PROPULSION AND POWER - Boundary-Layer Separation Due to Combustion-Induced Pressure Rise in a Supersonic Flow (TN)
AIAA journal ; 47 , 4
2009
Article (Journal)
English
Pressure rise associated with shock-induced boundary-layer separation
Engineering Index Backfile | 1955
|Boundary layer separation in two-dimensional supersonic flow
TIBKAT | 1956
|