Similarly shaped airfoils to Horten 10.00% thick 5.00% camber
New! Bulk download of polars in Excel format: Horten%2010.00%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. NACA45110.5
3. NACA35110
4. Horten 11.00% thick 5.00% camber
5. Horten 9.00% thick 5.00% camber
6. NACA44110
7. NACA35110.5
8. NACA44110.5
9. NACA45109
10. NACA35109
11. NACA44109
12. Horten 9.00% thick 4.00% camber
13. NACA45010
14. Horten 10.00% thick 4.00% camber
15. Horten 10.00% thick 6.00% camber
16. NACA45010.5
17. NACA44010
18. NACA44010.5
19. Horten 11.00% thick 6.00% camber
20. NACA45009
21. NACA34110