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GOE 332 (PFALZ 61) AIRFOIL (goe332-il)

GOE 332 (PFALZ 61) AIRFOIL - Gottingen 332 (Pfalz 61) airfoil


Airfoil goe332-il
Details Dat file Parser  
(goe332-il) GOE 332 (PFALZ 61) AIRFOIL
Gottingen 332 (Pfalz 61) airfoil
Max thickness 11.8% at 29.8% chord.
Max camber 6.4% at 39.8% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 332 (PFALZ 61) AIRFOIL
       17.       17.

 0.0000000 0.0000000
 0.0121300 0.0241900
 0.0244400 0.0358800
 0.0491500 0.0547600
 0.0739400 0.0681500
 0.0987700 0.0795300
 0.1485100 0.0963000
 0.1983200 0.1080700
 0.2981400 0.1198200
 0.3981200 0.1211700
 0.4982300 0.1142200
 0.5984500 0.0997800
 0.6987500 0.0808300
 0.7991000 0.0581900
 0.8994700 0.0339400
 0.9496900 0.0197200
 1.0000000 0.0015000

 0.0000000 0.0000000
 0.0127300 -.0140000
 0.0252500 -.0161100
 0.0502500 -.0162200
 0.0752400 -.0153300
 0.1002000 -.0130500
 0.1501200 -.0074700
 0.2000500 -.0034000
 0.2999700 0.0020500
 0.3999000 0.0062000
 0.4998800 0.0074500
 0.5998800 0.0075000
 0.6998800 0.0074500
 0.7999200 0.0054000
 0.8999700 0.0019500
 0.9499900 0.0007200
 1.0000000 -.0015000
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Lednicer format dat file
Selig format dat file

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Polars for GOE 332 (PFALZ 61) AIRFOIL (goe332-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe332-il50,000910.7 at α=3.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe332-il50,000529.5 at α=5.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe332-il100,000952.2 at α=9.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe332-il100,000559.4 at α=6.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe332-il200,000983.6 at α=6.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe332-il200,000584.3 at α=5.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe332-il500,0009120.7 at α=5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe332-il500,0005113.2 at α=3.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe332-il1,000,0009147.3 at α=4°Mach=0 Ncrit=9Xfoil predictionDetails
   goe332-il1,000,0005131.2 at α=3.75°Mach=0 Ncrit=5Xfoil predictionDetails
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