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
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. 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