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Estimation of Notched Composite Plates Fatigue Life Using Residual Strength Model Calibrated by Step-Wise Tests

机译:用逐步检验校准的残余强度模型估算带缺口复合板的疲劳寿命

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摘要

The proposed new technique of fatigue life prediction for notched composite plates is based on a residual strength model calibrated with the use of step-wise fatigue tests. It was proposed to calibrate the fatigue model with fatigue tests in which load conditions are in a step-wise fashion. The adopted fatigue model takes into account the most important loading parameters such as testing frequency, stress ratio, layer orientation and maximal fatigue stress. It was demonstrated that with the use of step-wise fatigue tests, it is possible to calibrate the fatigue model for a particular material and structure with the use of fewer samples. In the experimental tensile and fatigue tests TVR 380 M12/26%/R-glass/epoxy composite plates [+45°/−45°]4 with circular and elliptical cut-outs were used. The fatigue tests were performed under different loading conditions. The influence of testing frequency, stress ratio, maximal fatigue load and also geometry of the cut-out on damage growth rate and fatigue life were studied. The predicted fatigue life was in good agreement with the durability determined experimentally in all investigated samples.
机译:缺口复合板的疲劳寿命预测新技术的提出是基于使用逐步疲劳测试进行校准的残余强度模型。提出了通过疲劳试验来校准疲劳模型的方法,其中载荷条件是逐步的。所采用的疲劳模型考虑了最重要的载荷参数,例如测试频率,应力比,层取向和最大疲劳应力。事实证明,通过使用逐步疲劳测试,可以使用更少的样本来校准特定材料和结构的疲劳模型。在实验拉伸和疲劳测试中,使用了带有圆形和椭圆形切口的TVR 380 M12 / 26%/ R玻璃/环氧树脂复合板[+ 45°/ -45°] 4。疲劳测试在不同的负载条件下进行。研究了测试频率,应力比,最大疲劳载荷以及切口的几何形状对损伤增长率和疲劳寿命的影响。预测的疲劳寿命与在所有研究样品中通过实验确定的耐用性高度吻合。

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