Similarly shaped airfoils to MH 115 11.06%
New! Bulk download of polars in Excel format: mh115.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. GOE 239 (MVA H.31)
3. FX 63-120
4. NACA6410
5. Joukowsky 12.00% thick 6.00% camber
6. Joukowsky 11.00% thick 6.00% camber
7. GOE 500
8. GOE 330 (PFALZ 59)
9. GOE 480
10. GOE 363
11. EPPLER 395
12. GOE 303 (FRIEDRICHSHAFEN G03)
13. GOE 497
14. Joukowsky 13.00% thick 6.00% camber
15. GOE 165 (MVA MK.11)
16. GOE 190 (MVA MK.18)
17. Joukowsky 10.00% thick 6.00% camber
18. EPPLER 216
19. GOE 501
20. DAE-21
21. GOE 176 (ALBATROS 7020)