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The Effect of the Hump Position of the Wings on Aerodynamic Parameters

Yıl 2023, Cilt: 5 Sayı: 3, 191 - 200, 13.10.2023
https://doi.org/10.47933/ijeir.1307677

Öz

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.

Kaynakça

  • [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

Kanatlardaki kamburluk konumunun aerodinamik parametrelere etkisi

Yıl 2023, Cilt: 5 Sayı: 3, 191 - 200, 13.10.2023
https://doi.org/10.47933/ijeir.1307677

Öz

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.

Kaynakça

  • [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
Toplam 7 adet kaynakça vardır.

Ayrıntılar

Birincil Dil İngilizce
Konular Mühendislik
Bölüm Research Articles
Yazarlar

Ramazan Selver 0000-0002-9239-8700

Yusuf Can Akar 0000-0002-1408-3404

Erken Görünüm Tarihi 13 Ekim 2023
Yayımlanma Tarihi 13 Ekim 2023
Kabul Tarihi 24 Temmuz 2023
Yayımlandığı Sayı Yıl 2023 Cilt: 5 Sayı: 3

Kaynak Göster

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

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