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GOE 523 AIRFOIL (goe523-il)

GOE 523 AIRFOIL - Gottingen 523 airfoil


Airfoil goe523-il
Details Dat file Parser  
(goe523-il) GOE 523 AIRFOIL
Gottingen 523 airfoil
Max thickness 16.5% at 29.7% chord.
Max camber 9.7% at 49.7% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 523 AIRFOIL
       17.       17.

 0.0000000 0.0000000
 0.0117600 0.0372400
 0.0239000 0.0549800
 0.0484000 0.0799700
 0.0730400 0.0979600
 0.0977200 0.1139500
 0.1472300 0.1384400
 0.1969200 0.1539400
 0.2966100 0.1694300
 0.3965900 0.1704300
 0.4967600 0.1619400
 0.5971000 0.1449400
 0.6975600 0.1219500
 0.7981900 0.0904600
 0.8990000 0.0499800
 0.9494800 0.0259900
 1.0000000 0.0000000

 0.0000000 0.0000000
 0.0127600 -.0132400
 0.0253300 -.0164900
 0.0503700 -.0184900
 0.0753700 -.0184900
 0.1003500 -.0174900
 0.1502600 -.0129900
 0.2001600 -.0080000
 0.2999000 0.0050000
 0.3996300 0.0184900
 0.4993500 0.0324900
 0.5990900 0.0454800
 0.6989400 0.0529800
 0.7990300 0.0484800
 0.8993900 0.0304900
 0.9496601 0.0169900
 1.0000000 0.0000000
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Lednicer format dat file
Selig format dat file

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Polars for GOE 523 AIRFOIL (goe523-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe523-il50,00095.3 at α=8.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe523-il50,000520.5 at α=3.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe523-il100,000948.8 at α=5.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe523-il100,000550.9 at α=3.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe523-il200,000974.3 at α=1.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe523-il200,000571.5 at α=1.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe523-il500,0009102.1 at α=0.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe523-il500,000590.6 at α=0.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe523-il1,000,0009120.6 at α=0.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe523-il1,000,0005104.4 at α=2.25°Mach=0 Ncrit=5Xfoil predictionDetails
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