Similarly shaped airfoils to NACA32110


New! Bulk download of polars in Excel format: NACA32110.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
Dynamic plotter New!
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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1. NACA42010
2. NACA32010
3. NACA42110
4. NACA42010.5
5. NACA32010.5
6. NACA42110.5
7. NACA23110
8. NACA24110
9. NACA24110.5
10. NACA32110.5
11. NACA32109
12. NACA23010
13. NACA42109
14. NACA23010.5
15. NACA32009
16. NACA24010
17. Horten 10.00% thick 2.00% camber
18. NACA33110
19. BOEING-VERTOL V23010-1.58
20. NACA24010.5
21. MARSKE PIONEER IID TIP (NACA 431012A*.833 HYBRID)