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GOE 241 (MVA PR.1) AIRFOIL (goe241-il)

GOE 241 (MVA PR.1) AIRFOIL - Gottingen 241 (MVA PR.1) airfoil


Airfoil goe241-il
Details Dat file Parser  
(goe241-il) GOE 241 (MVA PR.1) AIRFOIL
Gottingen 241 (MVA PR.1) airfoil
Max thickness 18.9% at 29.5% chord.
Max camber 8.4% at 49.5% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 241 (MVA PR.1) AIRFOIL
       17.       17.

 0.0000000 0.0000000
 0.0112700 0.0381600
 0.0231500 0.0573500
 0.0472800 0.0846200
 0.0716700 0.1033100
 0.0961700 0.1189000
 0.1454300 0.1418800
 0.1950100 0.1548800
 0.2945700 0.1687900
 0.3946200 0.1670100
 0.4950000 0.1552400
 0.5956100 0.1364800
 0.6964400 0.1106300
 0.7974700 0.0786800
 0.8986200 0.0427400
 0.9492800 0.0223700
 1.0000000 0.0020000

 0.0000000 0.0000000
 0.0129900 -.0152800
 0.0256300 -.0195700
 0.0507200 -.0223700
 0.0757800 -.0242600
 0.1008300 -.0258500
 0.1509000 -.0278400
 0.2008900 -.0277300
 0.3006300 -.0195200
 0.4001600 -.0048200
 0.4995800 0.0130900
 0.5990500 0.0294900
 0.6988500 0.0357000
 0.7989300 0.0333300
 0.8993599 0.0199600
 0.9497100 0.0088800
 1.0000000 -.0020000
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Lednicer format dat file
Selig format dat file

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Polars for GOE 241 (MVA PR.1) AIRFOIL (goe241-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe241-il50,00094.8 at α=7.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe241-il50,000518.8 at α=0.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe241-il100,000942.4 at α=7.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe241-il100,000549 at α=4.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe241-il200,000968.1 at α=6.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe241-il200,000567.1 at α=3.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe241-il500,000994.5 at α=3.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe241-il500,000591.7 at α=3.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe241-il1,000,0009120.6 at α=3.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe241-il1,000,0005113.2 at α=3°Mach=0 Ncrit=5Xfoil predictionDetails
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