Buckling analysis of laminated composite and sandwich beams by the finite element method

被引：53

作者：

Kahya, Volkan ^{[1
]}

机构：

[1] Karadeniz Tech Univ, Fac Engn, Dept Civil Engn, TR-61080 Trabzon, Turkey

来源：

COMPOSITES PART B-ENGINEERING | 2016年 / 91卷

关键词：

Laminates; Layered structures; Buckling; Finite element analysis (FEA); Sandwich structures; GENERAL BOUNDARY-CONDITIONS; SHEAR DEFORMATION-THEORY; FREE-VIBRATION; DYNAMIC-ANALYSIS; MOVING LOADS; STABILITY; FORMULATION; BEHAVIOR;

D O I：

10.1016/j.compositesb.2016.01.031

中图分类号：

T [工业技术];

学科分类号：

08 ;

摘要：

Buckling of laminated composite beams is studied by the finite element method. A multilayered beam element presented here consists of N-layers, and includes totally 3N + 7 degrees of freedom (DOFs). Delamination and slip between the layers are avoided. Effect of shear deformation is considered according to the first-order shear deformation theory (FSDT). Numerical results for buckling loads of laminated beams with different boundary conditions and lamina stacking are presented. Comparisons show that results obtained agree well with those of previous works available in the literature. (C) 2016 Elsevier Ltd. All rights reserved.

引用

页码：126 / 134

页数：9

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