首页> 外文会议>The Third International Symposium on Fretting Fatigue: Advances in Basic Understanding and Applications; May 15-18, 2001; Nagaoka, Japan >Stress Intensity Factors K_Ⅰ and K_Ⅱ of Oblique Through Thickness Cracks in a Semi-Infinite Body Under Fretting Fatigue Conditions
【24h】

Stress Intensity Factors K_Ⅰ and K_Ⅱ of Oblique Through Thickness Cracks in a Semi-Infinite Body Under Fretting Fatigue Conditions

机译:微动疲劳条件下半无限体倾斜贯通厚度裂缝的应力强度因子K_Ⅰ和K_Ⅱ。

获取原文
获取原文并翻译 | 示例

摘要

In this paper the formulas for calculating K_Ⅰ and K_Ⅱ of an oblique crack under fretting fatigue loading conditions have been derived. The scheme of the formulation is based on a method using Green's functions and the principle of superposition, i.e. the Green's functions have been obtained through boundary element analysis for normal and tangential localized forces on oblique crack faces and superimposed their results to calculate two components of mode Ⅰ and Ⅱ. The formulas for K_Ⅰ and K_Ⅱ were expressed as functions of crack angle, crack length and applied loading conditions, such as bulk fatigue stress, contact pressure distribution and friction stress distribution. A user-friendly program based on these formulas, then, has been developed to compute the values of stress intensity factors K_Ⅰ and K_Ⅱ under arbitrary fretting fatigue conditions. The values of stress intensity factors for both normal and oblique cracks have been illustrated as examples to understand the effects of crack angle and pad load distribution.
机译:推导了微动疲劳载荷条件下斜裂纹K_Ⅰ和K_Ⅱ的计算公式。该公式的方案基于使用格林函数和叠加原理的方法,即通过边界元分析获得了斜裂纹面上的法向和切向局部力的格林函数,并将它们的结果叠加起来以计算模态的两个分量Ⅰ和Ⅱ。 K_Ⅰ和K_Ⅱ的公式表示为裂纹角度,裂纹长度和所施加的载荷条件(如整体疲劳应力,接触压力分布和摩擦应力分布)的函数。然后,开发了基于这些公式的用户友好程序,以计算任意微动疲劳条件下的应力强度因子K_Ⅰ和K_Ⅱ的值。举例说明了正常裂纹和倾斜裂纹的应力强度因子值,以了解裂纹角度和垫载荷分布的影响。

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