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GOE 632 AIRFOIL (goe632-il)

GOE 632 AIRFOIL - Gottingen 632 airfoil


Airfoil goe632-il
Details Dat file Parser  
(goe632-il) GOE 632 AIRFOIL
Gottingen 632 airfoil
Max thickness 14% at 30% chord.
Max camber 3.9% at 40% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 632 AIRFOIL
       17.       17.

 0.0000000 0.0000000
 0.0125000 0.0240400
 0.0250000 0.0365800
 0.0500000 0.0541500
 0.0750000 0.0652300
 0.1000000 0.0748000
 0.1500000 0.0884500
 0.2000000 0.0991000
 0.3000000 0.1089000
 0.4000000 0.1077000
 0.5000000 0.0990000
 0.6000000 0.0838000
 0.7000000 0.0656000
 0.8000000 0.0444000
 0.9000000 0.0232000
 0.9500000 0.0118500
 1.0000000 0.0000000

 0.0000000 0.0000000
 0.0125000 -.0169600
 0.0250000 -.0214200
 0.0500000 -.0253500
 0.0750000 -.0267800
 0.1000000 -.0282000
 0.1500000 -.0300500
 0.2000000 -.0309000
 0.3000000 -.0311000
 0.4000000 -.0293000
 0.5000000 -.0290000
 0.6000000 -.0302000
 0.7000000 -.0294000
 0.8000000 -.0251000
 0.9000000 -.0158000
 0.9500000 -.0091500
 1.0000000 0.0000000
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Lednicer format dat file
Selig format dat file

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Polars for GOE 632 AIRFOIL (goe632-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe632-il50,00097.4 at α=12°Mach=0 Ncrit=9Xfoil predictionDetails
   goe632-il50,000526 at α=3.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe632-il100,000948.5 at α=8.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe632-il100,000551.2 at α=6.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe632-il200,000972.3 at α=7°Mach=0 Ncrit=9Xfoil predictionDetails
   goe632-il200,000569.6 at α=6.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe632-il500,000998.8 at α=6.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe632-il500,000581.6 at α=6.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe632-il1,000,0009104.1 at α=6.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe632-il1,000,000588.6 at α=5°Mach=0 Ncrit=5Xfoil predictionDetails
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