45th AIAA Aerospace Sciences Meeting and Exhibit

45th AIAA Aerospace Sciences Meeting and Exhibit 

8 - 11 Jan 2007 Grand Sierra Resort Hotel (Formerly Reno Hilton) Reno, Nevada 

Monday Morning / 08 January 2007 

Session 1-AA-1 Jet Noise: Modeling N-10 

Chaired by: A. LYRINTZIS, Purdue University, West Lafayette, IN, and C. SHIEH, General Electric Global Research Center, Niskayuna, NY 

0800 

AIAA-2007-0011 

Numerical Study of 

Fluidic Injection for 

Noise Reduction 

M. Aberg, Lund 

University, Dept. Energy 

Sciences, Lund, Sweden 

0830 


Progress Toward 

Improving Jet Noise 

Predictions in Hot Jets 

A. Khavaran, NASA 

Glenn Research Center, 

Cleveland, OH 


0900 


Computational 

Aeroacoustics of a 

Separate Flow Exhaust 

System with Eccentric 

Inner Nozzle 

M. Mihaescu, University 

of Cincinnati, Cincinnati, 

OH 

0930 


Modeling Acoustic 

Effects on Coaxial 

Shear Injection Jet Flow 

using Molecular 

Dynamics Techniques 

J. Sailsman, Air Force 

Institute of Technology, 

Wright-Patterson AFB, 

OH 

1000 


Measurements in a Co- 

Axial Subsonic Jet 

A. Guitton, University of 

Poitiers, Poitiers, France 

1030 


Investigation of Noise 

Sources in Turbulent 

Hot Jets Using Large 

Eddy Simulation Data 

P. Lew, Purdue 

University, West 

Lafayette, IN 

Session 2-ABP-1 Compressors and Fans Whitney 

Chaired by: R. BRUCKNER, NASA Glenn Research Center, Cleveland, OH, and S. GORRELL, U.S. Air Force Research Laboratory, Wright-Patterson AFB, OH 

0800 


A Numerical Study of 

Water Injection on 

Transonic Compressor 

Rotor Performance 

I. Szabo, University of 

Cincinnati, Cincinnati, 

OH 

0830 


A Turbomachinery 

Gridding System 

M. Kamp, University of 

Cincinnati, Erlanger, KY 

0900 


Rotor Wake Variability in 

a Multistage Compressor 

N. Key, Purdue 


Lafayette, IN 

0930 


Aerodynamic Damping 

Effects on the Resonant 

Response of Mistuned 

IBRs 

Y. Choi, Purdue 


Lafayette, IN 

1000 


Modeling the 

Aerodynamic 

Performance of Modern 

Axial Flow Compressor 

Profiles: A Correlative 

Approach Using Current 

CFD Technology 

D. Bruna, DIMSET, 

Genova, Italy 

1030 


Design Refinement and 

Performance Analysis of 

Two- Stage Fan for 

Small Turbofan Engines 

J. Masud, National 

University of Sciences & 

Technology, Risalpur, 

Pakistan 

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=1064&dateget=all#session7328. 

Chaired by: D. LEWIS, ATK, Rocket Center, WV, and R. SPRINGER, Aerojet, Sacramento, CA 

0800 0830 0900 0930 1000 1030


Session 3-ABP-2 High Speed Propulsion I Cascade 2 

Chaired by: D. LEWIS, ATK, Rocket Center, WV, and R. SPRINGER, Aerojet, Sacramento, CA 

0800 


Numerical Investigation 

of a Super- Sonic Inlet 

Using Bleed and Micro- 

Ramps to Control 

Shock- Wave/Boundary 

Layer Interactions 

M. Atkinson, Air Force 

Research 

Laboratory/VAAC, 


OH 

0830 


Use of a Translating 

Cowl on a SSBJ for 

Improved Takeoff 

Performance 

A. Garzon, Aerion 

Corporation, Reno, NV 


Session 4-AD-1 Alternate Propulsion and Shape Optimization Crystal 3 


0900 


Analytical Computation 

of Leading Edge 

Truncation Effects on 

Inviscid Busemann Inlet 

Performance 

T. O'Brien, Aerojet, 

Sacramento, CA 

0930 


Study of Inlet Flow Field 

with Gas Jet Injection 

V. Vinogradov, Central 

Institute of Aviation 

Motors, Moscow, Russia 

1000 


Computational Fluid 

Dynamic Analysis of 

Scramjet Inlet 

D. Rozario, University of 

Wales, Wrexham, Great 

Britain 

Chaired by: D. SOBAN, Georgia Institute of Technology, Atlanta, GA, and M. PRICE, Queen's University, Belfast, Northern Ireland 

0800 


Flight Test Results for a 

Fuel Cell Unmanned 

Aerial Vehicle 

T. Bradley, Georgia 


Atlanta, GA 

0830 


A Comprehensive 

Global Model of 

Broadband Direct Solar 

Radiation for Solar Cell 

Simulation 

H. Ran, Georgia 


Atlanta, GA 

0900 


Operational 

Performance Prediction 

of a Hydrogen- Fueled 

Commercial Transport 

D. Maniaci, 

Pennsylvania State 

University, University 

Park, PA 

0930 


Development Nuclear 

Gas Core Reactor in 

Russia 

A. Koroteev, Keldysh 

Center, Moscow, Russia 

1000 


Multi- Objective / 

Multidisciplinary Design 

Optimisation of Blended 

Wing Body UAV via 

Advanced Evolutionary 

Algorithms 

D. Lee, University of 

Sydney, Sydney, 

Australia 

1030 


Numerical Analysis of 

Rectangular Plug Nozzle 

Considering Practical 

Geometry and Flow 

Conditions 

H. Miyamoto, Keio 

University, Yokohama, 

Japan 

1030 


An Investigation of the 

Attainable Efficiency of 

Flight at Mach One or 

Just Beyond 

A. Jameson, Stanford 

University, Stanford, CA 

1100 


A Study of Transport 

Aircraft High- Lift Design 

Approaches 

A. Antunes, 

Universidade de Sao 

Paulo, Sao Paulo, Brazil 

Session 5-AFM-1 Aeromechanics of Animal Flight (Invited) Carson 3 

Chaired by: J. EVERS, U.S. Air Force Research Laboratory, Eglin AFB, FL, and M. OL, U.S. Air Force Research Laboratory, Wright-Patterson AFB, OH 

0800 


Flight Control 

Mechanisms in Birds of 

Prey 

G. Taylor, Oxford 

University, Oxford, 

Great Britain 

0830 


Unique Properties of 

Lateral- Directional 

Stability and Control in 

Birds 

G. Sachs, Technische 

Universitat Munchen, 

Garching, Germany 

0900 


The Aerodynamics of 

Hummingbird Flight 

D. Warrick, Oregon 

State University, 

Corvallis, OR 

0930 


Wing Structure and the 

Aerodynamic Basis of 

Flight in Bats 

S. Swartz, Brown 

University, Providence, 

RI 

1000 


Use and Function of a 

Leading Edge Flap on 

the Wings of Eagles 

A. Carruthers, Oxford 

University, Oxford, Great 

Britain 

1030 


Experimental Study of 

Low Speed Turning 

Flight in Cockatoos and 

Cockatiels 

T. Hedrick, University of 

North Carolina, Chapel 

Hill, NC 

1100 


Flight Mechanic and 

Aerodynamic Aspects of 

Extremely Large 

Dihedral in Birds 

G. Sachs, Technische 

Universitat Munchen, 

Garching, Germany



Chaired by: N. CLEMENS, University of Texas at Austin, Austin, TX, and S. BERESH, Sandia National Laboratories, Albuquerque, NM 

0800 0830 0900 0930 1000 1030 1100 

Chaired by: R. HARTFIELD, Auburn University, Auburn University, AL 

0800 0830 0900 0930 1000 1030 1100 1130 

Chaired by: K. MASSEY, Georgia Technical Research Institute, Smyrna, GA 

0800 0830 0900 0930


Session 6-AMT-1 Development and Application of Velocimetry Techniques Shasta 2 

Chaired by: N. CLEMENS, University of Texas at Austin, Austin, TX, and S. BERESH, Sandia National Laboratories, Albuquerque, NM 

0800 


Time Resolved PIV for 

Space- Time 

Correlations in Hot Jets 

M. Wernet, NASA Glenn 

Research Center, 


0830 


A miniature 3simultaneous 

velocity 

component LDV probe 

O. Ivanchenko, 

University of Alabama, 

Tuscaloosa, AL 


Session 7-APA-1 Aerodynamic Design Optimisation Carson 1 


0900 


Aerodynamic Load 

Measurement of a Low 

Speed Airfoil Using 

Particle Image 

Velocimetry 

B. van Oudheusden, 

Delft University of 

Technology, Delft, The 

Netherlands 

Chaired by: R. HARTFIELD, Auburn University, Auburn University, AL 

0800 


Adjoint Formulations for 

Topology, Shape and 

Discrete Optimization 

S. Jameson, Stanford 


0830 


Sonic Boom Reduction 

via Remote Inverse 

Adjoint Approach 

S. Nadarajah, McGill 

University, Montreal, 

Canada 

0900 


Adjoint- Based 

Optimisation of a 

Blended Wing Body 

Aircraft with Shock 

Control Bumps 

N. Qin, University of 

Sheffield, Sheffield, 

Great Britain 

0930 



Velocimetry Based 

Loads Determination in 

Supersonic Flows 

L. Souverein, Delft 

University of 



1000 


Processing High- Speed 

Stereo Particle Image 

Velocimetry Data with an 

Integrated Cluster 

Supercomputer 

M. Perl, Utah State 

University, Logan, UT 

1030 


Measurements in the 

Near Field of a Swirling 

Jet Using CTA, LDA, 

and PLS 

J. Naughton, University 

of Wyoming, Laramie, 

WY 

1100 


Preliminary Tests of 

High Speed PIV 

Measurements in a 

Ludwieg- Tube 

Supersonic Wind Tunnel 

K. Juhany, King 

Abdulaziz Univesity, 

Jeddah, Saudi Arabia 

Session 8-APA-2 Aerodynamic Stability and Control N-9 

Chaired by: K. MASSEY, Georgia Technical Research Institute, Smyrna, GA 

0800 


Novel Locally Swept 

Lattice Wings for Missile 

Control at High Speeds 

D. Guyot, University of 

Technology Berlin, 

Berlin, Germany 

0830 


Aerodynamic Loading 

and Stability of an 

Aircraft with Outboard 

Horizontal Stabilizers 

J. Kentfield, University of 

Calgary, Calgary, 

Canada 

0900 


Development and 

Testing of MEMS Control 

Surfaces for High Speed 

Projectiles 

M. Deeds, Naval 

Surface Warfare Center, 

Indian Head, MD 

0930 


Numerical Study of the 

Optimization of 

Separation Control 

A. Carnarius, Technical 

University of Berlin, 


0930 


Novel Pitch Control 

Effectors for a Blended 

Wing Body Airplane in 

Takeoff and Landing 

Configuration 

Y. Staelens, University 

of Southern California , 

Los Angeles, CA 

1000 


Effect of Shape 

Parameterization on 

Aerodynamic Shape 

Optimization 

P. Castonguay, McGill 


Canada 

1030 


An Unsteady Discrete 

Adjoint Formulation for 

Two- Dimensional Flow 

Problems with 

Deforming Meshes 

K. Mani, University of 

Wyoming, Laramie, WY 

1100 


Accurate CFD Driven 

Optimization of Lifting 

Surfaces for Wing- Body 

Configuration 

S. Peigin, Israel Aircraft 

Industries, Ben-Gurion 

Airport, Israel 

1130 


A Universal Parametric 

Geometry 

Representation Method - 

"CST" 

B. Kulfan, Boeing 

Commercial Airplane 

Group, Seattle, WA 


http://www.aiaa.org/agenda.cfm?lumeetingid=1064&dateget=all#session7391.

Chaired by: S. HITZEL, European Aeronautic Defence and Space Company, Munich, Germany 

0800 0830 0900 0930 1000 1030 1100 1130 

Chaired by: G. JUMPER, U.S. Air Force Research Laboratory, Hanscom AFB, MA, and L. EHERNBERGER 

0800 0830 0900 0930 1000 1030 

Chaired by: A. BROEREN, University of Illinois at Urbana-Champaign, Urbana, IL, and T. RATVASKY, NASA Glenn Research Center, Cleveland, OH 

0800 0830 0900 0930 1000 1030


Session 9-APA-3 Flow with Moving Boundaries N-8 

Chaired by: S. HITZEL, European Aeronautic Defence and Space Company, Munich, Germany 

0800 


Computational 

Simulation of an 

Unmanned Air Vehicle 

Impacting Water 

A. Wick, Iowa State 

University, Ames, IA 

0830 


Aerodynamics of Low 

Reynolds Number 

Plunging Airfoil Under 

Gusty Environment 

Y. Lian, University of 

Michigan, Ann Arbor, MI 


Session 10-ASE-1 Clear Air Turbulence Crystal 2 


0900 


Viscous GBU38 Store 

Separation from Parent 

F15E Aircraft During 

Transonic Flight With 

Flight Test Comparison 

J. Dudley, U.S. Air 

Force SEEK Eagle 

Office, Eglin AFB, FL 

0930 


Numerical Simulation 

Based on CFD and 

Flight Dynamics for 

Morphing Body 

Y. Ueno, Nagoya 

University, Nagoya, 

Japan 

Chaired by: G. JUMPER, U.S. Air Force Research Laboratory, Hanscom AFB, MA, and L. EHERNBERGER 

0800 


Airborne Forward 

Looking Interferometer 

Turbulence Investigation 

G. Gimmestad, Georgia 

Tech Research Institute, 

Atlanta, GA 

0830 


Turbulence and 

Mountain Wave 

Conditions Observed 

with an Airborne 2- 

Micron Lidar 

E. Teets, NASA Dryden 

Flight Research Center, 

Edwards, CA 

0900 


In Situ Measurement of 

Waves and Turbulence 

in the T- REX Campaign 

G. Jumper, U.S. Air 

Force Research 

Laboratory, Hanscom 

AFB, MA 

0930 


Numerical Simulation of 

Clear Air Turbulence 

Using 4D- Var 

T. Misaka, Tohoku 

University, Sendai, 

Japan 

1000 


Dynamic Analysis of 

Atmospheric- Entry 

Probes and Capsules 

S. Murman, ELORET 

Corporation, Moffett 

Field, CA 

1000 


Role of Grid Adaptation 

in Optical Turbulence 

Prediction 

X. Xiao, North Carolina 


Raleigh, NC 

1030 


Application of the 

Unstructured Chimera 

Method for Rapid 

Weapons Trajectory 

Simulations 

J. Hooker, Lockheed 

Martin Corporation, 

Marietta, GA 

1030 


Simulations of Non- 

Hydrostatic Atmosphere 

Using Conservation 

Laws Package 

N. Ahmad, Science 

Applications 

International 

Corporation, McLean, VA 

1100 


Effect of Oscillation on 

Skin Friction Drag under 

the Influence of Adverse 

Pressure Gradients 

M. Amir, University of 

Manchester, 

Manchester, Great 

Britain 

1130 


Effect of Reduced 

Frequency and Surface 

Roughness on an Airfoil 

in Plunging Motion 

Session 11-ASE-2 Iced Aerodynamics Crystal 1 

Chaired by: A. BROEREN, University of Illinois at Urbana-Champaign, Urbana, IL, and T. RATVASKY, NASA Glenn Research Center, Cleveland, OH 

0800 


Airfoil Ice- Accretion 

Aerodynamic Simulation 

M. Bragg, University of 

Illinois at 

Urbana-Champaign, 

Urbana, IL 

0830 


Aerodynamic Simulation 

of a Horn- Ice Accretion 

on a Subscale Model 

G. Busch, University of 

Illinois at 


Urbana, IL 

0900 


Aircraft Performance 

Sensitivity to Icing Cloud 

Conditions 

S. Campbell, University 

of Illinois at 


Urbana, IL 

0930 


Two- and Three- 

Dimensional Iced Airfoil 

Separation Bubble 

Measurements by 


Velocimetry 

J. Jacobs, University of 

Illinois at 


Urbana, IL 

1000 


Flight Testing an Iced 

Business Jet for Flight 

Simulation Model 

Validation 

T. Ratvasky, NASA 



1030 


Developing Critical Ice 

Shapes for Use in 

Aircraft Development 

and Certification 

D. Parkins, American 

Kestrel Company, LLC, 

Ithaca, NY 


M. Soltani, Sharif 

University of 

Technology, Tehran, Iran


Chaired by: D. FERGUSON, NASA Marshall Space Flight Center, Huntsville, AL, and J. PREBOLA, Aerospace Testing Alliance, Arnold AFB, TN 

0800 0830 0900 0930 1000 1030 

Chaired by: B. SEKAR, U.S. Air Force Research Laboratory, Wright-Patterson AFB, OH, and C. NELSON, Innovative Technology Applications Company, LLC, Lynnwood, WA 

0800 0830 0900 0930 1000 

Chaired by: T. MCLAUGHLIN, U.S. Air Force Academy, Colorado Springs, CO, and L. CATTAFESTA, University of Florida, Gainesville, FL 

0800 0830 0900 0930 1000 1030


Session 12-ASE-3 Space Environments Ground and Flight Testing I Shasta 1 

Chaired by: D. FERGUSON, NASA Marshall Space Flight Center, Huntsville, AL, and J. PREBOLA, Aerospace Testing Alliance, Arnold AFB, TN 

0800 


Evaluation of 

Enhancements to the 

AEDC Combined Space 

Environment Chamber 

J. Prebola, Arnold 

Engineering 

Development Center, 

Arnold AFB, TN 

0830 


Comparative Analysis of 

Arcing in LEO and GEO 

Simulated Environments 

B. Vayner, Ohio 

Aerospace Institute, 



Session 13-FD-1 CFD Verification and Validation N-6 


0900 


Fabrication of Space 

Durable Polymer and its 

Performance under 

Space Environments 

S. Bhowmik, Delft 

University of 



0930 


Arc Testing of a Mockup 

Cable in a Simulated 

Space Radiation 

Environment 

D. Ferguson, NASA 

Marshall Space Flight 

Center, Huntsville, AL 

1000 


Internal Charge 

Distributions in PTFE 

Film by Numerical and 

Experimental Analysis 

R. Watanabe, Musashi 


Tokyo, Japan 

1030 


Proton Induced Internal 

Electrostatic Discharges 

and Charge Storage in 

Spacecraft Dielectrics 

N. Green, Jet Propulsion 

Laboratory, California 


Pasadena, CA 

Chaired by: B. SEKAR, U.S. Air Force Research Laboratory, Wright-Patterson AFB, OH, and C. NELSON, Innovative Technology Applications Company, LLC, Lynnwood, WA 

0800 


A Posteriori Method for 

Estimating and 

Correcting Grid- Induced 

Errors in CFD Solutions 

Part 1: Theory and 

Method 

T. Shih, Iowa State 


0830 


A Post Processing 

Approach for CFD Error 

Associated with Grid 

Resolution 

M. Mani, The Boeing 

Company, St. Louis, MO 

0900 


Estimation of Numerical 

Error for 3D Inviscid 

Flows on Cartesian Grids 

C. Roy, Auburn 

University, Auburn, AL 

0930 


Assessment of 

Turbulent Shock- 

Boundary Layer 

Interaction 

Computations Using the 

OVERFLOW Code 

A. Oliver, Purdue 


Lafayette, IN 

1000 


On Dependence of 

Structure of Numerical 

Solutions on Insertion of 

Random Errors 

I. Hataue, Kanazawa 

University, Kanazawa, 

Japan 

Session 14-FD-2 Closed Loop Flow Control Carson 2 

Chaired by: T. MCLAUGHLIN, U.S. Air Force Academy, Colorado Springs, CO, and L. CATTAFESTA, University of Florida, Gainesville, FL 

0800 


Closed- Loop Plasma 

Active Control 

Technology (CLOPACT) 

B. Snyder, U.S. Air 

Force Academy, 

Colorado Springs, CO 

0830 


MIMO Feedback Control 

of Flow Separation 

Q. Song, University of 

Florida, Gainesville, FL 

0900 


Effect of DFC 

Parameter on Flow 

Control Around Wings 

with PSJA 

M. Ohishi, Yamaguchi 

University, Ube, Japan 

0930 


Shift Modes and 

Transient Dynamics in 

Low Order, Design 

Oriented Galerkin 

Models 

, 

1000 


Low Dimensional POD 

Based Estimation of a 

3D Turbulent Separated 

Flow 

S. Siegel, U.S. Air Force 

Academy, Colorado 

Springs, CO 

1030 


A Closed- Loop Flight 

Control Experiment 

Using Active Flow 

Control Actuators 

A. Kutay, Georgia 


Atlanta, GA 




Session 15-FD-3 High Speed Flows N-3 

Chaired by: R. KIMMEL, U.S. Air Force Research Laboratory, Wright-Patterson AFB, OH, and R. BOWERSOX, Texas A&M University, College Station, TX 

0800 


Numerical Simulations 

of a Scramjet Isolator 

Using RANS and LES 

Approaches 

J. Allen, Utah State 


0830 


Detailed Study of Mixing 

Enhancement by Jet 

Modulation and Oblique 

Injection 

M. Dziuba, Rutgers 

University, Piscataway, 

NJ 


Session 16-FD-4 Unsteady Flows Crystal 4 


0900 


Visualization of 

Hypersonic 

Compression Corner 

Flows Using 

Temperature- and 

Pressure- Sensitive 

Paints 

Y. Ishiguro, Tohoku 

University, Miyagi, Japan 

0930 


Investigation of an 

Oblique Shock 

Reflection with 

Separation by PIV 

Measurements 

P. Dupont, Centre 

National de la 

Recherche Scientifique, 

Marseille, France 

1000 


Gas Kinetic Scheme for 

Continuum and Near- 

Continuum Hypersonic 

Flows 

W. Liao, Old Dominion 

University, Norfolk, VA 

Chaired by: M. GLAUSER, Syracuse University, Syracuse, NY, and S. SCHRECK, National Renewable Energy Laboratory, Golden, CO 

0800 


Simulation of 

Manoeuvring Aircraft 

with the Unstructured 

Chimera Approach 

K. Sorensen, European 

Aeronautic Defence and 

Space Company, 

Munich, Germany 

0830 


Unsteady Flow 

Measurements of a 

Slender Delta Wing in 

Wing Rock Motion 

Y. Hirose, Tohoku 


Japan 

0900 


Immersed Boundary 

Method for 

Compressible High- 


Viscous Flow around 

Moving Bodies 

Y. Cho, Pennsylvania 


University Park, PA 

0930 


Computational Method 

for Non- Conservation 

Form of 1- D Unsteady 

Euler Equations for 

Closed- Loop Transport 

Systems 

N. Nguyen, NASA Ames 


Moffett Field, CA 

1000 


Simulation of Film 

Cooling Flow from one 

Row of Inclined 

Cylindrical Jets by Using 

Lattice- Boltzmann 

Method 

Y. Li, Exa Corporation, 

Burlington, MA 

1030 


A Computational 

Analysis of 

Thermochemical Studies 

in the LENS Facilities 

M. MacLean, CUBRC, 

Aerothermal/Aero-optics 

Evaluation Center, 

Buffalo, NY 

1100 


Clustering Effects on 

Performance and 

Heating of a Linear 

Aerospike Nozzle 

S. Tsutsumi, University 

of Tokyo, Kanagawa, 

Japan 

Session 17-FD-5 Wake Flows I N-11 

Chaired by: D. WILLIAMS, Illinois Institute of Technology, Chicago, IL, and S. SIEGEL, U.S. Air Force Academy, Colorado Springs, CO 

0800 


Analysis of Vortex Pairs 

in the Wakes of Notched 

Wings 

L. Szkatula, University of 

Wales, Wrexham, Great 

Britain 

0830 



Vortical Flows Shedding 

from a Bluff Body with a 

Wavy Trailing Edge 

J. Cai, National 

University of Singapore, 

Singapore, Singapore 

0900 


The Formation Region 

Behind a Blunt Body 

Fitted with Splitter Plates 

M. Ortega, ITA, 

Technological Institute 

of Aeronautics, São 

José Dos Campos, SP, 

Brazil 

0930 


Three- Dimensional 

Inviscid Flowfield 

Computation Over 

Various Reentry 

Configurations 

R. Mehta, Vikram 

Sarabhai Space Centre, 

Trivandrum, India 

1000 


Modified DLM Method 

for Finite- Volume 

Simulation of Particle 

Flow 

A. Ardekani, University 

of California Irvine, 

Irvine, CA 

1030 


Unsteady Propulsion 

and Wake Structure of a 

Finite Aspect Ratio 

Pitching Plate 

J. Buchholz, Princeton 

University, Princeton, NJ 

1100 


Effects of Reynolds 

Number and Flapping 

Kinematics on Hovering 

Aerodynamics 

J. Tang, University of 


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: K. SACKSTEDER and F. KOHL, NASA Glenn Research Center, Cleveland, OH 


0800 0830 0900 0930 1000 

Chaired by: N. ULBRICH, Jacobs Technology, Inc, Moffett Field, CA, and R. DELOACH, NASA Langley Research Center, Hampton, VA 

0800 0830 0900 0930 1000 1030 

Chaired by: K. BURNS, Wyle Laboratories, San Diego, CA 

0800 0830 0900 0930 1000


Session 18-GPSE-1 Advanced Capabilities for the Exploration of Space I N-4 

Chaired by: K. SACKSTEDER and F. KOHL, NASA Glenn Research Center, Cleveland, OH 

0800 


The Exploration 

Technology 

Development Program 

C. Moore, NASA 

Headquarters, 

Washington, DC 

0830 


The Lunar Precursor 

Robotic Program 

D. Atkinson, NASA 

Headquarters, 



Session 19-GT-1 Advances in Strain-Gage Balance Design, Calibration and Analysis I (Invited) Sierra 2 


0900 


The Human Research 

Program 

D. Tomko, NASA 

Headquarters, 


0930 


NASA Utilization of the 

International Space 

Station and the Vision 

for Space Exploration 

J. Robinson, NASA 

Johnson Space Center, 

Houston, TX 

1000 


Commercial Objectives 

of the Lunar Architecture 

M. Nall, NASA Marshall 

Space Flight Center, 

Huntsville, AL 


0800 


Comparative Study of 

Strain- Gauge Balance 

Calibration Procedures 

Using the Balance 

Calibration Machine 

I. Philipsen, 

German-Dutch Wind 

Tunnels, Emmeloord, 

The Netherlands 

0830 


Stepwise Regression 

Analysis of MDOE 

Balance Calibration Data 

Acquired at DNW 

R. DeLoach, NASA 

Langley Research 

Center, Hampton, VA 

Session 20-HIS-1 History of Aeronautical Design Carson 4 


0800 


History of Test Facility 

Design Expertise at 

Aiolos Engineering 

Corporation 

G. Elfstrom, Aiolos 

Engineering 

Corporation, Toronto, 

Canada 

0830 


A Summary of a Half- 

Century of Oblique Wing 

Research 

M. Hirschberg, CENTRA 

Technology, Inc., 

Arlington, VA 

0900 


Analysis of Balance 

Calibration Machine 

Data Using 

Automatically Generated 

Math Models 

N. Ulbrich, Jacobs 

Technology, Inc., Moffett 

Field, CA 

0900 


The Early Development 

of JetPropelled Aircraft- 

A Review of German 

Contributions to 

Aerospace Technology 

J. McMasters, The 

Boeing Company, 

Seattle, WA 

0930 


Analysis of Calibration 

Data for the Multi- 

Component Rotor 

Balance Installed in the 

NFAC Large Rotor Test 

Apparatus 

J. van Aken, Jacobs 

Engineering, Moffett 

Field, CA 

0930 


The B- 29 And The 

Home Front Battle - An 

Engineering And 

Manufacturing 

Workforce Contribution 

To Victory 

M. Lavelle, Museum of 

Flight, Seattle, WA 

1000 


A Comparison of Two 

Balance Calibration 

Model Building Methods 




1000 


Reconstructing the 

Features and 

Performances of Historic 

Airplanes 

R. Martinez-Val, 

Universidad Politecnica 

de Madrid, Madrid, Spain 

1030 


The 2nd Generation 


Machine of Darmstadt 

University of Technology 

(TUD) 

K. Hufnagel, Darmstadt 

University of 

Technology, Griesheim, 

Germany 




Session 21-IS-1 Intelligent and Adaptive Control Cascade 1 

Chaired by: S. GARG, NASA Glenn Research Center, Cleveland, OH 

0800 


Robust Adaptive Fault- 

Tolerant Control with 

Trajectory Optimization 

Y. Huo, University of 

Southerm California, Los 

Angeles, CA 

0830 


Analytic Redundancy for 

Automatic Control 

Systems: Recursive 

Neural Network Based 

Virtual Sensors 

W. Faller, Applied 

Simulation 

Technologies, Cocoa 

Beach, FL 


Session 22-NSC-1 AIAA International Student Conference Undergraduate Division Crystal 5 


0900 


A Control Framework for 

Configurable Formation 

Flight of Autonomous 

Helicopters 

M. Saffarian, University 

of Alberta, Edmonton, 

Canada 

0930 


Optimal Static Soaring of 

UAVs Using Vehicle 

Routing with Time 

Windows 

N. Kahveci, University of 

Southern California, Los 

Angeles, CA 

Chaired by: B. LUND, The Boeing Company, Huntington Beach, CA, and C. TAVARES, The Boeing Company, St. Louis, MO 

0800 


Variability in Mixed- 

Mode Delamination 

Toughness with 

Implications for 

Research and Practical 

Applications 

S. Teller, Syracuse 

University, Syracuse, NY 

0830 


Enhanced Algorithms 

for an Underwater 

Visual Positioning 

System 

P. Rosendall, University 

of Maryland, Olney, MD 

0900 


Reducing Water Vapor 

Intrusion in Pressure 

Sense Line of an Upper- 

Stage Rocket Engine 

A. Longenecker, Duke 

University, Durham, NC 

Session 23-PC-1 Continuous Flow Combustion Teton 1 

Chaired by: J. OEFELEIN, Sandia National Laboratories, Livermore, CA 

0800 


A Detailed Investigation 

of Bluff Body Stabilized 

Flames 

B. Kiel, U.S. Air Force 

Research Laboratory, 


OH 

0830 


Dynamics of Bluff Body 

Flames Near Blowoff 

T. Lieuwen, Georgia 


Atlanta, GA 

0900 


LES Blowout Analysis of 

Premixed Flow Past Vgutter 

Flameholder 

C. Smith, CFD Research 

Corporation, Huntsville, 

AL 

0930 


Intentionally Triggered 

Dynamic Stall for 

Cascade Lift 

Enhancement 

B. Cukurel, Purdue 


Lafayette, IN 

0930 


Characterization of the 

Reacting Flowfield in a 

Liquid- Fueled 

Stagnation Point 

Reverse Flow 

Combustor 

P. Gopalakrishnan, 

Georgia Institute of 

Technology, Atlanta, GA 

1000 


Space- Based Antenna 

Morphing Using 

Reinforcement Learning 

H. Feldman, Texas 

A&M University, College 

Station, TX 

1000 


Product Recirculation 

and Mixing Studies in a 


Reverse Flow 

Combustor 

M. Bobba, Georgia 


Atlanta, GA 

1030 


Definition of AC- 130H 

Gunship Energy 

Maneuvering Capability 

M. Karmondy, U.S. Air 



1100 


Analysis of Pulsed 

Plasma Thruster Plume 

Characteristics 

T. Maruo, University of 

Washington , Seattle, 

WA 

1130 


Investigation of Free 

Pulsed Jets 

R. Cowling, Monash 

University, Melbourne, 

Australia 


Chaired by: T. LIEUWEN, Georgia Institute of Technology, Atlanta, GA 


0800 0830 0900 0930 1000 1030 1100 1130 

Chaired by: D. GAITONDE, U.S. Air Force Research Laboratory, Wright-Patterson AFB, OH 

0800 0830 0900 0930 1000 

Chaired by: J. MODER, NASA Glenn Research Center, Cleveland, OH, and F. MASHAYEK, University of Illinois at Chicago, Chicago, IL 

0800 0900 0930 1000 1030 1100 1130


Session 24-PC-2 Flames Studies I Teton 2 

Chaired by: T. LIEUWEN, Georgia Institute of Technology, Atlanta, GA 

0800 


Combined Effects of 

Stretch, Curvature, and 

Radiation on the 

Extinction of Tubular 

Premixed Flames 

Z. Chen, Princeton 

University, Princeton , 

NJ 

0830 


Linear Response of 

Premixed Flames to 

Flow Oscillations: 

Unsteady Stretch Effects 

P. Preetham, Georgia 


Atlanta, GA 


Session 25-PDL-1 / FD-6 Plasma Actuators I N-7 


0900 


Extinction and Near- 

Extinction Instability of 

Non- Premixed Tubular 

Flames 

S. Hu, Vanderbilt 

University, Nashville, TN 

0930 


Structural Study of Non- 

Premixed Tubular 

Hydrocarbon Flames 

S. Hu, Vanderbilt 

University, Nashville, TN 

Chaired by: D. GAITONDE, U.S. Air Force Research Laboratory, Wright-Patterson AFB, OH 

0800 


EHD Force in Dielectric 

Barrier Discharges 

Parametric Study and 

Influence of Negative 

Ions 

J. Boeuf, Université Paul 

Sabatier, Toulouse, 

France 

0830 


Air Plasma Actuators for 

Effective Flow Control 

S. Roy, University of 


0900 


Force Production 

Mechanisms of a 

Dielectric- Barrier 

Discharge Plasma 

Actuator 

J. Gregory, U.S. Air 



0930 


A Parametric 

Experimental Study for 

Momentum Transfer by 

Plasma Actuator 

T. Abe, Japan 

Aerospace Exploration 

Agency, Kanagawa, 

Japan 

1000 


OH and CH2O 

Measurement and 

Simulation Through 

Local Extinction in 

Nonpremixed Flames 

W. Carnell, University of 

Connecticut, Storrs, CT 

1000 


Plasma Discharge 

Characteristics and 

Experimentally 

Determined Boundary 

Conditions for a Plasma 

Actuator 

G. Font, U.S. Air Force 


Springs, CO 

1030 


Characteristics of 

Propagating H2- 

Enriched CH4- Air 

Flames 

A. Briones, University of 

Illinois at Chicago, 

Chicago, IL 

1100 


A Review of Flame 

Extinction Phenomena 

from the Perspective of 

Fire Suppression 

S. Aggarwal, University 

of Illinois at Chicago, 

Chicago, IL 

1130 


Oscillatory Response of 

Free- Anchor Laminar 

Premixed Flames with 

Non- Constant Flame 

Speed 

S. Shreekrishna, Indian 


Madras, Chennai, India 

Session 26-TES-1 Combustion Modeling in Energy Systems N-5 

Chaired by: J. MODER, NASA Glenn Research Center, Cleveland, OH, and F. MASHAYEK, University of Illinois at Chicago, Chicago, IL 

0800 


Invited Review: Reliable and Affordable 

Simulation of Turbulent Combustion 

P. Givi, University of Pittsburgh, Pittsburgh, PA 

0900 


RANS and Very Large 

Eddy Simulations of a 

Turbulent Flow in a Lean 

Direct Injection 

Hydrogen Combustor 

T. Shih, NASA Glenn 



0930 


Reacting Flow Studies in 

Counter- Current Dump 

Combustor 

K. Sengupta, University 


Chicago, IL 

1000 


Detonation Wave 

Propagation and 

Interaction with 

Transportation 

Infrastructure 

1030 


Combustion of Municipal 

Solid Waste Under 

HiTAC Conditions: 

