A numerical model of delamination in composite laminated beams using the LRZ beam element based on the refined zigzag theory

被引:35
作者
Eijo, A. [1 ]
Onate, E. [1 ]
Oller, S. [1 ]
机构
[1] Univ Politecn Cataluna, Int Ctr Numer Methods Engn CIMNE, ES-08034 Barcelona, Spain
基金
欧洲研究理事会;
关键词
Laminated beams; Delamination; LRZ beam element; Refined zigzag theory; SIMULATION; GROWTH; PLATES; SHEAR;
D O I
10.1016/j.compstruct.2013.04.035
中图分类号
O3 [力学];
学科分类号
08 ; 0801 ;
摘要
A method based on the Refined Zigzag Theory (RZT) to model delamination in composite laminated beam structures is presented. The novelty of this method is the use of one-dimensional finite elements to discretize the geometry of the beam. The key property of this beam element, named LRZ [1], is the possibility to capture the relative displacement between consecutive layers which occurs during delamination. The fracture mode that the LRZ element is capable to predict is mode II. In order to capture the relative displacement using the LRZ element it is necessary to adapt the RZT theory as presented in this paper. The mechanical properties of the layers are modeled using a continuum isotropic damage model [2]. The modified Newton-Raphson method is used for solving the non-linear problem. The RZT theory, the LRZ finite element and the isotropic damage model are described in the paper. Also, the implicit integrations algorithm is presented. The performance of the LRZ element is analyzed by studying the delamination in a beam for two different laminates, using the plane stress solution as a reference. (C) 2013 Elsevier Ltd. All rights reserved.
引用
收藏
页码:270 / 280
页数:11
相关论文
共 35 条
[1]  
Aitharaju VR, 1999, ASCE, V59, P502
[2]  
[Anonymous], 2001, FRACTURA MECANICA EN
[3]   Development of simple, robust finite elements based on refined theories for thick laminated beams [J].
Averill, RC ;
Yip, YC .
COMPUTERS & STRUCTURES, 1996, 59 (03) :529-546
[4]   An interface element for the simulation of delamination in unidirectional fiber-reinforced composite laminates [J].
Balzani, C. ;
Wagner, W. .
ENGINEERING FRACTURE MECHANICS, 2008, 75 (09) :2597-2615
[5]   MODELING OF DELAMINATION IN COMPOSITE LAMINATES USING A LAYER-WISE PLATE-THEORY [J].
BARBERO, EJ ;
REDDY, JN .
INTERNATIONAL JOURNAL OF SOLIDS AND STRUCTURES, 1991, 28 (03) :373-388
[6]   Delaminations in composite structures: Its origin, buckling, growth and stability [J].
Bolotin, VV .
COMPOSITES PART B-ENGINEERING, 1996, 27 (02) :129-145
[7]   Modeling of delamination using a discretized cohesive zone and damage formulation [J].
Borg, R ;
Nilsson, L ;
Simonsson, K .
COMPOSITES SCIENCE AND TECHNOLOGY, 2002, 62 (10-11) :1299-1314
[8]  
Carrera E., 2003, Applied Mechanics Review, V56, P287, DOI 10.1115/1.1557614
[9]   Delamination buckling growth in laminated composites using layerwise-interface element [J].
Hosseini-Toudeshky, Hossein ;
Hosseini, Samira ;
Mohammadi, Bijan .
COMPOSITE STRUCTURES, 2010, 92 (08) :1846-1856
[10]   C0 plate element for delamination damage analysis, based on a zig-zag model and strain energy updating [J].
Icardi, U ;
Zardo, G .
INTERNATIONAL JOURNAL OF IMPACT ENGINEERING, 2005, 31 (05) :579-606