激波强度的增加促使高波数不稳定模态很快被激发，从而导致了不同介质的混合。
The high unstable wave components can be excited quickly with increasing the shock strength, and this speeds the medium mixing.
以总压恢复系数最大为目标，采用等激波强度和等激波角设计方法建立进气道模型；
The inlet design calculating model was set up based on the theory of equal shock wave intensity and angle of supersonic airflow to get maximum total pressure coefficient.
数值模拟结果，在激波强度、分离点位置和再附点位置等方面，与实验结果吻合较好。
The computational results are in a good agreement well with the experimental data of Mach number before the shock wave, separation and reattachment positions.
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