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GOE 441 AIRFOIL (goe441-il)

GOE 441 AIRFOIL - Gottingen 441 airfoil


Airfoil goe441-il
Details Dat file Parser  
(goe441-il) GOE 441 AIRFOIL
Gottingen 441 airfoil
Max thickness 16% at 29.5% chord.
Max camber 7.7% at 39.5% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 441 AIRFOIL
       17.       17.

 0.0000000 0.0000000
 0.0115900 0.0296500
 0.0236800 0.0433200
 0.0479700 0.0663700
 0.0723600 0.0863100
 0.0969000 0.1013600
 0.1462100 0.1241700
 0.1957500 0.1389800
 0.2953400 0.1526200
 0.3954200 0.1498800
 0.4958000 0.1375500
 0.5962800 0.1219200
 0.6969900 0.0983900
 0.7978500 0.0704700
 0.8988301 0.0381600
 0.9493800 0.0203000
 1.0000000 0.0013500

 0.0000000 0.0000000
 0.0131400 -.0209000
 0.0257900 -.0258100
 0.0508900 -.0292500
 0.0759000 -.0295800
 0.1008500 -.0277200
 0.1507300 -.0238000
 0.2005400 -.0177700
 0.3002100 -.0067300
 0.3998400 0.0051200
 0.4995000 0.0163600
 0.5992800 0.0236100
 0.6991900 0.0266600
 0.7992401 0.0249200
 0.8995600 0.0143800
 0.9497600 0.0077200
 1.0000000 -.0013500
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Lednicer format dat file
Selig format dat file

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Polars for GOE 441 AIRFOIL (goe441-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe441-il50,00096 at α=1.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe441-il50,000531 at α=3.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe441-il100,000945.6 at α=2.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe441-il100,000552 at α=4°Mach=0 Ncrit=5Xfoil predictionDetails
   goe441-il200,000967 at α=5.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe441-il200,000572.5 at α=5.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe441-il500,0009102 at α=6°Mach=0 Ncrit=9Xfoil predictionDetails
   goe441-il500,0005101.7 at α=5.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe441-il1,000,0009132.4 at α=5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe441-il1,000,0005126.9 at α=7°Mach=0 Ncrit=5Xfoil predictionDetails
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