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GOE 440 AIRFOIL (goe440-il)

GOE 440 AIRFOIL - Gottingen 440 airfoil


Airfoil goe440-il
Details Dat file Parser  
(goe440-il) GOE 440 AIRFOIL
Gottingen 440 airfoil
Max thickness 15.3% at 30% chord.
Max camber 9.7% at 40% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 440 AIRFOIL
       17.       17.

 0.0000000 0.0000000
 0.0124900 0.0052200
 0.0249700 0.0147500
 0.0499000 0.0548900
 0.0748300 0.0914400
 0.0997800 0.1140900
 0.1497300 0.1421800
 0.1997000 0.1580800
 0.2996800 0.1699700
 0.3996800 0.1658600
 0.4997100 0.1534500
 0.5997500 0.1335400
 0.6997899 0.1079300
 0.7998500 0.0775200
 0.8999200 0.0407100
 0.9499600 0.0218000
 1.0000000 0.0013000

 0.0000000 0.0000000
 0.0125100 -.0031800
 0.0250100 -.0031500
 0.0500100 -.0026000
 0.0750000 -.0009600
 0.1000000 0.0011900
 0.1499900 0.0033800
 0.1999900 0.0076800
 0.2999700 0.0174700
 0.3999500 0.0281600
 0.4999300 0.0346500
 0.5999200 0.0396400
 0.6999199 0.0398300
 0.7999300 0.0347200
 0.8999600 0.0222100
 0.9499800 0.0123000
 1.0000000 -.0013000
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Lednicer format dat file
Selig format dat file

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Polars for GOE 440 AIRFOIL (goe440-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe440-il50,00099.5 at α=10.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe440-il50,000531.9 at α=1.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe440-il100,000953.2 at α=2.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe440-il100,000552.9 at α=2°Mach=0 Ncrit=5Xfoil predictionDetails
   goe440-il200,000971.1 at α=1.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe440-il200,000567.7 at α=2°Mach=0 Ncrit=5Xfoil predictionDetails
   goe440-il500,000992.2 at α=1.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe440-il500,000586.7 at α=0.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe440-il1,000,0009109.5 at α=0.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe440-il1,000,0005100.3 at α=0.25°Mach=0 Ncrit=5Xfoil predictionDetails
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