Determination of a Light Helicopter Flight Performance at the Preliminary Design Stage

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2261 Prenosov
Izvoz citacije: ABNT
PETROVIĆ, Zlatko ;STRUPAR, Slobodan ;KOSTIĆ, Ivan ;SIMONOVIĆ, Aleksandar .
Determination of a Light Helicopter Flight Performance at the Preliminary Design Stage. 
Strojniški vestnik - Journal of Mechanical Engineering, [S.l.], v. 56, n.9, p. 535-543, october 2017. 
ISSN 0039-2480.
Available at: <https://www.sv-jme.eu/sl/article/determination-of-a-light-helicopter-flight-performance-at-the-preliminary-design-stage/>. Date accessed: 22 nov. 2019. 
doi:http://dx.doi.org/.
Petrović, Z., Strupar, S., Kostić, I., & Simonović, A.
(2010).
Determination of a Light Helicopter Flight Performance at the Preliminary Design Stage.
Strojniški vestnik - Journal of Mechanical Engineering, 56(9), 535-543.
doi:http://dx.doi.org/
@article{.,
	author = {Zlatko  Petrović and Slobodan  Strupar and Ivan  Kostić and Aleksandar  Simonović},
	title = {Determination of a Light Helicopter Flight Performance at the Preliminary Design Stage},
	journal = {Strojniški vestnik - Journal of Mechanical Engineering},
	volume = {56},
	number = {9},
	year = {2010},
	keywords = {light helicopter; flight performance; preliminary design stage; },
	abstract = {Promising solutions for the problem of the extensively time-consuming modern urban transportation has been found in the use of light and very light helicopters. This paper presents a part of the preliminary design methodology, compiled at the Faculty of Mechanical Engineering, University of Belgrade and includes performance calculations of such helicopters. Due to limited budgets and an extremely demanding process of helicopter development, it is highly significantt that during all development stages reliable performance estimates are obtained in order to ensure assigned operational requirements. The scope of this paper is confined to the preliminary design stage, where it is customary to substitute the very complex helicopter rotor dynamics with its averaged mechanical and aerodynamic characteristics and apply certain empirically verified simplifications. Based on this approach, the independent, efficient and reliable computer programs for the calculation of different performance characteristics have been developed. In addition to their application on an actual on-going project, they have also been applied on several existing helicopters of a similar class for a more accurate determination of the empirical input parameters. The applied methodology and obtained results have been presented, verifying the overall algorithm efficiency.},
	issn = {0039-2480},	pages = {535-543},	doi = {},
	url = {https://www.sv-jme.eu/sl/article/determination-of-a-light-helicopter-flight-performance-at-the-preliminary-design-stage/}
}
Petrović, Z.,Strupar, S.,Kostić, I.,Simonović, A.
2010 October 56. Determination of a Light Helicopter Flight Performance at the Preliminary Design Stage. Strojniški vestnik - Journal of Mechanical Engineering. [Online] 56:9
%A Petrović, Zlatko 
%A Strupar, Slobodan 
%A Kostić, Ivan 
%A Simonović, Aleksandar 
%D 2010
%T Determination of a Light Helicopter Flight Performance at the Preliminary Design Stage
%B 2010
%9 light helicopter; flight performance; preliminary design stage; 
%! Determination of a Light Helicopter Flight Performance at the Preliminary Design Stage
%K light helicopter; flight performance; preliminary design stage; 
%X Promising solutions for the problem of the extensively time-consuming modern urban transportation has been found in the use of light and very light helicopters. This paper presents a part of the preliminary design methodology, compiled at the Faculty of Mechanical Engineering, University of Belgrade and includes performance calculations of such helicopters. Due to limited budgets and an extremely demanding process of helicopter development, it is highly significantt that during all development stages reliable performance estimates are obtained in order to ensure assigned operational requirements. The scope of this paper is confined to the preliminary design stage, where it is customary to substitute the very complex helicopter rotor dynamics with its averaged mechanical and aerodynamic characteristics and apply certain empirically verified simplifications. Based on this approach, the independent, efficient and reliable computer programs for the calculation of different performance characteristics have been developed. In addition to their application on an actual on-going project, they have also been applied on several existing helicopters of a similar class for a more accurate determination of the empirical input parameters. The applied methodology and obtained results have been presented, verifying the overall algorithm efficiency.
%U https://www.sv-jme.eu/sl/article/determination-of-a-light-helicopter-flight-performance-at-the-preliminary-design-stage/
%0 Journal Article
%R 
%& 535
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%J Strojniški vestnik - Journal of Mechanical Engineering
%V 56
%N 9
%@ 0039-2480
%8 2017-10-24
%7 2017-10-24
Petrović, Zlatko, Slobodan  Strupar, Ivan  Kostić, & Aleksandar  Simonović.
"Determination of a Light Helicopter Flight Performance at the Preliminary Design Stage." Strojniški vestnik - Journal of Mechanical Engineering [Online], 56.9 (2010): 535-543. Web.  22 Nov. 2019
TY  - JOUR
AU  - Petrović, Zlatko 
AU  - Strupar, Slobodan 
AU  - Kostić, Ivan 
AU  - Simonović, Aleksandar 
PY  - 2010
TI  - Determination of a Light Helicopter Flight Performance at the Preliminary Design Stage
JF  - Strojniški vestnik - Journal of Mechanical Engineering
DO  - 
KW  - light helicopter; flight performance; preliminary design stage; 
N2  - Promising solutions for the problem of the extensively time-consuming modern urban transportation has been found in the use of light and very light helicopters. This paper presents a part of the preliminary design methodology, compiled at the Faculty of Mechanical Engineering, University of Belgrade and includes performance calculations of such helicopters. Due to limited budgets and an extremely demanding process of helicopter development, it is highly significantt that during all development stages reliable performance estimates are obtained in order to ensure assigned operational requirements. The scope of this paper is confined to the preliminary design stage, where it is customary to substitute the very complex helicopter rotor dynamics with its averaged mechanical and aerodynamic characteristics and apply certain empirically verified simplifications. Based on this approach, the independent, efficient and reliable computer programs for the calculation of different performance characteristics have been developed. In addition to their application on an actual on-going project, they have also been applied on several existing helicopters of a similar class for a more accurate determination of the empirical input parameters. The applied methodology and obtained results have been presented, verifying the overall algorithm efficiency.
UR  - https://www.sv-jme.eu/sl/article/determination-of-a-light-helicopter-flight-performance-at-the-preliminary-design-stage/
@article{{}{.},
	author = {Petrović, Z., Strupar, S., Kostić, I., Simonović, A.},
	title = {Determination of a Light Helicopter Flight Performance at the Preliminary Design Stage},
	journal = {Strojniški vestnik - Journal of Mechanical Engineering},
	volume = {56},
	number = {9},
	year = {2010},
	doi = {},
	url = {https://www.sv-jme.eu/sl/article/determination-of-a-light-helicopter-flight-performance-at-the-preliminary-design-stage/}
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TY  - JOUR
AU  - Petrović, Zlatko 
AU  - Strupar, Slobodan 
AU  - Kostić, Ivan 
AU  - Simonović, Aleksandar 
PY  - 2017/10/24
TI  - Determination of a Light Helicopter Flight Performance at the Preliminary Design Stage
JF  - Strojniški vestnik - Journal of Mechanical Engineering; Vol 56, No 9 (2010): Strojniški vestnik - Journal of Mechanical Engineering
DO  - 
KW  - light helicopter, flight performance, preliminary design stage, 
N2  - Promising solutions for the problem of the extensively time-consuming modern urban transportation has been found in the use of light and very light helicopters. This paper presents a part of the preliminary design methodology, compiled at the Faculty of Mechanical Engineering, University of Belgrade and includes performance calculations of such helicopters. Due to limited budgets and an extremely demanding process of helicopter development, it is highly significantt that during all development stages reliable performance estimates are obtained in order to ensure assigned operational requirements. The scope of this paper is confined to the preliminary design stage, where it is customary to substitute the very complex helicopter rotor dynamics with its averaged mechanical and aerodynamic characteristics and apply certain empirically verified simplifications. Based on this approach, the independent, efficient and reliable computer programs for the calculation of different performance characteristics have been developed. In addition to their application on an actual on-going project, they have also been applied on several existing helicopters of a similar class for a more accurate determination of the empirical input parameters. The applied methodology and obtained results have been presented, verifying the overall algorithm efficiency.
UR  - https://www.sv-jme.eu/sl/article/determination-of-a-light-helicopter-flight-performance-at-the-preliminary-design-stage/
Petrović, Zlatko, Strupar, Slobodan, Kostić, Ivan, AND Simonović, Aleksandar.
"Determination of a Light Helicopter Flight Performance at the Preliminary Design Stage" Strojniški vestnik - Journal of Mechanical Engineering [Online], Volume 56 Number 9 (24 October 2017)

