EVENT AGENDA 48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition

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At A Glance | 04-Jan-2010 | 05-Jan-2010 | 06-Jan-2010 | 07-Jan-2010 | All |

Program For Monday, 04-Jan-2010 0800 - 1200 NASA Aeronautics Research: Then and Now Crystal Ballroom J2 Session Co-Chairs: Dr. Jaiwon Shin, Associate Administrator, Aeronautics Research Mission Directorate (ARMD), NASA Ms. Jean Wolfe, Deputy Director, Integrated Systems Research Program (ISRP), ARMD, NASA 0800-0900 X-15: To the Edge of Space Joe Engle, Retired U.S. Air Force Major General, Former Space Shuttle Astronaut and X-15 Test Pilot 0900-0930 NASA Aeronautics Update Dr. Jaiwon Shin, Associate Administrator, Aeronautics Research Mission Directorate NASA 0930-1000 Overview of NASA’s Integrated Systems Research Program (ISRP) Ms. Jean Wolfe, Deputy Director, Integrated Systems Research Program (ISRP), ARMD, NASA 1000-1030 Overview of NASA’s Environmentally Responsible Aviation (ERA) Project Dr. Fayette Collier, Project Manager, Environmentally Responsible Aviation (ERA) Project, NASA 1030-1100 NASA’s Current Plans for ERA Airframe Technology Anthony Washburn, Project Engineer (Acting), Airframe Technology Sub-project for ERA, NASA 1100-1130 NASA’s Current Plans for ERA Propulsion Technology Dr. Jim Heidmann, Project Engineer (Acting), Propulsion Technology Sub-project for ERA, NASA 1130-1200 NASA’s Current Plans for ERA Vehicle Systems Integration Steve Smith, Project Engineer (Acting), Vehicle Systems Integration Sub-project for ERA, NASA Session 1- AA-1 Airfoil & Airframe Noise Denver Chaired by: M. WANG, University of Notre Dame, Notre Dame, IN 0800 AIAA-2010-0006 The Noise of Turbulent Boundary- Layer Flow Over Small Steps M. Ji and M. Wang, University of Notre Dame, Notre Dame, IN 0830 AIAA-2010-0007 Characteristics of Separated Flow Surface Pressure Fluctuations on an Axisymmetric Bump G. Byun and R. Simpson, Virginia Polytechnic Institute and State University, Blacksburg, VA 0900 AIAA-2010-0008 The Near- Field Pressure of a Scaled Rotor During Hover J. Stephenson, C. Tinney, and J. Sirohi, University of Texas, Austin, Austin, TX 0930 AIAA-2010-0009 Simulation of Ares- I Liftoff Acoustic Loads Using a Boundary Element Model and Monopole Sources E. O'Keefe and D. Go, The Boeing Company, Friendswood, TX 1000 AIAA-2010-0010 Investigation of Near- Field Flow Unsteadiness Around a NACA0012 Wingtip Using Large- Eddy- Simulation Approach T. Imamura, Japan Aerospace Exploration Agency (JAXA), Chofu, Japan; T. Hirai, Ryoyu Systems Company, Ltd, Tokyo, Japan; S. Enomoto, Y. Yokokawa, H. Kato, and K. Yamamoto, Japan Aerospace Exploration Agency (JAXA), Chofu, Japan 1030 AIAA-2010-0011 Flyover Noise Measurements of a Spiraling Noise Abatement Approach Procedure L. Bertsch, German Aerospace Center (DLR), Braunschweig, Germany; G. Looye, German Aerospace Center (DLR), Wessling, Germany; E. Anton, RWTH Aachen University, Aachen, Germany; and S. Schwanke, Deutsche Flugsicherung GmbH (DFS), Langen, Germany 1100 AIAA-2010-0012 Vortex- Shedding Induced Trailing- Edge Acoustics U. Svennberg and C. Fureby, Swedish Defence Research Agency, Stockholm, Sweden Session 2- AA-2 Jet Noise Suppression I Tampa Chaired by: M. SAMIMY, Ohio State University, Columbus, OH 0800 AIAA-2010-0013 Noise Control of High Reynolds Number Mach 1.3 Heated Jet Using Plasma Actuators M. Kearney-Fischer, J. Kim and M. Samimy, Ohio State University, Columbus, OH 0830 AIAA-2010-0014 Assessment of Noise Reduction Concepts for Fighter Aircraft Application in Simulated Forward Flight K. Viswanathan, The Boeing Company, Seattle, WA; A. Krothapalli, Florida State University, Tallahassee, FL; J. Seiner, University of Mississippi, Oxford, MS; M. Czech, The Boeing Company, Seattle, WA; B. Greska, Florida State University, Tallahassee, FL; and B. Jansen, University of Mississippi, Oxford, MS 0900 AIAA-2010-0015 Development of Reduced- order Models for Feedback Control of Axisymmetric Jets A. Sinha, A. Serrani, and M. Samimy, Ohio State University, Columbus, OH 0930 AIAA-2010-0016 Large- Scale Simulations of Acoustic Synthetic Jets M. Mankbadi and R. Mankbadi, Embry-Riddle Aeronautical University, Daytona Beach, FL 1000 AIAA-2010-0017 Jet Noise Suppression Using Ultrasonic Powered Resonance Tubes K. Chaudhari, S. Sarpotdar and G. Raman, Illinois Institute of Technology, Chicago, IL 1030 AIAA-2010-0018 Unsteady Numerical Simulation of a Round Jet- Microjet Combination for Noise Suppresion P. Lew, A. Najafiyazdi, and L. Mongeau, McGill University, Montréal, Canada Session 3- AA-3 Turbomachinery, Core, and Combustion Noise Washington Chaired by: J. MILES, NASA Glenn Research Center, Cleveland, OH 0800 AIAA-2010-0019 Separating Direct and Indirect Turbofan Engine Combustion Noise Using the Correlation Function J. Miles, NASA Glenn Research Center, Cleveland, OH 0830 AIAA-2010-0020 A DES Study of the Transonic Trailing- Edge Flow of a Fan- Blade Section P. Ray and W. Dawes, University of Cambridge, Cambridge, Great Britain 0900 AIAA-2010-0021 Gas Turbine Single Annular Combustor Sector: Combustion Dynamics J. Cai, F. Ichihashi, B. Mohammad, S. Tambe, Y. Kao, and S. Jeng, University of Cincinnati, Cincinnati, OH 0930 AIAA-2010-0022 Proper Orthogonal Decomposition and Fourier Analysis on the Energy Release Rate Dynamics F. Ichihashi, S. Jeng and K. Cohen, University of Cincinnati, Cincinnati, OH 1000 AIAA-2010-0023 Inhibitor Vortex Shedding Acoustic Response Cold Flow Experiment E. Jacob and L. Blaette, University of Tennessee Space Institute, Tullahoma, TN 1030 AIAA-2010-0024 Numerical Analysis of Stability of Thermo- Acoustic Oscillation in a 2- D Closed Tube M. Ishigaki, Nagoya University, Nagoya, Aichi, Japan; S. Adachi, Tokyo International University, Kawagoe, Saitama, Japan; K. Ishii, Nagoya University, Nagoya, Aichi, Japan 1100 AIAA-2010-0025 Asymptotic Analysis of Thermoacoustic Instability in Rijke Tube S. Mariappan and R. Sujith, Indian Institute of Technology, Madras, Chennai, India 1130 AIAA-2010-0026 Formulation of Combustion Acoustic Coupling using Multiple Time and Length Scales S. Chakravarthy and B. Chellappan, Indian Institute of Technology, Madras, Chennai, India Session 4- ABP-1 NPARC Alliance/Wind-US Code Crystal Ballroom D Chaired by: A. CARY, The Boeing Company, St Louis, MO, and C. NELSON, Innovative Technology Applications Company, Lynnwood, WA 0800 AIAA-2010-0027 An Overview of the NPARC Alliance's Wind- US Flow Solver C. Nelson, Innovative Technology Applications Company, Lynnwood, WA 0830 AIAA-2010-0028 Unstructured Grid Solution Accuracy and Mesh Dependency A. Cary, A. Dorgan and M. Mani, The Boeing Company, St. Louis, MO 0900 AIAA-2010-0030 Finite Rate Chemistry Implementation and Validation for Unstructured Grids A. Dorgan, A. Cary and M. Mani, The Boeing Company, St. Louis, MO 0930 AIAA-2010-0031 A Modular Conjugate Heat Transfer Capability for the Wind- US CFD Code E. Perrell, Embry-Riddle Aeronautical University, Daytona Beach, FL; G. Power and C. Robinson, Arnold Engineering Development Center, Arnold AFB, TN 1000 AIAA-2010-0032 Modeling Vortex Generators in the Wind- US Code J. Dudek, NASA Glenn Research Center, Cleveland, OH 1030 AIAA-2010-0033 CFD Models of a Serpentine Inlet, Fan, and Nozzle R. Chima, D. Arend, R. Castner, and J. Slater, NASA Glenn Research Center, Cleveland, OH; and P. Truax, , Fort Worth, TX Session 5- AFM-1 Aerodynamic Prediction Methods Chicago Chaired by: P. WILLIAMS-HAYES, NASA Dryden Flight Research Center, Barstow, CA, and A. CRASSIDIS, Rochester Institute of Technology, Rochester, NY 0800 AIAA-2010-0034 Introducing a Combined Equation/Output Error Approach in Parameter Estimation E. Ozger, EADS Military Air Systems, Manching, Germany 0830 AIAA-2010-0035 An Aeroelastic, Flexible- Wing Model for Aircraft Simulation S. Andrews and A. Cooke, Cranfield University, Cranfield, Great Britain 0900 AIAA-2010-0036 Modeling of Helicopter Self- Defense System J. Blaszczyk and K. Sibilski, Air Force Institute of Technology, Warsaw, Poland 0930 AIAA-2010-0037 Near- Space Balloon Performance Predictions J. Conner and A. Arena, Oklahoma State University, Stillwater, OK 1000 AIAA-2010-0038 Modeling of Stratosphere Airship X. Wang, Shanghai Jiao Tong University, Shanghai, China (prc) 1030 AIAA-2010-0039 Modeling of a Quad- Rotot Airship with Wind and Freight Effect: a Newton- Euler Approach Y. Bestaoui, Université d’Evry, Evry, France 1100 AIAA-2010-0040 A Lagrangian Approach to Modeling of a Quad- Rotor Airship Y. Bestaoui, Université d'Evry, Evry, France 1130 AIAA-2010-0041 System Identification of an Aerodynamics Model for an Ornithopter J. Grauer, J. Hubbard and S. Humbert, University of Maryland, College Park, MD Session 6- AMT-1 Shear Stress Measurement Technology I Crystal Ballroom J1 Chaired by: T. LIU, Western Michigan University, Kalamazoo, MI, and M. BENNE, The Boeing Company, St Louis, MO 0800 AIAA-2010-0042 Skin Friction Measurements Using Elastic Films (Invited) J. Crafton, S. Fonov, R. Forlines and L. Goss, Innovative Scientific Solutions Inc., Dayton, OH 0830 AIAA-2010-0043 Oil Film Interferometry in the Development of Long- Endurance Aircraft (Invited) A. Drake, Northrop Grumman Corporation, San Diego, CA 0900 AIAA-2010-0044 Measurement of Skin Friction in Complex Flows (Invited) J. Schetz, Virginia Polytechnic Institute and State University, Blacksburg, VA 0930 AIAA-2010-0045 Experimental Examination of Skin Friction Topology in Separated Flows (Invited) T. Liu and S. Woodiga, Western Michigan UNiversity, Kalamazoo, MI 1000 AIAA-2010-0046 Hair- Like Capacitive MEMS Shear Sensor Array for Surface Shear Force Measurement S. Liu, R. Wlezien and R. White, Tufts University, Medford, MA 1030 AIAA-2010-0047 Dynamic Pressure Sensitivity and Calibration of Direct Shear Stress V. Chandrasekharan, J. Meloy, J. Sells, D. Arnold and M. Sheplak, University of Florida, Gainesville, FL 1100 AIAA-2010-0048 Fluctuating Wall Shear Stress Measurements Using Ionic Polymer Metal Composite Transducers P. Vlachos, Virginia Polytechnic Institute and State University, Blacksburg, VA; M. Bennett, Discover Technologies Inc, Research Triangle Park, NC; N. Cardwell and C. Weiland, Virginia Polytechnic Institute and State University, Blacksburg, VA Session 7- APA-1 Aerodynamic-Structural Dynamics Interaction Grand Ballroom 9 Chaired by: J. DESPIRITO, U.S. Army Research Laboratory, Aberdeen Proving Ground, MD, and K. STEWART, U.S. Air Force Research Laboratory, Eglin AFB, FL 0800 AIAA-2010-0049 Aeroelastic Analysis of Sensor Craft Configurations Using AVUS and Nastran E. Alyanak and G. Brooks, U.S. Air Force Research Laboratory, Wright-Patterson AFB, OH 0830 AIAA-2010-0050 Development of a Aerothermoelastic- Acoustics Simulation Capability of Flight Vehicles K. Gupta, NASA Dryden Flight Research Center, Edwards, CA; S. Choi, Advanced Engineering Solutions, Inc., Ormond Beach, FL; and A. Ibrahim, Norfolk State University, Norfolk, VA 0900 AIAA-2010-0051 Computational Study of Flexible Trailing Edge Extension for Improving Flapping Propulsion A. Lai and F. Liu, University of California Irvine, Irvine, CA 0930 AIAA-2010-0052 ALE- Based FSI Simulation of Solid Propellant Rocket Interior S. Han, H. Choi, and C. Kim, Seoul National University, Seoul, South Korea; C. Hwang, Seoul University of Venture & Information, Seoul, South Korea; G. Jung and J. Oh, Agency for Defense Development, Daejeon, South Korea 1000 AIAA-2010-0053 Detached Eddy Simulation of 3- D Wing Flutter with Fully Coupled Fluid- Structural Interaction X. Chen and G. Zha, University of Miami, Coral Gables, FL 1030 AIAA-2010-0054 In- Flight Deployment Dynamics of Inflatable Wings L. Ben and J. Jacob, Oklahoma State University, Stillwater, OK 1100 AIAA-2010-0055 Flutter Analysis of Balloon- Based Operation Vehicle for Precooled Turbojet Engine Demonstration K. Miyaji and J. Matsuwaki, Yokohama National University, Yokohama, Japan; T. Kojima and K. Fujita, Japan Aerospace Exploration Agency (JAXA), Tokyo, Japan; and S. Sawai, Japan Aerospace Exploration Agency (JAXA), Sagamihara, Japan 1130 AIAA-2010-0056 New Aeroelastic Studies for a Morphing Wing S. Courchesne, A. Popov, and R. Botez, ETS - LARCASE, Montréal, Canada Session 8- APA-2 Airfoil/Wing/Configuration Aerodynamics Grand Ballroom 10 Chaired by: J. GUGLIELMO, The Boeing Company, Saint Peters, MO, and K. WAITHE, Gulffstream Aerospace Corporation, Savannah, GA 0800 AIAA-2010-0057 Aerodynamic Optimization and Evaluation of KC- 135R Winglets, Raked Wingtips, and a Wingspan Extension J. Halpert, D. Prescott, T. Yechout, and M. Arndt, U.S. Air Force Academy, U.S. Air Force Academy, CO 0830 AIAA-2010-0058 Aerodynamics of Cambered Membrane Flapping Wings S. Shkarayev and D. Silin, University of Arizona, Tucson, AZ; G. Abate, U.S. Air Force Research Laboratory, Eglin, FL; and R. Albertani, Univeristy of Florida, Shalimar, FL 0900 AIAA-2010-0059 Detached- Eddy Simulation of a Double- Element Wing in Ground Effect J. Heyder-Bruckner and X. Zhang, University of Southampton, Southampton, Great Britain 0930 AIAA-2010-0060 Effect of Leading Edge Break Position on Performance of Double Delta Movable Tip Strakes V. Nikolic, Minnesota State University, Mankato, Mankato, MN 1000 AIAA-2010-0061 Surface Launch Simulations of an Unmanned Aerial Vehicle Loaded with Jet- Assisted Takeoff Motors D. Gonzalez, Naval Surface Warfare Center, Indian Head, MD 1030 AIAA-2010-0062 Passively Varying Pitch Propeller for Small UAS S. Heinzen, U.S. Air Force Research Laboratory, Raleigh, NC; C. Hall and A. Gopalarathnam, North Carolina State University, Raleigh, NC 1100 AIAA-2010-0063 Preliminary Design Drag Calculation Using Advanced Paneling Schemes V. Ahuja, R. Hartfield and J. Burkhalter, Auburn University, Auburn, AL 1130 AIAA-2010-0064 Transonic Drag Reduction with Contour Bump on a Supercritical Airfoil Y. Tao, G. Liu, Y. Sun, and J. Lin, China Aerodynamics Research and Development Center, Mianyang, China (prc) Session 9- APA-3 Low Speed, Low Reynolds Number Aerodynamics Grand Ballroom 11 Chaired by: F. COTON, University of Glasgow, Glasgow, United States, and C. BRUNER, Sandia National Laboratories, Albuquerque, NM 0800 AIAA-2010-0065 How Motion Trajectory Affects the Energy Extraction Performance of an Oscillating Foil Q. Xiao, University of Strathclyde, Glasgow, Great Britain; W. Liao, Old Dominion University, Norfolk, VA; and S. Yang, ZONATechnology, Inc, Scottsdale, AZ 0830 AIAA-2010-0066 Flow Visualization and Force Measurement of an Insect- Based Flapping Wing J. Han and J. Chang, Korea Aerospace University, Goyang, South Korea; I. Kang and S. Kim, Agency for Defense Development, Daejeon, South Korea 0900 AIAA-2010-0067 Simulation of Insect- Sized Flapping- Wing Aerodynamics W. Yuan and M. Khalid, National Research Council Canada, Ottawa, Canada 0930 AIAA-2010-0068 Numerical Analysis of the Flow Around the SD 7003 Airfoil P. Catalano, Centro Italiano Ricerche Aerospaziali (CIRA), Capua, Italy; and R. Tognaccini, University of Naples "Federico II", Napoli, Italy 1000 AIAA-2010-0069 Gust Encounters in Rigid and Flexible Wing MAVs J. Jacob, Oklahoma State University, Stillwater, OK 1030 AIAA-2010-0070 A Study of Trailing- Edge Scalloping on Flat Plate- Membrane Airfoil Performance T. Hicks and J. Hubner, University of Alabama, Tuscaloosa, AL 1100 AIAA-2010-0071 Effects of Ipsilateral Wing- Wing Interactions on Aerodynamic Performance of Flapping Wings H. Dong and Z. Liang, Wright State University, Dayton, OH 1130 AIAA-2010-0072 Low Reynolds Number Aerodynamics of Propellers Operating Perpendicular to Walls S. Henry and M. Selig, University of Illinois, Urbana-Champaign, Urbana, IL Session 10- ASE-1 Space Environment Ground Simulations and Testing Atlanta Chaired by: J. PREBOLA, Aerospace Testing Alliance, Arnold AFB, TN, and M. CHO, Kyushu Institute of Technology, Kitakyushu, Japan 0800 AIAA-2010-0073 Investigations into Delamination and Damage Processes of Advanced Aerospace Structures Subject to Hypervelocity Impact M. Rathnasabapathy, RMIT University, Melbourne, Australia 0830 AIAA-2010-0074 Preliminary Experiments for Establishing An ESD Ground Testing Method of Solar Array K. Toyoda, T. Wada, T. Yoke, T. Suzuki, H. Masui and M. Cho, Kyushu Institute of Technology, Kitakyushu, Japan 0900 AIAA-2010-0075 Arcing on Solar Arrays at Extremely Low Temperatures B. Vayner, Ohio Aerospace Institute, Cleveland, OH; J. Galofaro, NASA Glenn Research Center, Cleveland, OH 0930 AIAA-2010-0076 Development of Electron- Emitting Film for Spacecraft Charging Mitigation: Preparation for Flight Demonstration M. Cho, M. Iwata, K. Toyoda, and M. Khan, Kyushu Institute of Technology, Kitakyushu, Japan; S. Hatta, MUSCAT Space Engineering Co. Ltd., Kitakyushu, Japan; and T. Fujita, Japan Aerospace Exploration Agency (JAXA), Chofu, Japan 1000 AIAA-2010-0077 New Space Weather Mitigation Capabilities W. Tobiska, Space Environment Technologies, Los Angeles, CA 1030 AIAA-2010-0078 Numerical and Experimental Investigations of Charging on Lunar Surface J. Wang, University of Southern California, Los Angles, CA Session 11- EDU-1 New Directions in Course Instruction Crystal Ballroom Q Chaired by: M. MAUGHMER, Pennsylvania State University, University Park, PA 0800 AIAA-2010-0079 Instruction in Experimental Methods: What Should We Be Teaching In Laboratory Courses? D. Bridges, Mississippi State University, Mississippi State, MS 0830 AIAA-2010-0080 The Beginner's Guide to Wind Tunnels with TunnelSim and TunnelSys T. Benson and C. Galica, NASA Glenn Research Center, Cleveland, OH; A. Vila, Vanderbilt University, Nashville, TN 0900 AIAA-2010-0081 Cost Savings Using Modern Design of Experiments (MDOE) W. Line, DOES Institute, Winston-Salem, NC 0930 AIAA-2010-0082 An Aerodynamics Course Project to Illustrate Parasite Drag Coefficient Prediction E. Niemi, University of Massachusetts, Lowell, Lowell, MA 1000 AIAA-2010-0083 Incorporating Airworthiness into the Academic Curriculum S. Cook, Naval Air Systems Command, Patuxent River, MD 1030 AIAA-2010-0084 Design of Experiments Using 3DOF Spacecraft Simulators B. Stiltner, M. Bitzer, D. Heart, and T. Berman, Virginia Polytechnic Institute and State University, Blacksburg, VA 1100 AIAA-2010-0085 A Primer for University- Level Rocket Motor Research and Development J. Dennis and J. Villarreal, Arizona State University, Tempe, AZ Session 12- FD-1 Active Flow Control I Grand Ballroom 3 Chaired by: S. SIEGEL, and H. FASEL 0800 AIAA-2010-0086 Hybrid Flow Control of a Turret Wake, Part I: Aerodynamic Effects B. Vukasinovic and A. Glezer, Georgia Institute of Technology, Atlanta, GA; S. Gordeyev and E. Jumper, University of Notre Dame, Notre Dame, IN; and V. Kibens, The Boeing Company, Saint Louis, MO 0830 AIAA-2010-0087 Flow control effects on the length scales over a turret M. Andino and M. Glauser, Syracuse University, Syracuse, NY 0900 AIAA-2010-0088 Experimental Study of an Inclined Jet- in- Cross- Flow Interacting with a Vortex Generator K. Zaman, D. Rigby, and J. Heidmann, NASA Glenn Research Center, Cleveland, OH 0930 AIAA-2010-0089 Effect of Sinusoidal Forcing on the Wake of a Circular Cylinder S. Bhattacharya and A. Ahmed, Auburn University, Auburn, AL 1000 AIAA-2010-0090 Numerical Simulations of Vortex Generating Jets on Low Pressure Turbine Blades C. Memory, J. Bons and J. Chen, Ohio State University, Columbus, OH 1030 AIAA-2010-0091 Frequency Effect on Flow Field Behind an Oscillating Fence Submerged in Turbulent Boundary Layer M. Saini, University of Wyoming, Laramie, WY; P. Medina, Siemens, Boulder, CO; J. Strike, W. Lindberg, and J. Naughton, University of Wyoming, Laramie, WY 1100 AIAA-2010-0092 Proportional Aerodynamic Control of a Swept Divergent Trailing Edge Wing Using Synthetic Jets J. Sefcovic and D. Smith, University of Wyoming, Laramie, WY 1130 AIAA-2010-0093 Analysis of Low Speed Flow over an Adaptive Airfoil with Oscillating Camber R. LeBeau and A. Karam, University of Kentucky, Lexington, KY; N. Pern, General Electric Company, Schenectady, NY; and J. Jacob, Oklahoma State University, Stillwater, OK Session 13- FD-2 Droplet and Multi-Phase Flows Grand Ballroom 12 Chaired by: R. SCHMIT, U.S. Air Force Research Laboratory, Wright-Patterson AFB, OH 0800 AIAA-2010-0094 Droplet Dispersions in the Icing Research Tunnel A. Lee and E. Loth, University of Illinois, Urbana-Champaign, Urbana, IL 0830 AIAA-2010-0095 Modeling of the Internal Two- Phase Flow in a Gas- Centered Coaxial Fuel Injector N. Trask, J. Perot, and D. Schmidt, University of Massachusetts, Amherst, MA; M. Lightfoot and S. Danczyk, U.S. Air Force Research Laboratory, Edwards AFB, CA; and T. Meyer, Iowa State University, Ames, IA 0900 AIAA-2010-0096 Simulation of Multiphase Blast- Structure Interaction via Coupled CFD and CSD Codes R. Lohner and F. Camelli, George Mason University, Fairfax, VA; J. Baum and O. Soto, SAIC, McLean, VA 0930 AIAA-2010-0097 Simulation of Supercritical Ethylene Condensation Using Homogeneous Nucleation Theory J. Edwards, North Carolina State University, Raleigh, NC; K. Lin, Taitech, Inc., Beavercreek, OH; M. Ryan, Universal Technology Corporation, Dayton, OH; and C. Carter, U.S. Air Force Research Laboratory, Wright-Patterson AFB, OH 1000 AIAA-2010-0098 Numerical Simulation of Two- Phase Flow Within an Aerated Liquid Injector D. Cassidy and J. Edwards, North Carolina State University, Raleigh, NC; K. Lin, Taitech Inc, Beavercreek, OH 1030 AIAA-2010-0099 Turbulent Particulate Pressure for Two- Phase Flow Modelling C. Hug and P. Brenner, EADS Astrium Space Transportation, Les Mureaux, France; and F. Dubois, Conservatoire National des Arts et Métiers, Paris, France 1100 AIAA-2010-0100 Effects of Liquid and Surface Properties on Droplet- Film Collision K. Pan and C. Hung, National Taiwan University, Taipei, Taiwan (roc) Session 14- FD-3 Innovative Measurement Technologies and Experimental Observations Grand Ballroom 4 Chaired by: Z. MAHMUD, North Dakota State University, Fargo, ND, and L. UKEILEY, University of Florida, Shalimar, FL 0800 AIAA-2010-0101 Studying Complex Flow Characteristics Around a Circular Cylinder Using MEMS Thermal Film Sensors J. Miau, National Cheng Kung University, Tainan, Taiwan (roc) 0830 AIAA-2010-0102 Density Field Measurements of a Supersonic Impinging Jet with Microjet Control L. Venkatakrishnan, National Aerospace Laboratories, Bangalore, India; A. Wiley, R. Kumar, and F. Alvi, Florida A&M University-Florida State University, Tallahassee, FL 0900 AIAA-2010-0103 Virtual Shock Shaping Using Microjet Arrays A. Botu, Florida A&M University-Florida State University, Tallahassee, FL; L. Venkatakrishnan, National Aerospace Laboratories, Bangalore, India; R. Kumar and F. Alvi, Florida A&M University-Florida State University, Tallahassee, FL 0930 AIAA-2010-0104 Planar Imaging Measurements of Three Scalars in a Turbulent Jet C. Brownell, U.S. Naval Academy, Annapolis, MD; and L. Su, Johns Hopkins University, Baltimore, MD 1000 AIAA-2010-0105 Reynolds Stress and Turbulence Kinetic Energy Balances in Swirling Jets S. Toutiaei, R. Semaan and J. Naughton, University of Wyoming, Laramie, WY 1030 AIAA-2010-0106 Experimental Studies of Synthetic Radial Wall Jets G. Krishnan and K. Mohseni, University of Colorado, Boulder, Boulder, CO 1100 AIAA-2010-0107 Surface Pressure Fluctuations Due to an Impinging Supersonic Underexpanded Jet B. Pundir, Florida Atlantic University, Boca Raton, FL Session 15- FD-4 Shock-Wave/Turbulence Interactions Grand Ballroom 5 Chaired by: P. MARTIN, Princeton University, Princeton, NJ, and R. BALASUBRAMANIAN, ITT Industries, Seneca Falls, NY 0800 AIAA-2010-0108 Analysis of Low- Frequency Unsteadiness in Shockwave and Turbulent Boundary Layer Interactions S. Priebe and M. Martin, Princeton University, Princeton, NJ 0830 AIAA-2010-0109 Delayed- Detached- Eddy Simulation of Shock Wave/Turbulent Boundary Layer Interaction P. Coronado, B. Wang and G. Zha, University of Miami, Coral Gables, FL 0900 AIAA-2010-0110 Large- Eddy Simulation of Incident Shock Wave/Turbulent Boundary Layer Interaction A. Jammalamadaka, Z. Li and F. Jaberi, Michigan State University, East Lansing, MI 0930 AIAA-2010-0111 Imulation of Shock / Boundary Layer Interactions Using Improved LES/RANS Models D. Gieseking, J. Choi and J. Edwards, North Carolina State University, Raleigh, NC 1000 AIAA-2010-0112 Numerical Investigations of Shock- Turbulence Interaction in Planar Mixing Layer Z. Li and F. Jaberi, Michigan State University, East Lansing, MI 1030 AIAA-2010-0113 Large- Eddy Simulation of Shockwave/Isotropic Turbulence Interaction N. Grube and P. Martin, Princeton University, Princeton, NJ 1100 AIAA-2010-0114 Numerical Simulation of Shock- Turbulence Interactions Using High- Order Shock- Fitting Algorithms P. Rawat and X. Zhong, University of California, Los Angeles, Los Angeles, CA 1130 AIAA-2010-0115 Validation of a Wall- Layer Model for a Shock- Wave/Boundary- Layer Interaction R. Bond, F. Blottner and T. Smith, Sandia National Laboratories, Albuquerque, NM Session 16- FD-5 Time Integration and Solution Methods Boston Chaired by: D. KNIGHT, Rutgers University, Piscataway, NJ, and L. FUCHS, Lund Universiy, Lund, Sweden 0800 AIAA-2010-0116 A Parallel Newton- Krylov Flow Solver for the Navier- Stokes Equations Using the SBP- SAT Approach M. Osusky and D. Zingg, University of Toronto, Toronto, Canada 0830 AIAA-2010-0117 Implementation of a Robust Multigrid Algorithm in a Production- Level Overset CFD Solver S. Slimon, D. Davis and C. Wagner, Electric Boat Corporation, Groton, CT 0900 AIAA-2010-0118 Deflated Preconditioned Conjugate Gradient Solvers: Extensions and Improvements F. Mut and R. Lohner, George Mason University, Fairfax, VA; R. Aubry and G. Houzeaux, Barcelona Supercomputing Center, Barcelona, Catalunya, Spain; J. Cebral, George Mason University, Fairfax, VA 0930 AIAA-2010-0119 Computational Zone Adaptation Strategy in Convergence Acceleration over Unstructured Grid N. Fouladi, Sharif University of Technology, Tehran, Iran; M. Darbandi, Sharif University, Tehran, Iran; G. Schneider, University of Waterloo, Waterloo, Ontario, Canada 1000 AIAA-2010-0120 Time- Tensor for Rapid Convergence of CFD Solutions N. Domel, Lockheed Martin Aeronautics, Fort Worth, TX 1030 AIAA-2010-0121 Spatially Non- Uniform Time- Step Adaptation for Functional Outputs in Unsteady Flow Problems K. Mani and D. Mavriplis, University of Wyoming, Laramie, WY 1100 AIAA-2010-0122 Re- Evaluation of An Optimized Second- Order Backward Difference (BDF2OPT) Scheme for Unsteady Flow Applications V. Vatsa, M. Carpenter, and D. Lockard, NASA Langley Research Center, Hampton, VA 1130 AIAA-2010-0123 A Method To Accelerate LES Explicit Solvers Using Local Time- Stepping O. Esnault, M. Boileau, and R. Vicquelin, Centre National de la Recherche Scientifique (CNRS), Châtenay-Malabry, France; B. Fiorina and O. Gicquel, École Centrale Paris, Châtenay-Malabry, France Session 17- FD-6 Verification, Validation, and Uncertainty Quantification in CFD Grand Ballroom 6 Chaired by: C. ROY, Virginia Polytechnic Institute and State University, Blacksburg, VA, and W. OBERKAMPF, W L Oberkampf Consulting, Albuquerque, NM 0800 AIAA-2010-0124 A Complete Framework for Verification, Validation, and Uncertainty Quantification in Scientific Computing C. Roy, Virginia Polytechnic Institute and State University, Blacksburg, VA; and W. Oberkampf, , Albuquerque, NM 0900 AIAA-2010-0125 AIAA CFD Code Verification Project: Verification Test Cases and Reference Data for Code Verification U. Ghia, University of Cincinnati, Cincinnati, OH 0930 AIAA-2010-0126 Review of Discretization Error Estimators in Scientific Computing C. Roy, Virginia Polytechnic Institute and State University, Blacksburg, VA 1030 AIAA-2010-0127 Comprehensive Code Verification for an Unstructured Finite Volume CFD Code S. Veluri, Virginia Polytechnic Institute and State University, Blacksburg, VA; C. Roy, Virginia Polytechnic Institute and