Similarly shaped airfoils to FX 61-184
New! Bulk download of polars in Excel format: fx61184.xlsx
Info | DAT and DXF files | Shape | Venkataraman Fit | Applications (43) | 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. NACA63(3)-618
3. NACA64-718
4. NACA63-718
5. NACA64-719
6. NACA63-719
7. EPPLER 1098
8. FX S 03-182
9. NACA64-618 a=0.8
10. NACA63-618
11. NACA64-618
12. DU 80-176 V1
13. NACA63-618 a=0.8
14. NN7 MK20
15. NACA64-619 a=0.8
16. HQ 3.5/18
17. NACA63-518 a=0.8
18. NACA65-718
19. NACA64-518 a=0.8
20. NACA63-619 a=0.8
21. EPPLER 1200