Similarly shaped airfoils to NLF(2)-0415
New! Bulk download of polars in Excel format: nlf415.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. EPPLER 403
3. NACA66(2)-415
4. NACA66-414
5. NACA66-415
6. EPPLER STF 863-615
7. NACA66-314 a=0.8
8. NACA66A414
9. NACA66A314
10. NACA66A415
11. NACA66-515
12. EPPLER STE 871-514
13. NACA66-514
14. NACA66-315 a=0.8
15. NACA66-414 a=0.8
16. NACA66A315
17. NACA66-415 a=0.8
18. NACA65A415
19. NACA65A315
20. NLF-0414F
21. NACA65A314