Similarly shaped airfoils to EPPLER 476
New! Bulk download of polars in Excel format: e476.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. GA 35A017
3. GA 37-017
4. GA 35-017
5. GA 30-016
6. GA 37A017
7. GA 35A016
8. NACA63A016
9. NACA64-018
10. GA 37-018
11. GA 35-018
12. NACA63-018
13. Horten 17.00% thick 0.00% camber
14. NACA64-117 a=0.0
15. NACA63(3)-018
16. GA 30-017
17. NACA0016
18. GA 30A016
19. NACA64-117
20. Horten 16.00% thick 0.00% camber
21. EPPLER 837 HYDROFOIL