There are shocklets in the mixing layer with convective Mach number 1.2.
高对流马赫数混合层中存在较弱的小激波间断。
参考来源 - 应用BGK格式对可压缩混合层的数值研究The study of "supersonic-supersonic" mixing layer is one of the advanced domains in aerodynamics.
“超-超”混合层实验研究是当今空气动力学研究中的一个前沿领域。
参考来源 - “超—超”混合层风洞设计及调试实验研究·2,447,543篇论文数据，部分数据来源于NoteExpress
A useful method of enhancing the mixing for supersonic mixing layer is improving flow dynamics instability.
利用流动稳定性提高超音速混合层的混合效率，对于提高超音速流的高效混合是一个有效途径。
The ratio between the Reynolds stress and the turbulence energy in the inner regime of the mixing layer keeps almost constant.
但雷诺切应力与湍能的比值在混合层中心却保持不变。
This characteristic is also for supersonic and hypersonic mixing layer, which is useful method of enhancing the mixing for supersonic and hypersonic mixing layer.
对于高马赫数来流的超音速混合层，这一特性依然存在，这将有利于提高高超音速混合层的混合能力。
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