COMPUTATIONAL METHODOLOGY TO PREDICT DAMAGE GROWTH IN UNIDIRECTIONAL COMPOSITES .1. THEORETICAL FORMULATION AND NUMERICAL IMPLEMENTATION

被引:5
作者
BAKUCKAS, JG [1 ]
LAU, ACW [1 ]
TAN, TM [1 ]
AWERBUCH, J [1 ]
机构
[1] DREXEL UNIV,DEPT MECH ENGN & MECH,PHILADELPHIA,PA 19104
关键词
D O I
10.1016/0013-7944(94)00148-B
中图分类号
O3 [力学];
学科分类号
08 ; 0801 ;
摘要
The theoretical formulation and numerical implementation of a computational methodology for predicting both the initiation and growth of damage in a unidirectional composite monolayer is presented. The methodology has been implemented into a finite element program to form the Micromechanics Analysis and Damage Growth In Composites (MADGIC) code. A node splitting and nodal force relaxation algorithm that is capable of generating new crack surfaces has been incorporated to simulate damage initiation and growth. One of the unique features of this code is that the instantaneous direction of damage progression is dictated by the local mechanics and failure criteria. Thus, the crack path need not be preselected. Common modes of damage that take place in composites, including fiber breakage, matrix cracking and fiber-matrix debonding, are simulated using the node splitting mechanisms in conjunction with mechanistic failure criteria. An incremental elastic-plastic algorithm with J(2) flow theory and isotropic hardening has also been incorporated to account for matrix plastic deformation when analyzing damage growth in metal matrix composites. In order to efficiently model standard laboratory size composite specimens, a hybrid micromechanical-anisotropic continuum model has been used consisting of a heterogeneous region enclosing the micromechanical damage processing zone, and an outer homogeneous region to which the far-field load is applied.
引用
收藏
页码:937 / 951
页数:15
相关论文
共 22 条
[1]   ELASTOPLASTIC CRACK-PROPAGATION IN A TRANSVERSELY LOADED UNIDIRECTIONAL COMPOSITE [J].
ADAMS, DF .
JOURNAL OF COMPOSITE MATERIALS, 1974, 8 (JAN) :38-54
[2]  
ADAMS DF, 1982, UWMEDR2011011 U WY D
[3]  
ADAMS DF, 1981, UWMEDR1011021 U WY D
[4]   TENSILE FRACTURE OF LAMINATES WITH CRACKS [J].
ARONSSON, CG ;
BACKLUND, J .
JOURNAL OF COMPOSITE MATERIALS, 1986, 20 (03) :287-307
[5]   FRACTURE-ANALYSIS OF NOTCHED COMPOSITES [J].
BACKLUND, J .
COMPUTERS & STRUCTURES, 1981, 13 (1-3) :145-154
[6]   TENSILE FRACTURE OF LAMINATES WITH HOLES [J].
BACKLUND, J ;
ARONSSON, CG .
JOURNAL OF COMPOSITE MATERIALS, 1986, 20 (03) :259-286
[7]   COMPUTATIONAL METHODOLOGY TO PREDICT DAMAGE GROWTH IN UNIDIRECTIONAL COMPOSITES .2. CASE-STUDIES [J].
BAKUCKAS, JG ;
TAN, TM ;
LAU, ACW ;
AWERBUCH, J .
ENGINEERING FRACTURE MECHANICS, 1995, 52 (05) :953-&
[8]  
Bathe KJ., 2006, FINITE ELEMENT PROCE
[9]  
BIGELOW CA, 1992, AM SOC TEST MATER, V1120, P222, DOI 10.1520/STP20157S
[10]   FINITE-ELEMENT MODELING OF FRACTURE PROPAGATION IN ORTHOTROPIC MATERIALS [J].
BOONE, TJ ;
WAWRZYNEK, PA ;
INGRAFFEA, AR .
ENGINEERING FRACTURE MECHANICS, 1987, 26 (02) :185-201