Similarly shaped airfoils to NACA63-409 a=0.6
New! Bulk download of polars in Excel format: NACA63-409%20a%3D0.6.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. NACA63-409 a=0.5
3. NACA64-409 a=0.5
4. NACA63-409 a=0.8
5. NACA64-409 a=0.8
6. NACA65-409 a=0.6
7. SD2083 (9.0%)
8. HQ 2.5/9
9. NACA63-509
10. NACA65-409 a=0.5
11. NACA64-509
12. NACA3409
13. HN-424
14. JWL045 9.2/2.7
15. S4053
16. MH 32 8.7%
17. EPPLER 178
18. NACA63A409
19. HN-418
20. HQ 2.5/9 B
21. HQ 2.5/9.0 smoothed by Eppler