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GOE 7K AIRFOIL (goe07k-il)

GOE 7K AIRFOIL - Gottingen 7K airfoil


Airfoil goe07k-il
Details Dat file Parser  
(goe07k-il) GOE 7K AIRFOIL
Gottingen 7K airfoil
Max thickness 11% at 50% chord.
Max camber 4.5% at 50% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 7K AIRFOIL
       16.       16.

 0.0000000 0.0000000
 0.0250000 0.0231100
 0.0500000 0.0344300
 0.0750000 0.0433400
 0.1000000 0.0513500
 0.1500000 0.0641800
 0.2000000 0.0741000
 0.3000000 0.0891500
 0.4000000 0.0975000
 0.5000000 0.1004500
 0.6000000 0.0980000
 0.7000000 0.0871500
 0.8000000 0.0686000
 0.9000000 0.0409500
 0.9500000 0.0237800
 1.0000000 0.0000000

 0.0000000 0.0000000
 0.0250000 -.0102900
 0.0500000 -.0116800
 0.0750000 -.0124600
 0.1000000 -.0129500
 0.1500000 -.0136200
 0.2000000 -.0133000
 0.3000000 -.0120500
 0.4000000 -.0108000
 0.5000000 -.0095500
 0.6000000 -.0083000
 0.7000000 -.0070500
 0.8000000 -.0058000
 0.9000000 -.0045500
 0.9500000 -.0039300
 1.0000000 0.0000000
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Lednicer format dat file
Selig format dat file

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Polars for GOE 7K AIRFOIL (goe07k-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe07k-il50,000924.4 at α=9.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe07k-il50,000525.2 at α=8.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe07k-il100,000938.7 at α=7.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe07k-il100,000540.7 at α=7.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe07k-il200,000969.7 at α=6.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe07k-il200,000570.2 at α=6°Mach=0 Ncrit=5Xfoil predictionDetails
   goe07k-il500,0009122.3 at α=4.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe07k-il500,0005116.5 at α=3.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe07k-il1,000,0009159.9 at α=2.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe07k-il1,000,0005142.8 at α=2.75°Mach=0 Ncrit=5Xfoil predictionDetails
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