Schlieren photographs and internal pressure distributions for three-dimensional sidewall-compression scramjet inlets at a Mach number of 6 in CF4
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[1] Carl A. Trexler. Inlet starting predictions for sidewall-compression scramjet inlets , 1988 .
[2] J. Micol. Simulation of real-gas effects on pressure distributions for a proposed Aeroassist Flight Experiment vehicle and comparison to prediction , 1987 .
[3] J. R. Henry,et al. Design considerations for the airframe-integrated scramjet , 1973 .
[4] C. G. Miller. Measured pressure distributions, aerodynamic coefficients and shock shapes on blunt bodies at incidence in hypersonic air and CF4 , 1982 .
[5] C. A. Trexler. Inlet performance of the integrated Langley scramjet module , 1975 .
[6] Ajay Kumar,et al. Numerical study of the effects of reverse sweep on scramjet inlet performance , 1992 .
[7] Charles G. Miller,et al. Langley 20-inch hypersonic CF4 tunnel - A facility for simulating real-gas effects , 1992 .
[8] Scott D. Holland,et al. Internal Shock Interactions in Propulsion/Airframe Integrated Three-Dimensional Sidewall Compression Scramjet Inlets , 1992 .
[9] R. M. Williams,et al. National Aero-Space Plane : Technology for America's Future , 1986 .