FEM modeling of adaptive composite structures using a reduced higher-order plate theory via penalty functions

被引:24
作者
Fukunaga, H
Hu, N
Ren, GX
机构
[1] Tohoku Univ, Dept Aeronaut & Space Engn, Aoba Ku, Sendai, Miyagi 9808579, Japan
[2] Tsinghua Univ, Dept Engn Mech, Beijing 100084, Peoples R China
关键词
adaptive structures; composite laminates; piezoelectrics; C-0-type finite element; higher-order plate theory;
D O I
10.1016/S0020-7683(01)00072-5
中图分类号
O3 [力学];
学科分类号
08 ; 0801 ;
摘要
This paper presents a finite element model for analyzing the composite laminates containing the piezoelectrics statistically or dynamically. First, to model the moderately thick laminated plates, a simple higher-order plate theory, which can satisfy the free conditions of transverse shear strains on the top and bottom surfaces of plates, have been adopted. To set up a C-0-type FEM scheme, two artificial variables in the displacement field have been introduced to avoid the higher-order derivatives from the higher-order plate theory. The corresponding constraint conditions from two artificial variables have been enforced effectively through the penalty function method using the reduced integral scheme within the element area. Second, a generalized coupling FEM model for the mechanical and electric fields from the variational framework have been proposed. Finally, various examples studied in many previous researches have been employed to verify the justification, accuracy and efficiency of the present model. (C) 2001 Elsevier Science Ltd. All rights reserved.
引用
收藏
页码:8735 / 8752
页数:18
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