TY - GEN
T1 - A novel deep learning model for the flow field reconstruction of an oscillating airfoil
AU - Li, Yunzhu
AU - Liu, Tianyuan
AU - You, Jiarui
AU - Xie, Yonghui
N1 - Publisher Copyright:
© 2021 by Siemens Energy Global GmbH & Co. KG.
PY - 2021
Y1 - 2021
N2 - In this paper, a novel model is presented for reconstructing unsteady periodic fields of velocity vector and pressure scalar over an oscillating foil. This data-driven method based on convolutional neural network can be utilized to accomplish two objections: fields reconstruction from limited measurements and transient aerodynamic characteristics prediction. The verification results of an oscillating foil under low Reynolds number show that this method can accurately reconstruct all the fields only by limited pressure information at probes on the foil surface. The evaluation on aerodynamic characteristics prediction illustrates that our model outperforms four classical machine learning methods. Meanwhile, a well-trained CNN model can almost achieve real-time flow field prediction by leveraging the GPU acceleration. Finally, the exploration of the robustness for the CNN model is conducted on several aspects, including training size, probe layouts, probe numbers and measurement noises.
AB - In this paper, a novel model is presented for reconstructing unsteady periodic fields of velocity vector and pressure scalar over an oscillating foil. This data-driven method based on convolutional neural network can be utilized to accomplish two objections: fields reconstruction from limited measurements and transient aerodynamic characteristics prediction. The verification results of an oscillating foil under low Reynolds number show that this method can accurately reconstruct all the fields only by limited pressure information at probes on the foil surface. The evaluation on aerodynamic characteristics prediction illustrates that our model outperforms four classical machine learning methods. Meanwhile, a well-trained CNN model can almost achieve real-time flow field prediction by leveraging the GPU acceleration. Finally, the exploration of the robustness for the CNN model is conducted on several aspects, including training size, probe layouts, probe numbers and measurement noises.
KW - Aerodynamics characteristics
KW - Convolutional neural network
KW - Field reconstruction
KW - Oscillating foil
KW - Transient flow
UR - https://www.scopus.com/pages/publications/85115446022
U2 - 10.1115/GT2021-60075
DO - 10.1115/GT2021-60075
M3 - 会议稿件
AN - SCOPUS:85115446022
T3 - Proceedings of the ASME Turbo Expo
BT - Structures and Dynamics � Aerodynamics Excitation and Damping; Bearing and Seal Dynamics; Emerging Methods in Design and Engineering
PB - American Society of Mechanical Engineers (ASME)
T2 - ASME Turbo Expo 2021: Turbomachinery Technical Conference and Exposition, GT 2021
Y2 - 7 June 2021 through 11 June 2021
ER -