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Numerical Investigation on Vortex Shedding from a Hydrofoil with a Beveled Trailing Edge

机译:后缘斜面翼型涡流脱落的数值研究

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To better understand the vortex shedding mechanism and to assess the capability of our numerical methodology, we conducted numerical investigations of vortex shedding from truncated and oblique trailing edges of a modified NACA 0009 hydrofoil. The hybrid particle-mesh method and the vorticity-based subgrid scale model were employed to simulate these turbulent wake flows. The hybrid particle-mesh method combines the vortex-in-cell and the penalization methods. We have implemented numerical schemes to more efficiently use available computational resources. In thisstudy, we numerically investigated vortex shedding from various beveled trailing edges at a Reynolds number of 106. We then compared the numerical results with the experimental data, which show good agreement. We also conducted numerical simulations of wakes behind the hydrofoil at rest in periodically varying flows. Results reveal that vortex shedding is affected by the periodicity of a free-stream flow, as well as the trailing-edge shape.
机译:为了更好地理解涡旋脱落机理并评估我们的数值方法的能力,我们对改进的NACA 0009水翼的截尾和斜后缘进行了涡旋脱落的数值研究。混合粒子网方法和基于涡度的亚网格规模模型被用来模拟这些湍流尾流。混合粒子网格方法结合了单元内涡旋和惩罚方法。我们已经实施了数值方案来更有效地利用可用的计算资源。在本研究中,我们对雷诺数为106的各种斜切后沿的涡旋脱落进行了数值研究。然后,我们将数值结果与实验数据进行了比较,结果显示出良好的一致性。我们还进行了周期性变化流动中静水翼后尾流的数值模拟。结果表明,涡流脱落受到自由流的周期性以及后缘形状的影响。

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