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GOE 363 AIRFOIL (goe363-il)

GOE 363 AIRFOIL - Gottingen 363 airfoil


Airfoil goe363-il
Details Dat file Parser  
(goe363-il) GOE 363 AIRFOIL
Gottingen 363 airfoil
Max thickness 11.1% at 19.8% chord.
Max camber 5.7% at 39.8% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 363 AIRFOIL
       17.       17.

 0.0000000 0.0000000
 0.0121200 0.0242900
 0.0243900 0.0389800
 0.0490700 0.0597600
 0.0738300 0.0752500
 0.0986800 0.0847300
 0.1484700 0.0984100
 0.1983700 0.1050800
 0.2982900 0.1098400
 0.3983200 0.1081900
 0.4984400 0.1000500
 0.5986200 0.0887100
 0.6988800 0.0720700
 0.7992200 0.0503300
 0.8995800 0.0268900
 0.9497899 0.0136700
 1.0000000 0.0005500

 0.0000000 0.0000000
 0.0126500 -.0095000
 0.0251900 -.0119100
 0.0502200 -.0142200
 0.0752300 -.0149300
 0.1002200 -.0140400
 0.1501500 -.0094700
 0.2000900 -.0054900
 0.2999700 0.0019600
 0.3999000 0.0062200
 0.4998800 0.0077700
 0.5998900 0.0072300
 0.6999000 0.0065800
 0.7999099 0.0058400
 0.8999500 0.0032900
 0.9499800 0.0013700
 1.0000000 -.0005500
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Lednicer format dat file
Selig format dat file

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Polars for GOE 363 AIRFOIL (goe363-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe363-il50,000932.7 at α=4.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe363-il50,000537 at α=5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe363-il100,000953.3 at α=2.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe363-il100,000552.3 at α=3.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe363-il200,000970.1 at α=2°Mach=0 Ncrit=9Xfoil predictionDetails
   goe363-il200,000565.3 at α=5.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe363-il500,000989.5 at α=7.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe363-il500,000588.2 at α=6.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe363-il1,000,0009110.5 at α=6.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe363-il1,000,0005104.8 at α=5.25°Mach=0 Ncrit=5Xfoil predictionDetails
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