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GOE 494 AIRFOIL (goe494-il)

GOE 494 AIRFOIL - Gottingen 494 airfoil


Airfoil goe494-il
Details Dat file Parser  
(goe494-il) GOE 494 AIRFOIL
Gottingen 494 airfoil
Max thickness 5% at 20% chord.
Max camber 5.1% at 50% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 494 AIRFOIL
       17.       17.

 0.0000000 0.0000000
 0.0124200 0.0115900
 0.0248800 0.0171700
 0.0498200 0.0263500
 0.0747600 0.0345200
 0.0997200 0.0407000
 0.1496500 0.0500500
 0.1996000 0.0569000
 0.2995300 0.0666000
 0.3995000 0.0713000
 0.4995100 0.0705000
 0.5995400 0.0652000
 0.6996200 0.0539000
 0.7997200 0.0401000
 0.8998500 0.0218000
 0.9499199 0.0116500
 1.0000000 0.0000000

 0.0000000 0.0000000
 0.0125500 -.0074100
 0.0250500 -.0073200
 0.0500400 -.0061500
 0.0750300 -.0041700
 0.1000200 -.0023000
 0.1499900 0.0020500
 0.1999500 0.0074000
 0.2998700 0.0181000
 0.3998100 0.0268000
 0.4997800 0.0315000
 0.5997700 0.0327000
 0.6997899 0.0299000
 0.7998400 0.0226000
 0.8999100 0.0128000
 0.9499400 0.0066600
 1.0000000 0.0000000
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Lednicer format dat file
Selig format dat file

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Polars for GOE 494 AIRFOIL (goe494-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe494-il50,000944.5 at α=5.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe494-il50,000545.5 at α=5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe494-il100,000969.5 at α=4.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe494-il100,000569.6 at α=4°Mach=0 Ncrit=5Xfoil predictionDetails
   goe494-il200,000997 at α=3.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe494-il200,000595.6 at α=3.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe494-il500,0009135.4 at α=2.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe494-il500,0005121.9 at α=2.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe494-il1,000,0009164.3 at α=2.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe494-il1,000,0005112.3 at α=1.5°Mach=0 Ncrit=5Xfoil predictionDetails
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