Similarly shaped airfoils to GOE 677 (= M 6)
New! Bulk download of polars in Excel format: goe677.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
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2. NACA M6
3. NACA M12 (NACA-TR-221)
4. GOE 676 (= M 12)
5. NACA M12
6. ONERA OA212
7. TsAGI B 12.0% thick
8. NACA 2R112
9. ZAGI 12
10. TsAGI B 12.5% thick
11. TsAGI B 11.5% thick
12. RC-12(B)3
13. RAF 34
14. NACA 2R212
15. NACA25012
16. TsAGI B 13.0% thick
17. NACA2212
18. S8055 (12%)
19. GA 30A212
20. Europa Dykins 12%
21. NACA2312