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GOE 596 AIRFOIL (goe596-il)

GOE 596 AIRFOIL - Gottingen 596 airfoil


Airfoil goe596-il
Details Dat file Parser  
(goe596-il) GOE 596 AIRFOIL
Gottingen 596 airfoil
Max thickness 9.8% at 30% chord.
Max camber 4% at 40% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 596 AIRFOIL
       17.       17.

 0.0000000 0.0000000
 0.0125000 0.0212100
 0.0250000 0.0294300
 0.0500000 0.0418500
 0.0750000 0.0522700
 0.1000000 0.0607000
 0.1500000 0.0725500
 0.2000000 0.0809000
 0.3000000 0.0881000
 0.4000000 0.0873000
 0.5000000 0.0795000
 0.6000000 0.0682000
 0.7000000 0.0549000
 0.8000000 0.0381000
 0.9000000 0.0198000
 0.9500000 0.0101500
 1.0000000 0.0000000

 0.0000000 0.0000000
 0.0125000 -.0127900
 0.0250000 -.0150800
 0.0500000 -.0156500
 0.0750000 -.0157200
 0.1000000 -.0153000
 0.1500000 -.0144500
 0.2000000 -.0126000
 0.3000000 -.0094000
 0.4000000 -.0067000
 0.5000000 -.0045000
 0.6000000 -.0033000
 0.7000000 -.0026000
 0.8000000 -.0019000
 0.9000000 -.0007000
 0.9500000 -.0003500
 1.0000000 0.0000000
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Lednicer format dat file
Selig format dat file

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Polars for GOE 596 AIRFOIL (goe596-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe596-il50,000935.5 at α=9.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe596-il50,000537 at α=8.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe596-il100,000956.6 at α=8°Mach=0 Ncrit=9Xfoil predictionDetails
   goe596-il100,000557.4 at α=6.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe596-il200,000977.5 at α=6.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe596-il200,000575.6 at α=5.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe596-il500,0009105.7 at α=5.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe596-il500,000597.2 at α=4°Mach=0 Ncrit=5Xfoil predictionDetails
   goe596-il1,000,0009125.7 at α=4.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe596-il1,000,0005112.5 at α=4.5°Mach=0 Ncrit=5Xfoil predictionDetails
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