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The Effect of the Hump Position of the Wings on Aerodynamic Parameters
Abstract
In this article, the aerodynamic performances of 3D wings coded NACA 6415 and NACA 6615 are investigated at different angles of attack and speeds. Analyzes were performed at 200 km/h and 700 km/h speeds, between 0 and 36 degrees angle of attack. The obtained results showed the changes in lift, drag and moment coefficients depending on the angle of attack and speed of the wings. In addition, it was determined that the highest lift/drag ratios for both wing types were obtained at 0 degrees angle of attack. These results can be used as a reference source for the aerospace industry.
Keywords
References
- [1] Genç M. S., Özışık G., N. Kahraman, “Investigation of the Aerodynamic Performance of NACA 0012 Wing Profile with Plain Flaps” J. of Thermal Science and Technology, s1-8, 2008.
- [2] Gökdemir M., ÜRGÜN S., “Aerodynamic Analysis of Wing Profiles with Similar Camber”, Journal of Aviation, s25-35, 2020.
- [3] Güçlü M. C., Aerodynamic Performance Analysis and Control of Flow Over Airplane Wings: A Master's Thesis in the Institute of Science and Technology at TOBB University of Economics and Technology, Ankara, Türkiye, 2019.
- [4] Akar Y.C., Selver R., Başekin M., “Effect of Hump Ratio of The Wings on Aerodynamic Parameters” 4th International 5 Ocak congress on Applied Sciences Proceeding Book, 5-6 Jan 2023, s.66-74, https://www.inbak.org/_files/ugd/614b1f_b24fcbb45f544624884760221f300690.pdf
- [5] AirfoilTools, Coordinates of NACA 4415, http://airfoiltools.com/airfoil/details?airfoil=naca4415-il,
- [6] Davis J.R. ASM International “Metals Handbook Properties and Selection: Nonferrous Alloys and Special-Purpose Materials Vol.2”, 10th Ed. 1990
- [7] Akar Y.C. and Selver R., “The Effect of High-Speed Aif Flows on Different Airfoils”, Dicle University Journal of the Institute of Natural and Applied Science c.12, Vol.1, s.65-94, Jun 2023, doi:10.55007/dufed.1129899
Details
Primary Language
English
Subjects
Engineering
Journal Section
Research Article
Early Pub Date
October 13, 2023
Publication Date
October 13, 2023
Submission Date
May 31, 2023
Acceptance Date
July 24, 2023
Published in Issue
Year 2023 Volume: 5 Number: 3
APA
Selver, R., & Akar, Y. C. (2023). The Effect of the Hump Position of the Wings on Aerodynamic Parameters. International Journal of Engineering and Innovative Research, 5(3), 191-200. https://doi.org/10.47933/ijeir.1307677
AMA
1.Selver R, Akar YC. The Effect of the Hump Position of the Wings on Aerodynamic Parameters. IJEIR. 2023;5(3):191-200. doi:10.47933/ijeir.1307677
Chicago
Selver, Ramazan, and Yusuf Can Akar. 2023. “The Effect of the Hump Position of the Wings on Aerodynamic Parameters”. International Journal of Engineering and Innovative Research 5 (3): 191-200. https://doi.org/10.47933/ijeir.1307677.
EndNote
Selver R, Akar YC (October 1, 2023) The Effect of the Hump Position of the Wings on Aerodynamic Parameters. International Journal of Engineering and Innovative Research 5 3 191–200.
IEEE
[1]R. Selver and Y. C. Akar, “The Effect of the Hump Position of the Wings on Aerodynamic Parameters”, IJEIR, vol. 5, no. 3, pp. 191–200, Oct. 2023, doi: 10.47933/ijeir.1307677.
ISNAD
Selver, Ramazan - Akar, Yusuf Can. “The Effect of the Hump Position of the Wings on Aerodynamic Parameters”. International Journal of Engineering and Innovative Research 5/3 (October 1, 2023): 191-200. https://doi.org/10.47933/ijeir.1307677.
JAMA
1.Selver R, Akar YC. The Effect of the Hump Position of the Wings on Aerodynamic Parameters. IJEIR. 2023;5:191–200.
MLA
Selver, Ramazan, and Yusuf Can Akar. “The Effect of the Hump Position of the Wings on Aerodynamic Parameters”. International Journal of Engineering and Innovative Research, vol. 5, no. 3, Oct. 2023, pp. 191-00, doi:10.47933/ijeir.1307677.
Vancouver
1.Ramazan Selver, Yusuf Can Akar. The Effect of the Hump Position of the Wings on Aerodynamic Parameters. IJEIR. 2023 Oct. 1;5(3):191-200. doi:10.47933/ijeir.1307677
