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FX 74-130 WP1 (fx74130wp1-il)

FX 74-130 WP1 - Wortmann FX 74-130 WP1 airfoil


Airfoil fx74130wp1-il
Details Dat file Parser  
(fx74130wp1-il) FX 74-130 WP1
Wortmann FX 74-130 WP1 airfoil
Max thickness 13% at 46.7% chord.
Max camber 3.8% at 50% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Selig format
FX 74-130 WP1
1.00000     0.00000
0.99893     0.00051
0.99572     0.00169
0.99039     0.00328
0.98296     0.00531
0.97347     0.00776
0.96194     0.01066
0.94844     0.01406
0.93301     0.01794
0.91573     0.02232
0.89668     0.02729
0.87592     0.03286
0.85355     0.03902
0.82967     0.04568
0.80438     0.05284
0.77779     0.06055
0.75000     0.06850
0.72114     0.07606
0.69134     0.08272
0.66072     0.08829
0.62941     0.09301
0.59755     0.09694
0.56526     0.09991
0.53270     0.10187
0.50000     0.10290
0.46730     0.10318
0.43474     0.10278
0.40245     0.10170
0.37059     0.09999
0.33928     0.09768
0.30866     0.09481
0.27886     0.09142
0.25000     0.08755
0.22221     0.08323
0.19562     0.07850
0.17033     0.07342
0.14645     0.06802
0.12408     0.06235
0.10332     0.05646
0.08427     0.05042
0.06699     0.04428
0.05156     0.03808
0.03806     0.03192
0.02653     0.02589
0.01704     0.02003
0.00961     0.01450
0.00428     0.00923
0.00107     0.00426
0.00000     0.00000
0.00107     -0.00347
0.00428     -0.00616
0.00961     -0.00838
0.01704     -0.01051
0.02653     -0.01247
0.03806     -0.01428
0.05156     -0.01599
0.06699     -0.01755
0.08427     -0.01898
0.10332     -0.02030
0.12408     -0.02150
0.14645     -0.02260
0.17033     -0.02358
0.19562     -0.02445
0.22221     -0.02520
0.25000     -0.02584
0.27886     -0.02637
0.30866     -0.02679
0.33928     -0.02708
0.37059     -0.02725
0.40245     -0.02728
0.43474     -0.02719
0.46730     -0.02695
0.50000     -0.02657
0.53270     -0.02602
0.56526     -0.02530
0.59755     -0.02438
0.62941     -0.02322
0.66072     -0.02177
0.69134     -0.01997
0.72114     -0.01755
0.75000     -0.01433
0.77779     -0.01049
0.80438     -0.00657
0.82967     -0.00317
0.85355     -0.00050
0.87592     0.00151
0.89668     0.00290
0.91573     0.00372
0.93301     0.00405
0.94844     0.00400
0.96194     0.00364
0.97347     0.00305
0.98296     0.00234
0.99039     0.00160
0.99572     0.00093
0.99893     0.00032
1.00000     0.00000
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Selig format dat file

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Polars for FX 74-130 WP1 (fx74130wp1-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   fx74130wp1-il50,000924.1 at α=10°Mach=0 Ncrit=9Xfoil predictionDetails
   fx74130wp1-il50,000523.8 at α=9.75°Mach=0 Ncrit=5Xfoil predictionDetails
   fx74130wp1-il100,000939.7 at α=9°Mach=0 Ncrit=9Xfoil predictionDetails
   fx74130wp1-il100,000539.8 at α=8.25°Mach=0 Ncrit=5Xfoil predictionDetails
   fx74130wp1-il200,000972 at α=7.75°Mach=0 Ncrit=9Xfoil predictionDetails
   fx74130wp1-il200,000571.2 at α=6.75°Mach=0 Ncrit=5Xfoil predictionDetails
   fx74130wp1-il500,0009119.3 at α=5.75°Mach=0 Ncrit=9Xfoil predictionDetails
   fx74130wp1-il500,0005115.8 at α=4.75°Mach=0 Ncrit=5Xfoil predictionDetails
   fx74130wp1-il1,000,0009152.6 at α=4.75°Mach=0 Ncrit=9Xfoil predictionDetails
   fx74130wp1-il1,000,0005145.6 at α=3.75°Mach=0 Ncrit=5Xfoil predictionDetails
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