首页> 外文会议>International Conference on Manufacturing Science and Engineering >A simplified method study of aluminium alloy fatigue crack tip parameters computed by elastic-plastic finite element model
【24h】

A simplified method study of aluminium alloy fatigue crack tip parameters computed by elastic-plastic finite element model

机译:弹塑性有限元模型计算铝合金疲劳裂纹尖端参数的简化方法研究

获取原文

摘要

Fatigue crack propagation of aluminium alloy 7049-OA has been studied by non-linear finite element business-oriented software ABAQUS, and elastic-plastic finite element models of static fatigue crack and dynamic fatigue crack of center crack panel (CCP) specimens are also built. Based on the finite element computation results, the differences of stress and crack opening displacement around crack tip of static crack model have been compared with those of dynamic crack model. The compared results showed that the finite element computation results of dynamic crack model can be replaced by the results calculated by the static crack model. Fatigue crack tip parameters of aluminium alloy CCP specimens can be calculated by elastic-plastic finite element model of static crack. This is an effective method to cut down the computation expense and promote the computational efficiency.
机译:通过非线性有限元企业的软件ABAQUS研究了铝合金7049-OA的疲劳裂纹传播,并建成了中心裂纹板(CCP)标本的静态疲劳裂纹和动态疲劳裂缝的弹塑性有限元模型。基于有限元计算结果,与动态裂纹模型的静态裂纹模型的裂纹尖端应力和裂纹开口位移的差异。比较结果表明,动态裂纹模型的有限元计算结果可以通过静态裂纹模型计算的结果代替。铝合金CCP样品的疲劳裂纹尖端参数可以通过静态裂纹的弹性塑料有限元模型来计算。这是减少计算费用并促进计算效率的有效方法。

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