Similarly shaped airfoils to GA 35A314
New! Bulk download of polars in Excel format: GA%2035A314.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 40A314
3. GA 40-314
4. GA 37-314
5. NACA64-414 a=0.5
6. NACA65-414 a=0.5
7. NACA63A414
8. NACA64-414 a=0.6
9. NACA65-414 a=0.6
10. NACA64A414
11. CB2514
12. GA 37-315
13. GA 30-314
14. GA 35-314
15. NACA63-414 a=0.5
16. GA 35A313
17. GA 35A315
18. GA 30A314
19. NACA64-415 a=0.5
20. NACA63-414 a=0.6
21. NACA64-415 a=0.6