Similarly shaped airfoils to NACA64-515
New! Bulk download of polars in Excel format: NACA64-515.xlsx
Info | DAT and DXF files | Shape | Venkataraman Fit | Applications (1) | 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. NACA63-515
3. NACA64(2)-415
4. NACA63-415 a=0.8
5. NACA64-415 a=0.6
6. GA 37-315
7. NACA63A415
8. NACA65-515
9. NACA63-415 a=0.6
10. NACA65-415 a=0.8
11. EM J18 2515 DrW r0,8
12. NACA63A414
13. NACA65(2)-415
14. NACA64-516
15. GA 35-315
16. NACA64-514
17. NACA64-414 a=0.8
18. NACA64A415
19. NACA64-416 a=0.8
20. NACA63-514
21. NACA64-415