Aerodynamic optimization of winglets for an Unmanned Aerial Vehicle

Aerodynamic optimization of winglets for an Unmanned Aerial Vehicle

The main aim of this paper was to determine the influence of different parameters of winglet design on overall Unmanned Aerial Vehicle (UAV) aerodynamics. Looking from an aerodynamicist's point of view, the main reason for using such wingtip devices is to reduce induced drag component, which no...

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Bibliographic Details
Main Authors: Ivković Dušan, Kostić Ivan, Kostić Olivera, Dinulović Mirko, Simonović Aleksandar
Format: Article
Language:English
Published: Military Technical Institute, Belgrade 2024-01-01
Series:Scientific Technical Review
Subjects:
aerodynamics
hybrid calculation method
uav
vlm
optimization of winglets
cfd
Online Access:https://scindeks-clanci.ceon.rs/data/pdf/1820-0206/2024/1820-02062402048I.pdf
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