ANALYSIS OF THE PRE-ROTATION ENGINE LOADS IN THE AUTOGYRO
| 1 | Department of Thermodynamics, Fluid Mechanics and Aviation Propulsion Systems, Faculty of Mechanical Engineering, Lublin University of Technology, 36 Nadbystrzycka Str., 20-618 Lublin, Poland |
| 2 | Department of Airframe and Engine, Polish Air Force Academy, 35 Dywizjonu 303 Str., 08-521 Dęblin, Poland |
| 3 | URSUS S.A. Lublin, 7 Frezerów Str., 20-209 Lublin, Poland |
CORRESPONDING AUTHOR
Zbigniew Czyż
Department of Thermodynamics, Fluid Mechanics and Aviation Propulsion Systems, Faculty of Mechanical Engineering, Lublin University of Technology, 36 Nadbystrzycka Str., 20-618 Lublin, Poland, Nadbystrzycka 36, 20-618 Lublin, Poland
Department of Thermodynamics, Fluid Mechanics and Aviation Propulsion Systems, Faculty of Mechanical Engineering, Lublin University of Technology, 36 Nadbystrzycka Str., 20-618 Lublin, Poland, Nadbystrzycka 36, 20-618 Lublin, Poland
Publication date: 2016-09-01
Adv. Sci. Technol. Res. J. 2016; 10(31):169–176
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ABSTRACT
The paper presents the analyzes of the pre-rotation engine loads in the Taurus autogyro manufactured by Aviation Artur Trendak from Poland. Based on the NACA-9 H-12 airfoil characteristics of the drag coefficient, on which the rotor blade was made, forces acting on the rotor during pre-rotation have been calculated. The paper presents the characteristics of the drag coefficient as a function of angle of attack for Re = 1,800,000 and Re = 2,600,000. For the speed range of 0 to 400 rpm torque resulting from the drag forces and the power required to drive the rotor were calculated.
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