Similarly shaped airfoils to NACA0012
New! Bulk download of polars in Excel format: NACA0012.xlsx
Info | DAT and DXF files | Shape | Venkataraman Fit | Applications (289) | 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
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. GA 30A012
3. Horten 12.00% thick 0.00% camber
4. FX 76-120
5. J5012 12%
6. NACA M3
7. RAF 30
8. N-14
9. N-13
10. FX 71-120
11. EPPLER 171
12. EPPLER EA 6(-1)-012
13. GA 35A012
14. NACA63A012
15. NACA63-012A
16. GA 30A011
17. FX 79-L-120
18. GA 30-011
19. Horten 13.00% thick 0.00% camber
20. NACA0013
21. HN-478S