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GOE 243 (MVA PR.3) AIRFOIL (goe243-il)

GOE 243 (MVA PR.3) AIRFOIL - Gottingen 243 (MVA PR.3) airfoil


Airfoil goe243-il
Details Dat file Parser  
(goe243-il) GOE 243 (MVA PR.3) AIRFOIL
Gottingen 243 (MVA PR.3) airfoil
Max thickness 19% at 29.3% chord.
Max camber 8.4% at 59.4% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 243 (MVA PR.3) AIRFOIL
       17.       17.

 0.0000000 0.0000000
 0.0108300 0.0384700
 0.0225700 0.0559800
 0.0463900 0.0830200
 0.0705400 0.1025700
 0.0948600 0.1181300
 0.1440300 0.1372700
 0.1934400 0.1509100
 0.2928600 0.1642400
 0.3928800 0.1635900
 0.4933000 0.1539600
 0.5940900 0.1358400
 0.6952000 0.1102400
 0.7965800 0.0786500
 0.8981700 0.0420700
 0.9490700 0.0212800
 1.0000000 0.0015000

 0.0000000 0.0000000
 0.0134500 -.0219100
 0.0261500 -.0263600
 0.0513200 -.0302700
 0.0764000 -.0321800
 0.1014600 -.0335900
 0.1515800 -.0364100
 0.2015800 -.0362300
 0.3010800 -.0249000
 0.4003100 -.0070900
 0.4994500 0.0127300
 0.5985600 0.0330400
 0.6980300 0.0453600
 0.7980800 0.0442200
 0.8989500 0.0241000
 0.9495100 0.0113000
 1.0000000 -.0015000
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Lednicer format dat file
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Polars for GOE 243 (MVA PR.3) AIRFOIL (goe243-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe243-il50,00095.7 at α=-0.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe243-il50,000517.9 at α=3.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe243-il100,000944.6 at α=6.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe243-il100,000549.4 at α=3.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe243-il200,000970.4 at α=3.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe243-il200,000569.4 at α=2.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe243-il500,000999.1 at α=2.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe243-il500,000590.3 at α=2.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe243-il1,000,0009119.1 at α=3.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe243-il1,000,0005107.9 at α=2.5°Mach=0 Ncrit=5Xfoil predictionDetails
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