold AFB, TN

Chaired by: N. HARIHARAN, CREATE-AV, Patuxent River, MD1400AIAA-2010-1035 Landing Pitch ControlAnalysis of a BlendedWing Body UCAV

J. Chung, Naval AirSystems Command,Patuxent River, MD

1430AIAA-2010-1036 Effective Use of CFD forMilitary Aircraft Stabilityand Control Evaluations

D. Findlay, Naval AirSystems Command,Patuxent River, MD

1500AIAA-2010-1037 CFD Generation ofFlight Databases forUAVs for Use in theFlight Certification Air-Worthiness Process

T. Shafer, Naval AirSystems Command,Patuxent River, MD

1530AIAA-2010-1039 Demonstration of AnIntegrated Test andEvaluation(IT&E)Process for Airframe-Propulsion SystemsAsapplied to A CurrentWeapon System Program

M. Davis, AerospaceTesting Alliance, ArnoldAFB, TN


Wednesday Afternoon / 06 January 2010 Session 185-APA-18 High Angle of Attack and High Lift Aerodynamics Grand Ballroom 10

Wednesday Afternoon / 06 January 2010 Session 186-APA-19 Transonic, Supersonic, Hypersonic Aerodynamics II Grand Ballroom 11

Wednesday Afternoon / 06 January 2010 Session 187-APA-20 VSTOL/STOL Aerodynamics Grand Ballroom 12


Chaired by: J. AZEVEDO, National Institute for Space Research (INPE), São José dos Campos, Brazil, and S. MORRIS, Engineering Systems, Inc., Colorado Springs, CO1400AIAA-2010-1040 Assessment of StingEffect on X- 31 AircraftModel Using CFD

A. Jirasek, U.S. AirForce Academy,Colorado Springs, CO

1430AIAA-2010-1041 Influence of PlasmaActuations on ForebodySide Forces and Wakes

Z. Zhao, NorthwesternPolytechnical University,Xi'an, China (prc)

1500AIAA-2010-1043 Maximum Lift of theWing Shape Bodies forUnsteady MotionConverges to AboutCL=2.5

K. Izumi, JapanAerospace ExplorationAgency (JAXA), Chofu ,Japan

1530AIAA-2010-1044 A Computational Studyon the Effect of ChineNose Shapes on aSlender Body FlightVehicle at High Anglesof Attack

S. Lim, YeungnamUniversity, Gyeongsan,South Korea

1600AIAA-2010-1045 A Proposal of NewFuselage Configurationsfor Realizing ReusableLaunch Vehicles

T. Ishida, KyushuUniversity, Fukuoka,Japan

Chaired by: K. WAITHE, Gulffstream Aerospace Corporation, Savannah, GA, and J. DESPIRITO, U.S. Army Research Laboratory, Aberdeen Proving Ground, MD1400AIAA-2010-1046 Numerical Evaluation ofAerodynamicInterference BetweenWing and Fuselage forHypersonicExperimental Aircraft

A. Tanabe, KeioUniversity, Yokohama,Japan

1430AIAA-2010-1047 Simulation ofHypersonic ShockWave/Boundary LayerInteraction Using HighOrder WENO Scheme

Y. Shen, University ofMiami, Coral Gables, FL

1500AIAA-2010-1048 Explicit Exact and Third-Order Pressure-Deflection Solutions forOblique Shock andExpansion Waves

D. Mateescu, McGillUniversity, Montréal,Canada

1530AIAA-2010-1049 Interaction of HeatedFilaments with a BluntCylinder in SupersonicFlow

K. Anderson, , ,

1600AIAA-2010-1050 Numerical Investigationof an Elliptic Cone atHigh Angle of Incidencein Nonequilibrium Flow

M. Atkinson, U.S. AirForce ResearchLaboratory,Wright-Patterson AFB,OH

Chaired by: R. TRAMEL, Kratos/Digital Fusion Solutions, Inc., Huntsville, AL, and M. CALVERT, U.S. Army Research, Development and Engineering Command, Redstone Arsenal, AL1400AIAA-2010-1051 The Turbulent Structureof a Ground Vortex

J. Barata, UniversidadeBeira Interior, Covilhã,Portugal

1430AIAA-2010-1052 A Compact Method forModeling theAerodynamics of DuctedFan Vehicles

O. Ohanian, AVID LLC,Blacksburg, VA

1500AIAA-2010-1053 Design and Performanceof Circulation ControlFlap Systems

R. Golden, CaliforniaPolytechnic StateUniversity, San LuisObispo, CA

1530AIAA-2010-1054 Assessing the v2- fTurbulence Models forCirculation ControlApplications

T. Storm, CaliforniaPolytechnic StateUniversity, San LuisObispo, CA

Chaired by: G. PATNAIK, Naval Research Laboratory, Silver Spring, MD


Wednesday Afternoon / 06 January 2010 Session 188-CS-3 HPC II: CPU/Cluster Applications and Benchmarking Tampa

Wednesday Afternoon / 06 January 2010 Session 189-EDU-4 Workshop: Project-Based Learning Experiences Crystal Ballroom Q

Wednesday Afternoon / 06 January 2010 Session 190-FD-37 Boundary Layer Transition IV Grand Ballroom 3


Chaired by: G. PATNAIK, Naval Research Laboratory, Silver Spring, MD1400AIAA-2010-1057 CGNS I/O Performanceon Parallel File Systems

T. Hauser, NorthwesternUniversity, Evanston, IL

1430AIAA-2010-1058 PerformanceCharacterization ofOverflow on Multi- CoreBased Cluster Computers

T. Hauser, NorthwesternUniversity, Evanston, IL

1500AIAA-2010-1059 WITHDRAWN Java HPCC Multi-Physics Solver

T. Ludewig,HPCC-Space GmbH,Salzgitter, Germany

Chaired by: P. GRAY, U.S. Naval Academy, Annapolis, Maryland, and S. BANZAERT, Massachusetts Institute of Technology, Cambridge, MA1400Oral Presentation Workshop: Designing, Conducting, and Assessing Project- Based Learning Experiences in Engineering Education

E. Crawley, Massachusetts Institute of Technology, Cambridge, MA

Chaired by: S. SCHNEIDER, Purdue University, West Lafayette, IN, and M. HOLDEN, CUBRC, Buffalo, NY1400AIAA-2010-1061 Hypersonic Boundary-Layer TransitionExperiments in a Mach-6 Quiet Tunnel

D. Berridge, PurdueUniversity, WestLafayette, IN

1430AIAA-2010-1062 Boundary- LayerTransition on Cones atAngle of Attack in aMach- 6 Quiet Tunnel

E. Swanson, PurdueUniversity, WestLafayette, IN

1500AIAA-2010-1063 Infrared Measurementsof Boundary- Layertransition on an InclinedCone at Mach 6

A. van denKroonenberg, TechnicalUniversity ofBraunschweig,Braunschweig, Germany

1530AIAA-2010-1064 Simulation of BoundaryLayer Transition onElliptic Cones inHypersonic Flow

M. Bartkowicz,University of Minnesota,St Paul, MN

1600AIAA-2010-1065 Receptivity ofHypersonic BoundaryLayers over Straight andFlared Cones

P. Balakumar, NASALangley ResearchCenter, Hampton, VA

Chaired by: R. CUMMINGS, U.S. Air Force Academy, Colorado Springs, CO, and A. CARY, The Boeing Company, St Louis, MO1400 1430 1500 1530 1600 1630


Wednesday Afternoon / 06 January 2010 Session 191-FD-38 Error Estimates and Adaptive Mesh Methods Grand Ballroom 4

Wednesday Afternoon / 06 January 2010 Session 192-FD-39 Experimental and Computational Fluid Flow Problems Grand Ballroom 5

Wednesday Afternoon / 06 January 2010 Session 193-FD-40 Finite Difference and Finite Volume Methods Grand Ballroom 6


Chaired by: R. CUMMINGS, U.S. Air Force Academy, Colorado Springs, CO, and A. CARY, The Boeing Company, St Louis, MO1400AIAA-2010-1067 On 3- D Goal- OrientedAnisotropic MeshAdaptation Applied toInviscid Flows inAeronautics

A. Loseille, GeorgeMason University,Fairfax, VA

1430AIAA-2010-1068 An Adaptive Dual- MeshMethod for PremixedCombustion Using theLevel Set Approach

D. Hartmann, RWTHAachen University,Aachen, Germany

1500AIAA-2010-1069 Cell- Based ENO- MRAfor Mesh Adaptation andStructure Identification

H. Udaykumar,University of Iowa, IowaCity, IA

1530AIAA-2010-1070 Adaptive Remeshing forUnsteady RANSComputations

E. Gammacurta, ÉcolePolytechnique deMontréal , Montréal,Canada

1600AIAA-2010-1071 Error Analysis of aModified DiscontinuousGalerkin RecoveryScheme for DiffusionProblems

D. French, University ofCIncinnati, Cincinnati,OH

1630AIAA-2010-1072 An Efficient AdaptiveCartesian VorticityTransport Solver forRotorcraft FlowfieldAnalysis

R. Harris, CFDResearch Corporation,Huntsville, AL

Chaired by: S. OLCMEN, The University of Alabama, Tuscaloosa, AL, and Z. MAHMUD1400AIAA-2010-1073 Afterbody ConvectiveHeating of a MartianDescent Vehicle

I. Egorov, TsAGI,Zhukovsky, Russia

1430AIAA-2010-1075 Three DimensionalSimulations ofRichtmyer- MeshkovInstabilities in Shock-Tube Experiments

A. Gowardhan, LosAlamos NationalLaboratory, Los Alamos,NM

Chaired by: K. BERGERON, U.S. Air Force Academy, Colorado Springs, CO, and V. VATSA, NASA Langley Research Center, Hampton, VA1400AIAA-2010-1079 Comparison of Node-Centered and Cell-Centered UnstructuredFinite- VolumeDiscretizations: InviscidFluxes

B. Diskin, NationalInstitute of Aerospace,Hampton, VA

1430AIAA-2010-1080 Development of High-Order Realizable Finite-Volume Schemes forQuadrature- BasedMoment Method

V. Vikas, Iowa StateUniversity, Ames, IA

1500AIAA-2010-1081 New GradientCalculation Method forMUSCL Type CFDSchemes in ArbitraryPolyhedra

E. Shima, JapanAerospace ExplorationAgency (JAXA),Sagamihara, Japan

1530AIAA-2010-1082 Finite Volume DistanceField Solution Applied toMedial Axis Transform

H. Xia, University ofCambridge, Cambridge,Great Britain

1600AIAA-2010-1083 A Cell- Centered FiniteVolume Method forChemically ReactingFlows on Hybrid Grids

S. Spiegel, NorthCarolina StateUniversity, Raleigh, NC

1630AIAA-2010-1084 Characteristic BoundaryCondtitions forCompressible ViscousFlows on CurvilinearGrids

B. Landmann, Universityof Florida, Gainesville,FL

Chaired by: M. OL, U.S. Air Force Research Laboratory, Wright-Patterson AFB, OH


Wednesday Afternoon / 06 January 2010 Session 194-FD-41 High-Rate Unsteady Aerodynamics at Low Reynolds Number Tampa

Wednesday Afternoon / 06 January 2010 Session 195-FD-42 Joint PDL/WIG/FD/TP Plasma Actuator Session VI Miami

Wednesday Afternoon / 06 January 2010 Session 196-FD-43 Supersonic Flow Control New York


Chaired by: M. OL, U.S. Air Force Research Laboratory, Wright-Patterson AFB, OH1400

Break

,

1600AIAA-2010-1085 Résumé of the AIAA FDTC LowReynolds Number DiscussionGroup’s Canonical Cases

M. OL, Air Force Research Lab,Wright-Patterson, AFB, OH

1630AIAA-2010-1086 Unsteady Force Measurement ofSD7003 Foil Under Pitch- Up,Hold and Pitch- Down Motion atRe = 1 x 104

S. Srigrarom, NanyangTechnological University,Singapore, Singapore

Chaired by: G. FONT, U.S. Air Force Academy, Colorado Springs, CO, and S. ROY, University of Florida, Gainesville, FL1400AIAA-2010-1087 PIV Study on ForebodyVortex Cores underPlasma Actuations

J. Wang, NorthwesternPolytechnical University,Xi'an, China (prc)

1430AIAA-2010-1088 Control of Separationfrom the Flap of a High-Lift Airfoil with DBDPlasma Actuation

J. Little, Ohio StateUniversity, Columbus,OH

1500AIAA-2010-1089 Investigation of aPulsed- Plasma Jet forShock/Boundary LayercCntrol

V. Narayanaswamy,University of Texas,Austin, Austin, TX

1530AIAA-2010-1090 Separation ControlUsing DBD PlasmaActuators: ThrustEnhancement Studies

S. Guo, University ofMinnesota, Minneapolis,MN

1600AIAA-2010-1091 Effect of PlasmaActuator Excitation forControlling BypassTransition in BoundaryLayers

R. Hanson, University ofToronto, Toronto,Canada

1630AIAA-2010-1092 Physics- Based Analysisof Horseshoe PlasmaActuator for ImprovingFilm CoolingEffectiveness


Chaired by: J. SCHMISSEUR, U.S. Air Force, Arlington, VA, and I. GURSUL, University of Bath, Bath, Great Britain1400AIAA-2010-1094 PSP Measurements ofSupersonic Flow Acrossan Open Cavity withSerrations

O. Picolet, INSA, Lyon,France

1430AIAA-2010-1095 Preliminary NumericalInvestigation of a Mach3 Inlet Configuration withand without Aspirationand Micro- Ramps

D. Galbraith, Universityof Cincinnati, Cincinnati,OH

1500AIAA-2010-1096 Principles of a High-BandwidthMicroacutator ProducingSupersonic PulsedMicrojets

J. T Solomon, FloridaState University,Tallahassee, FL

1530AIAA-2010-1097 Micro- Vortex Generatorsand Recirculating FlowControl of Normal ShockStability and PositionSensitivity

T. Herges, University ofIllinois,Urbana-Champaign,Urbana, IL

1600AIAA-2010-1098 Flow Control UsingThermal Bumps inHypersonic Flow

E. Erdem, University ofManchester,Manchester, GreatBritain

Chaired by: P. TUCKER, Whittle Laboratory, Cambridge, Great Britain1400 1430 1500 1530 1600


Wednesday Afternoon / 06 January 2010 Session 197-FD-44 Turbulence Modeling and Methods Crystal Ballroom P

Wednesday Afternoon / 06 January 2010 Session 198-GPSE-5 ISS Research Results Crystal Ballroom A

Wednesday Afternoon / 06 January 2010 Session 199-GT-7 Modern Design of Experiments Crystal Ballroom G1


Chaired by: P. TUCKER, Whittle Laboratory, Cambridge, Great Britain1400AIAA-2010-1099 Multi- Wall Recycling /Rescaling Method forInflow TurbulenceGeneration

J. Boles, North CarolinaState University,Raleigh, NC

1430AIAA-2010-1101 Application of a Two-Layer Model for ImplicitLarge- Eddy SimulationsUsing a High- OrderCompact Scheme

