Similarly shaped airfoils to GA 37A617
New! Bulk download of polars in Excel format: GA%2037A617.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. GA 40A617
3. GA 40-617
4. NACA65-717 a=0.5
5. EPPLER 583
6. GA 37A618
7. NACA65-717 a=0.6
8. GA 37A616
9. GA 40A618
10. GA 35A616
11. GA 37-617
12. EPPLER 584
13. GA 40-618
14. GA 35A618
15. GOE 367
16. GA 37-618
17. FX 84-W-175
18. GA 40A616
19. NACA65-718 a=0.5
20. NACA64-717 a=0.5
21. GA 40-616