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GOE 406 AIRFOIL (goe406-il)

GOE 406 AIRFOIL - Gottingen 406 airfoil


Airfoil goe406-il
Details Dat file Parser  
(goe406-il) GOE 406 AIRFOIL
Gottingen 406 airfoil
Max thickness 11.7% at 29.9% chord.
Max camber 5.5% at 39.9% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 406 AIRFOIL
       17.       17.

 0.0000000 0.0000000
 0.0123600 0.0264700
 0.0248000 0.0371300
 0.0497100 0.0541700
 0.0746300 0.0680000
 0.0995700 0.0788400
 0.1494800 0.0960100
 0.1994300 0.1063800
 0.2993900 0.1137200
 0.3993900 0.1132600
 0.4994300 0.1064000
 0.5995000 0.0926400
 0.6996000 0.0738800
 0.7997100 0.0530200
 0.8998300 0.0307600
 0.9498900 0.0162100
 1.0000000 0.0000000

 0.0000000 0.0000000
 0.0125800 -.0147300
 0.0250900 -.0157600
 0.0500800 -.0151300
 0.0750700 -.0129900
 0.1000600 -.0111600
 0.1500500 -.0078700
 0.2000300 -.0058200
 0.3000200 -.0031800
 0.4000100 -.0026400
 0.5000100 -.0026000
 0.6000200 -.0035400
 0.7000300 -.0047200
 0.8000300 -.0062800
 0.9000500 -.0089400
 0.9500600 -.0082700
 1.0000000 0.0000000
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Lednicer format dat file
Selig format dat file

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Polars for GOE 406 AIRFOIL (goe406-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe406-il50,000917.8 at α=4.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe406-il50,000534.1 at α=6°Mach=0 Ncrit=5Xfoil predictionDetails
   goe406-il100,000954.1 at α=5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe406-il100,000553.1 at α=3.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe406-il200,000975.6 at α=3°Mach=0 Ncrit=9Xfoil predictionDetails
   goe406-il200,000568.1 at α=3.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe406-il500,000994.8 at α=3°Mach=0 Ncrit=9Xfoil predictionDetails
   goe406-il500,000589.3 at α=5.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe406-il1,000,0009114.2 at α=6°Mach=0 Ncrit=9Xfoil predictionDetails
   goe406-il1,000,0005112 at α=6.5°Mach=0 Ncrit=5Xfoil predictionDetails
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