Similarly shaped airfoils to GA 37A212
New! Bulk download of polars in Excel format: GA%2037A212.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 40A212
3. GA 40-212
4. NACA65-312 a=0.5
5. NACA64A312
6. NACA65-312 a=0.2
7. NACA63A312
8. NACA65-312 a=0.6
9. GA 37-212
10. NACA65(1)-212 a=0.6
11. NACA64-312 a=0.5
12. NACA65-312 a=0.0
13. NACA64-312 a=0.6
14. NACA65-312 a=0.8
15. NACA65-312
16. NACA64-312 a=0.2
17. S8055 (12%)
18. S8052 (11.88%)
19. Europa Dykins 12%
20. BOEING-VERTOL VR-1
21. NACA64-312 a=0.8