45th AIAA Aerospace Sciences Meeting and Exhibit

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http://www.aiaa.org/agenda.cfm?lumeetingid=1064&dateget=all#session7477. 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
Tuesday Morning / 09 January 2007 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 AIAA-2007-0554 Anisotropic Tetrahedral Meshing Based on Surface Deformation Techniques J. Steinbrenner, Pointwise, Inc., Fort Worth, TX 0830 AIAA-2007-0555 Viscous Layer Meshes from Level Sets on Cartesian Meshes W. Dawes, Cambridge University, Cambridge, Great Britain Tuesday Morning / 09 January 2007 Session 78-PC-5 Combustion Instability and Acoustic Interactions Teton 1 Tuesday Morning / 09 January 2007 0900 AIAA-2007-0556 Mesh Generation and Deformation Algorithm for Aeroelasticity Simulations J. Gargoloff, Texas A&M University, College Station, TX Chaired by: J. POWERS, University of Notre Dame, Notre Dame, IN 0800 AIAA-2007-0560 Investigation of Self Excited and Acoustically Forced Combustion Instabilities with Laser Diagnostics F. Scheel, Cambridge University, Cambridge, Great Britain 0830 AIAA-2007-0561 Design Considerations for Remote High- Speed Pressure Measurements of Dynamic Combustion Phenomena D. Straub, National Energy Technology Laboratory, Morgantown, WV 0900 AIAA-2007-0562 Development of a "Prime and Trigger" Concept for Compact Afterburner Combustion S. Birmaher, Georgia Institute of Technology, Atlanta, GA 0930 AIAA-2007-0557 A Mesh Deformation Strategy Optimized by the Adjoint Method on Unstructured Meshes Z. Yang, University of Wyoming, Laramie, WY 0930 AIAA-2007-0563 Impact on Microjet Actuation on Stability of a Backward- Facing Step Combustor M. Altay, Massachusetts Institute of Technology, Cambridge, MA 1000 AIAA-2007-0558 Solution Adaptive Mesh Generation Using Feature- Aligned Embedded Surface Meshes A. Shih, University of Alabama in Birmingham, Birmingham, AL 1000 AIAA-2007-0566 The Effect Steady Fluid Motion on One- Dimensional Wave Propagation B. Kiel, U.S. Air Force Research Laboratory, Wright-Patterson AFB, OH 1030 AIAA-2007-0559 Unstructured Adaptive Elliptic Smoothing S. Karman, University of Tennessee at Chattanooga, Chattanooga, TN 1030 AIAA-2007-0567 Non- Normality and Nonlinearity in Combustion- Acoustic Interaction in Diffusion Flames K. Balasubramanian, Indian Institute of Technology Madras, Chennai, India 1100 AIAA-2007-1416 Two- Parameter Extremum Seeking for Control of Thermoacoustic Instabilities and Characterization of Linear Growth J. Moeck, Technical University of Berlin, Berlin, Germany 1130 AIAA-2007-1417 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 AIAA-2007-0568 Novel Subgrid Modeling of the LES Equations Under Supercritical Pressure L. Selle, California Institute of Technology, Pasadena, CA 0830 AIAA-2007-0569 Experimental Study of Subcritical to Supercritical Jet Mixing S. Polikhov, University of Florida, Gainesville, FL 0900 AIAA-2007-0570 Effects of Fuel Density, Velocity, and Composition on Flame- Acoustic Interaction A. Ghosh, University of Maryland, College Park, MD 0930 AIAA-2007-0571 LOX/GH2 Shear Coaxial Injector Atomization Studies: Effect of Recess and Non- Concentricity R. Woodward, Pennsylvania State University, University Park, PA 1000 AIAA-2007-0572 Interaction of LOX/GH2 Spray- Combustion with Acoustics B. Knapp, DLR, German Aerospace Research Center, Hardthausen, Germany 1030 AIAA-2007-0573 Transient Cryogenic Flow and Mixing from a Coaxial Rocket Injector V. Gautam, University of Maryland, College Park, MD 1100 AIAA-2007-0574 Prediction of Non- Equilibrium Kinetics of Fuel- rich Kerosene/LOX Combustion in Gas Generator C. Lee, Konkuk University, Seoul, South Korea 1130 AIAA-2007-0575 Supercritical Combustion of Liquid Oxygen (LOX) and Methane Stabilized by a Splitter Plate N. Zong, Pennsylvania State University, State College, PA
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