Analysis of the aerodynamic performance of a morphing wing-tip demonstrator using a novel nonlinear Vortex Lattice Method

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DOIResolve DOI: https://doi.org/10.2514/6.2016-4036
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  1. National Research Council Canada. Aerospace
FormatText
TypeArticle
Proceedings title34th AIAA Applied Aerodynamics Conference
Conference34th AIAA Applied Aerodynamics Conference, 13-17 June 2016, Washington, D.C.
ISBN978-1-62410-437-4
Abstract
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PublisherAmerican Institute of Aeronautics and Astronautics
LanguageEnglish
Peer reviewedYes
NPARC number23000901
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Record identifier95c88c23-d712-409c-9707-643fa13099d4
Record created2016-11-09
Record modified2019-03-08
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