Similarly shaped airfoils to NACA25012


New! Bulk download of polars in Excel format: NACA25012.xlsx


Info | DAT and DXF files | Shape | Venkataraman Fit | Applications (2) | Similarly shaped airfoils
Plain Flapped Shapes: 25% flap chord | 30% flap chord | 35% flap chord | 40% flap chord
Dynamic plotter New!
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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1. NACA24012
2. NACA2212
3. NACA 2R212
4. EH 2.0/12
5. NACA 2R112
6. EPPLER 361
7. NACA2312
8. RAF 34
9. NACA25112
10. TsAGI B 11.5% thick
11. ZAGI 12
12. EPPLER 360
13. TsAGI B 12.0% thick
14. Horten 12.00% thick 2.00% camber
15. NACA25013
16. NACA M12 (NACA-TR-221)
17. GA 30A212
18. GA 30-212
19. NACA M6
20. NACA M6 (NACA-TR-221)
21. NACA33012