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GOE 374 AIRFOIL (goe374-il)

GOE 374 AIRFOIL - Gottingen 374 airfoil


Airfoil goe374-il
Details Dat file Parser  
(goe374-il) GOE 374 AIRFOIL
Gottingen 374 airfoil
Max thickness 6.5% at 30% chord.
Max camber 4.5% at 30% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 374 AIRFOIL
       17.       17.

 0.0000000 0.0000000
 0.0124100 0.0175600
 0.0248600 0.0281200
 0.0497900 0.0422500
 0.0747400 0.0518700
 0.0997100 0.0585000
 0.1496600 0.0682500
 0.1996300 0.0740000
 0.2996100 0.0775000
 0.3996300 0.0740000
 0.4996600 0.0675000
 0.5997100 0.0575000
 0.6997700 0.0465000
 0.7998400 0.0325000
 0.8999200 0.0170000
 0.9499600 0.0087500
 1.0000000 0.0000000

 0.0000000 0.0000000
 0.0125200 -.0039400
 0.0250100 -.0013700
 0.0499900 0.0017500
 0.0749800 0.0043700
 0.0999700 0.0065000
 0.1499600 0.0087500
 0.1999500 0.0110000
 0.2999400 0.0130000
 0.3999300 0.0135000
 0.4999400 0.0120000
 0.5999500 0.0105000
 0.6999600 0.0080000
 0.7999800 0.0050000
 0.8999900 0.0020000
 0.9500000 0.0002500
 1.0000000 0.0000000
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Lednicer format dat file
Selig format dat file

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Polars for GOE 374 AIRFOIL (goe374-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe374-il50,000932.6 at α=5.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe374-il50,000540.4 at α=6°Mach=0 Ncrit=5Xfoil predictionDetails
   goe374-il100,000951.8 at α=5.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe374-il100,000557.1 at α=6.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe374-il200,000972.4 at α=6.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe374-il200,000574.5 at α=6°Mach=0 Ncrit=5Xfoil predictionDetails
   goe374-il500,000998.7 at α=5.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe374-il500,000597.1 at α=5.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe374-il1,000,0009117.6 at α=4.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe374-il1,000,0005110.4 at α=5°Mach=0 Ncrit=5Xfoil predictionDetails
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