Similarly shaped airfoils to NLF(1)-0416


New! Bulk download of polars in Excel format: nlf416.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
Dynamic plotter New!
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.

1. FX 61-163
2. EM J18 2515 DrW r0,8
3. NACA63-516
4. NACA63-616
5. MS2.5/15GPV
6. SG6040
7. EPPLER 556
8. NACA64-616
9. NACA63-416 a=0.8
10. MID 393 UL
11. NACA64-516
12. NACA63-515
13. EM J18 3015 DrW r0,8
14. NACA63-516 a=0.8
15. HQ 3.0/15
16. GA 35-316
17. NACA63-615
18. NACA63-617
19. NACA63(420)-517
20. FX 61-168
21. NACA63-517