Simulating damage and delamination in fibre metal laminate joints using a three-dimensional damage model with cohesive elements and damage regularisation

被引:57
作者
Frizzell, R. M. [1 ]
McCarthy, C. T. [1 ]
McCarthy, M. A. [1 ]
机构
[1] Univ Limerick, Dept Mech & Aeronaut Engn, Mat & Surface Sci Inst, Composites Res Ctr, Limerick, Ireland
关键词
Hybrid composites; Computational mechanics; Modelling; CRITERIA; PLY;
D O I
10.1016/j.compscitech.2011.04.006
中图分类号
TB33 [复合材料];
学科分类号
摘要
This paper investigates the capability of a three-dimensional finite element model with damaging material behaviour, cohesive elements and damage regularisation to simulate complex damage patterns in fibre metal laminate (FML) joints. The model incorporates a three-dimensional continuum damage mechanics approach for the composite plies, a plasticity model for the aluminium layers, and a delamination model between layers. A nonlocal averaging scheme is implemented to mitigate the mesh sensitivity that occurs with strain-softening material models. Bearing stress-strain responses and variations in stiffness are calculated, and damage progression is described in detail for all plies and interfaces. Microscopy and stress-strain data from a parallel series of experimental tests are presented, and damage and failure phenomena observed in the tests are compared with the model. Generally, good agreement between model and tests was achieved but certain limitations of the numerical model were observed and are discussed. The combined numerical and experimental information provide a detailed understanding of the failure sequence of FML joints. (C) 2011 Elsevier Ltd. All rights reserved.
引用
收藏
页码:1225 / 1235
页数:11
相关论文
共 27 条
[1]  
*ABAQUS INC, 2006, ABAQUS AN US MAN VER
[2]   Mesomodeling of delamination: towards industrial applications [J].
Allix, O ;
Blanchard, L .
COMPOSITES SCIENCE AND TECHNOLOGY, 2006, 66 (06) :731-744
[3]  
Bazant PZ, 1983, Mater Et Constr, V16, P155, DOI DOI 10.1007/BF02486267
[4]   Nonlocal integral formulations of plasticity and damage:: Survey of progress [J].
Bazant, ZP ;
Jirásek, M .
JOURNAL OF ENGINEERING MECHANICS, 2002, 128 (11) :1119-1149
[5]  
BAZANT ZP, 1988, J STRUCT ENG-ASCE, V114, P2493
[6]   Finite element computation of woven ply laminated composite structures up to rupture [J].
Bordreuil, C ;
Hochard, C .
APPLIED COMPOSITE MATERIALS, 2004, 11 (03) :127-143
[7]  
De Borst R., 1993, Engineering Computations, V10, P99, DOI 10.1108/eb023897
[8]  
De Vries TJ, 2001, BLUNT SHARP NOTCH BE
[9]  
Donadon Mauricio V., 2009, International Journal of Aerospace Engineering, DOI 10.1155/2009/486063
[10]   An experimental investigation into the progression of damage in pin-loaded fibre metal laminates [J].
Frizzell, R. M. ;
McCarthy, C. T. ;
McCarthy, M. A. .
COMPOSITES PART B-ENGINEERING, 2008, 39 (06) :907-925