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GOE 593 AIRFOIL (goe593-il)

GOE 593 AIRFOIL - Gottingen 593 airfoil


Airfoil goe593-il
Details Dat file Parser  
(goe593-il) GOE 593 AIRFOIL
Gottingen 593 airfoil
Max thickness 11.9% at 30% chord.
Max camber 4.1% at 40% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 593 AIRFOIL
       17.       17.

 0.0000000 0.0000000
 0.0125000 0.0253700
 0.0250000 0.0357500
 0.0500000 0.0500000
 0.0750000 0.0612500
 0.1000000 0.0705000
 0.1500000 0.0840000
 0.2000000 0.0920000
 0.3000000 0.0990000
 0.4000000 0.0990000
 0.5000000 0.0935000
 0.6000000 0.0825000
 0.7000000 0.0675000
 0.8000000 0.0490000
 0.9000000 0.0270000
 0.9500000 0.0150000
 1.0000000 0.0000000

 0.0000000 0.0000000
 0.0125000 -.0116300
 0.0250000 -.0157500
 0.0500000 -.0200000
 0.0750000 -.0222500
 0.1000000 -.0230000
 0.1500000 -.0230000
 0.2000000 -.0225000
 0.3000000 -.0200000
 0.4000000 -.0180000
 0.5000000 -.0150000
 0.6000000 -.0120000
 0.7000000 -.0090000
 0.8000000 -.0060000
 0.9000000 -.0030000
 0.9500000 -.0015000
 1.0000000 0.0000000
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Lednicer format dat file
Selig format dat file

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Polars for GOE 593 AIRFOIL (goe593-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe593-il50,000924.3 at α=12°Mach=0 Ncrit=9Xfoil predictionDetails
   goe593-il50,000535.2 at α=7.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe593-il100,000952.9 at α=5.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe593-il100,000553.2 at α=5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe593-il200,000974.6 at α=4°Mach=0 Ncrit=9Xfoil predictionDetails
   goe593-il200,000569.9 at α=3.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe593-il500,0009101.4 at α=3°Mach=0 Ncrit=9Xfoil predictionDetails
   goe593-il500,000588.9 at α=5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe593-il1,000,0009117.1 at α=2.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe593-il1,000,0005107.1 at α=6°Mach=0 Ncrit=5Xfoil predictionDetails
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