A simple first-order shear deformation theory for laminated composite plates

被引：175
作者：
Huu-Tai Thai [1 ]
Choi, Dong-Ho [1 ]
机构：
[1] Hanyang Univ, Dept Civil & Environm Engn, Seoul 133791, South Korea
来源：
COMPOSITE STRUCTURES | 2013年 / 106卷
基金：
新加坡国家研究基金会;
关键词：
Laminated composite plate; Plate theory; Bending; Free vibration; FREE-VIBRATION ANALYSIS; FUNCTIONALLY GRADED PLATES; FINITE-ELEMENT FORMULATION; BUCKLING ANALYSIS; NATURAL FREQUENCIES; BENDING ANALYSIS; DYNAMIC-ANALYSIS; ORDER THEORY; EFFICIENT; BEHAVIOR;
D O I：
10.1016/j.compstruct.2013.06.013
中图分类号：
O3 [力学];
学科分类号：
08 ; 0801 ;
摘要：
In this paper, a simple first-order shear deformation theory is presented for laminated composite plates. Unlike the existing first-order shear deformation theory, the present one contains only four unknowns and has strong similarities with the classical plate theory in many aspects such as equations of motion, boundary conditions, and stress resultant expressions. Equations of motion and boundary conditions are derived from Hamilton's principle. Analytical solutions of simply supported antisymmetric cross-ply and angle-ply laminates are obtained and the results are compared with the exact three-dimensional (3D) solutions and those predicted by existing theories. Comparison studies show that this new first-order shear deformation theory can achieve the same accuracy of the existing first-order shear deformation theory which has more number of unknowns. (C) 2013 Elsevier Ltd. All rights reserved.
引用
收藏
页码：754 / 763
页数：10
相关论文
共 74 条
[1]   Static Analysis of Functionally Graded Sandwich Plates Using an Efficient and Simple Refined Theory [J].
Abdelaziz, Hadj Henni ;
Atmane, Hassen Ait ;
Mechab, Ismail ;
Boumia, Lakhdar ;
Tounsi, Abdelouahed ;
El Abbas, Adda Bedia .
CHINESE JOURNAL OF AERONAUTICS, 2011, 24 (04) :434-448
[2]   Two new hyperbolic shear displacement models for orthotropic laminated composite plates [J].
Akavci, S. S. .
MECHANICS OF COMPOSITE MATERIALS, 2010, 46 (02) :215-226
[3]   A new shear deformation theory for laminated composite plates [J].
Aydogdu, Metin .
COMPOSITE STRUCTURES, 2009, 89 (01) :94-101
[4]   A displacement-based finite element formulation for the analysis of laminated composite plates [J].
Castellazzi, G. ;
Krysl, P. ;
Bartoli, I. .
COMPOSITE STRUCTURES, 2013, 95 :518-527
[5]   Bending and vibration responses of laminated composite plates using an edge-based smoothing technique [J].
Cui, X. Y. ;
Liu, G. R. ;
Li, G. Y. .
ENGINEERING ANALYSIS WITH BOUNDARY ELEMENTS, 2011, 35 (06) :818-826
[6]   Natural frequencies of FSDT cross-ply composite shells by multiquadrics [J].
Ferreira, A. J. M. ;
Roque, C. M. C. ;
Jorge, R. M. N. .
COMPOSITE STRUCTURES, 2007, 77 (03) :296-305
[7]   Analysis of natural frequencies of composite plates by an RBF-pseudo spectral method [J].
Ferreira, A. J. M. ;
Fasshauer, G. E. .
COMPOSITE STRUCTURES, 2007, 79 (02) :202-210
[8]   Analysis of laminated shells by a sinusoidal shear deformation theory and radial basis functions collocation, accounting for through-the-thickness deformations [J].
Ferreira, A. J. M. ;
Carrera, E. ;
Cinefra, M. ;
Roque, C. M. C. ;
Polit, O. .
COMPOSITES PART B-ENGINEERING, 2011, 42 (05) :1276-1284
[9]   A high order collocation method for the static and vibration analysis of composite plates using a first-order theory [J].
Ferreira, A. J. M. ;
Castro, Luis M. S. ;
Bertoluzza, Silvia .
COMPOSITE STRUCTURES, 2009, 89 (03) :424-432
[10]   A formulation of the multiquadric radial basis function method for the analysis of laminated composite plates [J].
Ferreira, AJM .
COMPOSITE STRUCTURES, 2003, 59 (03) :385-392
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