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Machine Learning-augmented Predictive Modeling of Turbulent Separated Flows over Airfoils

机译:机械学习增强的湍流分离预测模型   飞过翼型

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摘要

A modeling paradigm is developed to augment predictive models of turbulenceby effectively utilizing limited data generated from physical experiments. Thekey components of our approach involve inverse modeling to infer the spatialdistribution of model discrepancies, and, machine learning to reconstructdiscrepancy information from a large number of inverse problems into correctivemodel forms. We apply the methodology to turbulent flows over airfoilsinvolving flow separation. Model augmentations are developed for the SpalartAllmaras (SA) model using adjoint-based full field inference on experimentallymeasured lift coefficient data. When these model forms are reconstructed usingneural networks (NN) and embedded within a standard solver, we show that muchimproved predictions in lift can be obtained for geometries and flow conditionsthat were not used to train the model. The NN-augmented SA model also predictssurface pressures extremely well. Portability of this approach is demonstratedby confirming that predictive improvements are preserved when the augmentationis embedded in a different commercial finite-element solver. The broader visionis that by incorporating data that can reveal the form of the innate modeldiscrepancy, the applicability of data-driven turbulence models can be extendedto more general flows.
机译:通过有效利用物理实验产生的有限数据,开发了一种建模范例以增强湍流的预测模型。我们方法的关键组成部分包括逆模型以推断模型差异的空间分布,以及机器学习以将大量逆问题中的差异信息重构为校正模型形式。我们将该方法应用于涉及流分离的机翼上的湍流。针对SpalartAllmaras(SA)模型开发了模型增强功能,它使用了基于伴随的全场推断,对实验测量的升力系数数据进行了推断。当使用神经网络(NN)重构这些模型形式并将其嵌入标准求解器中时,我们表明,对于未用于训练模型的几何形状和流动条件,可以得到大大提高的升力预测。 NN增强的SA模型还可以非常好地预测表面压力。通过确认将增强嵌入到不同的商业有限元求解器中,可以保持预测的改进,从而证明了该方法的可移植性。广义的观点是,通过合并可以揭示先天模型差异形式的数据,可以将数据驱动的湍流模型的适用性扩展到更通用的流程。

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