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dc.relation.isnodouble774f4e2a-e98e-447d-aa2f-24a7ca549e0a*
hal.structure.identifierInstitut de Mécanique et d'Ingénierie [I2M]
dc.contributor.authorAUDOUX, Yohann
hal.structure.identifierInstitut de Mécanique et d'Ingénierie [I2M]
dc.contributor.authorMONTEMURRO, Marco
IDREF: 171660978
hal.structure.identifierInstitut de Mécanique et d'Ingénierie [I2M]
dc.contributor.authorPAILHES, Jerome
IDREF: 067161731
dc.date.accessioned2021-05-14T09:34:04Z
dc.date.available2021-05-14T09:34:04Z
dc.date.issued2020-09
dc.identifier.issn0263-8223
dc.identifier.urihttps://oskar-bordeaux.fr/handle/20.500.12278/76099
dc.description.abstractEnThis study presents a new strategy to generate a surrogate model used for design purposes. The metamodel is based on Non-Uniform Rational Basis Spline (NURBS) hyper-surfaces and is able to fit non-convex sets of target points (TPs). The proposed method aims at determining all the parameters involved in the definition of the NURBS hyper-surface, i.e. control points (CPs) coordinates, weights, degrees, CPs number and knot-vector components. To this purpose, the problem of finding a suitable metamodel is formulated as a constrained non-linear programming problem (CNLPP) wherein the above variables are optimised in order to fit a set of TPs. Nevertheless, when the number of CPs and the degrees of the basis functions are included among the design variables, the resulting problem is defined over a space having a variable dimension. This problem is solved by means of a special genetic algorithm able to determine simultaneously the optimum value of both the design space size (related to the integer variables of the NURBS hyper-surface) and the NURBS hyper-surface continuous parameters. The NURBS-based metamodel is then used to emulate the first buckling load of a composite stiffened panel and it is used in the framework of a meaningful design problem.
dc.language.isoen
dc.publisherElsevier
dc.subject.enOptimisation
dc.subject.enGenetic algorithms
dc.subject.enNURBS hyper-surfaces
dc.subject.enSurrogate models
dc.subject.enStiffened panels
dc.subject.enComposite structures
dc.title.enA metamodel based on non-uniform rational basis spline hyper-surfaces for optimisation of composite structures
dc.typeArticle de revue
dc.identifier.doi10.1016/j.compstruct.2020.112439
dc.subject.halSciences de l'ingénieur [physics]
bordeaux.journalComposite Structures
bordeaux.page1-12
bordeaux.volume247
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-02894598
hal.version1
hal.origin.linkhttps://hal.archives-ouvertes.fr//hal-02894598v1
bordeaux.COinSctx_ver=Z39.88-2004&rft_val_fmt=info:ofi/fmt:kev:mtx:journal&rft.jtitle=Composite%20Structures&rft.date=2020-09&rft.volume=247&rft.spage=1-12&rft.epage=1-12&rft.eissn=0263-8223&rft.issn=0263-8223&rft.au=AUDOUX,%20Yohann&MONTEMURRO,%20Marco&PAILHES,%20Jerome&rft.genre=article


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