State University, Blackburg, VA; and E. Luke, Mississippi State University, Starkville, MS 1100 AIAA-2010-0128 Adjoint- Based Error Estimation for High Speed Flow Computations K. Duraisamy and J. Alonso, Stanford University, Stanford, CA; P. Chandrasekhar, TIFR-CAM, Bangalore, India 1130 AIAA-2010-0129 Non- Intrusive Polynomial Chaos Methods for Uncertainty Quantification in Fluid Dynamics S. Hosder, Missouri University of Science and Technology, Rolla, MO; and R. Walters, Virginia Polytechnic Institute and State University, Blacksburg, VA Session 18- GPSE-1 Space Agency Programs in Gravity-Dependent Research Grand Ballroom 13 Chaired by: F. KOHL and K. SACKSTEDER, NASA Glenn Research Center, Cleveland, OH 0800 Oral Presentation Advanced Capabilities Division Program Status and Outlook B. Neumann and J. Joshi, NASA Headquarters, Washington, DC 0830 AIAA-2010-0131 NASA Innovative Partnership Program D. Comstock, NASA Headquarters, Washington, DC 0900 AIAA-2010-0132 ISS as a National Laboratory M. Uhran, NASA Headquarters, Washington, DC 0930 AIAA-2010-0133 CSA Research Programs M. Dejmek, Agence Spatiale Canadienne/Canadian Space Agency, St. Hubert, Canada 1000 AIAA-2010-0134 Update of the German Microgravity Program in Physical Sciences R. Kuhl, German Aerospace Center (DLR), Bonn, Germany 1030 AIAA-2010-0135 JAXA's Strategy for Space Exploration and Research Program of Life and Physical Science M. Takayanagi, Japan Aerospace Exploration Agency (JAXA), Tsukuba, Ibaraki, Japan 1100 AIAA-2010-0136 CNES Research Program B. Zappoli, Centre National d’Études Spatiales (CNES), Toulouse, France 1130 AIAA-2010-0137 ESA Research Program O. Minster, ESA/ESTEC, Noordwijk, The Netherlands Session 19- GT-1 Future of Ground Testing Crystal Ballroom G1 Chaired by: F. STEINLE, and J. KEGELMAN, NASA Langley Research Center, Hampton, VA 0800 AIAA-2010-0138 A Historical Perspective of Design Requirements for AEDC's Propulsion Wind Tunnel and von Karman Facilities. D. Hiebert, Arnold Engineering Development Center, Arnold AFB, TN 0830 AIAA-2010-0139 Future Test Facility Capabilities Required To Re- Engineer the Aeronautical Development Process E. Kraft, Arnold Engineering Development Center, Arnold AFB, TN 0900 AIAA-2010-0140 Technical Workforce Needs for a New National Trisonic Ground Test Capability J. Best, Arnold Engineering Development Center, Arnold AFB, TN 0930 AIAA-2010-0141 A New Wind Tunnel Operations Concept for Expected 2020 Technology F. Jackson, Arnold Engineering Development Center, Arnold AFB, TN 1000 AIAA-2010-0142 Wind Tunnel Testing’s Future: A Vision of the Next Generation of Wind Tunnel Test Requirements and Facilities M. Melanson, Lockheed Martin Corporation, Fort Worth, TX 1030 AIAA-2010-0143 Ground Facility Testing in the 21st Century J. Kegelman, NASA Langley Research Center, Hampton, VA 1100 AIAA-2010-0145 Industry Expectations for Aerodynamic Test Facility Capabilities to Support Future Development Programs – A User Perspective L. McGill, Raytheon Company, Tuscon, AZ Session 20-GTE-1 0800 - 1200 Alternative Fuels - Government Funded Programs (Invited) Grand Ballroom 14 Chaired by: B. SEKAR and J. DATKO, U.S. Air Force Research Laboratory, Wright-Patterson AFB, OH Conventional aviation fuels are derived from petroleum-based crude oils. Increasing energy demand, cost and environmental concerns increase the need to seek alternate transportation fuels from natural gas, coal and biomass to achieve the goal of energy independence from petroleum-based energy sources. There has been considerable interest in recent years for alterative aviation fuels produced from non-petroleum sources. New technologies are being developed and supported by the Government and private enterprise to replace petroleum-based aviation fuels in a cost effective way. For example, natural gas or coal-liquid can be converted into paraffinic synthetic fuels using the Fischer-Tropsch (FT) process. Similarly, selective cracking and isomerization processes are used to produce paraffinic aviation grade synthetic jet fuels from biodiesel. As the new form of alternative fuels enter the aviation industry, a series of new engine technologies are also under development to use these fuels with the aim of achieving improved combustion stability and efficiency, and reduced emissions. As a result, there is a greater need for a coordinated strategic effort between the Government and private institutions to develop affordable and cost effective technologies for practical aviation applications. Therefore, this special topic will address the Government programs for the alternate fuel development and the technical efforts that are being currently pursued. Session 21- HAPB-1 Pulse Detonation Engines Crystal Ballroom E Chaired by: D. PAXSON, NASA Glenn Research Center, Cleveland, OH, and V. TANGIRALA, GE Global Research Center, Niskayuna, NY 0800 AIAA-2010-0146 Testing of a Rotating Detonation Wave Engine with Swirled Fuel Injection E. Braun, N. Dunn, and F. Lu, University of Texas, Arlington, Arlington, TX 0830 AIAA-2010-0147 Effects of a Catalyst Coating on a PDE Endothermic Fuel Heating System C. Stevens, P. King, and F. Schauer, U.S. Air Force Institute of Technology, Wright-Patterson AFB, OH; and J. Hoke, Innovative Scientific Solutions, Inc., Dayton, OH 0900 AIAA-2010-0148 Net Impulse Measurements of Pulse Detonation Tube by Using Fuel- Air Mixture S. Takeuchi, J. Kasahara and N. Doi, University of Tsukuba, Tsukuba, Japan; A. Matsuo, Keio University, Yokohama, Japan; M. Murayama, IHI, Tokyo, Japan 0930 AIAA-2010-0149 Unsteady Ejectors: The Physical Causes of a Thrust Augmentation of 2 R. Miller, Cambridge University, Cambridge, Great Britain 1000 AIAA-2010-0150 Numerical Investigation of Pre- Detonators for Pulse Detonation Engines R. Fievisohn and P. King, U.S. Air Force Institue of Technology, Wright-Patterson AFB, OH; F. Schauer, U.S. Air Force Research Laboratory, Wright-Patterson AFB, OH; J. Hoke and V. Katta, Innovative Scientific Solutions, Inc., Dayton, OH 1030 AIAA-2010-0151 Unsteady Flame Speed Control and DDT Transition Enhancement Using Fluidic Obstacles D. Forliti and B. Knox, State University of New York, Buffalo, Buffalo, NY; F. Schauer, U.S. Air Force Research Laboratory, Wright-Patterson AFB, OH; and J. Hoke, Innovative Scientific Solutions, Inc., Dayton, OH 1100 AIAA-2010-0152 Effect of Nozzle Shapes on the Performance of Continuously- Rotating Detonation Engine T. Yi, J. Lou and C. Turangan, Institute of High Performance Computing, Singapore, Singapore; B. Khoo, National University of Singapore, Singapore, Singapore; P. Wolanski, Warsaw University of Technology, Warsaw, Poland 1130 AIAA-2010-0153 Numerical Analysis of Threshold of Limit Detonation in Rotating Detonation Engine T. Yamada, K. Hayashi, and E. Yamada, Aoyama Gakuin University, Sagamihara, Japan; N. Tsuboi, Japan Aerospace Exploration Agency (JAXA), Sagamihara, Japan; V. Tangirala, General Electric Company, Niskayuna, NY; and T. Fujiwara, FF Labratory, Nagoya, Japan Session 22- HIS-1 History of Aviation Crystal Ballroom P Chaired by: S. EBERHARDT, The Boeing Company, Seattle, WA, and K. BURNS, Wyle Laboratories, San Diego, CA 0800 AIAA-2010-0154 Paleoaerodynamic Explorations Part I: Evolution of Biological and Technical Flight B. Kulfan, The Boeing Company, Seattle, WA 0830 AIAA-2010-0155 Paleoaerodynamic Explorations Part II: Options for Future Technology Innovations B. Kulfan, The Boeing Company, Seattle, WA 0900 AIAA-2010-0156 Gago Coutinho and the Aircraft Navigation F. Neves, J. Barata and A. Silva, Universidade Beira Interior, Covilhã, Portugal 0930 AIAA-2010-0157 The Centennial Events for 100 Years of Naval Aviation K. Burns, Wyle Laboratories, San Diego, CA; and R. Dann, U.S. Navy Reserve, O'Fallon, MO 1000 AIAA-2010-0158 To Boldly Go Where No Unmanned Aircraft Has Gone Before:A Half- Century of DARPA’s Contributions to Unmanned Aircraft M. Hirschberg, Centra Technology Inc, Arlington, VA 1030 AIAA-2010-0159 Tracing the Growth of U.S. Navy Aviation M. Spearman, NASA Langley Research Center, Hampton, VA 1100 AIAA-2010-0160 Historians, Practitioners, and Aerospace History: Past Performance and Future Prospects R. Hallion, Hallion Associates, Shalimar, FL Session 23- MVC-1 CFD Meshing Crystal Ballroom L Chaired by: A. SHIH, University of Alabama, Birmingham, Birmingham, AL, and A. IANNETTI, NASA Glenn Research Center, Cleveland, OK 0800 AIAA-2010-0161 A Surface Remeshing Approach R. Aubry, G. Houzeaux and M. Vazquez, BSC, Barcelona, Spain 0830 AIAA-2010-0162 Generation of Conjugate Meshes for Complex Geometries for Coupled Multi- Physics Simulations W. Dawes, Cambridge University, Cambridge, Great Britain; W. Kellar and S. Harvey, Cambridge Flow Solutions Ltd, Histon, Cambridge, Great Britain 0900 AIAA-2010-0163 Automatic Mesh Generation of Hybrid Mesh on Valves in Multiple Positions in Feedline Systems D. Ross, Y. Ito, F. Dorothy, and A. Shih, University of Alabama, Birmingham, Birmingham, AL; and J. Peugeot, NASA Marshall Space Flight Center, Marshall Space Flight Center, AL 0930 AIAA-2010-0164 A Classical Elasticity- Based Mesh Update Method for Moving and Deforming Meshes R. Smith, Naval Surface Warfare Center, Panama City, FL; and J. Wright, Streamline Numerics, Inc., Gainesville, FL 1000 AIAA-2010-0165 Explicit and Robust Inverse Distance Weighting Mesh Deformation J. Witteveen, Stanford University, Stanford, CA 1030 AIAA-2010-0166 Image- Based Computational Modeling of Complex Organisms and Biological Structures S. Dillard, J. Mousel, H. Udaykumar and J. Buchholz, University of Iowa, Iowa City, IA 1100 AIAA-2010-0167 An Improvement of Patched Grid by Using the High- Order Conservative Remapping Method Y. Zhang, H. Chen and S. Fu, Tsinghua University, Beijing, China (prc) Session 25- NSC-1 AIAA Foundation Masters Crystal Ballroom A Chaired by: N. BARLOW, U.S. Air Force Academy, U.S. Air Force Academy, CO 0800 AIAA-2010-0173 Experimental Methods for Impact of Composite Materials B. Gulker, Michigan State University, Lansing, MI 0830 AIAA-2010-0174 The Implicit Function Theorem with Applications in Dynamics and Control M. Harris and J. Valasek, Texas A&M University, College Station, TX 0900 AIAA-2010-0175 Flight Testing of a Prototype LOX/Propylene Upper Stage Engine D. Verma and K. Gemba, California State University Long Beach, Long Beach, CA 0930 AIAA-2010-0176 A "Free" Approach to Computational Aeroelasticity G. Romanelli, E. Serioli, and P. Mantegazza, Politecnico di Milano, Milan, Italy 1000 AIAA-2010-0177 Behavior of Magnetorheological Fluid Composites Employing Carrier Fluids Certified for Landing Gear Use L. Ahure and N. Wereley, University of Maryland, College Park, MD 1030 AIAA-2010-0178 Characteristics of Metal Combustion Obtained from Constant Volume Explosion Experiments P. Santhanam and E. Dreizin, New Jersey Institute of Technology, Newark, NJ 1100 AIAA-2010-0179 Unscented Kalman Filter for Thermal Parameter Identification M. Hazard, North Carolina State University, Charlotte, NC Session 26- NSC-2 AIAA Foundation Team Crystal Ballroom B Chaired by: C. TAVARES, The Boeing Company, St Louis, MO 0800 AIAA-2010-0180 Design, Fabrication, and Testing of a Surveillance/Attack UAV K. Albarado, Auburn University, Auburn, AL 0830 AIAA-2010-0181 High Performance Computing Implementation on a Risk Assessment Code J. Ocampo, C. Acosta, and H. Millwater, University of Texas, San Antonio, San Antonio, TX 0900 AIAA-2010-0182 FalconSAT- 3 and the Space Environment S. Gay and N. Schmiegel, U.S. Air Force Academy, Colorado Springs, CO 0930 AIAA-2010-0183 Design of a N20/HTPB Hybrid Rocket Motor Utilizing a Toroidal Aerospike Nozzle J. Dennis, F. Hernandez, S. Shark and J. Villarreal, Arizona State University, Tempe, AZ 1000 AIAA-2010-0184 Design and Construction of All- Composite UAVs Utilizing a Modified VARTM Process R. Vocke, T. Spiridonov and D. Pines, University of Maryland, Hyattsville, MD 1030 AIAA-2010-0185 Automated Pilot Control Assistance for a Micro- scale Helicopter J. Hudson, C. Weber, and P. Evans, Cornell University, Ithaca, NY Session 27- NSC-3 AIAA Foundation Undergraduate Crystal Ballroom C Chaired by: L. HANSEN, HRP Systems Inc, Rolling Hills Estates, CA 0800 AIAA-2010-0186 Fatigue Testing of Pneumatic Artificial Muscle Actuators M. Gentry and N. Wereley, University of Maryland, College Park, MD 0830 AIAA-2010-0187 Application of Proportional- Integral- Derivative Control to a Supersonic Wind Tunnel K. Busa, Syracuse University, Syracuse, NY 0900 AIAA-2010-0188 A Factorial Design Experiment to Analyze the Optical Strain Response of a Luminescent Photoelastic Coating D. Gerber, University of Alabama, Llincolnshire, IL; and J. Hubner, University of Alabama, Tuscaloosa, AL 0930 AIAA-2010-0189 A Study of Aircraft Wake Decay S. Lane, University of Notre Dame, Notre Dame, IN 1000 AIAA-2010-0190 Fatigue Study of a Nanocomposite Laminate J. Wilkerson, Texas A&M University, College Station, TX 1030 AIAA-2010-0191 Aerodynamic Investigation of NASA Crew Exploration Vehicle Forward Bay Cover Separation Characteristics B. Henicke and T. Yechout, U.S. Air Force Academy, Colorado Springs, CO 1100 AIAA-2010-0192 Bubble Behavior in Nucleate Boiling Experiment Aboard the Space Shuttle J. Koeln, J. Boulware and H. Ban, Utah State University, Logan, UT 1130 AIAA-2010-1599 Water Vapor Absorption Spectroscopy in a Simulated Helicopter Exhaust Using Vertical- Cavity Surface- Emitting Lasers L. Huynh and S. O'Byrne, University of New South Wales, Braddon, New South Wales, Australia Session 28- PC-1 Diagnostics and Measurements in Combustion Systems Crystal Ballroom F Chaired by: R. PITZ, Vanderbilt University, Nashville, TN, and Y. IKEDA, Imagineering Inc, Kobe, United States 0800 AIAA-2010-0193 Stability- Sensing in a Lean Direct Injection (LDI) Turbine Engine Combustor R. Bompelly, T. Lieuwen, and J. Seitzman, Georgia Institute of Technology, Atlanta, GA 0830 AIAA-2010-0194 Spray Structure of Aerated Liquid Jets Using Double- View