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The paper presents the results of numerical tests of the aerodynamics of the Gyro-One unmanned autogyro model. The geometry of the research object was developed using reverse engineering and CAD software. The created solid model of the aircraft was entered into the Ansys Meshing to generate amesh. The boundary conditions and turbulence model were defined withAnsys Fluent software. The calculated parametersinclude the aerodynamic forces and thepitching moment generated on individual elementscalculated with the CFD method for the selected values of the angle of attack, the velocity and pressure distributionsin the plane ofsymmetry,and the pressure distribution on the aircraft surface for the defined measurement points. The obtained results made it possible to analyse the flow around the research object and become anintroduction to further research intoahybrid multi-rotor aircraft based on the autogyro design.
