Evolution of damage during the fatigue of 3D woven glass-fibre reinforced composites subjected to tension-tension loading observed by time-lapse X-ray tomography

被引:80
|
作者
Yu, B. [1 ]
Blanc, R. [3 ]
Soutis, C. [2 ]
Withers, P. J. [1 ]
机构
[1] Univ Manchester, Sch Mat, Henry Moseley Xray Imaging Facil, Manchester M13 9PL, Lancs, England
[2] Univ Manchester, Aerosp Res Inst, Manchester M13 9PL, Lancs, England
[3] FEI SAS, 3 Impasse Rudolf Diesel,BP 50 227, F-33708 Merignac, France
基金
英国工程与自然科学研究理事会;
关键词
Debonding; Microstructure; Transverse cracking; Damage mechanics; LOW-VELOCITY IMPACT; PLY STITCHED PREFORMS; FAILURE MECHANISMS; COMPUTED-TOMOGRAPHY; TRANSVERSE CRACKING; TEXTILE COMPOSITES; HIGH-RESOLUTION; FRACTURE; MICROMECHANISMS; PROGRESSION;
D O I
10.1016/j.compositesa.2015.09.001
中图分类号
T [工业技术];
学科分类号
08 ;
摘要
The development of fatigue damage in a glass fibre modified layer-to-layer three dimensional (3D) woven composite has been followed by time-lapse X-ray computed tomography (CT). The damage was found to be distributed regularly throughout the composite according to the repeating unit, even at large fractions of the total life. This suggests that the through-thickness constraint provides a high level of stress redistribution and damage tolerance. The different types of damage have been segmented, allowing a quantitative analysis of damage evolution as a function of the number of fatigue cycles. Transverse cracks were found to initiate within the weft after just 0.1% of life, followed soon after (by 1% of life) by longitudinal debonding cracks. The number and extent of these multiplied steadily over the fatigue life, whereas the spacing of transverse cracks along with weft/binder debonding saturated at 60% of life and damage in the resin pockets occurred only just before final failure. (C) 2015 The Authors. Published by Elsevier Ltd. This is an open access article under the CC BY license (http://creativecommons.org/licenses/by/4.0/).
引用
收藏
页码:279 / 290
页数:12
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