Similarly shaped airfoils to MH 114 13.02%


New! Bulk download of polars in Excel format: mh114.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 501
2. MID 405w2
3. FX 63-137
4. Joukowsky 14.00% thick 7.00% camber
5. GOE 446
6. Joukowsky 13.00% thick 7.00% camber
7. FX 76-MP-140
8. MH 113 14.62%
9. USA 98
10. MID 405e
11. DAE-11
12. FX 63-137 13.7% smoothed
13. FX 76-MP-120
14. GOE 332 (PFALZ 61)
15. DAE-31
16. DAE-21
17. GOE 405
18. Joukowsky 15.00% thick 7.00% camber
19. Joukowsky 12.00% thick 7.00% camber
20. GOE 528
21. EPPLER 591