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An experimental investigation of flow-induced vibration of high-side-ratio rectangular cylinders

机译:高副比矩形圆柱体流动振动的实验研究

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This study reports an experimental investigation on the flow-induced vibration (FIV) of elastically mounted rectangular cylinders with high-side-ratio in free-stream flow. The side ratio (sigma), defined as the ratio of the cross-flow side width (h) to the streamwise side width (b) of the cylinder, namely sigma = h/b, was varied from 2.0 to 5.0. The fluid-structure system was modelled using a low-friction air-bearing system in conjunction with a free-surface water channel facility. The structural vibration was characterised over the reduced velocity range of 2 <= U* = U /(f(nw)h) <= 16, where U is the free stream velocity and f(nw) is the natural frequency of the system in quiescent water. The corresponding Reynolds number varied in the range of 940 <= Re = Uh/v <= 8200, where v is the fluid kinematic viscosity. The mass ratio, defined as the ratio of the oscillating mass to the displaced fluid mass, varied from 6.56 to 12.18, depending on the cylinder models. It was found that the vibration response was dominated by vortex-induced vibration (VIV) response for U* less than or similar to 8.4 for all the a cases tested. In the VIV lock-in regime, the local peak amplitude response was found to increase with a (i.e. from A/h similar or equal to 1.05 for sigma = 2.0 to A/h similar or equal to 1.69 for sigma = 5.0). Interestingly, beyond the VIV lock-in regime, while a galloping response was observed for the cases of sigma <= 4.0, where the vibration amplitude increased linearly with U*, the sigma = 5.0 case exhibited a bounded galloping regime with the amplitude increasing up to A/h similar or equal to 1.44 at U* = 10.8, prior to an abrupt drop to A/h approximate to 0.35 of a desynchronisation regime for higher U* values. The results suggest that this unexpected collapse of galloping response could be due to exceeding the relative incidence angle threshold for possible galloping. (C) 2019 Elsevier Ltd. All rights reserved.
机译:本研究报告了在自由流流动中具有高副比的弹性安装矩形圆柱体的流动诱导振动(FIV)的实验研究。定义为横流侧宽度(h)与圆柱的流动侧宽度(b)的比率,即sigma = h / b的比率从2.0到5.0变化。使用低摩擦空气轴承系统建模流体结构系统,与自由表面水通道设施相结合。结构振动的特征在于2 <= u * = U /(f(nw)h)<= 16的速度范围,其中U是自由流速度,f(nw)是系统的固有频率静态水。相应的雷诺数在940 <= re = uh / v <= 8200的范围内变化,其中V是流体运动粘度。定义为振荡质量与位移流体质量的比率的质量比率从6.56到12.18变化,这取决于气缸型号。发现振动响应由涡旋诱导的振动(VIV)响应为U *少于或类似于8.4所测试的涡流响应。在VIV锁定方案中,发现局部峰值振幅响应随着Sigma = 5.0的类似或等于1.69,用A(即/ h类似或等于1.05的局部峰值响应响应。有趣的是,除了VIV锁定方案之外,对于Sigma <= 4.0的病例观察到疾驰反应,其中振动幅度与U *线性增加,Sigma = 5.0案例表现出具有幅度增加的有界疾驰制度在U * = 10.8处相似或等于1.44,在突然下降到A / H近似为0.35的Desynchronisation制度,以获得更高的U *值。结果表明,这种意外崩溃的疾驰反应可能是由于可能疾驰的相对入射角阈值。 (c)2019年elestvier有限公司保留所有权利。

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