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