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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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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



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