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GOE 274 (DAIMLER V) AIRFOIL (goe274-il)

GOE 274 (DAIMLER V) AIRFOIL - Gottingen 274 (DAIMLER V) airfoil


Airfoil goe274-il
Details Dat file Parser  
(goe274-il) GOE 274 (DAIMLER V) AIRFOIL
Gottingen 274 (DAIMLER V) airfoil
Max thickness 8.7% at 29.9% chord.
Max camber 4.8% at 29.9% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 274 (DAIMLER V) AIRFOIL
       17.       17.

 0.0000000 0.0000000
 0.0123600 0.0201800
 0.0247900 0.0310700
 0.0496800 0.0481300
 0.0746000 0.0592000
 0.0995400 0.0684700
 0.1494700 0.0796000
 0.1994200 0.0865400
 0.2993900 0.0917100
 0.3994000 0.0893800
 0.4994400 0.0834500
 0.5994900 0.0755200
 0.6995700 0.0638900
 0.7996700 0.0485600
 0.8998100 0.0289300
 0.9498900 0.0170600
 1.0000000 0.0040000

 0.0000000 0.0000000
 0.0125700 -.0106200
 0.0250700 -.0099300
 0.0500400 -.0060600
 0.0750300 -.0043000
 0.1000200 -.0025300
 0.1499900 0.0008000
 0.1999800 0.0026400
 0.2999700 0.0052100
 0.3999500 0.0074800
 0.4999500 0.0081500
 0.5999400 0.0082200
 0.6999600 0.0062900
 0.7999700 0.0042600
 0.8999900 0.0014300
 0.9500000 -.0006300
 1.0000000 -.0040000
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Lednicer format dat file
Selig format dat file

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Polars for GOE 274 (DAIMLER V) AIRFOIL (goe274-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe274-il50,000937.6 at α=4.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe274-il50,000540.7 at α=5.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe274-il100,000955.8 at α=3°Mach=0 Ncrit=9Xfoil predictionDetails
   goe274-il100,000557 at α=5.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe274-il200,000973.2 at α=5.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe274-il200,000573.2 at α=5.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe274-il500,000999 at α=5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe274-il500,000592.3 at α=4.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe274-il1,000,0009115.1 at α=4.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe274-il1,000,0005105.5 at α=6°Mach=0 Ncrit=5Xfoil predictionDetails
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