Similarly shaped airfoils to GA 37A320
New! Bulk download of polars in Excel format: GA%2037A320.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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2. GA 40A320
3. GA 40-320
4. NACA64A420
5. GA 37A319
6. NACA65-420 a=0.6
7. NACA65-420 a=0.5
8. NACA63A420
9. GA 35A319
10. NACA65-520
11. NACA65-420 a=0.8
12. NACA64A520
13. GA 37-320
14. NACA65-421 a=0.5
15. NACA65(421)-420
16. GA 40A319
17. NACA65A420
18. NACA63A520
19. GA 40-319
20. NACA65-520 a=0.2
21. NACA64A419