Similarly shaped airfoils to Horten 18.00% thick 3.00% camber


New! Bulk download of polars in Excel format: Horten%2018.00%25%20thick%203.00%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. NACA25118
2. NACA34018
3. Horten 19.00% thick 3.00% camber
4. Horten 17.00% thick 3.00% camber
5. Horten 18.00% thick 4.00% camber
6. Horten 18.00% thick 2.00% camber
7. NACA35018
8. NACA25117
9. NACA34118
10. NACA33018
11. NACA34017
12. NACA24118
13. NACA34019
14. NACA25119
15. NACA33017
16. Horten 17.00% thick 4.00% camber
17. Horten 19.00% thick 4.00% camber
18. NACA25018
19. NACA35019
20. Horten 17.00% thick 2.00% camber
21. NACA34117