Similarly shaped airfoils to EH 2.0/12


New! Bulk download of polars in Excel format: eh2012.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. NACA25012
2. NACA24012
3. Horten 12.00% thick 2.00% camber
4. NACA 2R212
5. EPPLER 361
6. NACA25112
7. NACA2212
8. Borge-b3
9. EPPLER 360
10. RAF 34
11. Horten 11.00% thick 2.00% camber
12. TsAGI B 11.5% thick
13. NACA63-312 a=0.0
14. JWL067 11.5/1.7
15. ZAGI 12
16. TsAGI B 11.0% thick
17. NACA63-312 a=0.2
18. NACA24112
19. NACA33012
20. NACA 2R112
21. NACA64-312 a=0.0