Similarly shaped airfoils to GA 40A214
New! Bulk download of polars in Excel format: GA%2040A214.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 37A214
3. NACA65-314 a=0.5
4. NACA65-314 a=0.6
5. NACA65-314 a=0.2
6. GA 35A214
7. NACA65-314 a=0.8
8. NACA65-314
9. NACA64A314
10. GA 37-214
11. NACA65-314 a=0.0
12. NACA65-414 a=0.0
13. NACA64-314 a=0.5
14. NACA65-414
15. NACA63A314
16. NACA64-314 a=0.6
17. GA 40-215
18. GA 40A213
19. GA 40A215
20. GA 37A213
21. GA 40-213