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GOE 405 AIRFOIL (goe405-il)

GOE 405 AIRFOIL - Gottingen 405 airfoil


Airfoil goe405-il
Details Dat file Parser  
(goe405-il) GOE 405 AIRFOIL
Gottingen 405 airfoil
Max thickness 11.1% at 30% chord.
Max camber 6.5% at 40% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 405 AIRFOIL
       15.       15.

 0.0000000 0.0000000
 0.0125000 0.0212000
 0.0250000 0.0324000
 0.0500000 0.0498000
 0.0750000 0.0647000
 0.1000000 0.0771000
 0.2000000 0.1067000
 0.3000000 0.1188000
 0.4000000 0.1199000
 0.5000000 0.1140000
 0.6000000 0.1011000
 0.7000000 0.0822000
 0.8000000 0.0593000
 0.9000000 0.0314000
 1.0000000 0.0000000

 0.0000000 0.0000000
 0.0125000 -.0098000
 0.0250000 -.0126000
 0.0500000 -.0147000
 0.0750000 -.0148000
 0.1000000 -.0134000
 0.2000000 -.0018000
 0.3000000 0.0078000
 0.4000000 0.0109000
 0.5000000 0.0115000
 0.6000000 0.0106000
 0.7000000 0.0092000
 0.8000000 0.0068000
 0.9000000 0.0039000
 1.0000000 0.0000000
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Lednicer format dat file
Selig format dat file

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Polars for GOE 405 AIRFOIL (goe405-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe405-il50,00099.9 at α=5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe405-il50,000529.2 at α=6.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe405-il100,000954.3 at α=8.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe405-il100,000558.1 at α=6°Mach=0 Ncrit=5Xfoil predictionDetails
   goe405-il200,000982.3 at α=5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe405-il200,000580.3 at α=4.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe405-il500,0009115.4 at α=3.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe405-il500,0005104.6 at α=4.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe405-il1,000,0009137.5 at α=3°Mach=0 Ncrit=9Xfoil predictionDetails
   goe405-il1,000,0005126.2 at α=5°Mach=0 Ncrit=5Xfoil predictionDetails
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