Similarly shaped airfoils to NACA24013
New! Bulk download of polars in Excel format: NACA24013.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. NACA25013.5
3. NACA2213
4. Horten 13.00% thick 2.00% camber
5. NACA33013
6. RAF 34
7. Falcon (Carl Goldberg Falcon 56 Mk II R/C powerplane)
8. NACA24012
9. NACA25113
10. NACA24013.5
11. EPPLER 360
12. NACA33013.5
13. NACA25014
14. NACA42013
15. NACA25012
16. NACA24113
17. NACA25113.5
18. NACA 2R212
19. EPPLER 361
20. TsAGI B 12.5% thick
21. Horten 14.00% thick 2.00% camber