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GOE 123 AIRFOIL (goe123-il)

GOE 123 AIRFOIL - Gottingen 123 airfoil


Airfoil goe123-il
Details Dat file Parser  
(goe123-il) GOE 123 AIRFOIL
Gottingen 123 airfoil
Max thickness 5.4% at 25% chord.
Max camber 5.7% at 40% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 123 AIRFOIL
       17.       17.

 0.0000000 0.0000000
 0.0125000 0.0181300
 0.0250000 0.0262500
 0.0500000 0.0395000
 0.0750000 0.0487500
 0.1000000 0.0570000
 0.1500000 0.0685000
 0.2000000 0.0760000
 0.2500000 0.0805000
 0.3000000 0.0830000
 0.4000000 0.0840000
 0.5000000 0.0800000
 0.6000000 0.0720000
 0.7000000 0.0590000
 0.8000000 0.0420000
 0.9000000 0.0220000
 1.0000000 0.0020000

 0.0000000 0.0000000
 0.0125000 -.0088700
 0.0250000 -.0077500
 0.0500000 -.0035000
 0.0750000 0.0017500
 0.1000000 0.0070000
 0.1500000 0.0175000
 0.2000000 0.0230000
 0.2500000 0.0265000
 0.3000000 0.0290000
 0.4000000 0.0300000
 0.5000000 0.0270000
 0.6000000 0.0220000
 0.7000000 0.0170000
 0.8000000 0.0110000
 0.9000000 0.0060000
 1.0000000 0.0000000
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Lednicer format dat file
Selig format dat file

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Polars for GOE 123 AIRFOIL (goe123-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe123-il50,000940.7 at α=8.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe123-il50,000545.3 at α=6.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe123-il100,000965.8 at α=5.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe123-il100,000566.7 at α=4.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe123-il200,000992 at α=4.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe123-il200,000585 at α=4°Mach=0 Ncrit=5Xfoil predictionDetails
   goe123-il500,0009118.8 at α=3.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe123-il500,0005102.2 at α=5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe123-il1,000,0009129.1 at α=4.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe123-il1,000,0005110.8 at α=5.5°Mach=0 Ncrit=5Xfoil predictionDetails
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