The shock corner boundary layer interaction at a freestream Mach number of 3 and a ramp angle of 10° was simulated with four turbulence models: RSM, SA, k-ε, and k-ω SST. Their predictions were compared by examining the shock structure in the symmetry plane, the pressure distribution along the corner line, and the boun...
Xiang-Qian Wu, Rui Yang, Yu-Xin Zhao et al.· Journal of Physics, Conferen...· 0 citations
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