Similarly shaped airfoils to NACA63-410 a=0.8
New! Bulk download of polars in Excel format: NACA63-410%20a%3D0.8.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. NACA63-510
3. NACA64-510
4. HQ 2.5/10
5. NACA63A410
6. EM J8 2510 DrW
7. NACA63-410 a=0.6
8. NACA64-410 a=0.6
9. EM J18 2310
10. EM J20 2510
11. EPPLER 222
12. NACA64A410
13. NACA65-410 a=0.8
14. HN-1023
15. MH 117 9.8%
16. HN-969GS
17. NACA65-510
18. GA 35-310
19. GA 37-310
20. HN-380
21. CB2195