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A Comparison of Measurement Methods and Numerical Procedures for the Experimental Characterization of Fatigue Crack Closure

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The article was published on 1988-01-01. It has received 62 citations till now. The article focuses on the topics: Crack closure & Paris' law.

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Journal ArticleDOI

Finite element analysis of plasticity-induced fatigue crack closure: an overview

TL;DR: The state-of-the-art in finite element analysis for plasticity-induced fatigue crack closure can be found in this article, where a comprehensive overview is presented, summarizing issues which must be considered and emphasizing potential difficulties.
Journal ArticleDOI

Evaluation of overload effects on fatigue crack growth and closure

TL;DR: In this article, Fatigue crack propagation tests with single tensile peak overloads have been performed in 6082-T6 aluminium alloy at several baseline Δ K levels and stress ratios of 0.05 and 0.25.
Journal ArticleDOI

Assessment of the fatigue crack closure phenomenon in damage-tolerant aluminium alloy by in-situ high-resolution synchrotron X-ray microtomography

TL;DR: In this paper, a high-resolution experimental configuration and phase contrast imaging technique have enabled the reconstruction of crack images with an isotropic voxel with a 0.7 µm edge.
Journal ArticleDOI

Investigation of fatigue crack closure using multiscale image correlation experiments

TL;DR: In this paper, two full-field macro-scale methods are introduced for estimating fatigue crack opening levels based on digital image correlation (DIC) displacement measurements near the crack tip, and the results of these experiments point to a normalized crack tip opening level of 0.35 for R Â∼ 0 loading in grade 2 titanium.
Journal ArticleDOI

Influence of grain structure and slip planarity on fatigue crack growth in low alloying artificially aged 2xxx aluminium alloys

TL;DR: In this paper, the relationship between the crack path and the microstructure, i.e. grain structure and slip planarity, is assessed semi-quantitatively and a criterion to evaluate the propensity for slip band formation is derived and reasonable correlation is found between the fatigue fracture behaviour of the three alloys and this criterion.
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