The initiation point is not fixed on the focusing point but varies with the incident shock Mach number.

爆轰波爆点位置在对称轴上并不是固定的点，而是随着初始激波马赫数的变化而发生移动；

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The computational results are in a good agreement well with the experimental data of Mach number before the shock wave, separation and reattachment positions.

数值模拟结果，在激波强度、分离点位置和再附点位置等方面，与实验结果吻合较好。

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This paper presents the surface characteristics of the inter-action between shock wave and turbulent boundary layer induced by sharp fin with emphasis on Mach number effects.

本文介绍了尖前缘翼诱导激波和湍流边界层干扰流场壁面特性，着重强调马赫数影响。

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