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.
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.
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