Similarly shaped airfoils to NACA64-510
New! Bulk download of polars in Excel format: NACA64-510.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. NACA64-410 a=0.8
3. NACA63-410 a=0.8
4. NACA65-510
5. HQ 2.5/10
6. NACA63A410
7. NACA65-410 a=0.8
8. NACA64A410
9. EM J8 2510 DrW
10. NACA64-410 a=0.6
11. NACA63-410 a=0.6
12. EM J18 2310
13. EPPLER 852
14. EPPLER 222
15. HQ 2.5/9.0 smoothed by Eppler
16. HQ 2.5/9 B
17. NACA63A409
18. EM J20 2510
19. HN-1023
20. NACA64-511
21. NACA64-509