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GOE 435 AIRFOIL (goe435-il)

GOE 435 AIRFOIL - Gottingen 435 airfoil


Airfoil goe435-il
Details Dat file Parser  
(goe435-il) GOE 435 AIRFOIL
Gottingen 435 airfoil
Max thickness 26.1% at 27.8% chord.
Max camber 4.7% at 48% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 435 AIRFOIL
       17.       17.

 0.0000700 0.0000000
 0.0075500 0.0381800
 0.0177600 0.0555200
 0.0393100 0.0817600
 0.0618900 0.1001300
 0.0847400 0.1164400
 0.1316800 0.1396200
 0.1797900 0.1539500
 0.2780800 0.1668900
 0.3780900 0.1667600
 0.4798200 0.1535500
 0.5825100 0.1330700
 0.6863800 0.1036500
 0.7906600 0.0710800
 0.8952100 0.0364500
 0.9475901 0.0183500
 1.0000000 0.0013500

 0.0000700 0.0000000
 0.0177300 -.0391700
 0.0322200 -.0542600
 0.0592000 -.0693100
 0.0856300 -.0809300
 0.1122300 -.0904300
 0.1626500 -.0955900
 0.2128300 -.0969800
 0.3121500 -.0919100
 0.4098200 -.0742500
 0.5072800 -.0550200
 0.6047400 -.0357900
 0.7023400 -.0176400
 0.8003600 -.0026300
 0.8996900 0.0024400
 0.9498700 0.0010500
 1.0000000 -.0013500
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Lednicer format dat file
Selig format dat file

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Polars for GOE 435 AIRFOIL (goe435-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe435-il50,00092.8 at α=11.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe435-il50,00057.9 at α=4.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe435-il100,000925.1 at α=7.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe435-il100,000533.1 at α=4.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe435-il200,000952.4 at α=6.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe435-il200,000550.2 at α=5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe435-il500,000975.8 at α=5.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe435-il500,000569.9 at α=3.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe435-il1,000,000995.2 at α=4.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe435-il1,000,000579.6 at α=4.5°Mach=0 Ncrit=5Xfoil predictionDetails
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