Similarly shaped airfoils to NACA65A415
New! Bulk download of polars in Excel format: NACA65A415.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. NACA66A415
3. NACA66-415 a=0.8
4. NACA66-515
5. NACA65-415 a=0.8
6. NACA65-515
7. NACA66(2)-415
8. NACA65A416
9. NACA65A414
10. NACA65(2)-415
11. NACA66-415 a=0.6
12. NACA65-416 a=0.8
13. NACA64A416
14. NACA63A415
15. NACA65-516
16. NACA66A414
17. NACA66-414 a=0.8
18. NACA65-415 a=0.6
19. GA 37A315
20. NACA66-514
21. GA 40A315