Similarly shaped airfoils to EPPLER 548
New! Bulk download of polars in Excel format: e548.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
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2. NACA64-418 a=0.0
3. NACA64-417 a=0.0
4. GA 37-218
5. NACA64-418 a=0.2
6. GA 37-217
7. NACA65-417 a=0.0
8. NACA64-417 a=0.2
9. EPPLER 550
10. EPPLER 544
11. GA 35A217
12. NACA63-418 a=0.0
13. EPPLER 545
14. EPPLER 543
15. NACA63-417 a=0.0
16. GA 35-218
17. GA 37A217
18. GA 40-217
19. NACA65-317 a=0.2
20. NACA65-417 a=0.2
21. NACA63-418 a=0.2