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GOE 364 AIRFOIL (goe364-il)

GOE 364 AIRFOIL - Gottingen 364 airfoil


Airfoil goe364-il
Details Dat file Parser  
(goe364-il) GOE 364 AIRFOIL
Gottingen 364 airfoil
Max thickness 10.8% at 30% chord.
Max camber 6.5% at 30% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 364 AIRFOIL
       17.       17.

 0.0000000 0.0000000
 0.0125000 0.0320900
 0.0250000 0.0461700
 0.0500000 0.0653500
 0.0750000 0.0785200
 0.1000000 0.0887000
 0.1500000 0.1030500
 0.2000000 0.1114000
 0.3000000 0.1191000
 0.4000000 0.1158000
 0.5000000 0.1065000
 0.6000000 0.0912000
 0.7000000 0.0719000
 0.8000000 0.0506000
 0.9000000 0.0273000
 0.9500000 0.0136500
 1.0000000 0.0000000

 0.0000000 0.0000000
 0.0125000 -.0079100
 0.0250000 -.0078300
 0.0500000 -.0060500
 0.0750000 -.0039800
 0.1000000 -.0013000
 0.1500000 0.0030500
 0.2000000 0.0064000
 0.3000000 0.0111000
 0.4000000 0.0128000
 0.5000000 0.0135000
 0.6000000 0.0112000
 0.7000000 0.0089000
 0.8000000 0.0066000
 0.9000000 0.0023000
 0.9500000 0.0006500
 1.0000000 0.0000000
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Lednicer format dat file
Selig format dat file

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Polars for GOE 364 AIRFOIL (goe364-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe364-il50,000913.5 at α=4.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe364-il50,000534.8 at α=7.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe364-il100,000952.5 at α=5.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe364-il100,000557 at α=5.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe364-il200,000976.4 at α=5.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe364-il200,000576.6 at α=6°Mach=0 Ncrit=5Xfoil predictionDetails
   goe364-il500,0009107.8 at α=6.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe364-il500,0005104 at α=5.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe364-il1,000,0009133.4 at α=5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe364-il1,000,0005124.5 at α=4.25°Mach=0 Ncrit=5Xfoil predictionDetails
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