Avtorji

Inštitucije

  • University of Belgrade, Faculty of Mechanical Engineering, Serbia
  • University of Belgrade, Faculty of Mechanical Engineering, Serbia
  • University of Belgrade, Faculty of Mechanical Engineering, Serbia
  • University of Belgrade, Faculty of Mechanical Engineering, Serbia

Informacije o papirju

Strojniški vestnik - Journal of Mechanical Engineering 56(2010)9, 535-543

Promising solutions for the problem of the extensively time-consuming modern urban transportation has been found in the use of light and very light helicopters. This paper presents a part of the preliminary design methodology, compiled at the Faculty of Mechanical Engineering, University of Belgrade and includes performance calculations of such helicopters. Due to limited budgets and an extremely demanding process of helicopter development, it is highly significantt that during all development stages reliable performance estimates are obtained in order to ensure assigned operational requirements. The scope of this paper is confined to the preliminary design stage, where it is customary to substitute the very complex helicopter rotor dynamics with its averaged mechanical and aerodynamic characteristics and apply certain empirically verified simplifications. Based on this approach, the independent, efficient and reliable computer programs for the calculation of different performance characteristics have been developed. In addition to their application on an actual on-going project, they have also been applied on several existing helicopters of a similar class for a more accurate determination of the empirical input parameters. The applied methodology and obtained results have been presented, verifying the overall algorithm efficiency.

light helicopter; flight performance; preliminary design stage;