Similarly shaped airfoils to MH 108 11.98%
New! Bulk download of polars in Excel format: mh108.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. Horten 11.00% thick 1.00% camber
3. GOE 766
4. MJZ1211
5. Horten 12.00% thick 1.00% camber
6. HM391-1
7. GOE 767
8. NACA22012
9. NACA23012
10. NACA22010.5
11. HM391-2
12. NACA22110.5
13. NACA22112
14. NACA23112
15. Borge-b3
16. NACA23110.5
17. BOEING 737 MIDSPAN
18. Horten 11.00% thick 2.00% camber
19. JWL081 11/1.3
20. Horten 12.00% thick 2.00% camber
21. Ritz 1-30-12