Similarly shaped airfoils to FX 61-168
New! Bulk download of polars in Excel format: fx61168.xlsx
Info | DAT and DXF files | Shape | Venkataraman Fit | Applications (11) | 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. SG6040
3. FX 61-163
4. NACA63-717
5. NACA64-717
6. NACA63(420)-517
7. NACA63-716
8. NACA64-716
9. FX 60-160
10. NACA63-617
11. NACA64(3)-618
12. NACA64-617
13. NACA63(3)-618
14. NACA63-616
15. SM701
16. NACA64-616
17. FX 61-184
18. GA 35-417
19. GA 37-417
20. NACA64-617 a=0.8
21. NACA63-617 a=0.8