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Elastic-plastic finite element analysis of the effect of compressive loading on crack tip parameters and its impact on fatigue crack propagation rate

机译:压缩载荷对裂纹尖端参数的影响及其对疲劳裂纹扩展速率的影响的弹塑性有限元分析

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摘要

The effects of applied compressive stress on the crack tip parameters and their implications on fatigue crack growth have been studied. Four center-cracked panel specimens with different crack lengths are analysed using finite element method. The results show that under tension-compression loading the local crack tip parameters are determined by two loading parameters. The two loading parameters are the maximum stress intensity and the maximum compressive stress in the applied stress cycle. Predictions of fatigue crack propagation behaviour based on the maximum stress intensity and maximum compressive stress agree well with experimental observations.
机译:研究了施加压缩应力对裂纹尖端参数的影响及其对疲劳裂纹扩展的影响。使用有限元方法分析了四个裂纹长度不同的中心裂纹面板试样。结果表明,在拉压载荷作用下,局部裂纹尖端参数由两个载荷参数确定。两个加载参数是所施加应力循环中的最大应力强度和最大压缩应力。基于最大应力强度和最大压应力的疲劳裂纹扩展行为的预测与实验结果吻合良好。

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