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GOE 776 AIRFOIL (goe776-il)

GOE 776 AIRFOIL - Gottingen 776 airfoil


Airfoil goe776-il
Details Dat file Parser  
(goe776-il) GOE 776 AIRFOIL
Gottingen 776 airfoil
Max thickness 25% at 30% chord.
Max camber 0% at 60% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 776 AIRFOIL
       17.       17.

 0.0000000 0.0000000
 0.0125000 0.0395300
 0.0250000 0.0545700
 0.0500000 0.0741300
 0.0750000 0.0876900
 0.1000000 0.0977600
 0.1500000 0.1116900
 0.2000000 0.1200200
 0.3000000 0.1257800
 0.4000000 0.1218400
 0.5000000 0.1116000
 0.6000000 0.0965600
 0.7000000 0.0781200
 0.8000000 0.0567800
 0.9000000 0.0325400
 0.9500000 0.0192700
 1.0000000 0.0052000

 0.0000000 0.0000000
 0.0125000 -.0394700
 0.0250000 -.0544400
 0.0500000 -.0738700
 0.0750000 -.0873100
 0.1000000 -.0972400
 0.1500000 -.1109100
 0.2000000 -.1189800
 0.3000000 -.1242200
 0.4000000 -.1197600
 0.5000000 -.1090000
 0.6000000 -.0934400
 0.7000000 -.0744800
 0.8000000 -.0526200
 0.9000000 -.0278600
 0.9500000 -.0143300
 1.0000000 0.0000000
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Lednicer format dat file
Selig format dat file

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Polars for GOE 776 AIRFOIL (goe776-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe776-il50,00096.6 at α=3.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe776-il50,000519.2 at α=8.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe776-il100,000933.3 at α=9.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe776-il100,000528.8 at α=10.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe776-il200,000941.2 at α=10.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe776-il200,000535.1 at α=10°Mach=0 Ncrit=5Xfoil predictionDetails
   goe776-il500,000950 at α=8.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe776-il500,000548.5 at α=9°Mach=0 Ncrit=5Xfoil predictionDetails
   goe776-il1,000,000966.3 at α=9.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe776-il1,000,000561.4 at α=9.5°Mach=0 Ncrit=5Xfoil predictionDetails
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