Similarly shaped airfoils to NACA64A611
New! Bulk download of polars in Excel format: NACA64A611.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. NACA65-611 a=0.8
3. NACA65A611
4. NACA65-711
5. NACA64-611 a=0.8
6. NACA64-711
7. GOE 547
8. NACA63-611 a=0.8
9. NACA64-612 a=0.8
10. NACA63-711
11. NACA64A612
12. NACA65A610
13. NACA64A610
14. SG6042
15. NACA63A610
16. NACA65-612 a=0.8
17. NACA63A612
18. NACA64-712
19. NACA65-712
20. NACA66A611
21. RAF 32 MOD