Boundary-Layer Separation Due to Combustion-Induced Pressure Rise in a Supersonic Flow
AIAA Journal ; 47 , 4 ; 1050-1053
01.04.2009
Aufsatz (Zeitschrift)
Elektronische Ressource
Englisch
Pressure rise associated with shock-induced boundary-layer separation
Engineering Index Backfile | 1955
|Boundary layer separation in two-dimensional supersonic flow
TIBKAT | 1956
|