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#session7283. 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
Tuesday Morning / 09 January 2007 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 AIAA-2007-0473 Computational Evaluation of Controlling Flap- Edge Vortex and Tip Vortex Using Circulation Control Techniques Y. Liu, National Instittue of Aerospace, Hampton, VA 0830 AIAA-2007-0474 Effective Layout of Plasma Actuators for a Flow Separation Control on a Wing D. Tsubakino, University of Tokyo, Tokyo, Japan Tuesday Morning / 09 January 2007 Session 66-APA-8 Bio-Inspired Aerodynamics N-9 Tuesday Morning / 09 January 2007 0900 AIAA-2007-0475 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 AIAA-2007-0481 Aerodynamic Design Exploration of Flapping Wing, Viewpoint of Shape and Kinematics S. Takahashi, Tohoku University, Sendai, Japan 0830 AIAA-2007-0482 Numerical Study of Kinematic Wing Models of Hovering Insect Flight F. Bos, Delft University of Technology, Delft, The Netherlands 0900 AIAA-2007-0483 Aerodynamic Performance of a Corrugated Dragonfly Airfoil Compared with Smooth Airfoils at Low Reynolds Numbers M. Tamai, Iowa State University, Ames, IA 0930 AIAA-2007-0476 Control of Shock- Boundary Layer Interactions (SBLIs) Using An Oscillatory Jet A. Hassan, The Boeing Company, Mesa, AZ 0930 AIAA-2007-0484 Optimization of Flapping Motion of Airfoils in Biplane Configuration for Maximum Thrust and/or Efficiency M. Kaya, Middle East Technical University, Ankara, Turkey 1000 AIAA-2007-0477 Computational Investigation of Flow Control over Wings P. Vavilis, FORTH / IACM, Heraklion, Greece 1000 AIAA-2007-0486 Investigation of Strouhal Number Effect on Flapping Wing Micro Air Vehicle K. Aditya, Maturi Venkata Subba Rao Engineering College, Hyderabad, India 1030 AIAA-2007-0480 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 AIAA-2007-0487 Review of Cranked- Arrow Wing Aerodynamics Project: Its International Aeronautical Community Role J. Lamar, NASA Langley Research Center, Hampton, VA 0900 AIAA-2007-0488 Description of the F16- XL Geometry and Computational Grids Used in CAWAPI O. Boelens, National Aerospace Laboratory/NLR, Amsterdam, The Netherlands 0930 AIAA-2007-0489 Comparison of Measured and Simulated Flow Features for the Full- Scale F- 16XL Aircraft O. Boelens, National Aerospace Laboratory/NLR, Amsterdam, The Netherlands 1000 AIAA-2007-0490 Evaluation of Results from a Reynolds Averaged Multiblock Code Against F- 16XL Flight Data K. Badcock, University of Liverpool, Liverpool, Great Britain 1030 AIAA-2007-0491 PAB3D Simulations for the CAWAPI F- 16XL A. Elmiligui, Analytical Services & Materials, Inc, Hampton, VA 1100 AIAA-2007-0492 RANS Solutions for the CAWAPI F- 16XL in Solution Adapted Hybrid Grids W. Fritz, EADS Military Air Systems, Munich, Germany 1130 AIAA-2007-0493 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
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