Similarly shaped airfoils to NACA22110
New! Bulk download of polars in Excel format: NACA22110.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. NACA22110.5
3. NACA22010.5
4. NACA23110.5
5. Horten 10.00% thick 1.00% camber
6. HM391-2
7. NACA22109
8. GIII BL75
9. EPPLER 186
10. NACA32110.5
11. GIII BL86
12. NACA23110
13. MH 110 10.01%
14. Horten 11.00% thick 1.00% camber
15. GIII BL45
16. EPPLER 228
17. SIKORSKY SC1095
18. NACA22009
19. NACA23010
20. Horten 9.00% thick 1.00% camber
21. HM391-1