45th AIAA Aerospace Sciences Meeting and Exhibit
45th AIAA Aerospace Sciences Meeting and Exhibit
45th AIAA Aerospace Sciences Meeting and Exhibit
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Monday Afternoon / 08 January 2007<br />
Session 51-NSC-2 <strong>AIAA</strong> International Student Conference Masters Division Crystal 5<br />
Chaired by: B. LUND, The Boeing Company, Huntington Beach, CA, <strong>and</strong> C. TAVARES, The Boeing Company, St. Louis, MO<br />
1330<br />
<strong>AIAA</strong>-2007-0368<br />
Experimental<br />
Investigation of<br />
Embedded Cross- Flow<br />
Fan for Airfoil<br />
Propulsion/Circulation<br />
Control<br />
R. Dygert, Syracuse<br />
University, Syracuse, NY<br />
1400<br />
<strong>AIAA</strong>-2007-0369<br />
Sonic Boom Prediction<br />
Using Euler / Full<br />
Potential Methodology<br />
I. Ozcer, Old Dominion<br />
University, Norfolk, VA<br />
Monday Afternoon / 08 January 2007<br />
Session 52-PC-3 Flames Studies II Teton 2<br />
Chaired by: M. SMOOKE, Yale University, New Haven, CT<br />
1330<br />
<strong>AIAA</strong>-2007-0376<br />
Stabilization of an Edge-<br />
Flame in a Corner<br />
Region<br />
M. Matalon,<br />
Northwestern<br />
University, Evanston, IL<br />
1400<br />
<strong>AIAA</strong>-2007-0377<br />
Numerical Study of<br />
Neighboring Edge<br />
Flame Interactions<br />
S. Kostka, University of<br />
Connecticut, Storrs, CT<br />
Monday Afternoon / 08 January 2007<br />
1430<br />
<strong>AIAA</strong>-2007-0370<br />
Design of 3- DOF<br />
Testbed for Micro-<br />
Satellite Autonomous<br />
Operations<br />
F. Leve, University of<br />
Florida, Gainesville, FL<br />
1430<br />
<strong>AIAA</strong>-2007-0378<br />
On the Accurate<br />
Determination of Flame<br />
Speeds at Normal <strong>and</strong><br />
Elevated Pressures by<br />
Using a Spherical<br />
Bomb: The Effects of<br />
Compression <strong>and</strong> Stretch<br />
Z. Chen, Princeton<br />
University, Princeton , NJ<br />
1500<br />
<strong>AIAA</strong>-2007-0371<br />
Low Pressure Turbine<br />
Blade Separation<br />
Control Using Plasma<br />
Actuators<br />
K. Ramakumar,<br />
University of Kentucky,<br />
Lexington, KY<br />
1500<br />
<strong>AIAA</strong>-2007-0380<br />
Front- Tracking<br />
Simulation for Outward<br />
Propagation of Spherical<br />
Flames<br />
K. Pan, National Taiwan<br />
University, Taipei,<br />
Taiwan (roc)<br />
1530<br />
<strong>AIAA</strong>-2007-0372<br />
Acoustic Source<br />
Localization <strong>and</strong> the<br />
Echo Problem<br />
S. Beaver, Texas A&M<br />
University, College<br />
Station, TX<br />
1530<br />
<strong>AIAA</strong>-2007-0381<br />
Verified Computations of<br />
Laminar Premixed<br />
Flames<br />
A. Al-Khateeb,<br />
University of Notre<br />
Dame, Notre Dame, IN<br />
1600<br />
<strong>AIAA</strong>-2007-0373<br />
Numerical Simulation of<br />
the Splashdown Problem<br />
A. Wick, Iowa State<br />
University, Ames, IA<br />
1600<br />
<strong>AIAA</strong>-2007-0382<br />
Scaling Analysis on<br />
Dynamic Flammability<br />
Limits of Unsteady<br />
Premixed Methane/Air<br />
Flames<br />
G. Bansal, University of<br />
Michigan, Ann Arbor, MI<br />
1630<br />
<strong>AIAA</strong>-2007-0374<br />
A Numerical Blade<br />
Element Approach to<br />
Estimating Propeller<br />
Flowfields<br />
D. Hunsaker, Brigham<br />
Young University,<br />
Provo, UT<br />
1630<br />
<strong>AIAA</strong>-2007-0383<br />
Effect of Environmental<br />
Variables on Flame<br />
Spread Rates in<br />
Microgravity<br />
C. Lautenberger,<br />
University of California,<br />
Berkeley, Berkeley, CA<br />
1700<br />
<strong>AIAA</strong>-2007-0375<br />
Investigations Into the<br />
Visualization of Wall<br />
Shear Stress<br />
Distributions Using<br />
Infrared Thermography<br />
<strong>and</strong> Analysis of the<br />
Transient Data<br />
I. Rudolph, Technical<br />
University Berlin, Berlin,<br />
Germany<br />
Session 53-PC-4 Gas Turbine Combustion Teton 1<br />
Chaired by: R. ERICKSON, United Technologies Research Center, East Hartford, CT, <strong>and</strong> Y. IKEDA, Imagineering Inc, Kobe, Hyogo<br />
1330<br />
<strong>AIAA</strong>-2007-0385<br />
Reduced Combustion<br />
Time Model for Methane<br />
in Gas Turbine Flow<br />
Fields<br />
M. Lamnaouer,<br />
University of Central<br />
Florida, Orl<strong>and</strong>o, FL<br />
1400<br />
<strong>AIAA</strong>-2007-0386<br />
The Pratt & Whitney<br />
TALON X Low<br />
Emissions Combustor:<br />
Revolutionary Results<br />
with Evolutionary<br />
Technology<br />
R. McKinney, Pratt &<br />
Whitney, East Hartford,<br />
CT<br />
1430<br />
<strong>AIAA</strong>-2007-0389<br />
Improved Correlations<br />
for Augmentor Static<br />
Stability<br />
D. Knaus, Creare Inc.,<br />
Hanover, NH<br />
1500<br />
<strong>AIAA</strong>-2007-0390<br />
Interaction of a Gaseous<br />
Fuel Jet with Shock-<br />
Wave- Rich Airflow<br />
A. Abdelhafez,<br />
Department of<br />
Mechanical Engineering,<br />
University of Maryl<strong>and</strong>,<br />
College Park, MD<br />
1530<br />
<strong>AIAA</strong>-2007-0391<br />
Numerical Optimization<br />
of the "Tornado"<br />
Combustor Aerodynamic<br />
Parameters<br />
I. Matveev, Applied<br />
Plasma Technologies,<br />
McLean, VA<br />
1600<br />
<strong>AIAA</strong>-2007-0388<br />
Effects of Chemical<br />
Kinetics <strong>and</strong> Heat Loss<br />
on Near- LBO<br />
Combustion Dynamics -<br />
Stability Analysis<br />
T. Yi, University of<br />
Cincinnati, Cincinnati,<br />
OH
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