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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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Bernard, Cédric
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Topics
Publications (10/10 displayed)
- 2023Étude de l’origine physique de la non linéarité élastique en traction et compression des unidirectionnels à fibres continues de carbone
- 2023Intense shear band plasticity in metallic glass as revealed by a diametral compression testcitations
- 2019Strain rate sensitivity of germanium-selenium glasses
- 2017A sequential pre-cracking procedure to measure the mode-I fracture toughness of ultra pure bulk metallic glassescitations
- 2012Relationship between local strain jumps and temperature bursts due to the Portevin-Le Chatelier effect in an Al-Mg alloycitations
- 2011The Effect of Temperature on Anisotropy Properties of an Aluminium Alloycitations
- 2011High temperature elasticity and viscosity of GexSe1-x glasses in the transition rangecitations
- 2007Room temperature viscosity and delayed elasticity in infrared glass fibercitations
- 2006Toughness of Zr 55 Cu 30 Al 10 Ni 5 bulk metallic glass for two oxygen levelscitations
- 2006Indentation and rheology of inorganic glasses from 20 to 700 °C
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document
Étude de l’origine physique de la non linéarité élastique en traction et compression des unidirectionnels à fibres continues de carbone
Abstract
Unidirectional continuous carbon fibre composite laminates exhibit non-linear elastic behaviour, characterised by stiffening under tension and softening under compression. It has been shown, for a small range of deformation, that this non-linearity is due to the ply material and that the contribution of the ply-inner fibre waviness is negligible. However, the study was not carried out over the entire deformation range of the laminates, i.e. up to failure. This is the purpose of this paper, which uses experimental results from four-point bending tests and a numerical model of this test. The evolution of the position of the neutral fibre with loading is taken as an indicator of the non-linear behaviour. The introduction of the four (experimentally determined) parameters characterising the non-linearity into the numerical model allows to highlight the obvious contribution of the material to the non-linearity at the beginning of the loading. At the same time, the geometric contribution of fibre waviness is determined using a non-local numerical model. Its contribution to the non-linearity is evaluated.