首页> 外文期刊>Key Engineering Materials >Elastic-plastic Finite Element Analysis Of The Effect Of The Compressive Loading On Fatigue Crack Tip Parameters
【24h】

Elastic-plastic Finite Element Analysis Of The Effect Of The Compressive Loading On Fatigue Crack Tip Parameters

机译:压缩载荷对疲劳裂纹尖端参数影响的弹塑性有限元分析

获取原文
获取原文并翻译 | 示例
           

摘要

In this paper, a detailed elastic-plastic finite element analysis of the effect of the compressive loading on crack tip plasticity is studied based on the material's kinematic hardening model. Five centre-cracked panel specimens with different crack lengths are analyzed. The analysis shows that in a tension-compression loading the maximum spread of the crack tip reverse plastic zone increases with the increase of the compressive stress and the near crack tip opening displacement decreases with the increase of the compressive stress at the same nominal stress intensity factor. The applied compressive stress is the main factor controlling the near crack tip parameters.
机译:本文基于材料的运动硬化模型,对压缩载荷对裂纹尖端塑性的影响进行了详细的弹塑性有限元分析。分析了五个裂纹长度不同的中裂面板样本。分析表明,在相同的名义应力强度因子下,在拉压载荷下,裂纹尖端反向塑性区的最大展宽随压应力的增加而增大,近裂纹尖端开口位移随压应力的增大而减小。 。施加的压应力是控制近裂纹尖端参数的主要因素。

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