Similarly shaped airfoils to K3311 (smoothed)
New! Bulk download of polars in Excel format: k3311sm.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. MS3,3-11GP
3. MS3/11GPV
4. HQ 3.0/11
5. MID 343
6. MS3,3-11GPT
7. GA 30-411
8. GA 35A411
9. GA 35-411
10. GA 30A411
11. NACA63-511 a=0.6
12. GA 37-411
13. SBC3
14. S7055 (10.5%) Flat-Bottomed
15. NACA63-511 a=0.5
16. EPPLER E193gU-K24
17. NACA64-511 a=0.6
18. GA 30-410
19. NM Classic 12 saumon
20. EPPLER 193
21. GA 37A411