agenda

42nd AIAA Aerospace Sciences Meeting and Exhibit 5 - 8 Jan 2004 Grand Sierra Resort Hotel (Formerly Reno Hilton) Reno, Nevada

Monday Morning / 05 January 2004 Session 1-AA-1 Experimental Jet Aeroacoustics N7

Monday Morning / 05 January 2004 Session 2-AFM-1 Aerodynamic Prediction Methods Sierra 1

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=665&dateget=all#session2725.

Chaired by: D. PAPAMOSCHOU, University of California, Irvine, Irvine, CA0800AIAA-2004-0004 Mean Flow andAcoustics of Dual-Stream Jets

D. Papamoschou,University of California,Irvine, Irvine, CA

0830AIAA-2004-0005 Noise- and Flow- field ofJets from an EccentricCoannular Nozzle

K. Zaman, NASA GlennResearch Center,Brookpark, OH

0900AIAA-2004-0006 Acoustic Coupling ofTwin Jets from Single-Beveled Nozzles

P. Panickar, IllinoisInstitute of Technology,Chicago, IL

0930AIAA-2004-0007 Wind Tunnel Tests ofTurbofan ExhaustSystem Noise at CruiseConditions

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

1000AIAA-2004-0008 Effect of Nozzle InternalContour on JetAeroacoustics

K. Viswanathan, TheBoeing Company,Seattle, WA

1030AIAA-2004-0009 Acoustic Investigation ofa High Bypass RatioSeparate Flow ExhaustSystem with Chevrons

O. Rask, University ofCincinnati, Cincinnati,OH

1100AIAA-2004-0010 Designing an AnechoicChamber for theExperimental Study ofHigh Speed Heated Jets

C. Tinney, SyracuseUniversity, Syracuse, NY

1130AIAA-2004-0011 The Effect of MicrojetControl onAeroacoustics ofSupersonic Twin Jets

M. Alkislar, Florida A&MUniversity and FloridaState University,Tallahassee, FL

Chaired by: F. PRIOLO, Millennium Engineering and Integration Company, Arlington, VA0800AIAA-2004-0012 Lifting- Line Estimationfor the Contribution of aConventional Tail toAircraft Lateral StabilityDerivatives

E. Anderson, Utah StateUniversity, Logan, UT

0830AIAA-2004-0013 Accelerating CFD-Based Flight Mechanicsand Aeroelastic AnalysisUsing DistributedProcessing

A. Boeckman,Oklahoma StateUniversity, Stillwater, OK

0900AIAA-2004-0014 Navier- StokesComputations ofStability Derivatives forSymmetric Projectiles

S. Park, KoreaAdvanced Institute ofScience andTechnology, Daejeon,South Korea

0930AIAA-2004-0015 Computational Methodsfor Dynamic Stabilityand Control Derivatives

L. Green, NASA LangleyResearch Center,Hampton, VA

1000AIAA-2004-0016 An Approximate Methodto Estimate WingTrailing- Edge BluntnessEffects on Normal Force

F. Moore, AeropredictionInc., King George, VA

Chaired by: G. ELLIOTT, University of Illinois at Urbana-Champaign, Urbana, IL0800 0830 0900 0930 1000 1030 1100 1130

http://www.aiaa.org/agenda.cfm?lumeetingid=665&dateget=all#session2725

Monday Morning / 05 January 2004 Session 3-AMT-1 Velocimetry and Property Measurement Shasta 1

Monday Morning / 05 January 2004 Session 4-APA-1 Aerodynamic Design I Carson 1

Monday Morning / 05 January 2004 Session 5-APA-2 Flight Vehicle Aerodynamics Carson 2


Chaired by: G. ELLIOTT, University of Illinois at Urbana-Champaign, Urbana, IL0800AIAA-2004-0017 Bulk ViscosityMeasurements UsingCoherent Rayleigh-Brillouin Scattering

X. Pan, PrincetonUniversity, Princeton, NJ

0830AIAA-2004-0018 Measurements in FluidFlows Using MolecularFilter- based Techniques

M. Boguszko, Universityof Illinois atUrbana-Champagne,Urbana, IL

0900AIAA-2004-0019 Development of aMOPA Source forModulated FilteredRayleigh ScatteringVelocimetry

J. Jagodzinski,University of Texas atAustin, Austin, TX

0930AIAA-2004-0020 Design andDevelopment of aPulsed, NarrowLinewidth UV Source forFlow Dianostics

L. Qian, PrincetonUniversity, Princeton, NJ

1000AIAA-2004-0021 Filtered RayleighScattering Velocimetry –Accuracy Investigationin a M=2.22Axisymmetric Jet

J. Gustavsson,University of Florida,Gainesville, FL

1030AIAA-2004-0022 Planar Particle ImagingDoppler Velocimetry, A3- Component VelocityMeasurement Technique

M. Wernet, NASA GlennResearch Center,Cleveland, OH

1100AIAA-2004-0023 MHz Rate PlanarDoppler Velocimetry inSupersonic Jets

B. Thurow, Ohio StateUniversity, Columbus,OH

1130AIAA-2004-1358 Filtered RayleighScattering Thermometryin Vortex- Strained andSooting Flames

S. Kearney, SandiaNational Laboratories,Albuquerque, NM

Chaired by: S. MORRIS, Engineering Systems Inc, Colorado Springs, CO0800AIAA-2004-0025 Automated DesignOptimization of aSubsonic SubmergedInlet

E. Taskinoglu, RutgersUniversity, Piscataway,NJ

0830AIAA-2004-0026 Design of Three-dimensonal NozzleShapes Using HybridOptimization Techniques

X. Xing, NanyangTechnologicalUniversity, Singapore,Singapore

0900AIAA-2004-0027 Aerodynamic Design of3D Compressor BladeUsing an Adjoint Method

J. Chung, University ofIllinois atUrbana-Champaign,Urbana, IL

0930AIAA-2004-0028 Inverse Design ofAdaptive Airfoils withAircraft PerformanceConsiderations

J. Jepson, NorthCarolina StateUniversity, Raleigh, NC

1000AIAA-2004-0029 Aero- Structural WingPlanform Optimization

K. Leoviriyakit, StanfordUniversity, Stanford, CA

1030AIAA-2004-0031 Aero- Thermodynamicsfor Conceptual Design

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

1100AIAA-2004-0032 Optimal Gas GeneratorDesign for the LiquidRocket Engine

K. Jeon, KonkukUniversity, Seoul, SouthKorea

Chaired by: S. BAUER, NASA Langley Research Center, Hampton, VA0800AIAA-2004-0034 AerodynamicOptimization of NEXST-1 SST Model at Near-Sonic Regime

W. Yamazaki, TohokuUniversity, Sendai,Japan

0830AIAA-2004-0035 Experimental/ComputationalInvestigation of DragReduction by Electric- ArcAirspikes at Mach 10

C. Hartley, RensselaerPolytechnic Institute, Troy,NY

0900AIAA-2004-0037 Nose Bluntness for SideForce Control onCircular Cones at HighIncidence

R. Kumar, NationalAerospace Laboratories,Bangalore, India

0930AIAA-2004-0038 Induced Drag of High-Aspect Ratio Wings

T. Chen, San DiegoState University, SanDiego, CA

1000AIAA-2004-0039 A Parallel, Object-Oriented UnsteadyVortex Lattice Methodfor Flapping Flight

T. Fritz, PennsylvaniaState University,University Park, PA

1030AIAA-2004-1378 CFD Analysis ofAerodynamicInterference Between aDelta Wing and aHemisphere- Cylinder

K. Kitamura, NagoyaUniv., Nagoya, Japan

Chaired by: B. ROSEN, Northrop Grumman Integrated Systems, Bethpage, NY0800 0830 0900 0930 1000 1030


Monday Morning / 05 January 2004 Session 6-APA-3 Rotorcraft/Propeller Aerodynamics Crystal 1

Monday Morning / 05 January 2004 Session 7-APA-4 Unsteady Aerodynamics Crystal 2

Monday Morning / 05 January 2004 Session 8-ASE-1 Ice Physics and Thermal IPS N5


Chaired by: B. ROSEN, Northrop Grumman Integrated Systems, Bethpage, NY0800AIAA-2004-0041 Compressible DynamicStall Performance of aVariable Droop LeadingEdge Airfoil with aGurney Flap

M. Chandrasekhara,Naval PostgraduateSchool, Monterey, CA

0830AIAA-2004-0043 Development ofComputational Sensingand Active Flow Controlof Airfoils DuringDynamic Stall

O. Kandil, Old DominionUniversity, Norfolk, VA

0900AIAA-2004-0044 Effects of Synthetic JetActuation on a PitchingNACA 0015 Airfoil

L. Traub, Texas A&MUniversity, CollegeStation, TX

0930AIAA-2004-0045 The Application of Air-Jet Vortex Generators toSuppress FlowSeparation on HelicopterAerofoil Sections UnderQuasi- Steady andUnsteady Conditions

C. Singh, CityUniversity, London,Great Britain

1000AIAA-2004-0046 Comparison of Rotor-Airframe InteractionUtilizing Overset andUnstructured GridTechniques

S. Ruffin, GeorgiaInstitute of Technology,Atlanta, GA

1030AIAA-2004-0048 Discrete Blade CFDAnalysis of Ducted TailFan Flow

G. Ruzicka, NASAAmes Research Center,Moffett Field, CA

Chaired by: C. NELSON, Sverdrup Technology, Inc., Arnold AFB, TN0800AIAA-2004-0049 Unsteady Shock Motionon a NACA0012 Aerofoilat Low ReducedFrequencies

R. Fernie, University ofCambridge, Cambridge,Great Britain

0830AIAA-2004-0050 Low- Reynolds- NumberUnsteady TurbulentFlows Past OscillatingWings at Angles ofAttack Near Stall

W. Yuan, NationalResearch Council,Ottawa, Canada

0900AIAA-2004-0051 ComputationalModelling of TransientBlast Wave Effects

G. Kidd, Thales AirDefence Ltd., Belfast,Northern Ireland

0930AIAA-2004-0052 Towards NumericalModeling of CoupledVSTOL- Ship AirwakeFlowfields

S. Arunajatesan,CRAFT Tech,Pipersville, PA

1000AIAA-2004-0053 Hybrid RANS/LESSimulation of DeepCavity Flow

K. Chang, KoreaAdvanced Institute ofScience andTechnology, Daejon,South Korea

1030AIAA-2004-0054 A CFD Analysis ofSudden CockpitDecompression

C. Breard, AnalyticalMethods Inc., Redmond,WA

1100AIAA-2004-0055 Unsteady Reynolds-Averaged Navier-Stokes Predictions ofthe Flow Around aProlate Spheroid

N. Scott, NorthernArizona University,Flagstaff, AZ

1130AIAA-2004-0056 ComputationalEvaluation of the Steadyand Pulsed Jet Effectson the Performance of aCirculation Control WingSection

Y. Liu, Georgia Tech,Atlanta, GA

Chaired by: M. POLITOVICH, National Center for Atmospheric Research, Boulder, CO0800AIAA-2004-0057 Residual DropletImpacts and Thin FilmDynamics

A. Rothmayer, IowaState University, Ames,IA

0830AIAA-2004-0058 Impact of SurfaceRoughness on LocalAerodynamics Using aThree- DimensionalNavier- Stokes Solver

B. Matheis, Iowa StateUniversity, Ames, IA

0900AIAA-2004-0059 The Effects of Leading-Edge Ice Roughness onDownstream FrostFormation

E. Ogretim, WestVirginia University,Morgantown, WV

0930AIAA-2004-0062 An Evaluation of JetImpingement HeatTransfer Correlations forPiccolo Tube Application

W. Wright, QSS GroupInc., Cleveland, OH

1000AIAA-2004-0063 Surface Heat TransferStudy for Ice Accretionand Anti- icingPrediction in ThreeDimension

M. Fregeau, EcolePolytechnique deMontreal, Montreal,Canada


Monday Morning / 05 January 2004 Session 9-ETM-10800 - The Delta Forum: Designing and Integrating 21st Century Systems N10

Monday Morning / 05 January 2004 Session 10-FD-1 Applications of Hybrid Predictive Strategies Sierra 2

Monday Morning / 05 January 2004 Session 11-FD-2 CFD Methods I Carson 4


Chaired by: T. HOWARD, Raytheon, Lanham, MD0800 - Introduction of Topic, T. Gross, NASA Ames0805 - Society as a System - What are the Needs?, T. Howard, Raytheon ITSS0820 - What is a 21st Century System, M. Maier0840 - Optimizing the Design & Integration of the 21st Century System, R. Canfield, Air Force Institute of Technology0900 - Using Knowledge Management to Improve Design Results, J. Rocker, NASA Langley0920 - Policy Drivers for Systems Integration - How is the Law Changing our Industry?0940 - Case Studies for Cost Savings in Systems Integration, P. Collopy1000 - IP Issues in the Integration Environment: Teams and Partners, S. Johnson, McKee, Voorhees & Sease1020 - Managing for Integration, J. Afarin, NASA Glenn1040 - Panel Discussion

Chaired by: R. JOSLIN, Office of Naval Research, Arlington, VA, and C. FUREBY, Swedish Defence Research Agency, Stockholm, Sweden0800AIAA-2004-0065 DES and RANS ofUnsteady Free- SurfaceWave InducedSeparation

T. Xing, University ofIowa, Iowa City, IA

0830AIAA-2004-0066 Detached EddySimulation ofSupersonic Base Flowwith Bleed

P. Subbareddy,University of Minnesota,Minneapolis, MN

0900AIAA-2004-0067 Application of a newFlow SimulationMethodology forSupersonicAxisymmetric Wakes

R. Sandberg, Universityof Arizona, Tucson, AZ

0930AIAA-2004-0068 Computational Study ofa Supersonic Base FlowUsing LES/RANS HybridMethodology

S. Kawai, University ofTokyo, Tokyo, Japan

1000AIAA-2004-0071 Hybrid MILES- RANSMethod for moreDissipative Solvers andthe use of Non- linearLES

P. Tucker, University ofWarwick, Coventry,Great Britain

1030AIAA-2004-0072 VLES Study of ShipStack Gas Dynamics

F. Camelli, GeorgeMason University,Fairfax, VA

Chaired by: A. HASSAN, The Boeing Company, Mesa, AZ, and D. BUCKWALTER, Air Force Research Laboratory, Wright-Patterson AFB, OH0800AIAA-2004-0075 Solving the Navier-Stokes Equaitons by theCESE Method

M. Zhang, Ohio StateUniversity, Columbus,OH

0830AIAA-2004-0076 An Alternative to Limiterin DiscontinousGalerrkin Finite ElementMethod for Simulation ofCompressible Flows

S. Aliabadi, ClarkAtlanta University,Atlanta, GA

0900AIAA-2004-0077 Simulation of AircraftWake Vortex UsingPressure- Based UnifiedNumerical Approach forIncompressible andCompressible Flows

Y. Yamaguchi, HondaR&D Co Ltd, Wako,Japan

0930AIAA-2004-0078 Application of "TimeLimiters" in theNumerical Solution ofUnsteady AerodynamicEquations

K. Duraisamy, Universityof Maryland, CollegePark, MD

1000AIAA-2004-0080 A Non- Body ConformalGrid Method forSimulation ofCompressible Flows withComplex ImmersedBoundaries

R. Ghias, GeorgeWashington University,Washington, DC

Chaired by: R. MELVILLE, Air Force Research Laboratory, Wright-Patterson AFB, OH, and P. ORKWIS, University of Cincinnati, Cincinnati, OH


Monday Morning / 05 January 2004 Session 12-FD-3 Grid Adaptation Carson 4

Monday Morning / 05 January 2004 Session 13-FD-4 Pulsed and Synthetic Jet Actuators Crystal 3

Monday Morning / 05 January 2004 Session 14-FD-5 Subsonic Transition Crystal 4


Chaired by: R. MELVILLE, Air Force Research Laboratory, Wright-Patterson AFB, OH, and P. ORKWIS, University of Cincinnati, Cincinnati, OH0800AIAA-2004-0082 The Level Set Methodon Adaptive CartesianGrid for InterfaceCapturing

Z. Wang, Michigan StateUniversity, East Lansing,MI

0830AIAA-2004-0083 Advances in AdaptiveEmbedded UnstructuredGrid Methods

R. Lohner, GeorgeMason University,Fairfax, VA

0900AIAA-2004-0084 Efficient AnisotropicMesh Adaptation onWeak and MultipleShocks

L. Remaki, McGILLUniversity, Montreal,Canada

0930AIAA-2004-0085 Automatic CADReconstruction for CAD-Based Anisotropic MeshSmoothing andAdaptation

P. Lagace, NewmericalTechnologiesInternational, Montreal,Canada

1000AIAA-2004-0088 Adaptive Mesh Strategyfor Unstructured Gridson Multi- MechanicsInfrastructure

W. Tauber, SandiaNational Laboratories,Livermore, CA

Chaired by: D. SMITH, University of Wyoming, Laramie, WY, and D. WILLIAMS, Illinois Institute of Technology, Chicago, IL0800AIAA-2004-0089 Characterization ofSparkJet Actuators forFlow Control

K. Grossman, JohnsHopkins UniversityApplied PhysicsLaboratory, Laurel, MD

0830AIAA-2004-0090 A Study of theFormation and Scalingof a Synthetic Jet

J. Shuster, University ofWyoming, Laramie, WY

0900AIAA-2004-0091 Study of Three-Dimensional SyntheticJet Flowfields UsingDirect- NumericalSimulation

R. Byrganhalli, GeorgeWashington University,Washington, DC

0930AIAA-2004-0092 An ExperimentalInvestigation ofUnsteady ThrustAugmentation Using aSpeaker- Driven Jet

D. Paxson, NASA GlennResearch Center,Cleveland, OH

1000AIAA-2004-0093 Interaction of SyntheticJet Propulsion with WingAerodynamics at LowReynolds Numbers

J. Whitehead, Universityof Bath, Bath, GreatBritain

1030AIAA-2004-0095 Mixing and FrequencyAnalysis of a Forced Jetin Cross Flow

T. Barber, University ofConnecticut, Storrs, CT

1100AIAA-2004-0096 Vorticity Formulation foran Actuated Jet inCrossflow

Y. Marzouk,Massachusetts Instituteof Technology,Cambridge, MA

Chaired by: H. REED, Arizona State University, Tempe, AZ, and S. SCHNEIDER, Purdue University, West Lafayette, IN0800AIAA-2004-0097 Numerical-ExperimentalComparisons ofSecond- Mode Behaviorfor Blunted Cones

I. Lyttle, SchneiderElectric, Cedar Rapids,IA

0830AIAA-2004-0098 On the Calculation ofInitial Conditions forParabolized StabilityEquations for PredictingTransition

T. Cebeci, The BoeingCompany, Long Beach,CA

0900AIAA-2004-0099 Relaminarization onSwept Leading EdgesUnder High- LiftConditions

P. Viswanath, NationalAerospace Laboratories,Bangalore, India

0930AIAA-2004-0100 Numerical Calculation ofthe Transitional Flowover a Hydrofoil

F. Liu, University ofMichigan, Kalamazoo,MI

1000AIAA-2004-0101 The Problem ofBoundary Layer FlowEncountering a Three-dimensional HumpRevisited

A. Tumin, University ofArizona, Tucson, AZ

1030AIAA-2004-0102 Bifurcation and Stabilityof Near- criticalCompressible SwirlingFlows

J. Lee, RensselaerPolytechnic Institute,Troy, NY

1100AIAA-2004-0103 Numerical Simulationsof Transitional Flows asAffected by PassingWakes

Y. Suzen, University ofKentucky, Lexington, KY

Chaired by: F. ROOS, The Boeing Company, Saint Louis, MO


Monday Morning / 05 January 2004 Session 15-HIS-1 History of Aeronautics McKinley

Monday Morning / 05 January 2004 Session 16-MDO-1 Sensitivity and Approximation Methods N9

Monday Morning / 05 January 2004 Session 17-MSSP-1 Current Trends in Microgravity and Space Processing N6


Chaired by: F. ROOS, The Boeing Company, Saint Louis, MO0800AIAA-2004-0104 Predicted FlightPerformance of theWright 'Flyer" Based onFull- Scale Tunnel Data

C. Britcher, OldDominion University,Norfolk, VA

0830AIAA-2004-0105 Flying Qualities of theWright 1903 Flyer: FromSimulation to Flight Test

K. Kochersberger,Rochester Institute ofTechnology, Rochester,NY

0900AIAA-2004-0106 Santos Dumont and theDawn of Aviation

B. Mattos, EmpresaBrasileira deAeronáutica, Sao JoseDos Campos, Brazil

0930AIAA-2004-0107 High- SpeedAerodynamic Researchat the NACA/NASALangley ResearchCenter

M. Spearman, NASALangley ResearchCenter, Hampton, VA

1000AIAA-2004-0108 Some NASAAerodynamic ResearchRelated to ForeignSystems

M. Spearman, NASALangley ResearchCenter, Hampton, VA

Chaired by: J. RENAUD, University of Notre Dame, Notre Dame, IN, and C. MATTSON, Rensselaer Polytechnic Institute, Troy, NY0800AIAA-2004-0111 Low ComplexityOptimization of aSupersonic CivilTransport

B. Mohammadi,University Montpellier II,Montpellier, France

0830AIAA-2004-0112 On the BoundaryComputation of FlowSensitivities

O. Soto, George MasonUniversity, Fairfax, VA

0900AIAA-2004-0113 CAD- BasedAerodynamic Design ofComplex ConfigurationsUsing a CartesianMethod

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

0930AIAA-2004-0114 Post Optimality Analysisfor MultidisciplinarySystems Using aCumulative ResponseSurface Approximation

P. Chandila, Universityof Notre Dame, NotreDame, IN

1000AIAA-2004-0115 Robust Design ofCoupled Sub- SystemsUsing Visualization

D. Kanukolanu,University at Buffalo,Buffalo, NY

1030AIAA-2004-0116 Parametric MeshDeformation andSensitivity Analysis forDesign of a Joined-Wing Aircraft

J. Hur, Air ForceResearch Laboratory,Wright-Patterson AFB,OH

1100AIAA-2004-0118 Efficient OptimizationDesign Method UsingKriging Model

S. Jeong, JapanAerospace ExplorationAgency, Tokyo, Japan

Chaired by: F. KOHL, NASA Glenn Research Center, Cleveland, OH, and A. WHITAKER, NASA Marshall Space Flight Center, Huntsville, AL0800AIAA-2004-0119 NASA's PhysicalSciences ResearchProgram

E. Trinh, NASAHeadquarters,Washington, DC

0830AIAA-2004-0120 Meeting NASA'sMission ThroughCommercial Partnerships

M. Nall, NASA MarshallSpace Flight Center,Huntsville, AL

0900AIAA-2004-0121 The Canadian SpaceAgency MicrogravityScience ProgramOverview

C. Casgrain, CanadianSpace Agency,St-Hubert, Canada

0930AIAA-2004-0122 Status of the ProjectResearch in the NASDAMicrogravity ScienceProgram

A. Komiya, NationalSpace DevelopmentAgency, Tsukuba, Japan

1000AIAA-2004-0123 NASA's MicrogravityFluid Physics StrategicResearch Roadmap

B. Motil, NASA GlennResearch Center,Cleveland, OH

1030AIAA-2004-0124 Strategic ResearchDirections inMicrogravity MaterialsScience

R. Clinton, NASAMarshall Space FlightCenter, Huntsville, AL

1100AIAA-2004-0125 MicrogravityEnvironment on theInternational SpaceStation

R. DeLombard, NASAGlenn, Cleveland, OH

1130AIAA-2004-0126 An Overview of theGravity Probe B Mission

R. Geveden, NASAMarshall Space FlightCenter, Huntsville, AL

Chaired by: R. CUMMINGS, Cal Poly, San Luis Obispo, CA0800 0830 0900 0930 1000 1030


Monday Morning / 05 January 2004 Session 18-NSC-1 AIAA Foundation National Student Conference- Undergraduate Division Crystal 5

Monday Morning / 05 January 2004 Session 19-PC-1 Gas Turbine Combustion Cascade 1

Monday Morning / 05 January 2004 Session 20-PC-2 Laminar Flames Cascade 2


Chaired by: R. CUMMINGS, Cal Poly, San Luis Obispo, CA0800AIAA-2004-0127 Analysis of a Near-Vacuum Hall Thruster

T. Pigeon,Massachusetts Instituteof Technology,Cambridge, MA

0830AIAA-2004-0128 Flight Dynamics andControl of an Aircraftwith Segmented ControlSurfaces

M. Abdulrahim,University of Florida,Gainesville, FL

0900AIAA-2004-0129 A Comparison Study ofRectangular andChamfered IsolatorCross- Sectional Shapewith Varied Divergence

K. Grendell, Universityof Cincinnati, Cincinnati,OH

0930AIAA-2004-0130 Supercavitation andAerospace Technologyin the Development ofHigh- Speed UnderwaterVehicles

J. Hargrove, Texas A&MUniversity, CollegeStation, TX

1000AIAA-2004-0131 Drag Reduction andControl UsingEnergetics andElectrostatic Force-Fields for HypersonicApplications

T. Taylor, University ofMissouri - Rolla, Rolla,MO

1030AIAA-2004-0132 Preliminary DynamicSoaring Research UsingA Radio Control Glider

J. Parle, University ofSouthern California, LosAngeles, CA

Chaired by: A. AGRAWAL, University of Oklahoma, Norman, OK, and R. TACINA, NASA Glenn Research Center, Cleveland, OH0800AIAA-2004-0133 Experimental Study ofLarge CoherentStructure in MultipleSwirler Combustor

G. Li, University ofCincinnati, Cincinnati,OH

0830AIAA-2004-0134 Spray and Fuel- AirMixing of theSwirler/Venturi Injectorsfor Lean PremixedPrevaporized Combustor

K. Im, Wayne StateUniversity, Detroit, MI

0900AIAA-2004-0135 ExperimentalInvestigation of aMultiplex Fuel InjectorModule with Discrete JetSwirlers for LowEmission Combustors

R. Tacina, NASA GlennResearch Center,Cleveland, OH

0930AIAA-2004-0136 Detailed Characteristicsof Drop- Laden MixingLayers: LES PredictionsCompared to DNS

N. Okong'o, JetPropulsion Laboratory,Pasadena, CA

1000AIAA-2004-0137 Swirl Cup Modeling -Part IX: LiquidAtomization Modeling

S. Jeng, University ofCincinnati, Cincinnati,OH

1030AIAA-2004-0138 Lean Blowout Detectionin a Single NozzleCFM56 Swirl Cup

S. Nair, Georgia Tech,Atlanta, GA

1100AIAA-2004-0139 Numerical Modeling ofEvaporation Process inPorous Media for GasTurbine Applications

C. Periasamy, Universityof Oklahoma, Norman,OK

1130AIAA-2004-0140 Combustor Developmentfor Dual Fuel with GasOil and BiomassGasification Products

C. Syred, CardiffUniversity, Cardiff, GreatBritain

Chaired by: J. BUCKMASTER, University of Illinois at Urbana-Champaign, Urbana, IL, and W. ROBERTS, North Carolina State University, Raleigh, NC0800AIAA-2004-0141 Lift- off Behavior andFlame Structure ofInteracting Edge Flames

A. Wason, University ofConnecticut, Storrs, CT

0830AIAA-2004-0143 Determination ofLaminar Flame Speedsof Primary ReferenceFuel and Reformer GasMixtures Using DigitalParticle ImageVelocimetry

Y. Huang, CaseWestern ReserveUniversity, Cleveland,OH

0900AIAA-2004-0144 Oxygen- Enhanced HighTemperature LaminarFlames

Z. Cheng, VanderbiltUniversity, Nashville, TN

0930AIAA-2004-0145 Fuel Effects on NOxEmissions in PartiallyPremixed Flames

S. Aggarwal, Universityof Illinois at Chicago,Chicago, IL

1000AIAA-2004-0146 A Study of the Effects ofAir and Fuel Dilution onNitric Oxide Emissionsfrom Gas Jet DiffusionFlames

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

1030AIAA-2004-0147 An Experimental Studyon Buoyancy- InducedLow Stretch GaseousDiffusion Flames

B. Han, Case WesternReserve University,Cleveland, OH

1100AIAA-2004-0148 Stretch and CurvatureEffects on Flames

P. Wang, VanderbiltUniversity, Nashville, TN


Monday Morning / 05 January 2004 Session 21-PDL-1 Laser & Plasma Propulsion N8

Monday Morning / 05 January 2004 Session 22-TES-1 Comprehensive Combustion Modeling I N4

Monday Morning / 05 January 2004 Session 23-TP-1 Phase Change Heat Transfer Shasta 2


Chaired by: C. LAUX, Stanford University, Stanford, CA0800AIAA-2004-0149 The Vasimr Engine:Project Status andRecentAccomplishments

F. Chang Díaz, NASAJohnson Space Center,Houston, TX

0830AIAA-2004-0150 Velocity Phase SpaceStudies of Ion Dynamicsin the Vasimr Engine

E. Bering, University ofHouston, Houston, TX

0900AIAA-2004-0151 Simulation of ICRFPlasma Heating in theVASIMR Experiment

A. Ilin, NASA JohnsonSpace Center, Houston,TX

0930AIAA-2004-0154 Simulation of PlasmaExpansion Using a Two-Timescale AcceleratedParticle- In- Cell Method

M. Gibbons, ERC Inc.,Edwards AFB, CA

1000AIAA-2004-0155 Verification of SSM HallThruster Plume ModelConsidering the ElectricPlasma Processes

A. Korsun, TsNIIMASH,Korolev, Russia

1030AIAA-2004-1372 Flightweight Magnets forAdvanced Power andPropulsion Applications

J. Chapman, LyTec LLC,Tullahoma, TN

Chaired by: N. LIU and J. MODER, NASA Glenn Research Center, Cleveland, OH0800AIAA-2004-0156 Perspective of Combustion Modeling for GasTurbine Combustors

H. Mongia, GE Aircraft Engines, Cincinnati, OH

0900AIAA-2004-0157 Multi- Scale Modeling for LES of EngineeringDesigns of Large- Scale Combustors

S. Menon, Georgia Institute of Technology,Atlanta, GA

1000AIAA-2004-0159 Simulation ofCombustion andThermophysics inPractical PropulsionSystems

J. Oefelein, SandiaNational Laboratories,Livermore, CA

1030AIAA-2004-0160 From RANS TowardsLES for EngineTurbulent Flows

T. Shih, Ohio AerospaceInstitute, Cleveland, OH

Chaired by: J. OCHTERBECK, Clemson University, Clemson, SC, and E. SHORT, Raytheon, McKinney, TX0800AIAA-2004-0161 Numerical Model forBoiling Liquid VaporExplosion (BLEVE)

G. Pinhasi, College ofJudea and Samaria,Ariel, Israel

0830AIAA-2004-0162 Capillary Condensationon Micro- groovedSurfaces

C. Li, RensselaerPolytechnic Institute,Troy, NY

0900AIAA-2004-0164 Frost Formation andHeat Transfer on a ColdSurface in Ice Fog

P. Mago, MississippiState University,Mississippi State, MS

0930AIAA-2004-0165 Revisiting Hydrodynamicand Physico- ChemicalNature of Burnout inHigh Heat- Flux Boiling

N. Dinh, University ofCalifornia SantaBarbara, Goleta, CA

1000AIAA-2004-0166 Modeling ofHomogeneous WaterCondensation in RocketPlumes with a KineticApproach

J. Zhong, PennsylvaniaState University,University Park, PA

1030AIAA-2004-0167 Application of HeatBalance Integral Methodto Droplet Freezing inMelting Ablation

T. Zien, Naval SurfaceWarfare Center,Dahlgren, VA

1100AIAA-2004-0168 Two Phase RefrigerantFlow Through AdiabaticCapillary Tubes:Evaluation of TwoPhase ViscosityCorrelations and FrictionFactor Correlations onHomogenous ModelPrediction for R22 andR134a

B. Chandra, IndianInstitute of Technology,Guwahati, India


Monday Morning / 05 January 2004 Session 25-WIG-1 Plasma Discharge Physics I Teton

Monday Morning / 05 January 2004 Session 24-WE-1 Structures, Materials, and Fatigue Ruby

Monday Morning / 05 January 2004 1200 - 1400 Capability Based Research: New Horizons for Aeronautics Silver State Pavilion


Chaired by: D. VAN WIE, Johns Hopkins University, Applied Physics Laboratory, Laural, MD, and S. SURZHIKOV, Institute Problems in Mechanics, Moscow, Russia0800AIAA-2004-0177 Numerical Simulation ofGlow Discharges forHigh- Speed FlowControl

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

0830AIAA-2004-0178 To the Theory ofTransversal DirectCurrent Discharge inHigh Pressure GasSupersonic Flow

V. Chernikov, MoscowState University,Moscow, Russia

0900AIAA-2004-0179 Plasma Jet Generatorswith Divergent Nozzlesfor AerodynamicApplications

N. Ardelyan, MoscowState University,Moscow, Russia

0930AIAA-2004-0180 The Physical Basis ofthe High Ability of theStreamer MW Dischargeto a ResonantAbsorption of MWRadiation

K. Khodataev, RussianAcademy of Sciences,Moscow, Russia

1000AIAA-2004-0181 ExperimentalDetermination of theMicrowave FieldThreshold ParametersInsuring Realization of aStreamer Discharge ofthe High TemperatureForm

V. Bychkov, RussianAcademy of Sciences,Moscow, Russia

1030AIAA-2004-0182 Absolute H AtomDensity Measurement inShort Pulse MethaneDischarge

J. Parish, Air ForceResearch Laboratory,Wright-Patterson AFB,OH

1100AIAA-2004-0183 E- Beam Plasmas 2- Dand 3- D Analysis inMHD Applications

V. Soloviev, MoscowInstitute of Physics andTechnology, Moscow,Russia

Chaired by: T. ASHWILL, Sandia National Laboratories, Albuquerque, NM0830AIAA-2004-0169 Development ofPrototype Carbon-Fiberglass Wind TurbineBlades: Conventionaland Twist- CoupledDesigns

D. Griffin, Global EnergyConcepts LLC, Kirkland,WA

0900AIAA-2004-0170 Uncoupled and Twist-Bend Coupled Carbon-Glass Blades for theLIST Turbine

K. Wetzel, K. Wetzel &Co. Inc., Lawrence, KS

0930AIAA-2004-0171 Reducing Distortion inSimulated Injection-Molded Wind TurbineBlades

J. Tester, NorthernArizona University,Flagstaff, AZ

1000AIAA-2004-0172 Effect of Mean Stress onthe Damage of WindTurbine Blades

H. Sutherland, SandiaNational Laboratories,Albuquerque, NM

1030AIAA-2004-0173 The Effect of LoadPhase Angle on WindTurbine Blade FatigueDamage

D. White, NationalRenewable EnergyLaboratory, Golden, CO

1100AIAA-2004-0174 Compression Strength ofCarbon Fiber LaminatesContaining Flaws withFiber Waviness

D. Avery, Montana StateUniversity, Bozeman, MT

AIAA is pleased to host a special luncheon with Richard Wlezien, Vehicle Systems Manager, NASA Headquarters, Washington, DC. Richard Wlezien will discuss his vision for future NASA air vehicle systemsprograms. Make plans early as the first 800 attendees will receive complimentary boxed lunches.

