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GOE 462 AIRFOIL (goe462-il)

GOE 462 AIRFOIL - Gottingen 462 airfoil


Airfoil goe462-il
Details Dat file Parser  
(goe462-il) GOE 462 AIRFOIL
Gottingen 462 airfoil
Max thickness 11% at 9.9% chord.
Max camber 13.4% at 29.9% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 462 AIRFOIL
       17.       17.

 0.0000000 0.0000000
 0.0123000 0.0265900
 0.0246500 0.0466800
 0.0494100 0.0788700
 0.0742400 0.1010600
 0.0991200 0.1177400
 0.1489500 0.1396200
 0.1988700 0.1509900
 0.2988400 0.1552400
 0.3989000 0.1469900
 0.4990200 0.1307400
 0.5991700 0.1104900
 0.6993500 0.0867500
 0.7995500 0.0595000
 0.8997700 0.0312500
 0.9498700 0.0171200
 1.0000000 0.0000000

 0.0000000 0.0000000
 0.0125500 -.0064100
 0.0250500 -.0073100
 0.0500400 -.0056200
 0.0750000 -.0004400
 0.0999400 0.0082500
 0.1497200 0.0371200
 0.1994600 0.0720000
 0.2991600 0.1122400
 0.3991300 0.1159900
 0.4992000 0.1062400
 0.5993200 0.0904900
 0.6994700 0.0707500
 0.7996399 0.0485000
 0.8998200 0.0242500
 0.9499100 0.0126200
 1.0000000 0.0000000
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Lednicer format dat file
Selig format dat file

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Polars for GOE 462 AIRFOIL (goe462-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe462-il50,00098.9 at α=-0.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe462-il50,000529.2 at α=4.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe462-il100,000952.3 at α=3.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe462-il100,000546.4 at α=7°Mach=0 Ncrit=5Xfoil predictionDetails
   goe462-il200,000961.2 at α=8°Mach=0 Ncrit=9Xfoil predictionDetails
   goe462-il200,000562.4 at α=6.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe462-il500,0009175.7 at α=7°Mach=0 Ncrit=9Xfoil predictionDetails
   goe462-il500,000588.9 at α=6.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe462-il1,000,0009107.3 at α=6.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe462-il1,000,0005111.9 at α=6.25°Mach=0 Ncrit=5Xfoil predictionDetails
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