Airfoil Comparison
Select airfoils from the airfoil database or add your own airfoils and compare the airfoil shape and lift/drag polars.
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(ebambino7-il) E. Bambino | E. Bambino airfoil Max thickness 6% at 40% chord Max camber 1.9% at 20% chord | Remove Airfoil details Airfoil plotter |
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Polars for (ebambino7-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| ebambino7-il | 50,000 | 9 | 26.3 at α=8.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ebambino7-il | 50,000 | 5 | 28 at α=7.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| ebambino7-il | 100,000 | 9 | 35 at α=8.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ebambino7-il | 100,000 | 5 | 33 at α=6.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| ebambino7-il | 200,000 | 9 | 46.3 at α=8.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ebambino7-il | 200,000 | 5 | 37.5 at α=5.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| ebambino7-il | 500,000 | 9 | 53.6 at α=7.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ebambino7-il | 500,000 | 5 | 48.4 at α=6.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| ebambino7-il | 1,000,000 | 9 | 59.2 at α=6.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ebambino7-il | 1,000,000 | 5 | 58.4 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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