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GOE 622 AIRFOIL (goe622-il)

GOE 622 AIRFOIL - Gottingen 622 airfoil


Airfoil goe622-il
Details Dat file Parser  
(goe622-il) GOE 622 AIRFOIL
Gottingen 622 airfoil
Max thickness 8% at 30% chord.
Max camber 2.4% at 40% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 622 AIRFOIL
       17.       17.

 0.0000000 0.0000000
 0.0125000 0.0138000
 0.0250000 0.0216000
 0.0500000 0.0317000
 0.0750000 0.0393000
 0.1000000 0.0444000
 0.1500000 0.0526000
 0.2000000 0.0578000
 0.3000000 0.0632000
 0.4000000 0.0636000
 0.5000000 0.0590000
 0.6000000 0.0519000
 0.7000000 0.0428000
 0.8000000 0.0307000
 0.9000000 0.0171000
 0.9500000 0.0103000
 1.0000000 0.0020000

 0.0000000 0.0000000
 0.0125000 -.0092000
 0.0250000 -.0129000
 0.0500000 -.0168000
 0.0750000 -.0187000
 0.1000000 -.0191000
 0.1500000 -.0192000
 0.2000000 -.0187000
 0.3000000 -.0168000
 0.4000000 -.0144000
 0.5000000 -.0120000
 0.6000000 -.0096000
 0.7000000 -.0072000
 0.8000000 -.0048000
 0.9000000 -.0024000
 0.9500000 -.0012000
 1.0000000 0.0000000
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Lednicer format dat file
Selig format dat file

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Polars for GOE 622 AIRFOIL (goe622-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe622-il50,000935.5 at α=5.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe622-il50,000538.2 at α=5.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe622-il100,000953.2 at α=5.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe622-il100,000552.9 at α=5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe622-il200,000969.8 at α=4.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe622-il200,000564.9 at α=4.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe622-il500,000988.5 at α=3.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe622-il500,000575.5 at α=3°Mach=0 Ncrit=5Xfoil predictionDetails
   goe622-il1,000,000998.6 at α=3°Mach=0 Ncrit=9Xfoil predictionDetails
   goe622-il1,000,000582 at α=4.25°Mach=0 Ncrit=5Xfoil predictionDetails
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