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Numerical Approach Dedicated to Nozzle Tip Clearance Flow Analysis in Variable Geometry Radial Turbines

机译:变几何径向涡轮专用于喷嘴尖端间隙流动分析的数值方法

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摘要

The present paper consists in a numerical analysis of a variable geometry radial turbine stage, for three opening configurations. The presence of the endwall clearance in the stator creates additional secondary flows upstream from the rotor, which tend to increase the stator–rotor interactions. Those interactions are filtered in steady-state simulations, for which the accuracy is expected to decrease. A comparison between steady-state mixing plane simulations and a Non Linear Harmonic (NLH) approach is thus proposed, together with an analysis of the influence of the numbers of harmonics chosen for the NLH simulations. The results show that the implementation of clearances in the simulationsudincreases the discrepancies between the two methods, especially for configurations naturally sensitive to stator–rotor interactions (open stator configuration). Regarding the number of harmonics for the numerical setting, a criterion proposed in the literature is discussed at the end of the paper, and provides good guidelines in order to avoid a full harmonics convergence analysis.
机译:本文包括对三种开口配置的可变几何径向涡轮级的数值分析。定子中端壁间隙的存在会在转子上游产生额外的二次流,这会增加定子与转子之间的相互作用。这些相互作用在稳态仿真中被过滤,因此预计精度会降低。因此,提出了稳态混合平面仿真与非线性谐波(NLH)方法之间的比较,并分析了为NLH仿真选择的谐波数量的影响。结果表明,在间隙中实施间隙会增大两种方法之间的差异,特别是对于对定子-转子相互作用自然敏感的配置(开放式定子配置)。关于用于数值设置的谐波数量,本文末尾讨论了文献中提出的准则,该准则为避免全面的谐波收敛分析提供了良好的指导。

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