supported by the Project 1912,the National Natural Science Foundation of China (Grant Nos.52125603 and 11972139);the Fundamental Research Funds for the Central Universities (HIT.BRET.2021006 and FRFCU5710094620).
The interaction of cowl shock wave and boundary layer has a crucial effect on the stability,operability and performance of hypersonic inlets.Many studies on inhibiting the sep-aration and managing the strength of the ...