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GOE 358 AIRFOIL (goe358-il)

GOE 358 AIRFOIL - Gottingen 358 airfoil


Airfoil goe358-il
Details Dat file Parser  
(goe358-il) GOE 358 AIRFOIL
Gottingen 358 airfoil
Max thickness 10.9% at 20% chord.
Max camber 5.6% at 50% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 358 AIRFOIL
       14.       14.

 0.0000000 0.0000000
 0.0250000 0.0321600
 0.0500000 0.0460200
 0.1000000 0.0658500
 0.1500000 0.0787800
 0.2000000 0.0891000
 0.3000000 0.0970500
 0.4000000 0.0965000
 0.5000000 0.0907500
 0.6000000 0.0807000
 0.7000000 0.0664500
 0.8000000 0.0499000
 0.9000000 0.0290500
 1.0000000 0.0032000

 0.0000000 0.0000000
 0.0250000 -.0176400
 0.0500000 -.0214800
 0.1000000 -.0238500
 0.1500000 -.0225300
 0.2000000 -.0196000
 0.3000000 -.0067500
 0.4000000 0.0100000
 0.5000000 0.0231500
 0.6000000 0.0290000
 0.7000000 0.0289500
 0.8000000 0.0227000
 0.9000000 0.0117500
 1.0000000 0.0000000
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Lednicer format dat file
Selig format dat file

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Polars for GOE 358 AIRFOIL (goe358-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe358-il50,000937.5 at α=9.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe358-il50,000542.2 at α=5.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe358-il100,000958.5 at α=8.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe358-il100,000561.8 at α=5.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe358-il200,000979 at α=7°Mach=0 Ncrit=9Xfoil predictionDetails
   goe358-il200,000579 at α=7°Mach=0 Ncrit=5Xfoil predictionDetails
   goe358-il500,0009105.7 at α=7.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe358-il500,000599.2 at α=6.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe358-il1,000,0009119.2 at α=6°Mach=0 Ncrit=9Xfoil predictionDetails
   goe358-il1,000,0005115.3 at α=5.5°Mach=0 Ncrit=5Xfoil predictionDetails
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