M. Lu, Western MichiganUniversity, Kalamazoo,MI

1500AIAA-2010-1102 Analysis of a RealizableUnified RANS- LESModel

H. Gopalan, Universityof Wyoming, Laramie,WY

1530AIAA-2010-1103 Smooth- Wall BoundaryConditions forDissipation- BasedTurbulence Models

W. Phillips, Utah StateUniversity, Logan, UT

1600AIAA-2010-1104 Effects of TurbulenceModeling on RANSSimulations of TipVortices

J. Wells, VirginiaPolytechnic Institute andState University,Blacksburg, VA

Chaired by: J. ROBINSON, NASA Johnson Space Center, Houston, TX, and F. CHIARAMONTE, NASA Glenn Research Center, Cleveland, OH1400AIAA-2010-1105 Laminar Smoke Points inCoflow MeasuredAboard the InternationalSpace Station

K. Dotson, University ofMaryland, College Park,MD

1430Oral Presentation Phase Separation inMicrogravity

P. Lu, HarvardUniveristy, Cambridge,MA

1500AIAA-2010-1107 Extensional Propertiesof a Dilute PolymerSolution FollowingPreshear in Microgravity

J. Soulages,Massachusetts Instituteof Technology,Cambridge, MA

1530Oral Presentation CIR Operations Update

R. Corban, NASA GlennResearch Center,Cleveland, OH

1600Oral Presentation MCDA/FLEX

D. Dietrich, NASA GlennResearch Center,Cleveland, OH

Chaired by: D. GARRARD, Aerospace Testing Alliance, Arnold AFB, TN, and J. OSBORNE1400AIAA-2010-1111 Analysis of Variance inthe Modern Design ofExperiments


1430AIAA-2010-1112 Hypersonic Laminar-Turbulent TransitionExperiment Design:From Wind TunnelModel Definition toMDOE Approach

A. Marino, ItalianAerospace ResearchCenter (CIRA), Capua,Italy

1500AIAA-2010-1113 Design of Orion SoilImpact Study Using theModern Design ofExperiments


Chaired by: R. GAETA, Georgia Institute of Technology, Smyrna, GA, and I. HALLIWELL, Avetec, Springfield, OH


Wednesday Afternoon / 06 January 2010 Session 200-GTE-9 Gas Turbine Engines -Turbines II Crystal Ballroom B

Wednesday Afternoon / 06 January 2010 Session 201-HAPB-7 Hypersonic Vehicle Design Crystal Ballroom E

Wednesday Afternoon / 06 January 2010 Session 202-HAPB-8 Ramjet/Scramjet Performance Crystal Ballroom F


Chaired by: R. GAETA, Georgia Institute of Technology, Smyrna, GA, and I. HALLIWELL, Avetec, Springfield, OH1400AIAA-2010-1116 Unsteady Performanceof a Turbine Driven by aPulse Detonation Engine

K. Rouser, U.S. AirForce Institute ofTechnology, Dayton, OH

1430AIAA-2010-1117 Comparison of HeatTransfer Coefficient andThermal Performance ofa Narrow ImpingementChannel

M. Ricklick, University ofCentral Florida, Orlando,FL

1500AIAA-2010-1119 Active SeparationControl on HighlyLoaded LPT Bladesusing Microjets

E. Fernandez, FloridaA&M University-FloridaState University,Tallahassee, FL

1530AIAA-2010-1121 Fluid Dynamics ofImpinging Wakes andSeparation Control on aLow- Pressure TurbineProfile

K. Gompertz, The OhioState University,Columbus, OH

Chaired by: R. STARKEY, University of Colorado, Boulder, Boulder, CO, and R. SPRINGER, Johns Hopkins University Applied Physics Laboratory, Laurel, MD1400AIAA-2010-1122 Integrated Aero- Servo-Thermo- Propulso-Elasticity (ASTPE)Methodology forHypersonic ScramjetVehicle Design/Analysis

R. Starkey, University ofColorado, Boulder, CO

1430AIAA-2010-1125 Simulation of aCombined Cycle forHigh Speed Propulsion

V. Fernández-Villacé,von Karman Institute forFluid Dynamics,Rhode-St-Genèse,Belgium

Chaired by: T. O'BRIEN, Aerojet, Folsom, CA, and D. LUCIA, U.S. Air Force Scientific Advisory Board, Andrews AFB, MD1400AIAA-2010-1126 Experimental Study ofTest Medium VitiationEffects on Dual- ModeScramjet Mode Transition

R. Rockwell, Universityof Virginia,Charlottesville, VA

1430AIAA-2010-1127 Numerical Simulation ofVitiation Effects on aHydrogen- Fueled Dual-Mode Scramjet

M. Vyas, NASA GlennResearch Center,Cleveland, OH

1500AIAA-2010-1128 Numerically SimulatedComparativePerformance of aScramjet and Shcramjetat Mach 11

J. Chan, University ofToronto, Toronto,Canada

Chaired by: S. EBERHARDT, The Boeing Company, Seattle, WA, and K. BURNS, Wyle Laboratories, San Diego, CA1400 1430 1500


Wednesday Afternoon / 06 January 2010 Session 203-HIS-4 Human Space Exploration Crystal Ballroom N

Wednesday Afternoon / 06 January 2010 Session 204-IS-4 Intelligent Adaptation and Model Identification Crystal Ballroom M

Wednesday Afternoon / 06 January 2010 Session 239-MDO-2 Optimization Applications I Crystal Ballroom C


Chaired by: S. EBERHARDT, The Boeing Company, Seattle, WA, and K. BURNS, Wyle Laboratories, San Diego, CA1400AIAA-2010-1131 Denying the Apollo MoonLandings: Conspiracyand Questioning inModern American History

R. Launius, SmithsonianInstitution, Washington,DC

1430AIAA-2010-1132 Developing a SpatialHistory of Spaceflight:The Smithsonian Atlas ofSpace Exploration


1500AIAA-2010-1135 Constructing the Originsof the Solar System:Scientific Knowledgeand Public Perceptions


Chaired by: J. STECK, Wichita State University, Wichita, KS, and E. ATKINS, University of Michigan, Ann Arbor, MI1400AIAA-2010-1137 Noncertainty- EquivalentAdaptive Missile Controlvia Immersion andInvariance

K. Lee, KwandongUniversity, Kwandong ,South Korea

1430AIAA-2010-1138 Reconfigurable ControlAllocation TechnologyUsing Weighted LeastSquares for NonlinearSystem in UnmannedAerial Vehicle

Q. Zhou, ConcordiaUniversity, Montréal,Canada

1500AIAA-2010-1139 Advanced Static SoaringFlight Controls for InputConstrained Aircraft

N. Kahveci, Ford MotorCompany, Dearborn, MI

1530AIAA-2010-1140 Flow Field Data Miningof Pareto- OptimalAirfoils Using ProperOrthogonalDecomposition

A. Oyama, JapanAerospace ExplorationAgency (JAXA),Sagamihara, Japan

Chaired by: J. CHRISSIS, U.S. Air Force Institute of Technology, Wright-Patterson AFB, OH, and Y. KO, AVID LLC, Blacksburg, VA1400AIAA-2010-1316 On Structural LayoutUsing MultifidelityGeometry in AircraftConceptual Design

D. Lazzara,Massachusetts Instituteof Technology,Cambridge, MA

1430AIAA-2010-1317 Deterministic DesignOptimization of aBendable Load StiffenedUAV Wing

V. Jagdale, University ofFlorida, Gainesville, FL

1500AIAA-2010-1318 Metamodels forAerothermodynamicDesign Optimization ofHypersonic Spiked BluntBodies

M. Ahmed, University ofSheffield, Sheffield,Great Britain

1530AIAA-2010-1320 Whole MissionSimulation for AircraftPreliminary Design

P. Krus, LinköpingUniversity, Linköping,Sweden

1600AIAA-2010-1321 AdvancedMultidisciplinaryOptimizationTechniques for EfficientSubsonic Aircraft Design

S. Lehner, PurdueUniversity, W. Lafayette,IN

Chaired by: S. RADHAKRISHNAN, Jet Propulsion Laboratory, Pasadena, CA, and T. LIEUWEN, Georgia Institute of Technology, Atlanta, GA1400 1430 1500 1530 1600


Wednesday Afternoon / 06 January 2010 Session 205-PC-14 Combustion Modeling Los Angeles

Wednesday Afternoon / 06 January 2010 Session 206-PC-15 Fundamentals of Airbreathing Combustion Denver

Wednesday Afternoon / 06 January 2010 Session 207-PDL-12 Laser Applications Grand Ballroom 1


Chaired by: S. RADHAKRISHNAN, Jet Propulsion Laboratory, Pasadena, CA, and T. LIEUWEN, Georgia Institute of Technology, Atlanta, GA1400AIAA-2010-1142 Large Eddy Simulationof a Turbulent GaseousJet in OscillatingCrossflow

L. Zhang, GeorgiaInstitute of Technology,Atlanta, GA

1430AIAA-2010-1144 CFD- Simulation of theInjection andCombustion of LOX andH2 at SupercriticalPressures

M. Poschner, Universityof the Federal GermanArmed Forces, Munich,Germany

1500AIAA-2010-1145 Numerical Prediction ofInterior BallisticsPerformance ofProjectile Accelerator bySolid/Gas Two- PhaseReacting Flow Simulation

H. Miura, KeioUniversity, Yokohama,Japan

1530AIAA-2010-1146 Theoretical andNumerical Estimation ofAcoustic Damping of aModel CombustionChamber

T. Shimizu, JapanAerospace ExplorationAgency (JAXA),Kanagawa, Japan

1600AIAA-2010-1147 Numerical andExperimentalInvestigation of SyngasCombustion on a Semi-Technical Scale Burner

M. Di Domenico,German AerospaceCenter (DLR), Stuttgart,Germany

Chaired by: J. TISHKOFF, U.S. Air Force Office of Scientific Research, Arlington, VA, and K. MCMANUS, General Electric Company, Niskayuna, NY1400AIAA-2010-1148 Unsteady Aspects ofLean Premixed-Prevaporized (LPP) GasTurbine Combustors:Flame- FlameInteractions

S. Dhanuka, Universityof Michigan, Ann Arbor,MI

1430AIAA-2010-1149 Sub- to- Supercritical JetMixing and Core LengthAnalysis

A. Roy, University ofFlorida, Gainesville, FL

1500AIAA-2010-1150 Convective and FilmCooled NozzleExtension for a HighPressure RocketSubscale CombustionChamber


1530AIAA-2010-1151 Response of an AnnularBurner Nozzle toTransverse AcousticExcitation

J. O'Connor, GeorgiaInstitute of Technology,Atlanta, GA

1600AIAA-2010-1152 Extraction ofCombustion InstabilityMechanisms fromDetailed ComputationalSimulations

R. Smith, PurdueUniversity, WestLafayette, IN

1630AIAA-2010-1153 Non- Normality andInternal Flame Dynamicsin Premixed Flame-Acoustic Interaction

P. Subramanian, IndianInstitute of Technology,Madras, Chennai, India

Chaired by: T. MADDEN, U.S. Air Force Research Laboratory, Kirtland AFB, NM, and W. BEHRENS, Northrop Grumman Corporation, Rancho Palos Verdes, CA1400AIAA-2010-1154 Laser InducedAvalanche Ionization inGases or Gas Mixtureswith REMPI orFemtosecond LaserPulse Pre- Ionization

M. Shneider, PrincetonUniversity, Princeton, NJ

1430AIAA-2010-1155 Effect of Flow Coolingon Gain and OutputPower of an ElectricallyExcited Oxygen- IodineLaser

J. Bruzzese, Ohio StateUniversity, Columbus,OH

1500AIAA-2010-1156 Experimental andComputationalInvestigation of aConverging- DivergingNozzle- Diffuser withCross Flow Injection

C. Noren, U.S. Air ForceResearch Laboratory,Kirtland AFB, NM

1530AIAA-2010-1157 WITHDRAWN Progress inDevelopment of aCapabilities- BasedNear- Term HEL AreaDefense Weapon

Z. George, RaytheonCorporation, Tucson, AZ

1600AIAA-2010-1158 Optical Measurementsof a CompressibleShear Layer Using aLaser- Induced AirBreakdown Beacon

M. Rennie, University ofNotre Dame, NotreDame, IN


Wednesday Afternoon / 06 January 2010 Session 208-SEC-4 Challenges to Exploration of the Moon and Mars Crystal Ballroom D

Wednesday Afternoon / 06 January 2010 Session 209-SRU-2 Solar Thermal Lunar Resource Extraction and Processing Atlanta

Wednesday Afternoon / 06 January 2010 Session 210-TES-3 Combustion II Boston


Chaired by: N. RAMACHANDRAN, Jacobs Technology, Huntsville, AL, and M. BENTON, The Boeing Company, Huntington Beach, CA1400AIAA-2010-1160 Fatalities on PastAntarctic ExplorationExpeditions as MannedSpaceflight HazardIdentification Guides

P. Wallace, RocinanteAerospace, Simi Valley,CA

1430AIAA-2010-1161 On Rocket Plume, LunarCrater and Lunar DustInteractions

D. Liu, ZONATechnology, Inc.,Scottsdale, AZ

Chaired by: K. SACKSTEDER, NASA Glenn Research Center, Cleveland, OH, and G. SANDERS, NASA Johnson Space Center, Houston, TX1400AIAA-2010-1162 Solar Power System forLunar ISRU Applications

T. Nakamura, PhysicalSciences, Inc., Pleasanton,CA

1430AIAA-2010-1163 Demonstrating the SolarCarbothermal Reduction ofLunar Regolith to ProduceOxygen

R. Gustafson, ORBITEC,Madison, WI

1500AIAA-2010-1164 Pressure Controlled HeatPipe Solar Receiver forOxygen Production fromLunar Regolith

J. Hartenstine, AdvancedCooling Technologies,Lancaster, PA

1530AIAA-2010-1166 Solar Energy Systems forLunar Oxygen Generation

A. Colozza, AnalexCorporation, Cleveland, OH

1600AIAA-2010-1167 Solar Concentrator Conceptfor Providing Direct SolarEnergy for OxygenProduction at the LunarSouth Pole

A. Colozza, AnalexCorporation, Cleveland, OH

Chaired by: H. CHAMBERS, HFC Consulting, Westervile, OH, and P. ROHATGI, University of Wisconsin, Milwaukee, Milwaukee, WI1400AIAA-2010-1168 Studies of LargeCoherent Structures andTheir Effects on SwirlCombvustion

N. Syred, CardiffUniversity, Cardiff, GreatBritain

1430AIAA-2010-1169 Premixed SwirlCombustion andFlashback Analysis withHydrogen/MethaneMixtures

A. Bagdanavicius,Cardiff University,Cardiff, Great Britain

1500AIAA-2010-1170 Assessment ofTurbulence- ChemistryInteraction Models in theNational CombustionCode (NCC) - Part I

T. Wey, NASA GlennResearch Center,Cleveland, OH

1530AIAA-2010-1171 Combined Combustionand System Modeling ofSemi- Closed CyclePoWER Engine

B. Singh, University ofFlorida, Gainesville, FL

1600AIAA-2010-1172 Investigation ofFlashback Propensity inTurbines with SyngasFuels

