Damage characterization of titanium/GFRP hybrid laminates subjected to low-velocity impact

被引:88
|
作者
Nakatani, Hayato [1 ]
Kosaka, Tatsuro [1 ]
Osaka, Katsuhiko [1 ]
Sawada, Yoshihiro [1 ]
机构
[1] Osaka City Univ, Grad Sch Engn, Dept Mech & Phys Engn, Sumiyoshi Ku, Osaka 5588585, Japan
关键词
Layered structures; Delamination; Impact behaviour; Finite element analysis (FEA); FIBER; BEHAVIOR;
D O I
10.1016/j.compositesa.2011.03.005
中图分类号
T [工业技术];
学科分类号
08 ;
摘要
Low-velocity impact-induced damage in Ti/GFRP laminates as titanium-based Fibre-Metal Laminates (FMLs) was investigated to reveal the extent of internal damage in the in-plane direction and to evaluate the effects of titanium facesheets on impact damage in the GFRP core. It was found that interlaminar delamination in the GFRP layer expands widely due to crack initiation in the titanium layer on nonimpacted side. However, matrix cracks and residual out-of-plane deformation are suppressed by energy absorption achieved by the bottom titanium layer. Furthermore, impact responses and damages obtained by finite element analysis with detailed modelling agree well with the experimental results. Thus, this study confirmed that the impact behaviour of the Ti/GFRP laminates is dominated by a fracture in the titanium layer on non-impacted side that fails in tension and that this layer plays a major role in preventing impact damages in the GFRP core. (C) 2011 Elsevier Ltd. All rights reserved.
引用
收藏
页码:772 / 781
页数:10
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