Similarly shaped airfoils to Horten 12.00% thick 6.00% camber
New! Bulk download of polars in Excel format: Horten%2012.00%25%20thick%206.00%25%20camber.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
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 13.00% thick 6.00% camber
3. Horten 12.00% thick 5.00% camber
4. Horten 11.00% thick 6.00% camber
5. Horten 11.00% thick 5.00% camber
6. Horten 13.00% thick 5.00% camber
7. NACA45113
8. Horten 12.00% thick 7.00% camber
9. NACA45110.5
10. Horten 13.00% thick 7.00% camber
11. NACA45113.5
12. Horten 11.00% thick 7.00% camber
13. NACA35112
14. Horten 14.00% thick 6.00% camber
15. NACA45110
16. Horten 10.00% thick 6.00% camber
17. Horten 10.00% thick 5.00% camber
18. NACA35113
19. EPPLER 638
20. NACA44110.5
21. RAF 33