Isogeometric finite element analysis of composite sandwich plates using a higher order shear deformation theory

被引:153
作者
Nguyen-Xuan, H. [1 ,2 ]
Thai, Chien H. [2 ]
Nguyen-Thoi, T. [1 ,2 ]
机构
[1] Univ Sci, VNU HCMC, Dept Mech, Hcmc, Vietnam
[2] Ton Duc Thang Univ, Div Computat Mech, Hcmc, Vietnam
关键词
Plates; Buckling; Vibration; Computational modeling; Sandwich; MESHFREE THIN SHELL; C-0 FE MODEL; LAMINATED COMPOSITE; FREE-VIBRATION; BUCKLING ANALYSIS; STATIC ANALYSIS; PENALTY MODEL; STABILITY; FORMULATION; NURBS;
D O I
10.1016/j.compositesb.2013.06.044
中图分类号
T [工业技术];
学科分类号
08 ;
摘要
We present in this paper a simple and effective formulation based on a fifth-order shear deformation theory (FiSDT) in combination with isogeometric finite element analysis (IGA) for composite sandwich plates. The FiSDT yields non-linear distribution of the transverse shear stresses through the plate thickness and ensures a prior tangential stress-free boundary condition. The IGA uses same basis functions, namely B-splines or non-uniform rational B-splines (NURBS), for preserving the precisely geometric representation and providing the numerical solution. It enables to achieve easily the smoothness with arbitrary continuity order and in the present method the C-1-continuity requirement of higher order shear deformation models is fulfilled. The static, dynamic and buckling analysis of rectangular and circular plates is investigated for different boundary conditions. Numerical examples are given to show high accuracy of the proposed method. (C) 2013 Elsevier Ltd. All rights reserved.
引用
收藏
页码:558 / 574
页数:17
相关论文
共 77 条
[1]   FINITE STRIP ANALYSIS OF ANISOTROPIC LAMINATED COMPOSITE PLATES USING HIGHER-ORDER SHEAR DEFORMATION-THEORY [J].
AKHRAS, G ;
CHEUNG, MS ;
LI, W .
COMPUTERS & STRUCTURES, 1994, 52 (03) :471-477
[2]  
Allen H., 1969, Analysis and Design of Structural Sandwich Panels
[3]   Local maximum-entropy approximation schemes:: a seamless bridge between finite elements and meshfree methods [J].
Arroyo, M ;
Ortiz, M .
INTERNATIONAL JOURNAL FOR NUMERICAL METHODS IN ENGINEERING, 2006, 65 (13) :2167-2202
[4]   A PENALTY MODEL FOR THE ANALYSIS OF CURVED COMPOSITE BEAMS [J].
ASCIONE, L ;
FRATERNALI, F .
COMPUTERS & STRUCTURES, 1992, 45 (5-6) :985-999
[5]   A fully "locking-free" isogeometric approach for plane linear elasticity problems: A stream function formulation [J].
Auricchio, F. ;
da Veiga, L. Beirao ;
Buffa, A. ;
Lovadina, C. ;
Reali, A. ;
Sangalli, G. .
COMPUTER METHODS IN APPLIED MECHANICS AND ENGINEERING, 2007, 197 (1-4) :160-172
[6]   A large deformation, rotation-free, isogeometric shell [J].
Benson, D. J. ;
Bazilevs, Y. ;
Hsu, M-C ;
Hughes, T. J. R. .
COMPUTER METHODS IN APPLIED MECHANICS AND ENGINEERING, 2011, 200 (13-16) :1367-1378
[7]   Isogeometric shell analysis: The Reissner-Mindlin shell [J].
Benson, D. J. ;
Bazilevs, Y. ;
Hsu, M. C. ;
Hughes, T. J. R. .
COMPUTER METHODS IN APPLIED MECHANICS AND ENGINEERING, 2010, 199 (5-8) :276-289
[8]   Analysis of composite plates using various plate theories Part 1. Formulation and analytical solutions [J].
Bose, P ;
Reddy, JN .
STRUCTURAL ENGINEERING AND MECHANICS, 1998, 6 (06) :583-612
[9]   Bending, free vibrations and buckling of laminated composite and sandwich plates using a layerwise displacement model [J].
Cetkovic, M. ;
Vuksanovic, Dj. .
COMPOSITE STRUCTURES, 2009, 88 (02) :219-227
[10]   An improved C0 FE model for the analysis of laminated sandwich plate with soft core [J].
Chalak, H. D. ;
Chakrabarti, Anupam ;
Iqbal, Mohd. Ashraf ;
Sheikh, Abdul Hamid .
FINITE ELEMENTS IN ANALYSIS AND DESIGN, 2012, 56 :20-31