Fatigue design allowables for GRP laminates based on stiffness degradation measurements

被引:68
作者
Philippidis, TP [1 ]
Vassilopoulos, AP [1 ]
机构
[1] Univ Patras, Dept Aeronaut & Mech Engn, Sect Appl Mech, Patras 26500, Greece
关键词
stiffness degradation; S/N curves; reliability; glass/polyester; off-axis; fatigue;
D O I
10.1016/S0266-3538(00)00150-0
中图分类号
TB33 [复合材料];
学科分类号
摘要
The fatigue behaviour of a multidirectional, [0(+/-45)(2)/0](T) glass/polyester laminate under various loadings conditions is studied in this paper. Series of coupons cut on- and off-axis, at seven different orientations, were uniaxially loaded at constant amplitude over a wide range of R ratios. Test data were subjected to statistical analysis and S/N curves at specific reliability levels were calculated. Stiffness changes were continuously monitored during fatigue testing, and design curves corresponding to a certain level of stiffness reduction, and not to failure, were determined. It is shown, for the material studied in this work, that stiffness-based and reliability S./N curves are correlated and therefore determination of fatigue design allowables bearing information on both stiffness loss and strength can be formulated. (C) 2000 Elsevier Science Ltd. All rights reserved.
引用
收藏
页码:2819 / 2828
页数:10
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