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GOE 402 AIRFOIL (goe402-il)

GOE 402 AIRFOIL - Gottingen 402 airfoil


Airfoil goe402-il
Details Dat file Parser  
(goe402-il) GOE 402 AIRFOIL
Gottingen 402 airfoil
Max thickness 6.8% at 20% chord.
Max camber 5.7% at 30% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 402 AIRFOIL
       17.       17.

 0.0000000 0.0000000
 0.0125000 0.0200700
 0.0250000 0.0301500
 0.0500000 0.0448000
 0.0750000 0.0564500
 0.1000000 0.0646000
 0.1500000 0.0779000
 0.2000000 0.0862000
 0.3000000 0.0908000
 0.4000000 0.0884000
 0.5000000 0.0800000
 0.6000000 0.0676000
 0.7000000 0.0522000
 0.8000000 0.0368000
 0.9000000 0.0204000
 0.9500000 0.0107000
 1.0000000 0.0000000

 0.0000000 0.0000000
 0.0125000 -.0049300
 0.0250000 -.0036500
 0.0500000 0.0013000
 0.0750000 0.0044500
 0.1000000 0.0076000
 0.1500000 0.0129000
 0.2000000 0.0182000
 0.3000000 0.0238000
 0.4000000 0.0254000
 0.5000000 0.0230000
 0.6000000 0.0196000
 0.7000000 0.0152000
 0.8000000 0.0108000
 0.9000000 0.0054000
 0.9500000 0.0027000
 1.0000000 0.0000000
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Lednicer format dat file
Selig format dat file

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Polars for GOE 402 AIRFOIL (goe402-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe402-il50,000931.5 at α=10.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe402-il50,000540.4 at α=5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe402-il100,000955.1 at α=9.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe402-il100,000559.9 at α=5.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe402-il200,000975.7 at α=8.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe402-il200,000577.9 at α=6.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe402-il500,0009105.7 at α=7.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe402-il500,0005105.4 at α=6.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe402-il1,000,0009129.2 at α=6.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe402-il1,000,0005126.2 at α=5.75°Mach=0 Ncrit=5Xfoil predictionDetails
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