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WORTMANN FX 63-137 AIRFOIL (fx63137-il)

WORTMANN FX 63-137 AIRFOIL - Wortmann FX 63-137 human power aircraft airfoil (Liver Puffin) airfoil


Airfoil fx63137-il
Details Dat file Parser  
(fx63137-il) WORTMANN FX 63-137 AIRFOIL
Wortmann FX 63-137 human power aircraft airfoil (Liver Puffin) airfoil
Max thickness 13.7% at 30.9% chord.
Max camber 6% at 53.3% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
WORTMANN FX 63-137 AIRFOIL
      49.0      49.0

  0.000000  0.000000
  0.001070  0.009000
  0.004280  0.017500
  0.009610  0.027400
  0.017040  0.036250
  0.026530  0.044800
  0.038060  0.052480
  0.051560  0.060050
  0.066990  0.068360
  0.084270  0.075550
  0.103320  0.083130
  0.124080  0.089610
  0.146450  0.096220
  0.170330  0.101650
  0.195620  0.107040
  0.222210  0.111220
  0.250000  0.115220
  0.278860  0.117920
  0.308660  0.120240
  0.339280  0.121280
  0.370590  0.121910
  0.402450  0.121370
  0.434740  0.120420
  0.467300  0.118330
  0.500000  0.115780
  0.532700  0.112210
  0.565260  0.108230
  0.597550  0.103310
  0.629410  0.098040
  0.660720  0.092040
  0.691340  0.085900
  0.721140  0.079270
  0.750000  0.072730
  0.777790  0.066050
  0.804380  0.059620
  0.829670  0.053230
  0.853550  0.047110
  0.875920  0.041140
  0.896680  0.035530
  0.915730  0.030180
  0.933010  0.025160
  0.948440  0.020430
  0.961940  0.016010
  0.973470  0.011890
  0.982960  0.008180
  0.990390  0.005010
  0.995720  0.002490
  0.998930  0.000820
  1.000000  0.000000

  0.000000  0.000000
  0.001070 -0.002320
  0.004280 -0.005660
  0.009610 -0.009950
  0.017040 -0.012540
  0.026530 -0.015370
  0.038060 -0.016980
  0.051560 -0.018870
  0.066990 -0.019920
  0.084270 -0.021220
  0.103320 -0.021800
  0.124080 -0.022560
  0.146450 -0.022630
  0.170330 -0.022770
  0.195620 -0.022200
  0.222210 -0.021610
  0.250000 -0.020340
  0.278860 -0.018950
  0.308660 -0.016880
  0.339280 -0.014600
  0.370590 -0.011670
  0.402450 -0.008480
  0.434740 -0.004860
  0.467300 -0.001030
  0.500000  0.003070
  0.532700  0.007160
  0.565260  0.011120
  0.597550  0.014750
  0.629410  0.018130
  0.660720  0.020980
  0.691340  0.023450
  0.721140  0.025300
  0.750000  0.026680
  0.777790  0.027450
  0.804380  0.027680
  0.829670  0.027290
  0.853550  0.026310
  0.875920  0.024790
  0.896680  0.022840
  0.915730  0.020520
  0.933010  0.017940
  0.948440  0.015140
  0.961940  0.012190
  0.973470  0.009210
  0.982960  0.006300
  0.990390  0.003730
  0.995720  0.001690
  0.998930  0.000400
  1.000000  0.000000
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Lednicer format dat file
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Polars for WORTMANN FX 63-137 AIRFOIL (fx63137-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   fx63137-il50,000926.8 at α=11°Mach=0 Ncrit=9Xfoil predictionDetails
   fx63137-il50,000531.6 at α=6.5°Mach=0 Ncrit=5Xfoil predictionDetails
   fx63137-il100,000962.1 at α=7.5°Mach=0 Ncrit=9Xfoil predictionDetails
   fx63137-il100,000563.9 at α=6°Mach=0 Ncrit=5Xfoil predictionDetails
   fx63137-il200,000990.6 at α=6.25°Mach=0 Ncrit=9Xfoil predictionDetails
   fx63137-il200,000585.2 at α=3.75°Mach=0 Ncrit=5Xfoil predictionDetails
   fx63137-il500,0009119.1 at α=3.5°Mach=0 Ncrit=9Xfoil predictionDetails
   fx63137-il500,0005103.6 at α=1.25°Mach=0 Ncrit=5Xfoil predictionDetails
   fx63137-il1,000,0009132.5 at α=2.25°Mach=0 Ncrit=9Xfoil predictionDetails
   fx63137-il1,000,0005105.7 at α=1.5°Mach=0 Ncrit=5Xfoil predictionDetails
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