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"Experimental Investigation of a 3D Thermal Compression Scramjet Using Advanced Optical Techniques"
として
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Full Length Papers(Scramjet)(-2009)
2009・(AIAA2009-5067)Development of an In Flight Non-intrusive Mass Capture System
2008
・Shock tunnel studies on cowl/ramp shock interactions in a generic scramjet inlet
・Analysis of Shock Dynamics in Supersonic Intakes
・Boundary-layer-ingesting inlet flow control
・Gaseous Surrogate Hydrocarbons for a HIFiRE Scramjet that Mimic Opposed Jet Extinction Limits for Cracked JP Fuels
・Plasma-Assisted Ignition in Scramjets
2007
・Hypersonic Transporter
・Investigation of structure of turbulent boundary layer under action of large pressure gradients
・CFD designed experiments for shock wave/boundary layer interactions in hypersonic ducted flows
・Reynolds-Averaged Navier Stokes Simulation of Scramjet Inlet Flowfield
・(AIAA2007-4490)Comparisons of Transition Prediction using PSE-Chem to Measurements for a Shock Tunnel Environment
・(AIAA2007-2013)Aeroelastic and Aerothermoelastic Analysis of Hypersonic Vehicles: Current Status and Future Trends
2006
・(AIAA2006-8069)Design of actively cooled panels for scramjets
・NUMERICAL COMPUTATIONS FOR DESIGNING A SCRAMJET INTAKE
・Numerical Simulations of Flow in a 3-D Supersonic Intake at High Mach Numbers
・Control of Penetration and Mixing of an Excited Supersonic Jet Into a Supersonic Cross Stream
・User Guide for Compressible Flow Toolbox Version 2.1 for Use With MATLAB (Registered Trademark); Version 7
2005
・Airbreathing Hypersonic Flight Vehicle Modeling and Control, Review, Challenges, and a CFD-Based Example
・PERFECT GAS NAVIER-STOKES SOLUTIONS OF HYPERSONIC BOUNDARY LAYER AND COMPRESSION CORNER FLOWS
・Application of PIV in a Hypersonic Double-Ramp Flow
・Shock Interaction Control for Scramjet Cowl Leading Edges
2003
・Liquid fuels and propellants for aerospace propulsion: 1903-2003
・(AIAA2003-3804)NUMERICAL INVESTIGATION OF WAVERIDER-DERIVED HYPERSONIC TRANSPORT CONFIGURATIONS
・(AIAA2003-1275)Investigation of a Hartmann-Sprenger tube for passive heating of scramjet injectant gases
・(AIAA2003-0550)Numerical simulation and parametric study of Hartmann-Sprenger tube based powered device
・(AIAA2003-0032)Scramjet inlet control by off-body energy addition: a virtual cowl
・(AIAA2003-0013)Numerical Analysis of Streamline-Traced Hypersonic Inlets
2002
・Numerical study of film cooling in hypersonic flows
・Optimal Shape Design of Supersonic, Mixed-Compression, Fixed-Geometry Air Intakes for SSTO Mission Profiles.
・Evolutionary design of robust flight control for a hypersonic aircraft
2001
・Hypersonic Laminar Boundary Layers and Near-Wake Flows
・Research in Hypersonic Airbreathing Propulsion at the NASA Langley Research Center
・(AIAA2001-0675)Inviscid CFD analysis of streamline traced hypersonic inlets at off-design conditions
・Cavity Flame-Holders for Ignition and Flame Stabilization in Scramjets: An Overview
2000
・Analysis of Transient Thermal Choking Processes in a Model Scramjet Engine
1999
・(AIAA1999-4974)Design and analysis of streamline traced hypersonic inlets
1998
・EFFECTS OF INCOMPLETE FUEL-AIR MIXING ON THE PERFORMANCE CHARACTERISTICS OF MIXED COMPRESSION, SHOCK-INDUCED COMBUSTION RAMJET (SHCRAMJET) ENGINES
・Time Accurate Computation Of Unsteady Hypersonic Inlet Flows with a Dynamic Flow Adaptive Mesh
1997
・advances in coniputational capabilities for hypersonic flows
・Numerical studies of real-gas effects on two-dimensional hypersonic shock-wave/boundary-layer interaction
・(AIAA1997-1017)Future direction of supersonic combustion research: Air Force/NASA workshop on supersonic combustion
1995
・Experimental Investigation of Inlet-Combustor Isolators for a Dual-Mode Scramjet at a Mach Number of 4
・Mach 10 computational study of a three-dimensional scramjet inlet flow field
・Internal aerodynamics of a generic three-dimensional scramjet inlet at Mach 10
1993
・Experimental investigation of generic three-dimensional sidewall-compression scramjet inlets at Mach 6 in tetrafluoromethane
・(AIAA1993-0740)An experimental parametric study of geometric, Reynolds number, and ratio of specific heats effects in three-dimensional sidewall compression scramjet inlets at Mach 6
1992
・(AIAA1992-4026)Reynolds Number and Cowl Position Effects for a Generic Sidewall Compression Scramjet Inlet at Mach 10: A Computational and Experimental Investigation
・(AIAA1992-3099)Internal shock interactions in propulsion/airframe integrated three-dimensional sidewall compression scramjet inlets
1991
・(AIAA 91-3301CP)Generic Supersonic and Hypersonic Configurations
1990
・(AIAA1990-2340)Methods for determining the internal thrust of scramjet engine modules from experimental data
1988
・Chemical Kinetics of SCRAMJET Propulsion
1976
・DEVELOPMENT OF A COMPUTER CODE FOR CALCULATING THE STEADY SUPER/HYPERSONIC INVISCID FLOW AROUND REAL CONFIGURATIONS