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.
在不考虑攻角变化的条件
，
气道不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.
在不考虑攻角变化的条件，气道不起动边界主要与来流马赫数有关。
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