Similarly shaped airfoils to EPPLER 580
New! Bulk download of polars in Excel format: e580.xlsx
Info | DAT and DXF files | Shape | Venkataraman Fit | Applications (1) | 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. NACA63-716 a=0.8
3. FX 63-158
4. NACA64-716 a=0.8
5. SM701
6. NLF(1)-0215F
7. FX 62-K-153/20
8. NACA63-715 a=0.8
9. NACA64-715 a=0.8
10. NACA63A715
11. NACA63A716
12. NACA63-717 a=0.8
13. EPPLER EC 86(-3)-914
14. EPPLER 587
15. Dees Okay230
16. NACA64-717 a=0.8
17. NACA64A716
18. NACA64A715
19. MID 403
20. NACA65-716 a=0.8
21. NLF-1015