Similarly shaped airfoils to GA 35A617


New! Bulk download of polars in Excel format: GA%2035A617.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 37A617
2. GA 40A617
3. GA 40-617
4. GA 37-617
5. GA 37-618
6. GA 35A616
7. GA 35A618
8. GA 37A618
9. FX 84-W-175
10. GA 37A616
11. NACA65-717 a=0.5
12. EPPLER 583
13. GOE 367
14. NACA64-717 a=0.5
15. GA 30-617
16. NACA65-717 a=0.6
17. GA 35-617
18. NACA64-717 a=0.6
19. GA 30-616
20. GA 40A618
21. GA 30A616