期刊文献+

A THEORETICAL INVESTIGATION OF THE DEVELOPMENT OF STATIONARY CROSSFLOW VORTICES IN THE BOUNDARY LAYER ON A SWEPT WING 被引量:2

A THEORETICAL INVESTIGATION OF THE DEVELOPMENT OF STATIONARY CROSSFLOW VORTICES IN THE BOUNDARY LAYER ON A SWEPT WING
全文增补中
导出
摘要 Crossflow instability plays very important role in the transition of the boundary layer on a swept wing, typical in the engineering applications. Experiments revealed that the linear stability theory well predicted the form of the crossflow vortices, but usually much overpredicted their growth rate. Using nonlinear theory of hydrodynamic stability, combined with some other considerations, we were able to obtain the growth rate in good agreement with experimental observations. Crossflow instability plays very important role in the transition of the boundary layer on a swept wing, typical in the engineering applications. Experiments revealed that the linear stability theory well predicted the form of the crossflow vortices, but usually much overpredicted their growth rate. Using nonlinear theory of hydrodynamic stability, combined with some other considerations, we were able to obtain the growth rate in good agreement with experimental observations.
作者 罗纪生 周恒
出处 《Acta Mechanica Sinica》 SCIE EI CAS CSCD 1998年第2期97-103,共7页 力学学报(英文版)
基金 The project supported by the National Natural Science Foundation of China, Grant No.19572048
关键词 CROSSFLOW hydrodynamic stability swept wing crossflow hydrodynamic stability swept wing
  • 相关文献

参考文献8

二级参考文献9

  • 1周恒.A NECESSARY MODIFICATION FOR THE AMPLITUDE EQUATION OF THE WEAKLY NONLINEAR THEORY OF HYD ROD YNAMIC STABILITY[J].Chinese Science Bulletin,1991,36(5):372-376. 被引量:1
  • 2周恒,赵耕夫.К-Б方法在流动稳定性问题中的应用[J]力学学报,1982(03). 被引量:1
  • 3Fujimura K.The equivalence between two perturbation methods in weakly non-linear stability theory for parallel shear flows. Proceedings of the Royal Society of London . I989 被引量:1
  • 4Itoh N.Spatial growth of finite wave disturbances in parallel and nearly parallel flows, Part 1 Theoretical analysis and the numerical results for plane Poiseuille flow. Tran Japan Soc Aero Space Sci . 1974 被引量:1
  • 5Herbert,T.On perturbation methods in nonlinear stability theory. Journal of Fluid Mechanics . 1983 被引量:1
  • 6Zhou,H,You,X.Weakly nonlinear theory of hydrodynamic stability revisited. Science in China . 1992 被引量:1
  • 7Zhou H.1982, On the nonlinear theory of stability of plane Poiseuille flow in the subcritical range, Pro. Roy. Soc. Lond . 被引量:1
  • 8Fujimura,K.Methods of center manifold and multiple scales in the theory of weakly nonlinear stability for fluid motions. Proceedings of the Royal Society of London . 1991 被引量:1
  • 9Stuart JT.On the non-linear mechanics of wave disturbances in stable, unstable parallel flows. Part 1. The basic behaviour in plane Poiseuille flow. Journal of Fluid Mechanics . 1960 被引量:1

共引文献5

同被引文献31

  • 1Joslin R D. Overview of Laminar Flow Control[ M]. Virginia: National Aeronautics and Space Administration, Langley Research Center, 1998. 被引量:1
  • 2Saric W S, Reed H L, White E B. Stability and transition of three-dimensional boundary layers [ J]. Annual Review of Fluid Mechanics, 2003, 35(1) : 413-440. 被引量:1
  • 3Gray W E. The Effect of Wing Sweep on Laminar Row [ M ]. Royal Aircraft Establishment, 1952. 被引量:1
  • 4Deyhle H, Bippes H. Disturbance growth in an unstable three-dimensional boundary layer and its dependence on environmental conditions[J]. Journal of Iuid Mechanics, 1996, 316: 73- 113. 被引量:1
  • 5Bippes H. Basic experiments on transition in three-dimensional boundary layers dominated by crossflow instability[ J]. Progress in Aerospace Sciences, 1999, 35(4) : 363-412. 被引量:1
  • 6Bippes H, Nitschke-Kowsky P. Experimental study of instability modes in a three-dimensional boundary layer[J]. A/AA Journal, 1990, 28(10) : 1758-1763. 被引量:1
  • 7Bippes H. Instability features appearing on swept wing configurations [ C ]//Arnal D, Michel R, ed. Laminar-Turbulent Transition. Berlin, Heidelberg: Springer, 1990: 419-430. 被引量:1
  • 8Saric W S, Yeates L G. Experiments on the stability of crossflow vortices in swept-wing flows [ C ]//23rd Aerospace Sciences Meeting. Virginia: Langley Research Center, National Aero- nautics and Space Administration, 1985. 被引量:1
  • 9Dagenhart J R, Saric W S. Crossflow stability and transition experiments in swept-wing flow E R]. Virginia. Langley Research Center, National Aeronautics and Space Administration,1999. 被引量:1
  • 10Bippes H, Mtiller B. Disturbance growth in an unstable three-dimensional boundary layer[ C ]// Cebeci T, ed. Numerical and Physical Aspects of Aerodynamic Flows, IV. Berlin, Heidelberg: Springer, 1990: 345-358. 被引量:1

引证文献2

二级引证文献6

相关作者

内容加载中请稍等...

相关机构

内容加载中请稍等...

相关主题

内容加载中请稍等...

浏览历史

内容加载中请稍等...
;
使用帮助 返回顶部