Similarly shaped airfoils to NACA63-311 a=0.8
New! Bulk download of polars in Excel format: NACA63-311%20a%3D0.8.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. NACA63-411
3. NACA63-311 a=0.6
4. NACA64-411
5. NACA64-311 a=0.6
6. EM CY 1021 18104
7. NACA63-311 a=0.5
8. TP210-11%
9. NACA63A311
10. NACA63-311
11. GA 35-211
12. HN-951
13. SB95 10.5/2
14. GA 37-211
15. NACA64-311 a=0.5
16. NACA64-311
17. EM S104 20107
18. HQ 1.5/11
19. HN-1091b
20. SB98 VM5 mid
21. RG 15A-1.8/11.0