Transition in Hypersonic Wall-Bounded Flows

Yiding Zhu, Cunbiao Lee
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Abstract

The hypersonic boundary-layer transition is a strategic focus in the fluid mechanics community. This article reviews recent developments in the study of the hypersonic boundary-layer transition, especially at Peking University. The hypersonic quiet wind tunnel is introduced as a necessary device to obtain real flight data in near space. The most important issues in the recent development of the transition in the hypersonic boundary layer are addressed. The instability, its contribution to the aerodynamic heating and artificial control are discussed.
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高超声速壁面流动中的转捩
高超声速边界层转捩是流体力学领域的一个战略热点。本文综述了近年来北京大学对高超声速边界层转捩的研究进展。介绍了高超声速安静风洞作为获取近空间真实飞行数据的必要装置。讨论了近年来高超声速边界层过渡发展中最重要的问题。讨论了不稳定性及其对气动加热和人工控制的影响。
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