Preliminary approach to the study of flexural fatigue behavior of low Tg carbon/epoxy laminates

A. D’Amore, R. Dell’Aversano, A. Califano
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Abstract

The static strength of carbon/epoxy laminates with three different stacking sequence has been analyzed at different strain rates under three point flexural tests. The materials under study were low cost, low Tg carbon/epoxy laminates with nominal thickness of 1 mm obtained stacking four fabric 0/90 balanced prepregs. The Weibull distribution function was used to compare the data on statistical basis.Quasi–isotropic, cross-ply and angle ply laminates were tested and the strain dependence of static strength was accounted for in the framework of a phenomenological model for fatigue with the objective test the model reliability in predicting the fatigue life and residual strength under variable spectrum with block loadings characterized by different loading frequencies.Preliminary results show that the phenomenological approach can be suitably applied in a rather simple manner solving one of the most intricate tasks within the field of fatigue of composite materials. The research activity represents the last step to build up a software that under variable amplitude loadings comprehensively accounts simultaneously and cycle-by-cycle for the change in the loading ratio, R=σmin/σmax, the maximum applied stress, σmax, and the frequency of loading, f. Details of the approach and the physics behind it are briefly presented with a series of preliminary results.The static strength of carbon/epoxy laminates with three different stacking sequence has been analyzed at different strain rates under three point flexural tests. The materials under study were low cost, low Tg carbon/epoxy laminates with nominal thickness of 1 mm obtained stacking four fabric 0/90 balanced prepregs. The Weibull distribution function was used to compare the data on statistical basis.Quasi–isotropic, cross-ply and angle ply laminates were tested and the strain dependence of static strength was accounted for in the framework of a phenomenological model for fatigue with the objective test the model reliability in predicting the fatigue life and residual strength under variable spectrum with block loadings characterized by different loading frequencies.Preliminary results show that the phenomenological approach can be suitably applied in a rather simple manner solving one of the most intricate tasks within the field of fatigue of composite materials. The research activity represents the last ...
低Tg碳/环氧复合材料弯曲疲劳性能研究的初步探讨
在三点弯曲试验中,分析了三种不同堆叠顺序的碳/环氧复合材料在不同应变速率下的静强度。所研究的材料是低成本,低Tg碳/环氧复合材料,公称厚度为1mm,可堆叠四种织物0/90平衡预浸料。采用威布尔分布函数对数据进行统计比较。对准各向同性、交叉铺层和角铺层复合材料进行了试验,并在疲劳现象学模型框架内考虑了静强度的应变依赖性,客观检验了模型在不同加载频率的块加载变谱下预测疲劳寿命和残余强度的可靠性。初步结果表明,现象学方法可以以一种相当简单的方式解决复合材料疲劳领域中最复杂的问题之一。该研究是建立一个在变幅加载条件下,同时并逐周期综合计算加载比R=σmin/σmax、最大外加应力σmax和加载频率变化的软件的最后一步。本文简要介绍了该方法的细节及其背后的物理原理,并给出了一系列初步结果。在三点弯曲试验中,分析了三种不同堆叠顺序的碳/环氧复合材料在不同应变速率下的静强度。所研究的材料是低成本,低Tg碳/环氧复合材料,公称厚度为1mm,可堆叠四种织物0/90平衡预浸料。采用威布尔分布函数对数据进行统计比较。对准各向同性、交叉铺层和角铺层复合材料进行了试验,并在疲劳现象学模型框架内考虑了静强度的应变依赖性,客观检验了模型在不同加载频率的块加载变谱下预测疲劳寿命和残余强度的可靠性。初步结果表明,现象学方法可以以一种相当简单的方式解决复合材料疲劳领域中最复杂的问题之一。这项研究活动代表了最后的…
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