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
角变化的条件下，进气道不
动边界主要与来流马赫数有
。
速的飞行速度）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.
在不角变化的条件下，进气道不动边界主要与来流马赫数有。
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