Some new characteristics of the confined flow over circular cylinders at low reynolds numbers

被引:17
|
作者
Ooi, A. [1 ]
Chan, L. [1 ]
Aljubaili, D. [1 ]
Mamon, C. [1 ]
Leontini, J. S. [2 ]
Skvortsov, A. [3 ]
Mathupriya, P. [4 ]
Hasini, H. [4 ]
机构
[1] Univ Melbourne, Dept Mech Engn, Melbourne, Vic 3010, Australia
[2] Swinburne Univ Technol, Dept Mech Engn & Prod Design Engn, Hawthorn, Vic 3122, Australia
[3] Def Sci & Technol, Maritime Div, Fishermans Bend, Vic 3207, Australia
[4] Univ Tenaga Nas, Dept Mech Engn, Kajang 43000, Malaysia
关键词
Confined cylinder flows; Numerical simulations; Floquet analysis; LARGE-EDDY SIMULATION; NUMERICAL-SIMULATION; STABILITY ANALYSIS; INDUCED VIBRATION; SQUARE CYLINDER; WAKE; TRANSITION; LAMINAR;
D O I
10.1016/j.ijheatfluidflow.2020.108741
中图分类号
O414.1 [热力学];
学科分类号
摘要
This study summarises some new characteristics of the fluid flow over a confined circular cylinder at low Reynolds numbers. Results from both two- and three-dimensional direct numerical simulations are presented at blockage ratio between 0.1 and 0.9 and Reynolds number between 120 and 500. Floquet stability analysis of selected cases will also be presented. From the two-dimensional simulations, it is found that the fluctuating lift forces decreases with blockage ratio and becomes zero (where the flow is steady) at blockage ratio of approximately 0.7-0.8. Upon further increasing the blockage ratio to 0.9, the simulations show a dramatic increase in the fluctuating lift forces, nearly an order of magnitude greater than previously reported for an unconfined cylinder flow. It is also found that for blockage ratio of 0.5, there is a long term two-dimensional instability that becomes more prominent with increasing Reynolds number. This instability has a time scale of approximately 105 time units (D/U-max) at Reynolds number of 500. In addition, the transition between two- and three-dimensional flow at blockage ratios up to 0.5 is investigated. It is shown that the transition Reynolds number decreases with increasing blockage ratio. At high blockage ratio of 0.5, as we increase the Reynolds number, the transition to three-dimensional flow is shown to go from unsteady two-dimensional to steady three-dimensional before transitioning to unsteady three-dimensional flow.
引用
收藏
页数:11
相关论文
共 50 条
  • [11] Flow-induced vibrations of four circular cylinders with square arrangement at low Reynolds numbers
    Han, Zhaolong
    Zhou, Dai
    He, Tao
    Tu, Jiahuang
    Li, Chunxiang
    Kwok, Kenny C. S.
    Fang, Congqi
    OCEAN ENGINEERING, 2015, 96 : 21 - 33
  • [12] Uniform-shear flow over a circular cylinder at low Reynolds numbers
    Kang, S.
    JOURNAL OF FLUIDS AND STRUCTURES, 2006, 22 (04) : 541 - 555
  • [13] Characteristics of the flow over a NACA 0012 airfoil at low Reynolds numbers
    Derksen, R. W.
    Agelinchaab, M.
    Tachie, M.
    ADVANCES IN FLUID MECHANICS VII, 2008, 59 : 143 - 152
  • [14] Flow Characteristics over Double Delta Wings at Low Reynolds Numbers
    Karasu, Ilyas
    Durhasan, Tahir
    JOURNAL OF AEROSPACE ENGINEERING, 2020, 33 (04)
  • [15] SETTLING VELOCITIES OF CIRCULAR-CYLINDERS AT LOW REYNOLDS-NUMBERS
    KOMAR, PD
    JOURNAL OF GEOLOGY, 1980, 88 (03): : 327 - 336
  • [17] Wake transitions of six tandem circular cylinders at low Reynolds numbers
    Eizadi, Hamidreza
    An, Hongwei
    Zhou, Tongming
    Zhu, Hongjun
    Cheng, Liang
    PHYSICS OF FLUIDS, 2022, 34 (02)
  • [18] Flow-induced vibrations of two side-by-side circular cylinders at low Reynolds numbers
    Chen, Weilin
    Ji, Chunning
    Xu, Dong
    An, Hongwei
    Zhang, Zhimeng
    PHYSICS OF FLUIDS, 2020, 32 (02)
  • [19] NUMERICAL ANALYSIS OF FLOW-INDUCED VIBRATION OF TWO CIRCULAR CYLINDERS IN TANDEM AT LOW REYNOLDS NUMBERS
    Teixeira, Paulo R. F.
    Didier, Eric
    11TH WORLD CONGRESS ON COMPUTATIONAL MECHANICS; 5TH EUROPEAN CONFERENCE ON COMPUTATIONAL MECHANICS; 6TH EUROPEAN CONFERENCE ON COMPUTATIONAL FLUID DYNAMICS, VOLS II - IV, 2014, : 2160 - 2171
  • [20] ASSESSMENT OF FLOW INTERACTIONS BETWEEN CIRCULAR CYLINDERS AND NACA-0018 HYDROFOILS AT LOW REYNOLDS NUMBERS
    Kermani, Saman
    Ghadimi, Parviz
    BRODOGRADNJA, 2017, 68 (04): : 103 - 120