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The Reynolds stresses equation modelling in the prediction of flow past a rotating cylinder at high Reynolds number.

机译:雷诺兹应用方程模型来预测高雷诺数下旋转圆柱体的流动。

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摘要

This research presents the predictions of flow past a rotating cylinder at a sub-critical Reynolds number of 130,000. The main objective is to identify turbulence effective modelling strategies for unsteady RANS computations. For this reason both effective viscosity and stress-transport models have been used with different strategies for the modelling of near-wall turbulence which include standard log-law-based, and more refined wall functions, the latter based on the analytical solution of 1-D equations for the transport of wall-parallel momentum. The models' effectiveness is assessed through comparisons with available experimental and Large Eddy Simulation (LES) data. It is important that these present studies are in a good agreement with those obtained by the decreasing drag coefficient and increasing lift coefficient when a spin ratios (α : proportional tangential velocity of the cylinder wall to inlet flow velocity) of a cylinder grow up. Moreover, the stability of the flow domain is well improved with the suppressed vortex shedding, as well. Significantly, the prediction of the position of stagnation and separation flow position correspond to the magnitude of lift, drag coefficient and the rotation direction. Overall, this research has confirmed that the RSMs is capable to examine the external flow and more sensitized on the curvature surface flow .
机译:这项研究提出了在亚临界雷诺数为130,000时流过旋转圆柱体的流动的预测。主要目标是确定用于不稳定RANS计算的湍流有效建模策略。因此,有效的粘度模型和应力传递模型都已用于不同的近壁湍流建模策略,其中包括基于标准对数律和更精细的壁函数,后者基于1-的解析解壁平行动量传输的D方程。通过与可用的实验数据和大涡模拟(LES)数据进行比较来评估模型的有效性。重要的是,这些当前研究与当气缸的旋转比(α:气缸壁的切向速度与入口流速的比例成正比)增长时通过减小阻力系数和增大升力系数所获得的研究保持良好的一致性。此外,通过抑制涡旋脱落,也可以很好地改善流域的稳定性。重要地,停滞位置和分离流位置的预测对应于升力,阻力系数和旋转方向的大小。总的来说,这项研究已经证实,RSM能够检查外部流,并且对曲率表面流更加敏感。

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