Chaired by: J. HILEMAN, Ohio State University, Columbus, OH1400 1430 1500 1530 1600 1630 1700 1730


Monday Afternoon / 05 January 2004 Session 26-AA-2 Jet Noise Control N7

Monday Afternoon / 05 January 2004 Session 27-ABP-1 Turbomachinery High Cycle Fatigue Whitney

Monday Afternoon / 05 January 2004 Session 28-AEE-1 Advanced Engineering Environment I McKinley


Chaired by: J. HILEMAN, Ohio State University, Columbus, OH1400AIAA-2004-0184 Development andApplication of LocalizedArc Filament PlasmaActuators for Jet Flowand Noise Control

M. Samimy, Ohio StateUniversity, Columbus,OH

1430AIAA-2004-0185 Jet Noise Reduction bya Microjet on theCenterline of thePrimary Jet

J. Kim, Seoul NationalUniversity, Seoul, SouthKorea

1500AIAA-2004-0186 Exploring High- SpeedAxisymmetric Jet NoiseControl Using HartmannTube Fluidic Actuators

J. Kastner, Ohio StateUniversity, Columbus,OH

1530AIAA-2004-0187 Turbofan Jet NoiseReduction via Deflectionof the Bypass Stream


1600AIAA-2004-0188 Engine Validation ofNoise ReductionConcepts - SeparateFlow Nozzles

D. Weir, HoneywellEngines Systems andServices, Phoenix, AZ

1630AIAA-2004-0190 Subsonic Jet NoiseReduction VariableGeometry Chevron

F. Calkins, The BoeingCompany, Seattle, WA

1700AIAA-2004-0189 Mean Flow and NoisePrediction for aSeparate Flow Jet withChevron Mixers

L. Koch, NASA GlennResearch Center,Cleveland, OH

1730AIAA-2004-0191 A PIV Flow FieldInvestigation of ChevronNozzle Mechanisms

B. Callender, Universityof Cincinnati, Cincinnati,OH

Chaired by: M. WOLFF, Wright State University, Dayton, OH, and W. ENGBLOM, NASA Glenn Research Center, Cleveland, OH1400AIAA-2004-0192 Computation ofUncoupled and CoupledAeroelasticity of Three-Dimensional Blade Rows

M. Sadeghi, Universityof California, Irvine,Irvine, CA

1430AIAA-2004-0193 Finite ElementSimulation ofTurbomachine BladeRow ViscousInteractions – VaneVibratory StressPredictions

R. Kishore , PurdueUniversity, WestLafayette, IN

1500AIAA-2004-0195 A Study of ImpulseForcing on a SimplySupported Blade

T. Krausse, OklahomaState University,Stillwater, OK

1530AIAA-2004-0196 HCF Performance andFOD ToleranceImprovement in Ti- 6Al-4V Vane with LPBTreatment

P. Prevey, LambdaResearch, Cincinnati,OH

1600AIAA-2004-0197 Tip Clearance Effects onTransonic IGV/RotorInteractions

X. Zhou, Wright StateUniversity, Dayton, OH

1630AIAA-2004-0198 Steady Viscous FlowSolution of aTurbomachine Cascade

Q. Zhang, University ofKentucky, Paducah, KY

1700AIAA-2004-0199 Numerical Study onFlow Separation of aTransonic Cascade

Z. Hu, University ofMiami, Coral Gables, FL

Chaired by: J. MAPAR, Science Applications International Corporation, McLean, VA1400AIAA-2004-0202 The AdvancedEngineeringEnvironment (AEE)Project for NASA’s NextGeneration LaunchTechnologies (NGLT)Program

D. Monell, NASAMarshall Space FlightCenter, Huntsville, AL

1430AIAA-2004-0203 A OneNASAFramework: The VirtualSystem DesignEnvironment

J. Medina, NASAGoddard Space FlightCenter, Greenbelt, MD

1500AIAA-2004-0204 Application of Simulationand AnalysisTechnolgies in LaunchOperation Development

M. Conroy, NASAKennedy Space Center,Kennedy Space Center,FL

1530AIAA-2004-0206 The Launch VehicleLanguage Data ModelApplied to Analysis ToolConnectivity

J. Vander Kam, Eloret,Inc., Cincinnati, OH


Monday Afternoon / 05 January 2004 Session 29-AFM-2 Performance, Stability, and Control I Sierra 1

Monday Afternoon / 05 January 2004 Session 30-APA-5 Aerodynamic Design II Carson 1

Monday Afternoon / 05 January 2004 Session 31-APA-6 Flow Control Applications Carson 2


Chaired by: R. AGARWAL, Washington University, Saint Louis, MO1400AIAA-2004-0209 Comparison of TimeDomain Training Signalsfor CFD BasedAerodynamic SystemIdentification

C. O'Neill, OklahomaState University,Stillwater, OK

1430AIAA-2004-0210 Rapid Computation ofDynamic StabilityDerivatives

J. Stalnaker,SYColeman, Huntsville,AL

1500AIAA-2004-0211 A Retrospective:Development ofSimulation Models forthe 1903 and 1905Wright Flyers

R. Deters, University ofIllinois atUrbana-Champaign,Urbana, IL

Chaired by: A. GOPALARATHNAM, North Carolina State University, Raleigh, NC1400AIAA-2004-0213 Numerical WingletOptimization

N. Pfeiffer, RaytheonAircraft Company,Wichita, KS

1430AIAA-2004-0214 Propeller Slipstreamand Wing- FuselageInterference Effects onThree- Axis Stability AndControl

M. Renooij, DelftUniversity ofTechnology, Delft, TheNetherlands

1500AIAA-2004-0215 Building theAerodynamics Modulefor the IntegratedHypersonicAeromechanics Tool

A. Le, Advatech PacificInc., Redlands, CA

1530AIAA-2004-0216 Warp Design of aSupersonic Wing Usinga Nonlinear OptimizationMethod

Z. Lei, Japan AerospaceExploration Agnecy,Tokyo, Japan

1600AIAA-2004-0217 Zero- Lift Wave DragCalculation UsingSupersonic Area Ruleand Its Modifications

V. Nikolic, MinnesotaState University,Mankato, MN

1630AIAA-2004-0219 Post- Stall Prediction ofMultiple- Lifting- SurfaceConfigurations Using aDecambering Approach

R. Mukherjee, NorthCarolina StateUniversity, Raleigh, NC

1700AIAA-2004-0220 Analysis and Design ofWings and Wing/WingletCombinations at LowSpeeds

J. Chattot, University ofCalifornia Davis, Davis,CA

Chaired by: A. AHMED, Auburn University, Auburn, AL1400AIAA-2004-0221 Compliant Flows: TheAnswer to PracticalFlow Control Problems?

J. Fulker, QinetiQ,Bedford, Great Britain

1430AIAA-2004-0222 A Multigrid Method for2- D MGD Flow ControlAnalysis

S. Luo, Univ. of Texasat Arlington, Arlington,TX

1500AIAA-2004-0224 Distributed HingelessFlow Control and RotarySynthetic Jet Actuation

A. Miller, Texas A&MUniversity, CollegeStation, TX

1530AIAA-2004-0225 Optimization of Blowingand Suction Control onNACA0012 Airfoil UsingGenetic Algorithm

L. Huang, University ofKentucky, Lexington, KY

1600AIAA-2004-0226 Post- Stall Flow Controlof Sharp- Edged Wingsvia Unsteady Blowing

J. Rullan, Virginia Tech,Blacksburg, VA

1630AIAA-2004-0227 Oscillatory and PulsedJets for Improved AirfoilAerodynamics - ANumerical Simulation

A. Hassan, The BoeingCompany, Mesa, AZ

1700AIAA-2004-0228 Numerical Modeling ofCoanda Jet ControlledNacelle Configurations

J. Wu, Georgia Instituteof Technology, Atlanta,GA

Chaired by: W. SAND, Aviation Weather Consulting, Inc., Lyons, CO1400 1430 1500 1530 1600


Monday Afternoon / 05 January 2004 Session 32-ASE-2 Cloud Forcasting, Characterization, Sensing, and Measuring N5

Monday Afternoon / 05 January 2004 Session 33-EMMD-1 Energetic Materials, Modeling and Diagnostics N10

Monday Afternoon / 05 January 2004 Session 34-FD-6 CFD Methods II Carson 3


Chaired by: W. SAND, Aviation Weather Consulting, Inc., Lyons, CO1400AIAA-2004-0229 Inflight Icing Data: AComparison ofTasmania and BritishIsles/central France AirOperations IcingEncounters

A. Brown, NationalResearch Council,Ottawa, Canada

1430AIAA-2004-0230 Methods ofCharacterizing CloudDrop Spectra SpatialVariation

C. Ryerson, ColdRegions Research &Engineering Laboratory,Hanover, NH

1500AIAA-2004-0231 The Forecast IcingPotential Algorithm

F. McDonough, NationalCenter for AtmosphericResearch, Boulder, CO

1530AIAA-2004-0233 Preliminary Analysis ofX- band and Ka- bandRadar for Use in theDetection of IcingConditions Aloft

A. Reehorst, NASAGlenn Research Center,Cleveland, OH

1600AIAA-2004-0234 Using RADTRAN toSimulate an AircraftMicrowave Radiometerto Detect Icing Potential

G. Koenig, ColdRegions Research &Engineering Laboratory,Hanover, NH

Chaired by: J. MERSON, Sandia National Laboratories, Albuquerque, NM, and T. BLACHOWSKI, Naval Surface Warfare Center, Indian Head, MD1400AIAA-2004-0238 Combustion Behaviorsof Pre- HeatedNanocompositeThermites

J. Granier, Texas TechUniversity, Lubbock, TX

1430AIAA-2004-0239 Calculation of BlowoutPanels Response Timesand Experimental Testsof Panel Performance

D. Olander, GoodrichCorporation, Phoenix, AZ

1500AIAA-2004-0240 Effect of Heterogeneityof Solid Propellants onTheir Intrinsic Stability ofPyrolysis

P. Preetham, IndianInstitute of Technology,Chennai, India

Chaired by: M. VISBAL, Air Force Research Laboratory, Wright-Patterson AFB, OH, and A. HASSAN, The Boeing Company, Mesa, AZ1400AIAA-2004-0241 Multiscale Modeling forTurbulence Simulationin Complex Geometries

S. Ramakrishnan, RiceUniversity, Houston, TX

1430AIAA-2004-0242 CFD with HybridSymbolic- NumericMethodology

J. Camberos, Air ForceResearch Laboratory,Wright-Patterson AFB,OH

1500AIAA-2004-0243 A Flux ConsistentImplementation of FluxVector Splitting

C. Campbell, NASAJohnson Space Center,Houston, TX

1530AIAA-2004-0244 Flow Simulation Aroundan Airfoil Using LatticeBoltzmann Method onGeneralized Coordinates

T. Imamura, NationalAerospace Laboratory,Tokyo, Japan

1600AIAA-2004-0245 Analysis DifferentNumerical Schemes forthe Resolution ofConvection- DiffusionEquations Using FiniteVolume Methods onUnstructured Grids

C. Perez-Segarra,Technical University ofCatalonia, Terrassa,Spain

1630AIAA-2004-0246 Cartesian MeshGeneration and Highly-Compressed StorageUsing Hilbert Codes

D. Hill, Fluent Inc.,Lebanon, NH

1700AIAA-2004-0248 Development of aRobust IncompressibleSolver for CartesianGrids with ColocatedVariables

D. Mott, Naval ResearchLaboratory, Washington,DC


Monday Afternoon / 05 January 2004 Session 35-FD-7 High Speed Transition Crystal 2

Monday Afternoon / 05 January 2004 Session 36-FD-8 LES Approaches and Applications Crystal 3

Monday Afternoon / 05 January 2004 Session 37-FD-9 Modeling for High-Speed Combustors Crystal 4


Chaired by: S. SCHNEIDER, Purdue University, West Lafayette, IN, and H. REED, Arizona State University, Tempe, AZ1400AIAA-2004-0249 Receptivity ofSupersonic BoundaryLayer on a Blunt Plate toAcoustic Disturbances

I. Egorov, MoscowInstitute of Physics andTechnology, Zhukovski,Russia

1430AIAA-2004-0250 Bypass Transition on theNozzle Wall of theBoeing/AFOSR Mach- 6Quiet Tunnel

S. Schneider, PurdueUniversity, WestLafayette, IN

1500AIAA-2004-0251 CompressibleBoundary- LayerTransition on anAxisymmetric Body atIncidence

H. Sugiura, NationalAerospace Laboratory,Chofu, Japan

1530AIAA-2004-0252 DNS of Attachment-line/Crossflow BoundaryLayer Instability inSupersonic Swept WingFlows

S. Speer, University ofCalifornia, Los Angeles,Los Angeles, CA

1600AIAA-2004-0253 Receptivity of Mach 6Flow over a FlaredCone to FreestreamDisturbance

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

1630AIAA-2004-0254 Receptivity of aSupersonic BoundaryLayer over a SharpWedge to WallBlowing/Suction

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

1700AIAA-2004-0255 Nonlinear Aspects ofHypersonic BoundaryLayer Stability on aPorous Surface

A. Shiplyuk, RussianAcademy of Sciences,Novosibirsk, Russia

1730AIAA-2004-0256 Receptivity toFreestreamDisturbances of a Mach10 NonequilibriumReacting Oxygen Flowover a Flat Plate

Y. Ma, University ofCalifornia, Los Angeles,Los Angeles, CA

Chaired by: K. SQUIRES, Arizona State University, Tempe, AZ1400AIAA-2004-0257 Zonal Grid Refinementfor Large EddySimulation of TurbulentBoundary Layers

I. Mary, ONERA,Chatillon, France

1430AIAA-2004-0258 Anti- Aliasing forIntegrated LES- RANSComputations

J. Schluter, StanfordUniversity, Stanford, CA

1500AIAA-2004-0259 Prediction of the Flowover an Airfoil atMaximum Lift

K. Squires, ArizonaState University,Tempe, AZ

1530AIAA-2004-0260 Large Eddy Simulationof Supersonic Twin- JetImpingement

H. Toh, Virginia Tech,Blacksburg, VA

1600AIAA-2004-0261 Large- Eddy Simulationof Tip Vortex Flow atHigh Reynolds Number

O. Fleig, University ofTokyo, Tokyo, Japan

1630AIAA-2004-0262 LES Investigation ofNear Field WakesBehind Juncture of Wingand Plate

J. Cai, University ofTexas at Arlington,Arlington, TX

1700AIAA-2004-0263 Turbulence ModelingStrategy in Rocket Flow

B. Wasistho, Universityof Illinois atUrbana-Champaign,Urbana, IL

1730AIAA-2004-0264 Extra- Large EddySimulation of MassivelySeparated Flows

J. Kok, NationalAerospace LaboratoryNLR, Amsterdam, TheNetherlands

Chaired by: M. BARONE, Sandia National Laboratories, Albuquerque, NM, and A. CUTLER, George Washington University, Hampton, VA1400AIAA-2004-0265 Scalar Measurementsfor Combustion ModelValidation

R. Barlow, SandiaNational Laboratories,Livermore, CA

1430AIAA-2004-0266 Supersonic CombustionExperiments for CFDModel Development andValidation (Invited)

A. Cutler, NASA LangleyResearch Center,Hampton, VA

1500AIAA-2004-0267 Modeling of High SpeedReacting Flows:Established Practicesand Future Challenges

R. Baurle, NASALangley, Hampton, VA

1530AIAA-2004-0269 The q- L TurbulenceClosure for Wall-Bounded and FreeShear Flows

U. Goldberg, MetacompTechnologies, AgouraHills, CA

1600AIAA-2004-0271 Computational Study ofMach Reflection inChemically ReactingSteady Flows

A. Trotsyuk, Institute ofTheoretical and AppliedMechanics, Novosibirsk,Russia

Chaired by: K. BURNS, Veridian Engineering, San Diego, CA1400 1430 1500 1530


Monday Afternoon / 05 January 2004 Session 38-HIS-2 History of Space Flight Crystal 1

Monday Afternoon / 05 January 2004 Session 39-MDO-2 MDO Methods N9

Monday Afternoon / 05 January 2004 Session 40-MSSP-2 Science in Space: Achievements of STS-107 and ISS Increment 6 N6


Chaired by: K. BURNS, Veridian Engineering, San Diego, CA1400AIAA-2004-0272 The 2003 GoddardRocket Replica Project:A Reconstruction of theWorld's First FunctionalLiquid Rocket System

R. Farr, NASA MarshallSpace Flight Center,Huntsville, AL

1430AIAA-2004-0273 History of AmericanWomen in Space

B. Johnson, MerkelAirplane Company,Valley Center, KS

1500AIAA-2004-0274 Keeping the InternationalSpace Station Flying:The Challenge WithoutShuttles

M. Sanchez, NASAJohnson Space Center,Houston, TX

1530AIAA-2004-0275 Aerospace Engineeringat SDSU - A Brief History

J. Katz, San Diego StateUniversity, San Diego,CA

Chaired by: A. MESSAC, Rensselaer Polytechnic Institute, Troy, NY, and G. DULIKRAVICH, University of Texas at Arlington, Arlington, TX1400AIAA-2004-0278 Multi- Objective ParetoConcurrent SubspaceOptimization forMultidisciplinary Design

C. Huang, University atBuffalo, Buffalo, NY

1430AIAA-2004-0280 Aerodynamic DataModeling Using SupportVector Machines

H. Fan, University ofTexas at Arlington,Arlington, TX

1500AIAA-2004-0281 Synthesizing an MDOArchitecture in CAD

C. Crawford,Massachusetts Instituteof Technology,Cambridge, MA

1530AIAA-2004-0282 Integration ofAerodynamic, Structural,Cost and ManufacturingCosiderations During theConceptual Design of aThrust Reverser Cascade

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

Chaired by: K. SACKSTEDER, NASA Glenn Research Center, Cleveland, OH, and R. GEVEDEN, NASA Marshall Space Flight Center, Huntsville, AL1400AIAA-2004-0285 The Mission After theMission: STS- 107Payload Debris andData Recovery Efforts

A. Over, NASA GlennResearch Center,Cleveland, OH

1430AIAA-2004-0286 Investigation ofNonbuoyant Laminar JetDiffusion Flames: AParadigm for SootProcesses in TurbulentFlames

G. Faeth, University ofMichigan, Ann Arbor, MI

1500AIAA-2004-0287 Behavior of ParticulateMaterials at Very LowPressures

S. Sture, University ofColorodo, Boulder, CO

1530AIAA-2004-0288 The Mist Experiment onSTS- 107: Fighting Firein Microgravity

A. Abbud-Madrid,Colorado School ofMines, Golden, CO

1600AIAA-2004-0290 Reaching for the STARS- The STS- 107 Mission

K. Campbell,SPACEHAB Inc.,Houston, TX

Chaired by: R. CUMMINGS, Cal Poly, San Luis Obispo, CA


Monday Afternoon / 05 January 2004 Session 41-NSC-2 AIAA Foundation National Student Conference - Graduate Division Crystal 5

Monday Afternoon / 05 January 2004 Session 42-PC-3 Micro-Combustion Cascade 1

Monday Afternoon / 05 January 2004 Session 43-PC-4 / ABP-2 Pulsed Detonation Engines I - Fundamental Issues Cascade 2


Chaired by: R. CUMMINGS, Cal Poly, San Luis Obispo, CA1400AIAA-2004-0292 ComputationalContinuum and RarefiedFlow Results for BalluteApplications

B. Anderson, GeorgeWashington University,Yorktown, VA

1430AIAA-2004-0293 Fluid Mechanics in aNon- Axisymmetric ColdFlow Ejector System

D. Lineberry, Universityof Alabama in Huntsville,Huntsville, AL

1500AIAA-2004-0294 Porous Pressure-Sensitive Paint forMeasurement ofUnsteady Pressures inTurbomachinery

J. Gregory, PurdueUniversity, WestLafayette, IN

1530AIAA-2004-0295 Preliminary Results ofVehicle FormationControl Using DynamicInversion

R. Caicedo, Texas A&MUniversity, CollegeStation, TX

1600AIAA-2004-0296 Theta- D Control forAscent Phase ofReusable LaunchVehicles

D. Drake, University ofMissouri-Rolla, Rolla,MO

1630AIAA-2004-0297 ExperimentalInvestigation of RotorVortex Wakes in Descent

J. Stack, University ofCalifornia Berkeley,Berkeley, CA

Chaired by: C. BRUNO, University of Rome, Rome, Italy, and D. KYRITSIS, University of Illinois at Urbana-Champaign, Urbana, IL1400AIAA-2004-0298 Flame Propagation inChannels: Steady andPulsating Propagation

M. Matalon,Northwestern University,Evanston, IL

1430AIAA-2004-0300 Effect of Structural HeatConduction on thePower Density of Micro-Combustors

T. Leach, University ofMaryland, College Park,MD

1500AIAA-2004-0301 Fuel- Air MixingChallenges in Micro-Power Systems

K. Dellimore, Universityof Maryland, CollegePark, MD

1530AIAA-2004-0303 Catalyzed Combustionof Hydrogen- Oxygen inPlatinum Tubes forMicro- PropulsionApplications

G. Boyarko, CaseWestern ReserveUniversity, Cleveland,OH

1600AIAA-2004-0304 Numerical Modeling ofthe HeterogeneousCombustion in a MicroScale Chemical Reactor

B. Xu, PrincetonUniversity, Princeton, NJ

1630AIAA-2004-0305 Simulation of anElectrostatically DrivenMicroinjector Pump

G. Krishnan, Universityof Colorado, Boulder, CO

Chaired by: C. LI, Naval Research Laboratory, Washington, DC, and C. BROPHY, Naval Postgraduate School, Monterey, CA1400AIAA-2004-0306 Multiphase Detonationsin Pulse DetonationEngines

S. Cheatham, NavalResearch Laboratory,Washington, DC

1430AIAA-2004-0308 A New Ignition Systemfor Pulse DetonationEngine

H. Shimada, AoyamaGakuin University,Tokyo, Japan

1500AIAA-2004-0310 Numerical andExperimental Study ofDetonation Propagationin a Rectangular Tubewith Obstacles

S. Shiokawa, AoyamaGakuin University,Tokyo, Japan

1530AIAA-2004-0311 Three- Dimensional CJDetonation inRectangular Tube

K. Eto, AoyamagakuinUniv., Sagamihara,Japan

Chaired by: J. SHANG, Wright State University, Dayton, OH


Monday Afternoon / 05 January 2004 Session 44-PDL-2 MHD N8

Monday Afternoon / 05 January 2004 Session 45-SAT-11400 - Meeting Society's Needs with Supersonic Transportation Carson 4

Monday Afternoon / 05 January 2004 Session 46-ST-1 Space Tethers Sierra 2


Chaired by: J. SHANG, Wright State University, Dayton, OH1400AIAA-2004-0314 Anisotropy ofCompressible MHDTurbulence in a MeanMagnetic Field

F. Ladeinde, SUNYStony Brook, StonyBrook, NY

1430AIAA-2004-0315 Hartmann Flow StabilityAnalysis

T. Bose, MetacompTechnologies Inc,Agoura Hills, CA

1500AIAA-2004-0317 Numerical Simulation of3- D Supersonic ViscousFlow in an ExperimentalMHD Channel

H. Kato, Iowa StateUniversity, Ames, IA

1530AIAA-2004-0318 Flow Calculations withStrong Magnetic Effects

R. MacCormack,Stanford University,Stanford, CA

Chaired by: T. HOWARD, Raytheon, Lanham, MDPanel Discussion

Chaired by: A. SANTANGELO, Michigan Technic Corporation, Holland, MI1400AIAA-2004-0322 Changes in PolymericTether Properties Due toAtomic Oxygen

M. Finckenor, NASAMarshall Space FlightCenter, Huntsville, AL

1430AIAA-2004-0323 The Configuration andDynamics of an OrbitingED Tether BasedSatellite

A. Santangelo, MichiganTechnic Corp., Holland,MI

1500AIAA-2004-0325 Designing Twin- StationLEO SatelliteConstellation for ZonalCoverage

J. Zhang, NorthwesternPolytechnical University,Xi'an, China (prc)

1530AIAA-2004-0326 Nonholonomic Control ofa Multi- link- modeledTether System

T. Naka, YamaguchiUniversity, Ube, Japan

Chaired by: D. BULZAN and J. ROHDE, NASA Glenn Research Center, Cleveland, OH1400 1430 1500 1600 1700


Monday Afternoon / 05 January 2004 Session 47-TES-2 Comprehensive Combustion Modeling II N4

Monday Afternoon / 05 January 2004 Session 48-TP-2 Nonequilibrium and High Speed Flows Shasta 2

Monday Afternoon / 05 January 2004 Session 49-TP-3 Thermal Control and Protection Systems Shasta 1


Chaired by: D. BULZAN and J. ROHDE, NASA Glenn Research Center, Cleveland, OH1400AIAA-2004-0327 Current Status of theOverall Spray SolutionProcedure (CombinedCFD/Scalar- Monte-Carlo- PDF/SprayComputations)Developed Under NCC

M. Raju, NASA Glenn,Cleveland, OH

1430AIAA-2004-0328 CFD Design AnalysisMethodology:Hypersonics, ConjugateHeat Transfer and LiquidSpray Combustion

D. Hoecke, EnerconSystems, Inc, Cleveland,OH

1500AIAA-2004-0330 Large- Eddy Simulation of Realistic Gas TurbineCombustors

P. Moin, Stanford University, Stanford, CA

1600AIAA-2004-0331 Large- Eddy Simulation Needs for Gas TurbineCombustor Design

W. Kim, Pratt & Whitney, East Hartford, CT

1700AIAA-2004-0332 A Particle- TrackingAlgorithm for LES ofTwo- Phase Flow

B. Shotorban, Universityof Illinois at Chicago,Chicago, IL

Chaired by: D. GOLDSTEIN, University of Texas, Austin, TX, and I. WYSONG, EOARD, London, Great Britain1400AIAA-2004-0333 Nonequilibrium PlasmaEffects on TelemetryConsiderations for Air-Breathing HypersonicVehicle Design

R. Starkey, University ofMaryland, College Park,MD

1430AIAA-2004-0336 Use of Quasi- ClassicalTrajectory Methods inthe Modeling of OHProduction Mechanismsin DSMC

T. Ozawa, PennsylvaniaState University,University Park, PA

1500AIAA-2004-0337 Quantum ScatteringStudy of Ro- vibrationalExcitations in N+N_2Collisions Under Re-entry Conditions

D. Wang, NASA AmesResearch Center, MoffettField, CA

1530AIAA-2004-0338 NonequilibriumVibrational EnergyTransfer AcrossHypersonic BoundaryLayers

G. Inger, Iowa StateUniversity, Ames, IA

Chaired by: B. DROLEN, The Boeing Company, Altadena, CA, and J. MARONEY, Sverdrup Technology, Inc, Huntsville, AL1400AIAA-2004-0341 Thermal Response ofAblative Test Piece inArc- Heated Wind Tunnel

T. Suzuki, TohokuUniversity, Sendai,Japan

1430AIAA-2004-0342 TPS Selection andSizing Tool Implementedin an AdvancedEngineering Environment

M. McGuire, ELORETCorporation, MoffettField, CA

1500AIAA-2004-0343 Non- Metallic andStructurally EfficientThermal Energy StorageComposites for AvionicsTemperature Control,Part I: ThermalCharacterization

R. Wirtz, University ofNevada-Reno, Reno, NV

1530AIAA-2004-0344 Non- Metallic andStructurally EfficientThermal Energy StorageComposites for AvionicsTemperature Control,Part II: MechanicalCharacterization

T. Zhao, University ofNevada-Reno, Reno, NV

Chaired by: M. BALAS, University of Colorado, Boulder, CO


Monday Afternoon / 05 January 2004 Session 50-WE-2 Control of Loads and Power Ruby

Monday Afternoon / 05 January 2004 Session 51-WIG-2 Plasma Discharge Physics II Teton

Monday Afternoon / 05 January 2004 Session - Dryden Lectureship in Research Reno Ballroom


Chaired by: M. BALAS, University of Colorado, Boulder, CO1400AIAA-2004-0345 Design of Controls toAttenuate Loads in theControls AdvancedResearch Turbine

A. Wright, NationalRenewable EnergyLaboratory, Golden, CO

1430AIAA-2004-1365 Periodic and Non-Periodic DisturbanceAccommodating Controlof the ControlsAdvanced ResearchTurbine (CART)

B. Street, University ofColorado, Boulder, CO

1500AIAA-2004-0347 Baseline Results andFuture Plans for theNREL ControlsAdvanced ResearchTurbine

L. Fingersh, NationalRenewable EnergyLaboratory, Golden, CO

1530AIAA-2004-0348 Further Studies of RotorLoads Control in HighlySheared TurbulentWinds

A. Eggers, RANN Inc.,Palo Alto, CA

1600AIAA-2004-0350 Methods for IncreasingRegion 2 PowerCapture on a VariableSpeed HAWT

K. Johnson, NationalRenewable EnergyLaboratory, Golden, CO

1630AIAA-2004-0352 Energy Storage andReactive PowerCompensator in a LargeWind Farm

E. Muljadi, NationalRenewable EnergyLaboratory, Golden, CO

Chaired by: R. BARKER, Air Force Office of Scientific Research, Arlington, VA, and S. STARIKOVSKAIA, Moscow Institute of Physics and Technology, Moscow, Russia1400AIAA-2004-0353 Nonequilibrium PlasmaFormation by High-Voltage PulsedNanosecond GasDischarge at DifferentPressures

M. Nudnova, MoscowInstitute of Physics andTechnology,Dolgoprudny, Russia

1430AIAA-2004-0354 Ion Wind Effects in APositive DC CoronaDischarge inAtmospheric PressureAir

D. Lacoste, EcoleCentrale Paris,Chatenay-Malabry,France

1500AIAA-2004-0355 ATMOSPHERIC AIRAND NITROGEN DCGLOW DISCHARGESWITH THERMIONICCATHODES ANDSWIRL FLOW

Z. Machala, StanfordUniversity, Stanford, CA

1530AIAA-2004-0357 Microwave DischargeControl by MagneticField

V. Brovkin, RussianAcademy of Sciences,Moscow, Russia

1600AIAA-2004-0358 Microwave DischargeInitiated by Laser Spark

I. Mashek, SaintPetersburg StateUniversity, SaintPetersburg, Russia

1630AIAA-2004-0359 Electron- BeamGenerated Plasma inAir: Pulsed andContinuous Generation

R. Vidmar, University ofNevada Reno, Reno, NV

1700AIAA-2004-0360 Data Reduction Analysisfor a Cylindrical, DoubleLangmuir ProbeOperating in a HighSpeed Flow

S. Henderson, WrightState University,Dayton, OH

1800AIAA-2004-0001 Innovations inAeronautics

I. Kroo, StanfordUniversity, Stanford, CA

More than 90 Institute members will be inducted as AIAA Associate Fellows during the AIAA Foundation Associate Fellows Dinner. Each year, the Institute recognizes exemplary professionals for their


Monday Afternoon / 05 January 2004 1900 - 2130 AIAA Foundation Associate Fellows Dinner Tahoe

Tuesday Morning / 06 January 2004 0800 - 1200 AIAA Foundation Graduate Awards N4

Tuesday Morning / 06 January 2004 0800 - 1200 Career Workshop—Managing Your Career in the 21st Century Crystal 5


More than 90 Institute members will be inducted as AIAA Associate Fellows during the AIAA Foundation Associate Fellows Dinner. Each year, the Institute recognizes exemplary professionals for theiraccomplishments in engineering or scientific work, outstanding merit and contributions to the arts, sciences, or technology of aeronautics or astronautics. Please support your colleagues, and join us for theinduction of AIAA’s Associate Fellows class of 2004. Tickets to this prestigious gala event are available on a first-come, first-served basis for $50 and purchased in advance at the on-site registration desk.Business attire is requested.

