Similarly shaped airfoils to NACA63-411
New! Bulk download of polars in Excel format: NACA63-411.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. NACA63-311 a=0.8
3. NACA64-311 a=0.8
4. NACA63-311 a=0.6
5. EM S104 20107
6. HN-309
7. HN-808
8. HN-1091b
9. NACA64-311 a=0.6
10. EM CY 1021 18104
11. SB98 VM5 mid
12. HN-951
13. HN-474
14. SB95 10.5/2
15. EM S5 1811 121
16. TP210-11%
17. EM CY 1021 2010 X5 Fertig
18. NACA63-311 a=0.5
19. NACA63A311
20. RG 8
21. RG 15A-1.8/11.0