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FX 83-W-108 (fx83w108-il)

FX 83-W-108 - Wortmann FX 83-W-108 airfoil for use on wind turbines (W)


Airfoil fx83w108-il
Details Dat file Parser  
(fx83w108-il) FX 83-W-108
Wortmann FX 83-W-108 airfoil for use on wind turbines (W)
Max thickness 10.9% at 30.9% chord.
Max camber 4.2% at 53.3% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Selig format
FX 83-W-108
1.00000     0.00000
0.99893     0.00106
0.99572     0.00205
0.99039     0.00367
0.98296     0.00585
0.97347     0.00855
0.96194     0.01168
0.94844     0.01515
0.93301     0.01888
0.91573     0.02293
0.89668     0.02728
0.87592     0.03197
0.85355     0.03690
0.82967     0.04206
0.80438     0.04735
0.77779     0.05279
0.75000     0.05820
0.72114     0.06358
0.69134     0.06875
0.66072     0.07366
0.62941     0.07809
0.59755     0.08200
0.56526     0.08526
0.53270     0.08784
0.50000     0.08974
0.46730     0.09093
0.43474     0.09142
0.40245     0.09128
0.37059     0.09045
0.33928     0.08903
0.30866     0.08703
0.27886     0.08453
0.25000     0.08156
0.22221     0.07816
0.19562     0.07436
0.17033     0.07019
0.14645     0.06571
0.12408     0.06092
0.10332     0.05590
0.08427     0.05066
0.06699     0.04530
0.05156     0.03975
0.03806     0.03416
0.02653     0.02843
0.01704     0.02279
0.00961     0.01704
0.00428     0.01135
0.00107     0.00550
0.00000     0.00000
0.00107     -0.00420
0.00428     -0.00876
0.00961     -0.01252
0.01704     -0.01574
0.02653     -0.01841
0.03806     -0.02073
0.05156     -0.02267
0.06699     -0.02437
0.08427     -0.02577
0.10332     -0.02687
0.12408     -0.02762
0.14645     -0.02803
0.17033     -0.02803
0.19562     -0.02760
0.22221     -0.02675
0.25000     -0.02545
0.27886     -0.02376
0.30866     -0.02165
0.33928     -0.01916
0.37059     -0.01638
0.40245     -0.01358
0.43474     -0.01072
0.46730     -0.00804
0.50000     -0.00548
0.53270     -0.00312
0.56526     -0.00097
0.59755     0.00095
0.62941     0.00267
0.66072     0.00408
0.69134     0.00529
0.72114     0.00622
0.75000     0.00695
0.77779     0.00734
0.80438     0.00754
0.82967     0.00746
0.85355     0.00724
0.87592     0.00680
0.89668     0.00624
0.91573     0.00549
0.93301     0.00467
0.94844     0.00375
0.96194     0.00283
0.97347     0.00193
0.98296     0.00113
0.99039     0.00043
0.99572     -0.00014
0.99893     -0.00055
1.00000     0.00000
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Polars for FX 83-W-108 (fx83w108-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   fx83w108-il50,000936.8 at α=8°Mach=0 Ncrit=9Xfoil predictionDetails
   fx83w108-il50,000534.5 at α=7.75°Mach=0 Ncrit=5Xfoil predictionDetails
   fx83w108-il100,000961 at α=7°Mach=0 Ncrit=9Xfoil predictionDetails
   fx83w108-il100,000560.4 at α=6.25°Mach=0 Ncrit=5Xfoil predictionDetails
   fx83w108-il200,000990.5 at α=6°Mach=0 Ncrit=9Xfoil predictionDetails
   fx83w108-il200,000586.8 at α=4.75°Mach=0 Ncrit=5Xfoil predictionDetails
   fx83w108-il500,0009129.6 at α=4.25°Mach=0 Ncrit=9Xfoil predictionDetails
   fx83w108-il500,0005117.7 at α=3.25°Mach=0 Ncrit=5Xfoil predictionDetails
   fx83w108-il1,000,0009157.2 at α=3.5°Mach=0 Ncrit=9Xfoil predictionDetails
   fx83w108-il1,000,0005115.4 at α=2.75°Mach=0 Ncrit=5Xfoil predictionDetails
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