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GOE 592 AIRFOIL (goe592-il)

GOE 592 AIRFOIL - Gottingen 592 airfoil


Airfoil goe592-il
Details Dat file Parser  
(goe592-il) GOE 592 AIRFOIL
Gottingen 592 airfoil
Max thickness 14.3% at 29.7% chord.
Max camber 7.5% at 39.7% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 592 AIRFOIL
       17.       17.

 0.0000000 0.0000000
 0.0116700 0.0367600
 0.0238500 0.0510400
 0.0484200 0.0700900
 0.0731200 0.0836500
 0.0978600 0.0952000
 0.1474400 0.1138200
 0.1971400 0.1269400
 0.2968000 0.1421800
 0.3967300 0.1454300
 0.4968800 0.1386800
 0.5972300 0.1229400
 0.6977500 0.1002000
 0.7984000 0.0709600
 0.8992000 0.0357300
 0.9496200 0.0168700
 1.0000000 0.0000000

 0.0000000 0.0000000
 0.0128200 -.0142100
 0.0254300 -.0189300
 0.0504800 -.0213600
 0.0754500 -.0198000
 0.1004000 -.0177400
 0.1502400 -.0128000
 0.2001800 -.0080000
 0.3000100 -.0002500
 0.3999000 0.0045000
 0.4998400 0.0072500
 0.5998000 0.0090000
 0.6998000 0.0087500
 0.7998500 0.0065000
 0.8999000 0.0042500
 0.9499500 0.0023700
 1.0000000 0.0000000
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Lednicer format dat file
Selig format dat file

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Polars for GOE 592 AIRFOIL (goe592-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe592-il50,00095.3 at α=8.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe592-il50,000513.3 at α=4°Mach=0 Ncrit=5Xfoil predictionDetails
   goe592-il100,000932.1 at α=12.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe592-il100,000545.9 at α=5.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe592-il200,000976.5 at α=7.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe592-il200,000576.2 at α=4.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe592-il500,0009114.9 at α=4.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe592-il500,0005107 at α=3.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe592-il1,000,0009142.4 at α=3.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe592-il1,000,0005124.5 at α=4.5°Mach=0 Ncrit=5Xfoil predictionDetails
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