The AIAA Foundation awarded 14 graduate awards for the 2003/2004 academic year. Six of these award recipients will present their award-winning work at this conference. These students competed against alarge number of other students, but rose above the rest for their outstanding work. This year’s presenters are: Geoffrey Jeram, Georgia Institute of Technology, Carefree Maneuver Technology for Helicoptersand Robotic Control Vehicles Graduate Award; Michael Benoit, University of Colorado, Cellular Dynamics and Growth in Space Graduate Award; Jeffrey Jepson, North Carolina State University, Self ActuatingTelescopic Wings (John Leland Atwood Graduate Award winner); Pezhman Akbari, Michigan State University, Potential of Wave Devices in Gas Turbines Graduate Award; Thomas Hatfield, University ofColorado, Ultrasonic Physiological Measurement and Technology Graduate Award; Katie Grantham, University of Missouri-Rolla, William T. Piper, Sr. General Aviation Systems Graduate Award.

0800 Overview & Industry Trends J. Morrow, Boeing Space & Communications, Arlington, VA 0830 Industry Overview T. Howard, Raytheon Technical Services, Lanham, MD 0900 Job InterviewingTechniques J. Lutz, Consultant, Winter Park, FL 0930 To Stay or To Go- Personal Risk Analysis B. Wessels, Lockheed Martin, Denver, CO 1000 Diversity in the Workplace 1030 Authoring Your CareerCrossroads J. Lutz, Consultant, Winter Park, FL 1100 Panel Session

Chaired by: S. COLLIS, Rice University, Houston, TX0800 0830 0900 0930 1000 1030 1100

Chaired by: V. CAPECE, University of Kentucky, Paducah, KY, and F. LIU, University of California, Irvine, Irvine, CA0800 0830 0900 0930 1000


Tuesday Morning / 06 January 2004 Session 52-AA-3 Modeling/Mechanisms N7

Tuesday Morning / 06 January 2004 Session 53-ABP-3 Turbomachinery - Computational Whitney

Tuesday Morning / 06 January 2004 Session 54-AFM-3 Performance, Stability, and Control II Sierra 1


Chaired by: S. COLLIS, Rice University, Houston, TX0800AIAA-2004-0361 Philosophy andEvolution of a Semi-Empirical Model for JetNoise Prediction

J. Stone, ModernTechnologies Corp.,Middleburg Heights, OH

0830AIAA-2004-0362 Fine Scale TurbulenceNoise from Hot Jets

C. Tam, Florida StateUniversity, Tallahassee,FL

0900AIAA-2004-0363 Acoustic Radiation FromSubsonic andSupersonic MixingLayers With NonlinearPSE

L. Cheung, StanfordUniversity, Stanford, CA

0930AIAA-2004-0364 Toward Optimal Controlof Aeroacoustic FlowsUsing DiscontinuousGalerkin Discretizations

G. Chen, RiceUniversity, Houston, TX

1000AIAA-2004-0366 Temperature GradientEffects on Sound WavePropagation

C. Tarau, PolytechnicUniversity, Brooklyn, NY

1030AIAA-2004-0367 Analytical Solutions toTwo- DimensionalAcoustic Fields withTwo- DimensionalTemperature Variation

S. Tiyyagura, IndianInstitute of Technology,Chennai, India

1100AIAA-2004-0368 Similarity of FluctuatingVelocity and PressureSpectra UsingKolmogorov Scales ofTurbulence

A. Laganelli, ScienceApplicationsInternationalCorporation, King OfPrussia, PA

Chaired by: V. CAPECE, University of Kentucky, Paducah, KY, and F. LIU, University of California, Irvine, Irvine, CA0800AIAA-2004-0369 Integrated RANS- LESComputations in GasTurbines: Compressor-Diffusor Coupling

J. Schluter, StanfordUniversity, Stanford, CA

0830AIAA-2004-0370 Unsteady CooledTurbine SimulationUsing a PC- LinuxAnalysis System

M. List, University ofCincinnati, Cincinnati,OH

0900AIAA-2004-0371 High Fidelity SystemSimulation of AerospaceVehicles Using NPSS

R. Sampath, GE GlobalResearch Center,Niskayuna, NY

0930AIAA-2004-0372 Numerical Simulationsof Rotor 35 with andWithout Tip InjectionUsing an Arbitrary MachNumber Flow Solver

C. Sheng,ComputationalSimulation & DesignCenter, MississippiState, MS

1000AIAA-2004-0374 Improvements in Gas-Turbine PerformanceThrough the Use ofMultiple Turbine Inter-stage Burners

G. Chen, University ofCalifornia Davis, Davis,CA

Chaired by: K. IWANSKI, Air Force Research Laboratory, Wright-Patterson AFB, OH0800AIAA-2004-0377 Applications ofComputational Methodsfor Dynamic Stabilityand Control Derivatives

L. Green, NASA LangleyResearch Center,Hampton, VA

0830AIAA-2004-0378 Spin Recovery of anAircraft Using NonlinearDynamic InversionTechniques

P. Kumar, IndianInstitute of Technology,Mumbai, India

0900AIAA-2004-0379 Model- MatchingController Using RightInverse System and ItsVerification by FlightExperiments

M. Sato, Institute ofSpace Technology andAeronautics JapanAerospace ExplorationAgency, Mitaka, Japan

0930AIAA-2004-0380 An Analytical Study onDesign andPerformance of Dual-Bell Nozzles

M. Miyazawa, ShizuokaUniversity, Hamamatsu,Japan

1000AIAA-2004-0381 Calculated Drag of anAerial RefuelingAssembly ThroughAirplane PerformanceAnalysis

M. Vachon, NASADryden Flight ResearchCenter, Edwards, CA


Tuesday Morning / 06 January 2004 Session 55-AMT-2 Spectroscopic Techniques Shasta 1

Tuesday Morning / 06 January 2004 Session 56-APA-7 Drag Prediction Workshop II: Summary Session I Carson 4

Tuesday Morning / 06 January 2004 Session 57-APA-8 Unmanned/Micro Air Vehicle Aerodynamics Carson 2


Chaired by: S. BERESH, Sandia National Laboratories, Albuquerque, NM0800AIAA-2004-0383 A Review of theSpectroscopy of Gas-phase Flow: TheMolecules and ModernMethods

N. Glumac, University ofIllinois atUrbana-Champaign,Urbana, IL

0830AIAA-2004-0384 Simultaneous Imagingof Vapor and LiquidSpray ConcentrationUsing CombinedAcetone Fluorescenceand Phosphorescence

J. Seitzman, GeorgiaInstitute of Technology,Atlanta, GA

0900AIAA-2004-0385 A Preliminary Study onAcetone Laser- InducedFluorescenceTechnique for LowTemperature Flows

M. Kashitani, NationalDefense Academy,Yokosuka, Japan

0930AIAA-2004-0386 Carbon Dioxide UVLaser- InducedFluorescence Imaging inHigh- Pressure Flames

T. Lee, StanfordUniversity, Stanford, CA

1000AIAA-2004-0387 A Burst Mode OPOSystem for MHz FrameRate PLIF ImagingDiagnostics

W. Lempert, Ohio StateUniversity, Columbus,OH

1030AIAA-2004-0388 Measurements ofElectrothermal- PlasmaIgnition of SolidPropellants

M. Ryan, University ofTexas at Austin, Austin,TX

1100AIAA-2004-0389 Role of Non- StationaryCollisional Dynamics inDetermining Nitric OxideLIF Spectra

J. Daily, University ofColorado, Boulder, CO

1130AIAA-2004-0390 Kinetics of NO TagFormation in Air forUnseeded MolecularTagging Velocimetry

S. Nandula, VanderbiltUniversity, Nashville, TN

Chaired by: R. WAHLS, NASA Langley Research Center, Hampton, VA, and R. RUDNIK, DLR, Braunschweig, Germany0800AIAA-2004-0391 Airbus, ONERA, andDLR Results from the2nd AIAA DragPrediction Workshop

O. Brodersen, DLR,Braunschweig, Germany

0830AIAA-2004-0392 Drag Prediction ofEngine- AirframeInterference Effects withCFX 5

R. Langtry, Ansys CFX,Otterfing, Germany

0900AIAA-2004-0393 OVERFLOW DragPrediction for the DLR-F6 TransportConfiguration: A DPW-II Case Study

A. Sclafani, The BoeingCompany, HuntingtonBeach, CA

0930AIAA-2004-0394 Study of CFD Variationon TransportConfigurations from theSecond Drag- PredictionWorkshop

C. Rumsey, NASALangley ResearchCenter, Hampton, VA

1000AIAA-2004-0395 Aircraft Drag PredictionUsing Cobalt

K. Wurtzler, CobaltSolutions LLC,Cincinnati, OH

1030AIAA-2004-0396 Drag Prediction of theDLR- F6 Configuration

G. May, StanfordUniversity, Menlo Park,CA

1100AIAA-2004-0397 Drag Prediction of DLR-F6 Using the TurbulentNavier- StokesCalculations withMultigrid

Y. Kim, KoreaAdvanced Institute ofScience andTechnology, Daejeon,South Korea

1130AIAA-2004-0398 CFD Sensitivity of DragPrediction on DLR- F6Configuration byStructured Method andUnstructured Method

K. Yamamoto, JapanAerospace ExplorationAgency, Chofu, Japan

Chaired by: D. GRISMER, Air Force Research Laboratory, Wright-Patterson AFB, OH0800AIAA-2004-0399 Improved Performanceand Control of Flapping-Wing Propelled MicroAir Vehicles

K. Jones, NavalPostgraduate School,Monterey, CA

0830AIAA-2004-1373 Development and FlightTesting of a UAV withInflatable- RigidizableWings

M. Usui, University ofKentucky, Lexington, KY

0900AIAA-2004-0401 Aerodynamic Designand Optimization of theMars Airborne RemoteExploration ScoutAircraft

J. Vassberg, The BoeingCompany, HuntingtonBeach, CA

0930AIAA-2004-0402 FENSAP- ICEApplications toUnmanned AerialVehicles (UAV)

P. Tran, NewmericalTechnologiesInternational, Montreal,Canada

1000AIAA-2004-0403 Experimental andNumerical Studies ofGeometry Effects onUCAV's Aerodynamics

X. Huang, NationalResearch Council,Ottawa, Canada

1030AIAA-2004-0404 The Influence of FinRigidity and Gusts onthe Force Production inFishes and Insects: AComputational Study

R. Ramamurti, NavalResearch Laboratory,Washington, DC

1100AIAA-2004-0406 Comparison andValidation of Micro AirVehicle Design Methods

S. Boughton, RochesterInstitute of Technology,Rochester, NY

1130AIAA-2004-0040 Design andDevelopment ofFlapping Wing Micro AirVehicle

V. Malolan, MadrasInstitute of Technology,Chennai, India


Tuesday Morning / 06 January 2004 Session 58-ASE-3 Cloud Droplet Dynamics and Effects N5

Tuesday Morning / 06 January 2004 Session 59-EDU-1 Education: Design Pedagogy and Program Issues N10

Tuesday Morning / 06 January 2004 Session 60-FD-10 Flow Control of Boundary Layers, Cavities and Jets Crystal 1


Chaired by: D. MILLER, NASA Glenn Research Center, Cleveland, OH0800AIAA-2004-0407 Overview of High SpeedClose- Up Imaging in anIcing Environment

D. Miller, NASA GlennResearch Center,Cleveland, OH

0830AIAA-2004-0410 A Tentative Mass LossModel for SimulatingWater Droplet Splash

C. Tan, Wichita StateUniversity, Wichita, KS

0900AIAA-2004-0411 Role of DropletDistortion and Break- upin Large Droplet AircraftIcing

G. Luxford, CranfieldUniversity, Cranfield,Great Britain

0930AIAA-2004-0412 Semi- EmpiricalModelling of SLDPhysics

W. Wright, QSS GroupInc., Cleveland, OH

1000AIAA-2004-0413 Additional Study of MVDEffects on Ice Shapes

J. Tsao, Ohio AerospaceInstitute, Cleveland, OH

1030AIAA-2004-0414 Large Droplet Impact onWater Layers

R. Purvis, UniversityCollege London,London, Great Britain

0800AIAA-2004-0415 Recent Experiments inAerospace and DesignEngineering Education

W. Mason, VirginiaTech, Blacksburg, VA

0830AIAA-2004-0416 A New Capstone DesignCurriculum

D. Miller,Massachusetts Instituteof Technology,Cambridge, MA

0900AIAA-2004-0417 Exploiting the CreativeProcess for InnovativeAir Vehicle Design

D. Cummings, BoeingPhantom Works,Huntington Beach, CA

0930AIAA-2004-0419 Analysis of TeamPerformance and ReportQuality in a SophomoreDesign- Build Project

J. Craig, MassachusettsInstitute of Technology,Cambridge, MA

1000AIAA-2004-0420 Aerospace EngineeringProgram at IIUM

F. Lohar, InternationalIslamic UniversityMalaysia, KualaLumpur, Malaysia

1030AIAA-2004-0421 From Parks Air Collegeto Parks College ofEngineering & Aviation:75 Years of Legacy inAerospace Engineering

K. Ravindra, Saint LouisUniversity, Saint Louis,MO

1100AIAA-2004-0422 Education inEngineering ThroughVirtual Institutes: An E-Learning Case Study

I. Howes, CranfieldUniversity, Cranfield,Great Britain

Chaired by: C. TILMANN, Air Force Research Laboratory, Wright-Patterson AFB, OH, and A. SEIFERT, TelAviv University, TelAviv, Israel0800AIAA-2004-0424 Surface Shear StressReduction with MEMSSensors/Actuators inTurbulent BoundaryLayers

J. Lew, University ofCalifornia, Los Angeles,Los Angeles, CA

0830AIAA-2004-0425 Design Considerationsfor Using IndentedSurface Treatments toControl Boundary LayerSeparation

T. Robarge, U.S. AirForce Academy, USAFAcademy, CO

0900AIAA-2004-0426 Aerodynamics ofRecirculating FlowControl Devices forNormal Shock/BoundaryLayer Interactions

K. Srinivasan, Universityof Illinois atUrbana-Champaign,Urbana, IL

0930AIAA-2004-0427 Response of Time-Depended FlowfieldStructure Behind anActive VortexGenerators Pair

T. Shizawa, TokyoUniversity of ScienceSuwa, Chino-shi, Japan

1000AIAA-2004-0428 Flow Control of ShearLayers Over 2- DCavities Using PulsedJet and Aero- opticalAnalysis

Y. Tan, WashingtonUniversity in St. Louis,St. Louis, MO

1030AIAA-2004-0429 Numerical Simulationsof Fluidic Control forTransonic Cavity Flows

A. Hamed, University ofCincinnati, Cincinnati,OH

1100AIAA-2004-0430 Passive Mixing Controlof Parallel Jets

N. Bunderson, UtahState University, Logan,UT

Chaired by: J. EKATERINARIS, Forth/IACM, Heraklion, Greece, and J. CAMBEROS, Air Force Research Laboratory, Wright-Patterson AFB, OH0800 0900 0930 1000 1030 1100 1130


Tuesday Morning / 06 January 2004 Session 61-FD-11 High-order CFD Methods Crystal 2

Tuesday Morning / 06 January 2004 Session 62-FD-120800 - 1200 Workshop on LES Development & Validation Needs for Gas Turbines (Invited) Carson 3

Tuesday Morning / 06 January 2004 Session 63-FD-130800 - 1200 Modeling Versus Design for Micro Fluidics in Aerospace Systems Carson 4


Chaired by: J. EKATERINARIS, Forth/IACM, Heraklion, Greece, and J. CAMBEROS, Air Force Research Laboratory, Wright-Patterson AFB, OH0800AIAA-2004-0431 On the Use of High Order Methods for ComplexAerodynamic Problems

J. Ekaterinaris, Forth/IACM, Heraklion, Greece

0900AIAA-2004-0432 A Staggered Grid, High-Order Accurate Methodfor IncompressibleViscous Flow

N. Kampanis,Forth/IACM, Heraklion,Greece

0930AIAA-2004-0433 A Runge- Kutta-Newton- KrylovAlgorithm for Fourth-Order Implicit TimeMarching Applied toUnsteady Flows

S. Isono, University ofToronto, Toronto,Canada

1000AIAA-2004-0434 Building- Cube Methodfor Large- Scale, HighResolution FlowComputations

K. Nakahashi, TohokuUniversity, Sendai,Japan

1030AIAA-2004-0435 A Modified Upwind-Biased Strategy toCalculate Flow onStructured- UnstructuredGrid Topologies

M. Darbandi, Universityof Waterloo, Waterloo,Canada

1100AIAA-2004-0436 Development of aHigher- Order Solver forAerodynamicApplications

D. Darmofal,Massachusetts Instituteof Technology,Cambridge, MA

1130AIAA-2004-0437 Parallel, High- OrderOverset GridImplementation forSupersonic Flows

K. Alabi, ThaerocompTechnical Corp., StonyBrook, NY

Chaired by: F. GRINSTEIN, Los Alamos National Laboratory, Los Alamos, NM, and J. OEFELEIN, Sandia National Laboratories, Livermore, CAWorkshop organized by the FDTC TWG on LES.

0800-0810 – F. F. Grinstein, Welcome and Introduction0810-0835 – J. C. Oefelein, R. W. Schefer, R. S. Barlow, SNL, Livermore, CA, High-Fidelity LES and Target Validation Experiments in the Turbulent Combustion Laboratory0835-0900 – G. Richards and D. Maloney, NETL, Morgantown, WV, The SimVal Experiments and Generation of Validation Datasets0900-0925 – D. Bulzan, NASA GRC, Cleveland OH, Combustion Code Validation Experiments at Realistic Conditions0925-0950 – E. Gutmark, U. Cincinnati, Cincinnati OH, Laboratory Studies for Gas Turbine Research0950-1015 – J.P. Bonnet, U. Poitiers, France, S. Verfaillie, U. Cincinnati, and F.F. Grinstein, IGPP-LANL, The Laboratory-LES Inlet Condition Interface in Swirl Combustors1015-1040 – C. Fureby and T. Carlsson, FOI, Sweden, Laboratory and Computational Studies of Turbulent Flows with Emphasis on Gas Turbines1040-1105 – L. Fuchs, U. of Lund, Sweden, LES of Swirling Jets1105-1130 – S. Menon, GATECH, Atlanta GA, (Un)Acceptable Uncertainty in Experimental Data for LES Model Validation1130-1200 – Moderated Discussion

Chaired by: B. SHAPIRO, University of Maryland, College Park, MDThe goal of this workshop is to identify future needs in modeling of micro fluidic systems from a system design perspective. In other words, what form should micro fluidic models take, and how should they becreated, to allow analysis, design, control, and optimization of the entire system? The workshop brings together micro fluidic modeling researchers with experts in system analysis, system design, and control.

The first session of this two session workshop will consider aerospace systems with micro fluidic actuation such as UAVs controlled by synthetic jets or nano satellites controlled by micro thrusters.

0800 - Introduction and Welcome - B. Shapiro0830 - Liquids: The Holy Grail of Microfluidics Modeling, M. Gad-el-Hak, Virginia Commonwealth University0900 - Design Tools for Synthetic Jets in Flow Control, D. MacMartin, Caltech0930 - FEMLAB: A General CAD Tool for Solving Partial Differential Equations, B. Sjodin, FEMLAB1000 - Break1030 - Moderated Discussion, J. Burns, C. Cadou, A. Glezer, and B. Shapiro


Tuesday Morning / 06 January 2004 Session 64-FD-140800 - 1200 Transition Study Group Session Crystal 3

Tuesday Morning / 06 January 2004 Session 66-ISS-1 Technology Research Opportunities on the ISS Express Pallet Tahoe

Tuesday Morning / 06 January 2004 Session 67-MDO-3 Optimization Approaches N9


Chaired by: W. SARIC, Arizona State University, Tempe, AZ0800-1000: Laminar Flow Control Panel Discussion Moderator: Eli Reshotko, Case Western Reserve University1000 – 1030: Report on the Transition Study Group Workshop on Transition, John Schmisseur, AFOSR, Arlington, VA1030 – 1200: Transition Study Group Open Forum

Chaired by: J. BARTOE, NASA Johnson Space Center, Houston, TX0800AIAA-2004-0439 Capabilities andAccommodations on theISS EXPRESS Pallet

G. Cook, NASA JohnsonSpace Center, Houston,TX

0830AIAA-2004-0440 EXPRESS Pallet as anEngineering Test Bedfor SpacecraftTechnology

D. Boyle, Texas A&MUniversity, CollegeStation, TX

0900AIAA-2004-0442 Department of DefenseExperiments on theInternational SpaceStation Express Pallet

D. DeAtkine, TheAerospace Corporation,Houston, TX

0930AIAA-2004-0443 The Silicon X- rayImager (SIXI) on ISSExpress Pallet

K. Wood, NavalResearch Laboratory,Washington, DC

1000AIAA-2004-1380 The Navy's Experiencewith Small Experiments– Application to theExpress Pallet

H. Gursky, NavalResearch Laboratory,Washington, DC

Chaired by: C. BLOEBAUM, State University of New York at Buffalo, Buffalo, NY, and W. CROSSLEY, Purdue University, West Lafayette, IN0800AIAA-2004-0448 Data Driven DesignOptimizationMethodology - Part I

H. Zhao, RutgersUniversity, Piscataway,NJ

0830AIAA-2004-0449 Comparison of Bit-String Affinity andConsecutive GenerationStopping Criteria forGenetic Algorithms

W. Crossley, PurdueUniversity, WestLafayette, IN

0900AIAA-2004-0450 Data Transmission inMultidisciplinary DesignOptimization Using aPlatform- IndependentData Structure

S. Parashar, Universityat Buffalo, Buffalo, NY

0930AIAA-2004-0451 Ramjet Powered MissileDesign Using a GeneticAlgorithm

R. Hartfield, AuburnUniversity, Auburn, AL

1000AIAA-2004-0452 Variable Population-Based Sampling forProbabilistic DesignOptimization with aGenetic Algorithm

R. Hassan, PurdueUniversity, WestLafayette, IN

1030AIAA-2004-0453 MultiobjectiveEvolutionaryComputation forNoncircular MissileShape Optimization

H. Liu, Shanghai JiaoTong University,Shanghai, China (prc)

1100AIAA-2004-0454 Comparison ofOptimization AlgorithmsApplied to AerodynamicDesign

P. Liu, University ofToronto, Toronto,Canada

Chaired by: E. GUTMARK, University of Cincinnati, Cincinnati, OH, and K. YU, University of Maryland, College Park, MD0800 0830 0900 0930 1000 1030 1100


Tuesday Morning / 06 January 2004 Session 68-PC-5 Combustion Acoustics and Instabilities Cascade 1

Tuesday Morning / 06 January 2004 Session 69-PC-6 / ABP-4 Pulsed Detonation Engines II - Applications Cascade 2

Tuesday Morning / 06 January 2004 Session 70-PDL-3 / FD-15 Aero-Optics N8


Chaired by: E. GUTMARK, University of Cincinnati, Cincinnati, OH, and K. YU, University of Maryland, College Park, MD0800AIAA-2004-0455 Nonlinear Response ofa Premixed Combustorto Forced AcousticOscillations

B. Bellows, GeorgiaInstitute of Technology,Atlanta, GA

0830AIAA-2004-0456 Thermoacoustic FlameTransfer Function of aGas Turbine Burner inPremix and Pre- PremixCombustion

B. Schuermans,ALSTOM (Switzerland)Ltd, Baden, Switzerland

0900AIAA-2004-0457 Detection of the Onsetof Unstable Combustionin Lean PremixedCombustors

B. Lee, YeungnamUniversity, Kyongsan,South Korea

0930AIAA-2004-0459 Flame- AcousticInteractions in aCounterflow Field

A. Zambon, University ofVirginia, Charlottesville,VA

1000AIAA-2004-0460 Combustion and HeatTransfer Dynamics in aPremixed Laminar Flat-flame Burner

L. Haber, GE GlobalResearch, Niskayuna,NY

1030AIAA-2004-0461 Effect of Approach FlowTurbulenceCharacteristics onSound Generation fromPremixed Flames

R. Rajaram, GeorgiaInstitute of Technology,Atlanta, GA

1100AIAA-2004-0462 Response of One-Dimensional LaminarPremixed FlamePropagation to TravelingPressure Oscillations

P. Preetham, IndianInstitute of TechnologyMadras, Chennai, India

Chaired by: L. BAUWENS, University of Calgary, Calgary, Canada, and J. SINIBALDI, Naval Postgraduate School, Monterey, CA0800AIAA-2004-0463 Numerical Modeling ofPulse Detonation RocketEngine Gasdynamicsand Performance

C. Morris, NASAMarshall Space FlightCenter, Huntsville, AL

0830AIAA-2004-0464 Numerical Investigationof the PDREPerformance withDetailed Chemistry

S. Sato, Keio University,Yokohama, Japan

0900AIAA-2004-0465 Numerical Investigationof 2- D and 3- DMultitube PulseDetonation Using H2and JP8 Fuel

H. Ebrahimi, SverdrupTechnology Inc., ArnoldAFB, TN

0930AIAA-2004-0468 A New Facility for theStudy of Shock Wave –Induced Combustion ofLiquid Fuels

J. Kashdan, StanfordUniversity, Stanford, CA

1000AIAA-2004-0469 Performance and NoiseCharacteristics of PulseDetonation Engines

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

1030AIAA-2004-0470 Ion Based High-Temperature PressureSensor

J. Zdenek, Air ForceInstitute of Technology,Wright-Patterson AFB,OH

Chaired by: E. JUMPER, University of Notre Dame, Notre Dame, IN, and T. BEUTNER, Air Force Office of Scientific Research, Arlington, VA0800AIAA-2004-0471 Technique forSimulating andEvaluating Aero- opticalEffects in Optical Systems

J. Trolinger, MetroLaserInc, Irvine, CA

0830AIAA-2004-0472 Optical DisturbancesCaused by TransonicSeparated BoundaryLayer Behind a 20-Degree Ramp: Physicsand Control

S. Gordeyev, Universityof Notre Dame, NotreDame, IN

0900AIAA-2004-0473 Aerooptical Interactionsin TurbulentCompressible SeparatedShear Layers and theInterfacial- Fluid-Thickness Approach

R. Aguirre, University ofCalifornia Irvine, Irvine,CA

Chaired by: E. KHALIL, Cairo University, Cairo, Egypt, and A. GUPTA, University of Maryland, College Park, MD


Tuesday Morning / 06 January 2004 Session 71-TES-3 Terrestrial Energy Systems Sierra 2

Tuesday Morning / 06 January 2004 Session 72-TP-4 Aerothermodynamics Crystal 4

Tuesday Morning / 06 January 2004 Session 73-TP-5 Conduction and Convection N6


Chaired by: E. KHALIL, Cairo University, Cairo, Egypt, and A. GUPTA, University of Maryland, College Park, MD0800AIAA-2004-0476 Only Three Minutes fromIgnition to Inferno: It'sNot Unusual in Fires

D. Lilley, Lilley &Associates, Stillwater,OK

0830AIAA-2004-0477 Calculation of Volumeand Temperature ofSmoke in Fires


0900AIAA-2004-0478 Transient NumericalSimulation of AirCharacteristics inVentilated CompartmentFire

R. Kameel, CEB, Cairo,Egypt

0930AIAA-2004-0479 Phase DopplerMeasurements of LiquidFire Suppressants overa Heated Cylinder

C. Presser, NationalInstitute of Standardsand Technology,Gaithersburg, MD

1000AIAA-2004-0480 Transient Analysis ofPressure- InducedTransfer of CryogenicHydrogen in StorageSystems

A. Mahmoud, Universityof Florida, Gainesville,FL

1030AIAA-2004-0483 Interaction and Inductionof Shock Waves ofSupersonic TurbulentFlow with a TransverseSonic Injection Jet

D. Sun, University ofWisconsin-Milwaukee,Milwaukee, WI

Chaired by: R. BOND, Sandia National Laboratories, Albuquerque, NM, and J. CAMBEROS, Air Force Research Laboratory, Wright-Patterson AFB, OH0800AIAA-2004-1353 Radiation AnalysisBehind HypersonicShock Wave in NitrogenUsing a Spectroscopeand High Speed ICCDCamera

A. Hayashi, AoyamaGakuin University,Kanagawa, Japan

0830AIAA-2004-0485 Modeling SurfaceOxidation in TransientAerothermal HeatingEnvironments

J. Marschall, SRIInternational, MenloPark, CA

0900AIAA-2004-0486 Aeroheating Analysis forthe Afterbody of a TitanProbe

J. Olejniczak, NASAAmes Research Center,Moffett Field, CA

0930AIAA-2004-0487 Comparison of EnthalpyDetermination Methodsfor an Arc- Jet Facility

C. Park, ELORET Corp.,Moffett Field, CA

1000AIAA-2004-0488 A NumericalInvestigation onAerodynamic Propertyand Heat TransferEnhancement forSurfaces with ConcaveCavities

G. Lee, North CarolinaA&T State University,Greensboro, NC

1030AIAA-2004-0489 The IntegratedHypersonicAeromechanics ToolThermal Module

R. Morris, AdvatechPacific Inc., Redlands,CA

1100AIAA-2004-0490 Heat TransferCoefficients on a FlatSurface Impinged by theUnder- expanded SonicJet

M. Yu, Yonsei Univ.,Seoul, South Korea

1130AIAA-2004-0491 Improvement of AircraftAerodynamic Propertiesby Energy Supply intoAirflow when UsingHighly Efficient PlasmaGenerators

V. Ivanov, St.Petersburg StateUniversity,Saint-Petersburg, Russia

Chaired by: E. MAROTTA, Texas A&M University, College Station, TX, and M. YOVANOVICH, University of Waterloo, Waterloo, Canada0800AIAA-2004-0492 A Liquid Cooler Modulewith Carbon Foam forElectronics CoolingApplications

Y. Cao, FloridaInternational University,Miami, FL

0830AIAA-2004-0493 Fluid Flow and HeatTransfer from aCylinder BetweenParallel Planes:Analytical Approach

W. Khan, University ofWaterloo, Waterloo,Canada

0900AIAA-2004-0494 Numerical andExperimental PIV/PLIFStudies of EntropyProduction in NaturalConvection

O. Adeyinka, UniversityOf Manitoba, Winnipeg,Canada

0930AIAA-2004-0495 Application of aSensitivity EquationMethod to TransientNon- Linear HeatConduction

H. Hristova, EcolePolytechnique deMontreal, Montreal,Canada

1000AIAA-2004-0496 Analytical Modeling ofNatural Convection inConcentric SphericalEnclosures

P. Teertstra, Universityof Waterloo, Waterloo,Canada

1030AIAA-2004-0497 Natural Convection inRectangular LayeredPorous Cavities

J. Leong, University ofOklahoma, Norman, OK

1100AIAA-2004-0498 Parallel Computation ofMicroscale HeatConduction in Thin Films

S. Srinivasan, ClemsonUniversity, Clemson, SC

1130AIAA-2004-0499 Effects of Rib Turbulatoron Heat/Mass Transferfor Impingement/EffusionCooling with Crossflow

D. Rhee, YonseiUniversity, Seoul, SouthKorea


Tuesday Morning / 06 January 2004 Session 74-WE-3 Loads and Modeling Ruby

Tuesday Morning / 06 January 2004 Session 75-WIG-3 Boundary Layer Plasma Flow Control Teton

Tuesday Morning / 06 January 2004 1200 - 1400 Awards Luncheon Silver State Pavilion


Chaired by: A. WRIGHT, National Renewable Energy Laboratory, Golden, CO0800AIAA-2004-0500 Update of the Long-Term Inflow andStructural Test Program

H. Sutherland, SandiaNational Laboratories,Albuquerque, NM

0830AIAA-2004-1370 Wind Turbine ADAMSModel LinearizationIncluding Rotational andAerodynamic Effects

T. McCoy, GlobalEnergy Concepts LLC,Kirkland, WA

0900AIAA-2004-0502 A Comparison of WindTurbine Design Loads inDifferent Environmentsusing Inverse Reliability

K. Saranyasoontorn,University of Texas atAustin, Austin, TX

0930AIAA-2004-0503 Quantifying Uncertaintyin Estimates of ExtremeWind Turbine Loads

L. Fitzwater, StanfordUniversity, Stanford, CA

1000AIAA-2004-0504 New Developments forthe NWTC's FASTAeroelastic HAWTSimulator

J. Jonkman, NationalRenewable EnergyLaboratory, Golden, CO

1030AIAA-2004-0505 Stability Analysis ofThree- Bladed TurbinesUsing an EigenvalueApproach

M. Hansen, RisoeNational Laboratory,Roskilde, Denmark

1100AIAA-2004-0506 Ramifications ofAeroelastic AnalysisApproximations asBlade DesignsApproach StabilityBoundaries

D. Lobitz, SandiaNational Laboratories,Albuquerque, NM

1130AIAA-2004-1369 Passive Pitch Control ofSmall Horizontal AxisWind Turbines

J. Hertel, NorwegianAgricultural University,Ås, Norway

Chaired by: U. MEHTA, NASA Ames Research Center, Moffett Field, CA, and Y. GOLOVACHEV, IOFFE, St. Petersburg, Russia0800AIAA-2004-0508 Magneto- Fluid-Dynamics Interaction forHypersonic Flow Control

J. Shang, Wright StateUniversity, Dayton, OH

0830AIAA-2004-0509 Effect of SurfacePlasma Discharges onBoundary Layers atMach 5

R. Kimmel, Air ForceResearch Laboratory,Wright-Patterson AFB,OH

0900AIAA-2004-0510 Lorentz Force Effect ona Supersonic IonizedBoundary Layer

R. Meyer, Ohio StateUniversity, Columbus,OH

0930AIAA-2004-0511 Electromagnetic Controlof UnstableDisturbances in aWeakly Ionized EntropyLayer

D. Gaitonde, Air ForceResearch Laboratory,Wright-Patterson AFB,OH

1000AIAA-2004-0512 Study of Friction andSeparation Control bySurface Plasma

S. Leonov, IVTAN,Moscow, Russia

1030AIAA-2004-0513 Microwave Dischargesin Supersonic PlasmaAerodynamics

V. Shibkov, MoscowState University,Moscow, Russia

1100AIAA-2004-0514 Energy Deposition inSupersonic Cavity Flow

S. Aradag, RutgersUniversity, Piscataway,NJ

1130AIAA-2004-0515 MHD Control of theSeparationPhenomenon in aSupersonic XenonPlasma Flow II

