...
首页> 外文期刊>Fatigue & Fracture of Engineering Materials & Structures >Mixed mode fatigue and fracture in planar geometries: Observations on K_(eq) and crack path modelling
【24h】

Mixed mode fatigue and fracture in planar geometries: Observations on K_(eq) and crack path modelling

机译:平面几何中的混合模式疲劳和断裂:K_(eq)和裂纹路径建模的观察

获取原文
获取原文并翻译 | 示例
   

获取外文期刊封面封底 >>

       

摘要

The mixed mode I-II fatigue and fracture is briefly reviewed, addressing experimental and numerical modelling aspects, and focusing on planar specimens. One major challenge concerns the determination of equivalent stress intensity factor (K-eq) in mixed mode situations. Several approaches were compared through the determination of K-eq/K-I over a wide range of values of K-I/K-II or K-II/K-I. Whereas all different approaches converge to the same value as K-I/K-II increases, the same does not happen for large K-II/K-I, where differences between values of K-eq persist. In the regions of 0 K-I/K-II K-II/K-I < 2, no stable trend of results can be defined. Experimental fatigue crack growth results are presented for Al alloy AA6082-T6. Compact tension specimens, modified with holes, and four-point bending specimens under asymmetrical loading promoting mixed mode situations, were subjected to fatigue crack growth tests, where crack path and crack growth rate were measured. The presentation of the fatigue crack growth data was made using a Paris law based upon K-eq. Differences in the Paris law constants were found for the different K-eq criteria. Recent developments in numerical techniques, as the implementation of the extended finite element method (XFEM) in finite element software packages allows to determine accurately crack paths in mixed mode fracture. This article highlights concepts for mixed-mode fatigue and fracture and supporting data, identifying challenges still to be overcome.
机译:简要回顾了混合模式I-II的疲劳和断裂,解决了实验和数值建模方面的问题,并重点研究了平面试样。一个主要挑战涉及在混合模式下确定等效应力强度因子(K-eq)。通过在很大范围的K-I / K-II或K-II / K-I值中确定K-eq / K-I,比较了几种方法。尽管随着K-I / K-II的增加,所有不同的方法都收敛到相同的值,但是对于大型K-II / K-I,K-eq值之间的差异仍然存在,这不会发生相同的情况。在0 K-I / K-II K-II / K-I <2的区域中,无法确定稳定的结果趋势。给出了铝合金AA6082-T6的实验疲劳裂纹扩展结果。对致密的拉伸试样(经孔修饰)和在非对称载荷下促进混合模式的四点弯曲试样进行疲劳裂纹扩展测试,测量其裂纹路径和裂纹扩展速率。疲劳裂纹扩展数据的表示使用了基于Keq的巴黎定律。对于不同的K-eq标准,发现巴黎法律常数存在差异。数值技术的最新发展,是由于在有限元软件包中实施了扩展有限元方法(XFEM),因此可以准确确定混合模式裂缝中的裂纹路径。本文重点介绍了混合模式疲劳和断裂以及支持数据的概念,指出了仍需克服的挑战。

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