@article{article_802070, title={AERODYNAMIC ANALYSES OF NACA 63-215}, journal={The International Journal of Energy and Engineering Sciences}, volume={5}, pages={156–166}, year={2020}, author={Korkmaz, Ümit and Göv, İbrahim and Doğru, Mehmet Hanifi}, keywords={Airfoil, Aerodynamic, CFD}, 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 (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 (lift coeff. and drag coeff.) at different AoA values were investigated. Also, flow separation was investigated at different AoA values.}, number={2}, publisher={Gaziantep University}