Experimental Investigation of Aerodynamic Characteristics of Unmanned Aerial Vehicle with Lifted System of Shrouded Rotor

Аuthors

Mojzyh E. I., Zavalov O. A., Kuznetsov A. V.^*

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

*e-mail: alexkuzn@sumail.ru

Abstract

In the Paper there are the results of Experimental Investigation of Aerodynamic Characteristics of the model the disk-shaped Unmanned Aerial Vehicle (UAV) with Lifted System of Shrouded Rotor in the side flow mood. The obtained results provided to expose the features of the ring and rotor interaction on these moods. It was the base for development of the aerodynamic calculation method.

Keywords:

disk-shaped UAV; Shrouded Rotor; Aerodynamic Characteristics; Experimental Investigation

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