激波边界是太阳风在恒星间气体压力下减速的地带。
实验结果表明，在本实验范围内，激波边界层干扰中的上游影响区都呈现出柱形区或锥形区特性；
The results show that the conical or cylindrical upstream influence region appears, in the interactions for all models and Mach numbers.
在超声速或高超声速绕流中，一种很严重的脉动压力环境是由激波边界层相互作用引起的激波振荡。
One of the more severe fluctuating pressure environments encountered in supersonic or hypersonic flows is the shock wave oscillation driven by interaction of a shock wave with boundary layer.
本文探讨了一种新的激波——非定常边界层相互干扰现象。
In this paper, a new type of interaction of a moving shock with an unsteady boundary layer had been studied theoretically and experimentally.
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