Digital Holography K. Sallam, Oklahoma State University, Stillwater, OK; K. Lin, Taitech, Inc., Beavercreek, OH; and C. Carter, U.S. Air Force Research Laboratory, Wright-Patterson AFB, OH 0900 AIAA-2010-0196 A Second- Generation Aerosol Shock Tube for Combustion Research D. Haylett, D. Davidson and R. Hanson, Stanford University, Stanford, CA 0930 AIAA-2010-0197 Measurements of Extinction Limits and OH Radicals of Trimethylbenzene/n- Decane Diffusion Flames S. Won, W. Sun and Y. Ju, Princeton University, Princeton, NJ 1000 AIAA-2010-0198 Mulit- Species Measurements Behind Reflected Shock Waves in Hydrocarbons Using Laser Absorption D. Davidson, G. Pilla, A. Farooq, R. Cook, Z. Hong and R. Hanson, Stanford University, Stanford, CA 1030 AIAA-2010-0199 Velocity Measurements in Premixed Turbulent Flames and Thermophoresis S. Sattler, Union of Concerned Scientists USA, Boston, MA; F. Gouldin, Cornell University, Ithaca, NY 1100 AIAA-2010-0200 Numerical and Experimental Evaluation of the Optical Connectivity Technique for Measurement of Liquid Breakup Length in Atomizers G. Charalampous, Y. Hardalupas and A. Taylor, Imperial College London, London, Great Britain Session 29- PC-2 Large Eddy Simulation for Combustion Applications New Orleans Chaired by: J. OEFELEIN, Sandia National Laboratories, Livermore, CA, and E. MASTORAKOS, University of Cambridge, Cambride, United States 0800 AIAA-2010-0201 Unsteady Flame Embedding (UFE) Subgrid Model for Turbulent Premixed Combustion Simulations H. El-Asrag, J. Nave and A. Ghoniem, Massachusetts Institute of Technology, Cambridge, MA 0830 AIAA-2010-0202 Large Eddy Simulations of Supersonic Turbulent Reacting Flows A. Banaeizadeh, Z. Li and F. Jaberi, Michigan State University, East Lansing, MI 0900 AIAA-2010-0203 Large Eddy Simulation of Supersonic Combustion Using Direct Quadrature Method of Moments P. Donde, H. Koo, and V. Raman, University of Texas, Austin, Austin, TX 0930 AIAA-2010-0204 On Experimental Data for Validation of Large- Eddy Simulation of Evaporating Droplets in a Mxing Layer S. Radhakrishnan and J. Bellan, Jet Propulsion Laboratory, Pasadena, CA 1000 AIAA-2010-0205 Filtered Tabulated Chemistry for LES P. Auzillon, École Centrale Paris, Chatenay Malabry, France; R. Vicquelin, Gdf Suez, Saint Denis La Plaine, France; F. Benoît, O. Gicquel, N. Darabiha, and D. Veynante, École Centrale Paris, Chatenay Malabry, France 1030 AIAA-2010-0206 Large Eddy Simulations of Temporal Mixing Layers Under Supercritical Thermodynamic Conditions: O2/H2 E. Taskinoglu and J. Bellan, Jet Propulsion Laboratory, Pasadena, CA 1100 AIAA-2010-0207 The LES- ODT Model for Turbulent Combustion T. Echekki, North Carolina State University, Raleigh, NC 1130 AIAA-2010-0208 Large Eddy Simulation of LOX/GH2 Shear- Coaxial Jet Flame at Supercritical Pressure S. Matsuyama, J. Shinjo, S. Ogawa, and Y. Mizobuchi, Japan Aerospace Exploration Agency (JAXA), Chofu, Japan Session 30- PC-3 Liquid Injection and Atomization Los Angeles Chaired by: E. GUTMARK, University of Cincinnati, Cincinnati, OH, and A. AGRAWAL, University of Alabama, Tuscaloosa, AL 0800 AIAA-2010-0209 Operation and Control of a Pulsejet with High Pressure Liquid Fuel Injection A. Naples and J. Hoke, Innovative Scientific Solutions, Inc., Dayton, OH; D. Paxson, NASA Glenn Research Center, Cleveland, OH; and F. Schauer, U.S. Air Force Research Laboratory, Wright-Patterson AFB, OH 0830 AIAA-2010-0210 Investigation of Liquid Jet Atomization Using High Fidelity Eulerian- Lagrangian Simulation X. Li, M. Arienti and M. Soteriou, United Technologies Research Center, East Hartford, CT; M. Sussman, Florida State University, Tallahassee, FL 0900 AIAA-2010-0211 Atomization of A Superheated Jet Fuel J. Lee, M. Corn, and C. Fotache, United Technologies Corporation, East Hartford, CT; S. Gopalakrishnan and D. Schmidt, University of Massachusetts, Amherst, Amherst, MA 0930 AIAA-2010-0212 A Parametric Study of Primary Breakup of Turbulent Liquid Jets in Crossflow M. Pai, Stanford University, Standford, CA; O. Desjardins, University of Colorado Boulder, Boulder, CO; H. Pitsch, Stanford University, Stanford, CA 1000 AIAA-2010-0213 Operational Modeling of an Electrostatic Micro- Atomizer B. Spatafore, B. Van Poppel, and J. Daily, University of Colorado, Boulder, Boulder, CO 1030 AIAA-2010-0214 Liquid Fuel Jet in Crossflow –Trajectory Correlations Based on the Column Breakup Point Y. Gopala, M. Mar, O. Bibik, E. Lubarsky and B. Zinn, Georgia Institute of Technology, Atlanta, GA 1100 AIAA-2010-0215 On the Modeling of a Spray Impinging on a Surface A. Silva and J. Barata, Universidade Beira Interior, Covilhã, Portugal 1130 AIAA-2010-0216 Effect of Fuel Injection Location on Combustion Instability in a Dump Combustor R. Desai, Indian Institute of Technology, Madras, Ahmedabad, India; and S. Chakravarthy, Indian Institute of Technology, Madras, Chennai, India Session 31- PC-4 Turbulent Flames I Miami Chaired by: M. SMOOKE, Yale University, New Haven, CT, and C. BROPHY, Naval Postgraduate School, Monterey, CA 0800 AIAA-2010-0217 Numerical Simulation of Autoignition of a Diluted Hydrogen Plume in Co- Flowing Turbulent Hot Air S. Kerkemeier, C. Frouzakis and K. Boulouchos, Swiss Federal Institute of Technology, Zurich, Switzerland; E. Mastorakos, University of Cambridge, Cambridge, Great Britain 0830 AIAA-2010-0218 Direct Numerical Simulation of Non- Premixed Flame Extinction by Water Spray P. Arias and H. Im, University of Michigan, Ann Arbor, MI; P. Narayanan and A. Trouvé, University of Maryland, College Park, MD 0900 AIAA-2010-0219 Flame Structure and Turbulence- Chemistry Interaction of Lean Premixed Hydrogen- Methane- Air Mixtures X. Gao, M. Day, and J. Bell, Lawrence Berkeley National Laboratory, Berkeley, CA 0930 AIAA-2010-0220 Transitional Blowoff Behavior of Wake- Stabilized, Stratified Flames in Vitiated Flow S. Tuttle, S. Chaudhuri, S. Kostka, B. Cetegen, and M. Renfro, University of Connecticut, Storrs, CT 1000 AIAA-2010-0221 Autoignition of Low Temperature Heptane- Air Mixtures in a Turbulent Flow Reactor M. Christensen, A. Mouis, and R. Santoro, Pennsylvania State University, University Park, PA 1030 AIAA-2010-0222 Characterization and Sensitivity Analysis of a Turbulent Diffusion Flame in Diluted Hot Coflow Y. See and M. Ihme, University of Michigan, Ann Arbor, MI 1100 AIAA-2010-0223 Numerical and Experimental Study of A Gas Jet Diffusion Flame in A Venturi- Cascade Burner A. Qubbaj, University of Texas Pan-American, Edinburg, TX 1130 AIAA-2010-0224 Processes of Mixing and Burning in the Compact Combustor Under the Air Stream Swirling at the Entrance V. Strokin, V. Stepanov, and Y. Shikhman, CIAM, Moscow, Russia Session 32- PDL-1 Magnetohydrodynamic Numerical Simulations New York Chaired by: J. SHANG and H. YAN, Wright State University, Dayton, OH 0800 AIAA-2010-0225 Non- Equilibrium Ionized Flow Simulations Within Strong Electro- Magnetic Fields R. MacCormack, Stanford University, Stanford, CA 0830 AIAA-2010-0226 A Finite Volume Method for the Magnetohydrodynamic Equations on Unstructured Grids D. Spicer, Drexel University, Philadephia, PA; H. Luo, North Carolina State University, Raleigh, NC 0900 AIAA-2010-0227 Numerical Study of Magnetoaerodynamic Flow Around a Hemisphere N. Bisek and I. Boyd, University of Michigan, Ann Arbor, MI; and J. Poggie, U.S. Air Force Research Laboratory, Wright-Patterson AFB, OH 0930 AIAA-2010-0228 A Fifth- Order WENO Scheme for Non- Equilibrium Reacting Flow Simulations X. Wang and X. Zhong, University of California, Los Angeles, Los Angeles, CA 1000 AIAA-2010-0229 Low Magnetic Reynolds Number 3- D Hypersonic MHD Flow Using High- Order WENO Schemes J. Lee, M. Huerta and G. Zha, University of Miami, Coral Gables, FL 1030 AIAA-2010-0230 Parameter Study for Configuration of a Low Power Segmented Arc Heater J. Lee, G. Jeong and K. Kim, Seoul National University, Seoul, South Korea 1100 AIAA-2010-0231 Simulation Studies of Alternating- Current Microdischarges for Microthruster Applications H. Sitaraman and L. Raja, University of Texas, Austin, Austin, TX 1130 AIAA-2010-0232 The Effect of Magnetic Fields on Specific Thrust for the Allison J- 102 Engine with an MHD Generator T. Benyo, NASA Glenn Research Center, Cleveland, OH Session 33- TP-1 Non-Equilibrium Radiation Crystal Ballroom M Chaired by: B. DROLEN 0800 AIAA-2010-0233 Global Sensitivity Analysis of Nonequilibrium Plasma Flows M. Panesi, E. Prudencio, and S. Prudhomme, University of Texas, Austin, Austin, TX 0830 AIAA-2010-0234 Mixing of k- Distributions for Molecular Radiating Species in Hypersonic Nonequilibrium Flows A. Bansal, M. Modest and D. Levin, Pennsylvania State University , State College, PA 0900 AIAA-2010-0235 Comparative Analysis of Two- Temperature vs. Multi- Species, Multi- Temperature Modeling in Nonequilibrium Radiating Shock Layers C. Martin and R. Greendyke, U.S. Air Force Institute of Technology, Wright-Patterson AFB, OH 0930 AIAA-2010-0236 Role of Viscous Effects on NEQAIR Prediction of EAST Measurements E. McCorkle and H. Hassan, North Carolina State University, Harrisburg, NC 1000 AIAA-2010-0237 Analysis of Shock Layer Radiation in Vacuum- Ultraviolet Region for HAYABUSA Return Conditions G. Yamada, Univeristy of Tokyo, Kashiwa, Japan; H. Takayanagi, T. Suzuki, and K. Fujita, Japan Aerospace Exploration Agency (JAXA), Chofu, Japan 1030 AIAA-2010-0238 A Study of the Influence of Turbulent Fluctuations on the Thermal Radiation from Nonreacting Exhaust Plumes D. Blunck, M. Harvazinski, J. Gore and C. Merkle, Purdue University, West Lafayette, IN 1100 AIAA-2010-0239 Uncertainty Quantification of Radiative Heat Flux Modeling for Titan Atmospheric Entry S. Ghaffari, T. Magin and G. Iaccarino, Stanford University, Stanford, CA Session 34- TP-2 Orbiter Entry Aerothermo Flight Experiments: Recent Flight Testing Crystal Ballroom N Chaired by: T. HORVATH, NASA Langley Research Center, Hampton, VA, and C. CAMPBELL, NASA Johnson Space Center, Houston, TX 0800 AIAA-2010-0240 BLT Flight Experiment Overview and In- Situ Measurements B. Anderson, NASA Johnson Space Center, Houston , TX 0830 AIAA-2010-0241 The Hythirm Project: Flight Thermography of the Space Shuttle During Hypersonic Re- Entry T. Horvath, D. Tomek, S. Splinter, J. Zalameda, and P. Krasa, NASA Langley Research Center, Hampton, VA; R. Schwartz, ATK, Hampton, VA; D. Gibson, Johns Hopkins University Applied Physics Laboratory, Laurel, MD; and A. Tietjen, Computer Sciences Corporation, Kennedy Space Center, FL 0900 AIAA-2010-0242 Design and Implementation of the Boundary Layer Transition Flight Experiment on Space Shuttle Discovery T. Spanos, United Space Alliance, Kennedy Space Center, FL 0930 AIAA-2010-0243 Cast Glance Near Infrared Imaging Observations of the Space Shuttle During Hypersonic Re- entry S. Tack, Naval Air Systems Command, Pt. Mugu, CA; T. Horvath and D. Tomek, NASA Langley Research Center, Hampton, VA; H. Verstynen, Unisys Corporation, Hampton, VA; and E. Shea, Futron Corporation, Hampton, VA 1000 AIAA-2010-0244 HYTHIRM Radiance Modeling and Image Analyses in Support of STS- 119 and STS- 125 Space ShuttleHypersonic Re- Entries D. Gibson, T. Spisz, and J. Taylor, Johns Hopkins University Applied Physics Laboratory, Laurel, MD; J. Zalameda, T. Horvath, and D. Tomek, NASA Langley Research Center, Hampton, VA; A. Tietjen, Computer Sciences Corporation, Kennedy Space Center, FL; S. Tack, Naval Air Systems Command, Pt. Mugu, CA; and B. Bush, Raytheon/Photon Research Corp., La Jolla, CA 1030 AIAA-2010-0245 Calibration of a Near Infrared Imaging System for Thermographic Imaging of the Space Shuttle during Hypersonic Re- Entry J. Zalameda, T. Horvath, and D. Tomek, NASA Langley Research Center, Hampton, VA; A. Tietjen, Computer Sciences Corporation, Kennedy Space Center, FL; D. Gibson, Johns Hopkins University Applied Physics Laboratory, Laurel, MD; and D. Mercer, Aerospace Computing, Inc.,, Hampton, VA 1100 AIAA-2010-0246 Update to Orbiter Boundary Layer Transition Prediction Tool S. Berry, R. King, M. Kegerise, W. Wood and C. McGinley, NASA Langley Research Center, Hampton, VA 1130 AIAA-2010-0247 Roles of Engineering Correlations in Hypersonic Entry Boundary Layer Transition Prediction C. Campbell, NASA Johnson Space Center, Houston, TX Session 35- WE-1 Wind Turbine Control Algorithms Crystal Ballroom G2 Chaired by: M. LACKNER, University of Massachusetts, Amherst, MA, and A. WRIGHT, National Renewable Energy Laboratory, Golden, CO 0800 AIAA-2010-0248 Adaptive Disturbance Tracking Control for Wind Turbines M. Balas, Q. Li and R. Peterman, Univeristy of Wyoming, Laramie, WY 0830 AIAA-2010-0249 Modified Adaptive Control for Region 3 Operation in the Presence of Wind Turbine Structural Modes S. Frost, NASA Ames Research Center, Moffett Field, CA; M. Balas, University of Wyoming, Laramie, WY; A. Wright, National Renewable Energy Laboratory, Golden, CO 0900 AIAA-2010-0250 Combining Standard Feedback Controllers with Feedforward Blade Pitch Control for Load Mitigation in Wind Turbines F. Dunne and L. Pao, University of Colorado, Boulder, Boulder, CO; A. Wright, B. Jonkman, and N. Kelley, National Renewable Energy Laboratory, Golden, CO 0930 AIAA-2010-0251 Blade Pitch Control with Preview Wind Measurements J. Laks and L. Pao, University of Colorado, Boulder, Boulder, CO; and A. Wright, National Renewable Energy Laboratory, Golden, CO 1000 AIAA-2010-0252 Testing Further Controls to Mitigate Loads in the Controls Advanced Research Turbine A. Wright and L. Fingersh, National Renewable Energy Laboratory, Golden, CO; and K. Stol, University of Auckland, Auckland, New Zealand 1030 AIAA-2010-0253 The Impact of Higher Fidelity Models on Active Aerodynamic Load Control Fatigue Damage Reduction D. Berg, Sandia National Laboratories, Albuquerque, NM; and T. Barlas, Delft University of Technology, Delft, The Netherlands 1100 AIAA-2010-0254 Active Aerodynamic Blade Distributed Flap MIMO Control Design for Load Reduction on the UPWIND 5MW Wind Turbine