Similarly shaped airfoils to S7055 (10.5%) Flat-Bottomed
New! Bulk download of polars in Excel format: s7055.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. K3311 (original)
3. K3311 (smoothed)
4. GOE 602
5. MS3,3-11GPT
6. MS3,3-11GP
7. GOE 436
8. EPPLER E193gU-K24
9. GOE 438
10. S4158
11. NACA4410
12. GOE 546
13. GOE 389
14. S3024 9.84%
15. NACA63-511 a=0.5
16. NACA64-511 a=0.5
17. GA 30-410
18. EPPLER 193
19. GA 30A410
20. NACA63-511 a=0.6
21. JWL041 11/3.5