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GOE 12K AIRFOIL (goe12k-il)

GOE 12K AIRFOIL - Gottingen 12K airfoil


Airfoil goe12k-il
Details Dat file Parser  
(goe12k-il) GOE 12K AIRFOIL
Gottingen 12K airfoil
Max thickness 11.1% at 50% chord.
Max camber 4.1% at 60% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 12K AIRFOIL
       15.       15.

 0.0000000 0.0000000
 0.0250000 0.0287600
 0.0500000 0.0402200
 0.1000000 0.0554400
 0.1500000 0.0667600
 0.2000000 0.0755800
 0.3000000 0.0876200
 0.4000000 0.0930600
 0.5000000 0.0960000
 0.6000000 0.0944400
 0.7000000 0.0846800
 0.8000000 0.0670200
 0.9000000 0.0395600
 0.9500000 0.0239800
 1.0000000 0.0000000

 0.0000000 0.0000000
 0.0250000 -.0192400
 0.0500000 -.0226800
 0.1000000 -.0239600
 0.1500000 -.0228400
 0.2000000 -.0217200
 0.3000000 -.0194800
 0.4000000 -.0172400
 0.5000000 -.0150000
 0.6000000 -.0127600
 0.7000000 -.0105200
 0.8000000 -.0082800
 0.9000000 -.0060400
 0.9500000 -.0049200
 1.0000000 0.0000000
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Lednicer format dat file
Selig format dat file

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Polars for GOE 12K AIRFOIL (goe12k-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe12k-il50,000928.9 at α=8°Mach=0 Ncrit=9Xfoil predictionDetails
   goe12k-il50,000527.3 at α=8°Mach=0 Ncrit=5Xfoil predictionDetails
   goe12k-il100,000942.3 at α=7.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe12k-il100,000540.7 at α=6.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe12k-il200,000966.2 at α=6°Mach=0 Ncrit=9Xfoil predictionDetails
   goe12k-il200,000565.1 at α=4.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe12k-il500,0009114 at α=4°Mach=0 Ncrit=9Xfoil predictionDetails
   goe12k-il500,0005104.2 at α=2.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe12k-il1,000,0009146.7 at α=2.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe12k-il1,000,000584.6 at α=2.25°Mach=0 Ncrit=5Xfoil predictionDetails
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