Similarly shaped airfoils to FX 76-MP-140


New! Bulk download of polars in Excel format: fx76mp140.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. MH 113 14.62%
2. GOE 592
3. MH 114 13.02%
4. MH 112 16.2%
5. FX 76-MP-120
6. GOE 447
7. GOE 366
8. GOE 446
9. EPPLER 591
10. GOE 227 (MVA H.37)
11. USA 98
12. FX 72-LS-160
13. Joukowsky 15.00% thick 7.00% camber
14. Joukowsky 15.00% thick 8.00% camber
15. MID 405w2
16. GOE 441
17. Joukowsky 14.00% thick 7.00% camber
18. Joukowsky 16.00% thick 8.00% camber
19. Joukowsky 16.00% thick 7.00% camber
20. UAG 88-143/20
21. Joukowsky 14.00% thick 8.00% camber