Similarly shaped airfoils to NACA42010.5
New! Bulk download of polars in Excel format: NACA42010.5.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. NACA42010
3. NACA42110.5
4. NACA32110
5. NACA32010
6. NACA42110
7. NACA24110.5
8. NACA24110
9. NACA33010.5
10. NACA33110.5
11. NACA32110.5
12. NACA23110
13. NACA24010.5
14. NACA23010.5
15. NACA33110
16. NACA33010
17. MARSKE PIONEER IID TIP (NACA 431012A*.833 HYBRID)
18. NACA24010
19. NACA23010
20. NACA25110.5
21. JWL067 11.5/1.7