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GOE 500 AIRFOIL (goe500-il)

GOE 500 AIRFOIL - Gottingen 500 airfoil


Airfoil goe500-il
Details Dat file Parser  
(goe500-il) GOE 500 AIRFOIL
Gottingen 500 airfoil
Max thickness 10% at 30% chord.
Max camber 6% at 50% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 500 AIRFOIL
       17.       17.

 0.0000000 0.0000000
 0.0125000 0.0212600
 0.0250000 0.0300100
 0.0500000 0.0435200
 0.0750000 0.0545400
 0.1000000 0.0635500
 0.1500000 0.0780700
 0.2000000 0.0886000
 0.3000000 0.1016500
 0.4000000 0.1042000
 0.5000000 0.1003500
 0.6000000 0.0903000
 0.7000000 0.0748500
 0.8000000 0.0544000
 0.9000000 0.0279500
 0.9500000 0.0139800
 1.0000000 0.0000000

 0.0000000 0.0000000
 0.0125000 -.0117400
 0.0250000 -.0154900
 0.0500000 -.0184700
 0.0750000 -.0189600
 0.1000000 -.0174500
 0.1500000 -.0139300
 0.2000000 -.0094000
 0.3000000 0.0016500
 0.4000000 0.0117000
 0.5000000 0.0197500
 0.6000000 0.0248000
 0.7000000 0.0253500
 0.8000000 0.0204000
 0.9000000 0.0124500
 0.9500000 0.0064700
 1.0000000 0.0000000
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Lednicer format dat file
Selig format dat file

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Polars for GOE 500 AIRFOIL (goe500-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe500-il50,000935.6 at α=9.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe500-il50,000536.3 at α=8.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe500-il100,000964.4 at α=7.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe500-il100,000565.6 at α=6.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe500-il200,000992 at α=5.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe500-il200,000591.7 at α=4.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe500-il500,0009131.8 at α=3.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe500-il500,0005120.6 at α=3.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe500-il1,000,0009159.1 at α=3°Mach=0 Ncrit=9Xfoil predictionDetails
   goe500-il1,000,0005120.6 at α=3.5°Mach=0 Ncrit=5Xfoil predictionDetails
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