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GOE 563 AIRFOIL (goe563-il)

GOE 563 AIRFOIL - Gottingen 563 airfoil


Airfoil goe563-il
Details Dat file Parser  
(goe563-il) GOE 563 AIRFOIL
Gottingen 563 airfoil
Max thickness 8.9% at 29.8% chord.
Max camber 2.2% at 49.8% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 563 AIRFOIL
       17.       17.

 0.0000000 0.0000000
 0.0119400 0.0159200
 0.0241900 0.0228600
 0.0488200 0.0332300
 0.0735600 0.0406100
 0.0983700 0.0459900
 0.1480700 0.0542600
 0.1978900 0.0595200
 0.2977100 0.0645700
 0.3976700 0.0656200
 0.4977800 0.0626700
 0.5980000 0.0562300
 0.6983600 0.0462900
 0.7988200 0.0333600
 0.8993800 0.0174300
 0.9496900 0.0087100
 1.0000000 0.0000000

 0.0000000 0.0000000
 0.0129800 -.0135400
 0.0256200 -.0175900
 0.0507700 -.0217000
 0.0758500 -.0238100
 0.1008700 -.0244200
 0.1508900 -.0251400
 0.2008800 -.0248700
 0.3008600 -.0243200
 0.4007600 -.0212700
 0.5006300 -.0177300
 0.6005000 -.0141800
 0.7003800 -.0106400
 0.8002500 -.0070900
 0.9001300 -.0035500
 0.9500600 -.0017700
 1.0000000 0.0000000
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Lednicer format dat file
Selig format dat file

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Polars for GOE 563 AIRFOIL (goe563-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe563-il50,000935.9 at α=5.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe563-il50,000536.4 at α=5.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe563-il100,000954.1 at α=5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe563-il100,000551 at α=4.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe563-il200,000973.3 at α=4°Mach=0 Ncrit=9Xfoil predictionDetails
   goe563-il200,000564.2 at α=3.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe563-il500,000995.4 at α=2.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe563-il500,000576.6 at α=2.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe563-il1,000,0009105.6 at α=2.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe563-il1,000,000586.6 at α=5.25°Mach=0 Ncrit=5Xfoil predictionDetails
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