...
首页> 外文期刊>International Journal of Fatigue >Off-axis fatigue behavior of a carbon/epoxy cross-ply laminate and predictions considering inelasticity and in situ strength of embedded plies
【24h】

Off-axis fatigue behavior of a carbon/epoxy cross-ply laminate and predictions considering inelasticity and in situ strength of embedded plies

机译:碳/环氧树脂交叉层板的轴外疲劳行为以及考虑非弹性和嵌入层原位强度的预测

获取原文
获取原文并翻译 | 示例
           

摘要

The off-axis fatigue behavior of a carbon/epoxy symmetric cross-ply laminate at room temperature is examined, and a ply basis fatigue life prediction method is tested with a special emphasis on consideration of the inelastic deformation and in situ strength of the inclined plies embedded in the laminate. Constant amplitude tension-tension fatigue tests are first performed on the coupon specimens of the cross-ply laminate for various fiber orientations. The fiber orientation dependence of the off-axis fatigue data on the cross-ply laminate can be removed by normalizing the maximum fatigue stress levels with the help of the associated off-axis static strengths. The distribution of the normalized off-axis fatigue data on the cross-ply laminate almost agrees with the normalized fatigue data on the unidirectional laminate made of the same prepreg tape, indicating that the relative fatigue performance of the cross-ply laminate is almost indistinguishable from that of the unidirectional laminate. A simple off-axis fatigue analysis of the cross-ply laminate is then attempted on a ply basis, in which no effects of progressive damage are assumed. A ply fatigue model that takes into account the in situ principal strengths of the plies embedded in a general laminate is developed to this end, along with an analytical procedure for identifying the in situ strength ratios of the actual principal strengths to reference values. The actual stress components in the plies embedded in the cross-ply laminate are evaluated using a laminate constitutive model based on the classical lamination theory, in which the non-linear plastic deformation of inclined plies under in-plane off-axis loading is taken into account. It is demonstrated that good guesses about in situ strength ratios can be made on the basis of elastoplastic CLT analysis, and the off-axis fatigue lives of the cross-ply laminate predicted using appropriate in situ strength ratios are shown to agree well with the experimental results.
机译:研究了碳/环氧对称交叉层状层压板在室温下的轴外疲劳行为,并测试了基于层的疲劳寿命预测方法,并特别着重考虑了倾斜层的无弹性变形和原位强度嵌入层压板中。首先,对各种纤维取向的交叉层压板的试样样本进行恒定振幅的拉伸-拉伸疲劳试验。可以通过在相关的轴外静态强度的帮助下对最大疲劳应力水平进行归一化,来消除交叉层压板上的轴外疲劳数据对纤维取向的依赖性。正交层压板的归一化轴外疲劳数据的分布与由相同预浸料带制成的单向层压板的归一化疲劳数据几乎相符,这表明该正交层压板的相对疲劳性能几乎与单向层压板。然后,以层为基础对交叉层的层压板进行简单的离轴疲劳分析,其中不考虑进行性破坏的影响。为此目的,开发了一种考虑了嵌入到普通层压板中的板层的现场主强度的板层疲劳模型,以及一种用于识别实际主强度与参考值的现场强度比的分析程序。使用基于经典层合理论的层合本构模型评估嵌在交叉层合层板中的层板中的实际应力分量,其中将倾斜层板在面内轴外载荷下的非线性塑性变形考虑在内帐户。结果表明,可以在弹塑性CLT分析的基础上对原位强度比进行很好的猜测,并且使用适当的原位强度比预测的交叉层压板的轴外疲劳寿命与实验吻合得很好。结果。

著录项

相似文献

  • 外文文献
  • 中文文献
  • 专利
获取原文

客服邮箱:kefu@zhangqiaokeyan.com

京公网安备:11010802029741号 ICP备案号:京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有
  • 客服微信

  • 服务号