The results show that the unstart boundary of supersonic inlets is mainly concerned with Mach number of freestream without considering the variation of angle of attack.
虑攻角变化的条件下，进气道起动边界主要与来流马赫数有关。
The results show that the unstart boundary of supersonic inlets is mainly concerned with Mach number of freestream without considering the variation of angle of attack.
虑攻角变化的条件下，进气道起动边界主要与来流马赫数有关。
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