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GOE 140 (MVA H.17) AIRFOIL (goe140-il)

GOE 140 (MVA H.17) AIRFOIL - Gottingen 140 (MVA H.17) airfoil


Airfoil goe140-il
Details Dat file Parser  
(goe140-il) GOE 140 (MVA H.17) AIRFOIL
Gottingen 140 (MVA H.17) airfoil
Max thickness 8.8% at 29.9% chord.
Max camber 5.3% at 29.9% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 140 (MVA H.17) AIRFOIL
       17.       17.

 0.0000000 0.0000000
 0.0123500 0.0176100
 0.0247400 0.0299200
 0.0495900 0.0469300
 0.0744900 0.0590500
 0.0994100 0.0682600
 0.1492700 0.0839000
 0.1992000 0.0924300
 0.2991600 0.0968000
 0.3992000 0.0923700
 0.4992700 0.0834400
 0.5993800 0.0711100
 0.6995100 0.0564900
 0.7996500 0.0398600
 0.8998001 0.0224300
 0.9498900 0.0129600
 1.0000000 0.0029000

 0.0000000 0.0000000
 0.0125900 -.0108900
 0.0251000 -.0113800
 0.0500800 -.0086600
 0.0750300 -.0039500
 0.1000100 -.0007300
 0.1499600 0.0042000
 0.1999400 0.0064400
 0.2999200 0.0090100
 0.3999100 0.0104800
 0.4999100 0.0102500
 0.5999100 0.0099200
 0.6999300 0.0084900
 0.7999500 0.0053600
 0.8999800 0.0020300
 0.9500000 -.0004300
 1.0000000 -.0029000
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Lednicer format dat file
Selig format dat file

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Polars for GOE 140 (MVA H.17) AIRFOIL (goe140-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe140-il50,000928.2 at α=3.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe140-il50,000537.3 at α=5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe140-il100,000954.3 at α=9.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe140-il100,000556.3 at α=7.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe140-il200,000974.8 at α=7.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe140-il200,000574 at α=6.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe140-il500,0009100.7 at α=6.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe140-il500,000596.5 at α=5.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe140-il1,000,0009119.6 at α=5.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe140-il1,000,0005112 at α=4.75°Mach=0 Ncrit=5Xfoil predictionDetails
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