Similarly shaped airfoils to Rosner t=35.0 f=11.0, rN=0.9, te=12.8
New! Bulk download of polars in Excel format: Rosner%20t%3D35.0%20f%3D11.0%2C%20rN%3D0.9%2C%20te%3D12.8.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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2. GA 35A011
3. GA 37A011
4. GA 30-011
5. HN-478S
6. GA 30A011
7. N-12
8. Horten 11.00% thick 0.00% camber
9. GA 40A011
10. GA 40-011
11. NACA64-012
12. GA 37-011
13. GA 37-012
14. GA 35A012
15. NACA63-012A
16. NACA63A012
17. NACA63-012
18. SC(2)-0010
19. GA 37A012
20. GA 35-012
21. GA 35-011