Some General 

Calculations 

K. Isaac, University of D. Olinger, Lilley & 

Missouri-Rolla, Rolla, MO Associates, Stillwater, 

OK 

1100 


Investigation of A Large- 

Scale Circulating 

Fluidized Bed Boiler 

Y. Huang, Chongqing 

University, Chongqing, 

China (prc) 

1130 


Treatment of Chemicalcompounds 

with Heated 

Vapor Subtraction System 

R. Amano, University of 

Wisconsin-Milwaukee, 

Milwaukee, WI 



Chaired by: D. MUELLER, Indiana University–Purdue University Fort Wayne, Fort Wayne, IN, and E. MAROTTA, Texas A&M University, College Station, TX 

0800 0830 0900 0930 1000 1030 

Chaired by: E. JOSYULA, U.S. Air Force Research Laboratory, Wright-Patterson AFB, OH, and R. BOND, Sandia National Laboratories, Albuquerque, NM 

0800 0830 0900 0930 1000 1030 1100 

Chaired by: D. VAN WIE, Johns Hopkins University Applied Physics Laboratory, Laurel, MD, and V. BITYURIN, Russian Academy of Sciences, Moscow, Russia 

0800 0830 0900 0930 1000 1030


Session 27-TP-1 Conduction and Phase Change Heat Transfer Ruby 1 

Chaired by: D. MUELLER, Indiana University–Purdue University Fort Wayne, Fort Wayne, IN, and E. MAROTTA, Texas A&M University, College Station, TX 

0800 


Overall Heat- Transfer 

Coefficient for a Fin 

Cooled by Convection 

and Radiation 

D. Mueller, Indiana 

University-Purdue 

University, Fort Wayne, 

IN 

0830 


The Effect of Interstitial 

Material on Thermal 

Joint Resistance for 

Several Metallic Joints: 

Analytical and 

Experimental Study 

A. Vistamehr, Texas 


Station, TX 


Session 28-TP-2 Hypersonic and Nonequilibrium Flows Ruby 2 


0900 


Cooling Performance of 

a Partially- Confined FC- 

72 Spray: The Effect of 

Variable Gravity 

T. Michalak, U.S. Air 


Laboratory, 


OH 

0930 


Cooling Performance of 

a Partially- Confined FC- 

72 Spray: The Effect of 

Dissolved Air 

R. Puterbaugh, U.S. Air 


Laboratory, 


OH 

1000 


Transient Conduction 

Prediction in Nozzle 

Assembly of Solid 

Rocket Motors 

M. Ebrahimi, Aerospace 

Research Institute, 

Tehran, Iran 

1030 


Exponential Heating of 

Two- Dimensional Slabs 

L. Peterson, The 

Aerospace Corporation, 

El Segundo, CA 

Chaired by: E. JOSYULA, U.S. Air Force Research Laboratory, Wright-Patterson AFB, OH, and R. BOND, Sandia National Laboratories, Albuquerque, NM 

0800 


Investigation of 

Hypersonic Double- 

Cone Flow Experiments 

at High Enthalpy in the 

LENS Facility 

I. Nompelis, University 

of Minnesota, 

Minneapolis, MN 

0830 


Experimental Studies in 

LENS I and X to 

Evaluate Real Gas 

Effects on Hypevelocity 

Vehicle Performance 

M. Holden, 

Calspan-University of 

Buffalo Research 

Center, Buffalo, NY 

0900 


A Comparative Study of 

Navier- Stokes, Burnett, 

DSMC, and Boltzmann 

Solutions for Hypersonic 

Flow Past 2- D Bodies 

R. Chen, Washington 

University in St. Louis, 

St. Louis, MO 

0930 


Modeling of Plasma 

Formation in Rarefied 

Hypersonic Entry Flows 

I. Boyd, University of 


1000 


An Approach to Shock 

Envelope Grid Tailoring 

and Its Effect on 

Reentry Vehicle 

Solutions 

D. Saunders, ELORET 

Corporation, Sunnyvale, 

CA 

1030 


Velocity Slip and 

Temperature Jump in 

Hypersonic 

Aerothermodynamics 

A. Lofthouse, University 

of Michigan, Ann Arbor, 

MI 

1100 


Testing of the Unified 

Flow Solver (UFS) for 

Nozzle and Plume Flows 

E. Josyula, U.S. Air 


Laboratory, 


OH 

Session 30-WIG/PDL-1 Aerodynamics I: Plasma Aerodynamics Sierra 1 

Chaired by: D. VAN WIE, Johns Hopkins University Applied Physics Laboratory, Laurel, MD, and V. BITYURIN, Russian Academy of Sciences, Moscow, Russia 

0800 


Energy Based 

Framework for 

Assessment of 

Energetic Flow Control 

Techniques (Invited) 

C. Suchomel, U.S. Air 


Laboratory, 


OH 

0830 


Conical Navier- Stokes 

Modeling of Forebody 

Vortex Symmetry 

Plasma Control 

N. Malmuth, Teledyne 

Scientific Company, 

Thousand Oaks, CA 

0900 


Thermal Measurements 

at the Body Surface in a 

Supersonic Nitrogen 

Flow 

S. Bobashev, Ioffe 

Physico-Technical 

Institute of the Russian 

Academy of Sciences , 

Saint Petersburg, Russia 

0930 


Investigation of Plasma 

Jets Generated by 

Quasi- Stationary 

Magneto- Plasma 

Compressor under the 

High Static Pressure 

I. Mashek, Physical 

Department of 

Saint-Petersburg State 

University, 

Saint-Petersburg, Russia 

1000 


Magnetically Driven 

Surface Discharges for 

Shock- Wave Induced 

Boundary- Layer 


C. Kalra, Department of 

Mechanical and 

Aerospace Engineering 

Princeton University, 

Princeton, NJ 

1030 



the Discharge in 

Supersonic Flow Around 

a Sphere 

V. Bityurin, Institute of 

High Temperatures of 

Russian Academy of 

Sciences, Moscow, 

Russia



Chaired by: J. JONKMAN and P. MORIARTY, National Renewable Energy Laboratory, Golden, CO 

0830 0900 0930 1000 1030 1100 

Chaired by: R. STOKER, The Boeing Company, Seattle, WA, and J. DELFS, DLR, German Aerospace Research Center, Brunswick, Germany 

1330 1400 1430 1500 1530 

Chaired by: T. KAEMMING, The Boeing Company, Florissant, MO, and A. RASHEED, General Electric Global Research Center, Niskayuna, NY 

1330 1400 1430 1500 1530 1600 1630


Session 29-WE-1 Aeroelastics and CFD McKinley 

Chaired by: J. JONKMAN and P. MORIARTY, National Renewable Energy Laboratory, Golden, CO 

0830 


Rigid Body Modeling of 

Wind Turbines for 

Aeroelastic Stability 

Investigations 

J. Holierhoek, Delft 

University of 



0900 


Investigation into the 

Possibility of Flap- Lag- 

Stall Flutter 

J. Holierhoek, Delft 

University of 



Monday Afternoon / 08 January 2007 

Session 31-AA-2 Airframe Noise: Flaps, Slats, and Landing Gear N-10 


0930 



Verification of a Fully 

Coupled Simulator for 

Offshore Wind Turbines 

J. Jonkman, National 

Renewable Energy 

Laboratory, Golden, CO 

1000 


3D Rotational 

Corrections in ONERA 

Aeroelastic Predictions 

of NREL Wind Turbine 

M. Rapin, ONERA, 

Chatillon, France 

1030 



Wind Turbine Scale 

Effects by Using CFD 

Y. Park, Korea 

Aerospace Research 

Institute, Daejon, South 

Korea 

Chaired by: R. STOKER, The Boeing Company, Seattle, WA, and J. DELFS, DLR, German Aerospace Research Center, Brunswick, Germany 

1330 


Flap- Edge Flowfield 

and Noise in Civil 

Transport Aircraft Model 

M. Kuroda, Tohoku 


Japan 

1400 


Measurements of Flow 

Around a Split Flap 

Configuration 

, 

1430 


Simulation of the 

Broadband Noise from a 

Slat Using Zonal 

LES/RANS Hybrid 

Method 

T. Imamura, Japan 


Agency, Chofu, Japan 

1500 


Aeroacoustic 

Comparison of Airfoil 

Leading Edge High- Lift 

Geometries and 

Supports 

C. Andreou, Cambridge 

University, Cambridge, 

Great Britain 

1530 


Landing Gear for a 

Silent Aircraft 

A. Quayle, University of 

Cambridge, Cambridge, 

Great Britain 

1100 


3D Navier- Stokes 

Simulations of a Rotor 

Designed for Maximum 

Aerodynamic Efficiency 

J. Johansen, Risø 

National Laboratory, 

Roskilde, Denmark 

Session 32-ABP-3 PDE and Unsteady Flows I Cascade 2 

Chaired by: T. KAEMMING, The Boeing Company, Florissant, MO, and A. RASHEED, General Electric Global Research Center, Niskayuna, NY 

1330 


Simultaneous Mid- IR 

Measurement of 

Equivalence Ratio and 

Temperature in a JP- 

10- Fueled Pulsed 

Detonation Engine 

E. Barbour, High 

Temperature 

Gasdynamics 

Laboratory Department 

of Mechanical 

Engineering Stanford 


1400 


Design, Modeling and 

Evaluation of an Initiator 

Unit for a Split- Path JP- 

10/Air Pulse Detonation 

Combustor 

P. Hutcheson, Canadian 

Air Force, Monterey, CA 

1430 


Ignition and Detonation- 

Initiation Characteristics 

of Hydrogen and 

Hydrocarbon Fuels in a 

PDE 

T. Helfrich, U.S. Air 


Laboratory, 


OH 

1500 


Evaluation of Catalytic 

and Thermal Cracking in 

a JP- 8 Fueled Pulsed 


T. Helfrich, U.S. Air 


Laboratory, 


OH 

1530 


IGNITION AND 

DETONATION 

INITIATION OF 

MOVING HYDROGEN- 

AIR MIXTURES AT 

ELEVATED 

TEMPERATURE AND 

PRESSURE 

D. Chapin, GE Global 


Niskayuna, NY 

1600 


Development of a 

Compact Liquid Fueled 

PDE with Predetonator 

P. Panicker, University 

of Texas at Arlington, 

Arlington, TX 

1630 



Kerosene- Fueled Pulse 

Detonation Rocket 

Engine 

Q. Li, Northwestern 

Polytechnical University, 

Xi'an, China (prc)



Chaired by: R. CURRAN, Queen's University, Belfast, Northern Ireland 

1330 1400 1430 1500 1530 

Chaired by: G. SHAH, NASA Langley Research Center, Hampton, VA, and R. HESS, University of California, Davis, Davis, CA 

1330 1400 1430 1500 1530 1600 1630 

Chaired by: R. WAHLS, NASA Langley Research Center, Hampton, VA, and R. RUDNIK, DLR, German Aerospace Research Center, Brunswick, Germany 

1330 1400 1430 1500 1530 1600 1630


Session 33-AD-2 Launch Vehicle and Spacecraft Design Crystal 3 

Chaired by: R. CURRAN, Queen's University, Belfast, Northern Ireland 

1330 


Benefits From 

Incorporation of 

Combined Cycle 

Propulsion: X- 33 

Revisited 

P. Czysz, HyperTech 

Concepts LLC, St. 

Louis, MO 

1400 


Overview of a HTHL 

Hands- On SAV Design 

Synthesis Methodology 

X. Huang, University of 

Oklahoma, Norman, OK 


Session 34-AFM-2 Air Vehicle Dynamics and Flight Mechanics N-11 


1430 


Application of a HTHL 

SAV Design 

Methodology to 

Suborbital Tourism 

Vehicle 

X. Huang, University of 


1500 


Flight Testing and 

Simulation of a Mars 

Aircraft Design Using 

Inflatable Wings 

D. Reasor, University of 

Kentucky, Lexington, KY 

1530 


Mars Intelligent 

Reconaissance Aerial 

and Ground Explorer 

(MIRAGE) 

J. Aguirre, University of 

Miami, Coral Gables, FL 

Chaired by: G. SHAH, NASA Langley Research Center, Hampton, VA, and R. HESS, University of California, Davis, Davis, CA 

1330 


Obtaining Multi- Loop 

Pursuit- Control Pilot 

Models From Computer 

Simulation 

R. Hess, Dept. of 

Mechanical and 

Aeronautical 

Engineering University 

of California , Davis, CA 

1400 


High- Order Dynamic 

Overset Procedure 

Applied to Moving Body 

Calculations 

K. Alabi, Thaerocomp 

Technical Corp., Stony 

Brook, NY 

1430 


The Application of 

Quaternion Algebra to 

Gyroscopic Motion, 

Navigation, and 

Guidance 

G. Davailus, Old 

Dominion University, 

Norfolk, VA 

1500 


Formation Flying 

Commercial Aircraft - 

Assessment Using a 

New Approach - Wing 

Span Load and Camber 

Control 

R. Nangia, Nangia Aero 

Research, Bristol, Great 

Britain 

1530 


Derivation of the 

Dynamics Equations of 

Receiver Aircraft in 

Aerial Refueling 

J. Tucker, University of 

Texas at Arlington, 

Arlington, TX 

1600 


Optimal Turn- Back 

Maneuver After Engine 

Failure in a Single- 

Engine Aircraft During 

Climb- Out 

K. Brinkman, Delft 

University of 



1630 


A Closed- Loop 

Guidance Approximation 

for the Turn- Back 

Maneuver After Engine 

Failure During Climb- 

Out 

K. Brinkman, Delft 

University of 



Session 35-APA-4 Drag Prediction Workshop Summary Carson 1 

Chaired by: R. WAHLS, NASA Langley Research Center, Hampton, VA, and R. RUDNIK, DLR, German Aerospace Research Center, Brunswick, Germany 

1330 


Summary of the Third 

AIAA CFD Drag 

Prediction Workshop 

J. Vassberg, The Boeing 

Company, Huntington 

Beach, CA 

1400 


Statistical Analysis of 

CFD Solutions from the 

Third AIAA Drag 


(Invited) 

J. Morrison, NASA 



1430 


Structured and 

Unstructured Solvers for 

the 3rd CFD Drag 


(Invited) 

E. Tinoco, The Boeing 

Company, Seattle, WA 

1500 


Results from the 3rd 

Drag Prediction 

Workshop Using the 

NSU3D Unstructured 

Mesh Solver 

D. Mavriplis, University 


WY 

1530 


Drag Prediction for the 

DLR- F6 Wing/Body and 

DPW Wing Using 

CFL3D and 

OVERFLOW on an 

Overset Mesh 

A. Sclafani, The Boeing 

Company, Huntington 

Beach, CA 

1600 


Comparison Study of 


3rd CFD Drag 

Prediction Workshop by 

Structured and 

Unstructured Mesh 

Method (Invited) 

M. Murayama, Japan 



1630 


DLR Results from the 

Third AIAA CFD Drag 


(Invited) 

O. Brodersen, DLR, 

Institute of 

Aerodynamics and Flow 

Technology, 

Braunschweig, Germany



Chaired by: J. SLOTNICK, The Boeing Company, Huntington Beach, CA 

1330 1400 1430 1500 1530 1600 1630 1700 

Chaired by: H. MASSENGILL, Aerospace Testing Alliance, Arnold AFB, TN 

1330 1400 1430 1500 1530 1600 1630 1700 

Chaired by: M. CHO, Kyushu Insitute of Technology, Kitakyushu, Japan, and S. LAI, U.S. Air Force Research Laboratory, Hanscom AFB, MA 

1330 1400 1430 1500 1530 1600


Session 36-APA-5 High Lift Configuration N-9 

Chaired by: J. SLOTNICK, The Boeing Company, Huntington Beach, CA 

1330 


Numerical Validation of 

a Half Model High Lift 

Configuration in a Wind 

Tunnel 

P. Eliasson, Swedish 

Defence Research 

Agency, Stockholm, 

Sweden 

1400 



Effects on the 

Performance of a 

Hinged Slotted Flap 

D. Levy, Cessna Aircraft 

Company, Wichita, KS 


Session 37-APA-6 Wind Tunnel Experiments N-8 


1430 


Transport Aircraft 3D 

High Lift Wing 

Numerical Transition 

Prediction 

J. Perraud, ONERA, 

Toulouse, France 


1330 



Tip Leakage Flow in the 

Linear Compressor 

Cascade: Part I - 

Stationary Wall 

Q. Tian, Virginia 

Polytechnic Institute and 


Blacksburg, VA 

1400 



Tip Leakage Flow in the 

Linear Compressor 

Cascade: Part II - Effect 

of Moving Wall 





1430 


A Wind Tunnel 

Investigation of C- 130 

Aft Body Drag 

Reduction Approaches 

M. Karmondy, U.S. Air 



1500 


Control of Separation on 

the Flap of a Three- 

Element High- Lift 

Configuration 

B. Guenther, Technical 



1500 


Parametric Evaluation 

of Thin, Transonic 

Circulation- Control 

Airfoils 

R. Schlecht, NASA 



1530 


Numerical and 

Experimental 

Investigation of Mini- 

Flap Positions on an 

Airfoil 

E. Wassen, Technical 



1530 


Force and Moment 

Measurements on a 

Generic Finned Missile 

with Nose- Mounted 

Micro- Structures 

D. Corriveau, Defence 

R&D Canada, Quebec 

City, Canada 

1600 


Leading Edge Vortex 

Flaps on Moderate 

Sweep Wings- UCAV, 

Flow Improvement at 

High Lift 

R. Nangia, Nangia Aero 

Research, Bristol, Great 

Britain 

1630 


Automated Hybrid Mesh 

Generation for Industrial 

High- Lift Applications 

S. Munday, Aircraft 

Research Association, 

Bedford, Great Britain 

1700 


New Slat Concept for 

Flow Control over Airfoil 

R. Jozwiak, Warsaw 

University of 

Technology, Warsaw, 

Poland 

Session 38-ASE-4 Space Environments Ground and Flight Testing II Shasta 1 

Chaired by: M. CHO, Kyushu Insitute of Technology, Kitakyushu, Japan, and S. LAI, U.S. Air Force Research Laboratory, Hanscom AFB, MA 

1330 


Laboratory Test 

Campaign for ISO 

Standardization of Solar 

Array ESD Test Methods 

H. Masui, Kyushu 


Kitakyushu, Japan 

1400 


Verification of Multi- 

Utility Spacecraft 

Charging Analysis Tool 

(MUSCAT) Via 

Laboratory Test 

S. Hosoda, Kyushu 



1430 


A Critical Ionization 

Velocity Experiment on 

the ARGOS Satellite 

S. Lai, Space Vehicles 

Directorate, Air Force 


Hanscom AFB, MA 

1500 


Basic Experiment of 

Plasma Interaction with 

High Voltage Solar Array 

K. Tanaka, Japan 


Agency, Sagamihara, 

Japan 

1530 


Effect of Photoelectrons 

on Electric Field 

Antenna in Space 

H. Usui, Kyoto 

University, Uji, Japan 

1600 


Turbulent Separated 

Flow Over a Rounded 

Divergent Trailing Edge 

A. Hunter, Rensselaer 

Polytechnic Institute, 

Troy, NY 

1600 


Charge Control of 

Geosynchronous 

Spacecraft Using Field 

Effect Emitters 

M. Mandell, Science 

Applications 

International 

Corporation, San Diego, 

CA 

1630 


An Experimental 

Investigation on the 

Flow Separation on a 

Low- Reynolds- Number 

Airfoil 

Z. Yang, Iowa State 


1700 


A study of wake 

structures of a heaving 

two- dimensional elliptic 

airfoil using DPIV 

technique 

K. Lua, National 





Chaired by: J. HALLOCK, John A. Volpe National Transportation Systems Center, Cambridge, MA, and W. VAUGHAN, University of Alabama in Huntsville, Huntsville, AL 

1330 1400 1430 1500 1530 1600 

Chaired by: K. RINK, University of Idaho, Moscow, ID 

1330 1400 1430 

Chaired by: A. VIZZINI, Mississippi State University, Mississippi State, MS, and E. SCHROCK, Lockheed Martin Aeronautics Company, Palmdale, CA 

1330 1400 1430 1500 1530 1600 1630 1700


Session 39-ASE-5 Wake Vortices and Turbulence Crystal 2 

Chaired by: J. HALLOCK, John A. Volpe National Transportation Systems Center, Cambridge, MA, and W. VAUGHAN, University of Alabama in Huntsville, Huntsville, AL 

1330 


Flight Measurements of 

Wake Vortex Circulation 

in Crossflow Shear 

A. Brown, NRC Canada, 

Ottawa, Canada 

1400 


Derivation of Wake 

Vortex Circulation from 

Flight Data using Path 

Integrals 




Session 40-ECS-1 Technology of Energetic Devices Shasta 2 

Chaired by: K. RINK, University of Idaho, Moscow, ID 

1330 


Modeling of an 

Explosively Driven Micro- 

Valve 

K. Gonthier, Louisiana 

State University, Baton 

Rouge, LA 

1400 


Heterogeneous 

Processes Leading To 

Metal Ignition In 

Reactive Nanocomposite 

Materials 

S. Umbrajkar, New 

Jersey Institute of 

Technology, Newark, NJ 


1430 


The Development of a 


Turbulence Database for 

Wake Vortex 

Applications 

C. Ringley, North 

Carolina State 

University, Raleigh, NC 

1430 


Fuel- Rich Al- MoO3 

Nanocomposites 

Prepared by Arrested 

Reactive Milling 

S. Umbrajkar, New 

Jersey Institute of 

Technology, Newark, NJ 

1500 


Is the B757 Really a 

"Heavy" Aircraft? 

J. Hallock, U.S. DOT 

Volpe Center, 

Cambridge, MA 

1530 


In- Situ Measurements 

of Enroute Configuration 

Wake Vortex Scalar 

Field Characteristics 



1600 


High Altitude Turbulence 

Seasonal 


L. Ehernberger, Retired 

Aerospace Engineer / 

Meteorologist, 

Lancaster, CA 

Session 41-EDU-1 Education Pedagogy N-3 

Chaired by: A. VIZZINI, Mississippi State University, Mississippi State, MS, and E. SCHROCK, Lockheed Martin Aeronautics Company, Palmdale, CA 

1330 


An Experiential 

Introduction to 

Aerospace Engineering 

P. Washabaugh, 

University of Michigan, 

Ann Arbor, MI 

1400 


Key Challenges for the 

Aerospace Engineer of 

2015 

R. Bengelink, Arizona 


Tempe, AZ 

1430 


What Does the 

Aerospace Defense 

Industry Look for in a 

New Engineering Grad 

L. Nicolai, Lockheed 

Martin Aeronautics 

Company, Palmdale, CA 

1500 


Use of a Delphi Study 

Method in Avionics 

Curriculum Development 

T. Hofer, U.S. Naval 

Academy, Annapolis, 

MD 

1530 


Designing a Self- 

Assessment Process for 

ABET Accreditation 

P. Cinnella, Mississippi 


Mississippi State, MS 

1600 


A Framework for 

Collaborative Design in 

Engineering Education 

H. Jimenez, Georgia 


Atlanta, GA 

1630 


The Happy Accidents of 

Teaching Aircraft Design 

D. Hall, California 

Polytechnic State 

University, San Luis 

Obispo, CA 

1700 


Teaching of Simulation 

Based System 

Engineering 

P. Zipfel, Adjunct 

Associate Professor 

University of Florida, 

Shalimar, FL 




Session 42-FD-7 / TP-3 Boundary Layer Transition for Reentry Whitney 

Chaired by: R. KIMMEL, U.S. Air Force Research Laboratory, Wright-Patterson AFB, OH, and M. WRIGHT, NASA Ames Research Center, Moffett Field, CA 

1330 


Transition Issues for 

Atmospheric Entry 

E. Reshotko, Case 

Western Reserve 

University, Cleveland, 

OH 

1400 


Effects of Roughness 

on Hypersonic 

Boundary- Layer 

Transition 

S. Schneider, Purdue 


Lafayette, IN 


Session 43-FD-8 CFD Algorithms I N-6 


1430 


Transition Experiments 

on Blunt Bodies with 

Distributed Roughness 

in Hypersonic Free 

Flight 

D. Reda, NASA Ames 



1500 


Discrete Roughness 

Transition for 

Hypersonic Flight 

Vehicles 

S. Berry, NASA Langley 


Hampton, VA 

1530 



Transition and 

Hypersonic Flight 

Testing 

D. Kuntz, Sandia 

National Laboratories, 

Albuquerque, NM 

1600 


The Influence of 

Laminar Boundary Layer 

Transition on Entry 

Vehicle Design and Its 

Performance 

T. Lin, Northrop 

Grumman Mission 

Systems, San 

Bernardino, CA 

Chaired by: D. GAITONDE, U.S. Air Force Research Laboratory, Wright-Patterson AFB, OH, and W. KIM, Pratt and Whitney, East Hartford, CT 

1330 


Efficient Implicit LU- 

SGS Algorithm for High- 

Order Spectral 

Difference Method on 

Unstructured 

Hexahedral Grids 

Y. Sun, Iowa State 


1400 


CFD Methods Derived 

from Simplified 

Variational Principles 

A. Yahalom, College of 

Judea and Samaria, 

Ariel, Israel 

1430 


Probabilistic Collocation: 

An Efficient Non- 

Intrusive Approach for 

Arbitrarily Distributed 

Parametric Uncertainties 

G. Loeven, Delft 

University of 



1500 


A Fast Implicit 

Acoustics- Convection 

Galerkin Real- Gas 

Euler Solver with 

Minimal- Storage Non- 

Linearly Preconditioned 

GMRES- 2 

J. Iannelli, City 

University, London, 

Great Britain 

1530 


FCT and Direct 

Pressure Evaluation for 

Incompressible Flows 

J. Liu, Naval Research 

Laboratory, Washington, 

DC 

1630 


Hypersonic Boundary 

Layer Transition – 

Application to High 

Speed Vehicle Design 

K. Lau, The Boeing 


1700 


Boundary Layer Stability 

Analysis to Support the 

HIFiRE Transition 

Experiment 

H. Johnson, University 

of Minnesota, 


Session 44-FD-9 Flow Control Experiments Carson 2 

Chaired by: A. CAIN, Innovative Technology Applications Company, LLC, Chesterfield, MO, and W. SELLERS, NASA Langley Research Center, Hampton, VA 

1330 


Active Control of High 

Subsonic Jets 

J. Kim, Ohio State 

University, Columbus, 

OH 

1400 


Control of the Stingray 

UAV at Low Angles of 

Attack 

J. Farnsworth, 

Rensselaer Polytechnic 

Institute, Troy, NY 

1430 


Active Flow Control of 

Sprays with Synthetic 

Jets 

A. Pavlova, Rensselaer 


Troy, NY 

1500 


Effect of Traversal Jet 

Injections on Skin 

Friction in a Turbulent 

Channel 

C. Tay, National 



1530 


Shock / Boundary- Layer 

Interaction Control 

Using Three- 

Dimensional Bumps for 

Transonic Wings 

H. Ogawa, University of 


Great Britain 

1600 


Aero- Optical 

Interactions, Imaging, 

and Optimization in 

Turbulent Separated 

Flows 

, 

1630 


Similarities and 

Differences in Aero- 

Optical Structure over 

Cylindrical and 

Hemispherical Turrets 

with a Flat Window 

J. Cress, University of 

Notre Dame, NOtre 

Dame, IN



Chaired by: A. WASHBURN, NASA Langley Research Center, Hampton, VA, and S. GOGINENI, U.S. Air Force, Beavercreek, OH 

1330 1400 1430 1500 1530 

Chaired by: M. NEAVES, Naval Surface Warfare Center, Panama City, FL 

1330 1400 1430 1500 1530 1600 1630 1700 

Chaired by: C. MOORE, NASA Headquarters, Washington, DC, and A. OVER, NASA Glenn Research Center, Cleveland, OH 

1330 1400 1430 1500 1530


Session 45-FD-10 Fluid-Structure Interaction I Carson 3 

Chaired by: A. WASHBURN, NASA Langley Research Center, Hampton, VA, and S. GOGINENI, U.S. Air Force, Beavercreek, OH 

1330 


A Comparison of 

Overset Methods and 

Unstructured 

Remeshing for Modeling 

Large Rigid Body Motion 

A. McClung, Air Force 


Dayton, OH 

1400 


Aerodynamic Parameter 

Adaptation of CFD- 

Based Reduced- Order 

Models 

T. Lieu, Stanford 



Session 46-FD-11 Multiphase Flows Crystal 4 


1430 


A Parallel Multigrid 

Algorithm for 

Aeroelasticity 

Simulations 

J. Gargoloff, Texas A&M 

University, College 

Station, TX 

Chaired by: M. NEAVES, Naval Surface Warfare Center, Panama City, FL 

1330 


Local Adaptive 

Timestepping for 

Lagrangian Particle 

Tracking 

V. Lee, University of 

Illinois at 


Urbana-Champaign, IL 

1400 


Computations of 

Multiphase Fluid Flows 

Using Marker- Based 

Adaptive, Multilevel 

Cartesian Grid Method 

, 

1430 


Jet- Fuel Cavitation in a 

Converging- Diverging 

Nozzle 

M. Davis, University of 

Notre Dame, Notre 

Dame, IN 

1500 


Sensitivity Analysis of 

Unsteady Fluid- 

Structure Interaction 

Problems 

S. Etienne, Ecole 

Polytechnique de 

Montreal, Montreal, 

Canada 

1500 


Experimental and 

Theoretical Study of 

Interfacial Area 

Transport for Reduced- 

Gravity Two- Phase 

Flows 

S. Vasavada, Purdue 


Lafayette, IN 

1530 


Stable and Accurate 

Loosely- Coupled 

Scheme for Unsteady 

Fluid- Structure 

Interaction 

R. Jaiman, University of 

Illinois at 


Urbana, IL 

1530 


Numerical Modeling of 

Cavitation in Jet Fuel 

C. Bourassa, Honeywell, 

Inc, South Bend, IN 

1600 


Simulation of Unsteady 

Two- Phase Flows 

Using a Parallel 

Eulerian- Lagrangian 

Approach 

B. Mitchell, University of 

Tennessee at 

Chattanooga, 

Chattanooga, TN 

1630 


Estimation of 

Mechanical Erosion at 

Nozzle Inlet by Multiphase 

Flow Simulation 

in Solid Rocket Motor 

Considering Aluminium 

Droplets and Alumina 

Mist. 

K. Kato, Tohoku 


Japan 

1700 


Numerical Study of a 

Cylinder Impacting 

Water with a Flattened 

Striking Area 



Session 47-GPSE-2 Advanced Capabilities for the Exploration of Space II N-4 

Chaired by: C. MOORE, NASA Headquarters, Washington, DC, and A. OVER, NASA Glenn Research Center, Cleveland, OH 

1330 


Cryogenic Fluid 

Management 

Technologies for 

Advanced Green 

Propulsion Systems 

S. Motil, NASA Glenn 



1400 


In- Situ Resource 

Utilization for Lunar and 

Mars Exploration 

K. Sacksteder, NASA 



1430 


Gravity Effects on Lunar 

Mobility and the Human- 

Robotic Systems 

Program 

, 

1500 


Lunar and Martian Dust: 

Evaluation and Mitigation 

M. Hyatt, NASA Glenn 



1530 


Technology 

Development for Fire 

Safety in Exploration 

Spacecraft and Habitats 

G. Ruff, NASA Glenn 


Cleveland, OH




1330 1400 1430 1500 


1330 1400 1430 1500 1530 

Chaired by: T. TAKAHASHI, Raytheon, Tucson, AZ 

1330 1400 1430 1500 1530 1600


Session 48-GT-2 Advances in Strain-Gage Balance Design, Calibration and Analysis II (Invited) Sierra 2 


1330 


SG Balance 

improvements are 

slowing down - Europe 

cannot wait that long 

U. Jansen, ETW GmbH, 

Cologne, Germany 

1400 



Procedures for Time- 

Dependent Phenomenon 

F. Steinle, Aerospace 

Testing Alliance, Arnold 

AFB, TN 


Session 49-HIS-2 Aerospace History Carson 4 


1330 


Post Cold War 

Conversations with 

Paperclip Scientists 

B. Sarao, AIAA Member 

and Member of the AIAA 

History Technical 

Committee, 

Sammamish, WA 

1400 


Tracing the Growth of 

U.S. Air Power and the 

Aircraft Involved 

M. Spearman, NASA 




1430 


Calibration of a Six 

Component Air Flow 

Through Balance 

D. Booth, Allied 

Aerospace, San Diego, 

CA 

1500 


Load Envelope Analysis 

of Strain- Gage Balance 

Data 

N. Ulbrich, Jacobs 

Technology, Inc., Moffett 

Field, CA 

Session 50-MDO-1 Aerospace Systems Optimization Cascade 1 

Chaired by: T. TAKAHASHI, Raytheon, Tucson, AZ 

1330 


Optimization of Iris, a 

Small Autonomous 

Surveillance UAV 

D. Hunsaker, Brigham 

Young University, Provo, 

UT 

1400 


Surrogate- Based 

Design Optimization of a 

Large Asymmetric 

Launch Vehicle Payload 

Fairing 

P. Reisenthel, Nielsen 

Engineering & 

Research, Inc., 

Mountain View, CA 

1430 


50 Years of Aeronautical 

Research by Aeromobile 

Inc. 

