Similarly shaped airfoils to S8052 (11.88%)
New! Bulk download of polars in Excel format: s8052.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 30-212
3. GA 35A212
4. GA 35-212
5. GA 37-212
6. NACA2312
7. NACA63-312 a=0.2
8. NACA2212
9. NACA63-312 a=0.0
10. GA 30A212
11. NACA64-312 a=0.2
12. GA 35-213
13. Ritz 2-30-12
14. NACA64-312 a=0.0
15. NACA2412
16. GA 37A212
17. GA 37-213
18. NACA63-312
19. S8055 (12%)
20. NACA63-312 a=0.5
21. NACA63-313 a=0.2