Conical shock wave-turbulent boundary layer interaction data obtained for adiabatic wall conditions at supersonic free stream Mach numbers, including suction effects
An experimental study of the interaction of a conical shock wave and a turbulent boundary layer including suction effects.
AMERICAN INST. OF AERONAUTICS AND ASTRONAUTICS, PROPULSION JOINT SPECIALIST CONFERENCE ; 1969 ; COLORADO SPRINGS, COLO.
01.06.1969
Aufsatz (Konferenz)
Keine Angabe
Englisch
Interaction of a Conical Shock Wave with a Turbulent Boundary Layer
British Library Online Contents | 1992
|