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Experimental Investigation on Hover Performance of a Ducted Coaxial-Rotor UAV

This paper presents experimental investigations on aerodynamic performance of a ducted coaxial-rotor system to evaluate its potential application as a small unmanned aerial vehicle (SUAV). Aimed at determining the influence of design parameters (rotor spacing, tip clearance and rotor position within...

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Detalles Bibliográficos
Autores principales: Li, Hai, Chen, Zaibin, Jia, Hongguang
Formato: Online Artículo Texto
Lenguaje:English
Publicado: MDPI 2023
Materias:
Acceso en línea:https://www.ncbi.nlm.nih.gov/pmc/articles/PMC10386733/
https://www.ncbi.nlm.nih.gov/pubmed/37514706
http://dx.doi.org/10.3390/s23146413

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