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Simulation and Experimental Analysis of Fatigue Crack Growth under Cyclic Loading

机译:循环载荷下疲劳裂纹增长的仿真与实验分析

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The problem of crack growth is a major issue in the prediction and maintenance of engineering structural elements. Prediction of expected life of a structural element due to constant (static) and alternating loading (fatigue) is of major concern to the designers. Prediction of remaining life of the structural elements influences the decisions of maintenance engineers (checking intervals, corrections, and replacements).The fatigue crack growth rate, which determine the fatigue life of the components after crack initiation need to be experimentally and theoretically investigated. In this study, fatigue crack growth tests were conducted under constant amplitude loading at a stress ratio of 0.1, using three-point bend (TPB) specimens of ASTM A533 steel material. For the simulation part of this study, three fatigue crack growth models, i.e. the Paris, modified Forman and Austen were examined. None of the models has a fit for the fatigue crack growth rate data in a similar behaviour compared to others. The modified Forman model provided a closer fit than the Paris model with respect to the experimental results. However, the Austen model provided the best fit to the fatigue crack growth rate data as compared with the other two models. Therefore, this model is suggested for use in critical applications.
机译:裂缝增长的问题是工程结构元素预测和维护的主要问题。由于恒定(静态)和交替的负载(疲劳)预测结构元素的预期寿命是设计人员的主要问题。结构元素剩余寿命的预测影响了维护工程师的决定(检查间隔,校正和替代品)。疲劳裂纹生长速率,确定在裂纹启动后确定组分的疲劳寿命需要实验和理论上研究。在该研究中,使用ASTM A533钢材的三点弯曲(TPB)试样为0.1的应力比在恒定幅度负载下进行疲劳裂纹生长试验。对于本研究的模拟部分,研究了三种疲劳裂纹生长模型,即巴黎,改性式甲型和奥氏体。与他人相比,没有任何模型对疲劳裂纹扩展速率数据具有相应的疲劳裂纹扩展速率数据。修改的形式模型提供比实验结果更近于巴黎模型的配合。然而,与其他两个模型相比,AUSTEN模型提供了最适合疲劳裂纹扩展速率数据。因此,该模型被建议用于关键应用。

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