Effect of Inlet Mach Number on Shock-Boundary Layer Interactions in a Supersonic Turbine Cascade
AIAA AVIATION 2023 Forum
2023-01-01
Conference paper
Electronic Resource
English
Shock-Wave/Boundary-Layer Interactions in High-Mach-Number Flows
British Library Online Contents | 1996
|Supersonic cascade flows with subsonic axial mach number
TIBKAT | 1982
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