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GOE 496 AIRFOIL (goe496-il)

GOE 496 AIRFOIL - Gottingen 496 airfoil


Airfoil goe496-il
Details Dat file Parser  
(goe496-il) GOE 496 AIRFOIL
Gottingen 496 airfoil
Max thickness 10% at 30% chord.
Max camber 5% at 50% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 496 AIRFOIL
       15.       15.

 0.0000000 0.0000000
 0.0125000 0.0198100
 0.0250000 0.0291200
 0.0500000 0.0427500
 0.0750000 0.0533800
 0.1000000 0.0620000
 0.2000000 0.0825000
 0.3000000 0.0925000
 0.4000000 0.0945000
 0.5000000 0.0895000
 0.6000000 0.0795000
 0.7000000 0.0650000
 0.8000000 0.0470000
 0.9000000 0.0260000
 1.0000000 0.0000000

 0.0000000 0.0000000
 0.0125000 -.0136900
 0.0250000 -.0178800
 0.0500000 -.0212500
 0.0750000 -.0231300
 0.1000000 -.0225000
 0.2000000 -.0165000
 0.3000000 -.0070000
 0.4000000 0.0025000
 0.5000000 0.0105000
 0.6000000 0.0150000
 0.7000000 0.0175000
 0.8000000 0.0150000
 0.9000000 0.0100000
 1.0000000 0.0000000
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Lednicer format dat file
Selig format dat file

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Polars for GOE 496 AIRFOIL (goe496-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe496-il50,000937.4 at α=9.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe496-il50,000541 at α=7°Mach=0 Ncrit=5Xfoil predictionDetails
   goe496-il100,000962.9 at α=7°Mach=0 Ncrit=9Xfoil predictionDetails
   goe496-il100,000565 at α=6°Mach=0 Ncrit=5Xfoil predictionDetails
   goe496-il200,000989.6 at α=6°Mach=0 Ncrit=9Xfoil predictionDetails
   goe496-il200,000587.3 at α=5.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe496-il500,0009124.3 at α=5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe496-il500,0005115.1 at α=4°Mach=0 Ncrit=5Xfoil predictionDetails
   goe496-il1,000,0009150.2 at α=4.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe496-il1,000,0005124 at α=4.75°Mach=0 Ncrit=5Xfoil predictionDetails
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