Similarly shaped airfoils to GA 40A613
New! Bulk download of polars in Excel format: GA%2040A613.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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2. GA 37A613
3. GA 35A613
4. NACA65-713 a=0.5
5. GA 37-613
6. NACA65-613 a=0.5
7. NACA65-613 a=0.6
8. NACA65-713 a=0.6
9. NACA64-713 a=0.5
10. GA 40-614
11. GA 37A612
12. GA 40A612
13. GA 40A614
14. GA 40-612
15. GA 35A612
16. GA 37-614
17. NACA64-713 a=0.6
18. EPPLER 434
19. GA 35-613
20. GA 37A614
21. NACA64-613 a=0.6