Similarly shaped airfoils to GA 37-014


New! Bulk download of polars in Excel format: GA%2037-014.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 35-014
2. GA 35A014
3. NACA63A014
4. GA 40-014
5. GA 40A014
6. GA 37A014
7. NACA64-114 a=0.0
8. DU 86-137/25
9. NACA63A013
10. GA 35A013
11. LS(1)-0013
12. NACA64-114
13. NACA64-015
14. NACA63-114 a=0.0
15. GA 37-013
16. GA 37-015
17. NACA63-114
18. NACA64-114 a=0.2
19. GA 37A013
20. NACA63-015
21. GA 35-015