MITROVIĆ, Časlav ;BENGIN, Aleksander ;CVETKOVIĆ, Dragan ;BERKIĆ, Dragoljub . An Optimal Main Helicopter Rotor Projection Model Obtained by Viscous Effects and Unsteady Lift Simulation. Strojniški vestnik - Journal of Mechanical Engineering, [S.l.], v. 56, n.6, p. 357-367, october 2017. ISSN 0039-2480. Available at: <https://www.sv-jme.eu/article/an-optimal-main-helicopter-rotor-projection-model-obtained-by-viscous-effects-and-unsteady-lift-simulation/>. Date accessed: 26 dec. 2024. doi:http://dx.doi.org/.
Mitrović, ., Bengin, A., Cvetković, D., & Berkić, D. (2010). An Optimal Main Helicopter Rotor Projection Model Obtained by Viscous Effects and Unsteady Lift Simulation. Strojniški vestnik - Journal of Mechanical Engineering, 56(6), 357-367. doi:http://dx.doi.org/
@article{., author = {Časlav Mitrović and Aleksander Bengin and Dragan Cvetković and Dragoljub Berkić}, title = {An Optimal Main Helicopter Rotor Projection Model Obtained by Viscous Effects and Unsteady Lift Simulation}, journal = {Strojniški vestnik - Journal of Mechanical Engineering}, volume = {56}, number = {6}, year = {2010}, keywords = {unsteady lift; viscous effect simulation; potential flow; lifting surface; panel method; free-wake model; main helicopter rotor aerodynamics; }, abstract = {This paper presents an airfoil model which provides a method for optimal main helicopter rotor projection by viscous effect and unsteady lift simulation through algorithm and set of program entireties, applicable to the ideological and main project of helicopter rotor. Based on real rotors theoretical consideration and the, numerical analysis considerations in this paper can be applied with sufficient accuracy in the analysis and constructive realizations of helicopter rotor in real conditions. The method for unsteady viscous flow simulations by inviscid techniques is developed.The aim of this paper is to determine helicopter rotor blade lift with the highest possible accuracy by using a singularity method and to define an optimal conception model of aerodynamic rotor projection corresponding to rotor behavior in real conditions and with sufficient quality from the aspect of engineer use.}, issn = {0039-2480}, pages = {357-367}, doi = {}, url = {https://www.sv-jme.eu/article/an-optimal-main-helicopter-rotor-projection-model-obtained-by-viscous-effects-and-unsteady-lift-simulation/} }
Mitrović, .,Bengin, A.,Cvetković, D.,Berkić, D. 2010 October 56. An Optimal Main Helicopter Rotor Projection Model Obtained by Viscous Effects and Unsteady Lift Simulation. Strojniški vestnik - Journal of Mechanical Engineering. [Online] 56:6
%A Mitrović, Časlav %A Bengin, Aleksander %A Cvetković, Dragan %A Berkić, Dragoljub %D 2010 %T An Optimal Main Helicopter Rotor Projection Model Obtained by Viscous Effects and Unsteady Lift Simulation %B 2010 %9 unsteady lift; viscous effect simulation; potential flow; lifting surface; panel method; free-wake model; main helicopter rotor aerodynamics; %! An Optimal Main Helicopter Rotor Projection Model Obtained by Viscous Effects and Unsteady Lift Simulation %K unsteady lift; viscous effect simulation; potential flow; lifting surface; panel method; free-wake model; main helicopter rotor aerodynamics; %X This paper presents an airfoil model which provides a method for optimal main helicopter rotor projection by viscous effect and unsteady lift simulation through algorithm and set of program entireties, applicable to the ideological and main project of helicopter rotor. Based on real rotors theoretical consideration and the, numerical analysis considerations in this paper can be applied with sufficient accuracy in the analysis and constructive realizations of helicopter rotor in real conditions. The method for unsteady viscous flow simulations by inviscid techniques is developed.The aim of this paper is to determine helicopter rotor blade lift with the highest possible accuracy by using a singularity method and to define an optimal conception model of aerodynamic rotor projection corresponding to rotor behavior in real conditions and with sufficient quality from the aspect of engineer use. %U https://www.sv-jme.eu/article/an-optimal-main-helicopter-rotor-projection-model-obtained-by-viscous-effects-and-unsteady-lift-simulation/ %0 Journal Article %R %& 357 %P 11 %J Strojniški vestnik - Journal of Mechanical Engineering %V 56 %N 6 %@ 0039-2480 %8 2017-10-24 %7 2017-10-24
Mitrović, Časlav, Aleksander Bengin, Dragan Cvetković, & Dragoljub Berkić. "An Optimal Main Helicopter Rotor Projection Model Obtained by Viscous Effects and Unsteady Lift Simulation." Strojniški vestnik - Journal of Mechanical Engineering [Online], 56.6 (2010): 357-367. Web. 26 Dec. 2024
