A method based on the complex application of the actuator disk and finite-blade vortex theories is presented for aerodynamic design of the pusher propeller of a promising rotorcraft for vertical takeoff and landing. The software package was created that allows us to select the propeller parameters, create its 3D model and calculate aerodynamic characteristics in semi-automatic mode.
Aerodynamic Design of Pusher Propeller for a Promising Rotorcraft
Russ. Aeronaut.
Russian Aeronautics ; 63 , 2 ; 283-289
01.04.2020
7 pages
Aufsatz (Zeitschrift)
Elektronische Ressource
Englisch
Aerodynamic and Aeroacoustic Analysis of Installed Pusher-Propeller Aircraft Configurations
Online Contents | 2012
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