Publication: Design considerations for tandem wing configurations in small unmanned aerial vehicles
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Publishing House of “Henri Coanda” Air Force Academy
Abstract
This paper examines the design aspects of small unmanned aerial vehicles (UAVs) in tandem wing configuration. This type of wing configuration is gaining increasing attention due to its enhanced capabilities of stability, maneuverability, and efficiency. Through a detailed analysis of the main design aspects, this paper explores the integration of tandem wing configurations in small UAVs. The results and conclusions presented here aim to provide useful guidance into optimizing performance and improving operational characteristics of these aerial systems.
Description
This paper was presented at the International Conference of Scientific Research and Education in the Air Force – AFASES 2024, Brașov, Romania.
It was published in open access by the Henri Coandă Air Force Academy Publishing House in AFASES Proceedings, Vol. 25 (pp. 143–151).
DOI: 10.19062/2247-3173.2024.25.17
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Citation
G. R. Buican, S.-M. Zaharia, and C.-M. Agapie, “Design considerations for tandem wing configurations in small unmanned aerial vehicles,” in Proceedings of the Scientific Research and Education in the Air Force – AFASES 2024, Vol. 25, pp. 143–151, Brașov, Romania, 2024, doi:10.19062/2247-3173.2024.25.17