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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(ah93w480b-il) AH 93-W-480B | Althaus AH 93-W-480B airfoil for use on wind turbines (W) Max thickness 47.8% at 44.1% chord Max camber 3.6% at 44.1% chord | Remove Airfoil details Airfoil plotter |
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Polars for (ah93w480b-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| ah93w480b-il | 50,000 | 9 | 7.4 at α=5.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ah93w480b-il | 50,000 | 5 | 11.2 at α=4.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| ah93w480b-il | 100,000 | 9 | 18.3 at α=14.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ah93w480b-il | 100,000 | 5 | 20.6 at α=8.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| ah93w480b-il | 200,000 | 9 | 21.4 at α=14° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ah93w480b-il | 200,000 | 5 | 22.2 at α=7° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| ah93w480b-il | 500,000 | 9 | 24.9 at α=14.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ah93w480b-il | 500,000 | 5 | 23.7 at α=8° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| ah93w480b-il | 1,000,000 | 9 | 28 at α=13.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ah93w480b-il | 1,000,000 | 5 | 26.6 at α=9.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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