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GOE 310 (MVA H.42) AIRFOIL (goe310-il)

GOE 310 (MVA H.42) AIRFOIL - Gottingen 310 (MVA H.42) airfoil


Airfoil goe310-il
Details Dat file Parser  
(goe310-il) GOE 310 (MVA H.42) AIRFOIL
Gottingen 310 (MVA H.42) airfoil
Max thickness 8.1% at 29.9% chord.
Max camber 4.8% at 39.9% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 310 (MVA H.42) AIRFOIL
       17.       17.

 0.0000000 0.0000000
 0.0123100 0.0176300
 0.0247200 0.0259600
 0.0496100 0.0366300
 0.0744900 0.0483900
 0.0994000 0.0570500
 0.1492700 0.0686800
 0.1991900 0.0766100
 0.2990900 0.0856700
 0.3990800 0.0867300
 0.4991500 0.0803900
 0.5992600 0.0697500
 0.6994000 0.0566100
 0.7995700 0.0406800
 0.8997800 0.0211400
 0.9498800 0.0110700
 1.0000000 0.0000000

 0.0000000 0.0000000
 0.0126000 -.0094700
 0.0251100 -.0108300
 0.0501500 -.0137700
 0.0751600 -.0151000
 0.1001500 -.0145400
 0.1501100 -.0106100
 0.2000500 -.0042800
 0.2999500 0.0042800
 0.3999000 0.0095400
 0.4999200 0.0074000
 0.5999900 0.0010600
 0.7000300 -.0031800
 0.8000600 -.0058200
 0.9000599 -.0052600
 0.9500400 -.0037300
 1.0000000 0.0000000
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Lednicer format dat file
Selig format dat file

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Polars for GOE 310 (MVA H.42) AIRFOIL (goe310-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe310-il50,000937.3 at α=8.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe310-il50,000538.4 at α=6.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe310-il100,000959.6 at α=7°Mach=0 Ncrit=9Xfoil predictionDetails
   goe310-il100,000558.3 at α=5.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe310-il200,000980.1 at α=5.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe310-il200,000573 at α=4°Mach=0 Ncrit=5Xfoil predictionDetails
   goe310-il500,000999.9 at α=3.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe310-il500,000572.4 at α=5.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe310-il1,000,000987.1 at α=5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe310-il1,000,000587.4 at α=7.25°Mach=0 Ncrit=5Xfoil predictionDetails
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