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GOE 14K AIRFOIL (goe14k-il)

GOE 14K AIRFOIL - Gottingen 14K airfoil


Airfoil goe14k-il
Details Dat file Parser  
(goe14k-il) GOE 14K AIRFOIL
Gottingen 14K airfoil
Max thickness 12% at 50% chord.
Max camber 2.7% at 50% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 14K AIRFOIL
       15.       15.

 0.0000000 0.0000000
 0.0250000 0.0237500
 0.0500000 0.0340000
 0.1000000 0.0480000
 0.1500000 0.0581000
 0.2000000 0.0661000
 0.3000000 0.0776000
 0.4000000 0.0838000
 0.5000000 0.0870000
 0.6000000 0.0850000
 0.7000000 0.0776000
 0.8000000 0.0612000
 0.9000000 0.0380000
 0.9500000 0.0226000
 1.0000000 0.0000000

 0.0000000 0.0000000
 0.0250000 -.0176500
 0.0500000 -.0233000
 0.1000000 -.0300000
 0.1500000 -.0336000
 0.2000000 -.0353000
 0.3000000 -.0358000
 0.4000000 -.0344000
 0.5000000 -.0330000
 0.6000000 -.0316000
 0.7000000 -.0296000
 0.8000000 -.0262000
 0.9000000 -.0195000
 0.9500000 -.0134000
 1.0000000 0.0000000
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Lednicer format dat file
Selig format dat file

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Polars for GOE 14K AIRFOIL (goe14k-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe14k-il50,000925.3 at α=7.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe14k-il50,000525.4 at α=7.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe14k-il100,000936 at α=6.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe14k-il100,000538.8 at α=6°Mach=0 Ncrit=5Xfoil predictionDetails
   goe14k-il200,000960.8 at α=5.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe14k-il200,000559.8 at α=4.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe14k-il500,0009100.5 at α=3.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe14k-il500,000576.8 at α=2.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe14k-il1,000,000998.1 at α=3°Mach=0 Ncrit=9Xfoil predictionDetails
   goe14k-il1,000,000586.1 at α=1.5°Mach=0 Ncrit=5Xfoil predictionDetails
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