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GOE 587 AIRFOIL (goe587-il)

GOE 587 AIRFOIL - Gottingen 587 airfoil


Airfoil goe587-il
Details Dat file Parser  
(goe587-il) GOE 587 AIRFOIL
Gottingen 587 airfoil
Max thickness 5.8% at 40% chord.
Max camber 3% at 30% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 587 AIRFOIL
       17.       17.

 0.0000000 0.0000000
 0.0125500 0.0104400
 0.0250700 0.0148900
 0.0501000 0.0227700
 0.0751300 0.0296600
 0.1001600 0.0350500
 0.1502000 0.0448200
 0.2002300 0.0516000
 0.3002600 0.0581500
 0.4002600 0.0582000
 0.5002400 0.0527500
 0.6002000 0.0453000
 0.7001899 0.0354100
 0.8001100 0.0249000
 0.9000599 0.0134500
 0.9500300 0.0077200
 1.0000000 0.0000000

 0.0000000 0.0000000
 0.0124800 -.0050600
 0.0249700 -.0061100
 0.0499700 -.0057200
 0.0749800 -.0048400
 0.0999800 -.0034500
 0.1500100 -.0013200
 0.2000000 0.0001000
 0.3000100 0.0011500
 0.4000000 0.0002000
 0.4999800 -.0037500
 0.5999700 -.0067000
 0.6999600 -.0091500
 0.7999600 -.0091000
 0.8999800 -.0045500
 0.9499900 -.0017700
 1.0000000 0.0000000
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Lednicer format dat file
Selig format dat file

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Polars for GOE 587 AIRFOIL (goe587-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe587-il50,000936.6 at α=4.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe587-il50,000537 at α=4.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe587-il100,000950.1 at α=4°Mach=0 Ncrit=9Xfoil predictionDetails
   goe587-il100,000550.7 at α=4.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe587-il200,000963.5 at α=3.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe587-il200,000562.9 at α=3.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe587-il500,000977.8 at α=2.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe587-il500,000570.7 at α=2.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe587-il1,000,000977.9 at α=2.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe587-il1,000,000577.1 at α=2.5°Mach=0 Ncrit=5Xfoil predictionDetails
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