Electrical behavior of laminated composites with intralaminar degradation: A comprehensive micro-meso homogenization procedure

被引:24
作者
Selvakumaran, Lakshmi [1 ]
Lubineau, Gilles [1 ]
机构
[1] KAUST, Phys Sci & Engn Div, COHMAS Lab, Thuwal 239556900, Saudi Arabia
关键词
Laminates; Damage; Electrical homogenization; Mesomodel; Electrical impedance tomography; POTENTIAL CHANGE METHOD; DAMAGE MESOMODEL; MATRIX CRACK; DELAMINATION;
D O I
10.1016/j.compstruct.2013.10.057
中图分类号
O3 [力学];
学科分类号
08 ; 0801 ;
摘要
Electrical Resistance Tomography (ERT) is a promising health monitoring technique to assess damage in laminated composites. Yet, the missing link between the various complex degradation mechanisms within the laminate and its global change in resistivity prevents ERT from being used as a quantitative technique. We propose an electrical mesomodel that can establish this link between the various microscale degradations and the resistivity changes in the measurements. The mesoscale homogenization of transverse cracks with local delamination of the ply is first described for in-plane electrical loading for both the outer and the inner plies. The mesoscale model is then extended to include the out-of-plane loading. The relationship between the mesoscale damage indicators and the degradation morphology is identified. These damage indicators are found to be intrinsic to the ply. As such, this defines the first step towards the interpretation of resistivity measurement in terms of micromechanical damage. (C) 2013 Elsevier Ltd. All rights reserved.
引用
收藏
页码:178 / 188
页数:11
相关论文
共 32 条
[1]   In-situ monitoring of damage in CFRP laminates by means of AC and DC measurements [J].
Abry, JC ;
Choi, YK ;
Chateauminois, A ;
Dalloz, B ;
Giraud, G ;
Salvia, M .
COMPOSITES SCIENCE AND TECHNOLOGY, 2001, 61 (06) :855-864
[2]   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
[3]   Aircraft composites assessment by means of transient thermal NDT [J].
Avdelidis, NP ;
Almond, DP ;
Dobbinson, A ;
Hawtin, BC ;
Ibarra-Castanedo, C ;
Maldague, X .
PROGRESS IN AEROSPACE SCIENCES, 2004, 40 (03) :143-162
[4]   THE ANALYSIS OF CARBON-FIBER STRENGTH DISTRIBUTIONS EXHIBITING MULTIPLE-MODES OF FAILURE [J].
BEETZ, CP .
FIBRE SCIENCE & TECHNOLOGY, 1982, 16 (01) :45-59
[5]  
Campbell FlakeC., 2010, Structural composite materials
[6]   DETERMINATION OF SINGLE FIBER STRENGTH DISTRIBUTION FROM FIBER BUNDLE TESTINGS [J].
CHI, ZF ;
CHOU, TW ;
SHEN, GY .
JOURNAL OF MATERIALS SCIENCE, 1984, 19 (10) :3319-3324
[7]   Structural health monitoring techniques for aircraft composite structures [J].
Diamanti, K. ;
Soutis, C. .
PROGRESS IN AEROSPACE SCIENCES, 2010, 46 (08) :342-352
[8]   The detection of aeronautical defects in situ on composite structures using Non Destructive Testing [J].
Garnier, Christian ;
Pastor, Marie-Laetitia ;
Eyma, Florent ;
Lorrain, Bernard .
COMPOSITE STRUCTURES, 2011, 93 (05) :1328-1336
[9]   Fatigue damage characterization in carbon fibre composite materials using an electrical potential technique [J].
Irving, PE ;
Thiagarajan, C .
SMART MATERIALS & STRUCTURES, 1998, 7 (04) :456-466
[10]   A computational damage micromodel of laminated composites [J].
Ladevèze, P ;
Lubineau, G ;
Violeau, D .
INTERNATIONAL JOURNAL OF FRACTURE, 2006, 137 (1-4) :139-150