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dc.rights.licenseopenen_US
hal.structure.identifierLaboratoire des Composites Thermostructuraux [LCTS]
dc.contributor.authorLEVET, Cyril
hal.structure.identifierInstitut de Mécanique et d'Ingénierie [I2M]
dc.contributor.authorLACHAUD, Jean
dc.contributor.authorDUCAMP, Virginie
dc.contributor.authorMEMES, Régis
dc.contributor.authorCOUZI, Jacques
dc.contributor.authorMATHIAUD, Julien
hal.structure.identifierLaboratoire des Composites Thermostructuraux [LCTS]
dc.contributor.authorGILLARD, Adrien P.
hal.structure.identifierLaboratoire des Composites Thermostructuraux [LCTS]
dc.contributor.authorWEISBECKER, P.
hal.structure.identifierLaboratoire des Composites Thermostructuraux [LCTS]
dc.contributor.authorVIGNOLES, Gérard L.
dc.date.accessioned2021-11-18T13:14:55Z
dc.date.available2021-11-18T13:14:55Z
dc.date.issued2021
dc.identifier.issn86223en_US
dc.identifier.urihttps://oskar-bordeaux.fr/handle/20.500.12278/123860
dc.description.abstractEn3D carbon-fibre reinforced carbon composites (3D ) are used as thermal protection systems for atmospheric re-entry, where they are exposed to strong ablation. Particularly, sublimation of the carbonaceous material plays an important role during the re entry. To study this, an arc image furnace under controlled Argon flow is used, with heat fluxes of 8 MWm−2 to 10 MWm−2. The furnace and the sample thermal response have been numerically simulated prior to the experiments and match in-situ temperature measurements. Scanning electron microscopy and 3D profilometry with digital optical microscopy were used in order to characterise the epi-macro-structural and the epi-micro-structural roughness of the composite surface, evidencing a faster recession of the fibres as compared to the matrix. Carbon nanotextures have been assessed by using High-Resolution Transmission Electron Microscopy and Polarised Light Optical Microscopy, showing that the matrix is more organised than the fibre. This can explain the “inverse” behaviour under sublimation as compared to oxidation. The results have been qualitatively interpreted using numerical simulation of differential surface recession.
dc.language.isoENen_US
dc.subject.enCarbon/carbon composites
dc.subject.enAblation
dc.subject.enSublimation
dc.subject.enRoughness
dc.subject.enImage arc furnace
dc.subject.enModeling
dc.title.enHigh-flux sublimation of a 3D carbon/carbon composite: Surface roughness patterns
dc.title.alternativeCarbonen_US
dc.typeArticle de revueen_US
dc.identifier.doi10.1016/j.carbon.2020.11.023en_US
dc.subject.halSciences de l'ingénieur [physics]/Mécanique [physics.med-ph]en_US
bordeaux.journalCarbonen_US
bordeaux.page817-831en_US
bordeaux.volume173en_US
bordeaux.hal.laboratoriesLaboratoire des Composites Thermo Structuraux (LCTS) - UMR 5801en_US
bordeaux.hal.laboratoriesInstitut de Mécanique et d’Ingénierie de Bordeaux (I2M) - UMR 5295en_US
bordeaux.institutionUniversité de Bordeauxen_US
bordeaux.institutionCNRSen_US
bordeaux.institutionCEAen_US
bordeaux.peerReviewedouien_US
bordeaux.inpressnonen_US
hal.identifierhal-03312164
hal.version1
hal.date.transferred2021-11-18T13:15:12Z
hal.exporttrue
dc.rights.ccPas de Licence CCen_US
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