Similarly shaped airfoils to NACA65-515
New! Bulk download of polars in Excel format: NACA65-515.xlsx
Info | DAT and DXF files | Shape | Venkataraman Fit | Applications (2) | 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(2)-415
3. NACA64A415
4. NACA65-415 a=0.6
5. NACA63A415
6. GA 40-315
7. NACA64-515
8. GA 40A315
9. NACA65A415
10. NACA64-415 a=0.8
11. NACA65-516
12. NACA65-514
13. NACA65-414 a=0.8
14. NACA64(2)-415
15. NACA65-416 a=0.8
16. GA 37A315
17. NACA65-415
18. NACA65A414
19. NACA65-415 a=0.5
20. NACA65-615
21. NACA64A414