Similarly shaped airfoils to Rosner t=35.0 f=8.0, rN=0.5, te=9.4-19500 a=0.4
New! Bulk download of polars in Excel format: Rosner%20t%3D35.0%20f%3D8.0%2C%20rN%3D0.5%2C%20te%3D9.4-19500%20a%3D0.4.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. MD8135
3. PROPFAN CRUISE MISSILE WING
4. BOEING-VERTOL VR-8 WITH TAB
5. BOEING-VERTOL VR-8
6. DD928416
7. HN-462
8. Rosner t=30.0 f=8.0, rN=0.5, te=7.6-21700 a=0.3
9. NACA64-209 a=0.5
10. MC813
11. MH 23 8%
12. MD814
13. RG 14
14. GIII BL207
15. NACA64-209 a=0.6
16. GIII BL167
17. GIII BL288
18. MH 31
19. GIII BL145
20. NACA63-209 a=0.5
21. HQ 1.5/8