Similarly shaped airfoils to GA 37A614
New! Bulk download of polars in Excel format: GA%2037A614.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 40A614
3. GA 40-614
4. EPPLER 434
5. FX 84-W-140
6. NACA65-714 a=0.5
7. GA 37-614
8. GA 37A613
9. GA 37A615
10. GA 40A615
11. NACA65-714 a=0.6
12. NACA64-714 a=0.5
13. GA 35A613
14. GA 40-615
15. GA 37-615
16. GA 35A615
17. NACA65-614 a=0.6
18. NACA65-614 a=0.5
19. NACA64-714 a=0.6
20. GA 40A613
21. GA 35-614