Progresses in engineering application research on hypersonic flow stability and transition

HUANG Zhangfeng; WAN Bingbing; DUAN Maochang

doi:10.7638/kqdlxxb-2020.0047

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Progresses in engineering application research on hypersonic flow stability and transition

更新时间：2026-05-28

- Progresses in engineering application research on hypersonic flow stability and transition
- Vol. 38, Issue 2, Pages: 368-378(2020)
- 作者机构：
  
  1. 天津大学力学系,天津,300072
  2. 中国空气动力研究与发展中心空气动力学国家重点实验室,绵阳,621000
- 作者简介：
- 基金信息：
- DOI：10.7638/kqdlxxb-2020.0047
  CLC： O357.4+1;V211
- Published：2020
- 稿件说明：
移动端阅览
黄章峰, 万兵兵, 段茂昌. 高超声速流动稳定性及转捩工程应用若干研究进展[J]. 空气动力学学报, 2020, 38(2): 368-378.

HUANG Zhangfeng, WAN Bingbing, DUAN Maochang. Progresses in engineering application research on hypersonic flow stability and transition[J]. 2020, 38(2): 368-378.
黄章峰, 万兵兵, 段茂昌. 高超声速流动稳定性及转捩工程应用若干研究进展[J]. 空气动力学学报, 2020, 38(2): 368-378. DOI： 10.7638/kqdlxxb-2020.0047.

HUANG Zhangfeng, WAN Bingbing, DUAN Maochang. Progresses in engineering application research on hypersonic flow stability and transition[J]. 2020, 38(2): 368-378. DOI： 10.7638/kqdlxxb-2020.0047.

摘要

流动稳定性及转捩是高超声速流动研究的热点和难点，近年来在理论基础研究方面取得了很大进展，但在工程应用方面还存在明显的不足。本文回顾了近年来高超声速流动稳定性及转捩在工程应用研究的若干进展，介绍了流动稳定性在复杂外形流、非平行流、局部突变流、强三维流方面的工程化拓展研究，总结了转捩预测e

方法在感受性、积分方法、转捩判据、软件开发方面的工程化研究进展；结合风洞试验、弹道靶试验、飞行试验，对零迎角锥、椭圆锥、小迎角锥和大迎角锥的典型案例进行了应用；展望了高超声速流动稳定性和转捩在工程应用的未来。

Abstract

Flow stability and transition is a hot and difficult topic in the study of hypersonic flow. Recently

great progresses have been made in its theoretical basic research

but there are still obvious deficiencies in engineering application. Main progresses in engineering application research on hypersonic flow stability and transition in recent years are reviewed. The engineering application developments of flow stability in complex shape flow

non-parallel flow

local distortion flow and strong three-dimensional flow are introduced

and the engineering application developments of transition prediction e

method in receptivity

integrating method

transition criterion and software development are s

ummarized. Combined with the results of wind tunnel test

ballistic target test and flight test

the typical cases of cone with zero angle of attack

elliptical cone

cone with small angle of attack and cone with large angle of attack are applied. The future of hypersonic flow stability and transition in engineering application is prospected.

关键词

Keywords

references

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