STREAMWISE VORTICES AND TRANSITION TO TURBULENCE

被引:18
作者
HAMILTON, JM [1 ]
ABERNATHY, FH [1 ]
机构
[1] HARVARD UNIV,DIV APPL SCI,CAMBRIDGE,MA 02138
关键词
D O I
10.1017/S0022112094000637
中图分类号
O3 [力学];
学科分类号
08 ; 0801 ;
摘要
A series of experiments was conducted to determine the conditions under which streamwise vortices can cause transition to turbulence in shear flows. A specially designed obstacle was used to produce a single vortex in a water-table flow, and the design of this obstacle is discussed. Laser-Doppler velocimetry measurements of the streamwise and crossflow velocity fields were made in transitional and non-transitional flows, and flow visualization was also used. It was found that strong vortices (vortices with large circulation) lead to turbulence while weaker vortices do not. Determination of a critical value of vortex strength for transition, however, was complicated by ambiguities in calculating the vortex circulation. The profiles of streamwise velocity were found to be inflexional for both transitional and non-transitional flows. Transition in single-vortex and multi-vortex flows was compared, and no qualitative differences were observed, suggesting no significant vortex interactions affecting transition.
引用
收藏
页码:185 / 212
页数:28
相关论文
共 16 条
  • [1] [Anonymous], 1986, NUMERICAL RECIPES
  • [2] Batchelor C.K., 1967, INTRO FLUID DYNAMICS, V1st ed.
  • [3] BERTSCHY JR, 1979, THESIS HARVARD U
  • [4] CHIN RW, 1981, THESIS HARVARD U
  • [5] CRAIK A. D. D., 1985, WAVE INTERACTIONS FL
  • [6] Drazin P.G., 2004, HYDRODYNAMIC STABILI, DOI [10.1017/CBO9780511616938, DOI 10.1017/CBO9780511616938]
  • [7] HAMILTON JM, 1991, THESIS HARVARD U
  • [8] FLIGHT AND WIND-TUNNEL INVESTIGATIONS ON BOUNDARY-LAYER-TRANSITION
    HORSTMANN, KH
    QUAST, A
    REDEKER, G
    [J]. JOURNAL OF AIRCRAFT, 1990, 27 (02): : 146 - 150
  • [9] THE 3-DIMENSIONAL NATURE OF BOUNDARY-LAYER INSTABILITY
    KLEBANOFF, PS
    TIDSTROM, KD
    SARGENT, LM
    [J]. JOURNAL OF FLUID MECHANICS, 1962, 12 (01) : 1 - &
  • [10] Lighthill MJ., 1963, LAMINAR BOUNDARY LAY, P46