Similarly shaped airfoils to GA 35A415


New! Bulk download of polars in Excel format: GA%2035A415.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
Dynamic plotter New!
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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1. GA 37A415
2. GA 40A415
3. GA 40-415
4. GA 37-415
5. NACA65-515 a=0.5
6. NACA64-515 a=0.5
7. MRC-16
8. NACA64-515 a=0.6
9. NACA65-515 a=0.6
10. NACA65(2)-415 a=0.5
11. GA 37-416
12. GA 35A416
13. GA 35A414
14. GA 30-415
15. FX 79-W-151 A
16. GA 35-415
17. GA 37A416
18. NACA63A515
19. GA 37A414
20. GA 30A415
21. NACA64-516 a=0.6