Scramjet Engines: The First Forty Years
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[1] E. T. Curran,et al. Fluid Phenomena in Scramjet Combustion Systems , 1996 .
[2] Goro Masuya,et al. Effectiveness of plasma torches for ignition and flameholding in scramjet , 1989 .
[3] G. M. Makhviladze,et al. Flame propagation in a horizontal channel with cold side walls in a gravitational field , 1992 .
[4] G. S. Penny,et al. A study of free-jet and enclosed supersonic diffusion flames , 1969 .
[5] R. Clayton Rogers,et al. Experimental Supersonic Combustion Research at NASA Langley , 1998 .
[6] Richard J. Weber,et al. An Analysis of Ramjet Engines Using Supersonic Combustion , 1958 .
[7] Gordon L. Dugger,et al. Recent Advances in Ramjet Combustion , 1959 .
[8] E. A. Meshcheryakov,et al. Reduced heat production due to mixing and kinetic factors in supersonic combustion of unmixed gases in an expanding channel , 1988 .
[9] J. Weber,et al. Hydrocarbon scramjet propulsion system development, demonstration and application , 1999 .
[10] Sadatake Tomioka,et al. Mach 8 Testing of a Scramjet Engine Model , 2001 .
[11] A. Roudakov,et al. CIAM/NASA Mach 6.5 Scramjet Flight and Ground Test , 1999 .
[12] Antonio Ferri,et al. Analysis of fluid dynamics of supersonic combustion process controlled by mixing , 1969 .
[13] Paul J. Waltrup,et al. Upper Bounds on the Flight Speed of Hydrocarbon-Fueled Scramjet-Powered Vehicles , 2001 .
[14] Antonio Ferri,et al. Review of Problems in Application of Supersonic Combustion , 1964, The Journal of the Royal Aeronautical Society.
[15] Leo H. Townend,et al. The domain of the scramjet , 1999, Philosophical Transactions of the Royal Society of London. Series A: Mathematical, Physical and Engineering Sciences.
[16] R. Gross,et al. A Study of Supersonic Combustion , 1960 .
[17] Ching-Yi Tsai,et al. The Mach 10 Component of NASA's Hyper-X Ground Test Program , 1999 .
[18] A Paull,et al. Scramjet testing in the T4 impulse facility , 1998 .
[19] Paul J. Waltrup,et al. Liquid-fueled supersonic combustion ramjets - A research perspective , 1987 .
[20] Randall Voland,et al. NASP Concept Demonstration Engine and Subscale Parametric Engine tests , 1995 .
[21] F. Billig,et al. Combustion Processes in Supersonic Flow , 1988 .
[22] J. R. Henry,et al. Design considerations for the airframe-integrated scramjet , 1973 .
[23] Marc Bouchez,et al. Advanced carbon/carbon injection strut for actual scramjet , 1996 .
[24] O. Ferrandon,et al. A hydrogen cooled injection strut design for scramjet , 1996 .
[25] D. P. Hearth,et al. Hypersonic technology-approach to an expanded program , 1976 .
[26] V. A. Vinogradov,et al. Organization of kerosene combustion in a model hypersonic ramjet engine , 1992 .
[27] F. Billig. Research on supersonic combustion , 1992 .
[28] R. W. Guy,et al. Initial wind tunnel tests at Mach 4 and 7 of a hydrogen-burning, airframe-integrated scramjet , 1979 .
[29] Frederick Billig,et al. SCRAM - A Supersonic Combustion Ramjet Missile , 1993 .
[30] Shigeru Sato,et al. Comparison of Scramjet Engine Performance in Mach 6 Vitiated and Storage-Heated Air , 1997 .
[31] Wolfgang Koschel,et al. JAPHAR: A joint ONERA/DLR research project on high speed airbreathing propulsion , 1999 .
[32] Marc Bouchez,et al. Scramjet combustor design in French PREPHA program - Final status in 1998 , 1998 .
[33] E. H. Andrews,et al. Review of NASA's Hypersonic Research Engine Project , 1993 .
[34] V. Sabel’nikov,et al. Investigations into the Aerothermodynamic Characteristics of Scramjet Components. , 1997 .
[35] V. Semenov,et al. Comparative Flow Path Analysis and Design Assessment of an Axisymmetric Hydrogen Fueled Scramjet Flight Test Engine at a Mach Number of 6.5 , 1996 .
[36] R Chase,et al. A history of the NASP Program from the formation of the Joint Program Office to the termination of the HySTP Scramjet Performance Demonstration Program , 1995 .
[37] Goro Masuya,et al. Ignition and Combustion Performance of Scramjet Combustors with Fuel Injection Struts , 1995 .
[38] Sadatake Tomioka,et al. Geometrical effects to aerodynamic performance of scramjet engine , 1997 .
[39] Wolfgang Koschel. Basic Hypersonic Propulsion Research in German Universities , 1998 .
[40] Jürgen Zierep,et al. Theory of Flows in Compressible Media with Heat Addition , 1974 .
[41] Marc Bouchez,et al. Airbreathiiig space launcher interest of a fully variable geometry propulsion system and corresponding French-Russian partnership , 2000 .
[42] P. M. Rubins,et al. Review of shock-induced supersonic combustion research and hypersonic applications , 1994 .
[43] F. M. Pell BlLLIG. Two-Dimensional Model for Thermal Compression , 1972 .
[44] S B Chin,et al. Mixing Power Concepts in Scramjet Combustor Design , 1992 .
[45] R. J. Weber. A Survey of Hypersonic-Ramjet Concepts , 1959 .
[46] William O. T. Peschke. Approach to In Situ Analysis of Scramjet Combustor Behavior , 1995 .
[47] L. Ying,et al. Experimental Studies on Self-Ignition of Hydrogen/Air Supersonic Combustion , 1997 .
[48] C R McClinton,et al. Airbreathing Hypersonic Technology Vision Vehicles and Development Dreams , 1999 .
[49] Wallace Chinitz,et al. On the use of shock-induced combustion in hypersonic engines , 1996 .
[50] Antonio Ferri,et al. Mixing-Controlled Supersonic Combustion , 1973 .
[51] G. Y. Anderson,et al. Survey of supersonic combustion ramjet research at Langley , 1986 .
[52] Mark J. Lewis,et al. Experimentation, Test, and Evaluation Requirements for Future Airbreathing Hypersonic Systems , 2001 .