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Fatigue Crack Growth Life Prediction for Surface Crack Located in Stress Concentration Part Based on the Three-Dimensional Finite Element Method

机译:基于三维有限元法的应力集中部位表面裂纹疲劳裂纹扩展寿命预测

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摘要

Fatigue crack growth prediction methods using three-dimensional finite element analyses were investigated to improve the predictability of part-through surface crack growth life. First, a direct analysis method of cyclic finite element analysis was adopted. Fatigue crack growth was predicted on a step by step basis from the Paris' law using stress intensity factor range (ΔK) calculated by the three-dimensional finite element method. This method takes the procedure of cyclic operation of finite element analysis modeled with crack tip elements, crack growth increment calculation and remeshing of the finite element model. Second, a method based on the influence function method for the ΔK calculation directly using three-dimensional finite element method analysis result has been developed and applied. It was found that crack growth prediction based on the step by step finite element method and the method based on the influence function method showed good correlation with the experimental results if Paris' law coefficient C, determined by CT specimen, was appropriately used for a semi-elliptical surface crack.
机译:研究了使用三维有限元分析的疲劳裂纹扩展预测方法,以提高部分贯通表面裂纹扩展寿命的可预测性。首先,采用了循环有限元分析的直接分析方法。疲劳裂纹的扩展是根据巴黎定律,使用三维有限元方法计算出的应力强度因子范围(ΔK),逐步进行预测的。该方法采用以裂纹尖端单元为模型的有限元分析的循环操作,裂纹扩展增量的计算和有限元模型的重新网格化的过程。其次,已经开发并应用了一种基于影响函数法的直接使用三维有限元分析结果进行ΔK计算的方法。结果发现,如果将CT试样确定的巴黎定律系数C适当地用于半成品,则基于逐步有限元法和基于影响函数法的裂纹扩展预测与实验结果具有良好的相关性。 -椭圆形表面裂纹。

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