TY  - JOUR
T1  - The Effect of the Hump Position of the Wings on Aerodynamic Parameters
TT  - Kanatlardaki kamburluk konumunun aerodinamik parametrelere etkisi
AU  - Akar, Yusuf Can
AU  - Selver, Ramazan
PY  - 2023
DA  - October
Y2  - 2023
DO  - 10.47933/ijeir.1307677
JF  - International Journal of Engineering and Innovative Research
JO  - IJEIR
PB  - Ahmet Ali SÜZEN
WT  - DergiPark
SN  - 2687-2153
SP  - 191
EP  - 200
VL  - 5
IS  - 3
LA  - en
AB  - 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.
KW  - Airfoil
KW  - Numerical analysis
KW  - Aerodynamic
KW  - High flow rate
KW  - Hump position
N2  - Bu makalede, farklı hücum açıları ve hızlarda kodlanmış NACA 6415 ve NACA 6615 3D kanatların aerodinamik performansları incelenmektedir. Analizler, 0 ila 36 derece hücum açısı arasında 200 km/sa ve 700 km/sa hızlarda gerçekleştirilmiştir. Elde edilen sonuçlar, kanatların hücum açısı ve hızına bağlı olarak kaldırma, sürükleme ve moment katsayılarında değişikliklerin olduğunu göstermektedir. Ayrıca, her iki kanat tipi için en yüksek kaldırma/sürükleme oranının 0 derece hücum açısında elde edildiği belirlenmiştir. Bu sonuçlar havacılık endüstrisi için bir referans kaynağı olarak kullanılabilir.
CR  - [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.
CR  - [2]	Gökdemir M., ÜRGÜN S., “Aerodynamic Analysis of Wing Profiles with Similar Camber”, Journal of Aviation, s25-35, 2020.
CR  - [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.
CR  - [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
CR  - [5]	AirfoilTools, Coordinates of NACA 4415, http://airfoiltools.com/airfoil/details?airfoil=naca4415-il,
CR  - [6]	Davis J.R. ASM International “Metals Handbook Properties and Selection: Nonferrous Alloys and Special-Purpose Materials Vol.2”, 10th Ed. 1990
CR  - [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
UR  - https://doi.org/10.47933/ijeir.1307677
L1  - https://dergipark.org.tr/en/download/article-file/3179508
ER  -