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FX 84-W-175 (fx84w175-il)

FX 84-W-175 - Wortmann FX 84-W-175 airfoil for use on wind turbines (W)


Airfoil fx84w175-il
Details Dat file Parser  
(fx84w175-il) FX 84-W-175
Wortmann FX 84-W-175 airfoil for use on wind turbines (W)
Max thickness 17.6% at 37.1% chord.
Max camber 4.4% at 43.5% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Selig format
FX 84-W-175
1.00000     0.00000
0.99893     0.00016
0.99572     0.00068
0.99039     0.00168
0.98296     0.00321
0.97347     0.00536
0.96194     0.00817
0.94844     0.01169
0.93301     0.01594
0.91573     0.02092
0.89668     0.02661
0.87592     0.03295
0.85355     0.03988
0.82967     0.04731
0.80438     0.05512
0.77779     0.06320
0.75000     0.07140
0.72114     0.07958
0.69134     0.08758
0.66072     0.09526
0.62941     0.10249
0.59755     0.10912
0.56526     0.11505
0.53270     0.12016
0.50000     0.12438
0.46730     0.12762
0.43474     0.12985
0.40245     0.13103
0.37059     0.13114
0.33928     0.13019
0.30866     0.12818
0.27886     0.12516
0.25000     0.12119
0.22221     0.11632
0.19562     0.11067
0.17033     0.10432
0.14645     0.09734
0.12408     0.08980
0.10332     0.08179
0.08427     0.07342
0.06699     0.06483
0.05156     0.05612
0.03806     0.04740
0.02653     0.03876
0.01704     0.03029
0.00961     0.02210
0.00428     0.01431
0.00107     0.00696
0.00000     0.00000
0.00107     -0.00658
0.00428     -0.01269
0.00961     -0.01823
0.01704     -0.02317
0.02653     -0.02754
0.03806     -0.03140
0.05156     -0.03476
0.06699     -0.03763
0.08427     -0.04005
0.10332     -0.04205
0.12408     -0.04367
0.14645     -0.04493
0.17033     -0.04586
0.19562     -0.04649
0.22221     -0.04684
0.25000     -0.04694
0.27886     -0.04680
0.30866     -0.04643
0.33928     -0.04581
0.37059     -0.04495
0.40245     -0.04384
0.43474     -0.04246
0.46730     -0.04082
0.50000     -0.03891
0.53270     -0.03674
0.56526     -0.03431
0.59755     -0.03165
0.62941     -0.02879
0.66072     -0.02578
0.69134     -0.02265
0.72114     -0.01949
0.75000     -0.01634
0.77779     -0.01330
0.80438     -0.01041
0.82967     -0.00776
0.85355     -0.00541
0.87592     -0.00338
0.89668     -0.00172
0.91573     -0.00044
0.93301     0.00047
0.94844     0.00102
0.96194     0.00126
0.97347     0.00124
0.98296     0.00103
0.99039     0.00072
0.99572     0.00037
0.99893     0.00011
1.00000     0.00000
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Polars for FX 84-W-175 (fx84w175-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   fx84w175-il50,00094.5 at α=12°Mach=0 Ncrit=9Xfoil predictionDetails
   fx84w175-il50,000510.3 at α=8.75°Mach=0 Ncrit=5Xfoil predictionDetails
   fx84w175-il100,000926.6 at α=14°Mach=0 Ncrit=9Xfoil predictionDetails
   fx84w175-il100,000534.1 at α=8°Mach=0 Ncrit=5Xfoil predictionDetails
   fx84w175-il200,000968.4 at α=9.5°Mach=0 Ncrit=9Xfoil predictionDetails
   fx84w175-il200,000569.8 at α=6.75°Mach=0 Ncrit=5Xfoil predictionDetails
   fx84w175-il500,0009108.6 at α=7.25°Mach=0 Ncrit=9Xfoil predictionDetails
   fx84w175-il500,0005100.1 at α=6°Mach=0 Ncrit=5Xfoil predictionDetails
   fx84w175-il1,000,0009135.1 at α=6.75°Mach=0 Ncrit=9Xfoil predictionDetails
   fx84w175-il1,000,0005124 at α=6°Mach=0 Ncrit=5Xfoil predictionDetails
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