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GOE 362 AIRFOIL (goe362-il)

GOE 362 AIRFOIL - Gottingen 362 airfoil


Airfoil goe362-il
Details Dat file Parser  
(goe362-il) GOE 362 AIRFOIL
Gottingen 362 airfoil
Max thickness 6.6% at 20% chord.
Max camber 5.3% at 40% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 362 AIRFOIL
       17.       17.

 0.0000000 0.0000000
 0.0125000 0.0205700
 0.0250000 0.0296500
 0.0500000 0.0418000
 0.0750000 0.0509500
 0.1000000 0.0586000
 0.1500000 0.0699000
 0.2000000 0.0772000
 0.3000000 0.0833000
 0.4000000 0.0814000
 0.5000000 0.0755000
 0.6000000 0.0651000
 0.7000000 0.0522000
 0.8000000 0.0368000
 0.9000000 0.0194000
 0.9500000 0.0097000
 1.0000000 0.0000000

 0.0000000 0.0000000
 0.0125000 -.0049300
 0.0250000 -.0058500
 0.0500000 -.0052000
 0.0750000 -.0030500
 0.1000000 0.0001000
 0.1500000 0.0054000
 0.2000000 0.0112000
 0.3000000 0.0193000
 0.4000000 0.0244000
 0.5000000 0.0265000
 0.6000000 0.0256000
 0.7000000 0.0212000
 0.8000000 0.0168000
 0.9000000 0.0084000
 0.9500000 0.0037000
 1.0000000 0.0000000
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Lednicer format dat file
Selig format dat file

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Polars for GOE 362 AIRFOIL (goe362-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe362-il50,000937.3 at α=8.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe362-il50,000543.4 at α=6°Mach=0 Ncrit=5Xfoil predictionDetails
   goe362-il100,000958.4 at α=7.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe362-il100,000563.3 at α=5.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe362-il200,000979.6 at α=6.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe362-il200,000581.9 at α=4.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe362-il500,0009109.4 at α=5.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe362-il500,0005108.1 at α=4.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe362-il1,000,0009131.4 at α=5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe362-il1,000,0005127.7 at α=3.75°Mach=0 Ncrit=5Xfoil predictionDetails
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