International Journal of Numerical Methods for Heat & Fluid Flow ( IF 4.2 ) Pub Date : 2023-04-17 , DOI: 10.1108/hff-08-2022-0488 Cornelia Grabe , Florian Jäckel , Parv Khurana , Richard P. Dwight
Purpose
This paper aims to improve Reynolds-averaged Navier Stokes (RANS) turbulence models using a data-driven approach based on machine learning (ML). A special focus is put on determining the optimal input features used for the ML model.
Design/methodology/approach
The field inversion and machine learning (FIML) approach is applied to the negative Spalart-Allmaras turbulence model for transonic flows over an airfoil where shock-induced separation occurs.
Findings
Optimal input features and an ML model are developed, which improve the existing negative Spalart-Allmaras turbulence model with respect to shock-induced flow separation.
Originality/value
A comprehensive workflow is demonstrated that yields insights on which input features and which ML model should be used in the context of the FIML approach
中文翻译:
用于跨音速流预测的 RANS 湍流模型的数据驱动扩充
目的
本文旨在使用基于机器学习 (ML) 的数据驱动方法改进雷诺平均纳维斯托克斯 (RANS) 湍流模型。特别关注确定用于 ML 模型的最佳输入特征。
设计/方法/途径
场反演和机器学习 (FIML) 方法应用于负 Spalart-Allmaras 湍流模型,用于跨翼型上的跨音速流动,其中发生冲击引起的分离。
发现
开发了最佳输入特征和 ML 模型,改进了现有的关于冲击引起的流动分离的负 Spalart-Allmaras 湍流模型。
原创性/价值
展示了一个全面的工作流程,可以深入了解在 FIML 方法的上下文中应该使用哪些输入特征和哪个 ML 模型