W. Bertelsen, 

Aeromobile Inc., Rock 

Island, IL 

1430 


Genetic Algorithm 

Optimization of Liquid 

Propellant Missile 

Systems 

D. Riddle, Auburn 

University, Auburn 

University, AL 

1500 


Flight Activities at the 

1904 St. Louis World's 

Fair: Introducing 

America to Aeronautics 

F. Roos, The Boeing 


1500 


Reverse Engineering of 

Solid Rocket Missiles 

with a Genetic Algorithm 

J. Metts, Auburn 


1530 


The History of 

Aerospace Research at 

Cornell Aeronautical 

Laboratory and Calspan 

K. Burns, Wyle 

Laboratories, San Diego, 

CA 

1530 


Evolutionary Algorithm 

Use in Optimisation of a 

Launch Vehicle Stack 

Model 

G. Briggs, Australian 

Defence Force 

Academy, Canberra, 

Australia 

1600 


Optimal Solid Space 

Tower 

A. Bolonkin, C&R, 

Brooklyn, NY 




Session 51-NSC-2 AIAA International Student Conference Masters Division Crystal 5 

Chaired by: B. LUND, The Boeing Company, Huntington Beach, CA, and C. TAVARES, The Boeing Company, St. Louis, MO 

1330 


Experimental 


Embedded Cross- Flow 

Fan for Airfoil 

Propulsion/Circulation 

Control 

R. Dygert, Syracuse 


1400 


Sonic Boom Prediction 

Using Euler / Full 

Potential Methodology 

I. Ozcer, Old Dominion 



Session 52-PC-3 Flames Studies II Teton 2 

Chaired by: M. SMOOKE, Yale University, New Haven, CT 

1330 


Stabilization of an Edge- 

Flame in a Corner 

Region 

M. Matalon, 

Northwestern 

University, Evanston, IL 

1400 



Neighboring Edge 

Flame Interactions 

S. Kostka, University of 

Connecticut, Storrs, CT 


1430 


Design of 3- DOF 

Testbed for Micro- 

Satellite Autonomous 

Operations 

F. Leve, University of 


1430 


On the Accurate 

Determination of Flame 

Speeds at Normal and 

Elevated Pressures by 

Using a Spherical 

Bomb: The Effects of 

Compression and Stretch 

Z. Chen, Princeton 

University, Princeton , NJ 

1500 


Low Pressure Turbine 

Blade Separation 

Control Using Plasma 

Actuators 

K. Ramakumar, 

University of Kentucky, 

Lexington, KY 

1500 


Front- Tracking 

Simulation for Outward 

Propagation of Spherical 

Flames 

K. Pan, National Taiwan 

University, Taipei, 

Taiwan (roc) 

1530 


Acoustic Source 

Localization and the 

Echo Problem 

S. Beaver, Texas A&M 


Station, TX 

1530 


Verified Computations of 

Laminar Premixed 

Flames 

A. Al-Khateeb, 

University of Notre 

Dame, Notre Dame, IN 

1600 



the Splashdown Problem 



1600 


Scaling Analysis on 

Dynamic Flammability 

Limits of Unsteady 

Premixed Methane/Air 

Flames 

G. Bansal, University of 


1630 


A Numerical Blade 

Element Approach to 

Estimating Propeller 

Flowfields 

D. Hunsaker, Brigham 

Young University, 

Provo, UT 

1630 


Effect of Environmental 

Variables on Flame 

Spread Rates in 

Microgravity 

C. Lautenberger, 

University of California, 

Berkeley, Berkeley, CA 

1700 


Investigations Into the 

Visualization of Wall 

Shear Stress 

Distributions Using 

Infrared Thermography 

and Analysis of the 

Transient Data 

I. Rudolph, Technical 

University Berlin, Berlin, 

Germany 

Session 53-PC-4 Gas Turbine Combustion Teton 1 

Chaired by: R. ERICKSON, United Technologies Research Center, East Hartford, CT, and Y. IKEDA, Imagineering Inc, Kobe, Hyogo 

1330 


Reduced Combustion 

Time Model for Methane 

in Gas Turbine Flow 

Fields 

M. Lamnaouer, 

University of Central 

Florida, Orlando, FL 

1400 


The Pratt & Whitney 

TALON X Low 

Emissions Combustor: 

Revolutionary Results 

with Evolutionary 

Technology 

R. McKinney, Pratt & 

Whitney, East Hartford, 

CT 

1430 


Improved Correlations 

for Augmentor Static 

Stability 

D. Knaus, Creare Inc., 

Hanover, NH 

1500 


Interaction of a Gaseous 

Fuel Jet with Shock- 

Wave- Rich Airflow 

A. Abdelhafez, 

Department of 

Mechanical Engineering, 

University of Maryland, 

College Park, MD 

1530 


Numerical Optimization 

of the "Tornado" 

Combustor Aerodynamic 

Parameters 

I. Matveev, Applied 

Plasma Technologies, 

McLean, VA 

1600 


Effects of Chemical 

Kinetics and Heat Loss 

on Near- LBO 

Combustion Dynamics - 

Stability Analysis 

T. Yi, University of 


OH



Chaired by: J. LINEBERRY, Lytec LLC, Manchester, TN 

1330 1400 1430 1500 1530 1600 

Chaired by: S. SHERIF, University of Florida, Gainesville, FL, and N. MARUYAMA, Mie University, Tsu Mie, Japan 

1330 1400 1430 1500 1530 

Chaired by: R. CUNNINGTON, Raytheon Missile Systems, Tucson, AZ, and D. MOORHOUSE, U.S. Air Force Research Laboratory, Wright-Patterson AFB, OH 

1330 1400 1430 1500


Session 54-PDL-2 Magnetohydrodynamics N-7 

Chaired by: J. LINEBERRY, Lytec LLC, Manchester, TN 

1330 


Computational 

Simulation of 

Magnetohydrodynamics 

Acceleration 

Experiments Using 

Newton- Krylov- Schwarz 

Method 

T. Wan, University of 

Minnesota, Minneapolis, 

MN 

1400 


The Fundamental 

Properties of Disk- 

Shaped MHD 

Accelerator 

S. Takeshita, Nagaoka 

University of 

Technology, Nagaoka, 

Japan 


Session 55-TES-2 Flow Simulation in Energy Systems N-5 


1430 


Time Accurate Analysis 

of Supersonic Flows 

over a Backward- 

Facing Step with Applied 

Magnetic Fields 

O. Khan, Wichita State 

University, Wichita, KS 

1500 


Simulation of 

Hypersonic Flow Within 

a Strong Magnetic Field 

R. MacCormack, 

Professor, Department 

of Aeronautics and 

Astronautics, Stanford 


Chaired by: S. SHERIF, University of Florida, Gainesville, FL, and N. MARUYAMA, Mie University, Tsu Mie, Japan 

1330 


Identification of Flow 

Separation in Three and 

Four Dimensions 

G. Jacobs, San Diego 

State University, San 

Diego, CA 

1400 


Large- Eddy Simulation 

Using a Discontinuous 

Galerkin Spectral 

Element Method 

K. Sengupta, University 


Chicago, IL 

1430 


Simulation of Supersonic 

MHD Channel Flows 

Z. Xu, University of 

Wisconsin-Milwaukee, 

Milwaukee, WI 

1500 


An Excel/VBA 3- D CFD 

Program for Educational 

Purposes 

R. Fischer, Oklahoma 


Stillwater, OK 

1530 


Study of a Diagonal 

Channel MHD Power 

Generation 

T. Hardianto, Nagaoka 

University of 


Japan 

1530 


CFD with VBA 

D. Lilley, Oklahoma 



1600 


Experimental 


Magneto- Fluid- 

Dynamic Interaction in 

Cylindrical Inlet 

J. Shang, Wright State 

University, Dayton, OH 

Session 56-TP-4 / MDO-2 Multidisciplinary Design Optimization and Thermophysics Ruby 2 

Chaired by: R. CUNNINGTON, Raytheon Missile Systems, Tucson, AZ, and D. MOORHOUSE, U.S. Air Force Research Laboratory, Wright-Patterson AFB, OH 

1330 


Incorporation of 

Aerothermodynamic 

Analysis Tools into the 

Multi- Disciplinary 

Conceptual Design 

Process 

R. Cunnington, Raytheon 

Missile Systems, 

Tucson, AZ 

1400 


High- Speed External 

Aerodynamic Analysis 

Using Exergy Balance 

with Hypersonic Panel 

Code 

M. Baker, M4 

Engineering Inc., Signal 

Hill, CA 

1430 


An Inverse Data 

Analysis Technique for 

the Determination of 

Local Heat Transfer 

Phenomena 

M. Cochran, Kansas 


Manhattan, KS 

1500 


Thermodynamic 


Hypersonic Flying 

Vehicles 

E. Son, Moscow Institute 

of Physics and 

Technology, 

Dolgoprudny, Russia 


Chaired by: J. DEC and K. WURSTER, NASA Langley Research Center, Hampton, VA 


1330 1400 1430 1500 1530 1600 

Chaired by: S. SCHRECK, National Renewable Energy Laboratory, Golden, CO 

1330 1400 1430 1500 1530 1600 

Chaired by: V. BYCHKOV, Moscow State University, Moscow, Russia, and B. GANGULY, U.S. Air Force Research Laboratory, Wright-Patterson AFB, OH 

1330 1400 1430 1500 1530 1600 1630 1700


Session 57-TP-5 Thermal Protection Systems and Ablation Ruby 1 

Chaired by: J. DEC and K. WURSTER, NASA Langley Research Center, Hampton, VA 

1330 


A Simplified Approach 

for the Rapid Generation 

of Transient Heat- 

Shield Environments 

K. Wurster, NASA 



1400 


Orbiter Gap Filler 

Bending Model for Re- 

Entry 

C. Campbell, NASA 

Johnson Space Center, 

Houston , TX 


Session 58-WE-2 Wake Modeling McKinley 


1430 


Numerical Attempt for 

Reproducing the 

Surface Recession Data 

of Galileo Probe 

S. Matsuyama, Japan 



Chaired by: S. SCHRECK, National Renewable Energy Laboratory, Golden, CO 

1330 


Tower Shadow 

Simulation with 

Helicoidal Vortex Model 

J. Chattot, University of 

California Davis, Davis, 

CA 

1400 


Dynamic Prescribed 

Vortex Wake Model for 

AeroDyn 

H. Currin, Oregon 


Klamath Falls, OR 

1430 


The Inverse Vortex 

Wake Model: A 

Measurement Analysis 

Tool 

W. Haans, Delft 

University of 



1500 




Thermal Response of 

Ablator in an Arc- Jet 

Facility 

M. Mizuno, Japan 


Agency, Tokyo, Japan 

1500 



Numerical Survey in the 

Wake of a Wind Turbine 

F. Massouh, ENSAM, 

Paris, France 

1530 


Thermal 

Characterization of 

Emisshield 

B. Olson, University of 


1530 


Airfoil models in the 

actuator line code 

assessed with nearwake 

measurements on 

a yawed rotor 

W. Haans, Delft 

University of 



1600 


Experimental Studies on 

the Effect of Ply 

Orientation on the 

Thermal Performance of 

Silica Phenolic Ablative 

Material 

R. S.Pugazenthi, Indian 

Space Research 

Organisation, 


1600 


Wind Turbine Rotor- 

Tower Interaction Using 

an Incompressible 

Overset Grid Method 

F. Zahle, Risø National 

Laboratory, Roskilde, 

Denmark 

Session 59-WIG/PDL-2 Plasma I Sierra 1 

Chaired by: V. BYCHKOV, Moscow State University, Moscow, Russia, and B. GANGULY, U.S. Air Force Research Laboratory, Wright-Patterson AFB, OH 

1330 


Microwave Discharges: 

Fundamentals and 

Applications 

V. Shibkov, Moscow 


Moscow, Russia 

1400 


Microwave Gas- 

Discharge Source 

Based on the "Plasma 

Resonance" 

Phenomenon 

I. Kossyi, Prokhorov 

General Physics 

Institute of RAS, 


1430 

1500 

AIAA-2007-0429 AIAA-2007-0430 

Microwave Torch as a Surface Microwave 

Tool for an Airflow Discharge in 

Chemical Transformation Quasi–Optical Wave 

Beam 

I. Kossyi, Moscow State 

University, Moscow, 

Russia 

I. Esakov, Russian 

Academy of Sciences, 


1530 


Various Types of 

Initiators for Attached 

Undercritical MW 

Discharge Ignition 

K. Khodataev, MRTI, 


1600 


Influence of Kinetics on 

Transversal Discharge 

Gas Heating Region 

Size and Form in 

Supersonic Gas Flow 

A. Aleksandrov, 

Moscow State 


Russia 

1630 


Microwave Discharge in 

Quasi- optical Wave 

Beam 

I. Esakov, Moscow 

Radiotechnical Institute 

RAS, Moscow, Russia 

1700 


Influence of Magnetic 

Field on Gas Discharge 

Used for Air Ioniization 

A. Erofeev, Russian 


St. Petersburg, Russia



Chaired by: J. SHAW, NASA Glenn Research Center, Cleveland, OH, and D. MARCOTTE, National Research Council, Ottawa, Canada 

1400 Opening Remarks/AIRA Overview –Joe Shaw/Dave Marcotte 

0800-0900 hrs


1400 - 1800 5th Annual AIRA Research Implementation Forum Crystal 1 

Chaired by: J. SHAW, NASA Glenn Research Center, Cleveland, OH, and D. MARCOTTE, National Research Council, Ottawa, Canada 

1400 Opening Remarks/AIRA Overview –Joe Shaw/Dave Marcotte 

1430 AIRA 2007 Invited Lectureship I: "From Technology Development Through Certification-Commercial All Weather Helicopter Certification in the U.S." Robert Flemming, Sikorsky Aircraft 

1530 AIRA 2007 Invited Lectureship II: "The Future Outlook for Improved Icing Forecasting" Mark Andrews, Joint Program Development Office(JDPO) 

1630 AIRA Research Thrust I: "Forecasting and Remote Sensing for Hazardous Weather at HUB Airports" Stewart Cober, Environment Canada 

1700 AIRA Research Thrust II: "Propulsion System Icing" Jim MacLeod, Canadian National Research Council 

1730 AIRA Research Thrust III: "Physics of Ice Adhesion for Rotating Surfaces" Myron Oleskiw, Canadian National Research Council 

1800 Adjourn 


1730 - Dryden Lectureship in Research Reno Room 

Tuesday Morning / 09 January 2007 

0800 - 1200 Career Workshop: Managing Your Career in the 21st Century I Crystal 5 

0800-0900 hrs 

Intergenerational Workforce (Impact of Aging and Multi-Generational Workforce) 

Trudy Hu, IEEE-USA CWPC Committee and National Health Provider 

0900-0930 hrs 

To Go or To Stay - A Personal Risk Analysis 

Bob Wessels, Lockheed Martin Corporation 

0930-1000 hrs 

Mentoring 101 

Dave Paisley, The Boeing Company 

1000-1030 hrs 

Solving the Mystique of Interviewing 

Jerry Lutz, Consultant 

1030-1100 

How to Succeed in a Globalized "Flat" World 

Cathy Downen, Raytheon Aircraft Company 

1100-1130 hrs 

Authoring Your Career Crossroads 

Jerry Lutz, Consultant 

1130-1200 hrs 

Understanding Meyers Briggs Type Indicator (MBTI) 

Kathy Prem, University of Wisconsin



Chaired by: K. ZAMAN, NASA Glenn Research Center, Cleveland, OH, and J. MENDOZA, Honeywell, Phoenix, AZ 

0800 0830 0900 0930 1000 1030 1100 

Chaired by: D. PAXSON, NASA Glenn Research Center, Cleveland, OH, and W. ENGBLOM, Embry-Riddle Aeronautical University, Daytona Beach, FL 

0800 0830 0900 0930 1000 1030 

Chaired by: A. STRAZISAR, NASA Glenn Research Center, Cleveland, OH, and D. RIHN, Northrop Grumman Corporation, El Segundo, CA 

0800 0830 0900 0930 1000 1030


Session - Graduate Student Award Presentations N-2 


Session 60-AA-3 Jet Noise: Measurements and Control N-10 

Chaired by: K. ZAMAN, NASA Glenn Research Center, Cleveland, OH, and J. MENDOZA, Honeywell, Phoenix, AZ 

0800 

0830 


A PIV Flow Field Near Field Acoustics of 

Investigation of Medium Core and Fan Chevron 

Bypass Chevron Nozzles Nozzles 

O. Rask, University of 


OH 



OH 


0900 


Offset Stream 

Technology - 

Comparison of Results 

from UCI and GRC 

Experiments 

K. Zaman, NASA Glenn 



0930 


Jet Noise Reduction by 

Fluidic Injection on a 

Separate Flow Exhaust 

System 

S. Harrison, University 


OH 

1000 


Small- Aperture Phased 

Array Study of Noise 

from Coaxial Jets 

D. Papamoschou, 


Irvine, CA 

1030 


Limitations of the Three- 

Microphone Signal 

Enhancement Technique 

D. Nance, Georgia 


Atlanta, GA 

Session 61-ABP-4 PDE and Unsteady Flows II Cascade 2 

Chaired by: D. PAXSON, NASA Glenn Research Center, Cleveland, OH, and W. ENGBLOM, Embry-Riddle Aeronautical University, Daytona Beach, FL 

0800 


Transient Plasma 

Ignition for Delay 

Reduction in Pulse 

Detonation Engines 

C. Cathey, University of 

Southern California, Los 

Angeles, CA 

0830 


A Fundamental Study 

on the Acoustic Behavior 

of Pulse Detonation 

Engines 

A. Glaser, University of 


OH 

0900 


Acoustic Measurements 

of Multiple Pulse 

Detonation Engines 

Firing Out of Phase 

N. Caldwell, University 


OH 

0930 


Propagation of 

Detonations Across a 

Step Area Change in a 

Pulsed Detonation 

Engine 

D. Hopper, Air Force 



OH 

1000 



Ejectors Driven by a 

Pulse Detonation Engine 



OH 

1030 


Performance Estimation 

for Air- Breathing Pulse 

Detonation Engine with 

Bypass and 

Mix/Separate Exhaust 

H. Qiu, Northwestern 


Xi'an, China (prc) 

1100 


A Spatio- Temporal 

Decomposition of the 

Acoustic Source in a 

Mach 0.85 Jet 

J. Hall, Syracuse 





0800 0830 0900 0930 1000 1030


Session 62-AD-3 The Silent Aircraft Initiative Crystal 3 


0800 


Airframe Design for 

“Silent Aircraft” 

J. Hileman, 

Massachusetts Institute 

of Technology, 

Cambridge, MA 

0830 


Challenges in the Silent 

Aircraft Engine Design 

E. de la Rosa Blanco, 

Cambridge University, 

Cambridge, Great Britain 


Session 63-AFM-3 Projectile/Missile Aerodynamics and Flight Dynamics N-11 


0900 




Ingesting (BLI) 

Propulsion System 

A. Plas, Massachusetts 


Cambridge, MA 

0930 


Design and Operation 

for Ultra Low Noise 

Take- Off 

D. Crichton, Cambridge 


Great Britain 

1000 


Development of 

Approach Procedures 

for Silent Aircraft 

J. Hileman, 



Cambridge, MA 

1030 


Assessment of Silent 

Aircraft- Enabled 

Regional Development 

and Airline Economics in 

the UK 

R. Tam, Massachusetts 


Cambridge, MA 

Chaired by: F. PRIOLO, Millennium Engineering and Integration Company, Arlington, VA, and J. DESPIRITO, U.S. Army Research Laboratory, Aberdeen Proving Ground, MD 

0800 


Using Unsteady 

Aerodynamic Multi- Axis 

State- Space 

Formulation as a Tool to 

Represent Wing Rock 

P. De Oliveira-Neto, 

Virginia Polytechnic 

Institute and State 

University, Blacksburg, 

VA 

0830 


Analytic Model of 

Catastrophic Yaw 

J. Morote, National 

Institute of Aerospace 

Technology, Madrid, 

Spain 

0900 


Forebody Strake Effects 

on Air- Launch Rocket 

Aerodynamic 

Characteristics at High 

Angle of Attacks 

W. Logan, University of 

California , Davis, CA 

0930 


Effects of Forebody 

Geometry on the Flow 

and Control of a Blunt- 

Nose Projectile at High 

Angles of Attack 

J. Lopera, University of 

Toledo, Toledo, OH 

1000 


Application of Pressure- 

Based Coupled Solver 

to the Problem of 

Hypersonic Missiles with 

Aerospikes 

K. Kurbatskii, Fluent 

Inc., Lebanon, NH 

1030 


Recent NASA Research 

on Aerodynamic 

Modeling of Post- Stall 

and Spin Dynamics of 

Large Transport 

Airplanes 

A. Murch, NASA 



1100 


Fuzzy Controllers Based 

on Optimal Fuzzy 

Reasoning for Missile 

Terminal Guidance 

L. Zhang, Beihang 

University, Beijing, 

China (prc) 

Session 64-AMT-2 Diagnostics for Reacting and High-Speed Flows Shasta 2 

Chaired by: T. ROSSMANN, Rutgers University, Piscataway, NJ, and B. THUROW, Auburn University, Auburn University, AL 

0800 


Tunable Filter 

Absorption 

Spectroscopy for High 

Pressure Combustion 

Systems 

S. Boege, Rutgers 


NJ 

0830 


Chemiluminescence 

Measurements and 

Modeling in Syngas, 

Methane and Jet- A 

Fueled Combustors 

V. Nori, Georgia Institute 

of Technology, Atlanta, 

GA 

0900 


Measurements of NO 

and OH Concentrations 

in Vitiated Air Using 

Diode- Laser- Based 

Ultraviolet Absorption 

Sensors 

T. Anderson, Purdue 


Lafayette, IN 

0930 


Development of Diode 

Laser Absorption 

Instrument for Free 

Stream Measurements in 

Hypervelocity CO2 Flows 

J. Meyers, Von Kármán 

Institute for Fluid 

Dynamics, 

Rhode-Saint-Genèse, 

Belgium 

1000 


Optical Investigations of 

the Combustion 

Characteristics of a Gas 

Turbine Pilot Burner 

H. Seyfried, Lund 


Lund, Sweden 

1030 


Turbulence 

Measurements Using 

FARRS in a Supersonic 

Axisymmetric Jet 

R. Huffman, University of 

Illinois at 


Urbana, IL 

1100 


Electronic- Resonance- 

Enhanced (ERE) 

Coherent Anti- Stokes 

Raman Scattering 

(CARS) Detection of 

Minor Species in 

Reacting Flows 

S. Naik, Purdue 


Lafayette, IN



Chaired by: D. GRISMER, U.S. Air Force Research Laboratory, Wright-Patterson AFB, OH 

0800 0830 0900 0930 1000 1030 

Chaired by: N. QIN, University of Sheffield, Sheffield, Great Britain 

0800 0830 0900 0930 1000 

Chaired by: D. HUMMEL, Technical University of Brunswick, Brunswick, Germany 

0800 0900 0930 1000 1030 1100 1130


Session 65-APA-7 Aerodynamic Flow Control I Carson 1 

Chaired by: D. GRISMER, U.S. Air Force Research Laboratory, Wright-Patterson AFB, OH 

0800 


Computational 

Evaluation of Controlling 

Flap- Edge Vortex and 

Tip Vortex Using 

Circulation Control 

Techniques 

Y. Liu, National Instittue 

of Aerospace, Hampton, 

VA 

0830 


Effective Layout of 

Plasma Actuators for a 

Flow Separation Control 

on a Wing 

D. Tsubakino, University 

of Tokyo, Tokyo, Japan 


Session 66-APA-8 Bio-Inspired Aerodynamics N-9 


0900 


Limited Characterization 

of Dual Bimorph 

Synthetic Jet Actuators: 

Aeroelastic Load 

Control—Phase I 

A. Tucker, U.S. Air 

Force, Edwards AFB, CA 

Chaired by: N. QIN, University of Sheffield, Sheffield, Great Britain 

0800 


Aerodynamic Design 

Exploration of Flapping 

Wing, Viewpoint of 

Shape and Kinematics 

S. Takahashi, Tohoku 


Japan 

0830 



Kinematic Wing Models 

of Hovering Insect Flight 

F. Bos, Delft University 

of Technology, Delft, 


0900 


Aerodynamic 


Corrugated Dragonfly 

Airfoil Compared with 

Smooth Airfoils at Low 

Reynolds Numbers 

M. Tamai, Iowa State 


0930 


Control of Shock- 


Interactions (SBLIs) 

Using An Oscillatory Jet 

A. Hassan, The Boeing 

Company, Mesa, AZ 

0930 


Optimization of Flapping 

Motion of Airfoils in 

Biplane Configuration 

for Maximum Thrust 

and/or Efficiency 

M. Kaya, Middle East 

Technical University, 

Ankara, Turkey 

1000 


Computational 

Investigation of Flow 

Control over Wings 

P. Vavilis, FORTH / 

IACM, Heraklion, Greece 

1000 


Investigation of Strouhal 

Number Effect on 

Flapping Wing Micro Air 

Vehicle 

K. Aditya, Maturi 

Venkata Subba Rao 

Engineering College, 

Hyderabad, India 

1030 


Investigation of a 

Boundary- Layer Control 

System by Air Blowing in 

a Closed- Circuit 

Subsonic Wind Tunnel 

M. Assato, Pontifícia 

Universidade Católica, 

Rio De Janeiro, Brazil 

Session 67-APA-9 Cranked Arrow Wing Aerodynamics Project International I N-8 

Chaired by: D. HUMMEL, Technical University of Brunswick, Brunswick, Germany 

0800 


Review of Cranked- Arrow Wing Aerodynamics 

Project: Its International Aeronautical 

Community Role 

J. Lamar, NASA Langley Research Center, 

Hampton, VA 

0900 


Description of the F16- 

XL Geometry and 

Computational Grids 

Used in CAWAPI 

O. Boelens, National 

Aerospace 

Laboratory/NLR, 

Amsterdam, The 


0930 


Comparison of 

Measured and 

Simulated Flow 

Features for the Full- 

Scale F- 16XL Aircraft 

O. Boelens, National 

Aerospace 

Laboratory/NLR, 

Amsterdam, The 


1000 


Evaluation of Results 

from a Reynolds 

Averaged Multiblock 

Code Against F- 16XL 

Flight Data 

K. Badcock, University 

of Liverpool, Liverpool, 

Great Britain 

1030 


PAB3D Simulations for 

the CAWAPI F- 16XL 

A. Elmiligui, Analytical 

Services & Materials, 

Inc, Hampton, VA 

1100 


RANS Solutions for the 

CAWAPI F- 16XL in 

Solution Adapted Hybrid 

Grids 

W. Fritz, EADS Military 

Air Systems, Munich, 

Germany 

1130 


F- 16XL Unsteady 

Simulations for the 

CAWAPI Facet of RTO 

Task Group AVT- 113 

S. Morton, U.S. Air 

Force SEEK EAGLE 

Office, Eglin AFB, FL



Chaired by: W. TOBISKA, Space Environment Technologies, Pacific Palisades, CA, and J. MINOW, NASA Marshall Space Flight Center, Huntsville, AL 

0800 0830 0900 0930 1000 1030 

Chaired by: W. WRIGHT, ASRC Federal Holding Company, Cleveland, OH, and E. MONTREUIL, Office National d'Etudes et Recherches Aerospatiales, Chatillon, France 

0800 0830 0900 0930 1000 

Chaired by: D. DARMOFAL, Massachusetts Institute of Technology, Cambridge, MA, and B. MAINES, Lockheed Martin Aeronautics Company, Ft Worth, TX 

0800 0830 0900 0930 1000 1030


Session 68-ASE-6 Modeling of the Space Environment Crystal 2 

Chaired by: W. TOBISKA, Space Environment Technologies, Pacific Palisades, CA, and J. MINOW, NASA Marshall Space Flight Center, Huntsville, AL 

0800 


Final Development 

Status of Multi- Utility 

Spacecraft Charging 

Analysis Tool (MUSCAT) 

J. Kim, Kyushu Institute 



0830 


SOLAR2000 v2.30 and 

SOLARFLARE v1.01: 

New Capabilities for 

Space System 

Operations 

W. Tobiska, Space 

Environment 

Technologies, Pacific 

Palisades, CA 


Session 69-ASE-7 Numerical Methods in Aircraft Icing Crystal 1 


0900 


SEP Temporal 

Fluctuations Related to 

Extreme Solar Flare 

Events Detected by 

SOHO/CELIAS/SEM 

L. Didkovsky, University 

of Southern California, 

Los Angeles, CA 

0930 


Spacecraft Radiation 

Shielding Using Ultra 

Light- Weight 

Superconducting 

Magnets 

E. Kervendal, Florida 


Melbourne, FL 

1000 


Interstellar Space 

Missions: Ultra- 

Reliability Requirements 

and Engineering Issues 

H. Garrett, Jet 

Propulsion Laboratory, 

California Institute of 

Technology, Pasadena, 

CA 

1030 


Theory of Space 

Magnetic Sail and 

Electrostatic MagSail 


Brooklyn, NY 

Chaired by: W. WRIGHT, ASRC Federal Holding Company, Cleveland, OH, and E. MONTREUIL, Office National d'Etudes et Recherches Aerospatiales, Chatillon, France 

0800 


SmaggIce 2.0: 

Additional Capabilities 

for Interactive Grid 

Generation of Iced 

Airfoils 

R. Kreeger, NASA 



0830 


Q3D- Wing for Flight 

Control of Aircraft with 

Ice Accretion 

B. Williams, Iowa State 


0900 


Simulations of Finite 

Wings with 2- D and 3- D 

Ice Shapes: Modern 

Lifting- Line Theory 

Versus 3- D CFD 

K. Chi, Iowa State 


0930 


Icing Collection 

Efficiency from Direct 

Simulation 

J. Nathman, Analytical 

Methods, Inc, Redmond, 

WA 

1000 


Simulation of Ice 

Shedding from a 

Business Jet Aircraft 

M. Papadakis, Wichita 


Wichita, KS 

Session 70-FD-12 CFD Higher Order Methods I Crystal 4 

Chaired by: D. DARMOFAL, Massachusetts Institute of Technology, Cambridge, MA, and B. MAINES, Lockheed Martin Aeronautics Company, Ft Worth, TX 

0800 


Direct Numerical 

Simulation of 


Layer Receptivity over 

Parabola Using High- 

Order Nonlinear Scheme 

X. Liu, China 

Aerodynamics Research 

and Development 

Center, Mianyang, China 

(prc) 

0830 


Weighted Compact and 

Non- compact Scheme 

for Shock Tube and 

Shock Entropy 

Interaction 

X. Peng, University of 


Arlington, TX 

0900 


A Hermite WENO- 

Based Limiter for 

Discontinuous Galerkin 

Methods on 

Unstructured Grids 

H. Luo, Science 

Applications 

International 

Corporation, McLean, VA 

0930 


Engineering Application 

Oriented Discontinuous 

Galerkin Methods 

M. Kessler, Universität 

Stuttgart, Stuttgart, 

Germany 

1000 


A Parallel hp- Multigrid 

Solver for Three- 

Dimensional 


Discretizations of the 

Euler Equations 

C. Nastase, University of 


1030 



Solution of the Navier- 

Stokes Equations on 

Deformable Domains 

P. Persson, 



Cambridge, MA



Chaired by: B. SMITH, Lockheed Martin Aeronautics Company, Fort Worth, TX, and A. HAMED, University of Cincinnati, Cincinnati, OH 

0800 0830 0900 0930 1000 1030 1100 1130 

Chaired by: T. BEUTNER, Defense Advanced Research Projects Agency, Annandale, VA, and M. POST, U.S. Air Force Academy, Colorado Springs, CO 

0800 0830 0900 0930 1000 

Chaired by: M. TURNER, University of Cincinnati, Cincinnati, OH, and J. REED, University of Toledo, Belchertown, MA 

0800 0830 0900 0930 1000 1030


Session 71-FD-13 CFD RANS Modeling and Application N-6 

Chaired by: B. SMITH, Lockheed Martin Aeronautics Company, Fort Worth, TX, and A. HAMED, University of Cincinnati, Cincinnati, OH 

0800 


Personalized Ventilation 

for Commercial Aircraft 

Cabins 

N. Gao, Hong Kong 

Polytechnic University, 

Hong Kong, Hong Kong 

0830 


Application of Laminar- 

Turbulent Transition 

Criteria in Navier- 

Stokes Computation 

J. Cliquet, ONERA, 

Toulouse, France 


Session 72-FD-14 Flow Control Propulsion Applications Carson 2 


0900 


Computational Analysis 


Control for the Flow 

over a Wall- Mounted 

Hump Using a Synthetic 

Jet 

C. Bettini, DIMSET, 

Genova, Italy 

0930 


Computation of 

Turbulent Flow over 

Highly Curved 

Configuration Using a 

Conventional Two- 

Equation Turbulence 

Model 

M. Zakyani, Sharif 

University of 

Technology, Tehran, 

Iran 

1000 


Continuous Shape 

Sensitivity Equation 

Method for the kepsilon 

Model of 

Turbulence 

R. Di Caro, Ecole 



Canada 

1030 


Interaction of 

Turbomachinery 

Components in Large 

Scale Unsteady 

Computations of Jet 

Engines 

G. Kalitzin, Stanford 


Chaired by: T. BEUTNER, Defense Advanced Research Projects Agency, Annandale, VA, and M. POST, U.S. Air Force Academy, Colorado Springs, CO 

0800 


Investigation of Low- 

Pressure Turbine 


A. Gross, University of 

Arizona, Tucson, AZ 

0830 


Micro- Vortex Generator 

Flow Control for 

Supersonic Engine Inlets 

H. Babinsky, University 

of Cambridge, 


0900 


Supersonic- Inlet Start 

Amelioration and 

Unstart Mitigation via 

Mass and Heat Transfer 

J. Iannelli, City 

University, London, 

Great Britain 

0930 


Influence of Two- 

Dimensional vs. Discrete 

Disturbances on 

Separating Low 

Pressure Turbine 

Boundary Layers 

D. Reimann, Brigham 

Young University, Provo, 

UT 

1000 


Correction of Turbulence 

Quantities in 3D PIV 

Data 

M. Alkislar, The Boeing 


1100 


Assessment of Two 

Low- Reynolds- Number 

k- e Models in Turbulent 

Boundary Layers with 

Surface Roughness 

M. Lu, Western 

Michigan University, 

Kalamazoo, MI 

1130 


Computational Analysis 

of Turbulent Internal 

Flow in Ballistic Solid 

Rocket Motors 

A. Arabshahi, UT 

SimCenter at 

Chattanooga, 


Session 73-FD-15 Internal Wall-Bounded Flows N-3 

Chaired by: M. TURNER, University of Cincinnati, Cincinnati, OH, and J. REED, University of Toledo, Belchertown, MA 

0800 



Blood Flow Through 

Heart Valves 

A. Nejadmalayeri, 

Wichita State University, 

Wichita, KS 

0830 


Outer- Layer Similarity in 

the Presence of Highly- 

Irregular Surface 

Roughness 

Y. Wu, University of 

Illinois at 


Urbana, IL 

0900 


Investigation into the 

Understanding of Flow 

Stagnation in Fluid Tube 

Radiators 

N. Hahn, Paragon 

Space Development 

Corporation, Tucson, AZ 

0930 


Modification of Standard 

K- e Turbulence Model 

for Analysis and Design 

Refinement of Fuel 

Ejector Pump 

J. Masud, National 

University of Sciences 

and Technology, 

Risalpur, Pakistan 

1000 


Near Wall 

Measurements in 

Smooth/Rough 

Turbulent Boundary 

Layers 

B. Brzek, Rensselaer 


Troy, NY 

1030 


On the Composite 

Logarithmic Profile in 

Zero Pressure Gradient 


Layers 

K. Chauhan, Illinois 


Chicago, IL



Chaired by: E. WHITE, Texas A&M University, College Station, TX 

0800 0830 0900 0930 1000 1030 

Chaired by: F. CHIARAMONTE, NASA Headquarters, Washington, DC, and F. KOHL, NASA Glenn Research Center, Cleveland, OH 

0800 0830 0900 0930 1000 1030 1100 

Chaired by: P. STICH, Aerospace Testing Alliance, Arnold AFB, TN, and D. DRESS, NASA Langley Research Center, Hampton, VA 

0800 0830 0900 0930


Session 74-FD-16 Stability and Transition: High Speed Experiments and Facilities - Separation Whitney 

Chaired by: E. WHITE, Texas A&M University, College Station, TX 

0800 


HIFiRE- 1 Boundary 

Layer Transition 

Experiment Design 

R. Kimmel, U.S. Air 


Laboratory, 


OH 

0830 


Transition Research and 

Improved Performance 

in the Boeing/AFOSR 

Mach- 6 Quiet Tunnel 

T. Juliano, Purdue 


Lafayette, IN 


Session 75-GPSE-3 Advanced Capabilities for the Exploration of Space III N-4 


0900 


Fluorescence 


Hypersonic Flow Past 

Triangular and 

Rectangular Boundary- 

Layer Trips 

, 

0930 


Inducer- Induced 

Transition in Hypersonic 


H. Bottini, von Kármán 

Institute for Fluid 

Dynamics, Rhode Saint 

Genese, Belgium 

1000 



the Bursting of a 

Laminar Separation 

Bubble 

O. Marxen, Royal 


Stockholm, Sweden 

Chaired by: F. CHIARAMONTE, NASA Headquarters, Washington, DC, and F. KOHL, NASA Glenn Research Center, Cleveland, OH 

0800 


Energy Storage: 

