Similarly shaped airfoils to NACA63-612
New! Bulk download of polars in Excel format: NACA63-612.xlsx
Info | DAT and DXF files | Shape | Venkataraman Fit | Applications (5) | 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. NACA63-512 a=0.8
3. NACA64-512 a=0.8
4. HQ 3.0/12
5. EM J18 3012 DrW r1,2
6. SB96 11.6/3.0
7. EPPLER 853
8. EM J18 3212
9. NACA63A512
10. EPPLER 201
11. NACA63-613
12. NACA63-611
13. HQ 3.0/11
14. NACA65-612
15. NACA64-611
16. NACA64-613
17. NACA64A512
18. NACA63-511 a=0.8
19. NACA63-513 a=0.8
20. NACA63-512 a=0.6
21. NACA63A511