Micromechanical modelling of matrix cracks effect on shear and transverse response for unidirectional composites with a full field approach

被引:4
作者
Burgarella, B. [1 ]
Maurel-Pantel, A. [1 ]
Lahellec, N. [1 ]
Hochard, C. [1 ]
机构
[1] Aix Marseille Univ, CNRS, Cent Marseille, LMA, Marseille, France
关键词
Homogenization; Microcracked composite; Stiffness degradation; Transverse damage; CONTINUUM DAMAGE MODEL; NUMERICAL-METHOD; PLY;
D O I
10.1016/j.compstruct.2018.10.036
中图分类号
O3 [力学];
学科分类号
08 ; 0801 ;
摘要
Modelling the damage of composite materials is not an easy task because different modes of ruins coexist: Fiber matrix decohesion,matrix cracks, delamination, and fiber cracks. In the case of laminated composites, the matrix cracks have the particularity to remain parallel to the fibers. As a consequence of the orientation of this crack network, only shear and transverse moduli in the plane of the ply are degraded in proportion to the increase of the crack density. The main point of this work is to characterize the relation linking transverse and shear damage with respect to the crack density. Following this objective, full field calculations are run using CraFT, a software developed at the LMA. The modeling is done in two steps: first the undamaged composite is homogenized, then, as a second step, the damaged behavior is determined by introducing cracks into the healthy composite. The behavior is calculated from an optimal size of RVE (Representative Volume Element) in order to determine numerically the relation between transverse and shear moduli variables.
引用
收藏
页码:338 / 345
页数:8
相关论文
共 24 条
[1]  
[Anonymous], TEST METHOD TENSILE, DOI [10.1520/d3039d3039m-17, DOI 10.1520/D3039D3039M-17]
[2]  
[Anonymous], TEST METHOD SHEAR PR, DOI [10.1520/d5379d5379m-12, DOI 10.1520/D5379D5379M-12]
[3]  
[Anonymous], TEST METHOD PLANE SH, DOI [10.1520/d3518d3518m, DOI 10.1520/D3518D3518M]
[4]   Analysis of the transverse cracking of cross-ply laminates: a generalized approach [J].
Berthelot, JM .
JOURNAL OF COMPOSITE MATERIALS, 1997, 31 (18) :1780-1805
[5]   Micromechanical modeling and computation of elasto-plastic materials reinforced with distributed-orientation fibers [J].
Doghri, I ;
Tinel, L .
INTERNATIONAL JOURNAL OF PLASTICITY, 2005, 21 (10) :1919-1940
[6]   ANALYSIS OF CRACKED LAMINATES - A VARIATIONAL APPROACH [J].
HASHIN, Z .
MECHANICS OF MATERIALS, 1985, 4 (02) :121-136
[7]   A generalized damage model for woven ply laminates under static and fatigue loading conditions [J].
Hochard, Ch. ;
Thollon, Y. .
INTERNATIONAL JOURNAL OF FATIGUE, 2010, 32 (01) :158-165
[8]   Gradual failure in fibre/polymer laminates [J].
Knops, M ;
Bögle, C .
COMPOSITES SCIENCE AND TECHNOLOGY, 2006, 66 (05) :616-625
[9]   DAMAGE MODELING OF THE ELEMENTARY PLY FOR LAMINATED COMPOSITES [J].
LADEVEZE, P ;
LEDANTEC, E .
COMPOSITES SCIENCE AND TECHNOLOGY, 1992, 43 (03) :257-267
[10]   On a damage mesomodel for laminates:: micromechanics basis and improvement [J].
Ladevèze, P ;
Lubineau, G .
MECHANICS OF MATERIALS, 2003, 35 (08) :763-775