Similarly shaped airfoils to GA 37A310
New! Bulk download of polars in Excel format: GA%2037A310.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 40A310
3. GA 40-310
4. GA 37-310
5. NACA65-410 a=0.5
6. NACA64-410 a=0.5
7. DP2.47/9.48_DS
8. NACA65-410 a=0.6
9. NACA64-410 a=0.6
10. NACA65-410 a=0.2
11. GA 35-310
12. NACA63-410 a=0.5
13. GA 30-310
14. NACA64A410
15. NACA63A410
16. GA 30A310
17. NACA64-410 a=0.2
18. NACA63-410 a=0.6
19. SD7084 (9.6%)
20. EPPLER EB380
21. FX 84-W-097