Similarly shaped airfoils to GA 35A416


New! Bulk download of polars in Excel format: GA%2035A416.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 37A416
2. GA 40A416
3. GA 40-416
4. GA 37-416
5. NACA65-516 a=0.5
6. GA 37-417
7. NACA65-516 a=0.6
8. GA 35A415
9. GA 35A417
10. NACA64-516 a=0.6
11. NACA64-516 a=0.5
12. GA 37A417
13. GA 37A415
14. GA 30-416
15. NACA63A516
16. GA 35-416
17. NACA64A516
18. GA 30-415
19. NACA64-517 a=0.6
20. RONCZ 1082T VOYAGER TIP OUTER AFT WING
21. GA 30A416