A HIGHER-ORDER THEORY FOR BENDING ANALYSIS OF LAMINATED SHELLS OF REVOLUTION

被引：53

作者：

BHASKAR, K

VARADAN, TK

机构：

[1] Department of Aerospace Engineering, Indian Institute of Technology, Madras

来源：

COMPUTERS & STRUCTURES | 1991年 / 40卷 / 04期

关键词：

D O I：

10.1016/0045-7949(91)90310-I

中图分类号：

TP39 [计算机的应用];

学科分类号：

081203 ; 0835 ;

摘要：

A new higher-order shear deformation theory is presented for the analysis of laminated anisotropic shells of revolution. The theory is based on realistic approximation of the in-plane displacements through the thickness. The accuracy of the theory is verified by comparison with three-dimensional elasticity results for a laminated orthotropic cylindrical shell. Finally, an isoparametric quadrilateral shell of revolution finite element is presented. The example problems solved illustrate the performance of the element and the effects of transverse shear deformation.

引用

页码：815 / 819

页数：5

共 15 条

[1]

Ambartsumian SA, 1962, APPL MECH REV, V15, P245

[2]

BHASKAR K, J AERO SOC INDIA

[3]

BHASKAR K, COMPOSITE STRUCT

[4] LAMINATED ORTHOTROPIC SHELL THEORY INCLUDING TRANSVERSE SHEAR DEFORMATION [J].