Similarly shaped airfoils to NACA35010
New! Bulk download of polars in Excel format: NACA35010.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. JWL076 10/3
3. NACA34010
4. NACA34010.5
5. NACA44010
6. Ritz 3-30-10
7. NACA44010.5
8. Phoenix10
9. JWL079 9.7/2.7
10. FAD23
11. NACA34009
12. NACA35009
13. NACA63-510 a=0.0
14. HS 3.0/9.0
15. NACA64-510 a=0.0
16. Horten 10.00% thick 4.00% camber
17. NACA45010
18. NACA63-511 a=0.0
19. EPPLER 205
20. NACA45010.5
21. NACA64-511 a=0.0