Similarly shaped airfoils to NACA63A516
New! Bulk download of polars in Excel format: NACA63A516.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. NACA65-516 a=0.8
3. NACA64-516 a=0.8
4. NACA65-616
5. NACA64-616
6. NACA64-517 a=0.8
7. NACA63A517
8. NACA63A515
9. NACA64A517
10. NACA64-617
11. SG6040
12. GA 35A416
13. NACA64A515
14. GA 37A416
15. NACA63-516 a=0.8
16. NACA65A516
17. NACA63-616
18. NACA65-517 a=0.8
19. NACA65-617
20. USA 48
21. NACA63-517 a=0.8