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TRANSITION PREDICTION ON TURBINE BLADE PROFILE WITH INTERMITTENCY TRANSPORT EQUATION

机译:间歇传输方程的涡轮叶片轮廓过渡预测

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The paper presents the results of tests and validations of γ-Re_θ model proposed by Menter at al [10], which was extended by in-house correlations on onset location and transition length. The tests performed were based on experimental data on the flat plate Test Cases available at ERCOFTAC Data Base as well as on experimental data of turbine blade profile investigated at Czestochowa University of Technology. Further on, the model was applied for unsteady calculations of the blade profile test case, where chosen inlet conditions (turbulent intensity, wake parameters) were applied. For the selected case numerical results were compared not only with the experimental data, but also with the results obtained with other transition models.It was shown that the applied model was able to reproduce some essential flow features related to the bypass and wake-induced transitions and the simulations reveal good agreement with the experimental results in terms of localisation and extent of wake-induced transition.
机译:本文介绍了Menter等人[10]提出的γ-Re_θ模型的测试和验证结果,并通过内部相关的发病位置和转移长度对其进行了扩展。进行的测试基于ERCOFTAC数据库上可用的平板测试用例上的实验数据,以及在琴斯托霍瓦工业大学研究的涡轮叶片轮廓的实验数据。此外,该模型用于叶片轮廓测试用例的非稳定计算,其中应用了选定的入口条件(湍流强度,尾流参数)。对于选定的情况,数值结果不仅与实验数据进行了比较,而且还与其他过渡模型获得的结果进行了比较。 结果表明,所应用的模型能够重现与旁路和尾流引起的过渡有关的一些基本流动特征,并且模拟在尾流引起的过渡的位置和程度方面与实验结果很好地吻合。

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