A. Choudhuri, Universityof Texas, El Paso, ElPaso, TX

Chaired by: J. DEC, NASA Langley Research Center, Hampton, VA, and X. ZHONG, University of California, Los Angeles, Los Angeles, CA1400 1430 1500 1530 1600


Wednesday Afternoon / 06 January 2010 Session 211-TP-14 Ablation II New Orleans

Wednesday Afternoon / 06 January 2010 Session 212-TP-15 Aerothermodynamics III Grand Ballroom 13

Wednesday Afternoon / 06 January 2010 Session 213-TP-16 Heat Transfer II Grand Ballroom 14


Chaired by: J. DEC, NASA Langley Research Center, Hampton, VA, and X. ZHONG, University of California, Los Angeles, Los Angeles, CA1400AIAA-2010-1174 Prediction Accuracy ofThermal Response ofAblator Under ArcjetFlow Conditions

T. Suzuki, JapanAerospace ExplorationAgency (JAXA), Tokyo,Japan

1430AIAA-2010-1175 Chemistry Model forAblating Carbon-Phenolic Material DuringAtmospheric Re- Entry

A. Martin, University ofMichigan, Ann Arbor, MI

1500AIAA-2010-1176 Steady- State AblationModel Coupling withHypersonic Flow

R. Upadhyay, Universityof Texas, Austin, Austin,TX

1530AIAA-2010-1177 Understanding HighRecession Rates ofCarbon Ablators Seen inShear Tests in an ArcJet

D. Driver, NASA AmesResearch Center,Moffett Field, CA

1600AIAA-2010-1596 Shock- Tube Study ofSurface Reaction ofAtomic Hydrogen onSolid Carbon

S. Hyun, KAIST,Daejeon, South Korea

Chaired by: D. KUNTZ, Sandia National Laboratories, Albuquerque, NM, and M. WRIGHT, NASA Ames Research Center, Moffett Field, CA1400AIAA-2010-1179 Implicit SurfaceBoundary Conditions forBlowing, EquilibriumComposition, andDiffusion- LimitedOxidation

M. MacLean, CUBRC,Buffalo, NY

1430AIAA-2010-1180 Flowfield UncertaintyAnalysis for HypersonicCFD Simulations

A. Alexeenko, PurdueUniversity, WestLafayette, IN

1500AIAA-2010-1181 Aeroheatingmeasurements on areentry capsule model infree- piston shock tunnelHIEST

H. Tanno, JapanAerospace ExplorationAgency (JAXA),Kakuda, Japan

1530AIAA-2010-1183 The Influence ofStabilization Parametersin the SUPG FiniteElement Method forHypersonic Flows

B. Kirk, NASA JohnsonSpace Center, Houston,TX

1600AIAA-2010-1182 Stream FunctionCalculation on GeneralSurface MeshTopologies and GeneralGeometries

R. Bond, SandiaNational Laboratories,Albuquerque, NM

Chaired by: E. MAROTTA, Texas A&M University, College Station, TX, and E. SILK, NASA Goddard Space Flight Center, Greenbelt, MD1400AIAA-2010-1184 Towards Prediction ofTranspiration Cooling

A. Steingrimsson,Embry-RiddleAeronautical University,Daytona Beach, FL

1430AIAA-2010-1185 Influence of InteractionsBetween Turbulenceand Radiation onTransmissivities inHypersonic TurbulentBoundary Layers

A. Feldick, PennsylvaniaState University,University Park, PA

1500AIAA-2010-1186 WITHDRAWN Experimentation onDigitized Heat Transferfor Two- Phase Laminarflow in a Horizontal Tube

S. Shajiee, University ofColorado, Boulder,Boulder, CO

1530AIAA-2010-1187 Effect of Free SurfaceHeat Transfer onOscillatoryThermocapillary Flow inDifferentially HeatedCylindrical Annulus

S. Jafri, Air University,Islamabad, Pakistan

Chaired by: D. LAIRD and M. RUMSEY, Sandia National Laboratories, Albuquerque, NM


Wednesday Afternoon / 06 January 2010 Session 214-WE-6 Wind Turbine Structures, Materials, and Sensors Crystal Ballroom G2

Wednesday Afternoon / 06 January 2010 Session 215-WIG-7 / PDL-13 Characterization and Simulation of Plasmas Grand Ballroom 2

Wednesday Afternoon / 06 January 2010 1730 - 1830 2010 von Kármán Lectureship In Astronautics Crystal Ballroom H


Chaired by: D. LAIRD and M. RUMSEY, Sandia National Laboratories, Albuquerque, NM1400AIAA-2010-1188 Analysis of anEmbedded Blade RootCarrot Subject to ColdWeather Using a FiniteElement Model

P. Lillo, University ofVictoria, Victoria, Canada

1430AIAA-2010-1189 Strength and Fatigue ofWind Turbine RotorLaminates andSubcomponents

R. Nijssen, KnowledgeCentre Wind TurbineMaterials andConstructions (WMC),Wieringerwerf, TheNetherlands

1500AIAA-2010-1190 Small Wind TurbinePerformance EvaluationUsing Tower- andNacelle- MountedAnemometers

B. Ziter, University ofGuelph, Guelph, Canada

1530AIAA-2010-1192 Updating of a WindTurbine Model for theEvaluation of Methodsfor OperationalMonitoring Using InertialMeasurements

J. White, PurdueUniversity, Lafayette, IN

Chaired by: I. BLANKSON, NASA Glenn Research Center, Cleveland, OH, and A. EROFEEV, Russian Academy of Sciences, Saint Petersburg, Russia1400AIAA-2010-1193 Experimental Study ofSurface- VolumetricDischarge Transition atVarious Polarization andAngle of Falling ofMicrowave Radiation

K. Alexandrov, RussianAcademy of Sciences,Moscow, Russia

1430AIAA-2010-1194 Monte Carlo Simulationof NonequilibriumConductivity Producedby Electron Beam inMHD Flows

E. Sheikin,Saint-Petersburg StateUniversity, SaintPetersburg, Russia

1500AIAA-2010-1195 Role of Charged ParticleInertia in PulsedElectrical Discharges

J. Poggie, U.S. Air ForceResearch Laboratory,Wright-Patterson AFB,OH

1530AIAA-2010-1196 Evalution ofGasdynamic andElectrodynamicProperties ofNonequilibrium Plasmaof Shockwave

A. Kuranov,Saint-Petersburg StateUniversity, SaintPetersburg, Russia

1600AIAA-2010-1197 A System of DeeplySubcritical MicrowaveDischarges in aSupersonic Air Stream


Eileen M. CollinsColonel USAF Retired and Former Astronaut

Chaired by: W. SARIC, Texas A&M University, College Station, TXPanel Discussion


Wednesday Afternoon / 06 January 2010 Session 161-FD-341830 - 2200 Transition Study Group Open Forum New York

Thursday Morning / 07 January 2010 0800 - 0900 New Horizons Forum Keynote Address Crystal Ballroom H

Thursday Morning / 07 January 2010

0900 - 1130 New Horizons Forum Panel Discussion - Unmanned Air Systems: The NextGenerations Crystal Ballroom J2


Chaired by: W. SARIC, Texas A&M University, College Station, TXPanel Discussion

Distinguished Speaker: Lt General David A. DeptulaDeputy Chief of Staff, Intelligence, Surveillance and Reconnaissance

Intelligence, Surveillance and Reconnaissance Transformation

The panel will discuss issues and opportunities that are shaping these systems including emerging military roles & missions, new technologies and their implications, the importance of autonomy, culturalacceptance, the emerging civil and commercial markets, and the role of optionally piloted vehicles in shaping future UAS.

Moderator:Brian Argrow, Associate Dean for Education, Alfred and Betty Look Professor of Engineering, Director, Research and Engineering Center for Unmanned Vehicles (RECUV), Department of AerospaceEngineering Sciences, University of Colorado, Boulder, CO

Panelists:

John R. Stanton, Executive Director, National Air Security Operations for the Office of Air and Marine, U.S. Customs and Border Protection, Washington D.C.

Scott Winship, Vice President and Program Manager for Northrop Grumman Integrated Systems Sector's U.S. Navy Unmanned Combat Air System (N-UCAS), San Diego, CA

Ron Perkins, Director, Advanced Unmanned Air Systems, the Boeing Company, Kent, WA

Colonel Eric Mathewson, Director, U.S. Air Force Unmanned Aircraft Systems Task Force, Headquarters U.S. Air Force, Pentagon, Washington DC.

Capt. Robert Dishman, Program Manager, Naval Air Systems Command's Persistent Maritime Unmanned Aircraft Systems Program Office (PMA-262), Patuxent River, Md.

Chaired by: G. RAMAN, Illinois Institute of Technology, Glenview, IL0900 0930 1000 1030


Thursday Morning / 07 January 2010 Session 216-AA-9 Cavity and Duct Acoustics Washington

Thursday Morning / 07 January 2010 Session 217-AD-8 Aerospace Design Education Crystal Ballroom L

Thursday Morning / 07 January 2010 Session 218-AFM-7 Planetary Entry Chicago


Chaired by: G. RAMAN, Illinois Institute of Technology, Glenview, IL0900AIAA-2010-1198 Control of ResonantFlow Inside aSupersonic Cavity UsingHigh Bandwidth Micro-Actuators

M. Ali, Florida A&MUniversity - Florida StateUniversity, Tallahassee,FL

0930AIAA-2010-1200 Cavity Flow AssessmentUsing AdvancedTurbulence Modeling

N. Liggett, GeorgiaInstitute of Technology,Atlanta, GA

1000AIAA-2010-1202 Coupled RANS/LES forSOFIA Cavity AcousticPrediction

S. Woodruff, NASADryden Flight ResearchCenter, Edwards, CA

1030AIAA-2010-1203 WITHDRAWN On Resonances in aThree- DimensionalOpen Cavity

P. Cobo, Institute ofAcoustics (CSIC),Madrid, Spain

Chaired by: W. CROSSLEY, Purdue University, West Lafayette, IN, and D. KRAUSCHE, Florida Center for Engineering Education, Gainesville, FL0900AIAA-2010-1204 AeroMorph as aMorphing Design Tool inan EducationalEnvironment

C. Lafountain, Universityof Cincinnati, Cincinnati,OH

0930AIAA-2010-1205 Designing a GreenAircraft; Cal Poly's 2009Undergraduate AircraftDesigns

R. McDonald, CaliforniaPolytechnic StateUniversity, San LuisObispo, CA

1000AIAA-2010-1206 Design and FlightTesting of an ECO-Sport Aircraft

C. Jouannet, LinköpingUniversity, Linköping,Sweden

1030AIAA-2010-1208 CCSU MoonbuggyVehicle Design, Buildingand Competition

V. Naoumov, CentralConnecticut StateUniversity, New Britain,CT

1100AIAA-2010-1209 Numerical Simulation ofan Adaptive AirfoilSystem using SMAActuators

E. Abdullah, RMITUniversity, Bundoora,Australia

Chaired by: B. PAMADI and D. OWENS, NASA Langley Research Center, Hampton, VA0900AIAA-2010-1210 Mars Entry, Descent,and Landing Trajectoryand AtmosphereReconstruction

S. Dutta, GeorgiaInstitute of Technology,Atlanta, GA

0930AIAA-2010-1212 Analytic HypersonicAerodynamics forConceptual Design ofEntry Vehicles

M. Grant, GeorgiaInstitute of Technology,Atlanta, GA

Chaired by: S. GOGINENI, Spectral Energies, LLC, Dayton, OH, and H. HU, Iowa State University, Ames, IA0900 0930 1000 1030 1100


Thursday Morning / 07 January 2010 Session 219-AMT-8 Measurement Technology Applications Crystal Ballroom J1

Thursday Morning / 07 January 2010 Session 220-APA-21 Active Flow Control III Grand Ballroom 9

Thursday Morning / 07 January 2010 Session 221-APA-22 Aerodynamic Design Methodologies Grand Ballroom 10


Chaired by: S. GOGINENI, Spectral Energies, LLC, Dayton, OH, and H. HU, Iowa State University, Ames, IA0900AIAA-2010-1214 Influence ofUnsteadiness on ThrustMeasurements of PulseDetonation Engines

F. Lu, University ofTexas, Arlington,Arlington, TX

0930AIAA-2010-1215 Measurement andAnalysis of UnsteadyFlows in IC Engines

S. Olcmen, University ofAlabama, Tuscaloosa,AL

1000AIAA-2010-1216 PhotogrammetricMeasurement ofRecession Rates of LowTemperature Ablators inSupersonic Flow

D. Callaway, U.S. AirForce Institute ofTechnology,Wright-Patterson AFB,OH

1030AIAA-2010-1217 Optimization ofStochastic EstimationTechniques in a High-Speed, Axisymetric Jet

J. Kastner, University ofCincinnati, Cincinnati,OH

1100AIAA-2010-1218 Quantitative FlowVisualization of CorrectlyExpanded SupersonicJets by RainbowSchlieren Deflectometry

Y. Miyazato, Universityof Kitakyushu,Kitakyushu, Japan

Chaired by: J. LITTLE, Ohio State University, Columbus, OH, and J. GEORGE, Innovative Aerospace Solutions, Downey, CA0900AIAA-2010-1219 Experimental Studies ofPlasma ActuatorPerformance forSeparation Control

D. Poon, University ofMinnesota, Minneapolis,MN

0930AIAA-2010-1220 Separation ControlUsing Plasma Actuators:2- D and Edge Effects inSteady Flow in LowPressure Turbines

D. Burman, University ofMinnesota, Minneapolis,MN

1000AIAA-2010-1221 Plasma ActuatorSimulation: ForceContours and DielectricCharging Characteristics

M. Mamunuru,University of Minnesota,Minneapolis, MN

1030AIAA-2010-1222 Plasma Flow Control onLow Aspect Ratio Wingsat Low ReynoldsNumbers

S. Vey, Berlin Institute ofTechnology, Berlin,Germany

1100AIAA-2010-1223 Plasma Actuator withMultiple EncapsulatedElectrodes to Influencethe Induced Velocoty

C. Hale, University ofManchester,Manchester, GreatBritain

Chaired by: S. NADARAJAH, McGill University, Montréal, Canada, and A. FARINA, U.S. Army Research, Development and Engineering Command, Picatinny Arsenal, NJ0900AIAA-2010-1225 A New CokrigingMethod for Variable-Fidelity SurrogateModeling ofAerodynamic Data

Z. Han, GermanAerospace Center(DLR), Braunschweig,Germany

0930AIAA-2010-1226 An InteractivePreliminary DesignSystem of High SpeedForebody and Inlet Flows

M. Liou, NASA GlennResearch Center,Cleveland, OH

1000AIAA-2010-1227 Lift Superposition andAerodynamic TwistOptimization forAchieving Desired LiftDistributions

K. Lane, CaliforniaPolytechnic StateUniversity, San LuisObispo, CA

1030AIAA-2010-1228 Inverse Airfoil DesignUtilizing CSTParameterization

K. Lane, CaliforniaPolytechnic StateUniversity , San LuisObispo, CA

1100AIAA-2010-1229 A Coupled Kinematicsand Energetics Modelfor Flapping Flight

H. Salehipour, Universityof Massachusetts,Lowell , Lowell, MA


Thursday Morning / 07 January 2010 Session 222-APA-23 Create-AV: Testing and Evaluation of High Performance Computing Software II Grand Ballroom 11

