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WORTMANN FX 62-K-131 AIRFOIL (fx62k131-il)

WORTMANN FX 62-K-131 AIRFOIL - Wortmann FX 62-K-131/17 airfoil


Airfoil fx62k131-il
Details Dat file Parser  
(fx62k131-il) WORTMANN FX 62-K-131 AIRFOIL
Wortmann FX 62-K-131/17 airfoil
Max thickness 13.1% at 40.2% chord.
Max camber 3.9% at 53.3% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
WORTMANN FX 62-K-131 AIRFOIL
      49.0      49.0

   0.00000   0.00000
   0.00107   0.00516
   0.00428   0.01037
   0.00961   0.01606
   0.01704   0.02207
   0.02653   0.02855
   0.03806   0.03511
   0.05156   0.04175
   0.06699   0.04830
   0.08427   0.05477
   0.10332   0.06108
   0.12408   0.06721
   0.14645   0.07306
   0.17033   0.07859
   0.19562   0.08369
   0.22221   0.08829
   0.25000   0.09232
   0.27886   0.09577
   0.30866   0.09860
   0.33928   0.10084
   0.37059   0.10245
   0.40245   0.10337
   0.43474   0.10355
   0.46730   0.10300
   0.50000   0.10173
   0.53270   0.09983
   0.56526   0.09728
   0.59755   0.09402
   0.62941   0.09000
   0.66072   0.08523
   0.69134   0.07976
   0.72114   0.07374
   0.75000   0.06732
   0.77779   0.06076
   0.80438   0.05425
   0.82967   0.04797
   0.85355   0.04203
   0.87592   0.03645
   0.89668   0.03123
   0.91573   0.02637
   0.93301   0.02183
   0.94844   0.01759
   0.96194   0.01363
   0.97347   0.00994
   0.98296   0.00661
   0.99039   0.00394
   0.99572   0.00180
   0.99893   0.00034
   1.00000   0.00000

   0.00000   0.00000
   0.00107  -0.00159
   0.00428  -0.00386
   0.00961  -0.00613
   0.01704  -0.00837
   0.02653  -0.01061
   0.03806  -0.01282
   0.05156  -0.01486
   0.06699  -0.01682
   0.08427  -0.01862
   0.10332  -0.02037
   0.12408  -0.02195
   0.14645  -0.02345
   0.17033  -0.02476
   0.19562  -0.02596
   0.22221  -0.02696
   0.25000  -0.02776
   0.27886  -0.02828
   0.30866  -0.02853
   0.33928  -0.02846
   0.37059  -0.02814
   0.40245  -0.02752
   0.43474  -0.02666
   0.46730  -0.02548
   0.50000  -0.02395
   0.53270  -0.02199
   0.56526  -0.01962
   0.59755  -0.01683
   0.62941  -0.01370
   0.66072  -0.01025
   0.69134  -0.00646
   0.72114  -0.00239
   0.75000   0.00177
   0.77779   0.00573
   0.80438   0.00919
   0.82967   0.01191
   0.85355   0.01386
   0.87592   0.01503
   0.89668   0.01548
   0.91573   0.01523
   0.93301   0.01437
   0.94844   0.01293
   0.96194   0.01102
   0.97347   0.00876
   0.98296   0.00636
   0.99039   0.00427
   0.99572   0.00228
   0.99893   0.00062
   1.00000   0.00000
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Polars for WORTMANN FX 62-K-131 AIRFOIL (fx62k131-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   fx62k131-il50,000529 at α=9.25°Mach=0 Ncrit=5Xfoil predictionDetails
   fx62k131-il50,000030.5 at α=9.5°Mach=0 Ncrit=9Xfoil predictionDetails
   fx62k131-il100,000555.1 at α=7.25°Mach=0 Ncrit=5Xfoil predictionDetails
   fx62k131-il100,000056.4 at α=8.25°Mach=0 Ncrit=9Xfoil predictionDetails
   fx62k131-il200,000584.1 at α=5.5°Mach=0 Ncrit=5Xfoil predictionDetails
   fx62k131-il200,000083.7 at α=6.75°Mach=0 Ncrit=9Xfoil predictionDetails
   fx62k131-il500,0005125.5 at α=3.5°Mach=0 Ncrit=5Xfoil predictionDetails
   fx62k131-il500,0000124 at α=4.5°Mach=0 Ncrit=9Xfoil predictionDetails
   fx62k131-il1,000,0005153.3 at α=2.5°Mach=0 Ncrit=5Xfoil predictionDetails
   fx62k131-il1,000,0000162.4 at α=3.25°Mach=0 Ncrit=9Xfoil predictionDetails
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