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
2017-01-01
Conference paper
Electronic Resource
English
British Library Conference Proceedings | 2017
|Numerical simulation of laminar hypersonic shock-boundary layer interaction
Tema Archive | 1996
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