Numerical Investigation of the Effect of the Sweep Angle of a Cylindrical Blunt Fin on the Shock Wave/Laminar Boundary Layer Interaction in a Hypersonic Flow
47th AIAA Fluid Dynamics Conference
01.01.2017
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
British Library Conference Proceedings | 2017
|Numerical simulation of laminar hypersonic shock-boundary layer interaction
Tema Archiv | 1996
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