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Analysis of interacting semi-elliptical surface cracks in finite thickness plates under remote bending load

机译:有限弯曲作用下有限厚度板相互作用的半椭圆形表面裂纹分析

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Interaction effects of two coplanar self-same shallow and deep semi-elliptical surface cracks in finite thickness plates subjected to remote tension have been previously investigated by Sethuraman et al. Using the finite element based force method. In the present study, the effect of remote bending load on interacting semi-elliptical surface cracks in a finite thickness plate is analyzed. Stress intensity factors are evaluated along the entire crack front using a modified force method based on the three-dimensional finite element solution. The line spring model has also been used to evaluate stress intensity factors at the deepest point of a crack using shell finite element analysis. Parametric studies involving a wide ranges of geometric dimensions and crack configurations viz. crack shape aspect ratio (0.2 < = ale < = 1.0), crack depth ratio (0.2 < = alt < = 0.9), relative crack location (0.2 < =2c/d< =0.9) and normalized location on the crack front (0< =2 phi /pi < =2) are earned out for numerical estimation of crack interaction factors. Due to the crack interaction, the stress intensity factor distribution is observed to be asymmetric along the crack front. The interaction is also observed to cease when the distance between two cracks is more than five times the crack width (i.e. 2c/d less than 0.2) irrespective of crack shape aspect ratio. Finally, an empirical relation is proposed for the evaluation of crack interaction crack interaction factors for the range of parameters considered. For the ranges considered, the proposed empirical relation predicts the crack interaction factors at the inner and outer surface points of the crack within + 4 percent of the three-dimensional finite element solutions.
机译:Sethuraman等人先前已经研究了在有限厚度板上受远程拉力作用的两个共面自同一浅深深半椭圆形表面裂纹的相互作用。使用基于有限元的力法。在当前的研究中,分析了有限厚度板中远处弯曲载荷对相互作用的半椭圆形表面裂纹的影响。使用基于三维有限元解的修正力方法,沿着整个裂纹前沿评估应力强度因子。线弹簧模型也已用于通过壳有限元分析来评估裂纹最深处的应力强度因子。涉及范围广泛的几何尺寸和裂纹配置的参数研究。裂纹形状纵横比(0.2 <= ale <= 1.0),裂纹深度比(0.2 <= alt <= 0.9),相对裂纹位置(0.2 <= 2c / d <= 0.9)和裂纹前沿的归一化位置(0裂纹相互作用因子的数值估算得出<= 2 phi / pi <= 2)。由于裂纹相互作用,应力强度因子分布沿裂纹前沿是不对称的。当两个裂纹之间的距离大于裂纹宽度的五倍(即2c / d小于0.2)时,也观察到相互作用停止,而与裂纹形状的纵横比无关。最后,提出了一种经验关系式,用于在考虑的参数范围内评估裂纹相互作用。对于所考虑的范围,建议的经验关系式预测裂纹的内外表面点处的裂纹相互作用因子在三维有限元解的+ 4%之内。

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