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WORTMANN FX 057-816 (fx057816-il)

WORTMANN FX 057-816 - Wortmann FX 057-816 airfoil


Airfoil fx057816-il
Details Dat file Parser  
(fx057816-il) WORTMANN FX 057-816
Wortmann FX 057-816 airfoil
Max thickness 16.2% at 37.1% chord.
Max camber 5.1% at 37.1% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
WORTMANN FX 057-816
       13.       13.

  0.000000  0.000000
  0.017040  0.029790
  0.066990  0.062900
  0.146450  0.094790
  0.250000  0.118870
  0.370590  0.132260
  0.500000  0.122940
  0.629410  0.084080
  0.750000  0.051790
  0.853560  0.028300
  0.933020  0.012110
  0.982970  0.003340
  1.000000  0.000000

  0.000000  0.000000
  0.017040 -0.013530
  0.066990 -0.021280
  0.146450 -0.026730
  0.250000 -0.030190
  0.370590 -0.029580
  0.500000 -0.029060
  0.629410 -0.027280
  0.750000 -0.019190
  0.853560 -0.005420
  0.933020  0.001210
  0.982970  0.001360
  1.000000  0.000000
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Lednicer format dat file
Selig format dat file

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Polars for WORTMANN FX 057-816 (fx057816-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   fx057816-il50,00095 at α=10.5°Mach=0 Ncrit=9Xfoil predictionDetails
   fx057816-il50,000511.1 at α=15.25°Mach=0 Ncrit=5Xfoil predictionDetails
   fx057816-il100,000917.8 at α=13.75°Mach=0 Ncrit=9Xfoil predictionDetails
   fx057816-il100,000516.5 at α=13.5°Mach=0 Ncrit=5Xfoil predictionDetails
   fx057816-il200,000927.6 at α=12.25°Mach=0 Ncrit=9Xfoil predictionDetails
   fx057816-il200,000527.1 at α=11.5°Mach=0 Ncrit=5Xfoil predictionDetails
   fx057816-il500,0009113.8 at α=9.5°Mach=0 Ncrit=9Xfoil predictionDetails
   fx057816-il500,0005113.3 at α=8.25°Mach=0 Ncrit=5Xfoil predictionDetails
   fx057816-il1,000,0009155.8 at α=8.25°Mach=0 Ncrit=9Xfoil predictionDetails
   fx057816-il1,000,0005153 at α=7.25°Mach=0 Ncrit=5Xfoil predictionDetails
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