Similarly shaped airfoils to N-12


New! Bulk download of polars in Excel format: n12.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.

1. SC(2)-0010
2. GA 30A011
3. NACA63A011
4. GA 35A011
5. GA 30-011
6. GA 30A010
7. GA 37A011
8. Horten 11.00% thick 0.00% camber
9. ONERA D, BLUNT TRAILING EDGE
10. ONERA D, SHARP TRAILING EDGE
11. FX 76-100
12. GA 30-010
13. SD8020-010-88
14. NACA0010-64
15. NACA0010
16. HN-478S
17. RAF 27
18. LWK 80-100
19. RAE 103
20. NACA63A010
21. Horten 10.00% thick 0.00% camber