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GOE 369 AIRFOIL (goe369-il)

GOE 369 AIRFOIL - Gottingen 369 airfoil


Airfoil goe369-il
Details Dat file Parser  
(goe369-il) GOE 369 AIRFOIL
Gottingen 369 airfoil
Max thickness 5.9% at 30% chord.
Max camber 5.4% at 40% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 369 AIRFOIL
       17.       17.

 0.0000000 0.0010000
 0.0125000 0.0250000
 0.0250000 0.0350000
 0.0500000 0.0476400
 0.0750000 0.0560000
 0.1000000 0.0625000
 0.1500000 0.0715000
 0.2000000 0.0780000
 0.3000000 0.0835000
 0.4000000 0.0825000
 0.5000000 0.0750000
 0.6000000 0.0625000
 0.7000000 0.0480000
 0.8000000 0.0330000
 0.9000000 0.0180000
 0.9500000 0.0095000
 1.0000000 0.0000000

 0.0000000 0.0010000
 0.0125000 0.0000000
 0.0250000 0.0025000
 0.0500000 0.0060000
 0.0750000 0.0100000
 0.1000000 0.0135000
 0.1500000 0.0176400
 0.2000000 0.0210400
 0.3000000 0.0250000
 0.4000000 0.0265000
 0.5000000 0.0245000
 0.6000000 0.0205000
 0.7000000 0.0150000
 0.8000000 0.0100000
 0.9000000 0.0050000
 0.9500000 0.0020000
 1.0000000 0.0000000
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Lednicer format dat file
Selig format dat file

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Polars for GOE 369 AIRFOIL (goe369-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe369-il50,000937.9 at α=6.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe369-il50,000543.6 at α=6.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe369-il100,000959.2 at α=5.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe369-il100,000563.9 at α=5.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe369-il200,000980.2 at α=5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe369-il200,000583 at α=4.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe369-il500,0009105.9 at α=3.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe369-il500,000594.8 at α=5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe369-il1,000,0009121.8 at α=3°Mach=0 Ncrit=9Xfoil predictionDetails
   goe369-il1,000,0005112.6 at α=4°Mach=0 Ncrit=5Xfoil predictionDetails
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