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GOE 444 AIRFOIL (goe444-il)

GOE 444 AIRFOIL - Gottingen 444 airfoil


Airfoil goe444-il
Details Dat file Parser  
(goe444-il) GOE 444 AIRFOIL
Gottingen 444 airfoil
Max thickness 5.6% at 30% chord.
Max camber 0% at 0% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 444 AIRFOIL
       17.       17.

 0.0000000 0.0000000
 0.0125000 0.0060000
 0.0250000 0.0090000
 0.0500000 0.0130000
 0.0750000 0.0160000
 0.1000000 0.0190000
 0.1500000 0.0230000
 0.2000000 0.0255000
 0.3000000 0.0280000
 0.4000000 0.0280000
 0.5000000 0.0270000
 0.6000000 0.0240000
 0.7000000 0.0195000
 0.8000000 0.0140000
 0.9000000 0.0080000
 0.9500000 0.0045000
 1.0000000 0.0000000

 0.0000000 0.0000000
 0.0125000 -.0060000
 0.0250000 -.0090000
 0.0500000 -.0130000
 0.0750000 -.0160000
 0.1000000 -.0190000
 0.1500000 -.0230000
 0.2000000 -.0255000
 0.3000000 -.0280000
 0.4000000 -.0280000
 0.5000000 -.0270000
 0.6000000 -.0240000
 0.7000000 -.0195000
 0.8000000 -.0140000
 0.9000000 -.0080000
 0.9500000 -.0045000
 1.0000000 0.0000000
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Lednicer format dat file
Selig format dat file

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Polars for GOE 444 AIRFOIL (goe444-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe444-il50,000917.1 at α=3.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe444-il50,000516.5 at α=3.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe444-il100,000921.5 at α=2.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe444-il100,000524.8 at α=2.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe444-il200,000938.2 at α=2°Mach=0 Ncrit=9Xfoil predictionDetails
   goe444-il200,000535.2 at α=1.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe444-il500,000945.9 at α=1.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe444-il500,000531.8 at α=2.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe444-il1,000,000942.3 at α=2.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe444-il1,000,000534.1 at α=2.5°Mach=0 Ncrit=5Xfoil predictionDetails
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