S. Bobashev, The IoffeInstitute, St. Petersburg,Russia

The Small Business Forum

Chaired by: A. LYRINTZIS, Purdue University, West Lafayette, IN1400 1430 1500 1530 1600 1630 1700 1730


Tuesday Afternoon / 06 January 2004 1400 - 1800 Career Workshop—Managing Your Career in the 21st Century Crystal 5

Tuesday Afternoon / 06 January 2004 Session 76-AA-4 Computational Aeroacoustics N7

Tuesday Afternoon / 06 January 2004 Session 77-ABP-5 NPARC Alliance/Wind Code Whitney


The Small Business Forum

Chaired by: A. LYRINTZIS, Purdue University, West Lafayette, IN1400AIAA-2004-0516 Effects of Inflow Forcingon Jet Noise UsingLarge Eddy Simulation

P. Lew, PurdueUniversity, WestLafayette, IN

1430AIAA-2004-0517 Coupling of IntegralAcoustics Methods withLES for Jet NoisePrediction

A. Uzun, PurdueUniversity, WestLafayette, IN

1500AIAA-2004-0518 Computational StudiesSupporting Concepts forSupersonic Jet NoiseReduction

D. Kenzakowski,Combustion Researchand Flow TechnologyInc., Dublin, PA

1530AIAA-2004-0519 A Study of Dispersion-Relation- Preservingand OptimizedPrefactored CompactSchemes for WaveEquations

M. Popescu, Universityof Florida, Gainesville,FL

1600AIAA-2004-0520 3D Computation ofNoise Propagation fromDucted Fans Using aSpectral Element Method

F. Taghaddosi, McGillUniversity, Montreal,Canada

1630AIAA-2004-0521 Unsteady Validation of aMean Flow BoundaryCondition forComputationalAeroacoustics

R. Hixon, University ofToledo, Toledo, OH

1700AIAA-2004-0522 High- OrderDiscontinuous- GalerkinDiscretizations forComputationalAeroacoustics inComplex Domains

I. Toulopoulos,FORTH/IACM,Heraklion, Greece

1730AIAA-2004-0523 Optimum Attenuation ofFan Tone NoiseRadiation

C. Breard, AnalyticalMethods Inc., Redmond,WA

Chaired by: D. YODER, NASA Glenn Research Center, Cleveland, OH, and M. MANI, The Boeing Company, Saint Louis, MO1400AIAA-2004-0524 A Structured andHybrid- unstructuredGrid Euler and Navier-Stokes Solver forGeneral Geometry

M. Mani, The BoeingCompany, St. Louis, MO

1430AIAA-2004-0525 Wind- US FlowCalculations for theM2129 S- duct UsingStructured andUnstructured Grids

S. Mohler, QSS GroupInc., Cleveland, OH

1500AIAA-2004-0527 Recent Improvements tothe Wind(- US) Code atAEDC

C. Nelson, AerospaceTesting Alliance, ArnoldAFB, TN

1530AIAA-2004-0528 A Comparison of SteadyState and TimeAccurate CFD Methodsfor the PerformancePrediction of aTransonic Pitot Inlet

J. Ladd, The BoeingCompany, St. Louis, MO

1600AIAA-2004-0529 Validation andComparison of WINDand DPLR Results forHypersonic, LaminarProblems

M. MacLean,Calspan-UB ResearchCenter, Buffalo, NY

1630AIAA-2004-0530 Computational Study ofAxisymmetric Off-Design Nozzle Flows

T. DalBello, NASAGlenn Research Center,Cleveland, OH

1700AIAA-2004-0531 CFD Studies on FlowThrough Nozzles UsingWIND at Low MachNumbers

M. Patel, OrbitalResearch Inc.,Cleveland, OH

Chaired by: R. STUEVER, The Boeing Company, Wichita, KS1400 1500 1530 1600 1630 1700 1730


Tuesday Afternoon / 06 January 2004 Session 78-AD-1 Aircraft Design: Prospects, Methods, and Techniques Tahoe

Tuesday Afternoon / 06 January 2004 Session 79-AFM-4 Flight Control Methods Sierra 1

Tuesday Afternoon / 06 January 2004 Session 80-AMT-3 / SEN-1 Photonic Sensors and Sensing Techniques for Aerospace Sierra 2


Chaired by: R. STUEVER, The Boeing Company, Wichita, KS1400AIAA-2004-0532 Airplane Design and the Biomechanics of Flight– A More Completely Multi- DisciplinaryPerspective

J. McMasters, The Boeing Company, Seattle,WA

1500AIAA-2004-0533 Aerodynamic ShapeOptimization ofComplete AircraftConfigurations usingUnstructured Grids

A. Jameson, StanfordUniversity, Stanford, CA

1530AIAA-2004-0534 Modern Use ofSpreadsheet Methodsfor Aircraft Design,Sizing, and PerformanceAnalysis

D. Raymer, ConceptualResearch Corporation,Sylmar, CA

1600AIAA-2004-0535 Formulation of a Multi-Mission SizingMethodology forCompetingConfigurations

D. Mavris, GeorgiaInstitute of Technology,Atlanta, GA

1630AIAA-2004-0536 Aircraft ConfigurationDesign Using aMultidisciplinaryOptimization Approach

C. Rao, NationalUniversity of Singapore,Singapore, Singapore

1700AIAA-2004-0537 Feasibility Improvementof the Design SpaceUsing ProbabilisticMethod

Y. Jeon, Seoul NationalUniversity, Seoul, SouthKorea

1730AIAA-2004-0538 Quantification of theElements in theRelationship Matrix, aConceptual Study ofAircraft Fuel System

H. Gavel, SaabAerospace, Linköping,Sweden

Chaired by: S. BALAKRISHNAN, University of Missouri-Rolla, Rolla, MO1400AIAA-2004-0539 Autonomous Control of aMicro- Aircraft Networkin an AtmosphericBoundary Layer

A. Dorgan, University ofIllinois atUrbana-Champaign,Urbana, IL

1430AIAA-2004-0540 Spacecraft Position andAttitude Control withtheta- D Technique

M. Xin, University ofMissouri-Rolla, Rolla,MO

1500AIAA-2004-0541 Modeling andSimulation of theNonlinear DynamicBehavior of a FlappingWings Micro- Aerial-Vehicle

K. Sibilski, Air ForceInstitute of Technology,Warsaw, Poland

1530AIAA-2004-0542 Falling Leaf MotionSuppression in the F/A-18 Hornet with RevisedFlight Control Software

M. Heller, The BoeingCompany, St. Louis, MO

Chaired by: C. FITZPATRICK, Rice Systems Inc, Huntington Beach, CA, and M. WERNET, NASA Glenn Research Center, Cleveland, OH1400AIAA-2004-0544 A Distributed SensingTechnique forAerospace Applications

R. Duncan, LunaInnovations, Blacksburg,VA

1430AIAA-2004-0545 Design, Analysis, andInitial Tests of a Fiber-Optic Shear Gage for3D, High- TemperatureFlows

M. Orr, Virginia Tech,Blacksburg, VA

1500AIAA-2004-0546 Development of a Non-Intrusive TemperatureSensor in a Model GasTurbine Combustor

T. Jenkins, MetroLaserInc., Irvine, CA

1530AIAA-2004-0547 From Pulsed LaserVibrometer to OpticalDoppler Velocimeter:Laser Metrology UsingPhoto- EMF Sensors

C. Wang, BrimroseCorp. of America,Baltimore, MD

1600AIAA-2004-0548 Detection of ExplosiveMixtures in the Ullage ofAircraft Fuel Tanks

S. Chen, SouthwestSciences Inc., Santa Fe,NM

1630AIAA-2004-0549 Waveguide- BasedInertial NavigationSensor Architecture

C. Fitzpatrick, RiceSystems Inc.,Huntington Beach, CA

1700AIAA-2004-0551 High- Temperature,Fiber Optic Sensor Suitefor Air BreathingPropulsion Applications

R. Fielder, LunaInnovations Inc.,Blacksburg, VA

Chaired by: J. VASSBERG, The Boeing Company, Huntington Beach, CA, and D. MAVRIPLIS, National Institute of Aerospace, Hampton, VA


Tuesday Afternoon / 06 January 2004 Session 81-APA-9 Drag Prediction Workshop II: Summary Session II Carson 1

Tuesday Afternoon / 06 January 2004 Session 82-ASE-4 Iced Airfoil Flowfields: Measurements and Predictions N5

Tuesday Afternoon / 06 January 2004 Session 83-EDU-2 Education: Improving Conceptual Understanding N10


Chaired by: J. VASSBERG, The Boeing Company, Huntington Beach, CA, and D. MAVRIPLIS, National Institute of Aerospace, Hampton, VA1400AIAA-2004-0552 Drag Prediction with theZeus/CFL3D System(Invited)

E. Tinoco, BoeingCommercial Airplanes,Seattle, WA

1430AIAA-2004-0553 Drag, Lift, and MomentEstimates of TransonicAircraft Using theNavier- Stokes Equations

S. Klausmeyer, CessnaAircraft Company,Wichita, KS

1500AIAA-2004-0554 Transonic DragPrediction on a DLR- F6Transport ConfigurationUsing Unstructured GridSolvers

E. Lee-Rausch, NASALangley, Hampton, VA

1530AIAA-2004-0555 Summary of Data fromthe Second AIAA CFDDrag PredictionWorkshop (Invited)

K. Laflin, CessnaAircraft Company,Wichita, KS

1600AIAA-2004-0556 Statistical Analysis of CFD Solutions from 2ndDrag Prediction Workshop (Invited)

M. Hemsch, NASA Langley Research Center,Hampton, VA

1700AIAA-2004-0557 Reflections on theSecond Drag PredictionWorkshop

N. Pfeiffer, RaytheonAircraft Co., Wichita, KS

Chaired by: J. TSAO, Ohio Aerospace Institute, Cleveland, OH1400AIAA-2004-0559 Flowfield MeasurementsAbout an Airfoil withLeading- edge IceShapes

A. Broeren, University ofIllinois atUrbana-Champaign,Urbana, IL

1430AIAA-2004-0560 CFD Analysis of theAerodynamics of aBusiness- Jet Airfoil withLeading- Edge IceAccretion

X. Chi, Michigan StateUniversity, EastLansing, MI

1500AIAA-2004-0561 A Computational IcingEffects Study for aThree- Dimensional Wing

D. Thompson,Mississippi StateUniversity, MississippiState, MS

1530AIAA-2004-0562 Unsteady FlowfieldAbout an Iced Airfoil

H. Gurbacki, Universityof Illinois atUrbana-Champaign,Urbana, IL

1600AIAA-2004-0563 Numerical Simulation ofIcing Clouds in theNASA Glenn IcingResearch Tunnel

C. Bhargava, Universityof Illinois atUrbana-Champaign,Urbana, IL

1630AIAA-2004-0564 Detached EddySimulations for Airfoilwith Ice Shapes

J. Pan, University ofIllinois atUrbana-Champaign,Urbana, IL

1700AIAA-2004-0565 Water ImpingementExperiments on aNACA 23012 Airfoil withSimulated Glaze IceShapes

M. Papadakis, WichitaState University,Wichita, KS

1730AIAA-2004-0566 Grid Sensitivity Effectsin Collection EfficiencyComputation

L. Santos, EMBRAER,Sao Jose Dos Campos,Brazil

Chaired by: D. DARMOFAL, Massachusetts Institute of Technology, Cambridge, MA1400AIAA-2004-0570 Some Useful ConceptualAspects in FlightMechanics

M. Ananthasayanam,Indian Institute ofScience, Bangalore, India

1430AIAA-2004-0571 A Relook at theConcepts andCompetence of theKalman Filter

M. Ananthasayanam,Indian Institute ofScience, Bangalore, India

Chaired by: D. WILLIAMS, Illinois Institute of Technology, Chicago, IL, and D. MACMARTIN, Caltech, Pasadena, CA1400 1430 1500 1530 1600 1630 1700 1730


Tuesday Afternoon / 06 January 2004 Session 84-FD-16 Closed-Loop Flow Control: Algorithms and Applications Carson 3

Tuesday Afternoon / 06 January 2004 Session 85-FD-171400 - 1800 Modeling Versus Design for Micro Fluidics in Bio-Chem Applications Carson 4

Tuesday Afternoon / 06 January 2004 Session 86-FD-18 Numerical Treatment of Boundary Conditions Crystal 1


Chaired by: D. WILLIAMS, Illinois Institute of Technology, Chicago, IL, and D. MACMARTIN, Caltech, Pasadena, CA1400AIAA-2004-0572 Real- time AdaptiveControl of Flow- inducedCavity Tones (Invited)

M. Kegerise, NASALangley ResearchCenter, Hampton, VA

1430AIAA-2004-0573 Controller Design forActive Closed- LoopControl of Cavity Flows

H. Ozbay, Ohio StateUniversity, Columbus,OH

1500AIAA-2004-0575 Control Issues inReduced- OrderFeedback Flow Control

K. Cohen, US Air ForceAcademy, US Air ForceAcademy, CO

1530AIAA-2004-0576 Exploring Strategies forClosed- Loop CavityFlow Control

M. Samimy, Ohio StateUniversity, Columbus,OH

1600AIAA-2004-0577 Closed- loop Control ofVortex Shedding in aSeparated DiffuserUsing an Inverse Method

T. Suzuki, CaliforniaInstitute of Technology,Pasadena, CA

1630AIAA-2004-0578 Determination of anEffective SensorConfiguration forSuppression of the vonKarman Vortex Street

J. Cameron, U.S. AirForce Academy, U.S.Air Force Academy, CO

1700AIAA-2004-0579 Models for ControllingAirfoil Lift and Drag

H. Carlson, ClearScience Corp., Harford,NY

1730AIAA-2004-0580 Feedback Control of aCircular Cylinder Wakein a Water TunnelExperiment

S. Siegel, US Air ForceAcademy, ColoradoSprings, CO

Chaired by: B. SHAPIRO, University of Maryland, College Park, MDThe goal of this workshop is to identify future needs in modeling of micro fluidic systems from a system design perspective. In other words, what form should micro fluidic models take, and how should they becreated, to allow analysis, design, control, and optimization of the entire system? The workshop brings together micro fluidic modeling researchers with experts in system analysis, system design, and control.

The second session of this two session workshop will focus on biological and chemical microscale applications such as bio/chem sensing and detection, along with a discussion of the integration of underlyingtechnologies such as pumping, valving, mixing, and separation of fluids.

1300 - Numerical Modeling of Electrochemical Microchannel Flow: Protein Labeling and Dispersion Under Non-Ideal Conditions, O. Knio, Johns Hopkins University1330 - Flow Control on the Micro-Scale for Bio-Chemical Sensing and Actuation, B. Shapiro, University of Maryland1400 - Multi-Physics, Multi-Resolution Numerical Tools for Analysis and Design of Bio-MEMS, M. Athavale, CFDRC1430 - Break1500 - Moderated Discussion, B. Bamieh, T. Conlisk, C. Eggleton, B. Shapiro, and S. Wereley1630 - Wrap-up and Summary + Recommendations for Future Research

Chaired by: D. TAFTI, Virginia Tech, Blacksburg, VA1400AIAA-2004-0581 An Embedded BoundaryCartesian Grid Schemefor Viscous Flows Usinga New Viscous WallBoundary ConditionTreatment

D. Marshall, GeorgiaInstitute of Technology,Atlanta, GA

1430AIAA-2004-0582 Wall Function BoundaryConditions IncludingHeat Transfer andCompressibility forTransport TurbulenceModels

R. Nichols, University ofAlabama atBirmingham,Birmingham, TN

1500AIAA-2004-0583 A New Inviscid WallBoundary ConditionTreatment forEmbedded BoundaryCartesian Grid Schemes

D. Marshall, GeorgiaInstitute of Technology,Atlanta, GA

1530AIAA-2004-0584 Flutter Prediction by aCartesian Mesh EulerMethod with SmallPerturbation GridlessBoundary Conditions

D. Kirshman, Universityof California Irvine,Irvine, CA

1600AIAA-2004-0585 Far- field Coarseningand Mesh Adaptation forInviscid Flows onCartesian Grids

A. Dadone, Politecnicodi Bari, Bari, Italy

1630AIAA-2004-0586 Local Grid Refinementfor an ImmersedBoundary RANS Solver

G. Iaccarino, StanfordUniversity, Stanford, CA

1700AIAA-2004-0587 Dynamic SurfaceRoughness forAerodynamic FlowControl

W. Huebsch, WestVirginia University,Morgantown, WV


Tuesday Afternoon / 06 January 2004 Session 87-FD-19 Transition and Other Applications of Eddy-Resolving Methods Crystal 2

Tuesday Afternoon / 06 January 2004 Session 88-GT-2 Advancements in Measurement Techniques Crystal 3


Chaired by: K. SQUIRES, Arizona State University, Tempe, AZ, and R. JOSLIN, Office of Naval Research, Arlington, VA1400AIAA-2004-0588 Direct NumericalSimulation of UnstableDisturbances inSupersonic BoundaryLayer

I. Egorov, MoscowInstitute of Physics andTechnology, Zhukovsky,Russia

1430AIAA-2004-0589 Direct NumericalSimulations ofCrossflow Disturbancesin Supersonic BoundaryLayers

L. Jiang, University ofTexas at Arlington,Arlington, TX

1500AIAA-2004-0590 Direct NumericalSimulation of FlowTransition over a FlatPlate

S. Deng, University ofTexas at Arlington,Arlington, TX

1530AIAA-2004-0591 Inflow Conditions forNumerical Simulationsof Bypass Transition

V. Ovchinnikov,University of Maryland,College Park, MD

1600AIAA-2004-0592 Computation of BluntBody Wake Flow byVorticity Confinement

M. Fan, University ofTennessee SpaceInstitute, Tullahoma, TN

1630AIAA-2004-0593 Instability Mechanismsin Supersonic BaseFlows

R. Sandberg, Universityof Arizona, Tucson, AZ

1700AIAA-2004-0594 Implicit Large EddySimulation of aSubsonic Flow AroundNACA0012 Airfoil

S. Komurasaki, NihonUniversity, Tokyo, Japan

1730AIAA-2004-0595 DNS of 3D TurbulentNatural ConvectionFlows Using Low CostParallel Computers

F. Trias, TechnicalUniversity of Catalonia,Terrassa, Spain

1800AIAA-2004-0596 Forced Couette FlowSimulations Using DSMC

W. Liou, WesternMichigan University,Kalamazoo, MI

Chaired by: N. VERHAAGEN, Delft University of Technology, Delft, The Netherlands, and M. KAMMEYER, The Boeing Company, Saint Louis, MO1400AIAA-2004-0598 Molecular ImageSensing for Pressureand TemperatureSurface Mapping ofAerodynamic Flows

C. Wong, UMIST,Manchester, GreatBritain

1430AIAA-2004-0599 Surface Heat TransferMeasurements by LIF inReactive Flows

K. Kontis, University ofManchester,Manchester, GreatBritain

1500AIAA-2004-0600 Development andCharacterization of aLow- PressureCalibration System forHypersonic WindTunnels

D. Green, NASALangley ResearchCenter, Hampton, VA

1530AIAA-2004-0603 Factors InfluencingCamera Selection forthe Boeing Pressure-Sensitive Paint System

N. Brown, The BoeingCompany, St. Louis, MO

1600AIAA-2004-0604 The Effect ofLens/Aperture Selectionon Phase DopplerAnemometerMeasurements

J. Davis, University ofCincinnati, Cincinnati,OH

Chaired by: T. BRESSLER, The Boeing Company, Seattle, WA, and J. PATRICK, Lockheed Martin, Smyrna, GA1400 1430 1500 1530 1600


Tuesday Afternoon / 06 January 2004 Session 89-GT-3 Wall Interference and Measurement Techniques Crystal 4

Tuesday Afternoon / 06 January 2004 Session 90-ICG-1 Computational Analysis and Visualization Carson 2

Tuesday Afternoon / 06 January 2004 Session 91-MDO-4 MDO Applications N9


Chaired by: T. BRESSLER, The Boeing Company, Seattle, WA, and J. PATRICK, Lockheed Martin, Smyrna, GA1400AIAA-2004-0605 Validation of a WallInterference CorrectionSystem for a TransonicWind Tunnel

N. Ulbrich, SverdrupTechnology Inc., MoffettField, CA

1430AIAA-2004-0606 Streamwise MomentumAnalysis of SubsonicWall Interference onFlat- Plate Wings at HighAngles of Attack

M. Mokry, NationalResearch Council,Ottawa, Canada

1500AIAA-2004-0608 Slot WidthAugmentation in aSlotted- Wall TransonicLinear Cascade WindTunnel

A. Rona, University ofLeicester, Leicester,Great Britain

1530AIAA-2004-0609 Boundary InterferenceAssessment andCorrection for OpenTest Section WindTunnels Using PanelMethods

W. Mokhtar, OldDominion University,Norfolk, VA

1600AIAA-2004-1359 Skin FrictionMeasurements Using OilFilm Interferometry in the11' Transonic WindTunnel at NASA Ames

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

Chaired by: J. CHAWNER, Pointwise, Inc., Fort Worth, TX1400AIAA-2004-0610 Using Quilts and Chainsto Improve Structuredand UnstructuredSurface Grids

J. Dannenhoffer,Syracuse University,Syracuse, NY

1430AIAA-2004-0611 Toward a GlobalParameterization forQuilted CAD Entities

W. Jones, NASALangley ResearchCenter, Hampton, VA

1500AIAA-2004-0612 A Structured GridQuality Measure forSimulated HypersonicFlows

S. Alter, NASA LangleyResearch Center,Hampton, VA

1530AIAA-2004-0613 HierarchicalUnstructured MeshGeneration

S. Karman, University ofTennessee atChattanooga,Chattanooga, TN

1600AIAA-2004-0614 A Mesh MovementAlgorithm for HighQuality GeneralisedMeshes

D. Martineau, AircraftResearch AssociationLimited, Bedford, GreatBritain

1630AIAA-2004-0615 A Post- Processor toRender TurbomachineryFlows Using Phase- LagSimulations

X. Wang, MississippiState University,Starkville, MS

1700AIAA-2004-0616 An Integrated SimulationEnvironment for CFDand OtherComputationalDisciplines

R. Noack, University ofAlabama at Birmingham,Bel Air, MD

Chaired by: B. GROSSMAN, National Institute of Aerospace, Hampton, VA, and R. CANFIELD, Air Force Institute of Technology, Wright-Patterson AFB, OH1400AIAA-2004-0618 System LevelOptimization in theIntegrated HypersonicAeromechanics Tool(IHAT)

M. Baker, JacobsSverdrup, Long Beach,CA

1430AIAA-2004-0619 Multi- DisciplinaryOptimization Method foran Innovative MultiNozzle (MNG) Design

D. Chasman, RaytheonMissile Systems,Tucson, AZ

1500AIAA-2004-0620 Aerodynamical OptimalShapes Design ofIntegrated FlyingConfigurations inSupersonic Flow

A. Nastase,RWTH-Aachen, Aachen,Germany

1530AIAA-2004-0621 An Engineering Methodfor the Design ofOptimized Aircraft WingStructures

F. Ferguson, NorthCarolina A&T StateUniversity, Greensboro,NC

1600AIAA-2004-0622 Fleet Assignment UsingCollective Intelligence

N. Antoine, StanfordUniversity, Stanford, CA

1630AIAA-2004-0624 Optimal Shape Designof a Pressure- DrivenCurved Micro Channel

S. Lim, Seoul NationalUniversity, Seoul, SouthKorea

Chaired by: M. GLICKSMAN, Rensselaer Polytechnic Institute, Troy, NY, and R. SCHLAGHECK, NASA Marshall Space Flight Center, Huntsville, AL


Tuesday Afternoon / 06 January 2004 Session 92-MSSP-3 Microgravity Materials Science I N6

Tuesday Afternoon / 06 January 2004 Session 93-PC-7 Combustion Control Shasta 1

Tuesday Afternoon / 06 January 2004 Session 94-PC-8 Soot and Combustion Diagnostics Shasta 2

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:

Chaired by: M. GLICKSMAN, Rensselaer Polytechnic Institute, Troy, NY, and R. SCHLAGHECK, NASA Marshall Space Flight Center, Huntsville, AL1400AIAA-2004-0626 Mushy Zones EvolutionUnder MicrogravityConditions

A. Lupulescu,Rensselaer PolytechnicInstitute, Troy, NY

1430AIAA-2004-0627 Bubble Formation andTransport DuringDirectional Solidificationin Microgravity: ModelExperiments on theSpace Station

R. Grugel, NASAMarshall Space FlightCenter, Huntsville, AL

1500AIAA-2004-0628 Effect of VariableDensity in DendriticSolidification

P. Zhao, University ofArizona, Tucson, AZ

1530AIAA-2004-0629 Faceting Simulation ofBulk Crystal Growth with2d Nucleation andScrew Dislocation Theory

Y. Ma, SUNY StonyBrook, Stony Brook, NY

1600AIAA-2004-0630 Simulating the Effect ofSpace VehicleEnvironments onDirectional Solidificationof a Binary Alloy

D. Westra, NASAMarshall Space FlightCenter, Huntsville, AL

1630AIAA-2004-0631 Numerical Simulationsof Transient InterfacialPhenomena in MiscibleFluids

N. Bessonov, UniversiteLyon I, Lyon, France

1700AIAA-2004-0632 The MicrogravityScience Glovebox

C. Baugher, NASAMarshall, Huntsville, AL

Chaired by: H. CHELLIAH, University of Virginia, Charlottesville, VA, and K. MCMANUS, General Electric Corporate R&D Center, Niskayuna, NY1400AIAA-2004-0633 SimultaneousCombustion Instabilityand Emissions ControlUsing Air and FuelModulation

A. Wachsman,Massachusetts Instituteof Technology,Cambridge, MA

1430AIAA-2004-0634 OPEN LOOPCONTROL OF SEVERECOMBUSTIONINSTABILITIES BYFUEL FLOWMODULATION AT NONRESONANTFREQUENCIES

E. Lubarsky, GeorgiaInstitute of Technology,Atlanta, GA

1500AIAA-2004-0635 Combustion Instabilitiesand Control of a Multi-Swirl AtmosphericCombustor

T. Yi, University ofCincinnati, Cincinnati,OH

1530AIAA-2004-0636 Control of CombustionInstability andEmissions by Burner'sExit GeometryModifications

C. Paschereit, TechnicalUniversity Berlin, Berlin,Germany

1600AIAA-2004-0637 Blowout Control inTurbine EngineCombustors

T. Muruganandam,Georgia Institute ofTechnology, Atlanta, GA

1630AIAA-2004-0638 SystemsCharacterization ofCombustor Instabilitieswith Controls DesignEmphasis

G. Kopasakis, NASAGlenn, Cleveland, OH

1700AIAA-2004-0639 Experimental Study ofPOD- based Control forCombustion InstabilityUsing a LinearPhotodiode Array

S. Park, MassachusettsInstitute of Technology,Cambridge, MA

1730AIAA-2004-0640 Optimization ofOscillatory Flame in aSwirler CombustorUsing an Active ControlMethod

H. Sato, AoyamaGakuin University,Kanagawa, Japan

Chaired by: H. MONGIA, GE Aircraft Engines, Cincinnati, OH, and M. SMOOKE, Yale University, New Haven, CT1400AIAA-2004-0641 Effects of FlowProperties on SootFormation andOxidation Rates inFlame Environments

C. Kim, University ofMichigan, Ann Arbor, MI

1430AIAA-2004-0642 Fuel Jet Dilution Effectson the SootingCharacteristics ofPropylene DiffusionFlames near the SmokePoint

S. Goh, University ofOklahoma, Norman, OK

1500AIAA-2004-0643 Modeling of SootPrecursor and EarlyStage Soot Formation

N. Slavinskaya,DLR-German AerospaceCenter, Stuttgart,Germany

1530AIAA-2004-0644 Influence of the FuelNozzle Material on SootFormation andTemperature Field inCoflow LaminarDiffusion Flames

Ö. Gülder, University ofToronto, Toronto,Canada

1600AIAA-2004-0645 Modeling Soot in a SwirlCombustor

V. Katta, InnovativeScientific Solutions Inc,Dayton, OH

1630AIAA-2004-0647 Wavelength ModulationAbsorptionSpectroscopy with 2fDetection forCombustionTemperatureMeasurements UsingMultiplexed Near-Infrared Diode Lasers

J. Liu, StanfordUniversity, Stanford, CA

1700AIAA-2004-0648 Influence of projectionwidth and spatialgradient of concentrationon AlgebraicReconstructionTomography (ART) forMeasurements ofHydrocarbon Fuel/AirMixtures

B. Gillet, ImperialCollege, London, GreatBritain


http://www.aiaa.org/agenda.cfm?lumeetingid=665&dateget=all#session2644.

