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Numerical Computation for Vortex-Induced Vibrations of Two Tandem Circular Cylinders Arranged Exceeding the Critical Spacing

机译:超过临界间距布置的两个串联圆柱的涡激振动的数值计算

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We present numerical results for vibration responses of two circular cylinders which move to in-line and cross-flow directions along a smooth flow, and which are arranged at a spacing larger than the critical spacing of the centre-to-centre of the cylinders. When the Scruton number is low, it is well- known that two kinds of in-line vibrations, named first- and second-excited vibrations, occur in the range of low reduced velocities. On the other hand, when the reduced velocity exceeds approximately 5, it has been reported from many experimental data that the vortex-induced vibration (VIV) was observed in the wide range of the reduced velocity. In order to capture such vibration responses, numerical computations of the Navier-Stokes equations are carried out by means of the Petrov-Galerkin type finite element method and the arbitrary Lagrangian-Eulerian method. In addition, the numerical solution stabilization of the Navier-Stokes equations is performed by the third-order upwind scheme. From our numerical results, we discuss the response mechanisms of the cylinders in detail.
机译:我们给出了两个圆柱的振动响应的数值结果,这些圆柱沿着顺畅的流向沿直线和横流方向移动,并且其间距大于圆柱的中心到中心的临界间距。当Scruton数低时,众所周知,在降低的速度较低的范围内会发生两种直列振动,即第一和第二振动。另一方面,当减小的速度超过大约5时,从许多实验数据中已经报道,在减小的速度的宽范围内观察到涡激振动(VIV)。为了捕获这种振动响应,通过彼得罗夫-加勒金(Petrov-Galerkin)型有限元方法和任意拉格朗日-欧拉方法对Navier-Stokes方程进行了数值计算。另外,Navier-Stokes方程的数值解稳定化是通过三阶迎风方案进行的。从我们的数值结果,我们详细讨论了气缸的响应机制。

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