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GOE 679 AIRFOIL (goe679-il)

GOE 679 AIRFOIL - Gottingen 679 airfoil


Airfoil goe679-il
Details Dat file Parser  
(goe679-il) GOE 679 AIRFOIL
Gottingen 679 airfoil
Max thickness 18.3% at 29.1% chord.
Max camber 4.5% at 39.1% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 679 AIRFOIL
       17.       17.

 0.0000100 0.0000000
 0.0103800 0.0312100
 0.0218100 0.0469800
 0.0452400 0.0700800
 0.0691800 0.0857000
 0.0933200 0.0983400
 0.1421400 0.1156600
 0.1914400 0.1260200
 0.2908400 0.1347800
 0.3910200 0.1320900
 0.4916400 0.1229300
 0.5926000 0.1088000
 0.6939400 0.0891900
 0.7955101 0.0660900
 0.8973500 0.0390200
 0.9484000 0.0214900
 1.0000000 0.0000000

 0.0000100 0.0000000
 0.0142800 -.0260300
 0.0272900 -.0336400
 0.0529200 -.0429000
 0.0783100 -.0486700
 0.1035400 -.0519600
 0.1536800 -.0540500
 0.2036200 -.0531500
 0.3032300 -.0473800
 0.4027600 -.0406100
 0.5023000 -.0338400
 0.6018400 -.0270700
 0.7013800 -.0203100
 0.8009200 -.0135400
 0.9004600 -.0067700
 0.9502300 -.0033800
 1.0000000 0.0000000
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Lednicer format dat file
Selig format dat file

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Polars for GOE 679 AIRFOIL (goe679-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe679-il50,00095.4 at α=2.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe679-il50,000525.1 at α=6°Mach=0 Ncrit=5Xfoil predictionDetails
   goe679-il100,000942.7 at α=4.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe679-il100,000541.6 at α=5.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe679-il200,000958.1 at α=5.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe679-il200,000554.2 at α=5.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe679-il500,000976.3 at α=5.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe679-il500,000572.4 at α=5.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe679-il1,000,000995.9 at α=5.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe679-il1,000,000588.8 at α=5.75°Mach=0 Ncrit=5Xfoil predictionDetails
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