Similarly shaped airfoils to Rosner t=30.0 f=10.0, rN=0.8, te=9.5
New! Bulk download of polars in Excel format: Rosner%20t%3D30.0%20f%3D10.0%2C%20rN%3D0.8%2C%20te%3D9.5.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. Horten II Tropfen symmetric 10%
3. RAE 101
4. HN-840S
5. HN-275S
6. TP28-L
7. RAE 100
8. GA 35-010
9. RS001t10
10. HQ 0/10
11. RS001t
12. RYAN BQM-34 FIREBEE WING
13. HN-477S
14. TP36-9.5%
15. HN-312S
16. Horten 10.00% thick 0.00% camber
17. RAE 102
18. EPPLER 228
19. LWK 79-100
20. GA 37-010
21. RAF 27