Ground Effect on Aerodynamic Characteristics of Aerial Vehicle with Lifted System of Shrouded Rotor

Аuthors

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

The paper contains the Method of Lift Calculation of the Unmanned Aerial Vehicle (UAV) with Lifted System of Shrouded Rotor in the condition of Ground Effect. There was the investigation of the correlation of the elements of the total thrust (ring, rotor, bottom part) for the various ground clearance.

Keywords:

unmanned aerial vehicle, shrouded rotor, ground effect, aerodynamic characteristics.

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