首页> 外文期刊>Journal of Composite Materials >A stress-relaxation approach to determine onset of delamination in angle ply laminates
【24h】

A stress-relaxation approach to determine onset of delamination in angle ply laminates

机译:一种应力松弛方法,以确定角度层层叠成分的发生

获取原文
获取原文并翻译 | 示例
       

摘要

A new test method, named multi-relaxation test, is proposed for detecting on-set of delamination in fibre-reinforced polymers. Multi-relaxation test is based on the principle that uses change of stress relaxation behaviour of fibre-reinforced polymer to detect the occurrence of delamination. In this study, angle-ply laminated fibre-reinforced polymer (APL-FRP) is used to demonstrate and evaluate multi-relaxation test for detection of the delamination occurrence. The stress relaxation behaviour is characterized using a standard, three-element viscoelastic model in which the Eyring's law is used to govern the time-dependent stress response to deformation. Results suggest a high possibility of using the trend line change of viscous stress at the beginning of stress relaxation to determine the critical stroke for the onset of delamination. The results also suggest that value for the corresponding static stress is very close to the value reported in the literature for APL-FRP of the same fibre lay-up. The major advantage of multi-relaxation test over other tests for the same purpose is that multi-relaxation test is able to detect delamination without relying on ancillary information such as acoustic signals. Therefore, multi-relaxation test can be used to characterize critical loading and deformation in fibre-reinforced polymer structures of any size and geometry, even when subjected to a loading mode that mimics the in-service loading.
机译:提出了一种新的测试方法,称为多放松试验,用于检测纤维增强聚合物中的分层的一组。多松弛测试基于使用纤维增强聚合物的应力松弛行为变化来检测分层的原理。在该研究中,角度层层叠纤维增强聚合物(APL-FRP)用于证明和评估多松弛测试以检测分层发生。应力松弛行为使用标准的三元素粘弹性模型,其中眼镜的定律用于控制变形的时间依赖应力反应。结果表明,在应力松弛开始时使用粘性应力的趋势线变化的高可能性,以确定分层发作的临界行程。结果还表明,相应的静态应力的值非常接近与相同光纤叠层的APL-FRP中的文献中报告的值非常接近。多放松测试对其他测试的多放松测试的主要优点是多松弛测试能够检测分层而不依赖于诸如声学信号的辅助信息。因此,即使当经受用于模拟在役负载的加载模式时,也可以使用多松弛测试在任何尺寸和几何形状的纤维增强聚合物结构中表征临界负载和变形。

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