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GOE 393 AIRFOIL (goe393-il)

GOE 393 AIRFOIL - Gottingen 393 airfoil


Airfoil goe393-il
Details Dat file Parser  
(goe393-il) GOE 393 AIRFOIL
Gottingen 393 airfoil
Max thickness 6.1% at 19.9% chord.
Max camber 4.2% at 29.9% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 393 AIRFOIL
       17.       17.

 0.0000000 0.0000000
 0.0122700 0.0171600
 0.0246600 0.0251300
 0.0495100 0.0366600
 0.0744100 0.0444900
 0.0993200 0.0508300
 0.1491900 0.0604900
 0.1991000 0.0673600
 0.2990500 0.0709900
 0.3991100 0.0670300
 0.4992300 0.0576600
 0.5994100 0.0458100
 0.6995500 0.0338400
 0.7996900 0.0229800
 0.8998400 0.0120100
 0.9499199 0.0059800
 1.0000000 0.0006500

 0.0000000 0.0000000
 0.0126500 -.0110300
 0.0251700 -.0128600
 0.0501700 -.0129300
 0.0751300 -.0100000
 0.1000800 -.0056600
 0.1499800 0.0015000
 0.1999100 0.0066700
 0.2998200 0.0132000
 0.3998000 0.0148400
 0.4998300 0.0126700
 0.5999000 0.0090600
 0.6999300 0.0053400
 0.7999700 0.0021800
 0.9000000 0.0000100
 0.9500100 -.0008200
 1.0000000 -.0006500
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Lednicer format dat file
Selig format dat file

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Polars for GOE 393 AIRFOIL (goe393-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe393-il50,000934.7 at α=8.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe393-il50,000539.4 at α=7.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe393-il100,000955.9 at α=7.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe393-il100,000557.3 at α=7°Mach=0 Ncrit=5Xfoil predictionDetails
   goe393-il200,000975.4 at α=7°Mach=0 Ncrit=9Xfoil predictionDetails
   goe393-il200,000574.8 at α=6.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe393-il500,0009101.3 at α=6°Mach=0 Ncrit=9Xfoil predictionDetails
   goe393-il500,000597.5 at α=5.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe393-il1,000,0009120.4 at α=5.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe393-il1,000,0005113.4 at α=5°Mach=0 Ncrit=5Xfoil predictionDetails
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