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GOE 408 AIRFOIL (goe408-il)

GOE 408 AIRFOIL - Gottingen 408 airfoil


Airfoil goe408-il
Details Dat file Parser  
(goe408-il) GOE 408 AIRFOIL
Gottingen 408 airfoil
Max thickness 7.8% at 30% chord.
Max camber 4.1% at 30% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 408 AIRFOIL
       17.       17.

 0.0000000 0.0000000
 0.0124300 0.0180500
 0.0248900 0.0266000
 0.0498500 0.0387000
 0.0748000 0.0488000
 0.0997800 0.0559000
 0.1497400 0.0661000
 0.1997100 0.0733000
 0.2996800 0.0802000
 0.3996800 0.0796000
 0.4997000 0.0745000
 0.5997400 0.0654000
 0.6997800 0.0538000
 0.7998400 0.0412000
 0.8998900 0.0266000
 0.9499300 0.0173000
 1.0000000 0.0000000

 0.0000000 0.0000000
 0.0125400 -.0089500
 0.0250500 -.0114000
 0.0500400 -.0093000
 0.0750300 -.0072000
 0.1000200 -.0046000
 0.1500000 -.0009000
 0.1999900 0.0013000
 0.2999900 0.0027000
 0.3999900 0.0031000
 0.4999900 0.0025000
 0.5999900 0.0014000
 0.7000000 -.0002000
 0.8000100 -.0023000
 0.9000200 -.0049000
 0.9500300 -.0067000
 1.0000000 0.0000000
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Lednicer format dat file
Selig format dat file

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Polars for GOE 408 AIRFOIL (goe408-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe408-il50,000935.8 at α=8.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe408-il50,000540.8 at α=6.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe408-il100,000958.3 at α=6°Mach=0 Ncrit=9Xfoil predictionDetails
   goe408-il100,000559.2 at α=5.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe408-il200,000978.4 at α=5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe408-il200,000575.3 at α=4.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe408-il500,0009101.8 at α=4.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe408-il500,000594.7 at α=3.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe408-il1,000,0009119.8 at α=4.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe408-il1,000,0005102.2 at α=4.5°Mach=0 Ncrit=5Xfoil predictionDetails
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