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GOE 101 AIRFOIL (goe101-il)

GOE 101 AIRFOIL - Gottingen 101 airfoil


Airfoil goe101-il
Details Dat file Parser  
(goe101-il) GOE 101 AIRFOIL
Gottingen 101 airfoil
Max thickness 6.9% at 30% chord.
Max camber 4% at 30% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 101 AIRFOIL
       16.       16.

 0.0000000 0.0000000
 0.0125000 0.0150900
 0.0250000 0.0231800
 0.0500000 0.0353500
 0.0750000 0.0435200
 0.1000000 0.0507000
 0.1500000 0.0605500
 0.2000000 0.0674000
 0.3000000 0.0741000
 0.4000000 0.0713000
 0.5000000 0.0640000
 0.6000000 0.0542000
 0.7000000 0.0424000
 0.8000000 0.0296000
 0.9000000 0.0153000
 1.0000000 0.0000000

 0.0000000 0.0000000
 0.0125000 -.0069100
 0.0250000 -.0067300
 0.0500000 -.0054500
 0.0750000 -.0037700
 0.1000000 -.0023000
 0.1500000 0.0000500
 0.2000000 0.0019000
 0.3000000 0.0051000
 0.4000000 0.0075000
 0.5000000 0.0085000
 0.6000000 0.0082000
 0.7000000 0.0069000
 0.8000000 0.0051000
 0.9000000 0.0028000
 1.0000000 0.0000000
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Lednicer format dat file
Selig format dat file

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Polars for GOE 101 AIRFOIL (goe101-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe101-il50,000939.7 at α=7.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe101-il50,000541.1 at α=7.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe101-il100,000958.7 at α=7°Mach=0 Ncrit=9Xfoil predictionDetails
   goe101-il100,000559.5 at α=6.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe101-il200,000977.9 at α=6.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe101-il200,000577.2 at α=5.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe101-il500,0009104.4 at α=5.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe101-il500,0005100.5 at α=4.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe101-il1,000,0009123.8 at α=4.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe101-il1,000,0005114.7 at α=3.75°Mach=0 Ncrit=5Xfoil predictionDetails
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