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GOE 585 AIRFOIL (goe585-il)

GOE 585 AIRFOIL - Gottingen 585 airfoil


Airfoil goe585-il
Details Dat file Parser  
(goe585-il) GOE 585 AIRFOIL
Gottingen 585 airfoil
Max thickness 8.2% at 20% chord.
Max camber 3.4% at 40% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 585 AIRFOIL
       17.       17.

 0.0000000 0.0000000
 0.0125000 0.0187300
 0.0250000 0.0274600
 0.0500000 0.0394300
 0.0750000 0.0483900
 0.1000000 0.0553500
 0.1500000 0.0642700
 0.2000000 0.0692000
 0.3000000 0.0725500
 0.4000000 0.0714000
 0.5000000 0.0672500
 0.6000000 0.0591000
 0.7000000 0.0479500
 0.8000000 0.0348000
 0.9000000 0.0186500
 0.9500000 0.0100800
 1.0000000 0.0000000

 0.0000000 0.0000000
 0.0125000 -.0112700
 0.0250000 -.0140400
 0.0500000 -.0165800
 0.0750000 -.0171100
 0.1000000 -.0166500
 0.1500000 -.0147200
 0.2000000 -.0128000
 0.3000000 -.0079500
 0.4000000 -.0041000
 0.5000000 -.0022500
 0.6000000 -.0014000
 0.7000000 -.0010500
 0.8000000 -.0017000
 0.9000000 -.0008500
 0.9500000 -.0004300
 1.0000000 0.0000000
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Lednicer format dat file
Selig format dat file

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Polars for GOE 585 AIRFOIL (goe585-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe585-il50,000934.6 at α=4.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe585-il50,000537.4 at α=5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe585-il100,000952.7 at α=3.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe585-il100,000551 at α=5.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe585-il200,000970.3 at α=3°Mach=0 Ncrit=9Xfoil predictionDetails
   goe585-il200,000566.1 at α=6.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe585-il500,000990.4 at α=2°Mach=0 Ncrit=9Xfoil predictionDetails
   goe585-il500,000587.9 at α=6.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe585-il1,000,0009108.2 at α=6.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe585-il1,000,0005104.5 at α=5.75°Mach=0 Ncrit=5Xfoil predictionDetails
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