Similarly shaped airfoils to GA 37A615


New! Bulk download of polars in Excel format: GA%2037A615.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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1. GA 35A615
2. GA 40A615
3. GA 40-615
4. NACA65-715 a=0.5
5. FX 84-W-150
6. GA 37-615
7. NACA65-715 a=0.6
8. GA 37A616
9. GA 37A614
10. GA 40A616
11. GA 35A614
12. GA 40-616
13. AH 81-K-144/17
14. GA 35A616
15. NACA64-715 a=0.5
16. GA 37-616
17. FX 84-W-140
18. NACA64-715 a=0.6
19. GA 40A614
20. NACA65-615 a=0.6
21. EPPLER 431