D. Wilson, Sandia National Laboratories, Albuquerque, NM; T. Barlas, Delft University of Technology, Delft, The Netherlands; D. Berg, Sandia National Laboratories, Albuquerque, NM; and G. van Kuik, Delft University of Technology, Delft, The Netherlands 1130 AIAA-2010-1600 A Study of Dynamic Coupling and Composite Load Control for Wind Turbines J. Lazaro, M. Chakiath and K. Stol, University of Auckland, Auckland, New Zealand Session 36- WIG-1  /  PDL-2 Joint PDL/WIG/FD/TP Plasma Actuator Session I Grand Ballroom 1 Chaired by: O. AZAROVA, Russian Academy of Sciences, Moscow, Russia, and G. ELLIOTT, University of Illinois, Urbana, IL 0800 AIAA-2010-0256 Electrode Polarity Effects in Surface Plasma Discharges for Supersonic Flow Control Applications: a Computational Study S. Mahadevan and L. Raja, University of Texas, Austin, Austin, TX 0830 AIAA-2010-0257 Electrodynamic Control of Shock Interactions in a 25/55 Biconic Model in Hypersonic Flow K. Wasai and H. Makino, Tokai University, Hiratsuka, Japan; Y. Nagata, Universtiy of Tokyo, Tokyo, Japan; K. Yamada and T. Abe, Japan Aerospace Exploration Agency (JAXA), Sagamihara, Japan 0900 AIAA-2010-0258 The Development of Experimental Investigation of Magneto- Plasma Actuator for Supersonic Flows I. Mashek, V. Lashkov, and Y. Anisimov, Saint-Petersburg State University, Saint Petersburg, Russia; Y. Kolesnichenko and V. Brovkin, Russian Academy of Sciences, Moscow, Russia 0930 AIAA-2010-0259 High- Power Filamentary Pulse Discharge in Supersonic Flow S. Leonov and Y. Isaenkov, Russian Academy of Sciences, Moscow, Russia; and M. Shneider, Princeton University, Princeton, NJ 1000 AIAA-2010-0260 Active Steering of Shock Waves in Compression Ramp by Nonuniform Plasma S. Leonov, Russian Academy of Sciences, Moscow, Russia; F. Falempin, MBDA, Paris, France; and D. Yarantsev, Russian Academy of Sciences, Moscow, Russia 1030 AIAA-2010-0261 Shock Wave Dispersion on a Smooth Boundary for Extended Times of Interaction A. Markhotok, Maine Maritime Academy, Castine, ME; and S. Popovic, Old Dominion University, Norfolk, VA 1100 AIAA-2010-0262 Experimental Investigations on the Effect of a Pulsed Plasma in the Hypersonic Flow Around a Flat Plate R. Sriram, S. M. V., R. Narayan, S. Saravanan, G. Jagadeesh and K. Reddy, Indian Institute of Science, Bangalore, India Session 37- WIG-2  /  PDL-3 Plasma-Assisted Combustion I Grand Ballroom 2 Chaired by: C. CARTER, U.S. Air Force Research Laboratory, Wright-Patterson AFB, OH, and V. SHIBKOV, Moscow State University, Moscow, Russia 0800 AIAA-2010-0263 Plasma Assisted Flame Holding in Subsonic and Supersonic Flows (Invited) W. Kim, H. Do, M. Cappelli, and M. Mungal, , 0900 AIAA-2010-0264 Gradient Mechanism of Detonation Initiation for PDE Applications A. Rakitin, NEQLab Research BV, Delft, The Netherlands; and A. Starikovskii, Drexel University, Philadelphia, PA 0930 AIAA-2010-0265 Internal and External Ignition Under Condition of Combined Discharge V. Shibkov, L. Shibkova, A. Karachev and R. Konstantinovskij, Moscow State University, Moscow, Russia 1000 AIAA-2010-0266 Cavity Ignition and Flameholding in Ethylene- Air Flows by a Repetitively Pulsed Nanosecond Discharge A. Dutta, Z. Yin, and I. Adamovich, Ohio State University, Columbus, OH 1030 AIAA-2010-0267 Stable Plasma Formation in Flow of Propane- Air Mixture: Propagation and Transition to Explosion S. Kamenschikov, Moscow State University, Moscow, Russia 1100 AIAA-2010-0268 Millisecond Pulse Width Current- Voltage Induced Strong Perturbation of C3H8/air Flame J. Schmidt, Spectral Energies, LLC, Dayton, OH; and B. Ganguly, U.S. Air Force Research Laboratory, Wright-Patterson AFB, OH 1130 AIAA-2010-0269 Non- Selfmaintained Gas Discharge for Plasma Impact on Gas Flammable Mixtures V. Bychkov, S. Denisiuk, and V. Gudovich, Russian Academy of Sciences, Moscow, Russia; N. Ardelyan and K. Kosmachevskii, M.V. Lomonosov Moscow State University, Moscow, Russia Session 246- TES-4 Combustion I Crystal Ballroom K Chaired by: H. MONGIA, Purdue University, West Lafayette, IN, and N. SYRED, Cardiff University, Cardiff, Great Britain 0900 AIAA-2010-1353 Investigation of Non- Premixed and Premixed Distributed Combustion for GT Application V. Arghode, A. Gupta and K. Yu, University of Maryland, College Park, MD 0930 AIAA-2010-1354 Combustion Properties of Turbulent Canola Methyl Ester and Diesel Flames N. Dhamale, B. Goepfert, R. Parthasarathy and S. Gollahalli, University of Oklahoma, Norman, OK 1000 AIAA-2010-1355 Understanding of Chemical Kinetics in the Thermal Stage of Claus Process H. Selim and A. Gupta, University of Maryland, College Park, MD 1030 AIAA-2010-1356 Numerical Simulations of the Thermal Stage in Claus Process: Equilibrium and Kinetic Investigation N. Al Amoodi, A. Gupta, H. Selim, and M. Sassi, University of Maryland, College Park, MD; and A. Al Shoaibi, University of Maryland, College Park,, MD 1100 Oral Presentation Ignition of Methane- Hydrogen Mixtures at High Pressure B. Adhikary and S. Aggarwal, University of Illinois, Chicago, Chicago, IL 1300 - 1400 New Horizons Forum Keynote Address Crystal Ballroom H Distinguished Speaker: J. Randy Babbitt, Administrator, Federal Aviation Administration (Invited) 21st Century Air Transportation Management – Where Are We Headed? 1400 - 1630 New Horizons Forum Panel Discussion - Future of the Airspace: Issues and Solutions for NextGen and Beyond … Crystal Ballroom J1 The panel will discuss a variety of topics that are shaping access to the civil airspace, including the expectations for NextGen as an enabler, the new found urgency for change in airspace management, the evolving role of automation and its impact on the human controller; unmanned air systems and airspace access, expectations for flight safety in the 21st century, and more. Moderator: Victoria Cox,Senior Vice President for NextGen and Operations Planning, Air Traffic Organization, Federal Aviation Administration, Washington D.C Panelists: David W. Vos, Senior Director, Rockwell Collins Control Technologies, Warrenton, VA Gerald F. "Fred" Pease Jr., SES, Director of Air Operations and Executive Director of the Department of Defense Policy Board on Federal Aviation, Deputy Chief of Staff for Operations, Plans and Requirements, Headquarters U.S. Air Force, Washington, D.C Steve J. Vail, Senior Advisor, Global Air Traffic Operations, FedEx, Memphis TN Bill Shira, Vice President, Marketing and Sales Support, Gulfstream Aerospace Corporation, Savannah, GA Session 38- AA-4 Jet Noise I Washington Chaired by: D. MCLAUGHLIN, Pennsylvania State University, University Park, PA 1400 AIAA-2010-0270 Supersonic Jet Noise Prediction Using Non- Eddy Viscosity- Type LES Models N. Dittakavi, R. Kamakoti, P. Hu, S. Mao and H. Zhao, Advanced Dynamics Inc., Lexington, KY 1430 AIAA-2010-0271 Large- Eddy Simulations of Perfectly- Expanded Supersonic Jets: Quality Assessment and Validation S. Mendez, M. Shoeybi, A. Sharma, F. Ham, S. Lele and P. Moin, Stanford University, Stanford, CA 1500 AIAA-2010-0272 Numerical Simulation of Axisymmetric Jet Screech Tones Using a General Purpose Finite- Volume CFD Code K. Kurbatskii, ANSYS Inc., Lebanon, NH 1530 AIAA-2010-0273 Noise and Flowfield Characteristics of a Supersonic Jet Impinging on a Porous Surface A. Wiley, Florida A&M University-Florida State University, Tallahassee, FL; I. Choutapalli, Texas A&M University, College Station, TX; R. Kumar and F. Alvi, Florida A&M University-Florida State University, Tallahassee, FL 1600 AIAA-2010-0274 Large Eddy Simulation of Supersonic Impinging Jets A. Dauptain, G. Staffelbach, A. Roux, L. Gicquel, and T. Shoenfeld, CERFACS, Toulouse, France 1630 AIAA-2010-0275 Numerical Simulation of Broadband Shock- Associated Noise from A Circular Supersonic Jet J. Gao and X. Li, Beihang University, Beijing, China (prc) Session 39- ABP-2 Engine Systems and Optimization Crystal Ballroom D Chaired by: H. REEVE, United Technologies Research Center, East Hartford, CT, and W. WAINRIGHT, Piper, Vero Beach, FL 1400 AIAA-2010-0276 The Potential and Challenge of TurboElectric Propulsion for Subsonic Transport Aircraft A. Gibson, Empirical Systems Aerospace, Pismo Beach, CA; D. Hall and M. Waters, Empirical Systems Aerospace, Oceano, CA; P. Masson, Advanced Magnet Lab, Palm Bay, FL; B. Schiltgen and T. Foster, Empirical Systems Aerospace, Oceano, CA 1430 AIAA-2010-0277 Near Stall Flow Analysis in the Transonic Fan of the RTA Propulsion System C. Hah, NASA Glenn Research Center, Cleveland, OH 1500 AIAA-2010-0278 Statistical, Modular Systems Integration Using Combined Energy & Exergy Concepts J. Doty, University of Dayton, Dayton, OH; and J. Camberos, U.S. Air Force Research Laboratory, Wright-Patterson AFB, OH 1530 AIAA-2010-0279 Mission Performance Comparisons of Subsonic Airliners with Current and Future Propulsion Technologies B. Schiltgen and A. Gibson, Empirical Systems Aerospace, Pismo Beach, CA 1600 AIAA-2010-0280 Research on Switching Performance of an Aeroengine Control System J. Li, Northwestern Polytechnical University, Xi’an, China (prc) Session 40- AD-1 Subsonic Aircraft Design Crystal Ballroom K Chaired by: D. LEVY, Cessna Aircraft Company, Wichita, KS, and E. CRAMER, The Boeing Company, Seattle, WA 1400 AIAA-2010-0281 A Tradeoff Analysis of Future Small Aircraft Capacity from a Point- to- Point Operation Perspective J. Lewe, K. Meyer, T. Unton and D. Mavris, Georgia Institute of Technology, Atlanta, GA 1430 AIAA-2010-0282 Assessing New Aircraft and Technology Impacts on Fleet- Wide Environmental Metrics including Future Scenarios M. Mane, I. Tetzloff, A. Tyagi, P. Dikshit, J. Zhao and D. Agusdinata, Purdue University, West Lafayette, IN 1500 AIAA-2010-0283 A Design Methodology for Lifelong Aircraft Evolution D. Lim and D. Mavris, Georgia Institute of Technology, Atlanta, GA 1530 AIAA-2010-0284 Non- Symmetrical General Aviation Aircraft and Flight Control Law Design Using SEASIOM Software A. Khrabrov and M. Sidoryuk, TsAGI, Moscow, Russia 1600 AIAA-2010-0285 Parameter Estimation of Fundamental Technical Aircraft Information Applied to Aircraft Performance M. Vallone and R. McDonald, California Polytechnic State University, San Luis Obispo, CA 1630 AIAA-2010-0286 Fatigue Behaviour in Friction Stir Welded 2198- T8 Al- Li Alloy Joint for Integral Metal Fuselage Application Y. Ma, Cranfield University, Cranfield,, Great Britain; and W. Yang, First Aircraft Institute of AVIC-I, Xi'An City, China (prc) Session 41- AD-2 U.S. Air Force INVENT Program Crystal Ballroom L Chaired by: W. MASON, Virginia Polytechnic Institute and State University, Blacksburg, VA, and T. TAKAHASHI, Northrop Grumman Corporation, El Segundo, CA 1400 AIAA-2010-0287 An Overview of Basic Science Issues Related to INVENT M. Wolff, S. Iden, and P. Lamm, U.S. Air Force Research Laboratory, Wright-Patterson AFB, OH 1430 AIAA-2010-0288 Dynamic System Modeling Integration Opportunities – High Fidelity to Hardware in the Loop M. Corbett, U.S. Air Force Research Laboratory, Wright-Patterson AFB, OH; K. McCarthy and G. Russell, PCKA, West Lafayette, IN 1500 AIAA-2010-0289 Non- Equilibrium Thermodynamic Issues Related to On- Demand Systems M. von Spakovsky, Virginia Polytechnic Institute and State University, Blacksburg, VA; and D. Riggins, University of Missouri, Rolla, Rolla, MO 1530 AIAA-2010-0290 High Performance Electric Actuator Modeling and Experimental Issues M. Wolff and Q. Leland, U.S. Air Force Research Laboratory, Wright-Patterson AFB, OH 1600 AIAA-2010-0291 Issues Related to Micro Heat Exchanger Applications for Aircraft A. Heltzel, PCKA, West Lafayette, IN; and R. Watts, U.S. Air Force Research Laboratory, Wright-Patterson AFB, OH 1630 AIAA-2010-0292 Using Design of Experiments to Optimize Experimental and Computational Investigations of Energy Management M. Wolff, U.S. Air Force Research Laboratory, Wright-Patterson AFB, OH; and J. Doty, University of Dayton, Dayton, OH Session 42- AFM-2 Flight Dynamics and Flying Qualities Chicago Chaired by: K. SHWEYK, The Boeing Company, Huntington Beach, CA, and A. CRASSIDIS, Rochester Institute of Technology, Rochester, NY 1400 AIAA-2010-0293 Stability and Performance of a Light Unmanned Airplane in Ground Effect P. Boschetti, E. Cárdenas, A. Amerio and A. Arevalo, Universidad Simón Bolívar, Naiguatá, Vargas, Venezuela 1430 AIAA-2010-0294 Flight Performance Characteristics of a Tailless Folding Wing Morphing Aircraft T. Yue and L. Wang, Beijing University of Aeronautics and Astronautics, Beijing, China (prc); and J. Ai, First Aircraft Institute of AVIC-I, Xi'an, China (prc) 1500 AIAA-2010-0295 Developmental Flight Testing of the SPAARO UAV M. Cotting, A. Wolek, J. Murtha, and C. Woolsey, Virginia Polytechnic Institute and State University, Blacksburg, VA 1530 AIAA-2010-0296 Dynamic Stall Flight Research, T- 33 and Falcon 20 A. Brown, NRC Canada, Ottawa, Canada 1600 AIAA-2010-0297 Review of Pilot Modelling Techniques M. Lone and A. Cooke, Cranfield University, Cranfield, Bedfordshire, Great Britain 1630 AIAA-2010-0298 Evaluation of the Flying Qualities of a Half- Scale Unmanned Airplane via Flight Simulation P. González, Universidad Nacional Experimental Politécnica de la Fuerza Armada, Caracas, Miranda, Venezuela; P. Boschetti, E. Cárdenas and A. Amerio, Universidad Simón Bolívar, Naiguatá, Vargas, Venezuela Session 43- AMT-2 Spectroscopic and Scattering Techniques Miami Chaired by: T. ROSSMANN, and S. ZAIDI, Princeton University, Princeton, NJ 1400 AIAA-2010-0299 Laser Absorption Tomography for Determination of Spatially Resolved Water Concentration and Temperature E. Bryner and M. Sharma, University of Virginia, Charlottesville, VA; G. Diskin, NASA Langley Research Center, Hampton, VA; J. McDaniel, C. Goyne, M. Snyder, E. Martin, and R. Krauss, University of Virginia, Charlottesville, VA 1430 AIAA-2010-0300 Quantitative Laser- Induced Incandescence Measurements of Soot In Large Pool Fires S. Kearney, K. Frederickson and T. Grasser, Sandia National Laboratories, Albuquerque, NM 1500 