Similarly shaped airfoils to St. CYR 234 (Bartel 17-IC)


New! Bulk download of polars in Excel format: stcyr234.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

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.

1. Eiffel 385 (S.T. Ae)
2. GA(PC)1 landing flap
3. Dayton-Wright T-1
4. N-24
5. Rhode St. Genese 36
6. Rhode St. Genese 34
7. NACA44116.5
8. NACA44117
9. Horten 17.00% thick 4.00% camber
10. NACA35116.5
11. NACA34116.5
12. NACA35117
13. NACA44118
14. NACA35116
15. Horten 18.00% thick 4.00% camber
16. NACA34116
17. NACA34117
18. NACA33116.5
19. Horten 17.00% thick 3.00% camber
20. Horten 16.00% thick 3.00% camber
21. NACA33116