Similarly shaped airfoils to NACA22110.5
New! Bulk download of polars in Excel format: NACA22110.5.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
3. NACA22010
4. NACA23110.5
5. HM391-2
6. Horten 11.00% thick 1.00% camber
7. Horten 10.00% thick 1.00% camber
8. GIII BL45
9. NACA32110.5
10. GIII BL75
11. HM391-1
12. EPPLER 186
13. NACA23010.5
14. GIII BL86
15. MH 108 11.98%
16. GIII BL0
17. NACA23110
18. EPPLER 228
19. NACA63-111 a=0.0
20. NACA63-111 a=0.2
21. NACA64-111 a=0.0