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首页> 外文期刊>Modern Physics Letters, B. Condensed Matter Physics, Statistical Physics, Applied Physics >Transient cavitating vortical flows around a hydrofoil using k-omega partially averaged Navier-Stokes model
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Transient cavitating vortical flows around a hydrofoil using k-omega partially averaged Navier-Stokes model

机译:使用k-ω部分平均Navier-Stokes模型的水翼周围的瞬时空化涡流

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摘要

For accurate simulations of wall-bounded turbulent cavitating flows, the present paper proposed a partially averaged Navier Stokes (PANS) method derived from the k-omega turbulence model. Transient cavitating vortical flows around a NACA66 hydrofoil were simulated by using the k-omega PANS model with various filter parameters (f(k) = 0.2, 0.5 and 1, while f(w) = 1/f(k)) and a mass transfer cavitation model based on the Rayleigh Plesset equation. Compared with the available experimental data, the k-omega PANS model with f(k) = 0.2 can accurately reproduce the cavitation evolution with more complicated structures due to the reduction in the predicted eddy viscosity. Further analyses, using the vorticity transport equation, indicate that the transition of cavitation structure from two dimension to three dimension is associated with strong vortex cavitation interaction, where vortex stretching and dilation may play a major role. Therefore, the k-omega PANS model with the filter parameter of f(k) = 0.2 is an effective method to numerically predict the transient cavitating vortical flows around hydrofoils. The results obtained in this paper are helpful to provide a physical insight into the mechanisms of cavitation shedding dynamics.
机译:为了精确模拟壁面湍流空化流,本文提出了一种从k-ω湍流模型推导的局部平均Navier Stokes(PANS)方法。使用k-omega PANS模型模拟了具有各种过滤器参数(f(k)= 0.2、0.5和1,而f(w)= 1 / f(k))和质量的NACA66水翼周围的瞬时空化涡流。 Rayleigh Plesset方程的水汽化空化模型。与可用的实验数据相比,f-(k)= 0.2的k-omega PANS模型可以准确地重现具有更复杂结构的空化演化,这是因为预测的涡流粘度降低了。使用涡度输运方程进行的进一步分析表明,空化结构从二维向三维的过渡与强烈的涡流空化相互作用有关,其中涡旋拉伸和膨胀可能起主要作用。因此,滤波器参数为f(k)= 0.2的k-omega PANS模型是一种有效地数值预测水翼周围瞬态空化涡流的有效方法。本文获得的结果有助于对空化脱落动力学机制提供物理见解。

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