Similarly shaped airfoils to GA 37A215


New! Bulk download of polars in Excel format: GA%2037A215.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 35A215
2. GA 40A215
3. GA 40-215
4. NACA64A315
5. NACA65-315 a=0.5
6. NACA63A315
7. NACA65-315 a=0.6
8. NACA65-315 a=0.8
9. NACA65-315 a=0.2
10. GA 37-215
11. GA 37A216
12. NACA65-315
13. GA 37A214
14. GA 40A216
15. NACA64-315 a=0.5
16. NLF(1)-0115
17. NACA65A315
18. NACA65-415 a=0.0
19. NACA65-415
20. NACA64-315 a=0.6
21. GA 35A214