45th AIAA Aerospace Sciences Meeting and Exhibit

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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#session7356. 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
Tuesday Morning / 09 January 2007 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 AIAA-2007-0514 Personalized Ventilation for Commercial Aircraft Cabins N. Gao, Hong Kong Polytechnic University, Hong Kong, Hong Kong 0830 AIAA-2007-0515 Application of Laminar- Turbulent Transition Criteria in Navier- Stokes Computation J. Cliquet, ONERA, Toulouse, France Tuesday Morning / 09 January 2007 Session 72-FD-14 Flow Control Propulsion Applications Carson 2 Tuesday Morning / 09 January 2007 0900 AIAA-2007-0516 Computational Analysis of Flow Separation Control for the Flow over a Wall- Mounted Hump Using a Synthetic Jet C. Bettini, DIMSET, Genova, Italy 0930 AIAA-2007-0517 Computation of Turbulent Flow over Highly Curved Configuration Using a Conventional Two- Equation Turbulence Model M. Zakyani, Sharif University of Technology, Tehran, Iran 1000 AIAA-2007-0518 Continuous Shape Sensitivity Equation Method for the kepsilon Model of Turbulence R. Di Caro, Ecole Polytechnique de Montreal, Montreal, Canada 1030 AIAA-2007-0519 Interaction of Turbomachinery Components in Large Scale Unsteady Computations of Jet Engines G. Kalitzin, Stanford University, Stanford, CA Chaired by: T. BEUTNER, Defense Advanced Research Projects Agency, Annandale, VA, and M. POST, U.S. Air Force Academy, Colorado Springs, CO 0800 AIAA-2007-0520 Investigation of Low- Pressure Turbine Separation Control A. Gross, University of Arizona, Tucson, AZ 0830 AIAA-2007-0521 Micro- Vortex Generator Flow Control for Supersonic Engine Inlets H. Babinsky, University of Cambridge, Cambridge, Great Britain 0900 AIAA-2007-0522 Supersonic- Inlet Start Amelioration and Unstart Mitigation via Mass and Heat Transfer J. Iannelli, City University, London, Great Britain 0930 AIAA-2007-0525 Influence of Two- Dimensional vs. Discrete Disturbances on Separating Low Pressure Turbine Boundary Layers D. Reimann, Brigham Young University, Provo, UT 1000 AIAA-2007-0526 Correction of Turbulence Quantities in 3D PIV Data M. Alkislar, The Boeing Company, Seattle, WA 1100 AIAA-2007-1448 Assessment of Two Low- Reynolds- Number k- e Models in Turbulent Boundary Layers with Surface Roughness M. Lu, Western Michigan University, Kalamazoo, MI 1130 AIAA-2007-1449 Computational Analysis of Turbulent Internal Flow in Ballistic Solid Rocket Motors A. Arabshahi, UT SimCenter at Chattanooga, Chattanooga, TN 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 AIAA-2007-0527 Numerical Simulation of Blood Flow Through Heart Valves A. Nejadmalayeri, Wichita State University, Wichita, KS 0830 AIAA-2007-0528 Outer- Layer Similarity in the Presence of Highly- Irregular Surface Roughness Y. Wu, University of Illinois at Urbana-Champaign, Urbana, IL 0900 AIAA-2007-0529 Investigation into the Understanding of Flow Stagnation in Fluid Tube Radiators N. Hahn, Paragon Space Development Corporation, Tucson, AZ 0930 AIAA-2007-0530 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 AIAA-2007-0531 Near Wall Measurements in Smooth/Rough Turbulent Boundary Layers B. Brzek, Rensselaer Polytechnic Institute, Troy, NY 1030 AIAA-2007-0532 On the Composite Logarithmic Profile in Zero Pressure Gradient Turbulent Boundary Layers K. Chauhan, Illinois Institute of Technology, Chicago, IL
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Alan Lindenmoyer, Manager, NASA Com
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