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GOE 54 AIRFOIL (goe54-il)

GOE 54 AIRFOIL - Gottingen 54 airfoil


Airfoil goe54-il
Details Dat file Parser  
(goe54-il) GOE 54 AIRFOIL
Gottingen 54 airfoil
Max thickness 6.5% at 14.9% chord.
Max camber 3.5% at 19.9% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 54 AIRFOIL
       17.       17.

 0.0000000 0.0000000
 0.0123000 0.0246000
 0.0247200 0.0337000
 0.0496200 0.0461100
 0.0745500 0.0551100
 0.0995000 0.0605200
 0.1494500 0.0665300
 0.1994500 0.0669500
 0.2994900 0.0621700
 0.3995700 0.0518000
 0.4996600 0.0416200
 0.5997300 0.0325500
 0.6998000 0.0236700
 0.7998600 0.0168000
 0.8999299 0.0089200
 0.9499500 0.0055400
 1.0000000 0.0017500

 0.0000000 0.0000000
 0.0125800 -.0099000
 0.0250700 -.0083900
 0.0500200 -.0025900
 0.0750100 -.0009800
 0.0999900 0.0006200
 0.1499900 0.0017400
 0.1999800 0.0026500
 0.2999800 0.0029700
 0.3999700 0.0033000
 0.4999700 0.0032200
 0.5999800 0.0029500
 0.6999800 0.0027700
 0.7999800 0.0029000
 0.8999900 0.0009200
 0.9500100 -.0007600
 1.0000000 -.0017500
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Lednicer format dat file
Selig format dat file

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Polars for GOE 54 AIRFOIL (goe54-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe54-il50,000919.8 at α=3.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe54-il50,000529.3 at α=5.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe54-il100,000934.3 at α=5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe54-il100,000544.2 at α=6.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe54-il200,000958.7 at α=10.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe54-il200,000564.2 at α=8.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe54-il500,000987.4 at α=8.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe54-il500,000588.1 at α=7.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe54-il1,000,0009106.7 at α=7.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe54-il1,000,0005105.7 at α=8.5°Mach=0 Ncrit=5Xfoil predictionDetails
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