Similarly shaped airfoils to GA 40A412
New! Bulk download of polars in Excel format: GA%2040A412.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 37A412
3. NACA65-512 a=0.5
4. NACA65-512 a=0.6
5. GA 35A412
6. GA 37-412
7. NACA64-512 a=0.5
8. NACA64-512 a=0.6
9. GA 37A411
10. GA 40-413
11. GA 40A413
12. GA 40A411
13. GA 40-411
14. NACA63-512 a=0.5
15. NACA65-511 a=0.5
16. NACA65-512 a=0.8
17. GA 35-412
18. GA 35A411
19. GA 37-413
20. NACA63-512 a=0.6
21. NACA65-612