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GOE 590 AIRFOIL (goe590-il)

GOE 590 AIRFOIL - Gottingen 590 airfoil


Airfoil goe590-il
Details Dat file Parser  
(goe590-il) GOE 590 AIRFOIL
Gottingen 590 airfoil
Max thickness 5.7% at 30% chord.
Max camber 4% at 30% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 590 AIRFOIL
       17.       17.

 0.0000000 0.0000000
 0.0124900 0.0110100
 0.0249900 0.0165100
 0.0499900 0.0255200
 0.0749800 0.0330400
 0.0999800 0.0400500
 0.1499700 0.0510700
 0.1999700 0.0596000
 0.2999700 0.0686500
 0.3999700 0.0672000
 0.4999700 0.0592500
 0.5999800 0.0493000
 0.6999800 0.0368500
 0.7999900 0.0249000
 0.8999900 0.0124500
 0.9500000 0.0064700
 1.0000000 0.0000000

 0.0000000 0.0000000
 0.0125000 -.0049900
 0.0250000 -.0049900
 0.0500000 -.0034700
 0.0750000 -.0009600
 0.1000000 0.0015500
 0.1500000 0.0060700
 0.2000000 0.0091000
 0.2999900 0.0116500
 0.3999900 0.0107000
 0.5000000 0.0052500
 0.6000000 0.0003000
 0.7000000 -.0041500
 0.8000000 -.0046000
 0.9000000 -.0040500
 0.9500000 -.0025200
 1.0000000 0.0000000
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Lednicer format dat file
Selig format dat file

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Polars for GOE 590 AIRFOIL (goe590-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe590-il50,000937.3 at α=5.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe590-il50,000538.4 at α=5.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe590-il100,000952.2 at α=5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe590-il100,000553.7 at α=5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe590-il200,000967.6 at α=4.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe590-il200,000570.1 at α=4.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe590-il500,000994.7 at α=4.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe590-il500,000593.9 at α=4°Mach=0 Ncrit=5Xfoil predictionDetails
   goe590-il1,000,0009114.6 at α=3.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe590-il1,000,0005111.5 at α=3.75°Mach=0 Ncrit=5Xfoil predictionDetails
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