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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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Fiedler, B.
in Cooperation with on an Cooperation-Score of 37%
Topics
Publications (16/16 displayed)
- 2021Experimental and numerical mechanical characterization of additively manufactured Ti6Al4V lattice structures considering progressive damagecitations
- 2020Mechanical integrity of friction-riveted joints for aircraft applicationscitations
- 2020Low-velocity impact response of friction riveted joints for aircraft applicationcitations
- 2020Effect of laser surface treatment on the adhesive properties of bonded CFRP joints
- 2020Hierarchical carbon fibre reinforced plastics with tailored nanoparticle modification - Benefits and limitations
- 2019Damage mechanisms of tailored few-layer graphene modified CFRP cross-ply laminatescitations
- 2019Tailored crystalline width and wall thickness of an annealed 3D carbon foam composites and its mechanical propertycitations
- 2018Fundamentals of the temperature-dependent electrical conductivity of a 3D carbon foam—Aerographitecitations
- 2018Mechanistic aspects on molecular structure formation of polymeric networks from diisocyanates with amidine compoundscitations
- 2017Nanomaterials from Natural Products for Industrial Applicationscitations
- 2017Modelling strategy for microcracking in off-axis plies in CFRP laminates under monotonic and fatigue loading up to the VHCF regime
- 2016Electrical conductivity of melt-spun thermoplastic poly(hydroxy ether of bisphenol A) fibres containing multi-wall carbon nanotubescitations
- 2016Electrical and thermal conductivity of aerogel/epoxy composites
- 2016Influence of voids and impact damage on the fatigue behaviour of large scale composites: Einfluss von Poren und Schlagschäden auf das Ermüdungsverhalten von Großstrukturen,Einfluss von Poren und Schlagschäden auf das Ermüdungsverhalten von Großstrukturencitations
- 2015Voids and their effect on the strain rate dependent material properties and fatigue behaviour of non-crimp fabric composites materialscitations
- 2014Damage mechanisms of nanoparticle-modified CFRP under very high cycle fatigue-loading
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article
Tailored crystalline width and wall thickness of an annealed 3D carbon foam composites and its mechanical property
Abstract
<p>Carbon nanostructures in form of 3D carbon foams are mainly popular in materials community because of their ultralow densities, variable morphologies, and remarkable properties, etc. One of these foams is Aerographite, which exhibits a tetrapodal interconnected morphology. Similar to other synthetic carbon structures, the lattice defects are formed during the synthesis of Aerographite, which can be healed by a post-thermal treatment. Aerographite shows a property dependency on wall thickness (number of graphitic layers), which affects both, the electrical and mechanical properties. In this study, the wall thickness is tailored by varying of the total reaction time during the replication process. The influence of the thermal treatment of Aerographite on its mechanical performance in an Aerographite-epoxy nanocomposite, by determining the fracture toughness (K<sub>1C</sub>) in three-point bending tests (SEN-3PB), is investigated. An increase of the fracture toughness with increasing wall thickness is observed for untreated Aerographite. The graphitization of Aerographite leads to a reduction of the mechanical properties, by increasing the crystalline width. Consequently, the measured fracture toughness is dependent on the graphitization, the calculated crystalline width and the wall thickness of tubes in the hollow Aerographite tetrapodal network. Finally, based on these relations, a phenomenological mechanical failure model is developed and briefly discussed.</p>