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

机译:使用非线性两方程湍流模型的涡轮机刀片不稳定流动

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摘要

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规模涡流,具有厚的后缘的流动涡轮机叶片的流动是刺痛的。两个方程湍流模型预测涡轮叶片的近尾曲目的故障似乎主要是由于对大规模统计数据正常的无法计入。这里提出的调查应该揭示如果与线性的时间和非线性两方程模型结合的时间依赖性计算可以比稳态计算更好地规定这些流场,因为使用数值方案解决了Arge比例涡流并且湍流模型必须仅占小尺度。

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