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GOE 311 (MVA H.43) AIRFOIL (goe311-il)

GOE 311 (MVA H.43) AIRFOIL - Gottingen 311 (MVA H.43) airfoil


Airfoil goe311-il
Details Dat file Parser  
(goe311-il) GOE 311 (MVA H.43) AIRFOIL
Gottingen 311 (MVA H.43) airfoil
Max thickness 8.4% at 19.9% chord.
Max camber 6.1% at 39.9% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 311 (MVA H.43) AIRFOIL
       17.       17.

 0.0000000 0.0000000
 0.0123000 0.0192300
 0.0246800 0.0299600
 0.0495100 0.0461200
 0.0744000 0.0569900
 0.0992900 0.0673500
 0.1491300 0.0816800
 0.1990300 0.0912100
 0.2989300 0.1012700
 0.3989300 0.1007300
 0.4990400 0.0906900
 0.5991700 0.0784500
 0.6993500 0.0615100
 0.7995400 0.0434800
 0.8997600 0.0223400
 0.9498800 0.0111700
 1.0000000 0.0021000

 0.0000000 0.0000000
 0.0125900 -.0083700
 0.0251300 -.0119300
 0.0501300 -.0121700
 0.0751300 -.0119000
 0.1001000 -.0092400
 0.1500100 -.0005100
 0.1999300 0.0069200
 0.2998100 0.0180800
 0.3997800 0.0207400
 0.4998300 0.0165000
 0.5998900 0.0100600
 0.6999600 0.0037200
 0.8000200 -.0015200
 0.9000300 -.0028600
 0.9500300 -.0026300
 1.0000000 -.0021000
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Lednicer format dat file
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Polars for GOE 311 (MVA H.43) AIRFOIL (goe311-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe311-il50,000914.3 at α=2.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe311-il50,000534.5 at α=8°Mach=0 Ncrit=5Xfoil predictionDetails
   goe311-il100,000957.5 at α=9°Mach=0 Ncrit=9Xfoil predictionDetails
   goe311-il100,000559.5 at α=8°Mach=0 Ncrit=5Xfoil predictionDetails
   goe311-il200,000982.4 at α=7.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe311-il200,000582 at α=6.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe311-il500,0009114 at α=6.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe311-il500,0005106.4 at α=5.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe311-il1,000,0009136.2 at α=5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe311-il1,000,000597.8 at α=4°Mach=0 Ncrit=5Xfoil predictionDetails
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