Similarly shaped airfoils to NACA64A612
New! Bulk download of polars in Excel format: NACA64A612.xlsx
Info | DAT and DXF files | Shape | Venkataraman Fit | Applications (2) | 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. NACA65-612 a=0.8
3. NACA65-712
4. NACA65A612
5. NACA64-612 a=0.8
6. NACA64-712
7. EPPLER 67
8. NACA64A613
9. NACA63-612 a=0.8
10. NACA64A611
11. NACA64-613 a=0.8
12. NACA63A611
13. NACA65A611
14. NACA65-613 a=0.8
15. NACA63A613
16. NACA63-712
17. NACA64-713
18. NACA65-713
19. CLARK V
20. HQ 3.5/12
21. NACA65-612 a=0.6