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

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DOIResolve DOI: http://doi.org/10.1016/j.cja.2016.12.013
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TypeArticle
Journal titleChinese Journal of Aeronautics
ISSN1000-9361
Volume30
Issue1
Pages149163
Subjectartificial bee colony; airfoil optimization; genetic algorithm; morphing wing; optimization
Abstract
Publication date
PublisherElsevier
LanguageEnglish
AffiliationAerospace; National Research Council Canada
Peer reviewedYes
NPARC number23001664
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Record identifiere2f44b8b-4ccc-4752-90d0-0470cb3b3ee1
Record created2017-03-14
Record modified2017-03-14
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