Studies on Wingtip Geometries by Optimum Spanwise Lift Distribution Design Method
55th AIAA Aerospace Sciences Meeting
01.01.2017
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
Studies on Wingtip Geometries by Optimum Spanwise Lift Distribution Design Method (AIAA 2017-1657)
British Library Conference Proceedings | 2017
|Effect of Viscous Drag on Optimum Spanwise Lift Distribution
Online Contents | 1993
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