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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(pw75-pw) PW75 | Peter Wick. Modified PW51 with some more reflex Max thickness 8.9% at 27.5% chord Max camber 1.5% at 23.4% chord | Remove Airfoil details Airfoil plotter |
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Polars for (pw75-pw)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| pw75-pw | 50,000 | 9 | 24.7 at α=6.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| pw75-pw | 100,000 | 9 | 40.3 at α=6.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| pw75-pw | 200,000 | 9 | 57 at α=7.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| pw75-pw | 500,000 | 9 | 73.4 at α=5.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| pw75-pw | 1,000,000 | 9 | 83.6 at α=4.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| pw75-pw | 2,000,000 | 9 | 91.4 at α=4° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| pw75-pw | 5,000,000 | 9 | 107.2 at α=8° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
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