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GOE 533 AIRFOIL (goe533-il)

GOE 533 AIRFOIL - Gottingen 533 airfoil


Airfoil goe533-il
Details Dat file Parser  
(goe533-il) GOE 533 AIRFOIL
Gottingen 533 airfoil
Max thickness 13.7% at 30% chord.
Max camber 4.7% at 40% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 533 AIRFOIL
       16.       16.

 0.0000000 0.0000000
 0.0125000 0.0289000
 0.0250000 0.0410000
 0.0500000 0.0576000
 0.0750000 0.0709000
 0.1000000 0.0822000
 0.1500000 0.0968000
 0.2000000 0.1069000
 0.3000000 0.1146000
 0.4000000 0.1113000
 0.5000000 0.1005000
 0.6000000 0.0837000
 0.7000000 0.0654000
 0.8000000 0.0456000
 0.9000000 0.0238000
 1.0000000 0.0000000

 0.0000000 0.0000000
 0.0125000 -.0141000
 0.0250000 -.0177000
 0.0500000 -.0209000
 0.0750000 -.0231000
 0.1000000 -.0238000
 0.1500000 -.0247000
 0.2000000 -.0246000
 0.3000000 -.0224000
 0.4000000 -.0177000
 0.5000000 -.0100000
 0.6000000 -.0028000
 0.7000000 0.0044000
 0.8000000 0.0071000
 0.9000000 0.0053000
 1.0000000 0.0000000
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Lednicer format dat file
Selig format dat file

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Polars for GOE 533 AIRFOIL (goe533-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe533-il50,000910.5 at α=1.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe533-il50,000529.4 at α=5.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe533-il100,000946.5 at α=9.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe533-il100,000554.8 at α=6.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe533-il200,000973.8 at α=7.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe533-il200,000575.5 at α=6.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe533-il500,0009106.3 at α=7°Mach=0 Ncrit=9Xfoil predictionDetails
   goe533-il500,0005102.3 at α=6.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe533-il1,000,0009131.1 at α=6.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe533-il1,000,0005121.7 at α=5.75°Mach=0 Ncrit=5Xfoil predictionDetails
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