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Effect of adhesive de-bond and crack in adherent plate on single lap joint with bi-adhesive

Lokamanya Chikmath (Department of Aeronautical Engineering, KLS Gogte Institute of Technology, Belagavi, India)
M.N. Ramanath (Department of Aerospace Engineering, Indian Institute of Technology Madras, Chennai, India)
Syed Imtiaz (Department of Aerospace Engineering, Jain University, Bengaluru, India)
H. Murthy (Department of Aerospace Engineering, Indian Institute of Technology Madras, Chennai, India)

International Journal of Structural Integrity

ISSN: 1757-9864

Article publication date: 10 January 2023

Issue publication date: 21 March 2023

142

Abstract

Purpose

This paper aims to study the benefits of use of bi-adhesive (combination of two different adhesives) over conventional single adhesive in bonded lap joints. Characterise damage severity due to cohesive and adherent failure as feedback for operating load levels that assist in developing damage tolerance design of the adhesively bonded joints.

Design/methodology/approach

Single lap joint where the adherent plate is made up of aluminium alloy joined together with bi-adhesives is analysed. The nature of adhesives ranges from brittle, elastic-plastic, moderately ductile to largely ductile. Numerical analysis is performed considering the material and geometric non-linear behaviour of the joint. The optimum bond ratio of bi-adhesives and the effect of the location of adhesive on the stress distribution are studied. The cohesive zone modelling (CZM) is adopted to account for the cohesive failure of the joint. The adherent plate failure is also addressed by modelling and studying the behaviour of the crack at different locations in the plate using modified virtual crack closure integral (MVCCI).

Findings

The results obtained from the stress analysis show some important characteristic behaviour of the bi-adhesive joint. Although bi-adhesive is expected to result in improved joint strength, the purpose gets defeated if a brittle adhesive is used at the corners and ductile adhesive at the middle. The joint strength based on CZM, evaluated for a single adhesive, is in good comparison with the experimental results from the literature. Also, the location of the crack in the adherent plate plays a significant role in the failure of the joint.

Originality/value

Estimating joint strength for the bi-adhesive model using CZM and evaluating damage severity in the presence of de-bond and crack in the bi-adhesive lap joint model assists in developing robust damage tolerance design models of such joints.

Keywords

Citation

Chikmath, L., Ramanath, M.N., Imtiaz, S. and Murthy, H. (2023), "Effect of adhesive de-bond and crack in adherent plate on single lap joint with bi-adhesive", International Journal of Structural Integrity, Vol. 14 No. 2, pp. 229-247. https://doi.org/10.1108/IJSI-11-2022-0135

Publisher

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Emerald Publishing Limited

Copyright © 2022, Emerald Publishing Limited

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