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

机译:机翼湍流分离流的机器学习增强预测模型

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摘要

A modeling paradigm is developed to augment predictive models of turbulence by effectively using limited data generated from physical experiments. The key components of the current approach involve inverse modeling to infer the spatial distribution of model discrepancies and machine learning to reconstruct discrepancy information from a large number of inverse problems into corrective model forms. The methodology is applied to turbulent flows over airfoils involving flow separation. Model augmentations are developed for the Spalart-Allmaras model using adjoint-based full-field inference on experimentally measured lift coefficient data. When these model forms are reconstructed using neural networks and embedded within a standard solver, it is shown that much improved predictions in lift can be obtained for geometries and flow conditions that were not used to train the model. The neural-network-augmented Spalart-Allmaras model also predicts surface pressures extremely well. Portability of this approach is demonstrated by confirming that predictive improvements are preserved when the augmentation is embedded in a different commercial, finite element solver. The broader vision is that, by incorporating data that can reveal the form of the innate model discrepancy, the applicability of data-driven turbulence models can be extended to more general flows.
机译:通过有效利用物理实验生成的有限数据,开发了一种建模范例以增强湍流的预测模型。当前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,以及机器学习以将差异信息从大量逆问题重构为校正模型形式。该方法被应用于涉及流分离的翼型上的湍流。针对Spalart-Allmaras模型开发了模型增强功能,它使用了基于伴随的基于实测的升力系数数据的全场推断。当使用神经网络重构这些模型形式并将其嵌入标准求解器中时,可以证明,对于未用于训练模型的几何形状和流动条件,可以得到更大的升力预测。神经网络增强的Spalart-Allmaras模型还非常好地预测了表面压力。通过确认将扩展嵌入到不同的商业有限元求解器中,可以保留预测的改进,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。

著录项

  • 来源
    《AIAA Journal》 |2017年第7期|2215-2227|共13页
  • 作者单位

    Univ Michigan, Dept Aerosp Engn, Ann Arbor, MI 48104 USA;

    Altair Engn Inc, AcuSolve, Sunnyvale, CA 94086 USA;

    Univ Michigan, Dept Aerosp Engn, Ann Arbor, MI 48104 USA;

  • 收录信息 美国《科学引文索引》(SCI);美国《工程索引》(EI);
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
  • 关键词

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