Similarly shaped airfoils to GA 37A611
New! Bulk download of polars in Excel format: GA%2037A611.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 40A611
3. GA 40-611
4. GA 37-611
5. NACA65-611 a=0.5
6. NACA65-611 a=0.6
7. GA 35-611
8. GA 30-611
9. NACA64-611 a=0.5
10. NACA65-711 a=0.5
11. NACA64-611 a=0.6
12. GA 37-612
13. GA 30A611
14. GA 40A612
15. NACA64-711 a=0.5
16. GA 37A612
17. GA 37A610
18. GA 40-612
19. GA 35A610
20. GA 35A612
21. NACA63-611 a=0.5