Similarly shaped airfoils to GA 35A414
New! Bulk download of polars in Excel format: GA%2035A414.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 40A414
3. MRC-16
4. GA 40-414
5. GA 37-414
6. NACA64-514 a=0.5
7. NACA65-514 a=0.5
8. NACA64-514 a=0.6
9. GA 30-413.5
10. NACA65-514 a=0.6
11. S4233-136-84
12. GA 37-415
13. BOEING 106
14. GA 30-414
15. GA 35-414
16. NACA63-514 a=0.5
17. GA 35A413
18. GA 35A415
19. GA 30A414
20. NACA63-514 a=0.6
21. NACA63A514