A multiscale model for damage progression and detection in piezo/pyroelectric composite laminates

被引:5
作者
Bahei-El-Din, Yehia A. [1 ]
Micheal, Amany [1 ]
机构
[1] British Univ Egypt, Ctr Adv Mat, El Shorouk City, Egypt
关键词
Multifunctional composites; Laminates; Plates; Thermomechanical; Computational modeling; Damage mechanics; Laminate mechanics; Micro-mechanics; FIBRE-STRENGTHENED MATERIALS; FIBER-REINFORCED COMPOSITES; WOVEN COMPOSITES; MECHANICAL PROPERTIES; FAILURE ANALYSIS; MATRIX; PREDICTION; STRESS; ENERGY; RANGE;
D O I
10.1016/j.mechmat.2017.07.011
中图分类号
T [工业技术];
学科分类号
08 ;
摘要
Assessment of damage initiation and progression in composite structures reinforced with electrically active filaments is modeled in a multiscale analysis. The analysis developed is a two-tier, interactive analysis, which involves two length scales; macroscopic, and microscopic. The proposed multiscale analysis provides seamless integration of the mechanics at the two length scales, including piezoelectric and pyroelectric coupling effects and damage under overall thermomechanical loads and an electric field applied to electroactive fibers. The macromechanical analysis is performed for multidirectional, fibrous laminates using the lamination theory, including bending, and the micromechanical analysis is performed using a two-phase model and a periodic array model. The effect of eigenstrains caused by thermomechanical, electromechanical, and thermoelectric coupling at both the microscopic and macroscopic length scales is accounted for by a two-tier transformation field analysis (TFA). (C) 2017 Elsevier Ltd. All rights reserved.
引用
收藏
页码:77 / 88
页数:12
相关论文
共 48 条
[1]   Micromechanical analysis of fully coupled electro-magneto-thermo-elastic multiphase composites [J].
Aboudi, J .
SMART MATERIALS & STRUCTURES, 2001, 10 (05) :867-877
[2]  
[Anonymous], PLAST TODAY MODEL ME
[3]   Modelling electromechanical coupling in woven composites exhibiting damage [J].
Bahei-El-Din, Y. A. .
PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART G-JOURNAL OF AEROSPACE ENGINEERING, 2009, 223 (G5) :485-495
[4]  
Bahei-El-Din Y.A., 2012, P INT MECH ENG C EXP, P89304
[5]  
Bahei-El-Din Y.A., 2013, P ASME 2013 INT MECH, P62427
[6]   A micromechanical model for damage progression in woven composite systems [J].
Bahei-El-Din, YA ;
Rajendran, AM ;
Zikry, MA .
INTERNATIONAL JOURNAL OF SOLIDS AND STRUCTURES, 2004, 41 (9-10) :2307-2330
[7]   Analysis of progressive fiber debonding in elastic laminates [J].
Bahei-El-Din, YA ;
Botrous, AG .
INTERNATIONAL JOURNAL OF SOLIDS AND STRUCTURES, 2003, 40 (25) :7035-7053
[8]   MULTISCALE TRANSFORMATION FIELD ANALYSIS OF PROGRESSIVE DAMAGE IN FIBROUS LAMINATES [J].
Bahei-El-Din, Yehia A. ;
Khire, Ritesh ;
Hajela, Prabhat .
INTERNATIONAL JOURNAL FOR MULTISCALE COMPUTATIONAL ENGINEERING, 2010, 8 (01) :69-80
[9]   An analytical and numerical approach for calculating effective material coefficients of piezoelectric fiber composites [J].
Berger, H ;
Kari, S ;
Gabbert, U ;
Rodriguez-Ramos, R ;
Guinovart, R ;
Otero, JA ;
Bravo-Castillero, J .
INTERNATIONAL JOURNAL OF SOLIDS AND STRUCTURES, 2005, 42 (21-22) :5692-5714
[10]  
Berlincourt D., 2009, PROPERTIES MORGAN EL