| 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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Komorek, Andrzej
in Cooperation with on an Cooperation-Score of 37%
Topics
Publications (6/6 displayed)
- 2018ESTIMATION OF DEFORMATION ENERGY DURING IMPACT DESTRUCTION OF ADHESIVE JOINT SAMPLES
- 2018Effect of Glass-Fabrics and High-Melting Powder Fillers on Thermal Protective Properties of Thermosetting Laminates
- 2018The Possibility of a Visual Analysis of the Failure of Butt Adhesive Joints Made with Different Gluescitations
- 2017 Analiza przełomów udarowych połączeń klejowych blokowych
- 2016Sandwich Structured Composites for Aeronautics: Methods of Manufacturing Affecting Some Mechanical Propertiescitations
- 2016Effect of Sea Water and Natural Ageing on Residual Strength of Epoxy Laminates, Reinforced with Glass and Carbon Woven Fabricscitations
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article
Effect of Glass-Fabrics and High-Melting Powder Fillers on Thermal Protective Properties of Thermosetting Laminates
Abstract
<jats:title>Abstract</jats:title> <jats:p>The present work investigates the ablative and thermal properties of phenol formaldehyde glass-fabrics laminates filled with mixtures of corundum Al<jats:sub>2</jats:sub>O<jats:sub>3</jats:sub> and carbon C powders. The laminates specimens of dimensions 10x25x35 mm were treated with hot combustion gases having a temperature of more than 2800ºC. The carbonization of the thermosetting matrix was observed. Statistical methods for planning experiments were used, and the effect of components on the average rate of ablation, the maximum back side temperature of specimen and the average mass waste under intensive heat flow after 30 s of treatment with hot combustion gases was established. The best thermal protective properties were exhibited by the laminate containing 30% matrix, 25% fibre glass-fabric reinforcement, 9% corundum, and 36% carbon powder.</jats:p>