Similarly shaped airfoils to MH 112 16.2%


New! Bulk download of polars in Excel format: mh112.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 228 (MVA H.38)
2. MH 113 14.62%
3. GOE 441
4. Joukowsky 17.00% thick 8.00% camber
5. FX 72-LS-160
6. GOE 592
7. Joukowsky 16.00% thick 8.00% camber
8. FX 76-MP-140
9. GOE 222 (MVA H.33)
10. Joukowsky 18.00% thick 8.00% camber
11. EPPLER 591
12. Joukowsky 15.00% thick 8.00% camber
13. GOE 242 (MVA PR.2)
14. Joukowsky 17.00% thick 9.00% camber
15. Joukowsky 17.00% thick 7.00% camber
16. Joukowsky 19.00% thick 8.00% camber
17. Joukowsky 18.00% thick 9.00% camber
18. Joukowsky 16.00% thick 7.00% camber
19. FX 72-MS-150A
20. GOE 227 (MVA H.37)
21. Joukowsky 16.00% thick 9.00% camber