Similarly shaped airfoils to NACA22109
New! Bulk download of polars in Excel format: NACA22109.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 9.00% thick 1.00% camber
3. EH 1.0/9.0
4. NACA22110
5. NACA22010
6. NACA23109
7. MH 110 10.01%
8. Horten 10.00% thick 1.00% camber
9. EH 1.5/9.0
10. NACA23009
11. BOEING VERTOL V(1.95)3009-1.25
12. NACA63-109 a=0.0
13. PW75
14. PW51
15. PW75 sm
16. NACA63-109 a=0.2
17. NACA64-109 a=0.0
18. NACA64-109 a=0.2
19. SIKORSKY SC1095
20. EPPLER 186
21. AZ2005tip