Similarly shaped airfoils to GA 35A312
New! Bulk download of polars in Excel format: GA%2035A312.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 40A312
3. GA 40-312
4. GA 37-312
5. NACA64-412 a=0.5
6. LDS-2
7. NACA64-412 a=0.6
8. NACA65-412 a=0.5
9. GA 30-312
10. GA 35-312
11. NACA63-412 a=0.5
12. NACA63A412
13. EPPLER 207
14. NACA65-412 a=0.6
15. GA 30A312
16. NACA63-412 a=0.6
17. GA 37-313
18. NACA64A412
19. NM32 root
20. RAF 38
21. NACA64-413 a=0.5