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WORTMANN FX 082-512 AIRFOIL (fx082512-il)

WORTMANN FX 082-512 AIRFOIL - Wortmann FX 082-512 airfoil


Airfoil fx082512-il
Details Dat file Parser  
(fx082512-il) WORTMANN FX 082-512 AIRFOIL
Wortmann FX 082-512 airfoil
Max thickness 11.8% at 25% chord.
Max camber 4.2% at 62.9% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
 
WORTMANN FX 082-512 AIRFOIL
       13.       13.

  0.000000  0.000000
  0.017040  0.018340
  0.066990  0.035590
  0.146450  0.054400
  0.250000  0.069340
  0.370590  0.077630
  0.500000  0.079190
  0.629410  0.072920
  0.750000  0.060120
  0.853560  0.042850
  0.933020  0.024840
  0.982970  0.009150
  1.000000  0.000000

  0.000000  0.000000
  0.017040 -0.018020
  0.066990 -0.033030
  0.146450 -0.046340
  0.250000 -0.048660
  0.370590 -0.028110
  0.500000 -0.005910
  0.629410  0.010200
  0.750000  0.018980
  0.853560  0.019690
  0.933020  0.013900
  0.982970  0.005170
  1.000000  0.000000
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Lednicer format dat file
Selig format dat file

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Polars for WORTMANN FX 082-512 AIRFOIL (fx082512-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   fx082512-il50,000931.2 at α=5.5°Mach=0 Ncrit=9Xfoil predictionDetails
   fx082512-il50,000533.4 at α=5°Mach=0 Ncrit=5Xfoil predictionDetails
   fx082512-il100,000946.6 at α=4°Mach=0 Ncrit=9Xfoil predictionDetails
   fx082512-il100,000547.7 at α=3.25°Mach=0 Ncrit=5Xfoil predictionDetails
   fx082512-il200,000963.6 at α=2.5°Mach=0 Ncrit=9Xfoil predictionDetails
   fx082512-il200,000560.2 at α=1.5°Mach=0 Ncrit=5Xfoil predictionDetails
   fx082512-il500,000983.7 at α=0.75°Mach=0 Ncrit=9Xfoil predictionDetails
   fx082512-il500,000575.3 at α=-0.25°Mach=0 Ncrit=5Xfoil predictionDetails
   fx082512-il1,000,000999.1 at α=-0.5°Mach=0 Ncrit=9Xfoil predictionDetails
   fx082512-il1,000,000582.1 at α=5.25°Mach=0 Ncrit=5Xfoil predictionDetails
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