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GOE 758 AIRFOIL (goe758-il)

GOE 758 AIRFOIL - Gottingen 758 airfoil


Airfoil goe758-il
Details Dat file Parser  
(goe758-il) GOE 758 AIRFOIL
Gottingen 758 airfoil
Max thickness 13.9% at 30% chord.
Max camber 4.7% at 40% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 758 AIRFOIL
       17.       17.

 0.0000000 0.0000000
 0.0125000 0.0229300
 0.0250000 0.0343600
 0.0500000 0.0517300
 0.0750000 0.0645900
 0.1000000 0.0759500
 0.1500000 0.0931800
 0.2000000 0.1044000
 0.3000000 0.1143500
 0.4000000 0.1133000
 0.5000000 0.1032500
 0.6000000 0.0867000
 0.7000000 0.0686500
 0.8000000 0.0466000
 0.9000000 0.0235500
 0.9500000 0.0122700
 1.0000000 0.0000000

 0.0000000 0.0000000
 0.0125000 -.0145700
 0.0250000 -.0176400
 0.0500000 -.0217800
 0.0750000 -.0244100
 0.1000000 -.0255500
 0.1500000 -.0268200
 0.2000000 -.0271000
 0.3000000 -.0241500
 0.4000000 -.0197000
 0.5000000 -.0142500
 0.6000000 -.0083000
 0.7000000 -.0038500
 0.8000000 -.0014000
 0.9000000 -.0004500
 0.9500000 -.0002300
 1.0000000 0.0000000
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Lednicer format dat file
Selig format dat file

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Polars for GOE 758 AIRFOIL (goe758-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe758-il50,00097.6 at α=4°Mach=0 Ncrit=9Xfoil predictionDetails
   goe758-il50,000525.8 at α=6°Mach=0 Ncrit=5Xfoil predictionDetails
   goe758-il100,000945.4 at α=11.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe758-il100,000552.7 at α=7.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe758-il200,000973.7 at α=7.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe758-il200,000575.6 at α=6.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe758-il500,0009108.1 at α=6.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe758-il500,0005102.8 at α=5.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe758-il1,000,0009133.6 at α=5.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe758-il1,000,0005123.1 at α=6°Mach=0 Ncrit=5Xfoil predictionDetails
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