Similarly shaped airfoils to NACA/LANGLEY 0011SC SYMMETRICAL, SUPERCRITICAL
New! Bulk download of polars in Excel format: n0011sc.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. N-14
3. NACA0012-34
4. N-13
5. NACA M3
6. SC(2)-0012
7. J5012 12%
8. AH 85-L-120/17
9. NACA0010-65
10. S1012
11. NACA66-012
12. LWK 80-120/K25
13. NACA64-012A
14. GIII BL0
15. NACA0010-64
16. NACA67-111 a=0.0
17. GA 37A012
18. GA 30A012
19. NACA67-111
20. NACA67-112 a=0.0
21. NACA63-012A