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:18
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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