TY  - CONF
AU  - Svorcan, Jelena
AU  - Milić, Milica
AU  - Vasić, Vladimir
PY  - 2020
UR  - https://machinery.mas.bg.ac.rs/handle/123456789/4213
AB  - The number of light aircrafts is constantly increasing and this trend will continue in the future with further development of composite technology and hybrid and purely electric propulsion systems. Since these vehicles enable fast and comfortable transport to destinations in the region and will be employed more and more in urban environments, any improvement of aerodynamic performances together with size reduction would be more than beneficial. Therefore, this paper presents a comparative study of aerodynamic performances of two different configurations of lifting surfaces, single vs. double wing since biplane configuration enables more compact aircraft design. Lift and drag coefficients are obtained by simulating flow by finite volume method in ANSYS Fluent. The flow is considered incompressible and viscous. Reynolds-averaged Navier-Stokes equations are closed by transition SST turbulence model. Results are presented in the form of aerodynamic coefficients of lift and drag as well as flow visualizations by velocity contours. Main observations on aerodynamic performances of biplane wings are presented and discussed.
PB  - University of East Sarajevo, Faculty of Mechanical Engineering
C3  - 5th International Scientific Conference on Mechanical Engineering Technologies and Applications COMETa 2020
T1  - Numerical analysis of aerodynamic performances of single vs. double wing (biplane) configuration
EP  - 323
SP  - 315
UR  - https://hdl.handle.net/21.15107/rcub_machinery_4213
ER  - 

@conference{
author = "Svorcan, Jelena and Milić, Milica and Vasić, Vladimir",
year = "2020",
abstract = "The number of light aircrafts is constantly increasing and this trend will continue in the future with further development of composite technology and hybrid and purely electric propulsion systems. Since these vehicles enable fast and comfortable transport to destinations in the region and will be employed more and more in urban environments, any improvement of aerodynamic performances together with size reduction would be more than beneficial. Therefore, this paper presents a comparative study of aerodynamic performances of two different configurations of lifting surfaces, single vs. double wing since biplane configuration enables more compact aircraft design. Lift and drag coefficients are obtained by simulating flow by finite volume method in ANSYS Fluent. The flow is considered incompressible and viscous. Reynolds-averaged Navier-Stokes equations are closed by transition SST turbulence model. Results are presented in the form of aerodynamic coefficients of lift and drag as well as flow visualizations by velocity contours. Main observations on aerodynamic performances of biplane wings are presented and discussed.",
publisher = "University of East Sarajevo, Faculty of Mechanical Engineering",
journal = "5th International Scientific Conference on Mechanical Engineering Technologies and Applications COMETa 2020",
title = "Numerical analysis of aerodynamic performances of single vs. double wing (biplane) configuration",
pages = "323-315",
url = "https://hdl.handle.net/21.15107/rcub_machinery_4213"
}

Svorcan, J., Milić, M.,& Vasić, V.. (2020). Numerical analysis of aerodynamic performances of single vs. double wing (biplane) configuration. in 5th International Scientific Conference on Mechanical Engineering Technologies and Applications COMETa 2020
University of East Sarajevo, Faculty of Mechanical Engineering., 315-323.
https://hdl.handle.net/21.15107/rcub_machinery_4213

Svorcan J, Milić M, Vasić V. Numerical analysis of aerodynamic performances of single vs. double wing (biplane) configuration. in 5th International Scientific Conference on Mechanical Engineering Technologies and Applications COMETa 2020. 2020;:315-323.
https://hdl.handle.net/21.15107/rcub_machinery_4213 .

Svorcan, Jelena, Milić, Milica, Vasić, Vladimir, "Numerical analysis of aerodynamic performances of single vs. double wing (biplane) configuration" in 5th International Scientific Conference on Mechanical Engineering Technologies and Applications COMETa 2020 (2020):315-323,
https://hdl.handle.net/21.15107/rcub_machinery_4213 .