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首页> 外文期刊>Journal of Marine Science and Engineering >Large Eddy Simulation of Flow over Wavy Cylinders with Different Twisted Angles at a Subcritical Reynolds Number
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Large Eddy Simulation of Flow over Wavy Cylinders with Different Twisted Angles at a Subcritical Reynolds Number

机译:亚临界雷诺数下具有不同扭转角的波浪形圆柱体流动的大涡模拟

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The deformation of the cylinder has been proved to greatly reduce the fluctuation of lift and the vortex-induced vibration. In this article, a new form of deformation mode for the smooth cylinder is proposed in order to reduce the vortex-induced vibrations, which can be applied to marine risers and submarine pipelines to ensure the working performance and safety of offshore platforms. Large eddy simulation (LES) is adopted to simulate the turbulent flow over wavy cylinders with three different twisted angles at a subcritical Reynolds number Re = 28,712. Comparing with the results of smooth cylinder, the maximum drag and lift reduction of wavy cylinder A3 with α = 40° can reach 17% and 84%, respectively, and the corresponding vortex formation length increases significantly, while the turbulence intensity decreases relatively. Meanwhile, the circumferential minimum pressure coefficient is greater than that of the smooth cylinder, which also provides a greater drag reduction for the cylinder. The surface separation line, turbulent kinetic energy distribution, and wake vortex structure indicate that the elongation of separated shear layer and wake shedding position is larger than that of the smooth cylinder, and the vorticity value in the near wake region decreases. A periodic vortex structure is generated along the spanwise direction, and a weaker and more stable Karman vortex street is reformed at a further downstream position, which ultimately leads to the reduction of drag and fluctuating lift of the wavy cylinder.
机译:气缸的变形已被证明可以大大减小升力的波动和涡流引起的振动。为了减少涡流引起的振动,本文提出了一种新型的光滑圆柱体变形模式,可以应用于海洋立管和海底管道,以确保海上平台的工作性能和安全性。采用大涡模拟(LES)来模拟亚临界雷诺数Re = 28,712时具有三个不同扭转角的波浪形圆柱上的湍流。与光滑圆柱体的结果相比,α= 40°的波浪圆柱体A3的最大阻力和升力减小分别可以达到17%和84%,相应的涡流形成长度显着增加,而湍流强度则相对减小。同时,周向最小压力系数大于平滑圆柱体的圆周最小压力系数,这也为圆柱体提供了更大的阻力减小。表面分离线,湍动能分布和尾流涡结构表明,分离的剪切层的伸长率和尾流脱落位置大于光滑圆柱体的伸长率,近尾流区的涡度值减小。沿翼展方向生成周期性的涡旋结构,并且在更下游的位置处对较弱且更稳定的卡曼涡旋街进行了改造,最终导致了阻力的减小和波浪形圆柱体的起伏波动。

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