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
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. 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