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广布损伤裂纹间干涉效应及数值分析
引用本文:谭申刚.广布损伤裂纹间干涉效应及数值分析[J].科学技术与工程,2010,10(7).
作者姓名:谭申刚
作者单位:1. 北京航空航天大学,北京,100083
2. 中航第一飞机设计研究院,西安,710072
摘    要:进行了三种开裂模式无钉载平板的广布损伤裂纹扩展试验,研究发现裂纹间的干涉作用明显促进了裂纹的扩展,多裂纹情况下的裂纹扩展速率远大于单裂纹。同时,利用FRANC2D/L计算和分析了单裂纹、多孔相邻裂纹、多孔不相邻裂纹和多孔等长裂纹等四种开裂模式的裂纹扩展行为及应力强度因子分布。结果表明,裂纹扩展初始阶段主要受孔自身应力集中影响,裂纹间的干涉作用弱;随着裂纹扩展到一定长度时,裂纹间的干涉作用显著增大,且随着裂纹间韧带长度的减小而快速增加,与试验结果一致。

关 键 词:广布损伤  应力强度因子  裂纹干涉  有限元  
收稿时间:12/4/2009 5:57:03 PM
修稿时间:2009/12/11 0:00:00

Test and Numerical Simulation on Crack Interaction of Multiple Site Damage
Tan Shengang.Test and Numerical Simulation on Crack Interaction of Multiple Site Damage[J].Science Technology and Engineering,2010,10(7).
Authors:Tan Shengang
Institution:Beijing University of Aeronautics and Astronautics/a>;Beijing 100083/a>;P.R.China/a>;The First Aircraft Design Institute/a>;AVIC1/a>;Xi'an 710089/a>;P.R.China
Abstract:Panels with three kinds of cracking model were tested under cyclic loads to study the propagation of multiple cracks.The results showed that crack interaction could speed up the expansion of cracks significantly and the crack growth rate of multiple cracks was much faster than that of single crack.Four finite element cracking models,including single crack,adjacent cracks of multiple holes,non-adjacent cracks of multiple holes,equal-length cracks of multiple holes,were built by FRANC2D/L to study the growth ...
Keywords:multiple site damage stress intensity factor crack interaction finite element  
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