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GOE 529 AIRFOIL (goe529-il)

GOE 529 AIRFOIL - Gottingen 529 airfoil


Airfoil goe529-il
Details Dat file Parser  
(goe529-il) GOE 529 AIRFOIL
Gottingen 529 airfoil
Max thickness 9.7% at 29.9% chord.
Max camber 5.8% at 39.9% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 529 AIRFOIL
       17.       17.

 0.0000000 0.0000000
 0.0122600 0.0206400
 0.0246300 0.0317800
 0.0494500 0.0475700
 0.0743100 0.0603500
 0.0992000 0.0696400
 0.1490200 0.0852100
 0.1989000 0.0952900
 0.2987900 0.1049400
 0.3988000 0.1040900
 0.4988900 0.0962400
 0.5990600 0.0813900
 0.6992600 0.0645400
 0.7994900 0.0446900
 0.8997300 0.0233500
 0.9498600 0.0119200
 1.0000000 0.0000000

 0.0000000 0.0000000
 0.0126100 -.0098500
 0.0251300 -.0117100
 0.0501400 -.0119200
 0.0751200 -.0101400
 0.1000900 -.0078500
 0.1500300 -.0027700
 0.1999800 0.0018000
 0.2999100 0.0079500
 0.3998700 0.0116000
 0.4998600 0.0122500
 0.5998700 0.0109000
 0.6999000 0.0090500
 0.7999300 0.0062000
 0.8999600 0.0033500
 0.9499800 0.0019200
 1.0000000 0.0000000
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Lednicer format dat file
Selig format dat file

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Polars for GOE 529 AIRFOIL (goe529-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe529-il50,000912.9 at α=3.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe529-il50,000533.6 at α=5.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe529-il100,000954.8 at α=9.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe529-il100,000560 at α=6.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe529-il200,000981.4 at α=6.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe529-il200,000581.9 at α=6.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe529-il500,0009114.6 at α=5.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe529-il500,0005109 at α=5.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe529-il1,000,0009138.6 at α=5.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe529-il1,000,0005127.3 at α=4.5°Mach=0 Ncrit=5Xfoil predictionDetails
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