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GOE 372 AIRFOIL (goe372-il)

GOE 372 AIRFOIL - Gottingen 372 airfoil


Airfoil goe372-il
Details Dat file Parser  
(goe372-il) GOE 372 AIRFOIL
Gottingen 372 airfoil
Max thickness 6.2% at 29.9% chord.
Max camber 4.3% at 39.9% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 372 AIRFOIL
       17.       17.

 0.0000000 0.0000000
 0.0123800 0.0101400
 0.0248000 0.0172900
 0.0496700 0.0285700
 0.0745600 0.0378600
 0.0994900 0.0446400
 0.1493600 0.0548900
 0.1993000 0.0617900
 0.2991800 0.0709400
 0.3991700 0.0725900
 0.4992200 0.0682400
 0.5993000 0.0608900
 0.6994400 0.0490400
 0.7996000 0.0347000
 0.8997800 0.0188500
 0.9498900 0.0099200
 1.0000000 0.0000000

 0.0000000 0.0000000
 0.0126000 -.0088600
 0.0251300 -.0112100
 0.0501400 -.0119200
 0.0751200 -.0101400
 0.1000900 -.0078500
 0.1500300 -.0027700
 0.1999800 0.0018000
 0.2999000 0.0089500
 0.3998400 0.0136000
 0.4998200 0.0152500
 0.5998300 0.0144000
 0.6998600 0.0120500
 0.7999000 0.0087000
 0.8999600 0.0038500
 0.9499800 0.0014200
 1.0000000 0.0000000
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Lednicer format dat file
Selig format dat file

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Polars for GOE 372 AIRFOIL (goe372-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe372-il50,000943.2 at α=5.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe372-il50,000542.7 at α=5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe372-il100,000962.7 at α=4.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe372-il100,000560.1 at α=3.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe372-il200,000982.5 at α=3.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe372-il200,000577.1 at α=3.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe372-il500,0009108.6 at α=2.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe372-il500,000593 at α=2.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe372-il1,000,0009126.5 at α=1.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe372-il1,000,000589.6 at α=2.25°Mach=0 Ncrit=5Xfoil predictionDetails
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