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Numerical Study on Vortex Induced Vibrations of Four Cylinders in an In-Line Square Configuration

机译:在线方形配置中涡旋诱导涡旋振动的数值研究

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The two-dimensional numerical simulation of the vortex induced vibrations of four cylinders in an inline square arrangement is investigated at low Reynolds number in this paper. The mean and fluctuating aerodynamic forces, Strouhal number (St) and vortex shedding pattern in the wake for each cylinder are analyzed with the six spacing ratio L/d changing from 2.5 to 6.0.The results indicate that the mean drag force and the fluctuating lift forces and the transverse displacements of the upstreaM cylinders are relatively larger than the downstreaM cylinders, and the downstream cylinders usually undergoing serious fluctuating streamwise displacement. The dominant frequency of drag coefficient is equal to St of downstream cylinders for all spacing ratio, so the simultaneous resonance in the in-flow and cross-flow directions may occur for downstream structures of multi-body oscillating system. The streamwise oscillation of downstreaM cylinders which is free to move in two degrees of freedom could be as large as 0.75 diameter, and the maximum transverse amplitude of upstream cylinders may achieve 0.82 diameter, is much higher than the transverse amplitude of flow around a single cylinder at same parameter setting.
机译:在本文的低雷诺数,在内线方案中的涡旋诱导振动的二维数值模拟在内联方向上的低雷诺数。通过从2.5到6.0改变的六个间距比L / D分析了每个气缸的六个间距比L / D中的平均和波动的平均值和波动脱落图案。结果表明平均阻力和波动升降机上游气缸的力和横向位移比下游圆筒相对大,并且通常经历严重波动的流动位移的下游圆筒。用于所有间隔比的拖曳系数的主导频率等于下游圆筒的ST,因此可以出现流动和横流方向上的同时谐振,用于多体振荡系统的下游结构。下游气缸的流动振荡可以在两度自由中移动可以大约0.75直径,上游圆柱体的最大横向幅度可以实现0.82直径,远高于单个圆筒周围的流量的横向幅度在相同的参数设置。

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