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GOE 359 AIRFOIL (goe359-il)

GOE 359 AIRFOIL - Gottingen 359 airfoil


Airfoil goe359-il
Details Dat file Parser  
(goe359-il) GOE 359 AIRFOIL
Gottingen 359 airfoil
Max thickness 7.8% at 30% chord.
Max camber 5.8% at 40% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 359 AIRFOIL
       17.       17.

 0.0000000 0.0000000
 0.0125000 0.0175900
 0.0250000 0.0306900
 0.0500000 0.0458800
 0.0750000 0.0585600
 0.1000000 0.0677500
 0.1500000 0.0811300
 0.2000000 0.0890000
 0.3000000 0.0972500
 0.4000000 0.0955000
 0.5000000 0.0877500
 0.6000000 0.0755000
 0.7000000 0.0602500
 0.8000000 0.0425000
 0.9000000 0.0242500
 0.9500000 0.0146200
 1.0000000 0.0015000

 0.0000000 0.0000000
 0.0125000 -.0074100
 0.0250000 -.0073100
 0.0500000 -.0041200
 0.0750000 -.0024400
 0.1000000 0.0007500
 0.1500000 0.0066300
 0.2000000 0.0115000
 0.3000000 0.0192500
 0.4000000 0.0220000
 0.5000000 0.0217500
 0.6000000 0.0205000
 0.7000000 0.0162500
 0.8000000 0.0110000
 0.9000000 0.0052500
 0.9500000 0.0026200
 1.0000000 0.0000000
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Lednicer format dat file
Selig format dat file

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Polars for GOE 359 AIRFOIL (goe359-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe359-il50,000935.9 at α=9.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe359-il50,000541.5 at α=7.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe359-il100,000961.5 at α=7.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe359-il100,000563 at α=6°Mach=0 Ncrit=5Xfoil predictionDetails
   goe359-il200,000983.4 at α=5.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe359-il200,000582 at α=5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe359-il500,0009110.8 at α=4.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe359-il500,0005103.9 at α=3.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe359-il1,000,0009130.6 at α=3.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe359-il1,000,0005103.8 at α=4°Mach=0 Ncrit=5Xfoil predictionDetails
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