Similarly shaped airfoils to NACA63-611
New! Bulk download of polars in Excel format: NACA63-611.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. NACA63-511 a=0.8
3. NACA64-511 a=0.8
4. HQ 3.0/11
5. SB96 10.5/3.0
6. NACA63A511
7. NACA65-611
8. SB96 11.6/3.0
9. EPPLER 853
10. NACA64A511
11. NACA63-612
12. NACA63-610
13. HQ 3.0/10
14. EM J8 3010 DrW
15. NACA65-511 a=0.8
16. NACA64-610
17. K3311 (smoothed)
18. NACA64-612
19. NACA63A510
20. NACA63-510 a=0.8
21. K3311 (original)