Shock-wave/turbulent boundary layer interaction are complex flow-fields, commonly
encountered in many air and space transportation applications. A common flow control
technique to alleviate its adverse effects and to mitigate separation is the application of air-
jet vortex generators (AJVGs). AJVGs induce a system of streamwise vortices downstream of
jet injection and enhance the distribution of momentum in the boundary layer. Consequently,
the boundary layer is more resistant to separation and the shock-induced separation region …