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Experimental investigation and finite element analysis of fatigue crack growth in pipes containing a circumferential semi-elliptical crack subjected to bending

机译:包含半圆形椭圆形裂纹的弯管疲劳裂纹扩展的实验研究和有限元分析

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In this paper, a circumferential external surface flaw in a metallic round pipe under cyclic bending loading is considered. Because of very rapid changes in the geometrical parameters around the crack front region, the mesh generation of this region must be done with great care. This may lead to an increase in the run time which makes it difficult to reach valid results and conclusions. Because of the advantages of the sub-modeling technique in problems which need very high mesh density, this method is used. Stress intensity factors in mode I condition are determined using three-dimensional finite element modeling with 20 node iso-parametric brick elements in the ANSYS 9. 0 standard code and the singular form of these finite elements at the crack front. In order to estimate the analysis error, the structural parameter error in energy norm criterion was used. Because of the advantages of non-dimensional analysis, this method is employed, and the stress intensity factors are normalized. For the analysis of the fatigue crack growth, the Paris law is used. The propagation path of the surface flaw is obtained from the diagram of aspect ratio versus relative crack depth. The fatigue crack growth analysis (the relative crack depth against loading cycles diagram) of different initial crack aspect ratio under cyclic loading is also considered. Fatigue shape development of initially semi-elliptical external surface defects is illustrated. The effect of the Paris exponent (material constant) on fatigue crack propagation is shown as well. Moreover, the fatigue crack growth of several specimens is assessed experimentally using a manually-constructed experimental set up. Finally, the experimental results obtained by cyclic bending loading tests are compared with the numerical results. The experimental results show good conformity with the finite element results.
机译:在本文中,考虑了金属圆管在周期性弯曲载荷下的圆周外表面缺陷。由于裂纹前沿区域周围的几何参数变化非常快,因此必须非常小心地进行该区域的网格生成。这可能导致运行时间增加,从而难以获得有效的结果和结论。由于子建模技术在需要非常高的网格密度的问题中的优势,因此使用了此方法。使用三维有限元建模方法(在ANSYS 9中使用20个节点等参砖单元)来确定模式I条件下的应力强度因子。0标准代码以及这些有限元在裂纹前沿的单数形式。为了估计分析误差,使用了能量规范准则中的结构参数误差。由于无量纲分析的优势,因此采用了该方法,并对应力强度因子进行了归一化。为了分析疲劳裂纹扩展,使用了巴黎定律。表面缺陷的传播路径可从纵横比与相对裂纹深度的关系图中获得。还考虑了循环载荷下不同初始裂纹纵横比的疲劳裂纹扩展分析(相对裂纹深度与载荷循环的关系图)。示出了最初的半椭圆形外表面缺陷的疲劳形状发展。还显示了巴黎指数(材料常数)对疲劳裂纹扩展的影响。此外,使用手动构建的实验装置通过实验评估了多个试样的疲劳裂纹扩展。最后,将循环弯曲载荷试验获得的实验结果与数值结果进行了比较。实验结果与有限元结果吻合良好。

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