高超声速流动稳定性及转捩工程应用若干研究进展

黄章峰; 万兵兵; 段茂昌

doi:10.7638/kqdlxxb-2020.0047

欢迎来到能源电力期刊网！

English Version 期刊登录

您当前的位置：

首页 >

文章列表页 >

高超声速流动稳定性及转捩工程应用若干研究进展

专栏——中国流动稳定性和转捩研究40年 | 更新时间：2026-05-28

- 高超声速流动稳定性及转捩工程应用若干研究进展
- Progresses in engineering application research on hypersonic flow stability and transition
- 空气动力学学报 2020年38卷第2期页码：368-378
- 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：
  
  黄章峰*(1977-), 男, 湖南宜章人, 副教授, 博导, 研究方向:流动稳定性, 工程转捩预测, 计算流体力学.E-mail:hzf@tju.edu.cn
- 基金信息：
  
  国家数值风洞工程（2018-ZT1A03）;国家自然科学基金（11672351）;国家重点研发计划（2016YFA0401200）
- DOI：10.7638/kqdlxxb-2020.0047
  中图分类号： O357.4+1;V211
- 纸质出版：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

ZHANG H X, ZHOU H. On basic research of fluid mechanics[J]. World Sci-Tech R D, 2001, 23(1):15-18. (in Chinese)

ZHOU H. Requirements for fluid mechanics in the new century[J]. Progress in Natural Science, 2000, 10(6):491-494. (in Chinese)

ZHUANG F G, CUI E J, ZHANG H X. Some development of future spacecrafts and aerodynamics tasks[M]. Beijing:National Defense Industry Press, 2006, 1-12. (in Chinese)

FEDOROV A. Transition and stability of high-speed boundary layers[J]. Annual Review of Fluid Mechanics, 2011, 43(1):79-95.

ZHOU H. Preface of flow stability and transition column[J]. Acta Aerodynamica Sinica, 2018, 36(2):181-182. (in Chinese)

XIE S F, YANG W B, SHEN Q. Review of progresses in hypersonic boundary layer transition mechanism and its applications[J]. Acta Aeronautica et Astronautica Sinica, 2015, 36(3):714-723. (in Chinese)

CHEN J Q, YUAN X X, TU G H, et al. Recent progresses on hypersonic boundary-layer transition[J]. Scientia Sinica(Physica, Mechanica Astronomica), 2019, 49(11):125-138. (in Chinese)

CHEN J Q, TU G H, ZHANG Y F, et al. Hypersnonic boundary layer transition:what we know, where shall we go[J]. Acta Aerodynamica Sinica, 2017, 35(3):311-337. (in Chinese)

YANG W B, SHEN Q, ZHU D H, et al. Tendency and current status of hypersonic boundary layer transition[J]. Acta Aerodynamica Sinica, 2018, 36(2):183-195. (in Chinese)

HUANG Z F. The mechanism of breakdown in laminar-turbulent transition of a supersonic boundary layer on a flat plate-temporal mode[J]. Science in China Series G, 2005, 48(5):614.

LIU X H, LAI G W, WU J. Boundary-layer transition experiments in hypersonic flow[J]. Acta Aerodynamica Sinica, 2018, 36(2):196-212. (in Chinese)

YI S H, LIU X L, NIU H B, et al. Experimental study on flow stability of hypersonic boundary layer[J]. Acta Aerodynamica Sinica, 2020, 38(1):137-142. (in Chinese)

YUAN X X, HE K, CHEN J Q, et al. Preliminary transition research analysis of MF-1[J]. Acta Aerodynamica Sinica, 2018, 36(2):286-293. (in Chinese)

TU G H, WAN B B, CHEN J Q, et al. Investigation on correlation between wind tunnel and flight for boundary layer stability and transition of MF-1 blunt cone[J]. Scientia Sinica(Physica, Mechanica Astronomica), 2019, 49(12):118-128. (in Chinese)

ZHOU Y, YANG Q T, WANG A L, et al. Estimation of surface heat flux for MF-1 flight test[J]. Acta Aerodynamica Sinica, 2019, 37(6):938-944. (in Chinese)

LUO J S. Transition and prediction for hypersonic boundary layers[J]. Acta Aeronautica et Astronautica Sinica, 2015, 36(1):357-372. (in Chinese)

ZHOU L, YAN C, HAO Z H, et al. Transition model and transition criteria for hypersonic boundary layer flow[J]. Acta Aeronautica et Astronautica Sinica, 2016, 37(4):1092-1102. (in Chinese)

FU S, WANG L. Progress in turbulence/transition modelling[J]. Advances in Mechanics, 2007, 37(3):409-416. (in Chinese)

XIANG X H, ZHANG Y F, CHEN J Q, et al. Progress in transition models for cross-flow instabilities[J]. Acta Aerodynamica Sinica, 2018, 36(2):254-264, 180. (in Chinese)

SARIC W. Physical description of boundary-layer transition: Experimental evidence: AGARD-R-793[R]. Special Course on Progress in Transition Modelling, 1993.

