Similarly shaped airfoils to GA 37-013


New! Bulk download of polars in Excel format: GA%2037-013.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 35-013
2. GA 35A013
3. NACA63A013
4. EPPLER 171
5. GA 40-013
6. GA 40A013
7. GA 37A013
8. RAF 30
9. EPPLER EA 6(-1)-012
10. NACA63A012
11. NACA63-012A
12. GA 35A012
13. NACA64-113 a=0.0
14. NACA64-012
15. NACA64-113
16. GA 37-012
17. NACA63-113 a=0.0
18. GA 37-014
19. NACA63-012
20. GA 37A012
21. NACA63-113