Physical modelling of an aeronautical composite in fire

Abstract : The evaluation of fire behaviour of structural composites is done through experimental tests which are time consuming and costly for the aircraft manufacturers (e.g. ISO 2685 and burnthrough test). Concurrently, the amount of composites in aircraft structures has increased and each type of material has to be fire evaluated accordingly. Currently, the numerical simulation is largely used during the development phase of an aircraft. So, simulation tools are underdevelopment to predict the thermophysical behaviour of composite exposed to fire. Hence it is paramount to explore in detail the behaviour of composites upon fire in order to secure the design and the certification tests to match with the aircraft master planning.
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Soumis le : mercredi 17 octobre 2018 - 13:50:20
Dernière modification le : samedi 20 octobre 2018 - 01:12:45
Archivage à long terme le : vendredi 18 janvier 2019 - 14:19:14


BCC 2016 - Physical modelling ...
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  • HAL Id : hal-01897598, version 1



Pauline Tranchard, Fabienne Samyn, Sophie Duquesne, Jean-Luc Montes, Serge Bourbigot. Physical modelling of an aeronautical composite in fire. Foreign Language Association of Maine Annual Conference, FLAME 2016, May 2016, Stamford, CT, United States. ⟨hal-01897598⟩



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