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GOE 395 AIRFOIL (goe395-il)

GOE 395 AIRFOIL - Gottingen 395 airfoil


Airfoil goe395-il
Details Dat file Parser  
(goe395-il) GOE 395 AIRFOIL
Gottingen 395 airfoil
Max thickness 6.1% at 19.9% chord.
Max camber 7% at 49.9% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 395 AIRFOIL
       17.       17.

 0.0000000 0.0000000
 0.0123000 0.0189300
 0.0247000 0.0284600
 0.0495700 0.0415200
 0.0744600 0.0515800
 0.0993800 0.0593400
 0.1492500 0.0721600
 0.1991400 0.0818800
 0.2990300 0.0924200
 0.3990100 0.0949700
 0.4990400 0.0920100
 0.5991100 0.0835600
 0.6993200 0.0649100
 0.7995400 0.0441600
 0.8997600 0.0227000
 0.9498800 0.0114300
 1.0000000 0.0007500

 0.0000000 0.0000000
 0.0126000 -.0095700
 0.0251100 -.0109400
 0.0501000 -.0092800
 0.0750500 -.0044200
 0.0999900 0.0013400
 0.1498800 0.0118700
 0.1997800 0.0208900
 0.2996500 0.0339300
 0.3995600 0.0424800
 0.4995000 0.0475200
 0.5994900 0.0483600
 0.6996300 0.0356100
 0.7997600 0.0231600
 0.8998900 0.0104000
 0.9499500 0.0049300
 1.0000000 -.0007500
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Lednicer format dat file
Selig format dat file

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Polars for GOE 395 AIRFOIL (goe395-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe395-il50,000942.4 at α=8.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe395-il50,000543.1 at α=7.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe395-il100,000970.4 at α=7°Mach=0 Ncrit=9Xfoil predictionDetails
   goe395-il100,000571 at α=6°Mach=0 Ncrit=5Xfoil predictionDetails
   goe395-il200,0009102.8 at α=5.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe395-il200,0005100.8 at α=4.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe395-il500,0009149.9 at α=4.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe395-il500,0005117.3 at α=5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe395-il1,000,0009157.3 at α=4.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe395-il1,000,0005124.2 at α=4.5°Mach=0 Ncrit=5Xfoil predictionDetails
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