Similarly shaped airfoils to MH 113 14.62%


New! Bulk download of polars in Excel format: mh113.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. FX 76-MP-140
2. EPPLER 591
3. MH 112 16.2%
4. GOE 592
5. MH 114 13.02%
6. GOE 441
7. GOE 227 (MVA H.37)
8. Joukowsky 15.00% thick 8.00% camber
9. Joukowsky 16.00% thick 8.00% camber
10. Joukowsky 15.00% thick 7.00% camber
11. FX 73-CL2-152
12. GOE 242 (MVA PR.2)
13. USA 98
14. Joukowsky 14.00% thick 8.00% camber
15. Joukowsky 16.00% thick 7.00% camber
16. FX 76-MP-120
17. GOE 366
18. Joukowsky 14.00% thick 7.00% camber
19. GOE 447
20. GOE 228 (MVA H.38)
21. FX 72-MS-150A