Similarly shaped airfoils to EPPLER E193gU-K24
New! Bulk download of polars in Excel format: E193gU-K24.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. S3024 9.84%
3. GA 30-410
4. GA 30A410
5. MID 321c
6. NACA63-510 a=0.5
7. GA 35A410
8. NACA63-510 a=0.6
9. GA 35-410
10. GOE 602
11. MID 321b
12. NACA64-510 a=0.5
13. NACA64-510 a=0.6
14. GA 37-410
15. K3311 (original)
16. GA 35-411
17. K3311 (smoothed)
18. NACA4410
19. S7055 (10.5%) Flat-Bottomed
20. GA 37A410
21. GOE 546