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dc.contributor.authorCATAPANO, Anita
dc.contributor.author
 hal.structure.identifier
MONTEMURRO, Marco
164351 Institut de Mécanique et d'Ingénierie de Bordeaux [I2M]
dc.date.accessioned2016
dc.date.available2017
dc.date.issued2016
dc.date.submitted2016
dc.identifier.issn1931-6828
dc.identifier.urihttp://hdl.handle.net/10985/11387
dc.description.abstractIn this work the authors propose a new paradigm for the optimum design of variable angle tow (VAT) composites. They propose a generalisation of a multi-scale two-level (MS2L) optimisation strategy already employed to solve optimisation problems of anisotropic structures characterised by a constant stiffness distribution. In the framework of the MS2L methodology, the design problem is split into two sub-problems. At the first step of the strategy the goal is to determine the optimum distribution of the laminate stiffness properties over the structure, while the second step aims at retrieving the optimum fibres-path in each layer meeting all the requirements provided by the problem at hand. The MS2L strategy relies on: a) the polar formalism for describing the behaviour of the VAT laminate, b) the iso-geometric surfaces for describing the spatial variation of the stiffness properties and c) an hybrid optimisation tool (genetic and gradient-based algorithms) to perform the solution search. The effectiveness of the MS2L strategy is proven through a numerical example on the maximisation of the first buckling factor of a VAT plate subject to both mechanical and manufacturability constraints.
dc.language.isoen
dc.publisherSpringer
dc.rightsPost-print
dc.subjectComposite materials
dc.subjectVariable stiffness
dc.subjectAnisotropy
dc.subjectVariable angle-tow laminates
dc.subjectBuckling
dc.subjectOptimisation
dc.titleA new paradigm for the optimum design of variable angle tow laminates
ensam.embargo.terms2017-07-01
dc.identifier.doi10.1007/978-3-319-45680-5
dc.typdocChapitre d'ouvrage scientifique
dc.localisationCentre de Bordeaux-Talence
dc.subject.halMathématique: Optimisation et contrôle
dc.subject.halSciences de l'ingénieur: Mécanique
dc.subject.halSciences de l'ingénieur: Mécanique: Génie mécanique
dc.subject.halSciences de l'ingénieur: Mécanique: Mécanique des solides
dc.subject.halSciences de l'ingénieur: Mécanique: Mécanique des structures
ensam.audienceInternationale
ensam.title.proceedingMathematical Challenges for the Aerospace of the Future
ensam.page460
ensam.volume116
ensam.issue1
hal.description.error{"duplicate-entry":{"hal-01362349":{"doi":"1.0"}}}
hal.submission.permittedtrue
hal.statusunsent


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