Similarly shaped airfoils to FX 76-MP-120
New! Bulk download of polars in Excel format: fx76mp120.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. GOE 225 (MVA H.35)
3. MH 114 13.02%
4. GOE 630
5. Joukowsky 13.00% thick 8.00% camber
6. FX 76-MP-140
7. Joukowsky 12.00% thick 8.00% camber
8. GOE 227 (MVA H.37)
9. GOE 226 (MVA H.36)
10. Joukowsky 14.00% thick 8.00% camber
11. MID 405w2
12. MH 113 14.62%
13. DAE-31
14. FX 72-MS-150A
15. GOE 366
16. MID 405e
17. GOE 431
18. Joukowsky 13.00% thick 7.00% camber
19. Joukowsky 11.00% thick 8.00% camber
20. AH 79-100 C
21. Joukowsky 12.00% thick 7.00% camber