Similarly shaped airfoils to GA 40-019
New! Bulk download of polars in Excel format: GA%2040-019.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. GA 37A019
3. NACA65-119 a=0.0
4. NACA65-119
5. NACA65-119 a=0.2
6. EPPLER 838 HYDROFOIL
7. GA 40-018
8. GA 40-020
9. GA 40A018
10. GA 35A019
11. GA 40A020
12. NACA65-018
13. NACA65-119 a=0.8
14. GA 37A018
15. NACA65-119 a=0.5
16. GA 37-019
17. NACA65-119 a=0.6
18. NACA65-120 a=0.0
19. NACA65-120
20. NACA65-120 a=0.2
21. NACA64A119