Abstract

Under cyclic fatigue load, multiple cracks would significantly deteriorate the service life of the components with respect to the case of a single crack owing to the crack interaction. The present study aims to explore the effect of crack interaction on the fatigue growth behaviour of samples with different crack offset. In this study, fatigue crack growth tests were performed for samples containing a single crack and non-collinear cracks of different crack offset in an aluminum–lithium alloy. It was shown that the two facing non-collinear cracks changed their growth direction when the cracks were overlapped, resulting in load mode transfers from mode I to I + II mixed mode. Then, the interaction behaviour was studied by establishing the finite element models to calculate the stress intensity factor K of samples with different crack offset. The results indicated that the K decreased, largely owing to the shielding effect as the two cracks overlapped, leading to retardation of crack growth in the position of overlap, especially for the specimens with a small crack offset. It was also shown that the interaction effect could change from positive to negative during the process of the multiple cracks’ growth, thus leading to the acceleration or deceleration of crack growth rates, suggesting that the influence of interaction on cracks’ growth behaviour could vary with the different stages of crack growth.

Highlights

  • Multiple cracks may be initiated and propagated owing to fatigue and corrosion in structural components, especially at multiple riveted locations [1,2,3]

  • The crack propagation tests of 2060 aluminum–lithium alloy specimens with a single crack and non-collinear cracks of different crack offset were performed under the fatigue load at room temperature

  • The finite element method was used to calculate the K at the tip of the crack for different

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Summary

Introduction

Multiple cracks may be initiated and propagated owing to fatigue and corrosion in structural components, especially at multiple riveted locations [1,2,3]. The interaction might cause the increase of the crack growth rate when the adjacent cracks merge, resulting in the crack growth life being greatly reduced. Many investigations on the influence of interaction on the cracks’ growth behaviour have been conducted [4,6,7,8,9,10,11], detailed research on the effect of the interaction on multiple cracks’ growth behaviour of specimens with different crack offset is very limited. The stress intensity factor K is usually calculated by the finite element method and theoretical analysis method. Han et al [14] adopted the finite element approach to calculate the K of parallel cracks, indicating that the relative positions between cracks have a great effect on the interactions. Zhao et al [15] propose a modified analytical solution to obtain the K of multiple

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