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Autor:
Milenković-Babić Miodrag D., Ivković Dušan A., Ostojić Branislav G., Dovatov Biljana Z., Trifković Milenko S., Antonić Vuk D.
Publikováno v:
FME Transactions, Vol 52, Iss 4, Pp 556-562 (2024)
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 fi
Externí odkaz:
https://doaj.org/article/ab716ad757a54c5aa23cb9946a25bc3e