首页> 外文会议>International conference on composite materials (ICCM-14) >TIME-TEMPERATURE DEPENDENT FLEXURAL FATIGUEBEHAVIOR OF HONEYCOMB SANDWICH COMPOSITES
【24h】

TIME-TEMPERATURE DEPENDENT FLEXURAL FATIGUEBEHAVIOR OF HONEYCOMB SANDWICH COMPOSITES

机译:蜂窝夹芯复合材料随时间的弯曲挠曲行为

获取原文

摘要

The three-point bending tests on constant strain rate(CSR) and fatigue loading undervarious strain rates and temperatures were carried out for honeycomb cored sandwich(SW) panel withGFRP surface sheets and Nomex honeycomb core. The maximum bending moments by CSR andfatigue loadings strongly depend on time and temperature and the time-temperature superpositionprinciple for the storage modulus of matrix resin holds for the maximum bending moments by fatigueloading as well as CSR loading. Based on these results, the master curves of the bending moment byfatigue loading can be constructed and the long term fatigue life can be predicted using these mastercurves.
机译:采用GFRP蜂窝板和Nomex蜂窝芯对蜂窝芯夹芯板进行了三点弯曲试验,研究了不同应变速率和温度下的恒定应变率(CSR)和疲劳载荷。 CSR和疲劳载荷引起的最大弯矩在很大程度上取决于时间和温度,而基体树脂的储能模量的时间-温度叠加原理在疲劳载荷和CSR载荷下保持最大弯矩。基于这些结果,可以构造由疲劳载荷引起的弯矩的主曲线,并可以使用这些主曲线来预测长期疲劳寿命。

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