Crack tip strain evolution and crack closure during overload of a growing fatigue crack

De-Qiang Wang, Mingliang Zhu, F. Xuan
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引用次数: 12

Abstract

It is generally accepted that fatigue crack growth is retarded after an overload, which has been explained either by plasticity-induced crack closure or near-tip residual stress. However, any interpretation of overload effect is insufficient if strain evolution in front of crack tip is not properly considered. The current understanding of overload-induced retardation lacks the clarification of the relationship between crack closure at crack wake and strain evolution at crack tip. In this work, a material with low work hardening coefficient was used to study the effect of overload on crack tip strain evolution and crack closure by in-situ SEM observation and digital image correlation technique. Crack opening displacement (COD) and crack tip strain were measured before and after the overload. It was observed that the evolution of crack tip strain follows the crack opening behaviour behind the crack tip, indicating a smaller influence of overload on micro-mechanical behaviour of fatigue crack growth. After the overload, plastic strain accumulation was responsible for crack growth. The strain at a certain distance to crack tip was mapped, and it was found that the crack tip plastic zone size correlated well with crack growth rate during post-overload fatigue crack propagation.
扩展疲劳裂纹过载时裂纹尖端应变演化与裂纹闭合
人们普遍认为超载后疲劳裂纹的扩展被延缓,这可以用塑性裂纹闭合或近尖端残余应力来解释。然而,如果不考虑裂纹尖端前的应变演化,任何对过载效应的解释都是不够的。目前对过载迟滞的理解缺乏对裂纹尾迹闭合与裂纹尖端应变演化关系的澄清。本文采用低加工硬化系数材料,通过原位扫描电镜观察和数字图像相关技术,研究了过载对裂纹尖端应变演化和裂纹闭合的影响。测量了过载前后的裂纹张开位移(COD)和裂纹尖端应变。裂纹尖端应变的演化遵循裂纹尖端后的裂纹张开行为,表明过载对疲劳裂纹扩展微观力学行为的影响较小。超载后,塑性应变积累是裂纹扩展的主要原因。对裂纹尖端一定距离处的应变进行了映射,发现裂纹尖端塑性区尺寸与过载后疲劳裂纹扩展速率具有良好的相关性。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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