Similarly shaped airfoils to GA 37-412
New! Bulk download of polars in Excel format: GA%2037-412.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
Disclaimer: All information presented herein is delivered without guarantee or warranty of any kind. The user assumes the entire risk of use of this information.
2. NACA64-512 a=0.5
3. NACA63-512 a=0.5
4. NACA64-512 a=0.6
5. NACA63-512 a=0.6
6. GA 35A412
7. GA 40-412
8. GA 40A412
9. GA 37A412
10. EPPLER 195
11. GA 35A411
12. NACA65-512 a=0.5
13. EPPLER 201
14. BOEING-VERTOL VR-5
15. NACA65-512 a=0.6
16. GA 37-413
17. GA 37-411
18. GA 37A411
19. NACA64-511 a=0.5
20. GA 35-413
21. NACA63-511 a=0.5