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Three-dimensional numerical simulations of vortex-induced vibrations of tapered circular cylinders

机译:锥形圆柱体涡激振动的三维数值模拟

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Vortex-induced vibration (VIV) of a tapered cylinder is investigated numerically at a constant Reynolds number of 500 using three-dimensional numerical simulations. The objectives of the study is to identify the difference between the response of a tapered cylinder and that of a uniform cylinder. Simulations are conducted for the lengths and the taper ratios the same as those in the published experimental studies. Two, cylinders are considered: one with a length to diameter ratio of 4.3 and a mass ratio of 2.27 and another one with a length to diameter ratio of 12.3 and a mass ratio of 6.1. Detailed analysis of the vibration amplitude and frequency, the vortex shedding flow mode and the lift coefficient are performed for the longer cylinder. It was found that the frequencies of the vortex shedding and the lift coefficient synchronize with the vibration frequency in the lock-in regime, but vary along the cylinder span outside the lock-in regime. For some reduced velocities, it is found that vortex shedding is in 2P mode at the small diameter part and 2S mode at the larger-diameter part of the cylinder, forming a hybrid flow mode. The change of the flow mode on the cylinder span corresponds to the change of the phase difference between the lift coefficient and the displacement for about 180 degrees. The lock-in regime of a tapered cylinder is found to be wider than that of an equivalent uniform cylinder. (C) 2016 Elsevier Ltd. All rights reserved.
机译:使用三维数值模拟,以恒定的雷诺数500数值研究了锥形圆柱的涡激振动(VIV)。该研究的目的是确定锥形圆柱体和均匀圆柱体的响应之间的差异。长度和锥度比的仿真与已发表的实验研究相同。考虑两个圆柱体:一个圆柱体的长径比为4.3,质量比为2.27,另一个圆柱体的长径比为12.3,质量比为6.1。对于较长的气缸,将进行振动幅度和频率,涡流脱落模式和升力系数的详细分析。发现在锁定状态下涡旋脱落的频率和升力系数与振动频率同步,但是在锁定状态外沿着汽缸跨度变化。对于某些降低的速度,发现在圆柱体的小直径部分涡旋脱落处于2P模式,在大直径部分涡旋脱落处于2S模式,形成了混合流动模式。汽缸跨度上流动模式的变化对应于升力系数与位移之间大约180度的相位差变化。发现锥形圆柱体的锁定方式比等效的均匀圆柱体的锁定方式宽。 (C)2016 Elsevier Ltd.保留所有权利。

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