Aerodynamic Design of Unmanned Aerial Vehicle with Lifted System of Shrouded Rotor

Aviation technics and technology


Аuthors

Zavalov O. A., Shydakov V. I.*

Moscow Aviation Institute (National Research University), 4, Volokolamskoe shosse, Moscow, А-80, GSP-3, 125993, Russia

*e-mail: k102@mai.ru

Abstract

In the paper there are the results of Power Analysis of the Unmanned Aerial Vehicle (UAV) with Lifted System of Shrouded Rotor on the hover mode and horizontal flight. There was the estimation of the Power Characteristics of UAV of this type depending on the parameters of its aerodynamic layout.

Keywords:

unmanned aerial vehicle, shrouded rotor, aerodynamic design.


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