Analytical prediction of large mass impact damage in composite laminates

被引:190
作者
Olsson, R [1 ]
机构
[1] Swedish Def Res Agcy, Aeronaut Div, FFA, SE-17290 Stockholm, Sweden
关键词
plates; polymer-matrix composites (PMCs); impact behaviour; analytical modelling;
D O I
10.1016/S1359-835X(01)00073-2
中图分类号
T [工业技术];
学科分类号
08 ;
摘要
Analytical models are suggested for prediction of impact damage initiation and growth during quasi-static response caused by large mass impactors. Comparisons with experiments are presented for different layups, geometries and boundary conditions. The critical load for delamination growth is found almost insensitive to geometry and boundary conditions. The critical energy for delamination growth is separated in bending, shear and indentation contributions. Further growth depends on the number of delaminations developing, and is in thin laminates limited by the early occurrence of penetration. Observed delamination sizes are compared with a suggested upper bound and predictions based on the observed number of delaminations. (C) 2001 Elsevier Science Ltd. All rights reserved.
引用
收藏
页码:1207 / 1215
页数:9
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