Fifty years of hypersonics: where we've been, where we're going
暂无分享,去创建一个
[1] S. M. Derry,et al. Review of boundary layer transition flight data on the Space Shuttle Orbiter , 1991 .
[2] Donald M. Curry. Thermal protection systems manned spacecraft flight experience , 1992 .
[3] F. K. Owen,et al. Comparison of Wind Tunnel Transition and Freestream Disturbance Measurements , 1975 .
[4] E. T. Curran,et al. Fluid Phenomena in Scramjet Combustion Systems , 1996 .
[5] J. W. Keyes,et al. Analytical and experimental studies of shock interference heating in hypersonic flows , 1973 .
[6] Ahmed K. Noor,et al. Airbreathing Hypersonic Aircraft and Transatmospheric Vehicles , 1997 .
[7] H. F. Nelson,et al. Thermal design of aeroassisted orbital transfer vehicles , 1985 .
[8] Ronald W. Humble,et al. Space Propulsion Analysis and Design , 1995 .
[9] Steven P. Schneider,et al. Laminar-Turbulent Transition Research in the Boeing/AFOSR Mach-6 Quiet Tunnel , 2005 .
[10] I. E. Beckwith,et al. A survey of NASA Langley studies on high-speed transition and the quiet tunnel , 1972 .
[11] S. Schneider. Flight Data for Boundary-Layer Transition at Hypersonic and Supersonic Speeds , 1999 .
[12] Dietrich E. Koelle,et al. Saenger - The German aerospace vehicle program , 1989 .
[13] E. R. V. Driest,et al. Experiments on Boundary-Layer Transition at Supersonic Speeds , 1957 .
[14] K. Sutton,et al. Air radiation revisited , 1984 .
[15] Barry E. Edney,et al. Effects of shock impingement on the heat transfer around blunt bodies. , 1968 .
[16] H Julian Allen,et al. A Study of the Motion and Aerodynamic Heating of Missiles Entering the Earth's Atmosphere at High Supersonic Speeds , 1957 .
[17] E. R. V. Driest,et al. Calculation of the Stability of the Laminar Boundary Layer in a Compressible Fluid on a Flat Plate with Heat Transfer , 1952 .
[18] W. D. Goodrich,et al. The aerothermodynamic environment of the Apollo command module during superorbital entry , 1972 .
[19] Walter C. Engelund,et al. Hyper-X aerodynamics: The X-43A airframe-integrated scramjet propulsion flight-test experiments , 2001 .
[20] Donald Johnson,et al. Duel-fuel lifting body configuration development , 1996 .
[21] Larry Schwelkart,et al. The Hypersonic Revolution. Case Studies in the History of Hypersonic Technology. Volume 3: The Quest for the Orbital Jet: The National Aero-Space Plane Program (1983-1995) , 1997 .
[22] William J. D. Escher,et al. Studies of an extensively axisymmetric rocket based combined cycle (RBCC) engine powered single-stage-to-orbit (SSTO) vehicle , 1989 .
[23] Douglas L. Dwoyer,et al. Computational fluid dynamics for hypersonic airbreathing airplanes , 1987 .
[24] O Stanley Douglas,et al. Technology Requirements for Affordable Single-Stage Rocket Launch Vehicles , 1993 .
[25] Daniel W. Barnette,et al. Engineering Flowfields and Heating Rates for Highly Swept Wing Leading Edges , 1976 .
[26] J. C. Mankins. LOWER COSTS FOR HIGHLY REUSABLE SPACE VEHICLES , 1998 .
[27] Howard Goldstein. Reusable thermal protection system development: A prospective , 1992 .
[28] L. Lees. Laminar Heat Transfer Over Blunt-Nosed Bodies at Hypersonic Flight Speeds , 1956 .
[29] R. H. Petersen,et al. Performance tradeoffs and research problems for hypersonic transports , 1965 .
[30] Carl Gazley. Boundarv-Layer Stability and Transition in Subsonic and Supersonic Flow , 1953 .
[31] D. Reda,et al. Correlation of nosetip boundary-layer transition data measured in ballistics-range experiments , 1979 .
[32] J. Laufer,et al. Stability and transition of a supersonic laminar boundary layer on an insulated flat plate , 1960, Journal of Fluid Mechanics.
[33] F. R. Riddell,et al. Theory of Stagnation Point Heat Transfer in Dissociated Air , 1958 .
[34] S.N.B. Murthy,et al. Propulsion Systems from Takeoff to High-Speed Flight , 1991 .
[35] E. T. Curran,et al. High-Speed Flight Propulsion Systems , 1991 .
[36] Franklin Houchin. The Rise and Fall of Dyna-Soar: A History of Air Force Hypersonic R&D, 1944--1963. , 1995 .
[37] N. H. Johannesen,et al. Hypersonic Flow , 1967, Nature.
[38] Stewart W. Johnson,et al. Access to Space—Systems and Technologies to Support It , 1997 .
[39] Walter C. Engelund,et al. Wind tunnel testing, flight scaling and flight validation with Hyper-X , 1998 .
[40] George M Low. Boundary-layer transition at supersonic speeds , 1956 .
[41] Lee F. Scuderi,et al. A Hypersonic Cruiser Concept for the 21st Century , 1998 .
[42] Steven P. Schneider. Hypersonic Boundary-Layer Transition Research in the Boeing/AFOSR Mach-6 Quiet Tunnel , 2002 .
[43] D. Dunn,et al. On the Stability of the Laminar Boundary Layer in a Compressible Fluid , 1953 .
[44] D. Reda. Review and synthesis of roughness-dominated transition correlations for reentry applications , 2002 .
[45] Steven P. Schneider,et al. Effects of High-Speed Tunnel Noise on Laminar-Turbulent Transition , 2000 .
[46] Samuel L. Venneri,et al. Future Aeronautical and Space Systems , 1997 .
[47] Max L. Blosser,et al. Active cooling from the sixties to NASP , 1994 .
[48] Winston D. Goodrich,et al. High Velocity and Real-Gas Effects on Weak Two-Dimensional Shock-Interaction Patterns , 1975 .
[49] Alain Wagner,et al. Systems Challenges for Hypersonic Vehicles , 1997 .
[50] Winston D. Goodrich,et al. Aerothermodynamic aspects of shock-interference patterns for shuttle configurations during entry. , 1973 .
[51] Johnny G. Armstrong. Flight Planning and Conduct of the X-15A-2 Envelope Expansion Program , 1969 .
[52] Dennis M. Bushnell. Hypersonic Flight Experimentation - Status and Shortfalls , 1997 .
[53] Daniel J. Rasky,et al. Advanced ceramic matrix composites for TPS , 1992 .
[54] J. J. Bertin,et al. Shuttle Orbiter boundary-layer transition - A comparison of flight and wind tunnel data , 1983 .
[55] Eli Reshotko,et al. BOUNDARY LAYER STABILITY AND TRANSITION , 1976 .
[56] Edney. ANOMALOUS HEAT TRANSFER AND PRESSURE DISTRIBUTIONS ON BLUNT BODIES AT HYPERSONIC SPEEDS IN THE PRESENCE OF AN IMPINGING SHOCK. , 1968 .