Flying wing conceptual design and flight testing

Flying wing conceptual design and flight testing

The main aim of this paper is to present a method for the conceptual design of a flying wing unmanned aerial vehicle using open-source software for rapid airfoil comparison and design and parametric geometry design and analysis. After adopting the final geometry the aerodynamic characteristics have...

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Bibliographic Details
Main Authors: Milenković-Babić Miodrag D., Ivković Dušan A., Ostojić Branislav G., Dovatov Biljana Z., Trifković Milenko S., Antonić Vuk D.
Format: Article
Language:English
Published: University of Belgrade - Faculty of Mechanical Engineering, Belgrade 2024-01-01
Series:FME Transactions
Subjects:
uav
flying wing
conceptual design
flight test
aerodynamics
stability
control
Online Access:https://scindeks-clanci.ceon.rs/data/pdf/1451-2092/2024/1451-20922404556M.pdf
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https://scindeks-clanci.ceon.rs/data/pdf/1451-2092/2024/1451-20922404556M.pdf

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