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GOE 15 AIRFOIL (goe15-il)

GOE 15 AIRFOIL - Gottingen 15 airfoil


Airfoil goe15-il
Details Dat file Parser  
(goe15-il) GOE 15 AIRFOIL
Gottingen 15 airfoil
Max thickness 9% at 29.8% chord.
Max camber 7.8% at 29.8% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 15 AIRFOIL
       17.       17.

 0.0000000 0.0000000
 0.0120800 0.0273800
 0.0243600 0.0417700
 0.0490500 0.0621500
 0.0738200 0.0768300
 0.0986500 0.0882100
 0.1484100 0.1039700
 0.1982500 0.1144300
 0.2981200 0.1225600
 0.3982000 0.1182900
 0.4983300 0.1090200
 0.5985600 0.0938600
 0.6988800 0.0733900
 0.7992100 0.0519300
 0.8995900 0.0269600
 0.9497800 0.0142300
 1.0000000 0.0000000

 0.0000000 0.0000000
 0.0127100 -.0136100
 0.0252300 -.0149100
 0.0500800 -.0050300
 0.0749300 0.0048500
 0.0998100 0.0127300
 0.1496500 0.0229900
 0.1995800 0.0277500
 0.2995000 0.0325800
 0.3995300 0.0308100
 0.4995800 0.0273400
 0.5996900 0.0205800
 0.6998100 0.0121100
 0.7999000 0.0062400
 0.8999800 0.0014700
 0.9499900 0.0005300
 1.0000000 0.0000000
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Lednicer format dat file
Selig format dat file

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Polars for GOE 15 AIRFOIL (goe15-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe15-il50,00098.7 at α=2.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe15-il50,000531.5 at α=6.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe15-il100,000946.6 at α=7.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe15-il100,000553.4 at α=8.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe15-il200,000970.7 at α=8.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe15-il200,000572.4 at α=9°Mach=0 Ncrit=5Xfoil predictionDetails
   goe15-il500,0009126.4 at α=2.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe15-il500,000594.3 at α=8°Mach=0 Ncrit=5Xfoil predictionDetails
   goe15-il1,000,0009128.7 at α=9.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe15-il1,000,0005115.3 at α=7.5°Mach=0 Ncrit=5Xfoil predictionDetails
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