Zigzag theory for buckling of hybrid piezoelectric beams under electromechanical loads

被引:16
作者
Kapuria, S [1 ]
Alam, N [1 ]
机构
[1] Indian Inst Technol, Dept Appl Mech, New Delhi 110016, India
关键词
buckling; zigzag theory; hybrid beam;
D O I
10.1016/j.ijmecsci.2004.03.003
中图分类号
TH [机械、仪表工业];
学科分类号
0802 ;
摘要
A new efficient coupled one-dimensional (1D) geometrically nonlinear zigzag theory is developed for buckling analysis of hybrid piezoelectric beams, under electromechanical loads. The potential field is approximated layerwise as piecewise linear. The deflection is approximated to account for the normal strain due to electric field. The axial displacement is approximated as a combination of a global third-order variation and layerwise linear variation. It is expressed in terms of three primary displacement variables and a set of electric potential variables by enforcing exactly the conditions of zero transverse shear stress at the top and bottom and the conditions of its continuity at the layer interfaces. The governing coupled nonlinear field equations and boundary conditions are derived using a variational principle. Analytical solutions for buckling of simply supported beams under electromechanical loads are presented. Comparisons with the exact 2D piezoelasticity solution establish that the present zigzag theory is very accurate for buckling analysis. (C) 2004 Elsevier Ltd. All rights reserved.
引用
收藏
页码:1 / 25
页数:25
相关论文
共 24 条
[1]   Thick beam theory and finite element model with zig-zag sublaminate approximations [J].
Averill, RC ;
Yip, YC .
AIAA JOURNAL, 1996, 34 (08) :1627-1632
[2]   Analysis of non-linear piezothermoelastic laminated beams with electric and temperature effects [J].
Bao, Y ;
Tzou, HS ;
Venkayya, VB .
JOURNAL OF SOUND AND VIBRATION, 1998, 209 (03) :505-518
[3]   Active buckling control of smart composite plates - Finite-element analysis [J].
Chandrashekhara, K. ;
Bhatia, K. .
Smart Materials and Structures, 1993, 2 (01) :31-39
[4]   Optimal stabilization of plate buckling [J].
Chase, JG ;
Bhashyam, S .
SMART MATERIALS & STRUCTURES, 1999, 8 (02) :204-211
[5]   Exact elasticity solution for buckling of composite laminates [J].
Chattopadhyay, A ;
Gu, H .
COMPOSITE STRUCTURES, 1996, 34 (03) :291-299
[6]  
GOPINATHAN SV, 2000, SMART MATER STRUCT, V10, P229
[7]   Elasticity approach for delamination buckling of composite beam plates [J].
Gu, HZ ;
Chattopadhyay, A .
AIAA JOURNAL, 1998, 36 (08) :1529-1534
[8]   Exact two-dimensional piezoelasticity solution for buckling of hybrid beams and cross-ply panels using transfer matrices [J].
Kapuria, S ;
Alam, N .
COMPOSITE STRUCTURES, 2004, 64 (01) :1-11
[9]  
Kapuria S, 2003, ARCH APPL MECH, V73, P147, DOI 10.1007/S00419-003-0277-6
[10]   An efficient coupled layerwise theory for dynamic analysis of piezoelectric composite beams [J].
Kapuria, S ;
Dumir, PC ;
Ahmed, A .
JOURNAL OF SOUND AND VIBRATION, 2003, 261 (05) :927-944