Similarly shaped airfoils to Rosner t=35.0 f=10.0, rN=0.8, te=11.7
New! Bulk download of polars in Excel format: Rosner%20t%3D35.0%20f%3D10.0%2C%20rN%3D0.8%2C%20te%3D11.7.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. RAE 103
3. GA 35A010
4. RAE 102
5. GA 37A010
6. NACA64A-010
7. RAF 27
8. GA 30-010
9. HQ 0/10
10. RYAN BQM-34 FIREBEE WING
11. ONERA D, SHARP TRAILING EDGE
12. ONERA D, BLUNT TRAILING EDGE
13. GA 30A010
14. NACA0010
15. LWK 80-100
16. SD8020-010-88
17. SC(2)-0010
18. GA 40A010
19. Horten 10.00% thick 0.00% camber
20. GA 40-010
21. HN-840S