Similarly shaped airfoils to GA 37A412
New! Bulk download of polars in Excel format: GA%2037A412.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 40A412
3. GA 40-412
4. NACA65-512 a=0.5
5. NACA65-512 a=0.6
6. GA 37-412
7. NACA64-512 a=0.5
8. NACA64-512 a=0.6
9. NACA63-512 a=0.5
10. GA 40A413
11. GA 37A413
12. GA 37A411
13. GA 37-413
14. GA 35-412
15. GA 40-413
16. NACA64A512
17. GA 35A411
18. GA 30-412
19. NACA63-512 a=0.6
20. EPPLER 195
21. GA 35A413