Effects of wall cooling on performance parameters of hypersonic inlets

Research on supersonic combustion

F. S. Billig · Journal of Propulsion and Power · 1993 · 443 citations

Engineering, Aerospace Engineering, Mechanical Engineering +14

Aerodynamic Performance Analysis of a Hypersonic Inlet Isolator Using Computation and Experiment

Birgit Reinartz, Carsten Herrmann, Josef Ballmann et al. · Journal of Propulsion and Power · 2003 · 200 citations

Engineering, Aerospace Engineering, Aerodynamics +14

Prediction of Precombustion Wall Pressure Distributions in Scramjet Engines

P. J. Waltrup, F. S. Billig · Journal of Spacecraft and Rockets · 1973 · 158 citations

Engineering, Aerospace Engineering, Materials Engineering +17

Experimental Investigation of Inlet-Combustor Isolators for a Dual-Mode Scramjet at a Mach Number of 4

Saied Emami, Carl Trexler, Aaron H. Auslender et al. · NASA Technical Reports Server (NASA) · 1995 · 137 citations · Full text

Engineering, Aerospace Engineering, Mechanical Engineering +17

Incipient Separation of a Supersonic, Turbulent Boundary Layer, Including Effects of Heat Transfer

Frank W. Spaid, JOHN C. FRISHETT · AIAA Journal · 1972 · 97 citations

Engineering, Aerospace Engineering, Mechanical Engineering +17