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
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. GOE 676 (= M 12)
3. NACA M12
4. ONERA OA212
5. TsAGI B 12.0% thick
6. NACA 2R112
7. ZAGI 12
8. TsAGI B 12.5% thick
9. TsAGI B 11.5% thick
10. RC-12(B)3
11. RAF 34
12. NACA 2R212
13. NACA25012
14. TsAGI B 13.0% thick
15. NACA2212
16. S8055 (12%)
17. GA 30A212
18. Europa Dykins 12%
19. NACA2312
20. GA 30-212
21. NACA25112