Development of Machine-Learnt Turbulence Closures for Wake Mixing Predictions in Low-Pressure Turbines

Yuri Frey Marioni, P. Adami, Raul Vázquez Díaz, Andrea Cassinelli, S. Sherwin, F. Montomoli
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Abstract

In this work, a DNS – Machine Learning (ML) framework is developed for low-pressure turbine (LPT) profiles to inform turbulence closures in Reynolds-Averaged Navier-Stokes (RANS) calculations. This is done by training the coeffcients of Explicit Algebraic Reynolds Stress Models (EARSM) with shallow artificial neural networks (ANN) as a function of input flow features. DNS data are generated with the incompressible Navier-Stokes solver in Nektar++ and validated against experiments. All calculations include moving bars upstream of the profile to capture the effect of incoming wakes. The resulting formulations are then implemented in the Rolls-Royce solver HYDRA and tested a posteriori. The aim is to improve mixing predictions in LPT wakes, compared to the baseline model, Wilcox’s k-ω SST, in terms of velocity profiles, turbulent kinetic energy (TKE) production and mixing losses. LPT calculations are run at Reynolds numbers spanning from ≈ 80k to ≈ 300k, to cover the range of aircraft engine applications. Models for the low and high Reynolds datasets are trained separately and a method is developed to merge the two together. The resulting model is tested on an intermediate Reynolds case. This process is followed for two computational domains: one starting downstream of the profile trailing edge and one including the last portion of the profile. Finally, the developed closures are tested on the entire profile, to confirm the validity of the improvements when the additional effect of transition is included in the simulation. This work explains the methodology used to develop ML-driven closures and shows how it is possible to combine models trained on different datasets.
用于低压涡轮尾流混合预测的机器学习湍流闭包的发展
在这项工作中,为低压涡轮(LPT)剖面开发了DNS -机器学习(ML)框架,以通知reynolds - average Navier-Stokes (RANS)计算中的湍流闭包。这是通过用浅层人工神经网络(ANN)训练显式代数雷诺应力模型(EARSM)的系数作为输入流特征的函数来完成的。利用Nektar++中的不可压缩Navier-Stokes解算器生成DNS数据,并通过实验进行验证。所有的计算都包括在剖面的上游移动杆,以捕捉入射尾迹的影响。然后在Rolls-Royce求解器HYDRA中实施所得公式并进行后验测试。与基线模型(Wilcox’s k-ω SST)相比,其目的是在速度分布、湍流动能(TKE)产生和混合损失方面改进LPT尾迹的混合预测。LPT计算在≈80k到≈300k的雷诺数范围内运行,以覆盖飞机发动机应用的范围。低和高雷诺数数据集的模型分别训练,并开发了一种将两者合并在一起的方法。在中等雷诺数情况下对所得模型进行了验证。该过程适用于两个计算域:一个从剖面后缘下游开始,一个包括剖面的最后部分。最后,开发的闭包在整个剖面上进行测试,以确认在模拟中包含过渡的额外影响时改进的有效性。这项工作解释了用于开发ml驱动闭包的方法,并展示了如何将在不同数据集上训练的模型组合起来。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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