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CLARK YS AIRFOIL (clarkys-il)

CLARK YS AIRFOIL - CLARK YS airfoil


Airfoil clarkys-il
Details Dat file Parser  
(clarkys-il) CLARK YS AIRFOIL
CLARK YS airfoil
Max thickness 11.7% at 30% chord.
Max camber 2.4% at 30% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
CLARK YS AIRFOIL
       17.       17.

 0.0000000 0.0000000
 0.0125000 0.0195000
 0.0250000 0.0300000
 0.0500000 0.0440000
 0.0750000 0.0535000
 0.1000000 0.0610000
 0.1500000 0.0718000
 0.2000000 0.0786000
 0.3000000 0.0820000
 0.4000000 0.0790000
 0.5000000 0.0702000
 0.6000000 0.0565000
 0.7000000 0.0385000
 0.8000000 0.0190000
 0.9000000 0.0080000
 0.9500000 0.0030000
 1.0000000 0.0000000

 0.0000000 0.0000000
 0.0125000 -.0157000
 0.0250000 -.0203000
 0.0500000 -.0257000
 0.0750000 -.0287000
 0.1000000 -.0308000
 0.1500000 -.0335000
 0.2000000 -.0347000
 0.3000000 -.0350000
 0.4000000 -.0350000
 0.5000000 -.0350000
 0.6000000 -.0350000
 0.7000000 -.0350000
 0.8000000 -.0330000
 0.9000000 -.0190000
 0.9500000 -.0100000
 1.0000000 0.0000000
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Lednicer format dat file
Selig format dat file

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Polars for CLARK YS AIRFOIL (clarkys-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   clarkys-il50,000923.2 at α=8.5°Mach=0 Ncrit=9Xfoil predictionDetails
   clarkys-il50,000531.7 at α=7.25°Mach=0 Ncrit=5Xfoil predictionDetails
   clarkys-il100,000945.7 at α=7.5°Mach=0 Ncrit=9Xfoil predictionDetails
   clarkys-il100,000547 at α=7.25°Mach=0 Ncrit=5Xfoil predictionDetails
   clarkys-il200,000962.2 at α=8°Mach=0 Ncrit=9Xfoil predictionDetails
   clarkys-il200,000558.1 at α=7.75°Mach=0 Ncrit=5Xfoil predictionDetails
   clarkys-il500,000976.5 at α=7.5°Mach=0 Ncrit=9Xfoil predictionDetails
   clarkys-il500,000568.3 at α=7.5°Mach=0 Ncrit=5Xfoil predictionDetails
   clarkys-il1,000,000985.7 at α=7.75°Mach=0 Ncrit=9Xfoil predictionDetails
   clarkys-il1,000,000580.2 at α=6.75°Mach=0 Ncrit=5Xfoil predictionDetails
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