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GOE 143 (MVA H.20) AIRFOIL (goe143-il)

GOE 143 (MVA H.20) AIRFOIL - Gottingen 143 (MVA H.20) airfoil


Airfoil goe143-il
Details Dat file Parser  
(goe143-il) GOE 143 (MVA H.20) AIRFOIL
Gottingen 143 (MVA H.20) airfoil
Max thickness 7.4% at 19.9% chord.
Max camber 3.8% at 29.9% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 143 (MVA H.20) AIRFOIL
       17.       17.

 0.0000000 0.0000000
 0.0122700 0.0174600
 0.0246600 0.0262200
 0.0494700 0.0410400
 0.0743500 0.0499600
 0.0992700 0.0560900
 0.1491500 0.0653300
 0.1990800 0.0711800
 0.2990300 0.0747700
 0.3990700 0.0717700
 0.4991500 0.0655600
 0.5992600 0.0567600
 0.6994100 0.0453600
 0.8000000 0.0316000
 0.8997700 0.0174500
 0.9498800 0.0094000
 1.0000000 0.0014500

 0.0000000 0.0000000
 0.0126500 -.0113400
 0.0251800 -.0140700
 0.0501700 -.0131500
 0.0751400 -.0111300
 0.1001100 -.0085000
 0.1500700 -.0055600
 0.2000400 -.0032100
 0.2999900 0.0009800
 0.3999500 0.0034800
 0.4999400 0.0047700
 0.5999300 0.0054700
 0.6999400 0.0044600
 0.7999600 0.0034600
 0.8999800 0.0017500
 0.9500000 -.0001000
 1.0000000 -.0014500
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Lednicer format dat file
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Polars for GOE 143 (MVA H.20) AIRFOIL (goe143-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe143-il50,000935.3 at α=5.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe143-il50,000539.8 at α=5.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe143-il100,000953.7 at α=6°Mach=0 Ncrit=9Xfoil predictionDetails
   goe143-il100,000555.4 at α=6°Mach=0 Ncrit=5Xfoil predictionDetails
   goe143-il200,000972.3 at α=5.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe143-il200,000570.1 at α=5.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe143-il500,000994.9 at α=4.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe143-il500,000586.8 at α=4.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe143-il1,000,0009109.9 at α=4.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe143-il1,000,000598.2 at α=6.5°Mach=0 Ncrit=5Xfoil predictionDetails
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