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Random fatigue life prediction of carbon fibre-reinforced composite laminate based on hybrid time-frequency domain method

机译:基于杂交时频域法的碳纤维增强复合层压板的随机疲劳寿命预测

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摘要

To evaluate fatigue life of composite laminate with hole under random loading, a random fatigue life prediction model is established by hybrid time-frequency domain method in this paper. Firstly, dynamic response of composite laminate is obtained from FE model in frequency domain. Secondly, root mean square of stress of six stress components of critical damage point in frequency domain are transferred to stresses in time domain. At last, 3D Tsai Hill static failure criterion is adopted to convert the multiaxial stress into the uniaxial equivalent stress. Fatigue life is predicted by equivalent stress fatigue life code. The method is validated with the random vibration fatigue test of carbon fibre-reinforced composite laminate. Numerical results are compared with random fatigue experiments which show good agreement with numerical results.
机译:为了评估随机加载下具有孔的复合层压材料的疲劳寿命,本文通过混合时频域法建立了随机疲劳寿命预测模型。 首先,从频域中的Fe模型获得复合层压板的动态响应。 其次,频率域中临界损伤点的六应力分量的应力的根均值被转移到时域的应力。 最后,采用3D Tsai Hill静态故障标准将多轴应力转化为单轴等效应力。 通过等效的应力疲劳寿命守则预测疲劳寿命。 该方法验证了碳纤维增强复合层压板的随机振动疲劳试验。 将数值结果与随机疲劳实验进行比较,其与数值结果吻合良好。

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