Similarly shaped airfoils to GA 35A413


New! Bulk download of polars in Excel format: GA%2035A413.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 37A413
2. GA 40A413
3. GA 40-413
4. GA 37-413
5. NACA64-513 a=0.5
6. NACA64-513 a=0.6
7. NACA65-513 a=0.5
8. NACA65-513 a=0.6
9. GA 30-413
10. BOEING 106
11. GA 35-413
12. NACA63-513 a=0.5
13. GA 37-414
14. S4233-136-84
15. CB3013
16. GA 30A413
17. NACA63-513 a=0.6
18. GA 35A412
19. GA 35A414
20. NACA64-514 a=0.5
21. NACA63A513