Incipient thermal choking and stable shock-train formation in the heat-release region of a scramjet combustor. Part I: Shock-tunnel experiments

Shock train and pseudo-shock phenomena in internal gas flows

Kazuyasu MATSUO, Yoshiaki Miyazato, Heuy Dong Kim · Progress in Aerospace Sciences · 1999 · 608 citations

Engineering, Physics, Computational Fluid Dynamics +13

Experimental Investigation of Unstart in an Inlet/Isolator Model in Mach 5 Flow

Justin L. Wagner, Kemal Yuceil, Agustin Valdivia et al. · AIAA Journal · 2009 · 334 citations

Engineering, Aerospace Engineering, Aerodynamics +12

Flight Data Analysis of the HyShot 2 Scramjet Flight Experiment

Michael K. Smart, Neal Hass, Allan Paull · AIAA Journal · 2006 · 305 citations

Engineering, Aerospace Engineering, Mechanical Engineering +17

Fluid Phenomena in Scramjet Combustion Systems

Edward T. Curran, William H. Heiser, D. T. Pratt · Annual Review of Fluid Mechanics · 1996 · 290 citations

Engineering, Mechanical Engineering, Physics +13

Characteristics of multiple shock wave/turbulent boundary-layer interactions in rectangular ducts

Bruce Carroll, J. C. Dutton · Journal of Propulsion and Power · 1990 · 209 citations

Natural Sciences, Aerospace Engineering, Physics +17