Chaired by: H. KRIER, University of Illinois at Urbana-Champaign, Urbana, IL1400 1430 1500 1530 1600

Chaired by: J. REUTHER, NASA Ames Research Center, Moffett Field, CA, and R. THOMPSON, NASA Langley Research Center, Hampton, VA1400 1430

Chaired by: T. SHIH, Iowa State University, Ames, IA, and F. MASHAYEK, University of Illinois at Chicago, Chicago, IL1400 1500 1530 1600 1630 1700 1730


Tuesday Afternoon / 06 January 2004 Session 95-PDL-4 Laser & Plasma Propulsion II N8

Tuesday Afternoon / 06 January 2004 Session SS-1 Aerothermal Analysis Supporting the Space Shuttle Columbia Investigation

Tuesday Afternoon / 06 January 2004 Session 97-TES-4 Standards for CFD in the Aerospace Industry N4


Chaired by: H. KRIER, University of Illinois at Urbana-Champaign, Urbana, IL1400AIAA-2004-0649 BENEFIT OFCONSTANTMOMENTUMPROPULSION FORLARGE AV MISSIONS -APPPLICATION INLASER PROPULSION

C. Larson, Air ForceResearch Laboratory,Edwards AFB, CA

1430AIAA-2004-0650 Laser ImpulseGeneration in Flight

A. Sasoh, TohokuUniversity, Sendai,Japan

1500AIAA-2004-0651 Specific Impulse ofAblative LaserPropulsion

A. Pakhomov, Universityof Alabama in Huntsville,Huntsville, AL

1530AIAA-2004-0652 A Virtual TestingEnvironment for ElectricPropulsion- SpacecraftInteractions

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

1600AIAA-2004-0653 Computational Analysison Nozzle Performanceof a RP Laser Thruster

H. Katsurayama,University of Tokyo,Tokyo, Japan

Chaired by: J. REUTHER, NASA Ames Research Center, Moffett Field, CA, and R. THOMPSON, NASA Langley Research Center, Hampton, VA1400AIAA-2004-1387 ExperimentalAerothermodynamics inSupport of the ColumbiaAccident Investigation

T. Horvath, NASALangley, Hampton, VA

1430AIAA-2004-1384 ComputationalAerothermodynamicAnalysis for the STS-107 AccidentInvestigation

J. Reuther, NASA AmesResearch Center, MoffettField, CA

Chaired by: T. SHIH, Iowa State University, Ames, IA, and F. MASHAYEK, University of Illinois at Chicago, Chicago, IL1400AIAA-2004-0654 AIAA Committee on Standards forComputational Fluid Dynamics – Status andPlans

C. Rahaim, Yuma Proving Grounds, Yuma, AZ

1500AIAA-2004-0655 Verification andValidation ofPseudospectral ShockFitted Simulations ofSupersonic Flow over aBlunt Body

G. Brooks, Air ForceResearch Laboratory,Wright-Patterson AFB,OH

1530AIAA-2004-0656 Estimating Grid-Induced Errors in CFDby Discrete- Error-Transport Equations

Y. Qin, Michigan StateUniversity, East Lansing,MI

1600AIAA-2004-0657 Development andValidation of a Multi-Block Flow Solver forLarge Eddy Simulationof Turbulent Flows inComplex Geometries

A. Afshari, MichiganState University, EastLansing, MI

1630AIAA-2004-0658 Numerical Simulation ofFlow and Heat Transferin a Duct with SquareRibs and Bleed Holes

X. Gu,Siemens-Westinghouse,Orlando, FL

1700AIAA-2004-0659 Validation Study of aMultidomain SpectralElement Code forSimulation of TurbulentFlows

G. Jacobs, BrownUniversity, Providence,RI

1730AIAA-2004-0660 Transient NumericalSimulation of AirflowCharacteristics ofVentilated and Air-Conditioned Spaces



Tuesday Afternoon / 06 January 2004 Session 98-WE-4 Airfoil and Rotor Aerodynamics Ruby

Tuesday Afternoon / 06 January 2004 Session 99-WIG-4 Plasma Aerodynamics Teton


Chaired by: J. LEISHMAN, University of Maryland, College Park, MD1400AIAA-2004-0661 The LS(1)- 0417MODAirfoil AerodynamicFlow Characteristcs withthe Application of VortexGenerators

J. Janiszewska, OhioState University,Columbus, OH

1430AIAA-2004-0662 RNN Blade FlowModels of the UAEHAWT BladeUndergoing HarmonicOscillations

W. Faller, AppliedSimulationTechnologies, CocoaBeach, FL

1500AIAA-2004-0663 Tip Speed RatioInfluences onRotationally AugmentedBoundary LayerTopology andAerodynamic ForceGeneration

S. Schreck, NREL'sNational WindTechnology Center,Golden, CO

1530AIAA-2004-0664 Approximate Modelingof Deep Stall Effects onYawed Rotor Loads

A. Eggers, RANN Inc.,Palo Alto, CA

1600AIAA-2004-0665 The Effect ofTurbulence Intensity onPerformance of aNACA4421 AirfoilSection

K. Swalwell, MonashUniversity, Melbourne,Australia

1630AIAA-2004-0666 A Method for Deriving3D Airfoil Characteristicsfor a Wind Turbine

C. Bak, Risoe NationalLaboratory, Roskilde,Denmark

1700AIAA-2004-0667 Toward Blade- TipVortex Simulation withan Actuator- LiftingSurface Model

C. Leclerc, Ecole deTechnologieSuperieure, Montréal,Canada

1730AIAA-2004-0668 Design and Verificationof the Riso- B1 AirfoilFamily for Wind Turbines

P. Fuglsang, RisoeNational Laboratory,Roskilde, Denmark

1800AIAA-2004-1363 Optimum Performanceof Propeller WindTurbines with Non- IdealAirfoil Sections

A. Wortman, ISTAR Inc.,Santa Monica, CA

Chaired by: J. SCHMISSEUR, Air Force Office of Scientific Research, Arlington, VA, and S. LEONOV, IVTAN, Moscow, Russia1400AIAA-2004-0669 Basics in Beamed MWEnergy Deposition forFlow/Flight Control

Y. Kolesnichenko,Institute of HighTemperatures, Moscow,Russia

1430AIAA-2004-0671 Gas Dynamic Effect ofMicrowave Discharge onSupersonic Cone-shaped Bodies

V. Lashkov, SaintPetersburg StateUniversity, SaintPetersburg, Russia

1500AIAA-2004-0672 Numerical Modeling ofthe Lateral ForceCreation by SurfaceUndercritical MicrowaveDischarge

K. Khodataev, RussianAcademy of Sciences,Moscow, Russia

1530AIAA-2004-0673 Experimental andNumerical Studies onthe use of ConcentratedEnergy Deposition forAerodynamic DragReduction Around Re-entry Bodies

K. Satheesh, IndianInstitute of Science,Bangalore, India

1600AIAA-2004-0674 Energy Transfer inHypersonic Plasma Flowand Flow StructureControl by LowTemperatureNonequilibrium Plasma

E. Anokhin, MoscowInstitute of Physics andTechnology,Dolgoprudny, Russia

1630AIAA-2004-0675 On- Board GeneratedPlasma for SupersonicFlow Study

D. Bivolaru, PolytechnicUniversity, Brooklyn, NY

1700AIAA-2004-0676 Simulating MicrowaveDiagnostics for Weaklyionized Gas

J. Shang, Wright StateUniversity, Dayton, OH


Tuesday Afternoon / 06 January 2004 Session - Durand Lectureship in Public Service Reno Ballroom

Tuesday Afternoon / 06 January 2004 1830 - 2000 Reception honoring the Dryden, Durand, and von Kármán Lectures Recipients Hilton Pavilion

Wednesday Morning / 07 January 2004 Session 100-AA-5 Resonators and Cavity Aeroacoustics N7


Chaired by: L. UKEILEY, University of Mississippi, Oxford, MS0800AIAA-2004-0677 Nonlinear Oscillationsand Flow of Gas WithinClosed and OpenConical Resonators

C. Daniels, OhioAerospace Institute,Cleveland, OH

0830AIAA-2004-0678 Actuation SignalDirectivity and SupplyPressure Effects inPowered ResonanceTubes

S. Sarpotdar, IllinoisInstitute of Technology,Chicago, IL

0900AIAA-2004-0679 Large- Eddy Simulationof a Subsonic Flow overa Cavity on GeneralUnstructured Grids

N. Bertier, ONERA,Chatillon, France

0930AIAA-2004-0680 Computation of LowSpeed Cavity Noise

C. Loh, NASA Glenn,Cleveland, OH

1000AIAA-2004-0681 Low- DimensionalEstimation of CavityFlow Dynamics

N. Murray, University ofMississippi, University,MS

1030AIAA-2004-0682 Control of TransonicCavity Flow Instabilityby Streamwise AirInjection

A. Rona, University ofLeicester, Leicester,Great Britain

1100AIAA-2004-0683 Numerical Investigationof Subsonic 2D/ 3DCavity Flows

P. Bissessur, Universityof Southampton,Southampton, GreatBritain

1130AIAA-2004-0684 Numerical Simulationsof Fluidic Control forTransonic Cavity Flows

A. Hamed, University ofCincinnati, Cincinnati,OH

Chaired by: D. JENSEN, Rolls-Royce Corporation, Indianapolis, IN, and R. RAVINDRANATH, US Navy, Patuxent River, MD0800 0830 0900 0930 1000 1030 1100

Chaired by: R. STUEVER, The Boeing Company, Wichita, KS0800 0830 0900 0930 1000


Wednesday Morning / 07 January 2004 Session 101-ABP-6 Propulsion - Experimental Whitney

Wednesday Morning / 07 January 2004 Session 102-AD-2 Aircraft Design: Design Process and Case Studies Tahoe

Wednesday Morning / 07 January 2004 Session 103-AFM-5 Aerospace Vehicle Design and Simulation I Sierra 1


Chaired by: D. JENSEN, Rolls-Royce Corporation, Indianapolis, IN, and R. RAVINDRANATH, US Navy, Patuxent River, MD0800AIAA-2004-0685 Performance ofAdvanced Fan ExitGuide Vanes with aProduct Derived Fan

J. Gazzaniga, NASAGlenn Research Center,Cleveland, OH

0830AIAA-2004-0686 ExperimentalInvestigation of Flutter ina Single StageUnshrouded Axial- FlowFan

J. Gill, University ofKentucky, Paducah, KY

0900AIAA-2004-0688 Deterioration andRetention on Coatedand UncoatedCompressor andTurbine Blades

W. Tabakoff, Universityof Cincinnati, Cincinnati,OH

0930AIAA-2004-0689 Innovative SiC- SICCeramic Liner for theTrapped VortexCombustor (TVC)Concept

J. Mehta, TKEngineering, Cincinnati,OH

1000AIAA-2004-0690 Scaling of Losses inSmall IC Aero Engineswith Engine Size

S. Menon, University ofMaryland, College Park,MD

1030AIAA-2004-0691 The JT- 2XL DieselEngine System for SmallUnmanned AerialVehicles

A. Santangelo,sci_Zone, Holland, MI

1100AIAA-2004-0692 Pressure DropDistribution in SmoothSquare Channel withRound Ended Sharp180Deg Bend in thePresence of GuideVanes

D. Ratna Rao, IndianInstitute of Technology,Guwahati, India

Chaired by: R. STUEVER, The Boeing Company, Wichita, KS0800AIAA-2004-0693 Rethinking the AirplaneDesign Process - AnEarly 21st CenturyPerspective

J. McMasters, TheBoeing Company,Seattle, WA

0830AIAA-2004-0696 Flying Ocean Giant: AMulti- Fuselage Conceptfor Ultra- Large FlyingBoat

R. Onishi, MitsubishiResearch Institute,Tokyo, Japan

0900AIAA-2004-0697 Conceptual Design of aSonic Boom ConstrainedSupersonic BusinessAircraft

D. Aronstein, RaytheonAircraft Company,Wichita, KS

0930AIAA-2004-0698 Airframe Noise ModelingAppropriate forMultidisciplinary Designand Optimization

S. Hosder, VirginiaTech, Blacksburg, VA

1000AIAA-2004-0699 Preliminary WingOptimization for VeryLarge Transport Aircraftwith WingspanConstraints

J. Dalhuijsen, DelftUniversity ofTechnology, Delft, TheNetherlands

Chaired by: P. RAO, Lockheed Martin Astronautics, Denver, CO0800AIAA-2004-0700 Fuzzy Logic TrajectoryDesign and Guidancefor Terminal AreaEnergy Management

B. Burchett,Rose-Hulman Institute ofTechnology, TerreHaute, IN

0830AIAA-2004-0701 Test Results for EntryGuidance Methods forReusable LaunchVehicles

J. Hanson, NASAMarshall Space FlightCenter, Huntsville, AL

0900AIAA-2004-0702 An Integrated Approachfor Entry Mission Designand Flight Simulations

P. Lu, Iowa StateUniversity, Ames, IA

0930AIAA-2004-0704 Aerospace VehicleTrajectory Design andOptimization Within aMulti- DisciplinaryEnvironment

R. Windhorst, NASAAmes Research Center,Moffett Field, CA

1000AIAA-2004-0705 RLV Concept EmployingStaged Rocket Engines

R. Nelson, , Los AltosHills, CA


Wednesday Morning / 07 January 2004 Session 104-AMT-4 Diagnostics for Combustion, Plasmas, and High Speed Flows Sierra 2

Wednesday Morning / 07 January 2004 Session 105-APA-10 CFD Applications I Carson 1

Wednesday Morning / 07 January 2004 Session 106-APA-11 Wind Tunnel and Flight Test Applications Carson 2


Chaired by: P. VARGHESE, University of Texas at Austin, Austin, TX0800AIAA-2004-0706 Time- AverageMolecular RayleighScattering Techniquefor Measurement ofVelocity, Density,Temperature, andTurbulence Intensity inHigh Speed NozzleFlows

A. Mielke, NASA GlennResearch Center,Cleveland, OH

0830AIAA-2004-0707 Wide- Field PIV ofPulsed Jet InjectionUpstream of Mach 2Shock Wave/BoundaryLayer Interaction

P. Bueno, University ofTexas at Austin, Austin,TX

0900AIAA-2004-0708 Diagnostics of ShortPulsed SustainedPlasmas in a Cold AirMHD Channel

S. Zaidi, PrincetonUniversity, Princeton, NJ

0930AIAA-2004-0709 TemperatureMeasurements inAtmospheric GlowDischarge Plasma

V. Stepaniuk,Polytechnic University,Brooklyn, NY

1000AIAA-2004-0710 Dual- Pump CARSThermometry andSpecies ConcentrationMeasurements in aSupersonic Combustor

S. O'Byrne, NationalResearch Council,Hampton, VA

1030AIAA-2004-0711 Single- ShotThermometry andMultiple- SpeciesMeasurements UsingDual- Pump, Dual-Broadband CARS in aLiquid- Fueled CFM56Combustor

S. Roy, InnovativeScientific Solutions Inc.,Dayton, OH

1100AIAA-2004-0713 A Wavelength-Multiplexed Diode LaserSensor for TemperatureMeasurements in PulseDetonation Engines

K. Hinckley, StanfordUniversity, Stanford, CA

Chaired by: E. FOURNIER, DRDC Valcartier, ValBelair, Canada0800AIAA-2004-0714 Propulsion SimulationsUsing AdvancedTurbulence Models withthe Unstructured- GridCFD Tool, TetrUSS

K. Abdol-Hamid, NASALangley, Hampton, VA

0830AIAA-2004-0716 A System for MovingBody CFD Simulationson Overset Structuredand Unstructured Grids

G. Power, AerospaceTesting Alliance, ArnoldAFB, TN

0900AIAA-2004-0717 Application of VorticityConfinement to InviscidMissile Force andMoment Prediction

M. Robinson,SYColeman, Huntsville,AL

0930AIAA-2004-0718 Application of VorticityConfinement toCompressible Flow

W. Dietz, Flow AnalysisInc., Estill Springs, TN

1000AIAA-2004-0719 Calibration of VorticityConfinementTechniques for MissileAerodynamics: Part I –Surface Confinement

T. Suttles, University ofAlabama in Huntsville,Huntsville, AL

1030AIAA-2004-0720 Navier- StokesSimulation of a Missilewith a Free- SpinningTail Using UnstructuredGrids

E. Blades, MississippiState University,Mississippi State, MS

1100AIAA-2004-0721 Improvement of a PanelMethod by IncludingPanel Warp

J. Nathman, AnalyticalMethods Inc., Redmond,WA

Chaired by: D. ROMAN, The Boeing Company, Huntington Beach, CA0800AIAA-2004-0722 A Wind TunnelInvestigation of OrbitalSpace PlaneConfigurations andComparison to CFDPredictions

C. Wee, U.S. Air ForceAcademy, U.S. AirForce Academy, CO

0830AIAA-2004-0724 Research Wind Tunnelof the AeronauticalInstitute of Technology:Conceptual Design andCalibration

M. Assato, InstitutoTecnológico deAeonáutica, S"ao JoséDos Campos, Brazil

0900AIAA-2004-0725 Aerodynamics ofFormation Flight

Z. Bangash, AuburnUniversity, Auburn, AL

0930AIAA-2004-0726 Lift Dump on a Fighter-Type Wing at ApproachCondition

S. Hwang, KoreaAerospace ResearchInstitute, Deajeon, SouthKorea

1000AIAA-2004-0727 Reducing Wind TunnelData for Flowfield Studyover the Wing- CanardConfiguration UsingNeural Network

A. Abbasi Hoseini,Sharif University ofTechnology, Tehran, Iran

1030AIAA-2004-0729 Unsteady Force andMoment Data on aManeuvering UnderseaVehicle

K. Granlund, VirginiaTech, Blacksburg, VA

1100AIAA-2004-0723 Flow Analysis over andBehind a Wing withDifferent Winglet Shapes

M. Nazarinia, SharifUniversity ofTechnology, Tehran, Iran


Wednesday Morning / 07 January 2004 Session 107-ASE-5 Icing Testing and Flight Characterization N5

Wednesday Morning / 07 January 2004 Session 108-FD-20 CFD Verification and Validation Carson 3

Wednesday Morning / 07 January 2004 Session 109-FD-21 Flow Control Applications Carson 4


Chaired by: H. ADDY, NASA Glenn Research Center, Cleveland, OH0800AIAA-2004-0730 Development of a TotalLiquid Water ContentProbe

C. Tan, Wichita StateUniversity, Wichita, KS

0830AIAA-2004-0731 Ice Particle Impact onCloud Water ContentInstrumentation

E. Emery, NASA GlennResearch Center,Cleveland, OH

0900AIAA-2004-0733 Aircraft Characterizationin Icing Using Flight TestData

E. Whalen, University ofIllinois at UrbanaChampaign, Urbana, IL

0930AIAA-2004-0734 AerodynamicPerformance of a SweptWing with Simulated IceShapes

M. Papadakis, WichitaState University,Wichita, KS

1000AIAA-2004-0735 Icing at the McKinleyClimatic Laboratory

J. Bell, McKinleyClimatic Laboratory,Eglin AFB, FL

1030AIAA-2004-0736 The Design, Fabrication,and Testing ofSimulated Ice Shapesfor the S- 92A Helicopter

R. Flemming, SikorskyAircraft, Stratford, CT

1100AIAA-2004-0737 Artificial Icing Tests ofthe S- 92A Helicopter inthe McKinley ClimaticLaboratory

R. Flemming, SikorskyAircraft, Stratford, CT

Chaired by: C. ROY, Sandia National Laboratories, Albuquerque, NM, and S. ABDALLAH, University of Cincinnati, Cincinnati, OH0800AIAA-2004-0738 FFT ConvergenceCriterion for UnsteadyCFD Codes

M. Ahmed, University ofConnecticut, Storrs, CT

0830AIAA-2004-0739 CFD Code VerificationUsing Least SquareExtrapolation Method

R. Vaidyanathan,University of Florida,Gainesville, FL

0900AIAA-2004-0740 On the Validation of aGlobal Preconditionerfor the Euler Equations

B. Yildirim, MississippiState University,Mississippi State, MS

0930AIAA-2004-0741 Isolating Temporal-Discretization Errors forSeparate- VerificationAnalyses

J. Brock, Los AlamosNational Laboratory, LosAlamos, NM

1000AIAA-2004-0742 Second Order Sensitivityand UncertaintyAnalysis of LaminarAirfoil Flows

J. Mahieu, EcolePolytechnique deMontreal, Montreal,Canada

1030AIAA-2004-0743 Comparison ofOperators for Newton-Krylov Method forSolving CompressibleFlows on UnstructuredMeshes

T. Smith, SandiaNational Laboratories,Albuquerque, NM

Chaired by: A. SEIFERT, TelAviv University, TelAviv, Israel, and M. AMITAY, Rensselaer Polytechnic Institute, Troy, NY0800AIAA-2004-0745 Active Flow Control onthe STINGRAY UAV:Physical Mechanisms

A. Washburn, NASALangley ResearchCenter, Hampton, VA

0830AIAA-2004-0746 Flow Control withSynthetic and PulsedJets: Applications toVirtual Aeroshaping,Thrust- Vectoring, andControl of Separationand Cavity Osciallations

R. Agarwal, WashingtonUniversity, St. Louis, MO

0900AIAA-2004-0747 Unsteady CFDModeling ofAerodynamic FlowControl over a SpinningBody with Synthetic Jet

J. Sahu, U.S. ArmyResearch Laboratory,Aberdeen ProvingGround, MD

0930AIAA-2004-0748 Simulation of SteadyCirculation Control forMarine- Vehicle ControlSurfaces

E. Paterson,Pennsylvania StateUniversity, StateCollege, PA

1000AIAA-2004-0749 Prediction of OscillatoryFlow Excitation at theLeading Edge of aModified NACA 0015Airfoil

R. Yazzie, Univ. of NewMexico, Albuquerque,NM

1030AIAA-2004-0750 Numerical Investigationof Active Flow Controlfor Low- PressureTurbine BladeSeparation

D. Postl, University ofArizona, Tucson, AZ

1100AIAA-2004-0751 Active Control of aSeparating BoundaryLayer with SteadyVortex Generating Jets -Detailed FlowMeasurements

R. Eldredge, BrighamYoung University,Provo, UT

1130AIAA-2004-0753 MagnetogasdynamicFlow Control of IrregularMach Reflection

B. Earp, Air ForceInstitute of Technology,Wright-Patterson AFB,OH

Chaired by: A. CONLISK, Ohio State University, Columbus, OH, and B. SHAPIRO, University of Maryland, College Park, MD


Wednesday Morning / 07 January 2004 Session 110-FD-22 Micro and Nanofluidics (Invited) Crystal 1

Wednesday Morning / 07 January 2004 Session 111-FD-23 Multigrid, Preconditioning, and Convergence Acceleration Methods Crystal 2

Wednesday Morning / 07 January 2004 Session 112-GT-4 / APA-12 High Reynolds Number Aerodynamics and Testing (Invited) Crystal 3


Chaired by: A. CONLISK, Ohio State University, Columbus, OH, and B. SHAPIRO, University of Maryland, College Park, MD0800AIAA-2004-0754 Nano- Particle Image Velocimetry (NPIV): A NewTechnique for Measuring Near- Wall VelocityFields with Submicron Spatial Resolution

M. Yoda, Georgia Institute of Technology, Atlanta,GA

0900AIAA-2004-0756 Optically Controlled Mixing in Microdroplets

R. Grigoriev, Georgia Institute of Technology,Atlanta, GA

Chaired by: R. BUSH, Pratt & Whitney, East Hartford, CT, and B. SEKAR, Air Force Research Laboratory, Wright-Patterson AFB, OH0800AIAA-2004-0758 Multigrid Algorithms forthe Chimera Method

X. Juvigny, ONERA,Chatillon, France

0830AIAA-2004-0759 Agglomeration Multigridfor an Unstructured GridFlow Solver

M. Pandya, SwalesAerospace Inc.,Hampton, VA

0900AIAA-2004-0761 Parallel MultigridUnstructured Method forthe Solution of theNavier- StokesEquations

R. Corral, Industria deTurbo Propulsores S.A.,Madrid, Spain

0930AIAA-2004-0762 A PreconditionedSolution Scheme for theSimulation ofTurbomachinery Flow atArbitrary Mach Numbers

J. Anker, University ofStuttgart, Stuttgart,Germany

1000AIAA-2004-0763 Practical Implementationand Improvement ofPreconditioning Methodsfor Explicit MultistageFlow Solvers

K. Hosseini, StanfordUniversity, Palo Alto, CA

Chaired by: J. QUEST, European Transonic WIndtunnel GmbH, Cologne, Germany, and R. WAHLS, NASA Langley Research Center, Hampton, VA0800AIAA-2004-0764 Experimental andComputationalEvaluation of Flush-Mounted, S- Duct Inlets

B. Berrier, NASALangley ResearchCenter, Hampton, VA

0830AIAA-2004-0765 Compressibility andLeading- EdgeBluntness Effects for a65o Delta Wing

J. Luckring, NASALangley ResearchCenter, Hampton, VA

0900AIAA-2004-0767 Overview About theEuropean High LiftResearch ProgrammeEUROLIFT

H. Hansen,Airbus-Germany,Ruxtehude, Germany

0930AIAA-2004-0768 Exploitation by Airbus ofHigh Reynolds NumberTest Capabilities in theEuropean TransonicWind Tunnel

P. White, Airbus-UK,Bristol, Great Britain

1000AIAA-2004-0769 The ETW WallInterferenceAssessment for Full andHalf Models

J. Quest, ETW GmbH,Cologne, Germany

1030AIAA-2004-0770 Measuring WallInterference CorrectionAccuracy: An Overviewof the NTF Program

E. Walker, NASALangley ResearchCenter, Hampton, VA

1100AIAA-2004-0771 Measurement of ForceBalance Repeatabilityand Reproducibility inthe NTF

M. Hemsch, NASALangley, Hampton, VA

Chaired by: T. BENYO and J. HOROWITZ, NASA Glenn Research Center, Cleveland, OH


Wednesday Morning / 07 January 2004 Session 113-ICG-2 Integrated Computational and Visualization Environments Crystal 4

Wednesday Morning / 07 January 2004 Session 114-IS-1 Intelligent Systems I Crystal 5

Wednesday Morning / 07 January 2004 Session 115-MSSP-4 Strategic Research and Microgravity Environment N6


Chaired by: T. BENYO and J. HOROWITZ, NASA Glenn Research Center, Cleveland, OH

Chaired by: E. ATKINS, University of Maryland, College Park, MD, and J. NEIDHOEFER, Accurate Automation Corporation, Chattanooga, TN0800AIAA-2004-0773 Time Bounded NeuralNetwork CommandControl Design forUnstable Aircraft

S. Suresh, IndianInstitute of Science,Bangalore, India

0830AIAA-2004-0774 Intelligent Multi-Resolution Modeling:Application to SyntheticJet Actuation and FlowControl

P. Singla, Texas A&MUniversity, CollegeStation, TX

0900AIAA-2004-0777 Neurocontroller Designfor Nonlinear Control ofTakeoff of UnmannedAerospace Vehicles

J. Thomson, ClarksonUniversity, Potsdam, NY

0930AIAA-2004-0778 Robust OptimalAerodynamic DesignUsing EvolutionaryMethods and NeuralNetworks

M. Rai, NASA Ames,Moffett Field, CA

1000AIAA-2004-0779 Dynamic WaypointGeneration GivenReduced FlightPerformance

E. Atkins, University ofMaryland, College Park,MD

Chaired by: H. NAHRA and R. DELOMBARD, NASA Glenn Research Center, Cleveland, OH0800AIAA-2004-0781 Ground- based Testingof Radiation ShieldingMaterials

C. Zeitlin, LawrenceBerkeley NationalLaboratory, Berkeley, CA

0830AIAA-2004-0783 Evaluation of a Multi-parameter Sensor forAutomatedMonitoring ofLong- term MicrogravityCell Culture Experiments

D. Pappas, WyleLaboratories, Houston,TX

0900AIAA-2004-0784 Glovebox IntegratedMicrogravity IsolationTechnology (g- LIMIT):A Linearized State-Space Model

R. Hampton, U.S.Military Academy, WestPoint, NY

0930AIAA-2004-0785 MicrogravityEnvironment Predictionand Control for theFluids Integrated Rack

L. Moss, ZinTechnologies Inc., BrookPark, OH

1000AIAA-2004-0786 A State- Space Model ofARIS for OptimalController Design:MATLAB Implementation

R. Hampton, U. S.Military Academy, WestPoint, NY

1030AIAA-2004-0787 Passive Isolators for Useon the InternationalSpace Station

J. Houston, SverdrupTechnology Inc.,Huntsville, AL

Chaired by: J. POWERS, University of Notre Dame, Notre Dame, IN, and E. KIM, The Aerospace Corporation, Los Angeles, CA0800 0830 0900 0930 1000 1030 1100


Wednesday Morning / 07 January 2004 Session 116-PC-9 Heterogeneous Combustion and Detonations Shasta 1

Wednesday Morning / 07 January 2004 Session 117-PC-10 Turbulent Combustion Modeling Shasta 2

Wednesday Morning / 07 January 2004 Session 118-PDL-5 Laser Applications, Diagnostics & Effects N8


Chaired by: J. POWERS, University of Notre Dame, Notre Dame, IN, and E. KIM, The Aerospace Corporation, Los Angeles, CA0800AIAA-2004-0788 Influence of DistributedSolid- Phase Reactionson Deflagrations inConfined PorousPropellants

A. Telengator,University of CaliforniaSan Diego, La Jolla, CA

0830AIAA-2004-0789 Dehydrogenation andBurning of AluminumHydride at ElevatedPressures

T. Bazyn, University ofIllinois atUrbana-Champaign,Urbana, IL

0900AIAA-2004-0790 Effects ofHeterogeneous SurfaceReactions on theIgnition of AluminumParticles

P. George, StateUniversity of New Yorkat Buffalo, Buffalo, NY

0930AIAA-2004-0791 Supersonic CombustionHeater Development forHypersonic Materialsand Propulsion Testing

K. Wilson, Naval AirWarfare Center, ChinaLake, CA

1000AIAA-2004-0792 Numerical Study of theDetonation WaveStructure in Ethylene-oxygen Mixtures

A. Khokhlov, NavalResearch Laboratory,Washington, DC

1030AIAA-2004-0793 Direct Calculation ofSpherical DetonationInitiation of a H2/O2/ArMixture by the CESEMethod

B. Wang, Ohio StateUniversity, Columbus,OH

1100AIAA-2004-0794 Longitudinal OscillationMode of One-Dimensional H2- AirDetonations

Y. Daimon, KeioUniversity, Yokohama,Japan

Chaired by: P. DESJARDIN, State University of New York at Buffalo, Buffalo, NY, and E. BRIZUELA, University de Buenos Aires, Capital, Argentina0800AIAA-2004-0796 Laminar FlameletConcept for Laminarand Turbulent DiffusionFlames

K. Claramunt, TechnicalUniversity of Catalonia,Terrassa, Spain

0830AIAA-2004-0798 Finite Rate ChemistryEffects in Non-Premixed CH4/H2Flames

C. Safta, University atBuffalo, Buffalo, NY

0900AIAA-2004-0800 DNS of Moderate-Temperature GaseousMixing Layers Ladenwith Multicomponent-Fuel Drops

P. Le Clercq, CaliforniaInstitute of Technology,Pasadena, CA

0930AIAA-2004-0801 Subgrid Mixing Modelingfor Large EddySimulation ofSupersonic Combustion

V. Sankaran, GeorgiaInstitute of Technology,Atlanta, GA

1000AIAA-2004-0802 An Integrated Thermo-fluid, Chemical KineticModel for PulseCombustors

H. Heravi, AzadUniversity, Mashad, Iran

1030AIAA-2004-0803 Transient Prediction ofHeat TransferCharacteristics inFurnaces: Combustionand Heat TransferModeling


Chaired by: R. ACKERMAN, Raytheon, Manhattan Beach, CA0800AIAA-2004-0805 Simulation of FlowUnsteadiness inChemical LaserFlowfields

T. Madden, Air ForceResearch Laboratory,Kirtland AFB, NM

0830AIAA-2004-0807 Parametric FactorsAffecting Carbon PlumeDevelopment in SWNTLaser AblationProduction

R. Greendyke,University of Texas atTyler, Tyler, TX

0900AIAA-2004-0808 Ultrashort UV Laser:Drilling Holes in Nickel-Based Alloys for ABLCOIL- SOG

K. Kremeyer, PM & AMResearch, Tucson, AZ

0930AIAA-2004-0809 Laser- Induced ShockImpulse Generation andIts AerospaceApplications

K. Watanabe, TohokuUniversity, Sendai, Japan

Tutorial Session - Introduction to Systems Engineering - Why do we need it and What is it?


Wednesday Morning / 07 January 2004 Session 119-SE-10800 - Systems Engineering I McKinley

Wednesday Morning / 07 January 2004 Session 120-TES-5 Combustion and Flames N4

Wednesday Morning / 07 January 2004 Session 121-TP-6 Thermophysical Properties and Measurements N10


Tutorial Session - Introduction to Systems Engineering - Why do we need it and What is it?Instructor - John Hsu, The Boeing CompanyModerator - Mike McCoy

Chaired by: J. DAWSON, Cardiff School of Engineering, Cardiff, Great Britain, and C. MOEN, Sandia National Laboratories, Livermore, CA0800AIAA-2004-0810 Passive Control ofUnstable Combustion ina Swirl- Stabilized SprayCombustor

M. Linck, University ofMaryland, College Park,MD

0830AIAA-2004-0811 Low- frequencyCombustion Oscillationsin a Swirl Burner/furnace

J. Dawson, CardiffUniversity, Cardiff,Great Britain

0900AIAA-2004-0812 The Effect of CombutionInstability onRecirculation Zones in aSwirl Burner/furnace

J. Dawson, CardiffUniversity, Cardiff,Great Britain

0930AIAA-2004-0813 Effect of Swirl on FlowDynamics in Unconfinedand Confined GaseousFuel Flames

S. Archer, University ofMaryland, College Park,MD

1000AIAA-2004-0814 Characteristics ofNonbuoyant Elliptic JetDiffusion Flames

J. Camacho, Universityof Texas at El Paso, ElPaso, TX

1030AIAA-2004-0815 Effect of OscillatingExcitation on aMethane- Air DiffusionJet Flame

M. Ishizawa, NagoyaUniversity, Nagoya,Japan

1100AIAA-2004-0816 Time- ResolvedAnalysis of OHDistribuion in a Flameby PLIF Spectroscopy

A. Katoh, NagoyaUniversity, Nagoya,Japan

1130AIAA-2004-0817 Adiabatic FlameTemperatureCalculation: A SimpleApproach for GeneralCHONS Fuels


Chaired by: M. LAMBERT, San Diego State University, San Diego, CA, and H. NELSON, University of Missouri-Rolla, Rolla, MO0800AIAA-2004-0818 Study of Pre-emergencies in High-temperature Reactor

Y. Filimonov,Hypersonic SystemsResearch Institute,Saint-Petersburg, Russia

0830AIAA-2004-0819 Prediction of ThermalConductivity of Single-Wall Carbon Nanotubeswith Mecahanical Strains

C. Anderson, Universityof Minnesota,Minneapolis, MN

0900AIAA-2004-0820 Adsorbent- RefrigerantSelection for AutomotiveAdsorption Heat Pump

M. Lambert, San DiegoState University, SanDiego, CA

0930AIAA-2004-0821 Thermal Resistances ofGaseous Gap forConforming RoughContacts

M. Bahrami, Universityof Waterloo, Waterloo,Canada

1000AIAA-2004-0822 Thermal Resistances ofGaseous Gap for Non-Conforming RoughContacts

M. Bahrami, Universityof Waterloo, Waterloo,Canada

1030AIAA-2004-0823 Motivation for theDevelopment ofHeating/Cooling Rateand Heat Flux RateSensors for EngineeringApplications

J. Frankel, University ofTennessee, Knoxville,TN

1100AIAA-2004-0824 Feasibility of a Fiber-Optic Sensor for High-Speed High- PressureCryogenic Flow RateMeasurement

N. Torlak, FloridaInstitute of Technology,Melbourne, FL

1130AIAA-2004-0825 Shock Layer OpticalAttenuation andEmission SpectroscopyMeasurements DuringArc Jet Testing withAblating Models

G. Raiche, NASA AmesResearch Center,Moffett Field, CA

Chaired by: P. MORIARTY, NREL's National Wind Technology Center, Golden, CO0800 0830 0900 0930 1000 1030 1100 1130


Wednesday Morning / 07 January 2004 Session 122-WE-5 Rotor and Wake Aerodynamics Ruby

Wednesday Morning / 07 January 2004 Session 123-WIG-5 Plasma Assisted Ignition Teton

Wednesday Morning / 07 January 2004 Session 124-WIG-6 Subsonic Plasma Aerodynamic Flow Control N9


Chaired by: P. MORIARTY, NREL's National Wind Technology Center, Golden, CO0800AIAA-2004-0826 Current Efforts TowardImproved AerodynamicModeling Using theAeroDyn Subroutines

D. Laino, WindwardEngineering, Dundalk,MD

0830AIAA-2004-0827 Stability of Methods inthe Free- Vortex WakeAnalysis of WindTurbines

S. Gupta, University ofMaryland, College Park,MD

0900AIAA-2004-0828 Accuracy of the InducedVelocity of Wind TurbineWakes Using VortexSegmentation

S. Gupta, University ofMaryland, College Park,MD

0930AIAA-2004-0829 Helicoidal Vortex Modelfor Steady andUnsteady Flows

J. Chattot, University ofCalifornia Davis, Davis,CA

1000AIAA-2004-0830 Recent Improvement toa Combined Navier-Stokes/Full PotentialMethodology forModeling HorizontalAxis Wind Turbines

S. Benjanirat, GeorgiaTech, Atlanta, GA

1030AIAA-2004-0831 Drag Prediction forBlades at High Angle ofAttack Using CFD

N. Sørensen, RisoeNational Laboratory,Roskilde, Denmark

1100AIAA-2004-0832 Nacelle ThermalAnalysis of WindTurbines Operating inNordic Climate

A. Smaili, École deTechnologieSupérieure, Montreal,Canada

1130AIAA-2004-1362 A Three- TieredApproach for Designingand EvaluatingPerformanceCharacteristics of NovelWECS

