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
Dynamic plotter New!
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
Disclaimer: All information presented herein is delivered without guarantee or warranty of any kind. The user assumes the entire risk of use of this information.
2. NACA0012-34
3. N-13
4. S1012
5. N-14
6. NACA M3
7. NACA M3 (NACA-TR-221)
8. NACA/LANGLEY 0011SC SYMMETRICAL, SUPERCRITICAL
9. J5012 12%
10. LWK 80-120/K25
11. GOE 409
12. AH 85-L-120/17
13. EPPLER 836 HYDROFOIL
14. Ultimate (Carl Goldberg Ultimate Bipe R/C)
15. GA 37A013
16. GOE 459
17. NACA66-012
18. GOE 411
19. LS(1)-0013
20. NACA63A013
21. GA 35A013