Investigation on conical separation vortex generated by swept .
WEBOct 1, 2022 · To study the effects of Mach number, Reynolds number and deflection angle on the conical separation vortex generated by swept shock wave/turbulent boundary layer interaction, the experimental and numerical simulation methods are used. The Mach numbers are Ma = 2. 95 and Ma = deflection angles are 12 °, 15 ° and 18 °.The .