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dc.relation.isnodouble981a45e8-e4b7-4470-9446-31eaf6567fcc*
hal.structure.identifierInstitut de Mécanique et d'Ingénierie de Bordeaux [I2M]
dc.contributor.authorMONTEMURRO, Marco
IDREF: 171660978
hal.structure.identifierDipartimento di Ingegneria Meccanica e Aerospaziale [Torino] [DIMEAS]
dc.contributor.authorPAGANI, Alfonso
hal.structure.identifierInstitut de Mécanique et d'Ingénierie de Bordeaux [I2M]
hal.structure.identifierDipartimento di Ingegneria Meccanica e Aerospaziale [Torino] [DIMEAS]
dc.contributor.authorFIORDILINO, Giacinto Alberto
hal.structure.identifierInstitut de Mécanique et d'Ingénierie de Bordeaux [I2M]
dc.contributor.authorPAILHÈS, Jérôme
hal.structure.identifierDipartimento di Ingegneria Meccanica e Aerospaziale [Torino] [DIMEAS]
dc.contributor.authorCARRERA, Erasmo
dc.date.accessioned2021-05-14T09:39:42Z
dc.date.available2021-05-14T09:39:42Z
dc.date.issued2018-10
dc.identifier.issn0263-8223
dc.identifier.urihttps://oskar-bordeaux.fr/handle/20.500.12278/76515
dc.description.abstractThis work deals with the problem of the least-weight design of a composite stiffened panel subject to constraints of different nature (mechanical, geometrical and manufacturability requirements). To face this problem, a multi-scale two-level (MS2L) design methodology is proposed. This approach aims at optimising simultaneously both geometrical and mechanical parameters for skin and stiffeners at each characteristic scale (mesoscopic and macroscopic ones). In this background, at the first level (macroscopic scale) the goal is to find the optimum value of geometric and mechanical design variables of the panel minimising its mass and meeting the set of imposed constraints. The second-level problem focuses on the laminate mesoscopic scale and aims at finding at least one stacking sequence (for each laminate composing the panel) meeting the geometrical and material parameters provided by the first-level problem.The MS2L optimisation approach is based on the polar formalism to describe the macroscopic behaviour of the composites and on a special genetic algorithm to perform optimisation calculations.The quality of the optimum configurations is investigated, a posteriori, through a refined finite element model of the stiffened panel making use of elements with different kinematics and accuracy in the framework of the Carrera's Unified Formulation (CUF).
dc.language.isoen
dc.publisherElsevier
dc.subjectCeramics and Composites
dc.subjectCivil and Structural Engineering
dc.titleA general multi-scale two-level optimisation strategy for designing composite stiffened panels
dc.typeArticle de revue
dc.identifier.doi10.1016/j.compstruct.2018.06.119
dc.subject.halSciences de l'ingénieur [physics]/Mécanique [physics.med-ph]
dc.subject.halMathématiques [math]/Optimisation et contrôle [math.OC]
bordeaux.journalComposite Structures
bordeaux.page968-979
bordeaux.volume201
bordeaux.hal.laboratoriesInstitut de Mécanique et d’Ingénierie de Bordeaux (I2M) - UMR 5295*
bordeaux.institutionUniversité de Bordeaux
bordeaux.institutionBordeaux INP
bordeaux.institutionCNRS
bordeaux.institutionINRAE
bordeaux.institutionArts et Métiers
bordeaux.peerReviewedoui
hal.identifierhal-02354568
hal.version1
hal.origin.linkhttps://hal.archives-ouvertes.fr//hal-02354568v1
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