Similarly shaped airfoils to NACA45116
New! Bulk download of polars in Excel format: NACA45116.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 16.00% thick 5.00% camber
3. NACA45117
4. NACA45115
5. Horten 16.00% thick 6.00% camber
6. Horten 17.00% thick 5.00% camber
7. Horten 15.00% thick 5.00% camber
8. Horten 17.00% thick 6.00% camber
9. NACA44116
10. NACA45114.5
11. NACA35116
12. Horten 16.00% thick 4.00% camber
13. Horten 15.00% thick 6.00% camber
14. NACA35116.5
15. NACA44115
16. NACA45016
17. NACA35115
18. NACA35114.5
19. Fraser_f4fras15
20. NACA45016.5
21. Horten 15.00% thick 4.00% camber