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GOE 9K AIRFOIL (goe09k-il)

GOE 9K AIRFOIL - Gottingen 9K airfoil


Airfoil goe09k-il
Details Dat file Parser  
(goe09k-il) GOE 9K AIRFOIL
Gottingen 9K airfoil
Max thickness 2.5% at 50% chord.
Max camber 0.9% at 60% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 9K AIRFOIL
       15.       15.

 0.0000000 0.0000000
 0.0250000 0.0063200
 0.0500000 0.0088500
 0.1000000 0.0122000
 0.1500000 0.0147500
 0.2000000 0.0167000
 0.3000000 0.0193000
 0.4000000 0.0205000
 0.5000000 0.0212000
 0.6000000 0.0209000
 0.7000000 0.0187000
 0.8000000 0.0148000
 0.9000000 0.0090000
 0.9500000 0.0053500
 1.0000000 0.0000000

 0.0000000 0.0000000
 0.0250000 -.0042800
 0.0500000 -.0050500
 0.1000000 -.0053000
 0.1500000 -.0050500
 0.2000000 -.0048000
 0.3000000 -.0043000
 0.4000000 -.0038000
 0.5000000 -.0033000
 0.6000000 -.0028000
 0.7000000 -.0023000
 0.8000000 -.0018000
 0.9000000 -.0013000
 0.9500000 -.0010500
 1.0000000 0.0000000
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Lednicer format dat file
Selig format dat file

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Polars for GOE 9K AIRFOIL (goe09k-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe09k-il50,000920.1 at α=2.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe09k-il50,000518.7 at α=2.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe09k-il100,000923.8 at α=2°Mach=0 Ncrit=9Xfoil predictionDetails
   goe09k-il100,000523.8 at α=2°Mach=0 Ncrit=5Xfoil predictionDetails
   goe09k-il200,000929.3 at α=1.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe09k-il200,000529.1 at α=1.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe09k-il500,000979.4 at α=3.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe09k-il500,000560.5 at α=1°Mach=0 Ncrit=5Xfoil predictionDetails
   goe09k-il1,000,000977.7 at α=1°Mach=0 Ncrit=9Xfoil predictionDetails
   goe09k-il1,000,000563.4 at α=0.5°Mach=0 Ncrit=5Xfoil predictionDetails
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