Similarly shaped airfoils to NACA63-510
New! Bulk download of polars in Excel format: NACA63-510.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. NACA63-410 a=0.8
3. NACA64-410 a=0.8
4. HQ 2.5/10
5. EM J8 2510 DrW
6. EM J20 2510
7. EM J18 2310
8. NACA63A410
9. EPPLER 222
10. NACA63-410 a=0.6
11. NACA65-510
12. NACA64-410 a=0.6
13. HN-1023
14. HQ 2.5/9.0 smoothed by Eppler
15. HQ 2.5/9 B
16. NACA64A410
17. EM L3 2510
18. NACA65-410 a=0.8
19. MH 117 9.8%
20. HN-972
21. HN-969GS