Studies of film and transpiration-cooled flows in regions of shock interaction

Advances in CFD prediction of shock wave turbulent boundary layer interactions

“…Holden and Chadwick [84] conducted an experimental study of the effects of tangential film and transpiration cooling on surface heat transfer in a 2-D shock impingement at Mach 6 and 8. They concluded that film cooling was ineffective for all but weak shock interactions due to the dispersal of the film by the shock boundary layer interaction.…”