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Fatigue growth models for multiple long cracks in plates under cyclic tension based on △K_I, △J-integral and ACTOD parameter

机译:基于△K_I,△J积分和ACTOD参数的循环拉伸下板中多个长裂纹的疲劳增长模型

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This paper presents the implementation of fatigue crack growth power law equations based on △K, △J-integral and ACTOD fracture mechanics parameters determined in an FE analysis, to plates with multiple site damage (MSD). Results of fatigue tests with constant amplitude tensile loading carried out on mild steel plate specimens damaged with a single central crack and with three collinear cracks are presented. A relatively larger plastic zone occurred in the crack tip region at higher fatigue crack growth rate (FCGR), from 10~(-7) to 10~(-6) m/cycle. The crack growth models based on the elastic-plastic fracture mechanics (EPFM) parameters describe better fatigue crack growth in this range as compared to the liner elastic models.
机译:本文介绍了基于有限元分析中确定的△K,△J积分和ACTOD断裂力学参数的疲劳裂纹扩展幂律方程到多点损伤(MSD)板的实现。给出了在具有单个中心裂纹和三个共线裂纹的低碳钢板试样上进行的等幅拉伸载荷疲劳试验的结果。在较高的疲劳裂纹扩展速率(FCGR)下,裂纹尖端区域出现了相对较大的塑性区,范围从10〜(-7)到10〜(-6)m /周期。与衬里弹性模型相比,基于弹塑性断裂力学(EPFM)参数的裂纹扩展模型在此范围内描述了更好的疲劳裂纹扩展。

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