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Crack initiation and propagation from geometric microdefects: Experiment and transition fatigue behavior

机译:几何微碎裂的裂纹启动和传播:实验和过渡疲劳行为

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The present work aims to study short fatigue crack initiation and propagation induced by geometric microdefects. An empirical approach is used to evaluate the microstructural influences on crack growth behavior. Small fatigue crack test on titanium alloy Ti-6Al-4V is performed to investigate the crack induced from a geometric microdefect. Analyses on crack initiation and fracture are respectively performed to study the microstructural influences on the stages of initiation and fracture. Subsequently, an empirical multiscale model is employed to predict the short fatigue crack propagation of alloys underlining the transition features. Grain size variation is adopted to reflect the main microstructural contribution to the short crack propagation. An alpha factor is defined to demonstrate the transition interim from microstructurally short crack to physically short crack stages. Furthermore, a relationship between transition factor and grain size is correlated. The results indicate that the value of transition factor tends to decrease with the augment of average grain size. The empirical approach is validated through a variety of fatigue experimental data of alloys including Ti-6Al-4V, 2024-T3, and GH4169.
机译:目前的工作旨在研究几何微碎片诱导的短疲劳裂纹启动和传播。经验方法用于评估裂纹生长行为的微观结构影响。进行钛合金Ti-6AL-4V的小疲劳裂纹试验,以研究几何微炼制的裂缝。分析分析裂缝引发和骨折的分析,以研究对引发和裂缝阶段的微观结构影响。随后,采用经验多尺度模型来预测下划到过渡特征的合金的短疲劳裂纹繁殖。采用晶粒尺寸变化来反映对短裂纹繁殖的主要微观结构贡献。定义α因子以证明从微观结构短裂纹到物理短裂纹阶段的过渡临时。此外,过渡因子与晶粒尺寸之间的关系是相关的。结果表明,随着平均晶粒尺寸的增强,过渡因子的值趋于降低。通过包括Ti-6Al-4V,2024-T3和GH4169的各种疲劳实验数据,通过各种疲劳实验数据验证了经验方法。

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