A deep reinforcement learning optimization framework for supercritical airfoil aerodynamic shape design

被引:1
|
作者
Liu, Ziyang [1 ]
Zhang, Miao [2 ]
Sun, Di [3 ]
Li, Li [4 ]
Chen, Gang [1 ]
机构
[1] Xi An Jiao Tong Univ, Sch Aerosp Engn, Shaanxi Key Lab Environm & Control Flight Vehicle, State Key Lab Strength & Vibrat Mech Struct, Xian 710049, Peoples R China
[2] Shanghai Aircraft Design & Res Inst, Shanghai 201210, Peoples R China
[3] Northwestern Polytech Univ, Natl Key Lab Sci & Technol Aerodynam Design & Res, Xian 710072, Peoples R China
[4] Xian Aeronaut Comp Tech Res Inst, AVIC, Xian 710068, Peoples R China
基金
中国国家自然科学基金;
关键词
Aerodynamic shape optimization design; Deep reinforcement learning; Supercritical airfoil; Experience learning; NEURAL-NETWORKS; BUFFET;
D O I
10.1007/s00158-024-03755-5
中图分类号
TP39 [计算机的应用];
学科分类号
081203 ; 0835 ;
摘要
In the context of traditional aerodynamic shape optimization design methods, the necessity to re-execute the complete optimization process when the initial shape changes poses significant challenges in engineering applications. These challenges encompass problems like data wastage and restricted ability for experience learning. We propose a policy learning-based optimization method that can automatically learn optimization experience through interactions with the environment. This optimization framework is based on deep reinforcement learning and consists of the policy learning process and the policy execution process. The action network, trained during the policy learning process, serves as a black box model of optimization experience and can directly and efficiently participate in guiding the actual optimization process. The optimization framework is validated through two-dimensional Rosenbrock function optimization, demonstrating its exceptional performance in achieving high-precision optimal solutions. Then, the effectiveness of this optimization method is demonstrated in the multi-point optimization design of supercritical airfoils, which aims to improve the buffet onset lift within predefined design constraints while maintaining the cruise lift-drag ratio. With the datum-coupled state format, the optimization experience can be tailored to the optimization requirements of different initial states during the learning process, leading to an optimization success rate in the optimization space that can exceed 90%.
引用
收藏
页数:18
相关论文
共 50 条
  • [41] A novel inverse design method for morphing airfoil based on deep reinforcement learning
    Su, Jing
    Sun, Gang
    Tao, Jun
    AEROSPACE SCIENCE AND TECHNOLOGY, 2024, 145
  • [42] Missile aerodynamic shape optimization design using deep neural networks
    Wu, Pin
    Yuan, Wenyan
    Ji, Lulu
    Zhou, Ling
    Zhou, Zhu
    Feng, Weibing
    Guo, Yike
    AEROSPACE SCIENCE AND TECHNOLOGY, 2022, 126
  • [43] Deep Reinforcement Learning for Optimization at Early Design Stages
    Servadei, Lorenzo
    Lee, Jin Hwa
    Arjona Medina, Jose A.
    Werner, Michael
    Hochreiter, Sepp
    Ecker, Wolfgang
    Wille, Robert
    IEEE DESIGN & TEST, 2023, 40 (01) : 43 - 51
  • [44] Sequential Banner Design Optimization with Deep Reinforcement Learning
    Kondo, Yusuke
    Wang, Xueting
    Seshime, Hiroyuki
    Yamasaki, Toshihiko
    23RD IEEE INTERNATIONAL SYMPOSIUM ON MULTIMEDIA (ISM 2021), 2021, : 253 - 256
  • [45] Airfoil Optimization Using Practical Aerodynamic Design Requirements
    Buckley, Howard P.
    Zhou, Beckett Y.
    Zingg, David W.
    JOURNAL OF AIRCRAFT, 2010, 47 (05): : 1707 - 1719
  • [46] Aerodynamic design optimization for low Reynolds tandem airfoil
    Chen, Fangzheng
    Yu, Jianqiao
    Mei, Yuesong
    PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART G-JOURNAL OF AEROSPACE ENGINEERING, 2018, 232 (06) : 1047 - 1062
  • [47] Research on Multimodality in Aerodynamic/Stealth Airfoil Design Optimization
    Zhang Wei
    Gao Zhenghong
    Zhou Lin
    Deng Jun
    Xia Lu
    Zuo Yingtao
    2021 12TH INTERNATIONAL CONFERENCE ON MECHANICAL AND AEROSPACE ENGINEERING (ICMAE), 2021, : 384 - 393
  • [48] Airfoils optimization based on deep reinforcement learning to improve the aerodynamic performance of rotors
    Liu, Jiaqi
    Chen, Rongqian
    Lou, Jinhua
    Wu, Hao
    You, Yancheng
    Chen, Zhengwu
    AEROSPACE SCIENCE AND TECHNOLOGY, 2023, 143
  • [49] Aerodynamic optimization design of airfoil using DFFD technique
    Bai, J. (junqiang@nwpu.edu.cn), 1600, Chinese Society of Astronautics (35):
  • [50] Aerodynamic optimization design of airfoil based on genetic algorithm
    Wang, Xiaopeng
    Gao, Zhenghong
    Kongqi Donglixue Xuebao/Acta Aerodynamica Sinica, 2000, 18 (03): : 324 - 329