Buckling and post-buckling behaviors of 1/3 composite cylindrical shell with an opening

被引:5
|
作者
Ma, Yihao [1 ]
Cheng, Xiaoquan [1 ,2 ]
Wang, Zhaodi [3 ]
Guo, Xin [1 ]
Zhang, Jie [1 ]
Xu, Yahong [3 ]
机构
[1] Beihang Univ, Sch Aeronaut Sci & Engn, Beijing 100191, Peoples R China
[2] Beihang Univ, Minist Ind & Informat Technol, Key Lab Aircraft Adv Design Technol, Beijing 100191, Peoples R China
[3] CASIC, Inst 306, Acad 3, Beijing 100074, Peoples R China
关键词
composite shell; opening; post-buckling; Newton-Raphson method; FEM; axial compression; AXIAL-COMPRESSION; CONICAL SHELLS; SANDWICH PLATES; PANELS; IMPERFECTIONS; DEFORMATION; PRESSURE; COLLAPSE; FAILURE; CUTOUTS;
D O I
10.12989/scs.2018.27.5.555
中图分类号
TU [建筑科学];
学科分类号
0813 ;
摘要
A 1/3 composite cylindrical shell with a central rectangular opening was axially compressed experimentally, and its critical buckling load and displacement, and strains were measured. A finite element model (FEM) of the shell with Hashin failure criteria was established to analyze its buckling and post-buckling behaviors by nonlinear Newton-Raphson method. The geometric imperfection sensitivity and the effect of side supported conditions of the shell were investigated. It was found that the Newton-Raphson method can be used to analyze the buckling and post-buckling behaviors of the shell. The shell is not sensitive to initial geometric imperfection. And the support design of the shell by side stiffeners is a good way to obtain the critical buckling load and simplify the experimental fixture.
引用
收藏
页码:555 / 566
页数:12
相关论文
共 50 条
  • [1] Thermomechanical buckling and post-buckling of cylindrical shell with functionally graded coatings and reinforced by stringers
    Pham Toan Thang
    Nguyen Dinh Duc
    Nguyen-Thoi, T.
    AEROSPACE SCIENCE AND TECHNOLOGY, 2017, 66 : 392 - 401
  • [2] Buckling and Post-Buckling Behavior of Perfect/Perforated Composite Cylindrical Shells under Hydrostatic Pressure
    Shen, Ke-Chun
    Yang, Zhao-Qi
    Jiang, Lei-Lei
    Pan, Guang
    JOURNAL OF MARINE SCIENCE AND ENGINEERING, 2022, 10 (02)
  • [3] Buckling and Post-Buckling Behaviours of Adhesively Bonded Aluminium Beams: A Review
    Apalak, M. Kemal
    Gul, Kubra
    Arslan, Y. Erhan
    REVIEWS OF ADHESION AND ADHESIVES, 2022, 10 (01): : 1 - 46
  • [4] Buckling and post-buckling of laminated composite plates
    Dash, Padmanav
    Singh, B. N.
    MECHANICS RESEARCH COMMUNICATIONS, 2012, 46 : 1 - 7
  • [5] Buckling, post-buckling and delamination propagation in debonded composite laminates Part 1: Theoretical development
    Zhang, Y.
    Wang, S.
    COMPOSITE STRUCTURES, 2009, 88 (01) : 121 - 130
  • [6] Isogeometric degenerated shell formulation for post-buckling analysis of composite variable-stiffness shells
    Hao, Peng
    Liao, Hewei
    Wu, Tao
    Huo, Zekai
    Wang, Bo
    COMPOSITE STRUCTURES, 2023, 321
  • [7] Post-buckling behavior of carbon fiber epoxy composite plates
    Erdem, Serkan
    Kaman, Mete Onur
    Gur, Mustafa
    JOURNAL OF MECHANICAL SCIENCE AND TECHNOLOGY, 2019, 33 (04) : 1723 - 1730
  • [8] Buckling and post-buckling of a composite C-section with cutout and flange reinforcement
    Guo, Shijun
    Li, Daochun
    Zhang, Xiang
    Xiang, Jinwu
    COMPOSITES PART B-ENGINEERING, 2014, 60 : 119 - 124
  • [9] Effect of impact damage positions on the buckling and post-buckling behaviors of stiffened composite panel
    Feng, Yu
    Zhang, Haoyu
    Tan, Xiangfei
    He, Yuting
    An, Tao
    Zheng, Jie
    COMPOSITE STRUCTURES, 2016, 155 : 184 - 196
  • [10] Buckling and Post-Buckling Behaviors of a Variable Stiffness Composite Laminated Wing Box Structure
    Wang, Peiyan
    Huang, Xinting
    Wang, Zhongnan
    Geng, Xiaoliang
    Wang, Yuansheng
    APPLIED COMPOSITE MATERIALS, 2018, 25 (02) : 449 - 467