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GOE 459 AIRFOIL (goe459-il)

GOE 459 AIRFOIL - Gottingen 459 airfoil


Airfoil goe459-il
Details Dat file Parser  
(goe459-il) GOE 459 AIRFOIL
Gottingen 459 airfoil
Max thickness 12.7% at 30% chord.
Max camber 0% at 0% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 459 AIRFOIL
       17.       17.

 0.0000000 0.0000000
 0.0125000 0.0180000
 0.0250000 0.0265000
 0.0500000 0.0360000
 0.0750000 0.0430000
 0.1000000 0.0485000
 0.1500000 0.0555000
 0.2000000 0.0600000
 0.3000000 0.0635000
 0.4000000 0.0630000
 0.5000000 0.0580000
 0.6000000 0.0505000
 0.7000000 0.0405000
 0.8000000 0.0290000
 0.9000000 0.0160000
 0.9500000 0.0090000
 1.0000000 0.0000000

 0.0000000 0.0000000
 0.0125000 -.0180000
 0.0250000 -.0265000
 0.0500000 -.0360000
 0.0750000 -.0430000
 0.1000000 -.0485000
 0.1500000 -.0555000
 0.2000000 -.0600000
 0.3000000 -.0635000
 0.4000000 -.0630000
 0.5000000 -.0580000
 0.6000000 -.0505000
 0.7000000 -.0405000
 0.8000000 -.0290000
 0.9000000 -.0160000
 0.9500000 -.0090000
 1.0000000 0.0000000
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Lednicer format dat file
Selig format dat file

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Polars for GOE 459 AIRFOIL (goe459-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe459-il50,000928.6 at α=5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe459-il50,000527.8 at α=4.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe459-il100,000940.5 at α=4.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe459-il100,000537.3 at α=5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe459-il200,000949.3 at α=4.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe459-il200,000545.3 at α=6.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe459-il500,000959 at α=7.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe459-il500,000560.2 at α=8.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe459-il1,000,000975.6 at α=10.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe459-il1,000,000575.4 at α=9.75°Mach=0 Ncrit=5Xfoil predictionDetails
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