Similarly shaped airfoils to EPPLER 360


New! Bulk download of polars in Excel format: e360.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. EPPLER 361
2. NACA24012
3. RC-12(N)1
4. NACA25012
5. ZAGI 12
6. TsAGI B 12.0% thick
7. ONERA NACA CAMBRE
8. TsAGI B 11.5% thick
9. NACA64-313 a=0.0
10. RAF 34
11. NACA 2R212
12. EH 2.0/12
13. NACA24013
14. NACA2212
15. NACA63-313 a=0.0
16. Horten 12.00% thick 2.00% camber
17. NACA64-313 a=0.2
18. NACA25013
19. Europa Dykins 12%
20. NACA65-313 a=0.0
21. NACA64-213 a=0.2