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A MICROSTRUCTURE-BASED FATIGUE CRACK INITIATION MODEL FOR STRUCTURAL ALLOYS

机译:结构合金的基于微结构的疲劳裂纹引发模型

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The development of a microstructure-based fatigue crack initiation model that includes explicit crack size and microstructure-scale parameters is presented in this paper. In particular, Tanaka and Mura's model [1, 2] for crack initiation at slipbands has been extended to include crack size and relevant microstructural parameters in the response equations. The microstructure-based model is applied to predicting the crack size at initiation, small crack behavior, and notch fatigue in Ti-6Al-4V. The calculated results are compared against experimental data from the literature to assess the range of predictability and accuracy of the fatigue crack initiation model.
机译:本文介绍了包括显式裂缝尺寸和微观结构级参数的基于微观结构的疲劳裂纹启动模型。特别地,Tanaka和Mura的型号[1,2]在滑移带上的裂纹启动已经扩展到包括响应方程中的裂缝尺寸和相关的微观结构参数。基于微观结构的模型用于预测Ti-6Al-4V中的起始,小裂缝行为和Notch疲劳时的裂纹尺寸。将计算结果与来自文献的实验数据进行比较,以评估疲劳裂纹引发模型的可预测性和准确性的范围。

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