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Very Large-Eddy Simulations of the Flow Past an Oscillating Cylinder at a Subcritical Reynolds Number

机译:在子临界雷诺数的振动缸上的流量非常大的涡流模拟

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摘要

This work focuses on flow past a circular cylinder at a subcritical Reynolds number. Although this classical study has been a concern for many years, it is still a challenging task due to the complexity of flow characteristics. In this paper, a high-efficiency very large-eddy simulation method is adopted and verified in order to handle the oscillating boundary. A series of numerical simulations are conducted to investigate the transient flow around the oscillating cylinder. The results show that the vortex shedding mode varies with an increase in the excitation amplitude and the excitation frequency. Vortex shedding is a lasting process under the condition of a low excitation amplitude that leads to irregular fluctuations of the lift and drag coefficients. For a vortex shedding mode that exhibits a strong vortex pair and a weak vortex pair or a weak single vortex, the temporal evolution of the lift coefficient of the oscillating cylinder shows irregular ”jumping” at a specific time per cycle corresponding to the shedding of the strong vortex pair. The vortex shedding mode and the frequency and time of the vortex shedding co-determine the temporal evolutions of the lift and drag coefficient.
机译:这项工作侧重于在子临界雷诺数的圆柱体上流过来。虽然这种古典研究持续了很多年,但由于流动特征的复杂性,它仍然是一个具有挑战性的任务。在本文中,采用高效率非常大的涡流仿真方法,以便处理振荡边界。进行一系列数值模拟以研究振动缸周围的瞬态流动。结果表明,涡旋脱落模式随着激励幅度和激发频率的增加而变化。涡流脱落是在低激励幅度的条件下的持久过程,导致升力和拖动系数的不规则波动。对于呈现强涡体对的涡流脱落模式和弱涡流对或弱单涡流,振荡圆筒的升力系数的时间演变在对应于缩小的每个周期的特定时间时显示出不规则的“跳跃”强涡体对。涡旋脱落模式和涡旋脱落的频率和时间共确定电梯和拖曳系数的时间演变。

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