-
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.
###
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/
[ | E-mail | Share ] AAAS and EurekAlert! are not responsible
for the accuracy of news releases posted to EurekAlert! by
contributing institutions or for the use of any information through
the EurekAlert! system.
Page 1 of 1Distinguished lecturers to speak at 48TH AIAA
Aerospace Sciences Meeting and Exp...
14/10/2011file://C:\Users\U1007825\Desktop\Distinguished
lecturers to speak at 48TH AIAA Ae...
-
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
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#session12746.
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
http://www.aiaa.org/agenda.cfm?lumeetingid=1812&dateget=all#session12746
-
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
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#session12876.
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
http://www.aiaa.org/agenda.cfm?lumeetingid=1812&dateget=all#session12876
-
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
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#session12961.
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
http://www.aiaa.org/agenda.cfm?lumeetingid=1812&dateget=all#session12961
-
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
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#session12832.
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
http://www.aiaa.org/agenda.cfm?lumeetingid=1812&dateget=all#session12832
-
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
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#session12718.
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
http://www.aiaa.org/agenda.cfm?lumeetingid=1812&dateget=all#session12718
-
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
-
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#session13018.
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
http://www.aiaa.org/agenda.cfm?lumeetingid=1812&dateget=all#session13018
-
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
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#session12812.
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
http://www.aiaa.org/agenda.cfm?lumeetingid=1812&dateget=all#session12812
-
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
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#session12506.
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
http://www.aiaa.org/agenda.cfm?lumeetingid=1812&dateget=all#session12506
-
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
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#session12887.
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
http://www.aiaa.org/agenda.cfm?lumeetingid=1812&dateget=all#session12887
-
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
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#session13013.
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
http://www.aiaa.org/agenda.cfm?lumeetingid=1812&dateget=all#session13013
-
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
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#session12849.
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
http://www.aiaa.org/agenda.cfm?lumeetingid=1812&dateget=all#session12849
-
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
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#session13131.
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
http://www.aiaa.org/agenda.cfm?lumeetingid=1812&dateget=all#session13131
-
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
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#session12687.
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
http://www.aiaa.org/agenda.cfm?lumeetingid=1812&dateget=all#session12687
-
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
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#session12767.
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
http://www.aiaa.org/agenda.cfm?lumeetingid=1812&dateget=all#session12767
-
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
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#session12878.
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)
http://www.aiaa.org/agenda.cfm?lumeetingid=1812&dateget=all#session12878
-
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
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#session12828.
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
http://www.aiaa.org/agenda.cfm?lumeetingid=1812&dateget=all#session12828
-
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
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#session12757.
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
http://www.aiaa.org/agenda.cfm?lumeetingid=1812&dateget=all#session12757
-
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
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#session12725.
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
http://www.aiaa.org/agenda.cfm?lumeetingid=1812&dateget=all#session12725
-
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
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#session12743.
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
http://www.aiaa.org/agenda.cfm?lumeetingid=1812&dateget=all#session12743
-
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 andExperimen