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Comparison of two unsteady intermittency models for bypass transition prediction on a turbine blade profile

机译:两种非定常间歇模型在涡轮叶片轮廓上进行旁路过渡预测的比较

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摘要

The present paper evaluates two unsteady transition modelling approaches: the prescribed unsteady intermittency method PUIM, developed at Cambridge University and the dynamic unsteady intermittency method developed at Ghent University. The methods are validated against experimental data for the N3-60 steam turbine stator profile for steady and for unsteady inlet flow conditions. The characteristic features of the test case are moderately high Reynolds number and high inlet turbulence intensity, which causes bypass transition. The tested models rely both on the intermittency parameter and are unsteady approaches. In the prescribed method, the time-dependent intermittency distribution is obtained from integral relations. In the dynamic method, the intermittency distribution follows from time-dependent differential equations. For unsteady computations, self-similar wake profiles are prescribed at the inlet of the computational domain. Joint validation of the prescribed and the dynamic unsteady intermittency models against experimental data shows that both methods are able to reproduce the global features of the periodical evolution of the boundary layer under the influence of a periodically impinging wake. The overall quality of the dynamic method is better than that of the prescribed method.
机译:本文评估了两种非稳态过渡建模方法:剑桥大学开发的规定非稳态间歇方法PUIM和根特大学开发的动态非间歇方法。该方法已针对N3-60汽轮机定子轮廓的实验数据进行了验证,以验证稳态和非稳态进气流量情况。测试用例的特征是中等高的雷诺数和较高的入口湍流强度,这会导致旁路过渡。所测试的模型既依赖于间歇性参数,又是不稳定的方法。在规定的方法中,时间相关的间歇分布是从积分关系中获得的。在动态方法中,间断分布遵循与时间有关的微分方程。对于不稳定的计算,在计算域的入口处规定了自相似的唤醒轮廓。针对实验数据对规定的和动态的非连续性间歇模型进行的联合验证表明,两种方法都能够重现周期性撞击的影响下边界层周期性演化的整体特征。动态方法的整体质量优于规定方法。

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