Similarly shaped airfoils to FX 61-163
New! Bulk download of polars in Excel format: fx61163.xlsx
Info | DAT and DXF files | Shape | Venkataraman Fit | Applications (34) | 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 61-168
3. SG6040
4. NACA63-616
5. NACA64-616
6. NACA63-516
7. NACA63(420)-517
8. NACA63-617
9. NACA64-617
10. NACA64-516
11. NN7 MK20
12. NACA63-516 a=0.8
13. NACA64-516 a=0.8
14. GA 35-316
15. GA 37-316
16. EM J18 2515 DrW r0,8
17. HQ 3.0/15
18. NACA63-517
19. NACA63-416 a=0.8
20. NACA63-517 a=0.8
21. GA 35-416