Similarly shaped airfoils to NACA25013
New! Bulk download of polars in Excel format: NACA25013.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. NACA2213
3. NACA25013.5
4. RAF 34
5. NACA25113
6. Horten 13.00% thick 2.00% camber
7. TsAGI B 12.5% thick
8. NACA25113.5
9. NACA25014
10. NACA25012
11. NACA 2R212
12. Falcon (Carl Goldberg Falcon 56 Mk II R/C powerplane)
13. NACA24012
14. GA 30A213
15. GA 30-213
16. NACA2212
17. TsAGI B 13.0% thick
18. TsAGI B 12.0% thick
19. EPPLER 360
20. NACA33013
21. NACA 2R112