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
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 677 (= M 6)
3. NACA 2R112
4. S8055 (12%)
5. GA 30A212
6. AMSOIL1 RUTAN CANARD
7. GA 30-212
8. Ritz 2-30-12
9. GA 35A212
10. NACA2312
11. ONERA OA212
12. NACA M6
13. CB2012
14. GA 37A212
15. NACA2212
16. GA 35A213
17. TsAGI B 12.0% thick
18. GA 37A213
19. ZAGI 12
20. LDS-2
21. NACA2412