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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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Swolfs, Y.
in Cooperation with on an Cooperation-Score of 37%
Topics
Publications (8/8 displayed)
- 2022Detailed experimental validation and benchmarking of six models for longitudinal tensile failure of unidirectional compositescitations
- 2022Discontinuities in Aligned Discontinuous Fibers Composites: Microstructure Orientation Effect on Local Stress Concentration Factors
- 2021Blind benchmarking of seven longitudinal tensile failure models for two virtual unidirectional compositescitations
- 2021A synchrotron computed tomography dataset for validation of longitudinal tensile failure models based on fibre break and cluster developmentcitations
- 2020Fibre-direction strain measurement in a composite ply under quasi-static tensile loading using digital volume correlation and in situ synchrotron radiation computed tomographycitations
- 2020Predicting tensile behaviour of hybrid carbon fibre/SRPP composites
- 2019Carbon fibre sheet moulding compounds with high ine-mould flow: Linking morphology to tensile and compressive propertiescitations
- 2016Hybrid effects in thin ply carbon/glass unidirectional laminatescitations
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article
Hybrid effects in thin ply carbon/glass unidirectional laminates
Abstract
<p>Experimental results are presented which allow the hybrid effect to be evaluated accurately for thin ply carbon/epoxy-glass/epoxy interlayer hybrid composites. It is shown that there is an enhancement in strain at failure of up to 20% for very thin plies, but no significant effect for thicker plies. Hybrid specimens with thick carbon plies can therefore be used to measure the reference carbon/epoxy failure strain. The latter is significantly higher than the strain from all-carbon specimens in which there is an effect due to stress concentrations at the load introduction. Models are presented which illustrate the mechanisms responsible for the hybrid effect due to the constraint on failure at both the fibre and ply level. These results give a good understanding of how variability in the carbon fibre strengths can translate into hybrid effects in composite laminates.</p>