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GOE 526 AIRFOIL (goe526-il)

GOE 526 AIRFOIL - Gottingen 526 airfoil


Airfoil goe526-il
Details Dat file Parser  
(goe526-il) GOE 526 AIRFOIL
Gottingen 526 airfoil
Max thickness 12.3% at 29.7% chord.
Max camber 4.1% at 39.7% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 526 AIRFOIL
       17.       17.

 0.0000000 0.0000000
 0.0117400 0.0268300
 0.0239300 0.0376800
 0.0485100 0.0523800
 0.0732000 0.0630900
 0.0979500 0.0717900
 0.1476100 0.0839100
 0.1973500 0.0931200
 0.2971100 0.1014700
 0.3971300 0.1008200
 0.4972900 0.0951700
 0.5976200 0.0835300
 0.6981100 0.0664000
 0.7986799 0.0462600
 0.8993100 0.0241300
 0.9496601 0.0120700
 1.0000000 0.0000000

 0.0000000 0.0000000
 0.0130000 -.0176300
 0.0256600 -.0232700
 0.0508000 -.0280500
 0.0758500 -.0298400
 0.1008600 -.0301300
 0.1508000 -.0282000
 0.2007300 -.0257800
 0.3006100 -.0214300
 0.4005200 -.0180900
 0.5004300 -.0152400
 0.6003700 -.0128900
 0.7003601 -.0125400
 0.8002900 -.0101900
 0.9001700 -.0058500
 0.9500800 -.0029200
 1.0000000 0.0000000
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Lednicer format dat file
Selig format dat file

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Polars for GOE 526 AIRFOIL (goe526-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe526-il50,000924.8 at α=10.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe526-il50,000533.3 at α=7.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe526-il100,000952.2 at α=7.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe526-il100,000552.8 at α=6°Mach=0 Ncrit=5Xfoil predictionDetails
   goe526-il200,000973.9 at α=4.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe526-il200,000569.4 at α=5.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe526-il500,000998.4 at α=2.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe526-il500,000591.8 at α=5.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe526-il1,000,0009119.5 at α=5.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe526-il1,000,0005107.6 at α=5.25°Mach=0 Ncrit=5Xfoil predictionDetails
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