B. Cochran, CPP Inc.,Fort Collins, CO

Chaired by: S. WILLIAMS, Air Force Research Laboratory, Hanscom AFB, MA, and A. STARIKOVSKII, Moscow Institute of Physics and Technology, Moscow, Russia0800AIAA-2004-0833 Ignition of Hydrogen- Airand Methane- AirMixtures at LowTemperatures byNanosecond HighVoltage Discharge

N. Anikin, MoscowInstitute of Physics andTechnology,Dolgoprudny, Russia

0830AIAA-2004-0834 Transient PlasmaIgnition of Hydrocarbon-Air Mixtures in PulseDetonation Engines

F. Wang, University ofSouthern California, LosAngeles, CA

0900AIAA-2004-0835 Non- thermal Ignition ofPremixed Hydrocarbon-air and co- air Flows byNonequilibrium RFPlasma

N. Chintala, Ohio StateUniversity, Columbus,OH

0930AIAA-2004-0836 Long- Lived Plasmoidsas Initiators ofCombustion in GasMixtures

I. Kossyi, RussianAcademy of Sciences,Moscow, Russia

1000AIAA-2004-0837 Effect of Fuel Type onFlame Ignition byTransient PlasmaDischarges

J. Liu, University ofSouthern California, LosAngeles, CA

1030AIAA-2004-0838 Propane- Butane- AirMixture Ignition andCombustion in theAerodynamic Channelwith the Stagnant Zone

V. Shibkov, MoscowState University,Moscow, Russia

1100AIAA-2004-0839 Plasma Torch Ignitersfor a ScramjetCombustor

S. Kuo, PolytechnicUniversity, Brooklyn, NY

1130AIAA-2004-0840 Experiments on PropaneIgnition in High- SpeedAirflow Using a DeeplyUndercritical MicrowaveDischarge

I. Esakov, MoscowRadio TechnicalInstitute, Moscow, Russia

Chaired by: J. POGGIE, Air Force Research Laboratory, Wright-Patterson AFB, OH, and S. BOBASHEV, IOFFE, St Petersburg, Russia0800AIAA-2004-0841 Separation Controlusing Plasma Actuators- Stationary &Oscillating Airfoils

M. Post, University ofNotre Dame, NotreDame, IN

0830AIAA-2004-0842 Mechanism of ForebodyNose Vortex SymmetryBreaking Relevant toPlasma Flow Control

V. Shalaev, MoscowInstitute of Physics andTechnology, Zhukovski,Russia

0900AIAA-2004-0843 Plasma Control ofSeparated FlowAsymmetry on a Cone atHigh Angles of Attack

A. Maslov, ITAM,Novosibirsk, Russia

0930AIAA-2004-0844 Plasma Structure in theAerodynamic PlasmaActuator

C. Enloe, US Air ForceAcademy, ColoradoSprings, CO

1000AIAA-2004-0845 Flow FieldMeasurements ofParaelectric, Peristaltic,and Combined PlasmaActuators Based on theOne AtmosphereUniform Glow DischargePlasma (OAUGDP)

J. Roth, University ofTennessee, Knoxville,TN

1030AIAA-2004-0846 ParametricInvestigations of aSingle Dielectric BarrierPlasma Actuator

R. Van Dyken, US AirForce Academy,Colorado Springs, CO

1100AIAA-2004-0847 AC AND PULSEDPLASMA FLOWCONTROL

R. Rivir, Air ForceResearch Laboratory,Wright-Patterson AFB,OH


Wednesday Afternoon / 07 January 2004 Session 125-AA-6 Fan, Rotor and Airfoil Aeroacoustics N7

Wednesday Afternoon / 07 January 2004 Session 126-ABP-7 Hypersonic Propulsion Whitney

Wednesday Afternoon / 07 January 2004 Session 127-ABP-8 / PC-11 Pulse Detonation Engines III Cascade 2


Chaired by: D. HIXON, University of Toledo, Fairview Park, OH1300AIAA-2004-0848 Acoustic RadiationComputation from anEngine Inlet withAerodynamic Flow Field

S. Richards, Universityof Southampton,Southampton, GreatBritain

1330AIAA-2004-0849 Comparison ofNumerical Schemes fora RealisticComputationalAeroacousticsBenchmark Problem

R. Hixon, University ofToledo, Toledo, OH

1400AIAA-2004-0850 A Study of RotorcraftNoise Prediction inManeuvering Flight

H. Chen, PennsylvaniaState University,University Park, PA

1430AIAA-2004-0852 Prediction of BroadbandNoise: Airfoil in theWake of a Rod

J. Boudet, EcoleCentrale de Lyon,Ecully, France

1500AIAA-2004-0854 Broadband Noise fromthe Unsteady Flow in aSlat Cove

A. Agarwal,Pennsylvania StateUniversity, UniversityPark, PA

Chaired by: J. SHEELEY, Sverdrup Technology, Inc., Arnold AFB, TN, and J. DEBONIS, NASA Glenn Research Center, Cleveland, OH1300AIAA-2004-0855 Mesoflap and BleedFlow Control for a Mach2 Inlet

E. Loth, University ofIllinois atUrbana-Champaign,Urbana, IL

1330AIAA-2004-0856 Numerical Analysis andOptimization of Two-Dimensional HypersonicInlets

S. Hasegawa, RutgersUniversity, Piscataway,NJ

1400AIAA-2004-0857 CFD Analysis of theLow Speed PropulsionMode in an RBCCEngine

R. Bond, North CarolinaState Univ., Raleigh, NC

1430AIAA-2004-0858 The IntegratedHypersonicAeromechanics ToolPropulsion Module

J. Loundagin, JacobsSverdrup, Ridgecrest,CA

1500AIAA-2004-0859 Impact of Electro-Magnetics andIonization on Mixing andCombustion in ScramjetCombustors

D. Riggins, University ofMissouri - Rolla, Rolla,MO

1530AIAA-2004-0861 Experimental Study ofMulti- Row Disk Inletsfor Hypersonic AirBreathing Propulsion

H. Kobayashi, Instituteof Space andAstronautical Science,Sagamihara, Japan

1600AIAA-2004-0862 Quick, GridlessEstimations of MHDEffects on HypersonicInlet Ramp Shocks

N. Malmuth, RockwellScientific, ThousandOaks, CA

Chaired by: T. LIEUWEN, Georgia Institute of Technology, Atlanta, GA, and R. BRUCKNER, NASA Glenn Research Center, Cleveland, OH1300AIAA-2004-0864 ExperimentalInvestigation of a PulseDetonation Engine witha 2D Ejector

D. Allgood, University ofCincinnati, Cincinnati,OH

1330AIAA-2004-0865 Thrust ChamberDynamics andPropulsive Performanceof Single- Tube PulseDetonation Engines

F. Ma, PennsylvaniaState University, StateCollege, PA

1400AIAA-2004-0866 Thrust Augmentation inan Unsteady SupersonicEjector

K. Tacina, NASA GlennResearch Center,Cleveland, OH

1430AIAA-2004-0867 The Impact of aConverging- DivergingNozzle on PDEPerformance and itsAssociated Flowfield

E. Barbour, StanfordUniversity, Stanford, CA

1500AIAA-2004-0868 The Use of a FlashVaporization Systemwith Liquid HydrocarbonFuels in a PulseDetonation Engine

C. Tucker, Air ForceInstitute of Technology,Wright-Paterson AFB,OH

1530AIAA-2004-0869 ExperimentalInvestigation ofMomentum and HeatTransfer in PulseDetonation Rockets

J. Kasahara, Universityof Tsukuba, Tsukuba,Japan

1600AIAA-2004-0870 Deflagration- to-Detonation Control byNon- equilibrium GasDischarges and ItsApplications for PulsedDetonation Engine

E. Kukaev, MoscowInstitute of Physics andTechnology,Dolgoprudny, Russia

Chaired by: W. WEST, Eglin Air Force, Niceville, FL


Wednesday Afternoon / 07 January 2004 Session 128-AFM-6 Aerospace Vehicle Design and Simulation II Sierra 1

Wednesday Afternoon / 07 January 2004 Session 129-AMT-5 Surface and Near Surface Measurements Sierra 2

Wednesday Afternoon / 07 January 2004 Session 130-APA-13 Aerodynamic Structural Interaction Carson 1


Chaired by: W. WEST, Eglin Air Force, Niceville, FL1300AIAA-2004-0871 Computational Analysisof Opposing Jet fromVertical- Lander SpaceVehicle

T. Kitamura, TohokuUniversity, Sendai,Japan

1330AIAA-2004-0872 Air Launching Eart- to-Orbit Vehicles: Delta Vgains from LaunchConditions and VehicleAerodynamics

N. Sarigul-Klijn,University of California,Davis, CA

1400AIAA-2004-0873 Development andTesting of a DrogueParachute System for X-37 ALTV / B- 52HSeparation

S. Whitmore, NASADryden, Edwards, CA

1430AIAA-2004-0874 Determination of theSeparation Forces of theStrap- on Boosters

H. Ok, Korea AerospaceResearch Institute,Daejeon, South Korea

1500AIAA-2004-0875 Improved TrajectoryLinearization FlightController for ReusableLaunch Vehicles

T. Bevacqua, OhioUniversity, Athens, OH

1530AIAA-2004-0876 Ascent, StageSeparation andGlideback Performanceof a Partially ReusableSmall Launch Vehicle

B. Pamadi, NASALangley ResearchCenter, Hampton, VA

Chaired by: J. NAUGHTON, University of Wyoming, Laramie, WY1300AIAA-2004-0877 A Joint ComputationalFluid Dynamics andExperimental FluidDynamics Test Program

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

1330AIAA-2004-0878 Applications ofPressure- SensitivePaint to Testing at VeryLow Flow Speeds

J. Bell, NASA AmesResearch Center,Moffett Field, CA

1400AIAA-2004-0879 Effect of QuenchingKinetics on the UnsteadyResponse of Pressure-Sensitive Paint

J. Gregory, PurdueUniversity, WestLafayette, IN

1430AIAA-2004-0880 Assimilation of PhysicalChemistry Models forLifetime Analysis ofPressure- Sensitive Paint

W. Ruyten, JacobsSverdrup AEDC Group,Arnold AFB, TN

1500AIAA-2004-0881 Lifetime Analysis of thePressure- SensitivePaint PtTFPP in FIB

W. Ruyten, JacobsSverdrup AEDC Group,Arnold AFB, TN

1530AIAA-2004-0882 Correlation Based ImageRegistration forPressure Sensitive Paint

S. Park, KoreaAdvanced Institute ofScience andTechnology, Daejon,South Korea

Chaired by: J. NATHMAN, Analytical Methods Inc, Redmond, WA1300AIAA-2004-0884 CFD- basedAeroservoelasticAnalysis with Hyper- XApplications

K. Gupta, NASA Dryden,Edwards, CA

1330AIAA-2004-0885 Time- DomainAeroelastic Simulationon Stationary Body-Conforming Grids withSmall PerturbationBoundary Conditions

S. Yang, University ofCalifornia Irvine, Irvine,CA

1400AIAA-2004-0886 Time Dependent RANSComputation for anAeroelastic Wing

R. Kamakoti, Universityof Florida, Gainesville,FL

1430AIAA-2004-0887 Analytical Study ofVehicle StructuresSubjected to a TransientBlast Overpressure

M. Murray, Thales AirDefence Ltd., Belfast,Northern Ireland

1500AIAA-2004-0888 Parameter Adaptation ofReduced Order Modelsfor Three- DimensionalFlutter Analysis

T. Lieu, University ofColorado, Boulder, CO

1530AIAA-2004-0889 Improvements in LowDimensional Tools forFlow- StructureInteraction Problems:Using Global POD

R. Schmit, Air ForceResearch Laboratory,Wright-Patterson AFB,OH

Chaired by: C. WARSOP, British Aerospace, Bristol, Great Britain, and L. FORNASIER, EADS Deutschland GmbH, Munich, Germany


Wednesday Afternoon / 07 January 2004 Session 131-APA-14 CEAS Conference Highlights (Invited) Carson 2

Wednesday Afternoon / 07 January 2004 Session 132-APA-15 Configurational Aerodynamics I Carson 3

Wednesday Afternoon / 07 January 2004 Session 133-ASE-6 Atmospheric Support for Design and Operations of Space Vehicles N5


Chaired by: C. WARSOP, British Aerospace, Bristol, Great Britain, and L. FORNASIER, EADS Deutschland GmbH, Munich, Germany1300AIAA-2004-0895 Generic Process for Air-Vehicle Concept Designand Assessment

J. Doherty, QinetiQ Ltd,Farnborough, GreatBritain

Chaired by: S. SILTON, U.S. Army Research Laboratory, Aberdeen Proving Ground, MD, and W. HERLING, The Boeing Company, Bellevue, WA1300AIAA-2004-0899 The NumericalCalculation About Flow-fields at High Alpha ofComplete AircraftGeometry with Two-Equation k- g Model

X. Zhixiang, TsinghuaUniversity, BeiJing,China (prc)

1330AIAA-2004-0900 Simulation and Analysisof V- 22 Aircraft FuelDumping

T. Tai, Naval SurfaceWarfare Center, WestBethesda, MD

1400AIAA-2004-0901 Simple Trim DragPrediction MethodBased on the BiplaneTheory

K. Kusunose, TheBoeing Company,Seattle, WA

1430AIAA-2004-0902 Flextac: An AdvancedSubmarine ControlSurface and ActuationSystem

S. Gowing, NavalSurface Warfare Center,West Bethesda, MD

1500AIAA-2004-0904 ExperimentalInvestigation of BaseDrag Reduction on aTwo- Dimensional BodyUsing Boundary LayerManipulation

V. Durgesh, Universityof Wyoming, Laramie,WY

1530AIAA-2004-0905 A Parallel HybridOptimization Algorithmfor Robust Airfoil Design

T. Ray, NationalUniversity of Singapore,Singapore, Singapore

1600AIAA-2004-0906 Ideal Aerodynamics ofGround- Effect andFormation Flight

R. King, North CarolinaState University,Raleigh, NC

Chaired by: B. ROBERTS, NASA Marshall Space Flight Center, Huntsville, AL, and W. VAUGHAN, University of Alabama in Huntsville, Huntsville, AL1300AIAA-2004-0907 Evaluation of the SpaceShuttle TransatlanticAbort LandingAtmospheric SoundingSystem

F. Leahy, NASA MSFC,Huntsville, AL

1330AIAA-2004-0908 An Analysis of theAutomatedMeteorological ProfilingSystem Low ResolutionFlight Element

F. Leahy, RaytheonITSS, Huntsville, AL

1400AIAA-2004-0910 Status on UpdatedNASA Standard -Terrestrial Environment(Climatic) CriteriaHandbook for use inAerospace VehicleDevelopment

D. Johnson, NASAMarshall Space FlightCenter, Huntsville, AL

Chaired by: R. KIMMEL, Air Force Research Laboratory, Wright-Patterson AFB, OH, and M. MARTIN, Princeton University, Princeton, NJ


Wednesday Afternoon / 07 January 2004 Session 134-FD-24 CFD Validation/Comparisons to Experiment: High Speed Flows Carson 4

Wednesday Afternoon / 07 January 2004 Session 135-FD-25 Flow Control of Jets and Wakes Crystal 1

Wednesday Afternoon / 07 January 2004 Session 136-FD-26 Microfluidics Crystal 2


Chaired by: R. KIMMEL, Air Force Research Laboratory, Wright-Patterson AFB, OH, and M. MARTIN, Princeton University, Princeton, NJ1300AIAA-2004-0913 An Aerothermal Modelfor Ablating Heatshields

T. Lin, NorthropGrumman, SanBernardino, CA

1330AIAA-2004-0915 Simulation ofStreamwise Vortices atthe Flaps of Re- EntryVehicles

H. Luedeke, DLR,Braunschweig, Germany

1400AIAA-2004-0916 Experimental Studies inthe LENS Shock Tunneland Expansion Tunnelto Examine Real- GasEffects in HypervelocityFlows

M. Holden, Calspan-UBResearch Center,Buffalo, NY

1430AIAA-2004-0917 Summary ofExperimental Studies forCode Validation in theLENS Facility andComparisons withRecent Navier- Stokesand DSMC Solutions forTwo- and Three-dimensional SeparatedRegions in HypervelocityFlows

M. Holden, Calspan-UBResearch Center,Buffalo, NY

Chaired by: T. BEUTNER, Air Force Office of Scientific Research, Arlington, VA, and C. TILMANN, Air Force Research Laboratory, Wright-Patterson AFB, OH1300AIAA-2004-0919 Mean Flow ofMultistream RectangularJets Under Normal andMixing EnhancementConditions


1330AIAA-2004-0920 Vectoring a Self-sustained OscillatoryConfined Jet Flow bySecondary Cross- FlowInjection

M. Arruda, CranfieldUniversity, Shrivenham,Great Britain

1400AIAA-2004-0921 Aerodynamic JetVectoring Using SteadyBlowing and Suction

B. Smith, Utah StateUniversity, Logan, UT

1430AIAA-2004-0923 Effects ofCircumferential Microjetson the Near- fieldBehaviour of a RoundJet

T. New, TemasekLaboratories, Singapore,Singapore

1500AIAA-2004-0924 An Investigation of theWake Behind a CircularCylinder with SinusoidalRotational Forcing

C. Schmidt, University ofWyoming, Laramie, WY

1530AIAA-2004-0925 Phase Synchronizationof Vortex Shedding fromTwo Side- by- SideCircular Cylinders UsingPlasma Actuators

A. Asghar, University ofNotre Dame, NotreDame, IN

1600AIAA-2004-0926 Influence of a “Slip”Splitter Plate onTransonic ShockOscillation on Airfoils

Q. Xiao, NationalUniversity of Singapore,Singapore, Singapore

Chaired by: A. CONLISK, Ohio State University, Columbus, OH, and B. SHAPIRO, University of Maryland, College Park, MD1300AIAA-2004-0927 On the Characteristics ofMicro- Fluid JetsGenerated by Ho:YAGPulsed Laser Focusing

V. Menezes, TohokuUniversity, Sendai, Japan

1330AIAA-2004-0929 Numerical Study of Two-Phase Flows inMicrochannels Using theLevel Set Method

M. Tatineni, University ofCalifornia, Los Angeles,Los Angeles, CA

1400AIAA-2004-0930 On the Synthetic IonChannel Problem

K. Evers, Ohio StateUniversity, Columbus,OH

1430AIAA-2004-0931 Towards the Design ofEfficient Micromixers

C. Kaplan, NavalResearch Laboratory,Washington, DC


Wednesday Afternoon / 07 January 2004 Session 137-GT-5 Facility Control Crystal 3

Wednesday Afternoon / 07 January 2004 Session 138-GT-6 Support to the Columbia Accident Investigation (Invited) Crystal 4

Wednesday Afternoon / 07 January 2004 Session 139-IS-2 Intelligent Systems II Crystal 5


Chaired by: J. EDWARDS, DSTL, Cambridge, Great Britain, and F. STEINLE, Sverdrup Technology, Inc., Arnold AFB, TN1300AIAA-2004-0932 Experiences withCoupling Facility ControlSystems with ControlVolume Facility Models

J. Sheeley,Jacobs-Sverdrup/AEDCDivision, Arnold AFB, TN

1330AIAA-2004-0936 Aero- OpticMeasurement FacilityCharacterization

B. Carroll, University ofFlorida, Gainesville, FL

Chaired by: J. ROBINSON, Sverdrup Technology, Inc, Huntsville, AL, and J. HAAS, NASA Glenn Research Center, Cleveland, OH1300AIAA-2004-0938 Foam- on- Tile Impact Modeling for the STS- 107Investigation

R. Stallworth, NASA Marshall, Huntsville, AL

1400AIAA-2004-0939 Impact Testing of LargeFoam Projectiles

J. Kerr, NASA Johnson,Houston, TX

1430AIAA-2004-0940 Simulation of FoamImpact Effects onComponents of theSpace Shuttle ThermalProtection System

E. Fahrenthold,University of Texas,Austin, TX

1500AIAA-2004-0942 Analyses of FoamImpact onto theColumbia Shuttle WingLeading Edge PanelsUsing Pronto3d/SPH

K. Gwinn, SandiaNational Laboratories,Albuquerque, NM

1530AIAA-2004-0945 Material Characterizationof Shuttle ThermalProtection System forImpact Analyses

W. Lu, Sandia NationalLaboratories, Livermore,CA

Chaired by: K. WHITAKER, University of Alabama, Tuscaloosa, AL, and J. NEIDHOEFER, Accurate Automation Corporation, Chattanooga, TN1300AIAA-2004-0946 Spacecraft MissionAssessment andReplanning Tool(SMART) – A Real-Time, IntelligentAutonomous FlightManagement (AFM)System for IncreasedSafety and Performanceof Human SpaceflightVehicles

H. Hu, NASA Johnson,Houston, TX

1330AIAA-2004-0947 Mission SimulationFacility: SimulationSupport for AutonomyDevelopment

G. Pisanich, QSS GroupInc., Moffett Field, CA

1400AIAA-2004-0948 Actions, Observations,and Decision- Making:Biologically InspiredStrategies forAutonomous AerialVehicles

G. Pisanich, QSS GroupInc., Moffett Field, CA

1430AIAA-2004-0949 Controls and HealthManagementTechnologies forIntelligent AerospacePropulsion Systems

S. Garg, NASA GlennResearch Center,Cleveland, OH

1500AIAA-2004-0950 A Novel ClassificationSelection Algorithm ofGuide Star Using theSVM

S. Zheng, HuazhongUniversity of Science &Technology, Wuhan,China (prc)

1530AIAA-2004-0951 Regression Optimizationfor the On- board TripletDatabase

S. Zheng, HuazhongUniversity of Science &Technology, Wuhan,China (prc)

1600AIAA-2004-0952 Fusion of ExperimentalData and MathematicalModels in the Simulationof AerodynamicCoefficients

J. Navarrete, WilliamMarsh Rice University,Houston, TX


Wednesday Afternoon / 07 January 2004 Session 140-MSSP-5 Microgravity Combustion N6

Wednesday Afternoon / 07 January 2004 Session 141-MSSP-6 Microgravity Fluid Physics I N4

Wednesday Afternoon / 07 January 2004 Session 142-PC-12 Sprays and Liquid Jets Shasta 1


Chaired by: S. TSE, Rutgers University, Piscataway, NJ, and K. SACKSTEDER, NASA Glenn Research Center, Cleveland, OH1300AIAA-2004-0953 Burning VelocityMeasurements ofSooting PremixedFlames

A. Ibarreta, CaseWestern ReserveUniversity, Cleveland,OH

1330AIAA-2004-0954 Lifted Partially PremixedFlames in Microgravity

A. Lock, University ofIllinois at Chicago,Chicago, IL

1400AIAA-2004-0955 Acoustic Excitation ofBurning Fuel Droplets inNormal Gravity andMicrogravity

S. Dattarajan, Universityof California, LosAngeles, Los Angeles,CA

1430AIAA-2004-0956 The Cool FlamesExperiment: RecentResults at Reduced andPartial Gravity

H. Pearlman, DrexelUniversity, Philadelphia,PA

1500AIAA-2004-0957 SuppressionCharacteristics of Cup-Burner Flames in LowGravity

F. Takahashi, NationalCenter for MicrogravityResearch, Cleveland,OH

1530AIAA-2004-0958 Quantitative RainbowSchlieren Deflectometryas a TemperatureDiagnostic for SphericalFlames

D. Feikema, NASAGlenn Research Center,Cleveland, OH

1600AIAA-2004-0959 Thermal Characteristicsand Structure of Fully-Modulated, TurbulentDiffusion Flames inMicrogravity

J. Hermanson,University ofWashington, Seattle, WA

Chaired by: M. KASSEMI, NASA Glenn Research Center, Cleveland, OH, and J. HOCHSTEIN, University of Memphis, Memphis, TN1300AIAA-2004-0960 Numerical andExperimental Studies ofSplashing Droplets

J. Kizito, NASA Glenn,Cleveland, OH

1330AIAA-2004-0961 Instabilities in a LaterallyHeated Full- zone with aLarge Aspect Ratio

B. Houchens, Univ. ofIllinois atUrbana-Champaign,Urbana, IL

1400AIAA-2004-0962 Miscible Fluids inMicrogravity (MFMG)

N. Bessonov, UniversiteLyon I, Lyon, France

1430AIAA-2004-0963 Modeling of TransitionMechanism toOscillatory MarangoniFlow in a Liquid Bridge

A. Komiya, NationalSpace DevelopmentAgency, Tsukuba, Japan

1500AIAA-2004-0964 Gravity Effects on OpenCapillary Channel Flow

L. Chien, Institute ofPhysics AcademiaSinica, Taipei, Taiwan(roc)

1530AIAA-2004-0965 Effects of Gravity onBubble Formation in anAnnular Jet

R. Koepp, University ofOklahoma, Norman, OK

1600AIAA-2004-0966 Design of a MicrogravitySpray CoolingExperiment

K. Baysinger, Air ForceResearch Laboratory,Wright-Patterson AFB,OH

1630AIAA-2004-0967 Boiling andCondensationSimulation andInvestigation inMicrogravity Two- PhaseFlow

V. Naoumov, Universityof Tennessee, Knoxville,TN

Chaired by: Y. HARDALUPAS, Imperial College London, London, Great Britain, and J. BELLAN, Jet Propulsion Laboratory, Pasadena, CA1300AIAA-2004-0968 An Experimental Studyof Droplet Breakup inSupersonic Flow: TheEffect of Long- rangeInteractions

G. Li, University ofCalifornia, SantaBarbara, Santa Barbara,CA

1330AIAA-2004-0969 Properties ofNonturbulent RoundLiquid Jets in UniformCrossflows

C. Aalburg, University ofMichigan, Ann Arbor, MI

1400AIAA-2004-0970 Breakup of Aerated-Liquid Jets inSupersonic Crossflows

K. Sallam, University ofMichigan, Ann Arbor, MI

1430AIAA-2004-0971 Structures of Water Jetsin a Mach 1.94Supersonic Crossflow

K. Lin, Taitech Inc.,Wright-Patterson AFB,OH

1500AIAA-2004-0973 Interaction of ReflectedShock Waves with Solidor Liquid Particulates

E. Petersen, Universityof Central Florida,Orlando, FL

Chaired by: S. AGGARWAL, University of Illinois at Chicago, Chicago, IL, and I. GOKALP, CNRSLCSR, Orleans, France


Wednesday Afternoon / 07 January 2004 Session 143-PC-13 Turbulent Premixed and Plasma Enhanced Combustion Shasta 2

Wednesday Afternoon / 07 January 2004 Session 144-PDL-6 Laser & Plasma Technology N8

Wednesday Afternoon / 07 January 2004 Session 145-TP-7 Computational Heat Transfer N10


Chaired by: S. AGGARWAL, University of Illinois at Chicago, Chicago, IL, and I. GOKALP, CNRSLCSR, Orleans, France1300AIAA-2004-0976 Determination ofFlamelet Curvature fromCrossed- Plane ImageData

F. Gouldin, CornellUniversity, Ithaca, NY

1330AIAA-2004-0977 Numerical Simulationsof PremixedCombustion with Swirl

J. Choi, RensselaerPolytechnic Institute,Troy, NY

1400AIAA-2004-0978 Swirling Flow Structuresand FlameCharacteristics in aLean- PremixedCombustor

Y. Huang, PennsylvaniaState University,University Park, PA

1430AIAA-2004-0979 Structure of LocallyQuenched SwirlStabilized TurbulentPremixed Flames

G. Eggenspieler,Georgia Institute ofTechnology, Atlanta, GA

1500AIAA-2004-0980 Combustion in Meso-Scale VortexCombustors:ExperimentalCharacterization

M. Wu, PennsylvaniaState University,University Park, PA

1530AIAA-2004-0981 Numerical Study onSwirling Flow in aCylindrical Chamber

Y. Wang, PennsylvaniaState University,University Park, PA

1600AIAA-2004-0982 Stabilization of aCombustion Processnear Lean Blow Off byan Electric Discharge

W. Choi, Georgia Tech,Atlanta, GA

1630AIAA-2004-0983 Study of Plasma-Enhanced CombustionUsing Optical Diagnostics

D. Packan, ONERA,Palaiseau, France

Chaired by: K. KREMEYER, PM & AM Research, Tucson, AZ1300AIAA-2004-0984 Lines of Pulsed EnergyforSupersonic/HypersonicDrag Reduction:Generation andImplementation

K. Kremeyer, PM&AMResearch, Tucson, AZ

1330AIAA-2004-0985 The Electric Currentsand PotentialsGenerated by PlasmaPlume over SCStructure Elements

A. Korsun, TSNIIMASH,Korolev, Russia

1400AIAA-2004-0986 Nascap- 2K Simulationsof Spacecraft Chargingin Tenuous PlasmaEnvironments

M. Mandell, ScienceApplicationsInternationalCorporation, San Diego,CA

1430AIAA-2004-0987 Two- dimensionalComputational Modelingof the Structure ofDirect- currentMicrodischarges

P. Kothnur, University ofTexas at Austin, Austin,TX

1500AIAA-2004-0989 ComputationalSimulation of Laser-Induced Plasmas forSupersonic Flow Control

R. Kandala, University ofMinnesota, Minneapolis,MN

1530AIAA-2004-0990 Microwave Plasma Flareas a Way of MicrowaveEnergy Trasformationinto a Quasi- StationaryCurrent (Mechanismsand Applications)

G. Batanov, RussianAcademy of Sciences,Moscow, Russia

Chaired by: G. SCHNEIDER, University of Waterloo, Waterloo, Canada, and F. SHOPE, Sverdrup Technology, Inc., Arnold AFB, TN1300AIAA-2004-0993 Challenges in the HeatTransfer Computationsof High Speed Flows

J. Dietiker, Wichita StateUniversity, Wichita, KS

1330AIAA-2004-0994 Parallel Computation ofa Fully Implicit FiniteVolume Method usingDifferent OrderingStrategies

M. Darbandi, Universityof Waterloo, Waterloo,Canada

1400AIAA-2004-0995 Distributed MassWeighting of Non-Inverted ConvectionUpwind Variables forThree- DimensionalFlow SImulations

E. Ogedengbe,University of Manitoba,Winnipeg, Canada

1430AIAA-2004-0996 Coupling Heat Transferand Fluid Flow Solversfor Multi- DisciplinarySimulations

Q. Liu, Mississippi StateUniv., Mississippi State,MS

1500AIAA-2004-0997 Numerical Study on aThermal Response ofthe Jet Vane System ina Rocket Nozzle

M. Yu, YonseiUniversity, Seoul, SouthKorea

1530AIAA-2004-0998 3D Time- DependentCFD Model to Predictthe AirflowCharacteristics inDifferent Enclosures


1600AIAA-2004-1000 Numerical Simulation ofHigh- EnthalpyExperiments in theLENS X ExpansionTube Facility

I. Nompelis, Universityof Minnesta,Minneapolis, MN

Chaired by: M. SCHWARTZ, NREL's National Wind Technology Center, Golden, CO, and J. MANWELL, University of Massachusetts, Amherst, MA


Wednesday Afternoon / 07 January 2004 Session 146-WE-6 Environment, Inflow, and Offshore Ruby

Wednesday Afternoon / 07 January 2004 Session 147-WIG-7 Plasma Assisted Combustion Teton


Chaired by: M. SCHWARTZ, NREL's National Wind Technology Center, Golden, CO, and J. MANWELL, University of Massachusetts, Amherst, MA1300AIAA-2004-1001 Wind Turbine Responseto Analytic Inflow VortexParameter Variation

M. Hand, NationalRenewable EnergyLaboratory, Golden, CO

1330AIAA-2004-1002 On Estimation ofCoherence in InflowTurbulence Based onField Measurements

K. Saranyasoontorn,University of Texas atAustin, Austin, TX

1400AIAA-2004-1003 Simulations of theTurbulentCharacteristics of theLower AtmosphereUsing MM5V3

T. Parish, University ofWyoming, Laramie, WY

1430AIAA-2004-1004 Initial Studies of Low-Order TurbulenceModeling of the WindTurbine In- FlowEnvironment

J. Spitler, University ofWyoming, Laramie, WY

1500AIAA-2004-1005 Development of aPowerful Hybrid Tool forEvaluating Wind Powerin Complex Terrain:Atmospheric NumericalModels and WindTunnels

R. Derickson, CPP WindEngineeringConsultants, FortCollins, CO

1530AIAA-2004-1006 The Influence ofSpecific Rating on theCost of Wind Energy

D. Malcolm, GlobalEnergy Concepts LLC,Kirkland, WA

1600AIAA-2004-1007 Feasibility of FloatingPlatform Systems forWind Turbines

W. Musial, NationalRenewable EnergyLaboratory, Golden, CO

1630AIAA-2004-1008 Characterization ofExternal Conditions forthe Design of OffshoreWind Energy Systemsfor the United States

J. Manwell, University ofMassachusetts,Amherst, MA

1700AIAA-2004-1010 HVDC LightExperiences Applicablefor Power Transmissionfrom Offshore WindPower Parks

K. Eriksson, ABB,Ludvika, Sweden

Chaired by: C. CARTER, Air Force Research Laboratory, Wright-Patterson AFB, OH, and V. SHIBKOV, Moscow State University, Moscow, Russia1300AIAA-2004-1011 Effect of DischargeEnergy and CavityGeometry on FlameIgnition by TransientPlasma

J. Liu, University ofSouthern California, LosAngeles, CA

1330AIAA-2004-1012 Model and IgniterDevelopment forPlasma AssistedCombustion

S. Williams, Air ForceResearch Laboratory,Hanscom AFB, MA

1400AIAA-2004-1013 Propane- Air FlameControl by Non-Equilibrium Low-temperature PulsedNanosecond BarrierDischarge

