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20-32C AIRFOIL (2032c-il)

20-32C AIRFOIL - Dillner 20-32-C low Reynolds number airfoil


Airfoil 2032c-il
Details Dat file Parser  
(2032c-il) 20-32C AIRFOIL
Dillner 20-32-C low Reynolds number airfoil
Max thickness 8% at 20% chord.
Max camber 6.9% at 40% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
20-32C AIRFOIL
       18.       18.

  0.000000  0.000000
  0.012500  0.019300
  0.025000  0.031700
  0.050000  0.051300
  0.075000  0.066400
  0.100000  0.078000
  0.150000  0.093400
  0.200000  0.101300
  0.250000  0.104400
  0.300000  0.104800
  0.400000  0.100200
  0.500000  0.090500
  0.600000  0.077100
  0.700000  0.061000
  0.800000  0.042800
  0.900000  0.022900
  0.950000  0.012400
  1.000000  0.001600

  0.000000  0.000000
  0.012500 -0.005000
  0.025000 -0.004200
  0.050000 -0.001000
  0.075000  0.002800
  0.100000  0.006800
  0.150000  0.014500
  0.200000  0.021700
  0.250000  0.028200
  0.300000  0.033300
  0.400000  0.038500
  0.500000  0.038600
  0.600000  0.035000
  0.700000  0.028600
  0.800000  0.020200
  0.900000  0.010000
  0.950000  0.004400
  1.000000 -0.001600
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Lednicer format dat file
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Polars for 20-32C AIRFOIL (2032c-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   2032c-il50,000931.7 at α=2.25°Mach=0 Ncrit=9Xfoil predictionDetails
   2032c-il50,000540.8 at α=3.75°Mach=0 Ncrit=5Xfoil predictionDetails
   2032c-il100,000954.9 at α=9°Mach=0 Ncrit=9Xfoil predictionDetails
   2032c-il100,000558.2 at α=5°Mach=0 Ncrit=5Xfoil predictionDetails
   2032c-il200,000975.3 at α=7.75°Mach=0 Ncrit=9Xfoil predictionDetails
   2032c-il200,000576.6 at α=5°Mach=0 Ncrit=5Xfoil predictionDetails
   2032c-il500,0009103.7 at α=6.5°Mach=0 Ncrit=9Xfoil predictionDetails
   2032c-il500,0005103.6 at α=5.5°Mach=0 Ncrit=5Xfoil predictionDetails
   2032c-il1,000,0009126.8 at α=5.5°Mach=0 Ncrit=9Xfoil predictionDetails
   2032c-il1,000,0005124.9 at α=5°Mach=0 Ncrit=5Xfoil predictionDetails
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