WORTMANN FX 77-W-153 AIRFOIL (fx77w153-il)
WORTMANN FX 77-W-153 AIRFOIL - Wortmann FX 77-W-153 wind turbine airfoil
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(fx77w153-il) WORTMANN FX 77-W-153 AIRFOIL Wortmann FX 77-W-153 wind turbine airfoil Max thickness 15.2% at 27.9% chord. Max camber 4.5% at 27.9% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
WORTMANN FX 77-W-153 AIRFOIL
48.0 48.0
0.0000000 0.0000000
0.0010700 0.0059100
0.0042800 0.0136500
0.0096100 0.0214300
0.0170400 0.0308900
0.0265300 0.0403200
0.0380600 0.0504800
0.0515600 0.0601400
0.0669900 0.0701300
0.0842700 0.0792800
0.1033200 0.0883600
0.1240800 0.0963900
0.1464500 0.1037200
0.1703300 0.1095400
0.1956200 0.1144900
0.2222100 0.1179100
0.2500000 0.1203700
0.2788600 0.1210500
0.3086600 0.1204000
0.3392800 0.1169600
0.3705900 0.1128000
0.4024500 0.1075800
0.4347400 0.1020900
0.4673000 0.0960600
0.5000000 0.0899700
0.5327000 0.0836300
0.5652600 0.0774000
0.5975500 0.0711300
0.6294100 0.0651200
0.6607200 0.0591300
0.6913400 0.0535500
0.7211400 0.0480200
0.7500000 0.0429100
0.7777900 0.0379400
0.8043800 0.0333900
0.8296700 0.0290200
0.8535500 0.0250300
0.8759200 0.0211800
0.8966800 0.0175800
0.9157300 0.0140800
0.9330100 0.0109000
0.9484400 0.0080100
0.9619400 0.0056100
0.9734700 0.0036700
0.9829600 0.0023100
0.9903900 0.0014300
0.9957200 0.0009900
0.9989300 0.0008400
0.0000000 0.0000000
0.0010700 -.0046400
0.0042800 -.0111500
0.0096100 -.0148200
0.0170400 -.0181700
0.0265300 -.0201600
0.0380600 -.0225500
0.0515600 -.0241400
0.0669900 -.0259800
0.0842700 -.0271300
0.1033200 -.0284900
0.1240800 -.0292900
0.1464500 -.0302100
0.1703300 -.0306400
0.1956200 -.0312300
0.2222100 -.0313400
0.2500000 -.0316600
0.2788600 -.0314300
0.3086600 -.0315400
0.3392800 -.0310500
0.3705900 -.0308800
0.4024500 -.0302500
0.4347400 -.0298400
0.4673000 -.0290800
0.5000000 -.0284600
0.5327000 -.0275700
0.5652600 -.0268100
0.5975500 -.0257800
0.6294100 -.0249000
0.6607200 -.0237600
0.6913400 -.0227600
0.7211400 -.0215200
0.7500000 -.0204400
0.7777900 -.0191400
0.8043800 -.0179700
0.8296700 -.0166200
0.8535500 -.0153600
0.8759200 -.0139700
0.8966800 -.0126300
0.9157300 -.0111500
0.9330100 -.0096200
0.9484400 -.0079300
0.9619400 -.0062700
0.9734700 -.0046400
0.9829600 -.0032500
0.9903900 -.0021600
0.9957200 -.0014100
0.9989300 -.0009700
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Polars for WORTMANN FX 77-W-153 AIRFOIL (fx77w153-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| fx77w153-il | 50,000 | 9 | 7.8 at α=-1° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx77w153-il | 50,000 | 5 | 16 at α=3° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx77w153-il | 100,000 | 9 | 17.5 at α=2.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx77w153-il | 100,000 | 5 | 33.8 at α=8.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx77w153-il | 200,000 | 9 | 50.1 at α=12.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx77w153-il | 200,000 | 5 | 61.5 at α=11.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx77w153-il | 500,000 | 9 | 102.3 at α=10.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx77w153-il | 500,000 | 5 | 101.9 at α=9° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx77w153-il | 1,000,000 | 9 | 133.1 at α=8.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx77w153-il | 1,000,000 | 5 | 124 at α=7° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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