Similarly shaped airfoils to NACA M12


New! Bulk download of polars in Excel format: m12.xlsx


Info | DAT and DXF files | Shape | Venkataraman Fit | Applications (29) | 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. GOE 676 (= M 12)
2. NACA M12 (NACA-TR-221)
3. GOE 677 (= M 6)
4. NACA 2R112
5. S8055 (12%)
6. GA 30A212
7. AMSOIL1 RUTAN CANARD
8. GA 30-212
9. CB2012
10. Ritz 2-30-12
11. ONERA OA212
12. NACA M6 (NACA-TR-221)
13. NACA M6
14. GA 35A213
15. NACA2312
16. GA 35A212
17. GA 37A213
18. NACA2212
19. GA 37A212
20. LDS-2
21. TsAGI B 12.0% thick