可压缩横流失稳及其控制

徐国亮; 符松

doi:10.6052/1000-0992/11-059

可压缩横流失稳及其控制

doi: 10.6052/1000-0992/11-059

徐国亮^1,2,
符松^1, ,

1.
清华大学航天航空学院, 北京 100084
2. 中国空气动力学发展与研究中心, 绵阳 621000

基金项目: 国家自然科学基金项目(10932005) 资助

详细信息

通讯作者:
符松

计量
- 文章访问数: 1619
- HTML全文浏览量: 36
- PDF下载量: 1587
- 被引次数: 0
出版历程
- 收稿日期: 2010-11-15
- 修回日期: 2011-11-20
- 刊出日期: 2012-05-25

THE INSTABILITY AND CONTROL OF COMPRESSIBLE CROSS FLOWS

XU Guoliang^1,2,
FU Song^{1
, ,}

1.
School of Aerospace, Tsinghua University, Beijing 100084, China
2. China Aerodynamics Research and Development Center, Mianyang 621000, China

Funds: The project was supported by the National Natural Science Foundaion of China(10932005).

More Information

Corresponding author: FU Song

摘要

摘要: 边界层流动转捩的预测与控制一直是流体力学研究中的一个重要问题. 三维边界层流动工程中十分常见, 而横流失稳是导致三维边界层流动转捩的主要原因. 本文综述了近些年来三维边界层失稳和转捩方面的研究概况. 从机理上讨论了横流扰动的感受性、首次失稳、二次失稳和转捩控制等方面的研究进展. 在数值计算方面, 简要概述了线性稳定性理论、非线性稳定性理论和直接数值模拟方法在横流失稳和转捩方面的应用.本文对横流失稳研究当前存在的问题进行了讨论, 对今后研究的发展趋势作了相应展望.
- 横流 /
- 感受性 /
- 饱和横流涡 /
- 二次失稳 /
- 横流转捩
Abstract: Boundary layer transition prediction and control is one of the most ambitions topics of research activities in aerodynamics. The crossflow instability of a three-dimensional boundary layer is a main factor affecting the laminar transition. The current understanding of 3-d boundary-layer transition is reviewed. Recent advances in receptivity, primary instability, secondary instability and transition control of crossflow boundary layer flows are discussed. Challenges about compressible crossflow transition remain and prospects are presented as well.
- crossflow /
- receptivity /
- saturated crossflow vortex /
- secondary instability /
- crossflow transition

HTML全文

参考文献(12)

1 Gray W E. The nature of the boundary layer flow at the rose of a swept wing. Royal Aircraft Estabilishment, Rae Tm Aero 256. UK: Farnborough, England, 1952

2 Stetson K F. Mach 6 experiments of transition on a cone at angle of attack. Journal of Spacecr, 1982, 19(5): 397-403

3 Anthony R J, Jones T V, Lagraff J E. Unsteady surface heat flux under a three-dimensional crossflow boundary layer. AIAA paper 2004-1344, 2004

4 Reshotko E. Boundary-layer stability and transition. An- nual Review of Fluid Mechanics, 1976, 8(3): 11-40

5 Coustols E. Stabilite et transition en encoulement tridimensional: cas des ailes en fleche, Dissertation, L’Ecole National Superieure, 1983

6 Bippes H. On boundary layer transition & control. In R Aeronaut Soc Conf, Cambridge, UK, 1991

7 Dagenhart J, SaricWS, Mousseus M. Crossflow-vortex instability and transition on a 45 degree swept wing. AIAA paper 1989-1892, 1989

8 Goldstein M E. The evolution of Tollmien-Schlichting waves near a leading edge. Journal of Fluid Mechanics,1983, 127: 59-81

9 Reed H L, Saric W S. Stability of three-dimensional boundary layers. Annual Review of Fluid Mechanics,1989, 21: 235-284

10 Fransson Jens H M, Alessandro T, Luca B. Delaying transition to turbulence by a passive mechanism. Physical Review Letters, 2006, 9: 580-591

11 Radeztsky R H Jr, Reibert M S, Saric W S. Development of stationary crossflow vortices on a swept wing. AIAA paper 1994-2373, 1994

12 Muller B, Bippes H. Experimental study of instability modes in a three-dimensional boundary layer. In: Proc AGARD Symp On Fluid Dynamics of Three-Dimensional Turbulent Sheer Flows and Transition, Cesme, Turkey, AGARD C-P 438, 1988

施引文献

资源附件(0)

访问统计