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WORTMANN FX 66-17A-175 AIRFOIL (fx66a175-il)

WORTMANN FX 66-17A-175 AIRFOIL - Wortmann FX 66-17A-175 airfoil


Airfoil fx66a175-il
Details Dat file Parser  
(fx66a175-il) WORTMANN FX 66-17A-175 AIRFOIL
Wortmann FX 66-17A-175 airfoil
Max thickness 17.5% at 33.9% chord.
Max camber 4.2% at 40.2% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
WORTMANN FX 66-17A-175 AIRFOIL
       44.       44.

  0.000000  0.000000
  0.001070  0.004710
  0.004280  0.010260
  0.009610  0.017130
  0.017040  0.024960
  0.026530  0.033470
  0.038060  0.042400
  0.051560  0.051610
  0.066990  0.060870
  0.084270  0.070110
  0.103320  0.079110
  0.124080  0.087830
  0.146450  0.096040
  0.170330  0.103750
  0.195620  0.110670
  0.222210  0.116850
  0.250000  0.121920
  0.278860  0.125860
  0.308660  0.128090
  0.339280  0.128890
  0.370590  0.127680
  0.402450  0.125150
  0.434740  0.121020
  0.467300  0.115930
  0.500000  0.109860
  0.532700  0.103380
  0.565260  0.096470
  0.597550  0.089520
  0.629410  0.082500
  0.660720  0.075690
  0.691340  0.069060
  0.721140  0.062740
  0.750000  0.056560
  0.777790  0.050690
  0.804380  0.045060
  0.829670  0.039750
  0.853550  0.034690
  0.875920  0.029990
  0.915730  0.021460
  0.948440  0.014160
  0.973470  0.007810
  0.990390  0.002410
  0.998930  0.000140
  1.000000  0.000000

  0.000000  0.000000
  0.001070 -0.002600
  0.004280 -0.005930
  0.009610 -0.009380
  0.017040 -0.013070
  0.026530 -0.016730
  0.038060 -0.020430
  0.051560 -0.023980
  0.066990 -0.027460
  0.084270 -0.030710
  0.103320 -0.033810
  0.124080 -0.036630
  0.146450 -0.039210
  0.170330 -0.041470
  0.195620 -0.043400
  0.222210 -0.044970
  0.250000 -0.046060
  0.278860 -0.046770
  0.308660 -0.046830
  0.339280 -0.046270
  0.370590 -0.044580
  0.402450 -0.042020
  0.434740 -0.038070
  0.467300 -0.033420
  0.500000 -0.028530
  0.532700 -0.023840
  0.565260 -0.019390
  0.597550 -0.015340
  0.629410 -0.011730
  0.660720 -0.008560
  0.691340 -0.005900
  0.721140 -0.003680
  0.750000 -0.001910
  0.777790 -0.000510
  0.804380  0.000480
  0.829670  0.001220
  0.853550  0.001670
  0.875920  0.001900
  0.915730  0.001770
  0.948440  0.001270
  0.973470  0.000810
  0.990390  0.000270
  0.998930  0.000100
  1.000000  0.000000
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Lednicer format dat file
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Polars for WORTMANN FX 66-17A-175 AIRFOIL (fx66a175-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   fx66a175-il50,00094.9 at α=10.25°Mach=0 Ncrit=9Xfoil predictionDetails
   fx66a175-il50,000512.3 at α=1.75°Mach=0 Ncrit=5Xfoil predictionDetails
   fx66a175-il100,000912.6 at α=1.25°Mach=0 Ncrit=9Xfoil predictionDetails
   fx66a175-il100,000534.2 at α=5.25°Mach=0 Ncrit=5Xfoil predictionDetails
   fx66a175-il200,000970.1 at α=9.5°Mach=0 Ncrit=9Xfoil predictionDetails
   fx66a175-il200,000571.5 at α=9°Mach=0 Ncrit=5Xfoil predictionDetails
   fx66a175-il500,0009103.3 at α=8.25°Mach=0 Ncrit=9Xfoil predictionDetails
   fx66a175-il500,0005100.6 at α=7.75°Mach=0 Ncrit=5Xfoil predictionDetails
   fx66a175-il1,000,0009128.4 at α=7.5°Mach=0 Ncrit=9Xfoil predictionDetails
   fx66a175-il1,000,0005124.1 at α=7.25°Mach=0 Ncrit=5Xfoil predictionDetails
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