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GOE 623 AIRFOIL (goe623-il)

GOE 623 AIRFOIL - Gottingen 623 airfoil


Airfoil goe623-il
Details Dat file Parser  
(goe623-il) GOE 623 AIRFOIL
Gottingen 623 airfoil
Max thickness 12% at 30% chord.
Max camber 3.8% at 40% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 623 AIRFOIL
       17.       17.

 0.0000000 0.0000000
 0.0125000 0.0224100
 0.0250000 0.0328100
 0.0500000 0.0481300
 0.0750000 0.0604400
 0.1000000 0.0697500
 0.1500000 0.0818800
 0.2000000 0.0895000
 0.3000000 0.0972500
 0.4000000 0.0975000
 0.5000000 0.0902500
 0.6000000 0.0785000
 0.7000000 0.0637500
 0.8000000 0.0450000
 0.9000000 0.0247500
 0.9500000 0.0143800
 1.0000000 0.0030000

 0.0000000 0.0000000
 0.0125000 -.0125900
 0.0250000 -.0166900
 0.0500000 -.0218800
 0.0750000 -.0245600
 0.1000000 -.0262500
 0.1500000 -.0261200
 0.2000000 -.0255000
 0.3000000 -.0227500
 0.4000000 -.0195000
 0.5000000 -.0162500
 0.6000000 -.0130000
 0.7000000 -.0097500
 0.8000000 -.0065000
 0.9000000 -.0032500
 0.9500000 -.0016200
 1.0000000 0.0000000
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Lednicer format dat file
Selig format dat file

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Polars for GOE 623 AIRFOIL (goe623-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe623-il50,000927.4 at α=7.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe623-il50,000536 at α=7°Mach=0 Ncrit=5Xfoil predictionDetails
   goe623-il100,000953.5 at α=6.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe623-il100,000555 at α=6°Mach=0 Ncrit=5Xfoil predictionDetails
   goe623-il200,000975.4 at α=6°Mach=0 Ncrit=9Xfoil predictionDetails
   goe623-il200,000572.3 at α=5.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe623-il500,0009102.6 at α=5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe623-il500,000591.3 at α=3.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe623-il1,000,0009120.6 at α=4°Mach=0 Ncrit=9Xfoil predictionDetails
   goe623-il1,000,0005104.4 at α=6.25°Mach=0 Ncrit=5Xfoil predictionDetails
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