Similarly shaped airfoils to Rosner t=30.0 f=12.0, rN=1.1, te=11.3
New! Bulk download of polars in Excel format: Rosner%20t%3D30.0%20f%3D12.0%2C%20rN%3D1.1%2C%20te%3D11.3.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. HN-478S
3. GA 35-012
4. EPPLER 168
5. NACA63-012
6. EPPLER 171
7. Horten 12.00% thick 0.00% camber
8. HN-976S
9. Horten 11.00% thick 0.00% camber
10. GA 30-011
11. GA 37-012
12. EPPLER EA 6(-1)-012
13. Rosner t=30.0 f=13.0, rN=1.3, te=12.3
14. Rosner t=30.0 f=11.0, rN=0.9, te=10.4
15. NACA64-012
16. GOE 429
17. Joukowsky 12.00% thick 0.00% camber
18. GA 30A011
19. NACA0012
20. GA 30-012
21. JWL069 11/0