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GOE 79 (PFALZ 11) AIRFOIL (goe79-il)

GOE 79 (PFALZ 11) AIRFOIL - Gottingen 79 (Pfalz 11) airfoil


Airfoil goe79-il
Details Dat file Parser  
(goe79-il) GOE 79 (PFALZ 11) AIRFOIL
Gottingen 79 (Pfalz 11) airfoil
Max thickness 6.2% at 14.9% chord.
Max camber 6% at 29.9% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 79 (PFALZ 11) AIRFOIL
       17.       17.

 0.0000000 0.0000000
 0.0122800 0.0264000
 0.0246900 0.0366100
 0.0495800 0.0502200
 0.0745000 0.0594300
 0.0994300 0.0680400
 0.1493300 0.0796500
 0.1992800 0.0856700
 0.2992500 0.0893100
 0.3992700 0.0873500
 0.4993300 0.0791900
 0.5994400 0.0672400
 0.6995500 0.0534800
 0.7996800 0.0375200
 0.8998200 0.0209600
 0.9498900 0.0129800
 1.0000000 0.0028000

 0.0000000 0.0000000
 0.0125900 -.0110900
 0.0250700 -.0081900
 0.0500000 -.0001800
 0.0749600 0.0051300
 0.0999100 0.0109400
 0.1498500 0.0180600
 0.1998000 0.0240800
 0.2997400 0.0305200
 0.3997400 0.0313600
 0.4997500 0.0300000
 0.5997900 0.0252400
 0.6998300 0.0198800
 0.7999000 0.0123200
 0.8999600 0.0047600
 0.9499900 0.0006800
 1.0000000 -.0028000
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Lednicer format dat file
Selig format dat file

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Polars for GOE 79 (PFALZ 11) AIRFOIL (goe79-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe79-il50,000959.2 at α=4°Mach=0 Ncrit=9Xfoil predictionDetails
   goe79-il50,000542.7 at α=5.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe79-il100,000957.6 at α=4.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe79-il100,000559.4 at α=5.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe79-il200,000975.7 at α=5.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe79-il200,000575.6 at α=6.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe79-il500,0009102.2 at α=6.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe79-il500,000597.4 at α=6.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe79-il1,000,0009120.1 at α=6.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe79-il1,000,0005103.5 at α=7°Mach=0 Ncrit=5Xfoil predictionDetails
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