Similarly shaped airfoils to GA 37A219
New! Bulk download of polars in Excel format: GA%2037A219.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 40A219
3. NACA64A319
4. GA 40-219
5. NACA63A319
6. NACA65-319 a=0.5
7. NACA65-319 a=0.6
8. GA 37A218
9. GA 37A220
10. NACA65-319 a=0.8
11. GA 40A220
12. NACA65-419
13. GA 35A218
14. GA 35A220
15. GA 40-220
16. NACA64A320
17. NACA65A319
18. NACA65-320 a=0.6
19. NACA65-320 a=0.5
20. GA 37-219
21. NACA65-419 a=0.0