Similarly shaped airfoils to NACA24110.5
New! Bulk download of polars in Excel format: NACA24110.5.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
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. NACA24010.5
3. NACA32010.5
4. NACA25110.5
5. NACA42010.5
6. NACA24010
7. Horten 11.00% thick 2.00% camber
8. NACA32010
9. NACA25010.5
10. EH 2.0/10
11. NACA42010
12. Horten 10.00% thick 2.00% camber
13. NACA25110
14. NACA23110
15. NACA23010.5
16. NACA32110
17. NACA33010.5
18. RC_Milan
19. NACA25010
20. JWL067 11.5/1.7
21. NACA23010