A new nonlinear higher-order shear deformation theory with thickness variation for large-amplitude vibrations of laminated doubly curved shells

被引:38
作者
Amabili, M. [1 ]
机构
[1] McGill Univ, Dept Mech Engn, Canada Res Chair Tier 1, Montreal, PQ H3A 0C3, Canada
基金
加拿大创新基金会; 加拿大自然科学与工程研究理事会;
关键词
PLATES; FORMULATION; ELEMENT; PANELS;
D O I
10.1016/j.jsv.2013.03.024
中图分类号
O42 [声学];
学科分类号
070206 ; 082403 ;
摘要
A consistent higher-order shear deformation nonlinear theory is developed for shells of generic shape allowing for thickness variation by using six variables; geometric imperfections are also taken into account. The geometrically nonlinear strain-displacement relationships are derived retaining full nonlinear terms in the in-plane displacements. They are presented in curvilinear coordinates in a formulation that can be readily implemented in computer codes. This new theory is applied to laminated circular cylindrical shells complete around the circumference and simply supported at the ends. Linear (natural frequencies) and geometrically nonlinear (large-amplitude forced response) vibrations are studied by using the present theory and results are compared to those obtained by using the refined Amabili-Reddy higher-order shear deformation nonlinear shell theory, which neglects thickness variations. (C) 2013 Elsevier Ltd. All rights reserved.
引用
收藏
页码:4620 / 4640
页数:21
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