Temporal predictions of periodic flows using a mesh transformation and deep learning-based strategy

被引:22
作者
Deng, Zhiwen [1 ]
Liu, Hongsheng [1 ]
Shi, Beiji [1 ]
Wang, Zidong [1 ]
Yu, Fan [1 ]
Liu, Ziyang [2 ,3 ]
Chen, Gang [2 ,3 ]
机构
[1] Huawei Technol Co Ltd, Shenzhen 518129, Peoples R China
[2] Xi An Jiao Tong Univ, Sch Aerosp Engn, Shaanxi Key Lab Environm & Control Flight Vehicle, Xian 710049, Peoples R China
[3] Xi An Jiao Tong Univ, Sch Aerosp Engn, State Key Lab Strength & Vibrat Mech Struct, Xian 710049, Peoples R China
关键词
Unsteady flow prediction; Mesh transformation; Deep learning; Data driven; FRAMEWORK;
D O I
10.1016/j.ast.2022.108081
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
This paper focuses on the temporal prediction of unsteady flow based on a combination of mesh transformation and deep learning technology. To this end, a body-fitted mesh interpolation was first implemented to extract the flow information in the region of interest and maintain the detailed flow information in the boundary layer. Subsequently, a mesh transformation technique was applied to map the physical coordinates into the curvilinear coordinates to obtain a structural uniform mesh, which is facilitated for the implementation the structural neural networks. Ultimately, two advanced neural networks, i.e., Unet and Fourier Neural Operator (FNO), were used for establishing the relationship between flow at previous time steps and that at future time steps. Two flow configurations numerically simulated-i.e., a laminar flow around a cylinder at Re = 200 and a transonic buffet of a supercritical airfoil at Ma = 0.73-were selected as the benchmarks to demonstrate the effectiveness and robustness of the proposed strategy. The results indicated that the flow at future time steps can be accurately obtained using that at the previous time steps via both neural networks, even in a complicated flow scenario. The velocity and pressure of the periodic flow can be faithfully predicted with a remarkable accuracy. Additionally, the derived flow physical quantities were comprehensively compared, which demonstrated that better performance can be achieved using FNO with a lower relative loss and a shorter training time-consuming. (c) 2022 Elsevier Masson SAS. All rights reserved.
引用
收藏
页数:19
相关论文
共 32 条
[11]   NSFnets (Navier-Stokes flow nets): Physics-informed neural networks for the incompressible Navier-Stokes equations [J].
Jin, Xiaowei ;
Cai, Shengze ;
Li, Hui ;
Karniadakis, George Em .
JOURNAL OF COMPUTATIONAL PHYSICS, 2021, 426
[12]   Self-sustained shock oscillations on airfoils at transonic speeds [J].
Lee, BHK .
PROGRESS IN AEROSPACE SCIENCES, 2001, 37 (02) :147-196
[13]   Low-Reynolds-number airfoil design optimization using deep-learning-based tailored airfoil modes [J].
Li, Jichao ;
Zhang, Mengqi ;
Tay, Chien Ming Jonathan ;
Liu, Ningyu ;
Cui, Yongdong ;
Chew, Siou Chye ;
Khoo, Boo Cheong .
AEROSPACE SCIENCE AND TECHNOLOGY, 2022, 121
[14]   On deep-learning-based geometric filtering in aerodynamic shape optimization [J].
Li, Jichao ;
Zhang, Mengqi .
AEROSPACE SCIENCE AND TECHNOLOGY, 2021, 112
[15]   Unsteady aerodynamic reduced-order modeling based on machine learning across multiple airfoils [J].
Li, Kai ;
Kou, Jiaqing ;
Zhang, Weiwei .
AEROSPACE SCIENCE AND TECHNOLOGY, 2021, 119
[16]   Efficient prediction of transonic flutter boundaries for varying Mach number and angle of attack via LSTM network [J].
Li, Wencheng ;
Gao, Xiumin ;
Liu, Haojie .
AEROSPACE SCIENCE AND TECHNOLOGY, 2021, 110
[17]  
Li ZY, 2021, Arxiv, DOI [arXiv:2111.03794, DOI 10.48550/ARXIV.2111.03794]
[18]  
Li ZY, 2021, Arxiv, DOI arXiv:2010.08895
[19]  
Liu Z., 2022, AEROSP SCI TECHNOL
[20]  
Lu L, 2020, Arxiv, DOI [arXiv:1910.03193, DOI 10.48550/ARXIV.1910.03193]