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GOE 434 AIRFOIL (goe434-il)

GOE 434 AIRFOIL - Gottingen 434 airfoil


Airfoil goe434-il
Details Dat file Parser  
(goe434-il) GOE 434 AIRFOIL
Gottingen 434 airfoil
Max thickness 22.8% at 28.4% chord.
Max camber 5.2% at 48.5% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 434 AIRFOIL
       17.       17.

 0.0000300 0.0000000
 0.0083500 0.0412400
 0.0191100 0.0584300
 0.0417000 0.0822200
 0.0651000 0.0979900
 0.0887600 0.1111900
 0.1369100 0.1294600
 0.1857500 0.1409100
 0.2843600 0.1546000
 0.3842500 0.1556200
 0.4852800 0.1454500
 0.5874400 0.1241000
 0.6900900 0.0979000
 0.7930600 0.0685300
 0.8963400 0.0362000
 0.9481600 0.0181500
 1.0000000 0.0008000

 0.0000300 0.0000000
 0.0162200 -.0364600
 0.0298900 -.0479700
 0.0561400 -.0604100
 0.0818400 -.0673100
 0.1074100 -.0729200
 0.1579200 -.0780000
 0.2080700 -.0794200
 0.3072100 -.0709800
 0.4056500 -.0556100
 0.5039300 -.0386500
 0.6022100 -.0217000
 0.7007599 -.0074100
 0.7996900 0.0031100
 0.8994800 0.0051200
 0.9497800 0.0022100
 1.0000000 -.0008000
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Lednicer format dat file
Selig format dat file

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Polars for GOE 434 AIRFOIL (goe434-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe434-il50,00093.7 at α=9.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe434-il50,000511.1 at α=8.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe434-il100,000936 at α=9.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe434-il100,000536.7 at α=4.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe434-il200,000965.3 at α=6.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe434-il200,000562.8 at α=5.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe434-il500,000994.5 at α=5.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe434-il500,000583.2 at α=4.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe434-il1,000,0009110.6 at α=4.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe434-il1,000,000593.9 at α=3.25°Mach=0 Ncrit=5Xfoil predictionDetails
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