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FX 84-W-150 (fx84w150-il)

FX 84-W-150 - Wortmann FX 84-W-150 airfoil for use on wind turbines (W)


Airfoil fx84w150-il
Details Dat file Parser  
(fx84w150-il) FX 84-W-150
Wortmann FX 84-W-150 airfoil for use on wind turbines (W)
Max thickness 15% at 37.1% chord.
Max camber 4.2% at 40.2% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Selig format
FX 84-W-150
1.00000     0.00000
0.99893     0.00014
0.99572     0.00062
0.99039     0.00150
0.98296     0.00285
0.97347     0.00475
0.96194     0.00724
0.94844     0.01036
0.93301     0.01411
0.91573     0.01850
0.89668     0.02351
0.87592     0.02910
0.85355     0.03522
0.82967     0.04178
0.80438     0.04870
0.77779     0.05585
0.75000     0.06315
0.72114     0.07044
0.69134     0.07759
0.66072     0.08450
0.62941     0.09100
0.59755     0.09700
0.56526     0.10241
0.53270     0.10707
0.50000     0.11096
0.46730     0.11400
0.43474     0.11608
0.40245     0.11725
0.37059     0.11745
0.33928     0.11665
0.30866     0.11494
0.27886     0.11226
0.25000     0.10872
0.22221     0.10439
0.19562     0.09929
0.17033     0.09360
0.14645     0.08735
0.12408     0.08058
0.10332     0.07339
0.08427     0.06590
0.06699     0.05823
0.05156     0.05049
0.03806     0.04277
0.02653     0.03516
0.01704     0.02775
0.00961     0.02064
0.00428     0.01379
0.00107     0.00729
0.00000     0.00131
0.00107     -0.00413
0.00428     -0.00900
0.00961     -0.01343
0.01704     -0.01743
0.02653     -0.02090
0.03806     -0.02389
0.05156     -0.02643
0.06699     -0.02855
0.08427     -0.03028
0.10332     -0.03165
0.12408     -0.03271
0.14645     -0.03348
0.17033     -0.03400
0.19562     -0.03429
0.22221     -0.03439
0.25000     -0.03432
0.27886     -0.03409
0.30866     -0.03370
0.33928     -0.03315
0.37059     -0.03244
0.40245     -0.03156
0.43474     -0.03051
0.46730     -0.02929
0.50000     -0.02788
0.53270     -0.02629
0.56526     -0.02452
0.59755     -0.02258
0.62941     -0.02049
0.66072     -0.01828
0.69134     -0.01598
0.72114     -0.01366
0.75000     -0.01135
0.77779     -0.00910
0.80438     -0.00698
0.82967     -0.00502
0.85355     -0.00329
0.87592     -0.00181
0.89668     -0.00061
0.91573     0.00029
0.93301     0.00091
0.94844     0.00126
0.96194     0.00136
0.97347     0.00125
0.98296     0.00101
0.99039     0.00068
0.99572     0.00034
0.99893     0.00010
1.00000     0.00000
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Selig format dat file

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Polars for FX 84-W-150 (fx84w150-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   fx84w150-il50,00095.5 at α=9.25°Mach=0 Ncrit=9Xfoil predictionDetails
   fx84w150-il50,000514.6 at α=13.5°Mach=0 Ncrit=5Xfoil predictionDetails
   fx84w150-il100,000942.2 at α=10.75°Mach=0 Ncrit=9Xfoil predictionDetails
   fx84w150-il100,000547.4 at α=8°Mach=0 Ncrit=5Xfoil predictionDetails
   fx84w150-il200,000977.3 at α=8.5°Mach=0 Ncrit=9Xfoil predictionDetails
   fx84w150-il200,000577.4 at α=7.25°Mach=0 Ncrit=5Xfoil predictionDetails
   fx84w150-il500,0009116 at α=6.75°Mach=0 Ncrit=9Xfoil predictionDetails
   fx84w150-il500,0005111 at α=6.5°Mach=0 Ncrit=5Xfoil predictionDetails
   fx84w150-il1,000,0009146.3 at α=6°Mach=0 Ncrit=9Xfoil predictionDetails
   fx84w150-il1,000,0005133.3 at α=6°Mach=0 Ncrit=5Xfoil predictionDetails
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