Batteries and Fuel Cells 

for Exploration 

M. Manzo, NASA Glenn 



0830 


Exercise 

Countermeasures and a 

New Ground- Based 

Partial- g Analog for 

Exploration 

, 

0900 


Intravenous Solutions 

for Exploration Missions 

F. Miller, National 

Center for Space 

Exploration Research, 


0930 


Electronic Repair 

Concepts for Long- 

Duration Spaceflight 

J. Easton, National 




1000 


The Microgravity 

Science Glovebox 

(MSG), a Resource for 

Gravity- Dependent 

Phenomena Research 

on the International 

Space Station (ISS) 

R. Spivey, Tec-Masters 

Inc., Huntsville, AL 

1030 


On Instability Properties 

of Incompressible 

Laminar Separation 

Bubbles on a Flat Plate 

Prior to Shedding 

V. Theofilis, Universidad 

Politécnica de Madrid, 

Madrid, Spain 

Session 76-GT-3 Advances in Ground Test Techniques Sierra 2 

Chaired by: P. STICH, Aerospace Testing Alliance, Arnold AFB, TN, and D. DRESS, NASA Langley Research Center, Hampton, VA 

0800 


Combined Cycle Status 

Matching and Data 

Reconciliation through 

the Heat Balance Solver 

T. Lin, Georgia Institute 


GA 

0830 


Shuttle Debris Impact 

Tool Assessment Using 

the Modern Design of 

Experiments 




0900 


Experimental Space 

Shuttle Orbiter Studies 

to Acquire Data for Code 

and Flight Heating 

Model Validation 

T. Wadhams, 


Buffalo Research Center, 

Buffalo, NY 

0930 


A Method for Calculating 

the Probability of 

Successfully Completing 

a Rocket Propulsion 

Ground Test 

B. Messer, NASA 

Stennis Space Center, 

Stennis Space Center, 

MS 

1030 


Synergies Between 

Space Research and 

Space 

Operations—Examples 

from the International 

Space Station 

J. Tate, Engineering & 

Science Contract Group, 

Houston, TX 

1100 


Calculation of 

Excavation Force for 

ISRU on Lunar Surface 

X. Zeng, Case Western 

Reserve University, 




Chaired by: R. NOACK, University of Alabama in Birmingham, Aberdeen Proving Ground, MD, and S. ALTER, NASA Langley Research Center, Hampton, VA 

0800 0830 0900 0930 1000 1030 

Chaired by: J. POWERS, University of Notre Dame, Notre Dame, IN 

0800 0830 0900 0930 1000 1030 1100 1130 

Chaired by: J. BELLAN, Jet Propulsion Laboratory, California Institute of Technology, Pasadena, CA 

0800 0830 0900 0930 1000 1030 1100 1130


Session 77-MVC-1 Mesh Generation Carson 3 

Chaired by: R. NOACK, University of Alabama in Birmingham, Aberdeen Proving Ground, MD, and S. ALTER, NASA Langley Research Center, Hampton, VA 

0800 


Anisotropic Tetrahedral 

Meshing Based on 

Surface Deformation 

Techniques 

J. Steinbrenner, 

Pointwise, Inc., Fort 

Worth, TX 

0830 


Viscous Layer Meshes 

from Level Sets on 

Cartesian Meshes 

W. Dawes, Cambridge 


Great Britain 


Session 78-PC-5 Combustion Instability and Acoustic Interactions Teton 1 


0900 


Mesh Generation and 

Deformation Algorithm 

for Aeroelasticity 

Simulations 

J. Gargoloff, Texas A&M 


Station, TX 

Chaired by: J. POWERS, University of Notre Dame, Notre Dame, IN 

0800 


Investigation of Self 

Excited and Acoustically 

Forced Combustion 

Instabilities with Laser 

Diagnostics 

F. Scheel, Cambridge 


Great Britain 

0830 


Design Considerations 

for Remote High- Speed 

Pressure Measurements 

of Dynamic Combustion 

Phenomena 

D. Straub, National 

Energy Technology 

Laboratory, 

Morgantown, WV 

0900 



"Prime and Trigger" 

Concept for Compact 

Afterburner Combustion 

S. Birmaher, Georgia 


Atlanta, GA 

0930 


A Mesh Deformation 

Strategy Optimized by 

the Adjoint Method on 

Unstructured Meshes 

Z. Yang, University of 


0930 


Impact on Microjet 

Actuation on Stability of 

a Backward- Facing 

Step Combustor 

M. Altay, Massachusetts 


Cambridge, MA 

1000 


Solution Adaptive Mesh 

Generation Using 

Feature- Aligned 

Embedded Surface 

Meshes 

A. Shih, University of 

Alabama in Birmingham, 

Birmingham, AL 

1000 


The Effect Steady Fluid 

Motion on One- 

Dimensional Wave 

Propagation 

B. Kiel, U.S. Air Force 



OH 

1030 


Unstructured Adaptive 

Elliptic Smoothing 

S. Karman, University of 

Tennessee at 

Chattanooga, 


1030 


Non- Normality and 

Nonlinearity in 

Combustion- Acoustic 

Interaction in Diffusion 

Flames 

K. Balasubramanian, 

Indian Institute of 

Technology Madras, 

Chennai, India 

1100 


Two- Parameter 

Extremum Seeking for 

Control of 

Thermoacoustic 

Instabilities and 


Linear Growth 

J. Moeck, Technical 



1130 


Effect of Fuel/Air Mixing 

on NOx Emissions and 

Stability in a Gas 

Premixed Combustion 

System 

A. Lacarelle, Berlin 

University of 

Technology, Berlin, 

Germany 

Session 79-PC-6 Liquid Rocket Combustion Teton 2 

Chaired by: J. BELLAN, Jet Propulsion Laboratory, California Institute of Technology, Pasadena, CA 

0800 


Novel Subgrid Modeling 

of the LES Equations 

Under Supercritical 

Pressure 

L. Selle, California 


Pasadena, CA 

0830 



Subcritical to 

Supercritical Jet Mixing 

S. Polikhov, University 

of Florida, Gainesville, 

FL 

0900 


Effects of Fuel Density, 

Velocity, and 

Composition on Flame- 

Acoustic Interaction 

A. Ghosh, University of 

Maryland, College Park, 

MD 

0930 


LOX/GH2 Shear 

Coaxial Injector 

Atomization Studies: 

Effect of Recess and 

Non- Concentricity 

R. Woodward, 



Park, PA 

1000 


Interaction of LOX/GH2 

Spray- Combustion with 

Acoustics 

B. Knapp, DLR, German 


Center, Hardthausen, 

Germany 

1030 


Transient Cryogenic 

Flow and Mixing from a 

Coaxial Rocket Injector 

V. Gautam, University of 


MD 

1100 


Prediction of Non- 

Equilibrium Kinetics of 

Fuel- rich 

Kerosene/LOX 

Combustion in Gas 

Generator 

C. Lee, Konkuk 

University, Seoul, South 

Korea 

1130 


Supercritical 

Combustion of Liquid 

Oxygen (LOX) and 

Methane Stabilized by a 

Splitter Plate 

N. Zong, Pennsylvania 

State University, State 

College, PA



Chaired by: Y. HARDALUPAS, Imperial College London, London, Great Britain, and C. CADOU, University of Maryland, College Park, MD 

0800 0830 0900 0930 1000 1030 1100 

Chaired by: N. HARADA, Nagaoka University of Technology, Nagaoka, Japan 

0800 0830 0900 0930 1000 1030 1100 

Chaired by: S. RAGHUNATHAN, Queens University, Belfast, Northern Ireland, and E. NICHOLS, Orbital Sciences Corporation, Dulles, VA 

0800 0830 0900 0930 1000


Session 80-PC-7 Micro/Meso-Scale Combustion Shasta 1 

Chaired by: Y. HARDALUPAS, Imperial College London, London, Great Britain, and C. CADOU, University of Maryland, College Park, MD 

0800 


Kinetic Enhancement of 

Mesoscale Combustion 

by Using a Novel 

Nested Doll Combustor 

P. Galie, Princeton 

University, Cherry Hill, 

NJ 

0830 


Experimental 


Influence of Heat 

Recirculation on 

Temperature 

Distribution and Burning 

Velocity in a Simulated 

Micro- Burner 

A. Veeraragavan, 

University of Maryland, 

College Park, MD 


Session 81-PDL-3 Space Propulsion N-7 


0900 


Effect of Leakage on 

Optimal Compression 

Ratio for Small- Scale 

Rotary Engines 

S. Sprague, University 

of California, Berkeley, 

Berkeley, CA 

Chaired by: N. HARADA, Nagaoka University of Technology, Nagaoka, Japan 

0800 


Forward Expansion of 

Pulsed Ion Beam- 

Driven Ablation Plasma 

and Evaluation of 

Propulsive Forces 

C. Buttapeng, Nagaoka 

University of 


Japan 

0830 


Characterization of a 

Hall Effect Thruster 

Using Thermal Imaging 

J. Tomaszewski, Air 

Force Institute of 

Technology, 


OH 

0900 


MHD Analysis of Flow 

Fields Around Magneto 

Plasma Sail 

H. Nishida, University of 

Tokyo, Tokyo, Japan 

0930 



Spin Flames in 

Mesoscale Combustion 

B. Xu, Princeton 


0930 


High Power Ion 

Cyclotron Heating in the 

VASIMR Engine 

E. Bering, University of 

Houston, Houston, TX 

1000 


Flame Synthesis of 

Nanostructures of 

Semiconducting Metal 

Oxides 

F. Xu, Rutgers, The 

State University of New 

Jersey, Piscataway, NJ 

1000 


Feasibility Study of 

Magneto Plasma Sail by 

Using Numerical 

Simulation and 

Experiment 

Y. Kajimura, Kyushu 

University, Kasuga, 

Japan 

1030 


Micro- Size Pulse 


Performance 

S. Kitano, Aoyama 

Gakuin University, 

Kanagawa, Japan 

1030 


Experimental Study for 

the Optimal Electrode 

Geometry in an MPD 

Thruster 

D. Nakata, University of 

Tokyo, Bunkyo-ku, 

Japan 

1100 


Meso- Scale Burner 

Using Combustion 

Inside Porous Inert 

Media 

S. Vijaykant, University 

of Alabama, Tuscaloosa, 

AL 

1100 


Wireless Transfer of 

Electricity in Outer Space 


Brooklyn, NY 

Session 82-SE-1 Systems Engineering I Cascade 1 

Chaired by: S. RAGHUNATHAN, Queens University, Belfast, Northern Ireland, and E. NICHOLS, Orbital Sciences Corporation, Dulles, VA 

0800 


Systems Engineering for 

CDIO - Conceive, 

Design, Implement and 

Operate 

J. Hsu, The Boeing 

Company, Anaheim, CA 

0830 


Interoperability Patterns 

and Systems of 

Systems Acquisition 

J. Smith, Carnegie 

Mellon Software 

Engineering Institute, 

Arlington, VA 

0900 


Digital Design Synthesis 

and Virtual Lean 

Manufacture 

A. Murphy, Queen's 

University Belfast, 

Belfast, Northern Ireland 

0930 


Safety, and Results 

Oriented Risk 

Methodology 

J. Porter, , , 

1000 


Lessons Learned: 

Application of Small 

UAV for Urban Highway 

Traffic Monitoring 

K. Ro, Western 


Kalamazoo, MI



Chaired by: V. LYONS, NASA Glenn Research Center, Cleveland, OH, and D. PEPPER, University of Nevada, Las Vegas, NV 

0800 0900 0930 1000 1030 

Chaired by: E. ZOBY, NASA Langley Research Center, Hampton, VA, and M. WRIGHT, NASA Ames Research Center, Moffett Field, CA 

0800 0900 0930 1000 

Chaired by: D. LEVIN, Pennsylvania State University, University Park, PA, and M. IVANOV, Russian Academy of Sciences, Novosibirsk, Russia 

0800 0830 0900 0930 1000 1030 1100 1130


Session 83-TES-3 Reacting Flow in Energy Systems N-5 

Chaired by: V. LYONS, NASA Glenn Research Center, Cleveland, OH, and D. PEPPER, University of Nevada, Las Vegas, NV 

0800 


Partially- Premixed Flames: Applications and 

Issues 

I. Puri, Virginia Polytechnic Institute and State 

University, Blacksburg, VA 


Session 84-TP-6 Aerothermodynamics of the NASA Crew Exploration Vehicle Carson 4 


0900 


Stability and Global 

Emission Characteristics 

of Elliptic Burner 

Diffusion Flames in an 

Elliptic Co- Flow 

S. Chinthamony, The 

University of Oklahoma, 

Norman, OK 

0930 


Volume and 

Temperature of Smoke 

in Fires 

D. Lilley, Lilley & 

Associates, Stillwater, OK 

1000 


Numerical Methods with 

Excel/VBA: Some 

Applied Examples 

D. Lilley, Oklahoma 



Chaired by: E. ZOBY, NASA Langley Research Center, Hampton, VA, and M. WRIGHT, NASA Ames Research Center, Moffett Field, CA 

0800 


Crew Exploration Vehicle (CEV) Crew Module 

shape selection analysis and CEV Aeroscience 

Project Overview 

J. Greathouse, NASA Lyndon B. Johnson Space 

Center, Houston, TX 

0900 


An Asymmetric Capsule 

Vehicle Geometry Study 

for CEV 

J. Brown, NASA Ames 

Research Center, Moffett 

Field, CA 

0930 


FIRE II Calculations for 

Hypersonic 

Nonequilibrium 

Aerothermodynamics 

Code Verification: DPLR, 

LAURA, and US3D 

D. Hash, NASA Ames 


Field, CA 

1000 


Aerothermal Anchoring 

of CBAERO Using High 

Fidelity CFD 

D. Kinney, NASA Ames 


Field, CA 

1030 


Flame Characteristics of 

Hydrogen- Enriched 

Methane- Air Premixed 

Swirling Flames 

H. Kim, University of 


MD 

Session 85-TP-7 DSMC and Rarefied Flows Ruby 2 

Chaired by: D. LEVIN, Pennsylvania State University, University Park, PA, and M. IVANOV, Russian Academy of Sciences, Novosibirsk, Russia 

0800 


Non- Equilibrium Shock 

Structure Computation 

with a Kinetic BGK 

Scheme 

C. Cai, ZONA 

Technology Inc. , 

Scottsdale, AZ 

0830 


Parallel, 

Steady/Unsteady DSMC 

Simulations of the 

Aerodynamics of 

Sounding Rockets 



0900 


Modeling of the Stardust 

Reentry Flows with 

Ionization in DSMC 

, 

0930 


Modeling of Hypersonic 

Wake Flows of Slender 

and Blunt Bodies 

, 

1000 


Modular Implementation 

of a Hybrid DSMC- NS 

Algorithm for 

Hypersonic Non- 

Equilibrium Flows 

T. Schwartzentruber, 

University of Michigan, 

Ann Arbor, MI 

1030 


DSMC Dissociation 

Model Based on Two- 

Temperature Chemical 

Rate Constant 

Y. Bondar, 

Khristianovich Institute 

of Theoretical and 

Applied Mechanics 

(ITAM), Novosibirsk, 

Russia 

1100 


Leading Edge 

Thickness Impact on 

Drag and Lift in 

Hypersonic Wedge Flow 

W. Santos, National 

Institute for Space 

Research, Cachoeira 

Paulista, Brazil 

1130 


Multiple Temperature 

Kinetic Model for 

Continuum and Near 

Continuum Flows 

K. Xu, Hong Kong 

University of Science 

and Technology, , Hong 

Kong



Chaired by: B. BABIN, Kansas State University, Manhattan, KS, and F. LAI, University of Oklahoma, Norman, OK 

0800 0830 0900 0930 

Chaired by: C. SUCHOMEL, U.S. Air Force Research Laboratory, Wright-Patterson AFB, OH, and A. STARIKOVSKII, Moscow Institute of Physics and Technology, Dolgoprudny, Russia 

0800 0830 0900 0930 1000 1030 1100 

Chaired by: C. VAN DAM, University of California, Davis, Davis, CA 

0830 0900 0930 1000 1030 1100


Session 86-TP-8 Thermal Managment of Electronics Ruby 1 

Chaired by: B. BABIN, Kansas State University, Manhattan, KS, and F. LAI, University of Oklahoma, Norman, OK 

0800 


Comparison of 

Electrowetting on 

Dielectric and 

Dielectrophoresis Force 

Distributions 

E. Baird, University of 

Colorado, Boulder, CO 

0830 


Effects of Thermal and 

Vibrational Cycles on 

Stresses in Lead- Free 

Solder Joints 

N. Corbitt, Raytheon, 

Dallas, TX 


Session 88-WIG/PDL-3 Plasma Actuators II Sierra 1 


0900 


Finite Element Modeling 

of Thermoelectric 

Effects in ANSYS 

M. Cochran, Kansas 


Manhattan, KS 

0930 


Bridging of Spatial and 

Temporal 

Characterization in 

Superlattices and 

Periodic Thin- Film 

Strcutures Via the Cand 

F- Processes Heat 

Conduction Model 

C. Anderson, University 

of Minnesota, 


Chaired by: C. SUCHOMEL, U.S. Air Force Research Laboratory, Wright-Patterson AFB, OH, and A. STARIKOVSKII, Moscow Institute of Physics and Technology, Dolgoprudny, Russia 

0800 


Use of a Plasma Arc to 

Produce Large Surface 

Pressure Changes On a 

Flat Plate in a Mach 5 

Flow 

J. Menart, Wright State 


0830 



DC and RF Glow 

Discharges 

J. Poggie, Air Force 



OH 

0900 



Dielectric Barrier 


Actuators Driven By 

Repetitive Nanosecond 

Pulses 

A. Likhanskii, Princeton 


0930 


Scaling Effects of an 

Aerodynamic Plasma 

Actuator 

T. Ng, Orbital Research 

Inc., Cleveland, OH 

1000 


Use of Aggregate 

Plasma Synthetic Jet 

Actuators for Flow 

Control 

Session 87-WE-3 Aerodynamics and Aeroacoustics McKinley 

Chaired by: C. VAN DAM, University of California, Davis, Davis, CA 

0830 


Simulation of Low 

Frequency Noise from a 

Downwind Wind Turbine 

Rotor 

H. Madsen, Risø 

National Laboratory, 

Roskilde, Denmark 

0900 


Analysis of the Flow 


Several Non- Rotating 

Rotor Blades 

R. van Rooij, Delft 

University Wind Energy 

Research Institute, Delft, 


0930 


A Modified Dynamic 

Stall Model for Low 

Mach Numbers 

W. Sheng, University of 

Glasgow, , Great Britain 

1000 


Rotationally Augmented 

Flow Structures and 

Time Varying Loads on 

Turbine Blades 

S. Schreck, NREL's 

National Wind 

Technology Center, 

Golden, CO 

, 

1030 


Three- dimensional and 

Rotational 

Aerodynamics on the 

NREL phase VI Wind 

Turbine Blade 

A. Gonzalez, CENER 

(National Renewable 

Energy Center), 

Sarriguren, Spain 

1030 


Effects of an 

Aerodynamic Plasma 

Actuator on a HSNLF 

Airfoil 

M. Post, U.S. Air Force 

Academy, USAF 

Academy, CO 

1100 


The Influence of Free 

Stream Turbulence 

Intensity on the 

Unsteady Behavior of a 

Wind Turbine Blade 

Section 

, 

1100 


Aerodynamic Control of 

1303 UAV Using 

Windward Surface 

Plasma Actuators on a 

Separation Ramp 


Toledo, Toledo, OH

1400-1430 hrs 



The panel discussion will focus on the flow quality of Aeroacoustic Wind Tunnels, particularly as it relates to future reductions in airframe noise. 

Chaired by: M. BRADLEY, The Boeing Company, Huntington Beach, CA, and R. MOEHLENKAMP, Pratt and Whitney Rocketdyne, West Palm Beach, FL 

1400 1430 1500 1530 1600

Tuesday Afternoon / 09 January 2007 

1400 - 1530 Career Workshop: Managing Your Career in the 21st Century II Crystal 5 

1400-1430 hrs 

Vanishing Defined Benefit Pensions in Aerospace 

Bob Wessels, Lockheed Martin Corporation 

1430-1500 hrs 

Be Your Own Boss - Consulting 

Paul Kostek, The Boeing Company 

1500-1530 hrs 

Small Business Guide 

Paul Kostek, The Boeing Company 


Session 89-AA-4 

1400 - 1700 


Flow Quality Issues for Airframe Noise Testing (Joint AA/FD/GT Session) N-10 

The panel discussion will focus on the flow quality of Aeroacoustic Wind Tunnels, particularly as it relates to future reductions in airframe noise. 

Co-Sponsors: 

Fluid Dynamics, Aeroacoustics, and Ground Testing Technical Committees. 

Moderator: Clifton Horne - NASA Ames Research Center 

Panelists: 

Craig Streett - NASA Langley Research Center 

Werner Dobrzynski - DLR, German Aerospace Research Center 

Robert Stoker - The Boeing Company 

Gerd Heller - Airbus 

Krish Ahuja - Georgia Tech Research Institute 

Lou Cattafesta - University of Florida 

Ricardo Burdisso - Virginia Polytechnic Institute and State University 

Scott Morris - University of Notre Dame 

Session 90-ABP-5 High Speed Propulsion II Cascade 2 

Chaired by: M. BRADLEY, The Boeing Company, Huntington Beach, CA, and R. MOEHLENKAMP, Pratt and Whitney Rocketdyne, West Palm Beach, FL 

1400 


The Art of Extracting 

One- Dimensional Flow 

Properties from Multi- 

Dimensional Data Sets 

R. Baurle, NASA 



1430 



of the Performance of 

Scramjet Engine with 

Pylon Set and of the 

Supersonic Star- 

Shaped Inlet Flow 

A. Gonor, Hampton 

University, Hampton, VA 

1500 


Airframe/Scramjet 

Integrated Design of 

Hypersonic Cruise 

Vehicle 

C. Jing, Northwestern 



1530 


Quasi- One- 

Dimensional Parametric 

Study for MHD 

Generator in MHD 

Bypass Scramjet System 

C. Lee, Beihang 


China (prc) 

1600 


Parametric Study of 3- D 

Hydrocarbon Scramjet 

Engine with Cavity 

H. Ebrahimi, Arnold 

Engineering 

Development Center , 

Arnold AFB , TN



Chaired by: J. TOWNSEND, Olin College of Engineering, Needham, MA, and R. GAETA, Georgia Technical Research Institute, Atlanta, GA 

1400 1430 1500 1530 1600 1630 

Chaired by: E. CRAMER, The Boeing Company, Seattle, WA, and W. CROSSLEY, Purdue University, West Lafayette, IN 

1400 1430 1500 1530 1600 1630 1700 

Chaired by: J. VALASEK, Texas A&M University, College Station, TX, and T. DOWNEN, Raytheon, Wichita, KS 

1400 1430 1500 1530 1600 1630 1700


Session 91-ABP-6 Turbines and Combustors Whitney 

Chaired by: J. TOWNSEND, Olin College of Engineering, Needham, MA, and R. GAETA, Georgia Technical Research Institute, Atlanta, GA 

1400 


Turbine Blade Tip 

Leakage Flow Control: 

Thick/Thin Blade Effects 

J. Stephens, University 

of Notre Dame, Notre 

Dame, IN 

1430 


Stereo PIV of a Turbine 

Tip Clearance Flow with 

Plasma Actuation 

D. Van Ness, University 

of Notre Dame, Notre 

Dame, IN 


Session 92-AD-4 Aircraft Design Methods Crystal 3 


1500 



a Low Pressure Turbine 

Blade Employing Active 

Flow Control 

M. Galbraith, University 

of Cincinnati 


Dynamics Research 

Laboratory, Cincinnati, 

OH 

1530 


Numerical Study of an 

Inter- Turbine Burner 

(ITB) Concept with 

Curved Radial Vane 

H. Thornburg, 

Mississippi State 

University, , MS 

1600 


Parametric Cycle 

Analysis of Dual- Spool 

Mixed- Exhaust 

Turbofan with Interstage 

Turbine Burner 

Q. Li, Northwestern 



Chaired by: E. CRAMER, The Boeing Company, Seattle, WA, and W. CROSSLEY, Purdue University, West Lafayette, IN 

1400 


Aircraft Fuel System 

Synthesis Aided by 

Interactive Morphology 

and Optimization 

H. Gavel, Saab 

Aerosystems, 

Linköping, Sweden 

1430 


The Role of Error in the 

Conceptual Design of a 

Transport Aircraft 

R. McDonald, California 


University, San Luis 

Obispo, CA 

1500 


Multidisciplinary 

Integrated Preliminary 

Design Applied to Future 

Green Aircraft 


C. Werner-Westphal, 

Technical University of 

Braunschweig, 

Braunschweig, Germany 

1530 


Incorporation of Flight 

Control Design Tools 

into the Multi- 

Disciplinary Conceptual 

Design Process 

T. Takahashi, Raytheon 

Missile Systems, 

Tucson, AZ 

1600 


Flight Vehicle Design 

Heritage: Are We On the 

Road to the Same Fate 

as Alexandria? 

K. Roberts, The 

University of Texas at 

Arlington, Arlington, TX 

1630 


Engineering Model of 

Chemical Non- 

Equilibrium Combustion 

and Emission in Gas 

Turbine Combustor 

V. Naoumov, University 

of Tennessee, Knoxville, 

TN 

1630 


A Generic Stability and 

Control Tool for 

Conceptual Design, 

Prototype Styem 

Overview 

G. Coleman, The 



1700 


A Systems Engineering 

Approach to the Design 

of Control Surfaces for 

UAVs 

M. Sadraey, Daniel 

Webster College, 

Nashua, NH 

Session 93-AFM-4 Bio-Inspired and Micro Aerial Vehicle Aerodynamics N-11 

Chaired by: J. VALASEK, Texas A&M University, College Station, TX, and T. DOWNEN, Raytheon, Wichita, KS 

1400 


The Low Reynolds 

Number Aerodynamics 

of Leading Edge Flaps 

N. Bakhtian, University 

of Cambridge, 


1430 


Lateral Control and 

Observation of a Micro 

Aerial Vehicle 

J. Hall, University of 


1500 


Biomimic Sensors 

Guided Flight Stability 

and Control for Flapping 

Wings Autonomous 

Micro Air Vehicles 

(Entomopter) 

A. Jaroszewicz, 

Wroclaw University of 

Technology, Wroclaw, 

Poland 

1530 


Dynamics of a 

Compliant Membrane as 

Related to Mammalian 

Flight 

A. Song, Brown 


RI 

1600 


Design of the Air Force 

Research Laboratory 

Micro Aerial Vehicle 

Research Configuration 

K. Stewart, Air Force 

Research Laboratory 

Munitions Directorate, 

Eglin AFB, FL 

1630 


The Development of a 

Miniature Flexible 

Flapping Wing 

Mechanism for Use in a 

Robotic Air Vehicle 

G. Jadhav, Georgia 


Atlanta, GA 

1700 


A Comptational Study of 

the Aerodynamics of 

Hovering and 

Maneuvering in 

Drosophila 

R. Ramamurti, Naval 


Washington, DC



Chaired by: S. MORRIS, Engineering Systems Inc., Colorado Springs, CO 

1400 1430 1500 1530 1600 1630 1700 1730 

Chaired by: J. LUCKRING, NASA Langley Research Center, Hampton, VA 

1400 1430 1500 1530 1600 1630 

Chaired by: S. SILTON, U.S. Army Research Laboratory, Aberdeen Proving Ground, MD 

1400 1430 1500 1530 1600 1630 1700 1730


Session 94-APA-10 Configuration Aerodynamics Carson 1 

Chaired by: S. MORRIS, Engineering Systems Inc., Colorado Springs, CO 

1400 


Aerodynamic 

Investigations of an 

Advanced Over- the- 

Wing Nacelle Transport 

Aircraft Configuration 

G. Hill, Old Dominion 


1430 


Yaw Control of a Blunt- 

Nose Projectile at High 

Angles of Attack Using 

Strakes 


Toledo, Toledo, OH 


Session 95-APA-11 Cranked Arrow Wing Aerodynamics Project International II N-8 


1500 


AERODYNAMIC 

CHARACTERIZATION 

OF A CANARD GUIDED 

ARTILLERY 

PROJECTILE 

W. Su, U.S. Army 

RDECOM-ARDEC, 

Picatinny Arsenal, NJ 

Chaired by: J. LUCKRING, NASA Langley Research Center, Hampton, VA 

1400 


Steady and Unsteady 

CFD Analysis of the F- 

16XL using the 

Unstructured Edge Code 

S. Görtz, Royal Institute 

of Technology (KTH), 


1430 


BCFD Unstructured- 

Grid Predictions on the 

F- 16XL (CAWAPI) 

Aircraft 

T. Michal, The Boeing 


1500 


Hybrid Grid Solutions on 

the (CAWAPI) F- 16XL 

Using Falcon v4 

M. Davis, Aerodynamics 

and CFD, , 

1530 


Aerodynamic Origin of 

Jet/Fin Interaction on a 

Full- Scale Flight 

Vehicle Configuration 

S. Beresh, Sandia 



1600 


Space Shuttle SRB Aft 

End Orientation Biases 

After Linear Shape 

Charge Activation 

D. Gonzalez, Naval 


Indian Head, MD 

1630 


Assessment of Missile 

Plume Impact 


R. Gleissl, EADS 

Military Air Systems, 

Munich, Germany 

1700 


Aerodynamic Ground 

Effects of Tailless 

Chevron and Lambda- 

Shaped UCAV Models 

W. In, Air Force Institute 



OH 

1730 


Aerodynamic Evaluation 

of Wing- Strake 

Modification by Higher 

Order Panel Method 

A. Maqsood, National 

University of Sciences 

and Technology, 

Risalpur, Pakistan 

Session 96-APA-12 Transonic, Supersonic, and Hypersonic Aerodynamics N-9 

Chaired by: S. SILTON, U.S. Army Research Laboratory, Aberdeen Proving Ground, MD 

1400 


Pressures and Drag 


Bodies of Revolution at 

Near Sonic Speeds 

Including the Effects of 

Viscosity and Wind 

Tunnel Walls 

B. Kulfan, Boeing 

Commercial Airplane 

Group, Seattle, WA 

1430 


Extensive Supersonic 

Natural Laminar Flow on 

the Aerion Business Jet 

P. Sturdza, Desktop 

Aeronautics, Inc., Palo 

Alto, CA 

1500 



Supersonic Wing Shape 

Using Busemann 

Biplane Airfoil 

M. Yonezawa, Tohoku 


Japan 

1530 


Unstructured Grid 

Solutions of CAWAPI F- 

16XL by UT SimCenter 

S. Karman, University of 

Tennessee at 

Chattanooga, 


1530 


Consideration at Off- 

Design Conditions of 

Supersonic Flows 

around Biplane Airfoils 

D. Maruyama, Tohoku 


Japan 

1600 


USM3D Unstructured 

Grid Solutions for 

CAWAPI at NASA LaRC 

J. Lamar, NASA Langley 


Hampton, VA 

1600 


A Study of Busemann- 

Type Biplane for 

Avoiding Choked Flow 

H. Yamashita, Tohoku 


Japan 

1630 


What Was Learned from Numerical Simulations 

of F- 16XL (CAWAPI) at Flight Conditions 

A. Rizzi, Royal Institute of Technology, 


1630 


A Numerical Analysis on 


Flow Field in a 

Supersonic Bump Inlet 

S. Kim, Daegu 

University, Gyoungsan, 

South Korea 

1700 


Effect of Geometric 

Parameters on the 

Aerodynamic 

Characteristics of Grid- 

Fin Cells at Supersonic 

Speeds 

P. Theerthamalai, 

Defence Research and 

Development 

Laboratory, Hyderabad, 

India 

1730 


Application of High- 

Order Accurate 

Algorithm to Hypersonic 

Viscous Flows for 

Calculating Heat 

Transfer Distributions 

X. Liu, China 

Aerodynamics Research 

and Development 

Center, Mianyang, China 

(prc) 



Chaired by: R. MOSER, QinetiQ, Farnborough, Great Britain, and G. WELSH, Raytheon Aircraft Corporation, Maize, KS 

1400 1430 1500 1530 

Chaired by: E. SCHROCK, Lockheed Martin Aeronautics Company, Palmdale, CA, and A. VIZZINI, Mississippi State University, Mississippi State, MS 

1400 1430 1500 1530 1600 1630 1700 1730 

Chaired by: I. GURSUL, University of Bath, Bath, Great Britain, and M. AMITAY, RPI, Troy, NY 

1400 1430 1500 1530 1600 1630 1700


Session 97-ASE-8 Ice Protection and Detection Crystal 1 

Chaired by: R. MOSER, QinetiQ, Farnborough, Great Britain, and G. WELSH, Raytheon Aircraft Corporation, Maize, KS 

1400 


Thermo- Mechanical 

Expulsive Deicing 

System - TMEDS 

K. Al-Khalil, Cox and 

Company, Inc., New 

York, NY 

1430 


The FAA Ground Icing 

Research Program 

J. Riley, FAA William J. 

Hughes Technical 

Center, Atlantic City 

International Airport, NJ 


Session 98-EDU-2 Approaches to Education Shasta 1 


1500 


Inclement Weather 

Considerations for 

Aircraft Engines 

K. Venkataramani, GE 

Aviation, Cincinnati, OH 

1530 


"Aircraft Ice Detection 

Method" 

P. Jarvinen, 


of Technology (Ret.), 

Amherst , NH 

Chaired by: E. SCHROCK, Lockheed Martin Aeronautics Company, Palmdale, CA, and A. VIZZINI, Mississippi State University, Mississippi State, MS 

1400 


Challenging Projects in 

Aerospace and 

Mechanical Engineering 

Senior Capstone Design 

Experience 

M. Parang, University of 

Tennessee, Knoxville, 

TN 

1430 


The Lockheed SR- 71 

Blackbird - A Senior 

Capstone Re- 

Engineering Experience 

B. Mixon, The University 

of Texas at Arlington , 

Arlington, TX 

1500 


Simulator- Based Flight 

Test Engineering as a 

Capstone to the 

Dynamics and Control 

Curriculum 

M. Cotting, Virginia 




1530 


Flight Testing Education 

at Western Michigan 

University 

T. Liu, Western 


Kalamazoo, MI 

Session 99-FD-18 Airfoil Flow Control Carson 2 

Chaired by: I. GURSUL, University of Bath, Bath, Great Britain, and M. AMITAY, RPI, Troy, NY 

1400 


Analysis of a 

Methodology for 2- D 

High Lift Testing Using 

a Boundary- Layer 

Control System by Air 

Blowing 

M. Assato, Pontifícia 

Universidade Católica, 

Instituto de Energia da 

Puc-rio, Rio De Janeiro, 

Brazil 

1430 


High- Lift System for a 

Supercritical Airfoil: 

Simplified by Active 

Flow Control 

L. Pack-Melton, NASA 



1500 


Control of Airfoil 

Aerodynamic 

Performance Using 

Distributed Trapped 

Vorticity 

M. DeSalvo, Woodruff 

School of Mechanical 

Engineering, Georgia 


Atlanta, GA 

1530 


Low- Dimensional 

Models for Control of 

Leading- Edge Vortices: 

