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dc.rights.licenseopenen_US
hal.structure.identifierInstitut de Mécanique et d'Ingénierie [I2M]
dc.contributor.authorPANETTIERI, Enrico
IDREF: 228223156
hal.structure.identifierInstitut de Mécanique et d'Ingénierie [I2M]
dc.contributor.authorMONTEMURRO, Marco
IDREF: 171660978
dc.contributor.authorFANTERIA, Daniele
dc.contributor.authorCOCCIA, Francesco
dc.date.accessioned2021-04-07T14:00:06Z
dc.date.available2021-04-07T14:00:06Z
dc.date.issued2020-06-25
dc.identifier.issn0022-3239en_US
dc.identifier.urioai:crossref.org:10.1007/s10957-020-01693-y
dc.identifier.urihttps://oskar-bordeaux.fr/handle/20.500.12278/26903
dc.description.abstractEnIn this work, a multi-scale optimization strategy for lightweight structures, based on a global-local modelling approach is presented. The approach is applied to a realistic wing structure of a civil aircraft. The preliminary design of the wing can be formulated as a constrained optimization problem, involving several requirements at the different scales of the structure. The proposed strategy is characterized by two main features. Firstly, the problem is formulated in the most general sense, by including all design variables involved at each problem scale. Secondly, two scales are considered: (i) the structure macroscopic scale, where low-fidelity numerical models are used; (ii) the structure mesoscopic scale (or component-level), where enhanced models are involved. In particular, the structural responses are evaluated at both global and local scales, avoiding the use of approximated analytical methods. To this end, fully parametric global and local finite element models are interfaced with an in-house genetic algorithm. Refined models are created only for the most critical regions of the structure, and linked to the global one by means of a dedicated sub-modelling approach.
dc.language.isoENen_US
dc.sourcecrossref
dc.subject.enOptimization
dc.subject.enGeneticalgorithms
dc.subject.enWing
dc.subject.enSti enedpanels
dc.subject.enGlobal/lo calmo dellingapproach
dc.title.enMulti-scale Least-Weight Design of a Wing-Box Through a Global/Local Modelling Approach
dc.typeArticle de revueen_US
dc.identifier.doi10.1007/s10957-020-01693-yen_US
dc.subject.halSciences de l'ingénieur [physics]/Matériauxen_US
dc.subject.halSciences de l'ingénieur [physics]/Mécanique [physics.med-ph]en_US
dc.description.sponsorshipEuropeHorizon 2020 research and innovation programmeen_US
bordeaux.journalJournal of Optimization Theory and Applicationsen_US
bordeaux.hal.laboratoriesInstitut de Mécanique et d’Ingénierie de Bordeaux (I2M) - UMR 5295en_US
bordeaux.institutionUniversité de Bordeauxen_US
bordeaux.institutionBordeaux INPen_US
bordeaux.institutionArts et Métiersen_US
bordeaux.institutionCNRS
bordeaux.institutionINRAE
bordeaux.peerReviewedouien_US
bordeaux.inpressnonen_US
bordeaux.import.sourcedissemin
hal.exportfalse
workflow.import.sourcedissemin
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