Re-evaluation of mode I bridging traction modelling for z-pinned laminates based on experimental analysis

被引:67
|
作者
Mouritz, A. P. [1 ]
Koh, T. M. [1 ]
机构
[1] RMIT Univ, Sir Lawrence Wackett Aerosp Res Ctr, Sch Aerosp Mech & Mfg Engn, Melbourne, Vic 3000, Australia
关键词
Polymer-matrix composites (PMCs); Delamination; Analytical modelling; Z-pin; Z-PINS; DELAMINATION TOUGHNESS; FAILURE MECHANISMS; T-JOINTS; COMPOSITE; REINFORCEMENT; THICKNESS; FRACTURE; PULLOUT;
D O I
10.1016/j.compositesb.2013.09.016
中图分类号
T [工业技术];
学科分类号
08 ;
摘要
This paper re-evaluates the crack bridging traction analysis used to calculate the mode I interlaminar fracture toughness of z-pinned fibre-polymer laminates. Existing bridging traction models use several simplifying assumptions about the physical condition and failure mode of z-pins embedded within laminates which compromises their numerical accuracy. Microstructural analysis and z-pin bridging traction tests revealed that misalignment of z-pins, interfacial cracking around z-pins, porosity within z-pins, and failure mode of z-pins each affect the traction properties, albeit in different ways. The mode I bridging models have been modified to account for these factors. The accuracy of traction loads calculated using the modified model compare favourably against experimental loads measured for fibrous z-pins in carbon-epoxy laminate. (C) 2013 Elsevier Ltd. All rights reserved.
引用
收藏
页码:797 / 807
页数:11
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