Similarly shaped airfoils to GA 37A414
New! Bulk download of polars in Excel format: GA%2037A414.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
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 40A414
3. GA 40-414
4. NACA65-514 a=0.5
5. NACA65-514 a=0.6
6. MRC-16
7. AH 79-K-135/20 B
8. GA 37-414
9. NACA64-514 a=0.5
10. NACA64-514 a=0.6
11. GA 37A413
12. GA 37A415
13. GA 40A415
14. GA 35A413
15. NACA64A514
16. GA 40-415
17. GA 37-415
18. GA 35A415
19. BOEING 106
20. NACA63A514
21. GA 30-413.5