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
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. 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