Numerical study of shock/boundary layer interaction in supersonic overexpanded nozzles
2015
Aufsatz (Zeitschrift)
Englisch
Shock-induced boundary layer separation in overexpanded conical exhaust nozzles
Engineering Index Backfile | 1963
|Numerical Simulation of Shock/Boundary Layer Interaction in Supersonic Nozzles
British Library Conference Proceedings | 2005
|Phenomenon of flow separation in overexpanded supersonic or rocket nozzles
Engineering Index Backfile | 1956
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