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PLY-BY-PLY BASIS OFF-AXIS FATIGUE LIFE PREDICTION FOR CROSS-PLY CFRP LAMINATES AT ROOM TEMPERATURE

机译:逐层轴外疲劳寿命预测在室温下对CRIP CFRP层压板

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Off-axis fatigue behavior of a symmetric cross-ply carbon/epoxy laminate is examined at room temperature and a fatigue life prediction method that considers inelastic deformation and in-situ strength of embedded plies is developed. The fiber orientation dependence of the off-axis fatigue data on the cross-ply laminate can be removed by normalizing them with respect to static strength. The distribution of the normalized off-axis fatigue data of the cross-ply laminate almost agrees with the result for the unidirectional laminates made of the same prepreg tape. Then, off-axis fatigue analysis of cross-ply laminates is performed on a ply-by-ply basis. For this purpose, a ply fatigue model that takes into account in-situ static strengths of plies embedded in a laminate is proposed. Stresses in the cross-ply laminate are evaluated using a CLT-based laminate constitutive model that considers nonlinear deformation of embedded plies. Predicted off-axis fatigue lives of the cross-ply laminate are shown to correlate well with experimental results.
机译:离轴对称交叉帘布层碳的疲劳行为/环氧层压在室温下,并且考虑非弹性变形和原位嵌入帘布层的强度时的疲劳寿命预测方法检测。对交叉层层压材料的离轴疲劳数据的纤维取向依赖性可以通过相对于静态强度归它们被去除。交叉层层压材料的归一化离轴疲劳数据的分布几乎与结果对于由同样的预浸渍带的单向层压板一致。然后,对一个帘布层逐帘布层的基础上执行的交叉层层压的离轴疲劳分析。为了这个目的,一个帘布层的疲劳模型,该模型考虑到原位嵌入在层压板层的静态强度,提出了帐户。在交叉层层压材料的应力使用考虑嵌入帘布层非线性变形基于CLT层叠构模型评估。预测离轴疲劳交叉层层压材料的生活被示出与实验结果良好关联。

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