Similarly shaped airfoils to NACA35010.5


New! Bulk download of polars in Excel format: NACA35010.5.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
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. NACA35010
2. NACA34010.5
3. JWL076 10/3
4. NACA34010
5. NACA44010.5
6. NACA44010
7. NACA63-511 a=0.0
8. Ritz 3-30-10
9. NACA64-511 a=0.0
10. NACA45010.5
11. Phoenix10
12. EPPLER 332
13. FAD23
14. NACA63-511 a=0.2
15. Horten 10.00% thick 4.00% camber
16. Horten 11.00% thick 4.00% camber
17. NACA35110.5
18. JWL079 9.7/2.7
19. NACA64-511 a=0.2
20. EPPLER 205
21. NACA34110.5