Impact resistance and tolerance of interleaved tape laminates

被引:35
作者
Duarte, A
Herszberg, I
Paton, R
机构
[1] Royal Melbourne Inst Technol, Sir Lawrence Wackett Ctr Aerosp Design Technol, Melbourne, Vic 3001, Australia
[2] Royal Melbourne Inst Technol, Dept Aerosp Engn, Melbourne, Vic 3001, Australia
[3] Cooperat Res Ctr Adv Composites Struct Ltd, Fishermens Bend, Vic 3207, Australia
关键词
interleaving; impact resistance; damage tolerance; compression after impact; carbon/epoxy tape;
D O I
10.1016/S0263-8223(00)00049-0
中图分类号
O3 [力学];
学科分类号
08 ; 0801 ;
摘要
This paper presents and discusses the results of low-velocity impact and compression-after-impact (CAI) tests conducted on interleaved and non-interleaved carbon/epoxy tape laminates. Olefin film interleaves provided a strong interface bond, resulting in a reduction in projected damage area. These interleaves changed the stress distribution under impact and restricted delamination formation at the ply interface. An investigation into the compression behaviour of these laminates revealed a reduction in undamaged strength using olefin interleaves. This was attributed to the lack of lateral support for fibres at the fibre/interleaf interface, allowing fibre microbuckling to occur at a low load. Low modulus copolyamide web interleaves resulted in an increase in damage area and minor changes to CAI strength. Examination of laminate cross-sections revealed that this was due to both the open structure of the interleaf and Door resin/interleaf adhesion. High shear modulus polyethylene interleaves resulted in a significant decrease in damage area at various impact energies, with CAI strength improved compared to the non-interleaved laminates. (C) 2000 Published by Elsevier Science Ltd. All rights reserved.
引用
收藏
页码:753 / 758
页数:6
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