Similarly shaped airfoils to GA 37-312
New! Bulk download of polars in Excel format: GA%2037-312.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. NACA64-412 a=0.5
3. NACA63-412 a=0.5
4. NACA64-412 a=0.6
5. NACA63-412 a=0.6
6. GA 35A312
7. GA 40-312
8. GA 40A312
9. GA 37A312
10. EPPLER 207
11. NACA64-412 a=0.8
12. GA 35A311
13. NACA64-412 a=0.2
14. NACA63-412 a=0.8
15. NACA65-412 a=0.5
16. NM32 root
17. NACA63-412 a=0.2
18. NACA64-512
19. NACA63-512
20. NACA65-412 a=0.6
21. GA 37-313