Thursday Morning / 07 January 2010 Session 223-APA-24 Icing or Roughness Effects on Vehicle Aerodynamics Grand Ballroom 12

Thursday Morning / 07 January 2010 Session 224-APA-25 Innovative Aerodynamic Concepts and Designs Grand Ballroom 13


Chaired by: J. LAIOSA, Naval Air Warfare Center, Patuxent River, MD0900AIAA-2010-1230 Application of the HeliosComputational Platformto Rotorcraft Flowfields

J. Sitaraman, NationalInstitute of Aerospace,Hampton, VA

0930AIAA-2010-1231 Determining theApplicability andEffectiveness of CurrentCFD Methods in StoreCertification Activities

J. Dean, U.S. Air ForceSEEK EAGLE Office,Eglin AFB, FL

1000AIAA-2010-1232 CREATE- AV DaVinci:Computationally- BasedEngineering forConceptual Design

G. Roth, AeronauticalSystems Center,Wright-Patterson AFB,OH

1030AIAA-2010-1233 Rigid, Maneuvering, andAeroelastic Results forKestrel - A CREATESimulation Tool

S. Morton, DoDHPCMP/CREATEKestrel Team, EglinAFB, FL

1100AIAA-2010-1234 A Dual- MeshSimulation Strategy forImproved AV- 8B Aft-Fuselage Buffet LoadPrediction

N. Hariharan,CREATE-AV, PatuxentRiver, MD

Chaired by: M. CHANG, Lockheed Martin Corporation, Santa Clarita, CA, and R. KREEGER, NASA Glenn Research Center, Cleveland, OH0900AIAA-2010-1236 Eulerian Method for IceAccretion on Multiple-Element Airfoil Sections

J. Hospers, University ofTwente, Enschede, TheNetherlands

0930AIAA-2010-1237 Ice Accretion Effect onthe AerodynamicCharacteristics of KC-100 Aircraft

S. Jung, GyeongsangNational University,Jinju, South Korea

1000AIAA-2010-1238 Design optimization ofhot- air anti- icingsystems by FENSAP-ICE

M. Pellissier, McGillUniversity, Montréal,Canada

Chaired by: R. VERMELAND, Lockheed Martin Corporation, Lancaster, CA0900AIAA-2010-1239 Parametric Study ofPeripheral Nozzle Configurations for SupersonicRetropropulsion

N. Bakhtian, StanfordUniversity, Palo Alto, CA

0930AIAA-2010-1240 AerodynamicPerformance ofExtended FormationFlight

A. Ning, StanfordUniversity, Stanford, CA

Chaired by: A. FEDOROV, Moscow Institute of Physics and Technology, Zhukovsky, Russia, and X. WANG, University of California, Los Angeles, Los Angeles, CA0900 0930 1000 1030


Thursday Morning / 07 January 2010 Session 225-FD-45 Boundary Layer Transition: Stabilization Grand Ballroom 3

Thursday Morning / 07 January 2010 Session 226-FD-46 Contributions to RTO AVT-136 New Orleans

Thursday Morning / 07 January 2010 Session 227-FD-47 Environmental and Fundamental Turbulence Grand Ballroom 4


Chaired by: A. FEDOROV, Moscow Institute of Physics and Technology, Zhukovsky, Russia, and X. WANG, University of California, Los Angeles, Los Angeles, CA0900AIAA-2010-1242 Temporal Stability ofHypersonic BoundaryLayer on Porous Wall:Comparison of Theorywith DNS

A. Fedorov, MoscowInstitute of Physics andTechnology, Zhukovsky,Russia

0930AIAA-2010-1243 Effect of Porous Coatingon Boundary- LayerInstability

X. Wang, University ofCalifornia, Los Angeles,Los Angeles, CA

1000AIAA-2010-1244 Carbon Dioxide Injectionfor HypervelocityBoundary Layer Stability

R. Wagnild, University ofMinnesota, Minneapolis,MN

1030AIAA-2010-1245 Direct NumericalSimulation of supersonicBoundary LayerStabilization UsingGrooved Wavy Surface

A. Novikov, TsAGI,Zhukovsky, Russia

Chaired by: J. SCHMISSEUR, U.S. Air Force, Arlington, VA0900AIAA-2010-1246 A Review of TransitionStudies on Full- ScaleFlight Vehicles atDuplicated FlightConditions in the LENSTunnels andComparisons withPrediction Methods andFlight Measurement

T. Wadhams, CUBRC,Buffalo, NY

0930AIAA-2010-1247 Modeling Approachesfor Gas- SurfaceInteractions

G. Herdrich, Universityof Stuttgart, Stuttgart,Germany

1000AIAA-2010-1248 Catalysis PhenomenaDetermination inPlasmatron Facility forFlight ExperimentDesign (Invited)

O. Chazot, von KármánInstitute for FluidDynamics,Rhode-Saint-Genèse,Belgium

1030AIAA-2010-1249 Realization of a Gas-Surface Interaction TestCase for Model Validation

D. Fletcher, University ofVermont, Burlington, VT

1100AIAA-2010-1250 CFD Analysis ofCUBRC Base FlowExperiments

M. Barnhardt, Universityof Minnesota,Minneapolis, MN

1130AIAA-2010-1251 ExperimentalInvestigation of theSupersonic Wake of aReentry Capsule

F. Schrijer, DelftUniversity ofTechnology, Delft, TheNetherlands

Chaired by: M. PLESNIAK, George Washington University, Washington, DC, and K. MOHSENI, University of Colorado, Boulder, Boulder, CO0900AIAA-2010-1252 Effect of Isotropic Free-Stream Turbulence onthe Anisotropy ofFavorable PressureGradient TurbulentBoundary Layers

S. Torres-Nieves,Rensselaer PolytechnicInstitute, Troy, NY

0930AIAA-2010-1253 Comparison Of HighResolution Large- EddySimulations AndSynthetic TurbulentWind Fields

T. Auerswald, TechnicalUniversity ofBraunschweig,Braunschweig, Germany

1000AIAA-2010-1254 Direct NumericalSimulation of theTurbulent Ekman Layer:Turbulent EnergyBudgets

S. Marlatt, UnitedLaunch Alliance, Denver,CO

1030AIAA-2010-1255 Instantaneous TurbulentFlow Structures of theNumerically- SimulatedEkman Layer

S. Marlatt, UnitedLaunch Alliance,Littleton, CO

1100AIAA-2010-1257 A Numerical Study ofSpiral Turbulence

S. Dong, PurdueUniversity, WestLafayette, IN


Thursday Morning / 07 January 2010 Session 228-FD-48 Flow Control Actuators Grand Ballroom 5

Thursday Morning / 07 January 2010 Session 229-FD-49 Fluid Dynamics of Non-Aerospace Applications Crystal Ballroom K

Thursday Morning / 07 January 2010 Session 230-FD-50 New Developments in CFD Algorithms Crystal Ballroom M


Chaired by: J. GREGORY, Ohio State University, Columbus, OH0900AIAA-2010-1258 Effect of Inlet FlowConfiguration onCombustion PoweredActuators

A. Rajendar, GeorgiaInstitute of Technology,Atlanta, GA

0930AIAA-2010-1259 Miniature Shock TubeActuators for FlowControl Applications

R. Ramachandran,Illinois Institute ofTechnology , Chicago, IL

1000AIAA-2010-1260 Microjet Based ActiveFlow Control on a FixedWing UAV

P. Kreth, Florida A&MUniversity-Florida StateUniversity, Tallahassee,FL

1030AIAA-2010-1261 TurbulenceCharacteristics ofAxisymmetric and Non-Circular Synthetic Jets

L. Oren, University ofCincinnati, Cincinnati,OH

Chaired by: T. RAMSAY, Honda R&D Americas, Inc., Raymond, OH, and J. GREGORY, Ohio State University, Columbus, OH0900Oral Presentation CFD Use in theAutomotive Industry

T. Ramsay, Honda R&DAmericas, Inc.,Raymond, OH

0930AIAA-2010-1264 Fluid StructureInteraction Analysis inHuman Upper Airways toUnderstand Sleep Apnea

G. Mylavarapu,University of Cincinnati,Cincinnati, OH

1000AIAA-2010-1265 WITHDRAWN Numerical Simulationsof Blood Flow in Arteries

Y. Suzen, North DakotaState University, Fargo,ND

Chaired by: G. MAY, RWTH Aachen University, Aachen, Germany, and M. LIOU, NASA Glenn Research Center, Cleveland, OH0900AIAA-2010-1266 A DirectionalRenumbering Strategyfor ImprovingUnstructured Grid DataStructure

N. Fouladi, SharifUniversity ofTechnology, Tehran, Iran

0930AIAA-2010-1267 An Adaptive NonlinearFrequency DomainMethod for ViscousPeriodic Steady StateFlows

A. Mosahebi, McGillUniversity, Montréal,Canada

1000AIAA-2010-1268 Efficient HessianCalculations usingAutomatic Differentiationand the Adjoint Method

M. Rumpfkeil, Universityof Wyoming, Laramie,WY

1030AIAA-2010-1269 An Edge- AveragedSemi- MeshlessFramework forNumerical Solution ofConservation Laws

E. Chiu, StanfordUniversity, Stanford, CA

Chaired by: P. ORKWIS, University of Cincinnati, Loveland, OH, and J. SHANG, Wright State University, Dayton, OH0900 0930 1000 1030


Thursday Morning / 07 January 2010 Session 231-FD-51 New Developments in Flux Formulas and Equations Crystal Ballroom N

Thursday Morning / 07 January 2010 Session 232-FD-52 Reduced Order Models and Physical Modeling and Analysis Grand Ballroom 6

Thursday Morning / 07 January 2010 Session 233-FD-53 Shock Interaction Studies Under RTO AVT-136 Crystal Ballroom P


Chaired by: P. ORKWIS, University of Cincinnati, Loveland, OH, and J. SHANG, Wright State University, Dayton, OH0900AIAA-2010-1271 Updates to Multi-Dimensional FluxReconstruction forHypersonic Simulationson Tetrahedral Grids

P. Gnoffo, NASALangley ResearchCenter, Hampton, VA

0930AIAA-2010-1272 Performance of Low-Dissipation Euler Fluxesand PreconditionedImplicit Schemes in LowSpeeds

K. Kitamura, JapanAerospace ExplorationAgency (JAXA),Sagamihara, Japan

1000AIAA-2010-1273 Three- DimensionalCarbuncles and EulerFluxes

K. Kitamura, JapanAerospace ExplorationAgency (JAXA),Sagamihara, Japan

1030AIAA-2010-1274 Derivation andNumerical Simulation ofRegularized(Observable) EulerEquations

K. Mohseni, University ofColorado, Boulder,Boulder, CO

Chaired by: P. MORGAN, U.S. Air Force Research Laboratory, Wright-Patterson Air Force Base, OH, and C. VENKATASUBBAN0900AIAA-2010-1275 A Reduced- OrderModel for UnsteadyFlow over CircularCylinder

M. Ghommem, VirginiaPolytechnic Institute andState University,Blacksburg, VA

0930AIAA-2010-1276 Closure for ImprovedReduced- Order Modelsusing High PerformanceComputing

I. Akhtar, Virginia Tech,Blackburg, VA

1000AIAA-2010-1277 Assessment of theEffects of ComputationalParameters on Physics-based Models of IceAccretion

M. Nucci, GeorgiaInstitute of Technology,Atlanta, GA

1030AIAA-2010-1278 Estimating TurbulentWall Shear andBoundary LayerThickness for Hydro-dynamically RoughSurfaces by PerturbingKnown Smooth Results

L. DeChant, SandiaNational Laboratories,Albuquerque, NM

1100AIAA-2010-1279 Modeling of SnowFriction of an Aircraft Ski

L. Suhani, Embry-RiddleAeronautical University,Daytona Beach , FL

Chaired by: D. KNIGHT, Rutgers University, Piscataway, NJ, and B. REIMANN, German Aerospace Center (DLR), Lilienthalplatz, Germany0900AIAA-2010-1281 A Review ofExperimental Studieswith the Double Coneand HollowCylinder/FlareConfigurations in theLENS HypervelocityTunnels andComparisons withNavier- Stokes andDSMC Computations

M. Holden , CUBRC,Buffalo, NY

0930AIAA-2010-1282 Numerical Investigationof Double- Cone andCylinder Experiments inHigh Enthalpy FlowsUsing the DLR TAUCode

B. Reimann, GermanAerospace Center(DLR), Braunschweig,Germany

1000AIAA-2010-1283 Numerical Investigationof Double- Cone FlowExperiments with High-Enthalpy Effects

I. Nompelis, Universityof Minnesota,Minneapolis, MN

1030AIAA-2010-1284 An Assessment of CFDfor Prediction of 2- Dand 3- D High- SpeedFlows

D. Gaitonde, U.S. AirForce ResearchLaboratory,Wright-Patterson AFB,OH

1100AIAA-2010-1285 Chemically ReactingFlows Around a DoubleCone, Including AblationEffects (Invited)

D. Drikakis, CranfieldUniversity, Cranfield,Great Britain


Thursday Morning / 07 January 2010 Session 234-FD-54 Turbulent Jets and Mixing Layers Crystal Ballroom Q

Thursday Morning / 07 January 2010 Session 235-GPSE-6 Physics and Material Science I Crystal Ballroom D

Thursday Morning / 07 January 2010 Session 236-GT-8 High Reynolds Number Aerodynamics and Testing Crystal Ballroom G1


Chaired by: A. FERRANTE, University of Washington, Seattle, WA0900AIAA-2010-1287 LES of an Inclined Jetinto a SupersonicTurbulent Crossflow:Synthetic InflowConditions

A. Ferrante, Universityof Washington, Seattle,WA

0930AIAA-2010-1288 Large Eddy Simulationof Pulsed Jets in HighSpeed TurbulentCrossflow

R. Pasumarti, GeorgiaInstitute of Technology,Atlanta, GA

1000AIAA-2010-1289 Investigation of Non-Swirling and SwirlingTurbulent Jet Flowsusing Unified LES-RANS Models

H. Gopalan, Universityof Wyoming, Laramie,WY

1030AIAA-2010-1290 Investigation of LargeScale Flow Structures inan Offset Attaching JetUsing Spectral LinearStochastic Estimation

N. Gao, DalianUniversity ofTechnology, Dalian,China (prc)

1100AIAA-2010-1291 Investigation ofCoherent Structures inTurbulent Mixing LayersUsing Large EddySimulation

A. McMullan,LoughboroughUniversity,Loughborough, GreatBritain

1130AIAA-2010-1292 POD based spectralHigher- Order StochasticEstimation

W. Baars, University ofTexas at Austin, Austin,TX

Chaired by: H. NAHRA, NASA Glenn Research Center, Cleveland, OH, and J. MARCHETTA, University of Memphis, Memphis, TN0900AIAA-2010-1294 A Study of FluidInterface Configurationsin Exploration VehiclePropellant Tanks

