Similarly shaped airfoils to GA 35A211
New! Bulk download of polars in Excel format: GA%2035A211.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 40A211
3. GA 40-211
4. GA 37-211
5. NACA64-311 a=0.5
6. NACA63A311
7. NACA64-311 a=0.2
8. SD6060-104-88
9. GA 30-211
10. GA 35-211
11. NACA64-311 a=0.6
12. NACA64A311
13. HQ 1.5/11
14. NACA65-311 a=0.2
15. GA 30A211
16. NACA65-311 a=0.5
17. NACA63-311 a=0.5
18. BOEING-VERTOL VR-1
19. TP210-11%
20. NACA63-311 a=0.2
21. SB98 VM5 mid