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GOE 281 (DAIMLER XII) AIRFOIL (goe281-il)

GOE 281 (DAIMLER XII) AIRFOIL - Gottingen 281 (DAIMLER XII) airfoil


Airfoil goe281-il
Details Dat file Parser  
(goe281-il) GOE 281 (DAIMLER XII) AIRFOIL
Gottingen 281 (DAIMLER XII) airfoil
Max thickness 8% at 30% chord.
Max camber 4.5% at 40% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 281 (DAIMLER XII) AIRFOIL
       17.       17.

 0.0000000 0.0000000
 0.0124000 0.0165700
 0.0248400 0.0266500
 0.0497500 0.0425900
 0.0746900 0.0533400
 0.0996400 0.0607900
 0.1495800 0.0717800
 0.1995400 0.0783800
 0.2995000 0.0850700
 0.3995100 0.0838600
 0.4995300 0.0791500
 0.5995900 0.0688400
 0.6996700 0.0564300
 0.7997600 0.0412200
 0.8998600 0.0233100
 0.9499199 0.0128000
 1.0000000 0.0026000

 0.0000000 0.0000000
 0.0125500 -.0084300
 0.0250400 -.0074500
 0.0500300 -.0056000
 0.0750200 -.0040600
 0.1000200 -.0029100
 0.1500000 -.0005100
 0.1999900 0.0012800
 0.2999700 0.0046700
 0.3999600 0.0070600
 0.4999500 0.0076500
 0.5999600 0.0075400
 0.6999700 0.0051300
 0.7999900 0.0022200
 0.9000000 -.0000900
 0.9500100 -.0016900
 1.0000000 -.0026000
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Lednicer format dat file
Selig format dat file

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Polars for GOE 281 (DAIMLER XII) AIRFOIL (goe281-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe281-il50,000936.7 at α=6.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe281-il50,000542.1 at α=6°Mach=0 Ncrit=5Xfoil predictionDetails
   goe281-il100,000959 at α=5.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe281-il100,000559.6 at α=4.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe281-il200,000979.1 at α=4.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe281-il200,000575.2 at α=5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe281-il500,0009101.1 at α=4.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe281-il500,000595.3 at α=4°Mach=0 Ncrit=5Xfoil predictionDetails
   goe281-il1,000,0009118.2 at α=3.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe281-il1,000,000598.2 at α=5°Mach=0 Ncrit=5Xfoil predictionDetails
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