Similarly shaped airfoils to GA 40A618
New! Bulk download of polars in Excel format: GA%2040A618.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 37A618
3. NACA65-718 a=0.5
4. NACA65-718 a=0.6
5. GA 35A618
6. GA 40A619
7. GA 40A617
8. GA 40-619
9. GA 40-617
10. GA 37A617
11. FX 84-W-175
12. GA 37-618
13. NACA65-717 a=0.5
14. NACA65-719 a=0.5
15. GA 35A617
16. NACA65-719 a=0.6
17. GA 37A619
18. NACA65-717 a=0.6
19. EPPLER 655
20. GA 37-619
21. NACA65-618 a=0.6