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
变化的条件下，进气道不起动边界
要与来流马赫数有关。
;
;攻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.
在不考虑攻变化的条件下，进气道不起动边界要与来流马赫数有关。
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