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GOE 368 AIRFOIL (goe368-il)

GOE 368 AIRFOIL - Gottingen 368 airfoil


Airfoil goe368-il
Details Dat file Parser  
(goe368-il) GOE 368 AIRFOIL
Gottingen 368 airfoil
Max thickness 7.7% at 14.9% chord.
Max camber 3.8% at 29.9% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 368 AIRFOIL
       17.       17.

 0.0000000 0.0000000
 0.0122700 0.0147000
 0.0245800 0.0249200
 0.0493200 0.0398400
 0.0741400 0.0507600
 0.0990000 0.0586800
 0.1488600 0.0670300
 0.1988000 0.0708800
 0.2987800 0.0715800
 0.3988600 0.0667800
 0.4989900 0.0594800
 0.5991700 0.0486900
 0.6993600 0.0378900
 0.7995700 0.0255900
 0.8997600 0.0143000
 0.9498500 0.0075000
 1.0000000 0.0000000

 0.0000000 0.0000000
 0.0125900 -.0065300
 0.0251600 -.0095700
 0.0502300 -.0136500
 0.0752700 -.0157200
 0.1002500 -.0148000
 0.1501700 -.0099500
 0.2000600 -.0036000
 0.2999200 0.0046000
 0.3998700 0.0078000
 0.4998700 0.0075000
 0.5998900 0.0062000
 0.6999300 0.0044000
 0.7999500 0.0031000
 0.8999700 0.0018000
 0.9499800 0.0011500
 1.0000000 0.0000000
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Lednicer format dat file
Selig format dat file

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Polars for GOE 368 AIRFOIL (goe368-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe368-il50,000929.3 at α=3.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe368-il50,000536 at α=7.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe368-il100,000949.8 at α=7.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe368-il100,000550.2 at α=6°Mach=0 Ncrit=5Xfoil predictionDetails
   goe368-il200,000964.3 at α=6.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe368-il200,000563.9 at α=5.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe368-il500,000983.9 at α=5.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe368-il500,000583.6 at α=4.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe368-il1,000,000998.6 at α=5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe368-il1,000,000598.1 at α=4.75°Mach=0 Ncrit=5Xfoil predictionDetails
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