Production of high-Mach-number scramjet flow conditions in an expansion tube
暂无分享,去创建一个
[1] Allan Paull,et al. Test flow disturbances in an expansion tube , 1992, Journal of Fluid Mechanics.
[2] R. G. Morgan,et al. Effects of oxygen dissociation on hypervelocity combustion experiments , 1992 .
[3] J Jachimowski Casimir,et al. An Analysis of Combustion Studies in Shock Expansion Tunnels and Reflected Shock Tunnels , 1992 .
[4] John David Anderson,et al. Introduction to Flight , 1985 .
[5] M L Laster,et al. RDHWT/MARIAH II Hypersonic Wind Tunnel Research Program , 2001 .
[6] Thomas Jazra,et al. Comparison of Mach 10 Scramjet Measurements from Different Impulse Facilities , 2010 .
[7] John W. Hicks. Flight testing of airbreathing hypersonic vehicles , 1993 .
[8] R. J. STALKER,et al. Diaphragm-type Shock Tube for High Shock Speeds , 1968, Nature.
[9] John I. Erdos,et al. Use of an Expansion Tube to Examine Scramjet Combustion at Hypersonic Velocities , 1989 .
[10] John I. Erdos,et al. Expansion of the scramjet ground test envelope of the Hypulse facility , 1996 .
[11] Hans G. Hornung,et al. Role and techniques of ground testing for simulation of flows up to orbital speed , 1990 .
[12] Peter A. Jacobs. Shock Tube Modelling With L1d , 1998 .
[13] Mark Gruber,et al. Simulating Inlet Distortion Effects In A Direct-Connect Scramjet Combustor (Postprint) , 2006 .
[14] Johan Steelant,et al. Methodology of a combined ground based testing and numerical modelling analysis of supersonic combustion flow paths , 2010 .
[15] Peter A. Jacobs,et al. Simulation of CO2-N2 Expansion Tunnel Flows for the Study of Radiating Shock Layers , 2008 .
[16] Peter A. Jacobs,et al. Pilot study for a rarefied hypervelocity test facility , 1998 .
[17] John R. Olds,et al. Constant Dynamic Pressure Trajectory Simulation in POST , 1998 .
[18] Michael S. Holden. Aerothermal and Propulsion Ground Testing That Can Be Conducted to Increase Chances for Successful Hypervelocity Flight Experiments , 2005 .
[19] Michael Paul Scott. Development and Modelling of Expansion Tubes , 2007 .
[20] J Erdos,et al. Options for enhancement of the performance of shock-expansion tubes and tunnels , 1995 .
[21] E. T. Curran,et al. Scramjet Engines: The First Forty Years , 2001 .
[22] Harold Mirels,et al. TEST TIME IN LOW PRESSURE SHOCK TUBES , 1963 .
[23] Richard G. Morgan. Chapter 4.2 - Shock Tubes and Tunnels: Facilities, Instrumentation, and Techniques , 2001 .
[24] Peter A. Jacobs,et al. Scramjet Experiments in an Expansion Tunnel: Evaluated Using a Quasi-Steady Analysis Technique , 2010 .
[25] Richard G. Morgan,et al. Free piston-Driven expansion tubes , 2001 .
[26] Peter A. Jacobs,et al. Superorbital expansion tube operation: Estimates of flow conditions via numerical simulation , 2005 .
[27] Peter A. Jacobs,et al. Rocketdyne Hypersonic Flow Laboratory as High-Performance Expansion Tube for Scramjet Testing , 2003 .
[28] John I. Erdos,et al. Facility opportunities and associated stream chemistry considerations for hypersonic air-breathing propulsion , 1994 .
[29] David Gildfind,et al. Development of high total pressure scramjet flow conditions using the X2 expansion tube , 2012 .
[30] Con J. Doolan,et al. Comparison of Hydrogen and Hydrocarbon-Fueled Scramjet Engines for Orbital Insertion , 2007 .
[31] Richard G. Morgan,et al. Chapter 4.3 - Shock Tubes and Tunnels: Facilities, Instrumentation, and Techniques , 2001 .
[32] John I. Erdos,et al. Progress in hypersonic combustion technology with computation and experiment , 1990 .
[33] Shakil Ahmed,et al. High Speed/Hypersonic Aircraft Propulsion Technology Development , 2013 .
[34] M.R. Tetlow,et al. Orbital payload delivery using hydrogen and hydrocarbon fuelled scramjet engines , 2006, 2006 IEEE Aerospace Conference.
[35] Peter A. Jacobs,et al. Rarefied, superorbital flows in an expansion tube , 2004 .
[36] Richard G. Morgan,et al. A two-stage free-piston driver , 1999 .
[37] Peter A. Jacobs,et al. Helmholtz Resonance of Pitot Pressure Measurements in Impulsive Hypersonic Test Facilities , 2009 .
[38] Richard G. Morgan. Free Piston-Driven Reflected Shock Tunnels , 2001 .
[39] John I. Erdos,et al. Design, calibration and analysis of a tunnel mode of operation for the HYPULSE facility , 1996 .
[40] H. Mirels. Shock Tube Test Time Limitation Due to Turbulent-Wall Boundary Layer , 1964 .
[41] Ec Semple. Trajectory and Performance of an Expendable Scramjet Powered Launcher , 1992 .
[42] Charles E. Cockrell,et al. Technology Roadmap for Dual-Mode Scramjet Propulsion to Support Space-Access Vision Vehicle Development , 2002 .
[43] R. J. Stalker,et al. A study of the free-piston shock tunnel. , 1967 .
[44] K. Sato,et al. Hypersonic aerothermodynamic and scramjet research using high enthalpy shock tunnel , 2002 .
[45] Peter A. Jacobs,et al. Free-piston driver optimisation for simulation of high Mach number scramjet flow conditions , 2011 .
[46] F. Billig. Research on supersonic combustion , 1992 .
[47] R. J. Bakos,et al. Design of a shock-free expansion tunnel nozzle in HYPULSE , 2003 .
[48] Sebastian Karl,et al. Numerical Investigation of a Generic Scramjet Configuration , 2010 .