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Optimization and design of an aircraft’s morphing wing-tip demonstrator for drag reduction at low speed, Part I – Aerodynamic optimization using genetic, bee colony and gradient descent algorithms

Crossref DOI link: https://doi.org/10.1016/j.cja.2016.12.013

Published Print: 2017-02

Update policy: https://doi.org/10.1016/elsevier_cm_policy

Authors

Koreanschi, Andreea

Sugar Gabor, Oliviu

Acotto, Joran

Brianchon, Guillaume

Portier, Gregoire

Botez, Ruxandra Mihaela

Mamou, Mahmoud

Mebarki, Youssef
Funding

Funding for this research was provided by:

Bombardier Aerospace, Thales Canada, the Consortium in Research and Aerospace in Canada (CRIAQ) and the Natural Sciences and Engineering Research Council of Canada (NSERC)
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Text and Data Mining valid from 2017-02-01

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This article is maintained by: Elsevier

Article Title: Optimization and design of an aircraft’s morphing wing-tip demonstrator for drag reduction at low speed, Part I – Aerodynamic optimization using genetic, bee colony and gradient descent algorithms

Journal Title: Chinese Journal of Aeronautics

CrossRef DOI link to publisher maintained version: https://doi.org/10.1016/j.cja.2016.12.013

Content Type: article

Copyright: © 2017 Chinese Society of Aeronautics and Astronautics. Production and hosting by Elsevier Ltd.

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