Similarly shaped airfoils to Rosner t=30.0 f=11.0, rN=0.9, te=10.4
New! Bulk download of polars in Excel format: Rosner%20t%3D30.0%20f%3D11.0%2C%20rN%3D0.9%2C%20te%3D10.4.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-976S
3. GA 35-011
4. HN-477S
5. HN-478S
6. Horten 11.00% thick 0.00% camber
7. HN-275S
8. SD8020-010-88
9. GA 37-011
10. Horten 10.00% thick 0.00% camber
11. GA 30-010
12. FX 76-100
13. RYAN BQM-34 FIREBEE WING
14. HQ 0/10
15. HN-840S
16. EPPLER 228
17. GA 30-011
18. GOE 429
19. NACA0010
20. FX 79-L-100
21. GA 30A010