Similarly shaped airfoils to NACA0012-34
New! Bulk download of polars in Excel format: NACA0012-34.xlsx
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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2. NACA0012-64
3. NACA66-012
4. EPPLER 836 HYDROFOIL
5. LWK 80-120/K25
6. NACA/LANGLEY 0011SC SYMMETRICAL, SUPERCRITICAL
7. SC(2)-0012
8. N-13
9. N-14
10. NACA64-012A
11. R140 12.04% (smoothed)
12. NACA M3
13. GA 37A013
14. R140 (original)
15. NACA66-112 a=0.0
16. S1012
17. NACA66-112
18. J5012 12%
19. GA 37A012
20. GA 40A013
21. NACA67-112 a=0.0