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CLARK YH AIRFOIL (clarkyh-il)

CLARK YH AIRFOIL - CLARK YH airfoil


Airfoil clarkyh-il
Details Dat file Parser  
(clarkyh-il) CLARK YH AIRFOIL
CLARK YH airfoil
Max thickness 11.9% at 30% chord.
Max camber 2.5% at 30% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
 CLARK YH AIRFOIL
       16.       16.

  0.000000  0.041000
  0.025000  0.068000
  0.050000  0.081000
  0.075000  0.090000
  0.100000  0.098000
  0.150000  0.108000
  0.200000  0.113000
  0.300000  0.119000
  0.400000  0.114500
  0.500000  0.105000
  0.600000  0.091000
  0.700000  0.075500
  0.800000  0.056000
  0.900000  0.037000
  0.950000  0.028500
  1.000000  0.021000

  0.000000  0.041000
  0.025000  0.018500
  0.050000  0.012000
  0.075000  0.007000
  0.100000  0.004500
  0.150000  0.000000
  0.200000  0.000000
  0.300000  0.000000
  0.400000  0.000000
  0.500000  0.000000
  0.600000  0.000000
  0.700000  0.000000
  0.800000  0.004000
  0.900000  0.010000
  0.950000  0.013700
  1.000000  0.020000
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Lednicer format dat file
Selig format dat file

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Polars for CLARK YH AIRFOIL (clarkyh-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   clarkyh-il50,000929.1 at α=8.5°Mach=0 Ncrit=9Xfoil predictionDetails
   clarkyh-il50,000533 at α=6°Mach=0 Ncrit=5Xfoil predictionDetails
   clarkyh-il100,000947.7 at α=5.5°Mach=0 Ncrit=9Xfoil predictionDetails
   clarkyh-il100,000549.2 at α=5.5°Mach=0 Ncrit=5Xfoil predictionDetails
   clarkyh-il200,000966 at α=5.25°Mach=0 Ncrit=9Xfoil predictionDetails
   clarkyh-il200,000562.3 at α=4.25°Mach=0 Ncrit=5Xfoil predictionDetails
   clarkyh-il500,000984 at α=3.75°Mach=0 Ncrit=9Xfoil predictionDetails
   clarkyh-il500,000577.7 at α=6°Mach=0 Ncrit=5Xfoil predictionDetails
   clarkyh-il1,000,000997.4 at α=6.25°Mach=0 Ncrit=9Xfoil predictionDetails
   clarkyh-il1,000,000589.1 at α=5.25°Mach=0 Ncrit=5Xfoil predictionDetails
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