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GOE 564 AIRFOIL (goe564-il)

GOE 564 AIRFOIL - Gottingen 564 airfoil


Airfoil goe564-il
Details Dat file Parser  
(goe564-il) GOE 564 AIRFOIL
Gottingen 564 airfoil
Max thickness 8.2% at 30% chord.
Max camber 2.7% at 40% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 564 AIRFOIL
       17.       17.

 0.0000000 0.0000000
 0.0125000 0.0162900
 0.0250000 0.0235800
 0.0500000 0.0346500
 0.0750000 0.0417300
 0.1000000 0.0478000
 0.1500000 0.0554500
 0.2000000 0.0601000
 0.3000000 0.0659000
 0.4000000 0.0672000
 0.5000000 0.0645000
 0.6000000 0.0578000
 0.7000000 0.0491000
 0.8000000 0.0359000
 0.9000000 0.0202000
 0.9500000 0.0108500
 1.0000000 0.0000000

 0.0000000 0.0000000
 0.0125000 -.0117100
 0.0250000 -.0154300
 0.0500000 -.0193500
 0.0750000 -.0207800
 0.1000000 -.0207000
 0.1500000 -.0195500
 0.2000000 -.0184000
 0.3000000 -.0161000
 0.4000000 -.0138000
 0.5000000 -.0115000
 0.6000000 -.0092000
 0.7000000 -.0069000
 0.8000000 -.0046000
 0.9000000 -.0023000
 0.9500000 -.0011500
 1.0000000 0.0000000
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Lednicer format dat file
Selig format dat file

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Polars for GOE 564 AIRFOIL (goe564-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe564-il50,000937.1 at α=5.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe564-il50,000537.5 at α=5.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe564-il100,000956 at α=4.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe564-il100,000552.6 at α=4°Mach=0 Ncrit=5Xfoil predictionDetails
   goe564-il200,000975.4 at α=3.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe564-il200,000565.6 at α=3°Mach=0 Ncrit=5Xfoil predictionDetails
   goe564-il500,000995.7 at α=1.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe564-il500,000577.6 at α=5.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe564-il1,000,0009103.8 at α=2°Mach=0 Ncrit=9Xfoil predictionDetails
   goe564-il1,000,000589.2 at α=5.75°Mach=0 Ncrit=5Xfoil predictionDetails
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