Similarly shaped airfoils to Horten 14.00% thick 5.00% camber
New! Bulk download of polars in Excel format: Horten%2014.00%25%20thick%205.00%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. NACA35114
3. NACA45113.5
4. NACA45114.5
5. NACA35113.5
6. NACA35114.5
7. Horten 15.00% thick 5.00% camber
8. NACA44114
9. Horten 14.00% thick 4.00% camber
10. NACA44113.5
11. NACA44114.5
12. NACA45113
13. NACA35113
14. NACA45115
15. NACA44113
16. Horten 13.00% thick 5.00% camber
17. Horten 13.00% thick 4.00% camber
18. Horten 15.00% thick 4.00% camber
19. NACA35115
20. NACA44115
21. EPPLER 342