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GOE 396 AIRFOIL (goe396-il)

GOE 396 AIRFOIL - Gottingen 396 airfoil


Airfoil goe396-il
Details Dat file Parser  
(goe396-il) GOE 396 AIRFOIL
Gottingen 396 airfoil
Max thickness 4.7% at 30% chord.
Max camber 5.8% at 40% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 396 AIRFOIL
       17.       17.

 0.0000000 0.0000000
 0.0125000 0.0120400
 0.0250000 0.0200700
 0.0500000 0.0321500
 0.0750000 0.0412200
 0.1000000 0.0473000
 0.1500000 0.0584500
 0.2000000 0.0676000
 0.3000000 0.0779000
 0.4000000 0.0802000
 0.5000000 0.0765000
 0.6000000 0.0678000
 0.7000000 0.0551000
 0.8000000 0.0384000
 0.9000000 0.0207000
 0.9500000 0.0108500
 1.0000000 0.0000000

 0.0000000 0.0000000
 0.0125000 -.0039600
 0.0250000 -.0039300
 0.0500000 -.0018500
 0.0750000 0.0012300
 0.1000000 0.0053000
 0.1500000 0.0134500
 0.2000000 0.0206000
 0.3000000 0.0309000
 0.4000000 0.0352000
 0.5000000 0.0325000
 0.6000000 0.0278000
 0.7000000 0.0211000
 0.8000000 0.0134000
 0.9000000 0.0057000
 0.9500000 0.0018500
 1.0000000 0.0000000
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Lednicer format dat file
Selig format dat file

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Polars for GOE 396 AIRFOIL (goe396-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe396-il50,000944.8 at α=6.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe396-il50,000544.9 at α=6°Mach=0 Ncrit=5Xfoil predictionDetails
   goe396-il100,000967 at α=5.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe396-il100,000566.8 at α=4.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe396-il200,000589.1 at α=4°Mach=0 Ncrit=5Xfoil predictionDetails
   goe396-il200,000092.4 at α=4.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe396-il500,0009121.3 at α=3°Mach=0 Ncrit=9Xfoil predictionDetails
   goe396-il500,0005111.2 at α=2.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe396-il1,000,0009141.7 at α=2.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe396-il1,000,000599.8 at α=2.75°Mach=0 Ncrit=5Xfoil predictionDetails
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