Similarly shaped airfoils to NACA63A612
New! Bulk download of polars in Excel format: NACA63A612.xlsx
Info | DAT and DXF files | Shape | Venkataraman Fit | Applications (4) | 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. NACA64-612 a=0.8
3. NACA65-612 a=0.8
4. EPPLER 67
5. NACA65-712
6. NACA64-712
7. NACA63-612 a=0.8
8. NACA65A612
9. NACA64-613 a=0.8
10. NACA63-712
11. HQ 3.5/12
12. NACA64-713
13. NACA63A613
14. NACA63A611
15. NACA64A613
16. NACA63-613 a=0.8
17. NACA64A611
18. CB3512
19. CLARK V
20. NACA65-613 a=0.8
21. NACA63-713