Analysis of thickness locking in classical, refined and mixed theories for layered shells

被引:101
作者
Carrera, Erasmo [1 ]
Brischetto, Salvatore [1 ]
机构
[1] Politecn Torino, CASSEM Grp, Dept Aeronaut & Space Engn, I-10129 Turin, Italy
关键词
thickness locking; Poisson locking; plane-strain conditions; plane-stress conditions; layered shells; classical theories; advanced theories;
D O I
10.1016/j.compstruct.2007.10.009
中图分类号
O3 [力学];
学科分类号
08 ; 0801 ;
摘要
This paper is a sequel of the article: 'Analysis of Thickness Locking in Classical, Refined and Mixed Multilayered Plate Theories', Composite Structures, available online 9th February 2007. The analysis of thickness locking (TL) mechanism, (which is a plate/shell-theory mechanism, caused by the use of simplified kinematic assumptions) is herein extended to shell geometries. Bending problems have been analyzed for isotropic, one-layered and multilayered shells. TL has been investigated for a large variety of shell theories: thin shell theory, first order shear deformation theory, higher order theories, mixed theories and layer-wise theories. The unified formulation has been used to implement the whole considered shell modelings. Analytical closed form solutions have been considered. A comprehensive numerical investigation has been performed. The conclusions have been acquired: TL appears if and only if transverse normal strains epsilon(zz) are assumed constant; the use of LW models introduces benefits vs TL; mixed methods do not make any 'relevant' improvements with respect to TL; TL does not depend on geometrical curvature parameters. (c) 2007 Elsevier Ltd. All rights reserved.
引用
收藏
页码:83 / 90
页数:8
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