E. Mintoussov, MoscowInstitute of Physics andTechnology,Dolgoprudny, Russia

1430AIAA-2004-1014 External and InternalPlasma- AssistedCombustion

A. Klimov, RussianAcademy of Sciences,Moscow, Russia

1500AIAA-2004-1015 Mobilities andReactivities of MolecularIons in Combustion andHypersonics

S. Kato, University ofColorado, Boulder, CO

1530AIAA-2004-1016 Discharge and FlamePlasmas ProbeDiagnostics inSupersonic Air- PropaneFlows

A. Ershov, MoscowState University,Moscow, Russia

1600AIAA-2004-1017 Numerical Study ofPlasma Assisted Mixingand Combustion in Non-Premixed SupersonicFlows

V. Bityurin, IVTAN,Moscow, Russia

Chaired by: C. SUCHOMEL, Air Force Research Laboratory, Wright-Patterson AFB, OH, and A. KLIMOV, IVTAN, Moscow, Russia1300 1330 1400 1430 1500 1530 1600


Wednesday Afternoon / 07 January 2004 Session 148-WIG-8 Plasma Aerodynamic Phemomena N9

Wednesday Afternoon / 07 January 2004 Session - von Karman Lectureship in Astronautics Reno Ballroom

Wednesday Afternoon / 07 January 2004 1830 - 1930 Reception Hilton Pavilion


Chaired by: C. SUCHOMEL, Air Force Research Laboratory, Wright-Patterson AFB, OH, and A. KLIMOV, IVTAN, Moscow, Russia1300AIAA-2004-1018 Test Facility for PlasmaJets and Pellets Actionson Flow Over Body

S. Bobashev, IoffePhysico-TechnicalInstitute, St.Petersburg,Russia

1330AIAA-2004-1019 Bow Shock WaveStructures Control byPulse- Periodic EnergyInput

P. Georgievsky,Moscow StateUniversity, Moscow,Russia

1400AIAA-2004-1020 Acoustical Properties ofNonequilibrium Media

N. Molevich, Korolev'sSamara StateAerospace University,Samara, Russia

1430AIAA-2004-1021 Dispersion of andPropagation of WeakShock Waves ThroughMicrowave CavityDischarges

P. Kessaratikoon, OldDominion University,Norfolk, VA

1500AIAA-2004-1023 Shock Wave Interactionwith Non- equilibriumPlasma of Gas Discharge

D. Opaits, MoscowInstitute of Physics andTechnology,Dolgoprudny, Russia

1530AIAA-2004-1024 Modeling of MHD PowerGeneration on BoardReentry Vehicles

S. Macheret, PrincetonUniversity, Princeton, NJ

1600AIAA-2004-1025 Observation of MHDEffects with Non-Equlibrium Ionization inCold Supersonic AirFlows

R. Murray, PrincetonUniversity, Princeton, NJ

1730AIAA-2004-0003 The Exploration of Mars;Historical Context andCurrent Results

G. Hubbard, NASAAmes Research Center,Moffett Field, CA

Chaired by: M. SHEPLAK, University of Florida, Gainesville, FL0800 0830 0900 0930 1000


Thursday Morning / 08 January 2004 Session 149-AA-7 Experimental Aeracoustics N7

Thursday Morning / 08 January 2004 Session 150-ABP-9 Combustion Cascade 2

Thursday Morning / 08 January 2004 Session 151-AMT-6 / SEN-2 Sensors for Ground, Airborne, and Space Sierra 2


Chaired by: M. SHEPLAK, University of Florida, Gainesville, FL0800AIAA-2004-1029 TemporalCharacterization ofAircraft Noise Sources

F. Grosveld, LockheedMartin, Hampton, VA

0830AIAA-2004-1028 Boundary Layer Noise inAeroacoustic WindTunnels

E. Duell, JacobsSverdrup, Tullahoma, TN

0900AIAA-2004-1030 Design andCharacterization ofMEMS OpticalMicrophone forAeroacousticMeasurement

W. Hunt, University ofFlorida, Gainesville, FL

0930AIAA-2004-1031 Effects of Angle ofAttack and Velocity onTrailing Edge Noise

F. Hutcheson, NASALangley ResearchCenter, Hampton, VA

1000AIAA-2004-1032 ExperimentalInvestigation ofStatistical Moments ofTravel Time in Grid-Generated Turbulence

T. Andreeva, WorcesterPolytechnic Institute,Worcester, MA

Chaired by: B. SEKAR, Air Force Research Laboratory, Wright-Patterson AFB, OH, and M. MAWID, Engineering Research and Analysis Corporation, Dayton, OH0800AIAA-2004-1033 ThermodynamicAnalysis of CombustionProcesses forPropulsion Systems

J. Shepherd, CaliforniaInstitute of Technology,Pasadena, CA

0830AIAA-2004-1034 "Slow" Control ofCombustion Instabilitiesby Fuel SprayModification UsingSmart Fuel Injector

T. Conrad, GeorgiaInstitute of Technology,Atlanta, GA

0900AIAA-2004-1035 Numerical Study ofHydrogen and EthyleneInjected Normally in aTwo- dimensional Dual-mode ScramjetCombustor

R. Carson, OldDominion University,Norfolk, VA

0930AIAA-2004-1037 Investigation of anIntake Injected Hot WallScramjet

A. Kovachevich,University ofQueensland, Brisbane,Australia

1000AIAA-2004-1038 PIV Measurement of a3- Dimensional ReactingFlow in a ScramjetCombustion Chamber

F. Scheel, DLRLampoldshausen,Hardthausen, Germany

1030AIAA-2004-1039 Numerical Analysis ofUnsteady Combustion inScramjet Engine

J. Kim , Inha University,Inchon , South Korea

1100AIAA-2004-1040 Microporous Liquid FuelFlow Structures

E. Bushmanov, Instituteof Applied Mechanics,Moscow, Russia

Chaired by: S. MELLER, Luna Innovations, Blacksburg, VA, and N. CLEMENS, University of Texas at Austin, Austin, TX0800AIAA-2004-1041 A High- FrequencyOscillating- Hot- WireSensor for Near- WallDiagnostics inSeparated Flows

Y. Li, Michigan StateUniversity, East Lansing,MI

0830AIAA-2004-1042 A MicromachinedGeometric MoiréInterferometric Floating-Element Shear StressSensor

S. Horowitz, Universityof Florida, Gainesville, FL

0900AIAA-2004-1045 Technique to ExtractRigid- Body Data fromShock- InducedStructural Loads

F. Lu, University ofTexas at Arlington,Arlington, TX

0930AIAA-2004-1046 The Measurement ofPerformance ofCombustors UsingPassive AcousticMethods

J. Kleppe, University ofNevada, Reno, NV

1000AIAA-2004-1047 Transition Detection inCruise Flight Using aResistant Multi- SensorHot- Film Technique

F. Hausmann,AerodynamischesInstitut der RWTHAachen, Aachen,Germany

1030AIAA-2004-1048 Application of MolecularSensors to MicroObjects in SupersonicFlow

T. Osafune, JapanAerospace ExplorationAgency, Chofu,Tokyo,Japan

Chaired by: D. GREENWELL, University of Bristol, Bristol, Great Britain


Thursday Morning / 08 January 2004 Session 152-APA-16 Airfoil Aerodynamics Carson 1

Thursday Morning / 08 January 2004 Session 153-APA-17 Transonic, Supersonic and Hypersonic Aerodynamics Carson 2

Thursday Morning / 08 January 2004 Session 154-APA-18 Vortical Flows Carson 3


Chaired by: D. GREENWELL, University of Bristol, Bristol, Great Britain0800AIAA-2004-1049 Optimization Design ofNew High Lift Airfoils foran Unmanned AerialVehicle

J. Liu, LeaderUniversity, Tainan,Taiwan (roc)

0830AIAA-2004-1050 Some Examples ofAirfoil Design for FutureUnmanned Air VehicleConcepts

K. Biber, IstanbulTechnical University,Istanbul, Turkey

0900AIAA-2004-1051 ComputationalInvestigation of Airfoilswith Miniature TrailingEdge Control Surfaces

H. Lee, StanfordUniversity, Stanford, CA

0930AIAA-2004-1052 Development of HighAltitude LongEndurance Airfoils

M. Steinbuch, IsraelAircraft Industries LTD,Tel-Aviv, Israel

1000AIAA-2004-1053 Aerodynamic Analysisof Airfoils at Very LowReynolds Numbers

D. Mateescu, McGillUniversity, Montreal,Canada

1030AIAA-2004-1054 Parametric DesignStudy of the Thicknessof Airfoils at ReynoldsNumbers from 60,000 to150,000

M. Kellogg, BrighamYoung University,Provo, UT

1100AIAA-2004-1055 A Closed- FormSolution for the AirfoilCritical Mach Number

P. Kesic, University ofZagreb, Zagreb, Croatia

1130AIAA-2004-1056 A Numerical Study ofTransonic Buffet on aSupercritical Airfoil

Q. Xiao, NationalUniversity of Singapore,Singapore, Singapore

Chaired by: C. STEFFEN, NASA Glenn Research Center, Cleveland, OH0800AIAA-2004-1057 Parallel UnstructuredMesh Adaptation forTransient Moving Bodyand AeropropulsiveApplications

P. Cavallo, CombustionResearch and FlowTechnology Inc.,Pipersville, PA

0830AIAA-2004-1058 Effect of Dimples onGlancing Shock Wave-Turbulent BoundaryLayer Interactions

C. Lada, UMIST,Manchester, GreatBritain

0900AIAA-2004-1059 Passive Control ofShockwave- BoundaryLayer Interactions UsingUltrasonically AbsorptiveSurfaces

D. Cohen, UMIST,Manchester, GreatBritain

0930AIAA-2004-1060 Numerical and MeshResolutionRequirements forAccurate Sonic BoomPrediction of CompleteAircraft Configurations

S. Choi, StanfordUniversity, Stanford, CA

1000AIAA-2004-1062 Numerical Analysis ofHypersonic Flow over aDouble- Cone GeometryUsing Eu's GHEquations

J. Ahn, Seoul NationalUniversity, Seoul, SouthKorea

1030AIAA-2004-1063 A Numerical Study ofthe Shape Effect onDrag in Supersonic LowReynolds Number(Rarefied) Flows

S. Sushchikh, Universityof California SantaBarbara, Santa Barbara,CA

1100AIAA-2004-1064 Particle- to- ParticleLong Range Interactionand Drag in SupersonicFlows

G. Li, University ofCalifornia SantaBarbara, Santa Barbara,CA

Chaired by: T. MITCHELL, AOARD, Tokyo, Japan0800AIAA-2004-1065 The Flow on the Apex ofa Sharp- Edged DeltaWing

N. Verhaagen, DelftUniversity ofTechnology, Delft, TheNetherlands

0830AIAA-2004-1066 Unsteady Vortex Flowsand Buffeting of a LowSweep Delta Wing

G. Taylor, University ofBath, Bath, Great Britain

0900AIAA-2004-1067 Numerical Study ofFour- Vortex AircraftWakes and Layout ofCorresponding High- LiftConfigurations

E. Stumpf, DLR,Braunschweig, Germany

0930AIAA-2004-1068 Velocity Measurementsin Vortical Flow of aLEX- Delta WingConfiguration in aSideslip

M. Sohn, Korea AirForce Academy,Chonwon-gun, SouthKorea

1000AIAA-2004-1069 Experiments andComputations of RollTorque Induced byVortex- Fin Interaction

C. Peterson, SandiaNational Laboratories,Albuquerque, NM

1030AIAA-2004-1072 Stability of Vortex Pairsover Slender ConicalBodies - Theory andNumerical Computations

J. Cai, NationalUniversity of Singapore,Singapore, Singapore

Chaired by: J. EHERNBERGER, NASA Dryden Research Center, Edwards, CA


Thursday Morning / 08 January 2004 Session 155-ASE-7 Atmospheric Turbulence N5

Thursday Morning / 08 January 2004 Session 156-ASE-8 Space Plasma and Radiation Environment N4

Thursday Morning / 08 January 2004 Session 157-CS-1 High Performance Computing Crystal 5


Chaired by: J. EHERNBERGER, NASA Dryden Research Center, Edwards, CA0800AIAA-2004-1073 Wake Vortex AlleviationFlow Field Studies

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

0830AIAA-2004-1074 Flight- Simulator Studyof Airplane Encounterswith Perturbed TrailingVortices

R. Loucel, BoeingCommercial Airplanes,Seattle, WA

0900AIAA-2004-1075 A Two- DimensionalModel for Trailing VortexStructure

M. Miyazawa, ShizuokaUniversity, Hamamatsu,Japan

0930AIAA-2004-1077 Multi- Sensor Campaignto Correlate AtmosphericOptical Turbulence toGravity Waves

G. Jumper, Air ForceResearch Laboratory,Hanscom AFB, MA

Chaired by: D. FERGUSON, NASA Glenn Research Center, Cleveland, OH, and J. OWENS, NASA Marshall Space Flight Center, Huntsville, AL0800AIAA-2004-1078 Second GenerationSpace EnvironmentForecasting for Satelliteand Ground SystemOperations

W. Tobiska, SpaceEnvironmentTechnologies, PacificPalisades, CA

0830AIAA-2004-1079 Plasma Environmentand Models for L2

J. Minow, JacobsSverdrup MSFC Group,Huntsville, AL

0900AIAA-2004-1080 AutomatedProgrammableScanning PlaneOrientation of CERESInstruments

Z. Szewczyk, ScienceApplicationsInternationalCorporation, Hampton,VA

0930AIAA-2004-1084 The Chandra X- rayObservatory RadiationEnvironment Model -Update

W. Blackwell, JacobsSverdrup, Huntsville, AL

1000AIAA-2004-1085 Characterization ofCandidate Solar SailMaterial Exposed toSpace EnvironmentalEffects

D. Edwards, NASAMarshall Space FlightCenter, Huntsville, AL

Chaired by: L. LONG, Pennsylvania State University, University Park, PA0800AIAA-2004-1086 HPC Technology Trends– An ARL MSRCPerspective

C. Nietubicz, US ArmyResearch Laboratory,Adelphi, MD

0830AIAA-2004-1087 Multilevel ParallelizationModels for High- OrderCFD

S. Dong, BrownUniversity, Providence,RI

0900AIAA-2004-1088 Parallel I/O for theCGNS System

T. Hauser, Utah StateUniversity, Logan, UT

0930AIAA-2004-1089 A Sub- Optimal StaticLoad Balancing Strategyfor a HeterogeneousCluster of PCs

R. Sharif, University ofToledo, Toledo, OH

1000AIAA-2004-1090 STREAMFLO: an EulerSolver for StreamingArchitectures

M. Fatica, StanfordUniversity, Stanford, CA

1030AIAA-2004-1091 JUSTGrid: A Pure JavaHPCC Grid Architecturefor Multi- PhysicsSolvers Using ComplexGeometries

J. Hauser, HPC CLEGmbH, Salzgitter,Germany


Thursday Morning / 08 January 2004 Session 158-DE-10800 - How Well Does Academia Prepare Design Engineers? N3

Thursday Morning / 08 January 2004 Session 159-FD-27 Applied CFD Carson 4

Thursday Morning / 08 January 2004 Session 160-FD-28 CFD Validation/Comparisons to Experiment I Crystal 1


Chaired by: S. BAUMAN, NASA Glenn Research Center, Cleveland, OHThe Design Process Subcommittee sponsored a survey in conjuction with AIAA to determine the level of academic readiness that recent graduates have experienced for design engineering. This is inresponse to a preliminary survey that revealed questions about training for the specific skill that design engineers require. This panel session is a follow-on discussion involving academia andindustry/government concerning the roles each should play in the development of a young design engineer.

Chaired by: I. GIRGIS, Princeton University, Princeton, NJ, and N. GEORGIADIS, NASA Glenn Research Center, Cleveland, OH0800AIAA-2004-1092 Numerical Models ofHuman CirculatorySystem under AlteredGravity: Brain Circulation

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

0830AIAA-2004-1094 Numerical Attempt forCapturing Wing WakeFlows

K. Sawada, TohokuUniversity, Sendai,Japan

0900AIAA-2004-1095 Airfoil ShapeOptimization UsingNURBS RepresentationUnder ThicknessConstraint

S. Painchaud-Ouellet,Ecole Polytechnique,Montreal, Canada

0930AIAA-2004-1096 Adaptive PrecisionMethodology for FlowOptimization viaDiscretization andIteration Error Control

J. Lu, MassachusettsInstitute of Technology,Cambridge, MA

1000AIAA-2004-1097 Calculation of TransonicInternal Flows Using anEfficient High ResolutionUpwind Scheme

G. Zha, University ofMiami, Coral Gables, FL

1030AIAA-2004-1098 Parallel Computation ofThree- DimensionalDriven ViscousIncompressible Flows inEnclosures UsingSecond- OrderProjection Methods withMulti- Grid for LocalIterations

A. Chong, NanyangTechnologicalUniversity, Singapore,Singapore

Chaired by: M. GLAUSER, Syracuse University, Syracuse, NY0800AIAA-2004-1099 Numerical Prediction ofTwo- DimensionalTransverse InjectionFlows

A. Sriram, IndianInstitute of Science,Bangalore, India

0830AIAA-2004-1102 Investigation of FlowSeparation andTransition to Turbulencein an AxisymmetricDiffuser

A. Martin, TechnicalUniversity Berlin, Berlin,Germany

0900AIAA-2004-1103 High- Reynolds NumberViscous FlowComputations UsingUnstructured- GridMethod

H. Luo, ScienceApplicationsInternationalCorporation, McLean, VA

0930AIAA-2004-1104 Verification of the Wind-US CFD Code Using theMethod of ManufacturedSolutions

C. Nelson, AerospaceTesting Alliance, ArnoldAFB, TN

1000AIAA-2004-1106 Fine- Mesh Solutions forIncompressible Navier-Stokes Equations usingthe Direct MatrixInversion Method

S. Poondru, Universityof Cincinnati, Cincinnati,OH

Chaired by: J. JACOB, University of Kentucky, Lexington, KY, and S. GOGINENI, Innovative Scientific Solutions Inc, Wright-Patterson AFB, OH0800 0830 0900 0930 1000 1030 1100 1130


Thursday Morning / 08 January 2004 Session 161-FD-29 Jet Flows Crystal 2

Thursday Morning / 08 January 2004 Session 162-FD-30 Turbulent Boundary Layers and Their Modeling N9


Chaired by: J. JACOB, University of Kentucky, Lexington, KY, and S. GOGINENI, Innovative Scientific Solutions Inc, Wright-Patterson AFB, OH0800AIAA-2004-1107 Numerical Investigationof AxisymmetricCompressible TurbulentJets

L. Keysar, Technion -Israel Institute ofTechnology, Haifa, Israel

0830AIAA-2004-1108 Centrifugal Instability ina Turbulent Wall Jetover a Circular Cylinder

H. Joshi, University ofArizona, Tucson, AZ

0900AIAA-2004-1109 ExperimentalInvestigations of TwoSide- by- Side Jets in aCross Flow

C. Orrala, CaliforniaState University, LongBeach, CA

0930AIAA-2004-1110 Plume And Divert JetEffects On MissileFlowfields At HigherAltitudes

J. Papp, CombustionResearch and FlowTechnology Inc., Dublin,PA

1000AIAA-2004-1111 FundamentalInvestigation ofSupersonic Nozzle FlowSeparation

D. Papamoschou,University of California,Irvine, CA

1030AIAA-2004-1112 Penetration of aTransverse SupersonicJet into a SubsonicCompressible Crossflow

S. Beresh, SandiaNational Laboratories,Albuquerque, NM

1100AIAA-2004-1113 Large- Reynolds-Number Turbulent FluidInterfaces and theUpper Range of Scales

H. Catrakis, Universityof California, Irvine, CA

1130AIAA-2004-1114 Numerical Investigationof InstabilityMechanisms in Laminarand Turbulent Wall Jets

S. Wernz, University ofArizona, Tucson, AZ

Chaired by: E. LOTH, University of Illinois at Urbana-Champaign, Urbana, IL, and D. GAITONDE, Air Force Research Laboratory, Wright-Patterson AFB, OH0800AIAA-2004-1116 Statistical Imprints ofStructure in WallTurbulence

K. Christensen,University of NewMexico, Albuquerque,NM

0830AIAA-2004-1118 Boundary Layer LossMechanism andJustification of WallFunctions forTurbulence Modeling

G. Zha, University ofMiami, Coral Gables, FL

0900AIAA-2004-1120 New Advanced k- wTurbulence Model forHigh- Lift Aerodynamics

A. Hellsten, HelsinkiUniversity ofTechnology, Espoo,Finland

0930AIAA-2004-1121 ComprehensiveValidation of anIntermittency TransportModel for TransitionalLow- Pressure TurbineFlows

Y. Suzen, University ofKentucky, Lexington, KY

1000AIAA-2004-1122 Instabilities and VorticityShedding in Wall-Bounded Flows

K. Cassel, IllinoisInstitute of Technology,Chicago, IL

Chaired by: K. KREMEYER, PM & AM Research, Tucson, AZ, and D. SMITH, University of Wyoming, Laramie, WY0800 0830 0900 0930 1000 1030 1100 1130

1200


Thursday Morning / 08 January 2004 Session 163-FD-31 Unsteady Shock Waves N8

Thursday Morning / 08 January 2004 Session 164-GT-7 Advancements in Hypersonic Testing Crystal 3


Chaired by: K. KREMEYER, PM & AM Research, Tucson, AZ, and D. SMITH, University of Wyoming, Laramie, WY0800AIAA-2004-1123 Influences of theReactant Flow Controlon the DetonationFormation

T. Bormotova, Institutefor High EnergyDensities, Moscow,Russia

0830AIAA-2004-1124 The Effect of Wall HeatLoss on the Flow Fieldsin a Pulse- DetonationWave Engine

M. Radulescu, StanfordUniversity, Stanford, CA

0900AIAA-2004-1125 Computational Study ofFormation and Stabilityof Standing ObliqueDetonation Waves

G. Fusina, DefenceResearch andDevelopment Canada,Ottawa, Canada

0930AIAA-2004-1126 Simulation ofShockwave - StructureInteraction with theBrinkman PenalizationMethod

Y. Liew, PennsylvaniaState University,University Park, PA

1000AIAA-2004-1127 Theoretical Modeling ofSlender BodiesInteraction inSupersonic Flows

N. Malmuth, RockwellScientific, ThousandOaks, CA

1030AIAA-2004-1128 On the Dynamics ofShock Waves in Over-Expanded RocketNozzles

R. Schwane, EuropeanSpace Agency,Noordwijk, TheNetherlands

1100AIAA-2004-1129 Modeling the Effect ofShock Unsteadiness inShock- Wave /Turbulent BoundaryLayer Interactions

K. Sinha, University ofMinnesota, Minneapolis,MN

1130AIAA-2004-1130 Nonlinear Distortion ofFinite Amplitude WavesPropagating inConverging- DivergingNozzles

M. Tyagi, Indian Instituteof Technology Madras,Chennai, India

1200AIAA-2004-1131 Lines of Pulsed Energy:Shock Mitigation andDrag Reduction

K. Kremeyer, PM&AMResearch, Tucson, AZ

Chaired by: K. KONTIS, UMIST, Manchester, Great Britain, and J. LAFFERTY, Arnold Engineering Development Center, Silver Spring, MD0800AIAA-2004-1132 Pyrolysis of Methane ina Supersonic, Arc-Heated Flow

F. Lu, University ofTexas, Arlington, TX

0830AIAA-2004-1134 Results of the 1 MWRadiatively- DrivenHypersonic Wind TunnelExperiments

D. Mansfield, PrincetonUniversity, Princeton, NJ

0900AIAA-2004-1135 Flow Feature InducedSeparation over DoubleWedges

T. Hashimoto, TohokuUniversity, Sendai,Japan

0930AIAA-2004-1136 Unsteady NumericalSimulation of the 1 MWRadiatively- DrivenHypersonic Wind TunnelExperiment

I. Girgis, PrincetonUniversity, Princeton, NJ

1000AIAA-2004-1137 Analysis and Design ofRectangular- Cross-Section Nozzles forScramjet Engine Testing

R. Gaffney, NASALangley ResearchCenter, Hampton, VA

1030AIAA-2004-1138 Feasibility of Operatingthe AEDC SupersonicWind Tunnel (16S) up toMach Number 6

M. Mills,Jacobs-Sverdrup/AEDCGroup, Arnold AFB, TN

1100AIAA-2004-1139 Schlieren Imaging inHypersonic Plasmas

J. Estevadeordal,Innovative ScientificSolutions Inc., Dayton,OH

Chaired by: S. STEPHENS, Lockheed Martin Space Operations, Stennis Space Center, MS, and R. MORGAN, University of Queensland, Brisbane, Australia0800 0830 0900 0930


Thursday Morning / 08 January 2004 Session 165-GT-8 Ground Test Simulation & Analysis Crystal 4

Thursday Morning / 08 January 2004 Session 166-MSSP-7 Microgravity Fluid Physics II N6

Thursday Morning / 08 January 2004 Session 167-PC-14 Droplet and Spray Combustion Shasta 1


Chaired by: S. STEPHENS, Lockheed Martin Space Operations, Stennis Space Center, MS, and R. MORGAN, University of Queensland, Brisbane, Australia0800AIAA-2004-1141 Analysis of the WrightBrothers Wind Tunneland Design of anEducational Derivative

C. Britcher, OldDominion University,Norfolk, VA

0830AIAA-2004-1142 Development ofDynamic StabilityDerivatives of anAirplane from StaticWind Tunnel Tests

B. Chang, KoreaAerospace ResearchInstitute, Daejon, SouthKorea

0900AIAA-2004-1144 Simulation of SevereRain Storms Using AirAtomizing Water Nozzles

R. Mazzawy, TreborSystems Inc, S.Glastonbury, CT

0930AIAA-2004-1145 Productivity and QualityEnhancements in aConfigurationAerodynamics TestUsing the ModernDesign of Experiments

R. DeLoach, NASALangley ResearchCenter, Hampton, VA

Chaired by: I. ALEXANDER, Case Western Reserve University, Cleveland, OH, and N. RAMACHANDRAN, BAE SYSTEMS Analytical Solutions Inc., Huntsville, AL0800AIAA-2004-1147 Particle Response toLow Reynolds NumberOscillation of a Fluid inMicrogravity

D. L'Esperance,MetroLaser, Irvine, CA

0830AIAA-2004-1148 The Capillary FlowExperiments: HandheldFluids Experiments forInternational SpaceStation

M. Weislogel, TDAResearch Inc., WheatRidge, CO

0900AIAA-2004-1149 Experimental Study onthe Capillary Flow in theVane- Wall GapGeometry

Y. Chen, PurdueUniversity, WestLafayette, IN

0930AIAA-2004-1150 Approaches toValidation of Models forLow Gravity FluidBehavior

D. Chato, NASA GlennResearch Center,Cleveland, OH

1000AIAA-2004-1151 Simulation andPrediction of RealisticMagnetic PositivePositioning for SpaceBased FluidManagement Systems

J. Marchetta, Universityof Memphis, Memphis,TN

1030AIAA-2004-1152 Passive FluidsManagement in Low- g:Partially Wetting Systems

M. Weislogel, PortlandState University,Portland, OR

1100AIAA-2004-1153 Magnetic Retention ofLOX in an AcceleratingEnvironment

B. Simmons, TheUniversity of Memphis,Memphis, TN

Chaired by: D. MANN, U.S. Army Research Office, Research Triangle Park, NC, and C. PASCHEREIT, Technische Universität Berlin, Berlin, Germany0800AIAA-2004-1155 Breakup Model forAccelerating Liquid Jets

Y. Hardalupas, ImperialCollege London,London, Great Britain

0830AIAA-2004-1156 A Numerical Model forFlow Simulation in SprayNozzles

M. Fard, Simulent Inc.,Toronto, Canada

0900AIAA-2004-1157 A Model of FlamePropagation Through aLiquid Fuel Mist

J. Greenberg, Technion- Israel Institute ofTechnology, Haifa, Israel

0930AIAA-2004-1159 On the Dynamics ofHead- on DropletCollision: AnExperimental andSimulation Study

K. Pan, PrincetonUniversity, Princeton, NJ

1000AIAA-2004-1161 Responses of DropletEvaporation to High-Pressure Oscillations

W. Yoon, YonseiUniversity, Seoul, SouthKorea

1030AIAA-2004-1162 Characterization andControl of VortexDynamics in an UnstableDump Combustor

B. Pang, University ofMaryland, College Park,MD

Chaired by: R. ANTHENIEN, Air Force Institute of Technology, Wright-Patterson AFB, OH, and J. OEFELEIN, Sandia National Laboratories, Livermore, CA


Thursday Morning / 08 January 2004 Session 168-PC-15 Rocket Combustion Shasta 2

Thursday Morning / 08 January 2004 Session 169-SE-2 Systems Engineering II McKinley

Thursday Morning / 08 January 2004 Session 170-TP-8 Continuum and Rarefied Flows N10


Chaired by: R. ANTHENIEN, Air Force Institute of Technology, Wright-Patterson AFB, OH, and J. OEFELEIN, Sandia National Laboratories, Livermore, CA0800AIAA-2004-1163 Mixing and Combustionin Supercritical O2/CH4Liquid Rocket Injectors

N. Ierardo, FiatAvios.p.a., Colleferro, Italy

0830AIAA-2004-1164 Vorticity and TurbulenceEffects on CombustionStability of SolidPropellant Rocket Motors

R. Brown, Pratt &Whitney SpacePropulsion, Santa Clara,CA

0900AIAA-2004-1167 Characterization of thePrimary Ignition Processof a Coaxial GH2/LOXSpray

V. Schmidt, DLRLampoldshausen,Hardthausen, Germany

0930AIAA-2004-1169 X- 33 Base- HeatingCFD Analysis

S. Zhang, CFDResearch Corporation,Huntsville, AL

1000AIAA-2004-1170 Large Eddy Simulationof Jets Laden withEvaporating Drops

A. Leboissetier, JetPropulsion Laboratory,Pasadena, CA

Chaired by: J. HSU, The Boeing Company, Long Beach, CA0800AIAA-2004-1173 LVL Editor: A GraphicalTool for Visualizing andManaging Data in anEngineering ComponentHierarchy

E. Lau, ELORET,Moffett Field, CA

0830AIAA-2004-1172 Systems Frameworksand KnowledgeCapability: The VirtualSystem DesignEnvironment

C. Stone, NASAGoddard, Greenbelt, MD

0900AIAA-2004-1175 Risk Reduction as theProduct of ModelAssessed Reliability,Confidence, andConsequence

R. Logan, University ofCalifornia/LLNL,Livermore, CA

0930AIAA-2004-1174 Telemetry, Tracking, andGround StationArchitectures for SmallSatellite Clusters

A. Chandrasekaran,Design Net EngineeringGroup, Lakewood, CO

1000AIAA-2004-1376 Some Systemic Issuesin the Development ofthe Boeing TechnicalWorkforce of the Future

J. McMasters, TheBoeing Company,Seattle, WA

Chaired by: R. GREENDYKE, University of Texas at Tyler, Tyler, TX, and E. JOSYULA, Air Force Research Laboratory, Wright-Patterson AFB, OH0800AIAA-2004-1342 Modeling SingleComponent FluidTransport through MicroChannels and FreeMolecule Micro-Resistojet

R. Raju, KetteringUniversity, Flint, MI

0830AIAA-2004-1177 Unified Methods forContinuum and RarefiedFlows

V. Kolobov, CFDResearch Corporation,Huntsville, AL

0900AIAA-2004-1178 A Unified ComputationalMethodology forRarefied and ContinuumFlow Regimes

X. Cai, ThaerocompTechnical Corp., StonyBrook, NY

0930AIAA-2004-1179 Unified Gas- KineticComputationalAlgorithm for Continuumand Rarefied Flows

L. Tang, ZonaTechnology, Scottsdale,AZ

1000AIAA-2004-1180 A Hybrid CFD- DSMCMethod of ModelingContinuum- RarefiedFlows

H. Carlson, ClearSciences Corp.,Harford, NY

1030AIAA-2004-1182 Internal Energy ModeRelaxation in HighSpeed Continuum andRarefied Flows

E. Josyula, Air ForceResearch Laboratory,Wright-Patterson AFB,OH

1100AIAA-2004-1181 The Effect ofCompressibility onRarefied HypersonicFlow over Power LawLeading Edges

W. Santos, NationalInstitute for SpaceResearch, CachoeiraPaulista-SP, Brazil

1130AIAA-2004-1183 DSMC Modeling ofNear- Continuum FlowOver a Wedge with RealGas Effects

Y. Bondar, Institute ofTheoretical and AppliedMechanics, Novosibirsk,Russia

Chaired by: P. MIGLIORE, NREL's National Wind Technology Center, Golden, CO


Thursday Morning / 08 January 2004 Session 171-WE-7 Aeroacoustics Ruby

Thursday Morning / 08 January 2004 Session 172-WIG-9 MHD Teton

Thursday Afternoon / 08 January 2004 Session 173-ABP-10 Inlet/Nozzle & Jet Flows Cascade 2


Chaired by: P. MIGLIORE, NREL's National Wind Technology Center, Golden, CO0800AIAA-2004-1190 Numerical Simulation ofWind Turbine Tip Noise

O. Fleig, University ofTokyo, Tokyo, Japan

0830AIAA-2004-1185 Acoustic Tests of SmallWind Turbines

P. Migliore, NationalRenewable EnergyLaboratory, Golden, CO

0900AIAA-2004-1188 Wind TunnelAerodynamic Tests ofSix Airfoils for Use onSmall Wind Turbines

M. Selig, University ofIllinois atUrbana-Champaign,Urbana, IL

0930AIAA-2004-1186 Wind TunnelAeroacoustic Tests ofSix Airfoils for Use onSmall Wind Turbines

