Similarly shaped airfoils to NACA42110
New! Bulk download of polars in Excel format: NACA42110.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. NACA42110.5
3. NACA42010
4. NACA42010.5
5. NACA32010
6. NACA32010.5
7. NACA42109
8. NACA33110
9. NACA32110.5
10. NACA24110
11. NACA33110.5
12. NACA32109
13. NACA23110
14. MARSKE PIONEER IID TIP (NACA 431012A*.833 HYBRID)
15. NACA24110.5
16. NACA33010
17. NACA32009
18. NACA33010.5
19. EMX-07
20. NACA23010
21. Horten 10.00% thick 2.00% camber