Refined multilayered plate elements based on Murakami zig-zag functions

被引:99
作者
Demasi, L [1 ]
机构
[1] Univ Washington, Dept Aeronaut & Astronaut, Seattle, WA 98195 USA
关键词
FEM; RMVT; zig-zag; Murakami; transverse stresses; mixed formulation; layer-wise models; equivalent single layer models;
D O I
10.1016/j.compstruct.2004.08.036
中图分类号
O3 [力学];
学科分类号
08 [工学]; 0801 [力学];
摘要
This paper discusses the FEM use of Murakami zig-zag function (MZZF) in the two-dimensional modeling of multilayered plates. A literature overview is first conducted on the available works in which MZZF has been applied. MZZF is used to introduce the zig-zag effect in classical and higher order theories, which are formulated using only displacements as unknowns. MZZF is also considered to introduce the zig-zag effect in those theories, which are formulated on the basis of both displacement and transverse stress assumptions (mixed formulations). The present FEM formulation is validated by comparing the results with some available papers from the literature. A very thick plate (a/h = 4) is studied and the results are compared with the commercial code NAS-TRAN. Numerical results are presented to show both the effectiveness and limitations of MZZF in the modeling of layered plates. Linear up to forth order expansion for in-plane and out-of-plane displacements, in the thickness plate direction, has been compared. It has been concluded that MZZF consists of a valuable tool to enhance the performances of both classical and advanced theories. In particular, the conducted numerical evaluations have shown that it can be more convenient to enhance a plate theory by introducing the MZZF than refining it by adding two or three higher order terms. However, in order to well approximate local effects or study thick plates, advanced models (layer-wise or three-dimensional) are required. (C) 2004 Elsevier Ltd. All rights reserved.
引用
收藏
页码:308 / 316
页数:9
相关论文
共 26 条
[1]
Ambartsumian SA, 1961, Theory of Anisotropic Shells
[2]
AMBARTSUMIAN SA, 1969, THEORY ANISOTROPIC P
[3]
[Anonymous], 1935, VESTNIK INZHEN TEKHN
[4]
Refined first-order shear deformation theory models for composite laminates [J].
Auricchio, F ;
Sacco, E .
JOURNAL OF APPLIED MECHANICS-TRANSACTIONS OF THE ASME, 2003, 70 (03) :381-390
[5]
A HIGHER-ORDER THEORY FOR BENDING ANALYSIS OF LAMINATED SHELLS OF REVOLUTION [J].
BHASKAR, K ;
VARADAN, TK .
COMPUTERS & STRUCTURES, 1991, 40 (04) :815-819
[6]
Brank B, 2000, INT J NUMER METH ENG, V48, P843, DOI 10.1002/(SICI)1097-0207(20000630)48:6<843::AID-NME903>3.0.CO
[7]
2-E
[8]
A study of transverse normal stress effect on vibration of multilayered plates and shells [J].
Carrera, E .
JOURNAL OF SOUND AND VIBRATION, 1999, 225 (05) :803-829
[9]
Carrera E., 2003, Applied Mechanics Review, V56, P287, DOI 10.1115/1.1557614
[10]
On the use of the Murakami's zig-zag function in the modeling of layered plates and shells [J].
Carrera, E .
COMPUTERS & STRUCTURES, 2004, 82 (7-8) :541-554