Similarly shaped airfoils to Horten 13.00% thick 5.00% camber
New! Bulk download of polars in Excel format: Horten%2013.00%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. NACA45113.5
3. NACA35113
4. Horten 12.00% thick 5.00% camber
5. Horten 13.00% thick 6.00% camber
6. NACA35113.5
7. NACA45112
8. NACA45114
9. NACA35112
10. Horten 14.00% thick 5.00% camber
11. NACA35114
12. Horten 14.00% thick 6.00% camber
13. Horten 12.00% thick 6.00% camber
14. NACA44113
15. EPPLER 338
16. NACA45013
17. Horten 13.00% thick 4.00% camber
18. NACA44113.5
19. NACA45114.5
20. NACA45013.5
21. NACA44112