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GOE 482 AIRFOIL (goe482-il)

GOE 482 AIRFOIL - Gottingen 482 airfoil


Airfoil goe482-il
Details Dat file Parser  
(goe482-il) GOE 482 AIRFOIL
Gottingen 482 airfoil
Max thickness 16.5% at 29.6% chord.
Max camber 8.8% at 39.6% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 482 AIRFOIL
       17.       17.

 0.0000000 0.0000000
 0.0117300 0.0307900
 0.0238200 0.0471000
 0.0481700 0.0732000
 0.0726500 0.0938200
 0.0972500 0.1099300
 0.1466700 0.1331700
 0.1962600 0.1494100
 0.2958900 0.1644000
 0.3959200 0.1634000
 0.4957000 0.1506100
 0.5967400 0.1304200
 0.6974300 0.1029400
 0.7982500 0.0699600
 0.8990900 0.0364800
 0.9495400 0.0182400
 1.0000000 0.0000000

 0.0000000 0.0000000
 0.0128800 -.0151800
 0.0255300 -.0213600
 0.0505900 -.0237400
 0.0755800 -.0231100
 0.1005500 -.0219900
 0.1504300 -.0172400
 0.2003000 -.0119900
 0.3000100 -.0005000
 0.3996800 0.0129900
 0.4994500 0.0219900
 0.5992800 0.0289800
 0.6992300 0.0309800
 0.7993000 0.0279800
 0.8995500 0.0179900
 0.9497600 0.0097400
 1.0000000 0.0000000
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Lednicer format dat file
Selig format dat file

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Polars for GOE 482 AIRFOIL (goe482-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe482-il50,00094.9 at α=9.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe482-il50,000517.3 at α=1.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe482-il100,000935.8 at α=2.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe482-il100,000551 at α=3.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe482-il200,000971.2 at α=4.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe482-il200,000573.9 at α=4°Mach=0 Ncrit=5Xfoil predictionDetails
   goe482-il500,0009107.3 at α=4.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe482-il500,0005100.3 at α=5.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe482-il1,000,0009137.6 at α=4.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe482-il1,000,0005121.4 at α=4°Mach=0 Ncrit=5Xfoil predictionDetails
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