Similarly shaped airfoils to Eiffel 385 (S.T. Ae)


New! Bulk download of polars in Excel format: eiffel385.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
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

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1. Curtis C-72
2. N-22
3. CLARK YH
4. Dayton-Wright T-1
5. Rhode St. Genese 32
6. N-10
7. NACA CYH
8. St. CYR 234 (Bartel 17-IC)
9. Rhode St. Genese 34
10. USA-35B
11. Horten 13.00% thick 3.00% camber
12. nc0001
13. Horten 14.00% thick 3.00% camber
14. NACA34113.5
15. NACA25114
16. NACA33113
17. NACA33113.5
18. NACA34114
19. Rhode St. Genese 30
20. NACA42113.5
21. NACA33013