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GOE 530 AIRFOIL (goe530-il)

GOE 530 AIRFOIL - Gottingen 530 airfoil


Airfoil goe530-il
Details Dat file Parser  
(goe530-il) GOE 530 AIRFOIL
Gottingen 530 airfoil
Max thickness 12.9% at 29.8% chord.
Max camber 5.1% at 29.8% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 530 AIRFOIL
       17.       17.

 0.0000000 0.0000000
 0.0120000 0.0341700
 0.0243300 0.0463500
 0.0490900 0.0627100
 0.0739100 0.0750700
 0.0987500 0.0859300
 0.1485400 0.1006500
 0.1984200 0.1088800
 0.2983300 0.1153300
 0.3983700 0.1122800
 0.4985000 0.1037300
 0.5987100 0.0891800
 0.6989800 0.0701400
 0.7993000 0.0480900
 0.8996601 0.0235500
 0.9498300 0.0117700
 1.0000000 0.0000000

 0.0000000 0.0000000
 0.0127400 -.0163200
 0.0253100 -.0216300
 0.0503500 -.0242700
 0.0753400 -.0234100
 0.1003300 -.0225500
 0.1502900 -.0203200
 0.2002600 -.0176000
 0.3002000 -.0136500
 0.4001700 -.0117000
 0.5001500 -.0102500
 0.6001600 -.0113000
 0.7001800 -.0123500
 0.8001900 -.0134000
 0.9001500 -.0104500
 0.9500901 -.0062200
 1.0000000 0.0000000
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Lednicer format dat file
Selig format dat file

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Polars for GOE 530 AIRFOIL (goe530-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe530-il50,000914 at α=4.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe530-il50,000532.1 at α=6.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe530-il100,000949.8 at α=5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe530-il100,000550.3 at α=4.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe530-il200,000969 at α=4°Mach=0 Ncrit=9Xfoil predictionDetails
   goe530-il200,000566.7 at α=5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe530-il500,000994.3 at α=5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe530-il500,000589.6 at α=4.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe530-il1,000,0009115.4 at α=5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe530-il1,000,0005101.4 at α=7.5°Mach=0 Ncrit=5Xfoil predictionDetails
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