Similarly shaped airfoils to MH 49


New! Bulk download of polars in Excel format: mh49.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. MH 110 10.01%
2. EPPLER 186
3. EPPLER 228
4. RS006m75
5. LWK 79-100
6. RS001t10
7. Joukowsky 10.00% thick 0.00% camber
8. JHSYM-10
9. NACA22110
10. RS001t
11. Horten II Tropfen symmetric 10%
12. RS001m60
13. Joukowsky 11.00% thick 0.00% camber
14. HN-275S
15. HN-477S
16. Horten 10.00% thick 1.00% camber
17. NACA22010
18. NACA63-110 a=0.0
19. FX 79-L-100
20. RAE 100
21. NACA63-110 a=0.2