Effect of Inlet Mach Number on Shock-Boundary Layer Interactions in a Supersonic Turbine Cascade
AIAA Aviation Forum ; 2023 ; San Diego, Calif.; Online
2023
Conference paper
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
|