Similarly shaped airfoils to FX 72-LS-160


New! Bulk download of polars in Excel format: fx72ls160.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. GOE 592
2. MH 112 16.2%
3. FX 76-MP-140
4. MH 113 14.62%
5. GOE 441
6. FX 72-MS-150A
7. GOE 447
8. GOE 228 (MVA H.38)
9. GOE 482
10. GOE 366
11. EPPLER 421
12. USA 31
13. USA 34
14. JN-153
15. GOE 503
16. USA 32
17. GOE 711
18. UA(2)-180 smoothed
19. GOE 422
20. Joukowsky 16.00% thick 8.00% camber
21. Joukowsky 17.00% thick 8.00% camber