Conical shock wave-turbulent boundary layer interaction data obtained for adiabatic wall conditions at supersonic free stream Mach numbers, including suction effects
Conical shock-wave turbulent boundary-layer interaction including suction effects
AMERICAN INST. OF AERONAUTICS AND ASTRONAUTICS, PROPULSION JOINT SPECIALIST CONFERENCE, 5TH, U.S. AIR FORCE ACADEMY ; 1969 ; COLORADO SPRINGS, CO
1970-08-01
Miscellaneous
No indication
English
Interaction of a Conical Shock Wave with a Turbulent Boundary Layer
British Library Online Contents | 1992
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