G. Zimmerli, NASAGlenn Research Center,Cleveland, OH

0930AIAA-2010-1295 3- D Multiscale AdaptiveEulerian- LagrangianMethod for MultiphaseFlows with PhaseChange

J. Sim, University ofMichigan, Ann Arbor, MI

1000Oral Presentation Liquid AcquisitionStrategies forExploration Missions

D. Chato, NASA GlennResearch Center,Cleveland, OH

1030AIAA-2010-1297 Simulating Self-Pressurization inPropellant Tanks

A. Winter, University ofMemphis, Memphis, TN

1100AIAA-2010-1298 Heat Entrapment EffectsWithin Liquid AcquisitionDevices

W. Duval, NASA GlennResearch Center,Cleveland, OH

Chaired by: R. WAHLS, NASA Langley Research Center, Hampton, VA, and J. QUEST, European Transonic Windtunnel, Cologne, Germany0900Oral Presentation Providing AdequatePrerequisites forLaminar Testing at HighReynolds Number in theETW

D. Schimanski,European TransonicWindtunnel, Cologne,Germany

0930AIAA-2010-1300 Transonic HighReynolds NumberTransition Experimentsin the ETW CryogenicWind Tunnel

J. Perraud, ONERA,Toulouse, France

1000AIAA-2010-1301 Advanced MeasurementTechniques for HighReynolds NumberTesting in CryogenicWind Tunnels

U. Fey, GermanAerospace Center(DLR), Göttingen,Germany

1030Oral Presentation Natural Laminar FlowTesting in High UnitReynolds NumberFacilities

A. Garzon, , ,

1100AIAA-2010-1302 Assessment of theNational TransonicFacility for NaturalLaminar Flow Testing

J. Crouch, The BoeingCompany, Renton, WA

1130Oral Presentation Recent Progress at theU.S. National TransonicFacility

W. Kilgore, NASALangley ResearchCenter, Hampton, VA

Chaired by: D. SMITH, Aerospace Testing Alliance, Arnold AFB, TN, and D. SCHIMANSKI, European Transonic Windtunnel, Cologne, Germany


Thursday Morning / 07 January 2010 Session 237-GT-9 Instrumentation and Controls Grand Ballroom 14

Thursday Morning / 07 January 2010 Session 271-MDO-3 Optimization Algorithms and Methodology II Crystal Ballroom C

Thursday Morning / 07 January 2010 Session 240-MVC-3 Simulation Environments and Data Processing Crystal Ballroom B


Chaired by: D. SMITH, Aerospace Testing Alliance, Arnold AFB, TN, and D. SCHIMANSKI, European Transonic Windtunnel, Cologne, Germany0900AIAA-2010-1304 Advanced Capabilitiesfor Wind Tunnel Testingin the 21st Century

J. Kegelman, NASALangley ResearchCenter, Hampton, VA

0930AIAA-2010-1305 Fiber Optics for RemoteDelivery of High PowerPulsed Laser Beams

J. Kriesel,Opto-KnowledgeSystems Inc., Torrance,CA

1000AIAA-2010-1306 Requirements for Fly-the- Mission Control inAerodynamic WindTunnels

J. Sheeley, AerospaceTesting Alliance, ArnoldAFB, TN

1030AIAA-2010-1307 Reduction of DynamicResponse of a WindTunnel Sting MountUsing a Hub DamperUnit

R. Glaese, CSAEngineering, Inc.,Huntsville, AL

1100AIAA-2010-1308 Reduction of DynamicResponse of a WindTunnel Sting MountUsing Co- curedComposite andViscoelastic Materials

S. Hsu, StirlingDynamics, Inc., Kirkland,WA

1130AIAA-2010-1309 Model- Based PredictiveControl System in aTransonic AerodynamicTest Facility

J. Sheeley, AerospaceTesting Alliance, ArnoldAFB, TN

Chaired by: A. ARSLAN, Northrop Grumman Corporation, Torrance, CA0900AIAA-2010-1500 Multi- ObjectiveOptimization ofSupersonic Projectilesusing EvolutionaryAlgorithms

D. Lisk, Queen'sUniversity Belfast,Belfast, Northern Ireland

0930AIAA-2010-1501 Multi- ObjectiveOptimization of High-Speed Train NoseShape Using the VehicleModeling Function

Y. Ku, Hyundai KiaMotors , Hwaseong,Gyeonggi-Do, SouthKorea

1000AIAA-2010-1503 Sensitivity Analysis forOptimization of DynamicSystems with ReducedOrder Modeling

P. Beran, U.S. Air ForceResearch Laboratory,Wright-Patterson AFB,OH

1030AIAA-2010-1504 Control of BoundaryRepresentation Topologyin MultidisciplinaryAnalysis and Design

R. Haimes,Massachusetts Instituteof Technology,Cambridge, MA

Chaired by: D. THOMPSON, Mississippi State University, Mississippi State, MS, and G. POWER, Arnold Engineering Development Center, Arnold AFB, TN0900AIAA-2010-1322 Caedium: A UnifiedSimulation Environment

R. Smith, Symscape,Enfield, NH

0930AIAA-2010-1323 An Intelligent AgentArchitecture forConcurrent CFDFeature Extraction

C. Mortensen, BrighamYoung University, Provo,UT

1000AIAA-2010-1324 RCAAPS - RotorcraftComputationalAeroAcoustics Post-Processing System

E. Duque, IntelligentLight, Rutherford , NJ

1030AIAA-2010-1325 Data Compression ofLarge- Scale FlowComputation UsingDiscrete WaveletTransform

R. Sakai, TohokuUniversity, Sendai,Japan

1100AIAA-2010-1326 A Prototype System forEvaluating CivilAirplane's AirportCompatibility based onVirtual Reality

F. Haocheng, BeijingUniversity of Aeronauticsand Astronautics,Beijing, China (prc)


Thursday Morning / 07 January 2010 Session 241-PC-16 Advanced Combustion Concepts Los Angeles

Thursday Morning / 07 January 2010 Session 242-PC-17 Bluffbody and Obstacle Interaction with Flames Denver

Thursday Morning / 07 January 2010 Session 243-PDL-14 Plasma Physics and Kinetics Grand Ballroom 1


Chaired by: J. GORD, U.S. Air Force Research Laboratory, Wright-Patterson AFB, OH, and C. LI, Aerojet, Folsom, CA0900AIAA-2010-1328 Analysis and Predictionof Dual- Mode Chemicaland Electric Ionic LiquidPropulsion Performance

B. Donius, MissouriUniversity of Scienceand Technology, Rolla,MO

0930AIAA-2010-1329 On Continuous NOxReduction of Aero-propulsion Engines

H. Mongia, PurdueUniversity, WestLafayette, IN

1000AIAA-2010-1330 OH- PLIF Calibrationand Investigation Withinthe Ultra CompactCombustor

K. LeBay, U.S. Air ForceInstitute of Technology,Wright-Patterson AFB,OH

1030AIAA-2010-1331 Effects of Non-Equilibrium Plasma onCounterflow DiffusionFlames

W. Sun, PrincetonUniversity, Princeton, NJ

1100AIAA-2010-1332 Scalar MixingEnhancement In A SwirlStabilized CombustorTrough Passive AndActive Injection Control

A. Lacarelle, TechnicalUniversity of Berlin,Berlin, Germany

Chaired by: M. ANAND, Rolls-Royce, Indianapolis, IN, and Y. HARDALUPAS, Imperial College London, London, Great Britain0900AIAA-2010-1333 Effects of AcousticExcitation on BluffbodyStabilized PremixedReacting Flows

V. Sankaran, UnitedTechnologies ResearchCenter, East Hartford,CT

0930AIAA-2010-1334 On the Evolution ofVorticity for Bluff- bodyStabilized PremixedFlames

Z. Carr, State Universityof New York, Buffalo,Buffalo, NY

1000AIAA-2010-1335 Effects of Pylon- AidedFuel Injection on Mixingin a Supersonic Flowfield

Q. Tu, University ofFlorida, Gainesville, FL

1030AIAA-2010-1336 Detonation InitiationImprovements UsingSwept- Ramp Obstacles

C. Brophy, NavalPostgraduate School,Monterey, CA

1100AIAA-2010-1337 Blowoff Dynamics of V-Shaped Bluff BodyStabilized,TurbulentPremixed Flames in aPractical Scale Rig

S. Chaudhuri, Universityof Connecticut, Storrs,CT

Chaired by: D. LEVIN, Pennsylvania State University, University Park, PA, and S. ROY, University of Florida, Gainesville, FL0900AIAA-2010-1339 Low PressureSemiconductorProcessing TransportProperty Modeling UsingDirect Simulation MonteCarlo

H. Deng, PennsylvaniaState University,University Park, PA

0930AIAA-2010-1340 Inactivation of YeastCells Using DielectricBarrier Discharge

N. Mastanaiah,University of Florida,Gainesville, FL

1000AIAA-2010-1341 Ultra–Lean andUltra–Rich FlamesStabilization byHigh–VoltageNanosecond PulsedDischarge

A. Nikipelov, NEQLabResearch BV, TheHague,, The Netherlands

1030AIAA-2010-1343 Compact Catalyst–FreeLiquid Fuel to SyngasReformer withPlasma–Assisted FlameStabilization

A. Nikipelov, NEQLabResearch BV, TheHague,, The Netherlands

1100AIAA-2010-1344 Pulsed ThermionicPower Conversion withPositive Work FunctionDifference

B. Alderman, PrincetonUniversity, Princeton, NJ

Chaired by: J. LAUBE, Northrop Grumman Corporation, Redondo Beach, CA


Thursday Morning / 07 January 2010 Session 244-SOS-1 Space Operations and Support Crystal Ballroom F

Thursday Morning / 07 January 2010 Session 245-SST-1 Sensor Systems Crystal Ballroom E

Thursday Morning / 07 January 2010 Session 247-TES-5 Numerical Simulation II Boston


Chaired by: J. LAUBE, Northrop Grumman Corporation, Redondo Beach, CA0900AIAA-2010-1345 Economic Factors forLaunch ComplexDevelopment in CurrentEconomy

G. Finger, Reynolds,Smith & Hills, Inc.,Merritt Island, FL

0930AIAA-2010-1346 Probability of FailureEstimation for NewVehicles Using theBivariate Approach toLearning

C. Draper, ACTA,Torrance, CA

1000AIAA-2010-1347 Can Your AirportBecome a Spaceport?The Benefits of aSpaceport DevelopmentPlan

B. Gulliver, Reynolds,Smith & Hills, Inc.,Merritt Island, FL

1030AIAA-2010-1348 Ground SideInfrastructure for Space-Based Solar Power

B. Gulliver, Reynolds,Smith & Hills, Inc.,Merritt Island, FL

1100AIAA-2010-1349 Lessons Learned inOperational Space andAir Traffic Management

D. Murray, FederalAviation Administration,Washington, DC

Chaired by: M. NIXON, The Boeing Company, Albuquerque, NM, and V. OTUGEN, Southern Methodist University, Dallas, TX0900AIAA-2010-1350 A GPS- Based Pitot-Static Calibration MethodUsing Global OutputError Optimization

J. Foster, NASA LangleyResearch Center,Hampton, VA

0930AIAA-2010-1352 Improved signalprocessing techniqueleads to more robust SelfDiagnosticAccelerometer System

R. Tokars, NASA GlennResearch Center, BrookPark,, OH

Chaired by: G. JACOBS, San Diego State University, La Mesa, CA, and S. SHERIF, University of Florida, Gainesville, FL0900AIAA-2010-1358 Heat Transfer Past ASingle Cylinder:Numerical Investigations

A. Abdel Raouf, CairoUniversity, Cairo, Egypt

0930AIAA-2010-1359 Trajectories ofProjectiles in 3- D Spacewith an Excel/VBA Code

D. Lilley, Lilley &Associates, Stillwater,OK

1000AIAA-2010-1360 NME: Some UsefulExcel/VBA Codes forNumerical Methods inEngineering

D. Lilley, Lilley &Associates, Stillwater,OK

1030AIAA-2010-1361 Estimating Grid-Induced Errors inUnsteady CFD SolutionsUsing a Discrete ErrorTransport Equation

B. Williams, CFDResearch Corporation,Huntsville, AL

1100AIAA-2010-1362 A NumericalInvestigation of SwirlingTurbulent Buoyant Jetsat Transient ReynoldsNumbers

G. Taub, University ofFlorida, Gainesville, FL

Chaired by: E. SHORT, and J. OCHTERBECK, Clemson University, Clemson, SC0900 0930 1000


Thursday Morning / 07 January 2010 Session 248-TP-17 Heat Pipes, Loop Heat Pipes, and Innovative Heat Pipe Designs Miami

Thursday Morning / 07 January 2010 Session 249-TP-18 Non-Intrusive Methods New York

Thursday Morning / 07 January 2010 Session 250-WE-7 Wind Turbine Operating Environment Crystal Ballroom G2


Chaired by: E. SHORT, and J. OCHTERBECK, Clemson University, Clemson, SC0900AIAA-2010-1363 WITHDRAWN Pressure- ControlledHeat Pipe

D. Sarraf, AdvancedCooling Technologies,Lancaster, PA

0930AIAA-2010-1365 Titanium- Water LoopHeat Pipe OperatingCharacteristics UnderStandard and ElevatedAcceleration Fields

A. Fleming, U.S. AirForce ResearchLaboratory,Wright-Patterson AFB,OH

1000AIAA-2010-1366 Investigation ofGravitational Effects OnFractal Loop Heat PipePerformance

E. Silk, NASA GoddardSpace Flight Center,Greenbelt, MD

Chaired by: C. SEGAL, University of Florida, Gainesville, FL, and D. REDDY, NASA Glenn Research Center, Cleveland, OH0900AIAA-2010-1370 Shock Front RadiationStudies at CUBRC

R. Parker, CUBRC,Buffalo, NY

0930AIAA-2010-1597 Simulation of CryogenicsCavitation

S. Kelly, University ofFlorida, Gainesville, FL

Chaired by: N. KELLEY, National Renewable Energy Laboratory, Golden, CO, and L. MANUEL, University of Texas, Austin, Austin, TX0900AIAA-2010-1373 k- E Simulations of theNeutral ABL: AchievingHorizontal Homogeneityon Practical Grids

J. Sumner, École deTechnologie Supérieure,Montréal, Canada

0930AIAA-2010-1374 Compact Representationof Large EddySimulations of theAtmospheric BoundaryLayer Using ProperOrthogonalDecomposition

M. Saini, University ofWyoming, Laramie, WY

1000AIAA-2010-1376 Enhanced EnergyCapture Through Gust-Tracking in the UrbanWind Environment

T. Bertényi, QuietRevolution Ltd., London,Great Britain

1030AIAA-2010-1377 Interaction of anEulerian Flue GasPlume with WindTurbines

T. Fletcher, University ofGlasgow, Glasgow,Great Britain

Chaired by: D. KNIGHT, Rutgers University, Piscataway, NJ, and S. BOBASHEV, Russian Academy of Sciences, Saint Petersburg, Russia0900 0930 1000 1030


Thursday Morning / 07 January 2010 Session 251-WIG-8 / PDL-15 Plasma-Based Flow Control Grand Ballroom 2

Thursday Afternoon / 07 January 2010 1300 - 1600 Fluid Dynamics Challenges in Flight Dynamics Miami

Thursday Afternoon / 07 January 2010 1300 - 1700 National Science and Technology Council- Biannual Aeronautics R&D Plan Update Crystal Ballroom A


Chaired by: D. KNIGHT, Rutgers University, Piscataway, NJ, and S. BOBASHEV, Russian Academy of Sciences, Saint Petersburg, Russia0900AIAA-2010-1378 The Nature of SurfaceMW Discharge

K. Khodataev, MoscowRadiotechnical InstitueRAS, , Russia

0930AIAA-2010-1381 Interaction of a HeatedFilament with a BluntBody in Supersonic Flow

K. Anderson, RutgersUniversity, Piscataway,NJ

1000AIAA-2010-1382 Supersonic BodyStreamline at DifferentConfiguration GasDischarge

A. Erofeev, RussianAcademy of Sciences ,Saint Petersburg, Russia

1030AIAA-2010-1383 Boundary- Layer ControlBased on LocalizedPlasma Generation:Aerodynamic Problem

N. Yurchenko, NationalAcademy of Sciences ofUkraine, Kiev, Ukraine

Chaired by: S. MCPARLIN, QinetiQ, Farnborough, Great Britain, and M. OL, U.S. Air Force Research Laboratory, Wright-Patterson AFB, OH

Panel Discussion:

Dr. Holger Babinsky, University of Cambridge, UK: “European Research Program on Unsteady Shock-Induced Separation UFAST: Introduction and Summary of the Transonic Experiments”

Prof. Charles Hirsch, NUMECA, Belgium: "(U)RANS Simulations of UFAST Test Cases: Expected and Unexpected Lessons Learned.””

