Similarly shaped airfoils to GA 37A312
New! Bulk download of polars in Excel format: GA%2037A312.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 40A312
3. GA 40-312
4. NACA65-412 a=0.5
5. NACA65-412 a=0.6
6. GA 37-312
7. NACA64-412 a=0.5
8. NACA64-412 a=0.6
9. NACA64A412
10. NACA63A412
11. LDS-2
12. A7026
13. NACA65-412 a=0.2
14. NACA65-412 a=0.8
15. GA 40A313
16. NACA63-412 a=0.5
17. GA 37A313
18. GA 37A311
19. GA 37-313
20. NACA65(1)-412
21. GA 35-312