Similarly shaped airfoils to NLF-1015
New! Bulk download of polars in Excel format: nlf1015.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
Disclaimer: All information presented herein is delivered without guarantee or warranty of any kind. The user assumes the entire risk of use of this information.
2. FX 62-K-153/20
3. NACA65-715 a=0.8
4. EPPLER 694
5. EPPLER 435
6. NACA65A715
7. NACA64A715
8. NACA65-716 a=0.8
9. EPPLER 662
10. NACA66-715 a=0.8
11. NACA63A715
12. NACA65A714
13. NACA66A715
14. EPPLER STE 87(-3)-914
15. NACA64A716
16. NACA66-714 a=0.8
17. EPPLER 587
18. EPPLER EC 86(-3)-914
19. NACA65A716
20. EPPLER 433
21. NACA66A714