本文论述了入射激波与飞行器头部激波相交后的二维或轴对称干扰流场的计算方法。
This paper describes the numerical method determining two-dimensional and axisymmetric flow for head-on vehicle shock-planar incident shock interaction.
通过创建一个外地的非对称干扰，这项实验旨在质疑共同的地方，即两个人，当他们满足，项目的自觉性对方。
By creating a field of asymmetric interferences, this experiment aimed at questioning the common place whereby two persons, when they meet, project their consciousness on each other.
通过简捷的说明， 指出低干扰整流器的实质是不对称触发整流器， 并提出可行的数字触发方案。
The paper points out that the nature of low disturbance rectifier is unsymmetry trigger rectifier by concise description and puts forward feasible digital trigger programme.
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