Similarly shaped airfoils to NACA64-517


Direct link: NACA64-517
Info | DAT and DXF files | Shape | Venkataraman Fit | Applications (0) | Similarly shaped airfoils
Plain Flapped Shapes: 25% flap chord | 30% flap chord | 35% flap chord | 40% flap chord
Basic Data: cl vs α | cd vs α | cm vs α | cl/cd vs α | cd vs cl | cl/cd vs cl | cl vs cd | cm vs cl | Curve fits | Lift curve slopes
Data source comparison (Codes, CFD, Wind tunnel)
Compressibility Effects: cl vs α | cd vs α | cm vs α | cl/cd vs α | cd vs cl | cl/cd vs cl | cl vs cd | cm vs cl
Roughness Effects: cl vs α | cd vs α | cm vs α | cl/cd vs α | cd vs cl | cl/cd vs cl | cl vs cd | cm vs cl
Plain Flap Effects: cl,max vs flap deflection: all flap chords | 25% flap chord | 30% flap chord | 35% flap chord | 40% flap chord
Plain Flap Effects: cl vs α for various flap deflections: 25% flap chord | 30% flap chord | 35% flap chord | 40% flap chord
Plain Flap Effects: cm vs α for various flap deflections: 25% flap chord | 30% flap chord | 35% flap chord | 40% flap chord
Plain Flap Effects: cd vs α for various flap deflections: 25% flap chord | 30% flap chord | 35% flap chord | 40% flap chord

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1. NACA64-417 a=0.8
2. NACA63-517
3. NACA63-417 a=0.8
4. NACA64-417 a=0.6
5. GA 37-317
6. NACA63-417 a=0.6
7. NACA64-518
8. NACA64-516
9. GA 35-317
10. NACA64-416 a=0.8
11. NACA63A417
12. NACA63A416
13. NACA64-418 a=0.8
14. NACA65-517
15. NACA64-417
16. NACA65-417 a=0.8
17. NACA64(3)-418
18. NACA64-617
19. NACA63-516
20. NACA63-518
21. NACA64-417 a=0.5