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A new method for analysis of part-elliptical surface cracks in structures subjected to fatigue loading

机译:疲劳载荷结构中结构部分椭圆表面裂缝的一种新方法

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This paper presents a new analytical method for the analysis of fatigue growth of surface cracks in various structural components. The method is based on a governing equation describing the front evolution of surface cracks of elliptical and part-elliptical shapes. This method avoids the need for various numerical schemes for the calculation of the incremental crack front advance, which were used in all previous studies. Plasticity-induced crack closure models can also be incorporated into the method or these models can be deducted from a correlation of experimental data and the method predictions. When the plastic constraint conditions change significantly along the crack front, the implementation of the plasticity induced crack closure models can significantly improve the accuracy of fatigue life predictions. The method is validated against previous theoretical and experimental studies.
机译:本文介绍了一种新的分析方法,用于分析各种结构部件中表面裂纹的疲劳生长。 该方法基于用于描述椭圆形和部分椭圆形状的表面裂缝的前进展的控制方程。 该方法避免了需要计算在所有先前研究中使用的增量裂缝前进前进的各种数值方案。 塑性诱导的裂纹闭合模型也可以纳入该方法,或者可以从实验数据的相关和方法预测中扣除这些模型。 当塑料约束条件沿裂缝前沿发生显着变化时,可塑性诱导的裂纹闭合模型的实施可以显着提高疲劳寿命预测的准确性。 该方法针对以前的理论和实验研究验证。

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