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AIR FLOW ANALYSIS AROUND THE AUTOGYRO FUSELAGE
Author(s) -
Zbigniew Czyż,
İbrahim Ilhan,
Mert Akcay,
Jacek Czarnigowski
Publication year - 2017
Publication title -
journal of technology and exploitation in mechanical engineering
Language(s) - English
Resource type - Journals
ISSN - 2451-148X
DOI - 10.35784/jteme.533
Subject(s) - fuselage , drag , aerodynamics , fluent , aerodynamic force , lift (data mining) , mechanics , airfoil , lift to drag ratio , aerospace engineering , structural engineering , angle of attack , flow (mathematics) , engineering , rotor (electric) , mechanical engineering , marine engineering , physics , computational fluid dynamics , computer science , data mining
The paper presents the results of the simulation of the air flow around the gyroplane without the influence of the rotor and pusher propellers. Three-dimensional calculations were performed using ANSYS Fluent software. Based on the calculations, the values of the drag force and the lift force on each component of the rotorcraft were determined. Based on the results obtained, the effect of angle of attack on the aerodynamic forces was obtained.

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