Similarly shaped airfoils to FX 66-H-159


New! Bulk download of polars in Excel format: FX%2066-H-159.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. Horten 15.00% thick 4.00% camber
2. HG 41
3. SSV2316 VANS RV-10
4. NACA35115
5. EPPLER 342
6. Horten 16.00% thick 4.00% camber
7. NACA 5-H-15
8. Horten 14.00% thick 4.00% camber
9. HG 42
10. HG 40
11. NACA 747A315
12. NACA35114.5
13. Horten 15.00% thick 5.00% camber
14. EPPLER 341
15. NACA44015
16. NACA35116
17. NACA45015
18. NACA35015
19. TsAGI B 15.0% thick
20. NACA44014.5
21. NACA35114