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Vortex-induced vibrations of three staggered circular cylinders at low Reynolds numbers

机译:在低雷诺数的涡旋诱导的三个交错圆柱的振动

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摘要

Vortex- induced vibrations of three staggered circular cylinders are investigated via two-dimensional finite element computations. All the cylinders are of equal diameter (D) and are mounted on elastic supports in both streamwise (x-) and transverse (y-) directions. The two downstream cylinders are placed symmetrically on either side of the upstream body at a streamwise gap of 5D, with the vertical distance between them being 3D. Flow simulations are carried out for Reynolds numbers (Re) in the range of Re = 60-160. Reduced mass (m*) of 10 is considered and the damping is set to zero value. The present investigations show that the upstream cylinder exhibits initial and lower synchronization response modes like an isolated cylinder does at low Re. Whereas for both the downstream cylinders, the upper lock-in branch also appears. The initial and the upper modes are characterized by periodic oscillations, while the lower lock- in branch is associated with nonperiodic vibrations. The 2S mode of vortex shedding is observed in the near wake of all the cylinders for all Re, except for the upper branch corresponding to the downstream bodies. In the upper branch, both the downstream cylinders shed the primary vortices of the P+S mode. For the upstream cylinder, the phase between lift and the transverse displacement exhibits a 180 degrees jump at certain Re in the lower branch. On the other hand, the downstream bodies undergo transverse oscillations in phase with lift in all lock- in modes, while the phase jumps by 180 degrees as the oscillation response reaches the desynchronization regime. Published by AIP Publishing.
机译:通过二维有限元计算研究了三个交错圆柱体的涡旋振动。所有气缸都具有相同的直径(d),并且安装在流动(X-)和横向(Y型)方向上的弹性支撑上。两个下游圆筒在上游主体的两侧对称地放置在5d的流动间隙中,它们是3D之间的垂直距离。在RE = 60-160的范围内进行雷诺数(RE)的流动模拟。考虑减少10的质量(m *),阻尼被设定为零值。本研究表明,上游圆筒呈现出初始和较低的同步响应模式,如隔离的圆筒在低RE处。而对于下游气缸,也会出现上游锁定分支。初始和上部模式的特征在于周期性振荡,而下锁定分支与非周期性振动相关联。除了与下游体对应的上部分支外,在所有汽缸的近似尾部观察到2S涡流模式。在上部分支中,下游气缸都脱落了P + S模式的主涡旋。对于上游圆筒,升力与横向位移之间的相位在下部分支中的某些RE处跳跃180度。另一方面,下游体在所有锁定模式中升力地经历横向振荡,而振荡响应达到去异步制度,相位跳跃180度。通过AIP发布发布。

著录项

  • 来源
    《Physics of fluids 》 |2017年第8期| 共15页
  • 作者单位

    Aditya Inst Technol &

    Management Dept Mech Engn Tekkali 532201 AP India;

    ESI Software I Pvt Ltd 27th Cross Banashankari 2nd Stage Bangalore 560070 KA India;

    Indian Inst Technol Madras Dept Civil Engn Madras 600036 TN India;

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  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类 流体力学 ;
  • 关键词

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