An Optimal Main Helicopter Rotor Projection Model Obtained by Viscous Effects and Unsteady Lift Simulation

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Izvoz citacije: ABNT
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/sl/article/an-optimal-main-helicopter-rotor-projection-model-obtained-by-viscous-effects-and-unsteady-lift-simulation/>. Date accessed: 17 apr. 2021. 
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/sl/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/sl/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.  17 Apr. 2021
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/sl/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/sl/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/sl/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)

Avtorji

Inštitucije

  • University of Belgrade, Faculty of Mechanical Engineering, Serbia
  • University of Belgrade, Faculty of Mechanical Engineering, Serbia
  • University "Singidunum" Belgrade, Faculty of Informatics and Management, Serbia
  • University of Belgrade, Faculty of Mechanical Engineering, Serbia

Informacije o papirju

Strojniški vestnik - Journal of Mechanical Engineering 56(2010)6, 357-367

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.

unsteady lift; viscous effect simulation; potential flow; lifting surface; panel method; free-wake model; main helicopter rotor aerodynamics;