Computational Analysis of the 2415-3S Airfoil Aerodynamic Performance

This paper deals with the numerical simulation of the two-dimensional, incompressible, steady air flow past an airfoil for a solar powered unmanned aerial vehicle (UAV) with internal propulsion system. This airfoil results from a NACA 2415 four digits family base airfoil modification [7] and has a p...

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Bibliographic Details
Main Authors: Luis Velázquez-Araque, Jiří Nožička
Format: Article
Language:English
Published: International Institute of Informatics and Cybernetics 2014-02-01
Series:Journal of Systemics, Cybernetics and Informatics
Subjects:
Online Access:http://www.iiisci.org/Journal/CV$/sci/pdfs/FA475SF13.pdf