Similarly shaped airfoils to Horten 9.00% thick 6.00% camber


New! Bulk download of polars in Excel format: Horten%209.00%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
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.

1. Horten 10.00% thick 6.00% camber
2. NACA45109
3. NACA45110
4. Horten 9.00% thick 5.00% camber
5. Horten 9.00% thick 7.00% camber
6. GOE 746
7. Horten 10.00% thick 7.00% camber
8. NACA45110.5
9. Horten 10.00% thick 5.00% camber
10. Horten 11.00% thick 6.00% camber
11. NACA 11-H-09
12. NACA45107
13. Horten 11.00% thick 7.00% camber
14. NACA44109
15. NACA 6-H-10
16. NACA35109
17. NACA44110
18. Horten 11.00% thick 5.00% camber
19. NACA45009
20. NACA35110
21. GOE 318 (HANSA-BRANDENBURG VI.5)