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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| Main Authors: | , , , , |
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| Format: | Article |
| Language: | English |
| Published: |
Military Technical Institute, Belgrade
2024-01-01
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| Series: | Scientific Technical Review |
| Subjects: | |
| Online Access: | https://scindeks-clanci.ceon.rs/data/pdf/1820-0206/2024/1820-02062402048I.pdf |
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