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GOE 309 (MVA H.41) AIRFOIL (goe309-il)

GOE 309 (MVA H.41) AIRFOIL - Gottingen 309 (MVA H.41) airfoil


Airfoil goe309-il
Details Dat file Parser  
(goe309-il) GOE 309 (MVA H.41) AIRFOIL
Gottingen 309 (MVA H.41) airfoil
Max thickness 8.4% at 30% chord.
Max camber 4.7% at 30% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 309 (MVA H.41) AIRFOIL
       17.       17.

 0.0000000 0.0000000
 0.0125100 0.0158900
 0.0250200 0.0264800
 0.0500300 0.0430600
 0.0750400 0.0543500
 0.1000400 0.0633300
 0.1500500 0.0747900
 0.2000600 0.0820600
 0.3000600 0.0888900
 0.4000600 0.0866200
 0.5000600 0.0791500
 0.6000500 0.0674800
 0.7000400 0.0525100
 0.8000300 0.0365400
 0.9000100 0.0195700
 0.9500100 0.0102400
 1.0000000 0.0020000

 0.0000000 0.0000000
 0.0124900 -.0085100
 0.0249900 -.0101200
 0.0499900 -.0103300
 0.0749900 -.0090500
 0.1000000 -.0064700
 0.1500000 -.0027000
 0.2000000 0.0000600
 0.3000000 0.0045900
 0.4000000 0.0026200
 0.5000000 -.0017500
 0.6000000 -.0068200
 0.6999900 -.0101900
 0.7999900 -.0106600
 0.8999900 -.0075300
 0.9500000 -.0048600
 1.0000000 -.0020000
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Lednicer format dat file
Selig format dat file

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Polars for GOE 309 (MVA H.41) AIRFOIL (goe309-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe309-il50,000934.3 at α=9.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe309-il50,000537.7 at α=7.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe309-il100,000954.7 at α=7.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe309-il100,000555.2 at α=6.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe309-il200,000973.4 at α=6.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe309-il200,000571.1 at α=5.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe309-il500,000997 at α=5.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe309-il500,000590.6 at α=4.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe309-il1,000,0009113.8 at α=4.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe309-il1,000,0005101.2 at α=3.75°Mach=0 Ncrit=5Xfoil predictionDetails
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