Similarly shaped airfoils to GOE 409


New! Bulk download of polars in Excel format: goe409.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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1. GOE 459
2. NACA63A013
3. LS(1)-0013
4. GA 30A013
5. GA 35A013
6. GA 30-013
7. NACA0013
8. GOE 411
9. GA 37A013
10. S1012
11. SC(2)-0012
12. RAF 30
13. Ultimate (Carl Goldberg Ultimate Bipe R/C)
14. J5012 12%
15. NACA M3 (NACA-TR-221)
16. NACA M3
17. Horten 13.00% thick 0.00% camber
18. N-13
19. GA 35A014
20. NACA63A014
21. NACA0012-64