Similarly shaped airfoils to Rosner t=35.0 f=14.0, rN=1.5, te=16.2
New! Bulk download of polars in Excel format: Rosner%20t%3D35.0%20f%3D14.0%2C%20rN%3D1.5%2C%20te%3D16.2.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. NACA63A014
3. GA 30-014
4. GA 37A014
5. GA 30A014
6. Horten 14.00% thick 0.00% camber
7. NACA64-015
8. GA 37-015
9. S8035 (14%)
10. GA 37-014
11. GA 35A015
12. NACA63-015A
13. NACA63A015
14. GA 35-015
15. NACA63-015
16. GA 40A014
17. GA 40-014
18. GA 35-014
19. Rosner t=35.0 f=15.0, rN=1.7, te=17.3
20. Rosner t=35.0 f=13.0, rN=1.3, te=15.1
21. DU 86-137/25