ZHOU H, ZHAO G F. Hydrodynamic Stability[M]. Beijing:National Defense Industry Press, 2004. (in Chinese)

TANG D B. Boundary layer transition[M]. Beijing:Science Press, 2015. (in Chinese)

REED H L, SARIC W S, ARNAL D. Linear stability theory applied to boundary layers[J]. Annual Review of Fluid Mechanics, 1996, 28(1):389-428.

DUAN Y, YAO S Y, LI S Y, et al. Review of progress in some issues and engineering application of hypersonic boundary layer transition[J]. Acta Aerodynamica Sinica, 2020, 38(2):391-403. (in Chinese)

KACHANOV Y S, MICHALKE A. Three-dimensinoal instability of flat-plate bounday layers:Theory and experiment[J]. Eur J Mech B-Fluid, 1994, 13(4):401-422.

HERBERT T. Parabolized stability equations[J]. Annual Review of Fluid Mechanics, 1997, 29(1):245-283.

SARIC W S, REED H L, WHITE E B. Stability andtransition of three-dimensional boundary layers[J]. Annual Review of Fluid Mechanics, 2003, 35(1):413-440.

HUANG Z F, WU X S. A non-perturbative approach to spatial instability of weakly non-parallel shear flows[J]. Physics of Fluids, 2015, 27(5):054102.

YU G T, GAO J, LUO J S. Stability analysis method considering non-parallelism:EPSE method and its application[J]. Applied Mathematics and Mechanics, 2016, 37(1):27-36.

WU X S, DONG M. A local scattering theory for the effects of isolated roughness on boundary-layer instability and transition:transmission coefficient as an eigenvalue[J]. Journal of Fluid Mechanics, 2016, 794:68-108.

HUANG Z F, WU X S. A local scattering approach for the effects of abrupt changes on boundary-layer instability and transition:a finite-Reynolds-number formulation for isolated distortions[J]. Journal of Fluid Mechanics, 2017, 822:444-483.

CEBECI T, STEWARTSON K. On stability and transition in three-dimensional flows[J]. AIAA Journal, 1980, 18(4):398-405.

MALIK M, BALAKUMAR P. Instability and transition in three-dimensional supersonic boundary layers[C]//4th Symposium on Multidisciplinary Analysis and Optimization, Cleveland, OH, USA. Reston, Virigina: AIAA-92-5049, 1992.

SONG R J, ZHAO L, HUANG Z F. Improvement of the parabolized stability equation to predict the linear evolution of disturbances in three-dimensional boundary layers based on ray tracing theory[J]. Physical Review Fluids, 2020, 5(3):033901.

SU C H, ZHOU H. Transition prediction for supersonic and hypersonic boundary layers on a cone with angle of attack[J]. Science in China Series G:Physics, Mechanics and Astronomy, 2009, 52(8):1223-1232.

HUANG Z F, WANG H L. Linear interaction of two-dimensional free-stream disturbances with an oblique shock wave[J]. Journal of Fluid Mechanics, 2019, 873:1179-1205.

BALAKUMAR P, CHOU A. Transition prediction in hypersonic boundary layers using receptivity and freestream spectra[J]. AIAA Journal, 2018, 56(1):193-208.

SONG R J, ZHAO L, HUANG Z F. Conservation relation of generalized growth rate in boundary layers[J]. Applied Mathematics and Mechanics, 2018, 39(12):1755-1768.

CHANG C L. The langley stability and transition analysis codes (LASTRAC): LST, linear nonlinear PSE for 2D, axisymmetric, and infinite swept wing boundary layers[C]//41st Aerospace Sciences Meeting and Exhibit, Reno, Nevada. Reston, Virigina: AIAA 2003-974, 2003.

YU G T, LUO J S. Application of e-N method in three-dimensional hypersonic boundary layers[J]. Journal of Aerospace Power, 2014, 29(9):2047-2054. (in Chinese)

SONG W P, WU M M, ZHU Z, et al. Transition prediction methods towards significant drag reduction via laminar flow technology[J]. Acta Aerodynamica Sinica, 2018, 36(2):213-228. (in Chinese)

HAN Z H, CHEN J, ZHANG K S, et al. Aerodynamic shape optimization of natural-laminar-flow wing using surrogate-based approach[J]. AIAA Journal, 2018, 56(7):2579-2593.

HUANG Z F, XIAO L C, LUO J S. Transition prediction e N method and its software development for supersonic boundary layers[J ] . Acta Aerodynamica Sinica, 2018, 36(2):279-285. (in Chinese)

THOMAS J, STEVEN S. Instability and transition on the HIFiRE-5 in a Mach 6 quiet tunnel[R]. AIAA 2010-5004, 2010.

LIU S, WANG Z H, XIE A M, et al. Ballistic range experiments of hypersonic boundary layer transition on a cone-cylinder-flare configuration[J]. Journal of Experiments in Fluid Mechanics, 2013, 27(6):26-31. (in Chinese)

浏览量

下载量

CSCD

文章被引用时，请邮件提醒。

提交

工具集

关联资源

关键参数对高速圆锥边界层来流慢声波扰动感受性的影响规律

高温气体效应下流动转捩及超声速模态的线性演化

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

高超声速边界层转捩预测中的关键科学问题——感受性、扰动演化及转捩判据研究进展

高超声速边界层流动稳定性实验研究