Similarly shaped airfoils to GA 40A218
New! Bulk download of polars in Excel format: GA%2040A218.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. NACA65-318 a=0.5
3. NACA65-318 a=0.6
4. GA 37A218
5. NACA65-318 a=0.8
6. NACA65-418
7. NACA64A318
8. GA 35A218
9. NACA65-418 a=0.0
10. NACA65-318 a=0.2
11. NACA65-318
12. EPPLER 544
13. GA 40A219
14. GA 40A217
15. GA 40-219
16. GA 40-217
17. NACA65-418 a=0.2
18. GA 37A217
19. NACA65-319 a=0.5
20. NACA65-319 a=0.6
21. GA 37-218