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GOE 460 AIRFOIL (goe460-il)

GOE 460 AIRFOIL - Gottingen 460 airfoil


Airfoil goe460-il
Details Dat file Parser  
(goe460-il) GOE 460 AIRFOIL
Gottingen 460 airfoil
Max thickness 20.5% at 30% chord.
Max camber 0% at 0% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 460 AIRFOIL
       17.       17.

 0.0000000 0.0000000
 0.0125000 0.0275000
 0.0250000 0.0395000
 0.0500000 0.0555000
 0.0750000 0.0675000
 0.1000000 0.0760000
 0.1500000 0.0890000
 0.2000000 0.0960000
 0.3000000 0.1025000
 0.4000000 0.1005000
 0.5000000 0.0925000
 0.6000000 0.0800000
 0.7000000 0.0645000
 0.8000000 0.0450000
 0.9000000 0.0235000
 0.9500000 0.0115000
 1.0000000 0.0000000

 0.0000000 0.0000000
 0.0125000 -.0275000
 0.0250000 -.0395000
 0.0500000 -.0555000
 0.0750000 -.0675000
 0.1000000 -.0760000
 0.1500000 -.0890000
 0.2000000 -.0960000
 0.3000000 -.1025000
 0.4000000 -.1005000
 0.5000000 -.0925000
 0.6000000 -.0800000
 0.7000000 -.0645000
 0.8000000 -.0450000
 0.9000000 -.0235000
 0.9500000 -.0115000
 1.0000000 0.0000000
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Lednicer format dat file
Selig format dat file

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Polars for GOE 460 AIRFOIL (goe460-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe460-il50,000920.8 at α=4.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe460-il50,000525.8 at α=7.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe460-il100,000939.8 at α=7°Mach=0 Ncrit=9Xfoil predictionDetails
   goe460-il100,000534.1 at α=9.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe460-il200,000946.4 at α=9.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe460-il200,000539.4 at α=10.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe460-il500,000954.4 at α=10.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe460-il500,000550.6 at α=9.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe460-il1,000,000966.6 at α=10.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe460-il1,000,000557.5 at α=10.5°Mach=0 Ncrit=5Xfoil predictionDetails
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