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
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. 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