Similarly shaped airfoils to NACA63A415
New! Bulk download of polars in Excel format: NACA63A415.xlsx
Info | DAT and DXF files | Shape | Venkataraman Fit | Applications (54) | 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. NACA65-415 a=0.8
3. NACA64-415 a=0.8
4. GA 35A315
5. NACA64-515
6. NACA65-515
7. GA 37A315
8. NACA65(2)-415
9. NACA64-416 a=0.8
10. NACA64(2)-415
11. NACA64-516
12. NACA63A416
13. NACA63A414
14. NACA64A416
15. AVISTAR
16. EM CY 1016 20145
17. NACA63-415 a=0.8
18. NACA65-415 a=0.6
19. CB2515
20. NACA64A414
21. EM J18 2515 DrW r0,8