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GOE 769 AIRFOIL (goe769-il)

GOE 769 AIRFOIL - Gottingen 769 airfoil


Airfoil goe769-il
Details Dat file Parser  
(goe769-il) GOE 769 AIRFOIL
Gottingen 769 airfoil
Max thickness 13.8% at 20% chord.
Max camber 4.8% at 30% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 769 AIRFOIL
       17.       17.

 0.0000000 0.0000000
 0.0125000 0.0348200
 0.0250000 0.0507400
 0.0500000 0.0726800
 0.1000000 0.0967600
 0.1500000 0.1084400
 0.2000000 0.1137200
 0.2500000 0.1154000
 0.3000000 0.1139800
 0.4000000 0.1053400
 0.5000000 0.0917000
 0.6000000 0.0740600
 0.7000000 0.0554200
 0.8000000 0.0368800
 0.9000000 0.0185400
 0.9500000 0.0093200
 1.0000000 0.0000000

 0.0000000 0.0000000
 0.0125000 -.0218800
 0.0250000 -.0267600
 0.0500000 -.0304200
 0.1000000 -.0302400
 0.1500000 -.0274600
 0.2000000 -.0244800
 0.2500000 -.0212000
 0.3000000 -.0181200
 0.4000000 -.0131600
 0.5000000 -.0093000
 0.6000000 -.0064400
 0.7000000 -.0042800
 0.8000000 -.0028200
 0.9000000 -.0013600
 0.9500000 -.0006800
 1.0000000 0.0000000
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Lednicer format dat file
Selig format dat file

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Polars for GOE 769 AIRFOIL (goe769-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe769-il50,000916.6 at α=1.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe769-il50,000528.9 at α=4.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe769-il100,000939.1 at α=4.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe769-il100,000545.3 at α=6.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe769-il200,000959.1 at α=6°Mach=0 Ncrit=9Xfoil predictionDetails
   goe769-il200,000561.8 at α=6.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe769-il500,000985.9 at α=6°Mach=0 Ncrit=9Xfoil predictionDetails
   goe769-il500,000585.2 at α=7.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe769-il1,000,0009107.9 at α=7.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe769-il1,000,0005106 at α=8.25°Mach=0 Ncrit=5Xfoil predictionDetails
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