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
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 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