Specifically, the present work investigated the mechanisms that govern the mid-frequency range of separation shock unsteadiness in the fin shock wave–boundary layer interaction (SBLI) unit.

the structure of shock wave boundary layer interactions at high Mach number. Another reason for selecting a Mach number of 8 is that at this Mach number the flow is well into the hypersonic regime, ...

The HyperBLaF is a Mach 8 blowdown wind tunnel used for fundamental studies of compressible turbulence, shock wave/boundary layer interactions, shock/shock interactions and configuration studies of ...