AIAA-2010-0301 Fiber- Based Measurement of Bow- Shock Spectra for Reentry Flight Testing T. Schott, M. Munk, and G. Herring, NASA Langley Research Center, Hampton, VA, VA; and J. Grinstead, NASA Ames Research Center, Moffett Field, CA 1530 AIAA-2010-0302 Accuracy, Precision, and Scatter in TDLAS Measurements M. Brown, Innovative Scientific Solutions, Inc., Dayton, OH; D. Barone, U.S. Air Force Research Laboratory, Wright-Patterson AFB, OH; W. Terry, Innovative Scientific Solutions, Inc., Dayton, OH; T. Barhorst and S. Williams, U.S. Air Force Research Laboratory, Wright-Patterson AFB, OH 1600 AIAA-2010-0303 Mass- Flux Sensing via Tunable Diode Laser Absorption of Water Vapor L. Chang, J. Jeffries and R. Hanson, Stanford University, Stanford, CA 1630 AIAA-2010-0304 Hypersonic Flows Probing with a Compact Absorption Spectrometer Monitoring CO2 at 2.7µm R. Vallon and A. Mohamed, ONERA, Palaiseau, France; S. Paris and J. Meyers, von Kármán Institute for Fluid Dynamics, Rhode-Saint-Genèse, Belgium Session 44- AMT-3 Surface Measurement Techniques I Crystal Ballroom J1 Chaired by: V. CHANDRASEKHARAN, University of Florida, Gainesville, FL, and S. OLCMEN, University of Alabama, Tuscaloosa, AL 1400 AIAA-2010-0305 Measurement of Fluctuating Wall Pressures Beneath a Supersonic Turbulent Boundary Layer S. Beresh, J. Henfling, R. Spillers and B. Pruett, Sandia National Laboratories, Albuquerque, NM 1430 AIAA-2010-0306 MEMS Pressure Sensor Array for Aeroacoustic Analysis of the Turbulent Boundary Layer J. Krause and R. White, Tufts University, Medford, MA; M. Moeller, J. Gallman and G. Holup, Spirit AeroSystems Inc., Wichita, KS; R. DeJong, Calvin College, Grand Rapids, MI 1500 AIAA-2010-0307 Unsteady PSP Technique for Measuring Naturally- Disturbed Periodic Phenomena D. Yorita, H. Nagai, and K. Asai, Tohoku University, Sendai, Japan; and T. Narumi, Kyushu Institute of Technology, Kita-Kyushu, Japan 1530 AIAA-2010-0308 Fiber- Optic Pressure Sensor for Time- of- Flight Measurements of Detonation Wave K. Jagadevan, F. Lu, and H. Huang, University of Texas, Arlington, Arlington, TX 1600 AIAA-2010-0309 Determination of Transfer Function of Pressure- Sensitive Paint C. Klein, W. Sachs, and U. Henne, German Aerospace Center (DLR), Goettingen, Germany 1630 AIAA-2010-0310 Measurement of Hypersonic High- Enthalpy Boundary Layer Transition on 7- Degree Cone Model H. Tanno, T. Komuro, K. Sato, K. Itoh, M. Takahashi, M. Kodera, and K. Fujii, Japan Aerospace Exploration Agency (JAXA), Kakuda, Japan Session 45- APA-4 Applied CFD in Engineering Grand Ballroom 9 Chaired by: J. MARTEL, Jacobs Engineering, Eglin AFB, FL, and S. LEDOUX, The Boeing Company, Everett, WA 1400 AIAA-2010-0311 Process Improvement Through Tool Integration In Aero- Mechanical Design H. Briggs, Jet Propulsion Laboratory, Pasadena, CA 1430 AIAA-2010-0312 Rotor Wake Modeling with a Coupled Eulerian and Vortex Particle Method C. Stone and E. Duque, Intelligent Light, East Rutherford, NJ; C. Hennes, Vortex Consulting (LLC), Norman, OK 1500 AIAA-2010-0313 Computational Study - Aircraft Forebody Impact on Aerodynamic Forces Experienced During Pilot Ejection C. Tyler and M. Burkinshaw, U.S. Air Force Research Laboratory, Wright-Patterson AFB, OH 1530 AIAA-2010-0315 Loss Coefficient Estimation in a Controlled Diffusion Cascade Using Large Eddy Simulation A. McMullan and G. Page, Loughborough University, Loughborough, Great Britain 1600 AIAA-2010-0316 Develeopment of a Quadtree Based Multigrid Method for an Unstructured Viscous Flow Solver E. Mahmutyazicioglu, TUBITAK-SAGE, Ankara, Turkey; I. Tuncer and H. Aksel, Middle East Technical University, Ankara, Turkey Session 46- APA-5 Unsteady Aerodynamics I Grand Ballroom 10 Chaired by: J. GEORGE, Innovative Aerospace Solutions, North Hollywood, CA 1400 AIAA-2010-0317 A Study of the Skin Friction and Flow Separation Location on an Ellipsoidal Model Undergoing Constant- Yaw Turns with Roll Oscillation J. DeMoss and R. Simpson, Virginia Polytechnic Institute and State University, Blacksburg, VA 1430 AIAA-2010-0318 Aerodynamics of an Oscillating Wing in Ground Effect J. Molina and X. Zhang, University of Southampton, Southampton, Great Britain 1500 AIAA-2010-0319 Unsteady Force and Moment Measurements on a Non- Body of Revolution Vehicle Undergoing Oscillatory Roll S. Tanious and R. Simpson, Virginia Polytechnic Institute and State University, Blacksburg, VA 1530 AIAA-2010-0320 Experimental Study on Dynamic Instability of Re- Entry Capsule- Shaped Body using Pressure- Sensitive Paint D. Sugimoto, H. Nagai and K. Asai, Tohoku University, Sendai, Japan; K. Hiraki, Kyushu Institute of Technology, Kita-Kyushu, Japan 1600 AIAA-2010-0321 Vortex Structure Around Heaving Elastic Airfoils and Characteristics of Dynamic Thrust T. Kurinami, M. Fuchiwaki and K. Tanaka, Kyushu Institute of Technology, Iizuka, Japan 1630 AIAA-2010-0322 Unsteady Aerodynamics of Deformable Thin Airfoils W. Walker and M. Patil, Virginia Polytechnic Institute and State University, Blacksburg, VA Session 47- APA-6 Vortical/Vortex Flows Grand Ballroom 11 Chaired by: C. SHENG, Mississippi State University, Mississippi State, MS, and R. TRAMEL, Kord Technologies, Inc., Huntsville, AL 1400 AIAA-2010-0323 Effects of Leading- Edge Radius on Aerodynamic Characteristics of 50 Degree Delta Wings N. Verhaagen, Delft University of Technology, Delft, The Netherlands 1430 AIAA-2010-0324 A Method and Applications for Tracking Airplane Trailing Wakes Y. Yadlin, A. Shmilovich and R. Narducci, The Boeing Company, Huntington Beach, CA 1500 AIAA-2010-0325 Wind Tunnel Effects on Wingtip Vortices P. Durbin, X. Huang, H. Hu and H. Igarashi, Iowa State University, Ames, IA 1530 AIAA-2010-0326 Experimental Studies on Co- Axial Vortex Loops R. Mariani and K. Kontis, University of Manchester, Manchester, Great Britain 1600 AIAA-2010-0327 Unsteady Computations of a Ground Vortex R. Nunes, A. Silva and J. Barata, Universidade Beira Interior, Covilhã, Portugal 1630 AIAA-2010-0328 Comparison of Predictive Capabilities of DES and RANS Simulations of the Separated Flow Around a Circular Cylinder M. Xia, B. Song, D. Li and R. YE, Northwestern Polytechnical University, Xi'an, China (prc) Session 48- ASE-2 Space Flight Results and Lessons Learned Atlanta Chaired by: S. LAI, U.S. Air Force Research Laboratory, Hanscom AFB, MA, and D. FERGUSON, NASA Marshall Space Flight Center, Marshall Space Flight Center, AL 1400 AIAA-2010-0329 In- Situ O/N2 Ratios from the AFRL Mass Spectrometer on the TacSat2 Satellite J. Wise, J. Ballenthin, F. Marcos, and W. Thorn, U.S. Air Force Research Laboratory, Hanscom AFB, MA 1430 AIAA-2010-0330 Early Results from C/NOFS: Satellite and Radar Observations During a Convective Ionospheric Storm M. Kelley, Cornell University, Ithaca, NY; P. Roddy, D. Hunton, J. Retterer, and O. de La Beaujardiere, U.S. Air Force Research Laboratory, Hanscom Air Force Base, MA; and R. Ilma, Cornell University, Ithaca, NY 1500 AIAA-2010-0331 Dawn Depletions in the Equatorial Ionosphere as Observed by the C/NOFS Satellite O. De La Beaujardiere, U.S. Air Force Research Laboratory, Hanscom AFB, MA 1530 AIAA-2010-0332 The Effects of Eclipse- Exit Weather and Magnetic Latitude on ISS Rapid Charging Events D. Ferguson, P. Craven, and J. Minow, NASA Marshall Space Flight Center, Huntsville, AL; and K. Wright, Jr., University of Alabama, Huntsville, Huntsville, AL 1600 AIAA-2010-0333 Natural Environment and Aerospace Vehicles: Some Lessons Learned W. Vaughan, University of Alabama, Huntsville, Huntsville, AL; and D. Johnson, , Madison, AL 1630 AIAA-2010-1602 Flashover Plasma Characteristics on 5m2 Solar Array Panel Under Simulated Plasma Environment on Geostationary Orbit and Low Earth Orbit T. Okumura, Japan Aerospace Exploration Agency (JAXA), Tsukuba, Japan; T. Suzuki, Kyushu Institute of Technology, Kitakyushu, Japan; K. Nitta and M. Takahashi, Japan Aerospace Exploration Agency (JAXA), Tsukuba, Japan; and K. Toyoda, Kyushu Institute of Technology, Kitakyushu, Japan Session 49- ECS-1 Modeling the Performance of Energetic Materials Crystal Ballroom C   1400 AIAA-2010-0334 Modeling the Pyrotechnically- Induced Dissociation of Nitrous Oxide in Closed Vessels K. Rink, University of Idaho, Moscow, ID 1430 AIAA-2010-0335 A Modeling Study of Detonations Characterisitcs of Lead Azide H. Lee, Scot Incorporated, Downers Grove, IL 1500 AIAA-2010-0336 Atomistic Simulation Of the Aluminum Nanoparticle Oxidation Mechanism B. Henz, U.S. Army Research Laboratory, Aberdeen Proving Ground, MD; T. Hawa and M. Zachariah, University of Maryland, College Park, MD 1530 AIAA-2010-0337 A Simple Model for SiTV and AlTV Combustion S. Son, Purdue University, West Lafayette, IN Session 50- FD-7 Best Practice for the Industrial Application of Large Eddy Simulation New Orleans Chaired by: P. TUCKER, The Whittle Laboratory, Cambridge, Great Britain, and J. DEBONIS, NASA Glenn Research Center, Cleveland, OH 1400 Oral Presentation Status of Application of LES for Gas Turbine Analyses and Future Needs J. Coupland, Rolls-Royce, Derby, Great Britain; and M. Anand, Rolls-Royce, Indianapolis, 1430 AIAA-2010-0339 Best Practice for Industrial LES- Lessons from the Past and Future Possibilities A. Hutton, ERCOFTAC, Brussels, Belgium 1500 AIAA-2010-0340 On Application of Large Eddy Simulations for Gas Turbine Combustion System S. Hsieh, General Electric Company, Cincinnati, OH 1530 AIAA-2010-0341 European LESAID Activity and Best Practice B. Guerts, University of Twente, Enschede, The Netherlands 1600 AIAA-2010-0342 Towards Improved Understanding or Airframe Noise Sources Using Detached Eddy Simulation R. Langtry, The Boeing Company , Seattle, WA 1630 AIAA-2010-0343 Application of LES Methods to Military Aircraft Flow Problems B. Smith, Lockheed Martin Aeronautics, Fort Worth, TX Session 51- FD-8 Circulation Control Research and Applications Boston Chaired by: M. ROGERS, NASA Ames Research Center, Moffett Field, CA, and R. WAHLS, NASA Langley Research Center, Hampton, VA 1400 AIAA-2010-0344 NASA High- Reynolds- Number Circulation Control Research - Overview of CFD and Planned Experiments W. Milholen, G. Jones and M. Cagle, NASA Langley Research Center, Hampton, VA 1430 AIAA-2010-0345 Experimental Development of CC Airfoils and Pneumatic Powered Lift Systems R. Englar, G. Blaylock, and R. Gaeta, Georgia Institute of Technology, Atlanta, GA; G. Jones and W. Milholen, NASA Langley Research Center, Hampton, VA 1500 AIAA-2010-0346 An Investigation of Unsteady and Steady Blowing for a 2- D Circulation Control Airfoil D. Wetzel, A. Jones, F. Liu, A. Edstrand, M. Chandran and L. Cattafesta, University of Florida, Gainesville, FL 1530 AIAA-2010-0347 Calculation of the Turbulence Characteristics of Flow Around a Circulation Control Airfoil Using LES T. Nishino, NASA Ames Research Center, Moffett Field, CA; S. Hahn, Stanford University, Stanford, CA; K. Shariff, NASA Ames Research Center, Moffett Field, CA 1600 AIAA-2010-0348 Overview of Recent Circulation Control Modeling Activities at Cal Poly D. Marshall, California Polytechnic State University, San Luis Obispo, CA 1630 AIAA-2010-0349 Enabling Speed- Agile Mobility for the Air Force C. Zeune, U.S. Air Force Research Laboratory, Wright-Patterson AFB, OH Session 52- FD-9 Compressible Turbulence Grand Ballroom 3 Chaired by: G. BLAISDELL, and W. KIM, Pratt & Whitney, East Hartford, CT 1400 AIAA-2010-0350 Decay of Compressible Homogeneous Turbulence with Multi- Temperature Non- Equilibrium W. Liao, Y. Peng and L. Luo, Old Dominion University, Norfolk, VA 1430 AIAA-2010-0351 Detonation Turbulence Interaction H. Nagarajan, L. Massa, and F. Lu, University of Texas, Arlington, Arlington, TX 1500 AIAA-2010-0352 Numerical Simulation of Mixing in Compressible Multicomponent Shock Accelerated Flows Using Localized Artificial Diffusivity Method S. Shankar, S. Kawai and S. Lele, Stanford University, Stanford, CA 1530 AIAA-2010-0353 DNS of Hypersonic Turbulent Boundary Layers Varying Freestream Mach Number L. Duan and P. Martin, Princeton University, Princeton, NJ 1600 AIAA-2010-0354 Effect of Turbulent Fluctuations on Radiative Heat Flux in Hypersonic Boundary Layers L. Duan and N. Grube, Princeton University, Princeton, NJ; I. Sohn, Pennsylvania State University, University Park, PA; P. Martin, Princeton University, Princeton, NJ; M. Modest and D. Levin, Pennsylvania State University, University Park, PA 1630 AIAA-2010-0355 DNS of a Spatial ly Evolving Transitional/Turbulent Boundary Layer at M=2.0 Y. Tokura, Hiroshima University, Hiroshima, Japan; H. Maekawa, University of Electro-Communications, Chofu, Japan; D. Watanabe, Toyama University, Toyama, Japan; and Y. Ogata, Hiroshima University, Hiroshima, Japan Session 53- FD-10 Feedback Flow Control Grand Ballroom 4 Chaired by: J. SEIDEL, U.S. Air Force Academy, U.S. Air Force Academy, CO, and F. CANNELLE, Northrop Grumman Corporation, El Segundo, CA 1400 AIAA-2010-0356 Feedback Flow Control of a Shear Layer for Aero- Optic Applications J. Seidel, S. Siegel, and T. McLaughlin, U.S. Air Force Academy, U.S. Air Force Academy, CO 1430 AIAA-2010-0357 Feedback Stabilization of High- Lift State for A Low- Aspect- Ratio Wing K. Taira and C. Rowley, Princeton University, Princeton, NJ; T. Colonius, California Institute of Technology, Pasadena, CA 1500 AIAA-2010-0358 Closed- Loop Control of a Wing in an Unsteady Flow D. Williams and W. Kerstens, Illinois Institute of Technology, Chicago, IL; J. Pfeiffer and R. King, Technische Universität Berlin, Berlin, Germany; G. Tadmor, Northeastern University, Boston, MA; and T. Colonius, California Institute of Technology, Pasadena, CA 1530 AIAA-2010-0359 A Temporal Proper Orthogonal Decomposition (TPOD) Method for Closed- Loop Flow Control S. Gordeyev and F. Thomas, University of Notre Dame, Notre Dame, IN 1600 AIAA-2010-0360 Feedback Flow Control for a Pitching Turret (Part I) H. Carlson and V. Thirunavukkarasu, Clear Science Corp., Harford, NY; R. Wallace, P. Shea and M. Glauser, Syracuse