A GLOBAL STABILITY ANALYSIS OF THE STEADY AND PERIODIC CYLINDER WAKE

被引:173
作者
NOACK, BR
ECKELMANN, H
机构
[1] Max-Planck-Institut fur Stromungsforschung, D-37 073, Gottingen
关键词
D O I
10.1017/S0022112094004283
中图分类号
O3 [力学];
学科分类号
08 ; 0801 ;
摘要
A global, three-dimensional stability analysis of the steady and the periodic cylinder wake is carried out employing a low-dimensional Galerkin method. The steady flow is found to be asymptotically stable with respect to all perturbations for Re < 54. The onset of periodicity is confirmed to be a supercritical Hopf bifurcation which can be modelled by the Landau equations. The periodic solution is observed to be only neutrally stable for 54 < Re < 170. While two-dimensional perturbations of the vortex street rapidly decay, three-dimensional perturbations with long spanwise wavelengths neither grow nor decay. The periodic solution becomes unstable at Re = 170 by a perturbation with the spanwise wavelength of 1.8 diameters. This instability is shown to be a supercritical Hopf bifurcation in the spanwise coordinate and leads to a three-dimensional periodic flow. Finally the transition scenario for higher Reynolds numbers is discussed.
引用
收藏
页码:297 / 330
页数:34
相关论文
共 47 条
[1]  
AHLBORN B, 1994, UNPUB PHYS FLUIDS A
[2]  
ALBAREDE P, 1990, CR ACAD SCI II, V310, P459
[3]   A MODEL FOR THE FORMATION OF OBLIQUE SHEDDING AND CHEVRON PATTERNS IN CYLINDER WAKES [J].
ALBAREDE, P ;
MONKEWITZ, PA .
PHYSICS OF FLUIDS A-FLUID DYNAMICS, 1992, 4 (04) :744-756
[4]  
[Anonymous], 1986, NUMERICAL RECIPES
[5]  
BREDE M, 1994, UNPUB PHYS FLUIDS A
[6]   NUMERICAL-ANALYSIS OF SECONDARY AND TERTIARY STATES OF FLUID-FLOW AND THEIR STABILITY PROPERTIES [J].
BUSSE, FH .
APPLIED SCIENTIFIC RESEARCH, 1991, 48 (3-4) :341-351
[7]   CONVECTION AT VERY LOW PRANDTL NUMBERS [J].
CLEVER, RM ;
BUSSE, FH .
PHYSICS OF FLUIDS A-FLUID DYNAMICS, 1990, 2 (03) :334-339
[8]  
DETEMPLELAAKE E, 1989, EXP FLUIDS, V7, P217
[9]   3-DIMENSIONAL STRUCTURE OF WAKE OF A CIRCULAR CYLINDER [J].
GERRARD, JH .
JOURNAL OF FLUID MECHANICS, 1966, 25 :143-&
[10]  
HAMA FR, 1957, J AERONAUT SCI, V24, P156