Similarly shaped airfoils to NACA25116
New! Bulk download of polars in Excel format: NACA25116.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 3.00% camber
3. Horten 16.00% thick 2.00% camber
4. NACA24116
5. NACA33016
6. NACA25016
7. NACA24116.5
8. NACA33016.5
9. NACA34016
10. NACA25016.5
11. NACA25117
12. NACA25115
13. NACA24016
14. NACA34016.5
15. Horten 17.00% thick 3.00% camber
16. NACA33116
17. Horten 17.00% thick 2.00% camber
18. NACA24016.5
19. NACA24115
20. NACA33116.5
21. NACA33015