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GOE 532 AIRFOIL (goe532-il)

GOE 532 AIRFOIL - Gottingen 532 airfoil


Airfoil goe532-il
Details Dat file Parser  
(goe532-il) GOE 532 AIRFOIL
Gottingen 532 airfoil
Max thickness 12.5% at 30% chord.
Max camber 4.8% at 40% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 532 AIRFOIL
       17.       17.

 0.0000000 0.0000000
 0.0125000 0.0342900
 0.0250000 0.0465900
 0.0500000 0.0621800
 0.0765000 0.0738000
 0.1000000 0.0833500
 0.1500000 0.0950200
 0.2000000 0.1027000
 0.3000000 0.1100500
 0.4000000 0.1054000
 0.5000000 0.0942500
 0.6000000 0.0796000
 0.7000000 0.0629500
 0.8000000 0.0433000
 0.9000000 0.0226500
 0.9500000 0.0118300
 1.0000000 0.0000000

 0.0000000 0.0000000
 0.0125000 -.0127100
 0.0250000 -.0159100
 0.0500000 -.0183200
 0.0765000 -.0197000
 0.1000000 -.0206500
 0.1500000 -.0209800
 0.2000000 -.0198000
 0.3000000 -.0149500
 0.4000000 -.0086000
 0.5000000 -.0022500
 0.6000000 0.0031000
 0.7000000 0.0069500
 0.8000000 0.0078000
 0.9000000 0.0046500
 0.9500000 0.0023300
 1.0000000 0.0000000
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Lednicer format dat file
Selig format dat file

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Polars for GOE 532 AIRFOIL (goe532-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe532-il50,000917.7 at α=6.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe532-il50,000534.7 at α=5.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe532-il100,000953.3 at α=7.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe532-il100,000556 at α=6.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe532-il200,000976.6 at α=6.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe532-il200,000573.5 at α=5.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe532-il500,0009101.7 at α=4.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe532-il500,000589.7 at α=3°Mach=0 Ncrit=5Xfoil predictionDetails
   goe532-il1,000,0009115.7 at α=3.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe532-il1,000,0005102.7 at α=7°Mach=0 Ncrit=5Xfoil predictionDetails
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