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GOE 711 AIRFOIL (goe711-il)

GOE 711 AIRFOIL - Gottingen 711 airfoil


Airfoil goe711-il
Details Dat file Parser  
(goe711-il) GOE 711 AIRFOIL
Gottingen 711 airfoil
Max thickness 14.9% at 30% chord.
Max camber 6.3% at 30% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 711 AIRFOIL
       16.       16.

 0.0000000 0.0000000
 0.0125000 0.0271600
 0.0250000 0.0418200
 0.0500000 0.0626500
 0.0750000 0.0834700
 0.1000000 0.0978000
 0.1500000 0.1179500
 0.2000000 0.1301000
 0.3000000 0.1394000
 0.4000000 0.1382000
 0.5000000 0.1305000
 0.7000000 0.1001000
 0.8000000 0.0779000
 0.9000000 0.0492000
 0.9500000 0.0317500
 1.0000000 0.0140000

 0.0000000 0.0000000
 0.0125000 -.0108400
 0.0250000 -.0126800
 0.0500000 -.0123500
 0.0750000 -.0120200
 0.1000000 -.0117000
 0.1500000 -.0110500
 0.2000000 -.0104000
 0.3000000 -.0091000
 0.4000000 -.0078000
 0.5000000 -.0065000
 0.7000000 -.0039000
 0.8000000 -.0026000
 0.9000000 -.0013000
 0.9500000 -.0006500
 1.0000000 0.0000000
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Lednicer format dat file
Selig format dat file

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Polars for GOE 711 AIRFOIL (goe711-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe711-il50,000920.3 at α=4°Mach=0 Ncrit=9Xfoil predictionDetails
   goe711-il50,000533.2 at α=5.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe711-il100,000948.3 at α=4.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe711-il100,000549.2 at α=5.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe711-il200,000964.6 at α=5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe711-il200,000562.9 at α=4.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe711-il500,000986.3 at α=5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe711-il500,000583.1 at α=4.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe711-il1,000,0009107.2 at α=6.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe711-il1,000,0005102.2 at α=5.25°Mach=0 Ncrit=5Xfoil predictionDetails
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