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GOE 15K AIRFOIL (goe15k-il)

GOE 15K AIRFOIL - Gottingen 15K airfoil


Airfoil goe15k-il
Details Dat file Parser  
(goe15k-il) GOE 15K AIRFOIL
Gottingen 15K airfoil
Max thickness 15% at 50% chord.
Max camber 3.4% at 50% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 15K AIRFOIL
       15.       15.

 0.0000000 0.0000000
 0.0250000 0.0296400
 0.0500000 0.0424700
 0.1000000 0.0600500
 0.1500000 0.0726200
 0.2000000 0.0826000
 0.3000000 0.0969500
 0.4000000 0.1047000
 0.5000000 0.1087500
 0.6000000 0.1063000
 0.7000000 0.0969500
 0.8000000 0.0765000
 0.9000000 0.0474500
 0.9500000 0.0282200
 1.0000000 0.0000000

 0.0000000 0.0000000
 0.0250000 -.0221600
 0.0500000 -.0291200
 0.1000000 -.0374500
 0.1500000 -.0419800
 0.2000000 -.0441000
 0.3000000 -.0447500
 0.4000000 -.0430000
 0.5000000 -.0412500
 0.6000000 -.0395000
 0.7000000 -.0370500
 0.8000000 -.0327000
 0.9000000 -.0243500
 0.9500000 -.0167800
 1.0000000 0.0000000
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Lednicer format dat file
Selig format dat file

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Polars for GOE 15K AIRFOIL (goe15k-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe15k-il50,000923.7 at α=10.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe15k-il50,000520.8 at α=9.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe15k-il100,000932.5 at α=8.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe15k-il100,000530.7 at α=7.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe15k-il200,000949.4 at α=7.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe15k-il200,000549.1 at α=6°Mach=0 Ncrit=5Xfoil predictionDetails
   goe15k-il500,000992.8 at α=3.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe15k-il500,000567.7 at α=4°Mach=0 Ncrit=5Xfoil predictionDetails
   goe15k-il1,000,000992.4 at α=3.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe15k-il1,000,000583.1 at α=1.75°Mach=0 Ncrit=5Xfoil predictionDetails
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