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Two-degree-of-freedom flow-induced vibrations on isolated and tandem cylinders with varying natural frequency ratios

机译:具有不同固有频率比的隔离和串联气缸上的两自由度流动引起的振动

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A numerical study is performed on the flow-induced vibrations of isolated and tandem elastically mounted cylinders having two degrees of freedom and a variety of the in-line to the transverse natural frequency ratio, f_(nx)/f_(ny). The characteristic-based-split finite element method is utilized to obtain the solution of the incompressible flow equations in primitive variables. The Reynolds number, based on the upstream flow velocity U_∞ and the diameter of the cylinder D, is fixed at Re=150, and for a tandem arrangement, the centre-to-centre distance between the cylinders is 5.0D. The computation is carried out at a lower reduced mass ratio of M_r=2.0 and for a wide range of reduced velocities (U_r=3.0-12.0). The structural damping ratio is set to zero to maximize the vortex-induced response of the bodies. In this study, we mainly focused on the effect of the natural frequency ratio on the characteristics of vortex-induced vibration (VIV) responses, including wake frequencies, orbital trajectories, response amplitudes, hydrodynamic forces and wake mode patterns. The natural frequency ratio is varied in the range of f_(nx)/f_(ny) = 1.0-2.0 with an increment of 0.25. We found that the condition of the occurrence of a dual-resonant response exists over a broad range of tested natural frequency ratios. A third harmonic frequency component appears in the lift fluctuation, along with additional multi-harmonics, which also interact with the drag frequency. Instead of double response peaks, multiple small peaks occur in the amplitude response of the cylinder. These peaks are distributed over a narrow range of U_r from 4.45 to 5.15, and their magnitudes increase with the increase in U_r. For a tandem arrangement, the response characteristic of the upstream cylinder is similar to that of a single cylinder, whereas that of the downstream cylinder is greatly affected by the upstream wake. For a downstream cylinder, the in-line dynamic response is more sensitive to the natural frequency ratio than the response in the transverse direction. As the dual-resonance is excited, the isolated cylinder and the upstream cylinder of the tandem arrangement may show a P+S wake pattern, which strongly suppresses the vortex shedding of the downstream cylinder.
机译:对具有两个自由度和多种直插式与横向固有频率之比f_(nx)/ f_(ny)的隔离和串联弹性安装的气缸的流动引起的振动进行了数值研究。基于特征的分裂有限元方法被用于获得原始变量中不可压缩流方程的解。基于上游流速U_∞和气缸D的直径,雷诺数固定为Re = 150,对于串联布置,气缸之间的中心距为5.0D。在较低的降低质量比M_r = 2.0且针对较宽的降低速度范围(U_r = 3.0-12.0)进行计算。将结构阻尼比设置为零,以使涡旋感应的物体响应最大化。在这项研究中,我们主要关注自然频率比对涡激振动(VIV)响应特征的影响,包括尾迹频率,轨道轨迹,响应幅度,流体动力和尾迹模式模式。固有频率比在f_(nx)/ f_(ny)= 1.0-2.0的范围内变化,增量为0.25。我们发现发生双共振响应的条件存在于广泛的测试自然频率比范围内。三次谐波频率分量出现在升力波动中,同时还有其他多谐波,也与阻力频率相互作用。代替双响应峰,在圆柱体的幅度响应中出现多个小峰。这些峰值分布在从4.45到5.15的U_r窄范围内,并且它们的幅度随U_r的增加而增加。对于串联布置,上游气缸的响应特性类似于单个气缸的响应特性,而下游气缸的响应特性受上游尾流的影响很大。对于下游气缸,与横向响应相比,在线动态响应对固有频率比更敏感。随着双重共振的激发,串联布置的隔离圆柱体和上游圆柱体可能会显示P + S尾流模式,从而强烈抑制了下游圆柱体的涡旋脱落。

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