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Stress intensity factors for surface fatigue crack in a round bar under cyclic axial loading

机译:循环轴向载荷作用下圆棒表面疲劳裂纹的应力强度因子

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In this paper, the surface fatigue crack growth shape for an initial straight-fronted edge crack in an elastic bar of circular cross-section is determined through experiments under pure fatigue axial loading. Three different initial notch depths are discussed. The relations of the aspect ratio (b/c) and relative crack depth (b/D) are obtained, and it is shown that there is a great difference in the growth of cracks with different initial front shapes and crack depths. Further, using the three-dimensional finite element method, the stress intensity factors (SIFs) are determined under remote uniform tension loading. Since the relationship of b/c and b/D changes during the fatigue crack growth, the SIFs are determined for different surface crack configurations.
机译:在本文中,通过在纯疲劳轴向载荷下的实验确定了圆形截面弹性杆中初始直边边缘裂纹的表面疲劳裂纹扩展形状。讨论了三种不同的初始切口深度。得到了长宽比(b / c)和相对裂纹深度(b / D)的关系,结果表明,具有不同初始锋面形状和裂纹深度的裂纹扩展存在很大差异。此外,使用三维有限元方法,在远距离均匀张力载荷下确定应力强度因子(SIF)。由于在疲劳裂纹扩展期间b / c和b / D的关系发生了变化,因此针对不同的表面裂纹配置确定了SIF。

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