Similarly shaped airfoils to SD6060-104-88
New! Bulk download of polars in Excel format: sd6060.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. SB95 10.5/2
3. NACA64-311 a=0.5
4. GA 37-211
5. GA 35A211
6. NACA63-311 a=0.5
7. GA 30-210
8. GA 35A210
9. NACA64-311 a=0.6
10. SB98 VM5 mid
11. GA 35-211
12. GA 37A211
13. GA 30A210
14. NACA63-311 a=0.6
15. EM CY 1025 20098
16. NACA64-411 a=0.0
17. RAF 28
18. NACA2410
19. EPPLER 374
20. NACA63-411 a=0.0
21. GA 37A210