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GOE 308 (MVA H.40) AIRFOIL (goe308-il)

GOE 308 (MVA H.40) AIRFOIL - Gottingen 308 (MVA H.40) airfoil


Airfoil goe308-il
Details Dat file Parser  
(goe308-il) GOE 308 (MVA H.40) AIRFOIL
Gottingen 308 (MVA H.40) airfoil
Max thickness 8.1% at 29.9% chord.
Max camber 5% at 29.9% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 308 (MVA H.40) AIRFOIL
       17.       17.

 0.0000000 0.0000000
 0.0124000 0.0175700
 0.0248400 0.0270500
 0.0497500 0.0427900
 0.0746800 0.0547400
 0.0996200 0.0638900
 0.1495500 0.0761800
 0.1995000 0.0843800
 0.2994600 0.0908700
 0.3994800 0.0879600
 0.4995200 0.0811500
 0.5995800 0.0706400
 0.6996601 0.0573300
 0.7997600 0.0408200
 0.8998700 0.0228100
 0.9499300 0.0123000
 1.0000000 0.0000000

 0.0000000 0.0000000
 0.0125600 -.0093300
 0.0250600 -.0105500
 0.0500600 -.0109000
 0.0750600 -.0094600
 0.1000300 -.0058100
 0.1500000 -.0004100
 0.1999700 0.0048800
 0.2999400 0.0099700
 0.3999400 0.0101600
 0.4999600 0.0069500
 0.5999800 0.0035400
 0.7000000 -.0001700
 0.8000300 -.0051800
 0.9000300 -.0042900
 0.9500100 -.0023900
 1.0000000 0.0000000
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Lednicer format dat file
Selig format dat file

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Polars for GOE 308 (MVA H.40) AIRFOIL (goe308-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe308-il50,000932.2 at α=10.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe308-il50,000537.9 at α=6.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe308-il100,000954.3 at α=8.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe308-il100,000555.7 at α=6.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe308-il200,000974.2 at α=7.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe308-il200,000574.3 at α=6.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe308-il500,0009103 at α=6.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe308-il500,0005100.1 at α=5.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe308-il1,000,0009126.3 at α=5.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe308-il1,000,0005115.1 at α=5.25°Mach=0 Ncrit=5Xfoil predictionDetails
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