Available data in subsonic and supersonic flow for effects of free stream turbulence, surface curvature, pressure gradient, surface roughness, surface temperature, and Mach number on transition position; new supersonic data included from rocket flights, firing range tests, and wind tunnel tests.
Boundary-layer stability and transition in subsonic and supersonic flow
J Aeronautical Sciences
Journal of the Aeronautical Sciences ; 20 , n 1 ; p 19-28
1953
10 pages
Bibliography
Aufsatz (Zeitschrift)
Englisch
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Shockless Transition from Supersonic to Subsonic Flow
AIAA | 1995
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Online Contents | 1995
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