University, Syracuse, NY 1630 AIAA-2010-0361 Feedback Flow Control for a Pitching Turret (Part II) R. Wallace, P. Shea and M. Glauser, Syracuse University, Syracuse, NY; V. Thirunavukkarasu and H. Carlson, Clear Science Corp., Harford, NY Session 54- FD-11 High Order Methods I Grand Ballroom 5 Chaired by: C. RUMSEY, and N. DOMEL 1400 AIAA-2010-0362 A Hybridizable Discontinuous Galerkin Method for the Incompressible Navier- Stokes Equations N. Nguyen and J. Peraire, Massachusetts Institute of Technology, Cambridge, MA; and B. Cockburn, Univeristy of Minneostta, Minneapolis, MN 1430 AIAA-2010-0363 Hybridizable Discontinuous Galerkin Methods for the Compressible Navier- Stokes Equations J. Peraire and N. Nguyen, Massachusetts Institute of Technology, Cambridge, MA; and B. Cockburn, Univeristy of Minneostta, Minneapolis, MN 1500 AIAA-2010-0364 A Reconstructed Discontinuous Galerkin Method for the Compressible Navier- Stokes equations on Arbitrary Grids H. Luo and L. Luo, North Carolina State University, Raleigh, NC; R. Nourgaliev and V. Mousseau, Idaho National Laboratory, Idaho Falls, ID 1530 AIAA-2010-0365 Automated Quadrature Free Discontinuous Galerkin Method with a Tailored Recovery Formulation M. Galbraith and P. Orkwis, University of Cincinnati, Cincinnati, OH; and J. Benek, U.S. Air Force Research Laboratory, Wright-Patterson AFB, OH 1600 AIAA-2010-0366 A Parallel Reconstructed Discontinuous Galerkin Method for Compressible Flows on Arbitrary Grids H. Luo and A. Ali, North Carolina State University, Raleigh, NC; R. Nourgaliev and V. Mousseau, Idaho National Laboratory, Idaho Falls, ID 1630 AIAA-2010-0367 Unsteady Discrete Adjoint Formulation for High- Order Discontinuous Galerkin Discretizations in Time- Dependent Flow Problems L. Wang, University of Tennessee Chattanooga , Chattanooga, TN; D. Mavriplis, University of Wyoming, Laramie, WY; K. Anderson, University of Tennessee Chattanooga , Chattanooga, TN Session 55- FD-12 Injection/Mixing Flows for Combustion Crystal Ballroom F Chaired by: D. CULLEY and N. GEORGIADIS, NASA Glenn Research Center, Cleveland, OH 1400 AIAA-2010-0368 Effect of Parameter Variation on Nonuniformities in Gas- Centered Swirl- Coaxial Injectors S. Schumaker, S. Danczyk, and M. Lightfoot, U.S. Air Force Research Laboratory, Edwards AFB, CA 1430 AIAA-2010-0369 Further Studies on the Effect of Jet Recess in Coaxial Jet Mixing Under Acoustic Excitation S. Teshome, University of California, Los Angeles, Los Angeles, CA; J. Graham, I. Leyva, and D. Talley, U.S. Air Force Research Laboratory, Edwards AFB, CA 1500 AIAA-2010-0370 LES/RANS Simulation of a Supersonic Reacting Wall Jet J. Edwards, North Carolina State University, Raleigh, NC 1530 AIAA-2010-0371 Contrast Between Steady and Time- Averaged Unsteady Combustion Simulations C. Lian and C. Merkle, Purdue University, West Lafayette , IN 1600 AIAA-2010-0372 Direct Numerical Simulation of Electrohydrodynamic Atomization B. Van Poppel, O. Desjardins, and J. Daily, University of Colorado, Boulder, Boulder, CO Session 56- FD-13 Instability and Transition: Effects of Roughness Tampa Chaired by: G. DALE, U.S. Air Force, Wright-Patterson AFB, OH, and A. DRAKE 1400 AIAA-2010-0373 An Approach to Measuring Step Excrescence Effects in a Pressure Gradient A. Bender, J. Elliott, Y. Shinagawa, and A. Korntheuer, Northrop Grumman Corporation, El Segundo, CA; and A. Drake, Northrop Grumman Corporation, San Diego, CA 1430 AIAA-2010-0374 The Influence of Surface Steps on Transition in Pressure gradient Boundary Layers S. Gerashchenko and B. McKeon, California Institute of Technology, Pasadena, CA; R. Westphal, California Polytechnic State University, San Luis Obispo, CA; A. Bender and A. Drake, Northrop Grumman Corporation, El Segundo, CA 1500 AIAA-2010-0375 Step Excrescence Effects for Manufacturing Tolerances on Laminar Flow Wings A. Drake, A. Bender, and A. Korntheuer, Northrop Grumman Corporation, El Segundo, CA; R. Westphal, California Polytechnic State University, San Luis Obsipo, CA; W. Rohe and G. Dale, U.S. Air Force Research Laboratory, Wright-Patterson AFB, OH 1530 AIAA-2010-0376 Effect of Three- Dimensional Surface Perturbations on Boundary Layer Transitional Characteristics J. Early, Queen's University Belfast, Belfast, Northern Ireland; H. Medina, Coventry University, Coventry, Great Britain; R. McRoberts, Queen's University Belfast, Belfast, Northern Ireland 1600 AIAA-2010-0377 Direct Numerical Simulation of Distributed Roughness on a Swept Wing Leading Edge D. Rizzetta and M. Visbal, U.S. Air Force Research Laboratory, Wright-Patterson AFB, OH; H. Reed and W. Saric, Texas A&M University, College Station, TX 1630 AIAA-2010-0378 Excitation of Crossflow Instabilities in a Swept Wing Boundary Layer M. Carpenter, M. Choudhari, F. Li, C. Streett and C. Chang, NASA Langley Research Center, Hampton, VA Session 57- FD-14 Joseph A. Schetz Invited Session: Celebrating 45 Years of Graduate Education Grand Ballroom 2 Chaired by: W. PULLIAM, DARPA, Arlington, VA, and S. MAGILL, Talon Aircraft Holding GmbH, , Germany 1400 AIAA-2010-0379 Diamond Port Injector Gasdynamic Flame Holding Studies (Invited Paper) R. Srinivasan, Ramgen Power Systems, Bellevue, WA; K. Kobayashi, Japan Aerospace Exploration Agency (JAXA), Tsukuba, Japan; C. Carter, U.S. Air Force Research Laboratory, Wright-Patterson AFB, OH; and R. Bowersox, Texas A&M University, College Station, TX 1430 AIAA-2010-0380 Injectant Molecular Weight Effects in Circular Scramjet Combustors C. Rock and J. Schetz, Virginia Polytechnic Institute and State University, Blacksburg, VA; and R. Ungewitter, CRAFT Tech, Inc., Pipersville, PA 1500 AIAA-2010-0382 Study of Bow- Shock Wave Unsteadiness in Hypervelocity Flow from Reservoir Fluctuations E. Marineau, CUBRC, Buffalo, NY; and H. Hornung, California Institute of Technology, Pasadena, CA 1530 AIAA-2010-0383 Adaptiviy, Sensitivity, and Uncertainty: towards rigorous Verification and Validation in Flow Simulations D. Pelletier, , 1600 AIAA-2010-0384 Invited Paper for Joseph A Schetz Session D. Deturris, , , United States Session 58- FD-15 Pitching and Plunging Wing Aerodynamics Crystal Ballroom B Chaired by: M. OL, U.S. Air Force Research Laboratory, Wright-Patterson AFB, OH, and H. DONG, Wright State University, Dayton, OH 1400 AIAA-2010-0385 Experiments and Computation on a Low Aspect Ratio Pitching Flat Plate Y. Lian, University of Louisville, Louisville, KY; and M. Ol, U.S. Air Force Research Laboratory, Wright-Patterson AFB, OH 1430 AIAA-2010-0386 Lift Enhancement of a Rectangular Wing Undergoing a Small Amplitude Plunging Motion D. Calderon, Z. Wang and I. Gursul, University of Bath, Bath, Great Britain 1500 AIAA-2010-0387 Low Reynolds Number Unsteady Aerodynamic over a Pitching- Plunging Flat Plate A. Hart and L. Ukeiley, University of Florida, Shalimar, FL 1530 AIAA-2010-0388 Experimental Study of Strouhal Number Effects on Fluid Dynamics of Pitching and Plunging Airfoil Y. Baik, J. Rausch, L. Bernal, and W. Shyy, University of Michigan, Ann Arbor, MI; and M. Ol, U.S. Air Force Research Laboratory, Wright-Patterson AFB, OH 1600 AIAA-2010-0389 Fluid Dynamics of Rigid and Flexible Lifting Flat Plates in Pitch- Plunge Motion at Low Reynolds Numbers J. Rausch, Y. Baik, and L. Bernal, University of Michigan, Ann Arbor, MI; and M. Ol, U.S. Air Force Research Laboratory, Wright-Patterson AFB, OH 1630 AIAA-2010-0390 Vortex Mode Bifurcation and Lift Force of a Plunging Airfoil at Low Reynolds Numbers D. Cleaver, Z. Wang and I. Gursul, University of Bath, Bath, Great Britain Session 59- GPSE-2 NASA ISS Research Program Overviews Grand Ballroom 6 Chaired by: S. TSE, Rutgers University, Piscataway, NJ, and F. KOHL, NASA Glenn Research Center, Cleveland, OH 1400 AIAA-2010-0391 Science on the International Space Station in the Final Year of Assembly J. Robinson, NASA Johnson Space Center, Houston, TX; and T. Ruttley, NASA Headquarters, Washington, DC 1430 AIAA-2010-0392 ISS Research in Fluid Physics and Transport: Status, Recent Results and Future Plans B. Motil, NASA Glenn Research Center, Cleveland, OH 1500 AIAA-2010-0393 Microgravity Combustion and Reacting Systems: Status, Recent Results and Applications to Exploration Systems D. Urban, K. Sacksteder, G. Ruff and D. Dietrich, NASA Glenn Research Center, Cleveland, OH 1530 AIAA-2010-0394 US Materials Science on ISS: Status and Plans F. Szofran, NASA Marshall Space Flight Center, Huntsville, AL 1600 AIAA-2010-0395 Fundamental Space Biology: Past, Present, and Future S. Sun, NASA Ames Research Center, Moffet Field, CA 1630 Oral Presentation Status on Current Spaceflight and Ground- Based NASA Plant Studies H. Levine and R. Wheeler, NASA Kennedy Space Center, Kennedy Space Center, FL; and J. Cohen, NASA Headquarters, Washington, DC Session 60- GT-2 Aerodynamic Ground Testing Crystal Ballroom G1 Chaired by: R. WHITE, ViGYAN Inc, Hampton, VA, and T. WAYMAN 1400 AIAA-2010-0397 Low- Speed Wind Tunnel Blockage: Wake Aerodynamics of Vertical- Axis Wind Turbines I. Ross and A. Altman, University of Dayton, Dayton, OH; D. Bowman and T. Mooney, UDRI, Dayton, OH; D. Bogart, Twenty First Century Energy LLC, Fairborn, OH 1430 AIAA-2010-0398 Influence of Wing Elasticity on Dynamic Derivatives of Transport Aircraft T. Loeser, DNW, Braunschweig, Germany; and A. Hübner, German Aerospace Center (DLR), Braunschweig, Germany 1500 AIAA-2010-0399 Boundary Layer Trips for Low Reynolds Number Wind Tunnel Tests A. Rona, University of Leicester, Leicester, Great Britain; H. Soueid, Altran Technologies, Toulouse, France 1530 AIAA-2010-0400 Unstable At All Speeds: Flight Testing the 1903 Wright Flyer in 2003 N. Crabill, ViGYAN Inc., Hampton, VA; K. Hyde, Wright Experience, Warrenton, VA 1600 AIAA-2010-0401 Exploring the Effects of Freestream Turbulence on Sphere Drag Transition C. Lamb, Massachusetts Institute of Technology, Arlington, MA 1630 Oral Presentation Transonic Tunnel Comparison Test S. Helland, NASA Glenn Research Center, Cleveland, OH; and C. Henson, NASA Langley Research Center, Hampton, VA Session 61- GTE-2 Gas Turbine Engines - Turbines I Grand Ballroom 13 Chaired by: I. HALLIWELL, Avetec, Springfield, OH, and R. GAETA, Georgia Institute of Technology, Smyrna, GA 1400 AIAA-2010-0403 Prediction of Heat Transfer Characteristics of Turbine Rotor Pedestal Arrays T. Barber, G. Philbrick and D. Gindraux, University of Connecticut, Storrs, CT 1430 AIAA-2010-0404 Prediction of Adiabatic Effectiveness of Various Cratered Film Hole Configurations: Sensitivity Analysis for the Elliptical Shaped Mask C. Nguyen, N. Tran and J. Kapat, University of Central Florida, Orlando, FL 1500 AIAA-2010-0405 Applying Response Surface Methodology on a Trenched Film Cooling Effectiveness for a Real Cascade Annual Endwall C. Nguyen, University of Central Florida, Orlando, FL 1530 AIAA-2010-0406 Effect of Hole Shape on Blade Cooling Effectiveness J. Yao, S. Sian, J. Khan and Y. Yao, Kingston University, London, Great Britain 1600 AIAA-2010-0407 Side Wall Heat Transfer Augmentation in a Narrow Rectangular Channel with Dimples Applied to the Bottom Wall C. Slabaugh, L. Tran, and J. Kapat, University of Central Florida, Orlando, FL 1630 AIAA-2010-0408 Effects of Incidence Angle on Performance M. Creason, Rolls-Royce, , United States Session 62-GTE-3 1400 - Pressure-Gain Combustion for the Gas Turbine (Invited) Grand Ballroom 14 Chaired by: M. NALIM, Indiana University-Purdue University Indianaoplis, Carmel, IN, and D. PAXSON, NASA Glenn Research Center, Cleveland, OH There has been significant recent progress in developing non-steady pressure-gain combustors to enable engines to reduce fuel consumption and boost performance significantly. The theoretical potential of constant-volume combustion has led to investigation of various devices that approach this ideal, such as pulse detonation engines, wave rotors, and pulse combustors. This session aims to provide an overview of the advantages and challenges of these combustors, and the needed research to make them successful in gas turbine and aircraft engine core applications. Session 63- HAPB-2 Ramjet/Scramjet Simulation with URANS/LES/DES I Grand Ballroom 12 Chaired by: B. SEKAR, U.S. Air Force Research Laboratory, Wright-Patterson AFB, OH, and J. DRUMMOND, NASA Langley Research Center, Hampton, VA 1400 AIAA-2010-0409 Ignition Transient in an Ethylene Fueled Scramjet Engine with Air Throttling Part I: Non- Reacting flow Development and Mixing J. Li, F. Ma, J. Choi, and V. Yang, Pennsylvania State University, State College, PA; and K. Lin, Taitech, Inc., Beavercreek, OH 1430 AIAA-2010-0410 Ignition Transient in an Ethylene Fueled Scramjet Engine with Air Throttling Part II: Ignition and Flame Development J. Li, F. Ma, J. Choi, and V. Yang, Pennsylvania State University, State College, PA; and K. Lin, Taitech, Inc., Beavercreek, OH 1500 AIAA-2010-0411 Supersonic Combustor Simulations Using a Hybrid RANS/LES Approach D. Peterson and G. Candler, University of Minnesota, Minneapolis, MN 1530 AIAA-2010-0412 High Fidelity Numerical Analysis of a Fully Coupled Circular Scramjet Configuration F. Malo-Molina and D. Gaitonde, U.S. Air Force Research Laboratory, Wright-Patterson AFB, OH; and H. Ebrahimi, SEA, Carson City, NV 1600 AIAA-2010-0413 Numerical Comparison of Scramjet Combustor with Unsteady RANS and LES Simulation H. Ebrahimi, Software and Engineering Associate, Inc., Carson City, NV; F. Malo-Molina and D. Gaitonde, U.S. Air Force Research Laboratory, Wright-Patterson AFB, OH 1630 AIAA-2010-0414 Large- Eddy Simulation of Cavity Flame- Holding in a Mach 2.5 Cross Flow J. Choi, C. Ghodke and S. Menon, Georgia Institute of Technology, Atlanta, GA Session 64- IS-1 Intelligent Flight Planning and Guidance Crystal Ballroom Q Chaired by: L. LONG, Pennsylvania State University, University Park, PA, and E. ATKINS, University of Michigan, Ann Arbor, MI 1400 AIAA-2010-0415 3- D Flight Plan for an Autonomous Aircraft Y. Bestaoui, Université d’Evry, Evry, France 1430 AIAA-2010-0416 