Boundary-Layer Separation Due to Combustion-Induced Pressure Rise in a Supersonic Flow
AIAA Journal ; 47 , 4 ; 1050-1053
2009-04-01
Article (Journal)
Electronic Resource
English
Pressure rise associated with shock-induced boundary-layer separation
Engineering Index Backfile | 1955
|Boundary layer separation in two-dimensional supersonic flow
TIBKAT | 1956
|