Fatigue analysis of 7075-T6 aluminum alloy under high compressive residual stresses by considering the non-propagating crack region
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DOI: 10.1177/14644207221092375
Abstract: This article is a numerical investigation to determine the fatigue life of cold expanded fastener holes in 7075-T6 aluminum alloy. To estimate the numerical fatigue life, a combination of initiation and propagation lives was used.… read more here.
Keywords: crack; crack region; 7075 aluminum; non propagating ... See more keywords