LES study on traveling wave wall control for the wake of flow around a 3D circular cylinder at high Reynolds number

被引:2
|
作者
Xu, Feng [1 ,4 ]
Liu, Xin [1 ]
Chen, Wen-Li [2 ,3 ]
Duan, Zhong-Dong [1 ]
Ou, Jin-Ping [1 ]
机构
[1] Harbin Inst Technol Shenzhen, Sch Civil & Environm Engn, Shenzhen, Peoples R China
[2] Harbin Inst Technol, Minist Ind & Informat Technol, Key Lab Smart Prevent & Mitigat Civil Engn Disaste, Harbin, Peoples R China
[3] Harbin Inst Technol, Minist Educ, Key Lab Struct Dynam Behav & Control, Harbin, Peoples R China
[4] Univ Town Shenzhen, Harbin Inst Technol Shenzhen, Sch Civil & Environm Engn, Shenzhen, Peoples R China
基金
中国国家自然科学基金;
关键词
traveling wave wall; flow control; three-dimensional circular cylinder; wake; large eddy simulation; VORTEX-INDUCED VIBRATION; BOUNDARY-LAYER; DRAG REDUCTION; RECTANGULAR PRISMS; FLUID-DYNAMICS; SUPPRESSION; TURBULENCE; AERODYNAMICS; STREET; LIFT;
D O I
10.1177/13694332231216307
中图分类号
TU [建筑科学];
学科分类号
0813 ;
摘要
Flow around a cylinder is an important research problem in fluid mechanics. However, studies on traveling wave wall (TWW) flow control for the wake generated by the flow around a 3D cylinder remain limited. This study performs large eddy simulation (LES) to investigate the wake characteristics of flow around a three-dimensional (3D) circular cylinder with the TWW. The influence of the main control parameters of TWW on the aerodynamic forces and wake of the 3D cylinder is analyzed. The wake characteristics of the 3D cylinder at Re = 4 x 104 are obtained, and the traveling wave propagating downstream is achieved on the rear surface of the 3D cylinder using dynamic mesh. The control effects of wave amplitude, number of waves, and wave velocity of the traveling wave on the aerodynamic forces of the cylinder are analyzed, and the optimal control parameter combination is determined. The results demonstrate that the TWW control method completely eliminates the spanwise 3D flow characteristics of the cylinder when the amplitude ratio, number of waves, and velocity ratio are 0.02, 4, and 1.5, respectively. Moreover, it effectively suppresses the flow separation on the cylinder surface, eliminates the wake vortex, and suppresses vortex-induced vibration (VIV).
引用
收藏
页码:157 / 176
页数:20
相关论文
共 50 条
  • [21] 3D Printed Structured Porous Treatments for Flow Control around a Circular Cylinder
    Bathla, Pranjal
    Kennedy, John
    FLUIDS, 2020, 5 (03)
  • [22] Experimental and numerical study of the separation angle for flow around a circular cylinder at low Reynolds number
    Wu, MH
    Wen, CY
    Yen, RH
    Weng, MC
    Wang, AB
    JOURNAL OF FLUID MECHANICS, 2004, 515 : 233 - 260
  • [23] Three dimensionality in the wake of the flow around a circular cylinder at Reynolds number 5000 (vol 147, pg 102, 2017)
    Aljure, D. E.
    Lehmkhul, O.
    Rodriguez, I.
    Oliva, A.
    COMPUTERS & FLUIDS, 2017, 156 : 545 - 545
  • [24] On uniform planar shear flow around a circular cylinder at subcritical Reynolds number
    Sumner, D
    Akosile, OO
    JOURNAL OF FLUIDS AND STRUCTURES, 2003, 18 (3-4) : 441 - 454
  • [25] DNS of flow around a circular cylinder at a subcritical Reynolds number with cartesian grids
    Tremblay, F
    Manhart, M
    Friedrich, R
    ADVANCES IN TURBULENCE VIII, 2000, : 659 - 662
  • [26] Flow around a circular cylinder in linear shear flows at subcritical Reynolds number
    Cao, Shuyang
    Tamura, Yukio
    JOURNAL OF WIND ENGINEERING AND INDUSTRIAL AERODYNAMICS, 2008, 96 (10-11) : 1961 - 1973
  • [27] Numerical investigation of flow around a slotted circular cylinder at low Reynolds number
    Bao, Zhenzhong
    Qin, Guoliang
    He, Wenqiang
    Wang, Yazhou
    JOURNAL OF WIND ENGINEERING AND INDUSTRIAL AERODYNAMICS, 2018, 183 : 273 - 282
  • [28] Particle capture and low-Reynolds-number flow around a circular cylinder
    Espinosa-Gayosso, Alexis
    Ghisalberti, Marco
    Ivey, Gregory N.
    Jones, Nicole L.
    JOURNAL OF FLUID MECHANICS, 2012, 710 : 362 - 378
  • [29] Viscous near-wall flow in a wake of circular cylinder at moderate Reynolds numbers
    D. I. Okhotnikov
    V. M. Molochnikov
    A. B. Mazo
    A. V. Malyukov
    A. E. Goltsman
    I. I. Saushin
    Thermophysics and Aeromechanics, 2017, 24 : 873 - 882
  • [30] Viscous near-wall flow in a wake of circular cylinder at moderate Reynolds numbers
    Okhotnikov, D. I.
    Molochnikov, V. M.
    Mazo, A. B.
    Malyukov, A. V.
    Goltsman, A. E.
    Saushin, I. I.
    THERMOPHYSICS AND AEROMECHANICS, 2017, 24 (06) : 873 - 882