Similarly shaped airfoils to Horten 18.00% thick 4.00% camber


New! Bulk download of polars in Excel format: Horten%2018.00%25%20thick%204.00%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. NACA34118
2. NACA35118
3. Horten 19.00% thick 4.00% camber
4. Horten 17.00% thick 4.00% camber
5. Horten 18.00% thick 3.00% camber
6. NACA44118
7. NACA34117
8. NACA35018
9. NACA35117
10. NACA34018
11. NACA35119
12. NACA44117
13. NACA34119
14. Horten 19.00% thick 3.00% camber
15. Horten 17.00% thick 3.00% camber
16. NACA44019
17. NACA44018
18. NACA25118
19. NACA34116.5
20. NACA44119
21. NACA34017