Similarly shaped airfoils to MH 122 9.32%
New! Bulk download of polars in Excel format: mh122.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. NACA64A509
3. NACA65-609
4. NACA64-610
5. MH 121 8.76%
6. NACA65-610
7. NACA65-509 a=0.8
8. NACA65A509
9. NACA64-510 a=0.8
10. NACA64-609
11. NACA64A510
12. NACA63-610
13. NACA63A510
14. NACA65-510 a=0.8
15. NACA64-509 a=0.8
16. NACA63-609
17. NACA63-510 a=0.8
18. NACA63-509 a=0.8
19. NACA64-710
20. NACA66-609
21. EM J19 3010