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
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. 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