Similarly shaped airfoils to NACA65-516
New! Bulk download of polars in Excel format: NACA65-516.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. NACA64A416
3. NACA65-416 a=0.6
4. GA 40-316
5. GA 40A316
6. NACA63A416
7. NACA64-516
8. NACA65-517
9. NACA65-515
10. NACA65A416
11. NACA65-415 a=0.8
12. NACA64-416 a=0.8
13. NACA65-417 a=0.8
14. NACA65-416
15. GA 37A316
16. NACA65-616
17. NACA65(2)-415
18. NACA65-416 a=0.5
19. NACA64A415
20. NACA65A415
21. NACA64-517