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...
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
|
Similar Items
-
Analysis of Air Flow Past and through the 2415-3S Airfoil for an Unmanned Aerial Vehicle with Internal Propulsion System
by: Luis D. Mendoza, et al.
Published: (2014-08-01) -
Aerodynamic design of a double slotted morphed flap airfoil– a numerical study
by: S. S. Shahrokhi, et al.
Published: (2024-03-01) -
Aerodynamic performance characteristics of EYO-Series low Reynolds number airfoils for small wind turbine applications
by: Emmanuel Yeboah Osei, et al.
Published: (2022-12-01) -
RANS Simulations of Aerodynamic Performance of NACA 0015 Flapped Airfoil
by: Sohaib Obeid, et al.
Published: (2017-01-01) -
Aerodynamic Optimization of Micro Aerial Vehicle
by: Siew Ping Yeong, et al.
Published: (2016-01-01)