Multi-scale deterministic optimisation of blended composite structures: case study of a box-wing
dc.rights.license | open | en_US |
hal.structure.identifier | Institut de Mécanique et d'Ingénierie [I2M] | |
dc.contributor.author | PICCHI SCARDAONI, Marco | |
hal.structure.identifier | Institut de Mécanique et d'Ingénierie [I2M] | |
dc.contributor.author | IZZI, Michele Iacopo
IDREF: 228324289 | |
hal.structure.identifier | Institut de Mécanique et d'Ingénierie [I2M] | |
dc.contributor.author | MONTEMURRO, Marco
IDREF: 171660978 | |
hal.structure.identifier | Institut de Mécanique et d'Ingénierie [I2M] | |
dc.contributor.author | PANETTIERI, Enrico
IDREF: 228223156 | |
dc.contributor.author | CIPOLLA, Vittorio | |
dc.contributor.author | BINANTE, Vincenzo | |
dc.date.accessioned | 2023-01-30T09:11:45Z | |
dc.date.available | 2023-01-30T09:11:45Z | |
dc.date.issued | 2022-01-01 | |
dc.identifier.issn | 0263-8231 | en_US |
dc.identifier.uri | https://oskar-bordeaux.fr/handle/20.500.12278/171819 | |
dc.description.abstractEn | This work presents a multi-scale design methodology for the deterministic optimisation of thin-walled composite structures integrating a global–local approach for the assessment of the buckling strength and a dedicated strategy to recover blended stacking sequences. The methodology is based on the multi-scale two-level optimisation strategy for anisotropic materials and structures. In the first step, focused on the macroscopic scale, several design requirements are included in the problem formulation: lightness, feasibility, manufacturing, blending, buckling failure, static failure and stiffness. The second step, which focuses on the laminate mesoscopic scale, deals with the recovery of blended stacking sequences, for the structure at hand, matching the optimal geometric and elastic properties determined in the first step. As a case study, the unconventional PrandtlPlane box-wing system is used to show the effectiveness of the proposed design methodology. | |
dc.language.iso | EN | en_US |
dc.subject.en | Aircraft | |
dc.subject.en | Composite structures | |
dc.subject.en | Optimisation | |
dc.subject.en | Polar method | |
dc.subject.en | PrandtlPlane | |
dc.title.en | Multi-scale deterministic optimisation of blended composite structures: case study of a box-wing | |
dc.title.alternative | Thin-Walled Structures | en_US |
dc.type | Article de revue | en_US |
dc.identifier.doi | 10.1016/j.tws.2021.108521 | en_US |
dc.subject.hal | Sciences de l'ingénieur [physics]/Matériaux | en_US |
bordeaux.journal | Thin-Walled Structures | en_US |
bordeaux.volume | 170 | en_US |
bordeaux.hal.laboratories | Institut de Mécanique et d’Ingénierie de Bordeaux (I2M) - UMR 5295 | en_US |
bordeaux.institution | Université de Bordeaux | en_US |
bordeaux.institution | Bordeaux INP | en_US |
bordeaux.institution | CNRS | en_US |
bordeaux.institution | INRAE | en_US |
bordeaux.institution | Arts et Métiers | en_US |
bordeaux.peerReviewed | oui | en_US |
bordeaux.inpress | non | en_US |
bordeaux.identifier.funderID | Horizon 2020 | en_US |
hal.identifier | hal-03962256 | |
hal.version | 1 | |
hal.date.transferred | 2023-01-30T09:11:49Z | |
hal.export | true | |
dc.rights.cc | Pas de Licence CC | en_US |
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