Abstract

Static tensile experiments and progressive failure simulations of single-bolt, single- and double-lap joints were carried out to comparatively investigate secondary bending effects, which present significant eccentric-loading phenomena in single-lap joints but are almost non-existent in symmetric double-lap joints. Progressive damage models of single-lap and double-lap joints were established, from which the numerical predictions were found to be in good agreement with the experimental outcomes. Experimental macro-scope failure patterns and seven numerical micro-scope failure modes obtained from the progressive damage analyses were presented for the two types of joints. The effects of secondary bending on the mechanical degradation and failure mechanism of single-lap joints were revealed. Some characterizations of secondary bending in the joints, such as a characterized parameter on the AGARD points, joint deformations and contact states, were quantitatively traced during the total progressive damage process. All these characterizations increased the understanding of the effects of secondary bending on the failure process of a single-bolt, single-lap joint.

Highlights

  • Composite bolted joints are widely used in aircraft structures because of their high load carrying capacity, ease of maintenance and replaceability, among other factors

  • This paper describes comparative experimental investigations on single-lap and double-lap composite bolted joints that were carried out to highlight the effects of secondary bending

  • The results showed that the single-bolt, single-lap joint had a nonlinearity onset strength that was lower by half than that of the double-lap joint

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Summary

Introduction

Composite bolted joints are widely used in aircraft structures because of their high load carrying capacity, ease of maintenance and replaceability, among other factors. Schön [5] conducted detailed finite element analysis to investigate the influence of secondary bending on the strength prediction for composite joints All these aforementioned works, assumed that the joints were in a linear elastic and undamaged state, which failed to reflect the actual secondary bending effects during the damage process of the joints. This paper describes comparative experimental investigations on single-lap and double-lap composite bolted joints that were carried out to highlight the effects of secondary bending. A progressive damage method, which was recently developed for failure prediction of complex composite structures [21,22,23,24], was adopted here to reveal the effects of secondary bending on the failure behavior of composite bolted joints during the loading process.

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