利用灰尘激波管入射激波后平衡区两相流开展平板传热实验。
Heat transfer measurements on a flat plate are performed inthe vertical dust shock tube in which the equilibrium dust gas flow in 2range has been used.
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.
对波系起 实质影响作用的是入射激波强度，激波越强，则整个透射流场呈现偏向激波的趋势；
Meanwhile, the strength of the incident shock wave has the most important influence on the transmitted flow system, that is, strong shock induces the whole flow field towards the shock direction.
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