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GOE 113 AIRFOIL (goe113-il)

GOE 113 AIRFOIL - Gottingen 113 airfoil


Airfoil goe113-il
Details Dat file Parser  
(goe113-il) GOE 113 AIRFOIL
Gottingen 113 airfoil
Max thickness 6.7% at 30% chord.
Max camber 3% at 40% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 113 AIRFOIL
       16.       16.

 0.0000000 0.0000000
 0.0125000 0.0120700
 0.0250000 0.0201500
 0.0500000 0.0313000
 0.0750000 0.0404500
 0.1000000 0.0461000
 0.1500000 0.0539000
 0.2000000 0.0584000
 0.3000000 0.0638000
 0.4000000 0.0634000
 0.5000000 0.0580000
 0.6000000 0.0501000
 0.7000000 0.0407000
 0.8000000 0.0303000
 0.9000000 0.0184000
 1.0000000 0.0030000

 0.0000000 0.0000000
 0.0125000 -.0059200
 0.0250000 -.0058500
 0.0500000 -.0057000
 0.0750000 -.0053500
 0.1000000 -.0050000
 0.1500000 -.0043000
 0.2000000 -.0038000
 0.3000000 -.0027000
 0.4000000 -.0016000
 0.5000000 -.0010000
 0.6000000 -.0004000
 0.7000000 -.0003000
 0.8000000 -.0002000
 0.9000000 0.0001000
 1.0000000 0.0000000
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Lednicer format dat file
Selig format dat file

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Polars for GOE 113 AIRFOIL (goe113-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe113-il50,000937.7 at α=6.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe113-il50,000540 at α=5.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe113-il100,000954.7 at α=5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe113-il100,000554.3 at α=4.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe113-il200,000970 at α=4.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe113-il200,000566.8 at α=3.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe113-il500,000986.8 at α=3.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe113-il500,000578 at α=2.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe113-il1,000,000997.1 at α=2.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe113-il1,000,000583.3 at α=3.75°Mach=0 Ncrit=5Xfoil predictionDetails
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