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GOE 780 AIRFOIL (goe780-il)

GOE 780 AIRFOIL - Gottingen 780 airfoil


Airfoil goe780-il
Details Dat file Parser  
(goe780-il) GOE 780 AIRFOIL
Gottingen 780 airfoil
Max thickness 12% at 50% chord.
Max camber 1% at 40% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 780 AIRFOIL
       17.       17.

 0.0000000 0.0000000
 0.0125000 0.0080000
 0.0250000 0.0130000
 0.0500000 0.0200000
 0.0750000 0.0250000
 0.1000000 0.0300000
 0.1500000 0.0400000
 0.2000000 0.0480000
 0.3000000 0.0600000
 0.4000000 0.0680000
 0.5000000 0.0700000
 0.6000000 0.0650000
 0.7000000 0.0520000
 0.8000000 0.0340000
 0.9000000 0.0170000
 0.9500000 0.0080000
 1.0000000 0.0000000

 0.0000000 0.0000000
 0.0125000 -.0090000
 0.0250000 -.0130000
 0.0500000 -.0180000
 0.0750000 -.0230000
 0.1000000 -.0260000
 0.1500000 -.0320000
 0.2000000 -.0370000
 0.3000000 -.0440000
 0.4000000 -.0480000
 0.5000000 -.0500000
 0.6000000 -.0490000
 0.7000000 -.0440000
 0.8000000 -.0360000
 0.9000000 -.0210000
 0.9500000 -.0120000
 1.0000000 0.0000000
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Lednicer format dat file
Selig format dat file

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Polars for GOE 780 AIRFOIL (goe780-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe780-il50,000912.4 at α=7.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe780-il50,000519.5 at α=3.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe780-il100,000929.3 at α=2.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe780-il100,000531.8 at α=2.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe780-il200,000944.3 at α=1.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe780-il200,000534.3 at α=2.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe780-il500,000942.8 at α=2.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe780-il500,000542.1 at α=2.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe780-il1,000,000950.9 at α=2.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe780-il1,000,000544 at α=2.25°Mach=0 Ncrit=5Xfoil predictionDetails
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