Similarly shaped airfoils to GA 37A313
New! Bulk download of polars in Excel format: GA%2037A313.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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2. GA 40A313
3. GA 40-313
4. NACA65-413 a=0.5
5. NACA65-413 a=0.6
6. GA 37-313
7. NACA64-413 a=0.5
8. NACA64A413
9. RAF 38
10. NACA63A413
11. NACA64-413 a=0.6
12. Jedeslsky EJ1
13. EPPLER 231
14. PSU-90-125WL
15. NACA65-413 a=0.8
16. GA 37A312
17. GA 40A314
18. GA 37A314
19. NACA65-413 a=0.2
20. GA 40-314
21. GA 37-314