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GOE 330 (PFALZ 59) AIRFOIL (goe330-il)

GOE 330 (PFALZ 59) AIRFOIL - Gottingen 330 (Pfalz 59) airfoil


Airfoil goe330-il
Details Dat file Parser  
(goe330-il) GOE 330 (PFALZ 59) AIRFOIL
Gottingen 330 (Pfalz 59) airfoil
Max thickness 10.2% at 29.9% chord.
Max camber 5.8% at 39.9% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 330 (PFALZ 59) AIRFOIL
       17.       17.

 0.0000000 0.0000000
 0.0122600 0.0206400
 0.0246400 0.0312800
 0.0494400 0.0490700
 0.0742800 0.0623500
 0.0991500 0.0735400
 0.1489900 0.0882100
 0.1988700 0.0984900
 0.2987600 0.1074400
 0.3987700 0.1065900
 0.4988400 0.1009400
 0.5989800 0.0888900
 0.6991500 0.0735400
 0.7994000 0.0521900
 0.8996700 0.0283500
 0.9498300 0.0149200
 1.0000000 0.0005000

 0.0000000 0.0000000
 0.0126200 -.0106500
 0.0251300 -.0117100
 0.0501200 -.0107200
 0.0750900 -.0076400
 0.1000700 -.0058500
 0.1500300 -.0022700
 0.2000000 0.0003000
 0.2999400 0.0054500
 0.3999000 0.0086000
 0.4998800 0.0107500
 0.5998700 0.0109000
 0.6999000 0.0090500
 0.7999300 0.0062000
 0.9000000 0.0003500
 0.9500000 -.0000700
 1.0000000 -.0005000
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Lednicer format dat file
Selig format dat file

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Polars for GOE 330 (PFALZ 59) AIRFOIL (goe330-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe330-il50,000924.8 at α=12°Mach=0 Ncrit=9Xfoil predictionDetails
   goe330-il50,000538.4 at α=6.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe330-il100,000956.1 at α=5.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe330-il100,000558.6 at α=5.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe330-il200,000978.3 at α=4.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe330-il200,000575.3 at α=6°Mach=0 Ncrit=5Xfoil predictionDetails
   goe330-il500,0009103.9 at α=6.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe330-il500,0005101.6 at α=5.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe330-il1,000,0009128.1 at α=5.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe330-il1,000,0005121.9 at α=5.25°Mach=0 Ncrit=5Xfoil predictionDetails
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