Dr. George Barakos, University of Liverpool, UK: “Hybrid LES and DES Computations of Transonic Shockwave/Boundary-Layer Interaction: Recent Progress Reported in the UFAST Project.””

Mr. Kurtis R. Long (University of California, Santa Cruz) and Dr. Murray Tobak (NASA Ames Research Center): “Topological Aspects of the FAITH Experiment.” ”

Discussion during remaining time.

Chaired by: W. DAVIS, Office of Science and Technology Policy, Washington, DCThis session is the formal rollout of the biannual report, and an opportunity for attendees to find out more information about what the next steps for implementation of the National Aeronautics R&D Plan are, andwhat opportunities individuals will have to engage the administration on appropriate future actions or components update that is required under the Executive Order that created the original National Aero R&DPolicy and Plan in December of 2004.

Chaired by: J. PAGE, Wyle Laboratories, Arlington, VA1300 1330 1400 1430 1500 1530


Thursday Afternoon / 07 January 2010 Session 252-AA-10 Atmospheric Sound Propagation and Sonic Boom Washington

Thursday Afternoon / 07 January 2010 Session 253-AD-9 Student Aircraft Conceptual Designs Crystal Ballroom L

Thursday Afternoon / 07 January 2010 Session 254-AMT-9 Coherent Anti-Stokes Raman Spectroscopy Crystal Ballroom J1


Chaired by: J. PAGE, Wyle Laboratories, Arlington, VA1300AIAA-2010-1384 Nonlinear AcousticPropagation Predictionswith Applications toAircraft and HelicopterNoise

S. Lee, PennsylvaniaState University,University Park, PA

1330AIAA-2010-1385 Sonic Boom Modeling ofAdvanced SupersonicBusiness Jets inNextGen

J. Rachami, WyleLaboratories, Arlington,VA

1400AIAA-2010-1386 Slot Nozzle Effects forReduced Sonic Boom ona Generic SupersonicWing Section

R. Castner, NASA GlennResearch Center,Cleveland, OH

1430AIAA-2010-1387 Experimental Study ofInvestigations BetweenWeak Shock Wave andTurbulence

A. Matsuda, NagoyaUniversity, Nagoya,Japan

1500AIAA-2010-1388 Real Gas Effects onWeak Shock WavePropagation in anAtmosphere

T. Sakai, NagoyaUniversity, Aichi, Japan

1530AIAA-2010-1389 Global Variation of SonicBoom Intensity Due toSeasonal AtmosphericGradients

H. Yamashita, TohokuUniversity, Sendai,Japan

Chaired by: D. CARTER, U.S. Air Force Research Laboratory, Wright-Patterson AFB, OH, and C. BIL, RMIT University, Bundoora, Australia1300AIAA-2010-1391 Conceptual Design of aHybrid Lift Airship forIntra- Regional FlexibleAccess Transport

J. Agte, MassachusettsInstitute of Technology,Cambridge, MA

1330AIAA-2010-1392 Conceptual Design of anEnvironmentallyResponsible 150-Passenger CommercialAircraft

N. Smith, CaliforniaPolytechnic StateUniversity, San LuisObispo, CA

1400AIAA-2010-1393 Supersonic Bi-Directional Flying Wing,Part II: ConceptualDesign of A High SpeedCivil Transport

D. Espinal, University ofMiami, Coral Gables, FL

1430AIAA-2010-1394 Novel Senior DesignApproach of a HydrogenCitation X

B. Watters, University ofTexas, Arlington,Arlington, TX

1500AIAA-2010-1395 Parametric Design ofLow Emission Hybrid- liftCargo Aircraft

A. Donaldson,Massachusetts Instituteof Technology,Cambridge, MA

1530AIAA-2010-1396 Conceptual Design of aNext Generation, 150Passenger CommercialTransport

R. Halper, CaliforniaPolytechnic StateUniversity, San LuisObispo, CA

Chaired by: J. GORD, U.S. Air Force Research Laboratory, Wright-Patterson AFB, OH, and S. NAIK, Purdue University, West Lafayette, IN1300AIAA-2010-1397 CARS Spectral Fitting ofMultiple ResonantSpecies Using SparseLibraries

A. Cutler, GeorgeWashington University,Newport News, VA

1330AIAA-2010-1398 Single- Beam CoherentAnti- Stokes RamanScattering (CARS)Spectroscopy withTailored UltrashortLaser Pulses

J. Gord, U.S. Air ForceResearch Laboratory,Wright-Patterson AFB,OH

1400AIAA-2010-1399 PicosecondLaser–Based Fiber-Coupled CARSSpectroscopy for Gas-Phase Thermometry

P. Hsu, U.S. Air ForceResearch Laboratory,Wright-Patterson AFB,OH

1430AIAA-2010-1400 Beam Shaping forCARS Measurements inTurbulent Environments

G. Magnotti, GeorgeWashington University,Hampton, VA

1500AIAA-2010-1401 Dual- Pump CARSMeasurements in a GasTurbine CombustorFacility Using the NASA9- Point Lean DirectInjector

M. Thariyan, PurdueUniversity, WestLafayette, IN

1530AIAA-2010-1402 TemperatureMeasurements inFlames at 1000 HzUsing FemtosecondCoherent Anti- StokesRaman Spectroscopy

R. Lucht, PurdueUniversity, WestLafayette, IN

1600AIAA-2010-1403 Electronic- Resonance-Enhanced CoherentAnti- Stokes RamanScattering of NitricOxide: Non- PerturbativeTime- DependentModeling

N. Chai, PurdueUniversity, WestLafayette, IN


Thursday Afternoon / 07 January 2010 Session 255-AMT-10 Fluorescence-Based Techniques Crystal Ballroom K

Thursday Afternoon / 07 January 2010 Session 256-APA-26 Active Flow Control IV Grand Ballroom 9

Thursday Afternoon / 07 January 2010 Session 257-APA-27 Miscellaneous Topics in CFD and Applied Aerodynamics Grand Ballroom 10


Chaired by: S. KEARNEY, Sandia National Laboratories, Albuquerque, NM, and N. JIANG, Ohio State University, Columbus, OH1300AIAA-2010-1404 Multiple Velocity ProfileMeasurements inHypersonic Flows UsingSequentially- ImagedFluorescence Tagging

B. Bathel, NASALangley ResearchCenter, Hampton, VA

1330AIAA-2010-1405 Hydroxyl TaggingVelocimetry in aSupersonic Flow over aPiloted Cavity

N. Grady, VanderbiltUniversity, Nashville, TN

1400AIAA-2010-1406 High- Speed Multi- LineOH Planar Laser-Induced Fluorescence inUnsteady Flames

J. Miller, Iowa StateUniversity, Ames, IA

1430AIAA-2010-1407 MHz- Rate NO PLIFImaging in a Mach 10Hypersonic Wind Tunnel

N. Jiang, Ohio StateUniversity, Columbus,OH

1500AIAA-2010-1408 High- SpectralResolution PLIF Imagingof Compressible Flowsand Plasmas

A. Bhuiyan, PurdueUniversity, WestLafayette, IN

Chaired by: J. GEORGE, Innovative Aerospace Solutions, Downey, CA, and J. AZEVEDO, National Institute for Space Research (INPE), São José dos Campos, , Brazil1300AIAA-2010-1409 Flow Separation ControlBy Trapped Vortex

R. Donelli, ItalianAerospace ResearchCenter (CIRA), Capua,Italy

1330AIAA-2010-1411 Active Flow ControlTechnique for theReduction of HelicopterBVI Noise: A NumericalStudy Using LES


1400AIAA-2010-1412 PIV around a NACA0012Airfoil with a PlasmaActuator for NoiseReduction

S. Koike, JapanAerospace ExplorationAgency (JAXA), Chofu,Japan

1430AIAA-2010-1413 Boundary ConditionModels for Synthetic JetSimulation

I. Yoo, Inha University,Incheon, South Korea

Chaired by: M. CHAFFIN, Cessna Aircraft Company, Wichita, KS, and S. MORRIS, Engineering Systems, Inc., Colorado Springs, CO1300AIAA-2010-1414 Evaluation of RadialBasis Functions for CFDVolume DataInterpolation

T. Rendall, University ofBristol, Avon, GreatBritain

1330AIAA-2010-1416 Influence of TurbulenceModelling and GridResolution InComputations of theDPW4 CRMConfiguration

P. Eliasson, FOISwedish DefenceResearch Agency,Stockholm, Sweden

1400AIAA-2010-1417 Drag Prediction onNASA CRM UsingAutomatic HexahedraGrid Generation

A. Hashimoto, JapanAerospace ExplorationAgency (JAXA), Chofu,Japan

1430AIAA-2010-1418 MultidimensionalAdaptive Sampling forGlobal Metamodelling

T. Mackman, Universityof Bristol, Avon , GreatBritain

1500AIAA-2010-1419 An Aerodynamic Studyof an Urban MaglevVehicle

J. Wells, Old DominionUniversity, Norfolk, VA

Chaired by: W. ANDERSON, University of Tennessee, Chattanooga, Chattanooga, TN


Thursday Afternoon / 07 January 2010 Session 258-APA-28 Optimization Methods in Applied Aerodynamics Grand Ballroom 11

Thursday Afternoon / 07 January 2010 Session 259-APA-29 Unmanned Aerial Vehicle Designs/Tests Grand Ballroom 12

Thursday Afternoon / 07 January 2010 Session 260-FD-55 CFD Applications Including Optimization Grand Ballroom 3


Chaired by: W. ANDERSON, University of Tennessee, Chattanooga, Chattanooga, TN1300AIAA-2010-1420 Optimal Kinematics ofHovering Insect Flightfor Minimum MechanicalPower

M. Kurdi, UniversalTechnology Corp. , ,

1330AIAA-2010-1421 An Adjoint- BasedShape Optimization ofGas Turbine Blades

A. Mousavi, McGilluniversity, Montréal,Canada

1400AIAA-2010-1422 Optimization of Wings inGround Effect UsingMulti- Objective GeneticAlgorithm

J. Lee, Hoseo University,Asan, South Korea

1430AIAA-2010-1423 Optimization of FlatbackAirfoils for Wind TurbineBlades Using a GeneticAlgorithm with anArtificial Neural Network

X. Chen, WashingtonUniversity in St. Louis,St. Louis, MO

Chaired by: L. AUMAN, U.S. Army Research, Development and Engineering Command, Huntsville, AL, and C. COX, U.S. Air Force Research Laboratory, Wright-Patterson Air Force Base, OH1300AIAA-2010-1425 Evaluation of DES forWeapon Bays in UCAVs

S. Lawson, University ofLiverpool, Liverpool,Great Britain

1330AIAA-2010-1427 Aerodynamic Analysis ofa Multi- Mission Short-Shrouded Coaxial UAV:Part II – TranslationFlight

C. Thipyopas, ISAE,Toulouse, France

1400AIAA-2010-1428 Conceptual Design andComputationalInvestigation ofStabilator MountedCoplanar with Wing

M. Arndt, U.S. Air ForceAcademy, ColoradoSprings, CO

1430AIAA-2010-1429 Flow Sensory Actuatorsfor MAVs

V. Kumar, Florida A&MUniversity-Florida StateUniversity, Tallahassee,FL

Chaired by: N. GEORGIADIS, NASA Glenn Research Center, Cleveland, OH, and T. RAMSAY, Honda R&D Americas, Inc., Raymond, OH1300AIAA-2010-1430 Adjoint- Based Design ofPassive and ActiveShock Mitigation Devices

A. Stueck, HamburgUniversity ofTechnology, Hamburg,Germany

1330AIAA-2010-1431 A ComparativeAerodynamic Study ofCommercial BicycleWheels Using CFD

M. Godo, IntelligentLight, Rutherford, NJ

1400AIAA-2010-1432 Shape Optimization andFluid Dynamic Analysisof a Translating FlexibleBody

S. Thomson, BrighamYoung University, Provo,UT

1430AIAA-2010-1433 Higher Order TwoDimensionalAerodynamicOptimization UsingUnstructured Grids andAdjoint SensitivityComputations

M. Azab, University ofBritish Columbia,Vancouver, Canada

1500AIAA-2010-1434 Stability Analysis of FullGeometry Aircraftthrough CFD andResponse SurfaceMethod

W. Kim, KonkukUniversity, Seoul, SouthKorea

Chaired by: H. HU, Iowa State University, Ames, IA, and G. ZHA, University of Miami, Coral Gables, FL


Thursday Afternoon / 07 January 2010 Session 261-FD-56 Experimental Studies of Fluid Dynamic Phenomena Grand Ballroom 4

Thursday Afternoon / 07 January 2010 Session 262-FD-57 Fluid-Structure Interactions Grand Ballroom 5

Thursday Afternoon / 07 January 2010 Session 263-FD-58 High Order Methods IV Grand Ballroom 6


Chaired by: H. HU, Iowa State University, Ames, IA, and G. ZHA, University of Miami, Coral Gables, FL1300AIAA-2010-1437 High- Speed, Three-DimensionalQuantification ofLadybug (HippodamiaConvergens) FlappingWing Kinematics DuringTakeoff

R. George, BrighamYoung University, Provo,UT

1330AIAA-2010-1439 Low Pressure PLIFVisualization and MixingQuantification in a Multi-Stream Injection Nozzle

A. Ragheb, University ofIllinois,Urbana-Champaign,Urbana, IL

1400AIAA-2010-1440 The Effects of AtomicOxygen on the Sealingand MechanicalPerformance of anElastomer Seal

