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GOE 798 AIRFOIL (goe798-il)

GOE 798 AIRFOIL - Gottingen 798 airfoil


Airfoil goe798-il
Details Dat file Parser  
(goe798-il) GOE 798 AIRFOIL
Gottingen 798 airfoil
Max thickness 20% at 30% chord.
Max camber 6% at 40% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 798 AIRFOIL
       16.       16.

 0.0000000 0.0000000
 0.0125000 0.0345200
 0.0250000 0.0514400
 0.0500000 0.0753700
 0.0750000 0.0931100
 0.1000000 0.1069500
 0.1500000 0.1274300
 0.2000000 0.1427000
 0.3000000 0.1572500
 0.4000000 0.1605000
 0.5000000 0.1537500
 0.6000000 0.1365000
 0.7000000 0.1114500
 0.8000000 0.0822000
 0.9000000 0.0467500
 1.0000000 0.0075000

 0.0000000 0.0000000
 0.0125000 -.0267800
 0.0250000 -.0360600
 0.0500000 -.0451200
 0.0750000 -.0496900
 0.1000000 -.0504500
 0.1500000 -.0503700
 0.2000000 -.0485000
 0.3000000 -.0427500
 0.4000000 -.0370000
 0.5000000 -.0312500
 0.6000000 -.0255000
 0.7000000 -.0197500
 0.8000000 -.0140000
 0.9000000 -.0082500
 1.0000000 0.0000000
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Lednicer format dat file
Selig format dat file

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Polars for GOE 798 AIRFOIL (goe798-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe798-il50,00093.8 at α=11°Mach=0 Ncrit=9Xfoil predictionDetails
   goe798-il50,000510.4 at α=5.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe798-il100,000920.6 at α=6.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe798-il100,000531.9 at α=4.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe798-il200,000965.7 at α=6°Mach=0 Ncrit=9Xfoil predictionDetails
   goe798-il200,000561.7 at α=4°Mach=0 Ncrit=5Xfoil predictionDetails
   goe798-il500,000998.9 at α=4.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe798-il500,000583.8 at α=4.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe798-il1,000,0009120 at α=4.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe798-il1,000,000584.6 at α=5.25°Mach=0 Ncrit=5Xfoil predictionDetails
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