Similarly shaped airfoils to GOE 676 (= M 12)


New! Bulk download of polars in Excel format: goe676.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. NACA M12
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. Ritz 2-30-12
10. GA 35A212
11. NACA2312
12. ONERA OA212
13. NACA M6 (NACA-TR-221)
14. NACA M6
15. CB2012
16. GA 37A212
17. NACA2212
18. GA 35A213
19. TsAGI B 12.0% thick
20. GA 37A213
21. ZAGI 12