Similarly shaped airfoils to Horten 17.00% thick 3.00% camber
New! Bulk download of polars in Excel format: Horten%2017.00%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. NACA34017
3. NACA25116.5
4. NACA34016.5
5. Horten 18.00% thick 3.00% camber
6. Horten 16.00% thick 3.00% camber
7. Horten 17.00% thick 4.00% camber
8. Horten 17.00% thick 2.00% camber
9. NACA25116
10. NACA33017
11. NACA34117
12. NACA33016.5
13. NACA34116.5
14. NACA34016
15. NACA33117
16. NACA24117
17. NACA33116.5
18. NACA24116.5
19. NACA34018
20. NACA25118
21. NACA33016