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| Naji, M. |
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| Motta, Antonella |
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| Aletan, Dirar |
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| Mohamed, Tarek |
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| Ertürk, Emre |
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| Taccardi, Nicola |
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| Kononenko, Denys |
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| Petrov, R. H. | Madrid |
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| Alshaaer, Mazen | Brussels |
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| Bih, L. |
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| Casati, R. |
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| Muller, Hermance |
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| Kočí, Jan | Prague |
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| Šuljagić, Marija |
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| Kalteremidou, Kalliopi-Artemi | Brussels |
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| Azam, Siraj |
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| Ospanova, Alyiya |
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| Blanpain, Bart |
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| Ali, M. A. |
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| Popa, V. |
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| Rančić, M. |
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| Ollier, Nadège |
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| Azevedo, Nuno Monteiro |
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| Landes, Michael |
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| Rignanese, Gian-Marco |
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Ataş, Akın
in Cooperation with on an Cooperation-Score of 37%
Topics
Publications (21/21 displayed)
- 2022Strain rate effect on the tensile properties of plain weave aramid, carbon, and glass fabric reinforced monolithic and hybrid compositescitations
- 2021Effect of quasi-static and intermediate strain rates on the tensile properties of hybrid polymer compositescitations
- 2018Bolted joints in quasi-unidirectional glass-fibre NCF composite laminatescitations
- 2018Compression after low velocity impact tests of marine sandwich composites: Effect of intermediate wooden layerscitations
- 2018Experimental investigation of pinned joints in NCF Glass-Fibre reinforced composite platescitations
- 2016Bolted joints in three axially braided carbon fibre/epoxy textile composites with moulded-in and drilled fastener holescitations
- 2016Damage and failure analysis of bolted joints in composite laminatescitations
- 2015Open hole compressive strength and damage mechanismscitations
- 2014Application of cohesive zone elements in damage analysis of compositescitations
- 2014Strength prediction of bolted joints in CFRP composite laminates using cohesive zone elementscitations
- 2013Subcritical damage mechanisms of bolted joints in CFRP composite laminatescitations
- 2013Failure analysis of bolted joints in cross-ply composite laminates using cohesive zone elements
- 2012Modelling delamination onset and growth in pin loaded composite laminatescitations
- 2012Effect of clamping force on the delamination onset and growth in bolted composite laminatescitations
- 2012Effect of geometric parameters on the stress distribution in Al 2024-T3 single-lap bolted jointscitations
- 2012Progressive failure analysis of bolted joints in composite laminatescitations
- 2012Strength prediction of bolted joints in cross-ply laminates based on subcritical damage modelling
- 2011A qualitative comparison of stresses at aircraft bolted joint holes under initial clamping forcecitations
- 2009Failure analysis of laminated composite plates with two parallel pin-loaded holescitations
- 2009The effect of curing conditions and fiber end shapes on the mechanical properties of compositescitations
- 2008İki eksenli gerilme altındaki kompozit plakalarda dairesel delik çevresindeki gerilme dağılımları
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article
Effect of geometric parameters on the stress distribution in Al 2024-T3 single-lap bolted joints
Abstract
Purpose - The purpose of this paper is to investigate the effect of geometric variables on the stress and strain distributions, as well as non-linear deformation behaviour of aluminium alloy 2024-T3 single-lap bolted joints loaded in tension. Design/methodology/approach - The study has been conducted by using numerical and experimental approaches. In the numerical part, 3D FE models were generated using ANSYS software for different e/d and W/d ratios in which e and W are variables but the hole diameter (d) is constant. Stress and displacement results for each case have been discussed to better explain the mode of failure. In the experimental part, e/d=3 and W/d=6 ratios were selected as constant and testing specimens were produced accordingly. The aim was to obtain baseline experimental load-strain and load-displacement values for selected specimen geometry coordinated with the numerical analyses. Findings - The good agreement between the experimental and numerical analysis provided confidence in the numerical methodology used to evaluate the different geometric variables. The results showed that the single-lap bolted plates with optimised W/d and e/d ratios could shift the failure mode from net-tension and shear-out to bearing failure by directing the maximum damaging stresses from the stress concentration region and shear-out planes towards the bearing region, leading to higher failure loads. Originality/value - The paper develops a FE model of single-lap bolted joints with a non-linear material model and investigates 3D stress analysis as well as non-linear deformation behaviour of bolted plates; optimisation of plates' width (W) and edge distance (e) to control failure modes; and bigger W/d and e/d ratios shift net-tension and shear-out to bearing failure mode.