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广布损伤裂纹扩展试验与数值模拟

Test and numerical simulation on crack propagation of multiple site damage

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【作者】 谭申刚刘朝君王锋王新波

【Author】 Tan Shengang1 Liu Zhaojun2 Wang Feng3 Wang Xinbo3(Beijing University of Aeronautics and Astronautics,100083,Beijing.China)1(Xi’an Jiaotong University,710049,Xi’an,China)2(The First Aircraft Design Institute,AVIC,710072,Xi’an,China)3

【机构】 北京航空航天大学西安交通大学中航第一飞机设计研究院

【摘要】 对三种开裂模式无钉载平板的广布损伤裂纹扩展试验进行了研究,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、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。

【Abstract】 Panels with three kinds of cracking model are tested under cyclic loads to study the propagation of multiple cracks.The results show that crack interaction can speed up the expansion of cracks significantlyand the crack growth rate of multiple cracks is much bigger 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,are built by FRANC2D/L to study the growth behaviour of multiple cracks and the distribution of stress intensity factors.The numerical simulation results indicate that at the initial stage of crack growth,cracks are mainly influenced by the stress concentration of holes and the interference effects between cracks are weak.When cracks extend to a certain length,the interference effects between cracks enlarge obviously and the effects increase rapidly as ligament lengths decreased,which are in agreement with the test results.

  • 【文献出处】 应用力学学报 ,Chinese Journal of Applied Mechanics , 编辑部邮箱 ,2010年02期
  • 【分类号】O346.1
  • 【被引频次】4
  • 【下载频次】207
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