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A unified method of data assimilation and turbulence modeling for separated flows at high Reynolds numbers

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arxiv 2211.00601 v1 pith:BZSFS6IO submitted 2022-11-01 physics.flu-dyn cs.LG

classification physics.flu-dyncs.LG
keywords turbulencehighmodelsassimilationdataflowsnumbersreynolds
verification ladder T0 review T1 audit T2 compute T3 formal
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In recent years, machine learning methods represented by deep neural networks (DNN) have been a new paradigm of turbulence modeling. However, in the scenario of high Reynolds numbers, there are still some bottlenecks, including the lack of high-fidelity data and the convergence and stability problem in the coupling process of turbulence models and the RANS solvers. In this paper, we propose an improved ensemble kalman inversion method as a unified approach of data assimilation and turbulence modeling for separated flows at high Reynolds numbers. The trainable parameters of the DNN are optimized according to the given experimental surface pressure coefficients in the framework of mutual coupling between the RANS equations and DNN eddy-viscosity models. In this way, data assimilation and model training are combined into one step to get the high-fidelity turbulence models agree well with experiments efficiently. The effectiveness of the method is verified by cases of separated flows around airfoils(S809) at high Reynolds numbers. The results show that through joint assimilation of vary few experimental states, we can get turbulence models generalizing well to both attached and separated flows at different angles of attack. The errors of lift coefficients at high angles of attack are significantly reduced by more than three times compared with the traditional SA model. The models obtained also perform well in stability and robustness.

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  1. Enhanced State Estimation for turbulent flows combining Ensemble Data Assimilation and Machine Learning

    physics.flu-dyn 2025-01 conditional novelty 5.0 of 10

    Random Forest surrogates trained on Ensemble Kalman Filter outputs reproduce the filter's state estimation and IBM calibration for a turbulent channel flow at Re_tau~550, at lower runtime cost.

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