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GOE 610 B AIRFOIL (goe610b-il)

GOE 610 B AIRFOIL - Gottingen 610 B airfoil


Airfoil goe610b-il
Details Dat file Parser  
(goe610b-il) GOE 610 B AIRFOIL
Gottingen 610 B airfoil
Max thickness 7.8% at 39.9% chord.
Max camber 5.3% at 39.9% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 610 B AIRFOIL
       16.       16.

 0.0000000 0.0000000
 0.0148000 0.0201500
 0.0495900 0.0405000
 0.0744900 0.0507400
 0.0994200 0.0579900
 0.1492900 0.0714900
 0.1991800 0.0800900
 0.2991100 0.0887900
 0.3990800 0.0919900
 0.4991500 0.0854900
 0.5992800 0.0744900
 0.6994000 0.0599900
 0.7995900 0.0410000
 0.8997800 0.0220000
 0.9498900 0.0115000
 1.0000000 0.0000000

 0.0000000 0.0000000
 0.0151000 -.0098500
 0.0500800 -.0085000
 0.0750600 -.0062500
 0.1000300 -.0028000
 0.1499600 0.0031000
 0.1999300 0.0070000
 0.2998800 0.0122000
 0.3998600 0.0140000
 0.4998600 0.0140000
 0.5998900 0.0120000
 0.6999100 0.0090000
 0.7999600 0.0045000
 0.9000000 0.0000000
 0.9500100 -.0005000
 1.0000000 0.0000000
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Lednicer format dat file
Selig format dat file

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Polars for GOE 610 B AIRFOIL (goe610b-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe610b-il50,000937.4 at α=9.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe610b-il50,000538.8 at α=7.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe610b-il100,000961.2 at α=7.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe610b-il100,000562.7 at α=6.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe610b-il200,000986.5 at α=6.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe610b-il200,000584 at α=5.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe610b-il500,0009118 at α=5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe610b-il500,000595.1 at α=5.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe610b-il1,000,0009132.2 at α=4°Mach=0 Ncrit=9Xfoil predictionDetails
   goe610b-il1,000,000599.4 at α=5.25°Mach=0 Ncrit=5Xfoil predictionDetails
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