【24h】

Fatigue damage evolution in structural materials above and below the fatigue limit

机译:疲劳极限以上和以下的结构材料中的疲劳损伤演变

获取原文
获取原文并翻译 | 示例

摘要

The evolution of fatigue damage in four different structural materials has been studied experimentally and the main stages of the damage and the relevant mechanisms were demonstrated.The cyclic hardening-softening curves,the cyclic stress-strain curves and the fatigue life curves for polycrystalline copper,316L steel,duplex steel and Al-Li alloys were reported.The changes of their internal structure,the evolution of the surface relief and the kinetics of early crack growth were studied at the same time.The most important mechanisms that represent physical realisation of the fatigue damage were exposed and their relative importance for the determination of the fatigue life was discussed.
机译:通过实验研究了四种不同结构材料的疲劳损伤演变过程,并阐明了损伤的主要阶段及相关机理。多晶铜的循环硬化-软化曲线,循环应力-应变曲线和疲劳寿命曲线报道了316L钢,双相钢和Al-Li合金。同时研究了它们的内部结构变化,表面起伏的演变以及早期裂纹扩展的动力学。暴露了疲劳损伤,并讨论了它们对于确定疲劳寿命的相对重要性。

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