AIR FLOW ANALYSIS AROUND THE AUTOGYRO FUSELAGE

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Published: Jun 30, 2017
DOI: https://doi.org/10.35784/jteme.533
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DOI

https://doi.org/10.35784/jteme.533

Authors

Zbigniew Czyż

z.czyz@pollub.pl

Department of Thermodynamics, Fluid Mechanics and Aviation Propulsion Systems, Lublin University of Technology, 36 Nadbystrzycka Str., 20-618 Lublin, Poland, Poland
https://orcid.org/0000-0003-2281-1149
Ibrahim Ilhan

ibboilhan95@gmail.com

Faculty of Engineering, Necmettin Erbakan University, Mehmet Hulusi Baybal, PhD. Cd. No:12, 42060 Konya, Turkey, Turkey
Mert Akcay

akcay.mert@outlook.com

Department of Automotive Engineering, Cumhuriyet University, Kayseri Cd. 58070 Sivas/Merkez Turkey, Turkey
Jacek Czarnigowski

j.czarnigowski@pollub.pl

Department of Thermodynamics, Fluid Mechanics and Aviation Propulsion Systems, Lublin University of Technology, 36 Nadbystrzycka Str., 20-618 Lublin, Poland, Poland

Abstract

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.

Keywords:

CFD, Computational Fluid Dynamics, gyroplane, aerodynamics, lift force, drag force

References

Article Details

Czyż, Z., Ilhan, I. ., Akcay, M., & Czarnigowski, J. (2017). AIR FLOW ANALYSIS AROUND THE AUTOGYRO FUSELAGE. Journal of Technology and Exploitation in Mechanical Engineering, 3(1), 13–20. https://doi.org/10.35784/jteme.533