Equilibria and Linearized 

Models 

S. Ahuja, Princeton 


1600 


A Novel Technique for 

Educating Aeroelasticity 

Engineers 

D. Pitt, The Boeing 


1600 


Unsteadiness in Flow 

over a Flat Plate at 

Angle- of- Attack at Low 


K. Taira, California 


Pasadena, CA 

1630 


A Software System for 

Teaching Design and 

CFD Analysis Concepts 

for Supersonic Nozzles 

G. Briasco, Dimset – 

Università di Genova, 

Genova, Italy 

1630 


Minimizing Induced 

Drag with Blowing 

Variation Along the 

Span of a Circulation- 

Controlled Wing 

N. Alley, Utah State 


1700 


Gas Turbine Engine 

Testing Education at 

Western Michigan 

University 

W. Liou, Western 


Kalamazoo, MI 

1700 



Transonic Drag 

Reduction for Flow Past 

Airfoils Using Active 

Flow Control 

J. Vadillo, Mechanical 

and Aerospace 

Engineering 

Department, Washington 

University in St. Louis, 

St. Louis, MO 

1730 


Strategic Planning for 

Airport Systems: An 

Educational Perspective 

P. Roling, Delft 

University of 

Technology, Faculty of 

Aerospace Engineering, 

Delft, The Netherlands 



Chaired by: M. VISBAL, U.S. Air Force Research Laboratory, Wright-Patterson AFB, OH, and A. CARY, The Boeing Company, Saint Charles, MO 

1400 1430 1500 1530 1600 1630 1700 

Chaired by: M. MANI, The Boeing Company, St Louis, MO, and D. RIZZETTA, U.S. Air Force Research Laboratory, Wright-Patterson AFB, OH 

1400 1430 1500 1530 1600 1630 1700 1730 

Chaired by: K. COHEN, KAYOS Enterprise Inc, Colorado Springs, CO, and J. MYATT, U.S. Air Force Research Laboratory, Wright-Patterson AFB, OH 

1400 1430 1500 1530 1600


Session 100-FD-19 CFD Algorithms II Crystal 4 

Chaired by: M. VISBAL, U.S. Air Force Research Laboratory, Wright-Patterson AFB, OH, and A. CARY, The Boeing Company, Saint Charles, MO 

1400 


An Acceleration 

Approach for Reduced- 

Order Models Based on 

Proper Orthogonal 

Decomposition 

P. Cizmas, Department 

of Aerospace 

Engineering, Texas 


Station, TX 

1430 


A Regularization of 

Burgers Equation using 

a Filtered Convective 

Velocity 

G. Norgard, Department 

of Aerospace 

Engineering Sciences, 

University of Colorado, 

Boulder, CO 


Session 101-FD-20 CFD LES Modeling and Applications I N-6 


1500 


Assessment of a 

Lagrangian 

Incompressible Flow 

Code 

R. Aubry, George Mason 

University, Fairfax, VA 

1530 



2D/AXI Kinetic BGK 

Scheme for Hypersonic 

Nonequilibrium Flow 

Compuations 

C. Cai, ZONA 

Technogloy Inc., 

Scottsdale , AZ 

1600 


Image Base CFD for 

Blood Flow Analysis 

M. Garbey, Department 

of Computer Science, 

University of Houston, 

Houston, TX 

Chaired by: M. MANI, The Boeing Company, St Louis, MO, and D. RIZZETTA, U.S. Air Force Research Laboratory, Wright-Patterson AFB, OH 

1400 


Numerical Simulation 

Around Airfoil with High 

Resolution in High 


T. Kurotaki, Japan 



1430 


Subgrid Modeling 

Approaches for Scalar 

Transport and Mixing in 

LES of Turbulent Shear 

Flows 

1500 


Numerical and Modeling 

Issues in LES of 

Compressible 

Turbulence on 


O. Sun, Johns Hopkins N. Park, University of 

University, Baltimore, MD Minnesota, Minneapolis, 

MN 

1530 


LES and DES 

Simulations for Aircraft 

Design 

F. Chalot, Dassault 

Aviation, Saint Cloud, 

France 

1600 


LES for Interaction of 

Wingtip Vortex and 

Wakes 

L. Jiang, Department of 

Mathematics, University 


Arlington, TX 

1630 


Effect of Discretization 

Order on 

Preconditioning and 

Convergence of a 

Higher- Order 

Unstructured Newton- 

Krylov Solver for Inviscid 

Compressible Flows 

A. Nejat, Department of 

Mechanical Engineering, 

The University of British 

Columbia, Vancouver, 

Canada 

1630 



of Accelerating 


G. De Prisco, 

Department of 

Mechanical 

Engineering, University 

of Maryland, College 

Park, MD 

1700 


A Compressible Flow 

Simulation System 

Based on Cartesian 

Grids with Anisotropic 

Refinements 

F. Capizzano, Italian 


Center - CIRA, Capua 

(CE), Italy 

1700 


Application of a 

Dynamic Variational 

Multiscale Method to the 

LES of Separated 

Turbulent Flows 

A. Rajasekharan, 

Department of 


and Institute for 

Computational and 

Mathematical 

Engineering Stanford 


1730 


Numerical Study of a 

Scaling Parameter for 


Layer with Large 

Roughness 

E. Johnson, Florida 


Melbourne, FL 

Session 102-FD-21 Fluid-Structure Interaction II Carson 3 

Chaired by: K. COHEN, KAYOS Enterprise Inc, Colorado Springs, CO, and J. MYATT, U.S. Air Force Research Laboratory, Wright-Patterson AFB, OH 

1400 


The Analysis of High- 

Speed Printing Machine 

Using Fluid- Structure 

Interaction Method 

1430 


Integrated Analysis of 

Air- launched Rocket 

Using Fluid- Structure 

Interaction 

1500 


The Effects on 

Formation- Flight 

Aerodynamics due to 

Wake Rollup 

1530 


Flutter Simulation and 

Prediction with CFDbased 

Reduced- Order 

Model 

1600 


Fluid- Structure 

Interactions for Pulsatile 

Flow through Elastic 

Arteries

J. Kim, Konkuk 


Korea 

K. Noh, Konkuk 


Korea 

G. Bramesfeld, The 



Park, PA 

K. Lai, Temasek 

Laboratories, National 



E. Shaik, Department of 

Aerospace Engineering, 

Wichita State University, 

Wichita, KS 



Chaired by: W. SARIC, Texas A&M University, Bryan, TX 

Chaired by: P. SUNDERLAND, University of Maryland, College Park, MD, and G. RUFF, NASA Glenn Research Center, Cleveland, OH 

1400 1430 1500 1530 1600 1630 1700 1730 

Chaired by: J. MARCHETTA, University of Memphis, Memphis, TN, and H. NAHRA, NASA Glenn Research Center, Cleveland, OH 

1400 1430 1500 1530 1600


Session 103-FD-22 Transition Study Group Open Forum N-3 

Chaired by: W. SARIC, Texas A&M University, Bryan, TX 


Session 104-GPSE-4 Combustion Science / Spacecraft Fire Safety Shasta 2 

Chaired by: P. SUNDERLAND, University of Maryland, College Park, MD, and G. RUFF, NASA Glenn Research Center, Cleveland, OH 

1400 


Flame Radiation, 

Structure and Scalar 

Properties in 

Microgravity Laminar 

Fires 

D. Feikema, NASA 

Glenn Research Center 

at Lewis Field, 


1430 


Effects of Lewis 

Number on 

Temperatures of 

Spherical Diffusion 

Flames 

K. Santa, University of 

Hawaii, Honolulu, HI 


1500 


An Experimental 

Investigation of the 

Laminar Flamelet 

Concept for Soot 

Properties 

F. Diez, Rutgers 


NJ 

1530 


Microgravity Ignition 

Delay of Bio- Ester Fuel 

Droplets 

T. Vaughn, Rowan 

University, Glassboro, 

NJ 

1600 


Modeling Microgravity 

and Normal Gravity 

Opposed Flame Spread 

over Polymer/Glass 

Composites 

S. McAllister, 

Department of 



Berkeley, Berkeley, CA 

Session 105-GPSE-5 Fluid Physics in Low Gravity N-4 

Chaired by: J. MARCHETTA, University of Memphis, Memphis, TN, and H. NAHRA, NASA Glenn Research Center, Cleveland, OH 

1400 


Capillary Flow in 

Cylindrical Containers 

with Rounded Interior 

Corners 

Y. Chen, Portland State 

University, Portland, OR 

1430 


Capillary Driven Flows in 

Weakly 3- Dimensional 

Polygonal Containers 

M. Weislogel, Portland 


Portland, OR 

1500 


Interim Results from the 

Capillary Flow 

Experiment Aboard ISS: 

The Moving Contact 

Line Boundary Condition 

M. Weislogel, Portland 


Portland, OR 

1530 


Effect of Magnetic 

Fields on 

Thermocapillary and 

Buoyancy Driven Flow of 

Two Immiscible Liquids 

D. Ludovisi, University of 

Illinois at Chicago, 

Chicago, IL 

1600 


Drops in a Surfactant 

Solution: Oscillatory 

Regimes of Mass 

Transfer 

K. Kostarev, Institute of 

Continuous Media 

Mechanics, Perm, Russia 

1630 


Extinction of Counter- 

Flow and Stagnation 

Diffusion Flames with 

Fire- Extinguishing 

Agents 

D. Dietrich, NASA 



1700 


Stabilization and 

Suppression of 

Axisymmetric Diffusion 

Flames 

F. Takahashi, National 


Exploration Research on 

Fluids and Combustion 

NASA Glenn Research 

Center, Cleveland, OH 

1730 


Development of a Fire 

Suppression Simulation 

Tool for Various Low- 

Gravity Environments 

D. Schwer, Naval 





Chaired by: R. WAHLS, NASA Langley Research Center, Hampton, VA, and J. QUEST, European Transonic Windtunnel GmbH, Köln, Germany 

1400 1430 1500 1530


Session 106-GT-4 / APA-23 High Reynolds Number Aerodynamics and Testing (Invited) Sierra 2 

Chaired by: R. WAHLS, NASA Langley Research Center, Hampton, VA, and J. QUEST, European Transonic Windtunnel GmbH, Köln, Germany 

1400 


New Techniques for 

Operation in Cryogenic 

Windtunnels 

M. Schulz, European 

Transonic Windtunnel 

GmbH, 

Ernst-Mach-Strasse, 

Koeln, Germany 

1430 


Validation of Blockage 

Interference Corrections 

in the National Transonic 

Facility (Invited) 

E. Walker, NASA 




Session 107-IS-2 Intelligent Path Planning and Fault Diagnostics Cascade 1 


1500 


Progress in Flaps Down 

Flight Reynolds Number 

Testing Techniques at 

the NTF 

F. Payne, The Boeing 


Chaired by: F. FIGUEROA, NASA Stennis Space Center, Stennis Space Center, MS 

1400 


Automated Reasoning to 

Support Mixed- Initiative 

Command and Control 

of UAVs 

R. Penner, Iterativity, 

Inc., Minneapolis, MN 

1430 


An Agent- based 

Approach to Health 

Monitoring Systems 

Applied to the ISS Power 

System 

M. Lyell, Intelligent 

Automation, Inc., 

Rockville , MD 

1530 


Re- No. Scaling Effects 

on the EUROLIFT High 

Lift Configurations 

R. Rudnik, DLR, German 


Center, Braunschweig, 

Germany 

Session 108-MDO-3 Computational Design Optimization Carson 4 

Chaired by: J. GABLONSKY, The Boeing Company, Bellevue, WA 

1400 


Operations Based 

Optimisation Using 

Simulation and CFD 

J. Doherty, QinetiQ Ltd, 

Farnborough, Great 

Britain 

1430 


A Computational Design 

Framework for Flapping 

Micro Air Vehicles 

M. Blair, Air Force 



OH 

1500 


Multi- Point Aero- 

Structural Optimization 

of Wings Including 

Planform Variations 

A. Jameson, Stanford 


1530 


Applying Genetic 

Algorithms to Complex 


Dynamics Simulations 

R. LeBeau, University of 


1600 


Multi- Disciplinary 

Design of Aircraft 

Fuselage Structures 

M. van Tooren, Delft 

University of 



1630 


Effects of Flexibility on 

Aircraft Dynamic Loads 

and Structural 

Optimization 

H. Baluch, Delft 

University of 

Technology, Delft , The 





Session 109-PC-8 Combustion Chemistry, Mechanisms and Models Teton 2 

Chaired by: F. GOULDIN, Cornell University, Ithaca, NY 

1400 


Development of an Experimental Database and 

Kinetic Models for Surrogate Jet Fuels 

T. Edwards, Air Force Research Laboratories, 

Dayton, OH 


Session 110-PC-9 Rocket Combustion Processes and Modeling Teton 1 


1500 


Optimized Reduced 

Chemical Kinetic 

Mechanisms for 

Ethylene and JP- 8 

Combustion 

C. Montgomery, 

Reaction Engineering 

International, Salt Lake 

City, UT 

1530 



Implementation of 

Explicit Reduced 

Reaction Models in 

Supersonic Reacting 

Shear Flow Simulations 

A. Zambon, Mechanical 

and Aerospace 


of Virginia, 

Charlottesville, VA 

1600 


Improved Chemical 

Kinetic Models for 

Scramjet Combustion 

Simulation 

C. Montgomery, 

Reaction Engineering 

International, Salt Lake 

City, UT 

1630 


Shock Tube Studies of 

Soot Formation in 

Heptane and 

Heptane/DME Mixtures 

Z. Hong, Stanford 


Chaired by: B. GREENBERG, Technion - Israel Institute of Technology, Haifa, Israel, and J. MURPHY, The Aerospace Corporation, El Segundo, CA 

1400 


Simulation of Nozzle 

Erosion Process in a 

Solid Propellant Rocket 

Motor 

N. Liggett, The Georgia 


Atlanta, GA 

1430 


Non- Steady Burning 

Effect on Solid Rocket 

Motor Performance 

A. Tahsini, Sharif 

University of 

Technology, Tehran, Iran 

1500 


Graphite Nozzle 

Material Erosion in 

Solid- Propellant Rocket 

Motors 

P. Thakre, The 



Park, PA 

1530 


Coupling of Leading 

Edge Flames in the 

Combustion Zone of 

Composite Solid 

Propellants 

N. Mansu, Indian 

Institute of Technology – 

Madras, Chennai, India 

1600 


The Comparison of the 

Hot- Fire and Cold- Flow 

Observations of 

NTO/MMH Impinging 

Combustion 

T. Yuan, Institute of 

Aeronautics and 

Astronautics, National 

Cheng Kung University, 

Tainan, Taiwan (roc) 

1630 


Graphite Rocket Nozzle 

Erosion Rate Reduction 

by Boundary- Layer 

Control Using Ablative 

Materials 

R. Acharya, Dept. of 

Mechanical and Nuclear 

Engineering, The 


Univ., University Park, 

PA 

1700 


Kinetic Modeling for 

High Pressure, Fuel - 

Rich Methane / Oxygen 

Combustion 

N. Slavinskaya, German 

Aerospace Center, DLR 

Institute of Combustion 

Technology, Stuttgart, 

Germany 

1730 


A New Method in 

Modeling and 

Simulations of Complex 

Oxidation Chemistry 

K. Harstad, Jet 

Propulsion Laboratory, 

California Institute of 

Technology, Pasadena, 

CA 

Session 111-PDL-4 / FD-17 Plasma Actuators III N-7 

Chaired by: H. LOWRY, Aerospace Testing Alliance, Arnold AFB, TN 

1400 


Effect of Plasma 

Morphology on Flow 

Control Using Plasma 

Synthetic Jet Actuators 

A. Santhanakrishnan, 

Dept. of Mechanical 


1430 


Wall Normal Jet under 

Elevated Temperatures 

Produced by Surface 

Plasma Actuator 

T. Segawa, National 

Institute of Advanced 

Industrial Science and 

1500 


Switching Behavior of a 

Plasma- Fluidic Actuator 

J. Gregory, United 

States Air Force 

Academy, USAF 

Academy, CO 

1530 


Boundary Layer Control 

Using a DBD Plasma 

Actuator 

C. Porter, United State 

Air Force Academy, 

USAFA, CO 

1600 



Localized Arc Filament 

Plasma Actuators Used 

for High- speed Flow 

Control 

Y. Utkin, The Ohio State 


1630 


Characteristics of a 

Plasma Actuator in 

Mach 3 Flow 

J. Shin, The University of 

Texas at Austin, Austin, 

TX

of Kentucky, Lexington, 

KY 

Technology, Tsukuba, 

Japan 



Chaired by: G. FONT, U.S.Air Force Academy, Colorado Springs, CO 

1400 1430 1500 1530 

Chaired by: T. SHIH, Iowa State University, Ames, IA, and G. JACOBS, San Diego State University, San Diego, CA 

1400 1430 1500 

Chaired by: G. NATERER, University of Ontario Institute of Technology, Oshawa, Canada, and E. SHORT, Raytheon, Fairview, TX 

1400 1430 1500 1530 1600 1630 1700 

OH


Session 112-PDL-5 Plasmas and Materials Processing Crystal 2 

Chaired by: G. FONT, U.S.Air Force Academy, Colorado Springs, CO 

1400 


Binary Gas Mixture 

Separation Induced by 

an Optical Lattice in a 

Capillary 

M. Shneider, Princeton 


1430 


Simulation of Interacting 

Particles in a Cylindrical 

Plasma Reactor 


Session 113-TES-4 Hetergeneous Flow in Energy Systems N-5 


, 

1500 


Interaction of Molecular 

Gases with Pulsed 

Optical Lattices in 

Collisional Regime 

C. Ngalande, USC, Los 

Angeles, CA 

1530 


Effect of ion- neutral 

collisions on the 

charging of a dust particle 

Chaired by: T. SHIH, Iowa State University, Ames, IA, and G. JACOBS, San Diego State University, San Diego, CA 

1400 


Streamline- Based 

Modeling of Aerosol 

Microphysics in the Post- 

Combustor Flow Path 

and Sampling System 

T. Wey, Taitech Inc., 

Beavercreek, OH 

1430 


Analysis of Rotary- Vane 

Two- Phase 

Refrigeration Expanders: 

Geometric and 

Thermodynamic 

Modeling 

A. Mahmoud, University 

of Florida, Gainesville, FL 

1500 


Towards 

Microfabrication of a 

Thermoelectric Heat 

Engine in a Micro 

Energy Source 

P. Glockner, University 

of Manitoba, Winnipeg, 

Canada 

, 

Session 114-TP-9 Fluid Dynamic Methods for Convection Heat Transfer Ruby 1 

Chaired by: G. NATERER, University of Ontario Institute of Technology, Oshawa, Canada, and E. SHORT, Raytheon, Fairview, TX 

1400 


Exergy Recovery of 

Thermally Induced Wall 

Slip in Microchannels 

E. Ogedengbe, 

University of Manitoba, 

Winnipeg, Canada 

1430 



Effects of Buoyancy on 

Wake Instability of 

Heated Cylinder In 

Contra Flow 

K. Varma, Iowa State 

University, Rochester 

Hills, MI 

1500 


Application of h- , p- and 

hp- adaptation for 

Convective Heat 

Transfer Problems 

X. Wang, University of 

Nevada, Las Vegas, Las 

Vegas, NV 

1530 


Real Fluid Thermophysical 

and Transport 

Properties Calculations 

for Water 

T. Bose, Metacomp 

Technologies, Inc., 

Agoura Hills, CA 

1600 


Hypersonic Turbulent 

Reacting Flow 

Simulation of Fire II Reentry 

Vehicle 

K. Sinha, Indian Institute 

of Technology Bombay, 

Mumbai, India 

1630 


On the Estimation of 

Combustion Gas 

Temperature and 

Convective heat 

Transfer Coefficient 

R. Mehta, Vikram 

Sarabhai Space Centre, 


1700 



of the Airborne 

Contaminant Age in 

Surgical Operating 

Theatres 

R. Kameel, Consultant 

CEB, Cairo, Egypt 




Session 115-TP-10 Radiative Heating in Re-Entry Ruby 2 

Chaired by: K. FUJITA, Japan Aerospace Exploration Agency, Tokyo, Japan, and C. PARK, Korea Advanced Institute of Science and Technology, Daejeon, South Korea 

1400 


Calculation of Radiation 

from a Shock Layer 

Flow in an Arc- Jet 

Facility 

T. Sakai, Nagoya 


Japan 

1430 



Shock Wave with 

Precursor Heating 

R. Yoshizawa, 

University of Tokyo, 

Sagamihara, Japan 


Session 116-WE-4 Materials and Structures McKinley 


1500 


Shock- Tube 

Determination of CN 

Formation Rate in a CO- 

N2 Mixture 

E. Lee, Korea Advanced 

Institute of Science and 

Technology, Daejeon, 

South Korea 

1530 


Spectroscopic 

Properties of Diatomic 

Air Species 

D. Schwenke, NASA 

Ames Research Center, 


1600 


Titan Atmosphere 

Plasma Characterization 

Using Spectroscopic 

Measurement 

Techniques 

M. Playez, Von Karman 

Institute, Rhodes Saint 

Genèse, Belgium 

Chaired by: J. PAQUETTE, Sandia National Laboratories, Albuquerque, NM, and J. MANDELL, Montana State University, Bozeman, MT 

1400 


Structural Testing of 9m 

Carbon Fiber Wind 

Turbine Research 

Blades 

J. Paquette, Sandia 



1430 


Concepts to Facilitate 

Very Large Blades 

T. Ashwill, Sandia 



1500 


Comparison of Tensile 

Fatigue Resistance and 

Constant Life Diagrams 

for Several Potential 

Wind Turbine Blade 

Laminates 

D. Samborsky, Montana 


Bozeman, MT 

1530 


The Application of Pre- 

Cured Carbon 

Fiber/Epoxy Pultrusions 

as Reinforcement in 

Composite Wind Turbine 

Blades 

D. Cairns, Montana 


Bozeman, MT 

1600 


Comparison Between 

Inclusions and Holes as 

Stress Raisers in 

Composite Materials 

Used in Wind Turbine 

Components 

M. Elshabasy, Old 

Dominion University, 

Norfolk, VA 

1630 


Energy Spectral 

Distribution Behind 

Strong Shock Waves in 

CO:N2 Mixture 

E. Anokhin, Moscow 

Institute of Physics and 

Technology, 


1700 


Measurements of the UV 

Radiation Generated by 

the Soyuz Spacecraft 

Transport Capsule 

During Reentry 

Y. Plastinin, Central 

research institute of 

machine-building 

(TSNIIMASH), Korolev, 

Russia 

Session 117-WIG/PDL-4 Plasma II Sierra 1 

Chaired by: I. BLANKSON, NASA Glenn Research Center, Cleveland, OH, and A. KLIMOV, Russian Academy of Sciences, Moscow, Russia 

1400 


A Multi- Mode Plasma 

Pilot 

I. Matveev, Applied 

Plasma Technologies, 

McLean, VA 

1430 


Filamentary Pulsed- DC 

Discharges in Methane- 

Containing Mixtures 

M. Brown, Innovative 

Scientific Solutions, Inc., 

Dayton, OH 

1500 


Pulsed Surface 

Discharge for 

Hydrocarbon Fuel 

Inflammation 

A. Aleksandrov, Moscow 



1530 


3D Modelling of Glow 

Discharge with Physical- 

Chemical Kinetics 

A. Petrusev, Institute for 

Problems in Mechanics 


Science, Moscow, Russia 



Learn how AIAA Aerospace Standards are conceived and developed. Learn how these standards will impact your job and your company's products. 

Chaired by: K. VISWANATHAN, The Boeing Company, Seattle, WA, and A. PILON, Lockheed Martin Aeronautics Company, Palmdale, CA 

0800 0830 0900 0930 1000 

Chaired by: J. LEE, NASA Glenn Research Center, Cleveland, OH, and R. BAKOS, ATK, Ronkonkoma, NY 

0800 0830 0900 0930 1000 1030 1100 1130


1600 - 1730 Workshop: The ABCs of AIAA Standards Sierra 1 

Learn how AIAA Aerospace Standards are conceived and developed. Learn how these standards will impact your job and your company's products. 

Presenter: Frederick A. Slane, CEO 

Space Infrastructure Foundation, Inc. 


1730 - von Kármán Lectureship in Astronautics Reno Room 

Wednesday Morning / 10 January 2007 

Session 118-AA-5 Jet Noise: Supersonic N-10 

Chaired by: K. VISWANATHAN, The Boeing Company, Seattle, WA, and A. PILON, Lockheed Martin Aeronautics Company, Palmdale, CA 

0800 


Towards Predicting 

Supersonic, Hot Jet 

Noise 

X. Cai, Thaerocomp 

Technical Corporation, 

Stony Brook, NY 

0830 


High- Order Shock 

Capturing Schemes for 

Turbulence Calculations 

S. Lo, Purdue 


Lafayette, IN 

0900 


Correlation of Large- 

Scale Structure 

Dynamics and Far- Field 

Radiated Noise in a 

Mach 0.9 Jet 

J. Kastner, The Ohio 


Columbus, OH 

0930 


Shock Cell Modification 

Due to Chevrons 



OH 

1000 


Thermal Barrier Effects 

on Nonlinear Pressure 

Wave Propagation in 

Gases 

N. DiZinno, Polytechnic 

University, Brooklyn, NY 




0800 0830 0900 0930 1000 1030 1100 1130


Session 119-ABP-7 High Speed Propulsion III Cascade 2 


0800 


Finite Conductivity 

Evaporation Modeling of 

Liquid Jet in High- 

Speed Cross- Flow 

M. Balasubramanyam, 

University of Alabama in 

Huntsville, Huntsville, AL 

0830 


Pylon- Aided Fuel 

Injection into 

Supersonic Flow 

R. Balar, University of 


MD 


Session 120-ABP-8 Inlets, Combustors, Nozzles Whitney 


0900 



SCHOLAR Supersonic 

Combustion 

Experiments 

P. Keistler, North 

Carolina State 

University, Raleigh, NC 

0930 


A Comprehensive Study 

of Combustion 

Oscillations in a 

Hydrocarbon- Fueled 

Scramjet Engine 

J. Li, The Pennsylvania 

State University , 


1000 


Advance in Supersonic 

Combustion Modeling 

and Simulations 

A. Ingenito, University of 

Rome "La Sapienza", 

Rome, Italy 

Chaired by: K. BLODGETT, General Electric Aviation, Cincinnati, OH, and J. SAUNDERS, NASA Glenn Research Center, Cleveland, OH 

0800 


A Technique to Estimate 

Flow Distortion in 


Ingesting Serpentine 

Inlets Using Unsteady 

Wall- Pressures 

J. Anderson, Techsburg, 

Inc., Blacksburg, VA 

0830 



Experimental 


Serpentine Inlet Duct 

A. Kirk, Texas A&M 


Station, TX 

1030 


National Combustion 

Code Calculations of a 

NASA Low- NOx 

Hydrogen Injector 

Concept 

A. Iannetti, NASA Glenn 



1100 


Experimental Study on 

Supersonic Mixing Using 

Clover Nozzle 

Z. A Samitha, College of 

Engineering, 

Thiruvananthapuram, 

India 

1130 



of Igniter Jet Flow in 

Step Combustor 

Session 121-AD-5 Supersonic and Hypersonic Aircraft Design Crystal 3 

Chaired by: G. FUENTES, USB University, Bogata, Colombia 

0800 


The Development of 

Waveriders from an 

Axisymmetric Flowfield 

F. Ferguson, North 

Carolina A&T State 

University, Greensboro, 

NC 

0830 


What Price Supersonic 

Speed? - An Applied 

Market Research Case 

Study - Part 2 

B. Chudoba, The 



0900 


Experimental 

Investigation of Active 

Flow Control of a 


Ingesting Serpentine 

Inlet Diffuser 

N. Harrison, Techsburg, 

Inc., Blacksburg, VA 

0900 


What Price Supersonic 

Speed? - A Design 

Anatomy of Supersonic 

Transportation - Part 1 

B. Chudoba, The 



0930 


Application of Harmonic 

Balance Technique to 

the Compressible Euler 

and Navier- Stokes 

Equations 

G. Welch, U.S. Army 



0930 


Towards Developing a 

WaveRider Based Low 

Hypersonic Research 

Vehicle 

N. Saqib, Beihang 


China (prc) 

1000 


Measurements of the 

Flame Response to 

Harmonic Excitation in a 

Swirl Combustor 

S. Thumuluru, Georgia 


Atlanta, GA 

1000 


Propulsion/Airframe 

Integration and 

Optimization on a 

Supersonic Business Jet 

D. Rodriguez, Desktop 

Aeronautics, Inc., Palo 

Alto, CA 

1030 


Characteristics of the 

Swirling Flow in a 

Multipoint LDI 

Combustor 

Y. Fu, University of 


OH 




University of 



Session 122-AFM-5 Reusable Launch Vehicle, Reentry, and Aero-Assist Technologies N-11 

Chaired by: T. ZIEN, Naval Surface Warfare Center, Dahlgren, VA, and S. DUNN, Lockheed Martin Corporation, Sunnyvale, CA 

0800 


Supersonic Flight 

Testing of Unmanned 

Experimental Airplane 

for Next- generation SST 

S. Machida, Japan 


Agency, Mitaka, Japan 

0830 


Aerodynamic Control on 

a Lunar Return Capsule 

using Trim- Flaps 

B. Andersen, Utah State 



Session 123-AFM-6 Unmanned Aerial Vehicles N-3 


0900 


Autonomous 

Maneuvering Entry 

Guidance with Ground- 

Track Control 

M. Sudhir, Indian 


Kanpur, India 

0930 


Aerodynamic and 

Propulsion Assisted 

Maneuvering for Orbital 

Transfer Vehicles 

P. Jolley, Utah State 


1000 


Flight Control System of 

the NEXST- 1 

Experimental Vehicle for 

Supersonic 

Aerodynamic 

Measurement 

A. Tada, Japan 


Agency, Chofu City, 

Japan 

1030 


Autonomous 

Aerobraking Using 

Thermal Response 

Surface Analysis 

Chaired by: C. FROST, NASA Ames Research Center, Moffett Field, CA, and L. LIJEWSKI, U.S. Air Force Research Laboratory, Eglin AFB, FL 

0800 


External Pitching 

Moment (EPM) Due to 

Turbine Engine Exhaust 

Impingement on Rocket 

Assisted Take Off 

(RATO) Bottle 

J. Martel, Air Force 

SEEK EAGLE Office 

Computational 

Aeromechanic Team, 

Eglin AFB, FL 

0830 


Neutral Energy Cycles 

for a Vehicle in 

Sinusoidal and 

Turbulent Vertical Gusts 

P. Lissaman, Da Vinci 

Ventures, Santa Fe, NM 

0900 


Non- Linear High 

Bandwidth Control of 

UAVs for Autonomous 

Mission Capability 

F. Holzapfel, 

Industrieanlagen 

Betriebsgesellschaft 

mbH, Ottobrunn, 

Germany 

0930 


A Dynamical Model and 

Controller for the Silent 

Aircraft: The Effect of 

Maneuvering on Noise 

S. Thomas, Cambridge 

University Engineering 

Department, 


1000 


Guidance and Control of 

an Autonomous Soaring 

Vehicle with Flight Test 

Results 

M. Allen, NASA Dryden 

Flight Research Center, 

Edwards, CA 

J. Prince, NASA Langley 


Hampton, VA 

1030 


Landing Longitudinal 

Control System Design 

for a Fixed Wing UAV 

F. Hsiao, Institute of 


Astronautics, National 

Cheng Kung University, 

Tainan, Taiwan (roc) 

1100 


A Wind Tunnel 

Investigation of Shuttle 

Wing Damage Using a 

High Fidelity Wing 

B. Black, U.S. Air Force 


Springs, CO 

Session 124-AMT-3 Spectroscopic and Scattering Techniques Shasta 2 

Chaired by: P. DANEHY, NASA Langley Research Center, Hampton, VA, and A. MIELKE, NASA Glenn Research Center, Cleveland, OH 

0800 



Combined CARS and 

Interferometric Rayleigh 

Scattering System 

S. Tedder, College of 

William and Mary, 

Williamsburg, VA 

0830 


CARS Thermometry in a 

2- m- Diameter 

Methanol Pool Fire 

S. Kearney, Sandia 



0900 



Resonance Enhanced 

Raman NO Imaging Cell 

S. Zaidi, Princeton 

University , Princeton, NJ 

0930 


Trace Gas Detection 

Utilizing Optical 

Spectroscopy of 

Microresonant Cavities 

Q. Ma, Rutgers 


NJ 

1000 


Utilization of Laser- 

Based Measurements 

and Numerical 

Simulation for Analysis 

of Thermal- Fluid 

Systems Using Dynamic 

Data Driven Application 

Systems 

1030 


Microwave Scattering 

from a Plasma Produced 

by REMPI in Argon 

Z. Zhang, Princeton 

University, Princeton, NJ

Q. Ma, Rutgers 


NJ 



Chaired by: T. WAYMAN, Gulfstream Aerospace Corporation, Savannah, GA 

0800 0830 0900 0930 1000 1030 1100 

Chaired by: F. COTON, University of Glasgow, Glasgow, Great Britain 

Chaired by: C. STEFFEN, NASA Glenn Research Center, Cleveland, OH, and R. TRAMEL, Digital Fusion, Huntsville, AL 

0800 0830 0900 0930 1000 1030 1100


Session 125-APA-13 Aerodynamic Flow Control II Carson 1 


0800 


Modeling and 

Experiment of Leading 

Edge Separation 

Control Using SDBD 

Plasma Actuators 

D. Orlov, United States 

Air Force Academy 

Space Physics and 

Atmospheric Research 

Center Department of 

Physics, Colorado 

Springs, CO 

0830 


Effectiveness of an 

Integrated Aerodynamic 

Wake and Structural 

Vibration Control 

System at Transonic 

Speeds 

B. Maines, Lockheed 


Company, Fort Worth, 

TX 


Session 126-APA-14 CEAS Conference Highlights N-9 


0900 



Control Over Swept 

Wings and Wings with 

Diamond Planform 

J. Rullan, Virginia 




Chaired by: F. COTON, University of Glasgow, Glasgow, Great Britain 

0930 


Dynamic Compensator 

for a Synthetic- Jet- Like 

Compression Driver 

Actuator in Closed- Loop 

Cavity Flow Control 

K. Kim, The Ohio State 


OH 

1000 


Initial Results of an 


Oscillating Fence 

Actuators on a 

Stationary and Pitch 

Oscillating Wing 

M. Saini, University of 


1030 


Effects of Forebody Slot 

Blowing on Vortex 

Breakdown and Load 

over a Delta Wing 

Y. Cui, National 


Sinagpore, Singapore 

1100 


Modification of the Flow 

Structure over a UAV 

Wing for Roll Control 

R. Nelson, University of 


Dame , IN 

Session 127-APA-15 CFD Methods/Applied CFD N-8 

Chaired by: C. STEFFEN, NASA Glenn Research Center, Cleveland, OH, and R. TRAMEL, Digital Fusion, Huntsville, AL 

0800 



Unsteady Multi- stage 


Simulations Using the 

Harmonic Balance 

Technique 

A. Gopinath, Stanford 


0830 


Increasing Order of 

Accuracy of Weighted 

Compact Non- Linear 

Scheme 

T. Nonomura, Dept. of 


Astronautics, The 



0900 


Computational and 

Experimental 


Nonslender Delta Wing 

R. Gordnier, Air Force 



OH 

0930 


Euler Solutions of Flow 

Around a Rectangular 

Wing with Square Tip 

S. Yang, University of 

California, Irvine, CA 

1000 



DLR- F6 Wing- Body 

Configuration Using the 

Edge Solver 

P. Eliasson, FOI, 

Swedish Defence 

Research Agency, 


1030 


Predicting Maximum Lift 

Coefficient for Twisted 

Wings Using 


Dynamics 

N. Alley, Utah State 


1100 


Numerical Study to 

Minimize Induced Drag 

by Boundary Layer 

Control 

J. Posada, West Virginia 

University, Morgantown, 

WV 



Chaired by: J. TSAO, Ohio Aerospace Institute, Cleveland, OH, and K. VENKATARAMANI, General Electric Aviation, Cincinnati, OH 

0800 0830 0900 0930 1000 1030


Session 128-ASE-9 Icing Physics Crystal 1 

Chaired by: J. TSAO, Ohio Aerospace Institute, Cleveland, OH, and K. VENKATARAMANI, General Electric Aviation, Cincinnati, OH 

0800 


Observations on the 

Growth of Roughness 

Elements into Icing 

Feathers 

M. Vargas, National 

Aeronautics and Space 

Administration Glenn 


Shaker Heights, OH 

0830 


Properties of Thin Water 

Films Driven by Air 

Through Surface 

Roughness 

G. Wang, Iowa State 



Session 129-ASE-10 Space Environments and Effects Program Products I Crystal 2 


0900 


A Simple Boundary- 

Layer Water Film Model 

for Aircraft Icing 

S. Otta, Iowa State 


0930 


Measurements of Water 

Droplet Movement in a 



J. Schmucker, Case 



OH 

Chaired by: D. FERGUSON and J. MINOW, NASA Marshall Space Flight Center, Huntsville, AL 

0800 


The NASA Space 

Environments and 

Effects Program (SEE): 

Over a Decade of 

Useful Products for 

Spacecraft Designers 

and Operators 




0830 


Updated Version of the 

NASA SEE Program 

Spacecraft 

Contamination and 

Materials Outgassing 

Effect Knowledgebase 

B. Wood, Bob Wood 

Aerospace Consulting 

Services, Inc., 

Tullahoma, TN 

0900 


Lunar e- Library: A 

Research Tool Focused 

On The Lunar 

Environment 

T. McMahan, Qualis 

Corporation, Huntsville, 

AL 

0930 


Genesis Radiation 

Environment 

J. Minow, NASA 



1000 



Large Droplet Splashing 

and Breakup 

C. Tan, Wichita State 


1000 


Status of the L2 and 

Lunar Charged Particle 

Environment Models 




1030 


Dynamics of Icing in 

Aircraft Engines 

K. Venkataramani, GE 

Aviation, Cincinnati, OH 

Session 130-FD-23 CFD Higher Order Methods II Crystal 4 

Chaired by: J. EKATERINARIS, Institute of Applied and Computational Mathematics of FORTH, Heraklion Crete, Greece, and L. FUCHS, Lund University, Lund, Sweden 

0800 


Efficient Implementation 

of High- Order Spectral 

Volume Method for 

Multidimensional 

Conservation Laws on 


R. Harris, Iowa State 


0830 


Synchronization of 

Weighted Essentially 

Non- Oscillatory Methods 

E. Taylor, Princeton 


0900 


RANS Solutions Using 

High Order 


Methods 

N. Nguyen, 



Cambridge, MA 

0930 


Turbulent Flow 

Prediction Using a High- 

Accuracy CAA Code 

D. Gonzalez, Naval 


Indian Head, MD



Chaired by: C. FUREBY, FOI - Swedish Defence Research Agency, Stockholm, Sweden, and C. GAHARAN, Lockheed Martin, Palmdale, CA 

0800 0830 0900 0930 1000 1030 1100 1130 

Chaired by: A. VAKILI, University of Tennessee Space Institute, Tullahoma, TN, and D. YODER, NASA Glenn Research Center, Cleveland, OH 

0800 0830 0900 0930 1000 1030 

Chaired by: A. CUTLER, George Washington University, Hampton, VA, and A. SCRIBBEN, U.S. Air Force Research Laboratory, Wright-Patterson AFB, OH 

0800 0830 0900 0930 1000


Session 131-FD-24 CFD LES Modeling and Applications II N-6 

Chaired by: C. FUREBY, FOI - Swedish Defence Research Agency, Stockholm, Sweden, and C. GAHARAN, Lockheed Martin, Palmdale, CA 

0800 


Large Eddy Simulation 

of a turbulent flow past a 

pair of symmetric 

backward- facing steps: 

a sensitivity analysis. 

