Similarly shaped airfoils to MH 46 9.1%
New! Bulk download of polars in Excel format: mh46.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
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2. MH 62 9.3%
3. PW51 sm
4. MH 44 9.66%
5. JWL075 8.8/1.76
6. PW98 sm
7. MH 64 8.59%
8. SM8516m
9. TL55
10. RS004a
11. MH 42 8.94%
12. MH 43 8.5%
13. AZ2004_9
14. MVE8.516
15. NACA63-209 a=0.5
16. NACA63-309 a=0.0
17. DD928416
18. MH 45 9.85%
19. NACA63-209 a=0.2
20. AZ2002root
21. MVE8516f3