PrandtlPlane wing-box least-weight design: A multi-scale optimisation approach
| 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 | Centre de Recherche Public Henri-Tudor [Luxembourg] [CRP Henri-Tudor] | |
| hal.structure.identifier | Laboratoire d'Energétique et Mécanique Théorique et Appliquée [LEMTA ] | |
| 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.date.accessioned | 2021-04-07T13:58:28Z | |
| dc.date.available | 2021-04-07T13:58:28Z | |
| dc.date.issued | 2020 | |
| dc.identifier.uri | oai:crossref.org:10.1016/j.ast.2020.106156 | |
| dc.identifier.uri | https://oskar-bordeaux.fr/handle/20.500.12278/26902 | |
| dc.description.abstractEn | The PrandtlPlane (PrP) aircraft wing-box least-weight design is presented in thiswork. This design problem is formulated as a constrained non-linear programming prob-lem (CNLPP), by integrating static, buckling, fatigue and manufacturability requirements,under different loading conditions. The solution search is carried out by means of a suit-able multi-scale optimisation (MSO) approach. The physical responses involved into theCNLPP formulation are evaluated at the wing-box architecture level (macroscopic scale)and at the stiffened panel level (component scale), as well. The scale transition is ensuredby means of a suitable global-local (GL) modelling approach, while the CNLPP is solvedby means of an in-house genetic algorithm. The effectiveness of the proposed approach istested on the PrP wing-box structure, but the presented strategy can be easily extendedto conventional aircraft wings. | |
| dc.language.iso | EN | en_US |
| dc.source | crossref | |
| dc.subject.en | PrandtlPlane | |
| dc.subject.en | Aircraft Optimisation | |
| dc.subject.en | Wing-box; Thin-walled structures | |
| dc.subject.en | Genetic algorithms | |
| dc.title.en | PrandtlPlane wing-box least-weight design: A multi-scale optimisation approach | |
| dc.type | Article de revue | en_US |
| dc.identifier.doi | 10.1016/j.ast.2020.106156 | en_US |
| dc.subject.hal | Sciences de l'ingénieur [physics]/Matériaux | en_US |
| dc.subject.hal | Sciences de l'ingénieur [physics]/Mécanique [physics.med-ph] | en_US |
| bordeaux.journal | Aerospace Science and Technology | en_US |
| bordeaux.page | 106156 | 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 | Arts et Métiers | en_US |
| bordeaux.institution | INRAE | |
| bordeaux.peerReviewed | oui | en_US |
| bordeaux.inpress | non | en_US |
| bordeaux.identifier.funderID | Horizon 2020 | en_US |
| bordeaux.import.source | dissemin | |
| hal.export | false | |
| workflow.import.source | dissemin | |
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