Similarly shaped airfoils to GA 35-611
New! Bulk download of polars in Excel format: GA%2035-611.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. GA 35A611
3. NACA63-611 a=0.5
4. NACA63-611 a=0.6
5. NACA63-711 a=0.5
6. NACA64-611 a=0.5
7. S4310
8. NACA64-611 a=0.6
9. NACA64-711 a=0.5
10. GA 37A611
11. GA 40-611
12. GA 30-610
13. GA 40A611
14. GA 35-610
15. GA 35-612
16. GA 35A610
17. GA 37-610
18. NACA63-711 a=0.6
19. GA 30-611
20. GA 37-612
21. GA 30A610