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Impact of transverse shear on vortex induced vibrations of a circular cylinder at low Reynolds numbers

机译:低雷诺数下横向剪切对圆柱体涡激振动的影响

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摘要

This paper presents a numerical investigation on the vortex induced vibrations (VIV) of an elastically mounted circular cylinder in linear shear flows at low Reynolds numbers with an aim to shed light on a novel aspect of the VIV phenomena, i.e., the impact of transverse shear. In this regard, two-dimensional numerical computations are carried out by deploying a stabilized space-time finite-element formulation. The Reynolds number and the shear parameter are considered in the ranges 70 ≤ Re ≤ 500 (for a fixed reduced velocity of U~* = 4.92) and 0% ≤ β ≤ 40%, respectively. The cylinder of low dimensionless mass (m~* = 10) is allowed to vibrate along both the transverse and in-line directions. The structural damping coefficient is kept zero to maximize the displacement response. Phenomena of hysteresis are observed around Re ~ 84 and 325. Modes of vortex shedding are 2S, C(2S) and S + P for various values of Re and β. However, only one hysteresis is observed for β = 40% at Re ~ 84. It is further observed that the maximum displacement along the transverse direction does not get affected by the shear introduced at the inlet, however, the maximum in-line displacement depends on the shear parameter. The maximum displacement along the in-line direction increases as the shear parameter increases. For the first hysteresis (Re ~ 84), the extent of Re (for maximum in-line displacement) varies as the shear parameter is changed. The range of Re for the second hysteresis (for all response parameters) depends on the shear parameter such as for β = 0-10% the range is 300-325, for β = 20% and 30% it is 325-340 and 225-325, respectively. Strouhal number variation with Re is similar to that for other variables. Plots of pressure coefficient distribution for all shear parameters for instantaneous flow field indicate that the difference between the maximum and the minimum values of the pressure coefficient can vary significantly depending on the Reynolds number and the shear parameter.
机译:本文对低雷诺数的线性剪切流中弹性安装圆柱的涡激振动(VIV)进行了数值研究,旨在阐明VIV现象的一个新方面,即横向剪切的影响。在这方面,通过采用稳定的时空有限元公式来进行二维数值计算。雷诺数和剪切参数的范围分别为70≤Re≤500(对于固定的降低速度U〜* = 4.92)和0%≤β≤40%。低无量纲质量(m〜* = 10)的圆柱体可以沿横向和轴向振动。结构阻尼系数保持为零以最大化位移响应。在Re〜84和325附近观察到磁滞现象。对于各种Re和β值,涡旋脱落的模式分别为2S,C(2S)和S +P。然而,在Re〜84处,β= 40%时仅观察到一个磁滞。进一步观察到,沿横向的最大位移不受入口处引入的剪切力的影响,但是,最大轴向位移取决于在剪切参数上。沿轴向的最大位移随剪切参数的增加而增加。对于第一个磁滞(Re〜84),Re的范围(最大轴向位移)随剪切参数的变化而变化。第二个磁滞的Re范围(对于所有响应参数)取决于剪切参数,例如对于β= 0-10%,范围是300-325,对于β= 20%和30%,范围是325-340和225分别为-325。 Re的Strouhal数变化与其他变量相似。瞬时流场所有剪切参数的压力系数分布图表明,压力系数的最大值和最小值之间的差值可能会根据雷诺数和剪切参数而发生显着变化。

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