Similarly shaped airfoils to NACA65-411
New! Bulk download of polars in Excel format: NACA65-411.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. NACA64-411
3. NACA65-311 a=0.6
4. NACA64A311
5. NACA64-311 a=0.8
6. NACA63A311
7. NACA65A311
8. NACA65-311 a=0.5
9. NACA63-411
10. NACA64A411
11. NACA64-311 a=0.6
12. NACA65-412
13. NACA65-410
14. NACA65-411 a=0.8
15. NACA66-411
16. NACA63A411
17. NACA64-412
18. NACA63-311 a=0.8
19. NACA65(1)-412
20. GA 40-211
21. GA 40A211