Similarly shaped airfoils to GA 35-613
New! Bulk download of polars in Excel format: GA%2035-613.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. NACA63-713 a=0.5
3. NACA64-713 a=0.5
4. NACA63-713 a=0.6
5. GA 35A613
6. GA 35-614
7. GA 35-612
8. NACA63-613 a=0.6
9. NACA64-713 a=0.6
10. NACA63-613 a=0.5
11. GA 37-612
12. GOE 426
13. GA 30-612
14. GA 30U-612
15. GA 35A612
16. GA 37-614
17. NACA64-613 a=0.6
18. NACA64-613 a=0.5
19. GA 37A613
20. GA 40-613
21. GA 40A613