İbrahim Halil GÜZELBEY, Yüksel ERASLAN, Mehmet Hanifi DOĞRU

Numerical Investigation of Different Airfoils at Low Reynolds Number in terms of Aerodynamic Performance of Sailplanes by using XFLR5

Numerical Investigation of Different Airfoils at Low Reynolds Number in terms of Aerodynamic Performance of Sailplanes by using XFLR5

Karadeniz Fen Bilimleri Dergisi

2018-Cilt: 8 - Sayı: 1

47-65

Planör, Kanat tasarımı, Kanat kesit geometrisi, XFLR5, Aerodinamik performans

Sailplane, Wing design, Airfoil, XFLR5, Aerodynamic performance

4222