AERODYNAMIC ANALYSES OF NACA 63-215

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The International Journal of Energy and Engineering Sciences
Volume:5 Issue:2
AERODYNAMIC ANALYSES OF NACA 63-215

AERODYNAMIC ANALYSES OF NACA 63-215

Authors : Ümit KORKMAZ, İbrahim GÖV, Mehmet Hanifi DOĞRU

Pages : 156-166

View : 24 | Download : 30

Publication Date : 2020-10-16

Article Type : Research Paper

Abstract :In this study, aerodynamic performance of NACA 63-215 airfoil was investigated. Aerodynamic performance of the airfoils is changed with respect to angle of attack insert ignore into journalissuearticles values(AoA); values. The AoA increases, the separation of the boundary layers on the upper and lower surface of the wing increases. This situation is effect on the aerodynamic performance. So aerodynamic parameters insert ignore into journalissuearticles values(lift coeff. and drag coeff.); at different AoA values were investigated. Also, flow separation was investigated at different AoA values.
Keywords : Airfoil, Aerodynamic, CFD

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