Investigation of flow around a pair of side-by-side square cylinders using the lattice Boltzmann method

被引:141
作者
Agrawal, Amit [1 ]
Djenidi, Lyazid
Antonia, R. A.
机构
[1] Indian Inst Technol, Dept Mech Engn, Bombay 400076, Maharashtra, India
[2] Univ Newcastle, Discipline Mech Engn, Newcastle, NSW 2308, Australia
基金
澳大利亚研究理事会;
关键词
D O I
10.1016/j.compfluid.2005.05.008
中图分类号
TP39 [计算机的应用];
学科分类号
081203 ; 0835 ;
摘要
The low-Reynolds number flow around two square cylinders placed side-by-side is investigated using the lattice Boltzmann method (LBM). The effects of the gap ratio s/d (s is the separation between the cylinders and d is the characteristic dimension) on the flow are studied. These simulations reveal the existence of regimes with either synchronized or non-synchronized vortex-shedding, with transition occurring at s/d approximate to 2, which is larger than for circular cylinders. Detailed results are presented at Re = 73 for s/d = 2.5 and 0.7 corresponding to the synchronized and flip-flop regimes, respectively. Vortex-shedding from the cylinder occurs either in-phase or in-antiphase in the synchronized regime. However, linear stochastic estimate (LSE) calculations show that in-phase locking is the predominant mode. LSE is also employed to educe the underlying modes in the flip-flop regime, where evidence for both in-phase and anti-phase locked vortices is found, indicating that this regime is in a quasi-stable state between these two modes. The merging of the wakes, which is gradual for the synchronized regime, occurs rapidly in the flip-flop regime. The mean pressure on the upstream surface is symmetric and asymmetric for the synchronized and flip-flop regimes, respectively. Differences in results between the two regimes are interpreted in terms of the interaction of the jet formed between the cylinders with the adjoining wakes, the strength of this interaction depending on the spacing. (c) 2005 Elsevier Ltd. All rights reserved.
引用
收藏
页码:1093 / 1107
页数:15
相关论文
共 36 条
  • [1] ADRAIN RJ, 1994, APPL SCI RES, V53, P291
  • [2] Integral solution for the mean flow profiles of turbulent jets, plumes, and wakes
    Agrawal, A
    Prasad, AK
    [J]. JOURNAL OF FLUIDS ENGINEERING-TRANSACTIONS OF THE ASME, 2003, 125 (05): : 813 - 822
  • [3] Organizational modes of large-scale vortices in an axisymmetric turbulent jet
    Agrawal, A
    Prasad, AK
    [J]. FLOW TURBULENCE AND COMBUSTION, 2002, 68 (04) : 359 - 377
  • [4] Agrawal A, 2002, EXP FLUIDS, V33, P565, DOI [10.1007/S00348-002-0507-7, 10.1007/s00348-002-0507-7]
  • [5] INTERACTION BETWEEN A PAIR OF CIRCULAR-CYLINDERS NORMAL TO A STREAM
    BEARMAN, PW
    WADCOCK, AJ
    [J]. JOURNAL OF FLUID MECHANICS, 1973, 61 (NOV20) : 499 - &
  • [6] Accurate computations of the laminar flow past a square cylinder based on two different methods: lattice-Boltzmann and finite-volume
    Breuer, M
    Bernsdorf, J
    Zeiser, T
    Durst, F
    [J]. INTERNATIONAL JOURNAL OF HEAT AND FLUID FLOW, 2000, 21 (02) : 186 - 196
  • [7] Lattice Boltzmann method for fluid flows
    Chen, S
    Doolen, GD
    [J]. ANNUAL REVIEW OF FLUID MECHANICS, 1998, 30 : 329 - 364
  • [8] A cell boundary element method applied to laminar vortex shedding from circular cylinders
    Farrant, T
    Tan, M
    Price, WG
    [J]. COMPUTERS & FLUIDS, 2001, 30 (02) : 211 - 236
  • [9] LATTICE-GAS AUTOMATA FOR THE NAVIER-STOKES EQUATION
    FRISCH, U
    HASSLACHER, B
    POMEAU, Y
    [J]. PHYSICAL REVIEW LETTERS, 1986, 56 (14) : 1505 - 1508
  • [10] STOCHASTIC ESTIMATION OF MULTIPOINT CONDITIONAL AVERAGES AND THEIR SPATIOTEMPORAL EVOLUTION
    GIESEKE, TJ
    GUEZENNEC, YG
    [J]. APPLIED SCIENTIFIC RESEARCH, 1994, 53 (3-4): : 305 - 320