Similarly shaped airfoils to NACA25112


New! Bulk download of polars in Excel format: NACA25112.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
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

Disclaimer: All information presented herein is delivered without guarantee or warranty of any kind. The user assumes the entire risk of use of this information.

1. Horten 12.00% thick 3.00% camber
2. NACA 2R212
3. NACA33012
4. CLARK YS
5. EH 2.0/12
6. NACA25012
7. EH 3.0/12
8. NACA25113
9. NACA24012
10. NACA M6
11. NACA M6 (NACA-TR-221)
12. RAF 34
13. ZAGI 12
14. TsAGI B 12.0% thick
15. TsAGI B 11.5% thick
16. NACA34012
17. Horten 13.00% thick 3.00% camber
18. EPPLER 331
19. Horten 12.00% thick 2.00% camber
20. EPPLER 361
21. Horten 11.00% thick 3.00% camber