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
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.
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