Similarly shaped airfoils to Horten 14.00% thick 6.00% camber
New! Bulk download of polars in Excel format: Horten%2014.00%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. NACA45114
4. NACA45113.5
5. NACA45114.5
6. NACA45113
7. Horten 15.00% thick 7.00% camber
8. Horten 13.00% thick 5.00% camber
9. NACA45115
10. Horten 14.00% thick 5.00% camber
11. Horten 14.00% thick 7.00% camber
12. NACA35114
13. Fraser_f4fras15
14. Horten 13.00% thick 7.00% camber
15. Horten 16.00% thick 6.00% camber
16. NACA35113.5
17. Horten 12.00% thick 6.00% camber
18. Horten 15.00% thick 5.00% camber
19. NACA35114.5
20. NACA45112
21. NACA35113