Similarly shaped airfoils to Horten 17.00% thick 5.00% camber


New! Bulk download of polars in Excel format: Horten%2017.00%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. NACA45117
2. NACA45116.5
3. Horten 18.00% thick 5.00% camber
4. Horten 16.00% thick 5.00% camber
5. Horten 17.00% thick 6.00% camber
6. NACA35117
7. NACA35116.5
8. NACA45116
9. NACA45118
10. NACA35116
11. NACA44116
12. Horten 18.00% thick 6.00% camber
13. Horten 16.00% thick 4.00% camber
14. NACA35118
15. NACA45017
16. Horten 17.00% thick 4.00% camber
17. NACA45016.5
18. NACA44017
19. NACA44116.5
20. NACA44016.5
21. NACA44117