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Parameter Identification of RANS Turbulence Model Using Physics-Embedded Neural Network

Teacher Information

Name
CUI Jiahuan ZJU Faculty Homepage
Department
ZJUI
Research
CFD + turbomachinery, Machine learning + turbulence model, Aerodynamic Design of Aero-engine
Document Type
Book Chapter
High Performance Computing: ISC High Performance 2020 International Workshops, Frankfurt, Germany, June 2125, 2020, Revised Selected Papers

Publication

Chapter Title
Parameter Identification of RANS Turbulence Model Using Physics-Embedded Neural Network
Author
Shirui Luo, Madhu Vellakal, Seid Koric, Volodymyr Kindratenko & Jiahuan Cui
Page
pp 137–149
Source Title
High Performance Computing: ISC High Performance 2020 International Workshops, Frankfurt, Germany, June 2125, 2020, Revised Selected Papers
Author/Author of Source
Heike Jagode, Hartwig Anzt, Hatem Ltaief, Piotr Luszczek
Publisher
Springer
P-ISBN
9783030598501
Abstract

Identifying the appropriate parameters of a turbulence model for a class of flow usually requires extensive experimentation and numerical simulations. Therefore even a modest improvement of the turbulence model can significantly reduce the overall cost of a three-dimensional, time-dependent simulation. In this paper we demonstrate a novel method to find the optimal parameters in the Reynolds-averaged Navier–Stokes (RANS) turbulence model using high-fidelity direct numerical simulation (DNS) data. A physics informed neural network (PINN) that is embedded with the turbulent transport equations is studied, physical loss functions are proposed to explicitly impose information of the transport equations to neural networks. This approach solves an inverse problem by treating the five parameters in turbulence model as random variables, with the turbulent kinetic energy and dissipation rate as known quantities from DNS simulation. The objective is to optimize the five parameters in turbulence closures using the PINN leveraging limited data available from costly high-fidelity DNS data. We validated this method on two test cases of flow over bump. The recommended values were found to be
= 1.302,
= 1.862,
= 0.09,
= 0.75,
= 0.273; the mean absolute error of the velocity profile between RANS and DNS decreased by 22% when using these neural network inferred parameters.

DOI
https://doi.org/10.1007/978-3-030-59851-8

Print & Electronic Holdings

Holdings
International Campus Library-Special Collection
Call Number
TP3-532/LL1/12321/SC2
Barcode
000000337426
Database
Springer
Link