Similarly shaped airfoils to Horten 16.00% thick 5.00% camber


New! Bulk download of polars in Excel format: Horten%2016.00%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
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. NACA45116
2. NACA45116.5
3. Horten 17.00% thick 5.00% camber
4. Horten 15.00% thick 5.00% camber
5. NACA35116
6. Horten 16.00% thick 4.00% camber
7. NACA44116
8. NACA35116.5
9. NACA45115
10. NACA45117
11. NACA35115
12. NACA44115
13. Horten 17.00% thick 6.00% camber
14. Horten 15.00% thick 4.00% camber
15. NACA35117
16. NACA45016
17. NACA45114.5
18. NACA35114.5
19. Horten 16.00% thick 6.00% camber
20. NACA44114.5
21. NACA45016.5