Similarly shaped airfoils to Horten 11.00% thick 5.00% camber
New! Bulk download of polars in Excel format: Horten%2011.00%25%20thick%205.00%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 12.00% thick 5.00% camber
3. Horten 10.00% thick 5.00% camber
4. NACA35110.5
5. NACA44110.5
6. NACA45110
7. NACA45112
8. NACA35110
9. NACA44110
10. NACA35112
11. Horten 12.00% thick 6.00% camber
12. Horten 11.00% thick 4.00% camber
13. Horten 11.00% thick 6.00% camber
14. NACA45010.5
15. EPPLER 637
16. NACA44010.5
17. NACA 8-H-12
18. Horten 10.00% thick 4.00% camber
19. NACA44112
20. NACA45012
21. NACA45010