Similarly shaped airfoils to NACA45113.5


New! Bulk download of polars in Excel format: NACA45113.5.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
Dynamic plotter New!
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.

1. NACA45114
2. NACA45113
3. Horten 13.00% thick 5.00% camber
4. Horten 14.00% thick 5.00% camber
5. NACA35113.5
6. NACA45114.5
7. NACA35114
8. NACA35113
9. Horten 14.00% thick 6.00% camber
10. Horten 13.00% thick 6.00% camber
11. NACA35114.5
12. NACA44113.5
13. NACA44113
14. NACA45115
15. NACA44114
16. Horten 15.00% thick 5.00% camber
17. Horten 12.00% thick 5.00% camber
18. Horten 14.00% thick 4.00% camber
19. Horten 13.00% thick 4.00% camber
20. NACA35112
21. Horten 15.00% thick 6.00% camber