P. Migliore, NationalRenewable EnergyLaboratory, Golden, CO

1000AIAA-2004-1189 Development andValidation of a Semi-Empirical Wind TurbineAeroacoustic Code

P. Moriarty, NationalRenewable EnergyLaboratory, Golden, CO

1030AIAA-2004-1184 An AeroacousticAnalysis of WindTurbines

P. Morris, PennsylvaniaState University,University Park, PA

Chaired by: J. LINEBERRY, LYTEC, Tullahoma, TN, and V. BITYURIN, IVTAN, Moscow, Russia0800AIAA-2004-1191 Survey of Magneto-Gasdynamic Local FlowControl at High Speeds

D. Knight, RutgersUniversity, Piscataway,NJ

0830AIAA-2004-1192 Scramjet with MHDBypass Under "Ajax"Concept

E. Sheikin, HypersonicSystems ResearchInstitute,Saint-Petersburg, Russia

0900AIAA-2004-1193 Study of MHD-Interactions inHypersonic Streams

V. Fomin, ITAM,Novosibirsk, Russia

0930AIAA-2004-1194 Experimental andTheoretical Study ofMHD Interaction inHypersonic Ionized AirFlow Over a Wedge

J. Lineberry, LyTec,Tullahoma, TN

1000AIAA-2004-1195 MHD Controlled Inlet forScramjet with VariousConfigurations ofMagnetic Field

E. Sheikin, HypersonicSystems ResearchInstitute,Saint-Petersburg, Russia

1030AIAA-2004-1196 Simulation of Pulse-Mode Regime ofMagnetohydrodynamic(MHD) Section of theShock Tube

Y. Golovachov, IoffePhysical-technicalinstitute RAS, SaintPetersburg, Russia

1100AIAA-2004-1197 MHD Power Generationin Scramjet Engines inConjunction with InletControl

S. Macheret, PrincetonUniversity, Princeton, NJ

1130AIAA-2004-1198 MHD Effect Study atHigh FrequencyPlasmatron

A. Krasilnikov,TSNIIMASH, Korolev,Russia

Chaired by: N. BISSINGER, Eurojet, Hallbergmoos, Germany, and R. STARKEY, University of Maryland, College Park, MD1300AIAA-2004-1199 Computation ofTransverse Injection intoSupersonic Crossflowwith Various InjectorOrifice Geometries

L. Foster, NASA GlennResearch Center,Cleveland, OH

1330AIAA-2004-1200 Sensing for Active FlowControl in AdvancedPropulsion- AirframeIntegration Systems

J. Fleming, TechsburgInc., Blacksburg, VA

1400AIAA-2004-1201 Airframe- PropulsionIntegration Methodologyfor Waverider- DerivedHypersonic CruiseAircraft Design Concepts

K. Javaid, ImperialCollege London,London, Great Britain

1430AIAA-2004-1203 Active Flow Control on aBoundary- Layer-Ingesting Inlet

S. Gorton, NASALangley ResearchCenter, Hampton, VA

1500AIAA-2004-1204 Control of Penetrationand Mixing of aSupersonic Jet into aSupersonic Cross-Stream

S. Murugappan,University of Cincinnati,Cincinnati, OH

1530AIAA-2004-1205 Analysis of Jet- WingDistributed Propulsionfrom Thick Wing TrailingEdges

V. Dippold, VirginiaTech, Blacksburg, VA

1600AIAA-2004-1206 Improving Off- DesignNozzle PerformanceUsing Fluidic Injection

E. Gamble, SpiritechAdvanced Products Inc.,Jupiter, FL

Chaired by: H. EBRAHIMI, Sverdrup Technology, Inc., Arnold AFB, TN, and T. KAEMMING, The Boeing Company, Saint Louis, MO


Thursday Afternoon / 08 January 2004 Session 174-ABP-11 / PC-16 Pulse Detonation Engines IV Ruby

Thursday Afternoon / 08 January 2004 Session 175-AEE-2 Advanced Engineering Environment II McKinley

Thursday Afternoon / 08 January 2004 Session 176-AMT-7 Development and Use of Emerging Measurement Technologies Sierra 2


Chaired by: H. EBRAHIMI, Sverdrup Technology, Inc., Arnold AFB, TN, and T. KAEMMING, The Boeing Company, Saint Louis, MO1300AIAA-2004-1207 Interactions of a PulsedDetonation Engine witha 2D Blade Cascade

A. Rasheed, GeneralElectric GlobalResearch, Niskayuna,NY

1330AIAA-2004-1208 Interactions BetweenMultiple PDEsExhausting Into aCommon Nozzle

A. Glaser, University ofCincinnati, Cincinnati,OH

1400AIAA-2004-1209 Application of ReducedMechanisms forInvestigations ofHydrocarbon- AirPulsed DetonationEngines

V. Tangirala, GE GlobalResearch, Niskayuna,NY

1430AIAA-2004-1210 Numerical Investigationof the Effect of EnergyAddition Processes onPulsejet Performance

R. Erickson, GeorgiaInstitute of Technology,Atlanta, GA

1500AIAA-2004-1211 Statistical Design- of-Experiments for WaveEjector PerformanceImprovement

T. Geng, IndianaUniversity - PurdueUniversity, Indianapolis,IN

1530AIAA-2004-1212 Flow Test for PulseDetonation Engine

E. Gamble, SpiritechAdvanced Products Inc.,Jupiter, FL

1600AIAA-2004-1213 Development of Liquid-Fuel Initiator for Liquid-Fuel PDE

T. Yatsufusa, HiroshimaUniversity,Higashi-Hiroshima,Japan

1630AIAA-2004-1214 Homogeneous- DilutionModel of Partially-Fueled Pulse DetonationEngines

T. Endo, HiroshimaUniversity,Higashi-Hiroshima,Japan

Chaired by: J. MAPAR, Science Applications International Corporation, McLean, VA1300AIAA-2004-1215 RequirementsDevelopment for theNASA AdvancedEngineeringEnvironment (AEE)

E. Rogers, QTEC Inc.,Huntsville, AL

1330AIAA-2004-1216 SCDM in a DistributedEnvironment

S. Crowley, NASA,Cleveland, OH

1400AIAA-2004-1217 The JWST IntegratedModeling Environment

C. Stone, ConstellationSoftware Engineering,Huntingtown, MD

1430AIAA-2004-1218 Using Windchill ProductData ManagementPlatform for aDistributed SimulationSystem

T. Dunn, NorthropGrumman, VirginiaBeach, VA

1500AIAA-2004-1221 Generalized VehiclePerformance ClosureModel for Two- Stage-to- Orbit Launch Vehicles

M. Qu, AnalyticalMechanics Associates,Hampton, VA

Chaired by: D. FOURGUETTE, VioSense Corporation, Pasadena, CA, and G. ADAMOVSKY, NASA Glenn Research Center, Cleveland, OH1300AIAA-2004-1222 Laser AbsorptionSpectroscopy inInductive PlasmaGenerator Flows

M. Matsui, University ofTokyo, Tokyo, Japan

1330AIAA-2004-1223 Measurements inTurbulent Shear LayersUsing a Laser VorticityProbe

V. Stepaniuk,Polytechnic University,Brooklyn, NY

1400AIAA-2004-1224 Development of ThreeDimensional ParticleTracking Velocimetry forSupersonic Flow

N. Ponchaut, CaliforniaInstitute of Technology,Pasadena, CA

1430AIAA-2004-1226 Uncertainty Analysis ofLDV Measurements forCombustor Swirler Flow-Field

V. Iyer, GE GlobalResearch Center,Niskayuna, NY

1500AIAA-2004-1227 Theoretical Analysis ofthe UncertaintiesAssociated with OpticalPyrometry Techniques

R. Ames, Naval SurfaceWarfare Center,Dahlgren, VA

1530AIAA-2004-1229 Aerodynamic ForceMeasurements in ShockTunnels Using NovelFree Floating BalanceSystem

R. Joarder, IndianInstitute of Science,Bangalore, India

Chaired by: R. DOWGWILLO, The Boeing Company, Saint Louis, MO


Thursday Afternoon / 08 January 2004 Session 177-APA-19 CFD Applications II Carson 1

Thursday Afternoon / 08 January 2004 Session 178-APA-20 Configurational Aerodynamics II Carson 2

Thursday Afternoon / 08 January 2004 Session 179-APA-21 Weapons Aerodynamics Carson 3


Chaired by: R. DOWGWILLO, The Boeing Company, Saint Louis, MO1300AIAA-2004-1230 Solution of Euler andNavier- StokesEquations onUnstructured/StructuredMulti- layer Hybrid Grid

W. Sang, NorthwesternPolytechnical University,Xi'an, China (prc)

1330AIAA-2004-1231 CFD Visualization ofSecond Primary VortexStructure on a 65-Degree Delta Wing

K. Chiba, TohokuUniversity, Sendai,Japan

1400AIAA-2004-1232 Applications of Space-Filling- Curves toCartesian Methods forCFD

M. Aftosmis, NASAAmes Research Center,Moffett Field, CA

1430AIAA-2004-1233 Detached- EddySimulation of Slat andFlap Aerodynamics fora High- Lift Wing

R. Cummings, U.S. AirForce Academy, USAFAcademy, CO

1500AIAA-2004-1234 Variable- FidelityAerodynamicOptimization forTurbulent Flows Using aDiscrete AdjointFormulation

A. Le Moigne, Universityof Sheffield, Sheffield,Great Britain

1530AIAA-2004-1235 Computations of theWake Vortices Behind aCivil Aircraft High LiftModel

A. Dafa'Alla, Airbus UKLtd, Bristol, Great Britain

1600AIAA-2004-1236 Source Term Model forVortex Generator Vanesin a Navier- StokesComputer Code

K. Waithe, NASALangley, Hampton, VA

1630AIAA-2004-1237 A Cfd- ExperimentalComparison for a LowThrust Satellite Nozzlewith Estimation ofForces on a Jet VanePlaced at SupersonicExhaust

B. Bukhari, Computer &IT Center, Islamabad,Pakistan

Chaired by: S. KLAUSMEYER, Cessna Aircraft Company, Wichita, KS, and S. DODBELE, Department of Defense, Arlington, VA1300AIAA-2004-1238 The Fuel EconomyPotential of Outboard-Horizontal- StabilizerAircraft

J. Kentfield, Universityof Calgary, Calgary,Canada

1330AIAA-2004-1239 The Effect of the PorousDiverter Fairing on theAerodynamicPerformance of NaturalBlockage ThrustReverser

H. Yao, Queen'sUniversity Belfast,Belfast, Great Britain

1400AIAA-2004-1245 Design of High AspectRatio "Lambda- Wings"Incorporating LaminarFlow

R. Nangia, Nangia AeroResearch, Bristol, GreatBritain

1430AIAA-2004-1240 Edge Vortices of aDouble Element Wing inGround Effect

X. Zhang, University ofSouthampton,Southampton, GreatBritain

1500AIAA-2004-1241 Considerations AboutForward FuselageAerodynamic Design ofa Transport Aircraft

B. Mattos, Embraer, SaoJose Dos Campos,Brazil

1530AIAA-2004-1242 Vortex Generators nearShock/ Boundary LayerInteractions

H. Holden, University ofCambridge, Cambridge,Great Britain

1600AIAA-2004-1243 Separation Control bySelf- Activated MovableFlaps

M. Schatz, TechnischeUniversität Berlin,Berlin, Germany

1630AIAA-2004-1244 Characteristics of aDual- Slotted CirculationControl Wing of LowAspect Ratio Intendedfor Naval HydrodynamicApplications

E. Rogers, NavalSurface Warfare Center,West Bethesda, MD

Chaired by: F. TAVERNA, Naval Air Systems Command, Patuxent River, MD1300AIAA-2004-1246 AerodynamicPredictions,Comparisons, andValidations UsingMissile Datcom andAeroprediction 98 (AP98)

T. Sooy, TechnologyService Corporation,Silver Spring, MD

1330AIAA-2004-1249 Simulation of Missilewith Spinning Tail FinUsing Chimera MovingBody Methodology

L. Hall, Dynetics Inc.,Huntsville, AL

1400AIAA-2004-1250 Use of Cargo Aircraft forLaunching Precision-Guided Munitions

M. Franke, Air ForceInstitute of Technology,Wright-Patterson AFB,OH

1430AIAA-2004-1251 Beggar CodeImplementation of the(6+)DOF Capability forStores with MovingComponents

M. Rizk, JacobsSverdrup, Eglin AFB, FL

1500AIAA-2004-1252 Simulation and Analysisof Multiple- BodyDispense Event

W. Dietz, Flow AnalysisInc., Estill Springs, TN

1530AIAA-2004-1253 Flow Around an ObjectProjected from a Cavityinto a SupersonicFreestream

S. Bjorge, Air ForceInstitute of Technology,Wright Patterson AFB,OH


Thursday Afternoon / 08 January 2004 Session 180-ASE-9 Low-Earth-Orbit Space Environment N5

Thursday Afternoon / 08 January 2004 Session 181-CS-2 Computer and Information Systems Crystal 5

Thursday Afternoon / 08 January 2004 Session 182-FD-32 CFD Validation/Comparison to Experiment II Carson 4


Chaired by: J. MINOW, Sverdrup Technology, Inc., Huntsville, AL, and K. TOBISKA, Space Environment Technologies, Los Angeles, CA1300AIAA-2004-1254 Advances in SatelliteDrag Modeling

F. Marcos, Air ForceResearch Laboratory,Hanscom AFB, MA

1330AIAA-2004-1257 Sources of OH(A- X)Emission in the SpaceShuttle Environment

L. Bernstein, SpectralSciences Inc.,Burlington, MA

1400AIAA-2004-1258 Simulated SpaceEnvironment Exposureof Surface- ModifiedThermal ControlCoatings

J. Kleiman, IntegrityTesting Laboratory,Markham, Canada

1430AIAA-2004-1259 LEO SpacecraftCharging DesignGuidelines: A ProposedNASA Standard

G. Hillard, NASA GlennResearch Center,Cleveland, OH

1500AIAA-2004-1260 Paschen Considerationsfor High Altitude Airships

D. Ferguson, NASAGlenn Research Center,Cleveland, OH

Chaired by: R. MOORE, Johns Hopkins University, Applied Physics Laboratory, Laurel, MD1300AIAA-2004-1262 Application of Object-Oriented DesignPatterns to CFD Codewith AMR Technique

H. Katsurayama,University of Tokyo,Tokyo, Japan

1330AIAA-2004-1263 Advanced ComputerTechnology for NovelInformation ProcessingParadigms

C. Thiem, Air ForceResearch Laboratory,Rome, NY

1400AIAA-2004-1264 The Future of ArchivalJournals in theInformation Age:Communities of Practice

L. Long, PennsylvaniaState Univ., UniversityPark, PA

1430AIAA-2004-1265 Risks of Using COTSProducts in MissionCritical Systems

R. Kohl, R. J. Kohl &Associates Inc.,Jefferson, MD

1500AIAA-2004-1266 Wind Tunnel DataFormat for Test ResultsPresentation

R. Draai, German-DutchWind Tunnels,Amsterdam, TheNetherlands

Chaired by: M. GLAUSER, Syracuse University, Syracuse, NY, and R. KIMMEL, Air Force Research Laboratory, Wright-Patterson AFB, OH1300AIAA-2004-1268 Preconditioned UpwindSchemes for Simulationof Low Speed Flows onHybrid Grids

Z. Liu, HyperComp Inc.,Westlake Village, CA

1330AIAA-2004-1269 Comparison of 2D PODModes Extracted fromTwo and Three-Dimensional Simulationsof a Cylinder Wake

M. Luchtenburg, US AirForce Academy,Colorado Springs, CO

1400AIAA-2004-1270 Mixing Characteristics ofTwo- DimensionalParallel Jets

T. Abdel-Salam, EastCarolina University,Greenville, NC

1430AIAA-2004-1271 Aeroelastic Analysis ofan SST Typed Wing witha Trailing Edge FlapUsing a Chimera GridApproach

Y. Utaka, MitsubishiHeavy Industries Ltd.,Nagoya, Japan

1500AIAA-2004-1273 Implementation ofPremixed ChemicalEquilibrium Capability inOVERFLOW

M. Olsen, NASA Ames,Moffett Field, CA

Chaired by: Z. RUSAK, Rensselaer Polytechnic Institute, Troy, NY, and C. FUREBY, Swedish Defence Research Agency, Stockholm, Sweden1300 1330 1400 1430


Thursday Afternoon / 08 January 2004 Session 183-FD-33 Engineering Applications of CFD Crystal 1

Thursday Afternoon / 08 January 2004 Session 184-FD-34 Fundamental Experiments in Jets and Cavities Crystal 2

Thursday Afternoon / 08 January 2004 Session 185-FD-35 Multi-Phase Flows N8


Chaired by: Z. RUSAK, Rensselaer Polytechnic Institute, Troy, NY, and C. FUREBY, Swedish Defence Research Agency, Stockholm, Sweden1300AIAA-2004-1274 Using RANS to Predictthe Performance ofMixers in Reducing JetNoise

C. Wright, PurdueUniversity, WestLafayette, IN

1330AIAA-2004-1276 Effect of Coriolis andCentrifugal Forces onTurbulence andTransport at HighRotation and BuoyancyNumbers in InternalCooling U- Channelswith Smooth Walls

A. Sleiti, University ofCentral Florida, Orlando,FL

1400AIAA-2004-1277 Prediction of Helicopter'sRotor Airloads inTransition Flight Regime

Z. Rusak, RensselaerPolytechnic Institute,Troy, NY

1430AIAA-2004-1278 Numerical Studies ofBlade Sweep Effects onLosses

C. Xu, University ofWisconsin, Milwaukee,WI

Chaired by: S. GOGINENI, Innovative Scientific Solutions Inc, Wright-Patterson AFB, OH, and J. JACOB, University of Kentucky, Lexington, KY1300AIAA-2004-1279 ConcentrationMeasurements in Self-Excited Momentum-Dominated Low- DensityGas Jets

B. Yildrim, University ofOklahoma, Norman, OK

1330AIAA-2004-1280 Far- Field TurbulentMixing Efficiency andLarge- Scale Outer-Fluid- Interface Dynamics

J. Nathman, University ofCalifornia Irvine, Irvine,CA

1400AIAA-2004-1281 On the Occurrence ofAsymmetric Flow Withina Circular Concavity

T. New, NationalUniversity of Singapore,Singapore, Singapore

Chaired by: M. AMITAY, Rensselaer Polytechnic Institute, Troy, NY, and M. NEAVES, Coastal Systems Station, Panama City, FL1300AIAA-2004-1282 Time- Accurate All-Speed MultiphaseCalculations Using aLow- Diffusion Flux-Splitting Scheme

M. Neaves, NavalSurface Warfare Center,Panama City, FL

1330AIAA-2004-1283 Turbulence Models forFlows with FreeSurfaces and Interfaces

E. Shirani, University ofToronto, Toronto,Canada

1400AIAA-2004-1284 Direct NumericalSimulation of DisperseMultiphase High- SpeedFlows

R. Nourgaliev, Universityof California SantaBarbara, Santa Barbara,CA

Chaired by: D. GAITONDE, Air Force Research Laboratory, Wright-Patterson AFB, OH


Thursday Afternoon / 08 January 2004 Session 186-FD-36 Turbulent Boundary Layers with Roughness or Heat Transfer N7

Thursday Afternoon / 08 January 2004 Session 187-GT-9 Ground Test Applications Crystal 3

Thursday Afternoon / 08 January 2004 Session 188-IS-3 Intelligent Systems III Crystal 4


Chaired by: D. GAITONDE, Air Force Research Laboratory, Wright-Patterson AFB, OH1300AIAA-2004-1287 Rough SurfaceTurbulent BoundaryLayer: Part 2 TheComposite Profiles

J. Seo, RensselaerPolytechnic Institute,Troy, NY

1330AIAA-2004-1288 Similarity Analysis inTranspired TurbulentBoundary LayersSubject to ForcedConvection and ExternalPressure Gradients

R. Cal, RensselaerPolytechnic Institute,Troy, NY

1400AIAA-2004-1289 A Prediction of theComposite TemperatureProfile in ForcedConvection TurbulentBoundary Layers

X. Wang, RensselaerPolytechnic Institute,Troy, NY

1430AIAA-2004-1290 Aplication of aSensitivity EquationMethod to TurbulentFlows with Heat Transfer

E. Colin, EcolePolytechnique deMontreal, Montreal,Canada

1500AIAA-2004-1291 Wind Tunnel Modelingof Stack Dispersion inComplex Terrain

B. White, University ofCalifornia, Davis, Davis,CA

1530AIAA-2004-1286 Transport- rate Budgetsof Reynolds Stresses in2- D and 3- D Rough-wall Turbulent BoundaryLayers

J. George, Virginia Tech,Blacksburg, VA

Chaired by: F. JACKSON, Sverdrup Technology, Inc., Arnold AFB, TN, and J. MAGILL, Physical Sciences Inc, Andover, MA1300AIAA-2004-1292 Evaluation of WindTunnel Internal ForceBalances from MultipleVendors

D. Cahill, JacobsSverdrup AEDC Group,Arnold AFB, TN

1330AIAA-2004-1293 Structural Integrity of aWind Tunnel Balance

R. Karkehabadi, NASALangley, Hampton, VA

1400AIAA-2004-1294 A Study on Increase ofDuration of a FreePiston Shock Tunnel

M. Mizoguchi, NationalDefense Academy,Yokosuka, Japan

1430AIAA-2004-1295 ExperimentalCharacterization ofSupersonic Spin MotorNozzle Flow

C. Peterson, SandiaNational Laboratories,Albuquerque, NM

1500AIAA-2004-1296 Demonstration of a WireSuspension System forDynamic Wind TunnelTesting

J. Magill, PhysicalSciences Inc., Andover,MA

1530AIAA-2004-1297 Validation of StreamThrust Probes forTurbine Engine ThrustMeasurement

R. Hiers, JacobsSverdrup/AEDC Group,Arnold AFB, TN

1600AIAA-2004-1298 Subscale Testing of theFire II Vehicle in aSuperorbital ExpansionTube

B. Capra, University ofQueensland, Brisbane,Australia

Chaired by: M. HANSON, Charles River Analytics, Cambridge, MA, and J. NEIDHOEFER, Accurate Automation Corporation, Chattanooga, TN1300AIAA-2004-1302 Genetic AlgorithmTuned Fuzzy Logic forGliding ReturnTrajecotries

B. Burchett,Rose-Hulman Institute ofTechnology, TerreHaute, IN

1330AIAA-2004-1303 A Testbed forEvaluating SoftComputingTechnologies for RocketEngine Control

A. Watanabe, Universityof Alabama, Tuscaloosa,AL

1400AIAA-2004-1304 A New IntelligentGenetic Algorithm forAerodynamicOptimizations ofAdvanced Fighters

J. Liu, Leader University,Tainan, Taiwan (roc)

1430AIAA-2004-1305 Designing HumanSystem Interfaces forSupervising MultipleUAV Teams

M. Hanson, CharlesRiver Analytics Inc.,Cambridge, MA

1500AIAA-2004-1306 Flight Control Logic forStructural Life Extension

S. Yu, Old DominionUniversity, Norfolk, VA

Chaired by: A. OSTROGORSKY, Rensselaer Polytechnic Institute, Troy, NY, and R. GRUGEL, NASA Marshall Space Flight Center, Huntsville, AL1300 1330 1400 1430 1500 1530 1600 1630


Thursday Afternoon / 08 January 2004 Session 189-MSSP-8 Microgravity Materials Science II & Space Hardware N6

Thursday Afternoon / 08 January 2004 Session 190-MSSP-9 Outreach and Microgravity Fluid Physics III N4

Thursday Afternoon / 08 January 2004 Session 191-PC-17 Combustion Chemistry and Flames Shasta 1


Chaired by: A. OSTROGORSKY, Rensselaer Polytechnic Institute, Troy, NY, and R. GRUGEL, NASA Marshall Space Flight Center, Huntsville, AL1300AIAA-2004-1307 Free Form Fabricationin Space

K. Cooper, NASAMarshall, Huntsville, AL

1330AIAA-2004-1308 Modeling of ThermalField, KInetics andStresses of CdZnTeBridgman GrowthWithout Wall Contact

R. Ma, Stony BrookUniversity, Stony Brook,NY

1400AIAA-2004-1310 Experimental Techniquefor Studying High-Temperature Phases inReactive Molten Metal-Based Systems

A. Ermoline, NewJersey Institute ofTechnology, Newark, NJ

1430AIAA-2004-1311 The Effects of anUnsteady ReducedGravity Environment onthe Soldering Process

P. Struk, NASA Glenn,Cleveland, OH

1500AIAA-2004-1312 Microgravity Furnacesand SampleContainment: AReflective Perspective

D. Schaefer, NASAMarshall Space FlightCenter, Huntsville, AL

1530AIAA-2004-1313 The Reconfiguration ofthe Low TemperatureMicrogravity PhysicsFacility

M. Larson, JetPropulsion Laboratory,Pasadena, CA

1600AIAA-2004-1314 Hyperspectral Imagingon the InternationalSpace Station: AnInnovative Approach toCommercialDevelopment of Space

R. Robinson, NASAMarshall Space FlightCenter, Huntsville, AL

1630AIAA-2004-1388 Solidification of Te andZn Doped InSb in Space

A. Churilov, RensselaerPolytechnic Institute,Troy, NY

Chaired by: J. LACOMBE, University of Nevada Reno, Reno, NV, and S. COLLICOTT, Purdue University, West Lafayette, IN1300AIAA-2004-1315 High- school StudentTeams in a NationalNASA MicrogravityScience Competition

R. DeLombard, NASAGlenn, Cleveland, OH

1330AIAA-2004-1317 Numerical Simulationsof Buoyancy Effects inLow Density Gas Jets

R. Satti, University ofOklahoma, Norman, OK

1400AIAA-2004-1318 Numerical Modeling ofBuoyancy Induced Flowand Heat Transfer in aRotating ChamberUnder Zero GravityEnvironment

A. Gupta, University ofAlabama, Tuscaloosa,AL

1430AIAA-2004-1320 Characterization ofEnvironment in Micro-Bioreactor for Bone Cells

J. Kizito, National Centerfor MicrogravityResearch, Cleveland,OH

1500AIAA-2004-1321 Thermal Convection in aCylindrical Enclosure

K. Shukla, VikramSarabhai Space Center,Trivandrum, India

1530AIAA-2004-1371 Three- DimensionalConvection in RealisticMicrogravityEnvironment & Analysisof the MicroaccelerationsRequirements

V. Polezhaev, RussianAcademy of Sciences,Moscow, Russia

Chaired by: L. MAURICE, Federal Aviation Administration, Washington, DC, and C. SUNG, Case Western Reserve University, Cleveland, OH1300AIAA-2004-1322 A Shock Tube Study ofthe Oxidation of 1,3-Butadiene

C. Libby, StanfordUniversity, Stanford, CA

1330AIAA-2004-1323 Ignition Measurementsof Ethylene- Oxygen-Diluent Mixtures Withand Without SilaneAddition

D. Kalitan, TheAerospace Corporation,El Segundo, CA

1400AIAA-2004-1324 Heptane CombustionDatabase

W. Tsang, NationalInstitute of Standardsand Technology,Gaithersburg, MD

1430AIAA-2004-1325 Propane AutoignitionTheory

M. Petrova, University ofCalifornia, San Diego,La Jolla, CA

1500AIAA-2004-1326 Approaches toMechanism Reductionfor HydrocarbonOxidation: Ethylene

T. Lu, PrincetonUniversity, Princeton, NJ

1530AIAA-2004-1328 Effects of MixtureInhomogeneity on theAuto- Ignition ofReactants Under HCCIEnvironment

R. Sankaran, Universityof Michigan, Ann Arbor,MI

1600AIAA-2004-1329 Investigation of n-Heptane/Air PartiallyPremixed Flames UsingDetailed ReactionMechanisms

S. Naha, University ofIllinois at Chicago,Chicago, IL

1630AIAA-2004-1327 Theory of High-Temperature Hydrogen-Oxygen Autoignition

G. del Alamo Serrano,University of CaliforniaSan Diego, La Jolla, CA

Chaired by: O. HAIDN, DLR, Lampoldshausen, Germany, and D. KENDRICK, Pratt & Whitney, Bellevue, WA


Thursday Afternoon / 08 January 2004 Session 192-PC-18 Rocket Mixing, Combustion and Propellants Shasta 2

Thursday Afternoon / 08 January 2004 Session 193-TP-9 Heat Transfer Applications N10

Thursday Afternoon / 08 January 2004 Session 194-TP-10 Radiation and Plumes N9


Chaired by: O. HAIDN, DLR, Lampoldshausen, Germany, and D. KENDRICK, Pratt & Whitney, Bellevue, WA1300AIAA-2004-1330 The Effects of Pressureand Acoustic Field on aCryogenic Coaxial Jet

B. Chehroudi, Air ForceResearch Laboratory,Edwards AFB, CA

1330AIAA-2004-1332 Mixing and Combustionof Swirl Co- AxialInjectors for CryogenicPropellants atSupercritical Conditions

N. Zong, PennsylvaniaState University,University Park, PA

1400AIAA-2004-1333 Numerical Simulation ofAluminized CompositeSolid Propellants

X. Wang, University ofIllinois atUrbana-Champaign,Urbana, IL

1430AIAA-2004-1334 Electrolyzer PowerRequirements forOxidizer Production onMars

C. Iacomini, Universityof Arizona, Tucson, AZ

1500AIAA-2004-1335 An ExperimentalInvestigation ofHypergolic IgnitionDelay of HydrogenPeroxide with FuelMixtures

J. Blevins, NASAMarshall, Huntsville, AL

1530AIAA-2004-1337 Modeling of LiftedTurbulent Flame by theFlame Edge Theory andIts Implication in LiquidRocket CombustionInstability

J. Kim, Seoul NationalUniversity, Seoul, SouthKorea

1600AIAA-2004-1381 Atmospheric Effects onthe Chemical DelayTime for HypergolicBipropellants

C. Hampton, Universityof Alabama in Huntsville,Huntsville, AL

Chaired by: S. ROY, Kettering University, Flint, MI, and J. FRANKEL, University of Tennessee, Knoxville, TN1300AIAA-2004-1339 Thermal Managementof a Motor Drive PowerModule by LiquidImpingement Cooling

A. Bhunia, RockwellScientific Company,Thousand Oaks, CA

1330AIAA-2004-1340 Large Area SprayCooling

L. Lin, Universal EnergySystems, Inc., Dayton,OH

1400AIAA-2004-1341 Self- Pressurization andThermal Stratification ina Liquid Hydrogen TankUnder Varying GravityConditions

S. Venkat, University ofFlorida, Gainesville, FL

1430AIAA-2004-1176 Heat Transfer on aHypersonic Sphere withDiffuse Rarefied- GasInjection

V. Riabov, RivierCollege, Nashua, NH

1500AIAA-2004-1343 Effect of Pulse JetFrequency onImpingement HeatTransfer

R. Zulkifli, Queen'sUniversity of Belfast,Belfast, Northern Ireland

1530AIAA-2004-1344 Unsteady Surface HeatFlux Under a Three-Dimensional CrossflowBoundary Layer

R. Anthony, Air ForceResearch Laboratory,Wright-Patterson AFB,OH

1600AIAA-2004-1345 Gas Effects on SprayCooling of an IsothermalSurface: Visualizationand Time and SpaceResolved Heat TransferMeasurements

B. Horacek, Universityof Maryland, CollegePark, MD

1630AIAA-2004-1346 Rotating Disk HeatTransfer in a FluidSwirling as a ForcedVortex

I. Shevchuk, UkrainianNational Academy ofSciences, Kiev, Ukraine

Chaired by: D. MUELLER, Indiana University-Purdue Universtiy at Fort Wayne, Fort Wayne, IN, and C. MOEN, Sandia National Laboratories, Livermore, CA1300AIAA-2004-1348 Plume Interactions ofMultiple Jets ExpandingInto Vacuum:ExperimentalInvestigation

N. Selden, University ofSouthern California, LosAngeles, CA

1330AIAA-2004-1349 Radiation of SpalledParticles in Shock Layers

C. Park, ELORET Corp,Moffett Field, CA

1400AIAA-2004-1350 Modeling of SootOxidation and Predictionof Optical Radiation inUnderexpanded Plumes

K. Viswanath,Pennsylvania StateUniversity, UniversityPark, PA

1430AIAA-2004-1351 Development of a Two-Way Coupled Model forTwo Phase RarefiedFlows

J. Burt, University ofMichigan, Ann Arbor, MI

1500AIAA-2004-1352 Active Shock- tube-diaphragm Rupture withLaser Beam Irradiation

T. Takahashi, TohokuUniversity, Sendai,Japan

1530AIAA-2004-0484 The Impact of Flowfield-Radiation Coupling onAeroheating for TitanAerocapture

M. Wright, ELORETCorp., Moffett Field, CA

Chaired by: L. BAIN, Universal Technology Corporation, Dayton, OH, and Y. KOLESNICHENKO, IVTAN, Moscow, Russia


Thursday Afternoon / 08 January 2004 Session 195-WIG-10 Workshop Summary & Recommendations Teton

Chaired by: L. BAIN, Universal Technology Corporation, Dayton, OH, and Y. KOLESNICHENKO, IVTAN, Moscow, Russia1300AIAA-2004-1356 Test Cell for Study ofPlasma FormationsEffect on Ignition andCombustion Stabilization

V. Vinogradov, CentralInstitute of AviationMotors, Moscow, Russia

1330AIAA-2004-1357 Research IssuesResulting fromCataloging Efforts

C. Suchomel, Air ForceResearch Laboratory,Wright-Patterson AFB,OH

agenda

Documents

university of illinois

university of cincinnati

university of california

ny university

florida state university

control derivatives

acoustic coupling of

acoustics of dualstream