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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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Marques, Eas
in Cooperation with on an Cooperation-Score of 37%
Topics
Publications (26/26 displayed)
- 2023Study on out-of-plane tensile strength of angle-plied reinforced hybrid CFRP laminates using thin-plycitations
- 2022A study of the fracture mechanisms of hybrid carbon fiber reinforced polymer laminates reinforced by thin-plycitations
- 2021Determination of fracture toughness of an adhesive in civil engineering and interfacial damage analysis of carbon fiber reinforced polymer-steel structure bonded jointscitations
- 2021Novel torsion machine to test adhesive jointscitations
- 2020Displacement rate effect in the fracture toughness of glass fiber reinforced polyurethanecitations
- 2020Geometrical optimization of adhesive joints under tensile impact loads using cohesive zone modellingcitations
- 2020Numerical study of mode I fracture toughness of carbon-fibre-reinforced plastic under an impact loadcitations
- 2020Numerical study of similar and dissimilar single lap joints under quasi-static and impact conditionscitations
- 2020Experimental and numerical study of the dynamic response of an adhesively bonded automotive structurecitations
- 2019Fatigue performance of single lap joints with CFRP and aluminium substrates prior and after hygrothermal agingcitations
- 2019Adhesive joint analysis under tensile impact loads by cohesive zone modellingcitations
- 2019Dynamic behaviour in mode I fracture toughness of CFRP as a function of temperaturecitations
- 2019A strategy to reduce delamination of adhesive joints with composite substratescitations
- 2018Improvement in impact strength of composite joints for the automotive industrycitations
- 2018Adhesives and adhesive joints under impact loadings: An overviewcitations
- 2018Mechanical behaviour of adhesively bonded composite single lap joints under quasi-static and impact conditions with variation of temperature and overlapcitations
- 2018Numerical study of the behaviour of composite mixed adhesive joints under impact strength for the automotive industrycitations
- 2018Adhesive thickness influence on the shear fracture toughness measurements of adhesive jointscitations
- 2017Mode II fracture toughness of CFRP as a function of temperature and strain ratecitations
- 2017Mode I fracture toughness of CFRP as a function of temperature and strain ratecitations
- 2017Dynamic behaviour of composite adhesive joints for the automotive industrycitations
- 2015Surface treatment effect in thermoplastic rubber and natural leather for the footwear industrycitations
- 2015Effect of the surface treatment in polyurethane and natural leather for the footwear industrycitations
- 2014Effect of Cure Temperature on the Glass Transition Temperature and Mechanical Properties of Epoxy Adhesivescitations
- 2013Effect of post-cure on the glass transition temperature and mechanical properties of epoxy adhesivescitations
- 2012EFFECT OF CURE TEMPERATURE ON THE GLASS TRANSITION TEMPERATURE OF AN EPOXY ADHESIVE
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article
A study of the fracture mechanisms of hybrid carbon fiber reinforced polymer laminates reinforced by thin-ply
Abstract
The main stress component which creates delamination in bonded single lap joints with composite adherends is the transverse tensile stress. Therefore, the following study investigates the behavior of composite laminates (reference and hybrid laminates reinforced by thin-ply) under transverse tensile loading. Texipreg HS 160T700 and NTPT-TP415 were used as the conventional carbon fiber reinforced polymer (CFRP) and thin-ply respectively. Hybrid composite laminates were studied using different amounts of thin-ply, applied through the thickness. The manufactured laminates, of unidirectionally stacked construction, were tested under transverse tensile loading. Digital image correlation was performed to investigate the average peel strain distribution for the composite and to better understand the phenomena associated to the use of hybrid laminates. Experimental results show that the reinforced hybrid composite laminates, created using thin-plies, present higher failure load compared to the reference conventional CFRP or thin-ply laminates. This was found to be due to the higher ductility enabled by the presence of thin-plies. Distributing a constant amount of thin-ply through the thickness was found to increase the laminate transverse strength, as the thin-ply laminates act as a barrier against crack propagation. A representative volume element was studied for each configuration since this numerical method brings the opportunity to investigate the studied configurations in microscale.