Similarly shaped airfoils to Rosner t=35.0 f=13.0, rN=1.3, te=15.1
New! Bulk download of polars in Excel format: Rosner%20t%3D35.0%20f%3D13.0%2C%20rN%3D1.3%2C%20te%3D15.1.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
Disclaimer: All information presented herein is delivered without guarantee or warranty of any kind. The user assumes the entire risk of use of this information.
2. GA 35A013
3. LS(1)-0013
4. GOE 409
5. RAF 30
6. GOE 459
7. GA 37A013
8. GA 30-013
9. NACA0013
10. GA 30A013
11. Horten 13.00% thick 0.00% camber
12. GA 37-014
13. GA 37-013
14. GA 35A014
15. S1012
16. GA 40A013
17. NACA63A014
18. GA 40-013
19. J5012 12%
20. GA 35-014
21. SC(2)-0012