WORTMANN FX 77-W-258 AIRFOIL (fx77w258-il)
WORTMANN FX 77-W-258 AIRFOIL - Wortmann FX 77-W-258 wind turbine airfoil
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(fx77w258-il) WORTMANN FX 77-W-258 AIRFOIL Wortmann FX 77-W-258 wind turbine airfoil Max thickness 26.1% at 30.9% chord. Max camber 4.3% at 27.9% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
WORTMANN FX 77-W-258 AIRFOIL
48.0 48.0
0.0000000 0.0000000
0.0010700 0.0175200
0.0042800 0.0272200
0.0096100 0.0390200
0.0170400 0.0496100
0.0265300 0.0622100
0.0380600 0.0739700
0.0515600 0.0869600
0.0669900 0.0988900
0.0842700 0.1113400
0.1033200 0.1224800
0.1240800 0.1337000
0.1464500 0.1432900
0.1703300 0.1524100
0.1956200 0.1597500
0.2222100 0.1661600
0.2500000 0.1703900
0.2788600 0.1731600
0.3086600 0.1734000
0.3392800 0.1718500
0.3705900 0.1673000
0.4024500 0.1607400
0.4347400 0.1526300
0.4673000 0.1443300
0.5000000 0.1353000
0.5327000 0.1265400
0.5652600 0.1172800
0.5975500 0.1086300
0.6294100 0.0996300
0.6607200 0.0911300
0.6913400 0.0824600
0.7211400 0.0743300
0.7500000 0.0663300
0.7777900 0.0589900
0.8043800 0.0519300
0.8296700 0.0455500
0.8535500 0.0395100
0.8759200 0.0342000
0.8966800 0.0292300
0.9157300 0.0249500
0.9330100 0.0210400
0.9484400 0.0177300
0.9619400 0.0148300
0.9734700 0.0124000
0.9829600 0.0103500
0.9903900 0.0086700
0.9957200 0.0067370
0.9989300 0.0063600
0.0000000 0.0000000
0.0010700 -.0127300
0.0042800 -.0176400
0.0096100 -.0252400
0.0170400 -.0307000
0.0265300 -.0369900
0.0380600 -.0419300
0.0515600 -.0478700
0.0669900 -.0526100
0.0842700 -.0580300
0.1033200 -.0623900
0.1240800 -.0672400
0.1464500 -.0710400
0.1703300 -.0751700
0.1956200 -.0783200
0.2222100 -.0816300
0.2500000 -.0840100
0.2788600 -.0864000
0.3086600 -.0878500
0.3392800 -.0892000
0.3705900 -.0895800
0.4024500 -.0897000
0.4347400 -.0887000
0.4673000 -.0873200
0.5000000 -.0847200
0.5327000 -.0815500
0.5652600 -.0766000
0.5975500 -.0707000
0.6294100 -.0627300
0.6607200 -.0548900
0.6913400 -.0470700
0.7211400 -.0401000
0.7500000 -.0336000
0.7777900 -.0280300
0.8043800 -.0229800
0.8296700 -.0188100
0.8535500 -.0150900
0.8759200 -.0121700
0.8966800 -.0096900
0.9157300 -.0079400
0.9330100 -.0065600
0.9484400 -.0057200
0.9619400 -.0052100
0.9734700 -.0050600
0.9829600 -.0051200
0.9903900 -.0053500
0.9957200 -.0056300
0.9989300 -.0058300
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Polars for WORTMANN FX 77-W-258 AIRFOIL (fx77w258-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| fx77w258-il | 50,000 | 9 | 1.5 at α=7.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx77w258-il | 50,000 | 5 | 2.5 at α=7.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx77w258-il | 100,000 | 9 | 1.2 at α=5.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx77w258-il | 100,000 | 5 | 10.5 at α=2° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx77w258-il | 200,000 | 9 | 9.5 at α=0.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx77w258-il | 200,000 | 5 | 36.5 at α=6.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx77w258-il | 500,000 | 9 | 76 at α=11° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx77w258-il | 500,000 | 5 | 83.2 at α=9.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx77w258-il | 1,000,000 | 9 | 112.5 at α=9.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx77w258-il | 1,000,000 | 5 | 103.6 at α=8.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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