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Two-dimensional numerical study of vortex-induced vibration and galloping of square and rectangular cylinders in steady flow

机译:正方形和矩形圆柱体在稳定流动中涡流引起的振动和舞动的二维数值研究

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摘要

Flow induced vibrations of a square cylinder and a rectangular cylinder of an aspect ratio of 0.5 are investigated by two-dimensional numerical simulations. The two-dimensional unsteady Reynolds-averaged Navier-Stokes equations and the k-omega turbulence equations are solved by the finite element method. The numerical model is validated against the experimental data of flow past a stationary rectangular cylinder and flow induced vibration of a square cylinder. The focus of this study is to investigate the effects of the flow incidence angle on the response of the cylinder. The response of the square cylinder is dominated by galloping at the flow incidence angle of alpha=0 degrees and by vortex-induced vibration (VIV) at alpha=22.5 degrees and 45 degrees. The lower branch at alpha=45 degrees and the higher branch at alpha=22.5 degrees that are observed in the experiments in the previous studies are well predicted by the numerical model. The phase difference between the response displacement and the lift coefficient is found to be always close to 0 whenever galloping response occurs. The response of a rectangular cylinder of an aspect ratio of 0.5 is generally dominated by galloping at the flow incidence angle alpha=0 degrees and 90 degrees, with alpha=0 degrees corresponding to the case where the long boundary is perpendicular to the flow direction. The response of a rectangular cylinder at alpha=0 is the combination of galloping and VIV in the reduced velocity range of 7 <= V-r <= 11. At alpha=90 degrees, the galloping of a rectangular cylinder does not occur until the reduced velocity exceeds 22.5. As Vr < 22.5, the response amplitude for alpha=90 degrees is extremely small except in the very narrow lock-in regime of 4 <= V-r <= 6. The response frequency at galloping for a rectangular at alpha=90 degrees varies between 0.5 and 0.58. Galloping is not observed at alpha=45 degrees for a rectangular cylinder and at alpha=45 and 22.5 degrees for a square cylinder. (C) 2015 Elsevier Ltd. All rights reserved.
机译:通过二维数值模拟研究了纵横比为0.5的方圆柱和矩形圆柱的流动引起的振动。用有限元方法求解二维非稳态雷诺平均Navier-Stokes方程和k-omega湍流方程。根据流经固定矩形圆柱体的流动和矩形圆柱体的流动引起的振动的实验数据验证了该数值模型。这项研究的重点是研究流体入射角对气缸响应的影响。方形圆柱体的响应主要由在入射角为α= 0度时的疾驰和在α= 22.5度和45度时的涡激振动(VIV)决定。数值模型很好地预测了先前研究中在实验中观察到的α= 45度的较低分支和α= 22.5度的较高分支。发现响应位移和升力系数之间的相位差总是在出现驰豫响应时始终接近于0。长宽比为0.5的矩形圆柱体的响应通常由在入射角α= 0度和90度时的驰豫来决定,其中α= 0度对应于长边界垂直于流动方向的情况。矩形圆柱体在alpha = 0处的响应是在7 <= Vr <= 11的减小的速度范围内的舞动和VIV的组合。在alpha = 90度时,直到减小的速度,矩形圆柱体的舞动才发生超过22.5。当Vr <22.5时,除了在非常窄的锁定范围4 <= Vr <= 6之外,α= 90度的响应幅度非常小。矩形在α= 90度时疾驰的响应频率介于0.5和0.58。对于矩形圆柱体,在alpha = 45度处未观察到舞动,对于方形圆柱体,在alpha = 45和22.5度处未观察到舞动。 (C)2015 Elsevier Ltd.保留所有权利。

著录项

  • 来源
    《Ocean Engineering》 |2015年第15期|189-206|共18页
  • 作者单位

    Zhejiang Ocean Univ, Sch Math Phys & Informat Sci, Zhoushan 316000, Peoples R China;

    Univ Western Sydney, Sch Comp Engn & Math, Penrith, NSW 2751, Australia|Univ Western Sydney, Inst Infrastruct Engn, Penrith, NSW 2751, Australia;

    Dalian Univ Technol, State Key Lab Coastal & Offshore Engn, Dalian 116023, Peoples R China;

    Dalian Univ Technol, State Key Lab Coastal & Offshore Engn, Dalian 116023, Peoples R China|Univ Western Australia, Sch Civil Environm & Min Engn, Crawley, WA 6009, Australia;

  • 收录信息
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
  • 关键词

    Vortex-induced vibration; Numerical method; Vortex shedding; Square cylinder;

    机译:涡激振动;数值方法;涡脱落;方柱;

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