NONLINEAR IMPACT ANALYSIS OF LAMINATED CYLINDRICAL AND DOUBLY-CURVED SHELLS

被引：28
|
作者：
CHANDRASHEKHARA, K
SCHROEDER, T
机构：
[1] Department of Mechanical and Aerospace Engineering and Engineering Mechanics, University of Missouri-Rolla Rolla
来源：
JOURNAL OF COMPOSITE MATERIALS | 1995年 / 29卷 / 16期
关键词：
D O I：
10.1177/002199839502901604
中图分类号：
TB33 [复合材料];
学科分类号：
摘要：
The nonlinear impact response of laminated composite cylindrical and doubly curved shells is analyzed using a modified Hertzian contact law. A finite element model is developed based on Sander's shell theory and includes shear deformation effects and nonlinearity due to large deflection. A nine noded isoparametric quadrilateral element is used to model the curved shell. The nonlinear time dependent equations are solved using an iterative scheme and Newmark's method. Numerical results for the contact force and center deflection histories are presented for various impactor conditions, shell geometry and boundary conditions.
引用
收藏
页码：2160 / 2179
页数：20
相关论文
共 50 条
  • [21] Interlaminar Stress Analysis of Orthotropic Laminated Doubly-Curved Shells on Rectangular Planform under Concentrated Force
    Sayyad, Atteshamuddin S.
    Ghugal, Yuwaraj M.
    [J]. JOURNAL OF AEROSPACE ENGINEERING, 2021, 34 (02)
  • [22] Dynamic analysis of laminated doubly-curved shells with general boundary conditions by means of a domain decomposition method
    Guo, Jianghua
    Shi, Dongyan
    Wang, Qingshan
    Tang, Jinyuan
    Shuai, Cijun
    [J]. INTERNATIONAL JOURNAL OF MECHANICAL SCIENCES, 2018, 138 : 159 - 186
  • [23] Damping properties analysis of composite sandwich doubly-curved shells
    Zhai, Yanchun
    Su, Jianmin
    Liang, Sen
    [J]. COMPOSITES PART B-ENGINEERING, 2019, 161 : 252 - 262
  • [24] Free vibration analysis of joined doubly-curved shells of revolution
    Pang F.-Z.
    Li H.-C.
    Peng D.-W.
    Huo R.-D.
    Miao X.-H.
    [J]. Li, Hai-Chao (lihaichao@hrbeu.edu.cn), 1600, Nanjing University of Aeronautics an Astronautics (33): : 441 - 449
  • [25] Nonlinear stability analysis of rotationally-restrained imperfect doubly-curved composite shallow shells
    Huang, Sixin
    Qiao, Pizhong
    Lu, Linjun
    Qi, Yang
    [J]. THIN-WALLED STRUCTURES, 2019, 142 : 358 - 368
  • [26] THERMAL-STRESS ANALYSIS OF LAMINATED DOUBLY-CURVED SHELLS USING A SHEAR FLEXIBLE FINITE-ELEMENT
    CHANDRASHEKHARA, K
    BHIMARADDI, A
    [J]. COMPUTERS & STRUCTURES, 1994, 52 (05) : 1023 - 1030
  • [27] Three-dimensional free vibration analysis of doubly-curved shells
    Zhou, Ding
    Lo, Sia Huen
    [J]. JOURNAL OF VIBRATION AND CONTROL, 2015, 21 (12) : 2306 - 2324
  • [28] Free vibrations of composite laminated doubly-curved shells and panels of revolution with general elastic restraints
    Wang, Qingshan
    Shi, Dongyan
    Liang, Qian
    Pang, Fuzhen
    [J]. APPLIED MATHEMATICAL MODELLING, 2017, 46 : 227 - 262
  • [29] A radial basis functions solution for the analysis of laminated doubly-curved shells by a Reissner-Mixed Variational Theorem
    Ferreira, A. J. M.
    Carrera, E.
    Cinefra, M.
    Zenkour, A. M.
    [J]. MECHANICS OF ADVANCED MATERIALS AND STRUCTURES, 2016, 23 (09) : 1068 - 1079
  • [30] FGM and Laminated Doubly-Curved and Degenerate Shells Resting on Nonlinear Elastic Foundations: A GDQ Solution for Static Analysis with a Posteriori Stress and Strain Recovery
    Tornabene, Francesco
    Reddy, J. N.
    [J]. JOURNAL OF THE INDIAN INSTITUTE OF SCIENCE, 2013, 93 (04) : 635 - 688
12345