N. Garafolo, Universityof Akron, Cleveland, OH

1430AIAA-2010-1441 Normal- and Shear-Stress Over a Flat-Surface Established anInclined Cylinder on

T. Shizawa, TokyoUniversity of Science,Chino, Japan

Chaired by: D. LOCKARD, NASA Langley Research Center, Hampton, VA, and F. LADEINDE, TTC Technologies, Inc., Stony Brook, NY1300AIAA-2010-1442 Frequency Response ofCylindrical Resonators ina Viscous Fluid

M. Martin, LouisianaState University, BatonRouge, LA

1330AIAA-2010-1444 Philiadium GregariumVersus Aurelia Aurita:On PropulsionPropulsion of Jellyfish

S. Etienne, ÉcolePolytechnique deMontréal , Montréal ,Canada

1400AIAA-2010-1445 Implicit Runge- KuttaTime Integrators forFluid- StructureInteractions

J. Cori, ÉcolePolytechnique deMontréal, Montréal,Canada

1430AIAA-2010-1446 Spacecraft ThrusterEfficiency Optimizationwith Respect to CoupledSolid- Liquid Dynamics

A. Baeten, AugsburgUniversity of AppliedSciences, Augsburg,Germany

1500AIAA-2010-1447 WITHDRAWN A Hybrid InterpolationMethod for InformationExchange inComputationalAeroelasticity

X. Wang, Shanghai JiaoTong University,Shanghai, China (prc)

Chaired by: C. VENKATASUBBAN, and A. GROSS, University of Arizona, Tucson, AZ1300AIAA-2010-1448 Efficient SolutionTechniques forDiscontinuous GalerkinDiscretizations of theNavier- StokesEquations on HybridAnisotropic Meshes

N. Burgess, University ofWyoming, Laramie, WY

1330AIAA-2010-1449 Computation Of Flowswith Shocks UsingSpectral DifferenceScheme with ArtificialViscosity

S. Premasuthan,Stanford University,Stanford, CA

1400AIAA-2010-1450 A High Order Cut CellMethod for NumericalSimulation of ThreeDimensional HypersonicBoundary- LayerTransition with FiniteSurface Roughness

L. Duan, University ofCalifornia,, Los Angeles,CA

1430AIAA-2010-1451 Improved Seventh-Order WENO Scheme


1500AIAA-2010-1452 Low Diffusion E- CUSPScheme with High OrderWENO Scheme forPreconditioned Navier-Stokes Equations


1530AIAA-2010-1453 High Order InterpolationMethods and RelatedURANS Schemes onComposite Ggrids

J. Le Gouez, ONERA,Châtillon, France


Thursday Afternoon / 07 January 2010 Session 264-FD-59 / APA-30 Instability and Transition Crystal Ballroom M

Thursday Afternoon / 07 January 2010 Session 265-FD-60 Multiphysics Simulations Crystal Ballroom N

Thursday Afternoon / 07 January 2010 Session 266-FD-61 Overview of AVT-136: Flight Experiment Assessment via Ground Test and CFD New York


Chaired by: D. BRIDGES, Mississippi State University, Mississippi State, MS, and G. DALE, U.S. Air Force Research Laboratory, Wright-Patterson AFB, OH1300AIAA-2010-1454 Receptivity andTransition of SupersonicBoundary Layers OverSwept Wings

P. Balakumar, NASALangley ResearchCenter, Hampton, VA

1330AIAA-2010-1455 Optimization of aTransition CalibrationBody for Wind TunnelFlow Quality Assessment

J. Eppink, TuftsUniversity, Medford, MA

1400AIAA-2010-1456 Study of Mechanism ofRing- Like VortexFormation in Late FlowTransition

C. Liu, University ofTexas, Arlington,Arlington, TX

Chaired by: F. LIU, University of California, Irvine, Irvine, CA, and D. YODER, NASA Glenn Research Center, Cleveland, OH1300AIAA-2010-1460 Sharp InterfaceSimulations of HighSpeed MultimaterialImpact and PenetrationMechanics

S. Sambasivan,University of Iowa, IowaCity, IA

1330AIAA-2010-1461 ConjugateDesign/AnalysisProcedure for Film-Cooled Turbine AirfoilSections

R. Davis, University ofCalifornia,, Davis, CA

1400AIAA-2010-1462 Multiphysics Couplingfor Reentry Flows

P. Bauman, University ofTexas, Austin, Austin, TX

1430AIAA-2010-1463 Three DimensionalCompressible Multi-Material Flows

A. Kapahi, University ofIowa, Iowa City, IA

1500AIAA-2010-1464 Material Point MethodApplied to Fluid-Structure Interaction(FSI)/AeroelasticityProblems

P. Hu, AdvancedDynamics, Inc.,Lexington, KY

Chaired by: J. SCHMISSEUR, U.S. Air Force, Arlington, VA, and J. MUYLAERT, ESA, Noordwijk, The Netherlands1300AIAA-2010-1465 Shock InteractionsInvestigationsAssociated with AVT-136

D. Knight, Rutgers -State University of NewJersey , New Brunswick, NJ

1330AIAA-2010-1466 Summary of HypersonicTransition ResearchCoordinated ThroughNATO RTO AVT- 136

S. Schneider, PurdueUniversity, WestLafayette, IN

1400AIAA-2010-1467 Modeling Approachesfor Gas- SurfaceInteractions

G. Herdrich, Institut furRawmfahrtsysteme(IRS) , Stuttgart, Germany

1430AIAA-2010-1468 Base Flow Investigationof the Apollo CommandModule in the Frame ofAVT- 136

L. Walpot, AdvancedOperations andEngineering ServicesGroup, Leiden, TheNetherlands

Chaired by: W. LIOU, Western Michigan University, Kalamazoo, MI1300 1330 1400 1430 1500


Thursday Afternoon / 07 January 2010 Session 267-FD-62 Theoretical and Computational Fluid Flow Problems Crystal Ballroom P

Thursday Afternoon / 07 January 2010 Session 268-GPSE-7 Physics and Material Science II Crystal Ballroom D

Thursday Afternoon / 07 January 2010 Session 269-GT-10 Test Facilities Crystal Ballroom G1


Chaired by: W. LIOU, Western Michigan University, Kalamazoo, MI1300AIAA-2010-1469 Transition FlowOccurrence EstimationNew Method

P. Silisteanu, ETS -LARCASE, Montréal,Canada

1330AIAA-2010-1470 DNS for Late StageStructure of FlowTransition on a Flat-Plate Boundary Layer

L. Chen, University ofTexas, Arlington,Arlington, TX

1400AIAA-2010-1471 DNS for Ring - LikeVortices Formation andRoles in Positive SpikesFormation

X. Liu, University ofTexas, Arlington,Arlington, TX

1430AIAA-2010-1472 Towards EfficientViscous Modeling Basedon Cartesian Methodsfor Automated FlowSimulation

H. Zhao, AdvancedDynamics, Inc.,Lexington, KY

1500AIAA-2010-1473 On the SensitivityAnalysis of Angle- of-Attack in a ModelReduction Setting

A. Hay, VirginiaPolytechnic Institute ,Blacksburg, VA

Chaired by: J. HOCHSTEIN, University of Memphis, Memphis, TN, and S. TSE, Rutgers University, Piscataway, NJ1300AIAA-2010-1476 Liquid Plugs inRectangular ChannelsUnder a TransverseGravity Field

R. Manning, PurdueUniversity, WestLafayette, IN

1330AIAA-2010-1477 Simulation ofMicrogravity DiffusionFlames Using Sub-Atmospheric Pressures

N. Panek, University ofToronto, Toronto,Canada

1400AIAA-2010-1478 NanoparticleAgglomeration Payloadsfor MicrogravityExperimentation

S. Lösch, FraunhoferInstitute forManufacturingTechnology and AppliedMaterials Research(IFAM), Bremen,Germany

1430AIAA-2010-1480 Scaling Parameters inBuoyancy Flows


1500AIAA-2010-1481 The Constrained VaporBubble Experiment forthe ISS – Earth’s Gravityand Mu Gravity Results

A. Chatterjee,Rensselaer PolytechnicInstitute, Troy, NY

1530AIAA-2010-1482 Bubble Evolution andGrowth in Fluids underVacuum


1600AIAA-2010-1483 Capillary Stability inTilted Square Cylinders

S. Collicott, PurdueUniversity, WestLafayette, IN

Chaired by: I. PHILIPSEN, German-Dutch Wind Tunnels (DNW), Marknesse, The Netherlands, and D. WISHART, Pratt & Whitney, A United Technologies Company, Stuart, FL1300AIAA-2010-1484 Modification of aTransonic BlowdownWind Tunnel to ProduceOscillating FreestreamMach Number

K. Gompertz, OhioState University,Columbus, OH

1330AIAA-2010-1485 A Mach 4 Wind Tunnelfor Plasma / BoundaryLayer Interaction Studies

B. DeBlauw, Universityof Illinois,Urbana-Champaign,Urbana, IL

1400AIAA-2010-1486 Facility for Shock andDetonation WaveInteraction with aReactive Turbulent Field

F. Lu, University ofTexas, Arlington,Arlington, TX

1430AIAA-2010-1487 Lessons Learned duringRecent Upgrade: TheRejuvenation of theWichita StateUniversity’s Walter H.Beech 7x10 foot LowSpeed Wind Tunnel atthe National Institute forAviation Researc

E. Irani, Wichita StateUniversity, Wichita, KS

1500AIAA-2010-1488 WITHDRAWN New AltitudeCombustion StandFacility

B. Rosenthal, NASAGlenn Research Center,Cleveland, OH

1530AIAA-2010-1489 Ground TestingTechnical CommittteeWind Tunnel DatabaseDemonstration (Invited)

R. White, ViGYAN, Inc.,Hampton, VA

1600AIAA-2010-1490 Characteristics of theMars Wind Tunnel atTohoku University inCO2 Operation Mode

M. Anyoji, TohokuUniversity, Sendai,Japan


Thursday Afternoon / 07 January 2010 Session 270-GT-11 NASA New Millenium Program Technology and Ground Testing Grand Ballroom 14

Thursday Afternoon / 07 January 2010 Session 272-MDO-4 Optimization Applications II Crystal Ballroom C

Thursday Afternoon / 07 January 2010 Session 24-MVC-2 Solution Adaptive Meshing Crystal Ballroom B


Chaired by: J. STOCKY, Jet Propulsion Laboratory, Pasadena, CA, and J. NORRIS, Aerospace Testing Alliance, Silver Spring, MD1300AIAA-2010-1491 Validation of SAILMASTTechnology andModeling by GroundTesting of a Full- ScaleFlight Article

M. McEachen, ATK,Goleta, CA

1330AIAA-2010-1492 Confirmation of Non-Dimensionalized(Scalable) Closed- FormAnalytics for ModelingSlender Truss Behaviorunder Combined Loading

T. Trautt, ATK, Goleta,CA

1400AIAA-2010-1493 Multi- EvaporatorMiniature Loop HeatPipe for SmallSpacecraft ThermalControl, Part I: NewTechnologies andValidation Approach

J. Ku, NASA GoddardSpace Flight Center,Greenbelt, MD

1430AIAA-2010-1494 Multi- EvaporatorMiniature Loop HeatPipe for SmallSpacecraft ThermalControl, Part II:Validation Results

J. Ku, NASA GoddardSpace Flight Center,Greenbelt, MD

1500AIAA-2010-1495 NMP ST8 DependableMultiprocessor:Technology andTechnology ValidationOverview

J. Samson, HoneywellInternational, Inc.,Clearwater, FL

1530AIAA-2010-1496 NMP ST8 DependableMultiprocessor:Technology ValidationApproach and Results

E. Grobelny, HoneywellInternational, Inc.,Clearwater, FL

1600AIAA-2010-1497 ST8 ValidationExperiment:Ultraflex-175 Solar ArrayTechnology Advance:Deployment Kinematicsand Deployed DynamicsGround Testing andModel Validation

D. Eacret , ATK, Goleta,CA

1630AIAA-2010-1498 ST8 Ultraflex- 175 SolarArray- DeployedDynamics AnalyticalModeling andComparison toValidation Criteria

T. Trautt, ATK, Goleta,CA

Chaired by: T. TAKAHASHI, Northrop Grumman Corporation, Torrance, CA, and Y. KO, AVID LLC, Blacksburg, VA1300AIAA-2010-1505 Application of aTechnology ScreeningMethodology forRotorcraft AlternativePower Systems

M. Strauss, SikorskyAircraft Corporation,Stratford, CT

1330AIAA-2010-1506 Boom MinimizationFramework forSupersonic AircraftUsing CFD Analysis

I. Ordaz, NASA LangleyResearch Center,Hampton, VA

1400AIAA-2010-1508 A Knowledge- BasedGeometry RepairSystem for RobustParametric CAD Models

D. Li, University ofSouthampton,Southampton, GreatBritain

1430AIAA-2010-1509 Response SurfaceBased AerodynamicShape Optimization ofHigh Speed Train Nose

V. Vytla, Wright StateUniversity, Dayton, OH

1500AIAA-2010-1510 Design Optimization ofComposite Wing Box forFlutter and Stiffness

N. Chang, NorthwesternPolytechnical University,Xi'an, China (prc)

Chaired by: S. ALTER, NASA Langley Research Center, Hampton, VA, and T. MICHAL1300AIAA-2010-0168 Turbulent Output- BasedAnisotropic Adaptation

M. Park, NASA LangleyResearch Center,Hampton, VA

1330AIAA-2010-0169 Anisotropic AdaptiveSimulations inAerodynamics

A. Loseille, Center forCoputational FluidsDynamics, GeorgeMason University,Fairfax, VA

1400AIAA-2010-0170 Output- DrivenAnisotropic MeshAdaptation for ViscousFlows Using DiscreteChoice Optimization

M. Ceze, University ofMichigan, Ann Arbor, MI

1430AIAA-2010-0171 Feature- Driven AdaptiveMesh Refinement in theHelios Code

S. Kamkar, StanfordUniversity, Stanford, CA

Chaired by: F. GOULDIN, Cornell University, Ithaca, NY, and R. ANTHENIEN, Army Research Office, Research Triangle Park, NC


Thursday Afternoon / 07 January 2010 Session 273-PC-18 Chemical Kinetics Los Angeles

Thursday Afternoon / 07 January 2010 Session 274-PC-19 Combustion Instabilities Denver

Thursday Afternoon / 07 January 2010 Session 275-PC-20 Practical Aspects of Combustor Design New Orleans


Chaired by: F. GOULDIN, Cornell University, Ithaca, NY, and R. ANTHENIEN, Army Research Office, Research Triangle Park, NC1300AIAA-2010-1511 The Oxidative Crackingof Hydrocarbon Fuels

W. Tsang, NationalInstitute of Standardsand Technology,Gaithersburg, MD

1330AIAA-2010-1512 Ignition and Oxidation ofEthylene- Air Mixtures atElevated Pressures

M. Kopp, Texas A&MUnivversity, CollegeStation, TX

1400AIAA-2010-1514 Alkane KineticsReduction Consistentwith TurbulenceModeling using LargeEddy Simulation

