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FX 63-137 13.7% smoothed (fx63137sm-il)

FX 63-137 13.7% smoothed - Wortmann FX 63-137 airfoil (smoothed)


Airfoil fx63137sm-il
Details Dat file Parser  
(fx63137sm-il) FX 63-137 13.7% smoothed
Wortmann FX 63-137 airfoil (smoothed)
Max thickness 13.7% at 30.9% chord.
Max camber 5.8% at 56.5% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Selig format
FX 63-137 13.7% smoothed
1.000000  0.000000
0.995720  0.002261
0.982960  0.008222
0.961940  0.016421
0.933010  0.025814
0.896680  0.036153
0.853550  0.047568
0.804380  0.060006
0.750000  0.073047
0.691340  0.085959
0.629410  0.097879
0.565260  0.107990
0.500000  0.115624
0.434740  0.120314
0.370590  0.121797 
0.339280  0.121303
0.308660  0.119983
0.278860  0.117849
0.250000  0.114919
0.222210  0.111224
0.195620  0.106801
0.170330  0.101685
0.146450  0.095912
0.124080  0.089547
0.103320  0.082700
0.084270  0.075518
0.066990  0.068116
0.051560  0.060520
0.038060  0.052636
0.026530  0.044302
0.017040  0.035484
0.009610  0.026362
0.004280  0.017421
0.001070  0.009265
0.000000  0.002411
0.001070  -.002958
0.004280  -.007021
0.009610  -.010156
0.017040  -.012751
0.026530  -.015034
0.038060  -.017064
0.051560  -.018791
0.066990  -.020178
0.084270  -.021230
0.103320  -.021987
0.124080  -.022482
0.146450  -.022718
0.170330  -.022668
0.195620  -.022297
0.222210  -.021567
0.250000  -.020431
0.278860  -.018838
0.308660  -.016752
0.339280  -.014179
0.370590  -.011176
0.434740  -.004210
0.500000  0.003409
0.565260  0.010919
0.629410  0.017605
0.691340  0.022871
0.750000  0.026291
0.804380  0.027582
0.853550  0.026608
0.896680  0.023429
0.933010  0.018408
0.961940  0.012286
0.982960  0.006230
0.995720  0.001696
1.000000  0.000000
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Lednicer format dat file
Selig format dat file

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Polars for FX 63-137 13.7% smoothed (fx63137sm-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   fx63137sm-il50,000925.9 at α=11.75°Mach=0 Ncrit=9Xfoil predictionDetails
   fx63137sm-il50,000531.6 at α=7.25°Mach=0 Ncrit=5Xfoil predictionDetails
   fx63137sm-il100,000960.5 at α=7.25°Mach=0 Ncrit=9Xfoil predictionDetails
   fx63137sm-il100,000564.5 at α=6°Mach=0 Ncrit=5Xfoil predictionDetails
   fx63137sm-il200,000991.5 at α=5.75°Mach=0 Ncrit=9Xfoil predictionDetails
   fx63137sm-il200,000588.9 at α=4.75°Mach=0 Ncrit=5Xfoil predictionDetails
   fx63137sm-il500,0009125.6 at α=4°Mach=0 Ncrit=9Xfoil predictionDetails
   fx63137sm-il500,0005117.9 at α=3.75°Mach=0 Ncrit=5Xfoil predictionDetails
   fx63137sm-il1,000,0009151.5 at α=3°Mach=0 Ncrit=9Xfoil predictionDetails
   fx63137sm-il1,000,0005137.6 at α=2.75°Mach=0 Ncrit=5Xfoil predictionDetails
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