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GOE 483 AIRFOIL (goe483-il)

GOE 483 AIRFOIL - Gottingen 483 airfoil


Airfoil goe483-il
Details Dat file Parser  
(goe483-il) GOE 483 AIRFOIL
Gottingen 483 airfoil
Max thickness 5.5% at 15% chord.
Max camber 5.8% at 40% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 483 AIRFOIL
       17.       17.

 0.0000000 0.0000000
 0.0125000 0.0145600
 0.0250000 0.0231300
 0.0500000 0.0367500
 0.0750000 0.0468800
 0.1000000 0.0550000
 0.1500000 0.0667500
 0.2000000 0.0745000
 0.3000000 0.0815000
 0.4000000 0.0810000
 0.5000000 0.0750000
 0.6000000 0.0660000
 0.7000000 0.0525000
 0.8000000 0.0360000
 0.9000000 0.0185000
 0.9500000 0.0092500
 1.0000000 0.0000000

 0.0000000 0.0000000
 0.0125000 -.0044400
 0.0250000 -.0048800
 0.0500000 -.0032500
 0.0750000 -.0001300
 0.1000000 0.0040000
 0.1500000 0.0122500
 0.2000000 0.0210000
 0.3000000 0.0330000
 0.4000000 0.0355000
 0.5000000 0.0330000
 0.6000000 0.0270000
 0.7000000 0.0205000
 0.8000000 0.0140000
 0.9000000 0.0075000
 0.9500000 0.0037500
 1.0000000 0.0000000
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Lednicer format dat file
Selig format dat file

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Polars for GOE 483 AIRFOIL (goe483-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe483-il50,000942.8 at α=7.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe483-il50,000544.6 at α=6.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe483-il100,000962.7 at α=6.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe483-il100,000565.1 at α=5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe483-il200,000983.8 at α=5.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe483-il200,000585.6 at α=5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe483-il500,0009114.3 at α=4.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe483-il500,0005112.3 at α=4.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe483-il1,000,0009137.4 at α=3.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe483-il1,000,0005121.9 at α=4.75°Mach=0 Ncrit=5Xfoil predictionDetails
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