Heat transfer and wall temperature effects in shock wave turbulent boundary layer interactions
Heat transfer and wall temperature effects in shock wave turbulent boundary layer interactions
Direct numerical simulations are carried out to investigate the effect of the wall temperature on the behavior of oblique shock wave turbulent boundary layer interactions at free-stream Mach number 2.28 and shock angle of the wedge generator φ=8∘. Five values of the wall-to-recovery-temperature ratio (Tw/Tr) are considered, corresponding to cold, …