Similarly shaped airfoils to SB96 10.5/3.0
New! Bulk download of polars in Excel format: SB96%2010.5_3.0.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. EM J19 3010
3. HQ 3.0/10
4. NACA63-611
5. EM J18 3010 26 51
6. NACA63-610
7. NACA63-511 a=0.8
8. NACA63-510 a=0.8
9. NACA64-611
10. NM Classic 12 saumon
11. HQ 3.0/11
12. NACA64-610
13. NACA63A510
14. GOE 546
15. HS 602
16. MID 343
17. MS3,3-11GP
18. K3311 (smoothed)
19. NACA64-511 a=0.8
20. K3311 (original)
21. NACA64-510 a=0.8