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GOE 366 AIRFOIL (goe366-il)

GOE 366 AIRFOIL - Gottingen 366 airfoil


Airfoil goe366-il
Details Dat file Parser  
(goe366-il) GOE 366 AIRFOIL
Gottingen 366 airfoil
Max thickness 13.1% at 29.8% chord.
Max camber 7.2% at 39.8% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 366 AIRFOIL
       17.       17.

 0.0000000 0.0000000
 0.0120400 0.0298900
 0.0243000 0.0448800
 0.0489800 0.0659600
 0.0737400 0.0813400
 0.0985500 0.0933300
 0.1482500 0.1126000
 0.1980500 0.1257700
 0.2978700 0.1375200
 0.3978800 0.1366700
 0.4980100 0.1282200
 0.5982300 0.1142700
 0.6985700 0.0925300
 0.7989600 0.0669800
 0.8994400 0.0362400
 0.9496900 0.0200200
 1.0000000 0.0015000

 0.0000000 0.0000000
 0.0127600 -.0168000
 0.0252400 -.0155100
 0.0501900 -.0122200
 0.0751400 -.0091400
 0.1001000 -.0063500
 0.1500300 -.0021700
 0.1999700 0.0020000
 0.2999000 0.0061500
 0.3998700 0.0083000
 0.4998600 0.0087500
 0.5998700 0.0082000
 0.6998900 0.0071500
 0.7999099 0.0060000
 0.8999600 0.0027500
 0.9499900 0.0009200
 1.0000000 -.0015000
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Lednicer format dat file
Selig format dat file

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Polars for GOE 366 AIRFOIL (goe366-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe366-il50,00098.1 at α=3°Mach=0 Ncrit=9Xfoil predictionDetails
   goe366-il50,000530.9 at α=4.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe366-il100,000951.7 at α=4.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe366-il100,000555 at α=5.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe366-il200,000982.6 at α=-0.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe366-il200,000573.3 at α=5.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe366-il500,0009102.6 at α=5.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe366-il500,000597.5 at α=6°Mach=0 Ncrit=5Xfoil predictionDetails
   goe366-il1,000,0009128.5 at α=5.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe366-il1,000,0005121.1 at α=6.25°Mach=0 Ncrit=5Xfoil predictionDetails
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