Similarly shaped airfoils to NACA64-516
New! Bulk download of polars in Excel format: NACA64-516.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. NACA63-516
3. NACA63-416 a=0.8
4. NACA64-416 a=0.6
5. GA 37-316
6. NACA63-416 a=0.6
7. NACA63A416
8. NACA65-516
9. GA 35-316
10. NACA64-517
11. NACA64-515
12. NACA65-416 a=0.8
13. NACA63A415
14. NACA64-415 a=0.8
15. NACA64(2)-415
16. NACA64-417 a=0.8
17. NACA64-416
18. NACA63-515
19. NACA63-517
20. NACA64-616
21. NACA64A416