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GOE 331 (PFALZ 60) AIRFOIL (goe331-il)

GOE 331 (PFALZ 60) AIRFOIL - Gottingen 331 (Pfalz 60) airfoil


Airfoil goe331-il
Details Dat file Parser  
(goe331-il) GOE 331 (PFALZ 60) AIRFOIL
Gottingen 331 (Pfalz 60) airfoil
Max thickness 10.6% at 29.9% chord.
Max camber 6.9% at 39.9% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 331 (PFALZ 60) AIRFOIL
       17.       17.

 0.0000000 0.0000000
 0.0122100 0.0301200
 0.0245900 0.0424400
 0.0494100 0.0612800
 0.0742600 0.0758200
 0.0991600 0.0869600
 0.1489900 0.1037500
 0.1989000 0.1137300
 0.2988200 0.1212000
 0.3988200 0.1215700
 0.4988900 0.1145400
 0.5990200 0.1012100
 0.6992100 0.0815800
 0.7994400 0.0579500
 0.8996900 0.0322300
 0.9498400 0.0168100
 1.0000000 0.0013000

 0.0000000 0.0000000
 0.0126100 -.0108800
 0.0250800 -.0086600
 0.0500400 -.0041100
 0.0750000 -.0001700
 0.0999700 0.0029700
 0.1499200 0.0080500
 0.1998900 0.0114400
 0.2998600 0.0148100
 0.3998500 0.0157800
 0.4998500 0.0151500
 0.5998700 0.0134200
 0.6999000 0.0101900
 0.7999300 0.0068600
 0.8999700 0.0030300
 0.9499900 0.0009100
 1.0000000 -.0013000
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Lednicer format dat file
Selig format dat file

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Polars for GOE 331 (PFALZ 60) AIRFOIL (goe331-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe331-il50,000922.4 at α=5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe331-il50,000537.1 at α=5.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe331-il100,000958.8 at α=4.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe331-il100,000557.3 at α=4.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe331-il200,000979.3 at α=4.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe331-il200,000571.7 at α=5.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe331-il500,000997.1 at α=5.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe331-il500,000594.1 at α=6°Mach=0 Ncrit=5Xfoil predictionDetails
   goe331-il1,000,0009119.9 at α=6°Mach=0 Ncrit=9Xfoil predictionDetails
   goe331-il1,000,0005117.6 at α=6.5°Mach=0 Ncrit=5Xfoil predictionDetails
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