Similarly shaped airfoils to NACA45010.5
New! Bulk download of polars in Excel format: NACA45010.5.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. NACA44010.5
3. NACA44010
4. NACA35010.5
5. NACA63-611 a=0.0
6. USA 45 M
7. NACA35110.5
8. NACA35010
9. NACA64-611 a=0.0
10. FAD21
11. NACA35110
12. NACA63-611 a=0.2
13. NACA45012
14. NACA45009
15. JWL076 10/3
16. NACA64-611 a=0.2
17. EPPLER 334
18. NACA63-610 a=0.0
19. NACA63-711 a=0.0
20. NACA64-610 a=0.0
21. NACA65-611 a=0.0