Similarly shaped airfoils to MH 106 13.07%
New! Bulk download of polars in Excel format: mh106.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. MJZ1211
3. MH 108 11.98%
4. Horten 13.00% thick 1.00% camber
5. NACA22012
6. NACA23012
7. BOEING 737 MIDSPAN
8. NACA22112
9. GOE 766
10. NACA23112
11. NACA23013
12. NPL 9627
13. NACA63-113 a=0.2
14. NPL 9626
15. NACA63-113 a=0.0
16. NACA22013
17. NACA63-213 a=0.0
18. Ritz 1-30-12
19. NACA63-113 a=0.5
20. NACA23113
21. NACA22113