Low Velocity Impact Induced Delamination Control Using MFC Actuator

被引:7
作者
Dawood, M. S. I. Shaik [1 ]
Iannucci, L. [1 ,2 ,3 ]
Greenhalgh, E. [1 ]
Ariffin, A. K. [2 ]
机构
[1] Univ London Imperial Coll Sci Technol & Med, Dept Aeronaut, S Kensington Campus, London, England
[2] Univ Kebangsaan Malaysia, Dept Mech & Mat Engn, Bangi 43600, Malaysia
[3] Int Islamic Univ Malaysia, Dept Mech, Kuala Lumpur, Malaysia
来源
TRENDS IN AUTOMOTIVE RESEARCH | 2012年 / 165卷
关键词
Piezoelectric; delamination; low velocity impact; cohesive; INTERFACE ELEMENTS; PREDICTION; PLATES;
D O I
10.4028/www.scientific.net/AMM.165.346
中图分类号
TH [机械、仪表工业];
学科分类号
0802 ;
摘要
The potential use of MFC actuator as a tool for reducing low velocity impact induced delamination has been investigated using LS-DYNA explicit finite element code. An induced strain piezoelectric actuation model was implemented into LS-DYNA through its user defined material subroutine to simulate the piezoelectric effects while a cohesive based damage model was used to predict delamination. The numerical study confirmed that delamination could be reduced but the MFC required very high actuation voltages even in the case of very low energy impact which is not practically achievable with the existing actuator. Assuming powerful actuators are not something impossible in near future, this study provide useful information for advancing composite impact investigation using piezoelectric actuator as an integrated tool for improving its impact tolerance.
引用
收藏
页码:346 / +
页数:2
相关论文
共 12 条
[1]  
Agarwal B. D., 1990, ANAL PERFORMANCE FIB, V2nd, P193
[2]   Prediction of impact-induced delamination in cross-ply composite laminates using cohesive interface elements [J].
Aymerich, F. ;
Dore, F. ;
Priolo, P. .
COMPOSITES SCIENCE AND TECHNOLOGY, 2008, 68 (12) :2383-2390
[3]  
Cantwell W. J., 1992, J STRAIN ANAL ENG DE, V27
[4]   INDUCED STRAIN ACTUATION OF ISOTROPIC AND ANISOTROPIC PLATES [J].
CRAWLEY, EF ;
LAZARUS, KB .
AIAA JOURNAL, 1991, 29 (06) :944-951
[5]   Prediction of threshold impact energy for onset of delamination in quasi-isotropic carbon/epoxy composite laminates under low-velocity impact [J].
Davies, GAO ;
Hitchings, D ;
Wang, J .
COMPOSITES SCIENCE AND TECHNOLOGY, 2000, 60 (01) :1-7
[6]   The assessment of novel materials and processes for the impact tolerant design of stiffened composite aerospace structures [J].
Greenhalgh, E ;
Hiley, M .
COMPOSITES PART A-APPLIED SCIENCE AND MANUFACTURING, 2003, 34 (02) :151-161
[7]   Dynamic delamination modelling using interface elements [J].
Iannucci, L. .
COMPUTERS & STRUCTURES, 2006, 84 (15-16) :1029-1048
[8]   Progressive delamination using interface elements [J].
Mi, Y ;
Crisfield, MA ;
Davies, GAO ;
Hellweg, HB .
JOURNAL OF COMPOSITE MATERIALS, 1998, 32 (14) :1246-1272
[9]   Review of low-velocity impact properties of composite materials [J].
Richardson, MOW ;
Wisheart, MJ .
COMPOSITES PART A-APPLIED SCIENCE AND MANUFACTURING, 1996, 27 (12) :1123-1131
[10]   A MODIFIED DCB SPECIMEN FOR MODE-I TESTING OF MULTIDIRECTIONAL LAMINATES [J].
ROBINSON, P ;
SONG, DQ .
JOURNAL OF COMPOSITE MATERIALS, 1992, 26 (11) :1554-1577