Similarly shaped airfoils to GA 37-019
New! Bulk download of polars in Excel format: GA%2037-019.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. NACA64-119 a=0.0
3. NACA64-119
4. NACA64-119 a=0.2
5. GA 37-018
6. GA 37-020
7. GA 35A019
8. NACA63A018
9. GA 35A018
10. NACA63-119 a=0.0
11. NACA64-119 a=0.8
12. NACA64-119 a=0.5
13. EPPLER 838 HYDROFOIL
14. NACA64-018
15. NACA64-119 a=0.6
16. NACA63-119
17. GA 35-020
18. NACA64-120 a=0.0
19. GA 40-019
20. NACA63-119 a=0.2
21. GA 35-018