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Thermo-oxidation behaviour of organic matrix composite materials at high temperatures

Article dans une revue avec comité de lecture
Author
CINQUIN, Jacques
244009 Airbus Group Innovations [Suresnes]
COLIN, Xavier
86289 Laboratoire Procédés et Ingénierie en Mécanique et Matériaux [PIMM]
FAYOLLE, Bruno
86289 Laboratoire Procédés et Ingénierie en Mécanique et Matériaux [PIMM]
MILLE, Marion
86289 Laboratoire Procédés et Ingénierie en Mécanique et Matériaux [PIMM]
TEREKHINA, Svetlana
86289 Laboratoire Procédés et Ingénierie en Mécanique et Matériaux [PIMM]
CHOCINSKI-ARNAULT, Laurence
118112 Institut Pprime [PPRIME]
GIGLIOTTI, Marco
118112 Institut Pprime [PPRIME]
GRANDIDIER, Jean-Claude
118112 Institut Pprime [PPRIME]
LAFARIE-FRENOT, Marie-Christine
118112 Institut Pprime [PPRIME]
MINERVINO, Matteo
118112 Institut Pprime [PPRIME]
CLUZEL, Christophe
247321 Laboratoire de Mécanique et Technologie [LMT]
DAGHIA, Federica
247321 Laboratoire de Mécanique et Technologie [LMT]
LADEVEZE, Pierre
247321 Laboratoire de Mécanique et Technologie [LMT]
ZHANG, Fangzouh
247321 Laboratoire de Mécanique et Technologie [LMT]

URI
http://hdl.handle.net/10985/11315
DOI
10.12989/aas.2016.3.2.171
Date
2016
Journal
Advances in Aircraft and Spacecraft Science

Abstract

The present paper is a review of the main activities carried out within the context of the COMPTINN‟ program, a joint research project founded by a FUI program (Fonds Unifiés Interministériels) in which four research teams focused on the thermo-oxidation behaviour of HTS-TACTIX carbon-epoxy composite at „high‟ temperatures (120°C-180°C). The scientific aim of the COMPTINN‟ program was to better identify, with a multi-scale approach, the link between the physico-chemical mechanisms involved in thermo-oxidation phenomena, and to provide theoretical and numerical tools for predicting the mechanical behaviour of aged composite materials including damage onset and development.

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