Similarly shaped airfoils to EH 3.0/12


New! Bulk download of polars in Excel format: eh3012.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. EPPLER 636
3. EPPLER 332
4. NACA34012
5. Horten 11.00% thick 3.00% camber
6. NACA25112
7. Horten 12.00% thick 4.00% camber
8. NACA35012
9. M-35A-12.7
10. EPPLER 331
11. EPPLER 635
12. NACA34112
13. NACA33012
14. CLARK YS
15. Horten 11.00% thick 4.00% camber
16. HS 3.5/12
17. HS 3.4.12b
18. EPPLER 637
19. MH 80 12.72%
20. EH 2.0/12
21. NACA34013