The effects of NACA 0012 airfoil modification on aerodynamic performance improvement and obtaining high lift coefficient and post-stall airfoil

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Sogukpinar Haci

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Reference11 articles.

1. C.L. Ladson, “Effects of Independent Variation of Mach and Reynolds Numbers on the Low-Speed Aerodynamic Characteristics of the NACA 0012 Airfoil Section,” NASA TM 4074, 1988.

2. N. Gregory, and C.L. O’Reilly, “Low-Speed Aerodynamic Characteristics of NACA 0012 Aerofoil Section, including the Effects of Upper-Surface Roughness Simulating Hoar Frost,” A.R.C., R. & M. no. 3726, 1970.

3. UÇAK KANATLARINDA EN İDEAL HÜCUM AÇISINI BULMAK İÇİN 4 RAKAMLI NACA 00XX KANAT PROFİLLERİNİN NÜMERİK ANALİZİ

4. Numerical study of passive and active flow separation control over a NACA0012 airfoil

5. H. Sogukpinar, I. Bozkurt, “Calculation of Optimum Angle of Attack to Determine Maximum Lift to Drag Ratio of NACA 632-215 Airfoil,” Journal of Multidisciplinary Engineering Science and Technology, 2, 1103–1108, 2015.

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