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GOE 276 (DAIMLER VII) AIRFOIL (goe276-il)

GOE 276 (DAIMLER VII) AIRFOIL - Gottingen 276 (DAIMLER VII) airfoil


Airfoil goe276-il
Details Dat file Parser  
(goe276-il) GOE 276 (DAIMLER VII) AIRFOIL
Gottingen 276 (DAIMLER VII) airfoil
Max thickness 7.3% at 30% chord.
Max camber 4% at 30% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 276 (DAIMLER VII) AIRFOIL
       17.       17.

 0.0000000 0.0000000
 0.0124100 0.0173700
 0.0248600 0.0265300
 0.0497900 0.0396700
 0.0747300 0.0496000
 0.0997000 0.0563400
 0.1496400 0.0665100
 0.1996100 0.0723800
 0.2995900 0.0766200
 0.3996000 0.0734600
 0.4996300 0.0692000
 0.5996600 0.0623400
 0.6997200 0.0526800
 0.7997900 0.0387200
 0.8998700 0.0232600
 0.9499199 0.0152300
 1.0000000 0.0040000

 0.0000000 0.0000000
 0.0125500 -.0088300
 0.0250500 -.0087600
 0.0500300 -.0061300
 0.0750200 -.0040800
 0.1000100 -.0024600
 0.1500000 -.0005900
 0.1999900 0.0010300
 0.2999800 0.0040200
 0.3999700 0.0061600
 0.4999600 0.0067000
 0.5999700 0.0061400
 0.6999700 0.0050800
 0.7999800 0.0029200
 0.9000000 0.0002600
 0.9500100 -.0021700
 1.0000000 -.0040000
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Lednicer format dat file
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Polars for GOE 276 (DAIMLER VII) AIRFOIL (goe276-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe276-il50,000936.9 at α=4.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe276-il50,000540.4 at α=5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe276-il100,000953 at α=3.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe276-il100,000556.2 at α=6.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe276-il200,000972.3 at α=6.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe276-il200,000573.2 at α=6°Mach=0 Ncrit=5Xfoil predictionDetails
   goe276-il500,000997.6 at α=5.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe276-il500,000593.6 at α=5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe276-il1,000,0009114.1 at α=4.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe276-il1,000,0005107.1 at α=4.5°Mach=0 Ncrit=5Xfoil predictionDetails
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