Similarly shaped airfoils to NACA63-515
New! Bulk download of polars in Excel format: NACA63-515.xlsx
Info | DAT and DXF files | Shape | Venkataraman Fit | Applications (12) | 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. NACA64-515
3. NACA64-415 a=0.8
4. NACA64(2)-415
5. EM J18 2515 DrW r0,8
6. NACA63-415 a=0.6
7. GA 35-315
8. NACA64-415 a=0.6
9. GA 37-315
10. NACA63-516
11. NACA63-514
12. NACA63-414 a=0.8
13. NACA63-416 a=0.8
14. NACA64-514
15. NACA63-415
16. NACA64-516
17. NACA63-615
18. NACA64-414 a=0.8
19. NACA63-415 a=0.5
20. NACA63A415
21. EM CY 1016 20145