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。
This characteristic is also for supersonic and hypersonic mixing layer, which is useful method of enhancing the mixing for supersonic and hypersonic mixing layer.
为了掌握高超音速飞机复杂的动态特性，提出了一种研究高超音速飞机模型的新方法。
In order to grasp the hypersonic vehicle models complex dynamic characteristics, a new hypersonic vehicle model method was proposed.
本文给出高超音速湍流分离不稳定特性的实验研究结果。
This paper presents the results of an experimental study of the unsteady nature of a hypersonic separated turbulent flow.
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