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A novel profiling concept leading to a significant increase in the mechanical performance of metal to composite joints
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1-s2.0-S1359836823002949-main.pdf | Published version | 7.13 MB | Adobe PDF | View/Open |
Title: | A novel profiling concept leading to a significant increase in the mechanical performance of metal to composite joints |
Authors: | Whitehouse, AD Medeau, V Mencattelli, L Blackman, B Pinho, ST |
Item Type: | Journal Article |
Abstract: | Traditional adhesive joints with straight edged adherends suffer from a significant stress concentration in the composite coincident with the edge of the metal adherend, which can lead to accelerated translaminar failure of the substrate. In this work, we developed a novel profiling concept which improves the mechanical performance of adhesive joints between metallic adherends and composite substrates. We conducted quasi-static four-point bending (4PB) tests which showed that profiling the edge of the metallic adherend could improve the peak load by at least 27%, and that the stability of failure was simultaneously improved. We investigated varying the profile parameters and were able to conclude that further significant mechanical performance gains could be achieved by increasing any of the profile: amplitude, frequency, or number of fractal length-scales. By analysing in-situ acoustic emission (AE) monitoring data we were able to observe that profiling of the metallic adherend results in failure initiation occurring at higher loads, which suggests that the concept is successful in providing better stress distributions and lowering peak stresses. By analysing the fracture surfaces, it is apparent that the profiling concept is successful in deflecting the translaminar fracture path; and additionally that a debonding mechanism occurs at the profile tips which is thought to be an important additional mechanism for creating damage tolerant joints. |
Issue Date: | 15-Jul-2023 |
Date of Acceptance: | 3-May-2023 |
URI: | http://hdl.handle.net/10044/1/103930 |
DOI: | 10.1016/j.compositesb.2023.110791 |
ISSN: | 0961-9526 |
Publisher: | Elsevier |
Start Page: | 1 |
End Page: | 15 |
Journal / Book Title: | Composites Part B: Engineering |
Volume: | 261 |
Copyright Statement: | © 2023 The Author(s). Published by Elsevier Ltd. This is an open access article under the CC BY license (http://creativecommons.org/licenses/by/4.0/). |
Publication Status: | Published |
Article Number: | 110791 |
Online Publication Date: | 2023-05-09 |
Appears in Collections: | Mechanical Engineering Aeronautics Faculty of Engineering |
This item is licensed under a Creative Commons License