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dc.rights.licenseopenen_US
hal.structure.identifierInstitut de Mécanique et d'Ingénierie [I2M]
dc.contributor.authorGARULLI, Torquato
IDREF: 228324564
hal.structure.identifierInstitut de Mécanique et d'Ingénierie [I2M]
dc.contributor.authorCATAPANO MONTEMURRO, Anita
IDREF: 180013238
dc.contributor.authorFANTERIA, Daniele
hal.structure.identifierInstitut de Mécanique et d'Ingénierie [I2M]
dc.contributor.authorJUMEL, Julien
IDREF: 087926431
hal.structure.identifierLaboratoire des Composites Thermostructuraux [LCTS]
dc.contributor.authorMARTIN, Eric
dc.date.accessioned2021-09-03T11:09:44Z
dc.date.available2021-09-03T11:09:44Z
dc.date.issued2020
dc.identifier.urihttps://oskar-bordeaux.fr/handle/20.500.12278/112060
dc.description.abstractEnIn this paper, a procedure to obtain fully uncoupled multi-directional stacking sequences for delamination specimens is outlined. For such sequences, in-plane, membrane-bending and torsion–bending coupling terms are null (in closed-form solution in the framework of classical laminated plate theory) for the entire stack and for both its halves, which form two arms in the pre-cracked region of a typical delamination specimen. This is achieved exploiting the superposition of quasi-trivial quasi-homogeneous stacking sequences, according to appropriate rules. Any pair of orientations of the plies embedding the delamination plane can be obtained. To assess the effectiveness of the proposed approach, a fully uncoupled multi-directional sequence is designed and compared to other relevant sequences proposed in the literature. Finite element simulations of double cantilever beam test are performed using classic virtual crack closure technique and a revised state-of-the-art virtual crack closure technique formulation too. Some interesting conclusions regarding proper design of multidirectional stacks for delamination tests are drawn. Moreover, the results confirm the suitability of fully uncoupled multi-directional sequences for delamination tests. Thanks to their properties, these sequences might lay the foundations for the development of standard test procedures for delamination in angle-ply interfaces.
dc.language.isoENen_US
dc.subject.enLaminates
dc.subject.enfracture toughness
dc.subject.endelamination
dc.subject.enfinite element analysis
dc.title.enDesign and finite element assessment of fully uncoupled multi-directional layups for delamination tests
dc.typeArticle de revueen_US
dc.identifier.doi10.1177/0021998319868293en_US
dc.subject.halChimie/Matériauxen_US
bordeaux.journalJournal of Composite Materialsen_US
bordeaux.page773-790en_US
bordeaux.volume54en_US
bordeaux.hal.laboratoriesLaboratoire des Composites Thermo Structuraux (LCTS) - UMR 5801en_US
bordeaux.issue6en_US
bordeaux.institutionUniversité de Bordeauxen_US
bordeaux.institutionCNRSen_US
bordeaux.institutionCEAen_US
bordeaux.institutionArts et Métiersen_US
bordeaux.institutionBordeaux INP
bordeaux.institutionINRAE
bordeaux.peerReviewedouien_US
bordeaux.inpressnonen_US
hal.identifierhal-03294316
hal.exportfalse
dc.rights.ccPas de Licence CCen_US
bordeaux.COinSctx_ver=Z39.88-2004&rft_val_fmt=info:ofi/fmt:kev:mtx:journal&rft.jtitle=Journal%20of%20Composite%20Materials&rft.date=2020&rft.volume=54&rft.issue=6&rft.spage=773-790&rft.epage=773-790&rft.au=GARULLI,%20Torquato&CATAPANO%20MONTEMURRO,%20Anita&FANTERIA,%20Daniele&JUMEL,%20Julien&MARTIN,%20Eric&rft.genre=article


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