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Unsteady flow past a turbine blade using non-linear two-equation turbulence models

机译:使用非线性二方程湍流模型的非定常流过涡轮叶片

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The flow past turbine blades with thick trailing edges is chearacterized by periodically separating large scale vortices. The failure of two-equation turbulence models to predict the near wake of a turbine blade correctly appears to be mainly due to the inability of accounting properly for the large scale statistics. The investigation presented here should reveal if a time-dependent calculation in conjunction with a linear as well as a non-linear two-equation model can prescribe these flow fields better than a steady state calculation since the arge scale vortices are resolved by the numerical scheme and the turbulence model must account only for the small scales.
机译:通过周期性地分离大型旋涡,可以使流经具有厚后缘的涡轮叶片的流动得到特征化。两方程湍流模型无法正确预测涡轮机叶片的近尾流,这似乎主要是由于无法正确考虑大规模统计数据所致。此处进行的研究应该揭示,与线性和非线性二方程模型相结合的时变计算是否可以比稳态计算更好地规定这些流场,因为通过数值方案可以解决大规模涡旋问题湍流模型必须仅考虑小尺度。

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