Review of progress in some issues and engineering application of hypersonic boundary layer transition

DUAN Yi; YAO Shiyong; LI Siyi; YU Ping

doi:10.7638/kqdlxxb-2020.0041

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Review of progress in some issues and engineering application of hypersonic boundary layer transition

更新时间：2026-05-28

- Review of progress in some issues and engineering application of hypersonic boundary layer transition
- Vol. 38, Issue 2, Pages: 391-403(2020)
- 作者机构：
  
  中国运载火箭技术研究院空间物理重点实验室,北京,100076
- 作者简介：
- 基金信息：
- DOI：10.7638/kqdlxxb-2020.0041
  CLC： O357.4+1
- Published：2020
- 稿件说明：
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段毅, 姚世勇, 李思怡, 余平. 高超声速边界层转捩的若干问题及工程应用研究进展综述[J]. 空气动力学学报, 2020, 38(2): 391-403.

DUAN Yi, YAO Shiyong, LI Siyi, et al. Review of progress in some issues and engineering application of hypersonic boundary layer transition[J]. 2020, 38(2): 391-403.
段毅, 姚世勇, 李思怡, 余平. 高超声速边界层转捩的若干问题及工程应用研究进展综述[J]. 空气动力学学报, 2020, 38(2): 391-403. DOI： 10.7638/kqdlxxb-2020.0041.

DUAN Yi, YAO Shiyong, LI Siyi, et al. Review of progress in some issues and engineering application of hypersonic boundary layer transition[J]. 2020, 38(2): 391-403. DOI： 10.7638/kqdlxxb-2020.0041.

摘要

高超声速飞行器绕流存在着激波、边界层、流动分离、稀薄气体效应和高温气体效应等多种复杂流动现象的空气动力学问题，其中高超声速边界层转捩既是空气动力学的基础问题，也是高超声速流动研究的热点和难点。若能对边界层转捩进行准确预示及有效控制，则可以实现对飞行器气动力热特性的精细设计，改进飞行器性能，提高任务执行能力。文章针对工程中具有复杂外形飞行器存在的典型失稳特征进行了研究进展回顾，提出了工程实际中亟需解决的复杂边界层转捩问题，明确了高超声速边界层转捩研究的工程应用方向。文章最后还对高超声速边界层的流动控制进行了回顾，以期在今后高超声速飞行器设计中实现对边界层的流动控制，提高飞行器的飞行性能。

Abstract

A variety of complicated flow phenomena such as shock wave

boundary layer

flow separation

rarefied gas effects and real gas effects exist in the flows over hypersonic flight vehicles. The hypersonic boundary layer transition is not only a basic aerodynamics issue

but also a hot topic and challenging subject in the research of hypersonic flows. The accurate prediction and the effective control of boundary layer transition can achieve meticulous design of aerodynamic force and heating

thus improving the vehicle performance and enhancing the mission capability. In this paper

the research progress in typical instability characteristics commonly existed in the flight vehicles with complex configurations in engineering is reviewed

and the complicated issues of boundary layer transition in engineering practice which are urgent to be solved are proposed. Meanwhile

the engineering application direction of the research on hypersonic boundary layer transition is specified. Moreover

the investigations on flow control of hypersonic boundary layer are reviewed in order to realize the boundary layer control in the design of hypersonic vehicle in future to enhance the flight performance.

关键词

Keywords

references

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