Fluid Phenomena in Scramjet Combustion Systems
作者： E T Curran , W H Heiser , D T Pratt
DOI: 10.1146/ANNUREV.FL.28.010196.001543
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摘要: This paper reviews important advances in understanding and predicting the behavior of scramjet combustion systems since the classic article published in this series by Antonio F ed (…
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sci-hub.se 参考文章(48)
P. K. Tret'yakov, Determination of heat input to duct flow with pseudoshock Combustion, Explosion, and Shock Waves. ,vol. 29, pp. 320- 326 ,(1993) , 10.1007/BF00797650
G. Y. Anderson, F. D. Stull, P. J. Waltrup, Supersonic combustion ramjet /scramjet/ engine development in the United States ,(1976)
G. B. Northam, I. Greenberg, D. P. Capriotti, C. S. Byington, Mach 2 and Mach 3 mixing and combustion in scramjets AIAA paper 91-2394. ,(1991)
William H. Heiser, Hypersonic Airbreathing Propulsion ,(1994)
JOSEPH V. FOA, GEORGE RUDINGER, On the Addition of Heat to a Gas Flowing in a Pipe at Subsonic Speed Journal of the Aeronautical Sciences. ,vol. 16, pp. 84- 94 ,(1949) , 10.2514/8.11733
P.P. Wegener, L.M. Mack, Condensation in Supersonic and Hypersonic Wind Tunnels Advances in Applied Mechanics. ,vol. 5, pp. 307- 447 ,(1958) , 10.1016/S0065-2156(08)70022-X
John S. MacKay, Richard J. Weber, An Analysis of Ramjet Engines Using Supersonic Combustion ,(1958)
Robert S. Brodkey, Lawrence Talbot, The phenomena of fluid motions ,(1967)
Paul E. Dimotakis, Turbulent Free Shear Layer Mixing and Combustion aiaa. pp. 265- 340 ,(1991)