Similarly shaped airfoils to GA 35A320
New! Bulk download of polars in Excel format: GA%2035A320.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. NACA63A420
3. GA 40A320
4. GA 35A319
5. NACA64A420
6. GA 40-320
7. GA 37-320
8. GA 37A319
9. NACA65-420 a=0.6
10. NACA63A520
11. NACA65-420 a=0.5
12. NACA64A520
13. GA 30-319
14. GA 30-320
15. NACA65-520
16. GA 35-320
17. GA 30A319
18. NACA63A419
19. NACA65-420 a=0.8
20. NACA65(421)-420
21. NACA65-421 a=0.5