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GOE 10K AIRFOIL (goe10k-il)

GOE 10K AIRFOIL - Gottingen 10K airfoil


Airfoil goe10k-il
Details Dat file Parser  
(goe10k-il) GOE 10K AIRFOIL
Gottingen 10K airfoil
Max thickness 3.9% at 50% chord.
Max camber 1.4% at 60% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 10K AIRFOIL
       15.       15.

 0.0000000 0.0000000
 0.0250000 0.0100900
 0.0500000 0.0139800
 0.1000000 0.0192700
 0.1500000 0.0232600
 0.2000000 0.0263400
 0.3000000 0.0305100
 0.4000000 0.0323800
 0.5000000 0.0333500
 0.6000000 0.0328200
 0.7000000 0.0293900
 0.8000000 0.0232600
 0.9000000 0.0141300
 0.9500000 0.0084100
 1.0000000 0.0000000

 0.0000000 0.0000000
 0.0250000 -.0066100
 0.0500000 -.0078100
 0.1000000 -.0082300
 0.1500000 -.0078500
 0.2000000 -.0074600
 0.3000000 -.0066900
 0.4000000 -.0059200
 0.5000000 -.0051500
 0.6000000 -.0043800
 0.7000000 -.0036100
 0.8000000 -.0028400
 0.9000000 -.0020700
 0.9500000 -.0016900
 1.0000000 0.0000000
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Lednicer format dat file
Selig format dat file

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Polars for GOE 10K AIRFOIL (goe10k-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe10k-il50,000920.6 at α=3.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe10k-il50,000522.7 at α=3.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe10k-il100,000927.8 at α=3.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe10k-il100,000533.1 at α=2.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe10k-il200,000947.1 at α=2.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe10k-il200,000556.4 at α=2°Mach=0 Ncrit=5Xfoil predictionDetails
   goe10k-il500,000988.5 at α=1.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe10k-il500,000574.8 at α=1°Mach=0 Ncrit=5Xfoil predictionDetails
   goe10k-il1,000,0009111.6 at α=4°Mach=0 Ncrit=9Xfoil predictionDetails
   goe10k-il1,000,000561 at α=3°Mach=0 Ncrit=5Xfoil predictionDetails
Reynolds number calculator
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