Effect of negative Poisson's ratio on the postbuckling behavior of axially compressed FG-GRMMC laminated cylindrical shells surrounded by an elastic medium

被引:16
作者
Shen, Hui-Shen [1 ,2 ]
Xiang, Y. [3 ]
机构
[1] Shanghai Jiao Tong Univ, Sch Aeronaut & Astronaut, Shanghai 200240, Peoples R China
[2] Shanghai Jiao Tong Univ, Sch Ocean & Civil Engn, Shanghai 200240, Peoples R China
[3] Western Sydney Univ, Sch Engn, Locked Bag 1797, Penrith, NSW 2751, Australia
基金
中国国家自然科学基金;
关键词
Auxetic materials; Functionally graded; Temperature dependent; Postbuckling; Cylindrical shell; GRAPHENE REINFORCED ALUMINUM; NONLINEAR DYNAMIC-RESPONSE; BUCKLING ANALYSIS; MECHANICAL-PROPERTIES; COMPOSITE; VIBRATION; STRENGTH; PANELS; PLATE;
D O I
10.1016/j.euromechsol.2021.104231
中图分类号
O3 [力学];
学科分类号
08 ; 0801 ;
摘要
Auxetic composites are one of novel metamaterials which exhibit an interesting feature of negative Poisson's ratio (NPR). The current study reports the impact of in-plane NPR on the postbuckling responses of axially loaded cylindrical shells made of graphene-reinforced metal matrix composite (GRMMC) layers. Each layer of a GRMMC laminated cylindrical shell can vary its graphene volume fraction so that a functionally graded (FG) shell is achieved. The GRMMC layers possess temperature-dependent material properties that can be evaluated using an extended micromechanical Halpin-Tsai model. The governing equations for the postbuckling of GRMMC laminated shells are based on the Reddy's third order shear deformation theory. The von Karman nonlinear strain-displacement relationships together with the foundation support and temperature effects are also included. Analytical solutions are obtained by using a singular perturbation technique in associate with a two-step perturbation approach for the postbuckling of perfect and imperfect FG-GRMMC laminated cylindrical shells. Numerical results explicitly show that the in-plane NPR has a substantial effect on the postbuckling response and imperfection sensitivity of GRMMC laminated cylindrical shells under axial compression.
引用
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页数:14
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共 87 条
  • [1] [Anonymous], 2013, A Two-Step Perturbation Method in Nonlinear Analysis of beams, Plates and Shells
  • [2] [Anonymous], 2017, Postbuckling Behavior of Plates and Shells
  • [3] [Anonymous], 2014, NONLINEAR STATIC DYN
  • [4] Numerical study on the buckling and vibration of functionally graded carbon nanotube-reinforced composite conical shells under axial loading
    Ansari, Reza
    Torabi, Jalal
    [J]. COMPOSITES PART B-ENGINEERING, 2016, 95 : 196 - 208
  • [5] Nonlinear low-velocity impact analysis of functionally graded nanotube-reinforced composite cylindrical shells in thermal environments
    Bayat, M. R.
    Rahmani, O.
    Mashhadi, M. Mosavi
    [J]. POLYMER COMPOSITES, 2018, 39 (03) : 730 - 745
  • [6] Experimental buckling of thin composite cylinders in compression
    Bisagni, C
    [J]. AIAA JOURNAL, 1999, 37 (02) : 276 - 278
  • [7] Auxetic materials with large negative Poisson's ratios based on highly oriented carbon nanotube structures
    Chen, Luzhuo
    Liu, Changhong
    Wang, Jiaping
    Zhang, Wei
    Hu, Chunhua
    Fan, Shoushan
    [J]. APPLIED PHYSICS LETTERS, 2009, 94 (25)
  • [8] Enhanced strength in bulk graphene-copper composites
    Chu, Ke
    Jia, Chengchang
    [J]. PHYSICA STATUS SOLIDI A-APPLICATIONS AND MATERIALS SCIENCE, 2014, 211 (01): : 184 - 190
  • [9] An Overview of the Recent Developments in Metal Matrix Nanocomposites Reinforced by Graphene
    Dadkhah, Mehran
    Saboori, Abdollah
    Fino, Paolo
    [J]. MATERIALS, 2019, 12 (17)
  • [10] Graphene-Based Polymer Composites and Their Applications
    Das, Tapan K.
    Prusty, Smita
    [J]. POLYMER-PLASTICS TECHNOLOGY AND ENGINEERING, 2013, 52 (04) : 319 - 331