PSU-90-125WL (psu-90-125wl-il)
PSU-90-125WL - PSU-90-125WL sailplane winglet airfoil
| Details | Dat file | Parser | |
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(psu-90-125wl-il) PSU-90-125WL PSU-90-125WL sailplane winglet airfoil Max thickness 12.5% at 35.1% chord. Max camber 2% at 54.4% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Selig format |
PSU-90-125WL 1.00000 0.00000 0.99646 0.00062 0.98627 0.00269 0.97034 0.00630 0.94931 0.01099 0.92336 0.01635 0.89265 0.02238 0.85770 0.02912 0.81908 0.03646 0.77741 0.04423 0.73333 0.05217 0.68748 0.05999 0.64048 0.06725 0.59265 0.07341 0.54409 0.07826 0.49509 0.08194 0.44618 0.08446 0.39787 0.08580 0.35064 0.08593 0.30495 0.08482 0.26123 0.08249 0.21989 0.07893 0.18131 0.07420 0.14582 0.06835 0.11371 0.06149 0.08524 0.05373 0.06062 0.04523 0.04002 0.03617 0.02356 0.02681 0.01134 0.01745 0.00343 0.00850 0.00002 0.00063 0.00240 -0.00590 0.01088 -0.01194 0.02456 -0.01782 0.04321 -0.02324 0.06663 -0.02804 0.09462 -0.03211 0.12693 -0.03539 0.16327 -0.03786 0.20328 -0.03951 0.24657 -0.04033 0.29269 -0.04037 0.34116 -0.03965 0.39144 -0.03822 0.44300 -0.03610 0.49525 -0.03331 0.54770 -0.02975 0.60004 -0.02548 0.65193 -0.02083 0.70276 -0.01622 0.75178 -0.01192 0.79827 -0.00814 0.84149 -0.00502 0.88073 -0.00261 0.91534 -0.00093 0.94469 0.00007 0.96829 0.00051 0.98567 0.00049 0.99638 0.00018 1.00000 0.00000 |
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Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file |
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Polars for PSU-90-125WL (psu-90-125wl-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| psu-90-125wl-il | 50,000 | 9 | 32.2 at α=8.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| psu-90-125wl-il | 50,000 | 5 | 34.9 at α=7.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| psu-90-125wl-il | 100,000 | 9 | 54.1 at α=6.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| psu-90-125wl-il | 100,000 | 5 | 53.2 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| psu-90-125wl-il | 200,000 | 9 | 75.8 at α=5.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| psu-90-125wl-il | 200,000 | 5 | 70.3 at α=4.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| psu-90-125wl-il | 500,000 | 9 | 102.5 at α=4.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| psu-90-125wl-il | 500,000 | 5 | 87.8 at α=5.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| psu-90-125wl-il | 1,000,000 | 9 | 115.7 at α=5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| psu-90-125wl-il | 1,000,000 | 5 | 97.7 at α=5.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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