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GOE 423 AIRFOIL (goe423-il)

GOE 423 AIRFOIL - Gottingen 423 airfoil


Airfoil goe423-il
Details Dat file Parser  
(goe423-il) GOE 423 AIRFOIL
Gottingen 423 airfoil
Max thickness 16.9% at 39.7% chord.
Max camber 5.1% at 39.7% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 423 AIRFOIL
       17.       17.

 0.0000000 0.0000000
 0.0118000 0.0286900
 0.0240600 0.0388800
 0.0486600 0.0552800
 0.0733100 0.0695800
 0.0980300 0.0810800
 0.1475600 0.1002900
 0.1972300 0.1140900
 0.2968200 0.1307100
 0.3967100 0.1353400
 0.4969400 0.1258800
 0.5973600 0.1085200
 0.6978500 0.0885600
 0.7984700 0.0631000
 0.8991800 0.0336500
 0.9495900 0.0170700
 1.0000000 0.0008000

 0.0000000 0.0000000
 0.0130000 -.0204800
 0.0256900 -.0282800
 0.0508300 -.0342600
 0.0759000 -.0369600
 0.1009400 -.0385500
 0.1509500 -.0389300
 0.2009400 -.0388200
 0.3008800 -.0363900
 0.4008300 -.0339600
 0.5007300 -.0299300
 0.6006000 -.0247100
 0.7004901 -.0200800
 0.8003600 -.0149500
 0.9002100 -.0087200
 0.9501300 -.0053100
 1.0000000 -.0008000
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Lednicer format dat file
Selig format dat file

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Polars for GOE 423 AIRFOIL (goe423-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe423-il50,00094.7 at α=10°Mach=0 Ncrit=9Xfoil predictionDetails
   goe423-il50,000514.4 at α=0.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe423-il100,000922.8 at α=0.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe423-il100,000540.2 at α=8°Mach=0 Ncrit=5Xfoil predictionDetails
   goe423-il200,000969.3 at α=9.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe423-il200,000570.5 at α=7.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe423-il500,0009105.9 at α=7.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe423-il500,0005101.1 at α=6.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe423-il1,000,0009133.4 at α=6.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe423-il1,000,0005124.5 at α=5.25°Mach=0 Ncrit=5Xfoil predictionDetails
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