Trim State Discovery for an Adaptive Flight Planner G. Yi, University of Michigan, Ann Arbor, MI 1500 AIAA-2010-0417 Effective Fuzzy Logic Based Path Planning for a Wildland Fire- fighting Aircraft C. Sabo, K. Cohen, M. Kumar and S. Abdallah, University of Cincinnati, Cincinnati, OH 1530 AIAA-2010-0418 Dynamic Flight Plan Design for UAS Remote- SensingApplications S. Marc, E. Santamaria, C. Barrado and E. Pastor, Technical University of Catalonia, Barcelona, Spain 1600 AIAA-2010-0419 Fusion of Radar and Irst Measurements for Maneuvering Target Tracking V. Naidu, National Aerospace Laboratories, Bangalore, India 1630 AIAA-2010-0420 Synergistic Computing: Combining CFD and Neural Networks for Maneuvering Simulation W. Faller, Applied Simulation Technologies, Cocoa Beach, FL; D. Hess, K. Junghans, and J. Lewis, Naval Surface Warfare Center, Bethesda, MD Session 65- PC-5 Drops and Sprays I Los Angeles Chaired by: J. GREENBERG, Technion - Israel Institute of Technology, Haifa, United States, and P. LE CLERCQ, German Aerospace Center, Stuttgart, United States 1400 AIAA-2010-0421 Thixotropic Behavior of Hydrocarbon/SiO2 Gels R. Arnold, T. Kubal and W. Anderson, Purdue University, West Lafayette, IN 1430 AIAA-2010-0422 Experimental Investigation of Gelled Monomethylhydrazine (MMH) R. Arnold and W. Anderson, Purdue University, West Lafayette, IN 1500 AIAA-2010-1595 Effect of Near Injector Heat Release on Atomization and Heat Transfer in a Rocket Engine J. Deeken, D. Suslov, and O. Haidn, German Aerospace Center (DLR), Lampoldshausen, Germany 1530 AIAA-2010-0425 Edge Flames with a Fuel Spray and Reactants Having Different Diffusivities J. Greenberg and Y. Mindelis, Technion-Israel Institute of Technology, Haifa, Israel; and M. Matalon, University of Illinois, Urbana-Champaign, Urbana, IL 1600 AIAA-2010-0426 Decomposition and Ignition Characteristics of Liquid GAP R. Kaya, Nihon University, Funabash, Japan; Y. Okuda, G. Tamura, M. Tanabe, and T. Kuwahara, Nihon University, Funabashi, Japan Session 66- PC-6 Turbulent Flames II New York Chaired by: H. IM, and C. CADOU, University of Maryland, College Park, MD 1400 AIAA-2010-0427 Investigation into Combustion Instability Control by Microjet Actuation S. Shanbhogue, Z. LaBry, R. Speth and A. Ghoniem, Massachusetts Institute of Technology, Cambridge, MA 1430 AIAA-2010-0428 Varied Octane Rating Effects on a Small Spark Ignition Internal Combustion Engine C. Wilson and P. King, U.S. Air Force Institute of Technology, Wright-Patterson AFB, OH; J. Hoke, IInnovative Scientific Solutions, Inc., Dayton, OH; and F. Schauer, U.S. Air Force Research Laboratory, Wright-Patterson AFB, OH 1500 AIAA-2010-0429 Simulations of the Chemical Transformations In a Jet Engine Exhaust Plume A. Garmory and E. Mastorakos, University of Cambridge, Cambridge, Great Britain; R. Bilger, University of Sydney, Sydney, Australia 1530 AIAA-2010-0430 A Study of Lean Direct- Injection Flames Under Pressurized Conditions R. Villalva Gomez, R. DiMicco and E. Gutmark, University of Cincinnati, Cincinnati, OH 1600 AIAA-2010-0431 Swirling Flame Dynamics and Describing Function P. Palies, D. Durox, T. Schuller, and S. Candel, École Centrale Paris, Chatenay-Malabry, France 1630 AIAA-2010-0432 Numerical Simulation of the Diffusion Flame Aiming for the Evaluation of Combustion Instability D. Hori, Japan Aerospace Exploration Agency (JAXA), Sagamihara-shi, Japan; S. Matsuyama, Japan Aerospace Exploration Agency (JAXA), Chofu-shi, Japan; T. Shimizu, Japan Aerospace Exploration Agency (JAXA), Sagamihara-shi, Japan; S. Yoshida, S. Tachibana, and J. Shinjo, Japan Aerospace Exploration Agency (JAXA), Chofu-shi, Japan Session 67- PDL-4 Aero-Optics Crystal Ballroom E Chaired by: D. CARROLL, CU Aerospace, Champaign, IL, and J. HORKOVICH, Raytheon, Tucson, AZ 1400 AIAA-2010-0433 High Fidelity Aero- Optical Analysis M. White, P. Morgan, and M. Visbal, U.S. Air Force Research Laboratory, Wright-Patterson AFB, OH 1430 AIAA-2010-0434 Aero- Optical Measurements in a Heated, Subsonic, Turbulent Boundary Layer J. Cress, S. Gordeyev and E. Jumper, University of Notre Dame, Notre Dame, IN 1500 AIAA-2010-0435 Aero- Optic Effects of a Wing Tip Vortex C. Porter, M. Rennie and E. Jumper, University of Notre Dame, Notre Dame, IN 1530 AIAA-2010-0436 Use of Plasma Actuators to Force Shear Layer Instabilities K. Schjodt, R. Flick, E. Stephen, and T. McLaughlin, U.S. Air Force Academy, U.S. Air Force Academy, CO 1600 AIAA-2010-0437 Aerodynamic Design of an Aircraft- Mounted Pod for Improved Aero- Optic Performance M. Rennie, G. Crahan and E. Jumper, University of Notre Dame, Notre Dame, IN 1630 AIAA-2010-0438 Hybrid Flow Control of a Turret Wake, Part II: Aero- Optical Effects S. Gordeyev and E. Jumper, University of Notre Dame, Notre Dame, IN; B. Vukasinovic and A. Glezer, Georgia Institute of Technology, Atlanta, GA; V. Kibens, The Boeing Company, Saint Louis, MO Session 68- SAT-1 Society and Aerospace Sciences Denver Chaired by: S. O'BRIEN, Embry-Riddle Aeronautical University, Daytona Beach, FL, and J. CHRISTIAN, University of Texas, Austin, Austin, TX 1400 AIAA-2010-0439 Societal Impact of Aerosciences in Addressing the Problems of Energy and Environment R. Agarwal, Washington University in St. Louis, St. Louis, MO 1500 AIAA-2010-0440 Societal Benefits from the Mars Science Laboratory (MSL) Program L. Buettner, Embry-Riddle Aeronautical University, Pensacola, FL 1530 AIAA-2010-0441 Study on Social and Economic Benefits of Aerospace Technical Diffusion R. Li, X. Ju and J. Tang, Harbin Institute of Technology, Harbin, China (prc) 1600 AIAA-2010-0442 Open Source Philosophy and the Powered Flight B. Mattos and S. Damiao, ITA, São José dos Campos, Brazil Session 279- TES-6 Numerical Simulation I Crystal Ballroom A Chaired by: C. MOEN, Sandia National Laboratories, Livermore, CA, and F. JABERI, Michigan State University, East Lansing, MI 1400 AIAA-2010-1553 A WENO- Z Based Eulerian- Lagrangian Code for Simulation of Shocked Flows Laden with Evaporating Droplets. J. Meijerink and G. Jacobs, San Diego State University, San Diego, CA; W. Don, Hong Kong Baptist University, Hong Kong, Hong Kong 1430 AIAA-2010-1554 Modeling of Flow Regimes and Thermal Patterns Interactions in Complex Applications E. Khalil, Cairo University, Cairo, Egypt 1500 AIAA-2010-1555 AFTC: A Computer Code for General Fuel- Air Combustion of Waste for Energy Production with Minimal Pollution D. Lilley, Lilley & Associates, Stillwater, OK 1530 AIAA-2010-1556 Femtotechnology: Nuclear AB- Matter with Fantastic Properties A. Bolonkin, C&R, Brooklyn, NY Session 69- TP-3 Aerothermodynamics I Crystal Ballroom M Chaired by: N. DOUGHERTY, Jacobs Engineering, Huntsville, AL, and J. KAPAT, University of Central Florida, Oviedo, FL 1400 AIAA-2010-0443 A Review of Aerothermal Modeling for Current and Future Mars Entry Missions M. Wright, NASA Ames Research Center, Moffett Field, CA; K. Edquist, NASA Langley Research Center, Hampton, VA 1430 AIAA-2010-0444 A Computational Study of High Enthalpy Flow Over a Rearward Facing Step D. Narayan Ramanath, S. Gai, and A. Neely, University of New South Wales at the Australian Defence Force Academy, Canberra, Australia 1500 AIAA-2010-0445 Results & Analysis of Large Scale Article Testing in the Ames 60 MW Interaction Heating Arc Jet Facility M. Loomis, NASA Ames Research Center, Moffett Field, CA 1530 AIAA-2010-0446 Orion Crew Entry Vehicle Boundary Layer Transition at High- Enthalpy in T5 E. Marineau, CUBRC, Buffalo, NY; S. Laurence, German Aerospace Center (DLR), Goettingen, Germany; H. Hornung, California Institute of Technology, Pasadena, CA; and A. Amar, NASA Johnson Space Center, Houston, TX 1600 AIAA-2010-0447 Parameter Sensitivity Analysis for Hypersonic Viscous Flow Using a Discrete Adjoint Approach B. Lockwood and D. Mavriplis, University of Wyoming, Laramie, WY Session 70- TP-4 Direct Simulation Monte Carlo Methods I Crystal Ballroom N Chaired by: A. ALEXEENKO, Purdue University, West Lafayette, IN, and D. GOLDSTEIN, University of Texas, Austin, TX 1400 AIAA-2010-0449 Treatment of Electronic Energy Level Transition and Ionization Following the Particle- Based Chemistry Model D. Liechty, NASA Langley Research Center, Hampton, VA 1430 AIAA-2010-0450 A Three- Level Cartesian Geometry- Based Implementation of the DSMC Method D. Gao, C. Zhang and T. Schwartzentruber, University of Minnesota, Minneapolis, MN 1500 AIAA-2010-0451 Parallel Implementation of the Direct Simulation Monte Carlo Method For Shared Memory Architectures D. Gao and T. Schwartzentruber, University of Minnesota, Minneapolis, MN 1530 AIAA-2010-0452 Statistical Modeling of Detonation in H2/O2 Mixture Y. Bondar and M. Ivanov, Khristianovich Institute of Theoretical and Applied Mechanics, Novosibirsk, Russia Session 71- TP-5 Orbiter Entry Aerothermo Flight Experiments: Orbiter Computational Analyses Crystal Ballroom P Chaired by: M. CHOUDHARI, NASA Langley Research Center, Hampton, VA, and J. PAYNE, Sandia National Laboratories, Albuquerque, NM 1400 AIAA-2010-0453 Numerical Simulations of the Boundary Layer Transition Flight Experiment C. Tang and K. Trumble, NASA Ames Research Center, Moffett Field, CA; C. Campbell, NASA Johnson Space Center, Houston, TX; V. Lessard and W. Wood, NASA Langley Research Center, Hampton, VA 1430 AIAA-2010-0454 Comparison of CFD Predictions with Shuttle Global Flight Thermal Imagery and Discrete Surface Measurements W. Wood and W. Kleb, NASA Langley Research Center, Hampton, VA; C. Tang, NASA Ames Research Center, Palo Alto, CA; G. Palmer and A. Hyatt, ELORET Corporation, Sunnyvale, CA; A. Wise, AMA Inc., Hampton, VA 1500 AIAA-2010-0455 Hypersonic Navier Stokes Comparisons to Orbiter Flight Data C. Campbell, NASA Johnson Space Center, Houston, TX 1530 AIAA-2010-0456 Effects of Rarefaction on Hypersonic Boundary Layer Flow Over Discrete Surface Roughness K. Stephani, D. Goldstein, and P. Varghese, University of Texas, Austin, Austin, TX 1600 AIAA-2010-0457 Orbiter Boundary Layer Transition Stability Modeling at Flight Entry Conditions M. Bartkowicz, University of Minnesota, Minneapolis, MN 1630 AIAA-2010-0458 Boundary Layer Protuberance Simulations in Channel Nozzle Arc Jet J. Marichalar and M. Larin, Jacobs Technology, Houston, TX; C. Campbell, NASA Johnson Space Center, Houston, TX; M. Pulsonetti, NASA Langely Research Center, Hampton, VA Session 72- WE-2 Wind Turbine Aerodynamics Modeling and Analysis Crystal Ballroom G2 Chaired by: J. LAURSEN, Siemens, Brande, Denmark, and C. VAN DAM, University of California, Davis, Davis, CA 1400 AIAA-2010-0459 Hybrid RANS/LES Simulation of the NASA/NREL Phase- VI Horizontal Axis Wind Turbine C. Stone, Computational Science & Engineering, Athens, GA; C. Lynch and M. Smith, Georgia Institute of Technology, Atlanta, GA 1430 AIAA-2010-0460 Computational Predictions of Airfoil Roughness Sensitivity K. Standish and P. Rimmington, Siemens, Boulder, CO; J. Laursen and H. Paulsen, Siemens, Brande, Denmark; and D. Nielsen, Siemens, Taastrup, Denmark 1500 AIAA-2010-0461 Using the Actuator Surface Method to Model the Three- Bladed Mexico Wind Turbine S. Breton, C. Sibuet Watters, and C. Masson, École de Technologie Supérieure, Montréal, Canada; and N. Barthelemy, ENSAM Paris, Paris, France 1530 AIAA-2010-0462 Validating BEM, Direct and Inverse Free Wake Models with the MEXICO Experiment. D. Micallef, University of Malta, Msida, Malta; M. Kloosterman and C. Ferreira, Delft University of Technology, Delft, The Netherlands; T. Sant, University of Malta, Msida, Malta; and G. van Bussel, Delft University of Technology, Delft, The Netherlands 1600 AIAA-2010-0463 Comparison of Potential Flow Wake Models for Horizontal- Axis Wind Turbine Rotors S. Cline and C. Crawford, University of Victoria, Victoria, Canada 1630 AIAA-2010-0464 3- D Numerical Icing Simulation on a Rotating Wind Turbine N. Tarchoune, École de Technologie Supérieure, Montréal, Canada Session 73- WIG-3  /  PDL-5 Joint PDL/WIG/FD/TP Plasma Actuator Session II Grand Ballroom 1 Chaired by: D. VAN WIE, Johns Hopkins University Applied Physics Laboratory, Laurel, MD, and N. YURCHENKO, National Academy of Sciences, Kiev, Ukraine 1400 AIAA-2010-0465 Rate of Plasma Thermalization of Pulsed Nanosecond Surface Dielectric Barrier Discharge A. Starikovskiy, Drexel University, Philadelphia, PA 1430 AIAA-2010-0466 Modeling of Aerodynamic Forcing Induced by Surface Dielectric Barrier Discharge V. Soudakov, Moscow Institute of Physics and Technology, Zhukovsky, Russia; V. Krivtsov and V. Soloviev, Moscow Institute of Physics and Technology, Dolgoprudny, Russia; and A. Fedorov, Moscow Institute of Physics and Technology, Zhukovsky, Russia 1500 AIAA-2010-0467 Dielectric Barrier Discharge Initiation Under the Supersonic Airflow A. Saveliev, Moscow Institute of Physics and Technology, Dolgoprudny, Russia; V. Golub, Russian Academy of Sciences, Moscow, Russia; V. Sechenov, Moscow Institute of Physics and Technology, Dolgoprudny, Russia; and E. Son, Russian Academy of Sciences, Moscow, Russia 1530 AIAA-2010-0468 Separation Control With Vectoring Plasma Actuators S. Fleming and J. Jacob, Oklahoma State University, Stillwater, OK 1600 AIAA-2010-0469 DBD Plasma Actuators with Silicon Coatings D. Opaits, Princeton University, Princeton, NJ; A. Likhanskii, Pennsylvania State University, University Park, PA; S. Zaidi and M. Shneider, Princeton University, Princeton, NJ; S. Macheret, Lockheed Martin, Palmdale, CA; R. Miles, Princeton University, Princeton, NJ; and D. Ashpis, NASA Glenn Research Center, Cleveland, OH 1630 AIAA-2010-0470 Limitations of the Maximum DBD- Induced Flow Velocity A. Likhanskii, Tech-X, Boulder, CO; M. Shneider and D. Opaits, Princeton University, Princeton, NJ; S. Macheret, Lockheed Martin Aeronautics, Palmdale, CA; and R. Miles, Princeton University, Princeton, NJ 1730 - 1830 2010 Dryden Lectureship In Research Crystal Ballroom H D. Ian Poll Professor of Aerospace Engineering Cranfield University Bedfordshire, United Kingdom