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Numerical Simulation of Vortex-Induced Motion of a Circular Cylinder with Low Mass-Damping

机译:低质量阻尼的圆柱体涡激运动的数值模拟

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In this paper, our in-house RANS solver, naoe-FOAM-SJTU,rndeveloped using OpenFOAM is applied to numerically simulate thernVIM of a 2-D circular cylinder with low mass-damping. The responsernand vortex modes of an elastically mounted rigid circular cylinderrnconstrained to oscillate transversely to a free stream are numericallyrninvestigated. Computations are carried out for reduced velocities fromrn1.5 to 13, corresponding to a range of 1500 to 13000 in Reynoldsrnnumber. The mass ratio is 2.4 and the mass-damping is 0.013. Thesernparameters are set to be identical with those of the benchmarkingrnexperiment conducted by Khalak and Williamson (1996). The beatingrnphenomenon in initial branch is supported by two peak in FFT analysis.rnOne difference in the response of cylinder between present study andrnexperiment results from the system's tendency to keep its earlier state.rnThe intermittent change of vortex modes at U*= 2.9375, whichrncorresponds to maximum amplitude of vibration, indicates the upperrnbranch should be described as intermittent switching between initialrnand lower branch. The computational results of response of cylinderrnand the vortex mode in the wake are in good agreement with thernexperimental results except for the absence of upper branch.
机译:本文将我们使用OpenFOAM开发的内部RANS求解器naoe-FOAM-SJTU应用于数值模拟具有低质量阻尼的二维圆柱的rnVIM。数值研究了弹性安装的刚性圆柱的响应模式和涡旋模式,这些模式被约束为横向于自由流振荡。进行计算以将速度从rn1.5降低到13,相当于雷诺数在1500到13000之间。质量比为2.4,质量阻尼为0.013。这些参数设置为与Khalak和Williamson(1996)进行的基准测试相同。初始分支中的跳动现象由FFT分析中的两个峰支持.rn本研究与实验之间的圆柱体响应存在一个差异,是由于系统趋于保持其较早状态的趋势.rn U * = 2.9375时涡旋模式的间歇性变化,对应于最大振动幅度,指示上分支应描述为初始分支和下分支之间的间歇切换。尾流中圆柱体和涡旋模式的响应计算结果与实验结果吻合良好,只是没有上部分支。

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