首页 | 本学科首页   官方微博 | 高级检索  
     检索      

带裂纹三点弯曲试样的动态应力强度因子分析
引用本文:陈爱军,曹俊俊.带裂纹三点弯曲试样的动态应力强度因子分析[J].应用数学和力学,2011,32(2):194-201.
作者姓名:陈爱军  曹俊俊
作者单位:南京理工大学 理学院,南京 210094
基金项目:中国一航航空推进技术验证计划
摘    要:提出了计算带单边裂纹三点弯曲试样动态应力强度因子的新方法.首先由权函数的普遍形式和两种参考载荷下的应力强度因子,得到了带单边裂纹三点弯曲试样的权函数,然后考虑试样的转动惯性和剪切变形,根据振动理论推导出无裂纹梁内的动应力响应和分布,最后由权函数的思想推导出了带裂纹三点弯曲试样动态应力强度因子公式.通过有限元数值计算,验证了该方法的正确性,结果比较表明公式具有较高的精度.另外,还研究了冲击载荷下三点弯曲试样的动态应力强度因子随裂纹长度和加载速率的变化规律.

关 键 词:裂纹    动态应力强度因子    权函数法    三点弯曲试样    加载速率
收稿时间:2010-07-29

Analysis of Dynamic Stress Intensity Factors of Three-Point Bend Specimen Containing Crack
CHEN Ai-jun,CAO Jun-jun.Analysis of Dynamic Stress Intensity Factors of Three-Point Bend Specimen Containing Crack[J].Applied Mathematics and Mechanics,2011,32(2):194-201.
Authors:CHEN Ai-jun  CAO Jun-jun
Institution:School of Sciences, Nanjing University of Science and Technology, Nanjing 210094, P. R. China
Abstract:A new formula was produced to calculate dynamic stress intensity factors of three-point bend specimen containing a single edge crack. Firstly,the weight function for three-point bend specimen containing a single edge crack was derived from a general weight function form and two reference stress intensity factors. The coefficients of the weight function were given. Secondly,the history and distribution of dynamic stresses in unflawed three-point bend specimen which takes account of the effects of rotator inertia and shear deformation were inferred according to vibration theory. Finally,the dynamic stress intensity factor equations for three-point bend specimen with a single edge crack subjected to impact loadings were obtained by weight function method. The new formula was verified by the comparison with the numerical results of FEM(finite element method). Good agreement was achieved. And the law of dynamic stress intensity factors of three-point bend specimen under impact loadings changing with crack depths and loading rates was studied.
Keywords:
本文献已被 万方数据 等数据库收录!
点击此处可从《应用数学和力学》浏览原始摘要信息
点击此处可从《应用数学和力学》下载免费的PDF全文
设为首页 | 免责声明 | 关于勤云 | 加入收藏

Copyright©北京勤云科技发展有限公司  京ICP备09084417号