Similarly shaped airfoils to GA 37A311


New! Bulk download of polars in Excel format: GA%2037A311.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
Dynamic plotter New!
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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1. GA 35A311
2. GA 40A311
3. GA 40-311
4. NACA65-411 a=0.5
5. EPPLER 374
6. GA 37-311
7. NACA64-411 a=0.5
8. NACA65-411 a=0.6
9. NACA64-411 a=0.6
10. NACA64A411
11. NACA63A411
12. NACA65-411 a=0.2
13. NACA63-411 a=0.5
14. GA 35-311
15. GA 30-311
16. GA 37-312
17. GA 30A311
18. NACA63-411 a=0.6
19. GA 40A312
20. NACA65-411 a=0.8
21. GA 37A312