Similarly shaped airfoils to Rosner t=30.0 f=14.0, rN=1.5, te=13.2
New! Bulk download of polars in Excel format: Rosner%20t%3D30.0%20f%3D14.0%2C%20rN%3D1.5%2C%20te%3D13.2.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
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. EPPLER 169
3. GA 35-014
4. Horten 13.00% thick 0.00% camber
5. S8035 (14%)
6. Rosner t=30.0 f=15.0, rN=1.7, te=14.1
7. Rosner t=30.0 f=13.0, rN=1.3, te=12.3
8. HM50T
9. St. CYR 172 (Royer)
10. GA 30-013
11. Joukowsky 14.00% thick 0.00% camber
12. Horten 14.00% thick 0.00% camber
13. NACA0013
14. RAF 30
15. GA 37-014
16. GA 35-013
17. GA 30A013
18. FX 71-L-150/20
19. NACA63-114 a=0.0
20. FX 71-L-150/30
21. Rosner t=35.0 f=13.0, rN=1.3, te=15.1