Similarly shaped airfoils to NACA66-012
New! Bulk download of polars in Excel format: NACA66-012.xlsx
Info | DAT and DXF files | Shape | Venkataraman Fit | Applications (1) | 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. NACA0012-34
3. LWK 80-120/K25
4. EPPLER 836 HYDROFOIL
5. NACA66-112 a=0.0
6. NACA66-112
7. NACA66-112 a=0.2
8. NACA65-012
9. NACA0012-64
10. GA 40A012
11. GA 40-012
12. NACA64-012A
13. GA 40A013
14. NACA66A112
15. GA 40-013
16. R140 12.04% (smoothed)
17. NACA66-112 a=0.8
18. S1012
19. R140 (original)
20. GA 37A012
21. NACA66-112 a=0.5