C. Duwig, Division of 

Fluid Mechanics, Lund 

University, Lund, 

Sweden 

0830 



of Flow Past a 3- D 

Bump 

M. Visbal, Air Force 



OH 


Session 132-FD-25 Jets and Mixing I Shasta 1 


0900 


Understanding 

Crashback in Marine 

Propellers Using an 

Unsteady Actuator Disk 

Model 

M. Vysohlid, University 

of Minnesota, 


0930 


Flow and Acoustics 

Simulations Based on 

LES and an Acoustic 

Analogy; an Application 

to Laryngeal Airflow 

M. Mihaescu, University 


OH 

1000 


Implicit LES of 

Compressible Turbulent 

Flow 

K. Ishiko, Tohoku 


Japan 

1030 



of Compressible Flows 

in a Rectangular Duct 

Containing Cylindrical 

Rods - An Immersed 

Boundary Treatment 

W. Wang, Iowa State 


Chaired by: A. VAKILI, University of Tennessee Space Institute, Tullahoma, TN, and D. YODER, NASA Glenn Research Center, Cleveland, OH 

0800 


Application of Improved 

Gas/Liquid Methodology 

to High Speed Venting 

and Bulk- Flyout 

Problems 

G. Feldman, 

Combustion Research & 

Flow Technology, Inc. 

(CRAFT Tech), 

Huntsville, AL 

0830 


Multiphase CFD 

Analysis of Solid Rocket 

Motor Nozzle and 

Plume Flow 

F. Montanari, Fluent Inc., 

Lebanon, NH 

0900 



of Spray Dispersion and 

Mixing in a Swirl 

Stabilized Gas Turbine 

Burner 

M. Salewski, Division of 

Fluid Mechanics, Lund 

University, Lund, Sweden 

0930 


A RANS- LES Study of 

Swirling and Non- 

Swirling Jets 

M. Stoellinger, University 


WY 

1000 


Slot Film Cooling: LES 

and Heat Transfer 

Measurements 

C. Cruz, University of 


MD 

1030 


Hole Shape Comparison 

for Film Cooling Flows 

Using Large- Eddy 

Simulations 

P. Renze, Institute of 

Aerodynamics, RWTH 

Aachen University, 

Aachen, Germany 

1100 



of the Transient Flow 

Around a Submarine 

During Maneuver 

N. Alin, The Swedish 



Sweden 

1130 



of Breaking Waves 

Using Embedded- 

Boundary/Level- Set 

Method 

J. Yang, University of 

Iowa, Iowa City, IA 

Session 133-FD-26 Microfluidics Carson 2 

Chaired by: A. CUTLER, George Washington University, Hampton, VA, and A. SCRIBBEN, U.S. Air Force Research Laboratory, Wright-Patterson AFB, OH 

0800 


Compressible Gas Flow 

Inside a Two 

Dimensional Uniform 

Microchannel 

C. Cai, ZONA 

Technology Inc., 


0830 


Electroosmotic Flow in 

Micro/Nano Nozzles 

L. Chen, The Ohio State 


OH 

0900 


Prediction of Post- 

Contact Parameters of a 

Fluid Droplet Impact on 

a Smooth Surface 

B. Bathel, University of 

Iowa, Iowa City, IA 

0930 


Quantitative Scalar 

Measurements in Micro 

Jets and Flames 

R. Satti, University of 


1000 


Finite Volume 

Simulation of Gaseous 

Microflows Using 

Modified Boundary 

Conditions 

M. Darbandi, Sharif 

University of 




Chaired by: T. MCLAUGHLIN, U.S. Air Force Academy, Colorado Springs, CO 

0800 0830 0900 0930 1000 1030 1100 1130 

Chaired by: S. SCHNEIDER, Purdue University, West Lafayette, IN, and X. ZHONG, University of California, Los Angeles, Los Angeles, CA 

0800 0830 0900 0930 1000 1030 

Chaired by: J. HOCHSTEIN, University of Memphis, Memphis, TN, and D. CHATO, NASA Glenn Research Center, Cleveland, OH 

0800 0830 0900 0930 1000 1030 1100


Session 134-FD-27 / PDL-6 Plasma Actuators IV Crystal 5 

Chaired by: T. MCLAUGHLIN, U.S. Air Force Academy, Colorado Springs, CO 

0800 



Experimental Analysis 

of Plasma Flow Control 

over a Hump Model 

C. He, University of 


Dame, IN 

0830 



Plasma- Based Actuator 

Vortex Control of a 

Turbulent Cylinder Wake 

N. McMullin, Brigham 

Young University, 

Provo, UT 


Session 135-FD-28 Stability and Transition: High Speed Theory and Simulation Ruby 2 


0900 




Control in Low- 

Pressure Turbines 

Using Plasma Actuators 

Y. Suzen, North Dakota 

State University, Fargo, 

ND 

0930 



of Plasma- Based Flow 

Control for a 

Transitional Highly- 

Loaded Low- Pressure 

Turbine 

D. Rizzetta, Air Force 


Wright-Patterson Air 

Force Base, OH 

1000 


Bluff Body Flow 


Using Surface Dielectric 

Barrier Discharges 

H. Do, Stanford 


Chaired by: S. SCHNEIDER, Purdue University, West Lafayette, IN, and X. ZHONG, University of California, Los Angeles, Los Angeles, CA 

0800 


Is Retheta/Me a 

Meaningful Transition 

Criterion? 

E. Reshotko, Case 



OH 

0830 



Surface Roughness 

Effects on Receptivity of 

Hypersonic Flow Over 

Blunt Cones 

X. Zhong, University of 

California, Los Angeles, 

CA 

0900 


Receptivity of 


Layers Due to Acoustic 

Disturbances Over Blunt 

Cone 

K. Kara, Old Dominion 


0930 



Hypersonic Boundary- 

Layer Receptivity to Two 

and Three- Dimensional 

Wall Perturbations 

X. Wang, University of 

California, Los Angeles, 

CA 

1000 



Simulation of 

Supersonic Boundary- 

Layer Stabilization by 

Porous Coatings 

I. Egorov, Moscow 


Technology, Zhukovski, 

Russia 

1030 


Formation and Scaling 

of Plasma Synthetic Jet 

Actuators 

A. Santhanakrishnan, 

University of Kentucky, 

Lexington, KY 

1030 


Investigation of Oblique 

Breakdown in a 

Supersonic Boundary 

Layer at Mach 2 Using 

DNS 

C. Mayer, University of 

Arizona, Tucson, AZ 

1100 


Pulsed Discharge 

Actuators for 

Rectangular Wing 


A. Sidorenko, Institute of 

Theoretical and Applied 

Mechanics, Novosibirsk, 

Russia 

1130 


Effects of Pulsed- D.C. 


Actuators in a Separated 

Low Pressure Turbine 


J. Wall, Air Force 



OH 

Session 136-GPSE-6 Fluid and Thermal Management N-4 

Chaired by: J. HOCHSTEIN, University of Memphis, Memphis, TN, and D. CHATO, NASA Glenn Research Center, Cleveland, OH 

0800 


Cryogenic Propellant 

Stratification in a 

Rotating and Reduced 

Gravity Environment 

D. Kirk, Florida Institute 


Melbourne, FL 

0830 


A Three- Dimensional 

Computational 

Simulation of Magnetic 

Positive Positioning 

J. Marchetta, University 

of Memphis, Memphis, 

TN 

0900 


Three Dimensional 

Modeling of Jet- 

Induced Geysers in Low 

Gravity 

J. Marchetta, University 

of Memphis, Memphis, 

TN 

0930 


Validation of Tank Self- 

Pressurization Models in 

Normal Gravity 

S. Barsi, NASA Glenn 



1000 

1030 


Gas- Liquid Separation Development of 

Strategies in 

Consumable Transfer 

Microgravity Environment Systems for Sustainable 

Lunar Exploration 

B. Antar, The University 

of Tennessee Space 

Institute, Tullahoma, TN 

W. Notardonato, NASA 

Kennedy Space Center, 

, FL 

1100 


Cryogenic Technology 

Development for 

Exploration Missions 

D. Chato, NASA Glenn 

Research Center at 

Lewis Field, Cleveland, 

OH 



Chaired by: F. JACKSON, Aerospace Testing Alliance, Arnold AFB, TN, and J. HAAS, NASA Glenn Research Center, Cleveland, OH 

0800 0830 0900 0930 1000 1030 

Chaired by: P. BERAN, U.S. Air Force Research Laboratory, Wright-Patterson AFB, OH 

0800 0830 0900 0930 1000 1030 

Chaired by: W. JONES, NASA Langley Research Center, Hampton, VA, and B. SEKAR, University of Maryland, College Park, MD 

0800 0830 0900 0930 1000 1030 1100


Session 137-GT-5 Ground Test Facility Development and Testing Sierra 2 

Chaired by: F. JACKSON, Aerospace Testing Alliance, Arnold AFB, TN, and J. HAAS, NASA Glenn Research Center, Cleveland, OH 

0800 


Investigation of a Single- 

Jack Flexible 

Supersonic Nozzle 

K. Juhany, King 

Abdulaziz Univesity, 

Jeddah, Saudi Arabia 

0830 


Ultra Low Reynolds 

Number Airfoil Testing 

Facility 

M. Kerho, Rolling Hills 

Research Corporation, 

El Segundo, CA 


Session 138-MDO-4 Multidisciplinary Model Synthesis and Management Cascade 1 


0900 


Micro Wind Tunnel For 

Hazardous Chemical 

Fate Studies 

D. Weber, Edgewood 

Chemical and Biological 

Center (ECBC), 

Aberdeen Proving 

Ground, MD 

Chaired by: P. BERAN, U.S. Air Force Research Laboratory, Wright-Patterson AFB, OH 

0800 


Using CAD- Tools and 

Aerodynamic Codes in a 

Distributed Conceptual 

Design Framework 

K. Amadori, Linköping 

University, Linköping, 

Sweden 

0830 


Towards Web 

Standards- Based MDA 

and MDO 

R. Gloukhov, École 


Montréal, Montréal, 

Canada 

0900 


A Knowledge Based 

Engineering Approach to 

Support Automatic 

Generation of FE 

Models in Aircraft Design 

G. La Rocca, Delft 

University of 



0930 


Development of a Wind 

Tunnel Active Vibration 

Reduction System 

S. Balakrishna, ViGYAN, 

Inc., Hampton, VA 

0930 


A Knowledge Based 

Engineering approach to 

automation of 

conceptual design 

option selection 

E. Schut, Delft 

University of 



1000 


Application of the Two- 

Variable Correction 

Method to 

Measurements in an 

Open- Jet Test Section 

M. Mokry, NRC Institute 

for Aerospace 

Research, Ottawa, 

Canada 

1000 


Design of a Multi Agent 

Task Environment 

Framework to Support 

Multidisciplinary Design 

and Optimisation 

J. Berends, Delft 

University of 



1030 


Lunar Simulation in the 

Lunar Dust Adhesion 

Bell Jar 

J. Gaier, NASA Glenn 



Session 139-MVC-2 Geometry, Computational Environments and Post-Processing Carson 3 

Chaired by: W. JONES, NASA Langley Research Center, Hampton, VA, and B. SEKAR, University of Maryland, College Park, MD 

0800 


Rapid Geometry 

Creation for Computer- 

Aided Engineering 

Parametric Analyses 

V. Hawke, ELORET, 

Corp., Sunnyvale, CA 

0830 


Automatic Extraction of 

Configuration 

Approximations via 

Nested Geometric 

Refinements 

J. Dannenhoffer, 

Syracuse University, 

Syracuse, NY 

0900 


Post- Processing 

Techniques for Large- 

Scale Unsteady CFD 

Datasets 

E. Duque, Intelligent 

Light, Rutherford, NJ 

0930 


Mixing Time 

Visualization for 

Aerospace Applications 

M. Godo, JMSI dba 

Intelligent Light, 

Rutherford, NJ 

1000 


BPX - A Best Practices 

Expert System for CFD 

P. Stremel, Nielsen 

Engineering & 

Research, Inc., 

Mountain View, CA 

1030 


Wing- Nacelle Assembly 

Multidisciplinary 

Performance 

Optimization 

Y. Gisin, California 


University at San Luis 

Obispo, San Luis 

Obispo, CA 

1030 


Meshing Software 

Component Technology 


Integration 

P. Patel, MSC Software 

Corporation, Santa Ana, 

CA 

1100 


Integrating VR into 

Aerospace Simulation 

P. Panfilov, Moscow 

State Institute of 

Electronics and 

Mathematics, Moscow, 

Russia 



Chaired by: R. PITZ, Vanderbilt University, Nashville, TN, and P. PENKO, Ohio State University, Columbus, OH 

0800 0830 0900 0930 1000 

Chaired by: K. MCMANUS, General Electric Global Research Center, Niskayuna, NY, and C. BROPHY, Naval Postgraduate School, Monterey, CA 

0800 0900 0930 1000 1030 1100 

Chaired by: I. ADAMOVICH, Ohio State University, Columbus, OH 

0800 0830 0900 0930 1000 1030


Session 140-PC-10 Combustion Diagnostics and Processes Teton 2 

Chaired by: R. PITZ, Vanderbilt University, Nashville, TN, and P. PENKO, Ohio State University, Columbus, OH 

0800 



Supersonic Combustion 

Experiments for CFD 

Modeling 

A. Cutler, The George 

Washington University, 

Newport News, VA 

0830 


OH- PLIF 

Measurements of High- 

Pressure, Hydrogen 

Augmented Premixed 

Flames in the SimVal 

Combustor 

P. Strakey, National 

Energy Technology 

Laboratory, 

Morgantown, WV 


Session 141-PC-11 Pulse Detonation Engines I Teton 1 


0900 


A Small Angle 

Scattering Sensor 

System for the 


Combustion Generated 

Particulate 

D. Feikema, NASA 



0930 


Nonpremixed 

Combustion in an 

Accelerating Turning 

Transonic Flow 

Undergoing Transition 

F. Cheng, University of 

California, Irvine, Irvine, 

CA 

1000 


Catalytic Ignition and 

Upstream Reaction 

Propagation in Monolith 

Reactors 

P. Struk, NASA Glenn 



Chaired by: K. MCMANUS, General Electric Global Research Center, Niskayuna, NY, and C. BROPHY, Naval Postgraduate School, Monterey, CA 

0800 


A Review of PDE Development for Propulsion 

Applications 

A. Dean, General Electric Global Research 

Center, Niskayuna, NY 

0900 


Detonation Initiation on 

the Microsecond Time 

Scale: One and Two 

Dimensional Results 

Obtained from Adaptive 

Wavelet- Collocation 

Numerical Methods 

D. Kassoy, University of 


0930 


Stability of Idealized 

One- Reaction 

Detonations Revisited 

A. Tumin, The University 

of Arizona, Tucson, AZ 

1000 



a Detonation in a 

Coaxial Tube 

N. Tsuboi, Japan 



Japan 

1030 



on the Transverse Wave 

Property of Two- 

Dimensional H2- O2- 

Diluent Detonations 

D. Ando, Tokyo 

University of Science, 

Tokyo, Japan 

1100 



Shock- Induced 

Boundary Layers in Gaps 

K. Tanaki, Tokyo 


Tokyo, Japan 

Session 142-PDL-7 Plasma Science and Modeling N-7 

Chaired by: I. ADAMOVICH, Ohio State University, Columbus, OH 

0800 


Normal Microwave Glow 

Discharge in Transversal 

Magnetic Field 

S. Surzhikov, Russian 



0830 




Thermal Effects in 

Plasma/Turbulence 

Interaction 

S. Ghosh, University of 


MN 

0900 


Plasmadynamics of 

Glow Discharge in 

Hypersonic Internal 

Flows 

S. Surzhikov, Russian 

Academy of Science, 


0930 



Probe Measurements in 

a Non- equilibrium 

Plasma, Using a 

Detailed Model Electron 

Fluid 

J. Boerner, University of 


1000 




of Streamer Head 

Structure 

M. Nudnova, Moscow 


Technology, 


1030 


Non- Equilibrium 

Plasma Life Time 

Measurements and Flow 

Control 

N. Aleksandrov, Moscow 


Technology, 

Dolgoprudny, Russia



Chaired by: A. GUPTA, University of Maryland, College Park, MD, and K. ISAAC, University of Missouri-Rolla, Rolla, MO 

0800 0830 0900 

Chaired by: J. OLEJNICZAK, NASA Ames Research Center, Moffett Field, CA, and J. GREATHOUSE 

0800 0830 0900 0930 1000 

Chaired by: J. REUSTER, ERC Inc., Huntsville, AL, and H. KANNER, United Space Alliance, Cape Canaveral, FL 

0800 0830 0900 0930


Session 143-TES-5 Heat Transfer and Fluid Flow N-5 

Chaired by: A. GUPTA, University of Maryland, College Park, MD, and K. ISAAC, University of Missouri-Rolla, Rolla, MO 

0800 



Numerical Computations 

of Air Flow 

Characteristics in Air- 

Conditioned 

Multipurpose Hall 

A. Medhat, Housing, 

Buildings Research 

Centre (HBRC), Cairo, 

Egypt 

0830 


Indoor Air Quality and 

Fuzziness Evaluation of 

the Airflow Distributions 

in Enclosures 

R. Kameel, Consultant 

CEB, Cairo, Egypt 


Session 144-TP-11 Aerodynamics of the NASA Crew Exploration Vehicle Carson 4 


0900 


Power Transmission to a 

Micro Aerial Vehicle 

S. Komatsu, The 


Kashiwa, Japan 

Chaired by: J. OLEJNICZAK, NASA Ames Research Center, Moffett Field, CA, and J. GREATHOUSE 

0800 


Aerodynamic Testing in 

Support of Orion 

Spacecraft Development 

J. Ross, NASA Ames 



0830 


Testing of the Crew 

Exploration Vehicle In 

NASA Langley’s Unitary 

Plan Wind Tunnel 

K. Murphy, NASA 



0900 


Transonic/Supersonic 

Wind Tunnel Testing of 

the NASA Orion 

Command Module 

J. Bell, NASA Ames 


Field, CA 

0930 


Comparison of Crew 

Exploration Vehicle 

(CEV) Tests in Two 

Supersonic Wind 

Tunnels 

J. Bell, NASA Ames 



1000 


Proof of Concept for 

Testing Acceleration 

Compensation Force 

Balance Techniques in 

Short Duration Flows 

with a CEV Capsule 

G. Smolinski, 



Buffalo, NY 

Session 145-TP-12 Plumes Ruby 1 

Chaired by: J. REUSTER, ERC Inc., Huntsville, AL, and H. KANNER, United Space Alliance, Cape Canaveral, FL 

0800 

0830 


Progress in Modeling High Altitude Plume 

Missile Fuel Venting and Simulations for a Solid 

Plume Contrail Formation Propellant Rocket 

J. Chenoweth, 

Combustion Research 

and Flow Technology, 

Inc., Huntsville, AL 

J. Burt, University of 


0900 


Numerical Prediction of 

UV Radiation from Two- 

Phase Plumes at High 

Altitudes 

N. Gimelshein, ERC, 

Inc., Edwards AFB, CA 

0930 


CFD Simulation of Multi- 

Cycle Nanotube Laser- 

Ablation with Reduced 

Kinetics Model 

R. Greendyke, Air Force 


Kirtland AFB, NM



Chaired by: C. CARTER, U.S. Air Force Research Laboratory, Wright-Patterson AFB, OH, and V. SHIBKOV, Moscow State University, Moscow, Russia 

0800 0830 0900 0930 1000 1030 1100 

Chaired by: J. ZAYAS, Sandia National Laboratories, Albuquerque, NM, and A. WRIGHT, National Renewable Energy Laboratory, Golden, CO 

0830 0900 0930 1000 1030 1100 1130 

Chaired by: R. THOMAS, NASA Langley Research Center, Hampton, VA, and L. COLLOREC, Airbus, Blagnac, France 

1330 1400 1430 1500 1530


Session 147-WIG/PDL-5 Plasma-Assisted Combustion I Sierra 1 

Chaired by: C. CARTER, U.S. Air Force Research Laboratory, Wright-Patterson AFB, OH, and V. SHIBKOV, Moscow State University, Moscow, Russia 

0800 



Electrical Discharges in 

High Speed Reacting 

flows for the MHD 

Assisted Mixing and 

Combustion 

V. Bityurin, Institute of 

High Temperatures of 



Russia 

0830 


Ignition Enhancement 

Using Magnetic Gliding 

Arc 

T. Ombrello, Princeton 



Session 146-WE-5 Sensors and Controls McKinley 

Wednesday Afternoon / 10 January 2007 

0900 


Standing Sub- 

Compressed Detonation 

Wave in Hypersonic 

Combustible Mix Flow 

Sustained by 

Undercritical Microwave 

Discharge 

K. Khodataev, UFSF 

"Moscow Radiotechnical 

Institute of RAS", , 

Russia 

0930 


Effects of Corona, Spark 

and Surface Discharges 

on Ignition Delay and 

Deflagration- to- 

Detonation Times in 

Pulsed Detonation 

Engines 

K. Busby, National 

Research Council, 


OH 

1000 


Detonation Initiation by 

High- Voltage Pulsed 

Discharges 

V. Zhukov, Physics of 

Nonequilibrium Systems 

Lab, MIPT, 


Chaired by: J. ZAYAS, Sandia National Laboratories, Albuquerque, NM, and A. WRIGHT, National Renewable Energy Laboratory, Golden, CO 

0830 


Wind Tunnel Test on 

Wind Turbine Airfoil with 

Adaptive Trailing Edge 

Geometry 

C. Bak, Risoe National 

Laboratory, Roskilde, 

Denmark 

0900 


Computational 

Investigations of 

Deploying Load Control 

Microtabs on a Wind 

Turbine Airfoil 

R. Chow, University of 

California, Davis, CA 

0930 


Sensor Selection and 

State Estimation for 

Wind Turbine Controls 

J. Ehlers, Université du 

Québec a Rimouski, 

Rimouski, Canada 

1000 


Evaluation of NASA PZT 

Sensor/Actuator for 

Structural Health 

Monitoring of a Wind 

Turbine Blade 

J. Zayas, Sandia 



1030 


Designing and Testing 

Controls to Mitigate 

Tower Dynamic Loads in 

the Controls Advanced 

Research Turbine 

A. Wright, National 

Renewable Energy 

Laboratory, Golden, CO 

1030 


Calorimetric 

Measurements in Vortex 

Combustor 

A. Klimov, Institute for 

High Temperature RAS, 


1100 


Individual Blade Pitch 

for Active Yaw Control 

of a Horizontal- Axis 

Wind Turbine 

W. Zhao, The University 

of Auckland, Auckland, 

New Zealand 

1100 


Effect of nonequilibrium 

excitation of hydrogenoxygen 

mixture on 

ignition 

N. Popav, Moscow State 


Russia 

1130 


Adaptive Pitch Control of 

Variable- Speed Wind 

Turbines 

K. Johnson, Colorado 

School of Mines, 

Golden, CO 

1200 - Public Policy Luncheon Grand Theater 




1330 1400 1430 1500 1530


Session 148-AA-6 Aircraft Noise N-10 


1330 


Aero- Acoustics of 

Perforated Drag Plates 

for Quiet Transport 

Aircraft 

K. Sakaliyski, 



Cambridge, MA 

1400 


Engine Air- Brakes for 

Quiet Air Transport 

P. Shah, MIT Gas 

Turbine Laboratory, 

Cambridge, MA 


Session 149-ABP-9 / GT-9 Hypersonic Flight Vehicles and Ground Test Capabilities (Invited) Carson 3 


1430 


Support of Cost- Benefit 

Analyses of Noise 

Control Measures 

Around a Generic Airport 

S. Schwanke, 

Technische Universitaet 

Muenchen, Garching, 

Germany 

1500 



Simulations of Trailing- 

Edge Noise Generated 

by Turbulent Boundary- 

Layers 

R. Sandberg, University 

of Southampton, 

Southampton, Great 

Britain 

Chaired by: P. MONTGOMERY and J. SHEELEY, Aerospace Testing Alliance, Arnold AFB, TN 

1330 


Scramjet Engine Tests 

at Ramjet Engine Test 

Facility in JAXA- KSPC 

S. Tomioka, Japan 


Agency, Kakuda, Japan 

1400 


Aerothermodynamic and 

Scramjet Tests in High 

Enthalpy Shock Tunnel 

K. Itoh, Japan 


Agency, Kakuda, Japan 

1530 



Trailing Edge Noise in 

Low- Speed Wind Tunnel 

H. Ura, Japan 


Agency (JAXA), Osawa, 

Japan 

Session 150-AD-6 Subsonic Aircraft Design Crystal 3 

Chaired by: D. LEVY, Cessna Aircraft Company, Wichita, KS, and D. CARTER, U.S. Air Force Research Laboratory, Wright-Patterson AFB, OH 

1330 



Composite Bendable- 

Wing Micro Air Vehicle 

B. Johnson, University 


FL 

1400 


Propeller Slipstream 

Effects on Directional 

Aircraft Control with One 

Engine Inoperative 

M. Schroijen, Delft 

University of 



1430 


The 3X Propulsion 

Concept Applied to a 

Business Aircraft 

R. Slingerland, Delft 

University of 



1500 


"Smart Wings" as an 

Enabler of Future Highly 

Efficient Subsonic 

Aircraft and Technical 

Workforce Development 

J. McMasters, The 

Boeing Company, 

Seattle, WA 

1530 


High Altitude Long 

Endurance Air Vehicle 

Analysis of Alternatives 

and Technology 

Requirements 

Development 

C. Nickol, NASA Langley 


Hampton, VA 




Session 151-AFM-7 System ID, Parameter Estimation, Performance, and Stability and Control N-11 

Chaired by: E. MORELLI, NASA Langley Research Center, Hampton, VA, and A. DOGAN, University of Texas at Arlington, Arlington, TX 

1330 


Use of Bifurcation and 

Continuation Methods 

for Aircraft Trim and 

Stability Analysis - A 

State- of- the- Art 

A. Paranjape, Indian 


Bombay, Mumbai, India 

1400 


A New Optimal Control 

Allocation Method for 

Aircraft with Multiple 

Control Effectors 

L. Yang, Beihang 


China (prc) 


Session 152-AMT-4 Optical Diagnostics Carson 2 


1430 


Towards an Efficient 

Aircraft Stability and 

Control Analysis 

Capability Using High- 

Fidelity CFD 

S. Görtz, United States 

Air Force Academy, , CO 

1500 


Thrust and Drag Models 

for Performance 

Calculations for High- 

Speed Aircraft 

D. Bridges, Mississippi 

State University, , MS 

1530 



Minimum- Time- to- 

Climb Trajectories in 

Constrained Airspace 

R. Dai, Auburn 


Chaired by: D. FOURGUETTE, Michigan Aerospace Corporation, El Segundo, CA, and H. HU, Iowa State University, Ames, IA 

1330 


Planar Doppler 

Velocimetry System with 

Vibration Immunity 

T. Jenkins, MetroLaser, 

Irvine, CA 

1400 


Further Development of 

a High- Speed Three- 

Dimensional Flow 

Visualization System 

B. Thurow, Auburn 

University, , AL 

1430 


Surface Thermometry 

Using Laser Induced 

Phosphorescence 

Applied in the 

Afterburner of an 

Aircraft Turbofan Engine 

H. Seyfried, Lund 

University, Lund, 

Sweden 

1500 


Development of New 

Two- Component TSP 

for Cryogenic Testing 

Y. Egami, German 

Aerospace Center 

(DLR), Göttingen, 

Germany 

1530 


Fluorescence 


Hypersonic Flow Over 

Rapid Prototype Wind- 

Tunnel Models 

D. Alderfer, NASA 



1600 


Predicting the Safety of 

Airport Approaches from 

the Pilot's Perspective 

Based on Flight 

Mechanical 

Considerations 

M. Heiligers, Delft 

University of 



1600 


PIV Measurement of a 

High- Lift- Device Model 

in JAXA 6.5m × 5.5m 

Low- Speed Wind 

Tunnel 

H. Kato, Japan 



1630 


Predicting Near- Ground 

Vortex Lifetimes Using 

Weibull Density 

Functions 

L. Berk, U.S. DOT RITA 

John A. Volpe National 

Transportation Systems 

Center, Cambridge, MA 

1630 


PSP Measurement of a 

High- Lift- Device Model 

in JAXA 6.5m×5.5m 

Low- Speed Wind 

Tunnel 

K. Mitsuo, Japan 



1700 


Design of a Calibration 

Burner for Optical 

Combustion Diagnostics 

N. Jeyashekar, 

University of Mississippi, 

University, MS 

Session 153-APA-16 Aerodynamic Structural Interaction N-9 

Chaired by: J. AZEVEDO, Centro Técnico de Aeronáutica, São José dos Campos, Brazil 

1330 


Static Aeroelastic Model 

Validation of Membrane 

Micro Air Vehicle Wings 

B. Stanford, University 


FL 

1400 


Time Base 

Aeroservoelasticity Wind 

Tunnel Testing 

S. Therien, Bombardier 

Aerospace, Montreal, 

Canada 

1430 


Aeroelastic Behavior of 

Inflatable Wings: Wind 

Tunnel and Flight 

Testing 

A. Simpson, University 

of Kentucky, Lexington, 

KY 

1500 



Maneuvering Aircraft by 

Aerodynamic, Flight 

Mechanics and 

Structural Mechanics 

Coupling 

A. Schütte, German 


(DLR), Institute of 


1530 


Fast Prediction of Wing 

Rock Limit Cycle 

Oscillations Based on 


Dynamics 

K. Badcock, University 

of Liverpool, , Great 

Britain 

1600 


Analysis of Supersonic 

Aeroelastic Problem 

Based on Local Piston- 

Theory Method 

W. Zhang, Northwestern 



1630 


Aeroservoelastic 

Analysis for Supersonic 

and Hypersonic Missiles 

C. Zhang, Northwestern 


Xi' An, China (prc)

Technology, 





1330 1400 1430 1500 1530 1600 1630 

Chaired by: D. GROVE, Naval Air Systems Command, Patuxent River, MD 

1330 1400 1430 1500 1530 1600 1630 

Chaired by: D. MILLER, NASA Glenn Research Center, Cleveland, OH, and G. BOTURA, Goodrich, North Canton, OH 

1330 1400 1430 1500


Session 154-APA-17 Airfoil and Wing Aerodynamics I Carson 1 


1330 


Unsteady Aerodynamics 

of Free- to- Roll 

Nonslender Delta Wings 

A. McClain, University of 

Bath, Bath, Great Britain 

1400 


On the Return from 

Aerofoil Stall during 

Ramp- Down Pitching 

Motions 

W. Sheng, University of 

Glasgow, Glasgow, 

Great Britain 


Session 155-APA-18 Applied CFD N-8 


1430 



Numerical Investigations 

of Unsteady 

Aerodynamic 

Derivatives for Transport 

Aircraft Configurations 

A. Hübner, German 


(DLR), Institute of 


Technology, 


Chaired by: D. GROVE, Naval Air Systems Command, Patuxent River, MD 

1330 


Evaluation of Grid 

Convergence and 

Turbulence Model 

Constant Changes for 

the Airfoil Flow 

Simulation 

M. Rhee, Ames 



1400 


Turbulence Modeling 

and Supersonic Base 

Flows 

D. de Feo, Cranfield 

University, Cranfield, 

Great Britain 

1430 


Comparison of DES and 

URANS for Unsteady 

Vortical Flows over 

Delta Wings 

L. Schiavetta, University 

of Glasgow, Glasgow, 

Great Britain 

1500 


Icing Effect Study for 

Wing/Body and High- 

Lift Wing Configurations 

W. Sang, Northwestern 



1500 


Automatic Transition 

Prediction for RANS 

Computations Applied to 

a Generic High- Lift Wing 

T. Toulorge, Instituto 

Nacional de Técnica 

Aeroespacial (INTA), 

Torrejón De Ardoz 

(Madrid), Spain 

1530 


Computation of Induced 

Drag for 3D Wing with 

Volume Integral (Trefftz 

Plane) Technique 

S. Monsch, Clemson 

University, Clemson, SC 

1530 


Computational 

Simulation of Heavy 

Trucks 

K. Sreenivas, University 

of Tennessee at 

Chattanooga, 


1600 


Irreversibility 

Equivalence Ratio of 

Micropatterned Surface 

Roughness for Wall Slip 

Flow Control 

G. Naterer, University of 

Ontario Institute of 

Technology, Oshawa, 

Canada 

1600 


Computational 

Prediction of Forces and 

Moments for Transport 

Aircraft 

K. Sreenivas, University 

of Tennessee at 

Chattanooga, 


1630 


Effect of Surface 

Contamination on the 


Section of a Wind 

Turbine Blade 

M. Soltani, Sharif 

University of 


1630 


Simulation of the Flow 

Separation at the Wing- 

Body Junction with 

different Fairings 

C. Li, Northwestern 



Session 156-ASE-11 Experimental Icing Research Crystal 1 

Chaired by: D. MILLER, NASA Glenn Research Center, Cleveland, OH, and G. BOTURA, Goodrich, North Canton, OH 