TY - JOUR AU - Mitrović, Časlav AU - Bengin, Aleksander AU - Cvetković, Dragan AU - Berkić, Dragoljub PY - 2010 TI - An Optimal Main Helicopter Rotor Projection Model Obtained by Viscous Effects and Unsteady Lift Simulation JF - Strojniški vestnik - Journal of Mechanical Engineering DO - KW - unsteady lift; viscous effect simulation; potential flow; lifting surface; panel method; free-wake model; main helicopter rotor aerodynamics; N2 - This paper presents an airfoil model which provides a method for optimal main helicopter rotor projection by viscous effect and unsteady lift simulation through algorithm and set of program entireties, applicable to the ideological and main project of helicopter rotor. Based on real rotors theoretical consideration and the, numerical analysis considerations in this paper can be applied with sufficient accuracy in the analysis and constructive realizations of helicopter rotor in real conditions. The method for unsteady viscous flow simulations by inviscid techniques is developed.The aim of this paper is to determine helicopter rotor blade lift with the highest possible accuracy by using a singularity method and to define an optimal conception model of aerodynamic rotor projection corresponding to rotor behavior in real conditions and with sufficient quality from the aspect of engineer use. UR - https://www.sv-jme.eu/article/an-optimal-main-helicopter-rotor-projection-model-obtained-by-viscous-effects-and-unsteady-lift-simulation/
@article{{}{.}, author = {Mitrović, ., Bengin, A., Cvetković, D., Berkić, D.}, title = {An Optimal Main Helicopter Rotor Projection Model Obtained by Viscous Effects and Unsteady Lift Simulation}, journal = {Strojniški vestnik - Journal of Mechanical Engineering}, volume = {56}, number = {6}, year = {2010}, doi = {}, url = {https://www.sv-jme.eu/article/an-optimal-main-helicopter-rotor-projection-model-obtained-by-viscous-effects-and-unsteady-lift-simulation/} }
TY - JOUR AU - Mitrović, Časlav AU - Bengin, Aleksander AU - Cvetković, Dragan AU - Berkić, Dragoljub PY - 2017/10/24 TI - An Optimal Main Helicopter Rotor Projection Model Obtained by Viscous Effects and Unsteady Lift Simulation JF - Strojniški vestnik - Journal of Mechanical Engineering; Vol 56, No 6 (2010): Strojniški vestnik - Journal of Mechanical Engineering DO - KW - unsteady lift, viscous effect simulation, potential flow, lifting surface, panel method, free-wake model, main helicopter rotor aerodynamics, N2 - This paper presents an airfoil model which provides a method for optimal main helicopter rotor projection by viscous effect and unsteady lift simulation through algorithm and set of program entireties, applicable to the ideological and main project of helicopter rotor. Based on real rotors theoretical consideration and the, numerical analysis considerations in this paper can be applied with sufficient accuracy in the analysis and constructive realizations of helicopter rotor in real conditions. The method for unsteady viscous flow simulations by inviscid techniques is developed.The aim of this paper is to determine helicopter rotor blade lift with the highest possible accuracy by using a singularity method and to define an optimal conception model of aerodynamic rotor projection corresponding to rotor behavior in real conditions and with sufficient quality from the aspect of engineer use. UR - https://www.sv-jme.eu/article/an-optimal-main-helicopter-rotor-projection-model-obtained-by-viscous-effects-and-unsteady-lift-simulation/
Mitrović, Časlav, Bengin, Aleksander, Cvetković, Dragan, AND Berkić, Dragoljub. "An Optimal Main Helicopter Rotor Projection Model Obtained by Viscous Effects and Unsteady Lift Simulation" Strojniški vestnik - Journal of Mechanical Engineering [Online], Volume 56 Number 6 (24 October 2017)
Strojniški vestnik - Journal of Mechanical Engineering 56(2010)6, 357-367
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This paper presents an airfoil model which provides a method for optimal main helicopter rotor projection by viscous effect and unsteady lift simulation through algorithm and set of program entireties, applicable to the ideological and main project of helicopter rotor. Based on real rotors theoretical consideration and the, numerical analysis considerations in this paper can be applied with sufficient accuracy in the analysis and constructive realizations of helicopter rotor in real conditions. The method for unsteady viscous flow simulations by inviscid techniques is developed.The aim of this paper is to determine helicopter rotor blade lift with the highest possible accuracy by using a singularity method and to define an optimal conception model of aerodynamic rotor projection corresponding to rotor behavior in real conditions and with sufficient quality from the aspect of engineer use.