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GOE 424 AIRFOIL (goe424-il)

GOE 424 AIRFOIL - Gottingen 424 airfoil


Airfoil goe424-il
Details Dat file Parser  
(goe424-il) GOE 424 AIRFOIL
Gottingen 424 airfoil
Max thickness 19.9% at 38.5% chord.
Max camber 4.8% at 38.5% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 424 AIRFOIL
       17.       17.

 0.0000200 0.0000000
 0.0097500 0.0279600
 0.0208000 0.0425600
 0.0436100 0.0646200
 0.0668600 0.0823300
 0.0905200 0.0957800
 0.1384700 0.1164300
 0.1870800 0.1304500
 0.2855200 0.1461200
 0.3853900 0.1474300
 0.4866400 0.1347700
 0.5885800 0.1151800
 0.6908000 0.0928200
 0.7934300 0.0663100
 0.8964400 0.0359300
 0.9481800 0.0183600
 1.0000000 0.0008000

 0.0000200 0.0000000
 0.0142600 -.0164900
 0.0272200 -.0221000
 0.0527200 -.0277700
 0.0783600 -.0336300
 0.1038200 -.0383000
 0.1545600 -.0457700
 0.2049200 -.0493700
 0.3053300 -.0535100
 0.4051100 -.0514100
 0.5045900 -.0461400
 0.6038300 -.0385000
 0.7029600 -.0297700
 0.8020300 -.0204400
 0.9010600 -.0106200
 0.9505700 -.0057000
 1.0000000 -.0008000
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Lednicer format dat file
Selig format dat file

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Polars for GOE 424 AIRFOIL (goe424-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe424-il50,00093.6 at α=9.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe424-il50,000516.2 at α=1.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe424-il100,000922.4 at α=2°Mach=0 Ncrit=9Xfoil predictionDetails
   goe424-il100,000537.4 at α=5.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe424-il200,000959 at α=10°Mach=0 Ncrit=9Xfoil predictionDetails
   goe424-il200,000563.3 at α=7.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe424-il500,000996.4 at α=8.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe424-il500,000593.8 at α=7.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe424-il1,000,0009124.2 at α=7.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe424-il1,000,0005117.5 at α=6.75°Mach=0 Ncrit=5Xfoil predictionDetails
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