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 of Canada. Aerospace
FormatText, Article
Subjectartificial bee colony; airfoil optimization; genetic algorithm; morphing wing; optimization
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Peer reviewedYes
NPARC number23001664
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Record identifiere2f44b8b-4ccc-4752-90d0-0470cb3b3ee1
Record created2017-03-14
Record modified2020-05-30
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