Similarly shaped airfoils to GA 37A314


New! Bulk download of polars in Excel format: GA%2037A314.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
Dynamic plotter New!
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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1. GA 35A314
2. GA 40A314
3. GA 40-314
4. NACA65-414 a=0.5
5. NACA65-414 a=0.6
6. NACA64A414
7. GA 37-314
8. NACA63A414
9. NACA64-414 a=0.5
10. NACA64-414 a=0.6
11. GA 37A313
12. NACA65-414 a=0.8
13. GA 37A315
14. GA 40A315
15. GA 35A313
16. GA 40-315
17. NACA65-514
18. GA 37-315
19. GA 35A315
20. NACA65-414 a=0.2
21. Jedeslsky EJ1