Similarly shaped airfoils to GA 35A311
New! Bulk download of polars in Excel format: GA%2035A311.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 40A311
3. GA 40-311
4. GA 37-311
5. EPPLER 374
6. NACA64-411 a=0.5
7. GA 30-311
8. NACA64-411 a=0.6
9. GA 35-311
10. NACA65-411 a=0.5
11. NACA63-411 a=0.5
12. GA 30A311
13. NACA63-411 a=0.6
14. NACA65-411 a=0.6
15. NACA63A411
16. GA 37-312
17. HN-203
18. NACA64A411
19. MS2.5/11GPV
20. NACA64-411 a=0.2
21. MH 18 11.16%