Similarly shaped airfoils to NACA64A411
New! Bulk download of polars in Excel format: NACA64A411.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. NACA65-411 a=0.8
3. NACA65A411
4. NACA65-511
5. NACA64-411 a=0.8
6. NACA64-511
7. GOE 673
8. NACA65-411 a=0.6
9. GA 37A311
10. NACA63-411 a=0.8
11. EM S14 2511
12. GA 35A311
13. GA 40A311
14. NACA65-411
15. EPPLER 211
16. NACA63-511
17. GA 40-311
18. NACA64-411 a=0.6
19. NACA64-412 a=0.8
20. NACA65A410
21. NACA64A412