Similarly shaped airfoils to NACA22010
New! Bulk download of polars in Excel format: NACA22010.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. NACA22010.5
3. NACA22110.5
4. Horten 10.00% thick 1.00% camber
5. NACA23110.5
6. HM391-2
7. NACA22109
8. GIII BL75
9. SIKORSKY SC1095
10. GIII BL86
11. Horten 11.00% thick 1.00% camber
12. EPPLER 226
13. GIII BL45
14. EPPLER 228
15. EPPLER 186
16. NACA22009
17. NACA23110
18. Ritz 1-30-10
19. NACA23010
20. Horten 9.00% thick 1.00% camber
21. NACA63-110 a=0.0