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Experimental Study of the Crossing-Double-Crack Propagation in Q345R Plate

机译:Q345R板横穿双裂纹繁殖的实验研究

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In this paper, crossing-double-crack fatigue propagation in carbon steel Q345R was tested to investigate the mutual influence between cracks. The two notch-cracks have different lengths and are crossed in different angles. Finite element method was employed to calculate the stress intensity factors at crack tips. It is found that for the crossing-double-crack configuration, new cracks were firstly initiated from the notch-crack tips with the bigger stress intensity factors and then propagated along the paths perpendicular to the applied load. When two new cracks propagate, the other notch-cracks or initiated cracks are shielded without growing. The non-propagated notch-cracks have no obvious effects on the two propagated cracks in terms of the crack growth paths and the crack growth rates. But the two propagated cracks may change the loading state of the non-propagated notch-cracks. The relationships between fatigue crack propagation rates of both single cracks and crossing-double-cracks and the amplitude ranges of the mode I stress intensity factors AK i follow the Paris formula without clear difference.
机译:在本文中,测试了碳钢中的交叉双裂纹疲劳繁殖Q345R以研究裂缝之间的相互影响。两个凹口裂缝具有不同的长度,并以不同的角度交叉。采用有限元法计算裂纹尖端的应力强度因子。结果发现,对于交叉双裂纹配置,首先从凹口裂纹尖端开始具有更大的应力强度因子,然后沿着垂直于施加的载荷的路径传播的新裂缝。当两个新的裂缝繁殖时,其他凹口裂缝或引发的裂缝都被屏蔽而不会生长。在裂纹生长路径和裂纹生长速率方面,非繁殖的凹口裂缝对两个繁殖的裂缝没有明显影响。但是两个传播的裂缝可以改变非传播的凹口裂缝的加载状态。单个裂缝和交叉双裂纹的疲劳裂纹传播速率与模型I应力强度因子Ak的幅度范围之间的关系Ak I遵循巴黎公式而不清楚差异。

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