TY - JOUR
T1 - Fast simulation of airfoil flow field via deep neural network
AU - Zuo, Kuijun
AU - Ye, Zhengyin
AU - Bu, Shuhui
AU - Yuan, Xianxu
AU - Zhang, Weiwei
N1 - Publisher Copyright:
© 2024 Elsevier Masson SAS
PY - 2024/7
Y1 - 2024/7
N2 - Computational Fluid Dynamics (CFD) has become an indispensable tool in the optimization design, and evaluation of aircraft aerodynamics. However, solving the Navier-Stokes (NS) equations is a time-consuming, memory demanding and computationally expensive task. Artificial intelligence offers a promising avenue for flow field solving. In this work, we propose a novel deep learning framework for rapidly reconstructing airfoil flow fields. Channel attention and spatial attention modules are utilized in the downsampling stage of the UNet to enhance the feature learning capabilities of the deep learning model. Additionally, Embedding the predicted values of the deep learning model as initial values into the CFD solver to accelerate its iterative convergence. The NACA series airfoils were used to validate the prediction accuracy and generalization of the deep learning model. The experimental results represent the deep learning model achieving flow field prediction speed three orders of magnitude faster than CFD solver. Furthermore, the CFD solver integrated with deep learning model demonstrates a threefold acceleration compared to CFD solver. By extensively mining historical flow field data, an efficient solution is derived for the rapid simulation of aircraft flow fields.
AB - Computational Fluid Dynamics (CFD) has become an indispensable tool in the optimization design, and evaluation of aircraft aerodynamics. However, solving the Navier-Stokes (NS) equations is a time-consuming, memory demanding and computationally expensive task. Artificial intelligence offers a promising avenue for flow field solving. In this work, we propose a novel deep learning framework for rapidly reconstructing airfoil flow fields. Channel attention and spatial attention modules are utilized in the downsampling stage of the UNet to enhance the feature learning capabilities of the deep learning model. Additionally, Embedding the predicted values of the deep learning model as initial values into the CFD solver to accelerate its iterative convergence. The NACA series airfoils were used to validate the prediction accuracy and generalization of the deep learning model. The experimental results represent the deep learning model achieving flow field prediction speed three orders of magnitude faster than CFD solver. Furthermore, the CFD solver integrated with deep learning model demonstrates a threefold acceleration compared to CFD solver. By extensively mining historical flow field data, an efficient solution is derived for the rapid simulation of aircraft flow fields.
KW - Airfoil aerodynamics
KW - Deep learning
KW - Flow field prediction
KW - PHengLEI
UR - http://www.scopus.com/inward/record.url?scp=85193217132&partnerID=8YFLogxK
U2 - 10.1016/j.ast.2024.109207
DO - 10.1016/j.ast.2024.109207
M3 - 文章
AN - SCOPUS:85193217132
SN - 1270-9638
VL - 150
JO - Aerospace Science and Technology
JF - Aerospace Science and Technology
M1 - 109207
ER -