References [1] A review of three-dimensional shock wave–boundary-layer interactions. Progress in Aerospace Sciences (2023). [2] Experimental study of wall temperature effect on shock wave ...

We have found that low levels of helium injection near the leading edge stabilizes the turbulent boundary layer, apparently causing a reverse transition to laminar flow to take place. These results ...

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

Shock wave and turbulent boundary layer interactions are phenomena encountered in high-speed flows, where abrupt pressure changes associated with shock waves impinge upon the viscous layer of ...