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FX60-100 10.0% smoothed (fx60100sm-il)

FX60-100 10.0% smoothed - Wortmann FX 60-100 airfoil (smoothed)


Airfoil fx60100sm-il
Details Dat file Parser  
(fx60100sm-il) FX60-100 10.0% smoothed
Wortmann FX 60-100 airfoil (smoothed)
Max thickness 10% at 27.9% chord.
Max camber 3.5% at 56.5% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Selig format
   FX60-100 10.0% smoothed
   1.00000  0.0
   0.99572  0.00087
   0.98296  0.00344
   0.96194  0.00765
   0.93301  0.01342
   0.89668  0.02056
   0.85355  0.02875
   0.80438  0.03754
   0.75000  0.04643
   0.69134  0.05491
   0.62941  0.06255
   0.56526  0.06902
   0.50000  0.07402
   0.43474  0.07735
   0.37059  0.07880
   0.33928  0.07876
   0.30866  0.07819
   0.27886  0.07708
   0.25000  0.07543
   0.22221  0.07326
   0.19562  0.07059
   0.17033  0.06743
   0.14645  0.06383
   0.12408  0.05982
   0.10332  0.05545
   0.08427  0.05078
   0.06699  0.04584
   0.05156  0.04064
   0.03806  0.03517
   0.02653  0.02937
   0.01704  0.02331
   0.00961  0.01715
   0.00428  0.01123
   0.00107  0.00589
   0.0      0.00142
   0.00107 -0.00216
   0.00428 -0.00503
   0.00961 -0.00751
   0.01704 -0.00991
   0.02653 -0.01235
   0.03806 -0.01482
   0.05156 -0.01719
   0.06699 -0.01933
   0.08427 -0.02115
   0.10332 -0.02265
   0.12408 -0.02381
   0.14645 -0.02464
   0.17033 -0.02510
   0.19562 -0.02518
   0.22221 -0.02483
   0.25000 -0.02402
   0.27886 -0.02273
   0.30866 -0.02096
   0.33928 -0.01874
   0.37059 -0.01617
   0.43474 -0.01029
   0.50000 -0.00404
   0.56526  0.00192
   0.62941  0.00702
   0.69134  0.01081
   0.75000  0.01305
   0.80438  0.01367
   0.85355  0.01281
   0.89668  0.01080
   0.93301  0.00808
   0.96194  0.00514
   0.98296  0.00250
   0.99572  0.00066
   1.00000  0.0
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Lednicer format dat file
Selig format dat file

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Polars for FX60-100 10.0% smoothed (fx60100sm-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   fx60100sm-il50,000940.6 at α=6.5°Mach=0 Ncrit=9Xfoil predictionDetails
   fx60100sm-il50,000542.6 at α=5.75°Mach=0 Ncrit=5Xfoil predictionDetails
   fx60100sm-il100,000962.8 at α=5.5°Mach=0 Ncrit=9Xfoil predictionDetails
   fx60100sm-il100,000561.6 at α=4.75°Mach=0 Ncrit=5Xfoil predictionDetails
   fx60100sm-il200,000985.2 at α=4.25°Mach=0 Ncrit=9Xfoil predictionDetails
   fx60100sm-il200,000579.1 at α=3.75°Mach=0 Ncrit=5Xfoil predictionDetails
   fx60100sm-il500,0009112.7 at α=3.75°Mach=0 Ncrit=9Xfoil predictionDetails
   fx60100sm-il500,000591.5 at α=3.75°Mach=0 Ncrit=5Xfoil predictionDetails
   fx60100sm-il1,000,0009120.1 at α=4.75°Mach=0 Ncrit=9Xfoil predictionDetails
   fx60100sm-il1,000,0005100.7 at α=6.25°Mach=0 Ncrit=5Xfoil predictionDetails
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