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.
分析结果表明：在不考虑攻角变化的条件下，进气道不起动边界主要与
有
。
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.
分析结果表明：在不考虑攻角变化的条件下，进气道不起动边界主要与有。
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