PICCHI SCARDAONI, Marco; MONTEMURRO, Marco; PANETTIERI, Enrico

doi:10.1016/j.ast.2020.106156

Institut de Mécanique et d'Ingénierie [I2M]

MONTEMURRO, Marco

Centre de Recherche Public Henri-Tudor [Luxembourg] [CRP Henri-Tudor]
Laboratoire d'Energétique et Mécanique Théorique et Appliquée [LEMTA ]
Institut de Mécanique et d'Ingénierie [I2M]

PANETTIERI, Enrico

Institut de Mécanique et d'Ingénierie [I2M]

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Article de revue

Ce document a été publié dans

Aerospace Science and Technology. 2020p. 106156

Résumé en anglais

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.< Réduire

Mots clés en anglais

PrandtlPlane

Aircraft Optimisation

Wing-box; Thin-walled structures

Genetic algorithms

URI

https://oskar-bordeaux.fr/handle/20.500.12278/26902

DOI

http://dx.doi.org/10.1016/j.ast.2020.106156

Unités de recherche

Institut de Mécanique et d’Ingénierie de Bordeaux (I2M) - UMR 5295

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PrandtlPlane wing-box least-weight design: A multi-scale optimisation approach

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Résumé en anglais

Mots clés en anglais

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