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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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Bisagni, Chiara
in Cooperation with on an Cooperation-Score of 37%
Topics
Publications (13/13 displayed)
- 2024Resistance-welded thermoset compositescitations
- 2024Characterization and analysis of conduction welded thermoplastic composite joints considering the influence of manufacturingcitations
- 2023The importance of accounting for large deformation in continuum damage models in predicting matrix failure of compositescitations
- 2023Skin-stringer separation in post-buckling of butt-joint stiffened thermoplastic composite panelscitations
- 2022Experimental and numerical evaluation of conduction welded thermoplastic composite jointscitations
- 2022Damage arrest mechanisms in nanoparticle interleaved composite interfaces
- 2022Characterization and analysis of the interlaminar behavior of thermoplastic composites considering fiber bridging and R-curve effectscitations
- 2022FRACTURE TOUGHNESS AND PERFORMANCE OF RESISTANCE-WELDED AND CO-BONDED THERMOSET/THERMOPLASTIC POLYMER COMPOSITE HYBRID JOINTS
- 2021Multiscale damage in co-cured composites - Perspectives from experiments and modelling
- 2020Development of a Numerical Framework for Virtual Testing to Support Design of a Next Generation Thermoplastic Multifunctional Fuselagecitations
- 2019Geometrically nonlinear finite element model for predicting failure in composite structurescitations
- 2019Analysis and testing of a thermoplastic composite stiffened panel under compression
- 2018Virtual testing of thermoplastic composites
Places of action
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conferencepaper
Multiscale damage in co-cured composites - Perspectives from experiments and modelling
Abstract
Bonded and co-cured composites are popular alternatives to structures joined with mechanical fasteners in aircraft but the complex and coupled damage mechanisms in the co-cured/bonded region are poorly understood, thus making the evaluation of their strength and durability difficult with current modelling strategies. This study explores the potential of interleaf inclusion in failure-prone, critical regions of co-cured composite specimens in improving the joint strength and interface fracture toughness and strives to advance the understanding of damage initiation in the co-cured region using an atomistic model. A two-pronged approach is pursued here with bench-scale experimental testing and molecular modelling in this study. Experiments are performed for mode I fracture toughness with double cantilever beam (DCB) on composite laminates with an epoxy interleaf layer. Two epoxy resins and three methods for interleaf inclusion are explored in this study; we supplement the results from DCB testing with insights from confocal microscopy on the crack tip and the interleaf layer pre- and post-testing. Molecular dynamic (MD) simulations capture the cohesive interactions at the threephase interface containing the carbon fiber, the prepreg epoxy, and the interleaf epoxy. Results highlight that an interleaf layer made from partially-cured and filmed epoxy, further consolidated in the composite lay-up is the most effective way to suppress void formation, improve dispersion, and maximize cohesive interactions at the interface of co-cured composites. ; Aerospace Structures & Computational Mechanics