Similarly shaped airfoils to NACA63A311
New! Bulk download of polars in Excel format: NACA63A311.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. NACA64-311 a=0.8
3. NACA65-311 a=0.8
4. GA 35A211
5. NACA63-311 a=0.8
6. GA 37A211
7. SB98 VM5 mid
8. HN-951
9. NACA64-411
10. NACA64-311 a=0.6
11. NACA65A311
12. NACA65-311 a=0.6
13. NACA65-411
14. RG 15A-1.8/11.0
15. TP210-11%
16. EM S104 20107
17. EM CY 1021 18104
18. NACA65-311
19. NACA64-311
20. SG6041
21. HN-980