Experimental characterization and numerical modelling analyses of nano-adhesive-bonded joints

This paper presents an experimental and numerical characterization, typical for adhesive aerospace applications. The task is carrying two steps. The first consists on the analysis of a single lap joint produced by a carbon fiber fabric reinforced composite with five samples joined by injecting a nan...

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Main Authors: Fayssal Hadjez, Brahim Necib
Format: Article
Language:English
Published: Gruppo Italiano Frattura 2018-03-01
Series:Fracture and Structural Integrity
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Online Access:https://www.fracturae.com/index.php/fis/article/view/2008
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author Fayssal Hadjez
Brahim Necib
author_facet Fayssal Hadjez
Brahim Necib
author_sort Fayssal Hadjez
collection DOAJ
description This paper presents an experimental and numerical characterization, typical for adhesive aerospace applications. The task is carrying two steps. The first consists on the analysis of a single lap joint produced by a carbon fiber fabric reinforced composite with five samples joined by injecting a nanostructure epoxy resin (Graphene 2% by weight) while five others are not. The shear tests have been carried out on the specimens with the purpose of measuring the resistance of the bonded joint, to look forward the resulting differences of structural performances. The second deals with numerical models which have been developed based on the experimental tests for adhesive joints using the finite element techniques. The numerical simulation has been expressed using the ANSYS software in order to analyze the adhesive lap joint model. It has been noted that two options have been retained in attention which deals with and without nano-adhesive. In the two alternatives, we focused on the cooling process where the adhesive single-lap joints are mainly generated. Roughly speaking, the experimental tests and the numerical model show a good agreement. Moreover, the Graphene increases the stiffness of the lap joints under rational loads charges. On the other side, the nanostructure injection in the adhesive has increased the failure as the load increase. However, this increase of failure depends on parameters such as adhesive structural features and nanostructure’s structure. Finally, we were fortunate to observe that, the reinforced adhesive nanostructure has decreased the weight.
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series Fracture and Structural Integrity
spelling doaj-art-2ef6c1cc70bb4d2cbab57de9f049b2582025-01-03T00:40:25ZengGruppo Italiano FratturaFracture and Structural Integrity1971-89932018-03-011244Experimental characterization and numerical modelling analyses of nano-adhesive-bonded jointsFayssal Hadjez0Brahim Necib1Laboratory of Mechanics, Mechanical Engineering, University of the Frères Mentouri de Constantine. Campus Chaab Ersas 25000, Constantine, AlgeriaLaboratory of Mechanics, Mechanical Engineering, University of the Frères Mentouri de Constantine, Algeri. Campus Chaab Ersas 25000, Constantine, AlgeriaThis paper presents an experimental and numerical characterization, typical for adhesive aerospace applications. The task is carrying two steps. The first consists on the analysis of a single lap joint produced by a carbon fiber fabric reinforced composite with five samples joined by injecting a nanostructure epoxy resin (Graphene 2% by weight) while five others are not. The shear tests have been carried out on the specimens with the purpose of measuring the resistance of the bonded joint, to look forward the resulting differences of structural performances. The second deals with numerical models which have been developed based on the experimental tests for adhesive joints using the finite element techniques. The numerical simulation has been expressed using the ANSYS software in order to analyze the adhesive lap joint model. It has been noted that two options have been retained in attention which deals with and without nano-adhesive. In the two alternatives, we focused on the cooling process where the adhesive single-lap joints are mainly generated. Roughly speaking, the experimental tests and the numerical model show a good agreement. Moreover, the Graphene increases the stiffness of the lap joints under rational loads charges. On the other side, the nanostructure injection in the adhesive has increased the failure as the load increase. However, this increase of failure depends on parameters such as adhesive structural features and nanostructure’s structure. Finally, we were fortunate to observe that, the reinforced adhesive nanostructure has decreased the weight.https://www.fracturae.com/index.php/fis/article/view/2008AdhesiveLap jointsDeformationLoadAdhesively bondedNanostructures
spellingShingle Fayssal Hadjez
Brahim Necib
Experimental characterization and numerical modelling analyses of nano-adhesive-bonded joints
Fracture and Structural Integrity
Adhesive
Lap joints
Deformation
Load
Adhesively bonded
Nanostructures
title Experimental characterization and numerical modelling analyses of nano-adhesive-bonded joints
title_full Experimental characterization and numerical modelling analyses of nano-adhesive-bonded joints
title_fullStr Experimental characterization and numerical modelling analyses of nano-adhesive-bonded joints
title_full_unstemmed Experimental characterization and numerical modelling analyses of nano-adhesive-bonded joints
title_short Experimental characterization and numerical modelling analyses of nano-adhesive-bonded joints
title_sort experimental characterization and numerical modelling analyses of nano adhesive bonded joints
topic Adhesive
Lap joints
Deformation
Load
Adhesively bonded
Nanostructures
url https://www.fracturae.com/index.php/fis/article/view/2008
work_keys_str_mv AT fayssalhadjez experimentalcharacterizationandnumericalmodellinganalysesofnanoadhesivebondedjoints
AT brahimnecib experimentalcharacterizationandnumericalmodellinganalysesofnanoadhesivebondedjoints