Linear and nonlinear combined aerodynamic reduced order model based on residual network framework

被引:1
|
作者
Qi, Hui [1 ]
Yu, Jiaming [1 ]
Jiang, Jingjiang [1 ]
Guo, Jing [1 ,2 ]
机构
[1] Harbin Engn Univ, Coll Aerosp & Civil Engn, Harbin 150001, Heilongjiang, Peoples R China
[2] Harbin Engn Univ, Key Lab Vehicle Transmedia Technol, Harbin 150001, Heilongjiang, Peoples R China
关键词
FREQUENCY LOCK-IN; FLUTTER; MECHANISM;
D O I
10.1209/0295-5075/ac765e
中图分类号
O4 [物理学];
学科分类号
0702 ;
摘要
Residual convolutional neural network (ResNet) is a rising technology in the field of artificial intelligence due to its advantages of easy optimization, high accuracy, information fidelity and no gradient disappearance. Based on the powerful ability of machine learning to learn from big data features, a residual network aerodynamic reduced order model (ROM) framework based on CFD sample data was proposed. In this letter, a binary airfoil is taken as the research object, and the displacement information representing the movement characteristics of the flow field can be transmitted by two ways: one is that the input information is continuously captured and extracted by the deep convolution layer; the other is that the input information is directly transmitted around the convolutional layer. Then the characteristic information of the two approaches is integrated and activated through the output layer to complete the regression prediction of the wing aerodynamic characteristics. Finally, the ROM frame is used to predict the strongly nonlinear hysteresis loops of airfoil under pitching motion, and the results show that the ROM frame is effective. In addition, the framework can be applied to qualitative interpretation of complex flow phenomena and aeroelastic analysis. Copyright (C) 2022 EPLA
引用
收藏
页数:7
相关论文
共 50 条
  • [31] Residual Ratio Thresholding for Linear Model Order Selection
    Kallummil, Sreejith
    Kalyani, Sheetal
    IEEE TRANSACTIONS ON SIGNAL PROCESSING, 2019, 67 (04) : 838 - 853
  • [32] Effective Analysis of Nonlinear Aeroelasticity Based on Parameter Adaptive Reduced Order Model
    Lu Z.
    Xiao T.
    Chang L.
    Deng S.
    Fu B.
    Gao H.
    Beijing Ligong Daxue Xuebao/Transaction of Beijing Institute of Technology, 2024, 44 (01): : 29 - 38
  • [33] Reduced-order model based on volterra series in nonlinear unsteady aerodynamics
    Chen, Gang
    Xu, Min
    Chen, Shi-Lu
    Yuhang Xuebao/Journal of Astronautics, 2004, 25 (05): : 492 - 495
  • [34] A Reduced-Order Model for Wirelessly Excited Machine Based on Linear Approximation
    Kang, Jinsong
    Liu, Yusong
    Sun, Liangrong
    Zhong, Zaimin
    Fu, Minfan
    IEEE TRANSACTIONS ON POWER ELECTRONICS, 2021, 36 (11) : 12389 - 12399
  • [35] Reduced-order observer-based synchronization and output tracking in chain network of a class of nonlinear systems using contraction framework
    Ranjan, Ravi Kumar
    Sharma, Bharat Bhushan
    INTERNATIONAL JOURNAL OF DYNAMICS AND CONTROL, 2023, 11 (05) : 2523 - 2537
  • [36] Reduced-order observer-based synchronization and output tracking in chain network of a class of nonlinear systems using contraction framework
    Ravi Kumar Ranjan
    Bharat Bhushan Sharma
    International Journal of Dynamics and Control, 2023, 11 : 2523 - 2537
  • [37] Nonlinear Reduced Order Model of a 3-Phase Transformer For Electric Network Simulator Coupling
    Paquay, Yannick
    Bruls, Olivier
    Geuzaine, Christophe
    2016 IEEE CONFERENCE ON ELECTROMAGNETIC FIELD COMPUTATION (CEFC), 2016,
  • [38] Unsteady reduced order model with neural networks and flight-physics-based regularization for aerodynamic applications
    Ribeiro, Mateus Dias
    Stradtner, Mario
    Bekemeyer, Philipp
    COMPUTERS & FLUIDS, 2023, 264
  • [39] Study on a new aerodynamic model of HAWT based on panel method and Reduced Order Model using Proper Orthogonal Decomposition
    Wang, Q.
    Wang, Z. X.
    Song, J. J.
    Xu, Y.
    Xu, J. Z.
    RENEWABLE ENERGY, 2012, 48 : 436 - 447
  • [40] REDUCED ORDER MODEL OF NONLINEAR STRUCTURES FOR TURBOMACHINERY AEROELASTICITY
    Flament, T.
    Deu, J-F.
    Placzek, A.
    Balmaseda, M.
    Tran, D-M.
    PROCEEDINGS OF ASME TURBO EXPO 2023: TURBOMACHINERY TECHNICAL CONFERENCE AND EXPOSITION, GT2023, VOL 11B, 2023,