Similarly shaped airfoils to GA 35A410
New! Bulk download of polars in Excel format: GA%2035A410.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 40A410
3. GA 40-410
4. GA 37-410
5. S3024 9.84%
6. NACA64-510 a=0.5
7. EPPLER 193
8. GA 30-410
9. GA 35-410
10. NACA63-510 a=0.5
11. GOE 595
12. GA 30A410
13. EPPLER E193gU-K24
14. NACA65-510 a=0.5
15. NACA64-510 a=0.6
16. NACA63-510 a=0.6
17. EPPLER EB380
18. NACA65-510 a=0.6
19. GA 37-411
20. GA 35-411
21. NACA64-511 a=0.5