Experimental/Computational Investigation of Shock-Wave/Boundary-Layer Interaction on an Axisymmetric Cone
AIAA AVIATION FORUM AND ASCEND 2024
01.01.2024
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
Computational Investigation of Groove Controlled Shock Wave / Boundary Layer Interaction
British Library Conference Proceedings | 2003
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