Similarly shaped airfoils to GA 40-314
New! Bulk download of polars in Excel format: GA%2040-314.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. NACA65-414 a=0.5
3. NACA65-414 a=0.6
4. GA 37A314
5. GA 35A314
6. GA 37-314
7. NACA65-414 a=0.8
8. NACA64-414 a=0.5
9. NACA64-414 a=0.6
10. NACA65-514
11. NACA65-414 a=0.2
12. GA 40A313
13. NACA65-514 a=0.0
14. GA 40-313
15. GA 40-315
16. NACA64A414
17. GA 40A315
18. GA 37A313
19. NACA65-413 a=0.5
20. NACA65-413 a=0.6
21. NACA65-415 a=0.5