AIR FLOW ANALYSIS AROUND THE AUTOGYRO FUSELAGE
Zbigniew Czyż
z.czyz@pollub.plDepartment 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
Faculty of Engineering, Necmettin Erbakan University, Mehmet Hulusi Baybal, PhD. Cd. No:12, 42060 Konya, Turkey (Turkey)
Mert Akcay
Department of Automotive Engineering, Cumhuriyet University, Kayseri Cd. 58070 Sivas/Merkez Turkey (Turkey)
Jacek Czarnigowski
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 forceReferences
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Authors
Zbigniew Czyżz.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
Authors
Ibrahim IlhanFaculty of Engineering, Necmettin Erbakan University, Mehmet Hulusi Baybal, PhD. Cd. No:12, 42060 Konya, Turkey Turkey
Authors
Mert AkcayDepartment of Automotive Engineering, Cumhuriyet University, Kayseri Cd. 58070 Sivas/Merkez Turkey Turkey
Authors
Jacek CzarnigowskiDepartment of Thermodynamics, Fluid Mechanics and Aviation Propulsion Systems, Lublin University of Technology, 36 Nadbystrzycka Str., 20-618 Lublin, Poland Poland
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