共 87 条
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.
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页数:14
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