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>Numerical simulation of flows around two unyawed and yawed wavy cylinders in tandem arrangement
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Numerical simulation of flows around two unyawed and yawed wavy cylinders in tandem arrangement
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机译:串联排列的两个未偏航和偏航波浪圆柱体周围流动的数值模拟
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摘要
The turbulent flows around two fixed unyawed and yawed wavy cylinders in tandem arrangement at a subcritical Reynolds number of 3900 were studied using three-dimensional large eddy simulation. A range of spacing (L) between the cylinders from 1.5D m to 5.5D m with yaw angles of α=0°, 30° were investigated so as to identify the effects of cylinder spacing ratio and yaw angle as well as the coupling effects of the two wavy cylinders in tandem. The instantaneous near wake flow patterns around the cylinders were captured. Flows around circular cylinders with the same configurations were also obtained for comparison. The effects of the vortex shedding from the upstream cylinder on the fluid-dynamic forces acting on the downstream one were examined. Results show that vortex shedding behind the upstream wavy cylinder occurs at a further downstream position compared with that of the circular upstream cylinder. This leads to the weakening of the effect of bodies' vibration of the cylinders as well as an evident reduction of drag. With a yaw angle of 30°, the vortex formation lengths behind both the upstream and downstream cylinders decrease, typically for the wavy cylinders configuration. However, the effects of drag reduction and the control of bodies' vibration still exist except for the spacing ratio of L/D m=3.5, which is in the critical spacing ratio regime for two wavy cylinders in tandem.
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机译:利用三维大涡模拟研究了亚临界雷诺数为3900时,两个固定的未偏航和偏航的波浪圆柱体串联排列时的湍流。研究了偏航角为α= 0°,30°的1.5D m至5.5D m的气缸之间的间距(L)范围,以确定气缸间距比和偏航角的影响以及耦合效应串联的两个波浪圆柱体。捕获了圆柱周围的瞬时近尾流模式。为了比较,还获得了具有相同构造的圆柱体周围的流动。考察了涡流从上游气缸脱落对作用在下游气缸上的流体动力的影响。结果显示,与圆形上游圆柱体相比,上游波浪圆柱体后面的涡流脱落发生在更下游的位置。这导致气缸的车身振动效果减弱,阻力明显减小。当偏航角为30°时,上游和下游圆柱体后部的涡流形成长度会减小,通常对于波浪形圆柱体配置而言。但是,除了L / D m = 3.5的间距比(这是串联的两个波浪圆柱的临界间距比范围)外,减阻和控制车身振动的效果仍然存在。
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