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Fatigue of adhesively bonded epoxy-AA6061T651 joints: Fatigue crack propagation and S-N behaviours

António A.M.A. Campos (Department of Engineering, Universidade de Tras-os-Montes e Alto Douro Escola de Ciencias e Tecnologia, Vila Real, Portugal)
Abílio M.P. de Jesus (Department of Engineering, Universidade do Porto, Porto, Portugal) (Mecanica e Gestao UCVE, Instituto de Engenharia, Porto, Portugal)
José A.F.O. Correia (Department of Engineering, Universidade do Porto, Porto, Portugal)
José J.L. Morais (Department of Engineering, Universidade de Tras-os-Montes e Alto Douro, Vila Real, Portugal)

International Journal of Structural Integrity

ISSN: 1757-9864

Article publication date: 4 December 2017

139

Abstract

Purpose

Adhesively bonded joints are gaining importance in the structural joining processes competing against welding and bolting processes. However, long-term behaviour of adhesively bonded joints is still an open question. Due to the increasing interest in adhesively bonded joints, mainly in the transports industry, there is a need to deep the knowledge about the fatigue behaviour of adhesive joints with metallic substrates allowing the development of reliable joints to resist cyclic loadings. The paper aims to discuss these issues.

Design/methodology/approach

An experimental research aiming at characterizing the fatigue behaviour of adhesively bonded aluminium substrates is presented in this paper, covering both fatigue crack propagation and global S-N behaviours. Double cantilever beam (DCB), end notch flexure (ENF) and double lap joints (DLJ) specimens built using the AA6061T651 substrate and epoxy adhesive were used to evaluate the pure modes I and II fatigue crack propagation rates and the S-N fatigue behaviours.

Findings

DCB and ENF specimens allowed the formulation of pure modes I and II fatigue crack propagation laws including the propagation thresholds. DLJs showed higher static shear strength than recommended by the manufacturer for aluminium substrates, but fatigue resistance of the DLJs was lower than suggested by the manufacturer. The fatigue damage process in the DLJs was dominated by a fatigue crack initiation process.

Originality/value

A consistent fatigue research on adhesively bonded aluminium substrates is presented covering in the same study aspects of fatigue crack propagation and fatigue crack initiation. Data reduction schemes involving both numerical and analytical procedures were followed. Proposed work constitutes a rigorous basis for future fatigue prediction models developments.

Keywords

Acknowledgements

The authors acknowledge the Portuguese Science Foundation (FCT) for the financial support through the post-doctoral Grant No. SFRH/BPD/107825/2015. The authors gratefully acknowledge the funding of SciTech – Science and Technology for Competitive and Sustainable Industries (NORTE-01-0145-FEDER-000022), R&D project cofinanced by Programa Operacional Regional do Norte (“NORTE2020”), through Fundo Europeu de Desenvolvimento Regional (FEDER).

Citation

Campos, A.A.M.A., Jesus, A.M.P.d., Correia, J.A.F.O. and Morais, J.J.L. (2017), "Fatigue of adhesively bonded epoxy-AA6061T651 joints: Fatigue crack propagation and S-N behaviours", International Journal of Structural Integrity, Vol. 8 No. 6, pp. 707-724. https://doi.org/10.1108/IJSI-08-2017-0048

Publisher

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Emerald Publishing Limited

Copyright © 2017, Emerald Publishing Limited

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