Similarly shaped airfoils to FX 61-147
New! Bulk download of polars in Excel format: fx61147.xlsx
Info | DAT and DXF files | Shape | Venkataraman Fit | Applications (1) | 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. HQ 3.5/14
3. NACA63-715
4. NACA64-715
5. FX 75-141
6. HQ 3.0/14
7. NACA63-714
8. EM J18 1 3015
9. DU 80-141
10. HQ 3.0/15
11. NACA64-714
12. FX 63-147
13. FX 63-158
14. EM J18 3015 DrW r0,8
15. NACA63-615 a=0.8
16. MS3,3-15GP
17. NACA64-615 a=0.8
18. NACA63-615
19. NACA63-614 a=0.8
20. NLF(1)-0215F
21. HQ 3.5/13