A tensor basis neural network-based turbulence model for transonic axial compressor flows

被引:5
作者
Ji, Ziqi [1 ]
Du, Gang [1 ]
机构
[1] Beihang Univ, Sch Energy & Power Engn, Beijing 100191, Peoples R China
关键词
Transonic axial compressor; Turbulence model; Non-linear eddy viscosity model; Machine learning; Tensor basis neural network; Large eddy simulation;
D O I
10.1016/j.ast.2024.109155
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
Traditional turbulence models encounter limitations when simulating intricate flows within transonic axial compressors. In contrast, recent advancements in machine learning turbulence models have demonstrated enhanced potential in refining the precision of turbulence modeling. Notably, the tensor basis neural network (TBNN) methodology has successfully developed non-linear eddy viscosity turbulence models. These models possess the capability to capture the anisotropic characteristic of Reynolds stress. However, applying machine learning non-linear eddy viscosity models to aircraft turbomachinery remains relatively infrequent. Current research mainly focuses on linear eddy viscosity turbulence models based on the Boussinesq hypothesis that presupposes isotropy in Reynolds stress. In this work, we introduce a non-linear eddy viscosity turbulence model, denoted as the k-w-SST-TBNN model based on the TBNN framework. This model has been employed to simulate the transonic axial compressor NASA Rotor 37. The TBNN is trained using large eddy simulation (LES) results datasets. The importance of input scalar features is analyzed using the random forest method, from which significant and low -degree variables are selected as inputs for the TBNN. Furthermore, this study proposes including the turbulent Mach number as one of the extra features, representing fluid compressibility, thereby extending the computational mass flow rate range of compressor. Additionally, this paper proposes a method involving the weighted average of Reynolds stress, combining the high -precision but less robust TBNN predictions with results based on the Boussinesq assumption to enhance the turbulence model's robustness. The trained k-w-SST-TBNN model undergoes validation on Rotor 37, where it exhibits a marked improvement in the prediction of overall performance, tip -gap vortex, and radial distribution of flow parameters. The model also displays a commendable capacity for generalization.
引用
收藏
页数:14
相关论文
共 54 条
[1]  
Akolekar H.D., 2019, P 24 INT SOC AIR BRE, P22
[2]   Integration of Machine Learning and Computational Fluid Dynamics to Develop Turbulence Models for Improved Low-Pressure Turbine Wake Mixing Prediction [J].
Akolekar, Harshal D. ;
Zhao, Yaomin ;
Sandberg, Richard D. ;
Pacciani, Roberto .
JOURNAL OF TURBOMACHINERY-TRANSACTIONS OF THE ASME, 2021, 143 (12)
[3]  
Biau G., 2015, arXiv
[4]  
Chima R., 2009, 47 AIAA AER SCI M IN
[5]   The use of the Reynolds force vector in a physics informed machine learning approach for predictive turbulence modeling [J].
Cruz, Matheus A. ;
Thompson, Roney L. ;
Sampaio, Luiz E. B. ;
Bacchi, Raphael D. A. .
COMPUTERS & FLUIDS, 2019, 192
[6]  
DENTON J., 1997, J THERM SCI, V6, P1, DOI DOI 10.1007/S11630-997-0010-9
[7]  
Duraisamy K, 2015, 53 AIAA AEROSPACE SC, P1284, DOI DOI 10.2514/6.2015-1284
[8]   Turbulence Modeling in the Age of Data [J].
Duraisamy, Karthik ;
Iaccarino, Gianluca ;
Xiao, Heng .
ANNUAL REVIEW OF FLUID MECHANICS, VOL 51, 2019, 51 :357-377
[9]  
El Baz A.M. E., 1993, Engineering Turbulence Modelling and Experiments, P63
[10]   Numerical and experimental investigation of transverse injection flows [J].
Erdem, E. ;
Kontis, K. .
SHOCK WAVES, 2010, 20 (02) :103-118