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GOE 16K AIRFOIL (goe16k-il)

GOE 16K AIRFOIL - Gottingen 16K airfoil


Airfoil goe16k-il
Details Dat file Parser  
(goe16k-il) GOE 16K AIRFOIL
Gottingen 16K airfoil
Max thickness 18.2% at 50% chord.
Max camber 4.1% at 50% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 16K AIRFOIL
       15.       15.

 0.0000000 0.0000000
 0.0250000 0.0359200
 0.0500000 0.0515500
 0.1000000 0.0727000
 0.1500000 0.0879500
 0.2000000 0.1001000
 0.3000000 0.1174000
 0.4000000 0.1268000
 0.5000000 0.1316000
 0.6000000 0.1286000
 0.7000000 0.1173000
 0.8000000 0.0925000
 0.9000000 0.0574000
 0.9500000 0.0341500
 1.0000000 0.0000000

 0.0000000 0.0000000
 0.0250000 -.0266800
 0.0500000 -.0352500
 0.1000000 -.0452000
 0.1500000 -.0507500
 0.2000000 -.0533000
 0.3000000 -.0541000
 0.4000000 -.0520000
 0.5000000 -.0499000
 0.6000000 -.0478000
 0.7000000 -.0448000
 0.8000000 -.0396000
 0.9000000 -.0295000
 0.9500000 -.0203500
 1.0000000 0.0000000
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Lednicer format dat file
Selig format dat file

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Polars for GOE 16K AIRFOIL (goe16k-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe16k-il50,000921.5 at α=11.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe16k-il50,000516.6 at α=11.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe16k-il100,000926.4 at α=10.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe16k-il100,000523.7 at α=10°Mach=0 Ncrit=5Xfoil predictionDetails
   goe16k-il200,000935.9 at α=9.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe16k-il500,000969.2 at α=4.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe16k-il500,000550.6 at α=3°Mach=0 Ncrit=5Xfoil predictionDetails
   goe16k-il1,000,000980.2 at α=3.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe16k-il1,000,000570.9 at α=2.75°Mach=0 Ncrit=5Xfoil predictionDetails
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