Similarly shaped airfoils to Eiffel 430 (Lachassgne)


New! Bulk download of polars in Excel format: eiffel430.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
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. N-11
2. I.S.A. 962
3. I.S.A. 960
4. USA-35B
5. Eiffel 428 (Bleriot)
6. NACA35110
7. NACA35110.5
8. NACA35010
9. I.S.A. 961
10. JWL076 10/3
11. NACA35010.5
12. Rhode St. Genese 30
13. NACA45010
14. NACA45010.5
15. Horten 10.00% thick 4.00% camber
16. N-10
17. NACA44010
18. NACA35109
19. NACA44010.5
20. Horten 11.00% thick 4.00% camber
21. Rhode St. Genese 32