Similarly shaped airfoils to NACA0012-64
New! Bulk download of polars in Excel format: NACA0012-64.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. NACA0012-34
3. N-13
4. S1012
5. N-14
6. NACA M3
7. NACA/LANGLEY 0011SC SYMMETRICAL, SUPERCRITICAL
8. J5012 12%
9. LWK 80-120/K25
10. GOE 409
11. AH 85-L-120/17
12. EPPLER 836 HYDROFOIL
13. Ultimate (Carl Goldberg Ultimate Bipe R/C)
14. GA 37A013
15. GOE 459
16. NACA66-012
17. GOE 411
18. LS(1)-0013
19. NACA63A013
20. GA 35A013
21. NACA64-012A