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GOE 264 AIRFOIL (goe264-il)

GOE 264 AIRFOIL - Gottingen 264 airfoil


Airfoil goe264-il
Details Dat file Parser  
(goe264-il) GOE 264 AIRFOIL
Gottingen 264 airfoil
Max thickness 6.4% at 20.2% chord.
Max camber 5.7% at 28.9% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 264 AIRFOIL
       17.       17.

 0.0000000 0.0000000
 0.0122100 0.0165200
 0.0276500 0.0267600
 0.0497600 0.0382200
 0.0746800 0.0492800
 0.0996300 0.0577400
 0.1495400 0.0723600
 0.2017300 0.0818400
 0.2892600 0.0880200
 0.3994500 0.0863600
 0.4994900 0.0795000
 0.5995600 0.0689400
 0.6996400 0.0567800
 0.7997400 0.0409200
 0.8998500 0.0228600
 0.9499199 0.0126800
 1.0000000 0.0032000

 0.0000000 0.0000000
 0.0125600 -.0092200
 0.0261500 -.0109600
 0.0500500 -.0079800
 0.0750300 -.0040200
 0.1000000 0.0006400
 0.1499400 0.0100600
 0.1998900 0.0172800
 0.2998300 0.0259200
 0.3998300 0.0265600
 0.4998500 0.0235000
 0.5998700 0.0198400
 0.6999100 0.0145800
 0.7999400 0.0094200
 0.8999700 0.0046600
 0.9499900 0.0012800
 1.0000000 -.0032000
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Lednicer format dat file
Selig format dat file

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Polars for GOE 264 AIRFOIL (goe264-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe264-il50,000932.2 at α=3.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe264-il50,000541.8 at α=5.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe264-il100,000959.9 at α=7.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe264-il100,000560.8 at α=7°Mach=0 Ncrit=5Xfoil predictionDetails
   goe264-il200,000979.2 at α=7°Mach=0 Ncrit=9Xfoil predictionDetails
   goe264-il200,000579.7 at α=6°Mach=0 Ncrit=5Xfoil predictionDetails
   goe264-il500,0009106.8 at α=5.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe264-il500,0005104.3 at α=5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe264-il1,000,0009126.9 at α=5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe264-il1,000,0005121.8 at α=4.5°Mach=0 Ncrit=5Xfoil predictionDetails
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