Similarly shaped airfoils to NACA63(420)-517
New! Bulk download of polars in Excel format: NACA63%28420%29-517.xlsx
Info | DAT and DXF files | Shape | Venkataraman Fit | Applications (3) | 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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2. NACA64-617
3. NACA63-517 a=0.8
4. NACA64-517 a=0.8
5. SG6040
6. NACA63-618
7. NACA64-618
8. NACA63A517
9. NACA63-518 a=0.8
10. NN7 MK20
11. NACA63-517
12. NACA64-518 a=0.8
13. NACA63-717
14. NACA64-717
15. NACA63-616
16. NACA63A516
17. EPPLER 552
18. GA 35-417
19. NACA64-616
20. NACA64-517
21. GA 37-417