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Numerical simulation of super upper branch of a cylindrical structure with a low mass ratio

机译:低质量比圆柱结构超上部分支的数值模拟

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摘要

SST (shear stress transport) k-omega and Newmark-beta methods are used to comprehensively understand vortex-induc ed vibration (VIV) characteristics of a cylindrical structure with a mass ratio of 2.6 in a range of reduced velocity from 2.0 to 14.0. The details of drag and lift forces, cross-flow and streamwise displacements, vortex pattern, trajectory, and frequency of VIV are presented and compared systematically with the experimental work of Jauvtis and Williamson that first captured the super upper branch in VIV with the maximum value of 1.5 D (diameter). In this study, the numerical simulation results successfully captured the initial branch, the lower branch, and the super upper branch. Very few research studies have successfully simulated the super upper branch by numerical methods. The vibration amplitude corresponding to the super upper branch is stable and the maximum value of the super upper branch is 1.46 D, which is fairly consistent with the results of the Jauvtis and Williamson experiment. This research also successfully captured the law of trajectory under different reduced velocities. With the reduced velocity increasing, the trajectories switch from an irregular shape to a regular "Figure 8" shape and then enter into an irregular movement, finally again into a regular movement of a Figure 8 shape or crescent. In the range of the super upper branch, the vibration trajectories gradually change from a Figure 8 shape to a crescent shape with the increase of the transverse vibration amplitude. This work has successfully captured the different vortex patterns corresponding to each branch under different reduced velocities, and found the transitional forms of 2S to 2T, 2T to 2P, and 2P to 2S, respectively.
机译:SST(剪切应力传输)k-ω和Newmark-beta方法用于全面理解质量比为2.6的圆柱结构在2.0到14.0的降低速度范围内的涡激振动(VIV)特性。介绍了阻力和升力,横流和水流位移,涡流模式,轨迹和VIV频率的详细信息,并将其与Jauvtis和Williamson的实验工作进行了系统比较,Jauvtis和Williamson首先以最大值捕获了VIV的超上部分支1.5 D(直径)。在这项研究中,数值模拟结果成功捕获了初始分支,下部分支和超上部分支。很少有研究通过数值方法成功地模拟超高层分支。超上部分支所对应的振动幅度是稳定的,超上部分支的最大值为1.46 D,与Jauvtis和Williamson实验的结果相当一致。该研究还成功地捕获了不同降低速度下的轨迹定律。随着减小的速度增加,轨迹从不规则形状切换为规则的“图8”形状,然后进入不规则运动,最后再次变为图8形状或新月形的规则运动。在超上部分支的范围内,随着横向振动幅度的增加,振动轨迹从图8的形状逐渐变为新月形。这项工作成功地捕获了在不同降低速度下对应于每个分支的不同涡旋模式,并分别找到了2S到2T,2T到2P和2P到2S的过渡形式。

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