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GOE 375 AIRFOIL (goe375-il)

GOE 375 AIRFOIL - Gottingen 375 airfoil


Airfoil goe375-il
Details Dat file Parser  
(goe375-il) GOE 375 AIRFOIL
Gottingen 375 airfoil
Max thickness 6.5% at 20% chord.
Max camber 4.5% at 30% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 375 AIRFOIL
       17.       17.

 0.0000000 0.0000000
 0.0124100 0.0210600
 0.0248600 0.0321100
 0.0497900 0.0472200
 0.0747400 0.0573400
 0.0997100 0.0639500
 0.1496800 0.0721700
 0.1996600 0.0759000
 0.2996500 0.0773500
 0.3996700 0.0733000
 0.4997000 0.0662500
 0.5997400 0.0572000
 0.6998000 0.0451500
 0.7998600 0.0306000
 0.8999299 0.0165500
 0.9499600 0.0087700
 1.0000000 0.0000000

 0.0000000 0.0000000
 0.0125200 -.0039400
 0.0250000 -.0003900
 0.0499800 0.0042200
 0.0749700 0.0058400
 0.0999700 0.0074500
 0.1499600 0.0091700
 0.1999500 0.0109000
 0.2999400 0.0123500
 0.3999400 0.0123000
 0.4999500 0.0117500
 0.5999500 0.0102000
 0.6999700 0.0076500
 0.7999800 0.0041000
 0.8999900 0.0020500
 0.9500000 0.0002700
 1.0000000 0.0000000
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Lednicer format dat file
Selig format dat file

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Polars for GOE 375 AIRFOIL (goe375-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe375-il50,000932.6 at α=3.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe375-il50,000537.6 at α=5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe375-il100,000946.6 at α=4.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe375-il100,000552.1 at α=5.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe375-il200,000962.9 at α=4.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe375-il200,000567.5 at α=6.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe375-il500,000988.9 at α=7.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe375-il500,000591.5 at α=6.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe375-il1,000,0009109.9 at α=6.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe375-il1,000,0005108.4 at α=6.75°Mach=0 Ncrit=5Xfoil predictionDetails
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