Similarly shaped airfoils to NACA25110
New! Bulk download of polars in Excel format: NACA25110.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. EH 2.5/10
3. NACA25110.5
4. Horten 10.00% thick 3.00% camber
5. EMX-07
6. NACA24110
7. EH 2.0/10
8. NACA33010
9. NACA25010
10. NACA24110.5
11. NACA33010.5
12. RC(5)-10
13. Phoenix10
14. NACA25010.5
15. RC(4)-10
16. NACA25109
17. NACA24010
18. ZAGI 10
19. NACA33110
20. Horten 11.00% thick 3.00% camber
21. NACA24010.5