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

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  1. National Research Council of Canada. Aerospace
FormatText, Article
Conference34th AIAA Applied Aerodynamics Conference, 13-17 June 2016, Washington, D.C.
Publication date
PublisherAmerican Institute of Aeronautics and Astronautics
Peer reviewedYes
NPARC number23000901
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Record identifier95c88c23-d712-409c-9707-643fa13099d4
Record created2016-11-09
Record modified2020-06-04
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