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A Software Tool for the Fatigue Growth Analysis of Multiple 3D Cracks from Fastener Holes

机译:一种软件工具,用于紧固件孔的多个3D裂缝的疲劳生长分析

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A software tool is developed to carry on automatic fatigue crack propagation analysis for the multiple three-dimensional (3D) cracks initiated from fastener holes. It is a computer code package being capable of handling the cases of multiple 3D cracks with quadratic curve fronts. The object-oriented programming language is used to develop user interfaces for the input of the initial data and output of the simulation results. To achieve life-span numerical simulation for the multiple 3D crack growth, ANSYS Parametric Design Language is used to create finite element model, conduct the stress analysis and regenerate finite element mesh for new crack configurations. Stress intensity factors of the cracks are determined using the crack opening displacements and incorporated into crack propagation laws to estimate the crack extension. An algorithm for the fast integration of crack growth equations is adopted to predict the fatigue crack growth life. As examples, two scenarios of corner cracks initiated from countersunk fastener hole in 2324-T39 alloy sheets are analyzed throughout their fatigue growth lives. The simulation results correlate well with the experimental ones.
机译:的软件工具被显影以在自动疲劳裂纹扩展分析携带用于多个三维(3D)从紧固件孔发起裂纹。它是一种计算机代码包能够处理多个3D裂纹与二次曲线方面的情况下。面向对象的编程语言来开发用户界面的模拟结果的初始数据和输出的输入端。为了达到寿命数值模拟的多个3D裂纹生长,ANSYS参数设计语言被用来创建有限元模型,进行应力分析和再生有限元网格新裂缝配置。正在使用的裂缝开口的位移确定的,并纳入裂纹扩展法来估计裂缝扩展的裂纹的应力强度因子。用于快速整合裂纹生长方程的算法来预测疲劳裂纹扩展寿命。作为示例,在2324-T39合金薄片从埋头紧固件孔发起角部裂纹的两个方案在其整个疲劳生长的生命进行分析。仿真结果与实验结果很好的相关性。

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