Similarly shaped airfoils to GA 35-411
New! Bulk download of polars in Excel format: GA%2035-411.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
Disclaimer: All information presented herein is delivered without guarantee or warranty of any kind. The user assumes the entire risk of use of this information.
2. NACA63-511 a=0.5
3. NACA63-511 a=0.6
4. NACA64-511 a=0.5
5. MS3/11GPV
6. NACA64-511 a=0.6
7. GA 35A411
8. K3311 (smoothed)
9. K3311 (original)
10. EPPLER 193
11. EPPLER E193gU-K24
12. GA 37A411
13. GA 40-411
14. GA 30-410
15. GA 40A411
16. GA 35-410
17. GA 35-412
18. GA 35A410
19. S3024 9.84%
20. HQ 3.0/11
21. NACA63-510 a=0.5