Investigation of the effects of flat plate span on ramp-induced, adiabatic, laminar boundary- layer separation at supersonic and hypersonic speeds
4th Fluid and Plasma Dynamics Conference ; 1971 ; Palo Alto , CA , U.S.A.
1971-01-01
Conference paper
Electronic Resource
English
Supersonic laminar boundary layer along two-dimensional adiabatic curved ramp
Engineering Index Backfile | 1969
|Laminar boundary layer at hypersonic speeds
Engineering Index Backfile | 1961
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