Similarly shaped airfoils to NACA64-610
New! Bulk download of polars in Excel format: NACA64-610.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. NACA64-510 a=0.8
3. NACA63-510 a=0.8
4. NACA65-610
5. NACA63A510
6. NACA64A510
7. NACA65-510 a=0.8
8. HQ 3.0/10
9. EM J8 3010 DrW
10. EM J19 3010
11. NACA63A509
12. SB96 10.5/3.0
13. NACA64-611
14. NACA64-609
15. NACA64A509
16. NACA65-609
17. NACA63-609
18. NACA63-611
19. S7075 (9%)
20. NACA64-509 a=0.8
21. NACA64-510 a=0.6