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GOE 766 AIRFOIL (goe766-il)

GOE 766 AIRFOIL - Gottingen 766 airfoil


Airfoil goe766-il
Details Dat file Parser  
(goe766-il) GOE 766 AIRFOIL
Gottingen 766 airfoil
Max thickness 12% at 25% chord.
Max camber 1.5% at 20% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 766 AIRFOIL
       17.       17.

 0.0000000 0.0000000
 0.0125000 0.0264000
 0.0250000 0.0360000
 0.0500000 0.0481000
 0.1000000 0.0628000
 0.1500000 0.0709000
 0.2000000 0.0740000
 0.2500000 0.0743000
 0.3000000 0.0728000
 0.4000000 0.0654000
 0.5000000 0.0557000
 0.6000000 0.0453000
 0.7000000 0.0346000
 0.8000000 0.0237000
 0.9000000 0.0119000
 0.9500000 0.0061000
 1.0000000 0.0000000

 0.0000000 0.0000000
 0.0125000 -.0170000
 0.0250000 -.0233000
 0.0500000 -.0303000
 0.1000000 -.0383000
 0.1500000 -.0419000
 0.2000000 -.0443000
 0.2500000 -.0458000
 0.3000000 -.0465000
 0.4000000 -.0452000
 0.5000000 -.0421000
 0.6000000 -.0364000
 0.7000000 -.0289000
 0.8000000 -.0205000
 0.9000000 -.0110000
 0.9500000 -.0059000
 1.0000000 0.0000000
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Lednicer format dat file
Selig format dat file

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Polars for GOE 766 AIRFOIL (goe766-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe766-il50,000919.2 at α=2.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe766-il50,000527.4 at α=8°Mach=0 Ncrit=5Xfoil predictionDetails
   goe766-il100,000937.6 at α=8.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe766-il100,000542 at α=8°Mach=0 Ncrit=5Xfoil predictionDetails
   goe766-il200,000955.9 at α=8.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe766-il200,000557.2 at α=7.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe766-il500,000980.3 at α=7.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe766-il500,000577 at α=6.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe766-il1,000,000998 at α=6.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe766-il1,000,000587.2 at α=8°Mach=0 Ncrit=5Xfoil predictionDetails
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