1330 


Residual and Inter- cycle 

Ice for Lower- Speed 

Aircraft with Pneumatic 

Boots 

P. Pellicano, FAA 

Atlanta Certification 

Office, Atlanta, GA 

1400 


Spray Rig Design for 

Airborne Icing Tankers 

S. Wong, Wichita State 


1430 


Calibration of the CIRA 

IWT in the Low Speed 

Configuration 

M. Bellucci, C.I.R.A. 

S.c.p.A.- Centro Italiano 

Ricerche Aerospaziali, 

Via Maiorise Capue 

(CE), Italy 

1500 


Application of PDPA 

System with Different 

Optical Configuration to 

the IWT Calibration 

B. Esposito, C.I.R.A. 

S.c.p.A.- Centro Italiano 

Ricerche Aerospaziali, 

Via Maiorise Capue

(CE), Italy 



Chaired by: J. MINOW and D. FERGUSON, NASA Marshall Space Flight Center, Huntsville, AL 

1330 1400 1430 1500 1530 

Chaired by: W. VAUGHAN, University of Alabama in Huntsville, Huntsville, AL, and R. DECKER, NASA Marshall Space Flight Center, Huntsville, AL 

1330 1400 1430 1500 

Chaired by: C. LI, Aerojet, Folsom, CA 

1330 1400 1430 1500 1530 1600 1630 1700


Session 157-ASE-12 Space Environments and Effects Program Products II Crystal 2 

Chaired by: J. MINOW and D. FERGUSON, NASA Marshall Space Flight Center, Huntsville, AL 

1330 


Spacecraft Charging in 

Low Temperature 

Environments 




1400 


NASCAP- 2K 

Spacecraft- Plasma 

Environment 

Interactions Modeling: 

New Capabilities and 

Verification 

V. Davis, Science 

Applications 

International 

Corporation, San Diego, 

CA 


Session 158-ASE-13 Weather Concerns for Aerospace Operations Shasta 1 


1430 


Electric Propulsion 

Interactions Code 

(EPIC): Recent 

Enhancements and 

Goals for Future 

Capabilities 




1500 


Triggering Threshold 

Spacecraft Charging 

with Changes in Electron 

Emission from Materials 

J. Dennison, Utah State 


1530 


The Empirical Low 

Enegry Ion Flux Model 

for the Terrestrial 

Magnetospehere 

W. Blackwell, Marshall 

Space Flight Center 

Group, Huntsville, AL 

Chaired by: W. VAUGHAN, University of Alabama in Huntsville, Huntsville, AL, and R. DECKER, NASA Marshall Space Flight Center, Huntsville, AL 

1330 


Impact to Space Shuttle 

Trajectory on Day of 

Launch from change in 

Low Frequency Winds 

R. Decker, NASA 


Center, Huntsville , AL 

1400 


Uncertainty Analysis of 

Historical Hurricane Data 

L. Green, NASA Langley 


Hampton, VA 

1430 


Space Weather 

Nowcasting of 

Atmospheric Ionizing 

Radiation for Aviation 

Safety 

C. Mertens, NASA 



1500 


Next- Generation 

Spaceborne Precipitation 

Radar Instrument 

Concepts and 

Technologies 

E. Im, Jet Propulsion 

Laboratory, Pasadena, 

CA 

Session 159-CS-1 Computational Simulations and Computer Systems for Aerospace Applications Crystal 5 

Chaired by: C. LI, Aerojet, Folsom, CA 

1330 


foamDSMC: An Object 

Oriented Parallel 

DSMC Solver for 

Rarefied Flow 

Applications 



1400 


Timings of an 

Unstructured- Grid CFD 

Code on Common 

Hardware Platforms 

and Compilers 

F. Camelli, George 

Mason University, 

Fairfax, VA 

1430 


Performance 

Characteristics of an 

Unstructured CFD 

Solver on PC- Clusters 

M. Sillén, Saab 

Aerospace, Linkoping, 

Sweden 

1500 


Parallelization and 

Performance 


Bombardier Multiblock 

Structured Navier- 

Stokes Solver on IBM 

Eserver Cluster 1600 

K. Sermeus, 

Bombardier Aerospace, 

Montreal, Canada 

1530 


Performance Evaluation 

of Cache Optimized 

CFD Codes Applied to 

Complex Flow 

Applications 

S. Gupta, University of 


1600 


Single Processor 


OVERFLOW 

T. Hauser, Utah State 


1630 


JUSTGrid A Pure Java 

HPCC Grid Architecture for 

Multi- Physics Solvers 

Performance and efficiency 

results from various Java 

solvers. 

T. Ludewig, University of 

Applied Sciences 

Braunschweig/Wolfenbüttel, 

Wolfenbüttel, Germany 

1700 


Anywhere – Anytime: 

Enhancing Battlespace 

Vertical Mobility 

C. Ryerson, U.S. Army 

Corps of Engineers, 

Hanover, NH



Chaired by: K. SQUIRES, Arizona State University, Tempe, AZ, and A. CAIN, Innovative Technology Applications Company, LLC, Chesterfield, MO 

1330 1400 1430 1500 1530 

Chaired by: K. ZAMAN, NASA Glenn Research Center, Cleveland, OH, and P. ORKWIS, University of Cincinnati, Cincinnati, OH 

1330 1400 1430 1500 1530 1600 1630 

Chaired by: V. BURNLEY, U.S. Air Force Research Laboratory, Wright-Patterson AFB, OH, and G. POWER, Aerospace Testing Alliance, Arnold AFB, TN 

1330 1400 1430 1500 1530 1600 1630 1700


Session 160-FD-29 CFD Hybrid RANS/LES Methods and Application N-6 

Chaired by: K. SQUIRES, Arizona State University, Tempe, AZ, and A. CAIN, Innovative Technology Applications Company, LLC, Chesterfield, MO 

1330 


Grid Sensitivity of 

Detached Eddy 

Simulation of a Mach 16 

Re- Entry Configuration 


of Technology, Bombay, 

India 

1400 


Integrated RANS/LES 

Computations of an 

Entire Gas Turbine Jet 

Engine 

G. Medic, Stanford 



Session 161-FD-30 Flow Control Applications Carson 4 


1430 


Large- eddy simulation 

of flow over a swept 

wing with approximate 

near- wall modeling 

N. Li, Imperial College, 

London, Great Britain 

1500 



Sidewall Effects on the 

Acoustic Field in 

Transonic Cavity 

Z. Li, University of 


OH 

1530 


Effect of Reynolds 

Number on Detached 

Eddy Simulation of 

Hypersonic Base Flows 


of Technology Bombay, 

Bombay, India 

Chaired by: K. ZAMAN, NASA Glenn Research Center, Cleveland, OH, and P. ORKWIS, University of Cincinnati, Cincinnati, OH 

1330 


Active Flow Control for 

High Lift Airfoils: 

Separation Versus 

Circulation Control 

H. Nagib, Illinois Institute 

of Technology, Chicago, 

IL 

1400 


Active Flow Control for 

High Lift Airfoils: 

Dynamic Flap Actuation 

J. Kiedaisch, Illinois 


Chicago, IL 

1430 


Control of the Spanwise 

Distribution of 

Circulation on NACA 

0012 and Flat Plate 

Wings 

D. Williams, Illinois 


Chicago, IL 

1500 


Vortex Topology of Wing 

Tip Blowing 

P. Margaris, University 

of Bath, Bath, Great 

Britain 

1530 


Experiments on 

Interaction of a Jet with 

a Trailing Vortex 

P. Margaris, University 

of Bath, Bath, Great 

Britain 

1600 


Reduced Order Model 

for Feedback Control of 

Cavity Flow - the Effects 

of Control Input 

Separation 

E. Caraballo, The Ohio 


Columbus, OH 

Session 162-FD-31 General CFD Crystal 4 

Chaired by: V. BURNLEY, U.S. Air Force Research Laboratory, Wright-Patterson AFB, OH, and G. POWER, Aerospace Testing Alliance, Arnold AFB, TN 

1330 


Quantifying Non- 

Equilibrium using 

Entropy Generation 

R. Carr, Air Force 



OH 

1400 


A General Framework 

for the Optimal Control 

of Unsteady Flows with 

Applications 

M. Rumpfkeil, University 

of Toronto Institute for 

Aerospace Studies, 

Toronto, Canada 

1430 


Optimal Design of 

Airfoils Using NURBS 

and a Continuous 

Sensitivity Equation 

Method 

J. Cori, Ecole 


Montréal, Montréal, 

Canada 

1500 


Utilizing CFD- Based 

Exergy Calculations in 

the Design/Optimization 

of a Complete Aircraft 

System 

K. Alabi, Thaerocomp 

Technical Corp., Stony 

Brook, NY 

1530 


RANS Simulation of a 

Synthetic Jet in 

Quiescent Air 

S. Park, Konkuk 


Korea 

1600 


Toward a General 

Solution Verification 

Method for Complex 

PDE Problem with 

Hands Off Coding 

M. Garbey, University of 

Houston, Houston, TX 

1630 



Linear Stability Analysis 

of Cavity Flows 

G. Brès, California 


Pasadena, CA 

1630 


Comparison of Body- 

Fitted, Embedded and 

Immersed 3- D Euler 

Predictions for Blast 

Loads on Columns 

R. Lohner, George 


Fairfax, VA 

1700 


Effects of Random 

Roughness and 

Scattering of Shock 

Waves 

G. Lin, Brown 


RI 




Session 163-FD-32 High Speed Flows and Boundary Layer Interactions N-3 

Chaired by: T. HORVATH and S. BERRY, NASA Langley Research Center, Hampton, VA 

1330 


Analysis of Shock 

Motion in STBLI Induced 

by a Compression 

Ramp Configuration 

Using DNS Data 

M. Wu, Princeton 


1400 


Planar Measurements of 


Layers with Curvature 

Driven Pressure 

Gradients 

I. Ekoto, Texas A&M 


Station, TX 


Session 164-FD-33 Instruction in Experimental Methods N-5 


1430 


Coherent Structures in 

DNS of Turbulent 

Boundary Layers at 

Mach 3 

M. Ringuette, Princeton 


1500 


Experimental Studies of 

Transitional Boundary 

Layer Shock Wave 

Interactions 

Z. Murphree, University 

of Texas at Austin, 

Austin, TX 

1530 


An Experimental Study 

of Unsteady Separated 

Shock Wave / Boundary 

Layer Interactions 

P. Bruce, University of 


Great Britain 

Chaired by: D. BRIDGES, Mississippi State University, Mississippi State, MS, and J. JACOB, Oklahoma State University, Stillwater, OK 

1600 


Effects of Upstream 

Coherent Structures on 

Low- Frequency Motion 

of Shock- Induced 

Turbulent Separation 

B. Ganapathisubramani, 


Austin, Austin, TX 

1630 


Response of a 

Supersonic Turbulent 

Boundary Layer to 

Periodic Surface 

Roughness 

I. Ekoto, Texas A&M 


Station, TX 

Session 165-GPSE-7 Gravity Dependent / Low-Gravity Processes and Technologies N-4 

Chaired by: R. SCHLAGHECK, NASA Marshall Space Flight Center, Huntsville, AL, and S. TSE, Rutgers University, Piscataway, NJ 

1330 


Formation and Growth 

of Micro and Macro 

Bubbles on Copper- 

Graphite Composite 

Surfaces 

D. Chao, NASA Glenn 

Research Center at 

Lewis Field, Cleveland, 

OH 

1400 


Fluid Merging Viscosity 

Measurement (FMVM) 

Experiment on the 

International Space 

Station 

B. Antar, The University 

of Tennessee Space 


1430 


Microgravity Phase 

Separation Near the 

Critical Point in 

Attractive Colloids 

P. Lu, Harvard 


MA 

1500 


Lunar Dust 

Characterization for 

Exploration Life Support 

Systems 

J. Agui, NASA Glenn 



1530 


Electron Beam Freeform 

Fabrication in the Space 

Environment 

R. Hafley, NASA 



1600 


Direction- Controlled 

Artificial Gravity for 

Space Exploration 

B. Benjamin, University 

of Kansas, Lawrence, KS 

1630 


Droplet Entrainment in 

Two- Phase Flow Under 

Reduced Gravity 

V. Naoumov, University 

of Tennessee, Knoxville, 

TN 



Chaired by: K. KONTIS, University of Manchester, Manchester, Great Britain, and R. KAMYKOWSKI, Arnold Engineering Development Center, Arnold AFB, TN 

1330 1400 1430


Session 166-GT-6 Arc Jet and High Enthalpy Testing and Technology Whitney 

Chaired by: K. KONTIS, University of Manchester, Manchester, Great Britain, and R. KAMYKOWSKI, Arnold Engineering Development Center, Arnold AFB, TN 

1330 



Fabrication of 6- cm Arc 

Jet Segments 

T. Risch, Sierra Lobo, 

Inc., Moffett Field, CA 

1400 


Photogrammetric 

Recession Measurement 

of Ablative Materials 

During Arc- Jet Testing 

E. Schairer, NASA Ames 


Field, CA 


Session 167-GT-7 Measurements of Wind Tunnel Model Deformation (Invited) Sierra 2 


1430 


High Enthalpy Flow 

Generation by 2 kW 

Class CW Laser 

M. Matsui, University of 

Tokyo, Tokyo, Japan 

Chaired by: J. KEGELMAN, NASA Langley Research Center, Hampton, VA, and T. BRESSLER, The Boeing Company, Seattle, WA 

1330 


Angle Measurement 

System (AMS) for 

Establishing Model Pitch 

and Roll Zero, and 

Performing Single Axis 

Angle Comparisons 

B. Crawford, NASA 



1400 


Videogrammetric Model 

Deformation 

Measurement Technique 

for Wind Tunnel 

Applications 

D. Barrows, NASA 



Session 168-IS-3 Optimal Design Using Intelligent System Technologies Cascade 1 

Chaired by: E. ATKINS, University of Maryland, Glenwood, MD 

1330 


General Regression 

Neural Network 

Application to Axial 

Compressor 

Performance Map 

K. Ghorbanian, Sharif 

University of 


1400 


Neural Network 

Estimation of Transient 

Flow Fields Using 

Double Proper 

Orthogonal 

Decomposition 

Y. Shin, U.S. Air Force 


Springs, CO 

1430 


A Photogrammetric 

System for Model 

Attitude Measurement in 

Hypersonce Wind 

Tunnels 

T. Jones, NASA Langley 


Hampton, VA 

1430 


Multi- Objective Robust 

Design Optimisation 

Using Hierarchical 

Asynchronous Parallel 

Asynchronous 

Evolutionary Algorithms 

D. Lee, University of 

Sydney, Sydney, 

Australia 



Chaired by: J. AUSTIN, University of Illinois at Urbana-Champaign, Urbana, IL, and J. SINIBALDI, Naval Postgraduate School, Monterey, CA 

1330 1400 1430 1500 1530 1600 1630 1700 

Chaired by: O. HAIDN, DLR, German Aerospace Research Center, Lampoldshausen, Germany, and C. CARTER, U.S. Air Force Research Laboratory, Wright-Patterson AFB, OH 

1330 1400 1430 1500 1530 

Chaired by: D. CARROLL, CU Aerospace, Champaign, IL 

1330 1400 1430 1500 1530


Session 169-PC-12 Pulse Detonation Engines II Teton 1 

Chaired by: J. AUSTIN, University of Illinois at Urbana-Champaign, Urbana, IL, and J. SINIBALDI, Naval Postgraduate School, Monterey, CA 

1330 



H2/Air Detonation Wave 

Around Obstacles Using 

Detailed Reaction 

Models 

F. Togashi, George 


Fairfax, VA 

1400 


Wave Structure and 

Unsteadiness of 

Stabilized Oblique 

Detonation Waves 

Around Hypersonic 

Projectile 

Y. Daimon, Japan 



Japan 


Session 170-PC-13 Sprays and Spray Combustion Teton 2 


1430 


Deflagration- to- 

Detonation Transition in 

Premixed H2- Air in 

Channels with Obstacles 

V. Gamezo, U.S. Naval 



1500 


Investigations of Two- 

Phase Detonations for 

Performance 

Estimations of a Pulsed 


V. Tangirala, GE Global 


Niskayuna, NY 

1530 


Effect of a Rifle- Type 

Obstacle on DDT in PDE 

H. Adachi, Aoyama 


Kanagawa, Japan 

1600 


A CFD Analysis of 

Wave Interaction in a 

Multi- Tube PDE 

M. Hishida, Nagoya 


Japan 

1630 


Aerodynamic Effect of 

Turbine Blade Geometry 

in Pulse Detonation 

Combustor 

A. Nango, Tokyo 


Tokyo, Japan 

Chaired by: O. HAIDN, DLR, German Aerospace Research Center, Lampoldshausen, Germany, and C. CARTER, U.S. Air Force Research Laboratory, Wright-Patterson AFB, OH 

1330 


Cavitation in an Orifice 

Flow 

S. Dabiri, University of 

California, Irvine , Irvine, 

CA 

1400 


Measurements of Spray 

Characteristics in 

Preheated Crossflowing 

Air 

Y. Gopala, Georgia 


Atlanta, GA 

1430 


A Model of Organic Gel 

Spray Diffusion Flames 

with Droplet Drag 

J. Greenberg, 

Technion—Israel 


Haifa, Israel 

1500 

1530 


Effect of Droplet Initial Imaging Flashing 

Diameter on Droplet Injection of Acetone at 

Vaporization Regimes Jet Engine Augmentor 

for Kerosene Fuel Droplet Conditions 

Q. Khan, Korea 

Advanced Institute of 

Science and 

Technology, Daejeon, 

South Korea 

K. Lucas, Purdue 


Lafayette, IN 

1700 



Numerical Simulation for 

Detonation Waves 

Using WENO Schemes 

H. Dou, National 



Session 171-PDL-8 Laser Applications N-7 

Chaired by: D. CARROLL, CU Aerospace, Champaign, IL 

1330 


Laser- Ablative 

Propulsion Using 

Polyacetal at Low 

Ambient Pressures 

A. Sasoh, Nagoya 


Japan 

1400 


Spectroscopic 

Lineshape Prediction 

Using 3- D, Time 

Dependent Simulation of 

Chemical Oxygen- 

Iodine Laser (COIL) 

Flowfields 

T. Madden, U.S. Air 


Laboratory, Kirtland 

1430 


Impulse Generation by 

Nd:YAG Laser Ablation 

of Aluminum 

K. Mori, Nagoya 


Japan 

1500 


LSD Termination 

Conditions and Post- 

Shock Electron Density 

A. Fukui, University of 

Tokyo, Chiba, Japan 

1530 


Continuous Wave 

Operation of a Non- 

Self- Sustained Electric 

Disharge Pumped 

Owygen- Iodine Laser 

A. Hicks, Ohio State 


OH

AFB, NM 



Chaired by: J. EILER, Stellar Solutions, Littleton, CO 

1330 1400 1430 

Chaired by: P. DEBARBER, Ball Aerospace and Technologies Corporation, Boulder, CO, and G. ADAMOVSKY, NASA Glenn Research Center, Cleveland, OH 

1330 1400 1430 1500 1530 1600 1630 

Chaired by: T. ABE, Japan Aerospace Exploration Agency, Sagamihara, Japan, and G. BEITEL, Aerospace Testing Alliance, Arnold AFB, TN 

1330 1400 1430 1500 1530 1600


Session 172-SE-2 Systems Engineering II Shasta 2 

Chaired by: J. EILER, Stellar Solutions, Littleton, CO 

1330 


Systems Engineering, 

System Architecting, and 

Enterprise Architecting - 

- What's the Difference? 

C. Farrell, The Tauri 

Group, Alexandria, VA 

1400 


Concept Selection Using 

an Interactive 

Reconfigurable Matrix of 

Alternatives (IRMA) 

W. Engler, Georgia 


Atlanta, GA 


Session 173-SS-1 Sensor Technology for Aerospace Systems Cascade 2 


1430 


Cross Cutting Structural 

Design for Exploration 

Systems 

E. Semmes, NASA 


Center, Marshall Space 

Flight Center, AL 

Chaired by: P. DEBARBER, Ball Aerospace and Technologies Corporation, Boulder, CO, and G. ADAMOVSKY, NASA Glenn Research Center, Cleveland, OH 

1330 


Radio Frequency Mass 

Gauging of Propellants 

G. Zimmerli, NASA 



1400 


Investigation of a Micro- 

Optical Species 

Concentration Sensor 

Based on Whispering 

Galley Mode Resonators 

N. Das, Polytechnic 


1430 


Reentry Air Data for a 

Sub- orbital Spacecraft 

Based on X- 34 Design 

J. Ellsworth, Utah State 


1500 


Effects of Optical 

Artifacts in a Laser- 

Based Spacecraft 

Navigation Sensor 

J. LeCroy, The Boeing 

Company, Huntsville, AL 

1530 


Guidance and Control of 

Artillery Projectiles with 

Magnetic Sensors 

P. Rouger, Giat 

Industries, Bourges, 

France 

Session 174-TP-13 Heating in Re-Entry Flows Ruby 2 

Chaired by: T. ABE, Japan Aerospace Exploration Agency, Sagamihara, Japan, and G. BEITEL, Aerospace Testing Alliance, Arnold AFB, TN 

1330 


Aerothermodynamic 

Environments Definition 

for the Mars Science 

Laboratory Entry Capsule 

K. Edquist, NASA 



1400 


Analysis of the Forebody 

Aeroheating 

Environment during 

Genesis Sample Return 

Capsule Reentry 

C. Tang, ELORET 

Corporation, Moffett 

Field, CA 

1430 


Turbulent Aeroheating 

Testing of Mars Science 

Laboratory Entry Vehicle 

in Perfect- Gas Nitrogen 

B. Hollis, NASA Langley 


Hampton, VA 

1500 


Application of the 

Transpiration Cooling 

Method for Reentry 

Vehicles 

H. Otsu, Shizuoka 

University, Hamamatsu, 

Japan 

1530 


Ablation Modeling of 

Electro- Magnetic 

Launched Projectile for 

Access to Space 

R. Gosse, University of 


MN 

1600 


Three Model IMM- EKF 

for Tracking Targets 

Executing Evasive 

Maneuvers 

V. Naidu, National 

Aerospace Laboratories, 

Bangalore, India 

1600 


Catalytic Effects on Non- 

Equilibrium 

Aerothermodynamics of 

a Reentry Vehicle 

A. Viviani, Seconda 

Università di Napoli, 

Dipartimento di 

Ingegneria Aerospaziale 

e Meccanica, Aversa, 

Italy 

1630 


Target Interception by 

UAVs in a Sensor 

Network 

T. Lewis, University of 


Arlington, TX 




Session 175-TP-14 Thermal Management in Aerospace Systems Ruby 1 

Chaired by: C. GERHART, U.S. Air Force Research Laboratory, Albuquerque, NM, and M. PAUKEN, Jet Propulsion Laboratory, California Institute of Technology, Pasadena, CA 

1330 


Unrealised Thermal 

Control Issues Important 

for Future Spacecraft 

Thermal Control 

Systems Design 

A. Delil, Advanced 

Aerospace Thermal 

Control Systems, 

Emmeloord, The 


1400 


Start- Up Behavior of a 

Miniature Loop Heat 

Pipe with Multiple 

Evaporators and 

Multiple Condensers 

H. Nagano, Japan 



Japan 


Session 176-WE-6 Inflow: Loads and Resource McKinley 


1430 


Probabilistic Thermal 

Analysis During Mars 

Reconnaissance Orbiter 

Aerobraking 

J. Dec, NASA Langley 


Hampton, VA 

Chaired by: P. VEERS, Sandia National Laboratories, Albuquerque, NM 

1330 


Statistical Extrapolation 

Methods for Estimating 

Wind Turbine Extreme 

Loads 

P. Ragan, University of 

Texas, Austin, TX 

1400 


Uncertainty Analysis in 

Wind Resource 

Assessment and Wind 

Energy Production 

Estimation 

M. Lackner, University of 

Massachusetts, 

Amherst, MA 

1430 


Estimation of Wind 

Turbine Fatigue Loads 

using Time- Domain and 

Spectral Methods 

P. Ragan, University of 


TX 

1500 


Experimental 


Passive 

Deployable/Stowable 

Radiator 

H. Nagano, Japan 


Agency , Sagamihara, 

Japan 

1500 


Tall Tower Wind Shear 

Observations in the 

Stable Nocturnal 


K. Walter, Texas Tech 

University, Lubbock, TX 

1530 


Performance Predictions 

of a Blade Twist 

Actuator System 

N. Caldwell, University 


OH 

1530 


Addressing Ground 

Clutter Corruption of 

Sodar Measurements 

A. Rogers, University of 

Massachusetts, 

Amherst, MA 

1600 


Thermal Control of an 

Airborne Electronics Bay 

M. Engelhardt, BAE 

Systems, Greenlawn, NY 

1600 


On the Joint Wind- 

Wave Environment and 

its Influence on Offshore 

Wind Turbine Loads 

P. Agarwal, University of 

Texas, Austin, TX 

1630 


Thermal Analysis on 

Cryogenic Liquid 

Hydrogen Tank on an 

Unmanned Aerial 

Vehicle System 

X. Wang, NASA Glenn 



Session 177-WIG/PDL-6 Aerodynamics II: Energy Deposition for Flow Control Sierra 1 

Chaired by: Y. KOLESNICHENKO, Russian Academy of Sciences, Moscow, Russia, and D. KNIGHT, Rutgers University, Piscataway, NJ 

1330 


Optimization of Laser- 

Pulse- Controlled MW 

Energy Deposition 

Y. Kolesnichenko, 



Russia 

1400 


Control of the Shear 

Layer Above a 

Supersonic Cavity Using 


E. Lazar, University of 

Illinois 


Urbana, IL 

1430 



Influence on Supersonic 

Flow Over Axisymmetric 

Bodies 

A. Zheltovodov, 

Khristianovich Institute 

of Theoretical and 

Applied Mechanics, 

Novosibirsk, Russia 

1500 


Gas- Dynamic Effects 

Around the Body Under 

Energy Deposition in 

Supersonic Flow 

V. Lashkov, St. 

Petersburg State 

University, St. 

Petersburg, Russia 

1530 


Transformations of 

Front Separation 

Regions Controlled by 

Upstream Energy 

Deposition 

P. Georgievsky, 

Moscow State 


Russia 

1600 


Hot Filaments for 

Plasma Aerodynamic 

Applications 

N. Ardelyan, Moscow 



1630 



Localized Arc Filament 

Plasma Actuator in 


Layer 

H. Yan, Wright State 


1700 



Drag Reduction for 

Supersonic Blunt Body 

by Pulse Energy 

Deposition 

T. Shinichi, Tohoku 


Japan



The Public Policy Committee will continue its Excellence in Aerospace Discourse Series at the Aerospace Sciences Meeting with a discussion on the next generation of aerospace professionals. 

The International Space Station and the Next Decade of Human Space Exploration


1730 - Wright Brothers Lectureship in Aeronautics Reno Room 

Thursday Morning / 11 January 2007 

0800 - 1200 AIAA Workforce Panel Discussion Carson 3 

The Public Policy Committee will continue its Excellence in Aerospace Discourse Series at the Aerospace Sciences Meeting with a discussion on the next generation of aerospace professionals. 

Speakers include: 

Dr. Paul Nielsen 

President-Elect for AIAA and Director of Carnegie Mellon University’s Software Engineering Institute 

Dr. Lisa Porter 

Associate Administrator for Aeronautics at NASA 

Dr. Analissa Wiegle 

Assistant Professor of Aeronautics & Astronautics and Engineering Systems at MIT 

Dr. Robert Walters 

President-Elect for the Aerospace Department Chairman's Association and Chairman of Virginia Tech's Department of Aerospace and Ocean Engineering. 


0800 - 1200 ISS As A National Laboratory Carson 4 

The International Space Station and the Next Decade of Human Space Exploration 

This forum will present plans for the operation and utilization of the ISS in the upcoming decade, in the period beyond the retirement of the Space Shuttle and before the launch of human missions to the moon. 

During this era, the ISS will be the only platform available for human space habitation, and will be essential for the engineering and biomedical research and the technology development required by proposed 

lunar and Mars mission concepts. Plans for utilization of the ISS as a National Laboratory available to the broader community are also under development. Topics to be discussed by the forum will include: 

Post-shuttle transportation plans for ISS operations; exploration research and technology plans for the ISS; the ISS National Laboratory concept. 

Briefings from senior NASA managers will include: 

Commercial Orbital Transportation Services Valin Thorn, Deputy Manager, NASA Commercial Crew and Cargo Program 

ISS International Partner Relationships Dan Jacobs, Manager, ISS International Programs 

NASA Operations Research Plans Mark Uhran, Assistant Associate Administrator for ISS 

ISS Post-Assembly Accommodations & Resources Rod Jones, Manager, ISS Payloads Office 

NASA Human Research Plans Neal Pellis, Associate Director, NASA Human Research Program 

ISS Research Accomplishments Julie Robinson, ISS Program Scientist (acting) 

Following these briefings will be a panel discussion of “Prospects for the Next Decade on the ISS” 

Participants Include: 

Bill Gerstenmaier, Associate Administrator for Space Operations 

Jeff Bingham, US Senate Science and Space Subcommittee Staff Peter Banks, Principal, Red Planet Capital, Inc. 

