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GOE 446 AIRFOIL (goe446-il)

GOE 446 AIRFOIL - Gottingen 446 airfoil


Airfoil goe446-il
Details Dat file Parser  
(goe446-il) GOE 446 AIRFOIL
Gottingen 446 airfoil
Max thickness 12.9% at 29.7% chord.
Max camber 6.3% at 39.7% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 446 AIRFOIL
       17.       17.

 0.0000000 0.0000000
 0.0119600 0.0231800
 0.0241900 0.0345700
 0.0487400 0.0538400
 0.0734200 0.0677200
 0.0981700 0.0784000
 0.1477700 0.0954600
 0.1974700 0.1083200
 0.2971000 0.1239500
 0.3970300 0.1268900
 0.4971400 0.1222300
 0.5974300 0.1096800
 0.6979000 0.0897300
 0.7984700 0.0654800
 0.8991500 0.0364400
 0.9495600 0.0190200
 1.0000000 0.0016000

 0.0000000 0.0000000
 0.0129200 -.0178000
 0.0255000 -.0212000
 0.0505600 -.0238200
 0.0755400 -.0232300
 0.1004900 -.0210500
 0.1503800 -.0161800
 0.2002800 -.0118100
 0.3001100 -.0046800
 0.4000100 -.0002400
 0.4999400 0.0027000
 0.5998800 0.0050400
 0.6998900 0.0046800
 0.7999200 0.0033200
 0.8999700 0.0013600
 0.9499900 0.0004300
 1.0000000 -.0016000
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Lednicer format dat file
Selig format dat file

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Polars for GOE 446 AIRFOIL (goe446-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe446-il50,00097.6 at α=12.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe446-il50,000521.2 at α=3.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe446-il100,000950.9 at α=10.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe446-il100,000556.7 at α=6.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe446-il200,000983.8 at α=6.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe446-il200,000583.1 at α=5.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe446-il500,0009122 at α=4°Mach=0 Ncrit=9Xfoil predictionDetails
   goe446-il500,0005111.7 at α=3.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe446-il1,000,0009148.7 at α=2.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe446-il1,000,0005130.4 at α=4.5°Mach=0 Ncrit=5Xfoil predictionDetails
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