Afficher la notice abrégée

dc.rights.licenseopenen_US
dc.relation.isnodouble4e920c1f-9a54-4dee-ba62-95e04a986028*
dc.relation.isnodouble863d6ff2-cf9b-4e17-bcf5-7ee92333f94d*
dc.relation.isnodouble308ad7ae-3303-4935-a426-29ce9ebc215e*
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
hal.structure.identifierCentre d'études scientifiques et techniques d'Aquitaine [CESTA]
dc.contributor.authorMATHIAUD, Julien
IDREF: 111639530
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.accessioned2021-06-25T15:46:14Z
dc.date.available2021-06-23T09:05:08Z
dc.date.available2021-06-25T15:46:14Z
dc.date.issued2020-11-01
dc.identifier.issn0008-6223en_US
dc.identifier.urioai:crossref.org:10.1016/j.carbon.2020.11.023
dc.identifier.urihttps://oskar-bordeaux.fr/handle/20.500.12278/79262.2
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.sourcecrossref
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.typeArticle de revueen_US
dc.identifier.doi10.1016/j.carbon.2020.11.023en_US
dc.subject.halChimie/Matériauxen_US
bordeaux.journalCarbonen_US
bordeaux.page817-831en_US
bordeaux.volume173en_US
bordeaux.hal.laboratoriesLaboratoire des Composites Thermo Structuraux (LCTS) - UMR 5801*
bordeaux.hal.laboratoriesLaboratoire des Composites Thermo Structuraux (LCTS) - UMR 5801en_US
bordeaux.institutionUniversité de Bordeauxen_US
bordeaux.institutionCNRSen_US
bordeaux.institutionCEAen_US
bordeaux.institutionBordeaux INP
bordeaux.institutionINRAE
bordeaux.institutionArts et Métiers
bordeaux.peerReviewedouien_US
bordeaux.inpressnonen_US
bordeaux.import.sourcedissemin
hal.exportfalse
workflow.import.sourcedissemin
bordeaux.COinSctx_ver=Z39.88-2004&rft_val_fmt=info:ofi/fmt:kev:mtx:journal&rft.jtitle=Carbon&rft.date=2020-11-01&rft.volume=173&rft.spage=817-831&rft.epage=817-831&rft.eissn=0008-6223&rft.issn=0008-6223&rft.au=LEVET,%20Cyril&LACHAUD,%20Jean&DUCAMP,%20Virginie&MEMES,%20R%C3%A9gis&COUZI,%20Jacques&rft.genre=article


Fichier(s) constituant ce document

Thumbnail

Ce document figure dans la(les) collection(s) suivante(s)

Afficher la notice abrégée