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APPLICATION OF DELAYED DETACHED EDDY SIMULATION AND RANS TO COMPRESSOR CASCADE FLOW

机译:延迟分离涡模拟和转速在压气机叶栅流动中的应用。

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Spalart-Allmaras (S-A) model based Delayed Detached Eddy Simulation (DDES) is performed to investigate the flow field in a compressor cascade (NACA64A-905) with experimental data for calibration. The value of the modeling coefficient C_(DES) in DDES is open for revision and depends heavily on the numerical schemes. The effects of C_(DES) on the DDES results are studied and an optimal C_(DES) value is estimated for the specific case, with MUSCL reconstructed Roe scheme incorporated in in-house CFD codes. C_(DES) value of 0.2 is turned out reliable concerning both accuracy and convergence. S-A model is also performed for comparison. Results from different methods indicate that the time-averaged results by DDES with C_(DES) of 0.2 are more consistent with the experimental results than those by S-A model. The instantaneous flow field predictions show that DDES is well capable of capturing the unsteady features of the cascade flow, especially the wake mixing process.
机译:进行了基于Spalart-Allmaras(S-A)模型的延迟分离涡流仿真(DDES),以研究带有实验数据的压缩机叶栅(NACA64A-905)中的流场,以进行校准。 DDES中的建模系数C_(DES)的值可以修改,并且在很大程度上取决于数值方案。研究了C_(DES)对DDES结果的影响,并结合了内部CFD代码中的MUSCL重构Roe方案,针对特定情况估算了最佳C_(DES)值。事实证明C_(DES)值0.2在准确性和收敛性方面都是可靠的。还执行S-A模型以进行比较。不同方法的结果表明,C_(DES)为0.2的DDES的时间平均结果比S-A模型的时间平均结果更符合实验结果。瞬时流场预测表明,DDES能够很好地捕获级联流的不稳定特征,尤其是尾流混合过程。

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