DOI | Trouver le DOI : https://doi.org/10.2514/6.2017-1425 |
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Auteur | Rechercher : Botez, Ruxandra M.; Rechercher : Koreanschi, Andreea; Rechercher : Oliviu, Sugar Gabor; Rechercher : Mebarki, Yussef1; Rechercher : Mamou, Mahmoud1; Rechercher : Tondji, Yvan; Rechercher : Amoroso, Francesco; Rechercher : Pecora, Rosario; Rechercher : Lecce, Leonardo; Rechercher : Amendola, Gianluca; Rechercher : Dimino, Ignazio; Rechercher : Concilio, Antonio |
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Affiliation | - Conseil national de recherches du Canada. Aérospatiale
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Format | Texte, Article |
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Conférence | 55th AIAA Aerospace Sciences Meeting, 9-13 January 2017, Grapevine, Texas, USA |
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Résumé | A new wing-tip concept with morphing upper surface and interchangeable conventional and morphing ailerons was designed, manufactured, bench and wind tunnel tested. The development of this wing tip was done in the frame of an international CRIAQ project, and the purpose was to demonstrate the upper surface morphing and aileron morphing capabilities in improving the wing tip aerodynamic performances. During numerical optimization with ‘in-house’ genetic algorithm software, and during wind tunnel experimental tests, it was demonstrated that the air flow laminar state was extended and drag coefficient reduction were obtained. |
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Date de publication | 2017-01-09 |
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Maison d’édition | American Institute of Aeronautics and Astronautics |
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Dans | |
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Langue | anglais |
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Publications évaluées par des pairs | Oui |
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Numéro NPARC | 23003231 |
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Exporter la notice | Exporter en format RIS |
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Signaler une correction | Signaler une correction (s'ouvre dans un nouvel onglet) |
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Identificateur de l’enregistrement | 5176f28f-53e9-4e3c-8e50-cda51b41b6a2 |
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Enregistrement créé | 2018-05-08 |
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Enregistrement modifié | 2020-03-16 |
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