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GOE 256 (JUNKERS E) AIRFOIL (goe256-il)

GOE 256 (JUNKERS E) AIRFOIL - Gottingen 256 (JUNKERS E) airfoil


Airfoil goe256-il
Details Dat file Parser  
(goe256-il) GOE 256 (JUNKERS E) AIRFOIL
Gottingen 256 (JUNKERS E) airfoil
Max thickness 16% at 29.6% chord.
Max camber 4.7% at 39.6% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 256 (JUNKERS E) AIRFOIL
       17.       17.

 0.0000000 0.0000000
 0.0117200 0.0248700
 0.0238300 0.0375400
 0.0482000 0.0575100
 0.0727500 0.0719700
 0.0974100 0.0830400
 0.1468700 0.1000900
 0.1964700 0.1129400
 0.2960900 0.1252500
 0.3960700 0.1258800
 0.4962600 0.1197100
 0.5966500 0.1071500
 0.6973000 0.0864900
 0.7980800 0.0614400
 0.8989900 0.0323900
 0.9494600 0.0173700
 1.0000000 0.0012500

 0.0000000 0.0000000
 0.0131900 -.0220900
 0.0258900 -.0283900
 0.0510400 -.0334000
 0.0760900 -.0348200
 0.1011100 -.0356400
 0.1511300 -.0362800
 0.2011400 -.0365100
 0.3010800 -.0345900
 0.4009800 -.0314700
 0.5008900 -.0283500
 0.6007900 -.0252300
 0.7006900 -.0221000
 0.8005900 -.0189800
 0.9003800 -.0120600
 0.9502000 -.0064100
 1.0000000 -.0012500
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Lednicer format dat file
Selig format dat file

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Polars for GOE 256 (JUNKERS E) AIRFOIL (goe256-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe256-il50,00096.2 at α=3.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe256-il50,000522.5 at α=6.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe256-il100,000945.2 at α=7.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe256-il100,000548.3 at α=6.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe256-il200,000969.6 at α=4.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe256-il200,000564.5 at α=4.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe256-il500,000992.6 at α=2.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe256-il500,000586.2 at α=4.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe256-il1,000,0009112.9 at α=5.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe256-il1,000,0005103.5 at α=6.75°Mach=0 Ncrit=5Xfoil predictionDetails
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