A semi-analytical approach for the non-linear large deflection analysis of laminated rectangular plates under general out-of-plane loading

被引:24
作者
Shuffin, I. [1 ]
Rabinovitch, O. [1 ]
Eisenberger, M. [1 ]
机构
[1] Technion Israel Inst Technol, Fac Civil & Environm Engn, IL-32000 Haifa, Israel
关键词
extended Kantorovich method; laminated composite plate; large deflection analysis; patch loading; semi-analytical approach; geometrically non-linear analysis;
D O I
10.1016/j.ijnonlinmec.2007.12.018
中图分类号
O3 [力学];
学科分类号
08 ; 0801 ;
摘要
A semi-analytical approach for the geometrically non-linear analysis of rectangular laminated plates with general inplane and out-of-plane boundary conditions under a general distribution of out-of-plane loads is developed. The analysis is based on the elastic thin plate theory with geometrically non-linear von Karman strains. The solution of the non-linear partial differential equations is reduced to an iterative sequential solution of non-linear ordinary differential equations using the multi-term extended Kantorovich method. The efficiency, accuracy, and convergence of the proposed method are examined through a comparison with other semi-analytical methods and with finite element analyses. The capabilities of the approach and its applicability to the non-linear large deflection analysis of plate structures are demonstrated through various numerical examples. Emphasis is placed on combinations of lamination, boundary, and loading conditions that cannot be analyzed using alternative semi-analytical methods. (C) 2008 Elsevier Ltd. All rights reserved.
引用
收藏
页码:328 / 340
页数:13
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