Similarly shaped airfoils to Horten 19.00% thick 3.00% camber
New! Bulk download of polars in Excel format: Horten%2019.00%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
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.
2. NACA34019
3. NACA44019
4. Horten 20.00% thick 3.00% camber
5. Horten 18.00% thick 3.00% camber
6. NACA35019
7. Horten 19.00% thick 4.00% camber
8. NACA25118
9. NACA34119
10. NACA34018
11. NACA24119
12. NACA35018
13. Horten 18.00% thick 4.00% camber
14. Horten 20.00% thick 4.00% camber
15. NACA33018
16. Horten 18.00% thick 2.00% camber
17. NACA34118
18. NACA25019
19. NACA24118
20. NACA24019
21. NACA35119