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Numerical study of turbulent trailing-edge flows with base cavity effects using URANS

机译:基于URANS的具有基腔效应的湍流后缘流动数值研究。

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摘要

Turbulent flows over lifting surfaces exhibiting trailing-edge vortex shedding often cause adverse and complex phenomena, such as self-induced vibration and noise. In this paper, a numerical study on flow past a blunt-edged two-dimensional NACA 0015 section and the same section with various base cavity shapes and sizes at high Reynolds numbers has been performed using the unsteady Reynolds-averaged Navier-Stokes (URANS) approach with the realisable κ-ε turbulence model. The equations are solved using the control volume method of second-order accuracy in both spatial and time domains. The assessment of the application of URANS for periodic trailing-edge flow has shown that reasonable agreement is achieved for both the time-averaged and fluctuating parameters of interest, although some differences exist in the prediction of the near-wake streamwise velocity fluctuation magnitudes. The predicted Strouhal numbers of flows past the squared-off blunt configuration with varying degrees of bluntness agree well with published experimental measurements. It is found that the intensity of the vortex strengths at the trailing-edge is amplified when the degree of bluntness is increased, leading to an increase in the mean square pressure fluctuations. The numerical prediction shows that the presence of the base cavity at the trailing-edge does not change the inherent Strouhal number of the 2D section examined. However, it does have an apparent effect on the wake structure, local pressure fluctuations and the lift force fluctuations. It is observed that the size of the cavity has more influence on the periodic trailing-edge flow than its shape does.
机译:升力面上的湍流呈现出后缘涡旋脱落,通常会引起不利和复杂的现象,例如自感振动和噪声。在本文中,使用不稳定的雷诺平均Navier-Stokes(URANS)进行了流经钝边二维NACA 0015部分和具有不同基腔形状和尺寸的同一部分的流的数值研究,该部分具有高雷诺数可实现的κ-ε湍流模型的方法。在空间和时域中均使用二阶精度的控制量方法求解方程。对URANS在周期性后缘流动中的应用进行的评估表明,尽管在预测近尾流速度速度波动幅度方面存在一些差异,但对于感兴趣的时间平均和波动参数均实现了合理的一致。超过平方钝器构型且钝度程度不同的预测Strouhal流量与已发布的实验测量结果非常吻合。发现当钝度增加时,在后缘处的涡流强度的强度被放大,从而导致均方压力波动的增加。数值预测表明在后缘的基腔的存在不会改变所检查的2D截面的固有Strouhal数。但是,它确实对尾流结构,局部压力波动和升力波动具有明显的影响。可以看出,空腔的尺寸比其形状对周期性后沿流动的影响更大。

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