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
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(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