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Fatigue life prediction method for notched 3D woven composites based on progressive damage and field intensity

机译:基于渐进式损伤和场强的缺口3D编织复合材料的疲劳寿命预测方法

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摘要

To solve the problem of fatigue life prediction of notched 3D woven composites, a novel fatigue life prediction method based on progressive damage and field intensity theory is proposed. By analyzing the initial loading process of 3D woven composite structure based on progressive damage method, the stress field when the fatigue damage develops gently and the dangerous area where the fatigue damage occurs first are obtained. Then combining with the concept of notch field intensity function, the failure criteria of composites and the three-dimensional space vector stress field intensity method, the fatigue damage degree field intensity of the fiber yarns in the dangerous area is analyzed and the most damaged fiber yarn is found. The fatigue life of the structure is calculated with the field intensity equivalent stress and the S-N curve of this fiber yarn. In order to verify the effectiveness of this method, the fatigue life of notched 3D woven composites under several stress levels is predicted and compared with the existing experimental data. The compared results show that the fatigue life prediction values are all within the two-fold error bounds of the experimental data, which are in good agreement with experimental results. Compared with the progressive damage fatigue life prediction method of woven composites, the prediction accuracy of the method proposed in this paper is improved by 31.5% on average, and the calculation efficiency is also greatly improved.
机译:为了解决缺口3D编织复合材料的疲劳寿命预测问题,提出了一种基于渐进式损伤和场强度理论的新型疲劳寿命预测方法。通过分析基于渐进式损伤方法的3D编织复合结构的初始加载过程,获得疲劳损伤的压力场,并且首先获得疲劳损伤发生的危险区域。然后与陷波场强度函数的概念相结合,复合材料的故障标准和三维空间矢量应力场强度法,分析了危险区域中纤维纱的疲劳损伤度场强度,纤维纱线最损坏被发现。结构的疲劳寿命用该纤维纱的场强等同应力和S-N曲线计算。为了验证该方法的有效性,预测了在若干应力水平下的缺口3D编织复合材料的疲劳寿命并与现有的实验数据进行比较。比较结果表明,疲劳寿命预测值全部内在实验数据的两倍误差范围内,这与实验结果很好。与编织复合材料的渐进损伤疲劳寿命预测方法相比,本文提出的方法的预测精度平均提高了31.5%,计算效率也大大提高。

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