Influence of open holes on composites delamination induced by low velocity impact loads

被引:33
作者
Amaro, A. M. [1 ]
Reis, P. N. B. [2 ]
de Moura, M. F. S. F. [3 ]
Neto, M. A. [1 ]
机构
[1] Univ Coimbra, Dept Mech Engn, CEMUC, P-3030788 Coimbra, Portugal
[2] Univ Beira Interior, Dept Electromech Engn, P-6200 Covilha, Portugal
[3] Univ Porto, Fac Engn, P-4200465 Oporto, Portugal
关键词
Composites; Delamination; Holes; Impact; COMPRESSIVE FAILURE; DAMAGE; PREDICTION; MECHANISMS; SIMULATION; STRENGTH; BEHAVIOR; CFRP;
D O I
10.1016/j.compstruct.2012.09.041
中图分类号
O3 [力学];
学科分类号
08 ; 0801 ;
摘要
The aim of this study is to evaluate the influence of holes on delamination induced by low velocity impact on glass/epoxy composite laminates. Plates containing one and two holes were tested and the resulting damage was compared with the one of plate without hole. A finite element analysis including a cohesive mixed-mode damage model was performed in order to better understand the interaction between the resulting delamination and the presence of holes. It was verified that presence of holes increases the energy absorbed by damage as well as the delaminated areas. Delamination profile is also affected owing to alteration of interlaminar shear stress profiles which are the main responsible for delamination between different oriented layers. (C) 2012 Elsevier Ltd. All rights reserved.
引用
收藏
页码:239 / 244
页数:6
相关论文
共 30 条
[1]   A REVIEW OF DEFECT TYPES AND NONDESTRUCTIVE TESTING TECHNIQUES FOR COMPOSITES AND BONDED JOINTS [J].
ADAMS, RD ;
CAWLEY, P .
NDT INTERNATIONAL, 1988, 21 (04) :208-222
[2]   Residual strength after low velocity impact in carbon-epoxy laminates [J].
Amaro, A. M. ;
Reis, P. N. B. ;
Moura, M. F. S. F. .
ADVANCED MATERIALS FORUM III, PTS 1 AND 2, 2006, 514-516 :624-628
[3]   Damage detection on laminated composite materials using several NDT techniques [J].
Amaro, A. M. ;
Reis, P. N. B. ;
de Moura, M. F. S. F. ;
Santos, J. B. .
INSIGHT, 2012, 54 (01) :14-20
[4]   The Influence of the Boundary Conditions on Low-Velocity Impact Composite Damage [J].
Amaro, A. M. ;
Reis, P. N. B. ;
Magalhaes, A. G. ;
de Moura, M. F. S. F. .
STRAIN, 2011, 47 :E220-E226
[5]   Delamination Effect on Bending Behaviour in Carbon-Epoxy Composites [J].
Amaro, A. M. ;
Reis, P. N. B. ;
de Moura, M. F. S. F. .
STRAIN, 2011, 47 (02) :203-208
[6]   Prediction of low velocity impact damage in carbon-epoxy laminates [J].
de Moura, MFSF ;
Marques, AT .
COMPOSITES PART A-APPLIED SCIENCE AND MANUFACTURING, 2002, 33 (03) :361-368
[7]   Modelling the interaction between matrix cracking and delamination in carbon-epoxy laminates under low velocity impact [J].
de Moura, MFSF ;
Gonçalves, JPM .
COMPOSITES SCIENCE AND TECHNOLOGY, 2004, 64 (7-8) :1021-1027
[8]   Numerical simulation of the drilling process on carbon/epoxy composite laminates [J].
Durao, L. M. P. ;
de Moura, M. F. S. F. ;
Marques, A. T. .
COMPOSITES PART A-APPLIED SCIENCE AND MANUFACTURING, 2006, 37 (09) :1325-1333
[9]   STRESS-CONCENTRATION OF A LAMINATE WEAKENED BY MULTIPLE HOLES [J].
FAN, WX ;
WU, JG .
COMPOSITE STRUCTURES, 1988, 10 (04) :303-319
[10]   Compressive failure mechanisms in multi-fibre microcomposites [J].
Goutianos, S ;
Galiotis, C ;
Peijs, T .
COMPOSITES PART A-APPLIED SCIENCE AND MANUFACTURING, 2004, 35 (04) :461-475