文中群细推导了公式，讨论了附体激波和脱体激波的判别准则，并给出了具体算例。
The formula deduction was demonstrated in detail, the criterion of attached or detached waves has been given, some numerical examples are presented.
文章对急流激波的计算方法进行了分析比较，并对附体激波的最大河岸偏转角进行了分析。
The computational methods of shock wave are analysed, and the maximal riverside deflection angle is analysed also.
在激波附体的条件下，本文的方法可用于计算大迎角尖前缘任意翼型的超音速和高超音速俯仰安定性导数。
This method may be used to calculate the arbitrary airfoils with sharp leading edge provided that the shock wave is attached.
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