Franklin Chang-Diaz, CEO, Ad Astra Rocket Company

Alan Lindenmoyer, Manager, NASA Commercial Crew and Cargo Program 



Chaired by: R. SCHMIT, U.S. Air Force Research Laboratory, Wright-Patterson AFB, OH, and J. YU, Goodrich, San Diego, CA 

0800 0830 0900 0930 1000 1030 

Chaired by: V. TANGIRALA, General Electric Global Research Center, Niskayuna, NY, and J. DEBONIS, NASA Glenn Research Center, Cleveland, OH 

0800 0830 0900 0930 1000 1030 

Chaired by: G. CROUSE, Auburn University, Auburn University, AL 

0800 0830 0900 0930 1000 1030


Session 178-AA-7 Cavity, Rotor, and Sonic Boom Noise N-10 

Chaired by: R. SCHMIT, U.S. Air Force Research Laboratory, Wright-Patterson AFB, OH, and J. YU, Goodrich, San Diego, CA 

0800 


Features of the 

Interaction Between 

Twin- Cavities with 

Varying Separation 

P. Panickar, Illinois 


Chicago, IL 

0830 


Control of Pressure 

Loads in Complex Cavity 


L. Ukeiley, University of 

Florida, Shalimar, FL 


Session 179-ABP-10 PDE and Unsteady Flows III Cascade 2 


0900 


Flow Control for 

Enhanced Store 

Separation 

J. Shipman, Combustion 

Research and Flow 


Pipersville, PA, PA 

0930 


A Validation Study of the 

PSU- WOPWOP Rotor 

Noise Prediction Code 

J. Shirey, Pennsylvania 



1000 


Noise Benefits of Rotor 

Trailing Edge Blowing 

for a Model Turbofan 

R. Woodward, NASA 



1030 


Parametric Study and 

Effect of Nose- Piece 

Attachment on Sonic 

Boom Mitigation 

Chaired by: V. TANGIRALA, General Electric Global Research Center, Niskayuna, NY, and J. DEBONIS, NASA Glenn Research Center, Cleveland, OH 

0800 


Performance of an Axial 

Flow Turbine Driven by 

Multiple Pulse 

Detonation Combustors 



OH 

0830 


Performance on a Pulse 


Under Subsonic and 

Supersonic Flight 

Conditions 

V. Tangirala, GE Global 


Niskayuna, NY 

0900 


Application of a Pulsed 

Detonation Engine for 

Electric Power 

Generation 

P. Panicker, University 


Arlington, TX 

Session 180-AD-7 VTOL, ESTOL, STOL and Morphing Aircraft Crystal 3 

Chaired by: G. CROUSE, Auburn University, Auburn University, AL 

0800 


An Integrated Approach 

to Rotorcraft Conceptual 

Design 

J. Hirsh, The Boeing 

Company, Philadelphia, 

PA 

0830 


Ornicopter Yaw Control: 

Testing a Single Rotor 

Helicopter Without 

Reaction Torque 

D. van Gerwen, Delft 

University of 



0930 


Wave- Rotor Transition 

Duct Experiment 

G. Welch, U.S. Army 



0900 

0930 


Conceptual Design of an Analysis of Take- Off 

Unmanned Gyronplane and Landing of 

for an Endurance Mission Powered- Lift Aircraft 

G. Crouse, Auburn 


P. Bobbitt, Eagle 

Aeronautics, Inc., 

Hampton, VA 

1000 


Experimental Results of 

Performance Tests on a 

Four- Port Wave Rotor 

J. Wilson, ASRC 

Aerospace, Cleveland, 

OH 

1000 



Piezoelectric Servo Flap 

Actuator 

S. Duquette, University 

of Hartford, West 

Hartford, CT 



, 

1030 


Internal Flow Dynamics 

in a Valveless 

Airbreathing Pulse 

Detonation Combustor 

Facility 

F. Ma, Pennsylvania 



1030 


Morphing Aircraft 

Technology Survey 

A. Rodriguez, Florida 

International University, 

Miami, FL


Session 181-AMT-5 / SS-2 Sensors and Techniques for Aerodynamics Research and Applications Shasta 2 

Chaired by: A. DRAKE, Northrop Grumman Corporation, El Segundo, CA, and V. OTUGEN, Polytechnic University, Brooklyn, NY 

0800 


Color Moiré 

Interferometry for Shear 

Stress Sensor 

Application 

T. Chen, Taitech, Inc., 

Beavercreek, OH 

0830 



Whispering Gallery 

Mode Resonator- Based 

Micro- Optical Force 

Sensor 

T. Ioppolo, Polytechnic 



Session 182-APA-19 Airfoil and Wing Aerodynamics II Carson 1 


0900 


Measurements of Non- 

Steady Pressure and 

Skin Friction Fields on 

Wall Mounted Cube 

Using Surface Stress 

Sensitive Film 

S. Fonov, Innovative 

Scientific Solutions Inc., 

Dayton, OH 

Chaired by: R. VERMELAND, Lockheed Martin Aeronautics Company, Palmdale, CA 

0800 


Predicting Maximum Lift 

Coefficient for Twisted 

Wings Using Lifting- 

Line Theory 

W. Phillips, Utah State 


0830 


Far Field Effects of 

Wing Wakes 

D. Nixon, Retired, Los 

Altos, CA 

0900 


Numerical simulation of 

an airfoil at low 

Reynolds number 

J. Hall, University of 

Colorado at Boulder, 

Boulder, CO 

0930 


Design and 


Diamond- based 

Nanowire Temperature 

Sensor 

A. Zaitsev, College of 

Staten Island, Staten 

Island, NY 

0930 


Examining a Family of 

Movable Wing Tip 

Strakes Involving 

Varying Leading Edge 

Forms and Sweep 

Angles 

V. Nikolic, Minnesota 


Mankato, MN 

1000 


Measuring Aeroelastic 

Wing Characteristics 

Using Microsensor 

Systems (MEMS) 

J. Dhainaut, 

Embry-Riddle 

Aeronautical University, 

Daytona Beach, FL 

1000 


Aerodynamic 


Slender Delta Wing with 

Low Dorsal Fin 

X. Meng, Northwestern 



1030 


Effects of Turbulators on 

Airfoil at Low Reynolds 

Number in Turbulent 

Flow 

J. Delnero, Universidad 

Nacional de La Plata, La 

Plata, Argentina 

1100 


One- Shot Pseudo- 

Time Method for 

Aerodynamic Shape 

Optimization Using the 

Navier- Stokes Equations 

S. Hazra, University of 

Trier, Trier, Germany 

Session 183-APA-20 Rotorcraft N-9 

Chaired by: R. STRAWN, NASA Ames Research Center, Moffett Field, CA, and T. EGOLF, Sikorsky Aircraft, Glastonbury, CT 

0800 


Time- Varying Objective 

Functions for Optimum 

Shape Design via 

Control Theory 

C. Tatossian, McGill 


Canada 

0830 


CFD Analysis of Rotor- 

Fuselage Interactional 

Aerodynamics 

R. Steijl, University of 

Liverpool, Liverpool, 

Great Britain 

0900 


A Lifting Surface Study 

of Helicopter 

Aerodynamics in Ground 

Effect 

D. Pulla, Ohio State 


OH 

0930 


Application of a 

Turbulent Viscous 

Cartesian- Grid 

Methodology to 

Flowfields with Rotor- 

Fuselage Interaction 

J. Lee, Samsung Heavy 

Industry, Taejeon, South 

Korea 

1000 


Prediction of HART II 

Rotor BVI Loading and 

Wake System Using 

CFD/CSD Loose 

Coupling 

J. Lim, NASA Ames 


Moffett Field, CA




0800 0830 0900 0930 1000 1030 

Chaired by: J. WISE and D. DONATELLI, U.S. Air Force Research Laboratory, Hanscom AFB, MA 

0800 0830 0900 0930 1000 

Chaired by: T. MICHAL, The Boeing Company, Wentzville, MO 

0800 0830 0900 0930 1000 1030 1100


Session 184-APA-21 Vortical Flows N-8 


0800 


Throttling a Laval 

Nozzle by a Vortex: An 

Analytical Theory 

T. van Holten, Delft 

University of 



0830 


Influence of Initial 

Vorticity Distribution on 

Axisymmetric Vortex 

Breakdown and 

Reconnection 

L. Young, NASA Ames 




Session 185-ASE-14 Earth and Planetary Science Crystal 2 


0900 


Dynamics of the Vortex 

Core During Pitching of 

a High- Sweep Delta 

Wing 

M. Jones, Nagoya 


Japan 

0930 


Extraction of Vortical 

Flow Features in a 


simulation 

S. Zhang, Ansys/Fluent, 

Lebanon, NH 

Chaired by: J. WISE and D. DONATELLI, U.S. Air Force Research Laboratory, Hanscom AFB, MA 

0800 


Anomaly Trends for 

Robotic Missions to 

Mars: Mars Exploration 

Rovers Surface 

Operations 

N. Green, Jet Propulsion 

Laboratory, Pasadena, 

CA 

0830 


SABER at Five Years: A 

Phenomenal Instrument 

for Studying Sun- Earth 

Connections 

M. Mlynczak, NASA 



1000 


A Parametric Study of 

Incompressible 

Axisymmetric Internal 

Cavity Flows 

J. Smith, University of 

Tennessee Space 


1030 


Shock Waves, Vorticity 

and Vorticity Shocks 

D. Nixon, Retired, Los 

Altos, CA 

Session 186-FD-34 CFD Grid Methods Crystal 1 

Chaired by: T. MICHAL, The Boeing Company, Wentzville, MO 

0800 


Comparison of Body- 

Fitted, Embedded and 

Immersed Solutions of 

Low Reynolds- Number 

Incompressible Flows 

R. Lohner, George 


Fairfax, VA 

0830 


Functional Outputs Error 

Based Mesh Adaptation 

L. Remaki, McGill 


Canada 

0900 


Outline of JEM/SMILES, 

Japanese Earth 

Observation System 

Aboard ISS 

M. Takayanagi, Japan 


Agency, Tsukuba-City, 

Japan 

0900 


Unstructured Grid 

Generation Method and 

Flow Solutions for Two- 

Dimensional, High- Lift 

Aerofoil Configurations 

S. Marques, University 

of Salford, Salford, 

Great Britain 

0930 


Remote Sensing of 

Neutral Particles in 

Upper Atmosphere 

Using Artificial Ion Beam 

Y. Sakamoto, Japan 



Japan 

0930 


Combination of Body- 

Fitted and Embedded 

Grids for External 

Vehicle Aerodynamics 

R. Tilch, ESI Group, 

Rungis, France 

1000 


Earth Albedo 

Measurements from 

Earthshine 

Observations: Past, 

Present and Future 

E. Palle, Big Bear Solar 

Observatory, Big Bear 

City, CA 

1000 


Deformation and 

Regeneration of the 

Computational Grid for 

CFD with Moving 

Boundaries 

M. Liefvendahl, Swedish 



Sweden 

1030 


Turbulent Flow 

Simulation around 

Complex Geometries 

with Cartesian Grid 

Method 

T. Kamatsuchi, Honda 

R&D Co, Ltd., Wako, 

Japan 

1100 


Developing a Robust 

Ordering- Based 

Unstructured Moving 

Grid Strategy 

N. Fouladi, Sharif 

University of 




Chaired by: R. ANTHONY, U.S. Air Force Research Laboratory, Wright-Patterson AFB, OH, and D. BRIDGES, Mississippi State University, Mississippi State, MS 

0800 0830 0900 0930 1000 

Chaired by: R. JOSLIN, Office of Naval Research, Arlington, VA, and A. VAKILI, University of Tennessee Space Institute, Tullahoma, TN 

0800 0830 0900 0930 1000 

Chaired by: D. RIZZETTA, U.S. Air Force Research Laboratory, Wright-Patterson AFB, OH, and L. SU, Johns Hopkins University, Baltimore, MD 

0800 0830 0900 0930 1000 1030 1100 1130


Session 187-FD-35 Experimental Techniques in Fluid Dynamics Crystal 5 

Chaired by: R. ANTHONY, U.S. Air Force Research Laboratory, Wright-Patterson AFB, OH, and D. BRIDGES, Mississippi State University, Mississippi State, MS 

0800 


A Robust Procedure for 

the Analysis of Non- 

Evenly Spaced Velocity 

Time- Series Data 

K. Garwick, U.S. Air 


Laboratory, 


OH 

0830 


A 24" Access Laser- 

Doppler Velocimeter for 

Simultaneous Three- 

Velocity- Component 

Measurements 






Session 188-FD-36 Flow Control Modeling and Simulation Carson 2 


0900 


Experimental Studies in 

Hypersonic Flows for 

Facility and Code 

Validation 

M. Holden, 



Buffalo, NY 

0930 


Investigation of the 


Coherent Structures in a 


Layer with Tomographic- 

PIV 

G. Elsinga, Delft 

University of 



1000 


Calculating Surface 

Pressure Fluctuations 

from PIV Data Using 

Poisson's Equation 

N. Murray, Harding 

University, Searcy, AR 

Chaired by: R. JOSLIN, Office of Naval Research, Arlington, VA, and A. VAKILI, University of Tennessee Space Institute, Tullahoma, TN 

0800 



of Synthetic Jet Based 

Separation Control in a 

Canonical Separated 

Flow 

R. Kotapati, Mechanical 

& Aerospace 

Engineering, The 

George Washington 

University, Washington, 

DC 

0830 


Flow Past a Cylinder 

with a Flapping Element 

Attached to Its End 

W. Liou, Western 


Kalamazoo, MI 

0900 


Three- Dimension 

Numerical Simulation on 

Controlled Stability of a 

Planar Supersonic Free 

Shear Layer 

F. Guan, China 

Academy of Aerospace 

Aerodynamics, Beijing, 

China (prc) 

0930 


DNS of Riblets to 

Control the Growth of 

Turbulent Spots 

J. Strand, University of 


TX 

1000 


Low Order Galerkin 

Models for the Actuated 

Flow Around 2- D Airfoils 

G. Tadmor, 

Northeastern University, 

Boston, MA 

Session 189-FD-37 Jets and Mixing II Crystal 4 

Chaired by: D. RIZZETTA, U.S. Air Force Research Laboratory, Wright-Patterson AFB, OH, and L. SU, Johns Hopkins University, Baltimore, MD 

0800 


Experimental 

Investigations of Mixing 

in Turbulent Jets with 

Buoyancy 

D. Helmer, Johns 

Hopkins University, 

Baltimore, MD 

0830 



Variable Density Jets in 

Cross Flow 

R. Lakhamraju, 

University of Cincinnati, 

Cincinnati, OH 

0900 


The Effect of Crossflow 

on Vortex Rings 

R. Sau, University of 


MN 

0930 


Scale Relations and 

Spatial Spectra in a 

Differentially Diffusing Jet 

C. Brownell, Johns 

Hopkins University, 

Baltimore, MD 

1000 


Velocity Field of Isolated 

Turbulent Puffs 

E. Ghaem-Maghami, 

Worcester Polytechnic 

Institute, Worcester, MA 

1030 


Numerical Study of Jet 

Plume Instability from 

an Overexpanded 

Nozzle 

Q. Xiao, National 



1100 


Flow Separation Studies 

in a Subscale Truncated 

Ideal Contour Nozzle 

S. Verma, National 

Aerospace Laboratories, 

Bangalore, India 

1130 


Experimental 


Rectangular Confined 

Laminar Jet Subjected 

to Downstream Acoustic 

Excitation 

Y. Gopala, Georgia 

Institute of Technology,

Atlanta, GA 



Chaired by: C. TILMANN, U.S. Air Force Research Laboratory, Wright-Patterson AFB, OH, and J. SEIDEL, U.S. Air Force Academy, Colorado Springs, CO 

0800 0830 0900 

Chaired by: J. LAFFERTY, Arnold Engineering Development Center, Silver Spring, MD, and G. EITELBERG, German-Dutch Wind Tunnels, Marknesse, The Netherlands, and D. WISHART, Pratt and Whitney, 

0800 0830 0900 0930 

Chaired by: G. PARKER, U.S. Air Force Research Laboratory, Wright-Patterson AFB, OH 

0800 0830 0900 0930 1000 1030 1100


Session 190-FD-38 Wake Flows II Whitney 

Chaired by: C. TILMANN, U.S. Air Force Research Laboratory, Wright-Patterson AFB, OH, and J. SEIDEL, U.S. Air Force Academy, Colorado Springs, CO 

0800 


Flow- field and Acoustic 

Interaction behind a Wall 

Mounted Cylinder 

S. Murugappan, 



0830 


Flow- field and Acoustic 

Interaction behind a 

Ramped Step 

S. Murugappan, 




Session 191-GT-8 Hypersonic Ground Test Facilities and Testing Sierra 2 


0900 



Turbulent Wall- Function 

Based Viscous 

Cartesian- Grid 

Methodology 

J. Lee, Samsung Heavy 

Industries, Taejeon, 

South Korea 

Chaired by: J. LAFFERTY, Arnold Engineering Development Center, Silver Spring, MD, and G. EITELBERG, German-Dutch Wind Tunnels, Marknesse, The Netherlands, and D. WISHART, Pratt and Whitney, 

Stuart, FL 

0800 


Design and 


Hypervelocity Expansion 

Tube Facility 

A. Dufrene, University of 

Illinois at 


Urbana, IL 

0830 



Transition in an 

Expansion Tube at a 

Low Enthalpy Operating 

Condition 

M. McGilvray, University 

of Queensland, 

Brisbane, Australia 

0900 


Measuring Nitric Oxide 

Freestream Velocity 

Using Quantum 

Cascade Lasers at 

CUBRC 

R. Parker, Stratonics 

Inc., Laguna Hills, CA 

Session 192-MDO-5 Optimization Algorithms and Techniques Cascade 1 

Chaired by: G. PARKER, U.S. Air Force Research Laboratory, Wright-Patterson AFB, OH 

0800 


Characterizing Global 

Behavior of 

Approximation Functions 

J. Bourgeois, Ecole 



Canada 

0830 


A Methodology for 

Capability- Focused 

Technology Evaluation 

of Systems of Systems 

P. Biltgen, Georgia 


Atlanta, GA 

0900 


A Technique for 

Interactive Probabilistic 

Multiple Attribute 

Decision Making 

P. Biltgen, Georgia 


Atlanta, GA 

0930 


Aerothermal 

Measurement 

Improvements using 

Coaxial Thermocouples 

at AEDC Hypervelocity 

Wind Tunnel No. 9 

J. Coblish, AEDC White 

Oak, Silver Spring, MD 

0930 


An Interactive 

Visualization 

Environment for 

Decision Making in 

Aircraft Engine 

Preliminary Design 

A. Marsaw, Georgia 


Atlanta, GA 

1000 


Requirements 

Decomposition for 

Compact 

Multidimensional 

Visualization 

N. Borer, Charles Stark 

Draper Laboratory, Inc., 

Cambridge, MA 

1030 


Development of a Noise 

Allocation Planning Tool 

S. Heblij, Delft University 

of Technology, Delft, 


1100 


Uncertainty Propagation 

Through an Aircraft 

System Aeroelastic 

Model 

N. Lindsley, U.S. Air 


Laboratory, 


OH 



Chaired by: B. CHEHROUDI, U.S. Air Force Research Laboratory, Lancaster, CA, and T. NGUYEN, Aerojet, Sacramento, CA 

0800 0830 0900 0930 1000 1030 

Chaired by: H. IM, University of Michigan, Ann Arbor, MI, and V. SANKARAN, Sandia National Laboratories, Livermore, CA 

0800 0830 0900 0930 1000 

Chaired by: D. LEVIN, Pennsylvania State University, Univeristy Park, PA 

0800 0830 0900 0930 1000 1030 1100


Session 193-PC-14 Liquid Jet Injection Processes Teton 1 

Chaired by: B. CHEHROUDI, U.S. Air Force Research Laboratory, Lancaster, CA, and T. NGUYEN, Aerojet, Sacramento, CA 

0800 


A Novel Technique for 

Measurements of the 

Intact Liquid Jet Core in 

a Coaxial Airblast 

Atomizer 

G. Charalampous, 

Imperial College 

London, London, Great 

Britain 

0830 


PIV and LDV 

Measurements for 

Liquid Jets in Crossflow 

O. Elshamy, University 


OH 


Session 194-PC-15 Turbulent Flames: Measurements and Modeling Teton 2 


0900 


Breakup of a Round 

Liquid Jet in a Low 

Weber Number Cross 

Flow 

O. Pulat, University of 


0930 


Excited Liquid Jets in 

Subsonic Crossflow 

O. Elshamy, University 


OH 

1000 


Liquid Jets Injected 

Transversely into a 

Shear Layer 

S. Tambe, University of 


OH 

Chaired by: H. IM, University of Michigan, Ann Arbor, MI, and V. SANKARAN, Sandia National Laboratories, Livermore, CA 

0800 


Application of 

Simultaneous Stereo 

PIV and Double Pulsed 

Acetone PLIF to Study 

Turbulent Premixed 

Flames 

S. Filatyev, Purdue 


Lafayette, IN 

0830 


Emissions and 

Acoustics 

Measurements in a Low- 

Swirl Burner 

D. Sequera, University 

of Alabama, Tuscaloosa, 

AL 

0900 


Pulsed Microwave 

Enhancement of 

Laminar and Turbulent 

Hydrocarbon Flames 

E. Stockman, Princeton 


0930 


Flame Surface Fractal 

Characteristics in 

Premixed Turbulent 

Combustion at Medium 

to High Turbulence 

Intensities 

E. Cintosun, University 

of Toronto, Institute for 



1000 


Flame Surface Density 

of Turbulent Premixed 

Flames at Medium to 

High Turbulence 

Intensities 

S. Puranam, University 

of Toronto, Institute for 



1030 


Secondary Breakup of 

Aerated Liquid Jets in 

Subsonic Crossflow 

B. Miller, Oklahoma 



Session 195-PDL-9 Plasmas: Combustion and Kinetics N-11 

Chaired by: D. LEVIN, Pennsylvania State University, Univeristy Park, PA 

0800 


Effect of the Post - 

Pulse Discharge 

Channel’s Fast 

Turbulent Expansion on 

the Gas Flow 

S. Leonov, OIVTRAN, 


0830 


Studies of Chemi- 

Ionization and 

Chemiluminescence in 

Supersonice Flows of 

Combustion Products 

S. Keshav, Ohio State 


OH 

0900 


Plasmachemical 

Processes in Plasma- 

Assisted Combustion 

E. Mintoussov, Moscow 


Technology, 


0930 


Plasma Kinetics in Inert 

Gas Filled Thermionic 

Devices 

B. Pivtorak, Princeton 


1000 


Non Equilibrium and 

Elemental Demixing 

Analysis of C02 Flows 

Inside ICPs 

J. Thoemel, von Karman 

Institute, Rhode 

ST.Genese, Belgium 

1030 


Spatially and Temporally 

Resolved Atomic 

Oxygen Measurements 

in Short Pulse 

Discharges by Two 

Photon Laser Induced 

Fluorescence 

M. Uddi, Ohio State 


OH 

1100 


Ultrasensitive Absorption 

Measurements of 

Metastable Species: 

Pressure Broadening of 

the b1?g - a1?g (1,0) 

Band in Oxygen using 

off- axis integratedcavity 

output 

spectroscopy 

J. Gallagher, Air Force

Institute of Technology, , 

OH 



0800 0830 0900 0930 1000 

Chaired by: D. BERG, Sandia National Laboratories, Albuquerque, NM 

0800 0830 0900 0930 1000 1030 1100 

Chaired by: S. SCHNEIDER, NASA Glenn Research Center, Cleveland, OH, and S. BOBASHEV, Ioffe Physico-Technical Institute, Saint Petersburg, Russia 

0800 0830 0900 0930 1000


Session 196-SOS-1 Space Operations and Support Ruby 2 

0800 


Comprehensive Shuttle 

Foam Debris Reduction 

Strategies 

E. Semmes, NASA 


Center, Marshall Space 

Flight Center, AL 

0830 


Effects of Launch 

Environment on OAA 

“White Room”: Modeling, 

Analysis and Redesign 

G. Finger, Reynolds, 

Smith and Hills, Inc., 

Merritt Island, FL 


Session 197-WE-7 VAWTs and Innovative Concepts McKinley 


0900 


Unconventional Thermal 

Propellant Gauging 

System 

B. Yendler, Lockheed 

Martin Corporation, 

Sunnyvale, CA 

Chaired by: D. BERG, Sandia National Laboratories, Albuquerque, NM 

0800 


2D PIV Visualization of 

Dynamic Stall on a 

Vertical Axis Wind 

Turbine 

C. Simao Ferreira, Delft 

University of 



0830 


2D CFD Simulation of 

Dynamic Stall on a 

Vertical Axis Wind 

Turbine: Verification 

and Validation with PIV 

Measurements 

C. Simao Ferreira, Delft 

University of 



0900 


Optimizing the Energy 

Output of Vertical Axis 

Wind Turbines for 

Fluctuating Wind 

Conditions 

S. McIntosh, University 

of Cambridge, 


0930 


Repair of Electronics for 

Long Duration 

Spaceflight 

R. Pettegrew, National 




0930 


Hybrid Potential Flow- 

Streamtube Method for 

Modelling VAWT- 

Flowfield Interactions 

T. Bertényi, Quiet 

Revolution Ltd., London, 

Great Britain 

1000 


Water Reclamation for 

Remote Environments: 

An Ecologically Sound 

Approach 

L. Wickman, Azusa 

Pacific University, Long 

Beach, CA 

1000 


Optimum Blade 

Numbers and Solidities 

for Small HAWTs 

M. Brown, Clarkson 

University, Potsdam, NY 

1030 


Aerodynamic Design of 

a Small Contra- Rotating 

HAWT 

M. Rector, Clarkson 

University, Potsdam, NY 

Session 198-WIG/PDL-7 Magnetohydrodynamics Shasta 1 

Chaired by: S. SCHNEIDER, NASA Glenn Research Center, Cleveland, OH, and S. BOBASHEV, Ioffe Physico-Technical Institute, Saint Petersburg, Russia 

0800 



Electrical Discharges in 

High Speed Reacting 

Flows for the MHD 

Assisted Mixing and 

Combustion 

V. Bityurin, Russian 



0830 


A Plasma Flow Spectral 

Study in the UV Region 

at MHD Interaction 

A. Krasilnikov, 

TSNIIMASH, Korolev, 

Russia 

0900 


Initiation of 

Nonequilibrium 

Conductivity of a 

Hypersonic Flow and 

MHD- Interaction 

V. Fomin, Institute of 

Theoretical and Applied 

Mechanics, Novosibirsk, 

Russia 

0930 


Self- Consistent 

Approach in MHD Flow 

Control Simulation 

E. Sheikin, St. 

Petersburg State 

University, St. 

Petersburg, Russia 

1000 


Aerospace Applicatiions 

of the DOE MHD 

Program Results Part 1: 

Ignition, Combustion 

and Aerodynamics 

H. Chambers, HFC 

Consulting, Westerville, 

OH 

1100 


Icing Simulation of Wind 

Turbine Blades 

C. Hochart, Université 

du Québec à Chicoutimi, 

Chicoutimi, Canada 



Chaired by: S. LEONOV, Russian Academy of Sciences, Moscow, Russia, and I. ADAMOVICH, Ohio State University, Columbus, OH 

0800 0830 0900 0930 1000 1030 1100 

During the past year, NASA has conducted a restructuring of its aeronautics program to focus on long-term, cutting edge research that benefits the broad aeronautics community. At last year's AIAA Reno 

As a follow-up to the workforce development panel to be held on Thursday morning and the workforce development workshop hosted by NASA Aeronautics last summer, a series of breakout sessions will be 


As a follow-up to the workforce development panel to be held on Thursday morning and the workforce development workshop hosted by NASA Aeronautics last summer, a series of breakout sessions will be


Session 199-WIG/PDL-8 Plasma-Assisted Combustion II Sierra 1 

Chaired by: S. LEONOV, Russian Academy of Sciences, Moscow, Russia, and I. ADAMOVICH, Ohio State University, Columbus, OH 

0800 


Plasma- Assisted 

Combustion and Fuel 

Reforming 

E. Mintoussov, Moscow 


Technology, 


0830 


The Effects of Electric 

Fields on the 

Thermodiffusive 

Instability in 

Hydrocarbon/Air Flames 

D. Wisman, Miami 

University, Oxford, OH 

Thursday Afternoon / 11 January 2007 

1200 - 1300 Overview of NASA'a New Restructured Aeronautics Program Reno Room 


0900 


Application of MW 

Plasma Generator for 

Ignition of 

Hydrocarbon/Air Mixture 

V. Vinogradov, Central 

Institute of Aviation 

Motors, Moscow, Russia 

0930 


Air- Hydrocarbon 

Mixture Ionization 

Processes for 

Optimization of Ignition 

Description 

V. Bychkov, Moscow 



1000 


Kinetics in Gas Mixtures 

for Problem of Plasma 

Assisted Ignition 

N. Aleksandrov, Physics 

of Nonequilibrium 

Systems Lab, Moscow 


Technology , 


1030 


Methanol and Ethanol 

Ignition by Repetively 

pulsed, Nanosecond 

Pulse Duration Plasma 

A. Bao, Ohio State 


OH 

1100 


Non- Premixed Plasma- 

Assisted Combustion in 

High- Speed Vortex 

Airflow 

A. Klimov, Russian 



During the past year, NASA has conducted a restructuring of its aeronautics program to focus on long-term, cutting edge research that benefits the broad aeronautics community. At last year's AIAA Reno 

Conference, NASA announced its plans for the restructuring of its aeronautics program and during this year’s conference, an overview of the new restructured aeronautics program will be provided. Dr. Lisa 

Porter, Associate Administrator for NASA’s Aeronautics Research Mission Directorate, along with the Program Directors for the four programs under NASA’s restructured aeronautics program (Airspace 

Systems Program, Aviation Safety Program, Fundamental Aeronautics Program and Aeronautics Test Program) will provide program overview briefings and answer questions from the audience 

1300 - 1630 Higher Education Curriculum Development Carson 1 


held to further discuss the issues of workforce development with a primary focus on the higher education level. These workforce breakout sessions will focus on ideas for what can be done to provide an 

adequate future aerospace workforce in both numbers and technical skills and how the aeronautics community can work together to make this possible. 




As a follow-up to the workforce development panel to be held on Thursday morning and the workforce development workshop hosted by NASA Aeronautics last summer, a series of breakout sessions will be


1300 - 1630 Non-Traditional Methods Carson 2 





1300 - 1630 Students and the Real World Workforce Carson 3 





Session 200-AD-8 Energy Optimized Aircraft Equipment Systems Crystal 3 

Chaired by: J. GALLMAN, Cessna Aircraft Company, Wichita, KS 

1300 


Exploring the Role of 

Fuel Cell Electric Power 

Systems for 

Commercial Aviation 

Applications 

M. Krok, General 

Electric Global Research 

Center, Niskayuna, NY 

1330 


Fuel Cells for 

Commercial Transport 

Airplanes - Needs and 

Opportunities 

J. Breit, The Boeing 


1400 


Electric Actuation for 

Flight and Engine 

Control; Evolution and 

Current Trend 

J. Charrier, 

Hispano-Suiza, 

Colombes, France 

1430 


A Copper Bird for 

Aircraft Equipment 

Systems Integration and 

Electrical Network 

Characterization 

M. Félix, Hispano-Suiza, 

Colombes, France 

1500 


ITAPS: A Process and 

Toolset to Support 

Aircraft Level System 

Integration Studies 



, 

1530 


Performance and 

Weight Impact of Electric 

Environmental Control 

System and More 

Electric Engine on 

Citation CJ2 

T. Ensign, Cessna 

Aircraft Company, 

Wichita, KS 

Chaired by: D. TELIONIS, Virginia Polytechnic Institute and State University, Blacksburg, VA, and D. HALL, California Polytechnic State University, San Luis Obispo, CA 

1300 1330 1400 1430 1500 1530 1600 

1600 


Exergy Analysis as a 

Tool to Decision Making 

in Aircraft Design 

L. Pellegrini, Polytechnic 

School - University of 

São Paulo, São Paulo, 

Brazil


Session 201-APA-22 Fixed-Wing V/STOL Crystal 2 

Chaired by: D. TELIONIS, Virginia Polytechnic Institute and State University, Blacksburg, VA, and D. HALL, California Polytechnic State University, San Luis Obispo, CA 

1300 


A Jet Entrainment 

Theory for VTOL 

Aircraft Suckdown 

P. Bevilaqua, Lockheed 


Company, Palmdale, CA 

1330 


Assessment of a C- 17 

Flight Test of an ESTOL 

Transport Landing 

Approach for 

Operational Viability, 

Pilot Perceptions and 

Workload, and 

Passenger Ride 

Acceptance 

C. Hange, NASA Ames 




Session 202-FD-39 CFD Turbulence Modeling Crystal 1 


1400 


C- 17 Noise Footprint 

Measurements Using a 

Low- Cost Distributed 

Data Acquisition System 

N. Burnside, 

AerospaceComputing 

Inc., Moffett Field, CA 

1430 



Hovering Tilt- Rotor 

UAV for Minimum 

Download and Ground 

Effect Analysis 

C. Kim, Korea 


Institute, Daejon, South 

Korea 

1500 


Overview of the Aircraft 

Trajectory Analysis 

Using Conceptual 

Aircraft Trajectory 

Simulator 

M. Peperak, CENTRA 


Arlington, VA 

1530 


Flow Visualization and 

Measurements in a short 

take of vertical landing 

Fountain Flow 

A. Saddington, Cranfield 

University, Shrivenham, 

Great Britain 

Chaired by: N. GEORGIADIS, NASA Glenn Research Center, Cleveland, OH, and B. NICHOLS, Univeristy of Alabama at Birmingham, Tullahoma, TN 

1300 


Turbulence Modeling for 

Highly Separated Flows 

S. Nichols, University of 

Tennessee SimCenter, 


1330 


Formulation of the komega 

Turbulence 

Model Revisited 

D. Wilcox, DCW 

Industries, Inc., La 

Canada, CA 

1400 


A Compressible Wall- 

Layer Approach 

Compatible with Various 

Turbulence Models 

R. Bond, Sandia 



1430 


Measured Mean Flow 

Dissipation and 

Turbulence Kinetic 

Energy Budget of the 

Second Law 

O. Adeyinka, University 

of Alberta, Edmonton, 

Canada 

1500 



Massively Separated 

Flows 

M. Olsen, NASA Ames 



1600 


Circulation Control and 

Its Application to 

Extreme Short Take- Off 

and Landing Vehicles 

J. de la Montanya, 

California Polytechnic 

State University, San 

Luis Obispo, CA 

Session 203-FD-40 Combustion Crystal 4 

Chaired by: C. FUREBY, FOI - Swedish Defence Research Agency, Stockholm, Sweden, and B. SEKAR, University of Maryland, College Park, MD 

1300 


Comparison of Flamelet 

and Finite Rate 

Chemistry LES for 

Premixed Turbulent 

Combustion 

C. Fureby, Swedish 



Sweden 

1330 


LES/FMDF of Turbulent 

Combustion in Complex 

Flow Systems 

A. Afshari, University of 

Illinois at 

Urbana–Champaign, 

Urbana, IL 

1400 


A Numerical Method for 

DNS/LES of Turbulent 


J. Doom, University of 


MN 

1430 


Strongly- Pulsed 

Turbulent Non- 

Premixed Jet Flames in 

Cross- Flow 

M. Gamba, University of 


TX 

1500 


Ignition Transient 

Simulation in Solid 

Propellant Rocket Motors 


University of 




Chaired by: M. KEGERISE, NASA Langley Research Center, Hampton, VA, and C. ROWLEY, Princeton University, Princeton, NJ 

1300 1330 1400 1430 1500 

Chaired by: Y. JU, Princeton University, Princeton, NJ 

1300 1330 1400 1430 1500 1530 1600 

Chaired by: A. AGRAWAL, University of Alabama, Tuscaloosa, AL, and A. DEAN, General Electric Global Research Center, Niskayuna, NY 

1300 1330 1400


Session 204-FD-41 Flow Control Techniques and Strategies Carson 4 

Chaired by: M. KEGERISE, NASA Langley Research Center, Hampton, VA, and C. ROWLEY, Princeton University, Princeton, NJ 

1300 


Optimal Sensor/Actuator 

Placement Using an 

Adjoint Method 

H. Hamilton, U.S. Air 


Laboratory, Eglin AFB, 

FL 

1330 


Towards Physics Based 

Strategies for 

Separation Control over 

an Airfoil Using 

Synthetic Jets 

R. Raju, George 

Washington University, 



Session 205-PC-16 Fuel Combustion: Metals and Hydrogen Teton 2 

Chaired by: Y. JU, Princeton University, Princeton, NJ 

1300 


On Multiple Criticality in 

Hydrocarbon Ignition 

W. Liu, Princeton 


1330 


Ignition of Hydrogen 

Suddenly Leaked from a 

High Pressure Tank 

K. Aizawa, Aoyama 




1400 


Production and Diffusion 

Mechanism of 

Longitudinal Vortices 

Downstream of Active 

Vortex- Generators Pair 

T. Shizawa, Tokyo 


Suwa, Chino, Japan 

1400 


Counterflow Diffusion 

Flames of General 

Fluids: 

Oxygen/Hydrogen 

Mixtures 

G. Ribert, The 



Park, PA 

1430 


The Dynamics of Shock 

Dispersion and 

Interactions in 

Supersonic Freestreams 

with Counterflowing Jets 

E. Daso, NASA Marshall 

Space Flight Center, 


Center, AL 

1430 


Heating and Ignition of 

Metallic Particles by a 

CO2 Laser 

S. Mohan, New Jersey 


Newark, NJ 

1500 



Steady and Unsteady 

Pneumatic Trailing Edge 

Devices for Subsonic 

Flow Applications 

C. Wong, The University 

of Manchester, 

Manchester, Great 

Britain 

1500 


Production and 


Nano- Aluminum and its 

Effect in Solid Propellant 

Combustion 

1530 


COMBUSTION OF 

DECANE- BASED 

SLURRIES WITH 

METALLIC FUEL 

ADDITIVES 

K. Jayaraman, Indian E. Beloni, New Jersey 

Institute of Technology Institute of Technology, 

-- Madras, Chennai, India Newark, NJ 

1600 


Molecular Dynamics 

Study of Melting of Nano 

Aluminum Particles 

P. Puri, The 



Park, PA 

Session 206-PC-17 Turbulent Combustion Modeling Teton 1 

Chaired by: A. AGRAWAL, University of Alabama, Tuscaloosa, AL, and A. DEAN, General Electric Global Research Center, Niskayuna, NY 

1300 


Advanced 

Preconditioning 

Strategies for Chemically 


V. Sankaran, Sandia 


Livermore, CA 

1330 



of Turbulent Flames in 

Syn- Gas Fuel- Air 

Mixtures 

B. Sen, Georgia Institute 


GA 

1400 


A Combined Level- 

Set/Mixture 

Fraction/Progress- 

Variable Approach for 

Partially- Premixed 

Turbulent Reacting Flows 

C. Safta, Thaerocomp 

Technical Corporation, 

Stony Brook, NY



Chaired by: E. JOSYULA, U.S. Air Force Research Laboratory, Wright-Patterson AFB, OH 

1300 1330 1400 1430 1500


Session 207-PDL-10 / TP-15 Reentry Plasmas and Thermophysics Crystal 5 

Chaired by: E. JOSYULA, U.S. Air Force Research Laboratory, Wright-Patterson AFB, OH 

1300 


Experimental 

Investigation of the Hall 

Effect for the Interaction 

between the Weaklyionized 

Plasma Flow 

and Magnetic Body 

A. Matsuda, Institute of 

Space and Astronautical 

Science/JAXA, 


1330 


Communication Through 

a Non- Equlibrium 


Layer for Re- Entry 

Vehicles 

M. White, Air Force 



OH 

1400 


Particle Simulation of 

Electromagnetic Control 

of a Weakly Ionized 

Flow past a Blunt Body 

H. Katsurayama, Japan 


Agency, Kanagawa, 

Japan 

1430 


Gas- kinetic BGK 

Scheme for three 

dimensional 

magnetohydrodynamics 

C. Cai, ZONA 

Technology Inc., 


1500 


Magnetohydrodynamic 

Influence on a 

Supersonic Nitrogen 

Flow About a Body of 

Revolution 

S. Bobashev, Ioffe 

Physico-Technical 

Institute of the Russian 


Saint Petersburg, Russia

45th AIAA Aerospace Sciences Meeting and Exhibit

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