K. Harstad, JetPropulsion Laboratory,Pasadena, CA

1430AIAA-2010-1515 A Study on Detonationof Jet- A Using aReduced Mechanism

K. Ajmani, ASRCAerospace, Cleveland,OH

1500AIAA-2010-1516 Soot Modeling inPartially PremixedC2H4/Air Flames

T. Blacha, GermanAerospace Center(DLR), Institute ofCombustionTechnology, Stuttgart,Germany

Chaired by: D. TALLEY, U.S. Air Force Research Laboratory, Palmdale, CA, and J. DELAAT, NASA Glenn Research Center, Cleveland, OH1300AIAA-2010-1517 ThermoacousticInstability in SolidRocket Motor: Non-Normality and NonlinearInstabilities

S. Mariappan, IndianInstitute of Technology,Madras, Chennai, India

1330AIAA-2010-1518 Modeling CombustionInstability in Small MMH-NTO Liquid RocketEngines Using CFD:Injector- ChamberCoupling

M. Nusca, U.S. ArmyResearch Laboratory,Aberdeen ProvingGround, MD

1400AIAA-2010-1519 Time Delay and NoiseCoupling in LimitingControl Effectiveness inUnstable Combustors

J. Crawford, GeorgiaInstitute of Technology,Atlanta, GA

1430AIAA-2010-1522 On the Flame andVorticity Characteristicsof a Fluidically StabilizedPremixed TurbulentFlame

D. Forliti, StateUniversity of New York,Buffalo, Buffalo, NY

1500AIAA-2010-1523 Simulation ofAcoustically Forced H2-O2 Shear- CoaxialModel Injector

D. Gers, University ofMaryland, College Park,MD

1530AIAA-2010-1524 Instability Suppressionin a Swirl- StabilizedCombustor UsingMicrojet Air Injection

Z. LaBry, MassachusettsInstitute of Technology,Cambridge, MA

Chaired by: I. LEYVA, U.S. Air Force Research Laboratory, Edwards AFB, CA, and E. LYNCH, Pratt & Whitney, A United Technologies Company, Canoga Park, CA1300AIAA-2010-1525 Turbulence- ChemistryInteraction and HeatTransfer Modeling ofH2/O2 Gaseous InjectorFlows

E. Sozer, University ofMichigan, Ann Arbor, MI

1330AIAA-2010-1526 Supersonic MixingEnhancement andOptimization Using Fin-Guided Fuel Injection

C. Aguilera, University ofMaryland, College Park,MD

1400AIAA-2010-1527 Asymmetric InjectorDistribution for PassiveControl of Liquid RocketEngine CombustionInstabilities

J. Bennewitz, GeorgiaInstitute of Technology,Atlanta, GA

1430AIAA-2010-1529 On Initiating 3rdGeneration ofCorrelations forGaseous Emissions ofAero- Propulsion Engines


1500AIAA-2010-1530 Correlations forGaseous Emissions ofAero- PropulsionEngines from Sea- Levelto Cruise Operation


1530AIAA-2010-1532 Combustion in a RamjetCombustor with CavityFlame Holder

O. Tuncer, IstanbulTechnical University,Istanbul, Turkey


Thursday Afternoon / 07 January 2010 Session 276-PDL-16 Reentry Plasmas Grand Ballroom 1

Thursday Afternoon / 07 January 2010 Session 277-SOS-2 Public Safety in Launch and Reentry Operations Grand Ballroom 13

Thursday Afternoon / 07 January 2010 Session 278-SRU-3 Unit Operations in Lunar Resource Extraction Atlanta


Chaired by: R. MILES, Princeton University, Princeton, NJ, and S. BOBASHEV, Russian Academy of Sciences, Saint Petersburg, Russia1300AIAA-2010-1534 Simulation of MagneticField Impact on WallHeat Flux in PlasmaFlows

S. Bobashev, RussianAcademy of Sciences,Saint Petersburg, Russia

1330AIAA-2010-1535 ThermochemicalNonequilibrium FlowComputation of DragReduction by PulsedLaser

M. Tate, TohokuUniversity, Sendai,Japan

1400AIAA-2010-1536 Effects of Water VaporPresence in MartianAtmospheric EntryPlasma

D. Drake, Old DominionUniversity, Norfolk, VA

1430AIAA-2010-1537 Effects of a ConductingSphere Moving Througha Gradient MagneticField

A. Giffin, PrincetonUniversity, Princeton, NJ

1500AIAA-2010-1538 Simulations of ThermalPhenomena inNanosecond PulsedPlasma Discharges inSupersonic Flow

D. Breden, University ofTexas, Austin, Austin,TX

Chaired by: D. MURRAY and E. GONZALES, Federal Aviation Administration, Washington, DC1300AIAA-2010-1540 FAA’s Approaches toGround and NASSeparation Distances forCommercial RocketLaunches

E. Gonzales, FederalAviation Administration,Washington , DC

1330AIAA-2010-1541 Application of KernelDensity Estimation toImpact ProbabilityDensity Determinationfor Risk Analysis

E. Larson, ACTA,Torrance, CA

1400AIAA-2010-1542 Aircraft ProtectionStandards andImplementationGuidelines for RangeSafety

P. Wilde, FAA,Washington , DC

1430AIAA-2010-1543 A Safe Explosive SitePlan for Suborbital RLVs

D. Nolek, Reynolds,Smith & Hills, Inc.,Merritt Island, FL

1500AIAA-2010-1544 Risk Considerations forRandom Reentry ofSpace Debris

S. Millard, FederalAviation Administration,Washington, DC

Chaired by: D. LINNE, NASA Glenn Research Center, Cleveland, OH, and L. SIBILLE, ASRC Aerospace Corporation, Huntsville, AL1300AIAA-2010-1546 Heating- Rate CoupledModel for HydrogenReduction of JSC- 1A

U. Hegde, NationalCenter for SpaceExploration Research,Cleveland, OH

1330AIAA-2010-1547 Evolution of RegilithFeed Systems for LunarISRU O2 ProductionPlants

R. Mueller, NASAKennedy Space Center,Cape Canaveral, FL

1400AIAA-2010-1548 Lunar UndergroundMining andConstruction: ATerrestrial VisionEnabling SpaceExploration andCommerce

G. Baiden, Penguin ASI,Sudbury, Canada

1430AIAA-2010-1549 Effect of RegolithCompaction on RippingEfficiency

M. Iai, MissouriUniversity of Scienceand Technology, Rolla,MO

1500Oral Presentation Performance Testing ofMolten RegolithElectrolysis andTransfer of MoltenMaterial for Oxygenand Metals Productionon the Moon

L. Sibille, ASRCAerospace Corporation,Cape Canaveral, FL

1530AIAA-2010-1551 Creating Methane fromPlastics: Recycling at aLunar Outpost

J. Captain, NASAKennedy Space Center,Cape Canaveral, FL

1600AIAA-2010-1552 Self- Contained andSelf- PoweredCondensation Systemfor Reclamation ofWater from LunarRegolith Processing

P. Sforza, University ofFlorida, Gainesville, FL

Chaired by: R. GOSSE, U.S. Air Force Research Laboratory, Beavercreek, OH, and X. ZHONG, University of California, Los Angeles, Los Angeles, CA


Thursday Afternoon / 07 January 2010 Session 280-TP-19 High Speed Flows Crystal Ballroom Q

Thursday Afternoon / 07 January 2010 Session 281-TP-20 Non-Equilibrium Flows II Crystal Ballroom E

Thursday Afternoon / 07 January 2010 Session 282-TP-21 Orbiter Entry Aerothermo Flight Experiments: Ground Testing and Analyses Crystal Ballroom F


Chaired by: R. GOSSE, U.S. Air Force Research Laboratory, Beavercreek, OH, and X. ZHONG, University of California, Los Angeles, Los Angeles, CA1300AIAA-2010-1557 On the (In)Validation ofa ThermochemicalModel with EAST ShockTube RadiationMeasurements

K. Miki, The Universityof Texas, Austin, Austin,TX

1330AIAA-2010-1558 Investigation of theInteractions of ReactionControl Systems withMars ScienceLaboratory Aeroshell

E. Reed, University ofVirginia, Charlottesville,VA

1400AIAA-2010-1559 ExperimentalInvestigation of HeliumInjection in a HypersonicTurbulent BoundaryLayer

D. Sahoo, PrincetonUniversity, Princeton, NJ

1430AIAA-2010-1560 Stabilized FiniteElement Scheme forHigh Speed Flows withChemical Non-Equilibrium

S. Bova, SandiaNational Laboratories,Albuquerque, NM

1500AIAA-2010-1561 Simulation of FlowSeparation andReattachment on a Re-Entry Capsule AfterbodyFrustum

K. Sinha, Indian Instituteof Technology, Bombay,Mumbai, India

1530AIAA-2010-1562 Numerical andExperimentalCharacterization of HighEnthalpy Flow in anExpansion TunnelFacility

M. MacLean, CUBRC,Buffalo, NY

1600AIAA-2010-1563 WITHDRAWN Development of a PilotModel of HypersonicRarefied Wind- Tunnel

K. Fujita, JapanAerospace ExplorationAgency (JAXA), Chofu,Japan

1630AIAA-2010-1564 Characterization of theNew LENS ExpansionTunnel Facility

A. Dufrene, CUBRC,Buffalo, NY

Chaired by: E. JOSYULA, U.S. Air Force Research Laboratory, Wright-Patterson AFB, OH1300AIAA-2010-1566 Expansion TubeInvestigation of ShockStand- Off Distances inHigh- Enthalpy CO2Flow Over Blunt Bodies

M. Sharma, University ofIllinois, Urbana, IL

1330AIAA-2010-1567 Development of a Mach5 Nonequilibrium WindTunnel

M. Nishihara, Ohio StateUniversity, Columbus,OH

1400AIAA-2010-1568 Influences of MolecularRotation on VibrationalKinetics andDissociation of N2

K. Fujita, JapanAerospace ExplorationAgency (JAXA), Chofu,Japan

1430AIAA-2010-1569 Evaluation of a HybridBoltzmann- ContinuumMethod for High SpeedNonequilibrium Flows

J. Burt, University ofMichigan, Ann Arbor, MI

1500AIAA-2010-1570 Analysis of Chemistry-Vibration Coupling inDiatomics for HighEnthalpy Nozzle Flows

S. Doraiswamy,University of Minnesota,Minneapolis, MN

Chaired by: E. RESHOTKO, Case Western Reserve University, Cleveland, OH, and S. SCHNEIDER, Purdue University, West Lafayette, IN1300AIAA-2010-1571 Orbiter BLT FlightExperiment WindTunnel Simulations:Nearfield FlowfieldImaging and SurfaceThermography

P. Danehy, NASALangley ResearchCenter, Hampton, VA

1330AIAA-2010-1572 NumericalComputations ofHypersonic Boundary-Layer over SurfaceIrregularities

C. Chang, NASALangley ResearchCenter, Hampton, VA

1400AIAA-2010-1573 Simulations of High-Speed Flow Over anIsolated Roughness

S. Yoon, NASA AmesResearch Center,Moffett Field, CA

1430AIAA-2010-1574 Roughness- InducedInstability in a LaminarBoundary Layer at Mach6

B. Wheaton, PurdueUniversity, WestLafayette, IN

1500AIAA-2010-1575 LLaminar- TurbulentTransition behindDiscrete RoughnessElements in a High-Speed Boundary Layer

M. Choudhari, NASALangley ResearchCenter, Hampton, VA

1530AIAA-2010-1576 Experimental Studies ofSpace Shuttle OrbiterBoundary LayerTransition at MachNumbers from 10 to 18

T. Wadhams, CUBRC,Buffalo, NY

1600AIAA-2010-1577 Transition Induced byFence Geometries onShuttle Orbiter at Mach10

J. Everhart, NASALangley ResearchCenter, Hampton, VA

1630AIAA-2010-1578 Boundary LayerTransition ProtuberanceTests at NASA JSC Arc-Jet Facility

M. Larin, JacobsTechnology, Houston, TX

Chaired by: T. ASHWILL, Sandia National Laboratories, Albuquerque, NM, and C. CRAWFORD, University of Victoria, Victoria, Canada


Thursday Afternoon / 07 January 2010 Session 283-WE-8 Wind Turbine Design and Loads Crystal Ballroom G2

Thursday Afternoon / 07 January 2010 Session 284-WIG-9 / PDL-17 Plasma Kinetics and Surface Discharges Grand Ballroom 2

Chaired by: T. ASHWILL, Sandia National Laboratories, Albuquerque, NM, and C. CRAWFORD, University of Victoria, Victoria, Canada1300AIAA-2010-1579 The Influence of BladeCurvature and HelicalBlade Twist on thePerformance of aVertical- Axis WindTurbine

F. Scheurich, Universityof Glasgow, Glasgow,Great Britain

1330AIAA-2010-1580 Estimation of WindTurbine Blade Forceswith a State- AugmentedKalman Filter

J. Berg, New MexicoInstitute of Mining andTechnology, Socorro,NM

1400AIAA-2010-1581 Assessment of LoadExtrapolation Methodsfor Wind Turbines

H. Toft, AalborgUniversity, Aalborg,Denmark

1430AIAA-2010-1582 Development of theSweep- Twist AdaptiveRotor (STAR) Blade

T. Ashwill, SandiaNational Laboratories,Albuquerque, NM

1500AIAA-2010-1583 The Impact of AirfoilSelection on the Designof Small Horizontal AxisWind Turbines

B. Kanya, ClarksonUniversity, Potsdam, NY

1530AIAA-2010-1585 Experimental andNumerical Studies of aHigh Solidity, Low TipSpeed Ratio DAWT

M. Moeller, ClarksonUniversity, Potsdam, NY

Chaired by: S. LEONOV, Russian Academy of Sciences, Moscow, Russia, and J. TISHKOFF, U.S. Air Force Office of Scientific Research, Arlington, VA1300AIAA-2010-1586 Mechanisms of KineticCombustionEnhancement byO2(a1(delta)g)

T. Ombrello, U.S. AirForce ResearchLaboratory, PropulsionDirectorate,Wright-Patterson AFB,OH

1330AIAA-2010-1587 Surface Discharges:Possible Applications forPlasma- AssistedIgnition and ElectricField Measurements

S. Starikovskaia, ÉcolePolytechnique,Palaiseau Cedex,France

1400AIAA-2010-1588 Cracking of SelectedHydrocarbon Gases inLow- Power, Low-Pressure rf Plasma

C. Jiao, UES, Inc.,Dayton, OH

1430AIAA-2010-1589 On Pulsed Discharge inHumid Air

V. Bychkov, M.V.Lomonosov MoscowState University,Moscow, Russia

1500AIAA-2010-1590 Kinetics of Low-Temperature HydrogenOxidation and Ignitionby Repetitively PulsedNonequilibrium Plasmas

I. Choi, Ohio StateUniversity, Columbus,OH

1530AIAA-2010-1592 Discharges Over aSurface of LiquidHydrocarbons

V. Bychkov, M.V.Lomonosov MoscowState University,Moscow, Russia

1600AIAA-2010-1593 Kinetics of PlasmaAssisted Combustion atLow Reduced ElectricFields

A. Starikovskii, DrexelUniversity, Philadelphia,PA

Distinguished lecturers to speak at 48TH AIAA Ae 14/10/2011

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