Similarly shaped airfoils to Horten 19.00% thick 4.00% camber


New! Bulk download of polars in Excel format: Horten%2019.00%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. NACA34119
2. NACA35119
3. Horten 20.00% thick 4.00% camber
4. Horten 18.00% thick 4.00% camber
5. Horten 19.00% thick 3.00% camber
6. NACA44019
7. NACA44119
8. NACA34118
9. NACA35019
10. NACA35118
11. NACA34019
12. NACA44118
13. Horten 20.00% thick 3.00% camber
14. Horten 18.00% thick 3.00% camber
15. Horten 20.00% thick 5.00% camber
16. NACA45119
17. NACA25119
18. NACA34018
19. NACA35018
20. Horten 19.00% thick 5.00% camber
21. NACA25118