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NUMERICAL SIMULATION OF A CORNER CRACK GROWTH IN METALS UNDER MULTIAXIAL FATIGUE LOADING

机译:多轴疲劳负载下金属裂纹裂纹增长的数值模拟

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Fatigue is reported as the major cause of engineering failure. Traditionally, experimental methods are employed to characterise the fatigue behaviour of a material. Nevertheless, due to its high cost and time-consuming, numerical analysis is introduced as an alternative approach to analyse fatigue crack growth accurately.In this study, a boundary element method is employed in order to simulate the crack growth in prismatic metallic bar under multiaxial fatigue loading. For this purpose, commercial boundary element method software BEASY is utilized. The generalized NASGRO equation and J-integral method is used to evaluate stress intensity factor. Cyclic torsion and bending loads are applied accordingly. Fatigue parameters studied in this work included crack aspect ratio and load ratio. Hence, analysis and prediction of crack size increment, stress intensity factors and fatigue life can be executed. It is demonstrated that corner crack on the prismatic bar tends to grow in the direction of the crack depth rather than the crack length under cyclic bending and torsion loadings despite of the initial crack size. As for the stress intensity factor distribution, the stress intensity factors are found to be higher at the position with the larger crack size, due to the stress concentration at the sharp tip of the end of the crack.
机译:疲劳被报告为工程失败的主要原因。传统上,使用实验方法表征材料的疲劳行为。然而,由于其高成本和耗时的耗费高,将数值分析作为准确分析疲劳裂纹增长的替代方法。在本研究中,采用边界元法来模拟多轴下棱镜金属条的裂纹生长疲劳载荷。为此目的,利用商业边界元素方法软件BEASY。广义NASGRO方程和J-Integral方法用于评估应力强度因子。相应地施加循环扭转和弯曲载荷。在该工作中研究的疲劳参数包括裂缝纵横比和负荷比。因此,可以执行分析和预测裂缝尺寸增量,应力强度因子和疲劳寿命。据证明,尽管初始裂纹尺寸,棱镜杆上的角裂缝倾向于在裂纹深度方向而不是循环弯曲和扭转载荷下的裂缝长度。对于应力强度因子分布,由于裂纹末端的尖锐尖端处的应力浓度,发现应力强度因子在具有较大裂缝尺寸的位置处更高。

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