Similarly shaped airfoils to Horten 12.00% thick 5.00% camber
New! Bulk download of polars in Excel format: Horten%2012.00%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. NACA35112
3. Horten 13.00% thick 5.00% camber
4. Horten 11.00% thick 5.00% camber
5. Horten 12.00% thick 6.00% camber
6. NACA45113
7. NACA35113
8. Horten 13.00% thick 6.00% camber
9. NACA44112
10. HS 3.5/12
11. EPPLER 637
12. NACA45012
13. NACA45110.5
14. Horten 12.00% thick 4.00% camber
15. NACA45113.5
16. NACA35110.5
17. HS 3.4.12b
18. NACA44110.5
19. NACA44012
20. NACA35113.5
21. Horten 11.00% thick 4.00% camber