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: https://doi.org/10.1016/j.cja.2016.12.013
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  1. National Research Council Canada. Aerospace
FormatText
TypeArticle
Journal titleChinese Journal of Aeronautics
ISSN1000-9361
Volume30
Issue1
Pages149163
Subjectartificial bee colony; airfoil optimization; genetic algorithm; morphing wing; optimization
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PublisherElsevier
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LanguageEnglish
Peer reviewedYes
NPARC number23001664
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Record created2017-03-14
Record modified2019-03-08
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