Similarly shaped airfoils to GA 37-410
New! Bulk download of polars in Excel format: GA%2037-410.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. NACA64-510 a=0.5
3. NACA63-510 a=0.5
4. GA 35A410
5. GA 40-410
6. GA 40A410
7. GA 37A410
8. NACA64-510 a=0.6
9. NACA63-510 a=0.6
10. EPPLER 193
11. S3024 9.84%
12. EPPLER E193gU-K24
13. NACA65-510 a=0.5
14. EPPLER EB380
15. GA 30-410
16. NACA65-510 a=0.6
17. S3025 9.38%
18. GA 37-411
19. GA 35-411
20. HQ 3.0/10
21. NACA64-410 a=0.6