| People | Locations | Statistics |
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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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Jensen, Henrik Myhre
in Cooperation with on an Cooperation-Score of 37%
Topics
Publications (10/10 displayed)
- 2023Compressive strength prediction of carbon fiber-reinforced pultruded profiles including realistic volumetric fiber orientationscitations
- 2019Kink band predictions in fiber composites using periodic boundary conditionscitations
- 2018Micromechanics of kink band formation in open-hole fibre composites under compressive loadingcitations
- 2018Micromechanics of kink band formation in open-hole fibre composites under compressive loadingcitations
- 2016Experimental study of cracks at interfaces with voidscitations
- 2011Simulation of Post Failure Response in Fiber Composites
- 2007Interface fracture in adhesively bonded shell structurescitations
- 2006A Fracture Mechanical Model and a Cohesive Zone Model of Interface Fracture
- 2004Cohesive zone modelling of interface fracture near flaws in adhesive jointscitations
- 2003Crack initiation and growth in brittle bondscitations
Places of action
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article
Micromechanics of kink band formation in open-hole fibre composites under compressive loading
Abstract
<p>The micromechanics of kink band formation in open-hole fibre composites under compressive loading is described. The objective being the development of a methodology for designing of structural components with open-holes. Our results explain why failure by kink band formation propagates from the edges of an open-hole in a direction almost perpendicular to the loading direction and why the 0 plies govern the compressive failure of an open-hole laminate. The proposed design methodology accounts for the microstructure, including the fibre/matrix bonding, and the nonlinear behaviour of the constituents, enabling it to prevent local failure at the hole edges, or global failure, by kink banding of a laminate containing stress concentrations.</p>