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GOE 443 AIRFOIL (goe443-il)

GOE 443 AIRFOIL - Gottingen 443 airfoil


Airfoil goe443-il
Details Dat file Parser  
(goe443-il) GOE 443 AIRFOIL
Gottingen 443 airfoil
Max thickness 5% 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 443 AIRFOIL
       15.       15.

 0.0000000 0.0000000
 0.0125000 0.0060000
 0.0250000 0.0085000
 0.0500000 0.0115000
 0.0750000 0.0140000
 0.1000000 0.0160000
 0.2000000 0.0215000
 0.3000000 0.0250000
 0.4000000 0.0250000
 0.5000000 0.0235000
 0.6000000 0.0205000
 0.7000000 0.0165000
 0.8000000 0.0115000
 0.9000000 0.0065000
 1.0000000 0.0000000

 0.0000000 0.0000000
 0.0125000 -.0060000
 0.0250000 -.0085000
 0.0500000 -.0115000
 0.0750000 -.0140000
 0.1000000 -.0160000
 0.2000000 -.0215000
 0.3000000 -.0250000
 0.4000000 -.0250000
 0.5000000 -.0235000
 0.6000000 -.0205000
 0.7000000 -.0165000
 0.8000000 -.0115000
 0.9000000 -.0065000
 1.0000000 0.0000000
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Lednicer format dat file
Selig format dat file

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Polars for GOE 443 AIRFOIL (goe443-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe443-il50,000916.1 at α=3.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe443-il50,000516 at α=3°Mach=0 Ncrit=5Xfoil predictionDetails
   goe443-il100,000920.3 at α=2.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe443-il100,000526.2 at α=2.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe443-il200,000934 at α=2°Mach=0 Ncrit=9Xfoil predictionDetails
   goe443-il200,000532.2 at α=1.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe443-il500,000944.5 at α=1.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe443-il500,000532 at α=2.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe443-il1,000,000943.3 at α=2.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe443-il1,000,000560.2 at α=3.75°Mach=0 Ncrit=5Xfoil predictionDetails
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