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GOE 279 (DAIMLER X) AIRFOIL (goe279-il)

GOE 279 (DAIMLER X) AIRFOIL - Gottingen 279 (DAIMLER X) airfoil


Airfoil goe279-il
Details Dat file Parser  
(goe279-il) GOE 279 (DAIMLER X) AIRFOIL
Gottingen 279 (DAIMLER X) airfoil
Max thickness 7.4% at 30% chord.
Max camber 4.7% at 40% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 279 (DAIMLER X) AIRFOIL
       17.       17.

 0.0000000 0.0000000
 0.0124100 0.0235500
 0.0248800 0.0320000
 0.0498200 0.0454900
 0.0747900 0.0555900
 0.0997600 0.0624800
 0.1497200 0.0730800
 0.1996900 0.0795700
 0.2996800 0.0841500
 0.3996800 0.0837400
 0.4997000 0.0786200
 0.5997300 0.0702100
 0.6997700 0.0593900
 0.7998300 0.0433800
 0.8999100 0.0242600
 0.9499500 0.0135600
 1.0000000 0.0018500

 0.0000000 0.0000000
 0.0125200 -.0056500
 0.0250200 -.0051000
 0.0500100 -.0015100
 0.0750000 0.0006900
 0.0999900 0.0026800
 0.1499800 0.0052800
 0.1999700 0.0075700
 0.2999600 0.0098500
 0.3999600 0.0108400
 0.4999600 0.0099200
 0.5999700 0.0086100
 0.6999700 0.0069900
 0.7999800 0.0051200
 0.8999900 0.0021500
 0.9500000 0.0004600
 1.0000000 -.0018500
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Lednicer format dat file
Selig format dat file

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Polars for GOE 279 (DAIMLER X) AIRFOIL (goe279-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe279-il50,000937.6 at α=5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe279-il50,000542.3 at α=5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe279-il100,000958.3 at α=3.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe279-il100,000559 at α=4°Mach=0 Ncrit=5Xfoil predictionDetails
   goe279-il200,000977.4 at α=2.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe279-il200,000573.5 at α=3.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe279-il500,000996.9 at α=2.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe279-il500,000593 at α=4.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe279-il1,000,0009113.9 at α=4.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe279-il1,000,0005105 at α=3.75°Mach=0 Ncrit=5Xfoil predictionDetails
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