首页> 外文期刊>Key Engineering Materials >Numerical Studies of End Effect on Crack Propagation Behavior of Brittle Specimen Containing Pre-existing Crack under Uniaxial Compression
【24h】

Numerical Studies of End Effect on Crack Propagation Behavior of Brittle Specimen Containing Pre-existing Crack under Uniaxial Compression

机译:含裂纹的脆性试样单轴压缩下端部对裂纹扩展行为的数值研究

获取原文
获取原文并翻译 | 示例
       

摘要

In this paper, a Material Failure Process Analysis code (MFPA~(2D)) was employed to investigate the interaction of end effect zone of specimen with the wing crack propagation inside the brittle specimen containing pre-existing flaws under uniaxial compression comparing with the experimental results. The numerical results show that the shorter the distance between the pre-existing flaw and the specimen's end , the slower the crack propagation process and the shorter wing propagation length is , and vice versa. In addition, the end effect zone was also influenced by the wing crack propagation.
机译:本文使用材料破坏过程分析代码(MFPA〜(2D))来研究试样的端部效应区与单轴压缩下含预先存在缺陷的脆性试样内部的机翼裂纹扩展之间的相互作用,并与实验进行了对比。结果。数值结果表明,预先存在的裂纹与试样末端之间的距离越短,裂纹扩展过程越慢,机翼的扩展长度越短,反之亦然。此外,末端效应区也受到机翼裂纹扩展的影响。

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